Plane SenSe General aviation Information

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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.

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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

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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

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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