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
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
Related aircraft performance STCs
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