STC SR04510NY

FAA DRS lists SR04510NY as Current · Issued, held by Ultimate Aerostructures, for Airbus Helicopters Deutschland GmbH MBB-BK 117 B-2. Recorded change: Installation of the Fuel Filler Port Protective Plate. Snapshot dated June 30, 2026.

FAA-listed holder

Ultimate Aerostructures

Aircraft configurations

FAA revision date

June 24, 2020

FAA status

Current · Issued

Recorded modification

What the FAA record covers

SR04510NY 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 B-2. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Airbus Helicopters Deutschland GmbH MBB-BK 117 B-2H13EU

Buyer checks

Confirm before sourcing

ST00543ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights(Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45855 only).

FAA holder: Aircraft Modification Design Services

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ST00558ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only).

FAA holder: Aircraft Modification Design Services

View record

ST00617ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only).

FAA holder: Aircraft Modification Design Services

View record

ST00794ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights(max takeoff weight - 328,000 lbs., max landing weight - 258,000 lbs., max zero fuel weiht - 245,000 lbs.) (DC-8-71 SN 46099 only).

FAA holder: Aircraft Modification Design Services

View record

What the FAA record covers

Aircraft named in FAA DRS

Confirm before sourcing

Related fuel systems STCs

Increase in aircraft operating weights(Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45855 only).

Increase in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only).

Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only).

Increase in aircraft operating weights(max takeoff weight - 328,000 lbs., max landing weight - 258,000 lbs., max zero fuel weiht - 245,000 lbs.) (DC-8-71 SN 46099 only).