GOM Flashcards
PIC actions. Accident
Preserve Life: Assist EVAC, 911 etc.
Provide security for PAX
Preserve property: declare emergency, CFR etc.
Provide security for A/C and Property
PIC notify D.O. ASAP D.O. will notify closet ATC
The D.O.M. must actually weigh Multi Engine A/C and calculate C.G. Every____months
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Use actual PAX wts.
Ask Pax and add 10lbs. If in doubt the pilot will use the scale and actually weigh the passenger.
PIC complete load manifest
In duplicate for each leg containing passengers.
Original left at base, retain 30 day.
Copy carried on board until completion of flight.
D.O.
Albert Buccieri
Chief Pilot
Dave Roach
D.O.M.
Jim Frye
Aircraft Maintenance and Flight Record
“N” Number.
Current A/C status: “Do Not Fly Past” Date and Hobbs.
Date & Hobbs of next sched. Insp. and/or maint will be due.
When picking up A/C returned to service
PIC to receive complete brief with a summery of work preformed.
Preform complete and thorough preflight with maintenance personnel
Return to service flight is required when work has been done on the following systems:
Flight Controls.
Landing Gear other than tires and and brakes.
Phase Inspections.
Nav. Systems.
Any other items deemed necessary by DOM.
Aircraft maintenance and flight record
When a mechanical discrepancy or irregularity is found, employee finding the problem will record the discrepancy or irregularity in the aircraft maintenance and flight record. Immediately notify the DOM.
FAR 135.415 requires “service difficulty report” for any of the following items. See GOM chapter 6. Notify FAA administrator.
§135.415 Service difficulty reports.
(a) Each certificate holder shall report the occurrence or detection of each failure, malfunction, or defect in an aircraft concerning—
(1) Fires during flight and whether the related fire-warning system functioned properly;
(2) Fires during flight not protected by related fire-warning system;
(3) False fire-warning during flight;
(4) An exhaust system that causes damage during flight to the engine, adjacent structure, equipment, or components;
(5) An aircraft component that causes accumulation or circulation of smoke, vapor, or toxic or noxious fumes in the crew compartment or passenger cabin during flight;
(6) Engine shutdown during flight because of flameout;
(7) Engine shutdown during flight when external damage to the engine or aircraft structure occurs;
(8) Engine shutdown during flight due to foreign object ingestion or icing;
(9) Shutdown of more than one engine during flight;
(10) A propeller feathering system or ability of the system to control overspeed during flight;
(11) A fuel system that affects fuel flow or causes hazardous leakage during flight;
(12) An unwanted landing gear extension or retraction or opening or closing of landing gear doors during flight;
(13) Brake system components that result in loss of brake actuating force when the aircraft is in motion on the ground;
(14) Aircraft structure that requires major repair;
(15) Cracks, permanent deformation, or corrosion of aircraft structures, if more than the maximum acceptable to the manufacturer or the FAA; and
(16) Aircraft components or systems that result in taking emergency actions during flight (except action to shut-down an engine).
The PIC of the aircraft is directly responsible for determining that the aircraft is in an air worthy condition and ready for flight.
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Prior to flight, the PIC will refer to the aircraft maintenance and flight record and verify the following:
The flight will not exceed the “Do Not Fly Past “ Date and/or Hobbs time.
Any previous discrepancies have been repaired or deferred in accordance with the MEL.
Documents required on board for flight
Airworthiness certificate.
Registration certificate.
MEL
AFM.
GOM\ops specs.
Required Aircraft checklist per FAR 135.83
Pax briefing cards.
Aircraft maintenance and flight records.
Completed load manifest.
Pertinent aeronautical charts per FAR 135.83
