BOLDFACE EXAM REVISION Flashcards
What are the 11 conditions under which the engine must be shutdown?
R - unusual Roughness/vibration
U - Uncontrollable power
N - Nacelle overheat
L - excessive visible fluid Leak
T - Turbine overheat
F - engine Fire
O - an uncontrollable drop in Oil pressure
T - Throttle control failure
O - an uncontrollable rise in Oil temperature
T - uncontrollable rise in Turbine inlet Temperature
P - certain Prop malfunctions
Engine shutdown boldface
Warnings? (2)
1) “CONDITION LEVER” - “FEATHER” (NFP)
2) “FIRE HANDLE” - “PULLED” (NFP)
- for fire/nacelle overheat or visible fluid leak
3) “AGENT” - “DISCHARGED” (NFP)
- for fire/nacelle overheat
- For throttle control failure: DO NOT move condxn lever. Could cause cable fouling
- For fire or Nac O/H, a break in bleed manifold could exist, isolate the wing (close engine bleed air valve &wing isolation valve, discharge remaining bottle if rqd.)
APU shutdown boldface
Warning? (1)
1) “FIRE HANDLE” - “PULLED” (CP)
2) “AGENT” - “DISCHARGED” (CP)
- for fire
- If condxn persists, discharge remaining bottle
GROUD EVACUATION boldface
Warnings? (3)
1) “PILOTS BRIEF” - “ACKNOWLEDGED” (LM)
2) “PARK BRAKE” - “SET” (P)
3) PRESSURISATION - EMERGENCY DEPRESS (E)
4) DC BUS TIE SWITCHES - TIED (E)
5) “RAMP” - “GROUNDED” (LM)
- If required
6) CONDITION LEVERS - FEATHER (CP)
7) FIRE HANDLES - PULLED (CP)
8) DC POWER SWITCH - OFF (E)
- If ramp primary exit: ensure open prior to engine/APU shutdown
- Main wheel well fire: evacuate immediate area by >300ft (600ft w munitions on board). Appch from fore/aft only
- If ^^ exists (or hot brakes), chock Nose wheel only
NORMAL BRAKE FAILURE boldface
1) “FEET CLEAR, BRAKES EMERGENCY” -
“EMERGENCY” (E)
ABORT boldface
Warnings? (1)
1) THROTTLES - FLIGHT IDLE (FP)
2) BRAKES - APPLY as rqd (FP)
3) “CONDITION LEVER” (as rqd) - “FEATHER” (CP) - on command of pilot
4) THROTTLES - GROUND IDLE (P)
5) SYMMETRICAL ENGINES - REVERSE (P) - as rqd
- If aborting for prop malf/another scenario that causes asymmetric power, shut down affected engine when throttle in FI.
MULTI-ENGINE ROLL BACK boldface
Warnings? (5)
1) NO.2 CROSSFEED VALVE - OPEN (E)
2) MAIN TANK BOOST PUMPS - ON (E)
3) NO. 1,3 AND 4 CROSSFEED VALVES - CLOSED (E)
4) TD VALVES - NULL (E)
5) PROP GOVERNORS - MECHANICAL (CP)
6) SYNCHROPHASER MASTER - OFF (E)
7) ENGINE BLEED AIR VALVES - CLOSED (E)
- if condition persists
- If BF not initiated ASAP: flame out of all engs could occur
- APU gen: is rqd to start engines after 4 eng failiure. If No.2 crossfeed valve not open, APU start impossible due loss of LH DC power.
- Synchrophaser CBs: if Power loss condxs persist after pulling, remove synchrophaser from its mount
- BF: should correct for prop malfs arising from fuel system, loss of RPM or bleed issues. Crew to check all other systems for normal op
- Systems to be left in config laid out by BF actions. Fuel/bleed systems need operating, take extreme care. Start APU to have backup pwr available.
FOUR ENGINE FAILURE boldface
Warnings? (2)
1) APU - START, RUN (BELOW F200) (E)
2) THROTTLES - SET (1 INCH ABOVE FLT IDLE) (FP)
3) “APU GENERATOR” - “ON” (E)
if any engines do not start
4) “CONDITION LEVER(S)” - “FEATHER” (NFP)
- on command of pilot
5) CONTINUE WITH AIRSTART PROCEDURE
- Fx all engines: removes Hyd assistance to flight controls
- Systems to be left in config laid out by BF actions. Fuel/bleed systems need operating, take extreme care
PROPELLOR REVERSE ROTATION boldface
1) AIRSTART PROCEDURE (if possible)
if airstart not possible;
2) AIRSPEED - REDUCE TO VMCA2 (FP)
THROTTLE CONTROL FAILURE boldface
Warnings? (3)
1) “FIRE HANDLE” - “PULLED” (NFP)
- Do not attempt to restrain a throttle that moves on its own (prop may rev or full pwr)
- Binding/failure of throttle control system: potential for full pwr/full reverse or wrong indications. ESDP
- Do not move cndxn lever or throttle
SMOKE AND FUME ELIMINATION boldface
Warnings (5)
1) “OXYGEN” - “ON, 100 PERCENT” (ALL)
2) “PRESSURISATION” - “EMERGENCY DEPRESSURISATION” (E)
- on command of the pilot
3) “DESCENT” - “AS REQUIRED” (FP)
- Flammable fumes: elec equip not required should be turned off
- Issues with Oxy system: crew to change flight environmental/regulator setting or move onto oxy bottles
- > 5mins exposure to high concentration of extinguisher agent to be avoided (eye pro & oxy to be used)
- Lithium batteries: thermal runaway (extinguiser, vold water, jettison or contained & watched).
- Pax on board: descend lower for oxy
Loads: wear harness when operating ramp/doors
PRESSURISATION FAILURE boldface
Warnings (2)
1) “OXYGEN” - “ON, 100 PERCENT” (ALL)
- as required
2) “DESCENT” - “AS REQUIRED” (FP)
- Structural damage: assess before changing flap position
- Depress a/c before attempting lock/unlock of doors/hatches
INFLIGHT DOOR WARNING LIGHT boldface
Warnings? (2)
1) SEATBELTS - FASTENED (ALL)
- A/C pressurised: capt to direct pax to stay in flight deck until crew door confirmed safe
2, A/C completely depressed before eng checks doors/hatches (harness)
AILERON TRIM RUNAWAY boldface
1) AILERON TRIM - OPPOSE (FP)
2) AILERON TRIM TAB CB (6E2) - PULLED (E)
RUDDER TRIM RUNAWAY boldface
1) RUDDER TRIM - OPPOSE (FP)
2) RUDDER TRIM TAB CB (6E3) - PULLED (E)
ELEVATOR TRIM RUNAWAY boldface
Warnings: uncontrollable NOSE UP (4)
Warnings: uncontrollable NOSE DOWN (2)
1) ELEVATOR TRIM - OPPOSE (FP)
UP:
1. Bank
2. Reduce airspeed
3. Extend flaps
4. Reduce airpseed w flaps while decreasing bank to maintain ctrl
DOWN:
1. Reduce power
2. Reduce airspeed to maintain ctrl
2) ELEVATOR TRIM - OFF (FP)
HYDRAULIC PRESSURE LOSS DURING FLAP OPERATION boldface
1) FLAP LEVER - MATCH TO FLAP POSITION (NFP)
HYDRAULIC PRESSURE LOSS DURING LANDING GEAR OPERATION boldface
1) GEAR LEVER - UP (CP)
Lethal warning: High energy ignition
- Pull & tag CBs
- Ignition disarm switches: OFF
- Allow 5min for unit to dissipate charge
- Discharge igniter plug to earth before handling
- Nil work carried out if volatile fumes detected
Lethal warning: Propellor
keep clear of the prop arc if APU is operating or when external air unit is connected
Lethal warning: Cargo door
- Any time maintenance is performed in vicinity of cargo door, safety lock is to be installed & ensure all personnel clear when operating the doors
Lethal warning: counter measure expendables (CMDs)
- CMDS Safety pins on port side to be fitted at all times
- CMDS master power switch (Nav side panel): “SAFE” & guarded at all times
- WOW override switch (Nav side panel): “OFF” & guarded at all times
- Master CMDS switch Nav SPS CB panel): “OFF” & guarded at all times
What are the indications of a SP malfunction
- A temporary loss/misrepresentation of all MFDU info
- An SP swap (momentary red Xs on all MFDUs & change of SP master on FMS master switch)
- QNH reset to 1013hpa on each PFD
- FMC fail message on SFD MCDU
SP EVENT: boldface
Warning? (1)
1) Conduct a go-around to gain/maintain MSA - (FP)
2) If navaid/communications information is lost:
Select SYS > PWR CTRL > ALL ON - (N)
3) “ALTIMETERS” - “XXXFT SET” (CP,P,N)
4) Select LEGS > ACTIVATE > EXECUTE (N)
- Display services reset: QNH 1013, mins to 500ft (baro & rad)
Ditch warnings (9)
1) Do not exceed recommended airspeed, ROD not to exceed 200fpm, maintain constant backpressure on controls but DO NOT STALL (severe impact)
2) Do not lock ENG/NAV seats in a position that will block the copilot from evacuation. Ensure galley floor is up & locked
3) Crew/pax are not to leave ditch positions until a/c has stopped forward movement.
4) Side emergency exits & flight deck hinged windows not to be used in heavy seas or nose down condition.
5) In an emergency, pilot & co’s side windows can be used but heavy flooding can occur
6) exit via centre escape hatch is possible only from the RHS when escape ladder is fitted
7) Ensure personnel are clear of the aircraft & escape hatches before inflating lifevests
8) Life raft release handles must be pulled through complete travel.
9) With smoke/fumes present, there may be insufficient time of useful consciousness to attemp exit from more than one exit
