Maintenance Forms and Records Flashcards
- Where is the record of compliance with Airworthiness Directives or manufacturers’ service bulletins normally indicated?
A— FAA Form 337.
B— Aircraft maintenance records.
C— Flight manual.
B— Aircraft maintenance records.
The aircraft maintenance records (generally in the form of logbooks) are the correct place to record compliance with FAA Airworthiness Directives or manufacturer’s service bulletins.
- If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes
A— approval of the aircraft for return to service.
B— approval for return to service only for the work performed.
C— verification that the maintenance or alterations were performed referencing approved maintenance data.
B— approval for return to service only for the work performed.
The signature constitutes the approval for return to service only for the work performed.
- During an annual inspection, if a defect is found which makes the aircraft unairworthy, the person disapproving must
A— void the aircraft’s Airworthiness Certificate.
B— submit a Malfunction or Defect Report.
C— provide a written notice of the defect to the owner.
C— provide a written notice of the defect to the owner.
If, during an annual inspection, a defect is found which makes the aircraft unairworthy, the person disapproving the aircraft must give the owner a signed and dated written list of the discrepancies that caused the unairworthy condition.
- What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated?
A— Airworthiness Directives.
B— Aviation Maintenance Alerts.
C— Aviation Safety Data.
A— Airworthiness Directives.
If a condition is found that causes a particular design of aircraft to fail to meet its certification for airworthiness, the FAA can issue an AD.
An AD describes the conditions that must be met to allow the aircraft to continue to be operated.
- Which is an appliance major repair?
A— Overhaul of a hydraulic pressure pump.
B— Repairs to a propeller governor or its control.
C— Troubleshooting and repairing broken circuits in landing light circuits.
A— Overhaul of a hydraulic pressure pump.
Overhaul of pressure-type carburetors and pressure-type fuel, oil, and hydraulic pumps are examples of appliance major repairs.
- Where should you find this entry?
“Removed right wing from aircraft and removed skin from outer 6 feet. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer’s structural repair manual No. 28-1.”
A— Aircraft engine maintenance record.
B— Aircraft minor repair and alteration record.
C— FAA Form 337.
C— FAA Form 337.
The description of the repair, as is shown here, would be made on FAA Form 337 (Major Repair and Alteration Form).
This form must be completed when an airframe, engine, propeller, or appliance has been subjected to a major repair or major alteration.
- Which maintenance action is an airframe major repair? A— Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics.
B— Rewinding the field coil of an electrical accessory.
C— The repair of portions of skin sheets by making additional seams.
C— The repair of portions of skin sheets by making additional seams.
According to the list of major alterations, major repairs and preventive maintenance listed in 14 CFR Part 43, Appendix A, the repair of portions of skin sheets by making additional seams is considered to be an airframe major repair.
Neither of the other alternatives listed here is an airframe major repair.
- Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting?
A— Eight 1/4—20 inch standard heli-coils were replaced. The damaged inserts were extracted, the tapped holes gaged, then new inserts installed, and tangs removed.
B— Eight 1/4—20 inch standard heli-coils were installed in place of damaged ones.
C— Eight 1/4—20 inch standard heli-coil inserts were repaired by replacing the damaged inserts with a lock-type insert, after the tapped holes were checked for corrosion.
A— Eight 1/4—20 inch standard heli-coils were replaced. The damaged inserts were extracted, the tapped holes gaged, then new inserts installed, and tangs removed.
Heli-coils are patented, precision-formed screw-thread coils of 18-8 stainless steel wire having a diamond-shaped cross section.
Heli-coil inserts are replaced by extracting the damaged insert with a special extracting tool, gaging the holes with a Heli-coil thread gage, installing the new insert using the proper inserting tool and finally, breaking off the tang with the proper break-off tool.
- Which maintenance record entry best describes the action taken for a control cable showing approximately 20 percent wear on several of the individual outer wires at a fairlead?
A— Wear within acceptable limits, repair not necessary.
B— Removed and replaced the control cable and rerigged the system.
C— Cable repositioned, worn area moved away from fairlead.
A— Wear within acceptable limits, repair not necessary.
Flexible and extra-flexible control cable should be replaced when the individual wires in each strand appear to blend together (outer wires worn 40 to 50 percent).
Since these wires are only worn 20 percent, the wear is within acceptable limits and repair is not necessary.
- Which maintenance record entry best describes the action taken for a .125-inch deep dent in a straight section of 1/2-inch aluminum alloy tubing?
A— Dented section removed and replaced with identical new tubing flared to 45°.
B— Dent within acceptable limits, repair not necessary. C— Dented section removed and replaced with identical new tubing flared to 37°.
C— Dented section removed and replaced with identical new tubing flared to 37°
The dent is in a straight portion of the tube and is deep enough to warrant its removal. A dent of up to 0.1 inch (20 percent of the tube diameter) deep would be acceptable and would not have to be removed.
The dented section would have to be removed and replaced with identical new tubing flared to 37°.
8452-1.
Which statement is true regarding the requirements for maintenance record format?
A— Any format that provides record continuity and includes the required information may be used.
B— The format provided by the manufacturer of the aircraft must be retained.
C— Any desired change from manufacturer provided format requires approval from the Federal Aviation Administration.
A— Any format that provides record continuity and includes the required information may be used.
AC 43-9 paragraph 5.b. states that maintenance records may be kept in any format that provides record continuity, includes required contents, lends itself to the addition of new entries, provides for signature entry, and is intelligible.
8452-2.
When a 100-hour inspection is completed, if separate maintenance records for the airframe, powerplant(s), and propeller(s) are maintained, where is the entry for the inspection recorded?
A— In each record.
B— In the airframe record only.
C— In any one of the records.
A— In each record.
AC 43-9 paragraph 10.d. states that if the owner maintains separate records for the airframe, powerplants, and propellers, the entry for the 100-hour inspection is entered in each, while the annual inspection is only required to be entered into the airframe record.
8452-3.
For aircraft operated under Part 91, when is aircraft total time required to be recorded in aircraft maintenance records?
A— After satisfactorily completing maintenance, preventive maintenance, rebuilding, and alteration (excluding inspections).
B— After satisfactorily completing inspections.
C— After satisfactorily completing airframe, component, or propeller maintenance.
B— Records of maintenance, alterations, preventive maintenance, 100-hour, annual, and progressive inspections.
14 CFR §43.11 states that the person approving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with Part 91…shall make an entry in the maintenance record of that equipment containing the following information…(2) The date of the inspection and aircraft total time in service.
8452-4.
For aircraft operated under Part 91, what difference is there, if any, between the record entry requirements for maintenance (e.g., repair or alteration) and the record entry requirements for inspections (beyond the description of the work performed and the type and extent of inspection)?
A— There is no difference.
B— Aircraft total time is required to be included only in the maintenance entry.
C— Aircraft total time is required to be included only in the inspection entry.
C— Aircraft total time is required to be included only in the inspection entry.
14 CFR §43.11 states that the person approving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with Part 91…shall make an entry in the maintenance record of that equipment containing the following information…(2) The date of the inspection and aircraft total time in service.
Records specified in 14 CFR §43.9 do not require the recording of the aircraft total time.
8452-5.
If more space is needed for a work description entered on FAA Form 337, what information should be included on the attached sheet(s), in addition to the rest of the work description?
A— Make, model, and serial number of the aircraft.
B— Aircraft nationality and registration mark, and the date the work was accomplished.
C— Name, date, and office designator of the FAA inspector from the supervising office.
B— Aircraft nationality and registration mark, and the date the work was accomplished.
AC 43.9-1F paragraph 6.h.(3) states that if additional space is needed to describe the repair or alteration, attach sheets bearing the aircraft nationality and registration mark and the date the work was completed.