Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
73 Cards in this Set
- Front
- Back
|
MAX RAMP WT |
85,870 |
|
|
MAX TO WT |
85,517 |
|
|
MAX LAND WT |
74,957 |
|
|
MAX ZERO FUEL WT |
69,886 |
|
|
MAX AFT CARGO |
2,535 |
|
|
MAX FWD CARGO |
3,306 |
|
|
MIN RUNWAY WIDTH |
100' (SW) |
|
|
WING SPAN |
93'11'' (WINGLET 85'4'' |
|
|
AIRCRAFT LENGTH |
103'11''
|
|
|
TAIL HEIGHT |
32'3'' |
|
|
MAX OPS ALT |
41,000 |
|
|
MAX TO AND LND altitude
|
8,000
|
|
|
MAX TEMP TO/LND |
ISA+35C (52C)
|
|
|
MIN TEMP TO/LND |
-40C |
|
|
RWY SLOPE |
+-2% |
|
|
MAX TAILWIND |
15KT |
|
|
MAX SINGLE PACK OPERATIONS |
31,000 |
|
|
VMO |
SL-8000: 300 10,000-MACH TRANSITION (FL290): 320 |
|
|
MMO |
.82 |
|
|
VA |
240 |
|
|
ANYTHING W A GEAR |
250 |
|
|
V TIRE |
195 KTS (IF YOU'RE A NERD LIKE UPPER DECK, THATS 224 MPH) |
|
|
V RAT DEPLOY MAX |
Vmo/Mmo |
|
|
V RAT MIN |
130 (LOAD SHARING OCCURS) |
|
|
Vb (turbulance penetration) gigidy |
<10,000: 250 >= 10,000: 270/.76 (whichever is lower) |
|
|
V WIPER |
250 (SW) |
|
|
V WINDOW |
160 |
|
|
FLAPS |
1: 230 2: 215 3: 200 4: 180 5: 180 6: 165 |
|
|
MAX RECOMMENDED CROSSWIND |
DRY: 38 WET: 31 COMP SNOW: 20 STAND H20, SLUSH, WET SNOW, DRY SNOW: 18 ICE: 12 (STATIC TO NOT RECOMMENDED W X-WIND >25) |
|
|
MAX ALT FLAPS/SLATS EXTENDED |
20,000 (ENROUTE OPS PROHIBITED) |
|
|
MIN SPOILER SPEED |
180 |
|
|
CAT II APPROACH FLAP SETTING: |
MANDATORY FLAPS 5 |
|
|
LANDING FLAPS FULL G/A FLAPS TO... |
FLAPS 4 |
|
|
LANDING FLAPS 5 G/A FLAPS TO... |
FLAPS 2 |
|
|
MIN VOLTAGE BATTERY |
22.5V |
|
|
MIN. TEMP BATTERY |
-20C |
|
|
ENGINE START MAX: |
815C MAX NO MIN |
|
|
OIL TEMP FOR START: |
MIN: -40C ( NO MAX) |
|
|
OIL PRESSURE FOR START: |
MIN: 25PSI (NO MAX) |
|
|
ENGINE START CRANKING LIMITS (GROUND AND FLIGHT) |
GROUND: START 1 and 2: 90 SEC ON, 10 SEC OFF START 3-5: 90 sec ON, 5 MIN OFF IN FLIGHT: START 1 AND 2: 120 SEC ON, 10 SEC OFF START 3-5: 120 ON, 5 MINUTES OFF |
|
|
DRY MOTORING CYCLE LIMITS |
1: 90 ON, 5 MIN OFF 2-5: 30 ON, 5 MIN OFF (AFTER 5 SEQUENTIAL STARTS, PROCESS MAY BE REPEATED AFTER 15 MIN COOL DOWN) |
|
|
GROUND START TAILWIND |
IF NECESSARY TO PERFORM AN ENGINE START WITH TAILWIND, MONITOR N1 INDICATION. IF THERE IS NO POSITIVE INCREASE OF N1 BEFORE STARTER CUTOUT (50% N2), THE ENGINE START MUST BE MANUALLY ABORTED |
|
|
ENGINE THRUST (ATTCS) |
TAKE OFF WITH ATTCS OFF IS NOT AUTHORIZED |
|
|
MAX FUEL CAPACITY |
20,935 LB |
|
|
MAX FUEL IMBALANCE |
794 LB |
|
|
MIN FUEL TANK TEMP |
-40C |
|
|
X-FEED |
MUST BE OFF DURING TO AND LNDING |
|
|
APU EICAS LIMIT |
WAIT 30 SECONDS AFTER EICAS ENERGIZED TO START APU
(DO NOT LEAVE AC UNATTENDED FOR MORE THAT 5 MINUTES WITH APU RUNNING --> BELIEVE THIS IS DUE TO FIRE EXT NOT FIRING AUTOMATICALLY) (SIMULTANEOUS USE OF APU BLEED AND THE HP high pres CART IS PROHIBITED) |
|
|
APU STARTER CYCLE
|
START ATTEMP 1 AND 2: 60 SEC OFF
START 3: 5 MIN OFF |
|
|
APU START MAX AND MIN TEMP |
MIN: -54C MAX: ISA +35C |
|
|
APU MAX ALT START |
30,000 |
|
|
APU CONTINUOUS OP TEMP MAX AND MIN |
MIN: -54C MAX: ISA +35C (52C) |
|
|
APU MAX ALTITUDE |
33,000
|
|
|
APU MAX ELECTRIC GENERATOR USE |
33,000 |
|
|
APU MAX BLEED USE |
15,000 |
|
|
APU MAX ALTITUDE TO USE APU BLEED TO START AN ENGINE |
21,000 |
|
|
MAX DIFFERENTIAL PRESSURE |
<37,000: 7.8 PSI >37,000: 8.34 PSI
|
|
|
MAX DIFFERENTIAL OVER PRESSURE |
8.77 PSI |
|
|
MAX DIFF. NEG PRESS |
-.5 PSI |
|
|
MAX DIFF PRESS TO AND LND |
.2 PSI |
|
|
HYDRAULIC: MIN RESERVOIR TEMP FOR ENG START |
-18C |
|
|
BRAKE TEMPERATURE FOR T/O |
MUST BE IN THE GREEN FOR TO |
|
|
THRUST REVERSERS |
1. DO NOT ATTEMPT G/A AFTER DEPLOYED 2. AFTER SELECTING REVERSE THRUST, DO NOT MOVE THE T/L INTO THE FORWARD THRUST RANGE UNTIL THE REV ICON ON THE EICAS IS SHOWN IN AMBER OR GREEN 3. THRUST REVERS PROHIBITED DURING NORMAL TAXI 4. THRUST REVERS FOR POWER BACK PROHIB |
|
|
OPERATION IN ICING CONDITIONS: (NO TEMP LIMITATION FOR ANTI-ICING SYSTEM AUTOMATIC OPERATION) |
ON GROUND:
THE TO DATASET MENU ON THE MCDU MUST BE SET TO ENG IN THE FOLLOWING CASES WHEN OAT IS BETWEEN 5C AND 10C AND: -IF THERE IS ANY POSSIBILILTY OF ENCOUNTERING VISIBLE MOISTURE UP TO 1,700'AFE. -WHEN OPERATING ON RAMPS, TAXIWAYS, OR RUNWAYS WHERE SURFACE SNOW, ICE, STANDING WATER, OR SLUSH MAY BE INGESTED BY THE ENGINES OR FREEZE ON THE ENGINES, NACELLES, OR ENGINE SENSOR PROBES.
THE TO DATASET MENU ON THE MCDU MUST BE SET TO ALL IN THE FOLLOWING CASES WHEN OAT IS BELOW 5C AND: -IF THERE IS ANY POSSIBILITY OF ENCOUNTERING VISIBLE MOISTURE UP TO 1,700. -WHEN OPERATING ON RAMPS, TAXIWAYS, OR RUNWAYS WHERE SURFACE SNOW, ICE, STANDING WATER, OR SLUSH MAY BE INGESTED BY THE ENGINES OR FREEZE ON THE ENGINES, NACELLES, OR ENGINE SENSOR PROBES.
IN FLIGHT:
-THE ENGINE AND WING ANTI-ICE SYSTEMS OPERATE AUTOMATICALLY, IN CASE OF ICE ENCOUNTER WHEN THE ICE PROTECTION MODE SELECTOR IS IN THE AUTO POSITION. IF EITHER ONE OR BOTH ICE DETECTORS ARE FAILED, THE CREW MUST SET THE MODE SELECTOR TO ON WHEN ICING CONDITIONS EXIST OR ARE ANTICIPATED BELOW 10C TAT WITH VISIBLE MOISTURE.
NOTE: -ICING CONDITIONS MAY EXIST WHENEVERY THE OAT ON THE GRND OR FOR TO, OR TAT IN FLIGHT, IS 10C OR BELOW AND VISIBLE MOISTURE IN ANY FORM IS PRESENT (SUCH AS CLOUDS, FOG W/ VIS OF ONE MILE OR LESS, RAIN, SNOW, SLEET, AND ICE CRYSTALS) -ICING CONDITIONS MAY ALSO EXIST WHEN THE OAT ON THE GROUND AND FOR TO IS 10C OR BELOW WHEN OPERATING ON RAMPS, TAXIWAYS, OR RUNWAYS WHERE SURFACE SNOW, ICE, STANDING WATER, OR SLUSH MAY BE INGESTED BY THE ENGIINES, OR FREEZE ON EGINES, NACELLES, OR ENGINE SENSOR PROBES. |
|
|
AUTOPILOT MIN ENGAGEMENT HEIGHT |
400' |
|
|
A/P MIN USE HEIGHT |
50'
|
|
|
A/P MIN USE HEIGHT- NON PRECISION APPROACH |
MDA |
|
|
MIN AIRSPEED FOR TAS, TAT, AND SAT TO BE ACCURATE |
60KTS |
|
|
WHEN WILL STNDBY MAG COMPASS INDICATION NOT BE VALID? |
WHILE TRANSMITTING ON VHF 1 |
|
|
WHAT MINS MUST BE USED FOR ALL CAT 1 APPROACHES |
BAROMETRIC ALTIMETER MINS |
|
|
WHEN ARE BACK COURSE APPROACHES PROHIBITIED |
WHILE USING THE IESS |
|
|
EGPWS |
1. NAVIGATION IS NOT TO BE PREDICATED ON THE USE OF THE TERRAIN AWARENESS SYSTEM 2. EGPWS SHOULD BE INHIBITED WHEN LANDING AT FIELDS NOT IN THE DATABASE SO YOU DONT GET UNWANTED ALERTS 3. EGPSW FUNCTIONS SHOULD BE MANUALLY INHIBITED DURING QFE OPERATIONS, IF GPS DATA IS UNAVAIL OR INOP |
|
|
FMS LIMITS: |
-RNP INST APPROACHES ARE NOT AUTHORIZED (SW) -THE USE OF FMS SPEED MODE IS PROHIBITED IN THE EVENT OF AN ENGINE FAILURE. IE USE MANUAL MODE. |
