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Supplemental Type Certificate for CESSNA 310F

CESSNA 310F · Supplemental Type Certificate

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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 model, ensuring compliance with safety and performance standards set by aviation authorities. The STC is essential for owners and operators of the Cessna 310F who wish to implement the approved changes to their aircraft. It provides detailed information on the modifications, including technical specifications and operational guidelines, which are crucial for maintaining the airworthiness of the aircraft. This document is intended for aircraft maintenance personnel, pilots, and aviation enthusiasts interested in the regulatory aspects of aircraft modifications.

  • This document is a Supplemental Type Certificate (STC) for the Cessna 310F.
  • It outlines approved modifications and alterations for the aircraft.
  • Compliance with FAA regulations is mandatory for all modifications.
  • Accurate documentation of modifications is essential for airworthiness.
  • Operational guidelines are provided to ensure safe handling of the modified aircraft.

Document

Source

Originally published by luminary.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Supplemental Type Certificate
Pages
7
File size
4.7 MB
Publisher
luminary.aero
How rare is it?
49CESSNA 310F registered worldwide · 43 active

Common. Rarer than 2% of the aircraft models we track.

Documentation completeness
5/7

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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 adhering to the guidelines set forth in the document to ensure safety and compliance.

Modifications Approved

This section lists all the modifications that have been approved under the STC for the Cessna 310F. Each modification is described in detail, including the technical specifications and any necessary installation procedures.

Compliance Requirements

The compliance requirements section outlines the necessary steps that must be taken to ensure that the modifications are installed correctly and that the aircraft remains in compliance with FAA regulations.

Operational Guidelines

Operational guidelines are provided to assist pilots and maintenance personnel in understanding how the modifications affect the aircraft's performance and handling characteristics.

Documentation and Records

This section emphasizes the importance of maintaining accurate records of the modifications made under the STC, including installation dates and compliance checks.

Safety notes

  • Ensure all modifications are performed by certified personnel.
  • Follow all operational guidelines to maintain safety standards.

Full document text

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate This Certificate issued to Number SA00063LA Luminary Air Group, LLC 18321 Parkway Melfa, VA 23410 certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereen meets the airworthiness requirements of Part* of the * Regulations. Original Product Type Certificate Number: *See attached FAA Approved Model List Make: (AML) No. SA00063LA for list of approved airplane Model: models and applicable airworthiness regulations. Description of Type Design Change: Installation of Acoustical/Thermal insulation in accordance with Aero Sound Shield, Inc. installation instructions as listed on AML No. SA00063LA dated March 28, 1995, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the above models aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of the aircraft. A copy of this certificate and FAA approved AML No. SA00063LA, dated March 28, 1995, or later approved revision, must be maintained as part of the record for the modified aircraft. If the holder agrees to permit another person to use this certificate 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: February 3, 1995 Date of issuance: Date reissued: March 30, 1995 FEDERAL AVIATION Dale amended: Dec. 28, 1998, Jan. 05, 2005, November 1, 2016 By direction of the Administrator * TOMINISTRATION (Signature) Manager, Technical & Administrative Support Staff Los Angeles 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 2 This certificate may be transferred in accordance with FAR 21.47. INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate. The FAA will reissue the certificate in the name of the transferee and forward it to him. TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number_ to (Name of transferee) (Address of transfer) from (Name of grantor) (Print or type) (Address of grantor) Extent of Authority (if licensing agreement): Date of Transfer: Signature of grantor (In ink): (Number and street) (City, State, and Zip code) (Number and street) (City, State, and Zip code) Page 2 of 2 *U.S. GPO 1987-763-28 FAA Approved Model List Number SA00063LA Luminary Air Group, LLC For Installation Acoustical Thermal Insulation Revision D, Revision Date: August 21, 1996 Item Aircraft Make Aircraft Model Original Certification Basis for Controlled Controlled Date Issued: March 30, 1995 Rotorcraft Type Alteration Certificate Drawing List Drawing List Flight Manual AML Amendment Number Revision Number/Date Number/Date Date 1 Beechcraft 35, A35, B35, C35, E35, F35, G35, 35R, D35 A-777 CAR 3, dated AS1005-1 11/13/1945. AS1007-1 A 07/06/1995 A 03/07/1995 N/A 2 Beechcraft 35-33, 35-A33, 35-B33, 3A15 35-C33, 35-C33A, E33, CAR 3 as amended to May 15, 1956 and AS1005-1 AS1007-1 A 07/06/1995 A 03/07/1995 N/A E33A, E33C, F33, F33A, Amendment 3-8. F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B 3 Beechcraft 95, B95, B95A, D95A, E95, 95-55, 95-A55, 3A16 95-B55, 95-B55A, 95-B55B (7-42A), 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC CAR 3 amended May 15, 1956, and Paragraphs 23.1385(c), 23.1387(a), & 23.1387(e) of FAR. Part 23, dated Feb. 1, 1965 as amended by Amendment 23.12. AS1005-1 AS1007-1 A 07/06/1995 A 03/07/1995 N/A Page 1 of 5 FAA Approved Model List Number SA00063LA Luminary Air Group, LLC For Installation Acoustical Thermal Insulation Revision D, Revision Date: August 21, 1996 Date Issued: March 30, 1995 Item Aircraft Make Aircraft Original Certification Basis for Controlled Controlled Rotorcraft Model Type Alteration Certificate Drawing List Drawing List Flight Manual AML Amendment Number Revision Number/Date Number/Date Date 4 Beechcraft 36, A36, A36TC, B36TC 3A15 CAR 3 as amended to May 15, 1956 and AS1005-1 AS1027-1 A 07/06/1995 N/A N/C Amendment 3-8. Paragraphs 23.909, 23.1043, 23.1527(b), & 23.1583 of FAR Part 23 as amended by Amendment 23-18 dated Feb. 1, 1965 Part 36, through Amendment 36- 10. 5 Beechcraft 58, 58A, 58TCA A23CE FAR Part 23 as amended to Feb. 1, 1965, by AS1005-1 AS1027-1 A 07/06/1995 N/A N/C Amendments 23-1 through 23-12. FAR Part 36, by Amendments 36-1 through 36-10. Page 2 of 5 FAA Approved Model List Number SA00063LA Luminary Air Group, LLC For Installation Acoustical Thermal Insulation Item Aircraft Make Aircraft Model Original Type Certificate Revision D, Revision Date: August 21, 1996 Certification Basis for Alteration Date Issued: March 30, 1995 Number 6 Cessna 310, 310A, 310B, 310C, 3A10 310D, 310E, 310F, 310G, 310H, 310I, 310J, 310J-1, 310K, 310L, 310N, 310P, 310Q, T310Q, 310R, T310R CAR 3 as amended May 15, 1956, and Paragraphs 23.161, 23.171, 23.181 of FAR Part 23, dated Feb. 1, 1965 as amended by Amendment 23-23. Controlled Controlled Drawing List Drawing List Revision Rotorcraft Flight Manual Number/Date AML Amendment Date Number/Date AS1005-1 AS1057-1 A 07/06/1995 N/A N/C 7 Cessna 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F 3A25 CAR 3 as amended May AS1005-1

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15, 1965 by Amendments AS1057-1 A 07/06/1995 N/C N/A 3-1 through 3-5. Page 3 of 5 FAA Approved Model List Number SA00063LA Luminary Air Group, LLC For Installation Acoustical Thermal Insulation Revision D, Revision Date: August 21, 1996 Date Issued: March 30, 1995 Item Aircraft Make Aircraft Original Certification Basis for Controlled Controlled Model Type Certificate Alteration Drawing List Drawing List Rotorcraft Flight Manual AML Amendment Number Revision Number/Date Number/Date Date 8 Piper 46-310P, 46-350P A25SO FAR 23, effective Feb. 1, AS1005-1 A 7/6/1995 N/A 1965, through Amendment AS1077-1 N/C 11/7/1995 23-35, effective March 6, 1980. FAR 25.783(e) of Amendment 25-54, effective Oct. 14, 1980. FAR 25.831(c) and (d) of Amendment 25-41, effective Sept. 1, 1997. FAR 36 through Amendment 15, effective May 6, 1988. No equivalent safety findings. Special Conditions No. 23-ACE-53, Docket No. 082CE. Page 4 of 5 FAA Approved Model List Number SA00063LA Luminary Air Group, LLC For Installation Acoustical Thermal Insulation Revision D, Revision Date: August 21, 1996 Item Aircraft Aircraft Original Certification Basis for Controlled Controlled Date Issued: March 30, 1995 Rotorcraft Make Model Type Alteration 9 Mooney M20M Certificate Number 2A3 Drawing List Drawing List Flight Manual AML Amendment Revision Number/Date Number/Date Date CAR 3 as amended May AS1005-1 A 7/6/1995 N/A 15, 1956 and Amendment AS1217-1 N/C 7/9/1996 3-8. Date Reissued: November 1, 2016 Steven Bogucki Manager, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office Paragraphs 23.909, 23.1043, 23.1527(b) and 23.1583 of FAR Part 23 as amended by Amendment 23-18, dated Feb. 1, 1965. Page 5 of 5

Type certificate, explained

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.

TCDS 3A10Rev 62· Issued 2005
Read the full TCDS

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