# STC SR01682LA - Type: Supplemental type certificate - Status: Current, Issued - Holder: Tyler Camera Systems, United States - Description: Installation of cargo rack - Applied: July 1, 2004 - Status date: November 19, 2004 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 133 - Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE) - Certificate PDF: https://openairdocs.org/files/sha256/1d/fa/1dfa4e69f4b35494c385723cada52bc2c1820df36cbadc9ac3a6057e70e38d24 - Approved model list and other attachments: [SR01682LA.pdf](https://openairdocs.org/files/sha256/55/73/5573f0aa6786f0b030c6f1c748a71bf17bd25c92c65c557a989f8f1c80165656) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6F830476E16EA3AF86257505006BCFD7.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR01682LA ## ADs that name it (0) None. ## Approved models (11) - MD Helicopter Inc. 369 ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369A ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369D ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369E ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369F ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369FF ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369H ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369HE ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369HM ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369HS ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 500N ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. **FAA APPROVED MODEL LIST (AML) NO. SR01682LA** **TYLER CAMERA SYSTEMS FOR** INSTALLATION OF CARGO RACK ON HELICOPTER MODELS LISTED ISSUE DATE: November 19, 2004 MASTER DWG. LIST INSTALLATION REM AML ITEM AIRCRAFT AIRCRAFT ORIGINAL CERTIFICATION INSTRUCTIONS SUPPLEMENT AMENDMENT MAKE MODEL TYPE BASIS FOR NUMBER/REV. DATE CERTIFICATE ALTERATION NO. & DATE NUMBER REV. NO. REPORT & REPORT REV. NO. CR-RFM-002 NO. DATE NO. & DATE MDHI (HUGHES) 369 H3WE CAR 6 AND MD500-001 REV. N/C INST MD5- REV. N/C INITIAL N/A 369A AMENDMENTS 03/25/04 001 8/17/04 RELEASE 369H LISTED ON TCDS 11/15/04 369HM H3WE 369HS 369HE 369D 369E 369F 369FF 500N Original Signed by MAURICE P. COOK FAA APPROVED : **MANAGER, AIRFRAME BRANCH LOS ANGELES AIRCRAFT CERTIFICATION OFC.** ### SR01682LA.pdf United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ 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 3 This certificate may be transferred in accordance with FAR 21.47. Number SR01682LA This Certificate issued to 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. * Description of Type Design Change: Installation of cargo rack in accordance with FAA Approved Tyler Camera Systems Master Drawing List No. MD500-001, Revision N/C, dated March 25, 2004, and a copy of FAA Approved Rotorcraft Flight Manual Supplement No. CR-RFM-002, dated November 15, 2004 or later FAA Approved Revisions. Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed on AML No. SR01682LA 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 that aircraft. (Continued) 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. Tyler Camera Systems 14218 Aetna Street Van Nuys, California 91401 ** See attached FAA Approved Model List (AML) No. SR01682LA for list of approved rotorcraft * models and applicable airworthiness regulations. Original Product Type Certificate Number : Make : Model : Date of application : July 1, 2004 Date of issuance : November 19, 2004 Date reissued : Date amended : By direction of the Administrator _______________________________________________________ ( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office _______________________________________________________ ( Title) United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) _____________________________________________________________________________________________________________________________________ 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 3 of 3 This certificate may be transferred in accordance with FAR 21.47. Number SR01682LA Limitations and Conditions (Continued): The provisions of the Supplemental Type Certificate are applicable only to those aircraft which are listed on the attached FAA Approved Model List of MDHI (Hughes) Helicopter models. This cargo rack structure approved for all cargo only installations having a maximum payload weight of not more than 500 pounds per side and frontal area not to exceed 3.2 square feet. No passengers may be carried external to the aircraft on the cargo racks. Crew members or other persons necessary for the conduct of the external load operations may be carried in accordance with 14 CFR Section 133.35. The lateral center of gravity (CG) of models 369D (MD 500D), 369E (MD 500E), 369FF (MD 530F) and 500N (MD 520N) may be extended to ± 5.0 inches with a forward airspeed limitation of 70 KCAS and a sideward/rearward airspeed limitation of 20 KCAS. A copy of this Certificate and FAA Approved Model List (AML) No. SR01682LA, dated November 19, 2004, or later FAA Approved revision, must be maintained as part of the permanent records 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. - END - ## Every issue (1) - November 19, 2004: Issued, Current. [certificate](https://openairdocs.org/files/sha256/1d/fa/1dfa4e69f4b35494c385723cada52bc2c1820df36cbadc9ac3a6057e70e38d24), [SR01682LA.pdf](https://openairdocs.org/files/sha256/55/73/5573f0aa6786f0b030c6f1c748a71bf17bd25c92c65c557a989f8f1c80165656) --- 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.