104 terms

A300-BrownTail

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Terms in this set (...)

5-3-1, .2 profile before FAF
- 5 NM "Flaps 20, Gear Down, Speed 160"
- 3 NM "Flaps 40, Speed XX, Landing checklist, Set Missed Approach Altitude"
- 1 NM Walk FMA, deselect ALT/HLD for V/S APP (PROF Armed P.DES for PROF App)
- .2 NM Set 700 VVI (calculated)
Aborted Engine Start
1. Fuel lever - Off
2. Ignition - Off
Engine Stall
1. Throttle - Idle
2. Ignition - Cont Relight
Both Engine Flameout
1. Ignition - Cont Relight
2. RAT Handle - Pull
3. Throttles - Idle
Eng Rev Unlock
1. Throttle - Idle
2. Max Speed - 300 KIAS
Loss of Both Eng Generators
1. Ignition - Cont Relight
2. Gen 1 & 2 - Off, then On
Runaway Pitch Trim
1. Control Wheel - Hold
2. Trim Wheel - Hold
3. Autopilot - Disconnect
Emergency Descent
1. Oxygen Masks - On
2. Crew Communications - Establish
3. Emer Descent - Initiate
- MCP Alt - Set
- Lvl Ch - Select
4. Signs (Seat Belt) - On
5. Emer Descent - Announce
6. Throttles - Idle
7. Spd Brk - Extend
Unreliable Airspeed
1. All Airspeed Indications - Disregard
2. Pitch Attitude and Thrust - Check
3. Autopilot and Autothrottles - Disconnect
4. Flight Directors - Off
5. Pitch Attitude and Thrust - Adjust (Note: autopilot and flight directors may be left engaged if in level flight.)
Stop Rudder Inputs (if installed)
1. Rudder Pedals - Immediately Release
2. Aircraft Normal Handling - Recover
Ground Maneuvering Limitation
A/C GW > 360,520, 15 KT max taxi
Min runway width for 180 degree turn
148 feet (45 meters)
Max Operating Altitude
40,000 feet
Max Airport Elevation (takeoff and landing)
8500 feet
Runway Slope (mean)
+/- 2%
Tailwind Component (takeoff and landing)
10 knots
Crosswind Component (takeoff and landing)
32 knots
Max Crosswind on Wet and Contaminated Runways
30 knots (landing with one engine inoperative)
15 knots (landing weight below 198,410)
Turbulence Penetration
270 KIAS / .78M
Max Taxi Weight
377,870 pounds
Max Takeoff Weight (brake release)
375,880 pounds
Max Landing weight
308,650 pounds
Min Weight for Takeoff
198,410 pounds
Max Operating Speed (windshield wipers operating)
230 KIAS
Min autopilot engagement altitude after takeoff
500 feet AFE
Max Airport Elevation for Autoland Operations
8500 feet
Max Demonstrated Headwind for Autoland
30 knots
Max Demonstrated Crosswind for Autoland
15 knots*
*If braking action is reported as FAIR, maximum crosswind component is 10 knots.
Max Demonstrated Tailwind for Autoland
10 knots
Rollout limitation for Autoland
Do not use Rollout mode on runways covered with standing water, slush, snow, or ice.
APU starting limit
On the ground, three start attempts with a 1-minute cooling period between start cycles followed by a 60-minute cooling period.
APU min oil quantity indication before start
> 1/4
Min oil quantity with APU operating at 100% (stabilized condition)
MIN
Min Battery Voltage to Start APU on Battery Power
25 volts
Max Altitude to Operate (Extend or Retract) Slats
20,000 feet
Flaps and Speedbrakes
Do not operate with speedbrakes extended with Flaps 30/40.
Allowable Fuel Imbalance at Takeoff
Max inner tank imbalance is 2600#
Allowable Fuel Imbalance for Approach, Landing, and Go-Around
With outer tanks balanced, max inner imbalance is 1800#.

With inner tanks balanced, max outer imbalance is 900#

For mixed condition (I.e., inner and outer tanks both out of balance), of outer tank imbalance is less than 550#, maximum wing-to-wing imbalance is 1500#
Other Fuel Limits
Takeoff, landing and go-around with center tank feeding is prohibited.

Takeoff with inner tanks and center tank empty is prohibited of the fuel quantity in either outer tank is below 1984#
V LO (retraction)
240 KIAS/ .53M
V LO (extension)
270 KIAS / .59M
V LE
270 KIAS / .65M
Max Tire Speed
195 knots ground speed
Max Allowable Brake Temperature for Takeoff (with Brake Fans Off)
300 C
Navigation
Both FMCs (in GPS PRIMARY mode) must be operative to conduct GPS or RNAV (GPS) approaches.
Starting EGT limit
535 on ground
650 in flight
Min Oil Temperature for Takeoff
50 C
Min Oil Quantity for Start
12 quarts
Engine idle time
Engines must be operated near idle thrust for 5 minutes prior to takeoff if engines were shutdown for 2 hours or more.
Starter Re-Engagement
30% N2 maximum permissible
Reverse Thrust
Use if reverse thrust is limited to ground use only. Backing the aircraft with use of reverse thrust is prohibited.
Preflight Mnemonics
1. Exterior - P-TAG-CFW
2. Interior Safety (FO)- IWN-L-TRFR
3. Logbook - L-TA-DO
4. CDU - RIFPM
5. Cockpit Prep:
a. PFV-ESB-PSEF
b. CNP-SRT-FFE-RAR-ROSI
6. Final Cockpit - IF-IF-TT-LTM-WDD
7. Below Line - Memo
8. After Start - SAM
9. Before Takeoff - RT
10. Lineup - LTDS
11. After Takeoff - SGFIB
12. After Landing - LS
13. Shutdown - PFE-FCC
Exterior Safety
P-TAG-CFW
P - Pitot tubes
T - Tailstand
A - APU
G - Gear doors
C - Chocks
F - Flight controls
W - Left Wing upper area (frost)
Logbook
L-TA-DO
L - Logbook onboard
T - Tail # matches
A - AWR signed
D - DI Log
O - OFP deferrals match DI
Final Cockpit
(IF-IF-TT-LTM-WDD)
I - Initialization complete
F - FDP performance request
I - Init page FMC (taxi, ZFW, ZFW CG)
F - FDP Takeoff page V1, V2, VR
T - TRP
T - Takeoff page
L - Load Manifest
T - TRP/FMC takeoff
M - MCP speed
W - Windows
D - Door - cargo
D - Door - entry
BEFORE START - BELOW THE LINE - Flow
(Memo)
ECAM MEMO PAGE . . . . . . . . . CHECK
AFTER START - CPT Flow
(SAM)
Speedbrakes - Armed
Autobrakes - Max
ECAM Memo - check
After Start - FO Flow
(API-OO-U)
ANTI-ICE
Packs
Ignition
APU Master off
APU Bleed off
Trim set by U (FO)
BEFORE TAKEOFF - CPT Flow
(RT)
RUDDER . . . . . . . . . . . . . . . . . . . CHECK
TAKEOFF BRIEF . . . . . . . . . COMPLETE
Before Takeoff - FO Flow
(SIFST)
System Page - Flt Ctrl
Ignition
Flight Controls check
Status Page
Takeoff Config check button
CLEARED FOR TAKEOFF - CPT flow
(LTDS)
Lights (Exterior)
Terrain selected
Departure RWY verify
Supernumerary alerted
Cleared for Takeoff - FO flow
(RTB)
Radar
Transponder
Brake temp
AFTER TAKEOFF - flow
(SGFIB)
Speedbrakes - disarmed
Gear lever - Off
Flaps - Up
Ignition - Off
Bleeds/Packs
AFTER LANDING - CPT Flow
(LS)
Lights - set
Speedbrake - disarmed
SHUTDOWN - CPT Flow
(PEFSC)
Parking Brake - set
Fuel lever #1 - Off
Electrical power - transfer
Fuel lever #2 - Off
Slide - Disarmed (Doors clear, Pressure zero)
Cargo door - Open
SECURE - CPT flow
(PEPCL)
PFD and ND - Off
ECAM displays - dim
Panel Lights - Off
CVR Circuit Breakers - In
Logbook - Complete
5 FMA Columns
1. A/THR
2. Pitch
3. Roll
4. AP Land
5. AP/FD
FMA - Cockpit Set up
• MAN THR - amber
• V/S, P.Climb armed blue
• ALT in blue
• HDG
FMA (Non-profile Takeoff)
• THR in green (A/T engage)
o THR to blue (thrust or 100 knots)
• Pitch - SRS green (V 2+10)
o ALT- in blue (MCP altitude)
• Roll - RWY to green (if ILS freq set)
o HDG (if default)
• A/P CAT (no change)
• AP/FD (no change)
FMA (Profile Takeoff)
• THR in green (A/T engage)
o THR to blue (thrust or 100 knots)
• SRS green (V 2+10)
o P.CLB blue
• RWY to green (if ILS frequency is set)
o HDG (if default)
o NAV blue (armed)
FMA (Climbout - THR Reduc)
• P.THR in green
• P.CLB green
• NAV to green
• AP/FD - FD1 CMD (A/P on)
Climb Profile
Hydraulics
Fuel Capacity
Outer - 8
Outer - 8
Inner - 31
Inner - 31
Center - 31
Trim - 11
Total - 120,000
Normal Fuel Feed (CIO)
Engines from center tank
Then inner wings
Finally, outer wings
* T/O, LND G/A from wing tank
* APU left manifold
Hydraulics (Blue) FSSY
Blue - Smallest (3.2 gal) FSSY
• Flight Control (Primary)
• Slats
• Spoilers 1, 4, 7
• Yaw damper #1
Hydraulics (Yellow) FFSSYAABC
Yellow (4.9gal) (0.8 - RAT) FFSSYAABC
• Flight Control (Primary)
• Flaps 1 Motor
• Stab
• Spoilers 2, 3, 5
• Yaw damper #2
• Autopilot #2
• Anti-skid
• Brakes (Alternate and Parking)
• Cargo doors
Hydraulics (Green) FFSSSAAAABGG
Green - Largest (6.6 gal) FFSSSAAAABGG
• Flight Control (Primary)
• Flaps
• Slats and krugers
• Stab
• Spoiler 6
• Autopilot #1
• Anti-skid
• Autobrakes
Hydraulics-ECAM
Load Complete Time
8 mins to block out
Exterior Check Upon Arrival (P-TAG-CFW)
P - Pitot covers
T - Tailstand
A - APU area
G - Gear doors
C - Chocks
F - Flight Controls
W - Upper left wing
Interior Safety (FO) IWN-L-TRFR
I - Ignition
W - Windshield Wiper
N - Nav Lts
L - Landing Gear lever
T - Trottles
R - Reverser
F - Fuel levers
R - Radar/PWS
Logbook - L-TA-DO
L - Logbook onboard
T - Tail # matches
A - AWR
D - DI Log
O - OFP
CDU - Initial setup (RIFPM)
R - Reference
Database, Delete waypoints, navaids, Sec Fpl, engine out
I - Init (fill out both pages)
F - Flt Pln (build)
P - Prog key (check Dist)
M - Mode Control Panel (set info in windows)
Cockpit preflight (PFV-ESB-PSEF, CNP-SRT-FFE-RAR-ROSI)
P - PFD/ND
F - FD
V - VNI
E - EFIS
S - Slat/Flap Indic
B - Brakes
P - Parking Brake
S - Standby ADI-Altim
E - ECAM
F - Fuel

C - CDU
N - Nav Radio
P - Pitch trim
S - Speedbrake
R - Reverser
T - Throlle
F - Flap
F - Fuel Switches
E - Emergency cancel
R - Radar
A - Audio panel
R - Rudder Trim
R - Rat handle
O - Oxygen
S - Service Interphone
I - Instrument Light, Transfer Switches
TAKEOFF ROLL
• Throttles (1.10 EPR)
• TOGA levers
• "Set Takeoff Thrust"
• Yoke pressure until 80, none by 100
• "Checks"
• Removes hand from throttles at V1
• Rotates to 17.5° target
• "Gear Up"
400 Feet AFE
• "HDG/Select" or "NAV"
1000 Feet AFE
• "Autopilot 1 Command."
1500 Feet AFE
• Profile Takeoff
- P.THR and P.CLB displayed on FMA.
At S speed
• "Slats Retract, After Takeoff Checklist.
Pattern
Downwind/Turn to Base
• "Slats Extend, Speed 200"
Base
• "Flaps 15, Speed 180"
(Intcp hdg cleared for approach)
• Select LAND & V/N/I to ILS
• "Flaps 20, Gear Down, Speed 160"
- Gear lever Down
- Arm Speedbrakes
- Ignition - CONT RELIGHT
(Approaching G/S or 2000' AGL)
• "Flaps 40, Speed ___, Landing Checklist, Set Missed Approach Altitude"
• "Runway in Sight" or "Minimums (Alert Height) _____, "Cat 2/3"
• "Landing", "Continuing" or "Go-Around Thrust, Flaps"
Rejected Takeoff
1. Throttles - Idle
2. AutoThrottle - disconnect
3. MAX manual braking (if AUTOBRK lt)
4. Speedbrakes (if no auto) >85 kts
5. Max reverse (consistent with conditions)
6. Max braking until certain to stop
7. Reverse Idle by 60 KTS
When A/C stopped
8. Accomplish Red ECAM items.
9. Emergency Evacuation after red ECAM (if req'd)
10. Amber ECAM & QRH (if no Evacuation)
11. After Landing flow
12. Parking brake (if directed by ECAM)
Go-Around
1. Initiate Go-Around
2. "Go-Around Thrust, Flaps"
3. TOGA levers
4. Rotate to 17.5 degrees
5. "Positive Rate, Gear Up"
- 400'
6. "Heading Select" or "Nav"
- 1000' AFE
7. "Autopilot 1, Command"
- 1500' AFE
8. "Climb Thrust"
- At L/O Altitude
9. Dial in Green Dot while looking at A/S indicator
- At F-Speed
10. "Flaps Up"
- At S-Speed
11. "Slats Retract, After Takeoff Checklist"
12. "Level Change"
V1 Cut
"Gear Up"
- Rotate 10-degrees NU
- 6-units Rudder Trim
"Heading Select, 15-deg Bank, Track"
- EFP ALT (1000)
"Altitude Hold, Normal Bank"
"Autopilot One Command" (> 1000' AFE)
"Slats Retract"
"Level Change, MCT, ECAM to the secondaries"
- (Declare, WX, Divert)
"After Takeoff Checklist"
"Quick Return Checklist"
- (ADF-BBT-EHFB) ATIS, Destin, Flaps, Build, Bugs, Tune, Elevation, HOVER-AA, FDP, Brief
"Accomplish ECAM secondary items"
"Approach Checklist"
"Gear Down, Flaps 20, Speed ___(V APP),
Landing Checklist, Set Missed Approach Altitude"
Overhead Lts check
Amber
5 - Splr & Spd Brk
4 - Hyd Lo Press
3 - Servo Ctrl Lo Press
2 - Gen Fault

5 - Paddles
3 - Blue Lts (FDR, APU Pwr, Econ)
Load Manifest check
1. Manifest Wt = Init-B +/- 1000
2. Manifest + Taxi = Memo +/- 1000
3. Manifest CG +/- 1.5%
4. Ctr Fuel + ZFW < 286.6
HOVER-AA check once vectored off STAR:
H - HDG/S
O - Out of Profile mode (LVL or V/S)
V - VNI to ILS
E - Clean up FPLN and Extend Centerline
R - RNP clear edits (5L on PROG)
A - Activate final when at FAF altitude (non-ILS PROF)
A- APU
Change Destination on FPLN
1. FPLN
2. Lateral off any point downstream on FPLN
3. 5R - "New RTE/_____" Put new Identifier (KSTL)
Change Alternate on FPLN
1. FPLN
2. Select 1-down arrow
3. Lateral off 2L (which is 2nd Destination at end of FPLN)
4. 5R - "New RTE/_____" Put new Identifier (KRFD)
Discontinued Approach (Above 1000 AFE)
"Discontinued Approach"
"Altitude Hold"
"Speed 160"

"Level change" or "V/S 1000'"
"Heading Select" or "Nav"
"Flaps 20"
"Gear Up"

1500' AFE
"Climb Thrust" (At L/O Altitude)

(ALT*)
Dial in Green Dot looking at A/S

At F-Speed
"Flaps Up"

At S-Speed
"Slats Retract, After Takeoff Checklist"
CAT 2/3
Cat 3
RA 100 (Alert Height)
RVR 600, 600, 300

Contaminated Cat 3
• Set DH 50' on Cat 3
• Must disconnect A/P on nose wheel touchdown
• LO/MED columns controlling on FDP

Cat 2
DH 100 (Decision Height)
RVR 1000, 600, 300
Must see something at DH

Cat 3 Fully Operational & Contaminated require Autobrakes

Degraded or Contaminated = DH 50' (set in RA window)

Cat 3 Degraded or Cat 2 use "MAX MAN" value for regulatory only (LO or MED optional)
Autoland Sequence - LFRR
1. 1000' - "Alert Height 100, Cat 3" or "Decision Height 100, Cat 2/3"
2. 700' - ILS Lockout
3. 350' - LAND Mode ***
4. 200' - Autoland lights armed (only if failure)
5. 30' - FLARE ***
6. 30' - RETARD
7. TD - ROLLOUT / MAN THR
180° Turn
148 feet (45meters)

1. A/C right side of rwy (left gear on centerline)
2. left-turn toward edge of rwy at 25°
3. Until Captain just over edge
4. Then full-right nose wheel
5. Add power as req. on outboard
6. 5-8 KTS of speed
Windshear
After Takeoff
W/S AHEAD (Amber) - "Monitor Radar Display" - TOGA
W/S AHEAD (Red) - "Windshear ahead" (2x) - TOGA

Approach
W/S AHEAD (Amber) - "Monitor Radar Display" - Normal G/A
W/S AHEAD (Red) - "Windshear ahead" (2x) - Normal G/A

Reactive W/S
"WINDSHEAR" (Red) "Windshear" (3x) - Recovery maneuv.

• +/- 15 KIAS
• +/- 500 FPM vertical speed
• +/- 5° of pitch attitude
• +/- 1 dot G/S
• Unusual throttle sig. time
Windshear Recovery
1. TOGA
2. Firewall - A/T off and full forward
3. Rotate to FD (17.5 if not)
4. Speedbrakes - RET
5. Config - Maintain
Overspeed limit for write-up
Overspeed > VMO+20 KIAS or MMO+.02 M
< VMO+20 KIAS or MMO+.02 M if > 1.2g
Both engine flameout
260 or Green Dot (higher)
15 minutes/90 NM from FL350
Reject below 80 kts
1. Any bell, warning or light
2. Unusual noise
3. Slow acceleration
4. Tire failure