737 Limitations and Procedure Limits Flashcards
(119 cards)
1
Q
What should you do if fuel leak exceeds 90 drops per minute?
A
Shut down and restart; can only dispatch if reduced below 90 dpm
2
Q
Q: Which VHF radio should be used for ATC on the ground?
A
A: VHF 1 (upper antenna)
3
Q
Q: When must the girt bar be installed?
A
A: During taxi, Takeoff and Landing (Revenue flight)
4
Q
What is the minimum altitude for speedbrake use?
A
1,000 ft
5
Q
What is the RVSM altimeter limit between Capt and F/O on the ground - Sealevel to 5000ft?
A
50 ft
6
Q
Q: What is the maximum crosswind for takeoff on standing water on a 30m runway?
A
A: 15 kts
7
Q
Q: What is the G-limit with flaps up?
A
A: +2.5G to -1.0G
8
Q
Q: What should the fuel imbalance be scheduled to?
A
A: Zero. Fuel should be scheduled to remain in balance.
9
Q
Can an engine be started with a fuel leak observed on walkaround?
A
Yes, if it is not a continuous stream and is from the drain, not the cowl
10
Q
Q: When should weather radar not be operated?
A
A:
- With people near nose radome
- In an aircraft hanger
- Within 15m of a fuel spill
11
Q
Q: Why are intermediate speedbrake settings avoided?
A
A: They can cause unpredictable and rapid roll rates
12
Q
Q: What is the minimum altitude to disengage autopilot during a single channel approach?
A
A: 50 ft for ILS and RNP approaches
13
Q
Q: What is the maximum crosswind for landing on a wet 30m runway?
A
A: 33 kts
14
Q
Q: What must be verified on the overwing exits before flight?
A
A: Handle covers are in place
15
Q
Q: What is the maximum tailwind for HGS AIII?
A
A: 10 kts
16
Q
What colour indicates EGT caution?
A
Amber
17
Q
Is intentional inflight selection of reverse thrust allowed?
A
No, it is prohibited
18
Q
What is the maximum takeoff weight for VY’s excluding VYZ?
A
75,069 kg
19
Q
Does the standby altimeter meet RVSM tolerances?
A
No
20
Q
Q: When should center tank fuel pumps not be operated?
A
A: When LOW PRESSURE light is illuminated
21
Q
What is the maximum APU altitude for electrical use?
A
41,000 ft
22
Q
What is the maximum APU altitude for combined bleed and electrical use in flight?
A
10,000 ft
23
Q
Q: What is the maximum crosswind for HGS AIII?
A
A: 15 kts
24
Q
What is the in-flight RVSM limit between Captain and First Officer altimeters?
A
200 ft
25
Q: What is the procedure for Severe Turbulence?
A: (YAAET)
Yaw Damper ON
Autothrottle – Disengage
AUTOPILOT – CWS
ENGINE START Switches FLT
Thrust Set Speed (Climb or Descent) / Turb N1 (Cruise)
26
What is the maximum APU operating altitude?
41,000 ft
27
Q: Can ACARS be used for critical information such as loadsheets and PDS's?
A: Only if the data is verified; utilising ACARS where a mistaken input or mistaken reciever could result in an unsafe condition for the aircraft should be avoided.
28
Q: What is the maximum crosswind for takeoff on a wet 45m runway?
A: 25 kts or 30 kts*
30kt available if
-45 M runway only
- Braking action GOOD or better (5)
Flaps 5 or Greater
- COG < 25%
29
Q: What is the maximum tailwind component for takeoff or landing?
A: 15 kts
30
Q: What is the maximum crosswind for takeoff on a dry 45m runway?
A: 33 kts
31
What must be verified during engine warm-up?
An increase in oil temperature prior to takeoff
32
Q: What is the maximum crosswind for takeoff on a dry 30m runway?
A: 33 kts
33
Q: What is the maximum crosswind for landing on a wet 45m runway?
A: 37 kts
34
What is the crosswind limit landing on a Contaminated Standing Water RCAM 2 runway, requiring the use of asymetric reverse thrust?
12kts.
17kt Landing limit, Minus 5kts for the use of assymetric reverse thrust.
35
Can fuel be reintroduced after cutoff during start?
No, do not attempt to reintroduce fuel
36
What is the cabin differential pressure relief valve limit?
9.10 psi
37
Q: Can dispatch occur with nose gear steering inoperative on a runway <45m?
A: No
38
Q: What is the maximum wind speed for opening or closing aircraft doors on the ground?
A: 40 kts
39
Q: What is the recommended descent speed in severe turbulence?
A: 280 kts or Mach 0.76
250kt available if below MLW and < 15000ft
40
Q: What is the maximum crosswind limit for Autoland?
A: 20kts
(If utilising autoland below 550 RVR, then this must be reduced to low viz limit of 15kts)
41
What is the engine out maximum altitude for aircraft with ViaSat?
400 ft below standard engine out max altitude
42
Q: What is the maximum crosswind for landing on a dry 30m runway?
A: 33 kts
43
Q: What are the requirements for operating on a runway less than 45 meters wide?
A: Runway centerline must be clearly visible
44
Q: What is the maximum tailwind for Autoland?
A: 15 kts
45
Q: What is the maximum wind speed while doors are open?
A: 65 kts
46
Q: What is the maximum glideslope angle for autoland?
A: 3.25 degrees
47
What should be considered on the first start of the day above 2000 ft elevation and below 5°C?
Use BOTH igniters
48
Q: Can aileron trim be used with autopilot engaged?
A: No. Trim input will be unoticable and on autopilot disconnect could cause a roll upset.
49
Q: What is the recommended cruise setting in severe turbulence?
A: CRZ page Turb N1 setting or QRH if FMC unavailable
50
What is the RVSM altimeter limit when comparing Capt or F/O and field elevation?
75 ft
51
What is the maximum altitude for takeoff and landing?
8,400 ft
52
Q: What is the maximum takeoff weight for VX’s / VYZ/ VZ’s/ XZ’s ?
A: 79,015 kg
53
What is the difference between max taxi and max takeoff weight?
227 kg
54
When should you reselect GND if start fails and switch is in AUTO?
Only when N2 drops below 20%. Select GND then motor for 60 seconds before returning switch to AUTO.
55
Q: What is the maximum crosswind for takeoff on standing water on a 45m runway?
A: 15 kts
56
Q: What is the maximum fuel temperature?
A: 49°C
57
Q: What are the required configurations for autoland?
A: Both engines operating and flaps 30 or 40
58
Q: What is the maximum headwind for Autoland or HGS AIII?
A: 25 kts
59
Q: What is the maximum crosswind for landing on a dry 45m runway?
A: 37 kts
60
What is the maximum zero fuel weight for VZF to XZP aircraft?
62,731 kg
61
Q: What is the minimum altitude for speedbrake use?
A: Do not use below 1000ft
62
How long must you wait between engine starts?
10 seconds between starts, max 2 minutes total combined starter usage
63
If one altimeter is out by more than 60 ft but within 75 ft on the ground, what can you do?
Continue to first port and recheck there, if out by more than 60ft it is U/S
64
Q: Can dispatch occur with one thrust reverser inoperative on a runway <45m?
A: No
65
Q: What is the in-flight speedbrake extension limit?
A: Do not extend beyond FLIGHT DETENT
66
Q: What is the recommended speed for climb in severe turbulence?
A: 280 kts or Mach 0.76
67
What is the maximum landing weight?
66,360 kg
68
Q: How often must the flight deck door access system be checked?
A: Once per day
69
What is the maximum cabin differential pressure?
9.10 psi
70
What must you keep your hand on during start?
The start lever
71
Q: When is dispatch to a 45m runway not available?
A:
- With NWS inoperative (Turning on small runway)
- With one thrust reverser inoperative (Controlability on small runway)
72
What must you do if landing using asymetric reverse thrust?
Reduce any crosswind limit by 5kts.
73
Q: What is the maximum crosswind for landing on standing water on a 45m runway?
A: 17 kts
74
Q: Can fuel pump circuit breakers be reset in flight?
A: No
75
Q: What is the minimum altitude to engage autopilot after takeoff?
A: 400 ft
76
Q: What should flight crew do if a circuit breaker is tripped on the ground?
A: Consult with engineering before any reset
77
Q: What is the crosswind limit in low visibility below 550m RVR?
A: 15 kts
78
Q: What is the maximum crosswind for takeoff on a wet 30m runway?
A: 25 kts
(Note no 30kt exception here)
79
Q: What is the alternate flap duty cycle full extend/retract cooldown time?
A: 5 minutes between 0 to Flaps 15 and back
80
What is the maximum zero fuel weight for standard aircraft?
61,688 kg
81
Q: If a circuit breaker must be reset in flight, what must be observed?
A: A short cooling period must be observed. 2 minutes
82
Q: What is the maximum crosswind for Autoland?
A: 20 kts
(15 kts for RV550 or less as per low visibility crosswind limit)
83
Q: When should terrain display not be used?
A: Within 15 nm of airports not in the terrain database
84
What is the maximum operating altitude of the aircraft?
41,000 ft
85
What is the maximum APU altitude for combined bleed and electrical use on the ground?
15,000 ft
86
What is the maximum taxi weight for VX, VYZ, VZ, and XZ aircraft?
79,242 kg (+227 kg)
87
What is the maximum altitude with flaps extended?
20,000 ft
88
What is the maximum APU altitude for bleed air use?
17,000 ft
89
What Thrust cantt be used with anti-skid inoperative?
ATM is not allowed with anti-skid inop
90
Q: What is the limitation on flaps in icing conditions?
A: Holding in icing with flaps extended is prohibited
91
Q: When is HF radio use prohibited?
A: During refueling
92
Q: Is the HGS allowed to be used as the sole means of centerline tracking?
A: No
93
Q: What is the G-limit with flaps down?
A: +2.0G to 0.0G
94
Q: What is the maximum fuel imbalance allowed?
A: 453 kg
95
Q: What is the limitation on using speedbrake with flaps?
A: Avoid use with any flaps. If using with Flaps do not use beyond Flap 15 due to buffet.
96
Q: When must main tanks be full during fuel loading?
A: If the center tank has more than 453 kg
97
Q: What is the alternate flap duty cycle switch cooldown time?
A: 15 seconds between uses
98
Q: When must autopilot be disconnected on non-precision approaches?
A: Disengage before 50ft RA
99
Q: What is VA (design maneuvering speed)?
A: Speed where full single-axis control deflection is safe. This does not allow for rapid and alternating control inputs which may result in structual failure at any speed.
100
What should you do if a fuel leak from a drain is found on start, and the engineer advises it is less than 90 drops per minute?
Run at idle for 5 minutes, dispatch if still < 90 dpm after five minutes
101
Q: What is the minimum glideslope angle for autoland?
A: 2.50 degrees
102
What is the maximum EGT for engine start?
725°C
103
What is the maximum continuous EGT?
925°C
104
Q: What should be delayed during terminal area manuevering for the approach if in severe turbulence?
A: Delay flap extension as long as possible; flap up handles more G
105
Q: What is the warning regarding alternating control inputs?
A: Avoid rapid and large alternating inputs in pitch, roll or yaw or any combination of them. They may result in structual failure even below VA.
106
Q: What is the maximum allowable runway slope?
A: ±2%
107
How long is the required engine warm-up period?
2 minutes
108
Q: What is the maximum crosswind for landing on standing water on a 30m runway?
A: 17 kts
109
When should an engine start be aborted? (4 Cases)
- EGT doesn't rise by 15 seconds after IDLE DETENT
- EGT rapidly approaches/exceeds 725°C
- N1 or N2 does not increase or increases too slow after EGT rise
- No oil pressure when at stabilised idle
110
Q: Who should be consulted before resetting any circuit breaker in flight?
A: Maintenance Watch
111
What is the maximum EGT for takeoff?
Red line or 950°C
112
Q: What is the minimum autopilot disengage height for landing?
A: 50 ft unless autoland with FLARE armed
113
Q: Is cycling circuit breakers recommended?
A: No, unless dirtected to by a NNC.
114
What is prohibited when holding in icing conditions ?
Holding with Flaps extended in Icing conditions is prohibbited.
115
Q: When must diversion to a 45m runway (if available) over a 30m be made?
A:
- If there is a jammed or restricted flight control
- Trailing or Leading Edge Flap Assymetry
- Loss of System A or B Hydraulics
116
What is required after 3 engine starts?
15-minute cooling period
117
Q: What is the minimum fuel temperature?
A: -43°C or 3°C above the fuel freezing point
118
Q: When can 30 kt wet runway takeoff limit apply on a 45m runway?
A: 30kt available for takeoff WET if
-45 M runway only
- Braking action GOOD or better (5)
Flaps 5 or Greater
- COG < 25%
119
Q: When can other than fuel circuit breakers be reset in flight?
A: Only if there is an overriding safety of flight reason, and the PIC considers that it remaining tripped would place the aircraft in an unsafe condition.
