ExpressJet EMB-145

Minimum flight crew

The EMB-145 is certified in the transport category in the following conditions:

Maximum runway slope:

Runway surface:

Maximum tailwind:

Maximum temperature for aircraft is:

Minumum / Maximum takeoff & landing pressure altitude:

Minimum / Maximum SAT at FL370:

Minimum / Maximum SAT fro takeoff:

Minimum SAT below FL250:

TAT above FL250 in cruise flight is limited to:

MX insprction needed when landing below:

Vlo for retraction/extention:

Vle:

Va:

Maximum flap extention speed for flaps 9:

Maximum flap extention speed for flaps 18:

Maximum flap extention speed for flaps 22:

Maximum flap extention speed for flaps 45:

Maximum flap extention speed for flaps 45 XR:

Above 10,000' with the YD disengaged, maximum speed for flaps 22 (XR)

Above 10,000' with the YD disengaged, maximum speed for flaps 45 (XR)

For non-XR aircraft, the flap 45 Vfe of ____ KIAS must not be exceeded in any condition. However, if momentary deviations occur at speeds up to ____ KIAS during transition to or flight with flaps 45, no maintenance action is required. This does not constitute anautoorization to operate above Vfe.

Maximum airspeed after takeoff/climb without retriming:

Maximum airspeeed for turbulent air penetration below 10,000': _____


Maximum airspeeed for turbulent air penetration above 10,000': _____

Maximyum windshield wiper operating speed:

Do not operate windshield wiper on a _____

Maximum imbalance allowed between tanks:

The minumum / maximum fuel tank temperature is

Max N1:

For all models equipped with FADEC 7.6 or greater the minumum / maximum oil pressure < 88% N2:

note: 2
note: 5

Takeoff thrust is time limited to:

While this is abnormal condition during takeoff and go around, oil pressure operation between _____ and _____ PSI is permitted during takeoff and go around phases of flight.

On LR/EP/ER aircraft equipped with FADEC 7.6 or greater the minumum / maximum oil pressure
> 88% N2:

On XR aircraft equipped with FADEC 7.6 or greater the minumum / maximum oil pressure > 88% N2:

On XR aircraft, operation between 34 and 48 psi is permitted for a maximum of:

LP spool and HP spool exceedence:

Maximum oil pressure may be exceeded during start if the oil temperature is below _____. The engine must remain at IDLE until the oil pressure is less than _____ psi for aircraft equipped with FADEC 7.6 or greater.

Aircraft equipped with FADEC 7.6 or greater will display oil pressures up to and including _____ psi in green:

Operation in the oil pressure amber range between _______,_______ psi is permitted in all operational modes and is time limited to _____ minutes. Operation in the oil pressure amber range between _____ , _____ is permitted in all operational modes and is time limited to ______ minutes. However, total time above ______ may not exceed ______ minutes.

Minimum oil temperature for start:

To increase N2 above _____% the engine oil temperature ust be at _____ C minimum. In lieu of this limit it is acceptable to either: run the engine for at least _____ minutes or complete a static run-up to _____% N2, allow the engines to stabilize and check to ensure that the oil pressure is equal to or less than _____ psi.

Lp and HP spool vibration limits may be exceeded up to ( but not including) _____ IPS for _____ minutes for takoff and go-around phases of flight or for _____ seconds during any other phase of flight.

Max ITT for Start ____ C on all engines:

All ER/ EP/LR/XR takeoff thrust ratings and ITT limits are time limited to _____ minutes:

All XR's, takeoff thrust ITT between _____ are time limiteed to _____ seconds. Takeoff thrust temperatures up to _____ are permitted up to _____, _____ maximum.

Any engine exceedance or peak must be:

Dry motoring continuous operation:

Starting cycle - first to fourth _____, and then the fifth cycle should be _____:

After start, the engines must run at idle or taxi thrust for _____ minutes for cold engines or _____ for warm engines:

Engine is considered cold if it has been shut down for more than _____ minutes:

Engines must run for at least _____ minuts at idle or taxi thrust before shutdown:

Maximum altitude for starting APU is _____

Maximum operational altitude for APU is _____

The APU will automatically shut down at _____% rotor speed.

APU EGT may exceeded _____ up to _____ C for _____ minutes maximum.

Minimum battery temperture for APU start

Start cycle for the APU:

Max load APU generators above FL300 _____ A

Minimum AP engagement height after takeoff is _____

AP disengagement height is _____' for a visual approach _____' for Cat 1 _____ for Cat 2
and __________ for non-percision.

Maximum ISIS duration (non-XR) when operating only on batteries is _____ min. This may be extended to _____ minutes if pitot #3 is turned off when not operating in icing conditions.

The airplane must not be moved during power-up initization. Do not Cage peanut attitude indicator in turning flight.

Maximum altitude for flap extension:

Maximum differential pressure:

Maximum differential over pressure:

Maximum differential negitive pressure:

Minimum temperature for manual anti-ice operation _____

Maximum temperture for anti-ice operation _____

Holding configuration in icing: