Ops Limits Flashcards
Maximum Ramp Weight ___________ lb
840,000
Maximum Takeoff Weight __________ lb
840,000
Maximum Inflight Weight __________ lb
840,000
Maximum Landing Weight __________ lb
840,000
Maximum Fuel Weight __________ lb
332,500
Maximum Zero Fuel Weight (ZFW) __________ lb
686,190
Normal Landing Weight __________ lb
635,850
Normal Landing Fuel Weight __________ lb
142,600
Heavyweight __________ lb
635,850
Normal Pitch on Rotation _____°
8-10
Max Pitch on Rotation _____°
13
Pitch Attitude (Wind Shear Recovery) _____°
15-18
Max Pitch (Rapid Descent) _____°
15
Max Pitch (Below 200 Feet) _____°
10
Max Bank (Below 200 Feet) _____°
15
Max Bank (Below 50 Feet) _____°
5
Angle of Attack Clean, Holding _____°
4.5
Angle of Attack Vapp 100% Flaps _____°
6.9
Angle of Attack Vapp 40% Flaps _____°
7.8
Angle of Attack Vapp No Flap _____°
7.2
Angle of Attack Vapp 100% Flaps and Slats Up _____°
5
Angle of Attack Vstall Flaps Up _____°
13-14
Angle of Attack Vstall Flaps Down _____°
17-19
Oxygen Pressure Static (No Flow) _____-_____ PSIG
275 - 450
Oxygen Pressure Stabilized (Flow) _____-_____ PSI
275 - 400
MTO Below 15,000 ft _____ min / _____ °C
5 / 960
Engine EGT Limit Max Continuous _____ °C
925
Engine EGT Limit Starting (Ground) _____ °C
750
Engine EGT Limit Starting (Flight) _____ °C
960
Engine EGT Limit Max Reverse _____ °C
960
Engine EGT Limit Max Continuous _____ °C
925
Engine EGT Limit Starting (Ground) _____ °C
750
Engine EGT Limit Starting (Flight) _____ °C
960
Engine EGT Limit Max Reverse _____ °C
960
CG LIMITS _____-_____ %
19 - 41
Max NLG Steering Angle <732,500 lb
Asymmetric thrust and breaking _____°
60
Max NLG Steering Angle >732,500 lb
Symmetric thrust and breaking _____°
60
Max NLG Steering Angle >732,500 lb
Asymmetric thrust or breaking (Castered) _____°
60
Max NLG Steering Angle >732,500 lb
Asymmetric thrust or breaking (Centered) _____°
45
Max NLG Steering Angle >732,500 lb
Asymmetric thrust and breaking (Castered) _____°
45
Max NLG Steering Angle >732,500 lb
Asymmetric thrust and breaking (Centered) _____°
30
Starter Duty Cycle
____ Minutes On, _____ Minutes Off
____ Minutes On, _____ Minutes Off
____ Minutes On, _____ Minutes Off (Continuous)
5, 2
5, 2
5, 10
Hydraulic Pressure Normal _____±_____ PSI
3,000 ± 150
Hydraulic Overpressure _____ PSI
3,400
Hydraulic Pressure Min for NLG Emergency Extension _____ PSI
2,500
Hydraulic Pressure Min for 1 Full Brake Application _____ PSI
1,000
Icing on the Ground
Advance engines to > _____ % N1 every _____ minutes.
70, 5
Icing Inflight
Avoid prolonged operation below _____% N1
70
Icing Inflight
If prolonged operation can not be avoided, advance each engine individually for _____-_____ seconds to at least _____% N1 every _____ minutes when flying above _____ feet and every _____ minutes when flying below _____ feet.
10-30, 70, 10, 15,000, 6, 15,000
Max Speed Clean Recommended _____ KCAS / _____ M
350/.825
Max Speed Rapid Descent _____ KCAS / _____ M
350/.825
Max Speed Emergency Descent _____ KCAS / _____ M
350/.85
Max Speed Landing Light Extended _____ KCAS / _____ M
300/.825
Max Speed Yaw Aug Faulted/INOP _____ KCAS / _____ M
300/.825
Max Taxi > 732,500 lb _____ kt
30
Max Taxi > 772,000 lb _____ kt
15
Windshield Wiper Good rain clearing at speeds up to _____ KCAS
150
Windshield Wiper Adequate rain clearing at speeds up to _____ KCAS
175
Thrust Reversers Inflight
Max to deploy Inboard TR _____ KCAS / _____ M
300/.825
Thrust Reversers Inflight
Max with Inboard TR Extended _____ KCAS / _____ M
350/.825
Thrust Reversers Inflight
Max to stow Inboard TR _____ KCAS / _____ M
250/.77
Thrust Reversers Inflight
Min with Inboard TR Extended _____ KCAS
215
Thrust Reversers On the Ground TR Levers to Reverse Idle at _____ KCAS
60
Thrust Reversers On the Ground
If Rev Thrust Idle is exceeded below _____ KCAS an engine & TR system inspection is required.
50
Max Speed Landing Gear Extension _____ KCAS / _____ M
250/.6
Max Speed Landing Gear Operation _____ KCAS / _____ M
250/.6
Max Speed Landing Gear Recommended _____ KCAS
200
Vapp Increase for Ice on Wing/Tail _____ KCAS
5
Min Touchdown Speed Vapp minus _____ kt
6
Landing (≤ Normal Landing Weights) _____ ft/min
540
Landing (> Normal Landing Weights) _____ ft/min
360
Airstart EEC Prevents Starter Engagement Above _____% N2
30
Airstart Most Favorable Conditions N2 at or greater than _____%
Altitude below _____ ft
15
20,000
RAT Max Extension _____ KCAS / _____ M
350/.825
RAT Max Retraction _____ KCAS / _____ M
180/.45
RAT Min for Hydraulics ≥ 15,000 ft _____ KCAS
190
RAT Min for Hydraulics < 15,000 ft _____ KCAS
175
RAT Min for Flight Instruments _____ KCAS
155
Main Tank Low (If fuel mismanagement has occurred) _____ KCAS / _____ M
280/.825
Main Sump Low _____ KCAS / _____ M
280/.825
3 Engine en Route Climb > 600,000 lb
_____ KCAS / _____ M
270/.65
3 Engine En Route Climb ≤ 600,000 lb _____ KCAS / _____ M
250/.65
2 Engine En Route Climb > 600,000 lb _____ KCAS / _____ M
250/.50
2 Engine En Route Climb ≤ 600,000 lb _____ KCAS / _____ M
230/.50
Driftdown (2 or 3 engine) _____ KCAS / _____ M
250/.60
Turbulence
Clean (Severe Turbulence) _____ KCAS / _____ M
280/.825
Turbulence
Recommended Penetration _____ KCAS / _____ M
240/.74
Flaps and Slats
40% Flaps (Slats Ext/Retract) _____ KCAS / _____ M
215/.45
Flaps and Slats
62.5% Flaps _____ KCAS / _____ M
195/.45
Flaps and Slats
Landing Flaps _____ KCAS / _____ M
180/.45
Flaps and Slats
62.5% Flaps (No Slats) _____ KCAS / _____ M
185/.45
Flaps and Slats Landing Flaps (No Slats) \_\_\_\_\_ KCAS / \_\_\_\_\_ M
175/.45
Flaps and Slats Slats Extended (No Flaps) \_\_\_\_\_ KCAS / \_\_\_\_\_ M
215/.45
AR Door Open _____ KCAS / _____ M
350/.825
Normal Rendezvous _____ KCAS / _____ M
300/.72
Rendezvous Outside 3NM _____ KCAS
325
KC-135 at 1⁄2 NM _____ KCAS / _____ M
270/.65
KC-135 Contact _____ KCAS / _____ M
252/.62
KC-135 Max Refueling _____ KCAS / _____ M
265/.64
KC-10 at 1⁄2 NM _____ KCAS / _____ M
290/.70
KC-10 Contact _____ KCAS / _____ M
275/.66
KC-10 Max Refueling _____ KCAS / _____ M
300/.77
