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S For visual and non-precision approaches, the minimum autopilot use height is 400 feet
AGL.
S For precision approaches (ILS), with both engines operating, the minimum autopilot
use height is 80 feet AGL.
S For precision approaches (ILS), with one engine inoperative, the minimum autopilot
use height is 110 feet AGL.
S Operations with an ILS glidepath angle that exceeds 3.5 degrees are prohibited.
Effectivity: <1030>
S Airplanes equipped for operation in Reduced Vertical Separation Minimum (RVSM) airspace:
S The ADC source coupled to the active autopilot must be the same as that coupled to the
ATC transponder during flight in RVSM airspace.
3. ELECTRICAL SYSTEMS
A. Permissible Loads on AC System
Individual AC generator loading must not exceed the following values:
ALTITUDE
LOAD LIMITATION
(KVA)
(FEET) MAIN GENERATOR
(EACH)
APU GENERATOR
0 - 41,000 40 40
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Systems Limitations
02--08--2
3. ELECTRICAL SYSTEMS (CONT’D)
B. Permissible Loads on DC Systems
(1) In Flight
The maximum permissible continuous load on each TRU is 120 amps.
(2) Ground Operation
To protect the flight compartment CRT displays, the maximum permissible time for
ground operations with DC power only is 5 minutes.
C. Circuit Breaker Reset (In Flight)
A circuit breaker must not be reset or cycled (i. e., opened or closed) unless doing so is
consistent with explicit procedures specified in this Airplane Flight Manual or unless, in the
judgement of the Pilot-in-Command, that resetting or cycling of the circuit breaker is
necessary for the safe completion of the flight.
4. FLIGHT CONTROLS - LIFT/DRAG DEVICES
A. Slats / Flaps
S En-route use of slats / flaps is prohibited.
S Flight with slats / flaps extended at altitudes above 15,000 feet is prohibited.
B. Flight Spoilers
Flight spoilers must not be extended in flight below an altitude of 300 feet AGL.
To ensure adequate maneuver margins, flight spoilers must not be extended in flight at
airspeeds below the recommended approach speed plus 10 KIAS (refer to PERFORMANCE
- LANDING PERFORMANCE).
5. STALL PROTECTION SYSTEM
Both stall protection system switches must remain on for all phases of flight.
6. THRUST REVERSERS
S Thrust reversers are approved for ground use only, activation of the reverse thrust levers is
prohibited in-flight.
S The thrust reversers are intended for use during full stop landings. Do not attempt a
go-around maneuver after deployment of the thrust reversers.
S Take-off with any thrust reverser icons or EICAS warning and/or caution messages
displayed is prohibited.
S During landing, application of maximum reverse thrust is not permitted at airspeeds below
60 KIAS. Below 60 KIAS, reverse thrust should be reduced to idle.
S During pre-flight check of the thrust reversers with the airplane stationary, reverse thrust
must be limited to reverse idle.
S Backing-up using thrust reversers is prohibited.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
LIMITATIONS
Systems Limitations
02--08--3
7. NOSE WHEEL STEERING SYSTEM
Towbarless towing is prohibited <JAA>.
8. TAXI LIGHTS
The taxi lightsmust be switched OFFwhenever the airplane is stationary in excess of 10 minutes.
9. WHEEL BRAKE COOLING LIMITATIONS
Brake cooling times (established in accordance with PERFORMANCE - TAKE-OFF
PERFORMANCE -MAXIMUMALLOWABLE BRAKE TEMPERATURE FORTAKE-OFF)must be
observed between a landing or a low-energy rejected take-off (RTO) and a subsequent take-off,
to ensure that sufficient brake energy is available to bring the airplane to a complete stop, if the
subsequent take-off is rejected.
10. MINIMUM DESCENT ALTITUDE
When setting theMDAmarker on the barometric altimeter using the DH/MDA knob on the altitude
reference panel, the next highest 10 foot increment must be selected if the altitude is not at a 10
foot increment.
11. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance in order to comply
with a TCAS resolution advisory (RA) command.
12. INTEGRATED STANDBY INSTRUMENT (ISI)
Flight Operations
S When NAV 1 is tuned to a valid ILS frequency, the ISI will display localizer and glideslope
deviation while on the backcourse approach. Use of the ISI localizer and backcourse
information is prohibited during backcourse approaches.
13. CONFIGURATION DEVIATION LIST
If the aircraft is to be operated with certain secondary airframe and/or any nacelle parts missing,
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