N14609

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.

18 reports on file, 1999-05-23 – 2007-08-18.

OTHER · 2007-08-18 Matched by certificate designator
ATA 5320

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT CLIP AT STA 360, S11L. A REPAIR WAS INSTALLED IAW ECRA 5311-01352.

Source: SDR CALA0700442
OTHER · 2007-08-13 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 827 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.

Source: SDR CALA0700429
OTHER · 2007-08-13 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 867 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.

Source: SDR CALA0700432
OTHER · 2007-08-12 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 867 BELOW S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.

Source: SDR CALA0700430
OTHER · 2007-08-12 Matched by certificate designator
ATA 5311

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .5 INCH CRACK IN BELT FRAME AT STA 400 BELOW S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.

Source: SDR CALA0700433
OTHER · 2007-08-12 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 827, S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.

Source: SDR CALA0700431
OTHER · 2007-08-12 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT BRACKET ATTACH RIVET, STA 787, S8R. THE FRAME WAS REPAIRED IAW ECRA 5310-04649.

Source: SDR CALA0700425
OTHER · 2007-08-10 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,440 hrs · 19,855 cycles

INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT STA 986.5, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGE 201-204.

Source: SDR CALA0700417
Earlier reports · 1999–2006 · 10 reports

2006

NO TEST · 2006-08-03 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,611 hrs · 18,385 cycles

INSPECTION REPORTED THAT -HALF- OF THE PASSENGER CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE DURING A S-CHECK IN EWR. A NEW BATTERY PACK WAS INSTALLED AND OPERATIONAL CHECKS WERE GOOD.

Source: SDR CALA0600319

2005

OTHER · 2005-04-26 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,214 hrs · 16,643 cycles

FLOORBEAM CORRODED AT STA 986.5 AND LBL 43. INSTALLED DOUBLER PER ECRA 5321-01211.

Source: SDR CALA0500131
OTHER · 2005-03-25 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,042 hrs · 16,555 cycles

INSPECTION FOUND THE MAIN CABIN FLOORBEAM CORRODED AT STA 986.5, LBL 43. REPAIRED IAW ECRA 5321-01211.

Source: SDR CALA0500088
OTHER · 2005-03-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,042 hrs · 16,555 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 360-375, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Source: SDR CALA0500077

2003

OTHER · 2003-09-03 Matched by certificate designator
ATA 3397

Part: WIRE HARNESS — BROKEN (ROW 12ABC) · airframe 27,478 hrs · 14,668 cycles

INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 12ABC DUE TO A BROKEN WIRE. THE EMERGENCY ESCAPE PATH LIGHTING WIRE HARNESS WAS REPLACED. OPERATION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS RESTORED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-81.

Source: SDR CALA0300512
OTHER · 2003-09-03 Matched by certificate designator
ATA 5330

Part: SKIN — GOUGED (FUSELAGE) · airframe 27,478 hrs · 14,668 cycles

INSPECTION FOUND FUSELAGE SKIN REPAIR PLATE GOUGED AT STA 980 UNDER L-2 DOOR. THE REPAIR PLATE WAS REMOVED AND A NEW REPAIR PLATE WAS INSTALLED IAW SRM 53-00-01, PAGE 204-206.

Source: SDR CALA0300511

2002

OTHER · 2002-11-21 Matched by certificate designator
ATA 5314

Part: KEELBEAM — WORN (FUSELAGE) · airframe 25,712 hrs · 13,706 cycles

INSPECTION FOUND DEEP WEAR ON KEEL BEAM AT BS 710-727, RBL 8 (LOWER FILLET PANEL ATTACH FLANGE). A FILLER AND STRAP REPAIR WAS INSTALLED IAW ECRA 5311-01143.

Source: SDR CALA0200556
OTHER · 2002-11-15 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (STA 344-360) · airframe 25,712 hrs · 13,706 cycles

INSPECTION FOUND A 2" CRACK IN MAIN DECK WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Source: SDR CALA0200554

2000

OTHER · 2000-05-19 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 19,057 hrs · 10,143 cycles

INSPECTION FOUND CABIN FLOORBEAM GOUGED IN SEVERAL PLACES AT BS 986, RBL 15 - RBL 30. A REPAIR WAS INSTALLED IAW ECRA 5360-01040.

Source: SDR CALA0000719

1999

WARNING INDICATION · 1999-05-23 Matched by certificate designator
ATA 3230

Part: SENSOR — OUT OF ADJUST (LANDING GEAR)

THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. WHEN RETRACTING FLAPS THE TAKEOFF WARNING HORN SOUNDED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR GAP OUT OF TOLERANCE. THE SENSOR WAS ADJUSTED IAW MM 32-09-01. GEAR RETRACTION OPERATION CHECKED NORMAL.

Source: SDR CALA9900568