# STC SR00507NY - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dart Aerospace Limited, Canada - Description: Installation of Emergency Escape Ladder. - Applied: October 30, 1995 - Status date: March 28, 2019 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 25, Part 26, Part 29 - Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW), [TCDS H4SW](https://openairdocs.org/tcds/H4SW) - Certificate PDF: https://openairdocs.org/files/sha256/a4/9e/a49ea61cbae8af44e6577c1a2bc3a40e22779aeae5817fc43f93d60b91eb6ea8 - Approved model list and other attachments: [SR00507NY_AML.pdf](https://openairdocs.org/files/sha256/47/26/4726aba4e7e23198ea7fc01c50ffc0548b9e4c42daabe2432281723437d7fdbf) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AEBDF76400F68B29862585AB00572C05.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00507NY ## ADs that name it (0) None. ## Approved models (6) - Bell Textron Inc. 205A ([TCDS H1SW](https://openairdocs.org/tcds/H1SW)) - Bell Textron Inc. 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW)) - Bell Textron Inc. 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Textron Inc. 412 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Textron Inc. 412CF ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Textron Inc. 412EP ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate FAA Form 8110-2 (5/14) This certificate issued to: Dart Aerospace Ltd. 1270 Aberdeen Street Hawkesbury, Ontario Canada K6A 1K7 Part ** of the Federal Aviation Regulations. **See attached FAA Approved Model List (AML) No. SR00507NY for a list of approved aircraft models and applicable airworthiness regulations. 1. Installation of Emergency Escape Ladder in accordance with Transport Canada Civil Aviation (TCCA) approved Dart Aerospace Limited (Ltd) Installation Instructions IIN-D412-707, Revision A, dated September 29, 2016 or later Transport Canada approved revision. 2. Maintenance must be in accordance with TCCA accepted Dart Aerospace Ltd, Instructions for Continued Airworthiness ICA-D412-707, Revision 0, dated October 4, 2016 or later TCCA accepted revision. 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. Date of Application: October 30, 1995 Date of Issuance: September 16, 1996 Date Reissued: January 30, 2017, March 28, 2019 Date Amended: April 11, 2017 By Direction of the Administrator Signature Title Anthony E. GalloManager New York ACO Branch Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. Page 1 of 3 IMPORT Number: SR00507NY United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3FAA Form 8110-2 (5/14) Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR00507NY To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00507NY FAA Form 8110-2 (5/14) Page 3 of 3 Date Reissued: March 28, 2019 CERTIFICATION BASIS: 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 the aircraft of AML No. SR00507NY is as follows: (a) For parts not changed or not affected by the change: The existing type certification basis for the aircraft models as shown on their respective FAA Type Certificate Data Sheet in AML No. ST00507NY. (b) For parts changed or affected by the change: The existing type certification basis for the aircraft models as shown on the FAA Type Certificate Data Sheet in AML No. ST00507NY in addition to: 14 CFR Part 29 at Amendment 29-2 plus the following later amendment; 14 CFR Part 29.21 at Amdt 29-15, 29.337(a), and 29.613(d) at Amdt 29-30, 29.853(a)(2) at Amdt 29-23, 29.1529 at Amdt 29-20. ----------END---------- Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3992NM FAA Form 8110-2 (5/14) Page 4 of 5 Date Reissued: July 12, 2018 Limitations and Conditions (continued): Aircraft Equip. Model A/C Serial Number Mfg. Date Certificate Number Original Issue Date of Certificate of Airworthiness 737-476 24432 199005 E 236720 6/26/1990 737-476 24433 199005 E 236721 7/2/1990 737-476 24434 199008 E 236745 9/10/1990 737-4B3 24750 ‡ 199008 E 236748 9/21/1990 737-53A 24788 199008 E 236753 9/26/1990 737-405 24644 199009 E 236760 10/24/1990 737-53A 24877 199010 E 236763 11/5/1990 737-476 24435 199010 E 236772 12/3/1990 737-476 24436 199101 E 236440 2/20/1991 737-4B3 24751 199107 E 294016 8/28/1991 737-405 25303 199109 E 294034 10/9/1991 737-405 25348 199109 E 294047 10/24/1991 737-476 24437 199110 E 236955 11/12/1991 737-476 24438 199110 E 236965 11/26/1991 ‡ Limitations applicable to A/C Serial Number 24750 only: 1. Installation of Invicta Ignition Mitigation/Flammability Reduction Technology in the Center Wing Tank (CWT) in accordance with STC ST03450NY is a prerequisite to the change in operating procedures. 2. Installation of Cargo Door in accordance with STC SA2969SO is a prerequisite to the change in operating procedures. 3. Operation must be in accordance with Aircraft Flight Manual Supplement Doc #14002S000l-2, Rev. IR, dated September 02, 2016. 4. Operation must be in accordance with Supplement to Airplane Weight & Balance Control and Loading Manual Supplement, Doc # 14002S0003-2, Rev. IR, dated August 26, 2016. 5. Placard installation required per SB 737-28-51-014 Rev. IR, dated July 16, 2016. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3992NM FAA Form 8110-2 (5/14) Page 5 of 5 Date Reissued: July 12, 2018 Certification Basis for A/C Serial Number 24750 only: Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48, the certification basis for this modification to the Boeing Model 737-400 Series aircraft as listed on the STC is as follows: a) The type certification basis for the Boeing Model 737-400 Series aircraft as listed on the STC and as shown on TCDS A16WE (Rev. 56) for parts not changed or not affected by the change. b) The type certification basis for the Boeing Model 737-400 Series aircraft as listed on the STC and as shown on TCDS A16WE (Rev. 56) for parts changed or affected by the change with the following exceptions: • Compliance with 14 CFR §§25.25, 25.301, 25.303 at Amendment 25-23. • Compliance with 14 CFR §25.952 at Amendment 25-40. • Compliance with 14 CFR §25.1581(a), (b), (d) at Amendment 25-72. • Compliance with 14 CFR §25.305 at Amendment 25-86. • Compliance with 14 CFR §25.561 at Amendment 25-91. • Compliance with 14 CFR §25.981(c) at Amendment 25-125. • Compliance with 14 CFR §25.307, at Amendment 25-139. • Compliance with 14 CFR §25.343 at Amendment 25-141. • Compliance with 14 CFR §26.35 at Amendment 26-3. ----------END---------- ### SR00507NY_AML.pdf **FAA APPROVED MODEL LIST (AML) NUMBER SR00507NY DART AEROSPACE LTD.** FOR **INSTALLATION OF EMERGENCY ESCAPE LADDER** Issue Date: September 16, 1996 Date Reissued: March 28, 2019 Page 1 of 1 **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TYPE** **CERTIFICATE NUMBER** **CERTIFICATION BASIS FOR** **ALTERATION** **INSTALLATION INSTRUCTIONS INSTRUCTIONS** **FOR CONTINUED** **AIRWORTHINESS** **NUMBER/DATE AML** **AMENDMENT DATE** **DOCUMENT NUMBER REVISION NO.** AND DATE 1 Bell Helicopter Textron, Inc. 205A 205A-1 H1SW See Certification Basis Section of STC SR00507NY Dart Aerospace Ltd. IIN- D412-707 Revision A, dated September 29, 2016 or later TCCA approved revision. Dart Aerospace Ltd. Instructions for Continued Airworthiness ICA- D412-707, Revision 0, dated October 4, 2016 or later TCCA accepted revision. April 11, 2017 2 Bell Helicopter Textron, Inc. 212 412 412CF 412EP H4SW FAA Approved: _________________________________________ Anthony E. Gallo Manager New York ACO Branch ## Every issue (1) - March 28, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a4/9e/a49ea61cbae8af44e6577c1a2bc3a40e22779aeae5817fc43f93d60b91eb6ea8), [SR00507NY_AML.pdf](https://openairdocs.org/files/sha256/47/26/4726aba4e7e23198ea7fc01c50ffc0548b9e4c42daabe2432281723437d7fdbf) --- 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.