MCC QB - Limitations

Created by kirkb

VMO is based on
Indicated Airspeed

1/19

TermDefinition
VMO is based on
Indicated Airspeed
B737-800 service ceiling
41,000ft
B737-800 VMO
340kts
VMO is relevant at
Lower Levels
MMO is
referenced to Mcrit with a built in percentage margin
B737-800 MTOW
70535
B737-800 MMO
0.82
Engine TAI must be on when
when icing conditions exist or are expected
Minimum height for AP engagement during TO or climb is
400ft agl
B737-800 max tailwind component
15kts
Take-off thrust is limited to
5 minutes
When should engine ignition be on
Take-off, landing, heavy precipitation, anti-ice operation
is holding in icing conditions with flaps extended allowed
no
Fuel imbalance for TO or landing must not exceed
453kg
On a NPA the AP must be disconnected
before the aircraft descends more than 50ft below the DA/MDA
What must the allowable scheduled imbalance between main fuel tanks 1 & 2 be
0
If main tanks fuel balance differs by more than 453kgs, what colour is the IMBAL alert
amber
Max altitude for using the APU electrical load
41,000ft
Max altitude for using the APU bleed air
17,000ft