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FOM Flashcards

1
Q

LRPCC RESPONSIBILITIES

A
  1. ENSURING CREW PRER AND PLANNING FOR ALL MISIONS IS CARRIED OUT
  2. APPROVING TACTICS TO BE EMPLOYED IN ASSIGNED MISSIONS
  3. ENSURING STANDARD TACTICAL AND OPERATING PROCEDURES ARE FOLLOWED
  4. EFFECTIVE COMPLETION OF ASSIGNED MISSION
  5. TACTICAL TRAINING, CATEGORIZATION, QUALIFICATION, ADVANCEMENT, AND OPERATIONAL READINESS STATE OF CREW
  6. ADMINISTRATION OF CREW
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2
Q

LRPC RESPONSIBILITIES

A

TO THE SQUADRON CO :
1. EXERCISING COMMAND OF THE AIRCRAFT AND ALL PERSONS ONBOARD
2. SAFE EXECUTION OF FLIGHT
TO LRPCC
1. TASK ASSIGNMENT OF CREW PILOTS AND FES
2. TRAINING CATEGORIZATION, QUALIFICATION, AND ADVANCEMENT OF PILOTS AND FES ON THE CREW

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3
Q

AIRCRAFT CAPTAIN

A

DESIGNATED FOR FLIGHT, SHALL BE EITHER IN THE RIGHT OR LEFT SEAT FOR ALL TAKEOFFS AND LANDINGS

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4
Q

COREX CREW

A

SAME AS OPERATIONAL, INDIVIDUAL TACT CELL POSTIONS MAY BE VACANT AT DISCRETION OF SQUADRON CO WHILE MAINTAINING MIN CREW.

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5
Q

B CAT FE

A

MAY REPLACE A CAT ON PPF THAT ORIGINATES AND TERMINATES AT WING/BASE W/ CP-140 MAINT SERVICES ARE AVAILABLE W/ NO PLANNED ENGINE SHUTDOWNS,

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6
Q

EMERGENCIES AC

A

IF TIME PERMITS, AC SHALL OCCUPY LEFT SEAT WHILE EMERGENCY CONDITON EXISTS. AC SHALL PERFORM LANDING UNLESS CIRCUMSTANCES DICTATE OTHERWISE. IN ACTUAL EMERGENCIES, THIRD PILOT OR SECONDARY FE SHALL NOT BE ALLOWED ON FLIGHT DECK

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7
Q

MAX/MIN CREW AND PAX

A
  1. OPERATIONAL REQUIREMENTS ABD AVAILABILITY OF CRASH POSITIONS AND SAFETY/SURVIVAL EQUIPMENT WILL DICTATE NUMBER OF PERSONNEL CARRIED ON CP-140 FLIGHTS
  2. 1 CAD RESERVES RIGHT FOR LRPSET TO UTILIZE 2 SEATS FOR NO-NOTICE CHECKRIDES OR MONITORING DUTIES, AS REQ.
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8
Q

TAXI

A

MIN CREW FOR TAXI IS 2 QUALIFIED CP-140 PILOTS, QUALIFIED FE, AND ONE OTHER QUALIFIED CREW MEMBER. AT DISCRETION OF CO OR FAO, BOTH PILOTS MAY BE FOS IF WITH A CAT FE AND MIN PERSONNEL ON AIRCRAFT

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9
Q

MIN CREW FOR FLIGHT

A

AIRCRAFT COMMANDER, A CAT FE OR B CAT CERTIFIED IN ACCORDANCE WITH REFERENCE, AND ONE OTHER QUALIFIED CREW MEMEBER

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10
Q

FOURTH CREWMEMBER

A

PREVIOUSLY QUALIFIED MEMBERS CAN SIT FOURTH BEFORE REGAINING CATEGORY IF TRAINING, ALSE, WET AND DRY EGRESS ARE REGAINED. WIHTOUT A CATEGORY, MUST PERFORM FOURTH CREWMEMEBER EVERY 90 DAYS

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11
Q

THREE ENGINE FERRY TAKEOFF

A

CONSIDERED ABNORMAL PROCEDURE. APPROVAL FROM WCOMD REQ UNLESS AUTHORITY HAS BEEN DELEGATED TO SUBORDINATE.

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12
Q

IFR

A

PILOTS ARE ENCOURAGED TO CONDUCT, TO MAX EXTENT POSSIBLE, ALL ENROUTE FLIGHTS UNDER IFR

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13
Q

IFR OUTSIDE CANADIAN DOMESTIC AIRSPACE

A

FIXED WING FLIGHTS OUTSIDE CDA SHOULD BE UNDER IFR, UNLESS OPERATIONAL OR OPERATIONAL TRAINING REQUIREMENTS DICTATE VFR. FAO SHALL AUTHORIZE THESE VFR FLIGHTS

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14
Q

TAKEOFF WEIGHT

A

WEIGHT SHALL NOT EXCEED THAT WHICH WILL PERMIT THE AIRCRAFT, GIVEN CUREENT TEMP AND PRESSURE ALTITUDE, TO EXPERIENCE AN ENGINE FAILURE AT V1, TAKEOOF, AND MAINTAIN CLIMB GRADIENT THAT WILL ENSURE TERRAIN AND OBSTACLE CLEARANCE

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15
Q

FUEL REQUIREMENTS

A
  1. FUEL TO DESTINATION
  2. PLUS 5% OF PLANNED FUEL TO DESTINATION
  3. FUEL FOR INSTRUMENT APPROACH
  4. MIN DIVERSION FUEL W/ FUEL FOR FLIGHT FROM MDA/DH TO ALTERNATE AT REALISTIC ALTITUDE, FUEL FOR APPROACH AT ALTERNATE, FUEL FOR 30 MIN OF HOLDING (AT HOLDING CONSUMPTION RATE), UNUSABLE FUEL OR 5000 LBS FOR CP-140, AND ALLOWANCE SHALL BE MADE FOR FUEL USE FOR TAXI, RUN-UP, AND TAKEOFF ROLL
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16
Q

FUEL NOTE

A

FOR FLIGHTS STARTING AND ENDING IN CONTINENTAL US OR CANADIAN SOUTHERN AIRSPACE, 5% FUEL MAY BE WAIVED. DOES NOT APPLY TO EXTENDED OVERWATER FLIGHTS (MORE THAN 50NM)

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17
Q

THREE-ENGINE CLIMB

A

IN VMC IS 300FPM OR AS REQUIRED TO MAINTAIN OBSTACLE/TERRAIN CLEARANCE, WHICHEVER IS GREATER

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18
Q

TAKEOFF BELOW VMCA

A

DO NOT DO IT UNLESS 1 CAD APPROVES IT

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19
Q

ETP

A

EXPERIENCING A CRITICAL EMERGENCY OR 2 ENGINE SHALL NOT OVERFLY ETP. IF THREE ENGINE, SERIOUSLY CONSIDER GOING TO ETP AIRPORT

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20
Q

OVERFLYING ETP AERODROME ON 3 ENGINE

A

SHALL NOT BE DONE UNLESS:

  1. FLIGHT TO SUITABLE AERODROME CAN BE CONTINUED WITH SUFFICENT OXYGEN AND IFR FUEL RESERVES AND
  2. FLIGHT AT AN ALTITUDE MEETING ALL MINIMUM REQUIREMENTS AND OBSTACLE CLEARANCECAN BE MAINTAINED SHOULD ANOTHER ENGINE FAIL
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21
Q

SAR

A

INTERCEPTION AND ESCORT SHALL BE REQUESTED WHEN ON 2 ENGINES

22
Q

OVERWATER WEATHER LIMITS

A

CEILING 100 FEET OVER WHAT IS NEEDED FOR MANUEVERS. VISIBILIITY OF 2 NM.

23
Q

TRAFFIC PATTERN

A

IF ATC SAYS YES, 1000FT PATTERN IN SPEC VFR WITH 1000ST CEILINGS AND 2 MILES VIS OR GREATER AND CLEAR OF CLOUD AND IN SIGHT OF DND CONTROLLED AERODROME

24
Q

NON-OP X-COUNTRY

A

1 CAD APPROVAL NEEDED

( DELEGATED TO RACE A OR RACE P) REQUIRED FOR ALL CP-140 FLIGHTS GREATER THAN 850 NM FORM HOME OR SCHEDULED TO RON

25
DUCKBUTT
2.4.6.9 DUSCKBUTT AIRCRAFT ARRIVE ON SCENE WITHIN 1HR 30MIN OF EMERGENCY CALL
26
FUEL MANAGEMENT
LOITER SHUTDOWN SHOULD BE CONSIDERED TO SAVE FUEL. SHALL NOT BE FLOWN BELOW 1000FT AGL WITH 2 ENGINES LOITERED
27
DOUBLE ENGINE FAILURE
AC SHALL LAND AT NEAREST SUITABLE AERODROME
28
SINGLE ENGINE FAILURE OVERWATER
ON OVERWATER, AC SHALL PROCEED TO NEAREST SUITABLE AERODROME (2.4.5.5.2)
29
SINGLE ENGINE FAILURE OVER LAND
AC MAY PROCEED TO NEAREST WING/BASE, WHICH HAS CP-140 SERVICING, PROVIDED: 1. REQ FUEL RESERVES ARE AVAILABLE 2. AIRCRAFT WEIGHT PERMITS MIM EN ROUTE ALITUDE TO BE MAINTAINED IF SECOND FAILURE OCCURS 3. WEATHER AT SUITABLE EN ROUTE AIRPORTS AND AT DESTINATION IS AT ALTERNATE LIMITS OR ABOVE
30
SKAD
CARRIED ON ALL ATO SORTIES AND OVERWATER MISSIONS EXCEPT: 1.WHEN CARRYING BOMB BAY ARMAMENT 2. WHEN CONDUCTING SUB EXERCISES 3. CONDUCTING COREX WITH COCKED SHACKLES 4. A BACK UP AIRCRAFT IS BEING UTILIZED ABD INSTALLATION OF SKAD WOULD DELAY TAKEOFF (BOMB BAY DOORS SHALL NOT BE OPENED UNLESS DEPLOYING SKAD
31
DANGEROUS GOODS
GROUP A: (NO PANNIER) AIRCRAFT EQUIPMENT-CADS, SUS, TORPEDOES, FLARES AND TRANSPORTED AS ORDNANCE AND ARE NOT CONSIDERED DANGEROUS GOODS GROUP B: (NO PANNIER) CARRIED TO SUPPORT DEPLOYED OPS OR FOR A MRP (AEROSOLS, WET BATTERIES, AND AIRCRAFT PARTS). STANDING AUTHORITY GRANTED TO TRASPORT IF PACKAGED PROPERLY GROUP C: ITEMS THAT MAY OCCASIONALLY BE REQUESTED TO BE CARIED (FIREARMS, FUEL TANKS, ENGINES) REQUIRE AIRLIFT AUTHORIZATION FORM FROM 1 CAD
32
LIVE ORDNANCE
with live ordnance, avoid overflight of built up areas. no training and civilian airports or terminal area except those with authorized areas. AT MILITARY TERMINAL AREAS AND AIRPORTS ALL LANDINGS MUST BE FULL STOP AND WEAPONS MUST BE DOWNLOADED BEFORE CONDUCTING FURTHER TRAINING.
33
SAFE TRAINING PRACTICES
APPENDIX 3.1.1.15.A.1
34
TOUCH AND GO SAFE TRAINING PRACTICE
1. 70% XWIND COMPONENT OF MAX ALLOWABLE FOR RUNWAY CONDITIONS 2. MIN RUNWAY REQ TO ABORT DURING THE GO SHALL BE 3500 FT BARE AND DRY AND 4500 FT FOR OTHER THAN BARE AND DRY
35
RIGHT SEAT TOUCH AND GO STP
1. 70% MAX ALLOWABLE XWIND FOR RUNWAY CONDTIONS 2. MIN RUNWAY FOR ABORT ON GO IS 3500FT BARE AND DRY AND 4500 FT FOR OTHER 3. AIRCRAFT CAPTAIN MUST BE LRPC
36
RIGHT SEAT TAKEOFF AND RIGHT SEAT LANDING STP
1. 70%MAX ALLOWABLE XWIND FOR RUNWAY CONDITIONS. 2. AC MUST BE A LRPC OR A. SEQUENCE IS FLOWN BY AC WHO IS AN AC B. FOUR ENGINE SYMMTRIC REVERSE IS USED ON LANDING C. 50% MAX ALLOWABLE XWIND COMPONENT FOR RUNWAY CONDITIONS
37
SHORT FIELD STP
1. 50% XWIND COMPONENT OF MAX ALLOWABLE FOR RUNWAY CONDITIONS 2. MAX A/C WEIGHT 90000LBS 3. DAY VMC ONLY 4. REVERSE ONLY, NO MAX BRAKING 5. LRPC FROM LEFT SEAT ONLY 6. AC AND FO MUST TRAIN WITH SUPERVISOR 7. SUPES ALLOWED TO CONDUCT SEQUENCE FROM RIGHT SEAT
38
SYMMETRIC ABORT STP
1. SHALL NOT BE INITIATED BY RETARDING A POWER LEVER 2. 70% MAX XWIND COMPONENT FOR RUNWAY CONDITIONS 3. AC MUST BE LRPC
39
ASYMMETRIC ABORT STP
1. SHALL NOT BE INITIATED BY RETARDING THE POWER LEVER 2. PILOT SHALL REVERSE WITH ALL FOUR UNTIL BETA LIGHTS ILLUMINATE AND TRAINING PILOT CALL ENGINE. PILOT SHALL THEN COMPLETE LANDING ROLL USING REMAINING ENGINES 3. SEQ SHALL ONLY BE CONDUCTED WITH STANDARDS AND TRAINING PILOT OR IP AS AIRCRAFT CAPTAIN
40
THREE ENGINE OVERSHOOT STP
1. FLOWN AS A HANDLING EXERCISE 2. NOT TO BE CONDUCTED AS PART OF EMERGENCY 3. ENGINE SHALL NOT BE SHUT DOWN 4. ENGINE SHALL BE SET TO 0 SHP 5. MIN ALTITUDE 100FT AGL 6. 70% XWIND 7. SEQ SHALL ONLY BE CONDUCTED WITH LRPC as AC
41
THREE ENGINE APPROACH AND LANDING STP
1. FLOWN AS A HANDLING EXERCISE 2. NOT TO BE CONDUCTED AS PART OF AN AIRBONE EMERGENCY SIMULATION 3. ENGINE SHALL NOT BE SHUT DOWN 4. ENGINE SHALL BE 0 SHP 5. PILOT SHALL REVERSE WITH ALL FOUR UNTIL BETAS, AND TRAINING PILOT WILL CALL ENGINE AND PILOT REVERSES WITH REMAINING ENGINES 6. 70% XWIND COMPONENT 7. SEQ SHALL ONLY BE CONDUCTED WITH STANDARDS AND TRAINING PILOT OR IP AS AC
42
ZERO FLAP
FFS ONLY FOR LANDING.
43
FOUO
ALL STEPS BEYOND #1 IN CHECK SHALL BE SIMULATED ONLY IN-FLIGHT, NO CBS PULLED, NO SWITCHES MOVED
44
QUARTERLY CURRENCY REQUIREMENTS
ABORTED TAKEOFF, 3 ENG APPROACH, OVERSHOOT, LANDING, RIGHT SEAT LANDING, PRECISION AND NON-PRECISION APPROACH, MEDIUM AND STEEP TURNS BELOW 1000FT, AND ABNORMAL AND EMERGENCY TRAINING
45
SEMI ANNUAL REQUIREMENTS
ZERO FLAP LANDING, TWO ENGINE APPROACH, OVER SHOOT AND LANDING, PRACTICE EMERGENCIES IN SIMULATOR, NIGHT LANDING
46
ANNUAL REQUIREMENTS
IRT AND APC. 120 HOURS FLYING, 48 HOURS IN SIM
47
SIMULATOR FATIGUE AND CREW REST
MAX 4 HOURS
48
LIFE JACKETS
SUFFICIENT LIFE JACKETS SHALL BE AVAILABLE FOR EACH AIRCRAFT OCCUPANT DURING OVERWATER FLIGHTS AND WHEN DIRECTED BY AC
49
OVERWATER OPS
DAY-100, 200 M IMC/NIGHT RADALT-300 IMC/NIGHT NO RADALT WITH BARO-500 IMC/NIGHT NO RADALT/NO BARO-1000
50
SILLY ENGINE SHUTDOWN REQUIREMENT
2000 FT AGL. FOUND IN SECTION 3.1.1.5

Aurora (5 decks)

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