N14384

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.

14 reports on file, 1995-03-26 – 2003-02-11.

OTHER · 2003-02-11 Matched by certificate designator
ATA 5230

Part: SKIN — DENTED (BS 827) · airframe 23,447 hrs · 12,380 cycles

INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED AT BS 827. REPAIRED IAW SRM 52-00-01, FIGURE 202.

Source: SDR CALA0300038
OTHER · 2003-02-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (STA 1121) · airframe 23,447 hrs · 12,380 cycles

INSPECTION FOUND INNER FORMED FRAME CHORD DENTED AT STA 1121, RBL 28, WL 292. REPAIRED IAW SRM 51-70-11, FIGURE 1.

Source: SDR CALA0300039
OTHER · 2003-02-11 Matched by certificate designator
ATA 5320

Part: WEB — PUNCTURED (STA 1119-1125) · airframe 23,447 hrs · 12,380 cycles

INSPECTION FOUND THREE PUNCTURES IN HORIZONTAL BEAM WEB AT STA 1119-1125, LBL 18, WL 264. THE PUNCTURES WERE REPAIRED IAW SRM 51-70-13, FIGURE 1 AND 51-40-02, FIGURE 3.

Source: SDR CALA0300040
OTHER · 2003-02-11 Matched by certificate designator
ATA 5320

Part: STIFFENER — BENT (STA 1121) · airframe 23,447 hrs · 12,380 cycles

INSPECTION FOUND FUSELAGE SECTION 48 HORIZONTAL STIFFENER BENT AT STA 1121, LBL 24. REPAIRED IAW SRM 51-70-11.

Source: SDR CALA0300037
OTHER · 2003-02-10 Matched by certificate designator
ATA 5320

Part: STIFFENER — BENT (STA 1104) · airframe 23,447 hrs · 12,380 cycles

INSPECTION FOUND FUSELAGE SECTION 48 HORIZONTAL STIFFENER BENT AT STA 1104, LBL 24. REPAIRED IAW SRM 51-70-11, FIGURE 1.

Source: SDR CALA0300032
OTHER · 2003-02-10 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (STA 1121) · airframe 23,447 hrs · 12,380 cycles

INSPECTION FOUND INNER FORMED FRAME CHORD DENTED AT STA 1121, LBL 28, WL 292. REPAIRED IAW SRM 51-70-11, FIGURE 1.

Source: SDR CALA0300033
Earlier reports · 1995–2001 · 8 reports

2001

WARNING INDICATION · 2001-03-25 Matched by certificate designator
ATA 3230

Part: ACTUATOR — INOPERATIVE (RT MLG) · airframe 18,573 hrs · 9,875 cycles

THE RT MLG RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A MANUAL GEAR EXTENSION WAS PERFORMED SUCCESSFULLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG UPLOCK ACTUATOR AT FAULT. THE UPLOCK ACTUATOR WAS REPLACED IAW MM 32-32-41. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Source: SDR CALA0100252
OTHER · 2001-03-22 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,562 hrs · 9,869 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 500D BETWEEN STRINGER 26L AND 26R IN FORWARD CARGO AREA. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-30-53.

Source: SDR CALA0100245
OTHER · 2001-03-14 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (CABIN) · airframe 18,562 hrs · 9,869 cycles

INSPECTION FOUND INBOARD RIGHT SEAT TRACK CORRODED AT STA 360, RBL 10. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED.

Source: SDR CALA0100230

2000

OTHER · 2000-10-06 Matched by certificate designator
ATA 5320

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 17,356 hrs · 9,240 cycles

INSPECTION FOUND RT Z-CHANNEL CORRODED IN AFT PIT. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Source: SDR CALA0001508

1999

NO TEST · 1999-07-25 Matched by certificate designator
ATA 3350

Part: LIGHT — INOP (L-1 DOOR)

INSPECTION FOUND THE L-1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED.

Source: SDR CALA9900861

1998

FLUID LOSS · 1998-02-01 Matched by certificate designator
ATA 5730

Part: PANEL — LEAKING (RT WING)

A FUEL LEAK FROM RT WING OVERWING FUEL TANK ACCESS PANEL LOCATED IN LINE WITH RIGHT ENGINE PYLON WAS OBSERVED WHILE EN ROUTE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND SEVERAL LOOSE FASTENERS AND ONE STRIPPED NUT PLATE. THE PANEL WAS REMOVED AND THE NUT PLATE WAS REPLACED AND SEALED. A NEW PANEL AND SEAL WERE INSTALLED, LEAK CHECK WAS GOOD.

Source: SDR CALA9800145

1996

FLT CONT AFFECTED · 1996-08-26 Matched by certificate designator
ATA 2750

Part: GIMBALS — LACK OF LUBE (TE FLAPS)

WHEN FLAPS WERE SELECTED TO 30 DEGREES ON FINAL APPROACH TO SLC, THE FLAPS WOULD NOT EXTEND PAST 15 DEGREES. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE LUBRICATED ALL FLAP JACKSCREW GIMBALS PER MM 12-22-21. THE FLAPS OPERATIONALLY CHECKED GOOD SEVERAL TIMES IAW MM 27-51-00.

Source: SDR CALA9601220

1995

FLUID LOSS; WARNING INDICATION · 1995-03-26 Matched by certificate designator
ATA 2913

Part: HYD PUMP — LEAKING (NR 2 ENGINE)

EWR - FLT 1416 - THE B-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE HYDRAULIC LOW PRESSURE LIGHT WHILE ON APPROACH TO EWR. THE NR 2 ENGINE HYDRAULIC PUMP WAS TURNED OFF PER 'ABNORMAL' PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 2 PUMP WAS REMOVED AND REPLACED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X)

Source: SDR CAL950232