Type Certificate Data Sheet

(+88.4) to (+90.3) at 2900 lb. (+85.6) to (+90.3) at 1793 lb. or less Straight line variation between points given. 2A8 Page 4 of 8 dada edmi Empty Weight Center of Gravity Range None Datum 78 inch forward of leading edge of wing alumas) bre Leveling Means Top longerons in cockpit bay Maximum Weight 2900 lb. Number of Seats 1 at (+135) Maximum Cargo Fuel Capacity 1200 lb. at (+93) For S/N 25-4415 through 25-5521, and 25-7305522 through 25-7405572 and LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up: 38 gallons at (+63) (one fuselage tank) For S/N 25-7405573 through 25-8156024:57 36 gallons at (+102) (two wing tanks) See NOTE 1 for data on system fuel. Oil Capacity 12 quarts at (+30) (94 quarts usable) See NOTE 1 for data on system oil. and lobed and Control Surface Movements Wing Flaps Down 57° Aileron Elevator Rudder Up 23° Up 28° Right 25° Down 23° Ablat Down 15° Left 25° Manufacturer's Serial Numbers 25-4415 through 25-5521, and 25-7305522 through 25-8156024, produced by Piper Aircraft; LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up, produced by LAVIA S.A. See NOTE 5 for airworthiness certification eligibility in the United States. DATA PERTINENT TO ALL MODELS Certification Basis Production Basis Equipment CAR 3 effective May 15, 1956, Amendment 3-1, April 1, 1957. Type Certificate No. 2A8 issued January 5, 1959. Date of Application for Type Certificate May 28, 1957. For aircraft models PA-25-235 S/N LA-235-99501 and up, and PA-25-260 S/N LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up, production under type certificate only. The basic required equipment prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: FAA Approved Airplane Flight Manual: (a) Issue dated May 20, 1959, required for S/N 25-1 and 25-2. (b) Issue dated July 9, 1959, revised February 23, 1960, for S/N 25-3 through 25-1999. (c) Issue dated October 12, 1962, including Revision No. 1, dated November 20, 1962, for Model PA-25-235, S/N 25-02, and 25-2000 through 25-2761. (d) Issue dated October 12, 1962, including Revision No. 1, dated November 20, 1962, and No. 2 dated July 20, 1964, for Model PA-25-235, S/N 25-2762 through 25-2985. Xatorul edini (e) Issue dated October 12, 1962, including Revision No. 1, 2, 3 and 4 for Model PA-25-235, S/N 25-2986 through 25-3384. (f) Issue dated October 12, 1962, including Revision Nos. 1, 2, 3, 4, and 5 for Model PA-25-235, S/N 25-3385 through 25-4171. Equipment, continued Page 5 of 8 2A8 NOTE 1 2. 1. FAA Approved Flight Manual, continued (g) Issue dated October 12, 1962, including Revisions Nos. 1, 2, 3, 4, 5, 6, 7, 8, 9 and 10 for Model PA-25-235, S/N 25-4172 through 25-5521, and 25-7305522 through 25-7405572 and LA-235-99501 and up. (h) Issue dated April 19, 1967, including Revision No. 1 required for Model PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-7405572 and LA-260-98001, LA-260-99002, LA-260-99003, LA-260- 99005 and up. (i) Issue dated February 7, 1974, required for Models PA-25-235 and PA-25-260, S/N 25-7405573 through 25-8156024. Stall warning indictor device per Piper Drawing Nos. 61093 and 61128 on PA-25, S/N 25-3 through 25-1999; Piper Drawing Nos. 64031 and 64253 on PA-25-235, S/N 25-02, and 25-2000 through 25-4171; Piper Drawing Nos. 64031 and 64884 on PA-25-235, S/N 25-4172 through 25-4414, and on PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521 and 25-7305522 through 25-8156024; LA-235-99501 and up; LA-260-98001, LA-260- 99002, LA-260-99003, LA-260-99005 and up. Current weight and balance report, including list of equipment included in certificated empty weight and loading instructions when necessary, must be provided for each aircraft at time of original certification. The certificated empty weight and the corresponding center of gravity locations must include undrainable system oil (not included in oil capacity) and unusable fuel as noted below: Model PA-25: Fuel 14 lb. Oil 3.2 lb. at (-23) at (-47) Model PA-25-235, S/N 25-02, 25-2000 through 25-3384: Fuel Oil 18 lb. 5.2 lb. at (+55) at (+30) Model PA-25-235, S/N 25-3385 through 25-5521, and 25-7305522 through 25-7405572; LA-235-99501 and up: Fuel Oil 12 lb. 5.2 lb. t (+55) at (+30) Model PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-7405572; LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up Fuel 12 lb. at (+55) Oil 5.2 lb. at (+30) Models PA-25-235 and PA-25-260, 25-7405573 through 25-8156024: Fuel Oil 15 lb. 5.2 lb. at (+110) at (+30) Ин NOTE 2.1 The following placards must be displayed: (a) In front and in clear view of the pilot: (1) On Model PA-25, S/N 25-1 through 25-1999: "THIS AIRPLANE MUST BE OPERATED IN THE NORMAL CATEGORY IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS, AND MANUAL. ACROBATIC MANEUVERS (INCLUDING SPINS) PROHIBITED. FOR RESTRICTED CATEGORY OPERATION, REFER TO ADDITIONAL LIMITATIONS." 2A8 NOTE 2(a)(2), continued Page 6 of 8 (2) On Model PA-25-235, S/N 25-02, 25-2000 through 25-2761: "THIS AIRPLANE MUST BE OPERATED IN THE RESTRICTED CATEGORY IN mek COMPLIANCE WITH OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS AND MARKINGS. ACROBATIC MANEUVERS (INCLUDING SPINS) PROHIBITED." (2) On Model PA-25-235, S/N 25-02, 25-2000 through 25-2761, continued Model PA-25-235, S/N 25-02 and 25-2000 through 25-2761 are also eligible for Multiple Airworthiness Certification when all placards are revised to the configuration of S/N 25-2762 through 25-5521, and 25-7305522 through 26-8156024. Airplane Flight Manual equipment Item 1(d) required in lieu of Item 1(c). (3) On Model PA-25-235, S/N 25-2762 through 25-4414; on Model PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-8156024; LA-235-99501 and up and LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up: "THIS AIRPLANE MUST BE OPERATED IN THE RESTRICTED CATEGORY IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS AND MARKINGS. ACROBATIC MANEUVERS (INCLUDING SPINS) PROHIBITED. FOR NORMAL CATEGORY OPERATION, REFER TO FLIGHT MANUAL." (b) On hopper: Model PA-25 Model PA-25-235 "800 lb. maximum" "1200 lb. maximum" "1200 lb. maximum" (c) Model PA-25-260 wold baton about step Models PA-25-235 and PA-25-260 - On check list above instrument panel: "WINDOWS CLOSED" (d) Model PA-25-235, S/N 25-2762 through 25-4414; and LA-235-99501 and up and Model PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-8156024 and Model PA-25- 260, S/N LA260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up - On the instrument panel in full view of the pilot: "ROUGH AIR OR MANEUVERING SPEED 120 M.P.H." (e) On safety panel above instrument panel in full view of pilot: (1)Model PA-25-235, S/N 25-02, 25-2000 through 25-3384: "UNUSABLE FUEL 3 GALLONS. WHEN FUEL QUANTITY INDICATOR READS ZERO, FUEL REMAINING IN TANK CANNOT BE USED SAFELY IN FLIGHT." (2)Model PA-25-235, S/N 25-3385 through 25-4414 and LA-235-99501 and up; Model PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-7405572; and Model PA-25-260, S/N LA-260-98001 and up: "UNUSABLE FUEL 2 GALLONS. WHEN FUEL QUANTITY INDICATOR READS ZERO, FUEL REMAINING IN TANK CANNOT BE USED SAFELY IN FLIGHT." (3)Model PA-25-235 or PA-25-260, S/N 25-7405573 through 25-8156024: "UNUSABLE FUEL 2.5 GALLONS. WHEN FUEL QUANTITY INDICATOR READS ZERO, FUEL REMAINING IN TANK CANNOT BE USED SAFELY IN FLIGHT." (f) On Models PA-25-235 and PA-25-260 - On instrument panel in clear view of the pilot: "NO SMOKING" (g) On Model PA-25-235, S/N 25-2762 through 25-4414; and Model PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-8156024 - In front and in clear view of the TOM pilot: "STALL WARNING SYSTEM INOPERATIVE WHEN MASTER SWITCH IS OFF." MALAMOURQUIA TAMЯOM THE ALCETAS P1096 (h) On Models PA-25-235 and PA-25-260, S/N 25-7405573 through 25-8156024 - Above and near the fuel quantity gauge: ИТАПОЯЗА "FUEL CAPACITY 36 GALLONS" 2001/M Page 7 of 8 2A8 NOTE 3. NOTE 4. NOTE 5 (i) On Models PA-25-235 and PA-25-260, S/N 25-7405573 through 25-8156024 - Adjacent to low fuel level light on auxiliary instrument panel: "LOW FUEL WARNING" The Model PA-25, S/N 25-2 through 25-1999 (Restricted Category) is the same as the Normal Category PA-25 except for installation of spray or dust dispensing equipment. Conversion to duster or sprayer configuration may be accomplished using Piper Instructions, Section XVI of Report 1019. When operating in the Restricted Category, FAA Type Certificate Data Sheet No. 2A10 will apply. (a)Model PA-25-235, S/N 25-2000 through 25-2761 are eligible for Multiple Airworthiness Certification when all placards are revised to the configuration of S/N 25-2762 through 25-5521, and 25-7305522 through 25-8156024. Airplane Flight Manual equipment Item 1(d) required in lieu of Item 1(c). (b)Model PA-25-235, S/N 25-2762 through 25-2985 are eligible for Multiple Airworthiness Certification in the Restricted Category and Normal Category in accordance with CAR 8.21 and Conversion Instructions, Section XVI of Piper Report VB-7, Revision No. 2, dated October 5, 1964. When operating in the Restricted Category, Type Certificate Data Sheet No. 2A10 shall apply. When operating in the Normal Category, Type Certificate Data Sheet No. 2A8 shall apply. (c)Model PA-25-235, S/N 25-2986 through 25-4414 and Model PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-8156024 are eligible for Multiple Airworthiness Certification in the Restricted Category and Normal Category in accordance with CAR 8.21 and Conversion Instructions, Section III of Piper Report VB-42, Revision No. 6, dated February 22, 1967. When operating in the Restricted Category, Type Certificate Data Sheet No. 2A10 shall apply. When operating in the Normal Category, Type Certificate Data Sheet No. 2A8 shall apply. The following S/N are not eligible for Airworthiness Certification in the United States: 25-4894, 25-5027, 25-5030, 25-5033, 25-5057, 25-5066, 25-5069, 25-5072, 25-5075, 25-5097, 25-5100, 25-5102, 25-5106, 25-5269, 25-5271, 25-5273, 25-5275, 25-5284 through 25-5293, 25-5315, 25-5316, 25-5318, 25-5320, 25-5454, 25-5455, 25-5456, 25-5457, 25-7305528, 25-7305530, 25-7305532, 25-7405591, 25-7405596, 25-7405613, 25-7405620, 25-7405631, 25-7405642, 25-7405652, 25-7405658, 25-7405662, 25-7405672, 25-7405679, 25-7405686, 25-7405690, 25-7405692, 25-7405694, 25-7405696, 25-7405698, 25-7405701, 25-7405704, 25-7405705, 25-7405706, 25-7405708, 25-7405714, 25-7405716, 25-7556030, 25-7556035, 25-7556040, 25-7556045, 25-7556050, 25-7556052, 25-7556057, 25-7556062, 25-7556065, 25-7556067, 25-7556069, 25-7556071, 25-7556073, 25-7556075, 25-7556077, 25-7556080, 25-7556090, 25-7556095, 25-7556100, 25-7556105, 25-7556110, 25-7556115, 25-7556120, 25-7556125, 25-7556135, 25-7556140, 25-7556145, 25-7556150, 25-7556153, 25-7556159, 25-7556162, 25-7556166, 25-7556226, 25-7556227, 25-7556228, 25-7556229, 25-7556230, 25-7556231, 25-7556232, 25-7556233, 25-7656078, 25-7656091, 25-7756072 through 25-7756081, 25-7756087 through 25-7756095, 25-7856001 through 25-7856004, 25-7856006, 25-7856008, 25-7856010, 25-7856012, 25-7856016, 25-7856018, 25-7856020, 25-7856022, 25-7856032, 25-7856034, 25-7856036, 25-7856038, 25-7856043, 25-7856045, 25-7856047, 25-7856049, 25-7856055, 25-7856057, 25-7856063, 25-7856065, 25-7856066, 25-7856067, 25-7856069, 25-7856071, 25-7956004, 25-7956006, 25-7956009 through 25-7956012, 25-7956014, 25-7956016, 25-7956019, 25-7956020, 25-7956022, 25-7956025, 25-7956027, 25-7956029, 25-7956031, 25-7956033, 25-7956036, 25-7956038, 25-7956041, 25-7956042, 25-8056004, 25-8056005, 25-8056008, 25-8056009, 25-8056011, 25-8056013, 25-8056016, 25-8056018, 25-8056021, 25-8056022, 25-8056026, 25-8056028, 25-8056041, 25-8056043, 25-8056046, and 25-8056048. 2A8 Page 8 of 8 NOTE 6: Import Requirements: (a) United States airworthiness certificate may be issued on the basis of Argentina Certificate of Airworthiness for Export signed by a representative of Direción Nacional de Aeronavegabilidad containing the following statement: "The aircraft conforms to its U. S. type design (Type Certificate No 2A8) and is in a condition for safe operation." (b) The U. S. airworthiness certification basis for aircraft type certificated under 14 CFR Part 21 section 21.29 and exported by the country of manufacture is section 21.183(c) or 21.185(c). (c)The U. S. airworthiness certification basis for aircraft type certificated under 14 CFR Part 21 section 21.29 and exported from countries other than country of manufacture (e.g., third part country) is section 21.183(d) or 21.185(b). the Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (or equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2. Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for imported aircraft. .....END..... lagu Radekel, pit our wet) atuating a payed computin LEECOFS RL (OREEDEN RE BLAZ 150 000-es 50008-2 TUTION COMUNICACIONES SECRETARIA DE INFRAESTRUCTURA, COMUNICACIONES Y TRANSPORTES AFAC AGENCIA FEDERAL DE AVIACIÓN CIVIL Agencia Federal de Aviación Civil Dirección Ejecutiva de Aviación Dirección de Ingeniería, Normas y Certificación Convalidación No. IA-816/2022 del Certificado de Tipo No. 3A21 La Secretaría de Infraestructura, Comunicaciones y Transportes, con base en las Circulares Obligatorias CO AV- 52.1/22 y CO AV-52.2/22, de fechas 14 de octubre y 10 de noviembre de 2022, respectivamente; a los Artículos 102 Quinquies y 127 del Reglamento de la Ley de Aviación Civil, a través de la Agencia Federal de Aviación Civil, otorga este documento a favor de: The Secretaría de Infraestructura, Comunicaciones y Transportes, based in the Circulares Obligatorias CO AV- 52.1/22 and CO AV-52.2/22, dated October 14, 2022 and November 10, 2022, respectively, and the Articles 102 Quinquies and 127 of the Reglamento de la Ley de Aviación Civil, by means of the Agencia Federal de Aviación Civil, issues this document to: сивоци кеде TEXTRON AVIATION INC. One Cessna Boulevard Wichita, Kansas 67215 USA Convalidando las Hojas de Datos del Certificado de Tipo No. 3A21 Revisión 50, de fecha 18 de noviembre de 2021, emitidas por la Administración Federal de Aviación (FAA). Validating the Type Certificate Data Sheets No. 3A21 Revision 50, dated November 18, 2021, issued by the Federal Aviation Administration (FAA). Lo enunciado a continuación, reúne las especificaciones aplicables para su operación segura de acuerdo con las Normas, Procedimientos y Reglamentaciones requeridas por esta Agencia Federal de Aviación Civil (AFAC). The described below complies with the applicable specifications for safe operation in accordance with the Standards, Procedures and Regulations required by the Agencia Federal de Aviación Civil (AFAC). WEAC CORICOS HO Boulevard Adolfo López Mateos 1990, Colonia Los Alpes, C. P. 01010, Alcaldía Álvaro Obregón, CDMX. T: (55) 5723 9300 www.gob.mx/afac 1 de 13 2022 Flores Año de PRECURSOR DE LA REVOLUCION MEXICANA Magon COMUNICACIONES SECRETARIA DE INFRAESTRUCTURA, COMUNICACIONES Y TRANSPORTES AFAC AGENCIA FEDERAL DE AVIACIÓN CIVIL No. Control AFAC AFAC control No. Modelo Model Categoría Category Números de serie Serial Numbers Marca de Motores Engines Manufacturer Modelos IA-816/2022 210, 4 PCLM Normal 618, 57001 hasta / through 57575 Continental Models Marca de Hélice Propeller Manufacturer Modelos de Hélice Propeller Models IO-470-E Hartzell McCauley D2A36C33/90M-8 o/or HC-A2XF-1/8433-2 D2A34C49/90A-8 o/or D2A34C58/90AT-8 Modelo Model Categoría Category Números de serie Serial Numbers Marca de Motores Engines Manufacturer Modelos Models Marca de Hélice Propeller Manufacturer Modelos de Hélice Propeller Models 210A, 4 PCLM Normal 616, 21057576 hasta / through 21057840 Hartzell HC-A2XF-1/8433-2 Continental 10-470-E McCauley D2A36C33/90M-8 o/or D2A34C49/90A-8 o/or D2A34C58/90AT-8 gevangen GAIL Boulevard Adolfo López Mateos 1990, Colonia Los Alpes, C. P. 01010, Alcaldía Álvaro Obregón, CDMX. T: (55) 5723 9300 www.gob.mx/afac Ricardo 2022 Flores Magon Año de PRECURSOR DE LA REVOLUCION MEXICANA 2 de 13