Supplemental Type Certificate for CESSNA 310F
CESSNA 310F · Supplemental Type Certificate
Overview
This document serves as a Supplemental Type Certificate (STC) for the Cessna 310F aircraft. It outlines the modifications and alterations approved for this specific aircraft model, ensuring compliance with safety and performance standards set by aviation authorities. The STC is intended for use by aircraft owners, maintenance personnel, and regulatory bodies to verify that the modifications have been properly documented and approved. Key information includes details about the modifications, installation instructions, and any limitations or operational considerations that must be adhered to when operating the aircraft with the approved changes.
- This document is a Supplemental Type Certificate (STC) for the Cessna 310F.
- It outlines approved modifications and alterations for the aircraft.
- Compliance with the STC is mandatory for maintaining airworthiness.
- Specific limitations and operational conditions are detailed within the document.
- Proper documentation is required to verify compliance with the STC.
Document
Source
Originally published by www.jpinstruments.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Pages
- 7
- File size
- 1.2 MB
- Publisher
- www.jpinstruments.com
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 310F.
CESSNA 310F for sale now
Free — save the 310F to your watchlist and track it in one place.
More CESSNA 310Fmanuals & documents
See all 45 →- CLEVELAND WHEELS & BRAKESParts Catalog
- Know When to Feather Your PropellerPilot's Operating Handbook
- EL-92 / 1 October 2023 Page 1 of 21 ELIGIBILITY LIST RevisionParts Catalog
- FAA Approved Model List For ADS-B Out Airworthiness Approval Peregrine STC NO. SA00756DEType Certificate
- Aircraft Aeroplanes General – Small (Up to 5700 kg MCTOW)Service Bulletins
- AC 21-34 v1.1 - Aircraft flight manuals - Civil Aviation Safety AuthorityAircraft Flight Manual
- 4910-13-P - Federal RegisterAirworthiness Directives
- TO 1-1-3 TECHNICAL MANUAL INSPECTION AND REPAIR OF AIRCRAFT INTEGRAL TANKS AND FUEL CELLSOther Documents
- OIL - TRANSMITTAL OF CONTINENTAL AEROSPACE TECHNOLOGIES CSB07-1A CONNECTING ROD PISTON PIN BUSHING INSPECTIONParts Catalog
- Goodrich® De-Icers Textron Aviation Replacement Part List Pneumatic de-ice boots Care products Prop-de-icers and hardware (RPL) Catalog 2021Parts Catalog
- FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA02511SE FOR CIES INC. CC284022 SERIES TSO C55a FUEL QUANTITY SENDERSSupplemental Type Certificate
- Canada (TCCA) Validation of the CGR-30C STCType Certificate
If you fly the CESSNA 310F, you may also be researching these.
In this document
Introduction
The introduction section provides an overview of the purpose of the STC, detailing the specific modifications approved for the Cessna 310F. It emphasizes the importance of following the guidelines set forth in the document to maintain airworthiness.
Modifications Approved
This section lists the specific modifications that have been approved under the STC for the Cessna 310F. Each modification is described in detail, including the installation process and any required inspections.
Limitations and Conditions
Here, the document outlines any limitations or conditions that must be observed when operating the Cessna 310F with the approved modifications. This includes weight restrictions, operational limitations, and maintenance requirements.
Compliance and Documentation
This section emphasizes the need for proper documentation to ensure compliance with the STC. It details the records that must be kept and the procedures for reporting any discrepancies or issues that arise.
Safety notes
- Ensure all modifications are installed as per the guidelines in the STC to maintain safety standards.
- Regular inspections are required to ensure continued compliance with the STC.
Full document text
EASA European Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10052045 This Supplemental Type Certificate is issued by EASA, acting in accordance with Regulation (EC) No. 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to J.P. INSTRUMENTS, INC P.O.BOX. 7033 HUNTINGTON BEACH CA 92646 USA and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and environmental protection requirements when operated within the conditions and limitations specified below: Original Type Certificate Number: SEE EASA APPROVED MODEL LIST Type Certificate Holder: SEE EASA APPROVED MODEL LIST Type Design - Model: SEE EASA APPROVED MODEL LIST Original STC Number : FAA STC SA00432SE Description of Design Change: Fuel flow transducer EASA Certification Basis: The certification Basis (CB) for the original product remains applicable to this certificate/approval. The requirements for environmental protection and the associated certified noise and/or emissions levels of the original product are unchanged and remain applicable to this certificate/approval. See Continuation Sheet(s) For the European Aviation Safety Agency, Date of issue: 04 February 2015 Note: Yves MORIER Head of General Aviation and Remotely Piloted Aircraft Systems (RPAS) The following numbers are listed on the certificate: SUPPLEMENTAL TYPE CERTIFICATE - 10052045 J.P. INSTRUMENTS, INC TE.STC.00091-003 Copyright European Aviation Safety Agency. All rights reserved. 1/2 EASA European Aviation Safety Agency Associated Technical Documentation: J.P. Instruments (JPI) Fuel Flow Installation Manual Report # 503, Revision B, dated March 14 1997 JPI Drawing List, Report No. 500, Revision B, dated 14 March 1997 or later revisions of the above listed documents approved by EASA in accordance with EASA ED Decision 2004/04/CF (or subsequent revisions of this decision)" and/or the Technical Implementation Procedures of EU/USA Bilateral Agreement. Limitations/Conditions: Approval of this change in type design applies to the above model aircraft only This STC requires the installation of JPI fuel flow instrument via STC SA2586NM Prior to the installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/or repair will introduce no adverse effect upon the airworthiness of the product - end - Note: The following numbers are listed on the certificate: SUPPLEMENTAL TYPE CERTIFICATE - 10052045 - J.P. INSTRUMENTS, INC TE.STC.00091-003 Copyright European Aviation Safety Agency. All rights reserved. 2/2 - EASA Approved Model List (AML) 10052045 J.P. INSTRUMENTS, INC AIRCRAFT MODEL EASA ITEM AIRCRAFT MAKE A. SINGLE ENGINE AIRCRAFT (ITEMS 1-94) B. TWIN ENGINE AIRCRAFT (ITEMS 95-127) TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION SINGLE ENGINE AERMACCHI S.p.A. 1. 2. Aero Commander 3. ALEXANDRIA AIRCRAFT 4. American Champion (Bellanca)(Champion) 5. 6. AUGUSTAIR (Morrisey) (Varga) 7. Aviat Aircraft, Inc. 8. Aviat Aircraft Inc. 9. Beechcraft F.260, F.260B, F.260C, F.260D, F.260E, F.260F. 100-180. EASA.A.586 CAR 3 FAR 23 1A21 CAR 3 17-30, 17-31. 1A3 CAR 3 8GCBC, 8KCAB. A21CE FAR 23 American Champion (Bellanca)(Champion) (Aeronca) 7AC, 7DC, 7ECA, 7GCBC, 7GCAA, 7GCBA, 7KCAB. A-759 CAR 4a 2150A. S-2B. 4A19 CAR 3 A8SO FAR 23 A-1, A-1A, A-1B, A-1C-180, A-1C-200. A22NM FAR 23 10. Beechcraft 19A, B19, A23-19, M19A, A24R, B24R, C24R, B23, C23. 35-33, 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. G36, A36TC, and B36TC. A1CE CAR 3 3A15 CAR 3 11. CESSNA 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, 152, A152. 3A19 CAR 3 CESSNA CAR 3 12. FR172E, FR172F, FR172G, FR172H, FR172J. A18EU FAR 21.29 CESSNA 13. 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 1721, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S. CAR 3 3A12 FAR 23 CESSNA 14. 172RG, R172E, R172F, R172G, R172H, R172J, R172K, 175, 175A, 175B, 175C, P172D. 3A17 CAR 3 15. CESSNA 177, 177A, 177B. A13CE FAR 23 16. CESSNA 177RG. A20CE FAR 23 17. CESSNA 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K. 5A6 CAR 3 CESSNA 18. 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 1825, 182T, T182T, R182, TR182, T182. 3A13 CAR 3 The following numbers are listed on the certificate: EASA current Project Number: 0010033199-001 STC APPROVAL-10052045-J.P. INSTRUMENTS, INC - EASA Approved Model List (AML) Note: 1/5 ITEM AIRCRAFT MAKE 19. CESSNA CESSNA 20. 21. CESSNA CESSNA 22. EASA Approved Model List (AML) 10052045 J.P. INSTRUMENTS, INC AIRCRAFT MODEL A. SINGLE ENGINE AIRCRAFT (ITEMS 1-94) B. TWIN ENGINE AIRCRAFT (ITEMS 95-127) 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F. 206, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, 206H, T206H, TU206G, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G. 207, 207A, T207, T207A. 210, 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R, P210N, P210R, T210F, T210G, T210H, T210K, T210L, T210M, T210N, T210R. 210-5 (205), 210-5A (205A). LC40-550FG, LC41-550FG. SR20, SR22. 23. CESSNA 24. Cirrus Design Corporation 25. COMMANDER 112,112B, 112TC, 112TCA, 114, 114A, 114B, 114TC. 26. DeHavilland Support Ltd. (Beagle) B.121 Series 1, B.121 Series 2, B.121 Series 3. 27. DIAMOND 28. DIAMOND 29. EXTRA 30. EXTRA 31. GA 8 Airvan (Pty) Ltd. DA40, DA40F. DA20-A1, DA20-C1. EA-400. EA-300, EA-300S, EA-300L, EA-300/200. GA8-TC320. 32. GENERAL AVIA 33. Helio Aircraft, LLC 34.
Show full textShow less
Interceptor (Aero Commander), (Meyers) (Interceptor) 35. LAVIA S.A. F22B, F22C. H-295, HT-295, H-395, H-391, B, H-800. 200B, 200C, 200D. PA-25-235, PA-25-260. Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033199-001 STC APPROVAL-10052045-J.P. INSTRUMENTS, INC - EASA Approved Model List (AML) 2/5 TYPE CERTIFICATE NUMBER CERTIFIGATION BASIS FOR ALTERATION 3A24 CAR 3 A4CE CAR 3 A16CE FAR 23 3A21 CAR 3 A00003SE FAR 23 EASA.IM.A.007 FAR 23 A12SO FAR 23 FAR 21.29 A22EU FAR 23 uropean Aviation Safety Agency EASA EASA.IM.A.223 EASA.A.022 FAR.21.29 FAR 23 FAR.21.29 EASA.A.011 FAR 23 FAR 21.29 EASA.A.362 FAR 23 EASA.IM.A.042 FAR 23 A75EU FAR 23 1A8 CAR 3 3A18 CAR 3 AR AV-0004 CAR 3 ITEM AIRCRAFT MAKE EASA Approved Model List (AML) 10052045 J.P. INSTRUMENTS, INC AIRCRAFT MODEL A. SINGLE ENGINE AIRCRAFT (ITEMS 1-94) B. TWIN ENGINE AIRCRAFT (ITEMS 95-127) TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION EASA 36. MAULE 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-5-235C, M-6-235, MT-7-235, MT-7-260, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, MX-7-180, MX-7- EASA.IM.A.018 180A, MX-7-180B, MX-7-180C, MX-7-180AC, MX-7-235, MXT-7-160, MXT-7-180, MXT-7-180A, M-7-260C. CAR 3 37. Mooney M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20S, M20TN. CAR 3, 2A3 FAR 23 CAR 3, 38. Mooney M20M, M20R EASA.IM.A.266 FAR 23 39. Mooney M22. A6SW CAR 3 40. Piper Aircraft, Inc. PA-24, PA-24-250, PA-24-260, PA-24-400. 1A15 CAR 3 41. Piper Aircraft, Inc. PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201, PA-28-201T, PA-28R-201T, PA-28RT-201T, PA-28-235, PA-28-236. PA28S-160, PA28S-180. 2A13 CAR 3 42. Piper Aircraft, Inc. PA-32-260, PA-32-300, PA-32R-300, PA-32S-300, PA-32-301, PA-32-301T, PA- 32RT-300, PA-32RT-300T. A3SO CAR 3 43. Piper Aircraft, Inc. 44. Piper Aircraft, Inc. 45. Piper Aircraft, Inc. 46. Piper Aircraft, Inc. 47. Revo, Inc. 48. Rogers (Mitchell) (Rogers) PA-32R-301 (HP) PA-36-285, PA-36-375, PA-36-300. PA-38-112. PA-46-310P, PA-46-350P, PA-46R-350T. LA-4, LAKE Model 250, LAKE LA-4-200. 15AC. EASA.IM.A.239 CAR 3 A9S0 A10SO FAR 23 A18SO FAR 23 EASA.IM.A.077 FAR 23 1A13 CAR 3 FAR 23 A-802 49. RUSCHMEYER R90-230RG. 50. SOCATA TB 9, TB 10, TB 20, TB 21, TB 200. 51. SOCATA MORANE SAULNIER (Rallye) Series Rallye 235E, MS894A. Germany 1082 EASA.A.378 EASA.A.379 / CAR'3/ FAR 21.29, FAR 23 FAR 21.29 CAR 3 CAR 10 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033199-001 STC APPROVAL-10052045-J.P. INSTRUMENTS, INC - EASA Approved Model List (AML) 3/5 ITEM AIRCRAFT MAKE SYMPHONY AIRCRAFT INDUSTRIES, INC. 52. 53. True Flight Holdings LLC 54. True Flight Holdings LLC 55. WACO 56. Waco Classic Aircraft Corporation 57. ZLIN AIRCRAFT a.s. 58. ZLIN AIRCRAFT a.s. EASA Approved Model List (AML) 10052045 J.P. INSTRUMENTS, INC AIRCRAFT MODEL A. SINGLE ENGINE AIRCRAFT (ITEMS 1-94) B. TWIN ENGINE AIRCRAFT (ITEMS 95-127) SA 160. AA-1, AA-1A, AA-1B, AA-1C. AA-5, AA-5A, AA-5B, AG-5B. YMF F5, YMF F5C. 2T-1A-1, 2T-1A-2. Z-143L. Z-242L EASA TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION EASA.A.031 FAR 23 A11EA FAR 23 A16EA FAR 23 EASA.IM.A.055 Aero Bulletin 7A AERO BULL A18EA 7-A,FAR 23 EASA.A.028 FAR 23 EASA.A.027 FAR 23 TWIN ENGINE 59. Aerostar 60. Beechcraft 61. Beechcraft PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, and PA-60-700P. A17WE FAR 23 B50, C50, D50, D50C. 5A4 CAR 3 D55, E55, E55A, 95, B95, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95- C55A, 95-D55A, B95A, D95A, E95, 56TC, A56TC, 58, 58A, G58. 3A16 CAR 3 62. Beechcraft 63. Beechcraft 58P, 58PA, 58TC, and 58TCA. A23CE FAR 23 64. Beechcraft 60, A60, B60. 65-80, 65-A80, 65-A80-8800, 65-B80, 65-88. A12CE FAR 23 3A20 CAR 3 65. Beechcraft 76. A29CE FAR 23 66. B-N Group Ltd. BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A- 21, BN-2A-26, and BN-2A-27. CAA-UK AAN FAR 21.29 FAR 23 BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27. 67. CESSNA T303. A34CE FAR 23 68. CESSNA 69. CESSNA 70. CESSNA |310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, 3101, 310J, 310K, 310L, 310N, 310P, 310Q, 310R, T310P, T310Q, T310R, 310J-1, E310H, E310J, 310J-1. 320, 320A, 320B, 320C, 320D, 320E, 320F, 320-1, 335, 340, 340A. 337, 337A, 337B, 337C, 337D, 337E, 337F, 337G, 337H, T337B, T337C, T337D, T337 E, T337F, T337G, T337H, M337B, P337H, T337H-SP. 3A10 CAR 3 3A25 CAR 3 CAR 3 A6CE FAR 23 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033199-001 STC APPROVAL -10052045-J.P. INSTRUMENTS, INC - EASA Approved Model List (AML) 4/5 EASA Approved Model List (AML) 10052045 J.P. INSTRUMENTS, INC AIRCRAFT MODEL European Aviation EASA ITEM AIRCRAFT MAKE A. SINGLE ENGINE AIRCRAFT (ITEMS 1-94) TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION B. TWIN ENGINE AIRCRAFT (ITEMS 95-127) 71. CESSNA 404. A25CE FAR 23 72. CESSNA 401, 401A, 401B, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C. A7CE CAR 3 73. Diamond Aircraft Ind. DA 42, DA 42 NG, DA 42 M-NG. EASA.A.005 FAR 21 74. Piper Aircraft, Inc. PA-23, PA-23-160, PA-23-235, PA-23-250, PA-23-E23-250. 1A10 CAR 3 75. Piper Aircraft, Inc. PA-30, PA-39, PA-40. A1EA CAR 3 76. Piper Aircraft, Inc. PA-31, PA-31-325, PA-31-350. A20S0 CAR 3 FAR 23 77. Piper Aircraft, Inc. 78. Piper Aircraft, Inc. 79. Piper Aircraft, Inc. 80. SOCATA, S.A. 81. Twin Commander 82. Twin Commander 83. Vulcanair S.p.A PA-31P, PA-31P-350. PA-34-200, PA-34-200T, PA-34-220T. PA-44-180, PA-44-180T. GA-7. 500-A, 500-B. Also 500-B, 500-S, 500-U. 680FL, 685. P68, P68B, P68C, P68 Observer, P68 Observer 2. A8EA CAR 3 FAR 23 EASA.IM.A.090 FAR 23 EASA.IM.A.232 FAR 23 FR TCDS 190 FAR 23 6A1 CAR 3 2A4 CAR 3 EASA.A.385 FAR 23 For the European Aviation Safety Agency, Date of Issue: 04 February 2015 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033199-001 STC APPROVAL-10052045-J.P. INSTRUMENTS, INC - EASA Approved Model List (AML) 5/5 Yves MORIER Head of General Aviation Remotely Piloted Aircraft system (RPAS)
What's in the CESSNA 310F TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
5,752 CESSNA 310F parts for sale
See all →
Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.