N5740V

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
PDQ EXECUTIVEOperatoron 1979-07-25Operator named in NTSB report
PDQ AIR CHARTEOperatoron 1975-03-12Operator named in NTSB report

Accident & incident history

Accident · 1979-07-25 Operator named in NTSB report
BEECH 95-C55 No injuries — PDQ EXECUTIVE

Operated by PDQ EXECUTIVE (per NTSB report)

Source: NTSB case CHI79FEI35
Accident · 1975-03-12 Operator named in NTSB report
BEECH 95-C55 No injuries — PDQ AIR CHARTE

Operated by PDQ AIR CHARTE (per NTSB report)

Source: NTSB case CHI75AC064

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.

18 reports on file, 2003-08-19 – 2006-09-16.

OTHER · 2006-09-16 Matched by certificate designator
ATA 8530

Part: CYLINDER HEAD — CRACKED (ENGINE)

CYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)

Source: SDR XGN2007F00006
OTHER · 2006-09-16 Matched by certificate designator
ATA 8530

Part: CYLINDER HEAD — CRACKED (ENGINE)

CYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)

Source: SDR XGN2007F00008
OTHER · 2006-09-16 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)

Source: SDR XGN2007F00014
OTHER · 2006-09-16 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEAD CRACKED IN THE EXHAUST AREA. (K)

Source: SDR XGN2007F00013
OTHER · 2006-05-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00052
OTHER · 2006-05-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00053
OTHER · 2006-05-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00054
OTHER · 2006-05-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00055
OTHER · 2006-05-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00051
OTHER · 2006-05-04 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00043
OTHER · 2006-04-16 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00042
OTHER · 2006-03-20 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00041
OTHER · 2006-02-17 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00040
OTHER · 2006-01-04 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00039
Earlier reports · 2003–2005 · 4 reports

2005

OTHER · 2005-04-12 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00037
OTHER · 2005-04-12 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00038

2003

OTHER · 2003-09-29 Matched by certificate designator
ATA 5754

Part: HINGE — BROKEN (LT WING LE)

LT WING LEADING EDGE ASSY SAGGING AND FLEXING BETWEEN W/S 49.131 AND 91.131. WE WERE UNABLE TO DISASSEMBLE LEADING EDGE ASSEMBLY FROM THE FORWARD SPAR CAP DUE TO BROKEN (105774C-ZG18700) HINGE PIN. NOT ABLE TO DISASSEMBLE THE LEADING, COULD ONLY GUESS THAT THE HINGE AND PIN BOTHER WERE WORN. THIS WAS DISCOVERED DURING A 100 HOUR INSPECTION.

Source: SDR XGN2003F00003
INADEQUATE Q C; FLUID LOSS · 2003-08-19 Matched by certificate designator
ATA 8520

Part: CRANKCASE — CRACKED (ENGINE)

CRACK WAS DISCOVERED WHILE LOOKING FOR OIL LEAK DURING 100 HOUR INSPECTION. THIS HAS BEEN GOING ON FOR YEARS WITH MFG ENGINES. THEIR ATTEMPTS OF HEAVIER CRANKCASES AND 7TH STUD APPLICATIONS HAVE DOEN NOTHING TO GET RID OF THE PROBLEM.

Source: SDR XGN2003F00002