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Archive / Plane Sense — General Aviation Information / Plane Sense — General Aviation Information: Chapter 8

Chapter 8

Chapter 8 — Part 1

FAA-H-8083-19A (2008)

Plane Sense

Chapter 8: Aircraft Maintenance Records

Plane Sense

Chapter 8: Aircraft Maintenance Records

These records may be discarded when the work is

repeated or superseded by other work, or 1 year after

the work is performed.

m CAUTION: Keep in mind that as a result of

repairs or alterations, such as replacing radios and

installing speed kits, it may be necessary to amend

the weight and balance report, equipment list,

flight manual, etc.

logbooks

Most maintenance performed on an aircraft is recor-

ded in the aircraft logbooks. As an aircraft owner, it

is important to ensure that your aircraft’s logbooks

are complete and up to date at all times. The aircraft

logbooks outline the maintenance history of your air-

craft, and any prospective buyer will want to review

the aircraft and all maintenance performed. In addi-

tion, any A&P or certificated repair station performing

maintenance on your aircraft will want to review the

prior maintenance performed on the aircraft.

Airworthiness directives

An aircraft owner is required to comply with all

applicable ADs issued by the FAA for his or her

aircraft. The FAA issues ADs to notify aircraft owners

and other interested persons of unsafe conditions

and to specify the corrective action required,

including conditions under which the aircraft may

continue to be operated.

The aircraft’s maintenance records should indicate

the current status of all applicable ADs, including for

each:

• AD number,

• Method of compliance,

• Revision date, and

• Recurring action (if applicable) including the time

and date of the next action required.

safety directives

The owner or operator of an aircraft having a

special airworthiness certificate must comply with

each safety directive applicable to the aircraft that

corrects an existing unsafe condition or corrects

the condition in a manner different from safety

directive specifications if the person issuing the

directive agrees with the action. Otherwise, the

owner or operator may, in accordance with 14 CFR

part 91, section 91.327, “obtain an FAA waiver from

the provisions of the safety directive based on a

conclusion that the safety directive was

issued without adhering to the applicable consensus

standard.”

Light-sport category aircraft certificated pursuant

to 14 CFR part 21, section 21.190 have mandatory

compliance with all manufacturer safety directives.

service Bulletins

A service bulletin contains a recommendation from

the manufacturer, with which that manufacturer

believes the aircraft owner should comply, that often

reflects a safety-of-flight issue that the manufacturer

believes should be addressed within a certain time-

frame. It may result from an improvement developed

by the manufacturer, or it may address a defect in

a product or published documentation.

The manufacturer responds to one of these situa-

tions by issuing a service bulletin that recommends

a certain type of inspection, replacing certain

components, performing maintenance in a specific

manner, or limiting operations under specified

conditions. Sometimes, compliance with a service

bulletin may be triggered by the occurrence of

a particular event (e.g., the lapse of time or operation

under certain types of conditions).

FAA Form 337,

major repair and Alteration

A mechanic who performs a major repair or major

alteration shall record the work on FAA Form 337

and have the work inspected and approved by a

mechanic who holds an inspection authorization (IA).

(Light-sport aircraft do not require Form 337 when

altering a non-approved product.) A signed copy

shall be given to the owner and another copy sent

to the FAA Aircraft Registration Branch (AFS-750)

in Oklahoma City, Oklahoma within 48 hours of

aircraft approval for return to service. However,

when a major repair is done by a certificated repair

station, the customer’s work order may be used

and a release given as outlined in 14 CFR Part 43,

Appendix B, Recording of Major Repairs and Major

Alterations. You can obtain additional information

and instructions for completing FAA Form 337 in

Advisory Circular (AC) 43-9 (as revised), Aircraft

Maintenance Records. Figure 8-2 at the end of this

chapter is a sample FAA Form 337.

entries into Aircraft m aintenance records

Each time maintenance, including preventive main-

tenance, is performed on your aircraft, an appropriate

entry must be added to the maintenance records.

Plane Sense

Chapter 8: Aircraft Maintenance RecordsPlane Sense

Chapter 8: Aircraft Maintenance Records

14 CFR Part 43, Section 43.9,

Content, form, and disposition of

maintenance, preventive maintenance,

rebuilding, and alteration records (except

inspections performed in accordance

with part 91, part 125, §135.411(a)(1), and

§135.419 of this chapter

Any person who maintains, rebuilds or alters an

aircraft, airframe, aircraft engine, propeller, or

appliance shall make an entry containing:

• A description of the work or some reference

to data acceptable to the FAA,

• The date the work was completed,

• The name of the person who performed the

work, and

• If the work was approved for return to service,

the signature, certificate number, and kind of

certificate held by the person approving the

aircraft for return to service.

14 CFR Part 43, Section 43.11,

Content, form, and disposition of records for

inspections conducted under parts 91 and

125 and §§135.411(a)(1) and 135.419 of this

chapter

When a mechanic approves or disapproves an air-

craft for return to service after an annual, 100-hour,

or progressive inspection, an entry shall be made

including:

• Aircraft time in service,

• The type of inspection,

• The date of inspection,

• The signature, certificate number, and kind of

certificate held by the person approving or

disapproving the aircraft for return to service, and

• A signed and dated listing of discrepancies and

unairworthy items.

14 CFR Part 91, Section 91.409,

Inspections

Inspection entries for 14 CFR part 91, section

91.409(e) airplanes over 12,500 pounds, turbo jet,

or turbopropeller-powered multiengine airplanes

are made according to 14 CFR part 43, section 43.9,

and shall include:

• The kind of inspection performed,

• A statement by the mechanic that the inspection

was performed in accordance with the instruc-

tions and procedures for the kind of inspection

program selected by the owner, and

• A statement that a signed and dated list of any

defects found during the inspection was given to

the owner, if the aircraft is not approved for

return to service.

14 CFR Part 91, Section 91.411,

Altimeter system and altitude

reporting equipment tests and inspections

14 CFR part 91, section 91.411, requires that every

airplane or helicopter operated in controlled airspace

under instrument flight rules (IFR) conditions have

each static pressure system, each altimeter, and each

automatic pressure altitude reporting system tested

and inspected every 24 calendar months. The aircraft

maintenance records must include:

• A description of the work,

• The maximum altitude to which the altimeter

was tested, and

• The date and signature of the person approving

the aircraft for return to service.

14 CFR Part 91, Section 91.413,

ATC transponder tests and inspections

14 CFR part 91, section 91.413, requires that anyone

operating an Air Traffic Control (ATC) transponder

specified in 14 CFR part 91, section 91.215(a), have it

tested and inspected every 24 calendar months. The

aircraft maintenance records must include:

• A description of the work, and

• The date and signature of the person approving

the airplane for return to service.

14 CFR Part 91, Section 91.207,

Emergency locator transmitters

14 CFR part 91, section 91.207, requires that no

person may operate a U.S. registered civil airplane

unless there is attached to the airplane a personal

type or an automatic type emergency locator

transmitter (ELT) that is in operable condition

and meets applicable requirements of Technical

Standard Order (TSO)-C91.

m CAUTION: New ELT installations after June

21, 1995, must meet TSO-C91A (the first revised, or

amended, version).

Batteries used in ELT shall be replaced when:

• The transmitter has been in use for more than

1 cumulative hour, or

• 50 percent of the ELT’s useful life has expired.

Plane Sense

Chapter 8: Aircraft Maintenance Records

Plane Sense

Chapter 8: Aircraft Maintenance Records

The expiration date for replacing the battery shall be

legibly marked on the outside of the transmitter and

entered in the aircraft maintenance records.

Amateur-Built Aircraft

The condition inspection for amateur-built aircraft

replaces the annual inspection.

Available resources

Your local FSDO can help you establish your aircraft

maintenance program and the necessary maintenance

records. Additional information relating to aircraft

maintenance records can be obtained from:

• 14 CFR Part 39, Airworthiness Directives

• 14 CFR Part 43, Maintenance, Preventive

Maintenance, Rebuilding, and Alteration

• 14 CFR Part 91, General Operating and

Flight Rules

• AC 43-9 (as revised), Maintenance Records

These publications are available on the FAA website

at www.faa.gov and from U.S. Government Printing

Office (GPO) bookstores located throughout the

United States. For more information about obtaining

these publications, refer to the information contained

in chapter 11.

Plane Sense

Chapter 8: Aircraft Maintenance RecordsPlane Sense

Chapter 8: Aircraft Maintenance Records

maintenance records Checklist

stAtUs item notes

100-Hour inspection Keep records until the work is repeated or

superseded by other work, or 1 year after the work is

performed.

Annual inspection Keep records until the work is repeated or

superseded by other work, or 1 year after the work is

performed.

Progressive inspections Keep records until the work is repeated or

superseded by other work, or 1 year after the work is

performed.

Other required or approved inspections

(e.g., condition inspections/mandatory

tracking of safety directives for light-

sport aircraft)

Keep records until the work is repeated or

superseded by other work, or 1 year after the work is

performed.

Total Time in Service (airframe,

engine(s), propeller(s))

Records are retained by the owner and transferred

with the aircraft when it is sold.

Current status of life-limited parts

(airframe, engine(s), propeller(s), rotor,

and appliances)

Records are retained by the owner and transferred

with the aircraft when it is sold.

Time since last overhaul of all items

installed on the aircraft (required to be

overhauled on a specified time basis)

Records are retained by the owner and transferred

with the aircraft when it is sold.

Identification of current inspection

status of the aircraft (including time

since last inspection required by the

inspection program under which

aircraft and appliances are maintained)

Records are retained by the owner and transferred

with the aircraft when it is sold.

Current status of applicable ADs

(including method of compliance, the

AD number, and the revision date)

Records are retained by the owner and transferred

with the aircraft when it is sold.

Copy of current major alterations

(airframe, engine, propeller, and appli-

ances)

Records are retained by the owner and transferred

with the aircraft when it is sold.

Figure 8-1. Maintenance Records Checklist. This checklist includes the types of information that should

be kept with your aircraft’s maintenance records.

Plane Sense

Chapter 8: Aircraft Maintenance Records

Plane Sense

Chapter 8: Aircraft Maintenance Records

Figure 8-2. FAA Form 337, Major Repair and Alteration. You can obtain instructions for completing FAA

Form 337 on the FAA website at www.faa.gov or from your local FSDO.

Form Approved Electronic Tracking Number

OMB No. 2120-0020

11/30/2007

MAJOR REPAIR AND ALTERATION For FAA Use OnlyUS Department

of Transportation (Airframe, Powerplant, Propeller, or Appliance)

Federal Aviation

Administration

INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for

instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each

such violation. (49 U.S.C. §46301(a))

Nationality and Registration Mark Serial No.

1. Aircraft Make Model Series

Name (As shown on registration certificate) Address (As shown on registration certificate)

Address

2. Owner City State

Zip Country

3. For FAA Use Only

4. Type

Repair Alteration Unit

AIRFRAME

5. Unit Identification

Make Model

(As described in Item 1 above)

Serial No.

POWERPLANT

PROPELLER

Type

APPLIANCE Manufacturer

6. Conformity Statement

A. Agency's Name and Address B. Kind of Agency

U. S. Certificated Mechanic Name Manufacturer

Address Foreign Certificated Mechanic C. Certificate No.

City State Certificated Repair Station

Zip Country Certificated Maintenance Organization

D. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or attachments hereto

have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information

furnished herein is true and correct to the best of my knowledge.

Signature/Date of Authorized IndividualExtended range fuel

per 14 CFR Part 43

App. B

7. Approval for Return to Service

Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the

Administrator of the Federal Aviation Administration and is Rejected

Persons Approved by CanadianFAA Flt. Standards Maintenance OrganizationManufacturer Department of Transport

BY

Inspector

Other (Specify)

FAA Designee

Signature/Date of Authorized Individual

Designation No.

Approved

Inspection AuthorizationRepair Station

Certificate or

FAA Form 337 (10-06)

Ed Mechanic

N114AZ

CESSNA

O & W INC.

182L

1888 CIRRUS AVENUE

OKLAHOMA CITY OK

73405 U.S.

KATHY P. AILERON

411 GULFSTREAM DRIVE

OKLAHOMA CITY OK

73125 U.S. A&P 122234566

233346566 MARCH 26, 2002

SAMPLE

Kathy P. Aileron MARCH 23,2002

Plane Sense

Chapter 8: Aircraft Maintenance RecordsPlane Sense

Chapter 8: Aircraft Maintenance Records

Figure 8-2. FAA Form 337, Major Repair and Alteration (Page 2 of 2).

NOTICE

Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be

compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.

8. Description of Work Accomplished

(If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.)

Nationality and Registration Mark Date

Additional Sheets Are Attached

FAA Form 337 (10-06)

N114AZ MARCH 26, 2002

1. Removed right wing from aircraft and removed skin from

outer 6 feet. Repaired buckled spar 49 inches from tip

in accordance with attached photographs and figure 1 of

drawing dated March 23, 2002.

Date: March 26, 2002, inspected splice in Item 1 and

found it to be in accordance with data indicated. Splice

is okay to cover. Inspected internal wing assembly for

hidden damage and condition.

Ed Mechanic, A&P 233346566 IA

2. Primed interior wing structure and replaced skin P/N’s

63-0085, 63-0086, and 63-00878 with same skin 2024-T3,

.025 inches thick. Rivet size and spacing all the same as

original and using procedures in Chapter 2, Section 3,

of AC 43.13-1B CHG 1, dated 2001.

3. Replaced stringers as required and installed 6 splices

as per attached drawing and photographs.

4. Installed wing, rigged aileron, and operationally

checked in accordance with manufacturer’s maintenance

manual.

5. No change in weight or balance.

END

Ed Mechanic

SAMPLE

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