Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket

For questions visit www.gallagheraviationllc.com A TTACHMENTS 1. A TTACHMENT 1 – General Arrangement drawing GAL01-5720-001 2. A TTACHMENT 2 – GAL01-AMM-26156 Aircraft Maintenance Manual Supplement 3. A TTACHMENT 3 – GAL01-ICA-26155 Instructions for Continued Airworthiness PRIOR WRITTEN PERMISSION OF INNOVIATOR, LLC. THE INFORMATION HEREIN IS PRIVILEGED AND CONFIDENTIAL AND SHALL NOT BE DISSEMINATED, DUPLICATED, REUSED, OR DISCLOSED IN ANY WAY WITHOUT THE PROPRIETARY INFORMATION SIZE 125 SURFACE FINISH WEIGHT IN U.S. LBS. 0.50 ANGULAR DECIMAL 0.010 .X 0.1 .XX 0.03 .XXX UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES TOLERANCES ARE: APPROVED: STRESS: CHECKED: DRAWN: 3D MODEL: THIRD ANGLE PROJECTION DO NOT SCALE DRAWING DATE APPROVAL (PRINT AND SIGN) SOLIDWORKS DRAWING ACT WT. SOLIDWORKS DRAWING 6WW92 CAGE CALC WT. REV DWG. NO. B TITLE: IR SHEET 1 OF 3 SCALE: PART DASH NO. NHA TOTAL NEXT ASSY USED ON APPLICATION REVISIONS REV ZN DESCRIPTION DRAWN APPROVED DATE IR ALL SHTS INITIAL RELEASE Z. KAUFMAN S. MARSAN 04/30/2021 THIS DRAWING HAS BEEN GENERATED AND MUST BE MAINTAINED BY A 3D CAD SYSTEM. CHANGES SHALL BE INCORPORATED AS DIRECTED BY THE DESIGN ACTIVITY. THE MODEL 1. SHALL BE KEPT CURRENT WITH THE DRAWING AT ALL TIMES. THIS GENERAL ARRANGEMENT DRAWING IS A CONFIGURATION TOOL USED TO MANAGE COMBINATIONS OF INSTALLATIONS AS APPROVED CONFIGURATIONS OF A STC. THIS DRAWING 2. IS USED FOR CONFIGURATION MANAGEMENT ONLY AND SHALL BE USED IN CONJUNCTION WITH THE APPROVED INSTALLATION DATA LIST (IDL). IDL PROVIDES REVISION CONTROL TO ALL DESIGN DATA. CONTACT INNOVIATOR PLANNING FOR IDL DOCUMENT NUMBER AND LATEST REVISION LEVEL. INSTALLATION KIT NUMBERS CORRESPOND TO GENERAL ARRANGEMENT DEFINED HEREIN. 3. GENERAL NOTES : APPLICATION: : INSTALLATION REQUIREMENTS: : THIS STC IS APPLICABLE FOR THE AIRCRAFT LISTED IN THE APPLICABILITY LIST, BELOW. 1. IN ADDITION TO THE AIRCRAFT APPLICABILITY LISTING IN THE APPLICABILITY TABLE, BELOW, ALL CONDITIONS OF THE INSTALLATION REQUIREMENTS SECTION MUST BE SATISFIED 2. PRIOR TO INSTALLATION. THE INSTALLER MUST DETERMINE WHETHER THIS DESIGN CHANGE IS COMPATIBLE WITH PREVIOUSLY APPROVED MODIFICATIONS. 1. PRIOR TO INSTALLATION, THE AIRCRAFT OWNER MUST HAVE A LETTER OF AUTHORIZATION OR A PERMISSION OF USE LETTER PER 14 CFR PART 21.120 THAT PROVIDES AUTHORIZATION FOR THE INSTALLATION OF THIS STC. 2. THIS STC ONLY PROVIDES STRUCTURAL MOUNTING OF THE LIGHT AND DOES NOT PROVIDE ELECTRICAL INTEGRATION, LIGHT OPERATION, OR FUNCTIONAL CHECKS OF THE LIGHT. LIGHT ELECTRICAL INTEGRATION, 3. OPERATION, AND FUNCTION REQUIRE ADDITIONAL APPROVALS. INSTALLATION ON A FOREIGN REGISTERED AIRCRAFT REQUIRES FOREIGN VALIDATION OF FAA STC. 4. WEIGHT AND BALANCE EFFECTS DUE TO THE INSTALLATION OF CONFIGURATIONS DEFINED HEREIN ARE DEFINED IN DOCUMENT GAL01-ICA-26115, INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, AND SHALL BE 5. INCORPORATED INTO THE AIRCRAFT WEIGHT AND BALANCE DOCUMENTS. THE AIRCRAFT MUST BE MAINTAINED IN ACCORDANCE WITH THE LATEST FAA-APPROVED REVISION OF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, DOCUMENT GAL01-ICA-26115. 6. APPLICABLE TO -001 ARRANGEMENT ONLY. 4 APPLICABLE TO -003 ARRANGEMENT ONLY. 5 SEE SHEET 2 FOR PARTS LIST APPLICABILITY LIST MAKE MODEL(S) SERIES TCDS TEXTRON AVIATION, INC. 35, A35, B35, C35, D35, E35, F35, G35, 35R BONANZA A-777 TEXTRON AVIATION, INC. H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, 36, A36, A36TC, B36TC, G36, E33, E33A, E33C, F33, F33A, F33C BONANZA 3A15 TEXTRON AVIATION, INC. D55, D55A, E55, E55A, 56TC, A56TC, 58 BARON 3A16 TEXTRON AVIATION, INC. BARON AIRCRAFT SHOWN. APPLICABLE TO ALL MODELS IN APPLICABILITY LIST.. 6 NONE D C B A A B C D 1 2 3 4 5 6 7 8 8 7 6 5 4 3 2 1 Z. KAUFMAN Z. KAUFMAN S. MARSAN Z. KAUFMAN S.MARSAN 04/30/2021 04/30/2021 04/30/2021 04/30/2021 04/30/2021 RECOGNITION LIGHT SUPPORT BRACKET GENERAL ARRANGEMENT - WINGTIP POSITION/ANTICOLLISION AND GAL01-5720-001 PRIOR WRITTEN PERMISSION OF INNOVIATOR, LLC. THE INFORMATION HEREIN IS PRIVILEGED AND CONFIDENTIAL AND SHALL NOT BE DISSEMINATED, DUPLICATED, REUSED, OR DISCLOSED IN ANY WAY WITHOUT THE PROPRIETARY INFORMATION PRIOR WRITTEN PERMISSION OF INNOVIATOR, LLC. THE INFORMATION HEREIN IS PRIVILEGED AND CONFIDENTIAL AND SHALL NOT BE DISSEMINATED, DUPLICATED, REUSED, OR DISCLOSED IN ANY WAY WITHOUT THE PROPRIETARY INFORMATION 1 GAL01-5720-101-004 RH POSITION/ANTICOLLISION LIGHT PROVISIONS INSTL 0304D 1 GAL01-5720-101-003 LH POSITION/ANTICOLLISION LIGHT PROVISIONS INSTL 0308D 1 GAL01-5720-101-002 RH POSITION/ANTICOLLISION AND RECOGNITION LIGHT PROVISIONS INSTL 0304D 1 GAL01-5720-101-001 LH POSITION/ANTICOLLISION AND RECOGNITION LIGHT PROVISIONS INSTL 0308D --- -003 POSITION/ANTICOLLISION LIGHT PROVISIONS INSTL 0306A --- -001 POSITION/ANTICOLLISION AND RECOGNITION LIGHT PROVISIONS INSTL 0306A QTY QTY CAGE PART NUMBER NOMEN OR DESCRIPTION MATERIAL & SPECIFICATION NOTES WEIGHT IN LBS ZONE ITEM NO. CNF -003 -001 REVISIONS REV ZN DESCRIPTION DRAWN APPROVED DATE GAL01-5720-001 D C B A A B C D 1 2 3 4 5 6 7 8 8 7 6 5 4 3 2 1 ACT WT. SIZE IR 6WW92 CAGE SOLIDWORKS DRAWING SHEET 2 OF 3 SCALE: CALC WT. REV DWG. NO. B NONE PRIOR WRITTEN PERMISSION OF INNOVIATOR, LLC. THE INFORMATION HEREIN IS PRIVILEGED AND CONFIDENTIAL AND SHALL NOT BE DISSEMINATED, DUPLICATED, REUSED, OR DISCLOSED IN ANY WAY WITHOUT THE PROPRIETARY INFORMATION PRIOR WRITTEN PERMISSION OF INNOVIATOR, LLC. THE INFORMATION HEREIN IS PRIVILEGED AND CONFIDENTIAL AND SHALL NOT BE DISSEMINATED, DUPLICATED, REUSED, OR DISCLOSED IN ANY WAY WITHOUT THE PROPRIETARY INFORMATION GAL01-5720-001 D C B A A B C D 1 2 3 4 5 6 7 8 8 7 6 5 4 3 2 1 ACT WT. CAGE IR 6WW92 SIZE SOLIDWORKS DRAWING SHEET 3 OF 3 SCALE: CALC WT. REV DWG. NO. B NONE REVISIONS REV ZN DESCRIPTION DRAWN APPROVED DATE -001 GAL01-5720-101-004 GAL01-5720-101-001 GAL01-5720-101-003 5 4 -003 4 GAL01-5720-101-002 5 6 (GENERAL ARRANGEMENT, POSITION/ANTICOLLISION LIGHT PROVISIONS INSTL) (GENERAL ARRANGEMENT, POSITION/ANTICOLLISION AND RECOGNITION LIGHT PROVISIONS INSTL) 3189 Princeton Road Hamilton, OH 45011 513-907-4257 DOCUMENT NO. GAL01-AMM-26156 REVISION LEVEL IR AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT FOR Installation of Wingtip Position/Anticollision Light Support Bracket Textron Aviation Inc. Bonanza and Baron Aircraft FAA STC No.:_____________ Prepared By: (Signature on File) 04/30/2021 Z. Kaufman, Structural Engineering, Innoviator LLC Date Checked By: (Signature on File) 04/30/2021 S. Marsan, Structures DER, Innoviator LLC Date Approved By: (Signature on File) 04/30/2021 S. Marsan, Structures DER, Innoviator LLC Date PROPRIETARY DOCUMENT The information herein is privileged and confidential and shall not be disseminated, duplicated, reused or disclosed in any way without the prior written permission of Innoviator, LLC. Permission of use letter per 14 CFR §21.120 permits an operator to use Innoviator, LLC’s STC data to modify their aircraft. Innoviator, LLC. does not inhibit or restrict transmission or use of ICA data for the sole purpose of maintenance on an aircraft modified with Innoviator, LLC’s STC. © Innoviator, LLC 2021 All Rights Reserved Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 1 subject to the restriction notice contained on page i of this document. LIST OF REVISIONS Revision Level Pages Affected Description of Revision Approved Date IR All Initial Release See Cover Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 2 subject to the restriction notice contained on page i of this document. TABLE OF CONTENTS 57-00-01 – WING TIP POSITION/ANTICOLLISION LIGHT SUPPORT BRACKET ....................................... 3 Description and Operation ........................................................................................................... 3 Maintenance Practices ................................................................................................................. 4 Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 3 subject to the restriction notice contained on page i of this document. 57-00-01 – WING TIP POSITION/ANTICOLLISION LIGHT SUPPORT BRACKET Description and Operation This STC installs brackets for the structural mounting of LED wingtip anticollision lights. Aftermarket LED anticollision lights are not exact form/fit replacements for the OEM wingtip anticollision lights. Structure provided in this STC mounting provisions only and does not approve the function of the replacement LED wingtip anticollision lights. Additional approvals are required. This STC also provides mounting provisions for a forward recognition light should the operator choose to utilize the provisions to install a forward recognition light. Forward recognition lights do not require FAA- approval. Mounting and activation of the forward recognition light is the responsibility of the operator. Figure 1: Installation Detail The mounting bracket, shown in yellow in the figure above, is attached to the aircraft via 6 screws. Position/Anticollision light and recognition light (if used) are attached via screws as well. Configurations and the scope of the installation are defined below, as defined by configurations in the General Arrangement Drawing, drawing GAL01-5710-001. Table 1: STC Configurations Configuration Installation Data Description GAL01-5710-001-001 GAL01-5720-101-001 Position/Anticollision and Recognition Light Instl, LH Side GAL01-5720-101-002 Position/Anticollision and Recognition Light Instl, RH Side GAL01-5710-001-003 GAL01-5720-101-003 Position/Anticollision Light Instl, LH Side GAL01-5720-101-004 Position/Anticollision Light Instl, RH Side Position/Anticollision Light Recognition Light Mounting Bracket Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 4 subject to the restriction notice contained on page i of this document. Maintenance Practices The following maintenance practices cover the following maintenance activities associated with the installation of the wingtip position/anticollision support bracket installation: • Physical removal of wingtip position/anticollision lights • Physical removal of forward recognition light • Removal of wingtip position/anticollision bracket • Installation of wingtip position/anticollision bracket • Physical installation of wingtip position/anticollision lights • Physical installation of forward recognition light Removal and installation of the wingtip position/anticollision and forward recognition lights include physical mounting removal/installation only and does not account for wiring or function of the light assemblies. Wiring, activation, and function are provided under a separate design approval. Required equipment and materials are defined in the table below. Table 2: Maintenance Equipment and Materials ITEM DESIGNATION A. #2 Phillips Screwdriver Screwdriver B. Acetone per ASTM D239 Cleaning Agent Notes: Applicable to all Maintenance Activity: 1. Prior to performing any maintenance activity, the aircraft shall be in a safe condition for maintenance. 2. During all maintenance activity, remove all parts as serviceable and retain hardware for reinstallation. 3. Use maintenance best practices defined in Chapter 20 of the aircraft Maintenance Manual, AC 43.13, or equivalent. Position / Anticollision Light Removal Note: Light removal instructions are only for the physical removal of the light and do not address deactivation of the light. Prior to completing these steps to remove the light, ensure the light has been made safe for maintenance (disconnected from aircraft power) with the maintenance instructions provided with the light installation/activation (not covered under the scope of this STC). 1. Job Setup a. Gain Access to the wing tip b. Remove the attaching screws from the transparent shield (lens cover) and remove from the wingtip i. Retain shield (lens cover) and retain hardware for reinstallation. 2. Light Removal a. Remove the four screws from the LED light removing the light from the mounting plate as shown in Figure 2. b. Remove the light baseplate from the aircraft by removing the three countersunk screws in the baseplate common to the bracket. Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 5 subject to the restriction notice contained on page i of this document. Figure 2: Wingtip Position/Anticollision LED Light Detail Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 6 subject to the restriction notice contained on page i of this document. Forward Recognition Light Removal Note: Light removal instructions are only for the physical removal of the light and do not address deactivation of the light. Prior to completing these steps to remove the light, ensure the light has been made safe for maintenance (disconnected from aircraft power) with the maintenance instructions provided with the light installation/activation (not covered under the scope of this STC). 1. Job Setup a. Gain Access to the wing tip b. Remove the attaching screws from the transparent shield (lens cover) and remove from the wingtip i. Retain shield (lens cover) and retain hardware for reinstallation. 2. Light Removal a. Remove the MS35206-212 screw and corresponding NAS1149GN432P washer and MS35206-225 screw and corresponding NAS1149GN632P washer from the LH and RH side of the GAL01-5100- 401-007 bracket as shown in Figure 3. b. Remove the forward recognition light from the aircraft. Figure 3: Forward Recognition LED Light Removal Detail VIEW LOOKING INBD AT RH WINGTIP FWD Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 7 subject to the restriction notice contained on page i of this document. Bracket Removal, P/N GAL01-5100-401-001 or GAL01-5100-401-002 Note: In order to remove the bracket, P/N GAL01-5100-401-001 or GAL01-5100-401-002, any lights attached to the bracket (position/anticollision light and forward recognition light, as applicable) must be removed from the bracket. 1. Job Setup a. Gain Access to the wing tip b. Remove the attaching screws from the transparent shield (lens cover) and remove from the wingtip i. Retain shield (lens cover) and retain hardware for reinstallation. c. Ensure any lights attached to the bracket have been removed from the bracket in accordance with steps contained in the previous section. 2. Bracket Removal a. Remove the (4) MS27039-0805 screws and corresponding NAS1149G832P washers from the bracket, as identified in the figure below. b. Remove the bracket, P/N GAL01-5100-401-001 or GAL01-5100-401-002, from the aircraft. Retain for installation. Figure 4: Bracket Removal Detail VIEW LOOKING INBD AT RH WINGTIP, LH OPP FWD MS27039-0805 Screw NAS1149G832P Washer Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 8 subject to the restriction notice contained on page i of this document. Bracket Installation Note: In order to remove the bracket, P/N GAL01-5100-401-001 or GAL01-5100-401-002, any lights attached to the bracket (position/anticollision light and forward recognition light, as applicable) must be removed from the bracket. 1. Bracket Installation a. Use cleaning agent and a clean cloth to clean the wingtip area as required to remove any unwanted debris, dust, oil, dirt, or etc. prior to reinstallation. b. Install the MS35206-212 screw and corresponding NAS1149GN432P washer and MS35206-225 screw and corresponding NAS1149GN632P washer to the LH and RH side of the GAL01-5100- 401-007 bracket as identified in Figure 4. 2. Restore Access a. Ensure any lights attached to the bracket have been reinstalled to the bracket in accordance with steps contained in the subsequent section prior to returning the aircraft to service. Position / Anticollision Light Installation Note: Light installation instructions are only for the physical mounting of the light and do not address activation and operation of the light. Prior to completing these steps to install the light, ensure the mounting bracket has been installed on the aircraft. 1. Job Setup a. Ensure bracket, P/N GAL01-5100-401-001 or GAL01-5100-401-002, is installed on the aircraft. 2. Light Installation a. Install the light baseplate from the aircraft by installing the three MS24693-26 countersunk screws in the baseplate common to the bracket. b. Install the four screws from the LED light fastening the light to the mounting plate as shown in Figure 2. c. Ensure the light is correctly hooked up to the aircraft electrical system and is fully functional after installation. i. Function and operation of the light are not part of the scope of this STC. Refer to additional approval data for instructions on electrical integration and operational checks. 3. Restore Access a. Install the transparent shield (lens cover) with the attaching screws on the wingtip. Innoviator, LLC. AMM Supplement - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-AMM-26156 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 9 subject to the restriction notice contained on page i of this document. Forward Recognition Light Installation Note: Light installation instructions are only for the physical mounting of the light and do not address activation and operation of the light. Prior to completing these steps to install the light, ensure the mounting bracket has been installed on the aircraft. 1. Job Setup a. Ensure bracket, P/N GAL01-5100-401-001 or GAL01-5100-401-002, is installed on the aircraft. 2. Light Installation a. Locate the forward recognition light between the sheet metal bracket, P/N GAL01-5100-401-007, as shown in Figure 3. b. Install the MS35206-225 screw and corresponding NAS1149GN632P washer from the LH and RH side of the GAL01-5100-401-007 bracket as shown in Figure 3. c. Manipulate the forward recognition light to the desired angle and install the MS35206-212 screw and corresponding NAS1149GN432P washer on the LH and RH sides of the bracket to fix in place. 3. Restore Access a. Install the transparent shield (lens cover) with the attaching screws on the wingtip 3189 Princeton Road Hamilton, OH 45011 513-907-4257 DOCUMENT NO. GAL01-ICA-26115 REVISION LEVEL IR INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR Installation of Wingtip Position/Anticollision Light Support Bracket Textron Aviation Inc. Bonanza and Baron Aircraft Aircraft TCDS 3A15, A-777, 3A16 Aircraft Serial Number: ____________ Aircraft Registration Number: ______________ FAA STC: _________________ This supplement must be attached to the Airplane Instructions for Continued Airworthiness (Maintenance Manuals). The information contained herein supplements the basic Instructions for Continued Airworthiness only in those areas listed, when the aircraft is modified with the STC listed above. For limitations and procedures not contained in this supplement, consult the basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). The inspections specified in this document are FAA accepted. If applicable, the referenced airworthiness limitations are FAA approved. The Airworthiness Limitations section is FAA approved and specifies maintenance required under §43.16 and §91.403 of the Federal Aviation Regulations unless an alternative program has been approved. Prepared By: (Signature on File) 04/30/2021 Z. Kaufman, Structural Engineering, Innoviator LLC Date Checked By: (Signature on File) 04/30/2021 S. Marsan, Structures DER, Innoviator LLC Date Approved By: (Signature on File) 04/30/2021 S. Marsan, Structures DER, Innoviator LLC Date PROPRIETARY DOCUMENT The information herein is privileged and confidential and shall not be disseminated, duplicated, reused or disclosed in any way without the prior written permission of Innoviator, LLC. Permission of use letter per 14 CFR §21.120 permits an operator to use Innoviator, LLC’s STC data to modify their aircraft. Innoviator, LLC. does not inhibit or restrict transmission or use of ICA data for the sole purpose of maintenance on an aircraft modified with Innoviator, LLC’s STC. © Innoviator, LLC 2021 All Rights Reserved Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 1 subject to the restriction notice contained on page i of this document. LIST OF REVISIONS Revision Level Pages Affected Description of Revision Approved Date IR All Initial Release See Cover Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 2 subject to the restriction notice contained on page i of this document. TABLE OF CONTENTS 1.0 REFERENCES ............................................................................................................................................... 4 2.0 INTRODUCTION .......................................................................................................................................... 5 2.1 Purpose .................................................................................................................................. 5 2.2 Distribution of ICA Changes ................................................................................................. 5 2.3 Description ............................................................................................................................ 5 2.4 Acronyms, Abbreviations and Definitions ............................................................................. 7 3.0 CERTIFICATION REQUIREMENTS .......................................................................................................... 7 4.0 ATA CHAPTER 0010 – AIRCRAFT MANUALS........................................................................................ 8 5.0 ATA CHAPTER 5 – INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE ......................... 8 5.1 Position/Anticollision Light and Forward Recognition Light ............................................... 8 6.0 ATA CHAPTER 6 – DIMENSIONS & AREAS ........................................................................................... 8 6.1 Aircraft Features ................................................................................................................... 8 6.2 Location ................................................................................................................................. 8 7.0 LIFTING AND SHORING ............................................................................................................................ 9 7.1 Jacking Information............................................................................................................... 9 7.2 Lifting Instructions ................................................................................................................ 9 7.3 Shoring Instructions .............................................................................................................. 9 8.0 ATA CHAPTER 8 – LEVELING & WEIGHING ......................................................................................... 9 8.1 Leveling Information ............................................................................................................. 9 8.2 Weight and Determination of CG Instructions ...................................................................... 9 9.0 ATA CHAPTER 9 – TOWING & TAXING ............................................................................................... 10 9.1 Tow Information .................................................................................................................. 10 9.2 Taxiing Information ............................................................................................................. 10 10.0 ATA CHAPTER 10 – PARKING AND MOORING ................................................................................... 11 10.1 Mooring Information ........................................................................................................... 11 Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 3 subject to the restriction notice contained on page i of this document. 10.2 Parking Instructions ............................................................................................................ 11 10.3 Storing Limitations .............................................................................................................. 11 11.0 ATA CHAPTER 11 – PLACARD & MARKING ....................................................................................... 11 11.1 Placards and Marking Information ..................................................................................... 11 12.0 ATA CHAPTER 12 – SERVICING ............................................................................................................. 12 12.1 Component Removal/Installation ........................................................................................ 12 12.2 Lubrication Information ...................................................................................................... 12 12.3 Equipment Required for Servicing ...................................................................................... 12 12.4 Consumable Materials......................................................................................................... 12 13.0 AIRWORTHINESS LIMITATIONS SECTION ......................................................................................... 12 Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 4 subject to the restriction notice contained on page i of this document. 1.0 REFERENCES The most recent revisions of the following references are used in this document. Revisions to Innoviator documents are controlled by Innoviator Data lists. Contact Innoviator for latest document revisions at tech.support@innoviator.com. Table 1: References Data Title 14CFR Part 23 Airworthiness Standards: Commuter Category Airplanes 8110.54A Instructions for Continued Airworthiness, Responsibilities, Requirements, and Contents AC 120-27E Aircraft Weight and Balance Control GAL01-IDL-26168 Installation Data List GAL01-5710-001 General Arrangement – Wingtip Anticollision Light Support Bracket Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 5 subject to the restriction notice contained on page i of this document. 2.0 INTRODUCTION 2.1 Purpose This document provides a list of Instructions for Continued Airworthiness (ICA) for the installation of wingtip anticollision light support brackets on the Textron Aviation Inc. Bonanza and Baron Aircraft. Specific applicable models are detailed on the General Arrangement Drawing GAL01-5710-001. This document includes additional maintenance tasks in addition to and not covered by OEM maintenance activity and manuals. This manual satisfies the FAA requirement that Design Approval Holder (DAH) provide “Instructions for Continued Airworthiness” (ICA) as specified in CFR 14 Part 23.1529 and Appendix G to 14 CFR Part 23. The scheduled maintenance tasks in this document should not be considered all-inclusive. The operator has the final responsibility to decide what to do and when to do it. Additional temporary requirements in the form of Service Letters, Service Bulletins, and Airworthiness Directives are the responsibility of airline and/or operator to incorporate. 2.2 Distribution of ICA Changes All revisions to this document will be accounted for in the revision block and/or by use of vertical change bars in the left-hand margin where information has been changed or added. All revisions to this document must be submitted to and accepted by the FAA AEG prior to distribution. Changes to this document or to the reference data listed within this document shall be disseminated by Innoviator, within 14 days after FAA acceptance of the data to the Aircraft Operator/Owner to ensure continued safe operation and maintenance. A list of all aircraft affected by this modification is maintained by Innoviator. Revisions to this document will be distributed to all operators for the aircraft affected by this modification. Aircraft Owners/Operators are encouraged to provide up-to-date information to Innoviator to ensure timely access to new information. Contact Innoviator at: Innoviator Flight Science 15840 Pilot Dr. Sisters, Oregon 97759 2.3 Description This STC installs brackets for the structural mounting of LED wingtip position/anticollision lights. Aftermarket LED position/anticollision lights are not exact form/fit replacements for the OEM wingtip position/anticollision lights. Structure provided in this STC mounting provisions only and does not approve the function of the replacement LED wingtip position/anticollision lights. Additional approvals are required. This STC also provides mounting provisions for a forward recognition light should the operator choose to utilize the provisions to install a forward recognition light. Forward recognition lights do not require FAA- approval. Mounting and activation of the forward recognition light is the responsibility of the operator. Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 6 subject to the restriction notice contained on page i of this document. Figure 1: Installation Detail The mounting bracket, shown in yellow in the figure above, is attached to the aircraft via 6 screws. Position/Anticollision light and recognition light (if used) are attached via screws as well. Installation and removal of these lights and the bracket are defined within the AMM supplement defined in Table 4. Configurations and the scope of the installation are defined below, as defined by configurations in the General Arrangement Drawing, drawing GAL01-5710-001. Table 2: STC Configurations Configuration Installation Data Description GAL01-5710-001-001 GAL01-5720-101-001 Position/Anticollision and Recognition Light Instl, LH Side GAL01-5720-101-002 Position/Anticollision and Recognition Light Instl, RH Side GAL01-5710-001-003 GAL01-5720-101-003 Position/Anticollision Light Instl, LH Side GAL01-5720-101-004 Position/Anticollision Light Instl, RH Side Position/Anticollision Light Recognition Light Mounting Bracket Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 7 subject to the restriction notice contained on page i of this document. 2.4 Acronyms, Abbreviations and Definitions ABBREVIATION DEFINITION CFR Code of Federal Regulations DTA Damage Tolerance Analysis FAA Federal Aviation Administration ICA Instructions for Continued Airworthiness INBD Inboard INSTL Installation IPC Illustrated Parts Catalog LRU Line Replaceable Unit MDL Master Data List MM Maintenance Manual MRB Maintenance Review Board QTY Quantity SIRM Structural Inspection and Repair Manual STA Station (Fuselage Station) STC Supplemental Type Certificate TCDS Type Certificate Data Sheets 3.0 CERTIFICATION REQUIREMENTS This document shows compliance of the following regulations. Table 3: ICA Compliance FAR Amendment Level Description 23.1529 Amdt. 25-26 Instructions for Continued Airworthiness Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 8 subject to the restriction notice contained on page i of this document. 4.0 ATA CHAPTER 0010 – AIRCRAFT MANUALS The following documents are technical publications requiring implementation into current aircraft manuals as supplements to existing documents. This manual is the primary manual with subordinate, supporting manuals identified in Table 4, below; note that not all manuals are approved data as part of the STC type design. Manuals that are not part of the type design require operator action to implement into the maintenance program. Contact Innoviator for latest revision levels. Table 4: Manual Supplements Data ID Data Description GAL01-ICA-26115* Instructions for Continued Airworthiness GAL01-AMM-26156 Aircraft Maintenance Manual Supplement *Denotes top level manual 5.0 ATA CHAPTER 5 – INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE 5.1 Position/Anticollision Light and Forward Recognition Light 5.1.1 Inspection Requirements There are no additional equipment inspection requirements for the wingtip positon/anticollision light and forward recognition light support bracket. This STC provides structural mounting only and does not activate the light functionality. When the light is utilized in the context of an activated system, it is the responsibility of the integrator to ensure that the antenna is in good, working (serviceable) condition. Refer to maintenance instructions contained within the activation/operation approval of the light for maintenance of the light functionality itself. For changes to the Airworthiness Limitations of the aircraft resulting from the installation of the access panel or the anti-collision light relocation, refer to Section 0, Airworthiness Limitations. 5.1.2 Component Overhaul Schedule None of the components installed within this modification require overhaul maintenance. 6.0 ATA CHAPTER 6 – DIMENSIONS & AREAS 6.1 Aircraft Features No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 6.2 Location The bracket and light provisions are installed in the wingtip on the aircraft, underneath the transparent shield (lens cover) of the wintip. Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 9 subject to the restriction notice contained on page i of this document. 7.0 LIFTING AND SHORING 7.1 Jacking Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 7.2 Lifting Instructions No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 7.3 Shoring Instructions No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 8.0 ATA CHAPTER 8 – LEVELING & WEIGHING 8.1 Leveling Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 8.2 Weight and Determination of CG Instructions The scope of the installation does not affect the maximum certified gross weight, CG range, or flight envelope of the aircraft. Installed components weigh either 1.58lb (configuration GAL01-5720-001-001) or 0.88lb (configuration GAL01-5720-001-003). Removed components include position light (Qty 2 at 0.25lb each) and strobe light and mounting angles (Qty 2 at 0.50lb each). The net weight change of the modification is less than 1lb and therefore does not need to be documented in the aircraft logbook per AC 120-27E. Component removal weight shall be verified by the installer as any changes to installed lighting component may affect weight and balance changes. Weight changes for the each configuration are detailed blow: Table 5: Component Weight, Configuration GAL01-5720-001-001 P/N or Designator Description Weight (lb) QTY Total Weight (lb) 650E Wingtip Position Light 0.26 2 0.52 71125 Forward Recognition Light 0.3 2 0.60 Various Sheet Metal Structure and Hardware 0.23 2 0.56 Total 1.58 Table 6: Component Weight, Configuration GAL01-5720-001-003 P/N or Designator Description Weight (lb) QTY Total Weight (lb) 650E Wingtip Position Light 0.26 2 0.52 Various Sheet Metal Structure and Hardware 0.18 2 0.36 Total 0.88 Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 10 subject to the restriction notice contained on page i of this document. 9.0 ATA CHAPTER 9 – TOWING & TAXING 9.1 Tow Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 9.2 Taxiing Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 11 subject to the restriction notice contained on page i of this document. 10.0 ATA CHAPTER 10 – PARKING AND MOORING 10.1 Mooring Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 10.2 Parking Instructions No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 10.3 Storing Limitations No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 11.0 ATA CHAPTER 11 – PLACARD & MARKING 11.1 Placards and Marking Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). Innoviator, LLC. ICA - Wingtip Position/Anticollision Light Support Bracket Doc. No. GAL01-ICA-26115 Aircraft Type: Textron Aviation Inc. Bonanza and Baron Aircraft Rev. IR Use or disclosure of data contained on this page is 12 subject to the restriction notice contained on page i of this document. 12.0 ATA CHAPTER 12 – SERVICING 12.1 Component Removal/Installation For removal and installation of the modified horizontal stabilizer cover, antenna structural provisions, and installation and removal of the wingtip position/anticollision light and forward recognition light support bracket, reference AMM supplement, GAL01-AMM-26156. 12.2 Lubrication Information No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 12.3 Equipment Required for Servicing No special tooling or equipment is required for servicing. 12.4 Consumable Materials No change to basic Airplane Instructions for Continued Airworthiness (Maintenance Manuals). 13.0 AIRWORTHINESS LIMITATIONS SECTION The Airworthiness Limitations Section (ALS) is FAA Approved and specifies maintenance required under 14 CFR 43.16 and 91.403 of the Federal Aviation Regulations (FAR) unless an alternative program has been approved. There are no airworthiness limitations associated with the modification.