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The minimum autopilot use height for precision approaches (ILS) is 80 feet AGL.
Operations with an ILS glidepath angle that exceeds 3.5 degrees are prohibited.
3. BLEED AIR SYSTEMS
The bleed air 10th stage valves must be closed for take-off and landing if the engine cowl and/or wing anti-ice systems have been selected on.
If above 40,000 feet, one air-conditioning unit or cowl anti-ice system must be selected on for each engine.
4. ELECTRICAL SYSTEMS
A. Permissible Loads on AC System
Individual AC generator loading must not exceed the following values:
B. Permissible Loads on DC Systems
The maximum permissible continuous load on each TRU is 100 amps.
5. FLIGHT CONTROLS – LIFT/DRAG DEVICES
A. Flaps
Enroute use of flaps is prohibited.
Flight with flaps extended at altitudes above 15,500 feet is prohibited.
B. Flight Spoilers
Flight below an altitude of 300 feet AGL with flight spoilers extended is prohibited.
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 Chapter 6; PERFORMANCE – LANDING PERFORMANCE of the Airplane Flight Manual).
LIMITATIONS Systems Limitations Vol. 1 02.08.2
Oct 05/06
6. STALL PROTECTION SYSTEM
Both stall protection system pusher switches must remain on for all phases of flight.
The stall protection test indicator must only be used for stall protection system functional test purposes. The PFD normalized AOA indicator is advisory only, it does not replace the airspeed indicator as
primary speed instrument, and it does not replace the stick shaker as primary stall warning. The PFD normalized AOA indicator shall not be used during take-off.
7. THRUST REVERSERS
Thrust reversers are approved for ground use only.
The thrust reversers are intended for use during full stop landings. Do not attempt a go-around
maneuver after deployment of the thrust reversers.
Backing the airplane with the use of reverse thrust is prohibited.
Take-off with any of the following thrust reverser icons or EICAS messages displayed is
prohibited:
.
REV icon on N1 gauge,
.
L (R) REV UNLOCKED caution message, and
. L (R) REV UNSAFE caution message.
During landing, application of maximum reverse thrust is not permitted at airspeeds below 60 KIAS. Below 60 KIAS, reverse thrust must be reduced to 60% N1 or less.
The maximum demonstrated crosswind component approved for use of reverse thrust is 24 knots [at 33 feet (10 meters) tower height]. This value was demonstrated on a dry runway, and is considered limiting.
8. TAXI LIGHTS
The taxi lights must be selected off whenever the airplane is stationary in excess of 10 minutes.
9. WHEEL BRAKE COOLING LIMITATIONS
Brake cooling times (established in accordance with the procedures in Chapter 6; PERFORMANCE – TURN-AROUND TIME of the Airplane Flight Manual) 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.
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