Procedures (David's - DO NOT EDIT) Flashcards
1
Q
Order of Procedures
A
- Electrical Power-Up
- Interior Inspection
- Exterior Inspection
- Preflight Procedure FO
- ATIS and Clearance
- Preflight Procedures PF and PM
- Clearance Verification
- WWAARTTSSE Brief by PF
- CA calls for “Preflight Checklist”
- Receive ACARS
- FO inputs performance numbers
- CA verbalizes performance #s
- Pushback Procedure (FO)
- CA calls for “Pushback Checklist”
- FO calls ATC for pushback
2
Q
Electrical Power-Up
A
- MM01 - Check
- C/Bs - Check
- N/W STRG - OFF
- HYD PUMPS - OFF
- LDG GEAR Lever - DN
- Flight Spoilers - 0
- Flaps - Set to actual position
- Radar - Off
- Parking Brake - Set
- ADG Manual Release - Stowed
- Battery Master - ON
- ELECT x 2 (22V) then STAT
- NAV LTS - ON
- If AC AVAIL light illuminated, press the switchlight
- If APU is desired:
No APU FIRE FAIL on pages 1 or 2
FFOD: APU FIRE TEST
(FIRE DETECTION - TEST WARN, FIREX MONITOR APU - TEST 5 sec)
i. APU - START (P DIGS)
ii. 100% - 2 min timer
iii. AVAIL LIGHT
iv. APU GEN - ON
- Check for NOSE DOOR OPEN master warning message
- HYD PUMPS 3A/3B - ON
- FMS - STATUS and POS INIT
3
Q
Interior Inspection
A
- 6 Documents
* SARRAN *
- Sanitary Construction
- Airworthiness
- Registration
- Radio Station
- Air Operator
- Noise - MEL
- BRICK (COLOR)
Note: May be missing until
first arrival in a domicile - Observers’ O2, jumpseat and life vest - Check
- Systems Manual - Check
Note: May be missing for 2 days. - MM01 and MM02
- QRH
- ONE (1) ODH
- Speed Card,
Immediate Action Item Card, Jumpseat Card
Note: May be missing for 2 days. - Circuit Breakers - Check
- Emergency Equipment - Check:
- Crew Hatch
- Escape Rope
- Crash ax
- Fire extinguisher
- 2 Flashlights
- 2 Life Vests
- PBE - Gear and ADG Pins - Stowed
4
Q
Preflight Procedure (FO)
A
- MM01 - Check
- Seat/rudder pedals - Adjust
3. O2 Mask - Checked FFOD: O2 Test (INT/SVC, I/C, SPKR, MASK, 100%, Press to test - Push 2 sec, Center I/C, Hold press to test, emergency flow control switch (push once), mask operating levers, release "press to test", BOOM)
Normal: 100%, Press to Test
- Selector valves - As req’d
- Audio Warning Panel - Checked
- Lighting panel - As req’d
- Wiper - OFF/PARK
- Stall PTCT/PUSHER - ON
- Clocks - Set
- DCP - Set
- Air Data Reference Panel - Set
- Display Rever. Selector - NORM
- EFIS - Checked
- Altimeters - Set
- Audio Control Panel - Set
(BOTH, BOOM, NORM) - Fuel - Verify
- ATIS and CLEARANCE
5
Q
Preflight Procedure (PF)
A
- Both compass switches - MAG
- ACARS - Initialize
i. Flight #
ii. Departure airport
iii. Arrival airport
iv. Flight time and
employee numbers - FMS - Set
i. “I Pattern” and DEFAULTS
(290/.74, 300/.74, 290/.74, 3 dg)
ii. “J Pattern”.
Order:
“FPLN”: ORIG, DEST, FLT#, ALT
“DEP ARR”: SID, RWY, STAR
“FPLN”: Verify distance, EXEC,
COPY ACTIVE
“PERF”: OAT
“PERF INIT”: Do all pages, EXEC
“PERF” again: Enable VNAV and on page 2, PREDICTED fuel
“MFD MENU”: As req’d
“RADIO”: Auto Tune - Clearance Verification Procedure
- Departure Briefing:
WWAARTTSSE:
Weather Wind Abnormal procedures (CAPTAIN) Abort (CAPTAIN) Runway length, condition, HDG Taxi Terrain SID Specials Engine Failure Procedure
- Captain calls for
“Preflight Checklist”
6
Q
Preflight Procedure (PM)
-INCLUDING FFOD-
A
- Electrical power services panel - Set
- -FFOD-
FIRE TEST and
APU FIRE TEST:
LOOOOOONG press:
- FIRE DETECTION TEST WARN
- FIREX APU TEST
- External LTS panel - Set
* HYD 1 and 2 Switches ON!!!* - Fuel panel - Checked
- -FFOD-
BLEEDS TEST - Bleed Air Panel- Checked
- APU panel - Set
- L-ENG-R and IGN panel - Checked
- -FFOD-
HYDRAULIC SYSTEM TEST - Hydraulic Panel - Set
- ELT - ARM/RESET
- PASS OXY switchlight - Guarded
- CABIN PRESS panel - Set
- Air-Conditioning Panel - Set
- CARGO - COND AIR or
FAN (more than 15 C) - -FFOD-
ICE DETECTOR TEST - Anti-Ice Panel - Checked
- MISC LTS panel - Set
- EMER LTS panel - Set
- PASS SIGNS - ON
- Standby compass - Checked
- -FFOD-
EGPWS TEST
23. -FFOD- STALL TEST (Flaps 0, 5.8-6.2)
- Glareshield - Checked
- ISIS - Checked
- -FFOD-
MLG BAY OVHT and
OVHT TEST WARN FAIL - Upper pedestal - Checked
- Thrust lever quadrant - Checked
- Thrust reversers - ARMED
- Center pedestal - Checked
- -FFOD-
TCAS TEST - -FFOD-
STAB/MACH TRIM TEST - -FFOD-
AILERON/RUDDER TRIM TEST - YD 1 and YD 2 - Engage
- Jumpseat COM - INT/SVC
- Manual release landing gear handle - Stowed
- CARGO FIREX switchlights - OUT
- -FFOD-
PA TEST - EICAS - Checked
- Clearance Verification Procedure
7
Q
Preflight Procedure (PM)
A
- Electrical power services panel - Set
- External LTS - NAV ON
- Fuel panel - Checked
- Bleed Air Panel - Checked
- APU panel - Set
- L-ENG-R and IGN panel - Checked
- Hydraulic Panel - Set
- ELT - ARM/RESET
- PASS OXY switchlight - Guarded
- CABIN PRESS panel - Set
- Air-Conditioning Panel - Set
- CARGO - COND AIR or
FAN (more than 15 C) - Anti-Ice Panel - Checked
- MISC LTS panel - Set
- EMER LS panel - Set
- PASS SIGNS - ON
- Standby compass - Checked
- Glareshield - Checked
- ISIS - Checked
- Upper pedestal - Checked
- Thrust lever quadrant - Checked
- Thrust reversers - ARMED
- Center pedestal - Checked
- Jumpseat COM - INT/SVC
- Manual release landing gear handle - Stowed
- CARGO FIREX switchlights - OUT
- EICAS - Checked
- Clearance Verification Procedure
8
Q
Clearance Verification Procedure
A
- PF use FMS FPLN and
PM use clearance
(PM : Use release flight plan if “cleared as filed”)
2. PM reading from PDC and release flight plan: "FLT 3670 KMSP to KDFW, ALTERNATE IS KMEM ORSKY8 OVR J21 IRW UKW4, 266 MILES"
- PF presses NEXT PAGE as PM reads the clearance to him
- PF verifies any ALTITUDE and
SPEED RESTRICTIONS with the PM (who looks at FMS) - PM independently verifies, leg by leg, Jepp departure and release flight plan against the FMS
- WWAARTTSSE Brief
- CA calls for “Preflight Checklist”
9
Q
After receiving ACARS:
A
- Input flex temp in FMS
- Input ZFW in FMS
- Verify GWT less than MRTOW
- Flip Speed Card to GWT
- Set V-Speeds
- SPEED, HDG, ALT bugs
- Stab trim
10
Q
Close boarding door:
A
- PAX count and CLR
- MM01/2 on board
- GND air disconnected 4. Signed release given to station ops
- Copies of the:
release, TLR, and WX
11
Q
Pushback (FO)
A
- Doors - Closed
- Flight Deck Door - Closed and locked
- Crew Escape Hatch - Closed
- Boost Pumps - ON
- “APU ON, Bleeds on APU”
- Ignition - ARM A(B)
- Beacon - ON
- Transponder - PF Side
12
Q
Engine Start (FO)
A
- Packs - OFF
- “Set, Four, Arm”
- START/TIMER - Press
- “N2, Oil pressure,
N1, ITT less than 120 C” - 20% N2:
Thrust Lever - IDLE - Stable Start:
“2,4,6” and stop timer
- STABLE START - N1: 22-25% ITT: 450-600 C N2: 56.5-68% Fuel Flow ~ 350 LBS/HR Oil Press > 25 PSI
13
Q
Engine Start (FO) -FFOD Start #1-
A
- Packs - OFF
- “Set, Four, Arm”
- START/TIMER - Press
- “N2, Oil pressure,
N1, ITT less than 120 C” - 20% N2:
Thrust Lever - IDLE - Stable start:
“2,4,6” and stop timer - Boost Pumps - OFF
- “Pump, Pump, Press”
- Boost Pumps - ON
- STABLE START - N1: 22-25% ITT: 450-600 C N2: 56.5-68% Fuel Flow ~ 350 LBS/HR Oil Press > 25 PSI
14
Q
After Start (FO)
A
- GEN 1(2) - ON
- Boost pumps - Set
(Single engine taxi (#2) -
Turn off left boost pump)
(2 engine taxi - Both ON) - Packs - ON
- Ignition - OFF
- Anti-Ice - As req’d
- Probes - ON
- READ Status Page messages
- Electrics - Checked
- F/CTL Page
- -DTW ONLY-
ADG LAMP/UNIT Switch - UNIT
15
Q
After Start (FO) - INCLUDING FFOD -
A
- GEN 1(2) - ON
- Boost pumps - Set
- Packs - ON
- Ignition - OFF
- -FFOD-
WING A/ICE (x2), 14th ISOL, COWL - Anti-Ice - As req’d
- Probes - ON
- READ Status Page messages
9. -FFOD- APR TEST (x2)
- Electrics - Checked
- F/CTL Page
- -DTW ONLY-
ADG LAMP/UNIT Switch - UNIT
16
Q
Taxi Procedure (FO)
- After pushback…
when workload and conditions permit -
A
Flight Controls - Check
17
Q
Delayed Start (FO) - INCLUDING FFOD -
A
- Boost Pumps - ON
- Packs - OFF
- “Set, Four, Arm”
- START/TIMER - Press
- “N2, Oil pressure,
N1, ITT less than 120 C” - 20% N2:
Thrust Lever - IDLE - Stable start:
“2,4,6” and stop timer - GEN 1 and GEN 2 - ON
- Packs - ON
- Ignition - OFF
- WING A/ICE - Test
- Anti-Ice - As req’d
- READ Status Page messages
- APR - Test
- Electrics - Checked
- YD 2 - Press
18
Q
Delayed Start (FO)
A
- Boost Pumps - ON
- Packs - OFF
- “Set, Four, Arm”
- START/TIMER - Press
- “N2, Oil pressure,
N1, ITT less than 120 C” - 20% N2:
Thrust Lever - IDLE - Stable start:
“2,4,6” and stop timer - GEN 1 and GEN 2 - ON
- Packs - ON
- Ignition - OFF
- Anti-Ice - As req’d
- READ Status Page messages
- Electrics - Checked
19
Q
Engine Warm Up Period
A
2 minutes below 75% N1
OR
All operating indications are
in the normal range
(whichever is longer)
(CFM 4-58)