Limitations Flashcards
757-300 Weight Limits Maximum Values for: Taxi Mass T/O Mass Ldg. Mass Zero Fuel Mass
Max Taxi Mass 122.923kg
Max T/O Mass 122.469kg
Max Ldg. Mass 101.604kg
Max ZFM 96.025kg
What are the values on the Boeing 767 (UA-UI & UZ) for Max Taxi Mass? Min Takeoff Mass? Max Takeoff Mass? Max Landing Mass? Max Zero Fuel Mass?
Max Taxi Mass 185.500 kg Min Takeoff Mass 99.800 kg (no performance values below available) Max Takeoff Mass 184.600 kg Max Landing Mass 145.100 kg Max Zero Fuel Mass 132.100 kg
What is the minimum and maximum ILS glide slope angle for automatic landing?
For AUTOMATIC Landings:
Minimum ILS glideslope angle is 2,5 degrees.
Maximum ILS glideslope angle is 3,1 degrees.
What is the minimum and maximum glideslope angle for manual landings?
For manual landings the minimum glideslope angle is 2.2° and the maximum glideslope angle is 4.0°.
What is the maximum approved altitude for
A) B757?
B) B767?
Max. altitude for
A) B757 is 42.000ft
B) B767 is 43.000ft
However limit altitude to 39.000ft on B757-200 to reduce occurrence of pack overload.
What is the maximum runway slope limit?
The runway slope limit is +/- 2.0°
What is the max. allowable fuel imbalance between left and right main tanks on the B757?
Max. allowable fuel imbalance (left/right maintanks) is 800 kg.
What is the max. tire speed?
204 kts.
Describe the starter duty cycle for the RollsRoyce Engines on the B757.
Normal starter cycle:
Up to 2 min operation, then rundown to 0% N3.
This can be done 3 consecutive times before you need a 15 min cooling time.
Extended starter cycle:
Up to 4 min operation, followed by a 15 min cooling time.
What is the minimum engine oil quantity?
16
Engines are monitored by maintenance, troubleshooting my override this limit even for extended range ER operation.
What is the minimum APU oil value?
Verify EICAS APU oil indication is 0,75 or more.
APU not running or running stabilized for more than 5 min.
What is the recommended starting pressure for the engine start?
30 PSI is recommended.
Value may be decreased by 0,5 PSI per 1000 ft above MSL.
Use caution during engine start with less than 30 PSI.
What is the definition of a “Long Range Navigation System”?
Either:
1 IRU in NAV mode and 1 associated MCDU
or:
1 IRU in NAV mode, 1 FMC and 1 CDU
What is the maximum Tailwind Component
for Takeoff?
for Landing?
For T/O 15 kts
For Ldg 15 kts
For more than 5 kts TWC refer to OM A 8.3.4.5.1 “on CDRs discretion…”
During AUTOLAND:
max HWC?
max CWC?
max TWC?
max 25 kts HWC
max 25 kts CWC
max 15 kts TWC
757-300 mit Flaps 30 nur 12 kts TWC mit Flaps 25 15kts