N245AS

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.

13 reports on file, 1998-10-05 – 2001-12-17.

NO TEST · 2001-12-17 Matched by certificate designator
ATA 3350

Part: FUSE — BROKEN (CABIN)

FLT 4078 - DURING GROUND INSPECTION IN ATL, THE FIRST FOUR EMERGENCY FLOOR LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN FUSE IN THE FORWARD CLOSET. MAINTENANCE REMOVED AND REPLACED THE BROKEN FUSE AND ALSO CLEANED THE TERMINAL ENDS TO THE LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Source: SDR ASOA01289
OTHER · 2001-10-01 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE)

WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 18 RIGHT, BETWEEN FRAMES 19 AND 20. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIR AND REPLACEMENT. (M)

Source: SDR ASOA01194
OTHER · 2001-10-01 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE)

WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON THE SKIN SUPPORTS BETWEEN STRINGER 20 AND 21 RIGHT AT FRAMES 17, 18, 18A, 18B AND 21. CORROSION WAS ALSO FOUND ON THE SKIN SUPPORTS BETWEEN STRINGER 20 AND 19 RIGHT AT FRAMES 20 AND 21. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIR AND REPLACEMENT. (M)

Source: SDR ASOA01195
OTHER · 2001-10-01 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE)

WHILE PERFORMING MAINTENANCE IN MCN, CORROSION WAS FOUND ON STRINGER 21 RIGHT, BETWEEN FRAMES 19 AND 20 AND ALSO BETWEEN FRAMES 21 AND 22. MAINTENANCE WILL REPAIR CORROSION IAW SRM 53-10-04. THIS SRM OUTLINES REPAIR SPECIFICATIONS FOR FORWARD FUSELAGE REPAIR AND REPLACEMENT. (M)

Source: SDR ASOA01193
OTHER · 2001-09-25 Matched by certificate designator
ATA 5711

Part: SPAR CAP — CRACKED (LT WING)

DURING SCHEDULED MAINTENANCE IN MCN, THE LEFT WING FORWARD SPAR CAP WAS FOUND TO BE CRACKED. MAINTENANCE IS REPAIRING CRACKED LEFT WING SPAR CAP IAW ASA EO120-57-0114. (M)

Source: SDR ASOA01184
OTHER · 2001-08-11 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — INOPERATIVE (CABIN)

FLT 4011 - DURING DAILY INSPECTION IN ABY, MAINTENANCE FOUND THE FORWARD MOST SET OF EMERGENCY LIGHTS WENT OUT AFTER 30 SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Source: SDR ASOA01132
OTHER · 2001-07-29 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — INOPERATIVE (CABIN)

FLT 4934 - DURING GROUND INSPECTION IN DFW, FLIGHT ATTENDANT REPORTED AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LGIHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Source: SDR ASOA01121
FLUID LOSS · 2001-05-16 Matched by certificate designator
ATA 7900

Part: GARLOCK SEAL — LEAKING (ACCY GEAR BOX)

FLT 4857 - DURING FLIGHT FROM DFW TO ICT, PASSENGER REPORTED SEEING FLUID LEAKING OUT OF THE LEFT ENGINE. THE CREW VERIFIED THE LEAK AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ICT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND OIL LEAKING FROM THE DRAIN TUBE FOR THE STARTER GENERATOR. MAINTENANCE REMOVED AND REPLACED THE STARTER GENERATOR GARLOCK SEAL. OPS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Source: SDR ASOA01056
Earlier reports · 1998–2000 · 5 reports

2000

WARNING INDICATION · 2000-09-27 Matched by certificate designator
ATA 2450

Part: CIRCUIT BREAKER — INOPERATIVE (COCKPIT)

LFF-DFW - ON FINAL, CREW SELECTED FLAPS TO 45 DEGREES. CREW RECEIVED A SINGLE CHIME ELECTRICAL MESSAGE ON MAP. AT THE SAME TIME, EMERGENCY BUS OFF LIGHT CAME ON. CREW PERFORMED A GO AROUND, DECLARED AN EMERGENCY, AND LANDED SAFELY. MAINTENANCE REPLACED CIRCUIT BREAKER 0470 AND INSPECTED WIRING. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Source: SDR ASOA00105
ELECT. POWER LOSS-50 PC · 2000-02-21 Matched by certificate designator
ATA 2460

Part: CIRCUIT BREAKER — POPPED (COCKPIT)

FLT 4336 - CREW EXPERIENCED A LOSS OF EMERGENCY BUS ON SHORT FINAL. DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE FOUND CIRCUIT BREAKER POPPED. MAINTENANCE RESET CIRCUIT BREAKER. SYSTEM CHECKS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Source: SDR ASOA00027

1999

NO TEST · 1999-09-01 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Source: SDR ASOA99086
NO TEST · 1999-09-01 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Source: SDR ASOA99087

1998

OTHER · 1998-10-05 Unresolved
ATA 5320

Part: SUPPORT — CRACKED (WINDSCREEN)

DURING C-CHECK INSPECTION, WINDSHIELD CENTER POST ATTACH SUPPORT FITTINGS ARE INSPECTED IAW ASA EO-120-53-0021. THE UPPER SUPPORT FITTING WAS FOUND CRACKED ON THE LEFT SUPPORT LEG FROM THE BOLT ATTACHMENT HOLE AFT THROUGH THE LEG. THIS IS A DIFFICULT AREA TO COMPLETE A VISUAL AND/OR DYE PENETRANT INSPECTION. SUBMITTER RECOMMENDED AN EDDY CURRENT INSPECTION BE COMPLETED ON THE WINDSHIELD CENTER POST FITTINGS.

Source: SDR 98ZZZX4182