N405TJ

EUROCOPTER DEUTSCHLAND GMBH EC135T2 · 2005 · Valid Registration

Registered owner: AIR METHODS LLC, CO (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
AIR METHODS LLC (QMLA)Certificate holderMatched by certificate designator
AIR METHODS LLC (QMLA)Operator2025-02-17 – 2025-02-17Operator named in NTSB report

Accident & incident history

Acc · 2025-02-17 Operator named in NTSB report
EUROCOPTER DEUTSCHLAND GMBH EC135T2 None injury Part 135AIR METHODS LLC
Source: NTSB case ERA25LA129

Maintenance disclosures

C · 2025-02-17 Matched by certificate designator
ATA 6210

OBJECT STRUCK ON FINAL APPROACH TO JEFFERSON UNIVERSITY HOSPITAL. UPON SHUTDOWN, DAMAGE WAS NOTED TO THE TOP OF THE FUSELAGE AND WITNESS MARKS AND DAMAGE TO 3 OF THE ROTOR BLADES.

Source: SDR QMLA2025021720018 · FAA SDRS
O · 2021-04-20 Matched by certificate designator
ATA 5340

DURING 1000 HOUR INSPECTION, FOUND 3 ANGLES THAT ATTACH CONTROL POST TO FLOOR CORRODED. AFTER REMOVING THE ANGLES, FOUND THAT THE FLOOR UNDER THE ANGLES WAS ALSO CORRODED.

Source: SDR 2A6R2021042060106 · FAA SDRS
O · 2021-04-12 Matched by certificate designator
ATA 5311

DURING 1000 HOUR INSPECTION, THE FWD LOWER SIDE OF THE FRAME 3 BULKHEAD AT APPROX F.S. 3150 W.L. 1480 WAS FOUND TO HAVE CORROSION AT THE BOTTOM EDGE OF THE WEB.

Source: SDR 2A6R2021041260105 · FAA SDRS
O · 2021-04-12 Matched by certificate designator
ATA 5314

DURING 1000 HOUR INSPECTION, FOUND LH AND RH KEEL BEAM STRAPS (LH PN: L533M1009203 AND RH PN: L533M1010203) CORRODED NEAR THE FORWARD END OF THE CABIN FLOOR.

Source: SDR 2A6R2021041260104 · FAA SDRS
O · 2021-04-12 Matched by certificate designator
ATA 5310

PILOTS SIDE (RIGHT SIDE) COCKPIT FLOOR SKIN AT APPROX F.S. 1700 DURING 1000 HOUR INSPECTION, HEAVY CORROSION WAS FOUND ON THE TOP AND BOTTOM SKIN OF THE COCKPIT FLOOR AT THE GROUND SHEET.

Source: SDR 2A6R2021041260103 · FAA SDRS
O · 2021-03-30 Matched by certificate designator
ATA 5311

DURING INSPECTION, FOUND FRAME 1 CORRODED ON LH AND RH SIDES UNDER TAIL ROTOR CONTROL PEDALS.

Source: SDR 2A6R2021033060102 · FAA SDRS
O · 2021-03-30 Matched by certificate designator
ATA 5311

DURING INSPECTION, FOUND ONE CRACK ABOUT ONE HALF INCH LONG IN THE FRAME 5 WEB AT THE LOWER BULKHEAD ATTACH HOLE, AND ONE CRACK ABOUT ONE HALF INCH LONG AT THE LEFT SIDE LOWER BULKHEAD ATTACH HOLE.

Source: SDR 2A6R2021033060101 · FAA SDRS