N831CA

HAWKER BEECHCRAFT CORP G36 · 2008 · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: MAURER ALLEN L, OH (owner ≠ operator)

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.

13 reports on file, 1995-04-29 – 2004-01-28.

OTHER · 2004-01-28 Matched by certificate designator
ATA 2731

Part: GEAR — SLIPPED (ELE TAB DIAL) · airframe 3,652 hrs · 5,016 cycles

WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TRIM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSED ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT.

Source: SDR 8313882
OTHER · 2004-01-28 Matched by certificate designator
ATA 2731

Part: GEAR — SLIPPED (ELE TAB DIAL) · airframe 3,652 hrs · 5,016 cycles

WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TRIM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSED ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT.

Source: SDR 8473735
Earlier reports · 1995–2000 · 11 reports

2000

OTHER · 2000-03-23 Matched by certificate designator
ATA 6122

Part: GOVERNOR — FAILED (LT ENGINE)

LOUD NOISE ON TAKEOFF ROLL FROM LEFT ENGINE. MAXIMUM PROP RPM 1500 RPM. REMOVED AND REPLACED LEFT PROP GOVERNOR. SYSTEM GROUND AND FLIGHT CHECK SATISFACTORY. (M)

Source: SDR 20000516AP004

1999

OTHER · 1999-10-14 Matched by certificate designator
ATA 3242

Part: BRAKE — LEAKING (LT MLG)

NR 2 BRAKE SEEPING HYD FLUID. REPLACED NR 2 BRAKE ASSEMBLY IAW CLEVELAND MAINTENANCE MANUAL. (M)

Source: SDR 99ZZZM733

1998

FLUID LOSS · 1998-07-31 Matched by certificate designator
ATA 7314

Part: PUMP — LEAKING (LT ENGINE)

FUEL LEAK FROM LT COWLING. FUEL PUMP, ENGINE DRIVEN, LEAKING. REPLACED FUEL PUMP.

Source: SDR 98ZZZX3123
OTHER · 1998-07-07 Matched by certificate designator
ATA 2435

Part: START/GEN — FAILED (LT NACELLE)

LT GENERATOR INOP. GENERATOR FAILURE. REPLACED LEFT START/GEN.

Source: SDR 98ZZZM563

1997

OTHER · 1997-08-25 Matched by certificate designator
ATA 3230

Part: SERVICE VALVE — WORN (LT WING)

LANDING GEAR SLOW TO EXTEND.

Source: SDR 97ZZZX3961
OTHER · 1997-07-18 Matched by certificate designator
ATA 3425

Part: DPU — FAILED (AVIONICS BAY)

PILOTS DISPLAY PROCESSING UNIT INOPERATIVE.

Source: SDR 97ZZZM755
OTHER · 1997-07-18 Matched by certificate designator
ATA 3425

Part: DISPLAY PROCESSR — FAILED (COCKPIT)

NR 2 DISPLAY PROCESSOR FAILED ON DEPARTURE.

Source: SDR 97ZZZM786
OTHER · 1997-06-24 Matched by certificate designator
ATA 2350

Part: PUSH TO TALK SW — FAILED (COCKPIT)

CREW INTERCOM INOPERATIVE. NR 2 COMM INOPERATIVE. FOUND PUSH TO TALK SWITCH FAILED. (M)

Source: SDR 97ZZZM751
OTHER · 1997-05-18 Matched by certificate designator
ATA 2750

Part: FLAP MOTOR — FAILED (TE FLAPS)

FLAPS STUCK IN 17 DEGREE POSITION. REPLACED FLAP MOTOR.

Source: SDR 97ZZZX2977

1996

OTHER · 1996-01-03 Matched by certificate designator
ATA 5530

Part: RIVETS — LOOSE (VERT TAB)

DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE.

Source: SDR 96ZZZX1651

1995

OTHER · 1995-04-29 Matched by certificate designator
ATA 2562

Part: ELT — BROKEN (AFT FUSELAGE)

ELT TRANSMITTING (45 MINUTES). FOUND UNIT WET AND MOUNTING TRAY CRACKED. REMOVED AND REPLACED MOUNTING TRAY, P/N 452-3050.

Source: SDR 95ZZZM63