# STC ST00365NY-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: PATS Aircraft LLC, United States - Description: Installation of a two tank auxiliary fuel system within fuselage pressure vessel forward of baggage compartment. - Applied: September 27, 1994 - Status date: June 11, 2009 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA) - Certificate PDF: https://openairdocs.org/files/sha256/f5/0f/f50f5046568edaf86167c5f655e6d15d13894217f7cc8969df97bdbf9f11dfb5 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6006946EAE8810B2862575F4005464C1.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST00365NY-D ## ADs that name it (1) - [AD 2008-22-01](https://openairdocs.org/ad/2008-22-01): Auxiliary fuel tanks · Boeing 727-100 Series, 727-200 Series, 727 Series and 17 more. Effective Nov 26, 2008. Named in the applicability ## Approved models (1) - Bombardier Inc. CL-600-2B19 (Regional Jet Series 100) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00365NY-D This certificate issued to: PATS Aircraft, LLC. 21652 Nanticoke Avenue Georgetown, DE 19947 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meet's the airworthiness requirement's of Part 25 of the Federal Aviation Regulations. Original Product - Type Certificate Number: A21EA Маке: Bombardier, Inc. Model: CL 600-2B19 Description of Type Design Change: Configuration 1. Installation of a two tank Auxiliary Fuel System within the fuselage pressure vessel forward of the baggage compartment in accordance with PATS, Inc. Master Drawing List, Drawing No. RJA-1-001, Rev. D dated June 16, 1995. 1. PATS, Inc. Airplane Flight Manual Supplement No. 1, Rev. A FAA approved December 31, 1997 is required with configurations 1 and 2. 2. PATS Aircraft, LLC. Airplane Flight Manual Supplement No. 200, Rev. B, FAA approved June 11, 2009, is required with configurations 5 and 6. 3. No Airplane Flight Manual Supplement is required for Configurations 3 and 4. suspended, revoked or a termination date is otherwise established by the Administrator of the Frederal Sviation Administration. Date of Application: September 27, 1994 Date Reissued: July 20, 2004 Date of Issuance: August 24, 1995 Date Amended: November 18, 1996, December 31, 1997, January 17, 2006, August 04, 2006, FEDERAL AVIATION June 11, 2009 January 5, 2007, January 29, 2007, March 27, 2008, By Direction of the Administrator an DELains TOMINSTRAT (Signature) David E. Warner DAS administrator DAS-955292-NE (Title) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00365NY-D Date of Amendment: June 11, 2009 Description of Type Design Change: (Continued): Configuration 2. Installation of a two tank Auxiliary Fuel System within the fuselage pressure vessel forward of the baggage compartment in accordance with PATS, Inc. Master Drawing List, Drawing No. RJA-1-001, Rev. F dated October 15, 1996, ADCN #31, dated October 17, 1996. Configuration 3. Installation of structural provisions only, for a two (2) Cell Auxiliary Fuel System within the fuselage pressure vessel forward of the baggage compartment in accordance with PATS Aircraft, LLC. Master Drawing List No. RJA-1-002, Rev. A dated December 5, 2005. Configuration 4. Installation of a Non-operative Two (2) Cell Auxiliary Fuel System within the fuselage pressure vessel forward of the baggage compartment in accordance with PATS Aircraft, LLC. Installation Master Drawing List RJA-1- 004, Rev. A dated July 7, 2006. Configuration 5. Installation of a two tank Auxiliary Fuel System within the fuselage pressure vessel forward of the baggage compartment in accordance with PATS Aircraft, LLC. Master Drawing List, Drawing No. RJA-1-003, Rev. E dated January 24, 2007 or the installation of Configuration 4 and incorporation of Service Bulletins ST00365NY-D-28- SB-008, Rev. IR dated January 17, 2007 and ST00365NY-D-28-SB-009, Rev. IR dated January 17, 2007. Configuration 6. Installation of a two tank Auxiliary Fuel System within the fuselage pressure vessel forward of the baggage compartment in accordance with PATS Aircraft, LLC. Master Drawing List, Drawing No. 6000-0001-MDL, Rev. B dated March 16, 2009. Limitations and Conditions: (Continued): 4. Configurations 4 and 5 require Configuration 3, Installation of structural provisions, to be previously installed. All Configurations: PATS Aircraft, LLC. Aircraft Maintenance Manual Supplement No. 1, Report No. TO-417, Revision 4 dated January 18, 2008 with The Airworthiness Limitations Section approved June 11, 2009, is required for continued airworthiness of configurations 1, 2, 3, 4, 5 and 6. 2. The installer must determine whether this design is compatible with previously approved modifications. 3. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the person written evidence of that permission. FAA Form 8110-2-1 (10-69) Page 2 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00365NY-D Date of Amendment: June 11, 2009 Limitations and Conditions: (Continued): Configurations 5 & 6 1. This modification may not be installed after August 30, 2010 unless (1) previously approved electrical wiring interconnections system (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for these installations by the FAA, or (2) revised EWIS ICA have been approved by the FAA Oversight Office (Refer § 26.11). 2. This modification may not be installed after September 19, 2012 unless (1) the § 26.35(b) requirement for a flammability exposure analysis has been approved, (2) compliance with § 26.981 at Amendment 25-125, in accordance with the § 26.35(e), has been found for this STC, or (3) service instructions for design changes necessary to meet § 25.981 at Amendment 25-125 and associated airworthiness limitations have been approved for installations of this STC prior to September 19, 2012. Unless the STC is amended to remove this limitation after the accomplishment of the above tasks, the STC installer will need to have a letter from the FAA Oversight Office documenting compliance with these requirements in order to install this STC after September 19, 2012. 3. This modification may not be installed after December 11, 2009 unless the flammability exposure analysis required by 14 CFR 26.35 (b) has been FAA approved. Certification Basis. Configurations 5 & 6 1. Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for these modifications are as follows: The existing type certification basis for Bombardier Inc. CL600-219 as shown on FAA type certificate data sheet A21EA with the following exceptions: 25.561 Amendment 25-64 25.981 Amendment 25-102 SFAR 88 Compliant Part 26 regulations Part 14 CFR para. 21.101(g), applicable provisions of 14 CFR Part 26 must be met. ..END... FAA Form 8110-2-1 (10-69) Page 3 of 3 21652 Nanticoke Avenue DECRANE AEROSPACE Georgetown, DE 19947 USA PATS Aircraft Completions Tel: 302.855.5888 Fax: 302.855.5801 June 11, 2009 Federal Aviation Administration - NYACO Attention: Mr. Anthony Socias Manager - NYACO 1600 Stewart Avenue 4th Floor, Suite 410 Westbury, NY 11590 Subject: STC ST00365NY-D Transmittal Dear Mr. Socias, In accordance with our DAS Manual procedures, I have issued Supplemental Type Certificate (STC) ST00365NY-D for installation of a Configuration 6 Auxiliary Fuel System in Bombardier CL 600-2B19 Aircraft (per DAS Project No. DAS-GED-P057). Based upon my review of the data presented and results of the successful conformity inspections, I am issuing STC ST00365NY-D, date amended June 11, 2009, approving the installations. Fabrication of parts under this STC shall be in accordance with Master Drawing List 6000-0005- MDL revision B dated June 8, 2009. A copy of this STC must be maintained as part of the permanent records for the aircraft. If you have any questions, please do not hesitate to contact me. ncerely, SEtrainer David E. Warner VP & Administrator of DAS-955292-NE DEW/vg Enclosure Cc: M. Taylor & S. Coyne (QC), S. Etmanski, George Duckett - NYACO (OMT Lead), Doc. Control, DAS file, Project Book 1 of 1 ## Every issue (1) - June 11, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f5/0f/f50f5046568edaf86167c5f655e6d15d13894217f7cc8969df97bdbf9f11dfb5) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.