What it approves
Fabrication of Onboard Model 200-258-00 (without load weigh), 200-259-00 (with load weigh) or 200-259-01 (with load weigh and 5V Lighting) cargo hook system
What the certificate saysPartly OCR
Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers.
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:
(See Continuation Sheet Page 3 of 3 Pages) SR00898SE Onboard Systems International, LLC 13915 NW 3rd Court Vancouver, WA 98685 Part 6 the Civil Air Regulations H2SW Bell 206L; 206L-1; 206L-3; 206L-4; and 407 Fabrication of Onboard Model 200-258-00, 200-258-01, 200-259-00, 200-259-01, or 200-259-02 cargo hook system in accordance with Onboard Master Drawing List No. 155-058-00, Revision 12, dated August 15, 2011, or later Federal Aviation Administration (FAA) approved revision. Installation of these Onboard Systems kits in accordance with FAA-approved Onboard Systems Owner’s Manual listed in the table on the Continuation Sheet, or later FAA-approved revision. This modification must be inspected and maintained in accordance with FAA-approved Onboard Systems Instructions for Continued Airworthiness and Component Maintenance Manual listed in the table on the Continuation Sheet, or later FAA-approved revision.
Approval of this change in type design applies only to those Bell model rotorcraft listed above, which are equipped with an FAA approved installation of a Bell Auxiliary Equipment Kit Cargo Hook Provisions, part numbers (P/N) 206-706-341-7, -9, -103, -111, -113, -117, -123 or -125 or Onboard Systems Fixed Provisions Kit, P/N 200-328-00. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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 rotorcraft.
September 22, 2000 October 7, 2021 March 26, 2001 January 13, 2003; October 9, 2008;
January 11, 2010; February 9, 2012 For Acting Manager, Seattle ACO Branch 3
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:
SR00898SE 3
United States of America Department of Transportation Federal Aviation Administration TORIMISTRATO Supplemental Type Certificate (Continuation Sheet) Number: SR00898SE Description of the Type Design ChangeContinued:
System Part No. Owner's Manual No. Instructions for Continued Airworthiness and Component Maintenance Manual No 200-258-00 120-092-00, Revision 11, dated 123-007-00, Revision 8, dated March 11, 2010 December 22, 2009 122-005-00, Revision 21, dated April 7, 2011 200-258-01 120-092-01, Revision 0, dated 123-007-01, Revision 0, dated July 22, 2011 July 19, 2011 122-017-00, Revision 14, dated September 2, 2011 200-259-00 120-092-00, Revision 11, dated 123-007-00, Revision 8, dated March 11, 2010 December 22, 2009 122-005-00, Revision 21, dated April 7, 2011 200-259-01 120-092-00, Revision 11, dated 123-007-00, Revision 8, dated March 11, 2010 December 22, 2009 122-005-00, Revision 21, dated April 7, 2011 200-259-02 120-092-01, Revision 0, dated 123-007-01, Revision 0, dated July 22, 2011 July 19, 2011 122-017-00, Revision 14, dated September 2, 2011 Limitations and Conditions: Continued:
Rotorcraft modified in accordance with this STC must be operated in accordance with FAA approved Onboard Systems Rotorcraft Flight Manual Supplement (RFMS) No. 121-003-00, rev. 2, dated August 2, 2007, or later FAA approved revision, for the 200-258-00, 200-259-00, and 200-259-01 cargo hook kits or Onboard Systems RFMS No. 121-003-01, rev. 0, dated January 13, 2012, or later FAA approved revision, for the 200-258-01 and 200-259-02 cargo hook kits. A copy of this Certificate, Owner's Manual, Instructions for Continued Airworthiness, Component Maintenance Manual, and FAA approved RFMS must be maintained as part of the permanent records for the modified rotorcraft.
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 This
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 3 of 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 5
Every issue · 5
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 7, 2021 | Reissued, current | Certificate |
| February 9, 2012 | Amended, earlier issue | Certificate |
| January 11, 2010 | Amended, earlier issue | Certificate |
| October 9, 2008 | Amended, earlier issue | Certificate |
| January 13, 2003 | Amended, earlier issue | Certificate |