ENGINE

REVERSERS

100%

Note: Any exceedance or peak must be monitered and logged by the crew.

102.4% (8)

Note: For airplanes pre-mod the N2 limit is 102.5%

948°C (1)

Note 1: Takeoff Thrust is limited to 5 Min.

Min: 34 PSI

Max: 110 PSI (2) (7)

Note 2: May be exceeded during starts if oil temp. is below 21° C. The engine must remain at idle until the oil PSI is less than 110 PSI

Note 7: Operation in oil pressure amber range111 and 115 psi is permitted in all opeational modes and time limited to 5 Minutes, Or between 116 and 155 PSI in all operational modes time limited to 2 minutes. Total time above 110 PSI may not exceed 5 Min.

Min: 50 PSI (9)

Max: 110 PSI (7)

Note 9: While this is an abnormal condition, operation between 50 and 34 PSI is permitted during takeoff and go around phases (AE3007A Only) 

Note 7: Operation in oil pressure amber range111 and 115 psi is permitted in all opeational modes and time limited to 5 Minutes, Or between 116 and 155 PSI in all operational modes time limited to 2 minutes. Total time above 110 PSI may not exceed 5 Min.

LP Spool: 1.8 IPS (4)

HP Spool: 1.1 IPS (4)

Note 4: Vibration in the amber range below 2.5 IPS is time limited to 5 minutes during the takeoff or go- around phases or 10 seconds during the remainder of the flight phases. 

High vibration indicates a malfunction that may worsen and increase vibration severity. Therefore, a continuous engine operation with vibration in the amber range is not recommended. 
According to engine vibration limits, the pilot may not elect to reduce TLA for vibration below vibration 2.5 IPS time limited to 5 minutes during takeoff or go-around or 10 seconds during the remainder flight phases. If vibration returns to the green range within 5 minutes, the flight may continue but vibration causes should be investigated before the next flight.

Vibration in any flight phase in the amber range up to 1.5 IPS for less than 30 seconds does not require maintenance action.

Prior to take-off,the engines must be allowed to run at low thrust to stabilize the engine temperatures before take-off thrust is adjusted. 

After start, the engines must run at idle or taxi thrust during at least 4 minutes for cold engines (Shut down for more than 90 min) and 2 minutes for warm engines. 

To Increase N2 above 83% the engine oil must be at 40°C Minimum. In lieu of this limit, it is acceptable to either run the engine for at least 8 min. or complete a static run up to 88% N2, stabilize, and check to ensure that oil pressure is equal to or less than 83 PSI

Landing Gear- Up

Flaps-Up

Minimum Airspeed- 200Kias

Max Altitude- 15,000 Ft.

-Use Static Air Temperature (SAT) on ground or for takeoff operations and Total Air Temperature (TAT) for operations in flight.-

400 Amps below 30,000 Ft

300 Amps above 30,000 Ft

Maximum duration of ISIS when operating on batteries is 40 Min.

Note: The max duration of battery power can be extended to 45 Min if the Pitot 3 Sensor Heating buttion is turned off when not operating in icing conditions.

Airplane must not be moved during power-up initialization. Do not cage attitude in turning flight.

On airplanes equipped with a cockpit security door, two crewmembers must be in the cockput during all flight phases.

If one of the pilots leaves the flight deck, he must be replaced in the cockpit by another crewmember .

Positive identification of the person wishing to enter the flight deck must be obtained before opening the door.

The security cockpit door must be kept closed and locked at all times during flight except to permit access and egress according to GOM procedures 6-1.2.1 for opening, closing and locking the door.

Anytime that cockpit door is opened in flight, a challenge and response closing and locking verification procedure must be used to verify that the door is closed and locked.

Autopilot

Min. Altitude Coupled to ILS

Autopilot

Single-engine Go-around

Max Recommended Crosswind
(Non-AFM)

Dry Runway

Max Recommended Crosswind
(Non-AFM)

Wet Runway

Max Recommended Crosswind
(Non-AFM)

Runway with Compacted Snow

Max Recommended Crosswind
(Non-AFM)

Runway with Standing Water or Slush

Max Recommended Crosswind
(Non-AFM)

Runway with Ice (no melting)

Maximum operating altitude when one bleed or one pack is closed is 25,000 ft. (AFM).

When operating with APU bleed supplying Pack 1 (Eng. 1 bleed – closed) and engine 2 supplying Pack 2 (crossbleed closed), maximum operating altitude is 37,000 ft. (Non-AFM)

AE3007A1 (LR)

Oil Temperature MIN and MAX

MIN 21° C (3)

MAX 126° C

(3) Minimum oil temperature for starting is -40°C for lubrication oil specified by MIL-L-23699D.