737 Flash cards April 12 2024
Flight Maneuvering Load Acceleration Limits
Flaps Up +2.5gto -1.0g Flaps Down +2.0g to 0.0g
Max Operating Pressure Altitude *
41,000 feet
Max Takeoff/Landing Pressure Altitude
10,000 feet
Max Flight Operating Latitude
82N 82S exceptions for certain East and west longitudes
Runway Slope
2% + or -
Max Takeoff/Landing Tailwind *
15 KTS
Max Airspeed MMO
.82 Mach
Max gear retraction speed
235 KTS
Max gear extension speed
270 KTS/ .82M
Max gear extended speed
320 KTS/ .82M
Severe Turbulence Penetration Speed Cruise *
Turb N1 setting from cruise pg
Severe Turbulence Penetration Speed Climb and Descent *
280 KTS /.76Mach
Over wing Exits
Handle covers must be installed when ever pax are carried
On revenue flights the Girt bar must-
Be installed for Taxi, Takeoff, and Landing
Quick turn around weight limit exceeds chart value wait at least
67 Min. 48 Min with Carbon brakes
Crosswind Guidlines Takeoff and Landing Dry - code 6
Takeoff - 33 Landing - 37
Crosswind Guidlines Takeoff and Landing Wet - code 5
Takeoff - 25 Landing - 37
Gross Weight 737-800
Taxi-174,700 lbs. Takeoff - 174,200 lbs. Landing - 146,300 lbs. ZFW - 138,300 lbs.
Max Cabin Diff.
9.10 psi
Max Cabin Diff. for Takeoff and Landing
0.125
Duct pressure for Max cooling
20 - 25 psi
Min Duct Pressure for Two Pack Operation From Single Bleed Source
20 - 25 psi
Iceing conditions exist on the ground and for takeoff when… *
10c or below - visible moisture and orvisibility 1 mile or less in clouds or fog. - anytime on the ground when standing water rain slush or snow may be ingested.
Takeoff in Moderate/ Heavy Freezing Rain or Hail is..
Prohibited
Engine Anti Ice Must Be On Durring All flight Ops when…
- Icing conditions exist or are anticipated. - When Temp is below -40SAT Except during climb and cruise. - Ignition must be set to CONT. prior to using Engine Anti Ice.
Wing Anti Ice
Must be used during all ground ops from engine start to takeoff when icing conditions exist. Unless Type II or Type IV fluid is used. Do not use Wing Anti Ice above 10C / 50F. Do Not use Wing Anti Ice During Takeoff until After the First Power Reduction.
Windsheild wipers
Do not use on DRY Windshield
Widow Heat
Must be ON 10 Min. before takeoff.
Autopilot Engagemet *
400AGL
Autoland Max Winds
Headwind - 25 X-wind -15 Tailwind -10 (for flaps 30 or 40)
Aileron trim with Autopilot engaged
Is Prohibited
Autopilot use prohibited below 100’ RA at Airports above…
AT Airports with a Pressure Altitude above 8400’
Min. Altitude for Autopilot use on Approach *
ILS/GLS (not autoland) 50’AGL - Non Precision App 50’ below MDA/DA - Auto Lnd to Touchdown
Auto land can only be used when..
Runway is at or below 8400’ pressure Alt. - Flaps 30 or 40 used with two operating engines. - Max and Min Glideslope angle 3.25 and 2.5
Autoland should not be used for
Overweight landings
Do Not use the autopilot or autothrottle if
The associated radio altimeter is inoperative.
APU Bleed and Electrc Max Alt.
10000
APU Bleed Max Alt.
17000
APU Electric Load Max Alt.
41000
APU Starter duty cycle
15 Min cooling required after 3Rd start attempt on the ground or in the air
APU Warm up cool down
Operate APU “1” Min before using Bleed air. - Wait 120 Sec for APU shutdown then turn Batt sw OFF.
APU Bleed valve must be closed when…
Ground Pneumatic air on and ISOLATION valve OPEN. - Engine 1 Bleed vave open (engine1 running). - ISOLATION valve OPEN and Engine2 Bleed valve Open( engine2 running).
Max single Engine Generator load
75KVA - 215 Amps (ground ops)
Min Batt Volts for APU start
23V
Engine Ignition must be “ON” for..
-Takeoff - Landing - Engine Anti Ice Operation. - Heavy Rain
Min Oil Pressure
13psi
Max oil temp
155C
Max Continuous oil temp
140C
Max Allowable for 45min. Oil Temps
140C-155C
MAX EGT Takeoff 5min.
950C
MAX EGT Continuous
925C
MAX EGT Starting
725C
Engine Starter Duty Cycles
Do Not exceed 2 min for each start attempt. - A Min. of 10 sec. between starts.
MAX N1
104%
MAX N2
105%
Reduced Thrust Takeoffs are not permitted when…
Antiskid inop. - Runway is contaminated with standing water, ice, slush or snow.
EEC
both must be “ON” or “ALT” for takeoff. - Reduced thrust Takeoff not permitted in “ALT”mode.
Min Oil Quantity
70%
Starter Engagement
Do not engage starter above 20% N2
Engine starts in temp below -35C
Idle for 2 min before changing thrust lever position.
Lavatory fire extinguishing
Black dots or discharge nozzle tip turns an aluminium color. Maint. req.
Engine Fire Extinguishing bottles
800psi@70F
Flaps Altitude limitation
20,000
Holding in Icing conditions …
is prohibited
Speed brake lever limitations
Do not extend beyond the Flight detent. - Do not use RA less than 1,000’- Not used beyond Flaps 15
Alternate Flap duty cycle
Allow 15 sec.off after releasing Alt flap position switch. After a complete 0-15-0 cycle allow 5 Min. cooling.
Max Airspeed with Alternate Flap System
230 KTS
Mach trim fail (both channels) Max speed
280 KTS / .82 Mach
RVSM Max diff. between Captain and FO Altimeters in flight
200’
RVSM Max diff. between Captain and FO Altimeters on ground 0-5,000’
50’
RVSM Max diff between either pilot and field elevation
75’
JET A Min. Max temp
Min -37C Max +49C
The use of JP4 and JetB is..
Prohibited
Tank fuel must be……temperature
3C above Fuel Freezing point
7/8/9/ Wing Tank Qantity
8630 lbs
7/8/9/ Center Tank Quantity
28,803 lbs
Fuel Density
6.7 lbs/gal
Random Fuel Imbalance must not exceed
1,000lbs
The Center Tank “CONFIG” light will illuminate..
When Center tank fuel exceeds 1,600lbs with center tank fuel pumps off
Min. Wing tank fuel for cooling electric Hydraulic pumps on the ground..
1,675 lbs each
Min Hydraulic QTY
Above RF
Max Tire Speed
195 KTS
Engine Failure (V1 Cut) Take off profile LNAV/VNAV
“ROTATE” 7-11 degrees “POSATIVE RATE” “GEAR UP” climb V2 - 15 degree bank to 1500AGL ( unless special EO) fly runway centerline. At 400’ “Heading select” or “LNAV”, At 800’ or charted Alt retract flaps on schedule. At VM0 “Set Max Continuos Thrust” Engine Failure or Sever Damage or Engine Fire Checklist.
Engine Failure (V1 Cut) Take off profile HDG SEL and TOGA
“ROTATE” 7-11 degrees “POSATIVE RATE” “GEAR UP” climb V2 - 15 degree bank to 1500AGL (unless spcial EO) fly runway centerline. At 400’ “Heading select” , At 800’ or charted Alt. ‘Set Clean Mauvering Speed” retract flaps on schedule. At VM0 “Set Max Continuos Thrust” Engine Failure or Sever Damage or Engine Fire Checklist.
2 Engine ILS Profile Cat 1
“2500” “ In or Hpa”. At glideslope intercept “Set TDZE”. “1000” “Set missed approach altitude” Cleared to land” or “no landing clearance”. “500” “Stable” or “Unstable going around”. “minimums” “Landing” or “Going Around” (note) 1 1/2 dot gear down flaps15
1 Engine ILS Profile
Intercept Loc with Flaps 5. At 1 dot GS deviation “ Gear down flaps 15 “.
RNAV / Non-Precision Approach profile
4 Miles FAF “Gear down Flaps 15t” 2 Miles “Flaps__”
1 Engine missed approach.
“GOING AROUND”, “FLAPS 1”, “Check Thrust”, “Posative Rate, Gear Up”, “Set Missed Approach Altitude”at 400’ “Heading Select/LNAV”, at 800’ or higher if published “SET CLEAN MANEUVERING SPEED” Clean up on schedule. “SET MAX CONTINUOUS THRUST” accomplish “Abbreviated After Takeoff Checklist
2 Engine missed approach
“GOING AROUND”, “FLAPS 15” “ CHECK THRUST” “POSATIVE RATE GEAR UP” “SET MISSED APPROACH ALTITUDE” @ 400’ “HEADING SELECT or LNAV”, at 800’ or higher if published “LEVEL CHANGE SET CLEAN MANUEVERING SPEED” Clean up on schedule. “After Takeoff Checklist”.
Immediate Action APU FIRE
APU Fire Switch….Confirm….Pull….Rotate and Hold 1 Sec. APU SWITCH…OFF
Immediate Action LOSS OF THRUST BOTH ENGINES
ENGINE START SWITCHES (both)….FLT ENGINE START LEVERS (both)…CUTOFF ENGINE When EGT decreases START LEVERS (both)….IDLE
Immediate Action ENGINE FIRE or SEVERE DAMAGE
Autothrottle (if engaged)….Disengage Thrust Lever (affected engine)…. Confirm….Close
Immediate Action ENGINE OVERHEAT
Autothrottle (if engaged)….Disengage Thrust Lever (affected engine)…. Confirm….Close
Immediate Action ENGINE LIMIT SURGE or STALL
Autothrottle (if engaged)….Disengage Thrust Lever (affected engine)…. Confirm…RETARD (until within limits)
Immediate Action AIRSPEED UNRELIABLE
Autopilot (if engaged)….Disengage Autothrottle (if engaged)….Disengage FLIGHT DIRECTOR switches (both)….OFF / Set following gear up pitch attitude and thrust….Flaps Extended…….10deg and 80% N1 Flaps Up…4deg and 75% N1
Immediate Action SMOKE FIRE FUMES
Oxygen Masks and Regulators….ON(as needed), 100% CREW COMM…..Establish
Immediate Action CABIN WARNING / RAPID DECOMP
Oxygen Masks and Regulators….ON, 100% CREW COMM…..Establish Seatbelt Sign…..ON
Immediate Action Flight Deck Door
JAMCO…..Hardlock switch…..PUSH Boeing…..FLT Deck Door selector…..ROTATE to DENY
Immediate Action RUNAWAY STABILIZER
1.Control Column..Hold Firmly - 2.Autopilot (if engaged)…Disengage - 3.Autothrottle (if engaged)…Disengage
4.Controll Column and Thrust Levers -controll airplane pitch attitude and airspeed
5.Main Electric Stab Trim - Reduce controll collumn forces.
If runaway stops do not reengage autopilot or auto throttle.
If Runaway continues… STAB TRIM CUTOUT
if runaway continues…
Grasp and Hold
T.E.S.T
TYPE of nonnormal EVACUATION prep required or not SPECIAL instructions TIME remaining
Do Not use LVL CHG below…
1000 feet AFE
Engine Start Aborted Start*
Engine Start Lever effected engine…CUTOFF
