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8130.2D CHG 2 12/18/00 AIRWORTHINESS CERTIFICATION OF AIRCRAFT AND RELATED PRODUCTS 1. PURPOSE. This change incorporates revised guidance for the issuance of a U.S. Standard Airworthiness Certificate for new aircraft manufactured outside the United States along with general updates from field comments. Also included in this change are comments submitted from previous revisions that were not incorporated. 2. DISTRIBUTION. This change is distributed to the Washington headquarters branch levels of the Aircraft Certification Service, Flight Standards Service, and the Regulatory Support Division; to the Aviation System Standards Office; to the branch level in the Aircraft Certification Directorates and Regional Flight Standards Divisions; to all Aircraft Certification Offices; to all Manufacturing Inspection District and Satellite Offices; to all Flight Standards District Offices; to the Aircraft Certification Branch and Flight Standards Branch at the FAA Academy; to the Brussels Aircraft Certification Division and Flight Standards Staff; to applicable Representatives of the Administrator; and to all International Field Offices. 3. EXPLANATION OF CHANGES. Included in this change are: a. Incorporation of appendix 1, Issuance of U.S. Standard Airworthiness Certificates for New Aircraft Manufactured Outside the United States. b. Clarification of existing information, including previously submitted field comments. c. Removal of the, Jet Flow Forms reference at the bottom of each effected form. 4. DISPOSITION OF TRANSMITTAL. After filing the attached pages, this change transmittal shall be retained. PAGE CONTROL CHART Remove Pages Dated Insert Pages Dated vii viii xi xii 3 and 4 5 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 vii viii xi xii 3 and 4 5 12/18/00 9/30/99 9/30/99 12/18/00 12/18/00 12/18/00 A-W (IR/FS/VN) -3; A-X (CD/FS) -3; A-FFS-0 (LTD); A-FAC-0 (ALL); AMA-220 (50 copies); AMA-250 (10 copies); AFS-600 (3 copies); AVR-20 (ALL); AEU-100/200; A-FDR-1D AIR-200 8130.2D CHG 2 12/18/00 PAGE CONTROL CHART Remove Pages Dated Insert Pages Dated 6 13 thru 14 23 24 29 30 49 50 51 thru 54 67 thru 76 93 thru 98 101 102 105 106 109 110 111 and 112 123 124 127 128 135 136 141 (and 142) 157 thru 167 168 169 thru 171 172 181 182 thru 184 187 188 and 189 190 and 191 192 195 thru 198 201 202 209 thru 212 9/30/99 9/30/99 9/30/99 9/30/00 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/00 9/30/99 9/30/99 9/30/00 9/30/00 9/30/99 9/30/99 2/15/00 9/30/99 9/30/99 2/15/00 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 9/30/99 6 13 thru 14 23 24 29 30 49 50 51 thru 54 67 thru 76 93 thru 98 101 102 105 106 109 110 111 and 112 123 124 127 128 135 136 141 (and 142) 157 thru 167 168 169 thru 171 172 181 182 thru 184 187 188 and 189 190 and 191 192 195 thru 198 201 202 209 thru 212 9/30/99 12/18/00 12/18/00 9/30/99 9/30/99 12/18/00 9/30/99 12/18/00 12/18/00 12/18/00 12/18/00 12/18/00 9/30/99 12/18/00 9/30/99 9/30/99 12/18/00 12/18/00 12/18/00 12/18/00 12/18/00 12/18/00 9/30/99 12/18/00 12/18/00 12/18/00 9/30/99 12/18/00 9/30/99 9/30/99 12/18/00 9/30/99 12/18/00 9/30/99 12/18/00 12/18/00 12/18/00 9/30/99 12/18/00 Page 2 12/18/00 8130.2D CHG 2 PAGE CONTROL CHART Remove Pages Dated Insert Pages Dated 249 250 253 (and 254) 9/30/99 9/30/99 9/30/99 249 250 253 (and 254) Appendix 1, 1 thru 8 12/18/00 9/30/99 12/18/00 12/18/00 /S/ Frank P. Paskiewicz Manager, Production and Airworthiness Division Page 3 (and 4) 12/18/00 8130.2D CHG 2 Paragraph .............................................................................................................................. Page SECTION 5. PRIMARY CATEGORY AIRCRAFT AIRWORTHINESS CERTIFICATIONS 118. 119. 120. General ........................................................................................................................ 91 Certification Procedures.............................................................................................. 92 Reserved ...................................................................................................................... 92 SECTION 6. GENERAL EXPERIMENTAL AIRWORTHINESS CERTIFICATIONS 121. 122. 123. 124. * 125. 126. General.. ...................................................................................................................... 93 Eligibility..................................................................................................................... 94 Demilitarization of Former Military Aircraft.............................................................. 95 Aircraft Equipped with Ejection Seats or Jettisonable Stores..................................... 96 Flight Test Areas ......................................................................................................... 97 * Operating Outside Flight Test Areas........................................................................... 98 SECTION 7. EXPERIMENTAL AMATEUR-BUILT AIRWORTHINESS CERTIFICATIONS 127. 128. 129. 130. 131. 132. 133. 134. 135. General.. ...................................................................................................................... 99 Certification Procedures............................................................................................ 104 Evaluation of Amateur-Built Aircraft/Kits ............................................................... 106 Kit Evaluations at Manufacturers' Facilities ............................................................. 107 Changes to Eligible Kits............................................................................................ 108 Instructions for Completing Form 8000-38 .............................................................. 109 Flight Test Areas ....................................................................................................... 109 Issuance of Experimental Amateur-Built Operating Limitations ............................. 111 Reserved .................................................................................................................... 115 SECTION 8. CERTIFICATION AND OPERATION OF AIRCRAFT UNDER THE EXPERIMENTAL PURPOSE(S) OF EXHIBITION AND AIR RACING 136. 137. 138. 139. 140. 141. 142. 143. General ...................................................................................................................... 117 Former Military Aircraft ........................................................................................... 118 Brokering................................................................................................................... 119 Groups of Aircraft ..................................................................................................... 119 Special Certification Requirements........................................................................... 121 Certification Procedures............................................................................................ 123 Issuance of Experimental Exhibition and Air Racing Operating Limitations .......... 123 Reserved .................................................................................................................... 131 vii 8130.2D 9/30/99 Paragraph .............................................................................................................................. Page SECTION 9. CERTIFICATION AND OPERATION OF AIRCRAFT UNDER THE EXPERIMENTAL PURPOSE(S) OF RESEARCH AND DEVELOPMENT, SHOW COMPLIANCE WITH REGULATIONS, CREW TRAINING, MARKET SURVEYS, AND OPERATING KIT-BUILT AIRCRAFT 144. 145. 146. 147. 148.-149. General ...................................................................................................................... 133 Special Certification Requirements........................................................................... 134 PC/APIS Holder's Experimental Operating Procedure ............................................. 134 Issuance of Experimental Research and Development, Show Compliance with Regulations, Crew Training, Market Surveys, and Operating Kit-Built Aircraft Operating Limitations ............................................................................................... 136 Reserved .................................................................................................................... 141 SECTION 10. PROVISIONAL AIRWORTHINESS CERTIFICATION 150. 151. 152. 153. 154. 155. 156. 157.-170. General ...................................................................................................................... 143 Eligibility................................................................................................................... 143 Special Purpose Operations....................................................................................... 143 Statement of Conformity........................................................................................... 143 Certification Procedures............................................................................................ 143 Special Airworthiness Certificate, FAA Form 8130-7.............................................. 143 Operating Limitations ............................................................................................... 144 Reserved .................................................................................................................... 144 SECTION 11. SPECIAL FLIGHT PERMITS 171. 172. 173. 174. 175. 176. 177. 178. 179. General ...................................................................................................................... 145 Purposes .................................................................................................................... 146 Application and Issuance (General) .......................................................................... 147 Aircraft Inspections ................................................................................................... 147 Special Operating Limitations................................................................................... 148 Special Flight Permits for Operation of Overweight Aircraft................................... 149 Special Flight Permit for Production Flight Testing ................................................. 152 Special Flight Permit for Conducting Customer Demonstration Flights .................. 153 Special Flight Permit for Certain Large Aircraft to Which Part 125 is Not Applicable (Seating Capacity of 20 or More or Maximum Payload Capacity of 6000 Pounds or More) ........................................................................... 154 180.-183. Reserved .................................................................................................................... 156 Figure 4-1. Sample FAA Form 8130-7, Special Airworthiness Certificate (1 page) .................. 157 Figure 4-2. Sample FAA Form 8130-7, Special Airworthiness Certificate for Restricted Category Aircraft Certificated Under § 21.25(b)(7) (1 page).................. 158 Figure 4-3. Sample FAA Form 8130-6, Airworthiness Application for Primary Category Aircraft Certificated Under § 21.184(a) (2 pages) .................................................... 159 viii 9/30/99 8130.2D Paragraph .............................................................................................................................. Page 219. 220. 221. 222.-223. Identification and Marking........................................................................................ 205 Return to Service....................................................................................................... 206 Special Maintenance Records Consideration............................................................ 206 Reserved .................................................................................................................... 207 CHAPTER 7. SPECIAL FLIGHT AUTHORIZATIONS FOR NON-U.S. REGISTERED CIVIL AIRCRAFT 224. 225. 226. 227. 228. 229. 230. 231. 232.-235. Figure 7-1. Figure 7-2. Figure 7-3. Figure 7-4. Figure 7-5. Figure 7-6. Figure 7-7. Figure 7-8. Figure 7-9. General ...................................................................................................................... 209 Eligibility................................................................................................................... 209 Blanket Special Flight Authorizations ...................................................................... 210 Application ................................................................................................................ 210 Issuance ..................................................................................................................... 212 Duration..................................................................................................................... 213 Operating Limitations ............................................................................................... 213 Special Flight Authorizations for Operation of Canadian-Registered Amateur-Built Aircraft in the United States ............................................................. 217 Reserved .................................................................................................................... 218 Sample Special Flight Authorization for the Flight of an Aircraft to a Place Where Repairs or Alterations are to be Made (2 pages).................................. 219 Sample Special Flight Authorization for the Flight of an Aircraft to a New Country of Registry (2 pages)........................................................................... 221 Sample Special Authorization for the Purpose of Flight Testing (2 pages).............. 223 Sample "Blanket" Special Flight Authorization for Customer Crew Training (2 pages) ..................................................................................................... 225 Sample Special Flight Authorization for Export Delivery (2 pages) ....................... 227 Sample "Blanket" Special Flight Authorization for Delivering Aircraft for the Purpose of Export Delivery (2 pages) ........................................................... 229 Sample Special Flight Authorization for the Purpose of Demonstration (2 pages) .................................................................................................................... 231 Sample Special Flight Authorization for Canadian-Registered Amateur-Built Aircraft (2 pages) ...................................................................................................... 233 Sample "Blanket" Special Flight Authorization for Glider Meet (2 pages).............. 235 CHAPTER 8. PROCESSING FORMS, REPORTS, AND CERTIFICATION FILES 236. 237. 238. 239. 240. 241. 242. 243. General ...................................................................................................................... 237 Application for Airworthiness Certificate................................................................. 237 Completion of FAA Form 8100-2............................................................................. 245 Completion of FAA Form 8130-7............................................................................. 246 Reserved .................................................................................................................... 247 Completion of FAA Form 8130-4............................................................................. 247 Completion of FAA Form 8130-1............................................................................. 248 Examination, Review, and Routing of Certification Files ........................................ 250 xi 8130.2D CHG 2 12/18/00 Paragraph .............................................................................................................................. Page 244.-250. Reserved .................................................................................................................... 252 Figure 8-1. Forms Listing and Availability ................................................................................. 253 * APPENDIX 1. ISSUANCE OF U.S. STANDARD AIRWORTHINESS CERTIFICATES FOR NEW AIRCRAFT MANUFACTURED OUTSIDE THE UNITED STATES 1. 2. 3. 4. xii Purpose…………………………………………………………………………….…..1 Applicability……………………………………………………………………….…..1 Procedure…………………………………………………………………………..…..1 Administrative Requirements………………………………………………………….8 * 12/18/00 TPA TSO U.S. VFR VLA 8130.2D CHG 2 Turbine-Powered Aircraft Technical Standard Order United States Visual Flight Rules Very Light Aircraft 8. DEFINITIONS. Some of the definitions included in 14 CFR part 1, Definitions and Abbreviations, and other publications are listed below: a. Aircraft Category. The term "category," as used with respect to the certification of aircraft, means a grouping of aircraft based upon its intended use or operating limitations, e.g., Normal, Utility, Acrobatic, Primary, etc. For purposes of this order, gliders and balloons will be referred to as categories in lieu of classifications. b. Aircraft Classification. The term "classification," as used with respect to the certification of aircraft means a broad grouping of aircraft having similar characteristics of propulsion, flight, or landing, e.g., airplane, rotorcraft, glider, and balloon. c. Bilateral Agreement. An executive agreement between the United States government and the government of another country to facilitate the airworthiness approval or acceptance of civil aeronautical products exported from one country (contracting state) to the other. There are two types of bilateral agreements related to airworthiness: bilateral airworthiness agreements (BAA) and bilateral aviation safety agreements (BASA). These agreements are not trade agreements, but rather technical cooperation agreements. These agreements are intended to provide a framework for the airworthiness authority of the importing country to give maximum practicable credit to airworthiness certification functions performed by the airworthiness authority of the exporting country using its own certification system. d. Category of Special Airworthiness Certificates. The term "category" is also used to identify the six specific certification processes and certificates issued as special airworthiness certificates. * e. Certification Office. The FAA Certification Office at which the applicant applies for airworthiness certification or related approval (i.e., MIDO, MISO, FSDO, IFO, CMO, CMU, and the Brussels Aircraft Certification Division). f. Classification of Airworthiness Certificates. The term "classification" is also used to distinguish between the two certification processes and certificates, i.e., standard and special. g. Exception. Case to which a rule, general principle, etc., does not apply. h. Exemption. To free from a rule or obligation that others must observe; excuse; release. i. Manufacturer. Any PAH or DOA. Par 7 Page 3 * 8130.2D CHG 2 12/18/00 9. INTERPRETATION OF THE TERM "AIRWORTHY" FOR U.S. TYPE CERTIFICATED AIRCRAFT. The term "airworthy" is not defined in Title 49 or the regulations; however, a clear understanding of its meaning is essential for use in the agency's Airworthiness Certification program. Below is an analogy of the conditions necessary for the issuance of an airworthiness certificate. A review of case law relating to airworthiness reveals two conditions that must be met for an aircraft to be considered "airworthy." Title 49 Section 44704(c) and 14 CFR part 21, Certification Procedures for Products and Parts (part 21), § 21.183(a), (b), and (c), all relate to the two conditions necessary for issuance of an airworthiness certificate. The statutory language establishes the two conditions as: a. The aircraft must conform to its TC. Conformity to type design is considered attained when the aircraft configuration and the components installed are consistent with the drawings, specifications, and other data that are part of the TC, and would include any STC and field approved alterations incorporated into the aircraft. b. The aircraft must be in a condition for safe operation. This refers to the condition of the aircraft relative to wear and deterioration, e.g., skin corrosion, window delamination/crazing, fluid leaks, tire wear, etc. NOTE: If one or both of these conditions were not met, the aircraft would be considered unairworthy. Aircraft which have not been issued a TC must meet the requirements of paragraph 9b above. * 10. INFORMATION CURRENCY. Any deficiencies found, clarifications needed, or improvements suggested regarding the content of this order will be forwarded (written or electronically) to the Aircraft Certification Service, the Automated Systems Branch, AIR-520, Attention: Directives Management Officer, for consideration. FAA Form 1320-19, Directive Feedback Information, is located on the last page of this order for your convenience or you may obtain it from the AIR-200 Web Site at: http://www.faa.gov/avr/air200/200home.htm. A copy may be forwarded to the Production and Airworthiness Division, AIR-200, Attention: Comments to Order 8130.2. If an interpretation is urgently needed, you may contact AIR-100, AIR-200, or for Flight Standards concerns, AFS-300. * Always use Form 1320-19 to follow up each verbal conversation. 11. RESERVED. Page 4 Par 9 12/18/00 8130.2D CHG 2 CHAPTER 2. GENERAL POLICIES AND PROCEDURES SECTION 1. GENERAL INFORMATION 12. REPRESENTATIVES OF THE FAA AUTHORIZED TO ISSUE AIRWORTHINESS CERTIFICATES AND RELATED APPROVALS. a. Consistent with applicable Aircraft Certification Service policies and instructions, a Manufacturing ASI or Flight Standards Airworthiness ASI is authorized to issue airworthiness certificates and related approvals covered in this order. b. The FAA is authorized under 14 CFR part 183, Representatives of the Administrator (part 183), to designate private persons or organizations to act as representatives of the Administrator to issue airworthiness certificates and related approvals. A DMIR, DAR, and ODAR may issue standard and special airworthiness certificates, airworthiness approvals, export approvals, and may perform certain other examinations, inspections, and testing services relative to certification functions in the areas of manufacturing and maintenance. The designee's Certificate of Authority shall specify the type and limitation of authority granted. NOTE: The authority of a DMIR or manufacturing ODAR must be specifically linked to a PAH or PAH's approved supplier. * * c. The FAA is authorized under part 21, subpart J, Delegation Option Authorization Procedures, and subpart M, Designated Alteration Station Authorization Procedures to delegate to organizations for the purpose of issuing airworthiness certificates and related approvals. A DOA may issue airworthiness certificates, airworthiness approvals, conformity certifications, and export approvals. A DAS may issue experimental certificates and amend standard airworthiness certificates under the conditions prescribed in part 21. d. The use of electronic signatures on airworthiness certificates, including export certificates of airworthiness, is not permitted. 13. RESPONSIBILITIES OF FAA INSPECTORS AND DESIGNEES. a. The procedures in this order cover original airworthiness certification for which Manufacturing Inspectors are primarily responsible, and recurrent airworthiness certification for which Flight Standards Airworthiness Inspectors are primarily responsible. Manufacturing and Flight Standards ASI's may assist each other by mutual agreement. b. The FAA designees, within the limits of their authority, are authorized to issue original or recurrent airworthiness certificates and related approvals. They are responsible for determining that the products or parts submitted to them conform to the approved type design, are in a condition for safe Par 12 Page 5 8130.2D 9/30/99 operation, and meet any other specified requirements. They are also responsible for the completeness, accuracy, and processing of all official documents and paperwork as provided for in this order. All actions taken by the designees on behalf of the FAA are subject to the monitoring, review, and approval of the supervising FAA inspector. c. FAA inspectors are responsible for training and supervising designees assigned to them regarding airworthiness certification procedures and all related documentation. The supervising FAA inspector should also assure that designees have been provided (or have access to) the appropriate regulations, instructions, and forms necessary for the performance of their designated duties. d. FAA inspectors will supervise and maintain surveillance over the certification activities accomplished by designees to ensure that all certifications and approvals comply with the applicable rules, policies, and procedures. NOTE: Within the text of this order the term "FAA" refers to the FAA inspector and/or authorized designee. 14. POSSESSION AND DISPLAY OF AIRWORTHINESS CERTIFICATES. Any airworthiness certificate issued to a U.S.-registered civil aircraft must be displayed at the cabin or cockpit entrance so that the certificate is legible to passengers or crew (14 CFR part 91, General Operating and Flight Rules (part 91), § 91.203(b)). 15. AIRCRAFT REGISTRATION. a. Registration. The procedures for aircraft registration and issuance of registration numbers are contained in 14 CFR part 47, Aircraft Registration (part 47). The registration of aircraft is not a function of airworthiness certification; however, U.S. registration is a prerequisite for issuance of an airworthiness certificate. The FAA must ensure that an aircraft presented for airworthiness certification is properly registered (Title 49, § 44704(c), and § 21.173). b. Proof of Ownership. The applicant for registration of an aircraft must submit proof of ownership to the FAA Aircraft Registration Branch (AFS-750) that meets the requirements prescribed in part 47. The Aeronautical Center Form 8050-2, Aircraft Bill of Sale, or its equivalent may be used as proof of ownership. If the applicant did not purchase the aircraft from the last registered owner, the applicant must submit a complete chain of ownership from the last registered owner to the applicant. The purchaser under a contract of conditional sale is considered the owner for the purpose of registration. The contract of conditional sale may be submitted as proof of ownership in lieu of a bill of sale. c. Aircraft Operation Outside the United States Pending U.S. Registration. For aircraft operations to or from the U.S., including operations conducted wholly outside the U.S., a current airworthiness certificate and Aircraft Registration Certificate, Aeronautical Center Form 8050-3, must be carried in the aircraft. Pending receipt of Form 8050-3, AFS-750 will, upon request, transmit a telex/facsimile confirmation of registration to the party whose name appears on the application as owner or authorized agent. The telex/facsimile may be used as a temporary Certificate of Aircraft Registration pending receipt of the original certificate. Page 6 Par 13 12/18/00 8130.2D CHG 2 SECTION 2. AIRWORTHINESS CERTIFICATES AND CERTIFICATIONS 24. GENERAL. FAA Form 8100-2, Standard Airworthiness Certificate, and FAA Form 8130-7, Special Airworthiness Certificate, will be referred to as being either a standard or a special classification within the text of this order. 25. CLASSIFICATION AND CATEGORY OF AIRWORTHINESS CERTIFICATES. a. Standard Classification. Form 8100-2 may be issued for an aircraft that fully complies with all the requirements applicable to Normal, Utility, Aerobatic, Commuter and Transport category, Manned Free Balloons, or for any other special classes of aircraft designated by the Administrator. b. Special Classification. Form 8130-7 may be issued for an aircraft that does not meet the requirements for a standard airworthiness certificate. The certificate may be issued for an aircraft that meets the following: (1) Primary. Aircraft that satisfies the requirements of § 21.184. (2) Restricted. Aircraft that satisfies the requirements of § 21.185. (3) Limited. Aircraft that satisfies the requirements of § 21.189. (4) Provisional. Aircraft that satisfies the applicable requirements of part 21, subpart C, Provisional Type Certificates, and subpart I, Provisional Airworthiness Certificates. (5) Experimental. For any category aircraft, including amateur-built (§§ 21.191, 21.193, and 21.195). (6) Special Flight Permits. Form 8130-7 may be issued for an aircraft that does not currently meet applicable airworthiness requirements, but is capable of safe flight, and meets the requirements of §§ 21.197 and 21.199. 26. REPLACEMENT, EXCHANGE, OR AMENDMENT OF AIRWORTHINESS CERTIFICATES. a. Replacement. (1) The FAA may issue a replacement airworthiness certificate when a certificate is declared lost, has been mutilated, or is no longer legible. The replacement airworthiness certificate shall carry the original issue date of the certificate being replaced, preceded by a capital "R" in the date block of the certificate. Additionally, replacement certificates will be issued when the aircraft registration number has been changed. In this case a new application for airworthiness certification is not required. * (2) Request for a replacement certificate will be made to the applicable certification office. The registered owner or certificate operator will certify this by submitting a signed statement containing the * Par 24 Page 13 8130.2D CHG 2 12/18/00 * registration number (N number), serial number, make, and model of the aircraft, and a reason the replacement certificate is needed. Replacement of airworthiness certificates shall not be accomplished * by verbal agreement with the assigned inspectors or through procedures contained in air carrier's manuals that allow the continued operation of an aircraft without an airworthiness certificate. Such actions are contrary to §§ 91.203(b), 121.153(a)(1), and 14 CFR part 135, Operating Requirements: Commuter and On Demand Operations and Rules Governing Persons on Board Such Aircraft (part 135), § 135.25(a). (3) A replacement airworthiness certificate may be issued without supporting documentation from AFS-750 if the date of issuance and the airworthiness classification and/or category of the lost or mutilated certificate can be positively established from the aircraft records, or from the remains of the certificate. If there is insufficient data upon which to base issuance of the replacement certificate, the FAA inspector will request copies of the appropriate data (such as the application form or previously issued airworthiness certificate) from AFS-750. (4) Before issuing a replacement certificate, the FAA shall review the aircraft records, and if necessary, inspect the aircraft to ensure the applicant's request is justified, and the aircraft is eligible for the airworthiness certificate requested. (5) A copy of the replacement certificate must be forwarded to AFS-750. b. Amendment. (1) Either a standard or special airworthiness certificate may be amended under the following situations: (a) Modification, i.e., STC or amended TC, that changes the category of the aircraft specified in Block #4 of the standard airworthiness certificate. (b) A change to the "Exceptions" specified in Block #5 of the standard airworthiness certificate. (c) A change in the aircraft model specified in Block #2 of the standard airworthiness certificate. (d) A change in the operating limitations for an aircraft with a special airworthiness certificate. (2) A DAS may amend a standard airworthiness certificate under § 21.451(b)(3). (3) When a certificate is amended, the issuance date will be the current date; also the capital letter "A" will be typed in front of the date. (4) Any amendment of an airworthiness certificate will require submission of FAA Form 8130-6, Application for Airworthiness Certificate. An appropriate record entry, in accordance with chapter 8 of this order, will be made in the aircraft records documenting the issuance of the amended certificate. Page 14 Par 26 12/18/00 8130.2D CHG2 FIGURE 2-2. SAMPLE RESPONSE LETTER REGARDING IDENTIFICATION PLATES U.S. Department of Transportation Federal Aviation Administration March 3, 2000 Mr. William Blue 220 West Broad Street Boston, Massachusetts 26204 Dear Sir: This is in response to your letter dated February 14, 2000, concerning disposition of the identification plate from Cessna Model 305A, Registration No. N5297G, Serial No. 305A-12345. The aircraft will be scrapped as a result of an accident. It is requested that the aircraft registration, airworthiness certificate, identification plate, and a copy of this letter be forwarded to the address listed below. Federal Aviation Administration Aircraft Registration Branch, AFS-750 Mike Monroney Aeronautical Center P.O. Box 25504 Oklahoma City, Oklahoma 73125-0750 Sincerely, John J. Doe, Manager Burlington Manufacturing Inspection District Office Page 23 8130.2D 9/30/99 FIGURE 2-3. SAMPLE LIMITATIONS FOR THE OPERATION OF AN AIRCRAFT WITH A DOOR REMOVED U.S. Department of Transportation Federal Aviation Administration Make ________________ Model _______________Serial No.______ Registration No. ____________________ AIRCRAFT OPERATING LIMITATIONS The aircraft described above may be flown with not more than one cabin door removed for the purpose of (see note below), provided the aircraft is operated in accordance with the applicable Federal Aviation Regulations and the following limitations: Note: Show specific operations; e.g., intentional parachute jumping, skydiving, etc. 1. Maximum speed not to exceed any of the following: The approved maneuvering speed. 70 percent maximum level flight speed. 70 percent maximum structural cruising speed. 2. Aerobatic maneuvers are not permitted. 3. Maximum yaw angle 10 degrees; maximum bank angle 15 degrees. 4. An FAA-approved safety belt shall be provided and worn by each occupant during takeoff and landing and at all other times when required by the pilot-in-command. 5. All occupants shall wear parachutes when intentional parachute jumping and skydiving operations are conducted. 6. Smoking is not permitted. 7. When operations other than intentional parachute jumping and skydiving are conducted, a suitable guardrail or equivalent safety device shall be provided for the doorway. 8. All loose articles shall be tied down or stowed. 9. No baggage shall be carried. 10. Parachutist's static lines shall be kept free of pilot's controls and control surfaces. Page 24 9/30/99 8130.2D d. MIDO's and MISO's having CM responsibility for a particular manufacturer have access to and can provide pertinent information, technical data, etc., as necessary for the certification effort. It is the applicant's responsibility to provide the type design data for those parts and components for which a conformity determination must be made. 45. BASIC ELIGIBILITY REQUIREMENTS. Before a standard airworthiness certificate can be issued, the applicant must show that: a. The aircraft conforms to its approved type design and is in a condition for safe operation. b. Any alterations were accomplished in accordance with an approved STC or other FAA-approved data. c. All applicable AD's have been complied with. d. If altered while in another category, the aircraft continues to meet, or has been returned to, its approved type design configuration and is in a condition for safe operation. 46. CERTIFICATION PROCEDURES. The procedures described herein are consistent with any other specific procedures prescribed in paragraphs dealing with individual airworthiness categories. a. Obtain from the applicant a properly executed Form 8130-6, and any other documents required for certification. The applicant must have the form completed and the appropriate sections signed prior to submitting it to the FAA. The application for a U.S. airworthiness certificate must be made by the registered owner or an agent who has a notarized letter of authorization from the registered owner. b. Contact AFS-750 to determine that an application for airworthiness certification has not previously been denied. If it was denied, the reasons stated in the denial letter must be rectified prior to issuing an airworthiness certificate. c. Arrange with the applicant to make available for inspection and review the aircraft, aircraft records, and any other data necessary to establish conformity to its type design. d. Determine that the aircraft is properly registered in accordance with part 47. e. As applicable, ensure compliance with the noise standards of §§ 21.93(b), 21.183(e), 14 CFR part 36, Noise Standards: Aircraft Type and Airworthiness Certification (part 36), or part 91. Also ensure compliance with the fuel venting and exhaust emission requirements of 14 CFR part 34, Fuel Venting and Exhaust Emission Requirements for Turbine Engine Powered Airplanes (part 34), and the applicable passenger emergency exit requirements of § 21.183(f) and SFAR 41. f. Review records and documentation to the extent necessary to establish that: Par 44 Page 29 8130.2D CHG 2 12/18/00 (1) All of the required records and documentation are provided for the aircraft, i.e., an up-to-date approved flight manual, a current weight and balance report, equipment list, maintenance records, FAA-accepted ICAW and/or FAA-accepted maintenance manual(s) (MM), and any other manuals required by §§ 21.31, 21.50, 14 CFR part 23, Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes (part 23), § 23.1529, 14 CFR part 25, Airworthiness Standards: Transport Category Airplanes (part 25), § 25.1529, 14 CFR part 27, Airworthiness Standards: Normal Category Rotorcraft (part 27), § 27.1529, 14 CFR part 29, Airworthiness Standards: Transport Category Rotorcraft (part 29), § 29.1529, 14 CFR part 33, Airworthiness Standards: Aircraft Engines (part 33), § 33.4, and 14 CFR part 35, Airworthiness Standards: Propellers (part 35), § 35.4. These documents must be in the English language. * (2) The aircraft is eligible by make, model, and serial number, using the TCDS, aircraft specifications, and/or applicable aircraft listing. * (3) The inspection records and technical data reflect that the aircraft conforms to the type design, and all required inspections and tests have been satisfactorily completed, and the records are complete and reflect no unapproved design changes. (4) The aircraft has been flight tested in accordance with paragraph 61 of this order, if required. If it has not been flight tested, issue the appropriate special airworthiness certificate prescribed in chapter 4. The flight test must be recorded in the aircraft records in accordance with § 91.417(a)(2)(i) as time in service as defined in part 1. Aircraft assembled by a person other than the manufacturer (e.g., a dealer or distributor) must have been assembled and, when applicable, flight tested in accordance with the manufacturer's FAA-approved procedures. (5) Large airplanes, turbojet, or turbopropeller multi-engine airplanes comply with the inspection program requirements of part 91, subpart E, Maintenance, Preventive Maintenance, and Alterations, or other CFR referenced therein. A supplemental structural inspection program is also required for certain large transport category airplanes. Reference AC 91-56, Supplemental Structural Inspection Program for Large Transport Category Airplanes. (6) The TC holder or STC holder has furnished one set of FAA-accepted ICAW or one complete set of FAA-accepted Maintenance Manuals (MM's) to the owner of the aircraft when the first standard airworthiness certificate is issued, or has procedures in place that will positively ensure that FAA-accepted ICAW/MM are provided upon delivery of the aircraft, as required by §§ 21.17(a) and (b), 21.31, and 21.50. The ICAW/MM are also required for all TC and STC products. If no FAA-accepted ICAW/MM are available, the FAA inspector having certificate management responsibility over the manufacturer will contact the ACO and Aircraft Evaluation Group (AEG) to determine the status of the ICAW/MM. The FAA inspector is responsible for ensuring that the manufacturer and company designees are made aware of the status of the ICAW/MM. No deliveries will be allowed prior to the ICAW/MM approval. NOTE: For additional information relative to import products, reference AC 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers, and Related Products Imported to the United States. Page 30 Par 46 9/30/99 8130.2D 68. CERTIFICATION PROCEDURES. The following would be some of the typical steps taken by the FAA inspector toward certification of the aircraft in conjunction with those specified in paragraph 46 of this order. a. Ensure that the application is complete and correct. b. Inspect the aircraft and review records to determine: (1) Compliance and conformity to the TC, taking into account any STC's or any amendments to the TC. (2) Compliance with applicable AD's. (3) Currency of weight and balance from actual weighing; it is recommended that the inspector observe the actual weighing. (4) Which inspections and tests, including flight tests, are required to find that the aircraft is in a condition for safe operation. The FAA production flight test requirements will be coordinated with FAA flight test personnel. (5) An approved flight test procedure and flight check-off form has been established (when a flight test is deemed necessary) and that each aircraft is flight tested by the applicant's pilot in accordance with that procedure. The FAA production flight tests will not be conducted until an entry has been placed in the aircraft records to show that these tests have been satisfactorily completed by the applicant. (6) Compliance with the registration and marking requirements of parts 47 and 45. (7) The civil model designation is reflected on the identification plate and all the airworthiness documentation, including registration and airworthiness certificates, reflect the civil and military model designation and serial number. The military designation and serial number should be placed in parentheses in the same blocks as the civil model and serial number. 69. EXAMPLES OF FORMS. Figures 3-1 through 3-15 provide examples of forms used in the certification process. 70.-85. RESERVED. Par 68 Page 49 8130.2D CHG 2 12/18/00 FIGURE 3-1. SAMPLE FAA FORM 8100-2, STANDARD AIRWORTHINESS CERTIFICATE, NEW AIRCRAFT (FACE SIDE) UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2 MANUFACTURER AND MODEL 3 REGISTRATION MARKS 5 4 CATEGORY NUMBER Douglas DC-6A N12345 AIRCRAFT SERIAL 43219 Transport AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provide by Annex 8 to the Convention of International Civil Aviation, except as noted herein. Exceptions: None 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21, 43, and 91 of the Federal Aviation Regulations, as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE FAA REPRESENTATIVE 1/20/00 E.R. White DESIGNATION NUMBER E.R. White NE-XX Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000, or imprisonment not exceeding 3 AFT IN ACCORDANCE WITH APPLICABLE FEDER AL years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCR AVIATION RE GULATIONS. FAA Form 8100-2 (8-82) SAMPLE FAA FORM 8100-2, STANDARD AIRWORTHINESS CERTIFICATE, SPARE AND SURPLUS PARTS (FACE SIDE) UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND 2 MANUFACTURER AND MODEL 3 REGISTRATION MARKS * 5 4 CATEGORY NUMBER Jackson 47G-4 N54321 AIRCRAFT SERIAL 3191HG Normal AUTHORITY AND BASIS FOR ISSUANCE This airworthiness certificate is issued pursuant to the Federal Aviation Act of 1958 and certifies that, as of the date of issuance, the aircraft to which issued has been inspected and found to conform to the type certificate therefor, to be in condition for safe operation, and has been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provide by Annex 8 to the Convention of International Civil Aviation, except as noted herein. Exceptions: None 6 TERMS AND CONDITIONS Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator, this airworthiness certificate is effective as long as the maintenance, preventative maintenance, and alterations are performed in accordance with Parts 21, 43, and 91 of the Federal Aviation Regulations, as appropriate, and the aircraft is registered in the United States. DATE OF ISSUANCE FAA REPRESENTATIVE 1/20/00 E.J. Smith E.J. Smith DESIGNATION NUMBER SW-XX Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000, or imprisonment not exceeding 3 TIFICATE MUST BE DISPLAYED IN THE AIR CRAFT IN ACCORDANCE WITH APPLICABLE FEDER AL years or both. THIS CER AVIATION RE GULATIONS. FAA Form 8100-2 Page 50 (8-82) * 12/18/00 8130.2D CHG 2 FIGURE 3-2. SAMPLE FAA FORM 8130-6, APPLICATION FOR AIRWORTHINESS CERTIFICATE, VLA UNDER § 21.183(a) Form Approved O.M.B. No. 2120-0018 APPLICATION FOR AIRWORTHINESS CERTIFICATE U.S. D epartment of Tr ansportation Federal Aviation Administration INSTRUCTIONS - Print or type. Do not write in shaded areas; these are for FAA use only. Submit o riginal only to an authorized FAA Representative . If additional space is required, use an attachment. For special flight permits complete Sections II and VI or VII as applicable. 2. AIRCRAFT BU ILDER'S NAME (Make) 3. AIRCRAFT MODEL DESIGNATION 4. YR. MFR. N18CE Lite-Flight LF-1-A 93 5. AIRCR AFT SER IAL NO. 6. ENGINE BUILDER 'S NAME (Make) 7. ENGINE MODEL DE SIGNATION LF010 Rotax 912 8. NUMBER OF ENGINES 9. PROP ELLER B UILDER' S NAME (Make) 10. PROPELLER MODEL DESIGNATION One I. AIRCRAFT DESCRIPTION 1. REGISTR ATION MARK Wood Built FAA CODING Good-1 11. AIRC RAFT IS (Check if appl icable) IMPORT APPLICATION IS HEREBY MADE FOR: (Check applicabl e items) A 1 STANDARD AIRWORTH INESS CERTIFICATE (Indicate category) B NORMAL UTILITY ACROBATIC TRANSPORT GLIDER BALLOON SPECIAL AIR WORTHINESS CERTIFICATE (Check appropriate items) 2 LIMITED 5 PROVISIONAL (Indicate class) 3 RESTRICTED (Indi cate operation( s) to be c onducted) AERIAL ADVER TISING 6 WEATHER CONTROL CARRIAGE OF CARGO 0 OTHER (Specify) RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION 4 RACING 5 CREW TRAINING TO SHOW COMPLIANCE WITH FAR FERRY FLIGHT FOR REPAIRS, ALTERATIONS, MAINTENANCE OR STORAGE 2 EVACUATE FROM AREA OF IMPENDING DANGER 3 OPERATION IN EXCESS OF MAX IMUM CERTIF ICATED TAKE -OFF WEIGHT 4 DELIVERING OR EXPORT 6 6 3 PATROLLING 1 C AERIAL 5 0 8 2 FOREST (Wildlife c onservation) 1 SPECIAL FLIGHT PERMIT (Indi cate oper ati on to be conduc ted, then complete Secti on VI or VII as applicable on rev erse side) AGRICULTURE AN D PEST CONTROL 4 EXPERIM ENTAL (Indicate operati on(s) to be c onduct ed) CLASS II 7 4 CLASS I 2 1 II. CERTIFI CATION REQUESTED 1 CUSTOMER DEMONSTRATION FLIGHTS 5 MKT. SURVEY PRODUCTION FLIGHT TESTING MULTIPLE AIR WORTHINESS CERTIFICATE (Check ABOVE "R estri cted Operation" and "Standard" or " Limited," as applicable.) A. REGISTER ED OWNER (As show n on certificate of aircraft registration) IF DEALER, CHECK HERE NAME ADDRESS Lite-Flight Corp. 1801 Airport Rd. Wichita, KS 67209 B. AIRCRAFT CERTIFICAT ION BASIS (Check appli cable bloc ks and com plete item s as indic ated) AIRCRAFT SP ECIFICAT ION OR T YPE CERT IFICATE DATA SHEET (Give No. and Revision No.) AIRWORTHINESS DIR ECTIVES (Check if all applicable AD' s complied w ith and give latest AD No.) AIRCRAFT LISTING (Give page num ber(s)) SUPPLEMEN TAL TYP E CERTIFICATE (List number of each ST C inc orpor ated) N/A N/A III. OWNER'S CERTIFICATION A2WI Rev. 1 92-25 C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS CHECK IF RECORDS IN COMPLIANCE WITH FAR 91.173. EXPERIMENTAL ONLY (Enter hour s flow n sinc e last certi ficate issued or renewed) TOTAL AIRFRAME HOURS 2.0 3 -0- D. CERTIFICATION - I hereby certify that I am the r egis tered ow ner (or his agent) of the ai rcraft desc ribed above; that the aircr aft is r egis tered w ith the Federal Aviation Administration in accordance with Section 501 of the Federal Aviation Act of 1958, and appli cable Federal Aviation R egulat ions; and that the ai rcr aft has been inspected and is airworthy and eli gibl e for the ai rwor thiness certific ate requested. DATE OF APPLI CATION NAME AND TITLE ( Print or type) SIGNATURE 01/27/2000 K.H. Good, Director Q.A. KA Good IV. INSPECTION AGENCY VERIF ICATION A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED A ND FOUND AIR WORTHY BY: ( Complete this section only i f FAR part 21 .183(d) applies) . 2 FAR part 121 or 127 CERTIF ICATE HOLDER (Give Certific ate No.) 3 CERTIFICATED REPAIR STATION (Give Certificate No.) 6 5 DATE TITLE SIGNATURE (Check ALL appli cable bloc ks in item s A and B) A. I find that the ai rcraft descr ibed in Sect ion I or VII meets r equi rements for: V. FAA REPRESENTATIVE CERTIFICATION CERTIFICATED MECHANIC (Give Certifi cate N o.) AIRCRAFT MANUFA CTURER (Give name or firm) THE CERTIFICATE REQUESTED 4 B. Inspecti on for a special fli ght permit under Sec tion VII was c onducted by: DATE FAA DE SIGNEE CERTIFICATE HOLDER UNDER: DISTRICT OFFICE 01/28/2000 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE FAA INSPECTOR DESIGNEE'S SIG NATURE AND NO. CE43 FAR 65 FAR 121, 127 or 135 FAR 145 FAA INSPECTOR 'S SIGNATURE 4 1 A.J. Kool A.J. Kool VIII. AIRWORTHINESS DOCUMENTATI ON (FAA use only) FAA Form 8130-6 (11-88) SUPERSEDES PREVIOUS EDITION A. Operating Limi tati ons and Mark ings in Compliance w ith FAR 91.31 as appl icable G. Statement of Confor mity, FAA Form 8130-9 (Attach when required) B. Current Operating Li mitati ons Attac hed H. Foreign Airworthiness Cer tification for Import Ai rcraft (Attac h when r equi red) C. Data, Draw ings , Photographs, etc. (Attach when required) I. Previous Airwor thiness Certifi cate Issued in Accor dance with D. Current Weight and Balance I nfor mati on Avail able in Airc raft E. Major Repair and Alter ation, F AA F orm 337 (Attach when required) F. This inspection Rec orded in Aircraft Records FAR 21.191(b) CAR (Original Attached) J. Current Airwor thiness Certifi cate Issued in Accor dance with FAR 21.191(a) (Copy attached) Page 51 8130.2D CHG 2 12/18/00 FIGURE 3-3. SAMPLE FAA FORM 8100-2, STANDARD AIRWORTHINESS CERTIFICATE, VLA UNDER § 21.183(a) UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS MANUFACTURER AND MODEL Lite-Flight LF-1-A N18CE 5 2 3 AIRCRAFT SERIAL NUMBER LF010 4 CATEGORY VLA Special Class AUTHORITY AN D BASIS FO R ISSUANCE This airworthiness certific ate is i ssued pursuant t o the Federal Av iati on Act of 1958 and c erti fies that, as of the dat e of issuance, the aircraft to which iss ued has been ins pected and found to conform to the type certif icat e theref or, to be in condition for safe operati on, and has been shown t o meet t he r equi rements of t he appli cabl e comprehens ive and detailed airwort hiness c ode as provi de by Annex 8 to the Convent ion of I nter nati onal Civ il Aviat ion, exc ept as noted her ein. Exceptions: N one 6 TERMS AND CONDITIONS Unless sooner surrendered, s uspended, revoked, or a termination date is otherwis e es tabl ished by the Adminis trat or, this airworthiness c ertif icate is effect ive as long as the maintenance, preventative maint enanc e, and alt erati ons are performed in accordance w ith Parts 21, 43, and 91 of the Federal Aviat ion R egulations , as appropriat e, and the airc raft is registered i n the United Stat es. DATE OF ISSUANCE FAA REPRESENTATIVE DESIGNATION NUMBER 08/10/00 A.J. Ko ol A.J. Kool CE43 Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000, or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) Page 52 12/18/00 8130.2D CHG 2 FIGURE 3-4. SAMPLE FAA FORM 8130-6, APPLICATION FOR AIRWORTHINESS CERTIFICATE, JAR/VLA UNDER § 21.183(c) Form Approved O.M.B. No. 2120-0018 APPLICATION FOR AIRWORTHINESS CERTIFICATE U.S. D epartment of Tr ansportation Federal Aviation Administration INSTRUCTIONS - Print or type. Do not write in shaded areas; these are for FAA use only. Submit o riginal only to an authorized FAA Representative . If additional space is required, use an attachment. For special flight permits complete Sections II and VI or VII as applicable. 2. AIRCRAFT BU ILDER'S NAME (Make) 3. AIRCRAFT MODEL DESIGNATION 4. YR. MFR. N7569K Aero-K AK-1A 1989 5. AIRCR AFT SER IAL NO. 6. ENGINE BUILDER 'S NAME (Make) 7. ENGINE MODEL DE SIGNATION AK901 Rotax 912 8. NUMBER OF ENGINES 9. PROP ELLER B UILDER' S NAME (Make) 10. PROPELLER MODEL DESIGNATION One I. AIRCRAFT DESCRIPTION 1. REGISTR ATION MARK Goodprop FAA CODING 1-GP-008 11. AIRC RAFT IS (Check if appl icable) IMPORT APPLICATION IS HEREBY MADE FOR: (Check applicabl e items) A 1 STANDARD AIRWORTH INESS CERTIFICATE (Indicate category) B NORMAL UTILITY ACROBATIC TRANSPORT GLIDER BALLOON SPECIAL AIR WORTHINESS CERTIFICATE (Check appropriate items) 2 LIMITED 5 PROVISIONAL (Indicate class) 3 RESTRICTED (Indi cate operation( s) to be c onducted) AERIAL ADVER TISING 6 WEATHER CONTROL CARRIAGE OF CARGO 0 OTHER (Specify) RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION RACING 5 CREW TRAINING TO SHOW COMPLIANCE WITH FAR 1 FERRY FLIGHT FOR REPAIRS, ALTERATIONS, MAINTENANCE OR STORAGE 2 EVACUATE FROM AREA OF IMPENDING DANGER 3 OPERATION IN EXCESS OF MAX IMUM CERTIF ICATED TAKE -OFF WEIGHT 4 DELIVERING OR EXPORT 6 6 3 PATROLLING 0 C AERIAL 5 4 SPECIAL FLIGHT PERMIT (Indi cate oper ati on to be conduc ted, then complete Secti on VI or VII as applicable on rev erse side) 2 FOREST (Wildlife c onservation) 1 8 AGRICULTURE AN D PEST CONTROL 4 EXPERIM ENTAL (Indicate operati on(s) to be c onduct ed) CLASS II 7 4 CLASS I 2 1 II. CERTIFI CATION REQUESTED 1 CUSTOMER DEMONSTRATION FLIGHTS 5 MKT. SURVEY PRODUCTION FLIGHT TESTING MULTIPLE AIR WORTHINESS CERTIFICATE (Check ABOVE "R estri cted Operation" and "Standard" or " Limited," as applicable.) A. REGISTER ED OWNER (As show n on certificate of aircraft registration) IF DEALER, CHECK HERE NAME ADDRESS I.R. Applicant 14 David Road. Wichita, KS 67209 B. AIRCRAFT CERTIFICAT ION BASIS (Check appli cable bloc ks and com plete item s as indic ated) AIRCRAFT SP ECIFICAT ION OR T YPE CERT IFICATE DATA SHEET (Give No. and Revision No.) AIRWORTHINESS DIR ECTIVES (Check if all applicable AD' s complied w ith and give latest AD No.) AIRCRAFT LISTING (Give page num ber(s)) SUPPLEMEN TAL TYP E CERTIFICATE (List number of each ST C inc orpor ated) N/A A89NE III. OWNER'S CERTIFICATION A 2EU Rev. 1 92-25 C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS CHECK IF RECORDS IN COMPLIANCE WITH FAR 91.173. EXPERIMENTAL ONLY (Enter hour s flow n sinc e last certi ficate issued or renewed) TOTAL AIRFRAME HOURS 132.0 3 -0- D. CERTIFICATION - I hereby certify that I am the r egis tered ow ner (or his agent) of the ai rcraft desc ribed above; that the aircr aft is r egis tered w ith the Federal Aviation Administration in accordance with Section 501 of the Federal Aviation Act of 1958, and appli cable Federal Aviation R egulat ions; and that the ai rcr aft has been inspected and is airworthy and eli gibl e for the ai rwor thiness certific ate requested. DATE OF APPLI CATION NAME AND TITLE ( Print or type) SIGNATURE 01/23/1993 J.B. Wright J.B. Wright IV. INSPECTION AGENCY VERIF ICATION A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED A ND FOUND AIR WORTHY BY: ( Complete this section only i f FAR part 21 .183(d) applies) . 2 FAR part 121 or 127 CERTIF ICATE HOLDER (Give Certific ate No.) 3 CERTIFICATED REPAIR STATION (Give Certificate No.) 6 5 DATE TITLE SIGNATURE (Check ALL appli cable bloc ks in item s A and B) A. I find that the ai rcraft descr ibed in Sect ion I or VII meets r equi rements for: V. FAA REPRESENTATIVE CERTIFICATION CERTIFICATED MECHANIC (Give Certifi cate N o.) AIRCRAFT MANUFA CTURER (Give name or firm) THE CERTIFICATE REQUESTED 4 B. Inspecti on for a special fli ght permit under Sec tion VII was c onducted by: DATE FAA DE SIGNEE CERTIFICATE HOLDER UNDER: DISTRICT OFFICE 01/27/2000 AMENDMENT OR MODIFICATION OF CURRENT AIRWORTHINESS CERTIFICATE FAA INSPECTOR DESIGNEE'S SIG NATURE AND NO. NW78 FAR 65 FAR 121, 127 or 135 FAR 145 FAA INSPECTOR 'S SIGNATURE 4 1 Joe Mendez Joe Mendez VII I. AIRWORTHINESS DOCUMENTATI ON (FAA use only) FAA Form 8130-6 (11-88) SUPERSEDES PREVIOUS EDITION A. Operating Limi tati ons and Mark ings in Compliance w ith FAR 91.31 as appl icable G. Statement of Confor mit y, FAA Form 8130-9 (Attach when required) B. Current Operat ing Li mit ati ons Attac hed H. Foreign Airworthiness Cer tification f or Import Ai rcraft (Attac h when r equi red) C. Data, Draw ings , Photographs, etc. (Attach when required) I. Previous Airwor thiness Certifi cate Issued in Accor dance with D. Current Weight and Balance Infor mati on Avail able in Airc raft E. Major Repair and A lter ation, F AA F orm 337 (Attach when required) F. This inspection Rec orded in Aircraft Records CAR FAR (Original Att ached) J. Current Airwor thiness Certifi cate Issued in Accor dance with FAR 21.183(c) (Copy attached) Page 53 8130.2D CHG 2 12/18/00 FIGURE 3-5. SAMPLE FAA FORM 8100-2, STANDARD AIRWORTHINESS CERTIFICATE, JAR/VLA UNDER § 21.183(c) UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS MANUFACTURER AND MODEL Aero-K AK-1A N569K 5 2 3 AIRCRAFT SERIAL NUMBER AK901 4 CATEGORY VLA Special Class AUTHORITY AN D BASIS FOR ISSUANCE This airworthiness certific ate is i ssued pursuant t o the Federal Av iati on Act of 1958 and c erti fies that, as of the dat e of issuance, the aircraft to which iss ued has been ins pect ed and found to conform to the type certif icat e theref or, to be in condition for safe operati on, and has been shown t o meet t he r equi rements of the appli cabl e comprehens ive and detailed airwort hiness c ode as provi de by Annex 8 to the Convent ion of I nter nati onal Civ il Aviat ion, exc ept as noted her ein. Exceptions: N one 6 TERMS AND CONDITIONS Unless sooner surrendered, s uspended, revoked, or a terminat ion date is otherwis e es tabl ished by the Adminis trat or, this airworthiness c ertif icate is effect ive as long as the maintenance, preventative maint enanc e, and alt erati ons are performed in accordance w ith Parts 21, 43, and 91 of the Federal Aviat ion R egulations , as appropriat e, and the airc raft is registered i n the United Stat es. DATE OF ISSUANCE FAA REPRESENTATIVE DESIGNATION NUMBER 01/20/00 Tom Kick Tom Kick NW78 Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000, or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) Page 54 12/18/00 8130.2D CHG 2 FIGURE 3-11. SAMPLE FAA FORM 8100-2, STANDARD AIRWORTHINESS CERTIFICATE, SURPLUS MILITARY AIRCRAFT UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE 1 NATIONALITY AND REGISTRATION MARKS MANUFACTURER AND MODEL 3 Hughes 369A N34561 5 2 AIRCRAFT SERIAL NUMBER 4 CATEGORY Normal 1441 AUTHORITY AN D BASIS FO R ISSUANCE This airworthiness certific ate is i ssued pursuant t o the Federal Av iati on Act of 1958 and c erti fies that, as of the dat e of issuance, the aircraft to which iss ued has been ins pected and found to conform to the type certif icat e theref or, to be in condition for safe operati on, and has been shown t o meet t he r equi rements of t he appli cabl e comprehens ive and detailed airwort hiness c ode as provi de by Annex 8 to the Convent ion of I nter nati onal Civ il Aviat ion, exc ept as noted her ein. Exceptions: N one 6 TERMS AND CONDITIONS Unless sooner surrendered, s uspended, revoked, or a termination date is otherwis e es tabl ished by the Adminis trat or, this airworthiness c ertif icate is effect ive as long as the maintenance, preventative maint enanc e, and alt erati ons are performed in accordance w ith Parts 21, 43, and 91 of the Federal Aviat ion R egulations , as appropriat e, and the airc raft is registered i n the United Stat es. DATE OF ISSUANCE FAA REPRESENTATIVE DESIGNATION NUMBER 01/20/00 B. Potrer B. Porter SW-XX Any alteration, reproduction, or misuse of this certificate may be punishable by a fine not exceeding $1,000, or imprisonment not exceeding 3 years or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORDANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 (8-82) Page 67 8130.2D CHG 2 12/18/00 FIGURE 3-12. SAMPLE FAA FORM 8130-6, APPLICATION FOR AIRWORTHINESS CERTIFICATE, USED AIRCRAFT, NO PREVIOUS U.S. AIRWORTHINESS CERTIFICATE (FACE SIDE) Form Approved O.M.B. No. 2120-0018 APPLICATION FOR AIRWORTHINESS CERTIFICATE U.S. D epartment of Tr ansportation Federal Aviation Administration INSTRUCTIONS - Print or type. Do not write in shaded areas; these are for FAA use only. Submit o riginal only to an authorized FAA Representative . If additional space is required, use an attachment. For special flight permits complete Sections II and VI or VII as applicable. 2. AIRCRAFT BU ILDER'S NAME (Make) 3. AIRCRAFT MODEL DESIGNATION 4. YR. MFR. N12345 Douglas DC-6A 1952 5. AIRCR AFT SER IAL NO. 6. ENGINE BUILDER 'S NAME (Make) 7. ENGINE MODEL DESIGNATION 43218 Pratt & Whitney CB-16 8. NUMBER OF ENGINES 9. PROPELLER BUILDER' S NAME (Make) 10. PROPELLER MODEL DESIGNATION 4 I. AIRCRAFT DES CRIPTION 1. REGISTR ATION MARK Hamilton Standard FAA CODING 43E60-300 11. AIRC RAFT IS (Check if appl icable) IMPORT APPLICATION IS HEREBY MADE FOR: (Check applicabl e items) A 1 B STANDARD AIRWORTH INESS CERTIFICATE (Indicate category) NORMAL UTILITY ACROBATIC TRANSPORT GLIDER BALLOON SPECIAL AIR WORTHINESS CERTIFICATE (Check appropriate items) 2 LIMITED 5 PROVISIONAL (Indicate class) WEATHER CONTROL CARRIAGE OF CARGO 0 OTHER (Specify) RESEARCH AND DEVELOPMENT 2 AMATEUR BUILT 3 EXHIBITION RACING 5 CREW TRAINING TO SHOW COMPLIANCE WITH FAR FERRY FLIGHT FOR REPAIRS, ALTERA TIONS, MAINTENANCE OR STORAGE 2 EVACUATE FROM AREA OF IMPENDING DANGER 3 OPERATION IN EX CESS OF MAXIMUM CERTIF ICATED TAKE -OFF WEIGHT 4 DELIVERING OR EXPORT 6 6 AERIAL ADVER TISING 6 1 C 3 PATROLLING 0 8 AERIAL 5 4 SPECIAL FLIGHT PERMIT (Indi cate oper ati on to be conduc ted, then complete Secti on VI or VII as applicable on rev erse side) 2 FOREST (Wildlife c onservation) 1 EXPERIM ENTAL (Indicate operati on(s) to be c onducted) AGRICULTURE AN D PEST CONTROL 7 4 CLAS S II 4 RESTRICTED (Indi cate operation( s) to be c onduct ed) 3 CLAS S I 2 1 II. CERTIFICATION REQUESTED 1 CUSTOMER DEMONSTRATION FLIGHTS 5 MKT. SURVEY PRODUCTION FLIGHT TESTING MULTIPLE AIR WORTHINESS CERTIFICATE (Check ABOVE "R estri cted Operation" and "Standard" or " Limited," as applicable.) A. REGISTER ED OWNER (As show n on certificate of aircraft regist ration) IF DEALER, CHECK HERE NAME ADDRESS Tiger Aviation Corp. 234 Jane Ave. Jackson, MS 78965