-
1.) What is an important consideration regarding thrust reverser operation during TO & Landing?
- TO & Landing are not authorized if either thrust reverser is inoperative;
- - AND the runway is contaminated with clutter.
- - OR the braking action is less than GOOD.
(AOM 3.8.5, pg 3-14)
-
What is the minimum altitude for engaging the autopilot?
- 400’ AGL
- (Flt. Ops. bulletin 23-11, 6-9-23)
-
3.) What is the minimum altitude for LNAV engagement after TO or missed approach?
– Can be engaged on the ground.
-
4.) What is the Max operating speed with the Mach Trim inoperative?
.82/280
(AOM, 3.2.3)
-
5.) What is the Max. Tailwind comp, including gusts, for TO & Land?
10 kts.
- * 15 kt for takeoff and landing from
- SJO/MROC only. *
(AOM(NG), pg 3-4, [NG&MAX] 3.2.7)
-
6.) What is the Max. allowable in-flight difference between Capt. & First Officer altimeters for RVSM ops.?
200’
-
7.) What is the Max. pressure altitude for TO & Landing?
8400’
-
8.) What is the Max wind velocity for all TO’s & Landings?
- 50 kts steady,
- 70 kts peak gusts
(AOM[NG&MAX] 3.2.7, pg 3-5)
-
9.) How long should the APU be operated before opening the bleed valves?
2 minutes
(AOM[NG&MAX] 3.8.6, pg 3-11)
-
10.) Can an airplane be dispatched on a revenue flt. if all lavatories are inop?
No.
-
11.) With the speedbrake load alleviation system inop, what are the speed & weight limitations?
-700 w/winglets = 320 kts & 143,000 lbs
-
12.) What is the Max. gear extension speed?
270 kts / .82 mach
(AOM [NG&MAX] 3.14.1, pg 3-21)
-
13.) What is the Max. Turbulence Penetration Speed above 15,000’?
[NG] 280 kts / .76 Mach
(AOM [NG&MAX] 3.2.3, pg 3-3)
-
14.) Can an aircraft be dispatched on a revenue flt. if the landing gear must remain down?
No.
-
15.) When are the autothrottles Required to be disengaged?
In SEVERE turbulence.
(AOM [NG&MAX] 3.6.2)
-
16.) What is the minimum runway MU value for TO & Landing?
TO or Landing is not authorized if the most current runway friction Mu report includes a value of 20 or Less for any section of the runway.
(AOM 3.2.5, pg 3-3)
-
17.) What is the Max. gear extended speed?
320 KIAS / .82 MACH
(AOM [NG&MAX] 3.14.1, pg 3-21)
-
18.) What is the Max. gear retraction speed?
235 KIAS
(AOM [NG&MAX] 3.14.1, pg 3-21)
-
19.) When must AUTOBRAKES be used for landing?
- - On any runway that is reported < 5-GOOD,
- - Or, if the reported vis. is < 4000 RVR or ¾ mile,
- - Or, if landing with < flaps 30 (e.g., single-eng. landing or abnormal config.)
- - Autobrakes, if operable, are to be used for landing in strong/gusty crosswinds
- or when uniform brake application due to rudder input may be affected.
(AOM, 3-14-2)
-
20.) What is the Max cabin differential for TO & landing?
.125 psi
-
21.) How long should you wait after APU shutdown before turning the battery off?
- - [NG] > 2 min.
- - [Max] > 5 min.
- after the APU GEN OFF BUS light extinguishes prior to positioning the battery switch OFF.
(AOM, 3.8.6)
-
22.) When is Engine Anti-Ice required?
- Operate with anti-ice on:
- - During all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise below -40°C SAT.
- - Prior to and during descent in all icing conditions, including temperatures below -40°C SAT.
(AOM, 3.5)
-
23.) When can VNAV be engaged?
Do not engage VNAV on a go-around/missed approach until flaps are fully retracted.
(AOM 3.11.2, pg 3-18)
-
24.) Can an aircraft be dispatched on revenue flights if the aircraft must remain unpressurized?
No.
(AOM, 3.4.1)
-
25.) What are the minimum engine oil quantity requirements?
- 60%NG / 66%Max (Non-maintenance station/base), OR
- 70%(both) for flights departing from a maintenance base.
The captain must arrange for engine oil servicing when terminating at a non-maintenance base when the oil quantity is <65% [70%Max]
(Note: With oil quantities of <65NG/70M%, low quantity alerts may be experienced during initial TO & climb.)
(AOM, 3.8.4)
-
26.) What are the engine starter duty cycle limitations?
- - [NG]
- - 2 minutes on with 10 sec. off
between start attempts - - Motoring (fuel off): 15 minutes
- - [MAX]
- - 3 minutes ON, 10 sec. OFF
- between start attempts.
- - Motoring: 5 minutes. A minimum of 5
- minutes is needed between the first
- two extended engine motorings.
(AOM, 3.8.3, pg 3-14), ( Max AOM, 3.8.3)
-
27.) What is the Max. X-wind comp. for landing with braking action reported as 3-MED?
15 KIAS
(AOM, 3.2.7)
-
28.) What is the Max headwind component for HGS AIII mode?
25 KIAS
(AOM, 3.2.7)
-
29.) What is the Max. Turbulence Penetration Speed < 15,000’?
250 KIAS
(AOM [NG&MAX] 3.2.3, pg 3-3)
-
30.) What is the Minimum onboard fuel for ground operation of the electric hydraulic pumps?
- - 1,675 pounds in the respective wing tank.
- - But No Flt Deck crew action required if below, unless the
- amber HYDRAULIC PUMP OVERHEAT light comes on.
- Mostly a caution for maintenance personnel.
- * (Now just a caution, not a limitation, 11/19/20) *
- (FOM bulletin, 20-28)
-
31.) What is the Maximum fuel imbalance?
1,000 pounds
(AOM, 3.12.1)
-
32.) How long should you wait before turning on Engine & APU bleeds after de-icing?
1 Minute.
(AOM, 3.5)
-
33.) What is the Safety Relief Differential pressure?
- [NG] 9.10 psi
-
34.) When must the APU bleed air valve be closed?
- - When Ground air is connected & isolation valve is OPEN,
- - OR when isolation valve & # 2 engine bleed valve OPEN,
- - OR when the #1 engine bleed valve is OPEN.
- Note: The APU bleed valve may be OPEN during engine start, provided engine power is not above idle.
(AOM, 3.8.6)
-
35.) What is the maximum X-wind comp. for landing with RVR < 4000 or ¾ mile?
15 KIAS
(AOM, 3.2.7)
-
36.) What is the minimum altitude for disengaging the autopilot during approach?
DA/DDA -50’, but not < 50 AGL.
(AOM, 3.6.1)
-
37.) What is the normal battery voltage range?
23-30 volts
(AOM, 3.7, Table 3.12)
-
38.) What is the maximum brake temp for ground turn around on the -700?
425º F.
The Temp must be measured between 10 & 15 minutes after arrival parking.
(AOM, 3.14.1)
-
39.) What 3 things should you do when landing with the RCC reported < 3-MED?
- 1. - Flap 40 recommended
- 2. - Apply MAX reverse thrust
- 3. - Autobrakes required
(AOM, 12.1.3.2)
-
40.) If extremely heavy precipitation is inadvertently encountered, what should you do?
- ● Maintain the required turbulent air penetration airspeed.
- ● Engine Start Switches—CONT.
- ● Do not make thrust changes unless excessive airspeed variations occur.
- ● If thrust changes are necessary, move the thrust levers very slowly.
- ● Rapid thrust lever movements during flight in extremely heavy precipitation
- may cause engine stall and damage.
- ● Avoid changing thrust lever direction until engines have stabilized at a
- selected setting.
(AOM, 15.3.1)
-
41.) When is the use of LNAV prohibited?
Do not use LNAV if the message “UNABLE REQD NAV PERF-RNP” is active.
(AOM, 3.11.1)
-
42.) What is the Max. X-wind component for landing with braking action reported as 1-POOR?
10 KIAS
(AOM, 3.2.7)
-
43.) What is the Max. X-wind comp. for TO &
Landing?
• 35 KIAS
(AOM, 3.2.7)
-
44.) When is verification of the overwing exit handle cover required?
Prior to departure with passengers
(AOM, 3.2.8)
-
45.) What is the maximum tire speed?
- • 195 KIAS [-700]
- • 205 KIAS [-800S and Max]
(AOM, 3.2.3)
-
46.) What is the minimum ground turn around time for an -800 if the maximum quick turnaround weight is exceeded?
• 48 minutes, non-reducible
Note: Only applies to landings, not rejected TO's
(AOM, 3.14.1)
-
47.) What is the normal AC frequency?
• 400 cps
(FRM, 6.2.1.1)
-
48.) What is the requirement for starting the APU while airborne?
- Only when directed by a QRH procedure or by
- PWB performance considerations.
(AOM, 3.8.6)
-
49.) Maximum external air pressure?
60 psi.
(AOM 3.4.1)
-
50.) Is the use of a pack authorized when a preconditioned air source is being used to heat or cool the aircraft?
No.
(AOM 3.4.1)
-
51.) What condition will require us to switch the igniters to the FLT position?
- Severe turbulence.
* * * Used to be: * * * - In, or in the vicinity of Moderate or Greater Precipitation, (moderate to heavy rain, hail, or sleet.)
- - In these conditions, you should also follow turbulent air penetration procedures.* * * Now, Severe Precip (if not accompanied by severe turbulence) only requires the engine start switches to be moved to the CONT position. * * *
(AOM, 15.3.1 - 15.4)
-
52.) Flight operation within ____ miles of thunderstorm activity should be avoided?
- - Avoid ALL echoes by >5 NM- When flight level temps are below 0°C, avoid all by >10 NM- Avoid by >20 NM: - all echo tops above 15,000'
- - as well as anything you can't top by at least 5000', and
- - any time you are above 23,000'.
- - Never fly near any echo with a top above 30,000'
(FOM, 15.2.4)
-
53.) On the first flight of the day, operate engines at or near idle, after rollback, for a minimum of ____ minutes prior to applying takeoff thrust?
5 minutes
(AOM[NG&MAX] 3.8.2)
-
54.) Reverse thrust, if operative, must be used on all landings at a minimum of detent ___ unless a higher level is specified?
Detent 2
(AOM[NG&MAX] 3.8.5)
-
55.) What 2 things must be done before an aircraft can be towed forward?
- - Both engines will be shut down, &
- - Hydraulic system A depressurized
(AOM, 3.13)
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