N117MK

EUROCOPTER DEUTSCHLAND GMBH MBB-BK 117-B2 · 1989 · Rotorcraft · 1 engine · 4 seats · Valid Registration

Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (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
OMNIFLIGHT HELICOPTERS INCOperatoron 2005-09-22Operator named in NTSB report

Accident & incident history

Accident · 2005-09-22 Operator named in NTSB report
Eurocopter Deutschland BK-117-B2 No injuries Part 91OMNIFLIGHT HELICOPTERS INC

Operated by Omniflight Helicopters (per NTSB report)

Source: NTSB case NYC05LA145

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.

17 reports on file, 1998-09-22 – 2016-10-03.

WARNING INDICATION · 2016-10-03 Matched by certificate designator
ATA 2612

Part: FIRE WARNING — ILLUMINATED (NR 2 ENGINE) · airframe 11,167 hrs · 44,694 cycles

NR 2 ENGINE FIRE LIGHT ILLUMINATED.

Source: SDR QMLA2016100316114
FALSE WARNING · 2016-09-04 Matched by certificate designator
ATA 2612

Part: WARNING LIGHT — INTERMITTENT (FIRE DETECTION) · airframe 11,158 hrs · 44,672 cycles

NR 2 ENGINE FIRE LIGHT ILLUMINATED INTERMITTENTLY.

Source: SDR QMLA2016090416102
Earlier reports · 1998–2012 · 15 reports

2012

OTHER · 2012-10-19 Matched by certificate designator
ATA 5302

Part: CASTING — CRACKED (TAIL BOOM) · airframe 10,391 hrs · 42,316 cycles

WHILE INSPECTING THE TAIL BOOM, FOUND THE CASTING FOR THE TAIL ROTOR GEARBOX CRACKED. AWAITNG ACFT MFG TO COME AND REPAIR.

Source: SDR 2A6R201210193081
OTHER · 2012-06-25 Matched by certificate designator
ATA 5302

Part: SKIN — CRACKED (RT TAILBOOM) · airframe 10,268 hrs

ON POST FLIGHT, FOUND CRACK ON L/E OF RT VERTICAL STABILIZER THAT EXTENDED AROUND TO BOTH INBD AND OTBD SIDES.

Source: SDR QMLA2012062512106
SMOKE/FUMES/ODORS/SPARKS · 2012-03-25 Matched by certificate designator
ATA 7200

Part: UNKNOWN — SMOKE (ENGINE) · airframe 10,173 hrs

DURING RUN-UP, BOTH ENGINES STARTED & GENERATORS PLACED IN "ON" POSITION FOLLOWING NORMAL START. WHILE PILOT WAS PLACING SYS & SWITCHES TO THE CHECKLIST, PARAMEDIC IN LT SEAT ALERTED HIM TO SMOKE. LOOKED FOR SIGNS OF SMOKE, VERIFIED NO FIRE WARNING LIGHTS, & LACK OF SYS INDICATIONS OUT OF LIMITS WHILE SIMULTANEOUSLY EXECUTING EMERGENCY SHUTDOWN PROCEDURES. DURING SHUTDOWN, PILOT NOTED A 30 PERCENT NG & MGT OF 0. SHUTDOWN OF REMAINING ENGINE. CONDUCTED VISUAL INSPECTION OF THE COWLING AREA, EXHAUST AREA, AND PROCEEDED BOTH ENGINE BAYS. NOTED NOTHING ABNORMAL ON INSPECTION. FOLLOWING INSPECTION AND GROUND RUNS BY MX, CAUSE REMAINED IN QUESTION. DUE TO LACK OF CAUSE, LACK OF ANY INDICATIONS OF EXCEEDENCES, AND NORMAL GROUND RUNS, AIRCRAFT RETURNED TO SERVICE.

Source: SDR QMLA2012032512036

2009

SMOKE/FUMES/ODORS/SPARKS · 2009-04-19 Matched by certificate designator
ATA 5242

Part: PROCESSOR — SHORTED (ZONE 100) · airframe 9,311 hrs · 38,065 cycles

ACFT WAS ENROUTE FOR AN INTERFACILITY MISSION. SHORTLY AFTER LIFTING THE SHADIN UNIT BEGAN FLASHING L2 EXCEEDED. A CHECK OF ALL GAUGES INDICATED NORMAL. THEN THE COCKPIT LIGHTING AND INSTRUMENTS STARTED TO FLICKER AS IF A LOSS OF PWR. A THICK SMELL OF SMOKE WAS NOTED BY ENTIRE CREW OF AN ELECTRICAL NATURE. THE SHADIN UNIT THEN BEGAN SHOWING ROM FAILURE. ALL CREW AGREED THAT AN IMMEDIATE PRECAUTIONARY LANDING WAS PRUDENT. TWR WAS NOTIFIED ALONG WITH HCA OPERATIONS. THE ACFT WAS SAFELY PLACED IN A FIELD. PIP WAS INITIATED BY HCA OPERATIONS. CREW DEBRIEFING WAS MADE. ARRIVED AT LOCATION AND TALKED TO PILOT WHO INFORMED ME OF THE CODES RECEIVED ON THE SHADIN ETM REMOTE PROCESSOR. REMOVED THE ETM REMOTE PROCESSOR FROM THE CTR CONSOLE AND IMMEDIATELY SMELLED THE STRONG ODOR OF AN ELECTRICAL SHORT COMING FROM THE BACK OF THE ETM REMOTE PROCESSOR. HAD THE PILOT SMELL THE BACK OF THE ETM REMOTE PROCESSOR AS WELL AND HE ALSO VERIFIED THAT WAS THE SAME SMELL THAT CAUSED HIM TO MAKE A PRECAUTIONARY LANDING. FURTHER CHECK BEHIND THE CTR CONSOLE FOR POSSIBLE ELECTRICAL PROBLEMS AND COULD NOT FIND ANY. ONCE TALKING WITH THE FMS THE ETM REMOTE PROCESSOR WAS PLACARD INOP AND SIGNED OFF FOR CONTINOUS OPERATIONS IAW MEL CH. 31, ITEM 4, CATEGORY C. AS OF TODAY’S DATE 04-20-09 THE ITEM HAS BEEN MEL'D.

Source: SDR RMXA117MK007196

2007

OTHER · 2007-10-04 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (TAILCONE) · airframe 8,535 hrs

DURING SCHEDULED INSPECTION A 18MM LONG CRACK WAS DISCOVERED ON THE LT 'A' FUSELAGE FRAME 2L. THE CRACK IS ON THE LOWER SKIN ONLY OF A DOUBLE SKIN ASSEMBLY. THE CRACK ORIGINATES FROM A BOLT HOLE, EXTENDS 9MM IN EACH DIRECTION FROM THE BOLT HOLE. THE BOLT IS USED FOR THE LOWER FORWARD ATTACHING SUPPORT FOR THE ECU (ENVIRONMENTAL CONTROL UNIT)

Source: SDR RMXA2007002

2001

OTHER · 2001-06-18 Matched by certificate designator
ATA 3160

Part: SYMBOL GENERATOR — MALFUNCTIONED (COCKPIT)

SIGNAL GENERATOR, INTERMITTENTLY CAUSES EFIS TO GO TO (TEST IN PROGRESS)-THEN ERROR OF SIGNAL ON EFIS T, REMOVED AND REPLACED.

Source: SDR TI1R001481
OTHER · 2001-05-12 Matched by certificate designator
ATA 3421

Part: GYRO — TUMBLES (ATTITUDE)

ATTITUDE GYRO, TUMBLING, REMOVED AND REPLACED.

Source: SDR TI1R001467
OTHER · 2001-04-09 Matched by certificate designator
ATA 3421

Part: LIGHT — INOPERATIVE (ATTITUDE GYRO)

ATTITUDE GYRO, INTERNAL LIGHTING, INOPERATIVE. REMOVED AND REPLACED.

Source: SDR TI1R001428

2000

WARNING INDICATION · 2000-11-14 Matched by certificate designator
ATA 3416

Part: ALTIMETER — INOPERATIVE (COCKPIT)

ENCO ALTIMETER, CODE OFF, FLAG WILL NOT PULL. REMOVED AND REPLACED.

Source: SDR TI1R001371
OTHER · 2000-01-24 Matched by certificate designator
ATA 3416

Part: ENCODER — MALFUNCTIONED (COCKPIT)

ALTIMETER OUT OF CALIBRATION. DOES NOT AGREE WITH COPILOT''S ALTIMETER OR TEST BOX. OFF AT 3,000 FEET. REMOVED AND REPLACED. (X)

Source: SDR 20000413SH039

1999

OTHER · 1999-10-21 Matched by certificate designator
ATA 3340

Part: LIGHT — INOPERATIVE (FUSELAGE)

SEARCH LIGHT WILL NOT EXTEND. REMOVED AND REPLACED. (X)

Source: SDR 20000406SH034
OTHER · 1999-04-18 Matched by certificate designator
ATA 7931

Part: INDICATOR — FAILED (ENGINE OIL)

OIL PRESSURE DROPPED TO ZERO. REF: MCN 39. REMOVED AND REPLACED.

Source: SDR 99ZZZX2900
OTHER · 1999-04-08 Matched by certificate designator
ATA 2430

Part: WIRE — BROKEN (DC SYSTEM)

CABLES BROKEN. REF: MCN 32. REMOVED AND REPLACED.

Source: SDR 99ZZZX2841

1998

OTHER · 1998-10-06 Matched by certificate designator
ATA 7323

Part: GOVERNOR — MALFUNCTIONED (ENGINE)

ENGINE MGT, NG, AND TORQUE SURGES 10 TO 20 PERCENT. REMOVED AND REPLACED GOVERNOR WHICH CURED PROBLEM.

Source: SDR 99ZZZX1285
OTHER · 1998-09-22 Matched by certificate designator
ATA 3160

Part: SYMBOL GEN — FAILED (COCKPIT)

UNIT SMOKED ON POWER UP. REMOVED AND REPLACED.

Source: SDR 99ZZZX1277