DEPARTMENT OF
TRANSPORTATION Revision: 7
Date: 06/05/2003
FEDERAL AVIATION
ADMINISTRATION
M A S T E R M I N I M U M E Q U I P M E N T L I S T
PIPER
PA-34-200/200T/220T
FEDERAL AVIATION
ADMINISTRATION
KANSAS CITY AIRCRAFT
EVALUATION GROUP
ROOM 332
TELEPHONE: (816) 329-3233
FAX: (816) 329-3241
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PIPER
PA-34-200/200T/220T
Table of Contents
SYSTEM NO. SYSTEM PAGE
--
Table of Contents
I
--
Log of Revisions
II
--
Control Page
III, IV
--
Highlights of Change
V, VI
--
Definitions
VII, VIII, IX, X
--
Definitions
XI, XII, XIII, XIV
--
Preamble
XV, XVI
--
Guidelines for (O) & (M) Procedures XVII, XVIII
21
Air Conditioning
21-1
22
Auto Flight
22-1
23
Communications
23-1, 2, 3
25
Equipment/Furnishings
25-1, 2
26
Fire Protection
26-1
27 Flight Controls 27-1
28
Fuel
28-1
30
Ice and Rain Protection
30-1
31
Indicating/Recording Systems
31-1
32
Landing Gear
32-1
33
Lights
33-1, 2
34
Navigation
34-1, 2, 3, 4, 5
34
Navigation
34-6, 7, 8
35
Oxygen 35-1
37
Vacuum/Pressure
37-1
61
Propellers
61-1
77
Engine Indicating
77-1
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Log of Revisions
----------------------------------------------------------------------
¦ REV.NO. ¦ DATE ¦ PAGE NUMBERS ¦ INITIALS ¦
----------------------------------------------------------------------
¦ ORIGINAL ¦ 02/22/1980 ¦ COMPLETE ¦ ¦
¦ 1
¦ 04/02/1980 ¦ 29-1 REMOVED ¦ ¦
¦ 2
¦ 06/11/1985 ¦ ALL PAGES ¦ ¦
¦ 3
¦ 08/27/1987 ¦ 27-1 ¦ ¦
¦ 4
¦ 04/14/1989 ¦ ALL PAGES ¦ ¦
¦ 5
¦ 06/26/1989 ¦ HIGHLIGHTS OF REV.,DEFINITIONS
¦ ¦
¦ 5
¦ 06/26/1989 ¦ PREAMBLE ¦ ¦
¦ 6
¦ 10/07/1993 ¦ HIGHLIGHTS OF REV.,DEFINITIONS
¦ ¦
¦ 6
¦ 10/07/1993 ¦ GUIDELINES ¦ ¦
¦ 6
¦ 10/07/1993 ¦ 21-1,22-1,23-1,25-1,25-2 ¦
¦
¦ 6
¦ 10/07/1993 ¦ 26-1,27-1,30-1,31-1,32-1 ¦ ¦
¦ 6
¦ 10/07/1993 ¦ 33-1,33-2,34-1,34-2,34-3 ¦ ¦
¦ 6
¦ 10/07/1993 ¦ 35-1,37-1,61-1 ¦ ¦
¦ 6a
¦ 12/08/1995 ¦ HIGHLIGHTS OF REV.,DEFINITIONS
¦ ¦
¦ 6a
¦ 12/08/1995 ¦ GUIDELINES ¦ ¦
¦ 6a
¦ 12/08/1995 ¦ 28-1 ¦ ¦
¦ 6b
¦ 08/05/1996 ¦ HIGHLIGHTS OF REV.,DEFINITIONS
¦ ¦
¦ 6b
¦ 08/05/1996 ¦ 34-1,34-2,34-3 ¦ ¦
¦ 6c
¦ 02/10/1999 ¦ HIGHLIGHTS OF REV.,DEFINITIONS
¦ ¦
¦ 6c
¦ 02/10/1999 ¦ GUIDELINES ¦
¦
¦ 6c
¦ 02/10/1999 ¦ 23-1,25-1,25-2,26-1,28-1 ¦ ¦
¦ 6c
¦ 02/10/1999 ¦ 33-1,33-2,34-1,34-2,34-3 ¦ ¦
¦ 6c
¦ 02/10/1999 ¦ 34-4,34-5 ¦ ¦
¦ 7
¦ 06/05/2003 ¦ HIGHLIGHTS OF REV.,DEFINITIONS
¦ ¦
¦ 7
¦ 06/05/2003 ¦ GUIDELINES ¦ ¦
¦ 7
¦ 06/05/2003 ¦ 22-1,23-1,23-2,23-3,25-1 ¦ ¦
¦ 7
¦ 06/05/2003 ¦ 25-2,26-1,27-1,33-1,33-2 ¦ ¦
¦ 7
¦ 06/05/2003 ¦ 34-1,34-2,34-3,34-4,34-5 ¦ ¦
¦ 7
¦ 06/05/2003 ¦ 34-6,34-7,34-8,37-1,77-1 ¦ ¦
----------------------------------------------------------------------
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Control Page
SYSTEM PAGE REV NO. CURRENT DATE
Cover Page - 7
06/05/2003
Table of Contents I 7
06/05/2003
Log of Revisions II 7
06/05/2003
Control Page III 7
06/05/2003
IV 7
06/05/2003
Highlights of Change V 7
06/05/2003
VI 7 06/05/2003
Definitions VII
6 01/31/1995
VIII 6 01/31/1995
IX 6 01/31/1995
X 6 01/31/1995
XI 6 01/31/1995
XII 6 01/31/1995
XIII 6 01/31/1995
XIV 6
01/31/1995
Preamble XV 2
06/14/1989
XVI 2 06/14/1989
Guidelines for (O) & (M) Procedures XVII
7 06/05/2003
XVIII 7 06/05/2003
21
21-1 6 10/07/1993
22
22-1 7
06/05/2003
23
23-1 7 06/05/2003
23-2 7 06/05/2003
23-3 7 06/05/2003
25
25-1 7 06/05/2003
25-2 7 06/05/2003
26
26-1 7 06/05/2003
27 27-1 7
06/05/2003
28
28-1 6 c 02/10/1999
30
30-1 6 10/07/1993
31 31-1
6 10/07/1993
32
32-1 6 10/07/1993
33
33-1 7 06/05/2003
33-2 7 06/05/2003
34
34-1 7 06/05/2003
34-2 7 06/05/2003
34-3 7 06/05/2003
34-4 7
06/05/2003
34-5 7 06/05/2003
34-6 7 06/05/2003
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Control Page
SYSTEM PAGE REV NO. CURRENT DATE
34-7 7 06/05/2003
34-8 7 06/05/2003
35
35-1 6 10/07/1993
37
37-1 7 06/05/2003
61
61-1 6 10/07/1993
77
77-1 7 06/05/2003
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Revision: 7
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LIST Date: 06/05/2003
PIPER
PA-34-200/200T/220T
Highlights of
Change
Multiple Deleted the word "OR" for
clarification and reformatted the
ATA
Remarks or Exceptions in accordance with Policy Letter 31,
Numbers
designated as Global Change 83.
ATA 22-1 Changed relief for Autopilot system in
accordance with Policy
Letter 101, designated as
Global Change 103.
ATA 22-2 Added relief for Autopilot Disconnect
in accordance with
Policy
Letter 93.
ATA 23-1 Changed relief for Communications
Equipment in accordance with
Policy Letter 95, designated
as Global Change 111 and moved
High Frequency (HF) Communications to
ATA 23-7.
ATA 23-4
Changed relief for Cockpit Voice Recorder in accordance with
Policy Letter 29, designated
as Global Change 48.
ATA 23-5
Changed relief in accordance with Policy Letter 09, designated
as Global Change 117.
ATA 23-6
Added relief for Boom Microphones in accordance with Policy
Letter 58, designated as
Global Change 100.
ATA 23-7
Added relief for High Frequency (HF) Communication system in
accordance with Policy Letter
106, designated as Global
Change 89.
ATA 25-2
Changed Repair Category Interval relief from "D" to
"C" for
Passenger Seats in accordance
with Policy Letter 79, designate
as Global Change 96.
ATA 25-5
Changed the number required for dispatch for Passenger
Convenience Item(s) from a
variable quantity to "0" in
accordance with Policy Letter
33, designated as Global
Change 99.
ATA 25-6
Changed System Equipment Title from First Aid Kits to Emergency
Medical Equipment in
accordance with Policy Letter 73,
designated as Global Change
104.
ATA 34-10 Changed relief for ATC
Transponders and Automatic Altitude
Reporting Systems in
accordance with Policy Letter 76,
designated as Global Change
110.
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Highlights of
Change
ATA 34-12 Deleted relief for Altitude
Encoder and combined it with Item
34-10, ATC Transponders and
Automatic Altitude Reporting
Systems
ATA 34-13 Added relief for Microwave
Landing System (MLS) and Flight
Management System (FMS).
ATA 34-14 Changed relief for DME in
accordance with Policy Letter 03.
ATA 34-15 Retitled System Item and
changed relief for Altitude Alerting
System in accordance with
Policy Letter 39, designated as
Global Change 95.
ATA 34-19 Redesignated Traffic Alert and
Collision Avoidance System
TCAS II as TCAS I, changed
relief and rewrote remarks in
accordance with Policy Letter
32, designated as Global
Change 115.
ATA 34-20 Redesignated Traffic Alert and
Collision Avoidance System
TCAS I as TCAS II, changed
relief and rewrote remarks in
accordance with Policy Letter
32, designated as Global
Change 115.
ATA 34-21 Changed relief for Ground
Proximity Warning System (GPWS) in
accordance with Policy Letter
54, designated as Global
Change 107.
ATA 34-23 Added relief for Flight
Management System Navigation Databases
in accordance with Policy
Letter 98, designated as Global
Change 71.
ATA 34-24 Added relief for Navigation
Management System Navigation
Databases in accordance with
Policy Letter 98, designated as
Global Change 71.
ATA 77-1
Added relief for Exhaust Gas Temperature (EGT) gauges.
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Definitions
1.
System Definitions.
System numbers are based on the Air
Transport Association (ATA)
Specification Number 100 and items are
numbered sequentially.
a. "Item" (Column 1) means the
equipment, system,
component, or function listed in
the "Item"
column.
b. "Number Installed" (Column 2)
is the number
(quantity) of items
normally installed in the
aircraft. This number represents the aircraft
configuration considered
in developing this MMEL.
Should the number be a
variable (e.g., passenger
cabin items) a number is
not required.
c. "Number Required for
Dispatch" (Column 3) is the
minimum number (quantity)
of items required for
operation provided the
conditions specified in
Column 4 are met.
NOTE:
Where the MMEL shows a variable number required for
dispatch, the MEL must reflect the
actual number required for
dispatch or an alternate means of
configuration control approved
by the Administrator.
d. "Remarks or Exceptions"
(Column 4) in this column
includes a statement
either prohibiting or
permitting operation with
a specific number of
items inoperative,
provisos (conditions and
limitations) for such operation, and
appropriate
notes.
e. A vertical bar (change bar) in the
margin
indicates a change,
addition or deletion in the
adjacent text for the
current revision of that
page only. The change bar is dropped at the next
revision of that page.
2.
"Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document
required for type certification and
approved by the responsible
FAA Aircraft Certification Office. The FAA approved AFM/RFM for
the specific aircraft is listed on the
applicable Type
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Definitions
Certificate Data Sheet.
3.
"As required by FAR" means that the listed item is subject to
certain provisions (restrictive or
permissive) expressed in the
Federal Aviation Regulations operating
rules. The number of
items required by the FAR must be
operative. When the listed
item is not required by FAR it may be
inoperative for time
specified by repair category.
4.
Each inoperative item must be placarded to inform and remind
the crewmembers and maintenance
personnel of the equipment
condition.
NOTE:
To the extent practical, placards should be located
adjacent to the control or indicator for
the item affected;
however, unless otherwise specified,
placard wording and location
will be determined by the operator.
5.
"-" symbol in Column 2 and/or Column 3 indicates a variable
number (quantity) of the item installed.
6.
"Deleted" in the remarks column after a sequence item
indicates that the item was previously
listed but is now required
to be operative if installed in the aircraft.
7.
"ER" refers to extended range operations of a two-engine
airplane which has a type design
approval for ER operations and
complies with the provisions of Advisory
Circular 120-42A. ¦
8.
"Federal Aviation Regulations" (FAR) means the applicable
portions of the Federal Aviation Act and
Federal Aviation
Regulations.
9.
"Flight Day" means a 24 hour period (from midnight to
midnight) either Universal Coordinated
Time (UCT) or local time,
as established by the operator, during
which at least one flight
is initiated for the affected aircraft.
10.
"Icing Conditions" means an atmospheric environment that may
cause ice to form on the aircraft or in
the engine(s).
11.
Alphabetical symbol in Column 4 indicates a proviso
(condition or limitation) that must be
complied with for
FEDERAL AVIATION ADMINISTRATION Page: IX
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PA-34-200/200T/220T
Definitions
operation with the listed item inoperative.
12.
"Inoperative" means a system and/or component malfunction to
the extent that it does not accomplish
its intended purpose
and/or is not consistently functioning
normally within its
approved operating limit(s) or
tolerance(s).
13.
"Notes:" in Column 4 provides additional information for
crewmember or maintenance
consideration. Notes are used to
identify applicable material which is
intended to assist with
compliance, but do not relieve the
operator of the responsibility
for compliance with all applicable
requirements. Notes are not a
part of the provisos.
14.
Inoperative components of an inoperative system:
Inoperative items which are components
of a system which is
inoperative are usually considered
components directly associated
with and having no other function than
to support that system.
(Warning/caution systems associated with
the inoperative system
must be operative unless relief is
specifically authorized per
the MMEL).
15.
"(M)" symbol indicates a requirement for a specific
maintenance procedure which must be accomplished
prior to
operation with the listed item
inoperative. Normally these
procedures are accomplished by
maintenance personnel; however,
other personnel may be qualified and
authorized to perform
certain functions. Procedures requiring specialized knowledge or
skill, or requiring the use of tools or
test equipment should be
accomplished by maintenance
personnel. The satisfactory
accomplishment of all maintenance
procedures, regardless of
who performs them, is the responsibility
of the operator.
Appropriate procedures are required to
be published as part of
the operator's manual or MEL.
16.
"(O)" symbol indicates a requirement for a specific
operations procedure which must be
accomplished in planning for
and/or operating with the listed item
inoperative. Normally
these procedures are accomplished by the
flight crew; however,
other personnel may be qualified and
authorized to perform
certain functions. The satisfactory accomplishment of all
procedures, regardless of who performs
them, is the
responsibility of the operator. Appropriate procedures are
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Definitions
required to be published as a part of the
operator's manual or
MEL.
NOTE:
The (M) and (O) symbols are required in the operator's MEL
unless otherwise authorized by the
Administrator.
17.
"Deactivated" and "Secured" means that the specified
component must be put into an acceptable
condition for safe
flight.
An acceptable method of securing or deactivating will be
established by the operator.
18.
"Visual Flight Rules" (VFR) is as defined in FAR Part 91.
This precludes a pilot from filing an
Instrument Flight Rules
(IFR) flight plan.
19.
"Visual Meteorological Conditions" (VMC) means the
atmospheric environment is such that
would allow a flight to
proceed under the visual flight rules
applicable to the flight.
This does not preclude operating under
Instrument Flight Rules.
20.
"Visible Moisture" means an atmospheric environment
containing water in any form that can be
seen in natural or
artificial light; for example, clouds,
fog, rain, sleet, hail, or
snow.
21.
"Passenger Convenience Items" means those items related to
passenger convenience, comfort or
entertainment such as, but not
limited to, galley equipment, movie
equipment, ash trays, stereo
equipment, overhead reading lamps, etc.
22.
Repair Intervals: All users of an
MEL approved under FAR
121, 125, 129 and 135 must effect
repairs of inoperative systems
or components, deferred in accordance with the MEL, at or prior
to the repair times established by the
following letter
designators:
Category A. Items in this category shall be repaired
within
the time interval specified in the remarks
column of the
operator's approved MEL.
Category B. Items in this category shall be repaired
within
three (3) consecutive calendar days (72
hours), excluding the day
the malfunction was recorded in the
aircraft maintenance
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Definitions
record/logbook. For example, if it were recorded at 10 a.m.
on
January 26th, the three day interval
would begin at midnight the
26th and end at midnight the 29th.
Category C. Items in this category shall be repaired
within
ten (10) consecutive calendar days (240
hours), excluding the day
the malfunction was recorded in the
aircraft maintenance
record/logbook. For example, if it were recorded at 10 a.m.
on
January 26th, the 10 day interval would
begin at midnight the
26th and end at midnight February 5th.
Category D. Items in this category shall be repaired
within
one hundred and twenty (120) consecutive
calendar days (2880
hours), excluding the day the
malfunction was recorded in the
aircraft maintenance log and/or record.
The letter designators are inserted
adjacent to Column 2.
23. Electronic fault alerting system -
General ¦
New generation aircraft display system
fault indications to the ¦
flight crew by use of computerized
display systems. Each ¦
aircraft manufacturer has incorporated
individual design ¦
philosophies in determining the data
that would be ¦
represented. The following are customized definitions
(specific¦
to each manufacturer) to help determine
the level of messages ¦
affecting the aircraft's dispatch
status. When preparing the ¦
MEL document, operators are to select
the proper Definition No. ¦
23 for their aircraft, if
appropriate. ¦
a.
BOEING (B-757/767, B-747-400,
B-777) ¦
Boeing airplanes equipped with Engine
Indicating and Crew ¦
Alerting
Systems (EICAS), provide different priority levels of ¦
system messages (WARNING, CAUTION, ADVISORY, STATUS and ¦
MAINTENANCE). Any messages that affects airplane
dispatch ¦
status will be displayed at a STATUS
message level or higher. ¦
The absence of an EICAS STATUS or higher
level (WARNING, ¦
CAUTION, ADVISORY) indicates that the
system/component is ¦
operating within its approved operating
limits or tolerances. ¦
System conditions that result only in a
maintenance level ¦
message, i.e. no correlation with a
higher level EICAS message, ¦
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PA-34-200/200T/220T
Definitions
do not affect dispatch and do not
require action other than as ¦
addressed within an operators standard
maintenance program. ¦
b.
DOUGLAS (MD-11) ¦
Some Douglas aircraft are equipped with
an alerting function ¦
which is a subsystem within the
Electronic Instrument System ¦
(EIS).
The alerting function provides various levels of system ¦
condition alerts (WARNING, CAUTION,
ADVISORY, MAINTENANCE and ¦
STATUS).
¦
Alerts that affect aircraft dispatch
will include WARNING, ¦
CAUTION, STATUS or MAINTENANCE
level. MAINTENANCE alerts are ¦
displayed on the status page of the EIS
display panel under the ¦
maintenance heading. ¦
A MAINTENANCE alert on the EIS indicates
the presence of a ¦
system fault which can be identified by
the Central Fault ¦
Display System (CFDS)
interrogation. The systems are
designed ¦
to be fault tolerant, however, for any
MAINTENANCE alert, the ¦
MEL must be verified for dispatch
purposes. ¦
c.
AIRBUS (A-300-600, A-310,
A-320/319/321, A-330, A-340 ¦
Airbus aircraft equipped with Electronic
Centralized Aircraft ¦
Monitoring (ECAM) provide different
levels of system condition ¦
messages (WARNING, CAUTION, STATUS, and
ADVISORY). A-320/319/ ¦
321, A-330, and A-340 also provide
MAINTENANCE status messages. ¦
Any message that effects airplane
dispatchability will normally ¦
be at the WARNING, CAUTION or STATUS
level. MAINTENANCE ¦
messages (A-320/319/321, A-330, and
A-340 only) are also ¦
indicated on ECAM Status Page below the
white Maintenance label.¦
A MAINTENANCE status (Class II) message
on ECAM indicates the ¦
presence of a system fault which can be
identified by CFDS ¦
(A-320/319/321) or CMS (A-330/A-340)
interrogation. The systems ¦
are designed to be fault tolerant,
however for any MAINTENANCE ¦
status (Class II) message, the
A-320/319/321 MEL must be ¦
verified for dispatch capability. For
the A-330 and A-340, ¦
MAINTENANCE status messages do not
affect dispatch. ¦
d.
FOKKER (FK-100) ¦
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PA-34-200/200T/220T
Definitions
Fokker aircraft are equipped with Multi
Function Display System ¦
(MFDS) which provides electronic message
referring to the ¦
different priority levels of system
information (WARNING (red), ¦
CAUTION (amber), AWARENESS (cyan) AND
STATUS (white). Any ¦
messages that affects aircraft dispatch
will be at the WARNING, ¦
CAUTION or AWARENESS level. In these cases the MEL must be ¦
verified for dispatch capability and
maintenance may be ¦
required.
¦
System conditions that only require
maintenance are not ¦
presented on the flight deck. These maintenance ¦
indications/messages may be presented on
the Maintenance & Test ¦
Panel (MAP) or the Centralized Fault
Display Unit (CFDU) and by ¦
dedicated Built In Test Evaluation
(BITE) of systems. ¦
24.
"Administrative control item" means an item listed by the
operator in the MEL for tracking and
informational purposes. It
may be added to an operator's MEL by
approval of the Principal
Operations Inspector provided no relief
is granted, or provided
conditions and limitations are contained
in an approved document
(i.e. Structural Repair Manual,
airworthiness directive, etc.).
If relief other than that granted by an
approved document is
sought for an administrative control
item, a request must be
submitted to the Administrator. If the request results in review
and approval by the FOEB, the item
becomes an MMEL item rather
than an administrative control item.
25.
"***" symbol in Column 1 indicates an item which is not
required by regulation but which may
have been installed on some
models of aircraft covered by this
MMEL. This item may be
included on the operator's MEL after the
approving office has
determined that the item has been
installed on one or more of the
operator's aircraft. The symbol, however, shall not be carried
forward into the operator's MEL. It should be noted that neither
this policy nor the use of this symbol
provide authority to
install or remove an item from an
aircraft.
26.
"Excess Items" means those items that have been installed
that are redundant to the requirements
of the FARs.
27.
"Day of Discovery" is the calendar day an
equipment/instrument malfunction was
recorded in the aircraft
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PA-34-200/200T/220T
Definitions
maintenance log and or record. This day is excluded from the
calendar days or flight days specified
in the MMEL for the
repair of an inoperative item of
equipment. This provision is
applicable to all MMEL items, i.e.,
categories "A, B, C, and
D."
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PIPER
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Preamble
(Effective 6/14/89)
The following is applicable for
authorized certificate holders operating
under Federal Aviation Regulations (FAR)
Parts 121, 125, 129, 135: The
FAR require that all equipment installed
on an aircraft in compliance
with the Airworthiness Standards and the
Operating Rules must be
operative. However, the Rules also permit the
publication of a Minimum
Equipment List (MEL) where compliance
with certain equipment
requirements is not necessary in the interests
of safety under all
operating conditions. Experience has shown that with the various
levels
of redundancy designed into aircraft,
operation of every system or
installed component may not be necessary
when the remaining operative
equipment can provide an acceptable
level of safety. A Master Minimum
Equipment List (MMEL) is developed by
the FAA, with participation by the
aviation industry, to improve aircraft
utilization and thereby provide
more convenient and economic air
transportation for the public. The FAA
approved MMEL includes those items of
equipment related to airworthiness
and operating regulations and other
items of equipment which the
Administrator finds may be inoperative
and yet maintain an acceptable
level of safety by appropriate
conditions and limitations; it does not
contain obviously required items such as
wings, flaps, and rudders. The
MMEL is the basis for development of
individual operator MELs which take
into consideration the operator's
particular aircraft equipment
configuration and operational
conditions. Operator MELs, for
administrative control, may include
items not contained in the
MMEL;
however, relief for administrative control items must be
approved by the Administrator. An operator's MEL may differ in
format from the MMEL, but cannot be less
restrictive than the MMEL.
The individual operator's MEL, when
approved and authorized, permits
operation of the aircraft with
inoperative equipment.
Equipment not required by the operation
being conducted and equipment in
excess of FAR requirements are included
in the MEL with appropriate
conditions and limitations. The MEL must not deviate from the Aircraft
Flight Manual Limitations, Emergency
Procedures or with Airworthiness
Directives. It is important to remember that all
equipment related to
the airworthiness and the operating
regulations of the aircraft not
listed on the MMEL must be operative.
FEDERAL AVIATION
ADMINISTRATION Page: XVI
Revision: 2
MASTER MINIMUM EQUIPMENT
LIST Date: 06/14/1989
PIPER
PA-34-200/200T/220T
Preamble
(Effective 6/14/89)
Suitable conditions and limitations in
the form of placards, maintenance
procedures, crew operating procedures
and other restrictions as
necessary are specified in the MEL to
ensure that an acceptable level of
safety is maintained.
The MEL is intended to permit operation
with inoperative items of
equipment for a period of time until
repairs can be accomplished. It is
important that repairs be accomplished
at the earliest opportunity. In
order to maintain an acceptable level of
safety and reliability the MMEL
establishes limitations on the duration
of and conditions for operation
with inoperative equipment. The MEL provides for release of the
aircraft for flight with inoperative
equipment. When an item of
equipment is discovered to be
inoperative, it is reported by making an
entry in the Aircraft Maintenance
Record/Logbook as prescribed by FAR.
The item is then either repaired or may
be deferred per the MEL or other
approved means acceptable to the
Administrator prior to further
operation. MEL conditions and limitations, do not
relieve the operator
from determining that the aircraft is in
condition for safe operation
with items of equipment inoperative.
When these requirements are met, an
Airworthiness Release, Aircraft
Maintenance Record/Logbook entry, or
other approved documentation is
issued as prescribed by FAR. Such documentation is required prior to
operation with any item of equipment
inoperative.
Operators are responsible for exercising
the necessary operational
control to ensure that an acceptable
level of safety is maintained.
When operating with multiple inoperative
items, the interrelationships
between those items and the effect on
aircraft operation and crew
workload will be considered.
Operators are to establish a controlled
and sound repair program
including the parts, personnel,
facilities, procedures, and schedules to
ensure timely repair.
WHEN USING THE MEL, COMPLIANCE WITH THE
STATED INTENT OF THE PREAMBLE,
DEFINITIONS, AND THE CONDITIONS AND
LIMITATIONS SPECIFIED IN THE MEL IS
REQUIRED.
FEDERAL AVIATION
ADMINISTRATION Page XVII
Revision: 7
MASTER MINIMUM
EQUIPMENT LIST Date: 06/05/2003
PIPER
PA-34-200/200T/220T
Guidelines for (O) & (M)
Procedures
The FOEB has identified a need for
certain procedures to provide an
adequate level of safety while providing
relief for the following items.
These procedures must be established by
the operator. The following
guidelines are to help establish these
required procedures.
21-1
(M)Maintenance procedure to ensure no fuel leak or electrical
fault exists.
21-2
(M)Maintenance procedure to ensure no mechanical or electrical
fault exists that may cause
further damage or affect other
aircraft systems.
21-3
(O)Operations procedure for recording heater hours of operation.
22-1
(M)Maintenance procedure to ensure no electrical or mechanical
fault exists that will have
an adverse effect on any flight
control function.
23-7
(O)Operations procedure to verify that the SATCOM System
operates normally.
27-1
(M)Maintenance procedure to ensure there will be no adverse
effect on any flight control.
28-1
(O)Operations procedure to determine that the available fuel
quantity meets the regulatory
requirements for the intended
flight.
31-2
(O)Operations procedure for recording aircraft flight time.
32-1
(O)Operations procedure to prevent movement of the aircraft when
stopped or parked.
34-15
(O)Operations procedure to ensure crew awareness of altitude.
34-19
(M)Maintenance procedure to deactivate and secure the system.
34-19
(O)Operations procedure to ensure that TCAS I system is not
required for the intended
flight.
34-20
(M)Maintenance procedure to deactivate and secure the system.
FEDERAL AVIATION
ADMINISTRATION Page XVIII
Revision: 7
MASTER MINIMUM
EQUIPMENT LIST Date: 06/05/2003
PIPER
PA-34-200/200T/220T
Guidelines for (O) & (M)
Procedures
34-20
(O)Operations procedure to ensure that the TCAS II system is
not required for the intended
flight.
34-20-2 (O)Operations procedure to ensure
all TA functions are operative
and TA only mode is selected.
34-20-3 (O)Operations procedure to
ensure all RA display and audio
functions are operative and
enroute or approach procedures
do not require its use.
34-21
(O)Operations procedure to ensure alternate procedures are
established and used for
altitude awareness.
34-21-1 (O)Operations procedure to
ensure alternate procedures are
established and used for
altitude awareness.
34-21-4 (O)Operations procedure to
ensure alternate procedures are
established and used for
advisory callouts.
34-21-5 (O)Operations procedure to
ensure alternate procedures are
established and used for an
inoperative windshear mode.
34-23
(O)Operations procedure to identify and verify status and
suitability of navigation
facilities for the intended route
of flight.
34-24
(O)Operations procedure to identify and verify status and
suitability of navigation
facilities for the intended route
of flight.
37-1
(M)Maintenance procedure to ensure no unsafe condition exists
that could affect engine
operations or system function.
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION
¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 6 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 10/07/1993 ¦ 21-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
21 AIR CONDITIONING ¦
¦ ¦ ¦
¦
1. Combustion Heater C ¦
1 ¦ 0
¦ (M)
¦
¦
2. Air Conditioner C ¦ 1
¦ 0 ¦ (M) ¦
¦
3. Heater Hour Meter C ¦ 1
¦ 0 ¦ (O) ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER
MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦ PAGE:
¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 22-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
22 AUTO FLIGHT ¦
¦ ¦ ¦
¦
1. Autopilot C ¦ - ¦ 0 ¦
(M) May be inoperative provided | ¦
¦ ¦
¦ ¦ operations do not require
its use. | ¦
¦
2. Autopilot C ¦ - ¦ - ¦
One may be inoperative provided | ¦
¦ Disconnect ¦
¦ ¦ the autopilot is not
utilized at | ¦
¦ ¦ ¦
¦ less than initial approach
| ¦
¦ ¦ ¦
¦ altitude.
| ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 23-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM
¦ ¦ 3. NUMBER REQUIRED FOR
DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
23 COMMUNICATIONS ¦
¦ ¦ ¦
¦
1. Communications D ¦ -
¦ - ¦ Any in excess of those
required | ¦
¦ Equipment ¦ ¦
¦ by FAR may be inoperative provided
| ¦
¦ (VHF and UHF) ¦
¦ ¦ it is not powered by the
emergency | ¦
¦ ¦ ¦
¦ power supply and not required for
| ¦
¦ ¦ ¦
¦ emergency procedures.
| ¦
¦
2. Cockpit Speaker C ¦ 1
¦ 0 ¦ May be inoperative provided
two ¦
¦ ¦ ¦
¦ operative headsets are available
¦
¦ ¦ ¦
¦ to the flight crew.
¦
¦
3. Audio Amplifier C ¦ 1
¦ 0 ¦ May be inoperative provided
two ¦
¦ ¦ ¦
¦ operative headsets are available
¦
¦ ¦ ¦
¦ to the flight crew.
¦
¦
4. Cockpit Voice A ¦ 1
¦ 0 ¦ | ¦
¦ *** Recorder
(CVR) ¦ ¦
¦
| ¦
¦ 1) With Flight A ¦ 1
¦ 0 ¦ May be inoperative
provided: | ¦
¦ Data Recorder ¦
¦ ¦ a) Flight Data Recorder | ¦
¦ (FDR) installed ¦
¦ ¦ operates normally, and | ¦
¦ ¦ ¦
¦ b) Repairs are made
within | ¦
¦ ¦ ¦
¦ three flight days. | ¦
¦ 2) Without Flight A ¦ 1
¦ 0 ¦ May be inoperative provided
repairs | ¦
¦ Data Recorder ¦
¦ ¦ are made within three
flight days. | ¦
¦ installed ¦
¦ ¦ | ¦
¦
5. Passenger Address ¦
¦ ¦ ¦
¦ ***
System ¦ ¦
¦
¦
¦ 1) Passenger C ¦ 1
¦ 0 ¦ May be inoperative
provided: | ¦
¦ Configuration ¦
¦ ¦ a) PA System not required by | ¦
¦ ¦ ¦
¦ FAR, and | ¦
¦ ¦ ¦
¦ b) Alternate, normal
and | ¦
¦ ¦ ¦
¦ emergency procedures,
and/or | ¦
¦ ¦ ¦
¦ operating restrictions
are | ¦
¦ ¦ ¦
¦ established and
used. | ¦
¦ 2) Cargo D ¦ 1 ¦ 0
¦
¦
¦ Configuration ¦
¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 23-2
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
23 COMMUNICATIONS ¦
¦ ¦ ¦
¦ 6. Boom Microphones ¦
¦ ¦ | ¦
¦ COCKPIT VOICE ¦
¦ ¦ | ¦
¦ RECORDER (CVR) WITH ¦
¦ ¦ | ¦
¦ FLIGHT DATA RECORDER ¦
¦ ¦ | ¦
¦ (FDR) INSTALLED ¦
¦ ¦ | ¦
¦ 1) Cockpit Voice A ¦ -
¦ 0 ¦ May be inoperative
provided: | ¦
¦ Recorder equipped ¦ ¦
¦ a) Flight Data Recorder | ¦
¦ to record Boom ¦
¦ ¦ operates normally, and | ¦
¦ Microphone per ¦
¦ ¦ b) Repairs are made within | ¦
¦ 14 CFR 135.151(d) ¦
¦ ¦ three flight days. | ¦
¦ ***
2) Cockpit Voice D ¦ - ¦ 0 ¦
Any in excess of those required by | ¦
¦ Recorder not ¦
¦ ¦ FAR may be
inoperative. | ¦
¦ equipped to record ¦ ¦
¦ | ¦
¦ Boom Microphone ¦
¦ ¦ | ¦
¦ COCKPIT VOICE ¦
¦ ¦ | ¦
¦ RECORDER WITHOUT ¦
¦ ¦ | ¦
¦ FLIGHT DATA RECORDER ¦
¦ ¦ | ¦
¦ INSTALLED ¦ ¦
¦
| ¦
¦ 1) Cockpit Voice A ¦ -
¦ 0 ¦ May be inoperative provided
repairs | ¦
¦ Recorder equipped ¦
¦ ¦ are made within three
flight days. | ¦
¦ to record Boom ¦
¦ ¦ | ¦
¦ Microphone per ¦
¦ ¦ | ¦
¦ 14 CFR 135.151(d) ¦
¦ ¦ | ¦
¦ ***
2) Cockpit Voice D ¦ - ¦ 0 ¦
Any in excess of those required by | ¦
¦ Recorder not ¦
¦ ¦ FAR may be
inoperative. | ¦
¦ equipped to record ¦ ¦
¦ | ¦
¦ Boom Microphone ¦
¦ ¦ | ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 23-3
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM
¦ ¦ 3. NUMBER REQUIRED FOR
DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
23 COMMUNICATIONS ¦
¦ ¦ ¦
¦
7. High Frequency D ¦ -
¦ - ¦ Any in excess of those
required | ¦
¦ (HF) Communication ¦
¦ ¦ by FAR may be
inoperative. | ¦
¦ System ¦ ¦
¦ | ¦
¦ C ¦ - ¦ 1 ¦
(O) May be inoperative while | ¦
¦ ¦ ¦
¦ conducting operations that require
| ¦
¦ ¦ ¦
¦ two Long-Range Communication
| ¦
¦ ¦ ¦
¦ Systems (LRCS) provided:
| ¦
¦ ¦ ¦
¦ a) Satellite Communications | ¦
¦ ¦ ¦
¦ (SATCOM) (High or Low
Gain) | ¦
¦ ¦ ¦
¦ Data Link system operates | ¦
¦ ¦ ¦
¦ normally, and | ¦
¦ ¦ ¦
¦ b) SATCOM Data Link | ¦
¦ ¦ ¦
¦ communication
operates | ¦
¦ ¦ ¦
¦ normally over the
intended | ¦
¦ ¦ ¦
¦ route of flight. | ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 25-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦ -------------------------
¦ ¦
¦ 4. REMARKS OR EXCEPTIONS
¦
¦
25 EQUIPMENT/FURNISHINGS ¦ ¦
¦
¦
¦
1. Cockpit Shoulder B ¦ -
¦ - ¦ Right side may be
inoperative for ¦
¦ Harness
¦ ¦
¦ single pilot operations, but seat
¦
¦ ¦ ¦
¦ must remain unoccupied.
¦
¦
2. Passenger Seat(s) C ¦ -
¦ - ¦ May be inoperative
provided: | ¦
¦ ¦ ¦
¦ a) Seat does not block an ¦
¦ ¦ ¦
¦ Emergency Exit, ¦
¦ ¦ ¦
¦ b) Seat does not restrict any ¦
¦ ¦ ¦
¦ passenger from access to
the ¦
¦ ¦ ¦
¦ main aircraft aisle,
and ¦
¦ ¦ ¦
¦ c) The affected seat(s)
are ¦
¦ ¦ ¦
¦ placarded "DO NOT
OCCUPY". ¦
¦ ¦ ¦
¦ NOTE 1: A seat with an inoperative
¦
¦ ¦ ¦
¦ seatbelt is considered inoperative.
¦
¦ ¦ ¦
¦ NOTE 2: Affected seat(s) may
¦
¦ ¦ ¦
¦ include the seat(s) behind and/or
¦
¦ ¦ ¦
¦ adjacent outboard seats.
¦
¦ 1) Recline C ¦ -
¦ - ¦ May be inoperative and
seat | ¦
¦ Mechanism ¦
¦ ¦ occupied provided seat is
secured ¦
¦ ¦ ¦
¦ in the up-right position.
¦
¦ 2) Underseat C ¦ -
¦ - ¦ May be inoperative
provided: | ¦
¦ Baggage ¦
¦ ¦ a) Baggage is not stowed under ¦
¦ Restraining Bars ¦
¦ ¦ seat with inoperative ¦
¦ ¦ ¦
¦ restraining bar, and ¦
¦ ¦ ¦ ¦ b) Associated seat is placarded ¦
¦ ¦ ¦
¦ "DO NOT STOW BAGGAGE
UNDER ¦
¦ ¦ ¦
¦ THIS SEAT". ¦
¦
3. Flotation C ¦ - ¦ - ¦
As required by FAR. ¦
¦ Equipment ¦ ¦
¦
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 25-2
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
25 EQUIPMENT/FURNISHINGS ¦ ¦
¦ ¦
¦
4. Emergency Locator C ¦ 1
¦ 0 ¦ As required by FAR. ¦
¦ Transmitter (ELT) ¦
¦ ¦ ¦
¦ C ¦ 1 ¦ 0 ¦
May be inoperative for published ¦
¦ ¦ ¦
¦ scheduled flights in scheduled air
¦
¦ ¦ ¦
¦ carrier service.
¦
¦
5. Passenger Convenience ¦ - ¦ 0 ¦
Passenger convenience items, as | ¦
¦ Item(s) ¦ ¦
¦ expressed in this MMEL, are those
¦
¦ ¦ ¦
¦ related to passenger convenience,
¦
¦ ¦ ¦
¦ comfort or entertainment such as,
¦
¦ ¦ ¦
¦ but not limited to, galley
¦
¦ ¦ ¦
¦ equipment, movie equipment, ash
¦
¦ ¦ ¦
¦ trays, stereo equipment, overhead
¦
¦ ¦ ¦
¦ reading lamps, etc. Items ¦
¦ ¦ ¦
¦ addressed elsewhere in this
¦
¦ ¦ ¦
¦ document shall not be included.
¦
¦ ¦ ¦ ¦
(M) and (O) procedures may be ¦
¦ ¦ ¦
¦ required and included in the air
¦
¦ ¦ ¦
¦ carrier's appropriate document.
¦
¦
6. Emergency Medical D ¦ -
¦ - ¦ Any in excess of those
required by | ¦
¦ Equipment ¦ ¦
¦ FAR may be incomplete or missing
| ¦
¦ ¦ ¦
¦ provided required distribution
¦
¦ ¦ ¦
¦ is maintained. ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 26-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦ ---------------------------------------
¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
26 FIRE PROTECTION ¦
¦ ¦ ¦
¦
1. Portable Fire D ¦ -
¦ - ¦ Any in excess of those
required by ¦
¦ Extinguishers ¦
¦ ¦ FAR may be inoperative
or ¦
¦ ¦ ¦
¦ missing provided:
¦
¦ ¦ ¦
¦ a) The inoperative fire ¦
¦ ¦ ¦
¦ extinguisher is
tagged ¦
¦ ¦ ¦
¦ inoperative, removed from ¦
¦ ¦ ¦
¦ the installed location,
and ¦
¦ ¦ ¦
¦ placed out of sight so
it ¦
¦ ¦ ¦
¦ can not be mistaken for a ¦
¦ ¦ ¦
¦ functional unit, and ¦
¦ ¦
¦ ¦ b) Required distribution is ¦
¦ ¦ ¦
¦ maintained. ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION
¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 27-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦ --------------------------------------------
¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
27 FLIGHT CONTROLS ¦
¦ ¦ ¦
¦
1. Electric Elevator C ¦ 1
¦ 0 ¦ (M)May be inoperative
provided: ¦
¦ Trim ¦ ¦
¦ a) Manual trim is operative ¦
¦ ¦
¦ ¦ and unaffected, and ¦
¦ ¦ ¦
¦ b) Autopilot is unaffected ¦
¦ ¦ ¦
¦ or not used. ¦
¦
2. Trim Position C ¦ 2
¦ 0 ¦ May be inoperative
provided: ¦
¦ Indicators ¦
¦ ¦ a)
Tab is visually checked for ¦
¦ (Rudder - Elevator) ¦
¦ ¦ full range of operation, ¦
¦ ¦ ¦
¦ b) Tab operation is not ¦
¦ ¦ ¦
¦ affected, and ¦
¦ ¦ ¦
¦ c) Tab is positioned to ¦
¦ ¦ ¦
¦ neutral prior to each ¦
¦ ¦ ¦
¦ departure and
neutral ¦
¦ ¦ ¦
¦ position is verified by ¦
¦ ¦ ¦
¦ visual inspection. ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM
EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT: ¦ REVISION NO: 6 c ¦ PAGE:
¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 02/10/1999 ¦ 28-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
28 FUEL ¦ ¦
¦
¦
¦
1. Fuel Quantity C ¦ 2
¦ 1 ¦ (O)One may be inoperative
provided ¦
¦ Indicators ¦
¦ ¦ a reliable means is used
to ¦
¦ ¦ ¦
¦ determine that fuel on board is
¦
¦ ¦ ¦
¦ sufficient to meet the regulatory
¦
¦ ¦ ¦
¦ requirements of the intended
¦
¦ ¦ ¦
¦ flight.
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 6 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 10/07/1993 ¦ 30-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦ --------------------------------------------
¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 30 ICE AND RAIN ¦
¦ ¦ ¦
¦ PROTECTION ¦
¦ ¦ ¦
¦
1. Pitot Heater B ¦ 1
¦ 0 ¦ Left unit must be operative
for ¦
¦ ¦
¦ ¦ IFR passenger carrying and
for ¦
¦ ¦ ¦
¦ flight in known or forecast icing
¦
¦ ¦ ¦
¦ conditions. Two heated
pitot ¦
¦ ¦ ¦
¦ tubes are required for these
¦
¦ ¦ ¦
¦ conditions if a second airspeed
¦
¦ ¦ ¦
¦ indicator is installed and
¦
¦ ¦ ¦
¦ operative.
¦
¦
2. Surface Deicing C ¦ 1
¦ 0 ¦ May be inoperative
provided ¦
¦ System (Wing, ¦
¦ ¦ aircraft is not operated in
known ¦
¦ Vertical and ¦
¦ ¦ or forecast icing conditions. ¦
¦ Horizontal ¦
¦ ¦ ¦
¦ Stabilizer) ¦
¦ ¦ ¦
¦
3. Heated Windshield C ¦ 1
¦ 0 ¦ May be inoperative
provided ¦
¦ Panel ¦ ¦
¦ aircraft is not operated in known
¦
¦ ¦ ¦
¦ or forecast icing conditions.
¦
¦
4. Propeller Deicing C ¦ 1
¦ 0 ¦ May be inoperative
provided ¦
¦ System ¦ ¦
¦ aircraft is not operated in known
¦
¦ ¦ ¦
¦ or forecast icing conditions.
¦
¦
5. Stall Warning C ¦ 2
¦ 0 ¦ May be inoperative
provided ¦
¦ Heaters ¦
¦ ¦ aircraft is not operated in
known ¦
¦ ¦ ¦
¦ or forecast icing conditions.
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 6 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 10/07/1993 ¦
31-1 ¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦ SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
31 INDICATING/RECORDING ¦
¦ ¦ ¦
¦ SYSTEMS ¦ ¦
¦
¦
¦
1. Clock with sweep C ¦ 1
¦ 0 ¦ May be inoperative for
VFR ¦
¦ second hand or ¦
¦ ¦ operations. ¦
¦ electric digital ¦
¦ ¦ ¦
¦ clock ¦ ¦
¦
¦
¦
2. Flight Hour C ¦ 1
¦ 0 ¦ (O) ¦
¦ Recorder ¦ ¦
¦
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 6 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 10/07/1993 ¦ 32-1
¦
¦ ---------------------------------------------------------------------------
¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
32 LANDING GEAR ¦
¦ ¦ ¦
¦
1. Parking Brake C ¦ 1
¦ 0 ¦ (O) ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 33-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM
¦ ¦ 3. NUMBER REQUIRED FOR
DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
33 LIGHTS ¦ ¦
¦
¦
¦
1. Anti-collision B ¦ 1
¦ 0 ¦ May be inoperative for
day ¦
¦ Beacon Light System ¦
¦ ¦ operations. ¦
¦
2. Position Lights C ¦ 3
¦ 0 ¦ May be inoperative for
day ¦
¦ ¦ ¦
¦ operations.
¦
¦
3. Cockpit/Flight Deck C ¦ - ¦ - ¦
Individual lights may be ¦
¦ and Instrument ¦
¦ ¦ inoperative provided
remaining ¦
¦ Lighting System ¦
¦ ¦ lights are: ¦
¦ ¦ ¦
¦ a) Sufficient to
clearly ¦
¦ ¦ ¦
¦ illuminate all required ¦
¦ ¦ ¦
¦ instruments,
controls ¦
¦ ¦ ¦
¦ and other devices for
which ¦
¦ ¦ ¦
¦ it is provided, ¦
¦ ¦ ¦
¦ b) Positioned so that
direct ¦
¦ ¦ ¦
¦ rays are shielded
from ¦
¦ ¦ ¦
¦ flight crewmembers eyes,
and ¦
¦ ¦
¦ ¦ c) Lighting configuration and ¦
¦ ¦ ¦
¦ intensity is acceptable
to ¦
¦ ¦ ¦
¦ the flight crew. ¦
¦
4. Landing Light C ¦ 1
¦ 0 ¦ May be inoperative for
day ¦
¦ ¦ ¦
¦ operations.
¦
¦
5. Taxi Light C ¦ 1
¦ 0 ¦ ¦
¦
6. Wing Ice Detection C ¦ 1
¦ 0 ¦ May be inoperative provided
a ¦
¦ Light ¦ ¦
¦ lamp/light of adequate capacity for
¦
¦ ¦ ¦
¦ wing and/or control surface
¦
¦ ¦ ¦
¦ inspection is available for night
¦
¦ ¦ ¦
¦ operations in icing conditions.
¦
¦
7. Strobe Light C ¦ 1
¦ 0 ¦ ¦
¦ System ¦ ¦
¦
¦
¦
8. Cabin Lights C ¦ -
¦ - ¦ May be inoperative
provided ¦
¦ ¦ ¦
¦ lighting configuration is
¦
¦ ¦ ¦
¦ acceptable to the flight crew.
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM
EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT: ¦ REVISION NO: 7 ¦ PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 33-2
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
33 LIGHTS ¦ ¦
¦
¦
¦
9. Recognition Lights C ¦ 2
¦ 0 ¦ May be inoperative
provided ¦
¦ ***
installed in ¦ ¦
¦ certificated anticollision light
¦
¦ accordance with ¦
¦ ¦ system is operative. ¦
¦ STC No. SA01038AT ¦
¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT
LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT: ¦ REVISION NO: 7 ¦ PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦
1. Altimeter B ¦ 2 ¦ 1 ¦
Right side may be inoperative. ¦
¦ Barometric Pressure ¦
¦ ¦ ¦
¦ (Adjustable) ¦
¦ ¦ ¦
¦ ¦ ¦
¦ NOTE: Where a servoed electric
¦
¦ ¦
¦ ¦ altimeter is installed, a ¦
¦ ¦ ¦
¦ functioning pneumatic ¦
¦ ¦ ¦
¦ indicator is
required. ¦
¦
2. Airspeed Indicator C ¦ 2
¦ 1 ¦ Right side may be
inoperative. ¦
¦ ¦ ¦
¦ NOTE: Where a servoed electric
¦
¦ ¦ ¦
¦ airspeed is installed,
a ¦
¦ ¦ ¦
¦ functioning pneumatic ¦
¦ ¦ ¦
¦ indicator is
required. ¦
¦
3. Gyroscopic Pitch B ¦ 2
¦ 1 ¦ Right side may be
inoperative. ¦
¦ and Bank Indicators ¦
¦ ¦ ¦
¦
4. Gyroscopic B ¦ 2
¦ 1 ¦ Right side may be
inoperative. ¦
¦ Directional ¦
¦ ¦ ¦
¦ Indicators ¦
¦ ¦ ¦
¦
5. Gyroscopic Rate B ¦ 2
¦ 0 ¦ Must be operative on left
side for ¦
¦ of Turn/Slip Skid ¦
¦ ¦ IFR, passenger carrying VFR
over ¦
¦ Indicators ¦
¦ ¦ the top and passenger
carrying ¦
¦ ¦ ¦
¦ VFR night operations.
¦
¦
6. Vertical Speed B ¦ 1
¦ 0 ¦ Must be operative on left
side ¦
¦ Indicator ¦ ¦
¦ for IFR passenger carrying.
¦
¦
7. Flight Director C ¦ 1
¦ 0 ¦ ¦
¦
8. Radar Altimeter C ¦ 1
¦ 0 ¦ ¦
¦
9. Weather Radar/ C ¦ 1
¦ 0 ¦ As required by FAR. ¦
¦ Thunderstorm ¦
¦ ¦ ¦
¦ Detection Equipment ¦
¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-2
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 10.
ATC Transponders C ¦ - ¦ - ¦
May be inoperative provided: | ¦
¦ and Automatic ¦
¦ ¦ a) Enroute operations do not | ¦
¦ Altitude Reporting ¦
¦ ¦
require its use, and | ¦
¦ Systems ¦ ¦
¦ b) Prior to flight, approval
is | ¦
¦ ¦ ¦
¦ obtained from ATC
facilities | ¦
¦ ¦ ¦
¦ having jurisdiction over
the | ¦
¦ ¦ ¦
¦ planned route of flight. | ¦
¦ D ¦ - ¦ 1 ¦
Any in excess of those required by | ¦
¦ ¦ ¦
¦ FAR may be inoperative. | ¦
¦ 11.
Marker Beacon C ¦ 1 ¦ 0 ¦
May be inoperative provided ¦
¦ ¦ ¦
¦ approach procedure does not
¦
¦ ¦ ¦
¦ require its use.
¦
¦ 12.
Altitude Encoder ¦ ¦
¦ DELETED REVISION 7. Combined
with | ¦
¦ ¦ ¦
¦ Item 10.
| ¦
¦ 13.
Navigation C ¦ - ¦ - ¦
As required by FAR. ¦
¦ Equipment (VOR/ILS, ¦
¦ ¦ ¦
¦ Loran, RNAV, Omega/ ¦
¦ ¦ ¦
¦ VLF, INS, Doppler, ¦
¦ ¦ ¦
¦ GPS, MLS, FMS) ¦
¦ ¦ | ¦
¦ 14.
Distance Measuring D ¦ - ¦ - ¦
Any in excess of those required by | ¦
¦ Equipment (DME) ¦
¦ ¦ FAR may be
inoperative. | ¦
¦ Systems ¦ ¦
¦ | ¦
¦ 15.
Altitude Alerting A ¦ - ¦ 0 ¦
(O) May be inoperative provided: | ¦
¦ ***
System ¦ ¦
¦ a) Autopilot with
altitude | ¦
¦ ¦ ¦
¦ hold is operative, | ¦
¦ ¦ ¦
¦ b) Enroute operations do not | ¦
¦ ¦ ¦
¦ require its use, and | ¦
¦ ¦ ¦
¦ c) Repairs are made
within | ¦
¦ ¦ ¦
¦ three flight days. | ¦
¦ C ¦ - ¦ 0 ¦
May be inoperative provided it is | ¦
¦ ¦ ¦
¦ not required by FAR.
| ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM
EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT: ¦ REVISION NO: 7 ¦ PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-3
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 16.
ADF C ¦ 1 ¦ 0 ¦
As required by FAR. ¦
¦ 17.
RMI C ¦ 1 ¦ 0
¦
¦
¦ 18.
Nonstabilized B ¦ 1 ¦ 0 ¦
May be inoperative provided ¦
¦ Magnetic Compass ¦
¦ ¦ any combination of three
gyro ¦
¦ ¦ ¦
¦ or INS (IRU) stabilized compass
¦
¦ ¦ ¦
¦ systems are operative.
¦
¦ B ¦ 1 ¦ 0 ¦
May be inoperative provided: ¦
¦ ¦
¦ ¦ a) Any combination of two gyro ¦
¦ ¦ ¦
¦ or INS stabilized compass ¦
¦ ¦ ¦
¦ systems operate normally, ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦
¦ b) Airplane is operated with ¦
¦ ¦ ¦
¦ dual independent
navigation ¦
¦ ¦ ¦
¦ capability and under ¦
¦ ¦ ¦
¦ positive radar control by ¦
¦ ¦ ¦
¦ ATC on the enroute
portion ¦
¦ ¦ ¦
¦ of the flight. ¦
¦ B ¦ 1 ¦ 0 ¦
May be inoperative for flights ¦
¦ ¦ ¦
¦ that are entirely within areas of
¦
¦ ¦ ¦
¦ magnetic unreliability provided at
¦
¦ ¦ ¦
¦ least two stabilized directional
¦
¦ ¦ ¦
¦ gyro systems are installed,
¦
¦ ¦ ¦
¦ operate normally and are used in
¦
¦ ¦
¦ ¦ conjunction with approved
free ¦
¦ ¦ ¦
¦ gyro navigation techniques.
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION
¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-4
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 19.
Traffic Alert and B ¦ - ¦ 0 ¦
(M)(O) May be inoperative provided: | ¦
¦ ***
Collision Avoidance ¦ ¦
¦ a) System is deactivated and | ¦
¦ System (TCAS I) ¦
¦ ¦ secured, and | ¦
¦ ¦ ¦
¦ b) Enroute or approach | ¦
¦ ¦ ¦
¦ procedures do not require | ¦
¦ ¦ ¦
¦ its use. | ¦
¦ C ¦ - ¦ 0 ¦
(M)(O) May be inoperative provided: | ¦
¦ ¦ ¦
¦ a) Not required by FAR, | ¦
¦ ¦ ¦
¦ b) System is deactivated
and | ¦
¦ ¦ ¦
¦ secured, and | ¦
¦ ¦ ¦
¦ c) Enroute or approach | ¦
¦ ¦ ¦
¦ procedures do not require | ¦
¦ ¦ ¦
¦ its use. | ¦
¦ 20.
Traffic Alert and B ¦ - ¦ 0 ¦
(M)(O) May be inoperative provided: | ¦
¦ ***
Collision Avoidance ¦ ¦
¦ a) System is deactivated and | ¦
¦ System (TCAS II) ¦
¦ ¦ secured, and | ¦
¦ ¦ ¦
¦ b) Enroute or approach | ¦
¦ ¦ ¦
¦ procedures do not require | ¦
¦ ¦
¦ ¦ its use. | ¦
¦ C ¦ - ¦ 0 ¦
(M)(O) May be inoperative provided: | ¦
¦ ¦ ¦
¦ a) Not required by FAR, | ¦
¦ ¦ ¦ ¦
b) System is deactivated and |
¦
¦ ¦ ¦
¦ secured, and | ¦
¦ ¦ ¦
¦ c) Enroute or approach | ¦
¦ ¦ ¦
¦ procedures do not
require | ¦
¦ ¦ ¦
¦ its use. | ¦
¦ 1) Combined C ¦ 2
¦ 1 ¦ May be inoperative on
the | ¦
¦ Traffic Alert (TA) ¦ ¦
¦ non-flying pilot side provided:
| ¦
¦ and Resolution ¦
¦ ¦ a) TA and RA visual display | ¦
¦ Advisory (RA) Dual ¦ ¦
¦ is operative on the
flying | ¦
¦ Display System(s) ¦
¦ ¦ pilot side, and | ¦
¦ ¦ ¦
¦ b) TA and RA audio function
is | ¦
¦ ¦ ¦
¦ operative on the
flying | ¦
¦ ¦ ¦
¦ pilot side. | ¦
¦ (CON'T.) ¦ ¦
¦
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-5
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH
¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 20. Traffic
Alert and ¦ ¦
¦
¦
¦ ***
Collision Avoidance ¦ ¦
¦
¦
¦ System (TCAS II) ¦
¦ ¦ ¦
¦ (CON'T.) ¦ ¦
¦
¦
¦ 2) Resolution C ¦ 2
¦ 1 ¦ May be inoperative on
the | ¦
¦ Advisory (RA) ¦
¦ ¦ non-flying pilot's
side. | ¦
¦ Display System(s) ¦
¦ ¦ ¦
¦ C ¦ - ¦ 0 ¦
(O) May be inoperative provided: | ¦
¦ ¦ ¦
¦ a) Traffic Alert (TA) visual | ¦
¦ ¦ ¦
¦ display and audio
functions | ¦
¦ ¦ ¦
¦ are operative, | ¦
¦ ¦ ¦
¦ b) TA only mode is selected
by | ¦
¦ ¦ ¦
¦ the crew, and | ¦
¦ ¦ ¦
¦ c) Enroute or approach | ¦
¦ ¦ ¦
¦ procedures do not require | ¦
¦ ¦ ¦
¦ its use. | ¦
¦ 3) Traffic Alert C ¦ -
¦ 0 ¦ (O) May be inoperative
provided: | ¦
¦ Display System(s) ¦
¦ ¦ a) RA visual display and audio | ¦
¦ ¦ ¦
¦ functions are operative,
and | ¦
¦ ¦
¦ ¦ b) Enroute or approach | ¦
¦ ¦ ¦
¦ procedures do not require | ¦
¦ ¦ ¦
¦ its use. | ¦
¦ 21.
Ground Proximity A ¦ - ¦ 0 ¦
(O) May be inoperative provided: ¦
¦ ***
Warning System ¦ ¦
¦ a) Alternate procedures are ¦
¦ (GPWS) ¦ ¦
¦ established and used,
and ¦
¦ ¦ ¦
¦ b) Repairs are made
within ¦
¦ ¦ ¦
¦ two flight days. ¦
¦ C ¦ - ¦ 0 ¦
(O) May be inoperative provided: | ¦
¦ ¦ ¦
¦ a) It is not required by
FAR, | ¦
¦ ¦ ¦
¦ and | ¦
¦ ¦ ¦
¦ b) Alternate procedures are | ¦
¦ ¦ ¦
¦ established and
used. | ¦
¦ (CON'T.) ¦ ¦
¦
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S. DEPARTMENT
OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-6
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 21.
Ground Proximity ¦ ¦
¦
¦
¦ ***
Warning System ¦ ¦
¦
¦
¦ (GPWS) (CON'T.) ¦ ¦
¦
¦
¦ 1) Modes 1-4 A ¦ -
¦ 0 ¦ (O) May be inoperative
provided: ¦
¦ ¦ ¦
¦ a) Alternate procedures are ¦
¦ ¦ ¦
¦ established, used,
and ¦
¦ ¦ ¦
¦ b) Repairs are made within
two ¦
¦ ¦ ¦
¦ flight days. ¦
¦ C ¦ - ¦ 0 ¦
(O) May be inoperative provided: | ¦
¦ ¦
¦ ¦ a) It is not required by FAR, | ¦
¦ ¦ ¦
¦ and | ¦
¦ ¦ ¦
¦ b) Alternate procedures are | ¦
¦ ¦ ¦
¦ established and used. | ¦
¦ 2) Test Mode A ¦ 1
¦ 0 ¦ May be inoperative
provided: ¦
¦ ¦ ¦
¦ a) The GPWS is
considered ¦
¦ ¦ ¦
¦ inoperative, and ¦
¦ ¦ ¦
¦ b) Repairs are made within
two ¦
¦ ¦ ¦
¦ flight days. ¦
¦ C ¦ - ¦ 0 ¦
May be inoperative provided: | ¦
¦ ¦ ¦
¦ a) It is not required by
FAR, | ¦
¦ ¦ ¦
¦ and | ¦
¦ ¦ ¦
¦ b) GPWS is considered | ¦
¦ ¦ ¦
¦ inoperative. | ¦
¦ 3) Glideslope B ¦ 2
¦ 0 ¦ ¦
¦ Deviation ¦
¦ ¦ ¦
¦ (Mode 5) ¦
¦ ¦ ¦
¦ C ¦ 2 ¦ 0 ¦
May be inoperative provided it is | ¦
¦ ¦ ¦
¦ not required by FAR.
| ¦
¦ ***
4) Advisory C ¦ - ¦ 0 ¦
(O) May be inoperative provided ¦
¦ Callouts ¦
¦ ¦ alternate procedures
are ¦
¦ ¦ ¦
¦ established and used.
¦
¦ (CON'T.) ¦ ¦
¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-7
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦
¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 21.
Ground Proximity ¦ ¦ ¦ ¦
¦ ***
Warning System ¦ ¦
¦
¦
¦ (GPWS) (CON'T.) ¦ ¦
¦
¦
¦ 5) Windshear Mode C ¦ -
¦ 0 ¦ (O) May be inoperative
provided: | ¦
¦ ¦ ¦
¦ a) Alternate procedures are | ¦
¦ ¦ ¦
¦ established and used, and | ¦
¦ ¦ ¦
¦ b) Windshear detection and | ¦
¦ ¦ ¦
¦ avoidance system operates | ¦
¦ ¦ ¦
¦ normally. | ¦
¦ C ¦ - ¦ 0 ¦
(O) May be inoperative provided: | ¦
¦ ¦ ¦
¦ a) Alternate procedures
are | ¦
¦ ¦ ¦
¦ established and used, and | ¦
¦ ¦ ¦
¦ b) Takeoffs and landings are | ¦
¦ ¦
¦ ¦ not conducted in known or | ¦
¦ ¦ ¦
¦ forecast windshear | ¦
¦ ¦ ¦
¦ conditions. | ¦
¦ ***
6) TAWS C ¦ - ¦ 0
¦
| ¦
¦ ¦ ¦
¦
| ¦
¦ 22.
Flight Profile D ¦ 1 ¦ 0
¦
¦
¦ ***
Advisory System ¦ ¦
¦ ¦
¦ 23.
Flight Management C ¦ - ¦ 0 ¦
(O) May be out of currency | ¦
¦ ***
System Navigation ¦ ¦
¦ provided:
| ¦
¦ Databases ¦ ¦
¦ a) Current aeronautical
charts | ¦
¦ ¦ ¦
¦ are used to verify | ¦
¦ ¦ ¦
¦ navigation fixes prior to | ¦
¦ ¦ ¦
¦ dispatch, | ¦
¦ ¦ ¦
¦ b) Procedures are
established | ¦
¦ ¦ ¦
¦ and used to verify status | ¦
¦ ¦ ¦
¦ and suitability of | ¦
¦ ¦ ¦
¦ navigation facilities
used | ¦
¦ ¦ ¦
¦ to define route of
flight, | ¦
¦ ¦ ¦
¦ and | ¦
¦ ¦ ¦
¦ c) Approach navigation
radios | ¦
¦ ¦ ¦
¦ manually tuned and | ¦
¦ ¦ ¦
¦ identified. | ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦ PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 34-8
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦ SYSTEM
& ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
34 NAVIGATION ¦
¦ ¦ ¦
¦ 24.
Navigation C ¦ - ¦ - ¦
(O) May be out of currency | ¦
¦ ***
Management System ¦ ¦ ¦ provided: | ¦
¦ Navigation Databases ¦
¦ ¦ a) Current aeronautical charts | ¦
¦ ¦ ¦
¦ are used to verify | ¦
¦ ¦ ¦
¦ navigation fixes prior
to | ¦
¦ ¦ ¦
¦ dispatch, | ¦
¦ ¦ ¦
¦ b) Procedures are
established | ¦
¦ ¦ ¦
¦ and used to verify status | ¦
¦ ¦ ¦
¦ and suitability of | ¦
¦ ¦ ¦
¦ navigation facilities
used | ¦
¦ ¦ ¦
¦ to define route of
flight, | ¦
¦ ¦ ¦
¦ and | ¦
¦ ¦ ¦
¦ c) Approach navigation
radios | ¦
¦ ¦ ¦
¦ are manually tuned
and | ¦
¦ ¦
¦ ¦ identified. | ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 6 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 10/07/1993 ¦ 35-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
35 OXYGEN ¦ ¦
¦
¦
¦
1. Oxygen System C ¦ 1
¦ 0 ¦ As required by FAR. ¦
¦ (Passengers) ¦
¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 37-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦ --------------------------------------------
¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
37 VACUUM/PRESSURE ¦
¦ ¦ ¦
¦
1. Vacuum/Pressure C ¦ 2
¦ 1 ¦ (M) One may be inoperative
for ¦
¦ Pumps ¦ ¦
¦ day VFR operations.
¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT
LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT: ¦ REVISION NO: 6 ¦ PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 10/07/1993 ¦ 61-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
61 PROPELLERS ¦
¦ ¦ ¦
¦
1. Propeller C ¦ 1 ¦ 0
¦
¦
¦ Synchrophaser ¦
¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S.
DEPARTMENT OF TRANSPORTATION ¦
¦
MASTER MINIMUM EQUIPMENT LIST ¦
¦
FEDERAL AVIATION ADMINISTRATION ¦
¦
--------------------------------------------------------------------------- ¦
¦
AIRCRAFT:
¦ REVISION NO: 7 ¦
PAGE: ¦
¦ PIPER PA-34-200/200T/220T ¦ DATE: 06/05/2003 ¦ 77-1
¦
¦
--------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER
INSTALLED ¦
¦
SYSTEM & ¦
-------------------------------------------- ¦
¦
SEQUENCE ITEM ¦
¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦
NUMBERS ¦ ¦
--------------------------------------- ¦
¦
------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦
77 ENGINE INDICATING ¦
¦ ¦ ¦
¦
1. Exhaust Gas C ¦ 2
¦ 0 ¦ | ¦
¦ Temperature (EGT) ¦
¦ ¦ | ¦
¦ Gauges ¦ ¦
¦
| ¦
-------------------------------------------------------------------------------