Reading...
Play button
Play button
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;
90 Cards in this Set
- Front
- Back
- 3rd side (hint)
|
Regardless of the nature and severity of the emergency, the overriding consideration will be to: |
1. Maintain aircraft control
2. Analyze the situation 3. Take appropriate action |
*Blank*
|
|
|
Five standard terms/phraseology:
|
1. Due to the seriousness of the malfunction, the aircraft shall be landed or ditched without delay. If extreme sea/terrain conditions seriously jeopardize aircrew survivability, the aircraft may be air taxied to the nearest suitable site and landed or ditched immediately. {Warning: Potential loss of airframe not sufficient to continue flight.} |
1. Land/Ditch Immediately |
|
|
1. Loss of XMSN Lubrication OR GB/MGB chip in conjunction with (Yaw kicks, Noises, or High power)
2. Loss of XMSN Lubrication AND GB/MGB CHIP |
*1. Landing/Hover Checklist - Complete (200ft checks min)
*2. Land/Ditch Immediately |
Main Gearbox Failure Imminent
W: Potential loss of airframe not sufficient cause to continue flight |
|
|
1. FLI exceeds 10.0/8.8 Possible 2. MGB Qt capture on Engine Exceedance Page 3. Aural "gong" and LIMIT light |
*1. Reduce torque to within limits, when able If no ECMS capture: 2. Continue flight as appropriate If ECMS capture below 130%: If ECMS capture above 130%: 3. Land as soon as practicable |
MGB Overtorque Hover/Transition Flight : 0-80KIAS, 10.0 |
|
|
1. MGB Fire Light |
*1. Attempt to confirm presence of fire (Alert crew) |
Main Gearbox Fire |
|
|
1. Fire Warning Light
2. Red light in EFSL 3. Flames/Smoke |
*1. Attempt to confirm presence of fire (Alert crew)
*2. Single engine flight profile - Establish CONFIRMED: *3. FADEC control switch - CONFIRM; Idle; CONFIRM; Off *4. EFSL - CONFIRM; Off *5. Boost Pumps (Affected) - Off *6. Pri Fire EXT (Affected) - CONFIRM; Push *7. Sec Fire EXT (Affected) - Push *8. Landing/Hover Checklist - Complete (200ft checks min) PERSISTS *9. Land/Ditch Immediately NO LONGER EVIDENT *9. Land as soon as possible NOT CONFIRMED 3. Land as soon as practicable |
Engine Compartment Fire In Flight |
|
|
1. Fire Warning Light
2. Hand/Voice Signals from ground crew 3. Red light on EFSL |
1. Attempt to confirm presence of fire (Alert crew)
2. FADEC control switches - Both Off 3. EFSLs - Both Off 4. Boost Pumps - All Off CONFIRMED 5. Pri Fire EXT (Affected) - CONFIRM; Push 6. Sec Fire EXT (Affected) - Push 7. Emergency Electrical Cutoff - Off 8. Rotor Brake - On 9. Evacuate Aircraft |
Engine Compartment Fire on Deck
|
|
|
Cabin, Electrical, Avionics smoke or fire
|
{C: Popped CB may be reset once. Repeated reset = Fire.}
*1. Designate crewmember to fight fire *2. Affected equipment - Off *3. Heat/Cool Switches - Off *4. Ram Air - Closed *5. Cabin Sliding Door - Closed *6. Pilot Windows - Closed *7. Rack Blower CB (Rack Fire) - Pull (R5#4) *8. Circuit Breakers - Pull (Affected) *9. Landing/Hover Checklist - Complete (200ft checks min) {W: Fire severity and flight conditions dictates following procedure. Advise secure power after VMC} {W: Secure Emergency Electrical Cutoff = No Floats} {N: AV rack fire, Short blasts, only open enough for nozzle} {N: Comms and Lighting lost after Emer Elex Cutoff} {N: Emer Elex Cutoff secures Tail Hyd Iso valve = Pedal feedback} FIRE PERSISTS *10. Emergency Electrical Cutoff - Off FIRE PERSISTS *11. Land/Ditch Immediately FIRE GOES OUT *11. Land as soon as possible |
Internal Fire (Cabin, Electrical, and/or Avionics)
|
|
|
1. Smoke
2. Fumes |
*1. Heat/Cool Switches - off
*2. Ram Air - Open *3. Cabin Sliding Door - Open *4. Pilot Windows - Open 5. Land as soon as practicable {W: Fuel fumes, limit radio xmsn, use Comm1} {C: Avoid blade or structure damage, do not jettison unless essential} {N: SEAS bottle source of air} |
Smoke and Fume Elimination
|
|
|
1. TOT rises rapidly/doesn't decrease after 10 sec after FCS Off
|
*1. FADEC Control Switch - Check Off
*2. Boost Pumps - Check Off HIGH TOT AFTER 10SEC *3. EFSL - Shut Off {C: Cranking with EFSL off will damage fuel pump} *4. Crank Button - Depress until TOT decreases TOT DOESN'T DECREASE *5. Emergency Electrical Cutoff - Off *6. Rotor Brake - On *7. Evacuate Aircraft |
Engine Post-Shutdown Fire
{N: After shutdown and N1=0, TOT may increase slightly} {C: Solenoid valve failure, FADEC will shutdown. Don't move EFSL until 10sec} |
|
|
1. Rotor blade damage known/suspected
2. Secondary indications(vibs) more than moderate |
*1. Landing/Hover Checklist - completed (200ft checks min)
*2. Land/Ditch Immediately |
Rotor Blade Damage (More than moderate)
|
|
|
Vibrations Levels
|
Slight - Not apparent unless total attention directed
Moderate - Noticeable, but does not affect work Severe - Immediately apparent and tasks only completed with difficulty Intolerable - Sole preoccupation to reduce vibration level |
Slight, Moderate, Severe, Intolerable
|
|
|
1. Rotor blade damage known/suspected, less than moderate secondaries
|
*1. Land as soon as possible
|
Rotor Blade Damage (Less than moderate)
|
|
|
1. Severe/Intolerable vibrations
|
*1. Landing/Hover Checklist - Complete (200ft checks min)
*2. Land/Ditch Immediately |
Abnormal Vibrations (Severe/Intolerable)
|
|
|
1. Moderate vibrations
|
*1. Cruise Airspeed - 75-120KIAS
*2. Avoid abrupt maneuvers *3. Land as soon as possible |
Abnormal Vibrations (Moderate)
|
|
|
1. Any uncommanded left yaw not attributable to mechanical failure of tail rotor
|
*1. Immediate full right pedal, max deflection
*2. Altitude/Obstacles permitting, smoothly apply forward cyclic to increase forward airspeed *3. Altitude permitting, reduce collective *4. NR Switch - HI {W: Rapid collective lowering may result in undesirable decent rate. Large collective pull may cause ULY} {C: Gradual pedal won't stop yaw. 300 degree lag. Lag not loss of thrust} |
Uncommanded Left Yaw
|
|
|
1. GB/TGB CHIP Light
|
*1. Establish safe altitude and airspeed for possible loss of tail rotor thrust
*2. Land as soon as possible |
TGB Chip Detected
|
|
|
1. Immediate RAPID left yaw
2. Pedals movable with no effect 3. Abnormal vibs/noise from tail 4. GB/TGB CHIP light |
*1. EFSLs - Both Off
*2. Maintain landing attitude *3. Cushion landing with collective |
Loss of Tail Rotor Thrust while Hovering
|
|
|
1. Uncommanded yaw
2. Pedals movable without effect 3. Abnormal vibs/noise from tail 4. GB/TGB CHIP light 5. Stuck Pedals |
*1. Directional Control - Maintain using cycle and collective
2. Redbook |
Loss of Tail Rotor Thrust in Forward Flight OR Fixed Tail Rotor Pitch
|
|
|
Any suspected engine malfunction
|
*1. NR - Maintain
*2. Airspeed/Altitude - Control and set limits *3. Wheels/Floats - As required *4. Analyze {C: 30Sec range = Major maintenance, Land ASA Prac, Further flight only after inspection and release} |
Big 4
Engine Emergencies In-Flight - General |
|
|
1. Low NR Horn
2. NR decaying 3. Engine parameters decreasing 4. Possible right yaw |
*1. NR - Maintain
Max Glide - 105KIAS, 360rpm Min Rate - 75KIAS, 360rpm |
Dual Engine Failure In-Flight
|
|
|
Visual Autorotation Procedures
|
*1. Complete Big 4 (75-105KIAS)
*2. Turn toward desired landing area and/or into the wind *3. 200' RADALT - Wheels Recheck *4. 125' RADALT - Intitiate Flare; Inflate floats as required *5. Assume landing attitude, Eliminate yaw/drift prior to touchdown *6. Collective - Cushion the landing |
*Blank*
|
|
|
Instrument Autorotation Procedures
|
*1. Complete Big 4
*2. Turn toward desired landing area and/or into the wind *3. 200' RADALT - Wheels Recheck *4. 125' RADALT - Initiate Flare, Arrive 20deg nose up at 75' RADALT; Inflat floats as required *5. Maintain flare until Airspeed = 30 plus 1/2 wind *6. Assume 5deg nose up, wings level, landing attitude *7. 25' RADALT - Collective - Cushion the landing |
*Blank*
|
|
|
1. NR Droop
2. Abnormal ENG Parameters 3. DIF N1 Light 4. Low NR Horn 5. Torque, TOT, N1, N2 decreasing 6. ENG spool down (GEN Fail, ENG oil P) 7. FLI switch to OEI mode 8. ECS disengages 9. Bleed air shuts off |
*1. NR - Maintain
*2. Airspeed/Altitude - Control *3. Wheels/Floats - As required *4. Land back or Continue flight LAND BACK *5. Assume landing attitude, eliminate yaw and drift prior to touchdown CONTINUED FLIGHT *6. Collective - Adjust to Max power, maintain Min NR (345+) *7. Airspeed - Climb at 70-75KIAS *8. NR/OEI - Set as necessary *9. Analyze {W: Keep NR above 300} |
Single-Engine Failure In Flight: Low/High Hover, Takeoff/Landing Transition
|
|
|
1. NR Droop
2. Abnormal ENG Parameters 3. DIF N1 Light 4. Low NR Horn 5. Torque, TOT, N1, N2 decreasing 6. ENG spool down (GEN Fail, ENG oil P) 7. FLI switch to OEI mode 8. ECS disengages 9. Bleed air shuts off |
*1. Complete the Big 4
*2. Engine Shutdown Procedure - Complete {N: Unable to restart, recover ECS with COOL switch} |
Flameout
|
|
|
1. ENG CHIP Light
2. ENG CHIP on VEMD |
*1. Complete the Big 4
*2. FADEC Control Switch (Affected) - CONFIRM; Idle *3. Engine - Monitor ABNORMAL INDICATIONS *4. Engine Shutdown Procedure - Complete NORMAL (Redbook) (Land ASA Prac, FCS to FLT as reqd) |
Engine Chip Detected
|
|
|
1. N2 significantly above NR
2. Zero torque on malfunctioning ENG 3. Possible loud noises from ENG |
*1. Complete the Big 4
*2. Engine Shutdown Procedure - Complete |
Engine Gearbox/Output Shaft Failure
{N: N2 reaches 122.4+/-1%, FADEC operates stop electro-valve via BIM} |
|
|
1. DIF N1 Light
2. OEI GOV mode 3. N1 difference above 6% |
*1. Complete the Big 4
(Redbook) |
N1 Divergence/Partial Power Loss
{N: N1 above 40%, OEI GOV mode. N1 below 40%, OEI mode.} |
|
|
1. FADEC FAIL Light
2. Red light on EFSL 3. OEI GOV mode 4. Affected ENG doesn't respond to collective |
*1. Complete the Big 4 |
Major FADEC/Governor Failure
|
|
|
1. GOV Light
|
*1. Completed the Big 4
(Redbook) (Abort Mission) {W: Loss of crosstalk may result in stable NR below 345. Engines may provide level flight. Analyze using all parameters. Consider NR HI and running landing} |
Minor FADEC/Governor Failure
|
|
|
1. ENG OIL P Light
2. ENG oil pressure flux, incr, decr abnormally 3. Red light on EFSL 4. ENG oil pressure <25psi |
*1. Complete the Big 4
*2. Engine Shutdown Procedure - Complete |
Lubrication System Failure
{C: Low oil pressure AND OIL P Light is not indication malfunction. Shall not wait for additional symptoms} {N: Oil pump failure may be preceeded with pressure spike and CHECK CDU} |
|
|
1. Popping or rumbling noises
2. TOT increases 3. Torque/N1 decreases 4. Airframe Vibration |
*1. Complete the Big 4
NORMAL INDICATIONS (Redbook) 2. Land ASA Prac ABNORMAL INDICATIONS *2. FADEC Control Switch (Affected) - CONFIRM; Idle 3. Engine - Monitor ABNORMAL IDLE *4. Engine Shutdown Procedure - Complete NORMAL IDLE (Redbook) 4. Land ASA Prac {N: If power needed, may use FLT. Surge possible} |
Engine Surge or Compressor Stall In-Flight
|
|
|
1. Popping or rumbling noises
2. TOT increases 3. Torque/N1 decreases 4. Airframe Vibration/Shuddering (On Deck) |
*1. FADEC Control Switch (Affected) - Off
*2. Fuel Boost Pumps (Affected) - Off *3. TOT - Monitor for Post Shutdown Fire |
Engine Surge or Compressor Stall on Deck
|
|
|
Engine Shutdown Procedure In-Flight
|
*1. Single-Engine Flight Profile - Establish
*2. FADEC Control Switch (Affected) - CONFIRM; Idle; CONFIRM; Off (Redbook) (Land ASA Prac) |
*Blank*
|
|
|
1. Insufficient voltage (<17VDC)
2. FADEC FAIL Light 3. TOT underlined in red 4. No rise N1/TOT within 10sec 5. TOT rises rapidly, likely exceed 750degC 6. Main rotor doesn't turn prior to 25% 7. N1 doesn't reach 45% by 30sec and holding 8. ENG OIL P Light doesn't extinguish by 70% 9. N2 passes NR |
*1. FADEC Control Switch - Off
*2. Boost Pumps - Off *3. TOT - Monitor for Post Shutdown Fire {C: Failed start with OAT below 0degC and TOT above 120degC, crank for 20sec before next start} |
Engine Start Emergencies
{N: FADEC auto shuts down TOT exceeding 840degC. Shall initiate shutdown likely exceed 750degC} |
|
|
1. FLI DEGR on VEMD
2. TRQ/TOT/N1 value missing with yellow boldface 3. GOV Light 4. All other ENG parameters normal |
*1. Complete the Big 4
(Redbook) (Abort Mission) |
Torque, TOT, N1 Indicating System Failure
|
|
|
1. PRI SERVO P Light
2. SERVO JAM Light 3. LIMIT Light 4. HYD2 PRESS <720psi 5. SERVO LIMIT on VEMD 6. High pitched noise from XMSN 7. Stiffness in flight controls |
*1. Cruise Airspeed - 75-100KIAS
*2. Avoid abrupt maneuvers 3. Land ASA Prac |
Primary Hydraulic System Failure
|
|
|
1. SEC SERVO P Light
2. SEC HYD LO PRESS Light 3. SERVO JAM Light 4. HYD1 PRESS <720psi 5. SEC HYD ISOLATE Light (Fluid loss) POSSIBLE 6. High pitches noise from XMSN 7. Stiffness in flight controls |
*1. Cruise Airspeed - 75-100KIAS
*2. Avoid abrupt maneuvers (Redbook) |
Secondary Hydraulic System Failure
|
|
|
1. SEC HYD ISOLATE Light
2. SERVO JAM Light POSSIBLE 3. High pitched noise from XMSN 4. Stiffness in flight controls |
*1. Tail Hyd Isolate Switch - NORM
{C: If pedals not relaxed before switch, possible rapid right yaw and overtorque} (Redbook) (Land ASA Prac) |
Secondary Hydraulic System Low Fluid Level
|
|
|
1. SEC HYD HI PRES Light
2. SEC HYD LO PRESS Light |
*1. Landing Gear Handle - Down (Check wheels down)
(Redbook) (Land ASA Prac) |
Secondary Hydraulic Pressure High/Low
|
|
|
1. BATT TEMP Light
2. Smoke/fumes from radome 3. Noises from radome |
*1. BATT relay switches - Both Off
(Land ASA Prac) |
Battery Over Temperature/Thermal Runaway
|
|
|
1. Low battery LED flashing
2. Partial/complete degredation of NVG image |
*1. Announce failure to crew
IF PAC *2. Flight controls - Conduct positive transfer to safety pilot, conditions permitting (Redbook) |
NVG Failure
|
|
|
1. ENG FUEL P Light
|
*1. Complete the Big 4
*2. Engine - Monitor ABNORMAL INDICATIONS *3. Engine Shutdown Procedure - Complete NORMAL (Redbook) 3. Land ASA Prac |
Engine Fuel Pressure Low
|
|
|
1. FUEL FILT Light
|
BOTH ILLUMINATED
*1. Land ASA Possible ONE ILLUMINATED 1. Land ASA Prac |
Fuel Filter Contamination
{C: Do not transfer fuel unless absolutely necessary} |
|
|
1. FEED TANK Light with fuel in system
2. Boost pump pressure flux, 0, incr, decr, or blanks 3. FUEL PARAMETER OVERLIMIT |
*1. Fuel Boost Pumps (Affected) - Both On
(Redbook) (Abort Mission) |
Single Fuel Boost Pump/Ejector/Indicator Failure
{W: Do not reset CBs} {C: Above 8000', use both} |
|
|
HIFR Emergency Breakaway
|
*1. Crew - Alerted "Breakaway" x3
*2. Emergency Quick-Disconnect Handle - Pull {C: To prevent damage and spill, should not shear. Use emer quick disconnect} (Redbook) |
*Blank*
|
|
|
Gyro Reversionary |
*1. Flight Controls - Stabilize aircraft |
Attitude Gyro Failure During Reversionary Operation
|
|
|
1. Affected FD bar/pointer hidden
2. FD flags on ADIs |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Detected FD Failure
|
|
|
1. Deviation of aircraft from desired flight path
2. FD bar/pointer centered |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Undetected FD Failure
|
|
|
1. AFCS Light
2. One of more AFCS channels disengaged 3. Channel Lights flashing 4. P/R/Y Trim Light possible 5. TRIM OFF Light possible |
*1. Flight Controls - Stabilize Aircraft
*2. Disengaged Channels - Attempt to re-engage (Redbook) |
AFCS Computer or Series Actuator Failure
|
|
|
1. Uncommanded aircraft displacement
2. P/R/Y TRIM Light |
*1. Flight Controls - Stabilize Aircraft
*2. Affected Channels - Disengage (Abort Mission) |
AFCS Series Actuator Hardover (Undetected)/Parallel Servo Hardover
|
|
|
1. Uncommanded movement of collective
2. Command pointer directs proper direction |
*1. Flight Controls - Stabilize Aircraft
*2. Collective - C-Sync Depress and Stabilize (Redbook) |
Collective Parallel Servo Hardover
|
|
|
1. Unable to reposition cyclic force feel using SYNC/TRIM button or overhead TRIM switch
OR 2. Cyclic has no artificial force feel |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Cyclic Artificial Feel (Feel/Trim) Failure
|
|
|
1. CDUs - NO DATA on both
2. Loss of all avionics except Comms |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Dual Data Bus Lockup
|
|
|
1. CHECK STATUS in CDU
2. STAT FAIL - STR 3. Loss of FMS FD guidance |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Steering Guidance (STR) Failure
|
|
|
1. Red DCP on MFD
2. Heading Bug disappears 3. MFD does not respond to DCP 4. MFD pages cycle without DCP input |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Display Control Panel (DCP) Failure
|
|
|
1. Audio tone in headset when interrogated
|
*1. Select M4A/M4B as appropriate
(Redbook) |
Mode 4 Audio Tone
{N:Valid but not compatible code} |
|
|
1. Complete loss of audio (All)
2. All ICS/XMIT inop 3. Constant squeal/hum |
*1. Pilot/CP Audio Bypass Switches - BYPASS
(Redbook) |
Audio System Failure
|
|
|
1. Lateral vibs when rolling. May be violent.
|
*1. Lift aircraft off ground immediately or reduce taxi speed.
{C: Excessive/abrupt aft cyclic may tail strike} (Redbook) |
Nosewheel Shimmy Damper Failure
|
|
|
1. HEATER O/HEAT Light
2. ECS CB popped on CP FWD panel |
*1. Heat Switch - Off
(Redbook) |
Heater Overheat
|
|
|
1. CP altimeter/VSI erratic or erroneous
2. Erratic FDS |
*1. Flight Controls - Stabilize Aircraft
*2. Affected Flight Director Modes - De-select (Redbook) |
Copilot Static System Failure
|
|
|
1. Erratic/erroneous CP IAS
2. MFDs - IAS erratic/erroneous 3. Erratic FDS 4. Possible loss of auto turn coordination |
*1. Flight Controls - Stabilize Aircraft
*2. Affected Flight Director Modes - De-select (Redbook) |
Copilot Pitot System Failure
|
|
|
Hoisting Warning
|
{W: If hoist cable damaged, shall not use, shall not retrive into drum, consider quick splice}
|
*Blank*
|
|
|
1. Hoist cable fouled/caught
2. Hoist cable visually damaged |
IMMINENT DAMAGE/INJURY
*1. Activate Hoist Shear switch while announcing "SHEAR"x3 CONDITIONS PERMIT *1. Pay out slack in cable *2. Advise Pilot *3. Direct the vessel's crew to free cable *4. If unable to free or damaged, wrap and sever *5. If mission urgency dictates, assemble quick splice {C: Quick splice = no speed reduction or up limit switch} |
Hoist Cable Fouled/Damaged
|
|
|
1. Hoist fails to respond to FM inputs
|
*1. Advise pilot "COMMITTED" or "NOT COMMITTED"
NOT COMMITTED *2. Abort the hoist COMMITTED *2. Check the cable and drum for fouling *3. Activate Emergency Hoist Power and continue hoist HOIST POWER NOT RESTORED *4. Activate Manual Override and continue the hoist {C: Override = no limit switches, shall close Step1Valve with device in cabin to prevent creep} (Redbook) |
Hoist Failure
|
|
|
1. Hoist boom does not respond to electrical control inputs
|
*1. Hoist Master Switch - Check CREW position
*2. Hoist ACT Control and Hoist ACT Power CBs - Pull, Reset (R1#1,R2#2) NO RESPONSE *3. Hoist ACT CBs - Pull *4. Hoist Operator Pendant - Disconnect *5. Manual Crank - Install *6. Manually crank boom to stowed position. *7. Manual Crank - Remove (Redbook) |
Hoist Boom Failure
{N: Stow and In/Out switches separate, Stow works as long as #1DC Bus powered} |
|
|
1. Hoist Cable extends/retracts without input
|
*1. Secure hoist power at hoist control panel ONLY
*2. Advise the Pilot "COMMITTED" no "NOT COMMITTED" COMMITTED *3. Activate Manual Override and continue hoist NOT COMMITTED (Redbook, Abort hoist) {W: Do not secure cockpit switch, lose shear} {C: Manual Override = limit switches inop, shall close Step1Valve with device in cabin to prevent creep} |
Hoist Electrical Runaway
|
|
|
1. Pilot/FM unable to listen/talk during hoist
|
*1. Flight Mech - Tap Pilot and give HOLD signal (fist)
*2. Advise the Pilot "COMMITTED" or "NOT COMMITTED" NOT COMMITTED *3. Abort Hoist COMMITTED *3. Flight Mech - Hot Mic selected, Helmets connected, Attempt Hot Mic comms NO COMMS *4. Press Push-to-talk switch, Attempt PTT comms NO COMMS *5. Audio Control Panel - Select ALTN, Attempt comms (no ALL or HOT) NO COMMS AND COMMITTED *6. Communicate by vocal commands and continue hoist |
Lost Communications during Hoisting Operations
|
|
|
Lost Swimmer Day
|
*1. Mark position
*2. Transition and establish right orbit *3. Look/Listen for RS Signals *4. When visual - Resume hover position UNABLE TO LOCATE *5. Complete Leaving Rescue Swimmer On Scene Procedure (Signals - Radio, Smoke, Mirror) |
*Blank*
|
|
|
Lost Swimmer Night
|
*1. Mark position
*2. Flash Landing/Hover Light *3. Look/Listen for RS Signals *4. When visual - Cease flashing lights NOT LOCATED *5. Complete Leaving Rescue Swimmer On Scene Procedure (Signals - Radio, Strobe, Flare) |
*Blank*
|
|
|
Emergency Recovery of Rescue Swimmer
|
*1. Rescue Basket - If rigged and empty
{N: Rescue brief not reqd} {N: If 2 swimmers, they may disconnect and hoist together} *2. Bare Hoist Hook - If basket not readily available |
*Blank*
|
|
|
Rescue Swimmer Falls Through Ice
|
HOIST CABLE ATTACHED
*1. RS - Extract by rolling out, pulling with ice awls, or hoist cable *2. Establish hover. FM conns helo into position so RS may be hoisted HOIST CABLE NOT ATTACHED *1. RS - Extract by rolling out or pulling with ice awls UNABLE TO EXTRACT *2. Complete Emergency Recovery of RS |
*Blank*
|
|
|
Emergency breakaway of Disembarked Rescue Swimmer on Ice
|
*1. On prebriefed freq, Pilot announce "BREAKAWAY"x3
*2. FM shear/cut hoist cable *3. Complete Leaving Rescue Swimmer On Scene Procedures |
*Blank*
|
|
|
Leaving Rescue Swimmer On Scene
|
*1. Mark and record position
*2. Deploy lighted raft *3. Deploy DMB (Redbook) |
*Blank*
|
|
|
1. Severe Vibrations unknown origin
2. Insufficient power/control to maintain flight 3. Other confirmed EPs leading to land/ditch immediately |
*1. Crew and PAX - Alerted
*2. Wheels/Floats - As Required *3. Land/Ditch Aircraft *4. EFSLS - Both Off *5. Emergency Electrical Cutoff - As Required *6. Rotor Brake (Land) *7. Emergency Egress Procedure - Execute {W: Consider jettisoning egress hazards} {W: Activating floats may create burning elex smell, not elex malf or fire} |
Immediate Emergency Landing/Ditching
|
|
|
MH Emergency Egress Procedures
|
*1. Wait for all violent motion to stop |
*Blank*
|
|
|
1. Cabin sliding door does not fully open or secure close
|
*1. Flight Mech - Remain secured to aircraft
|
Malfunctioning Cabin Sliding Door
|
|
|
1. Any unintentional, undesirable, or unsafe aircraft attitude
|
*1. Level the wings
*2. Nose on the horizon *3. Center the ball *4. Power - Adjust to maintain level flight |
Unusual Attitude Recovery
|
|
|
1. Unplanned entry into IMC from VMC without proper ATC clearance
2. Undesirable or unsafe aircraft attitude |
*1. Announce "IIMC"
*2. Establish an instrument scan *3. Establish safe altitude, airspeed, and heading. (Redbook) (4. External Comms) |
Inadvertent IMC
|
|
|
1. HUD monocle flickers or blanks 2. HUD display parameters flash, blank or do not correlate to aircraft instrument panel |
*1. Announce failure to the crew |
HUD Failure |
|
|
DELTA
1. AFCS pitch and roll channels disengaged 2. Pilot and copilot ADIs failed 3. Loss of cockpit instrument lighting 4. Loss of all AC powered equipment |
*1. Flight Controls - Stabilize aircraft
(Redbook) |
Dual AC Bus Failure |
|
|
DELTA
1. One 26 VAC FAIL light illuminated 2. AFCS pitch and roll channels disengaged 3. ADI failed on one side 4. All equip on one main AC bus inop and/or loss of equipment powered by 115VAC and 26VAC by respective xformer 5. Alternator FAIL light (Maybe) 6. BTC CLOSED light (Maybe) |
*1. Flight Controls - Stabilize aircraft
*2. 26VAC XFER SWITCH - Move in direction of illuminated FAIL light *3. AFCS - Reengage (Redbook) |
AC System Failure
Main AC Bus Short Alternator Failure Alternator Control Unit Failure 115/26VAC System Failure |
|
|
DELTA
1. Loss of equipment on one main DCbus 2. EGI failure EP symptoms 3. SERVO JAM, SEC HYD ISOLATE, HEATER O/HEAT lights (#2 Bus) 4. Loss of radar display on MFD2 (#2 Bus) 5. Associated generator FAIL light 6. Associated battery relay OPEN light |
*1. Flight Controls - Stabilize aircraft
*2. AFCS Gyro Selector Switch - Move in direction of the operating EGI *3. AFCS pitch and roll - Reengage {N: AFCS Yaw needs both EGIs. Yaw not regained with one.} *4. Affected audio control panel - ALTN (FM to ALTN for #1 Bus short) (Redbook) |
Main DC Bus Short
|
|
|
DELTA
1. AFCS Light 2. AFCS Channel Light flashing 3. AFCS Channel disengaged 4. ATT Flag and Turn pointer hidden 5. FDS bars/pointer disappears (CP) 6. FD UCPL (CP) 7. Red HDG Flag on MFDs 8. Yellow CWM on unaffected MFD 9. STAT Fail: EGI1, HDG1 or EGI2, HDG2 |
*1. Flight Controls - Stabilize aircraft
*2. AFCS Gyro Selector Switch - Move in the direction of the operating EGI *3. AFCS Pitch/Roll - Re-engage {N: Yaw cannot be regained with 1 EGI} (Redbook) |
EGI Failure
|
|
|
DELTA
1. Undesired movement of the collective 2. RADALT cycle, freeze, mask 3. FDS pointer centered 4. CDU Check Status 5. RALT on STAT page 6. "L GEAR" if gear up 7. NO TRACK on Radalts 8. Altitude pointer masked 9. RA flag on MFD hover page 10. No vertical guidance for THOV or HOVAUG 11. ALT flag in ADIs |
*1. Collective C-Sync - Depress and Stabilize
(Redbook) |
Radar Altimeter Cycle or Failure
|
|
|
DELTA
1. Loss of avionics on either side (SCC, CDU, COMM, EGI, IFF) or entire shed bus |
*1. Flight Controls - Stabilize Aircraft
*2. AFCS Gyro Selector Switch - Move in the direction of the operating EGI. *3. AFCS Pitch/Roll - Re-engage (Redbook) |
Single Avionics (Electrical) Bus Failure
|
|
|
DELTA |
*1. Flight Controls - Stabilize Aircraft |
CDU Failure |
|
|
DELTA
1. CDU Check Status 2. STAT Fail: SCC, ADF, VOR, RRU, STR |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
SCC Failure
|
|
|
DELTA
1. CDU Check Status 2. Yellow CWM on good MFD 3. STAT Fail: MFD1, HDG1 or MFD2, HDG2 4. MFD status page failures 5. Degraded operation of 1 MFD 6. Possible loss of roll guidance |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
MFD Failure
|
|
|
DELTA
1. CDU Check Status 2. STAT Fail - MFD1, MFD2, HDG1, HDG2 3. MFD Status page fails 4. Degraded operation of MFDs 5. Loss of FMS guidance 6. FMS info lost 7. TCAS failure |
*1. Flight Controls - Stabilize Aircraft
(Redbook) |
Dual MFD Failure
|
