8
8-6
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 Only
US 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 Individual
Extended 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 Canadian FAA Flt. Standards
Maintenance Organization Manufacturer Department of Transport
BY
Inspector
Other (Specify)
FAA Designee
Signature/Date of Authorized Individual
Designation No.
Approved
Inspection Authorization Repair Station
Certificate or
FAA Form 337 (10-06)
Ed Mechanic
N114AZ
CESSNA
O & W INC.
18259223
182L
X
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
X
X
X
SAMPLE
Kathy P. Aileron MARCH 23,2002
Chapter 8: Aircraft Maintenance Records
8
8-7
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
Plane Sense
8
8-8
Chapter 8: Aircraft Maintenance Records
A
n Airworthiness Directive (AD) is an important tool used by the Federal Aviation
Administration (FAA) to communicate unsafe operating conditions relating to aircraft
and aircraft equipment to aircraft owners. A primary safety function of the FAA is to require
the correction of unsafe conditions found in an aircraft, aircraft engine, propeller, rotor, or
appliance when such conditions exist or are likely to exist or develop in other products of the
same design. These unsafe conditions can exist because of a design defect, maintenance, or
other causes.
Title 14 of the Code of Federal Regulations (14 CFR) Part 39, Airworthiness Directives, defines
the authority and responsibility of the Administrator in requiring the necessary corrective
action to address unsafe conditions. ADs are used to notify aircraft owners and other interested
persons of unsafe conditions and to specify the conditions under which the product may
continue to be operated.
types of Ads issued
The FAA issues two categories of ADs:
•Normal Issue
•Emergency Issue
standard Ad Process
The standard AD process is to issue a Notice of Proposed Rulemaking (NPRM), followed by
a Final Rule. After an unsafe condition is discovered, a proposed solution is published in the
Federal Register as an NPRM, which solicits public comment on the proposed action. After the
comment period closes, the final rule is prepared, taking into account all substantive comments
received, with the rule perhaps being changed as warranted by the comments. The preamble
to the Final Rule AD provides response to the substantive comments or states there were no
comments received.
emergency Ad
In certain cases, the critical nature of an unsafe condition may warrant the immediate adoption
of a rule without prior notice and solicitation of comments. The intent of an Emergency AD
is to rapidly correct an urgent safety of flight situation. This is an exception to the standard
process. If time by which the terminating action must be accomplished is too short to allow for
public comment (that is, less than 60 days), then a finding of impracticability is justified for
the terminating action, and it can be issued as an immediately adopted rule. The immediately
adopted rule will be published in the Federal Register with a request for comments. The Final
Rule AD may be changed later if substantive comments are received.
9
Airworthiness directives
1
EMERGENCY AIRWORTHINESS DIRECTIVE
Aircraft Certification Service
Washington, DC
U.S. Department
of Transportation
Federal Aviation
Administration
We post Emergency ADs on the internet at www.faa.gov/aircraft/safety/alerts.
DATE: March 12, 2008
AD #: 2008-06-51
This emergency airworthiness directive (AD) 2008-06-51 is sent to all owners and operators
of Lycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO series reciprocating
engines, Teledyne Continental Motors (TCM) TSIO-360-RB reciprocating engines, and Superior Air
Parts, Inc. IO-360 series reciprocating engines with certain Precision Airmotive LLC RSA-5 and
RSA-10 series fuel injection servos.
Background
This emergency AD results from eighteen reports of fuel injection servo plugs, part number
(P/N) 383493, that had loosened or completely backed out of the threaded plug hole on the regulator
cover of the fuel injection servo. These servo plugs were installed with servo plug gasket, P/N
365533, under the plug hex-head. Precision Airmotive LLC investigated and determined that servo
plug gasket, P/N 365533, can shrink from engine heat, causing the plug to lose torque against the
servo regulator cover, allowing the plug to vibrate out. The threads on the plugs were also found
damaged. Servo plug gaskets, P/N 365533, installed on RSA-5 and RSA-10 series fuel injection
servos since August 22, 2006, are made of a different material than the previous gasket part number
used. This condition, if not corrected, could result in a substantial loss of engine power and
subsequent loss of control of the airplane.
Explanation of Relevant Service Information
We have reviewed Precision Airmotive LLC Mandatory Service Bulletin (MSB) No. PRS-
107, Revision 1, dated March 6, 2008. The MSB describes procedures for inspecting servo plugs for
looseness and damage, inspecting the servo regulator cover threads for damage, on fuel injection
servos that have a servo plug gasket, P/N 365533, installed, inspecting the gasket for damage,
reinstalling acceptable parts, and torquing the servo plug to a new, higher torque to help maintain the
proper clamp-up force against the plug and cover.
Interim Action
These actions are interim actions and we might take additional rulemaking actions in the
future.
FAA’s Determination and Requirements of the Rule
We have identified an unsafe condition that is likely to exist or develop on other RSA-5 and
RSA-10 series fuel injection servos of this same type design. This AD requires inspecting servo plugs
for looseness and damage on fuel injection servos that have a servo plug gasket, P/N 365533,
9-1
Plane Sense
9-2
9
superseded Ad
An AD is no longer in effect when it is superseded
by a new AD. The superseding AD identifies the AD
that is no longer in effect. There are no compliance
requirements for a superseded AD.
Compliance with Ads
For purposes of compliance, ADs may be divided
into two categories:
•Those of an emergency nature requiring
immediate compliance before further flight, or
•Those of a less urgent nature requiring
compliance within a relatively longer period of
time.
ADs are the “final rule”and compliance is required
unless specific exemption is granted. Aircraft owners
are responsible for ensuring compliance with all
pertinent ADs. This includes those ADs that require
recurrent or continuing action. For example, an AD
may require a repetitive inspection each 50 hours
of operation, meaning the particular inspection must
be accomplished and recorded every 50 hours of
time in service.
m CAUTION: Aircraft owners are reminded
that there is no provision to overfly the maximum
hour requirement of an AD unless it is specifically
written into the AD.
Amateur-Built Aircraft
For help in determining if an AD applies to your
amateur-built aircraft, contact your local Flight
Standards District Office (FSDO).
summary of Ads
14 CFR part 91, section 91.417, requires a record
to be maintained that shows the current status of
applicable ADs, including:
•Method of compliance;
•AD number and revision date;
•Date and time when due again, if recurring;
•Certified mechanic’s signature;
•Type of certificate; and
•Certificate number of the repair station or
mechanical performing the work.
For ready reference, many aircraft owners keep a
chronological listing of the pertinent ADs in the back
of their aircraft and engine records. Generally, a
summary of ADs contains all the valid ADs previously
published. Figure 9-1 is a sample form of summary
of ADs.
obtaining Ads
Both AD categories (small and large aircraft) are
published in biweekly supplements. All ADs are
available on the FAA website at www.faa.gov.
Advisory Circular (AC) 39-7 (as revised), Airworthiness Directives, provides additional guidance and
information for aircraft owners and operators about
their responsibilities for complying and recording
ADs. For more information, contact the FAA
Regulatory Support Division, Delegation and
Airworthiness Programs Branch (AIR-140). AIR-140
contact information is available in the FAA Contact
Information appendix on pages A1–A2 of this
handbook.
Chapter 9: Airworthiness Directives
9-3
9
AirWortHiness direCtive ComPliAnCe reCord
Aircraft: PA-22-135 N2631A S/N 22-903
Engine: Lycoming 0-290-D2 S/N 4563-21
Propeller: Sensenich M 76AM2 S/N 6662
Ad &
Amend
nUm.
rev.
nUm. &
dAte
sUBjeCt dAte/
HoUrs
At ComP.
metHod
oF ComP.
one
time
reCUr-
rinG
ComP. dUe
dAte/Hrs
AUtHorized
siGnAtUre &
nUmBer
76-07-12
39-3024
R-1
8-30-77
Bendix
ignition
switch
11-11-94
1850TT
Operational
check and
inspection
X Phil Lomax
A&P
000000000
93-18-03
39-8688
Original
10-29-93
Onepiece
venturi
3-17-95
1850OTT
Installed
one-piece
venturi
Carb S/N
BR-549
X 1900TT Phil Lomax
A&P
000000000
Figure 9-1. Sample Airworthiness Directives Compliance Record. This sample AD Compliance Record is
intended to show you an acceptable format for recording the required information to evidence your aircraft’s
compliance with applicable ADs. The FAA does not prescribe a specific format; however, the information
discussed in this chapter must be maintained with the aircraft’s maintenance records.
Plane Sense
9-4
9
service diffculty Program
10
10-1
T
he Service Difficulty Program is an information system designed to provide assistance
to aircraft owners, operators, maintenance organizations, manufacturers, and the Federal
Aviation Administration (FAA) in identifying aircraft problems encountered during service.
Background
The Service Difficulty Program provides for the collection, organization, analysis, and
dissemination of aircraft service information to improve service reliability of aeronautical
products. The primary sources of this information are aircraft maintenance facilities, owners,
and operators. The incentive for early detection is to expedite corrective actions and ultimate
solutions, thereby minimizing the effect of equipment failure on safety.
Each problem reported contributes to the improvement of aviation safety through the
identification of a potential problem area and the alerting of other persons to it. This focusing
of attention on a problem has led to improvements in the design and maintainability of
aircraft and aircraft products.
Advisory Circular (AC) 20-109 (as revised), Service Difficulty Program (General Aviation),
describes the Service Difficulty Program as it applies to general aviation. It also includes
instructions for completing FAA Form 8010-4, Malfunction or Defect Report. The
information from these reports is compiled and published as Maintenance Alerts.
By pooling everyone’s knowledge about a situation, the FAA can detect mechanical problems
early enough to correct them before they might possibly result in accidents/incidents which
should make flying safer, more enjoyable, and certainly less expensive.
FAA Form 8010-4, malfunction or defect report
General aviation aircraft service difficulty information is normally submitted to the FAA by
use of FAA Form 8010-4. However, information will be accepted in any form or format when
FAA Form 8010-4 is not readily available for use.
The information contained in the FAA Form 8010-4 is stored in a computerized data bank
for retrieval and analysis. Items potentially hazardous to flight are telephoned directly to the
Regulatory Support Division, Aviation Data Systems Branch (AFS-620) personnel by FAA
aviation safety inspectors (ASIs) in local Flight Standards District Offices (FSDOs). These
items are immediately referred to, and promptly handled by, the appropriate FAA offices.
ADVISORY CIRCULAR
43-16A
AVIATION MAINTENANCE ALERTS
ADVISORY CIRCULAR
43-16A
AVIATION MAINTENANCE ALERTS
ALERT
JANUARY
ADVISORY CIRCULAR
43-16A
AVIATION MAINTENANCE ALE
ALERT
NUMBER
10-2
Plane 10
Sense
Aircraft owners, pilots, and mechanics are urged to
report all service problems promptly, using FAA
Form 8010-4 or any other form or format. You may
obtain a copy of the form from any FSDO. No postage
is required.
FAA Form 8010-4 is also available in a fillable
PDF format on the FAA website at
http://forms.faa.gov/forms/faa8010-4.pdf
for mailing, or it can be submitted electronically
on the FAA website at www.faa.gov. Figure 10-1
at the end of this chapter is a sample FAA
Form 8010-4.
maintenance Alerts
The FAA publishes AC 43-16 (as revised), Aviation
Maintenance Alerts, monthly on its website to
provide the aviation community with a means for
interchanging service difficulty information and
sharing information on aviation service experiences.
Background
The Maintenance Alert program leads to improved
aeronautical product durability, reliability, and safety.
The articles contained in the Maintenance Alerts are
derived from the Malfunction or Defect Reports submitted by aircraft owners, pilots, mechanics, repair
stations, and air taxi operators.
Maintenance specialists review the reports and select
pertinent items for publication in the Maintenance
Alerts. The information is brief and advisory and
compliance is not mandatory. However, the information is intended to alert you to service experience,
and, when applicable, direct your attention to the
manufacturer’s recommended corrective action.
Accessing Maintenance Alerts
You can access current and back issues of this
publication on the FAA website at http://www.faa.
gov/aircraft/safety/alerts/aviation_maintenance/,
which allows free access to each month’s Main-
tenance Alerts.
Contact Information
You can contact the FAA Aviation Systems Data
Branch (AFS-620) regarding the Maintenance Alert
Program. AFS-620 contact information is available
in the FAA Contact Information appendix on pages
A1–A2 of this handbook.
Chapter 10: Service Diffculty Program
10-3
Chapter 10: Service Diffculty Program
10
Figure 10-1. FAA Form 8010-4, Malfunction or Defect Report. You can obtain instructions for completing
FAA Form 8010-4 on the FAA website at www.faa.gov or from your local FSDO.
During a local flight, a fuel odor was
apparent. Flight was terminated at the
local airport with a normal landing.
After engine shutdown and exiting the
aircraft the pilot observed fuel leaking
from the lower engine cowl. Investigation revealed an aluminum fuel pressure
gauge line cracked at the B nut where
it attached to a carburetor fitting (see
attached drawing). Line appears to be
original (40+ yrs.). A combination of age
and vibration may have caused the crack.
Recommend checking line every 100 hrs.
and replacing as necessary.
N404DH
D-3311 Beechcraft C-35
Continental E-225 30904
Hartzell HCA2U20 AK-710
4A1
Tube-fuel 35-924126 N/A B-nut
pressure Carb end
N/A
David Waterski
405 555 4316
N/A N/A N/A
N/A 4100 4-28-05
Cracked
v
SAMPLE
10-4
Plane Sense
10
Chapter 10: Service Diffculty Program
T
here are several ways to obtain various Federal Aviation Administration (FAA)
publications. The easiest way to locate a particular FAA document and/or
Title 14 of the Code of Federal Regulations (14 CFR) part is on the FAA website at
www.faa.gov. In addition, you can order some FAA publications directly from the
FAA or from the Government Printing Office (GPO). The FAA Records Checklist in
Figure 11-1 at the end of this chapter is a list of addresses to assist you in obtaining
the publications and records discussed in this chapter.
FAA publications and supporting regulatory guidance material fall into several
specific categories, which are explained in this chapter. If you cannot find the
information you are seeking, refer to the FAA website, which contains a great deal
of useful information for aircraft owners and operators.
Advisory Circulars
The FAA issues an Advisory Circular (AC) to inform the aviation public, in a
systematic way, of nonregulatory material of interest. The content of an AC is not
binding on the public unless it is incorporated into a regulation by reference.
AC 00-2 (as revised) , Advisory Circular Checklist, contains a list of current FAA ACs
and provides detailed instructions on obtaining copies. It also contains a list of
U.S. GPO bookstores throughout the United States that stock many Government
publications. This AC may be accessed on the FAA website at www.faa.gov by
selecting “Regulations & Policies”from the main menu bar.
Airworthiness directives
The FAA uses an Airworthiness Directive (AD) to notify aircraft owners and other
interested persons of unsafe conditions and to specify the conditions under which the
product may continue to be operated. You can access ADs on the FAA website at
www.faa.gov by selecting “Regulations & Policies”from the main menu bar.
You can subscribe to ADs at the FAA Regulatory & Guidance Library (RGL) website,
http://rgl.faa.gov. Current and historical ADs are also available on the RGL website.
obtaining FAA Publications and records
11
11-1
11-2
Plane 11
Sense
temporary Flight restrictions
A Temporary Flight Restriction (TFR) is a geographically limited, short term, airspace restriction, typically
in the United States. TFRs often encompass major
sporting events, natural disaster areas, air shows,
space launches, and Presidential movements. You
can access current TFRs on the FAA website at
www.faa.gov by selecting “Regulations & Policies”
from the main menu bar.
m CAUTION: You should check the current TFRs
every time you fly.
notice to Airmen
You can obtain the most recent Notice to Airmen
(NOTAMs) from the FAA website at www.faa.gov
by selecting “Regulations & Policies”from the main
menu bar. Current NOTAMs are also available from
Flight Service Stations at 1-800-WX-BRIEF
(1-800-992-7433).
14 CFr
While aircraft owners and operators are responsible
for compliance with all applicable 14 CFR parts, you
may find the following parts most relevant to your
aircraft operations:
•14 CFR Part 1, Definitions and Abbreviations
•14 CFR Part 21, Certification Procedures for
Products and Parts
•14 CFR Part 23, Airworthiness Standards:
Normal, Utility, Acrobatic, and Commuter
Category Airplanes
•14 CFR Part 33, Airworthiness Standards: Aircraft
Engines
•14 CFR Part 35, Airworthiness Standards:
Propellers
•14 CFR Part 39, Airworthiness Directives
•14 CFR Part 43, Maintenance, Preventive
Maintenance, Rebuilding, and Alteration
•14 CFR Part 45, Identification and Registration
Marking
•14 CFR Part 47, Aircraft Registration
•14 CFR Part 49, Recording of Aircraft Titles and
Security Documents
•14 CFR Part 61, Certification: Pilots, Flight
Instructors, and Ground Instructors
•14 CFR Part 65, Certification: Airmen Other than
Flight Crewmembers
•14 CFR Part 91, General Operating and Flight
Rules
AC 00-44 (as revised), Status of Federal Aviation
Regulations, contains the current status of the
14 CFR parts, including changes issued, price
list, and ordering instructions. This AC may be
obtained on the FAA website at www.faa.gov.
Handbooks and manuals
The FAA publishes a series of handbooks and
manuals designed for aircraft, general aviation enthusiasts, examiners, and inspectors. You can find
most of these handbooks and manuals, including
Plane Sense, on the FAA website at www.faa.gov
by selecting “Regulations & Policies”from the main
menu bar.
Aircraft records
The FAA Civil Aviation Registry Aircraft Registration
Branch (AFS-750) maintains registration records
on individual aircraft and serves as a warehouse for
airworthiness documents received from FAA field
offices. You can access information on requesting
aircraft records, as well as current fee information,
on the FAA website at www.faa.gov by selecting
“Licenses & Certificates”from the main menu bar.
Request Aircraft Records
You can mail or fax your request for aircraft records
to AFS-750, or submit your request online.
Written requests from outside the United States
must include a check or money order (in U.S. funds)
payable to the FAA to cover the projected fee. You
can obtain the correct fee by contacting AFS-750.
AFS-750 contact information is available at the end
of this chapter in Figure 11-1, FAA Records Checklist,
and in the FAA Contact Information appendix on
pages A1–A2 of this handbook.
Format
You can order paper copies or electronic copies (on
CD-ROM) of aircraft records. Each CD-ROM contains one aircraft record. You can view the CD-ROM
files using Adobe Acrobat Reader. The FAA includes
a copy of the latest reader on the CD-ROM.
Most records for aircraft removed from the U.S.
Civil Aircraft Register before 1984 are in storage and
available only in paper format. You can ask the FAA
to retrieve these records.
11-3
Chapter 11: Obtaining FAA Publications and Records
11
Airman records
The FAA Civil Aviation Registry Airmen Certification
Branch (AFS-760) maintains airman records. You
can access information on requesting airman records,
as well as current fee information, on the FAA website
at www.faa.gov by selecting “Licenses & Certificates”
from the main menu bar.
There are two ways to obtain copies of your airman
records. You can mail the FAA Aeronautical Center
(AC) Form 8060-68, Request for Copies of My
Complete Airman File; or a signed, written request
stating your name, date of birth, and social security
number or certificate number. Figure 11-2 at the end
of this chapter is a sample FAA Form 8060-68.
You can also have copies of your airman records
released to a third party. Requests for airman records
can be mailed to AFS-760. AFS-760 contact information is available at the end of this chapter in
Figure 11-1, FAA Records Checklist, and in the FAA
Contact Information appendix on pages A1–A2 of
this handbook.
When the FAA receives your request, they will notify
you of the total charges due and payment options.
For an airman or third party to obtain copies of
medical records or a duplicate medical certificate,
the Freedom of Information Act (FOIA) request
should be mailed to the FAA Civil Aerospace
Medical Certification Division, Medical Certification
Branch (AAM-331). AAM-331 contact information
is available at the end of this chapter in Figure 11-1,
FAA Records Checklist, and in the FAA Contact
Information appendix on pages A1–A2 of this
handbook.
11-4
11
Plane Sense
FAA reCords CHeCKlist
stAtUs reCords ContACt inFormAtion
•Aircraft Documents Federal Aviation Administration
Aircraft Registration Branch, AFS-750
P.O. Box 25504
Oklahoma City, OK 73125
(405) 954-3116
•Airman Records (Replacement
Certificate)
Federal Aviation Administration
Airmen Certification Branch, AFS-760
P.O. Box 25082
Oklahoma City, OK 73125
(405) 954-3261
•Airman Medical Records Federal Aviation Administration
Aeromedical Certification Branch, AAM-331
P.O. Box 26080
Oklahoma City, OK 73126-5063
(405) 954-4821
•FOIA Desk (Third Party Request,
Duplicate Medical Certificate)
Federal Aviation Administration
Aeromedical Certification Branch, AAM-331
Attention: FOIA Desk
P.O. Box 26200
Oklahoma City, OK 73125-9914
Figure 11-1. FAA Records Checklist. The easiest way to locate information on obtaining records from the FAA
is on the FAA website at www.faa.gov. You can also use this checklist to determine which FAA branch to contact
regarding the records requested.
11-5
Chapter 11: Obtaining FAA Publications and Records
11
Figure 11-2. FAA Form 8060-68, Request for Copies of My Complete Airman File. You can obtain instructions
for completing FAA Form 8060-68 on the FAA website at www.faa.gov or from your local FSDO.
WILLIAM THOMAS WRIGHT
9-12-53 WICHITA, KANSAS
111-22-3333
341 PIPER ROAD
OKLAHOMA CITY OK 73125
4-28-08
William Thomas Wright
SAMPLE
11-6
Plane Sense
11
A-1
A
Appendix A: FAA Contact information
The information contained in this appendix will help you contact the appropriate Federal Aviation Administration
(FAA) office.
FAA offce Page(s)
U.S. Department of Transportation
Federal Aviation Administration
800 Independence Avenue, SW
Washington, DC 20591-0004
(866) TELL-FAA
(866-835-5322) toll-free
www.faa.gov
vii
Federal Aviation Administration
Airman Testing Standards Branch, AFS-630
P.O. Box 25082
Oklahoma City, OK 73125-0082
(405) 954-4151 phone
afs630comments@faa.gov
iii
Federal Aviation Administration
Aircraft Registration Branch, AFS-750
P.O. Box 25504
Oklahoma City, OK 73125-0504
(866) 762-9434 toll-free
(405) 954-3116 phone
(405) 954-3548 or (405) 954-8068 fax
2-2, 2-3, 4-1, 4-3, 4-4, 4-5,
11-2, 11-4
Federal Aviation Administration
Light Sport Aviation Branch, AFS-610
P.O. Box 25082
Oklahoma City, OK 73125-0082
(405) 954-6400 phone
(405) 954-4104 fax
2-4, 4-5, 6-2
Federal Aviation Administration
Delegation & Airworthiness Programs Branch, AIR-140
P.O. Box 26460
Oklahoma City, OK 73125-4902
(405) 954-4103 phone
9-2
A-2
Plane Sense
A
FAA offce Page(s)
Federal Aviation Administration
Aviation Systems Data Branch, AFS-620
ATTN: AFS-620 ALERTS
P.O. Box 25082
Oklahoma City, OK 73125-0082
(405) 954-4391 phone
10-2
Federal Aviation Administration
Airmen Certification Branch, AFS-760
P.O. Box 25082
Oklahoma City, OK 73125-0082
(405) 954-3261 phone
11-3, 11-4
Federal Aviation Administration
Aeromedical Certification Branch, AAM-331
P.O. Box 26080
Oklahoma City, OK 73126-5063
(405) 954-4821 phone
11-3, 11-4
Federal Aviation Administration
Aeromedical Certification Branch, AAM-331
ATTN: FOIA Desk
P.O. Box 26200
Oklahoma City, OK 73125-9914
(405) 954-4821 phone
11-4
B-1
B
Code of Federal regulations (CFr) Page(s)
14 CFR .. iii, 1-4, 2-2, 3-1, 6-1, 7-1,7-2, 7-3, 11-1
14 CFR part 1 .........................................................11-2
14 CFR part 1, section 1.1 ........................................6-1
14 CFR part 21 ..................................... 3-1, 3-3, 11-2
14 CFR part 21, subpart C .......................................3-2
14 CFR part 21, subpart H ......................................3-3
14 CFR part 21, subpart I ........................................3-2
14 CFR part 21, section 21.24 .................................3-2
14 CFR part 21, section 21.25 .................................3-2
14 CFR part 21, section 21.181 ................................3-3
14 CFR part 21, section 21.184 ...............................3-2
14 CFR part 21, section 21.185 ................................3-2
14 CFR part 21, section 21.187 ................................3-2
14 CFR part 21, section 21.189 ...............................3-2
14 CFR part 21, section 21.190 ....3-2, 4-5, 6-2, 7-1,
7-3, 8-2
14 CFR part 21, section 21.191 ....................... 3-2, 6-2
14 CFR part 21, section 21.193 ................................3-2
14 CFR part 21, section 21.195 ................................3-2
14 CFR part 21, section 21.197........................3-2, 5-2
14 CFR part 23 ......................................................11-2
14 CFR part 33 ......................................................11-2
14 CFR part 35 ......................................................11-2
14 CFR part 39 .....................................8-4, 9-1, 11-2
14 CFR part 43 ...1-2, 3-1, 3-3, 7-2, 7-3, 8-2, 11-2
14 CFR part 43, section 43.9 ................. 2-4, 8-3, 8-4
14 CFR part 43, section 43.11 .........................7-2, 8-3
14 CFR part 43, appendix A ...........................7-2, 7-3
14 CFR part 43, appendix B ....................................8-2
14 CFR part 43, appendix D ...................................7-3
14 CFR part 43, appendix E ....................................7-3
14 CFR part 43, appendix F ....................................7-3
14 CFR part 45 ..............................................3-3, 11-2
Code of Federal regulations (CFr) Page(s)
14 CFR part 47 .....................................4-5, 4-6, 11-2
14 CFR part 47, section 47.2 ...................................4-2
14 CFR part 47, section 47.41 ........................ 1-1, 4-4
14 CFR part 49 ......................................................11-2
14 CFR part 61 ..............................................1-2, 11-2
14 CFR part 65 ......................................................11-2
14 CFR part 67 ........................................................1-2
14 CFR part 91 ...1-2, 3-1, 5-2, 7-2, 8-3, 8-4,11-2
14 CFR part 91, subpart D ......................................3-3
14 CFR part 91, subpart E ..............................7-1, 7-2
14 CFR part 91, section 91.203 ...............................4-3
14 CFR part 91, section 91.207 ...............................8-3
14 CFR part 91, section 91.213 ....................... 2-4, 7-3
14 CFR part 91, section 91.215 ................................8-3
14 CFR part 91, section 91.305 ...............................2-5
14 CFR part 91, section 91.313 ................................3-3
14 CFR part 91, section 91.317 ................................3-2
14 CFR part 91, section 91.319 ................................2-5
14 CFR part 91, section 91.327 ..... 7-1, 7-2, 7-3, 8-2
14 CFR part 91, section 91.403 ...................... 2-4, 7-1
14 CFR part 91, section 91.409 ..............7-2, 8-1, 8-3
14 CFR part 91, section 91.411 ................................8-3
14 CFR part 91, section 91.413 ................................8-3
14 CFR part 91, section 91.417 ................................9-2
14 CFR part 91, section 91.715 ................................3-3
14 CFR part 121 .......................................................5-1
14 CFR part 125.......................................................8-3
14 CFR part 135 .......................................................5-1
14 CFR part 145.......................................................5-2
14 CFR part 183 ......................................................3-3
14 CFR part 183, section 183.33 .............................4-4
14 CFR part 375 ......................................................3-3
49 CFR part 830 .....................................................1-2
49 CFR part 830, section 830.5 .............................1-3
Appendix B: regulatory Guidance index
The information contained in this appendix will help you locate regulatory guidance information including
pertinent Code of Federal Regulations parts, FAA Orders, and Advisory Circulars.
B-2
Plane Sense
B
FAA orders (as revised) Page(s)
Order 8100.8 ..........................................................4-5
Order 8130.2 ........................ 2-5, 3-1, 3-3, 5-2, 6-2
Order 8130.33 .........................................................6-2
Order 8900.1 ..........................................................3-3
Advisory Circulars (ACs) (as revised) Page(s)
AC 00-2 ................................................................11-1
AC 00-44 ..............................................................11-2
AC 20-27 .................................................................3-3
AC 20-109 ............................................................10-1
AC 20-139 ...............................................................3-3
AC 21-4 ....................................................................3-3
AC 21-12 ..................................................................3-3
AC 39-7 ...................................................................9-2
AC 43-9 ..........................................................8-2, 8-4
AC 43-16 ...............................................................10-2
AC 45-2 ...................................................................3-3
AC 90-89 .................................................................3-3
