Supplemental Type Certificate for CESSNA 550 Citation II
CESSNA 550 Citation II · Supplemental Type Certificate
Overview
This document serves as a Supplemental Type Certificate (STC) for the Cessna 550 Citation II. It outlines the modifications and alterations approved for this specific aircraft model, ensuring compliance with safety and regulatory standards. The STC is intended for use by aircraft owners, operators, and maintenance personnel who are involved in the operation and upkeep of the Cessna 550 Citation II. It provides essential information regarding the approved modifications, installation procedures, and any limitations that may apply to the aircraft. The document is crucial for maintaining the airworthiness of the aircraft following the modifications detailed within.
- This document is a Supplemental Type Certificate for the Cessna 550 Citation II.
- It details approved modifications and alterations for the aircraft.
- Installation procedures are provided to ensure safety and compliance.
- Limitations on the operation of the aircraft with modifications are specified.
- Accurate record-keeping of all modifications is essential for compliance.
Document
Source
Originally published by 560wiringdiagrams.z13.web.core.windows.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Pages
- 20
- File size
- 943 KB
- Publisher
- 560wiringdiagrams.z13.web.core.windows.net
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In this document
Introduction
The introduction section provides an overview of the Supplemental Type Certificate, detailing its purpose and the specific modifications approved for the Cessna 550 Citation II. It emphasizes the importance of adhering to the guidelines set forth in the STC to ensure safety and compliance.
Modifications Approved
This section lists the specific modifications that have been approved under the STC for the Cessna 550 Citation II. Each modification is described in detail, including the installation process and any necessary adjustments to the aircraft systems.
Installation Procedures
Detailed installation procedures for the approved modifications are outlined in this section. It includes step-by-step instructions to ensure that the modifications are carried out correctly and safely.
Limitations
The limitations section specifies any restrictions or conditions that must be observed when operating the Cessna 550 Citation II with the approved modifications. This is critical for maintaining compliance and ensuring the safety of the aircraft.
Compliance and Record Keeping
This section emphasizes the importance of maintaining accurate records of all modifications made under the STC. It outlines the documentation required to demonstrate compliance with regulatory standards.
Safety notes
- Ensure all modifications are performed by qualified personnel.
- Follow installation procedures closely to maintain safety standards.
- Adhere to the limitations specified in the STC to ensure airworthiness.
Full document text
FELERAL ADMIN VIATION Ni RATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00796DE This certificate, issued to: Teledyne Battery Products. 840 West Brockton Avenue Redlands, California 92374 100022289 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 Federal Aviation Regulations. - Original Product Type Certificate Number: Make: Model: * See attached Federal Aviation Administration (FAA) Approved Model List (AML) ST00796DE for approved aircraft models and applicable airworthiness regulations. Description of the Type Design Change: Installation of Teledyne Battery Products P/N 7638-44T Lead-Acid Battery in accordance with Document No. TD34-4-01, Master Drawing List, Revision IR dated 3/4/2016 or later FAA approved revision. Instructions for Continued Airworthiness (ICA) are required to be made available at installation, refer to AML ST00796DE for model specific. ICA document. Limitations and Conditions: 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. (See Continuation Sheet on Page 3 for Certification Basis) This certificate and the supporting data which is the bases 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: Date of Issuance: November 30, 2015 April 3, 2016 Date Reissued: April, 15, 2016 Date Amended: By direction of the Administrator Signature Todd Dixon Title G.Jahnay for.T.Dixch Northwest Mountain Regional Manager Denver Aircraft Certification Office Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred or made available to third persons by licensing agreements in accordance with, 14, CFR 21.47, Possession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to aller an aircraft, aircraft engine, or propeller. The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to use the STC to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (5/14) Page 1 of 3 FEDERA AVIATION ADMINIST RATION Certification Basis: United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00796DE Date of Issuance: April 3, 2016 Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows: a. The certification basis for parts not changed or not affected by this change is shown on the attached AML. b. The certification basis for parts changed or affected by the change since the reference date of application, November 30, 2015, is based upon 14 CFR Part 25, Amendment 25-1 through 25-98. 14 CFR Sections: 25.301 Amdt. 25-23; 25.303 Amdt. 25-23; 25.305(a),(b) Amdt. 25-86; 25.307(a) Amdt. 25-72; 25.337 Amdt. 25-23; 25.341 Amdt. 25-86; 25.561(c) Amdt. 25-91; 25.601 Amdt. - ; 25.603 Amdt. 25-46; 25.605(a) Amdt. 25-46; 25.609 Amdt. - ; 25.611 Amdt. 25-23; 25.613(a),(b),(c),(d) Amdt. 25-72; 25.619 Amdt. 25-23; 25.625(a),(b), (c) Amdt. 25-72; 25,1301 Amdt. - ; 25.1309(a),(b),(c),(d)(e1,2,3,4),(f),(g) Amdt. 25-41; 25.1351(a), (d) Amdt. 25-72; 25.1353(a), (c)(1),(c)(2),(c)(3),(c)(4) Amdt. 25-42; 25.1529 Amdt. 25-54 -END-- : Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data rior to alter an aircraft, aircraft engine, or propeller. The STC's supporting documentation (drawings, Instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to use the STC to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (5/14) Page 3 of 3 FAA Approved Model List (AML) ST00796DE Installation of Teledyne Battery Products 7638-44T battery in Cessna aircraft. FEDERAL AVIATION 10MINISTRATION FAA Approved силк Kreg R. Voorhies, ODA administrator Cert Works ODA ODA(AIR)-833887-NM Issued Date: APR - 3 2016 Page 1 of 3 FAA Approved Model List (AML) ST00796DE Installation of Teledyne Battery Products 7638-44T battery in Cessna aircraft. Date 4/3/2016 Description Initial Release AML Revision Log Page 2 of 3 FAA Approved Model List (AML) ST00796DE Installation of Teledyr Battery Products 7638-44T battery in Cessna aircraft. Initial Model/ Model Specific Approve Amender Item Make Series Cert Basis/Amdt TCDS No. Instwg¹ FMS ICA² Notes 1 Cessna 500. Part 25, Amdt.25-1 through 25-17 A2ZCE 387 None TD34-8-01 None Date 4/3/2016 Date Rev - (1/5/2015) Rev. A (12/7/2015) 2 Cessna 501 Part 23, Amdt 23-1 A27CE 337 None TD34-8-01 None 4/3/2016 through 23-16. Rev - (1/5/2015) Rev. A (12/7/2015) 3 Cessna 550 Part 25, Amdt 25-1 A22CE 387 None TD34-8-01 None 4/3/2016 through 25-17 Rev- (1/5/2015) Rev. A (12/7/2015) 4 Cessna 551
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Part 23, Amdt 23-1 A27CE 337 None TD34-8-01 None 4/3/2016 through 23-16. Rev - (1/5/2015) Rev. A (12/7/2015) 5 in Cessna S550 Part 25, Amdt 25-1 A22CE 37 Noņe TD34-8-01 None 4/3/2016 through 25-17 Rev - (1/5/2015) Rev. A (12/7/2015) 6 Cessna 560 Part 25, Amdt 25-1 through 25-17 A22CE 337 None TD34-8-01 None 4/3/2016 Rev - (1/5/2015) Rev. A (12/7/2015) 7 Cessna 560XL 8 00 Cessna 650 9 Cessna 680 10 10 Cessna 750 Part 25, Amdt 25-1 through 25-82 Part 25, Amdt 25-1 through 25-39 Part 25, Amdt 25-1 through 25-98 Part 25, Amdt 25-1 through 25-74 AZZCE 337 None TD34-8-01 None 4/3/2016 Rev (3/5/2015) Rev. A (12/7/2015) A9NM T00012WI T00007WI 37 Rev- (1/5/2015) 37 Rev - (1/5/2015) 337 None TD34-8-01 None 4/3/2016 Rev. A (12/7/2015) None TD34-8-01 None 4/3/2016 Rev. A (12/7/2015) None TD34-8-01 None 4/3/2016 Rev - (1/5/2015) Rev. A (12/7/2015) 1 Or later FAA approved revision. 2 Or later FAA accepted revision. Page 3 of 3 CERT WORKS Master Data List (MDL) Installation of Teledyne Battery Products 7638-44T in Cessna Aircraft Models: 500, 501, 550, S550, 551, 560, 560XL, 650, 680, 750 Document Number: Revision : Date: TD34-4-01 IR 3/4/2016 This data is hereby approved by the Cert Works, LLC ODA, ODA(AIR)-833887-NM DOR Kreg R. Voorhies ODA Lead administrator Cert Works LLC, ODA APR 3 2016 Date: PROPRIETARY. ALL RIGHTS RESERVED. NO PORTION OF THIS DOCUMENT MAY BE REPRODUCED OR TRANSMITTED IN ANY FORM OR BY ANY MEANS, ELECTRONIC OR MECHANICAL, INCLUDING BY PHOTOCOPYING, RECORDING, OR USE OF ANY INFORMATION STORAGE AND RETRIEVAL SYSTEM WITHOUT EXPRESS WRITTEN PERMISSION OF CERT WORKS, LLC. ©2016 CERT WORKS, LLC, TD34-4-01: Master Drawing List, Teledyne Battery 7638-44T- Cessna Aircraft IR; 3/4/2010 I. Revisions Revision Revision Date Description IR 3/4/2016 Initial Release Prepared By: Reviewed By: Released By: K. Voorhies. ск II. Table of Contents REVISIONS............ I. II. TABLE OF CONTENTS SECTION 1: INTRODUCTION.. SECTION 2: LIMITATIONS. SECTION 3: DATA CERT WORKS Page 2 of 4 * 2 2 3 4 TD34-4-01: Master Drawing List, Teledyne Battery 7639-44T IR; 3/4/2016 Section 1: Introduction Cessna Aircraft The Master Data List provides definition of the documentation to support the Supplemental Type Certificate (STC) installation of the Teledyne Battery Products 7638-44T in the following aircraft: Cessna: ° 500 • 501 • 550 S550 • 551 560 . 560XL 650 • 680 • 750 This installation installs the Teledyne Battery Products 7638-44T battery in replacement of the original aircraft main battery. Section 2: Limitations Installation is replacement of the original equipment battery and requires the original equipment connections and tie downs. No other installation limitations. CERT WORKS Page 3 of 4 TD34-4-01: Master Drawing List, Teledyne Battery 7638-44T - Cessna Aircraft IR; 3/4/2010 Section 3: Data Document No. Title Revision 3437 Battery Installation, Cessna Aircraft (Part 25) ".w 10/5/15 CERT WORKS Page 4 of 4 Ar VERMOUNT A WHY WAT VERECT T be" rtoerKIN STEREO" 12.DLL SPIODIC IATES** HEGATIVE VEM ASSEMBLY BATTERY ITEM 12 CLECTRIC PUVER DISTRIBUTION PANEL WING NUT STUD FLAT WASHER NOTE: THIS BATTERY PYSTALLATION FIGURE IS ACPRESENTATIC. RETER TO THE AIRCRARY HAINBETMUCE HAMLIN PUR MODEL SPECIFIC HATTERY RISTALLATION INITORMATION. TEMPERATURE SENSOR CKT CONNECTOR -CLAMP FUSITIVE "VENT HOSE BATTERY CONNECTOR TMP SENSUR CONNECTOR EXIST FOVER VIRC (EXESTING> GROUND WIRK (EXIS FATTERY BATTERY COMPARTHENT PARTS LIST Gr FART HOW TULO DELT VALVE REINLAICE LEAD- -7420-44) TELL geçer 17- #14 b hel BIJ har A 10/3.85 A to rinh Dim RAL INJUNG RAITERY INSTALLATION CES AIRCAF (PART 23) 9454 THE THE D 3-137 E CERT WORKS, LLC INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Document No: TD34-8-01 Revision A dated 12/7/2015 For TSO-C173/C173a Authorized Teledyne Battery Products (GILL®) 7638-44T LT Valve-Regulated Lead-Acid Aircraft Battery STC ST00796DE: Cessna Models 500, 501, 550, $550, 551, 560, 560XL, 650, 680, 750 STC SA00797DE: Cessna Models 525, 525A, 525B, 525C Aircraft Serial Number: 560-5344 Aircraft Reg. Number: NINA Instructions for Continued Airworthiness Teledyne Battery Products 7638-44T Cessna Battery Installation REVISIONS Rev. Description Approved Date No. NC Initial Release KRV 10/12/2015 A Revised to correct STC - Model references. KRV 12/7/2015 | Note: For any revision, all pages will be revised. Changes to the current revision will be indicated within the document by change bars. Cert Works, LLC 44110 East Arkansas Place Bennett, CO 80102 Document Number Page Revision ii - A TD34-8-01' Instructions for Continued Airworthiness Teledyne Battery Products 7638-44T Cessna Battery Installation TABLE OF CONTENTS 1. AIRWORTHINESS LIMITATIONS 1.1 Airworthiness Limitations Information 2 INTRODUCTION. 2.1 Scope 2,2 Service Difficulties. 2.3 Language .2 2 1 122 2 2.4 Unit of Measure.. 2.5 Torque Values 2.6 2.7 2.8 3 3.1 3.2 4.1 4.2 4.3 Precautions Abbreviations Revision to ICA.. System Description. General Parts List........ 4 Inspection Requirements Description.... Inspection Program Daily Inspection Program. 4.4 4.5 Recurrent Inspection Program.. Conditional Inspection Checks 4.6 5.1 6 6.2 21 Markings. 8 System Maintenance.. 8.1 8.2 Installation Instructions. 8.3 Removal Instructions....... 8.4 Repairs. 8.5 Replacement of Parts.. 8.6 Troubleshooting Special Inspection Requirements 5 Weight and Balance.. Weight and Balance information......... Placards and Markings.... 7 Servicing...... Control and Operation. 5 5 5 6 6 6 6 6 6 7 2 3. .3. 3. 3 .4 4 .4 4 4 .5 .5 5 Cert Works, LLC 44110 East Arkansas Place Bennett, CO 80102 Document Number Page Revision iii A TD34-8-01 Instructions for Continued Airworthiness Teledyne Battery Products 7638-44T Cessna Battery Installation 1. AIRWORTHINESS LIMITATIONS The Airworthiness Limitations section is FAA-approved and specifies maintenance required under Sec. 43.16 and 91.403 of the Federal Aviation Regulations, unless an alternative program has been FAA approved. 1.1 Airworthiness Limitations Information No airworthiness limitations are associated with the Teledyne Battery Products 7638-44T Installation type design change (STC's ST00796DE or SA00797DE). DATE APPROVED APR 3 2016 Kreg. R. Voorhies, ODA administrator Cert Works ODA(AIR)-833887-NM Document Number Page Revision Cert Works, LLC 44110 East Arkansas Place Bennett, CO 80102 1 A TD34-8-01 Instructions for Continued Airworthiness Teledyne Battery Products 7638-44T Cessna Battery Installation 2 INTRODUCTION 2.1 Scope This manual provides Maintenance Procedures for the installation of the Teledyne Battery Products (GILL) 7638-44T battery in Cessna "Citation" aircraft. This ICA covers the following Supplemental Type Certificate Installations: STC ST00796DE: Cessna Aircraft Models 500, 501, 550, S550, 551, 560, 560XL, 650,680, 750 STC SA00797DE: Cessna Aircraft Models 525, 525A, 525B, 525C For battery Instructions for Continued Airworthiness and Component Maintenance refer to Teledyne Battery Products Document TD14-8-01, Instructions for Continued Airworthiness and Component Maintenance Manual for TSO-C173/C173a Authorized Teledyne Battery Products (GILL) 7000 Series LT Valve-Regulated Lead-Acid Aircraft Batteries, Revision C or later accepted revision. 2.2 Service Difficulties Report service difficulties with the Teledyne Battery Products 7638-44T Installation modification to: Cert Works 965 S. 1st Street, Unit 6F-144 Bennett, Colorado 80102 info@certworks.com 305.578.0493 2.3 Language This manual is written to the Simplified English (SE) specification. This International Aerospace Maintenance Language Specification is important to maintenance personnel whose first language is not English. 2.4 Unit of Measure Unless otherwise noted, measurements throughout this manual are shown in American Standard unit. Cert Works, LLC 44110 East Arkansas Place Bennett, CO 80102 Example: 12.55 in Document Number Page Revision 2 А TD34-8-01