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N411HU

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2003 Schweizer 269D · Rolls-Royce 250 20&30 series

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Registered owner
Dodson International Parts Inc
Location
Rantoul, KS
Owner type
Corporation
Serial number
0040
Year built
2003
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
October 31, 2003
Certificate issued
March 9, 2019
Expires
March 31, 2029
Mode S code
A4D899
Schweizer 269DAirframe model · 3 seats · 1 engine · 12 registeredTCDS 4H12Airframe · Schweizer 269DEngine modelRolls-Royce 250 20&30 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rolls-Royce 250 20&30 model are included below.

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Airworthiness directives that may apply · 12

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1976In forceSuperseded2026
See all 16 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

NTSB ERA18LA192Accident · Minor injuriesClass 3 · LimitedFinal reportStewartstown, PAThe pilot's inability to maintain yaw control while transitioning to an out of ground effect hover due to a loss of tail rotor effectiveness.Jul 14, 2018 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Accident 20180714011209AHover/Holding · Stewartstown, PA[privacy data omitted] Was flying N411HU a Schweizer 269D with one passenger at Shoestring Airport (0P2). After approach on runway 24 and near the intersection area of runways 24 and 33 the helicopter started spinning in a clockwise direction contacted the…Jul 14, 2018 · Substantial damage

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR UH02008F00000Support Bracket · crackedUPON INSP OF TAIL ROTOR DAMPER ASSY, CRACK WAS FOUND IN SUPPORT BRACKET ASSY. (PN 269A332511) STOPPED DRILLED CRACK AND REPAIRED WITH A DOUBLER USING 2024T3 .025 FOR REINFORCEMENT PRO SEALED AND RIVETED IN PLACE. (K)Feb 26, 2008 · N411HU · Scwzer 269D · Rotorcraft Tail BoomSDR UH02008F00001Scroll · crackedUPON INSPECTION OF OIL COOLER FAN ASSY FOUND MANY CRACKS AROUND THE TOP MOUNT OF SCROLL ASSY. (K)Feb 20, 2008 · N411HU · Scwzer 269D · Engine Oil CoolerSDR 2008FA0000221Scroll · crackedUPON INSPECTION OF OIL COOLER FAN ASSY, FOUND MANY CRACKS AROUND THE TOP MOUNT OF SCROLL ASSY. (K)Feb 20, 2008 · N411HU · Scwzer 269D · Engine Oil CoolerSDR 2007FA0001007Skid · damagedUPON LANDING THE HELICOPTER IN A SLIGHT FWD AND LT MOTION IN FLAT GRASS AREA HEARD SLIGHT CLICK OR CLUNK, PIC DIDN`T SEE ANY DAMAGE, PICKED UP AIRCRAFT TO A HOVER AND GROUND CREW SAW FWD END OF LT SKID TUBE HANGING BELOW THE AIRCRAFT. (K)Oct 31, 2007 · N411HU · Scwzer 269D · Wheel/Ski/FloatSDR UH02007F00000None · noneDURING PRACTICE AUTOROTATION, ENGINE SHUTDOWN DUE TO THROTTLE INADVERTENTLY CLOSING INTO FUEL CUTOFF POSITION. STUDENT`S LEG CONTACTED IDLE, IDLE RELEASE BUTTON ON COLLECTIVE STICK HEAD AND THIS ALLOWED THROTTLE TO ROTATE BEYOND IDLE POSITION. HAVE CONTACTEDJun 1, 2007 · N411HU · Scwzer 269D · Standard Practices/StructuresSDR 2006F00022Sump · leakingFUEL LEAKAGE WAS DETECTED ON BOTH FUEL TANK SUMP PLATES. RH FUEL SUMP PLATE LEAKAGE WAS DRIPPING ONTO FIRESHIELD ABOVE EXHAUST DUCT (ENGINE EXHAUST). SUMP PLATES FASTENERS FOUND WITH CORRECT TORQUE. MOST LIKELY CAUSE IS AGING OF SEALANT BETWEEN CELL AND SUMP PMar 17, 2006 · N411HU · Scwzer 269D · Fuel Storage

STCs that may be installed · 45

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 45 STCs