Procedures & Other Limitations Flashcards
ABORT START IF
- N1 or N2 does not increase or increase very slowly after the EGT increases;
- There is no oil pressure indication by the time that the engine is stabilized at idle;
- EGT does not increase by 10 seconds after the start lever is move to IDLE
- The EGT quickly bears or exceeds the start limit.
- The FUEL SPAR VALVE CLOSED indication light on the overhead panel does not change from dim to bright, and then extinguish.
QRH NNC.7
Max motoring:
1% increase in approx 5 seconds
Preflight Brake pressure minimum
2,800 psi
IF <2,800 PSI THEN HYD B ON until >2,800 psi, HYD B OFF
Min Oil level for dispatch
12 QTS
CALL MX @ 16 if in a Delta station, 14 if out-station
IF HYD QTY > 102%
Vol 1 5.13.1 - Contact MX - pumps OFF
WARTS Briefing
FOM 5.1.4
(conducted prior to preflight checklist, verbalize highest threat to departure segment)
Weather/wind considerations
Abnormal/normal procedures and abort considerations
Runway considerations
Taxi and terrain considerations, transition altitude/height
SID/Departure and Company Pages considerations
Nav Briefing FOM 5.1.5 Trigger: receiving taxi clearance to departure runway.
R- Runway
D- Departure
F - First Fix
H- Heading
A - Altitude clearance limit (+transition if applicable)
A - Airspeed restrictions (if applicable)
NATS Briefing FOM 5.1.6 for all approaches
N - NOTAMS
A - Arrival/approach chart/automation
T - Transition level/height/terrain/taxi
S - Specific Company Information (Co. Pages)
Fuel Quantity low alert
< 2,000 lbs in associated tank
Fuel CONFIG alert.
- either engine running
- center fuel tank quantity greater than 1600 lbs.; and both center fuel tank pumps produce low or no pressure.
fuel IMBAL alert
- main tanks differ by more than 1000 lbs.
- displayed below main tank with lower fuel quantity.
- displayed when airplane is on the ground or in the air.
- inhibited by fuel LOW indication when both indications exist.
- displayed until imbalance is reduced to 200 lbs.
Max Holding Speeds (USA - see screenshot for others Airway Manual 4.1.5)
< 6,000’ - 200 KIAS
> 6,000’ < 14,000’ - 230 KIAS
> 14,000’ - 265 KIAS
Timing
< 14,000’ = 1 min,
>14,000’ = 1.5 min
4 instances requiring an LPR (or check ODM)
- RWY length < QRH landing lengths
- Contaminated RWY
- Braking action < GOOD
- NOI for F15 landing
* discretionary: overweight landing on ground
ENGINE START switch automatically moves from GRD to OFF at ___% N2; if not, position start switch to ___.
56%
OFF
Fuel load differs from flight plan +___lbs/-___lbs. Call dispatch.
+ 1,000 lbs / - 200 lbs
5 CRM Skills
- Decision Making
- Planning
- Communication
- Workload Management
- Monitoring
Conditions that will cause the Intermittent Takeoff Configuration Warning VOL 2 / 15.2.4.1
- trailing edge flaps are not in the flaps 1-25 takeoff range, or are in a skew or asymmetry condition, or have uncommanded motion,
- leading edge devices are not configured for takeoff or uncommanded motion,
- SPEED BRAKE lever is not in the DOWN position, 4. spoiler control valve is open providing pressurized hydraulic fluid to the ground spoiler interlock valve
- parking brake is set
- stabilizer trim not set in the takeoff range. (green band)
TTSR FOM 17.3.2.2
T - Type of Emergency (Red/Yellow)
T - Time to prepare the cabin
S - Special instructions
R - Repeat information back to the captain
Minimum altitude for flap retraction
400’
Items that require coordination with dispatch
- Lateral deviations > 100nm from planned route
- Altitude deviations > 400 nm
- ETA +/- 15 mins
- Arrival fuel < FAR reserves
- Fuel consumption greater than planned
- Changes in destination weather
- Any diversion to an alternate unless previously discussed with dispatcher
- Any change in intended destination or intended alternate airport
- ATC issues a supplementary route or CDR
Fuel Reserves FOM 14.3
Domestic
- fly to destination then
- alternate if required, then
- 45 mins at normal cruise
MINTO = Flight plan plus
- required contingency fuel
- ballast/unusable
See FOM 14.3 for International, B043, B044, etc.
DIMENSIONS
Turning Radius 737-800
- Minimum pavement for a 180 degree turn ___
- CAUTION: do not attempt to make a turn away from an obstacle within ___ of the wingtip or ___ of the nose.
- 79.7 ft (24.3 m)
- 17.8 ft (5.4 m)
- 24.3 ft (7.4 m)
DIMENSIONS
Turning Radius 737-900ER
Minimum pavement for a 180 degree turn ___
CAUTION: do not attempt to make a turn away from an obstacle within ___ of the wingtip or ___ of the nose.
86.4 ft (26.2 m)
16.4 ft (5 m)
21.8 ft (6.6 m)
DIMENSIONS
Wingspan
117’4” - 117’10”
