N135WJ

EUROCOPTER DEUTSCHLAND GMBH EC 135 P2 · 2003 · Rotorcraft · 2 engines · 7 seats · 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 Corp. (QMLA)Certificate holderMatched by certificate designator
Air Methods Corp. (QMLA)Operatoron 2019-06-17Operator named in NTSB report

Accident & incident history

Accident · 2019-06-17 Operator named in NTSB report
Eurocopter EC135 No injuries Part 135Air Methods Corp.

Operated by Air Methods Corporation (per NTSB report)

Source: NTSB case GAA19CA405

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

8 reports on file, 2004-02-19 – 2024-09-18.

WARNING INDICATION · 2024-09-18 Matched by certificate designator
ATA 7300

Part: FADEC — FAILED · airframe 8,179 hrs

THE CREW AND I DEPARTED SHORTLY AFTER FOR AN APPROXIMATELY 22 MINUTE FLIGHT TO THE PICKUP LOCATION. WHILE THE AIRCRAFT WAS IN-GROUND EFFECT TO LAND AT THE SCENE; THE MASTER CAUTION, FADEC FAIL, FADEC MINR, AND FLI DEGR LIGHTS ON THE CAD APPEARED AND THE LOSS OF TOT AND TQ ON THE RESPECTIVE ENGINE #2 SIDE. IN RESPONSE, I FOCUSED ON STABILIZING THE AIRCRAFT IN HOVER AND ALLOWED THE HELICOPTER TO CONTINUE SLOWLY DOWN TO THE PAD. AFTER THE HELICOPTER WAS ON THE GROUND SAFELY, I VERIFIED THE AFFECTED ENGINE AND COMPLETED THE EMERGENCY AND SHUT DOWN PROCEDURE. INFORMED THE GROUP ONCE ENGINES WERE SECURED THAT WE HAD A FADEC FAILURE AND THAT THE AIRCRAFT WAS OUT OF SERVICE. THE PATIENT WENT BY GROUND TO THE NEAREST HOSPITAL AND THE CREW ARRANGED TRANSPORTATION BACK TO OUR BASE.

Source: SDR QMLA202409182011
OTHER · 2004-04-04 Matched by certificate designator
ATA 2497

Part: MASTER SWITCH — INOPERATIVE (COCKPIT) · airframe 119 hrs

WARRANTY. NR 2 BUS TIE OPEN ON UNIT. THIS UNIT WAS INSTALLED BY HDS AT 11.4 HRS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/26/2004

Source: SDR BAQA094251
OTHER · 2004-03-10 Matched by certificate designator
ATA 7714

Part: INDICATOR — INOPERATIVE (TRIPLE RPM) · airframe 77 hrs

BOTH N2 NEEDLES INOPERATIVE ON TRIPLE RPM INDICATOR. REPLACED WITH SERVICABLE UNIT. 03/12/2004

Source: SDR BAQA093339
NO TEST · 2004-02-29 Matched by certificate designator
ATA 2432

Part: MASTER BOX — WILL NOT TEST · airframe 58 hrs

MASTERBOX WILL NOT SELF TEST. REPLACED WITH SERVICEABLE UNIT. 03/05/2004

Source: SDR BAQA093489
OTHER · 2004-02-29 Matched by certificate designator
ATA 2432

Part: MASTER BOX — WILL NOT TEST · airframe 58 hrs

BOX WILL NOT TEST AND IS CAUSING LT GENERATOR TO FAIL. REPLACED WITH SERVICABLE MASTER BOX, 03/05/2004

Source: SDR BAQA093490
OTHER · 2004-02-19 Matched by certificate designator
ATA 6330

Part: MOUNT — CRACKED (M/R GEARBOX) · airframe 37 hrs

MAIN ROTOR GEARBOX MOUNT HAS A CRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004

Source: SDR BAQA093318
OTHER · 2004-02-19 Matched by certificate designator
ATA 6330

Part: MOUNT — CRACKED (M/R GEARBOX) · airframe 37 hrs

MAIN ROTOR GEARBOX MOUNT HAS A CRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004

Source: SDR BAQA093317
OTHER · 2004-02-19 Matched by certificate designator
ATA 6330

Part: MOUNT — CRACKED (M/R GEARBOX) · airframe 37 hrs

MAIN ROTOR GEARBOX MOUNT HAS ACRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004

Source: SDR BAQA093319