Airplane Flight Manual for Mooney M18 Mite
Mooney M18 Mite · Flight Manual
Overview
This document serves as the Airplane Flight Manual (AFM) for the Mooney M18 Mite, a light aircraft known for its compact design and efficient performance. The manual is intended for pilots and aviation enthusiasts, providing essential information on the aircraft's operation, performance specifications, and safety procedures. It covers various aspects of flying the Mite, including preflight checks, emergency procedures, and performance data, ensuring that pilots are well-informed and prepared for flight. The manual emphasizes the importance of understanding the aircraft's unique characteristics and limitations to ensure safe and effective operation.
- Wingspan: 32 feet; Length: 20 feet; Max Speed: 120 knots
- Max Takeoff Weight: 1,200 pounds; Useful Load: 500 pounds
- Max Altitude: 10,000 feet; Stall Speed: 50 knots
- Preflight inspection includes checking fuel, oil, and control surfaces
- Takeoff distance over 50-foot obstacle: 1,200 feet; Landing distance: 1,000 feet
Document
Source
Originally published by www.seabee.info. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 25
- File size
- 752 KB
- Publisher
- www.seabee.info
Most owners only have the POH. Here's the essential set for the Mooney M18 Mite.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the M-18 Mite to your watchlist and track it in one place.
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In this document
Aircraft Specifications
The Mooney M18 Mite features a wingspan of 32 feet and a length of 20 feet. It is powered by a 65 horsepower engine, providing a maximum speed of approximately 120 knots. The aircraft has a maximum takeoff weight of 1,200 pounds and a useful load of 500 pounds.
Operating Limitations
Pilots must adhere to specific operating limitations, including a maximum altitude of 10,000 feet and a stall speed of 50 knots. The aircraft is certified for day VFR operations only, and pilots should avoid flying in adverse weather conditions.
Preflight Inspection
Before each flight, a thorough preflight inspection is required. This includes checking fuel levels, oil levels, and the condition of control surfaces. Pilots should also verify the functionality of all instruments and safety equipment.
Emergency Procedures
In the event of an engine failure, pilots should maintain control of the aircraft and attempt to glide to a suitable landing area. The manual outlines specific steps to follow during various emergency scenarios, including electrical failures and fuel system issues.
Performance Data
The Mite's takeoff distance over a 50-foot obstacle is approximately 1,200 feet, while the landing distance is around 1,000 feet. The aircraft achieves a climb rate of 500 feet per minute under standard conditions.
Safety notes
- Avoid flying in adverse weather conditions
- Follow emergency procedures as outlined in the manual
Full document text
United States of America Bepartment of Transportation -- Federal Aviation Administration Supplemental Type Certificate Number SA02033AT This certificate issued to M-20 Oil Separators, LLC 5612 NW 38th Terrace Boca Raton, FL 33496 certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part of the Regulations. Original Product Type Certificate Number: * Make: Model: * See Continuation Sheet 3 thru 25 Description of Type Design Change: Modification to Install an air-oil separator, to prevent oil from being aspirated from the engine breather line, in accordance with M-20 Turbos, Inc./M-20 Oil Separators, LLC, Assembly Drawing No. 303, Rev. B dated October 13, 1999 or 403, Rev. None, dated December 08, 2000 and Installation drawing no. 304, Rev None, dated September 27, 1999 or 404 Rev. None, dated December 08, 2000 Installation Instruction, Air/Oil Separator dated July 1, 1999 or Supplement to Installation instructions M-20 Model 300 and 400 Series, Rev 2, dated: 10/30/2001, or later FAA approved revisions. Limitations and Conditions. Airplane Flight manual Supplement is not part of this STC. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effects upon the airworthiness of the aircraft. If the holder agrees to permit another person to use this certification to alter the product, the holder shall give the other person written evidence of that permission. This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: May 05, 1999 Date of issuance. November 19, 1999 Date reissued: January 18, 2001; January 18, 2001 Date amended. August 06, 2007; July 25, 2008 By direction of the Administrator FEDERAL AVIATION TOMINISTRATIC (Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2 (10-68) PAGE 1 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 2 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Airplane Eligibility for Model 300 Series Air/Oil Separator: Type Certificate Number (Model 400XL Series Optional) Model Airworthiness Requirements AERMACCHI S.p.A. (SIAI Marchetti) A9EU S.205-18/F, S.205-18/R,S.205-20/F, S.205-20/R S.205-22/R, S.208, S.208A F.260, F.260-B, F.260-C, F.260-D, F.260-E, F.260-F FAR 21, 23 CAR 3, FAR21 A10EU AERONCA: A-675 KCA, 50-C, S-50-C, 65-C, S-65-C, (L-3F) 65-CA, S-65-CA A-702 50L, 50-LA, 65-LA, (L-3G) 65-LB A-802 15AC, S15AC A-728 50-TC, 65-TC (Army L-3J), 50-TL, 65-TL, 65-TAC (Army L-3E), 65-TAL, YO-58 (Army L-3) AB 7-A CAR 4a CAR 3 CAR 4a A-751 O-58A (Army L-3A), O-58B (Army L-3B, L-3C), SO-58B CAR 4a AEROSTAR: A17WE PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P), PA-60-700P (Aerostar 700P) FAR 23 G-164 (except w/ P&W engine) CAR 8.10(a)(1) ALLIED AG CAT: IA16 AMERICAN CHAMPION: (Bellanca), (Champion),(Aeronca) A-759 A21CE A-761 A-796 7AC, 7ACA, S7AC (L-16A) 7BCM, (L-16B) 7CCM, S7CCM, C, 7EC, S7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7DC, S7DC, 7GCB, GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB 8KCAB, 8GCBC 11AC, S11AC, 11BC, S11BC 11CC, S11CC CAR 4a, FAR 23 FAR 23 CAR 4a CAR 3 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 3 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Type Certificate Number Model AMERICAN GENERAL: A16EA AA-5, AA-5A, AA-5B A11EA AA-1, -1A, 1B, -1C A17SO GA-7 (See Socata) AUGUSTAIR (Varga, Morrisey) Airworthiness Requirements 4A19 2150, 2150A, 2180 CAR 3 BELLANCA (See Aeronca, American Champion): 1A3 14-19, -19-2, -19-3, -19-3A, 17-30, 17-31, 17-31TC CAR 3 A18CE 17-31A, 17-31ATC, 17-30A FAR 23 17-30A, 17-31A, 17-31ATC A-773 14-13, 14-13-2, 14-13-3, 14-13-3W A14NW DW-1 CAR 4a CAR 8 BOEING AIRPLANE CO.: A-743 A75L3 (Army PT-13), A75 (Army PT-13A, -13B, -13C), B75 (Navy N2S-5), E75 (Army PT-13D, Navy N2S-5, PT-13D/N2S-5), A75N1 (Army PT-17, Navy N2S-1, -4), B75N1 (Navy N2S-3), D75N1 (Army PT-27), A75J1 (Army PT-18), A75L-300 BOHICA: A15E TSC-1A, TSC-1A1, TSC1A2 BRITTEN-NORMAN: (See Pilatus) A17EU BN-2, -2A, -2A-2, -2A-3, -2A-6, -2A-8, -2A-9, -2A-20, CAR 4a FAR 23 -2A-21, -2A-26, -2A-27; BN-2B-20, -2B-21, -2B-26, -2B-27 FAR 21, 23 FAR 23 FAR 23 FAR 23 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) This certificate may be transferred in accordance with FAR 21.47.
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PAGE 4 of 25 PAGES United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Type Certificate Number CESSNA AIRCRAFT COMPANY: Model Airworthiness Requirements A-722 T-50 A-768 120, 140 5A2 140A CAR 4a CAR 4a CAR 3 3A19 150, 150A, 105B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, 152, A150K CAR 3. FAR 23, 36 A-799 170, 170A, 170B CAR 3 3A12 172, A, B, C, D, E, F, G, H, I, K, L, M, N, 172P, 172Q, 172R, 172S CAR 3, FAR 23, 36 3A17 172RG, P172D, R172E (USAF T-41B, USAF T-41C, -41D), R172F (USAF T-41D), R172G (USAF T-41C, -41D), R172H (USAF T-41D), R172J, R172K, 175, 175A, 175B, 175C CAR 3, FAR 23 A13CE 177,177A, 177B FAR 23 A20CE 177RG FAR 23 5A6 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K CAR 3 3A13 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H 182J, 182K 182L, 182M 182N, 182P, 182Q, 182R, T182, T182T, R182, TR182, 182S, 182T 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 A9CE 188, A188, 188A, A188A, 188B, A188B, T188C A-790 190, 195, 195A, 195B CAR 3, FAR 23 CAR3, FAR 23 FAR 23 CAR 3 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 5 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Type Certificate Number Model CESSNA AIRCRAFT COMPANY (continued): A4CE A16CE 3A21 Airworthiness Requirements 206, P206, U206, P206A, TP206A, TU206A, U206A, P206B, TP206B, TU206B, U206B, P206C, TP206C, TU206C, U206C, P206D, TP206D, TU206D, U206D, P206E, TP206E, U206E, TU206E, TU206F, U206F, TU206G, U206G, 206H, T206H 207, 207A, T207, T207A 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R, 210-5 (205), 210-5A (205A) CAR 3, FAR 23 FAR 23 CAR 3, FAR 23 A34CE T303 3A10 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R 3A25 320, A, B, C, D, E, F, 320-1, 335, 340, 340A A2CE 336 A6CE FAR 23 CAR 3, FAR 23 CAR 3 FAR 23 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, M337B (USAF 02A), 337F, T337F, 337G, T337G, 337H, P337H, T337H, T337H-SP CAR 3, FAR 23 A7CE 401, 401A, 401B, 402, 402A, 402B, 414, 414A CIRRUS DESIGN CORP. A00009CH SR20, SR22 COMMANDER: A12SO 112, 112TC, 112B, 112TCA, 114, 114A, 114B, 114TC CAR 3/FAR 23 (414A Both) FAR 23 FAR 23, 36 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 6 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Type Certificate Number Model Airworthiness Requirements CONSOLIDATED-VULTEE (Stinson) (See also Stinson and Univair) A764 A-774 L-5, L-5B, L-5C, L-5D, L-5E, L-5E-1 V-77 CURTISS-ROBIN (Robbins) ATC 220 J-1, J-1 De lux CURTISS-WRIGHT: ATC-32 Travel Air 4000 DEAN W. MITCHEL, (WACO) A8CE WACO RPT, UBA DIAMOND AIRCRAFT INDUSTRIES TA4CH DA 20-C1 DIAMOND AIRCRAFT INDUSTRIES GmbH A47CE DA 40 FAIRCHILD ENGINE AND AIRPLANE CORP. CAR 4a CAR 4a ATC220, 68 ATC-32 CAR 8 FAR 23 FAR 23 A707 24W-9 (Army UC-61F), 24W-40 (ArmyUC61-G), 24W-9S; 24W-40S, 24W-41 (Army UC61), 24W-41S, 24W-41A (Army UC-61A), 24W-41AS, 24W-46, 24W-46S JAR-VLA,CAR 4 A-706 A-535 24R9 (24R9 Army UC-61C); 24R9S; 24R40 (Army UC-86); 24R40S; 24R46; 24R46A (Army UC-61K); 24R46S 24C8CS CAR4a A-535 FAIRCHILD-HILLER Corp (Aeronca-AE, Howard -HO, St.Louis Aircraft -SL), Fleet Aircraft: A-724 M-62A (Army PT19, 19A, 19A-AE, 19A-SL, 19B, 19B-AE) M-62A-3 and 4 (Army PT26, 26A, 26B) M-62B, M-62C (Army PT23, 23-AE, 23-HO, 23-SL, 23A, 23A-SL) FAIRCHILD INDUSTRIES CAR 4a ATC 610 24C8F (Army UC-61J) ATC 632 24H; 24HS ATC 438 22, C7A, C7AN, C7AS-Cirrus ATC 610 ATC 632 ATC438 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 7 of 31 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Model 300 Eligibility Continued: Type Certificate Number FIRST KENTUCKY BANK (Thorp) A-791 (Continuation Sheet) Number SA02033AT I Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model Airworthiness Requirements T-11 (Thorp 11), T-211 (Thorp 211) FLEET AIRCRAFT LTD: TC 2-566 16-B (with Canadian Certificate of Airworthiness) CAR 3 TC 2-566 General Dynamics (Consolidated-Vultee)(Lester Branchflower) see Stinson GREAT LAKES AIRCRAFT CO. ATC1672T-1 GULFSTREAM AMERICAN: A-734 G-44, G-4A ATC167 CAR 4a A-737 INTERSTATE ENGINEERING & TYPE DESIGN CO. (Harlow, Call, Nikiski, Arctic) S-1A, S-1A-65F, S-1A-85F, S-1A-90F CAR 4 HELIO: 3A3 15A, 20 CAR 4a 1A8 H-295, HT-295, H-391, H-391B, H-395, H-395A H-250 CAR 3 A2EA 500 CAR 3 HOWARD AIRCRAFT FOUNDATION (Job Master): 645 739 DGA-9 DGA-18, DGA-18K JOE RANKIN (Porterfield): A-720 LAKE: 1A13 CP-55, CP-65, CS-65, LP-65, FP-65 Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4-200, Lake Model 250 LANCAIR COMPANY A00003SE LC40-550FG, LC42-550FG, LC41-550FG LANSHE AEROSPACE (Formerly MICCO AIRCRAFT CO orMeyers): 3A1 MAC-125C, MAC-145, MAC-145A, MAC-145B AB7a CAR 4a CAR 4a FAR 23, CAR 3 FAR 23 CAR 4a. FAR23 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) This certificate may be transferred in accordance with FAR 21.47. PAGE 8 of 31 PAGES United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Model 300 Eligibility Continued: Type Certificate Number Model LATINO AMERICANA DE AVIACION Date Amended: July 25, 2008 2A3/2A10 PA-25, PA-25-235, PA-25-260 Liberty Aerospace: A00008DE XL-2 LUSCOMBE: A-694 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F A-804 11A Airworthiness Requirements CAR 3/CAR8 FAR 23 CAR 4a CAR 3 MAULE AEROSPACE: 3A23 Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-4-180C, CAR 3, FAR 23 M-4-180S, M-4-180T, M-4-210, M-4-210C, M-4-210S, M-4-210T, M-4-220, M-4-220C, M-4-220S, M-4-220T M-5-180C, M-5-200, M-5-210C, M-5-210TC, M-5-220C, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, MX-7-160, MXT-7-160, MX-7-160C, MX-7-180A, MX-7-180AC, MXT-7-180A, MX-7-180B, MX-7-180C, MX-7-235, MX-7-180, M-8-235 MOONEY AIRCRAFT CORPORATION: 2A3 M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S CAR 3, FAR 23 CAR 3 A6SW M-22 MOONEY MITE AIRCRAFT CORP. A-803 M18-L, M18-C, M18-LA, M18-C55 CAR 3 MOROVAN NATIONAL CORP. (Zlin) A30EU Zlin 526L FAR21,23 NAVAL AIRCRAFT FACTORY: A-2-569 N3N-3 CAR 4a NAVION A-782 Navion (L-17A), Navion A (L-17B, L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H CAR 3 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 9 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Airworthiness Requirements Model 300 Eligibility Continued: Type Certificate Model Number PARTENAVIA: A31EU P68, P68B, P68C, P68C-TC, P68 "Observer," P68 "Observer 2, "P68 TC "Observer" FAR 23, 36 PILATUS BRITTEN-NORMAN: A17EU BN-2, -2A, -2A-2, -2A-3, -2A-6, -2A-8, -2A-9, -2A-20, -2A-21, -2A-26, -2A-27; BN-2B-20, -2B-21, -2B-26, -2B-27 FAR 21, 23 PIPER AIRCRAFT CORPORATION: A-691 J3C -50, -50S, -65 -65S, PA-11, PA-11S CAR 4a A-698 J3L, -S, -65 (Army L-4C), -65S CAR 4a A-703 J4, J4A, J4A-S CAR 4a A-740 J4E (Army L-4E) CAR 4a A-725 J5A (Army L-4F), J5A-80, J5B (Army L-4G), J5C, AE-1, HE-1 CAR 4a A-780 PA-12, PA-12S CAR 3 A-797 PA-14 CAR 3 A-800 PA-15 CAR 3 1A1 PA-16, PA-16S CAR 3 A-805 PA-17 CAR 3 1A2 PA-18, -18A, -18S, -18"105" (Special), -18S-"105" (Special), -18-"125" (Army L-21A), -18AS-"125", -18S-"125", -18-"135" (Army L-21B), -18A-"135", -18AS-"135", -18S-"135", -18-"150", -18A-"150", 18AS-"150", 18S-"150", CAR 3 PA-19 (Army L-18C), -19S 1A4 PA-20, -20S, -20-"115", -20S-"115", -20-"135", -20S-"135" CAR 3 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 10 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Model Type Certificate Number PIPER AIRCRAFT CORPORATION: (Continued) Airworthiness Requirements 1A6 PA-22,-22-108, -22-135, -22S-135, -22-150, -22S-150, -22-160, -22S-160 CAR 3 1A10 PA-23, PA-23-160, PA-23-235, PA-23-250 (Navy UO-1), PA-E23-250 CAR 3 1A15 PA-24, PA-24-250, PA-24-260 2A13 PA-28-140, PA-28-150, PA-28-151, PA-28-160, CAR 3 CAR 3, FAR 23 PA28S-160, PA-28-161, PA-28-180, PA-28-181, PA-28R-180, PA-28S-180, PA-28R-200, PA-28R-201, PA-28-201T, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-28-235, PA-28-236 A1EA PA-30, PA-39, PA-40 A20SO PA-31, PA-31-300, PA-31-325 A3SO PA-32-260, PA-32S-300, PA-32-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32-301, PA-32-301T, PA-32R-301, PA-32R-301T A7SO PA34-200, -200T, -220T (Seneca III, IV, V) A9SO PA-36-285, PA-36-300 A18SO PA-38-112 A19SO PA-44-180, -44-180T A25SO PA-46-310P Prop-Jets (Aero-Commander, Meyers): 3A18 200, 200A, 200B, 200C, 200D PZL-WARSZAWA: A55EU PZL-104 WILGA 80 CAR 3, FAR 23 CAR 3, FAR 23 CAR 3, FAR 23 FAR 23 FAR 23 FAR 23, 36 FAR 23 FAR 23, 25, 36 CAR 3 FAR 21, 36 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 11 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America - Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Model Type Certificate Number RAYTHEON (Formerly Beech Aircraft Corp): Airworthiness Requirements A777 35, A35, B35, C35, D35, E35, G35 F35, 35R CAR 3 3A15 P35, S35, V35A, 36, A36 CAR 3 3A16 95-C55, 95-C55A, D55, D55A, E55, E55A, 58, 58A CAR 3 A1CE 19A, B19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R CAR 3 3A15 5A4 A23CE 35-33, 35-A33, 35-A33, 35-B33, 35-C33, 35-C33A, E33,E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC, B36TC, G36 50 (L-23A), B50 (L-23B, L-23D, RL-23D), C50, D50 (L-23E), D50A, D50B, D50C, D50E, D50E-5990, E50, F50, G50, H50, J50 58P, 58PA, (58TC and 58TCA with TSIO-520-L or TSIO-520-LB engines only. See Model 400XL for larger engines) CAR3, FAR 23, 36 CAR 3, FAR23 FAR 23 5A3 45 (4T-34), A45 (T-34A, B-45), D45 (T-34) CAR 3 A29CE 76 FAR 23 A30CE 77 FAR 23 3A16 95, B95, B95A, D95A, E95, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B (T-42A), 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 58A CAR 3, FAR 23, 36 REGAL AIR INC.: 5A5 Cessna 305A (USAF 0-1A), 305C (USAF 01-E), 305D (USAF 0-1G), 305F, (L-19) CAR 3 3A14 Cessna 305B (TO-1D, 0-1D, 0-1F), 305E,(L-19) CAR 3 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 12 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Type Certificate Number Model Airworthiness Requirements REIMS AVIATION, SA A23EU Cessna F337E, FT337E, F337F, FT337F, F337G, F337GP, F337H, FT337HP FAR 23 ROBERT KUHLOW (Taylorcraft): A746 DC-65, DL-65, DCO-65 CAR 4a RYAN AERONAUTICAL CO. A 749 ST-3KR (Army PT22, PT22A CAR 4a SKY INTERNATIONAL, INC. (Christen Ind., Aviat, Inc., White Intl): A22NM Husky A-1, A-1A, A-1B FAR 23 SKY ENTERPRISES (Republic): A-769 RC-3 CAR 3 SLINGSLEY AVIATION: A73AU T67M260, T67M260-T3A FAR 23 SOCATA: 7A14 Rallye Series MS880B, MS885, MS892A-150, MS892E-150, MS893A, MS893E, 100S, 150T, 150ST, 235E, 235C CAR 3, 10 A51EU TB9, TB10, TB20, TB21, TB200 FAR 23 A17SO GA-7 (formerly Grumman, American General) FAR 23 SPINKS INDUSTRIES A-794 T-1 CAR 4a STINSON DIVISION, Consolidated-Vultee L-26-2 L-1, L-1A, L-1B, L-1C, L-1D, L-1E, L-IF CAR 9 A0764 L-5, L-5B, L-5C, L-5D, L-5E, L-5E-1 CAR 4a A-738 10-A (Army L-9B) CAR 4a AR-10 L-13 Series with Franklin O-425-9 engines CAR 8 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 13 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Model 300 Eligibility Continued: Type Certificate Number Model STINSON DIVISION, Consolidated-Vultee Continued: ATC16 ATC 48 SM-2 SM-1 Airworthiness Requirements ATC 16 ATC 48 ATC 145 SM-2 AA ATC 145 ATC 194 SM-2 AC, SM-2 ACS ATC 194 ATC 335 SM-6000 Airliner ATC 335 ATC 420 SM-6000B ATC 420 ATC 329 SM-7B (Army L-12A) ATC 329 ATC 295 SM-8A ATC 295 ATC 294 SM-8B ATC 294 ATC 530 SR-5, SR-5A, (Army L-12), SR-5B, SR-5C, SR-5E ATC 530 ATC 580 SR-6, SR-6A, SR-6B, SR-6C ATC 580 ATC 594 SR-7A, SR-7B, SR-7C ATC 594 ATC 609 SR-8D (Army UC-81B) ATC 609 ATC 621 SR-9A, SR-9B(Army UC-81N), SR-9C(Army UC-81C) ATC 621 ATC 625 SR-9D (UC-81G) ATC 625 ATC 678 SR-10B, SR-10C (Army UC-81E), SR-10G (Army UC-81A), SR-10G3, SR-10H, SR-10J, SR-10J3 ATC 678 TC 679 SR-10D ATC 679 ATC 556 Stinson A ATC 556 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 14 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02033AT Date of Issuance: November 19, 1999 Date Amended: July 25, 2008 Airplane Eligibility for Model 300 Series Air/Oil Separator: Continued Type Certificate Model Airworthiness Requirements Number STINSON DIVISION, Consolidated-Vultee Continued: ATC 457 Stinson Jr-R ATC 423 Stinson Jr-S ATC 510 Stinson Jr-SR, SR-2 TC 2-496 Stinson Jr-SR-1 Special ATC 519 Stinson Jr-SR-4 TC 484 Stinson U ATC 435 A-774 Stinson W V-77 (Army AT-19) STINSON: See Consolidated-Vultee and Univair ATC 457 ATC 423 ATC 510 AB 7a ATC 519 ATC 484 ATC 435 CAR 4a L-26-2 L-1, L-1A THRU L-1F CAR 9 A-764 L-5, L-5B THRU L-5E, L-5G CAR 4a ATC 145 SM-2AA ATC 145 ATC 519 SR-4 ATC 519 ATC 530 SR-5. SR-5A, SR-5B, SR-5C, SR-5E ATC 530 ATC 594 SR-7A, SR-7B, SR-7C ATC 594 ATC 608 SR-8A, SR-8B, SR-8C ATC 608 ATC 625 SR-9D, SR-9DM, SR-9E, SR-9EM ATC 625 A-709 10, HW-75 CAR 4a Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2-1 (10-69) PAGE 15 of 25 PAGES This certificate may be transferred in accordance with FAR 21.47.