Airworthiness requirements Flashcards

1
Q

What documents are required on board an aircraft prior to flight? CFR 91. 203, 91.9

A
Airworthiness certificate, 
registration certificate, 
radio station license, 
operating limitations – AFM/POH and supplements, placard’s, markings, weight and balance data – current, compass deviation card, 
external data plate/serial number
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2
Q

What is an airworthiness certificate?

A

An airworthiness certificate is issued by the FAA to all aircraft that have been proven to meet the minimum requirements of 14 CFR part 21 and that are in condition for safe operation. Under any circumstances, the aircraft must meet the requirements of the original type certificate or it is no longer airworthy. Airworthiness certificates come in two different classifications: standard airworthiness and special airworthiness.

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3
Q

If the airworthiness certificate of a particular aircraft is indicated as one of the following categories, what significance would this have? 14 CFR part 23

normal category
utility category

A

a) Normal category- aircraft structure capable of withstanding a load factor of 3.8 Gs without structural failure. Applicable to aircraft intended for non-aerobatic operation.
b) Utility category – aircraft structure must be capable of withstanding a load factor of 4.4 Gs. This would usually permit limited aerobatics, including spins if approved for the aircraft.

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4
Q

What are special airworthiness information bulletins? Are they regulatory?

A

A special airworthiness information bulletin SAIB is an information tool that alerts, educates, and makes recommendations to the aviation community. SAIBs contain non-regulatory information and guidance that does not meet the criteria for an airworthiness directive (AD). Guidance on when to use an SAIB and how to develop an issue an SAIB is provided in FAA order 8110.100.

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5
Q

What is a type certificate data sheet?

A

The type certificate data sheet (TCDS) lists the specifications, conditions and limitations under which airworthiness requirements are met with a specified product, such as engine make and model, fuel type, engine limits, airspeed limits, maximum weight, minimum crew, etc.

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6
Q

What is a supplemental type certificate?

A

A supplemental type certificate (STC) is the FAA‘s approval of a major change in the type design and a previously approved type certificated product. The certificate authorizes an alteration to an air frame, engine, or component that has been granted an approved type certificate. Sometimes alterations are made that are not specified or authorized in the TCDS. When that condition exist, an STC will be issued. STC’s are considered a part of the permanent records of an aircraft and should be maintained as part of the aircraft’s logs.

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7
Q

Where can you find information on the placards and marking information required to be in the airplane?

A

The principal source of information for identifying the required airplane flight manuals, approved manual materials, markings, and placards is the FAA type certificate data sheet or aircraft specification issued for each airplane eligible for an airworthiness certificate. The required placards are also reproduced in the limitations section of the AFM or as directed by an airworthiness directive (AD).

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8
Q

What are the required test and inspections to be performed on an aircraft? Include inspections for IFR.

A

A - Airworthiness directives and life limited parts complied with as required 14 CFR 91.403, 91.417

V - VOR Equipment check every 30 days for IFR operations 14 CFR 91.171

I - Inspections - annual inspection within the precededing 12 calendar months 14 CFR 91. 409; 100- hour Inspection, if used for hire or flight instruction in aircraft CFI provides 14 CFR 91. 409

A - Altimeter, altitude recording equipment, and static pressure systems tested and inspected for IFR operations every 24 calendar month 14 CFR 91.411

T - Transponder test and inspections, every 24 calendar months 14 CFR 91. 413

E - Emergency locator transmitter, operation and battery condition inspected every 12 calendar months 14 CFR 91. 207

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9
Q

If the annual inspection date has passed, can an aircraft be operated to a location where the inspection can be performed?

A

An aircraft overdue for an annual inspection may be operated under a special flight permit issued by the FAA for purpose of flying the aircraft a location for the annual inspection to be performed. However, all applicable ADs that are due must be complied with before the flight.

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10
Q

What are special flight permits, and when are they necessary? 14 CFR 91.213, 14 CFR 21.197

A

A special flight permit may be issued for an aircraft that may not currently meet applicable airworthiness requirements but is capable of safe flight. These permits are typically issued for the following purposes:

a) Flying an aircraft to a base where repairs, alterations or maintenance are to be performed, or to a point of storage.
b) Delivering or exporting an aircraft.
c) Production flight testing new production aircraft.
d) Evacuating aircraft from areas of impending danger.
e) Conducting customer demonstration flights in a new production aircraft that have satisfactorily completed production flight tests.

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11
Q

How are special flight permits obtained ?

A

If a special flight permit is needed, assistance and the necessary forms may be obtained from the local FSDO or designated airworthiness representative (DAR).

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12
Q

After aircraft inspections have been made and defects have been repaired, who is responsible for determining that the aircraft is in an airworthy condition? 14 CFR 91.7

A

The pilot in command of a civil aircraft is responsible for determining whether that aircraft is in a condition safe for flight. The pilot in command shall discontinue the flight when unairworthy, mechanical, electrical, or structural conditions occur.

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13
Q

Can a pilot legally conduct flight operations with known inoperative equipment on board? 14 CFR 91. 213, AC 91–67

A

Yes, under specific conditions. 14 CFR part 91 describes acceptable methods for the operation of an aircraft for certain inoperative instruments and equipment that are not essential for safe flight. These acceptable methods are:

a) Operation of an aircraft with a minimum equipment list MEL, as authorized by 14 CFR 91. 213(a) or
b) Operation of an aircraft without a MEL under 14 CFR 91. 213(d)

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14
Q

During the preflight inspection in an aircraft that doesn’t have an MEL, you notice that an instrument or equipment item is inoperative. Describe how you would will determine if the aircraft is still airworthy for flight. 14 CFR 91.213(d), AC 91–67

A

I will ask myself the following questions to determine if I can legally fly the airplane with the inoperative equipment item:

a) Are they in operative instruments or equipment part of the VSR – day type certification?
b) Are the inoperative instruments or equipment listed as required on the aircraft equipment list or kinds of operation equipment list (KOEL) for the kind of flight operation being conducted?
c) Are the inoperative instruments or equipment required by 14 CFR 91.205, 91.207, or any other rule of 14 CFR part 91 for the specific kind of flight operation being conducted (e.g. VFR, IFR, day, night)?
d) Are the an operative instruments or equipment required to be operational by air worthiness directive AD?

If the answer is “yes” to any of these questions, the aircraft is not airworthy and maintenance is required before I can fly. If the answer is “no” to all of these questions, then the operative instruments or equipment must be removed by A&P from the aircraft or be deactivated and placarded “inoperative.”

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15
Q

What is a kind of operations equipment list KOEL?

A

A Kinds of Operation Equipment list (KOEL) identifies the systems and equipment upon which type certification for each kind of operation was predicated (I.e., day or night VFR, day or night IFR, icing conditions) and which must be installed and operable for the particular kind of operation indicated. The KOEL is located in the limitation section of the FAA approved airplane flight manual.

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16
Q

What are the minimum equipment lists? AC 91–67

A

The minimum equipment list MEL is a precise listing of instruments, equipment and procedures that allows an aircraft to be operated under specific conditions with inoperative equipment. The MEL is the specific inoperative equipment document for a particular make and model aircraft by serial and registration numbers. The FAA approved MEL includes only those items of equipment that the FAA deems may be inoperative and still maintain an acceptable level of safety with appropriate conditions and limitations.

17
Q

What instruments and equipment are required for VFR day flight? 14 CFR 91.205

A

A- Anti-collision light system – aviation red or white for small airplanes certificated after March 11, 1996

T- Tachometer for each engine

O- Oil pressure gauge for each engine

M- Manifold pressure gauge (for each altitude engine i.e. turbo charged)

A- Altimeter

T- Temperature gauge for each liquid cooled engine

O- Oil temperature gauge for each air cooled engine

F- Fuel gauge indicating the quantity in each tank

L- Landing gear position indicator, if the airplane has retractable gear

A- Airspeed indicator

M- Magnetic direction indicator

E- Emergency locator transmitter if required by 14 CFR 91.207

S- Safety belts and shoulder harnesses for each front seat in aircraft manufactured after 1978

18
Q

What instruments and equipment are required for VFR night flight? 14 CFR 91.205

A

F- Fuses – one spare set or three fuses of each kind required accessible to the pilot in flight

L- Landing light – if the aircraft is operated for hire

A- Anticollision light system-approved aviation red or white (strobes and beacon)

P- Position lights – (navigation lights- green, red & white)

S- Source of electrical energy – adequate for all installed electrical and radio equipment

19
Q

Aircraft maintenance records must include what information? 14 CFR 91.417

A

Records of the maintenance, preventative maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approve inspections, as appropriate, for each aircraft including the air frame and each engine, propeller, rotor, and appliance of an aircraft. The records must include:

1) a description or reference to that acceptable to the administrator of the work performed; and
2) the date of completion of the work performed; and
3) the signature certificate of the person approving the aircraft for return to service.

20
Q

Define preventative maintenance. 14 CFR 43.3

A

c) Preventive maintenance. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations:

(1) Removal, installation, and repair of landing gear tires.
(2) Replacing elastic shock absorber cords on landing gear.
(3) Servicing landing gear shock struts by adding oil, air, or both.
(4) Servicing landing gear wheel bearings, such as cleaning and greasing.
(5) Replacing defective safety wiring or cotter keys.
(6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings.

7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers’ instructions) not requiring load tape repair or replacement.
(8) Replenishing hydraulic fluid in the hydraulic reservoir.
(9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required.
(10) Applying preservative or protective material to components where no disassembly of any
primary structure or operating system is involved and where such coating is not prohibited or is
not contrary to good practices.
(11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft.
(12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow.
(13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc.
(14) Replacing safety belts.
(15) Replacing seats or seat parts with replacement parts approved for the aircraft, not involving disassembly of any primary structure or operating system.
(16) Trouble shooting and repairing broken circuits in landing light wiring circuits.
(17) Replacing bulbs, reflectors, and lenses of position and landing lights.
(18) Replacing wheels and skis where no weight and balance computation is involved.
(19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls.
(20) Replacing or cleaning spark plugs and setting of spark plug gap clearance.
(21) Replacing any hose connection except hydraulic connections.
(22) Replacing prefabricated fuel lines.
(23) Cleaning or replacing fuel and oil strainers or filter elements.
(24) Replacing and servicing batteries.
(25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer’s instructions.
(26) Replacement or adjustment of nonstructural standard fasteners incidental to operations.

21
Q

Who can update the navigation database of installed avionics in an airplane? 14 CFR 43.3

A

Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided:

(1) The database upload is:
(i) Initiated from the flight deck;
(ii) Performed without disassembling the avionics unit; and
(iii) Performed without the use of tools and/or special equipment