N7136J

No registry detail on file · not in current registry

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

36 reports on file, 1995-02-14 – 1997-05-28.

OTHER · 1997-05-28 Matched by certificate designator
ATA 7120

Part: BIPOD — PITTED (ENG MT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9930
OTHER · 1997-05-28 Matched by certificate designator
ATA 7120

Part: BEARING CUP — PITTED (ENG MT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9932
OTHER · 1997-05-28 Matched by certificate designator
ATA 5320

Part: SUPPORT LOWER — PITTED (TB SUPPORT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9935
OTHER · 1997-05-28 Matched by certificate designator
ATA 7120

Part: BEARING CUP — PITTED (ENG MT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9933
OTHER · 1997-05-28 Matched by certificate designator
ATA 7120

Part: BIPOD — PITTED (ENG MT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9931
OTHER · 1997-05-28 Matched by certificate designator
ATA 5500

Part: BEARING — PITTED (ENG MT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9934
OTHER · 1997-05-28 Matched by certificate designator
ATA 6710

Part: CONTROL ROD — CORRODED (M/R CONTROL)

ONE TUBE DENTED AND OTHERS CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE TUBES.

Source: SDR HAIHEEA9929
OTHER · 1997-05-28 Matched by certificate designator
ATA 6220

Part: CONTROL ROD — CORRODED (M/R)

TUBES CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE TUBES.

Source: SDR HAIHEEA9928
OTHER · 1997-05-28 Matched by certificate designator
ATA 5320

Part: BEARING — PITTED (TB SUPPORT)

PITTED BEYOND LIMITS IN BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9936
OTHER · 1997-05-13 Matched by certificate designator
ATA 5500

Part: SUPPORT — PITTED (EMPENNAGE)

PITTED BEYOND LIMITS ON BEARING SEAT AREA. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9873
OTHER · 1997-04-23 Matched by certificate designator
ATA 6710

Part: ROD END ASSY — CORRODED (M/R)

ROD END ASSY CORROSION PITS ON THREADS. REPLACED WITH SERVICEABLE PARTS.

Source: SDR HAIHEEA9515
OTHER · 1997-04-23 Matched by certificate designator
ATA 6700

Part: ROD END ASSY — CORRODED (FLT CONTROL)

ROD ASSY CORROSION PITS ON THREADS. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9516
OTHER · 1997-04-23 Matched by certificate designator
ATA 6700

Part: ROD END BEARING — CORRODED (FLT CONTROL)

BEARINGS ROUGH AND CORROSION PITS ON THREADS. REPLACED WITH SERVICEABLE PARTS.

Source: SDR HAIHEEA9514
OTHER · 1997-04-23 Matched by certificate designator
ATA 6710

Part: END BEARING — FROZEN (M/R CONTROL)

BEARINGS FROZEN. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9520
OTHER · 1997-04-23 Matched by certificate designator
ATA 7120

Part: BUSHING — CORRODED (ENG MOUNT)

CORROSION PITS ON INSIDE OF BUSHING BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9519
OTHER · 1997-04-23 Matched by certificate designator
ATA 7120

Part: FLANGE — PITTED (ENG MOUNT)

FLANGE PITTED BEYOND LIMITS ON SPINDLES AND CHAFED ON FLANGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9518
OTHER · 1997-04-23 Matched by certificate designator
ATA 6700

Part: ROD END ASSY — CORRODED (FLT CONTROL)

ROD END ASSY CORROSION PITS ON THREADS. REPLACED WITH SERVICEABLE PART.

Source: SDR HAIHEEA9517
OTHER · 1997-04-16 Matched by certificate designator
ATA 3453

Part: LORAN — INOPERATIVE (COCKPIT)

LORAN INOPERATIVE.

Source: SDR HAIHEEA9386
OTHER · 1997-03-27 Matched by certificate designator
ATA 6410

Part: BLADE — PAINT PEEL (T/R)

BLADE PAINT PEELING.

Source: SDR HAIHEEA9247
OTHER · 1997-01-29 Matched by certificate designator
ATA 6240

Part: INDICATOR — ERRATIC (TRIPLE TACH)

ROTOR NEEDLE HAS ERRATIC INDICATION. TIME SINCE REPAIR 7:50.

Source: SDR HEEA978963
Earlier reports · 1995–1996 · 16 reports

1996

OTHER · 1996-12-13 Matched by certificate designator
ATA 7714

Part: INDICATOR — WIRE BROKEN (TRIPLE TACH)

TRIPLE TACH REAR CONNECTOR SEPARATED FROM CAN AND WIRE BROKEN. TIME SINCE REPAIR 0:00.

Source: SDR HEEA968721
OTHER · 1996-12-11 Matched by certificate designator
ATA 2562

Part: ELT — MALFUNCTION (COCKPIT)

ELT COMES ON WITH EACH LIGHTNING BOLT.

Source: SDR HEEA968693
OTHER · 1996-12-10 Matched by certificate designator
ATA 6410

Part: BLADE — PAINT PEEL (T/R)

ORIGINAL PAINTS PEELING AND RUBBER COATINGS DAMAGED ON BOTH BLADES. SEE MMIR# HEEA0008651 FOR ADDITIONAL T/R BLADE REPLACED.

Source: SDR HEEA968652
OTHER · 1996-12-10 Matched by certificate designator
ATA 6410

Part: BLADE — PAINT PEEL (T/R)

ORIGINAL PAINTS PEELING AND RUBBER COATINGS DAMAGED ON BOTH BLADES. SEE MMIR# HEEA0008652 FOR ADDITIONAL T/R BLADE REPLACED.

Source: SDR HEEA968651
INADEQUATE Q C · 1996-10-17 Matched by certificate designator
ATA 7250

Part: LAB SEAL — EXCESS RUNOUT (POWER SECT)

RECEIVING INSPECTION REVEALED: EXCESSIVE RUNOUT ON LAB SEAL BORE. TIR .006 INSTALLED AND NOT INSTALLED IN SUPPORT. INSTALLED A NEW LAB SEAL.

Source: SDR HEEA968378
OTHER · 1996-10-11 Matched by certificate designator
ATA 2562

Part: ELT — MALFUNCTION (COCKPIT)

ELT GOES OFF INADVERTENTLY.

Source: SDR HEEA968242
INADEQUATE Q C · 1996-08-13 Matched by certificate designator
ATA 7250

Part: INTERNAL SUMP — LEAKING (TURBINE)

RECEIVING INSPECTION REVEALED: LEAKING THROUGH INTERNAL SUMP GRAPHITE DURING PRESSURE CHECK. REPLACED DISCREPANT PART.

Source: SDR HEEA967648
OTHER · 1996-08-13 Matched by certificate designator
ATA 7240

Part: LINER — DEFECTIVE (COMBUSTION SEC)

ENGINE REMOVED DUE TO TURBINE OVERHAUL. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL (-1.1). TURBINE PRODUCED (+3.2) POWER WITH OVERHAULED REPLACEMENT COMB LINER. REPLACED DISCREPANT PART.

Source: SDR HEEA967647
OTHER · 1996-08-02 Matched by certificate designator
ATA 7250

Part: NOZZLE — OUT OF SPEC (1ST STAGE)

PART INSTALLED IN TURBINE AND TEST CELL RAN PRODUCED -5.9-4.5-4.5 (NOTE TURBINE PRODUCED -1.1,+0.5+0.5 WITH DALLAS AIRMOTIVE OH #1 NOZZLE) UPON INSPECTION OF PART NOTED THE FOLLOWING: OUT OF OVERHAUL SPECS.A,B,E & F. REPLACED DISCREPANT PART.

Source: SDR HEEA967628
OTHER · 1996-07-02 Matched by certificate designator
ATA 7230

Part: TIE BOLT — DEFECTIVE (ENG COMP)

UPON ASSEMBLY OF COMPRESSOR NOTED THE FOLLOWING: UNABLE TO ENGAGE THREADS INTO 1ST STAGE WHEEL. UPON INSPECTION OF PART NOTED THE FOLLOWING: IMPROPERLY MACHINED THREADS ON TIE BOLT FWD END. REPLACED DISCREPANT PART.

Source: SDR HEEA967494

1995

OTHER · 1995-11-07 Matched by certificate designator
ATA 2822

Part: BEARING — FAILED (PUMP)

BEARING IS ROUGH AND COMING APART. BEARING RECEIVED WITH OVERHAUL KIT P/N D107318-21.

Source: SDR HEEA955975
OTHER · 1995-07-24 Matched by certificate designator
ATA 6240

Part: TRANSMITTER — DEFECTIVE (MAST MOMENT)

TRANSMITTER CAUSES INDICATOR TO READ LOW.

Source: SDR HEEA955419
OTHER · 1995-07-24 Matched by certificate designator
ATA 6240

Part: INDICATOR — READS LOW (MAST MOMENT)

TRANSMITTER CAUSES INDICATOR TO READ LOW.

Source: SDR HEEA955420
OTHER · 1995-05-12 Matched by certificate designator
ATA 2840

Part: TRANSDUCER — INOPERATIVE (FUEL PRESS)

NO INDICATION WHEN CONNECTED TO AIRCRAFT.

Source: SDR HEEA954991
WARNING INDICATION · 1995-03-24 Matched by certificate designator
ATA 7210

Part: ENGINE ASSY — CHIP LIGHT (NR 1)

#1 ENGINE CHIP LIGHT CAME ON IN FLIGHT. (FOUND METAL ON THE LOWER PLUG) INSTALLED SERVICEABLE ENGINE AND RETURNED AIRCRAFT TO SERVICE.

Source: SDR HEEA954637
OTHER · 1995-02-14 Matched by certificate designator
ATA 7920

Part: FILTER ASSEMBLY — BUTTON POPS (BY PASS)

BY-PASS BUTTON POPS OUT AFTER RUNNING AIRCRAFT APPROXIMATELY 5 MINUTES.

Source: SDR HEEA954349