STC SR01074DE
FAA DRS lists SR01074DE as Current · Amended, held by Metro Aviation Inc, for Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2, Airbus Helicopters Deutschland GmbH MBB-BK 117 D-2, and Airbus Helicopters Deutschland GmbH MBB-BK 117 D-3. Recorded change: Installation of Stryker 6086 Performance-PRO XT Gurney system and Performance Pro MX Locking System. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of Stryker 6086 Performance-PRO XT Gurney system and Performance Pro MX Locking System.
SR01074DE identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2, Airbus Helicopters Deutschland GmbH MBB-BK 117 D-2, and Airbus Helicopters Deutschland GmbH MBB-BK 117 D-3. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 and Airbus Helicopters Deutschland GmbH MBB-BK 117 D-2, and 1 more aircraft configuration model, serial range, and configuration?
- 02Which limits, loading assumptions, performance data, and supplements apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft performance STCs
Installation of a maximum payload weight reduction to 7500 lbs in accordance with STC document AMER 2004-01, Revision 0, dated June 30, 2004, or later FAA approved revision. The Airplane Flight Manual Supplement (AFMS) document number AMER 2004-01C, Revision 0, dated October 5, 2004, or later FAA approved revision is required.
FAA holder: Ameristar Jet Charter
Incorporation of change in aircraft weight and balance by supplementing the current aircraft weight and balance manual with Newport Aeronautical Development Report No. NAD 2004-101, Revsion A, dated June 16, 2004, or later FAA approved revision.
FAA holder: Newport Aeronautical Development
Installation of side-facing divan certified for take-off and landing use.
FAA holder: Gulfstream Aerospace Corporation
Approval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY).
FAA holder: Structural Integrity Engineering