DB's SY 737 Limitations Flashcards
0
Q
Max landing tailwind component
A
10 kts
1
Q
Max takeoff tailwind component
A
820SY-821SY are 15 kts
All others are 10 kts
2
Q
Max autoland headwind component
A
25 kts
3
Q
Max takeoff crosswind component:
- With scimitar/blended wing
- Without blended wing
A
- 34 kts
2. 36 kts
4
Q
Max landing crosswind component:
A
40 kts
5
Q
Max autoland crosswind component
A
15 kts
6
Q
Max operating altitude
A
41,000 ft
7
Q
Max takeoff and landing altitude
A
8,400 ft pressure
8
Q
Severe Turbulence Air Penetration speed during climb or descent
A
280KIAS/.76M, whichever is lower
9
Q
Vfe flaps 1
A
250
10
Q
Vfe flaps 2
A
250
11
Q
Vfe flaps 5
A
250
12
Q
Vfe flaps 10
A
210
13
Q
Vfe flaps 15
A
800’s - 200
700’s - 195
14
Q
Vfe flaps 25
A
800’s - 190
700’s - 170
15
Q
Vfe flaps 30
A
800’s - 175
700’s - 165
16
Q
Vfe flaps 40
A
800’s - 162
700’s - 156
17
Q
Vlo (ret)
A
235 kts
18
Q
Vlo (ext)
A
270 kts or .82 M
19
Q
Vle
A
320 kts or .82M
20
Q
Takeoffs are prohibited in what types of precip?
A
- Moderate or heavy freezing rain
- Heavy ice pellets
- Hail
21
Q
Engine EGT Limits:
Takeoff
A
950°C for 5 minutes
22
Q
Engine EGT Limits:
Max Continuous
A
925°C
23
Q
Engine EGT Limits:
Starting
A
725°C
24
Engine ignition must be on for what conditions?
1. Takeoff
2. Landing
3. Heavy rain
4. Anti-ice operation
5. Severe turbulence (SCA)
25
Reduced thrust is not allowed when?
1. Anti-skid is INOP
2. Runway is contaminated with:
•Standing water
•Ice
•Slush
•Snow
3. Windshear (FOM 3.4.18)
26
Max flaps extension altitude?
20,000 ft
27
In what weather condition is holding with flaps prohibited?
Icing
28
What must the lateral fuel imbalance between tanks 1 and 2 be scheduled to?
Zero
29
Max random fuel imbalance?
1,000 lbs
30
Max fuel tank temp
49°C
31
Min fuel tank temp prior to takeoff and inflight
-43°C or 3°C above the fuel freezing point (typically-40° for Jet A and -47°C for Jet A-1)
32
When must main fuel tanks be full?
If center fuel tank contains more than 1000 lbs
33
When must BOTH center tank fuel pump switches be off?
1. Ground operations
2. Ground and Air
1. On ground, < 1000 lbs in center tank (except defueling or transferring fuel)
2. Ground and flight ops, when the first center tank fuel pump low pressure light illuminates if the center tank is empty
34
When must the CORRESPONDING center tank fuel pump switch be off?
For ground and air ops, when a center tank fuel pump low pressure light illuminates.
35
What operation of a center fuel tank pump is prohibited?
Intentional dry running
| LOW PRESSURE light illuminated
36
What TCAS II indication authorizes pilots to deviate from their current ATC clearance to the extent necessary?
Resolution Advisory (RA)
37
What is prohibited when the PSEU light is illuminated and cannot be reset?
Takeoff
38
Max runway slope
+/-2%
39
Max allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations
200 ft
40
Max allowable on-the-ground altitude display differences for RVSM operations between CA and FO?
50 ft
or
60 ft when above 5,000 ft field elevation.
41
Max allowable on-the-ground altitude display differences for RVSM operations between CA or FO and field elevation?
75 ft
42
Flight Crew Oxygen Requirements
| See chart if below what PSI for 2 crew?
735
43
Flight Crew Oxygen Requirements
| See chart if below what PSI for 3 crew?
1055
44
Which trim usage is prohibited with the autopilot engaged?
Aileron trim
45
What autopilot mode is prohibited on final approach below 1000 ft AFE?
LVL CHG
46
Max cabin differential pressure
Red radial (8.75 PSI)
47
With engine bleed air switches ON, do not operate the air conditioning packs in HIGH during what phases of flight?
Takeoff, approach and landing.
48
Minimum Altitude with Autopilot Engaged for takeoff
1000 ft AGL
49
Minimum Altitude with Autopilot Engaged enroute
1000 ft AGL
50
Minimum Altitude with Autopilot Engaged for ILS coupled approach? (Non autoland - single channel autopilot)
50 ft AGL
51
Minimum Altitude with Autopilot Engaged for ILS coupled approach? (Autoland)
After touchdown
52
Minimum Altitude with Autopilot Engaged for non-precision approach?
50 feet below MDA(H), VNAV DA(H)
53
Boom microphones must be used below what altitude?
18,000 feet (except as permitted by SCA MEL)
54
Reduced (SEL TEMP in FMC) or derated thrust is not allowed when?
When EEC is in Alternate Mode.
55
APU Max Altitudes:
| Ground only, APU bleed + electrical load
15,000 ft
56
APU Max Altitudes:
| Inflight, APU bleed + electrical load
10,000 ft
57
APU Max Altitudes:
| APU bleed only
17,000 ft
58
APU Max Altitudes:
| APU electrical load only
41,000 ft
59
When must the APU bleed valve be closed?
1. Ground air connected and isolation valve open
2. Engine no.1 bleed valve open
3. Isolation and engine no.2 bleed valves open
60
Can APU bleed valve be open during engine start?
Yes, but avoid engine power above idle.
61
After three consecutive aborted starts, what is required?
A 15 minute cooling period.
62
Max Taxi weight
1. 700's
2. 800's
1. 155,000 lbs
| 2. 174,700 lbs
63
Max Takeoff weight
1. 700's
2. 800's
1. 154,500 lbs
| 2. 174,200 lbs
64
Max Zero Fuel weight
1. 700's
2. 801SY-805SY
3. 808SY-822SY
1. 121,700 lbs
2. 136,000 lbs
3. 138,300 lbs
65
Max Landing weight
1. 710SY-712SY, 714SY-716SY
2. 713SY
3. 801SY-805SY
4. 808SY-822SY
1. 129,200
2. 128,000
3. 146,000
4. 146,300
66
Min altitude to deploy speed brakes
1,000 RA
67
In flight, do not extend the SPEED BRAKE lever beyond what point?
The FLIGHT DETENT.
68
Max Alt Flaps speed for 1, 2, and 5?
230
69
Min oil quantity for dispatch?
12 quarts
70
When extending or retracting flaps with the alternate flaps position switch, how long should you allow after releasing the switch before moving it again? Why?
15 seconds
| To avoid damage to the alt flap motor clutch.
71
Alt Flap Duty Cycle
| How much cooling after a complete extend/retract cycle is needed before attempting another extension?
5 minutes
72
Are QFE altitudes acceptable?
No.
73
What is required if actual landing weight exceeds maximum permissible quick turn-around weight?
A waiting period of 67 minutes (ramp time) is required before takeoff, which includes a visual inspection by the PM after the 67 mins expires to ensure thermal plug integrity.
74
What are the approved fuel types for:
1. Unlimited use?
2. Acceptable alternatives?
3. Specifically prohibited?
1. Jet A or Jet A1
2. JP-5, JP-8 or F-24
3. Wide cut Jet B
75
737-800W dimensions
1. Height?
2. Wingspan?
3. Length?
1. 41' 2"
2. 117' 5"
3. 129' 6"
76
Engine type
Two GE CFM56-7B
77
Fuel capacity:
1. Tank 1?
2. Tank 2?
3. Center?
4. Total?
1. 8,630
2. 8,630
3. 28,803
4. 46,063
78
What publications are mandatory for flight release?
1. FPM (Vol I)
2. AML
3. QRH
4. Performance Inflight
5. Jepps
(FOM INTRO.09)
79
What are the critical aircraft surfaces?
Anything that has an aerodynamic, control, sensing, movement or measuring function including:
1. Wings
2. Flight controls
3. Vertical and horizontal stabilizers
4. Engine inlets
5. Pitot heads/masts
6. Static ports/masts
7. Ram air intakes
8. Fuel vents
