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and operable unless:
1. The airplane is approved to be operated in accordance with a current Minimum Equipment
List (MEL) issued by the FAA.
Or;
2. An alternate procedure is provided in the basic FAA Approved Airplane Flight Manual for the
inoperative state of the listed equipment and all limitations are complied with.
NOTE
The following systems and equipment list does not include all equipment required by
the 14 CFR Parts 91 and 135 Operating Requirements. It also does not include
components obviously required for the airplane to be airworthy such as wings,
primary flight controls, empennage, engine, etc.
(Continued Next Page)
System and/or Component
KIND OF
OPERATION
COMMENTS
VF
R
DAY
VF
R
N
I
GHT
I
F
R
DAY
I
F
R
NI
GHT
I
CI
N
G
AUTO FLIGHT
1 - Autopilot (1) 0* 0* 0* 0* 0* * Required for single-pilot operation and
in RVSM airspace.
2 - Yaw Damper (1) 0* 0* 0* 0* 0* * Required above FL300. Autopilot will be
inoperative with inoperative yaw
damper.
3 - Electric Elevator Trim (1) 0 0 0 0 0 Manual elevator trim must be
operational.
4 - Yoke Autopilot Disconnect
Switches (2)
1* 1* 1* 1* 1* * Left side is required for single-pilot
operations. Both sides required for twopilot
operation.
**These items are part of the EICAS displayed on the MFD.
2-34 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
KINDS OF OPERATIONS EQUIPMENT LIST (Continued)
(Continued Next Page)
System and/or Component
KIND OF
OPERATION
COMMENTS
VF
R
DAY
VF
R
N
I
GHT
I
F
R
DAY
I
F
R
NI
GHT
I
CI
N
G
AIR CONDITIONING / PRESSURIZATION
1 - Flow Control Valves (2) 2 2 2 2 2
2 - Pressure Regulating Shutoff
Valves (2)
2 2 2 2 2
3 - Cabin Outflow Valves (2) 2 2 2 2 2
4 - Cabin Differential Pressure
Gauge** (1)
1 1 1 1 1
5 - Cabin Altitude Warning
System (1)
1 1 1 1 1
6 - Cabin Altitude Display** (1) 1 1 1 1 1
7 - Cabin Differential Pressure
Display** (1)
1 1 1 1 1
8 - Cockpit Temperature Control
System (except Air
Conditioner) (1)
1 1 1 1 1
9 - Cabin Temperature Control
System (except Air
Conditioner (1)
1 1 1 1 1
10 - Air Conditioning System (1) 0* 0* 0* 0* 0* * Temperature limits reduced with
inoperative air conditioner. Refer to
Figure 2-13.
11 - Pressurization Control
System (1)
1 1 1 1 1
12 - Cockpit Fan (1) 1 1 1 1 1
13 - Cabin Fan (1) 1 1 1 1 1
14 - Fresh Air Fan (1) 1 1 1 1 1
15 - Glareshield Avionics Fans
(3)
3 3 3 3 3
16 - Emergency Pressurization
Dump System (1)
1 1 1 1 1
**These items are part of the EICAS displayed on the MFD.
510FM-07 AA 2-35
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
KINDS OF OPERATIONS EQUIPMENT LIST (Continued)
(Continued Next Page)
System and/or Component
KIND OF
OPERATION
COMMENTS
VF
R
DAY
VF
R
N
I
GHT
I
F
R
DAY
I
F
R
NI
GHT
I
CI
N
G
COMMUNICATIONS
1 - Communication Systems
(VHF) (2)
* * 1* 1* 1* * Or as required by operating regulation.
2 - Audio Control Panels (Pilot
and Copilot) (2)
1* 1* 1* 1* 1* * Left side is required for single-pilot
operations. Both sides required for twopilot
operation.
3 - Static Wicks (16) 14* 14* 14* 14* 14* * One may be missing from any control
surface. No more than two total may be
missing.
4 - Hand Microphone (1) 1 1 1 1 1
ELECTRICAL POWER
1 - DC Generator (2) 2 2 2 2 2
2 - DC Generator VOLTS
Display** (2)
2 2 2 2 2
3 - DC Generator AMPS
Display** (AMPS) (2)
2 2 2 2 2
4 - Main Battery (1) 1 1 1 1 1
5 - Battery VOLTS Display** (1) 1 1 1 1 1
6 - Battery AMPS Display** (1) 1 1 1 1 1
7 - Battery Temperature
Monitoring System (1)
1* 1* 1* 1* 1* * Required only with NiCad battery
option.
8 - Standby Instrument Battery
(1)
1 1 1 1 1
EQUIPMENT / FURNISHINGS
1 - Passenger Seat Belts (4) * * * * * * One per occupied seat
2 - Crewmember Seat Belts (2) 1* 1* 1* 1* 1* * Left side required. Right side may be
inoperative if seat is not occupied.
3 - Aircraft Emergency Locator
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Citation Mustang airplane flight manual 1(22)
