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”
DIMENSIONS
Tail Height
41’2”
DIMENSIONS
Length
129’6”
DIMENSIONS
Wheel Base
distance between nose & main
18’8”
51’1”
FO Takeoff visibility mins
RVR 1600 or 1/4 SM
Low time FO Restrictions [Airway Manual 4.8.4]
When a first officer has less than 100 hours in the aircraft type (previous captain time does not count) the captain is required to make all takeoffs (ground roll initiation through cleanup), and landings under the following conditions:
- Special qualification airports.
- Controlling RVR or visibility value in the latest weather report for the airport is at or below RVR 4000 or 3/4 mile.
- The runway to be used has standing water, snow, slush, or similar conditions that may adversely affect airplane performance.
- The braking action on the runway to be used is reported to be less than “good” or RwyCC less than 5.
- The crosswind component for the runway to be used is in excess of 15 knots including gust.
- Windshear is reported in the vicinity of the airport.
- Any other condition in which the captain determines it to be prudent to exercise the captain’s authority.
*These restrictions do not apply when a line check pilot is PIC.
Required Documents [Vol 1 3.4.1 - FO Preflight Inspection]
- Aircraft Logbook
- Normal checklists (2, 1 required for dispatch)
- QRH (2, 1 required for dispatch - logbook entry)
- Engine performance logbook
- Registration certificate
- Airworthiness Certificate
Altitude display limits for RVSM operations (ground)
Max difference between CA & FO
- Seal Level - 5,000’: 50 ft
- 5,000’ - 10,000’: 60 ft
Max difference between CA or FO & Field Elevation
- Any altitude: 75 ft
