1
AR 72
FLIGHT CREW
OPERATING MANUAL
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INTRODUCTION
1st PART SYSTEMS DESCRIPTION
2nd PART OPERATING PROCEDURES
3rd PART PERFORMANCE
FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
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F.C.O.M.
0.00.00
CONTENTS
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CONTENTS
LIST OF TEMPORARY REVISIONS (L.T.R.)
0.02.00 REASON OF TEMPORARY REVISIONS (R.T.R.)
SHIPPING NOTE TEMPORARY PAGES (S.N.T.P.)
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LIST OF EFFECTIVE TEMPORARY PAGES (L.E.T.P.)
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LIST OF NORMAL REVISIONS (L.N.R.)
0.06.00
REASON OF THE REVISION
0.07.00
SHIPPING NOTE NORMAL PAGES (S.N.N.P.)
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LIST OF EFFECTIVE NORMAL PAGES (L.E.N.P.)
0.09.00
LIST OF MOD/MP/SB (L.O.M.)
0.10.00
CROSS REFERENCE TABLE (C.R.T.)
0.40.00
ORGANIZATION OF THE MANUAL
0.50.00
STANDARD NOMENCLATURE
0.60.00
UNITS CONVERSION TABLE
ROFA-00-00-10-001-A001AA
AR 72
F.C.O.M.
FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
ORGANIZATION OF THE MANUAL
0.40.00
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The Flight Crew Operating Manual (FCOM) provides operating crew members with
information on the ATR 72 technical procedures and performance characteristics. It
will be used as a crew manual for training purposes.
The contents are divided into four parts:
• INTRODUCTION
• Part 1 Systems description
• Part 2: Procedures and techniques
Part 3: Performances.
FCOM is complementary to the approved airplane flight manual.
Any comment or suggestion related to the content of the FCOM should be
addressed to
AVION DE TRANSPORT REGIONAL
DIRECTION SUPPORT EXPLOITATION
1, ALLEE PIERRE NADOT
31712 BLAGNAC CEDEX
FRANCE
FOR PRINTING
AND
DISTRIBUTION
ATR TRAINING CENTER
ATC/T/GSO
1. ALLEE PIERRE NADOT
31712 BLAGNAC CEDEX
TEL: 61-93-13-80
FAX: 61-93-13-67
FOR TECHNICAL
OR
PROCEDURAL
CONTENT
FLIGHT CREW OPERATING MANUAL
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DEFINITION OF THE PAGE
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A page is defined by:
a reference: Part / Chapter / Section / page number
Example: 2.05.10 page 20
effectivity criteria determining the page sequence
Example: Equipment, Modification, Engine...
A page with a given reference may have several sequences:
Example: 2.05.10 page 20
Mod XXXX
4
I
Mod XXXX + YYYY
Sequence 001
Sequence 002
+
Sequence 003
All the sequences cover, for a given reference, all aircraft of a specific type. These
airlines receive a part of these sequences to cover their float.
A sequence can be valid for several aircraft but an aircraft can not have several
sequences.
PAGINATION
TOP OF PAGE
RDFA-00-00-10-002-A001AA
1
2
3
A
5
AFCS
1.04.20
P 1
100
NR72
F.C.O.M.
CONTROLS
DEC 86
GIE ATR logo (or airline logo)
• aircraft type
• manual type
10
9
8
7
��
2) Title of Chapter
3 Number of part, chapter and section in the manual
4 Page Numbering
Particular case: a page followed by an alphabetic letter must be inserted
between 2 pages.
Example: page 11A must be inserted between page 11 and 12.
5) Sequence number: this code is used by the manufacturer for the manual
management. It depends on the modification, engine, unit, etc.
AR 72
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6 Zone for airline: if 2 letters (XX) are indicated on the page, this one is customized
to airline XX.
Date of revision (date of page issue)
8) Zone for standard
9) Zone for unit
10) Title of section
BOTTOM OF PAGE
ROFA-OD-00-10-003-AD01AA
Mod.: 1175
Eng. :
Model:
1
2
3
This modification zone can contain up to 4 modifications applicable for this page.
Above 4 modifications, a GM N�� (9 XXX) relative to several modifications will be
indicated. This number will also be indicated in the table, page 0.00.45.
? Indication of engine type installed on aircraft; if there is no indication, the page is
valid for all engines (PW124, PW127...).
3 Indication of aircraft type and modet.
MANUAL UPDATE
Your manual comprises 2 types of pages:
-white pages (normal)
- yellow pages (temporary)
These 2 families of pages (white and yellow) have a separated management.
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FLIGHT CREW OPERATING MANUAL
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Refer to SHIPPING NOTE NORMAL PAGES (SNNP) which precises if it is a total
shipment. In that case, throw all the pages of your last manual and replace them by
the new shipment.
IF IT IS NOT A TOTAL SHIPMENT
You must received:
the LIST OF NORMAL REVISIONS (LNR)
- the revised or new white pages
- the SHIPPING NOTE NORMAL PAGES (SNNP)
This note lists all revised, new or cancelled white pages, and only these pages,
during the last revision. This note serves as guide to update your manual.
Example:
I
<<< ADD >>
>>> : 1.05.20 p.1: replace the old page by the revised page
: 1.06.40 p.2: add new page
« DESTROY » : 1.10.20 p.3: delete old page
When you have finished the update, you can throw the SHIPPING NOTE NORMAL
PAGES (SNNP)
a new LIST OF EFFECTIVE NORMAL PAGES (LENP) :
This list sums up all white pages to be found in your manual after the update.
YELLOW PAGES (TEMPORARY]
They are issued during a temporary revision, as it is impossible to wait until the issue
of a Normal Revision.
You receive a temporary revision (yellow)
the LIST OF TEMPORARY REVISIONS (LTR)
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appear in column « Output Date »
the revised or new yellow pages
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the LIST OF EFFECTIVE TEMPORARY PAGES (LETP): it lists all yellow pages to be
found in your manual after update of your last Temporary Revision.
Note:
A Temporary Revision may be cancelled only by a Normal Revision or
by another Temporary Revision numerically higher.
in case you have a yellow page and a white page for one page :
��
you keep the white page
you place yellow page on the white page and until next revision, the
information of yellow pages have priority.
In any case, please pay attention to sheets effectivity on the lists of
effective pages.
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FLIGHT CREW OPERATING MANUAL
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2
On your manual, on pages having a technical revision, code «R» may
appear on the LH margin. This code identifies the part of the text which
has been modified on the page.
The FCOM is customized for each airline.
In the lists of effective pages, each sheet is represented by 2 lines:
the first line concerns the recto
- the second line concerns the verso,
when recto and verso are printed.
If only recto sheet is printed, it is represented by a line.
Each sheet is associated with one (or several) number which represents the aircraft
FSN (Fleet Serial Number). The sheet is exclusively associated with a specific aircraft
in an airline.
At page 0.00.47, you will find the list of the different registrations of your aircraft.
To understand the effectivity of the sheets, you must read:
Example: XX 001 003 XX 001 to 003 �� 3 aircraft valid
XX 001 + XX 003 - XX 001 and 003�� only 2 aircraft valid
AR 72
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STANDARD NOMENCLATURE
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GLOSSARY OF STANDARD NOMENCLATURE
Anti-icing Advisory System
AAS
ABNORM (ABN)
Abnomal
AC
ACARS
AC BTC
AC BTR
ACCU
AC EBTC
ACW
ADC
ADF
ADI
ADS
ADU
A/EREC
AFCS
A/FEATH
AFT
AFU
AGB
AGL
AH
AHRS
Alternating Current
ARINC Communication Addressing and Reporting System
AC Bus Tie Contactor
AC Bus Tie Relay
Accumulator
AC Emer Bus Transfer Contactor
Alternating Current Wild Frequency
Air Data Computer
Automatic Direction Finding
Attitude Director Indicator
Air Data System
Advisory Display Uni
Aulo Erection
Automatic Flight Control System
Auto Feathering
Rear Part
Auto Feather Unit
Accessory Gear Box
Above Ground Level
Ampere - Hours
Attitude and Heading Reference System
Attitude and Heading Reference Unit
Angle of Attack
Auto-Pilot
AHRU
AIL
Aileron
ALT
Altitude
ALTM
Altimeter
ALTN
Alternate
AMP
Ampere
ANN
Annunciator
AOA
AP
APC
APP
Approach
APU
ARM
Armed
ASAP
ASCB
ASD
ASI
ASTR
ASYM
ATC
Active Phase Control
Auxiliary Power Unit
As Soon As Possible
Avionics Standard Communication Bus
Accelerate Stop Distance
Air Speed indicator
AC Stand by Bus Transfer Relay
Asymmetry
Air Traffic Control
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FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
STANDARD NOMENCLATURE
Automatic Test Equipment
Automatic Take off Power Control System
AR 72
F.C.O.M.
AA
ATE
ATPCS
ATT
Attitude
ATTND
Attendant
AUTO
Automatic
AUX
Auxiliary
AVAIL
Available
AZ
BARO
BAT
BC
BITE
BPCU
BPU
BRG
BRK
B-RNAV
BRT
BSC
BTC
BTR
BXR
CAB
CAC
CAP
CAPT
CAT
C/B
CCAS
CCW
CD
CDI
CFC
CG
CHAN
CHC
CHG
C/L
CL
CL
CLA
CLB
Azimuth
Barometric
Battery
Back Course
Built in Test Equipment
Bus Power Control Unit
Battery Protection Unit
Bearing
Brake
Basic Area Navigation
Bright
Battery Start Contactor
Bus Tie Contactor
Bus Tie Relay
Battery Transfer Relay
Cabin
Crew Alerting Computer
Crew Alerting Panel
Captain
Category
Circuit Breaker
Centralized Crew Alerting System
Counter clockwise
Coefficient of Drag
Course Deviation Indicator
Constant Frequency Contactor
Center of Gravity
Channel
Charge Contactor
Charge
Check List
Condition Lever
Coefficient of Lift
Condition Lever Angle
Climb
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AR 72
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AA
CLR
CM
CMPTR
FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
STANDARD NOMENCLATURE
Clear
Crew Member
Computer
Communication
Compartment
Configuration
Continuous
Correction
Auto Pilot Coupling
Continuous Repetitive Chime
Course
COM
COMPT
CONFIG
CONT
CORRECT
CPL
CRC
CRS
CRT
CRZ
Cruise
CTL
Control
CVR
CW
DADC
DADS
DC
DEC
DELTA P
DEV
DFDR
DFZ 600
DGR
DH
DIFF
DISCH
DIM
DIST
DME
DN
DSPL
EADI
EBCC
EBTC
ECU
EEC
Cathodic Ray Tube
Cockpit Voice Recorder
Clockwise
Digital Air Data Computer
Digital Air Data System
Direct Current
Declination, Decrease
Differential Pressure
Deviation
Digital Flight Data Recorder
Flight Control Computer
Degraded
Decision Height
Differential
Discharge
Light Dimmer
Distance
Distance Measuring Equipment
Down
Display
EFIS
EGHR
EHSI
EHV
ELEC
Electronic Attitude Director Indicator
Emergency Battery Charge Contactor
Emer Bus Transfer contactor
Electronic Control Unit
Engine Electronic control
Electronic Flight Instrument System
External Ground Handling Relay
Electronic Horizontal Situation Indicator
Electro Hydraulic Valve
Electrical
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FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
Engine
External Power Contactor
Equipment
Essential
AR7
F.C.O.M.
STANDARD NOMENCLATURE
ELV
Elevation
EMER
Emergency
ENG
EPC
EQPT
ESS
ET
ETOPS
EXT
EXC
F
FAIL
FCOC
FD
FDAU
FDEP
FEATH, FTR
FF
FGC
FGS
FI
FLT
FMA
FMS
F/O
FOS
FQI
FT
FTO
FU
FWD
GA
GAL
GC
GCU
GEN
GI
GMT
GND
GNSS
GPS
GPU
GPWS
GRD
G/S
Elapsed Time
Extended Twin Operations
Exterior, External
External Power/Service Bus Contactor
Farenheit
Failed, Failure
Fuel Cooled Oil Cooler
Flight Director
Flight Data Acquisition Unit
Flight Data Entry Panel
Feathered, Feathering
Fuel Flow
Flight Guidance Computer
Flight Guidance System
Flight Idle
Flight
Flight Modes Annunciators
Flight Monitoring System
First Officer
Flight Operations Software
Fuel Quantity Indication
Foot, Feet
Final Take Off
Fuel Used
Forward
Go Around
Galley
Generator Contactor
Generator Control Unit
Generator
Ground Idle
Greenwitch Mean Time
Ground
Global Navigation Satellite System
Global Positioning System
Ground Power Unit
Ground Proximity Warning System
Ground
Glide Slope
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ART
F.C.O.M.
AA
GSPD
GXS
HBV
HD
HDG
HDLG (HDL)
HEBTC
HF
HI
HLD
HMBTC
HMU
HOBV
HP
HSI
HTG
R HU
HYD
IAF
IAS
IDT
IGN
ILS
IMU
IN
INC
IND
IN/HG
INHI
INOP
INS
INST
INT
INU
INV
IRS
ISOL
ISV
ITT
KHZ
KT
LAT
LAV
STANDARD NOMENCLATURE
Ground Speed
ACW Generator/Service Bus Contactor
Handling Bleed Valve
Head Down
Heading
Handling
Hot Emer Battery Transfer Contactor
High Frequency
High
Hold
Hot Main Battery Transfer Contactor
Hydromechanical Unit
Handling Overboard Valve
High Pressure
Horizontal Situation Indicator
Heating
Head Up
Hydraulic
Initial Approach Fix
Indicated Air Speed
Ident
Ignition
Instrument Landing System
Initial Measurement Unit
Inertial Navigation
Increase
Indicator
Inches of Mercury
Inhibit
Inoperative
Inertial Navigation System
Instrument
Interphone
Inertial Navigation Unit
Inverter
Inertial Reference System
Isolation
Isolation Shut-off Valve
Inter Turbine Temperature
Kilo-Hertz
Knot
Lateral
Lavatory
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STANDARD NOMENCLATURE
Pound
AA
LB
LBA
LDG
L/G
LH
LIM
Lowest Blade Angle
Landing
Landing Gear
LOC
LO-PR
LP
LT
LVL
MAC
MAN
MAP
MAX
MB
MBCC
MBTC
MC
MCDU
MCT
MEA
MECH
MFC
MFCU
MGT
MHZ
LNAV
LO
Left Hand
Limitation
Lateral Navigation
Low
Localizer
Low Pressure
Low Pressure
Light
Level
Mean Aerodynamic Chord
Manual
Ground Mapping
Maximum
Millibar
Main Battery Charge Contactor
Main Bus Transfer Contactor
Master Caution
Multifunction Control Display Unit
Maximum Continous
Miniinum En route Altitude
Mechanic
Multi Function Computer
Mechanical Fuel Control Unit
Management
Megahertz
MIC
Microphone
MIN
Minimum
MISC
Miscellaneous
MKR
Marker
MLS
MLW
MM
Microwave Landing System
Maximum Landing Weight
Millimeter
MMO
Maximum Operating Mach
MOD
Modification
MSG
Messages
MSN
Manufacturer Serial Number
MTOW
MW
MZFW
NAC
Maximum Take off Weight
Master Warning
Maximum Zero Fuel Weight
Nacelle
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F.C.O.M.
NAV
NDB
NDB (GPS)
NEG
NH
NIL
NL
NM
NORM
NP
NPU
N/W
FLIGHT CREW OPERATING MANUAL
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STANDARD NOMENCLATURE
Navigation
Non Directional Beacon
Navigation Data Base
Negative
High Pressure Spool Rotation Speed
Nothing, No Object
Low Pressure Spool Rotation Speed
Nautical Mile
Normal
Propeller Rotation Speed
Navigation Processor Unit
Nose Wheel
Nose Wheel Steering
Outside Air Temperature
Omni Bearing Selector
Other traffic
Outboard
Overboard
NWS
OAT
OBS
���
OUTB
OVBD
OVERTEMP
OVHT
Overtemperature
Overheat
OVRD
Override
OXY
Oxygen
PA
PB
PCU
PEC
PF
PFTS
PIU
PL
PLA
PNF
PNL
POS
PRESS
Passenger Address
Push Button
Propeller Control Unit
Propeller Electronic Control
Pilot Flying
Power Feeder Thermal Sensor
Propeller Interface Unit
Power Lever
Power Lever Angle
Pilot Non Flying
Panel
Position
Pressurization, Pressure
PRIM
Primary
PRKG
Parking
PROC
Procedure
PROP
PRV
PSEU
PSI
PSU
PSV
PT
PT (TCAS)
Propeller
Pressure Regulating Valve
Proximity Switch Electronic Unit
Pound per Square Inch
Pax Service Unit
Propeller Servo Valve
Point
Proximity traffic
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AA
AR 72
F.C.O.M.
PTT
PTW
PVM
PWM
PWR
QAR
QT
QTY
RA (TCAS)
RA
RAD/ALT
RAD/INT
RAIM
RCAU
RCDR
RCL
RCU
RECIRC
REV
RGA
RGB
RH
RLY
RMI
RNP
RPM
RQD
RTO
RUD
SAT
SB
SBTC
SBY
SC
SCU
SDTC
SEL
SGL
SGU
SID
SMK
FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
STANDARD NOMENCLATURE
Push To Talk, Push To Test
Pitch Thumb Wheel
Propeller Valve Module
Pulse Width Modulation
Power
Quick Access Recorder
Quart
Quantity
Resolution Advisory
Radio Altitude
Radio Altitude
Radio/Interphone
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Receiver Autonomous Integrity Monitoring
Remote Control Audio Unit
Recorder
Recall
Releasable Centering Unit
Recirculation
Reverse
Reserve Go-Around
Reduction Gear Box
Right Hand
Relay
Radio Magnetic Indicator
Required Navigation Performance
Revolution Per Minute
Required
Reserve Take-Off
Rudder
Static Air Temperature
Service Bulletin
Stand By bus Transfer Contactor
Stand By
Single Chime, Starter Contactor
Signal Conditioning Unit
Static Inverter Override Transfer Contactor
Selector
Single
Symbol Generator Unit
Standard Instrument Departure
Smoke
SMKG
Smoking
S/O (SO)
Shut Off
SOV
Shut Off Valve
SPD
SPLR
Speed
Spoiler
F.C.O.M.
AA
SPLY
SSR
STAB
AR 72
FLIGHT CREW OPERATING MANUAL
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STANDARD NOMENCLATURE
Supply
Service Bus Select Relay
Stabilizer
STAR
Standard Arrival
STBY
STR
Stand By
Service Bus Transfer Relay
STRG
Steering
SVCE
Service
SW
Switch
SYNPHR
Synchrophaser
SYS
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TOW
TQ
TRU
TTG
UBC
U/F
UHF
UNCPL
UNDV
TA (TCAS)
TAS
TAT
TBD
TCS
TEMP
TGT
TK
TLU
TM
T/O (TO)
TOD
TOR
System
TRAFFIC Advisory
True Air Speed
Total Air Temperature
To be Determined
Touch Control Steering
Temperature
Target
Tank
Travel Limiting Unit
Torque Motor
Take off
Take-Off Distance
Take-Off Run
Take off weight
Torque
Transformer Rectifier Unit
Time To Go
Utility Bus Contactor
Underfloor
Ultra High Frequency
Uncouple
Undervoltage
UNLK
Unlock
UTLY
Utility
VC
VENT
Calibrated Airspeed
Ventilation
VERT
VHF
VMCA
VMCG
VMCL
VMO
VNAV
Vertical
Very High Frequency
Minimum Control Speed in flight
Minimum Contorl Speed on ground
Minimum Conrol Speed during landing approach
Maximum Operating Speed
Vertical Navigation
AR 72
F.C.O.M.
AA
VOR
VSI
VU
WARN
WAT
WBM
WOW
XFEED
XFR
YD
ZA
ZCTH
ZFW
ZP
ZRA
FLIGHT CREW OPERATING MANUAL
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STANDARD NOMENCLATURE
VHF OMNI Directional Range
Vertical Speed Indicator
Visual Unit
Warning
Weight Altitude Temperature
Weight and Balance Manual
Weight On Wheel
Cross feed
Transfer
Yaw Damper
Aircraft Altitude
Theoretical Cabin Altitude
Zero Fuel Weight
Pressure Altitude
Radio Altimeter Altitude
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ARD
F.C.O.M.
AA
FLIGHT CREW OPERATING MANUAL
PRELIMINARY PAGES
UNITS CONVERSION TABLE
0.60.00
P1
001
JUL 99
METRIC
�� US
US > METRIC
1 millimeter (mm)
1 meter (m)
1 meter (m)
1 kilometer (km)
0
1.
5
=
.0394 inch (in)
1 inch (in)
3.281 feet (ft)
1 foot (ft)
25.4 millimeters (mm)
.3048 meter (m)
1.094 yard (yd)
1 yard (yd)
-LLL
.914 meter (m)
--
540 nautical mile (nm)
1 nautical mile (nm)
1.852 kilometer (km)
10
15
20
25
30
35
inches
F
.2
.3
4
.5
.6
,7
.8
.9
meter
feet
���
5
10
0
A
1
1
2
3
9+0
15
20
25
30
+
4
5
6
7
8
9
10
meters
0
1
N-
2
3
4
5
nautical miles
.....
T
0
2
3
4
LO
5
6
7
8
9
ROFA-00-00-50-001-A001AA
10
meters x 1000
LENGTH
VO DE LEI LO
1 meter/second (m/s) 3.281 Feet/second (ft/s)
1 foot/second (ft/s)
1 Kilometer/hour(km/h)= .540 knot (kt)
1 knot (kt)
.3048 meter/second (m/s)
1.852 kilometer/hour (km/h)
feet/second
5
10
15
20
25
30
.[
3
4
5
6
8
9
meters/second
10
knots
2-
3
5
2
3
4
5
6
7
8
9
10
0
ROFA-00-00-60-001-8001AA
1 gramme (g)
1 kilogramme
1 ton (t)
W
3E-KIT
kilometers/hour
=
0.0353 ounce (oz)
1 ounce (oz)
28.35 grammes (g)
==
2.205 pounds (lb)
1 pound (lb)
=
- 2.205 pounds (lb)
1 pound (lb)
T
.4535 kilogramme (kg)
.0004535 ton (1)
1
.....
1
2
3
-
17
5
10
+
0
2
3
4
5
1
5000
10000
2
3
ROPA-00-00-60-001-C001AA
-N
க.
3
ounces
T
7
10
grammes
15
20 pounds
----་་ ་
!
6
7
8
10
kilogrammes
pounds
15000
20000
LO
5
6
7
8
9
10
tons
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FLIGHT CREW OPERATING MANUAL
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UNITS CONVERSION TABLE
0.60.00
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! Newton (N)
1 deca Newton (daN)
METRIC ������ US
.2248 pound-force (lbf)
-
US > METRIC
1 pound force (ibf)
4.448 Newtons (N)
F
2.248 pound-force (lbf) 1 pound-force ([bf)
.4448 deca Newton (daN)
Pound-force (lbf)
0
5
10
15
20
누
...
0
1
2
3
4
5
6
7
8
9
10
Newtons (N)
P
ROFA-00-00-60-002-A001AA
1 bar- 14.505 pound-force per square inch (P.S.I.) | 1 pound-force per square inch (PS.I.) – .0689 bar
} millibar (mbar) = .0145 PS.I.
1 P.S.t. 68.92 millibars (mbar)
0
0
1
5
2
3
4
ROFA-OD-00-60-002-B001AA
1 liter (}} .2642 U.S. Gallons
1 cubic meter (m³)
tw
264.2 U.S. Gallons
P.S.!
10
15
LO
5
6
7
8
9
Milllbars x 100
10
1 US Gallon 3.785 liters (1)
—
1 US Gallon = .003785 cubic meter (m³)
US Gallons
0
5
10
15
20
25
I..
M
T
0
1
2
3
4
5
6
7
8
9
10
Liters x 10
M
0
M
ROFA-00-00-60-002-C001AA
1 meter x deca Newton (m.daN)
- 08.50 pound-force x inch (Ibf.in)
1 pound-force x inch (Ibf.in)
= .0113 meter x deca Newton (mdaN)
pound-force x inch(x 100)
0
1
2
3
4
5
6
7
0
1
2
3
4
10
5
6
7
8
M
ROFA-00-00-60-002-0001AA
8
9
9
10
meters x deca Newton
P
TENFE
t (��C)
=
5
g
9
{1 (��F)
-
32)
t { · F)
t(C) + 32
5
M
*F
R
-60 -40 -20 0 20 40 60 80 100 120 140 160 160 200 220 240 260 280 300 320
+
T
1����
-60
40
20
0
20
40
60
BO 100 120 140
- 1
160
'C
R
ROFA-00-00-60-002-E001AA
m:
E
AR 72
F.C.O.M.
AIRCRAFT GENERAL
CONTENTS
1.00.00
P 1
001
DEC 96
1.00.00
CONTENTS
R 1.00.10
GENERAL
1.09.20
COCKPIT
1.00.30
DOORS
R
30.1 DESCRIPTION
R
30.2
CONTROLS
R
30.3
ELECTRICAL SUPPLY/MFC LOGIC/SYSTEM MONITORING
1.00.40
LIGHTING
R
40.1 DESCRIPTION
R
40.2
CONTROLS
R
40.3
ELECTRICAL SUPPLY/MFC LOGIC
1.00.50
WATER AND WASTE SYSTEM
R
50.1 DESCRIPTION
R
50.2
ELECTRICAL SUPPLY
