N14079
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.
31 reports on file, 1998-08-16 – 2000-11-03.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND A 4 INCH CRACK IN RT HORIZONTAL STABILIZER UPPER AFT O/B SKIN. THE RT UPPER AFT O/B SKIN PANEL WAS REPAIRED IAW ECRA 5511-01035.
Part: FITTING — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND LAV E O/B SUPPORT BEAM CORRODED AT AFT ATTACHMENT FITTING, STA Y = 1831-1887, X = 31L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND LAV E I/B SUPPORT BEAM CORRODED AT STA. Y = 1831-1887, X = 5L. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (LAVATORY) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND LAV F I/B SUPPORT BEAM CORRODED. A NEW BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (GALLEY) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND GALLEY G-6 O/B SUPPORT BEAM CORRODED AT FORWARD END. A NEW SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND LAV F O/B SUPPORT BEAM CORRODED AT Y = 1831-1887, X = 31R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND LONGITUDINAL SUPPORT BEAM AFT OF GALLEY G-1 CORRODED AT STA Y = 412-487, X = 24L. A NEW SECTION OF SUPPORT BEAM WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND GALLEY G-1 SUPPORT BEAM CORRODED AT STA Y = 392-422, X = 20L. A REPAIR WAS PERFORMED IAW GMM 10-900-01 AND SRM 53-11-1.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND GALLEY G-2 SUPPORT BEAM CORRODED AROUND FORWARD ATTACHMENT BOLT HOLE AT STA Y = 392-412, X = 8R. A REPAIR WAS INSTALLED IAW GMM 10-900-01 AND 53-11-01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND GALLEY G-2 FLOOR SUPPORT CHANNEL SECTION CORRODED AT STA Y = 392-459, X = 40R. A NEW FLOOR SUPPORT CHANNEL SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM J SECTION AT BASE OF FLIGHT DECK STEP CORRODED AT STA Y = 392, X = 20L-20R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP AFT OF LAVS E AND F AT STA Y = 1887, X = 5R-24R CORRODED. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING SECTIONS AFT OF LAVS E & F AT STA Y = 1887, X = 5L-24L AND X = 27R-53R CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT LAVS E & F, STA Y = 1887, X = 38R-58R. A REPAIR WAS ACCOMPLISHED BY INSTALLING A NEW J SECTION IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND GALLEY G3 LATERAL FLOORBEAM J SECTION CORRODED AT STA Y = 459, X = 18L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIP FORWARD OF GALLEY 6 AND 7 CORRODED AT STA Y = 1914, X = 17L-17R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM J SECTION CORRODED AT STA Y = 421, X = 24L-24R. A NEW SECTION WAS INSTALLED IAW GMM 10-900-01 AND SRM 53-11-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM CAPPING STRIPS AFT OF LAVS E & F AT STA Y = 1887, X = 28L-32L AND X = 38L-58L CORRODED. NEW SECTIONS WERE INSTALLED IAW GMM 10-900-01 AND SRM 53-16-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND FLOOR SUPPORT BEAM FWD OF LAV H CORRODED AT STA Y = 1914, X = 44L-66L. A NEW SUPPORT SECTION WAS INSTALLED IAW SRM 53-16-01 AND GMM 10-900-01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 97,096 hrs · 21,484 cycles
INSPECTION FOUND LATERAL FLOORBEAM CORRODED AT STA Y = 459, X = 38R-41R. A SPLICE REPAIR WAS PERFORMED IAW SRM 53-30-00.
Part: FUSE — FAILED (MLG)
THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM HNL. THE A/C WAS RETURNED TO HNL WHERE IT LANDED W/O INCIDENT. MX FOUND THE MLG INTERLOCK CYLINDER RETRACTED. RESET TRIM CYLINDER FUSE. INTERLOCK CYLINDER NOW IN PROPER POSITION IAW MM 32-31-06, PAGE 201.
Earlier reports · 1998–1999 · 10 reports
1999
Part: SAFETY WIRE — OUT OF POSITION (GEAR HANDLE)
CREW RECEIVED RED GEAR WARNING LIGHTS WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND GEAR WAS EXTENDED MANUALLY. ALL GEAR LIGHTS WERE GREEN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR CONTROL HANDLE WAS NOT MAKING CONTACT WITH SWITCH. MAINTENANCE FOUND SAFETY WIRE ON LANDING GEAR CONTROL CABLE AT HANDLE ASSEMBLY BINDING TO FRAME. THE SAFETY WIRE WAS REMOVED AND REPOSITIONED. THE HANDLE ASSEMBLY WAS CLEANED AND LUBRICATED. A GEAR SWING WAS PERFORMED IAW MM 32-00. GEAR OPERATION AND INDICATIONS CHECKED NORMAL.
Part: ANGLE — CRACKED (NR 1 ENGINE)
INSPECTION FOUND NR 1 ENGINE INTAKE EXTERNAL SIDE AFT SUPPORT ANGLES(2) CRACKED. THE CRACKS WERE 1 LONG. THE SUPPORT ANGLES WERE REPLACED IAW SRM 51-30-00.
Part: ANGLE — CRACKED (WS 414.125)
INSPECTION FOUND A 3 CRACK IN RT WING FIXED L/E SUPPORT ANGLE AT STA XOS 414.125. A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01.
Part: SKIN — CRACKED (WS 455&506)
INSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CRACKED AT STA XORS 455 AND STA XORS 506. BOTH CRACKS WERE 1 LONG. REPAIRS WERE INSTALLED IAW DRAWING ARB2933-46, DRAWING ARB2933-10, SRM 57-10-00, FIGURE 49 AND 51-31-01.
Part: STRIP — CRACKED (NR 2 LE SLAT)
INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT O/B STRIP. PERFORMED REPAIR IAW SRM 57-10-00.
Part: SKIN — CRACKED (WS 783)
INSPECTION FOUND A 0.9 INCH CRACK IN RT WING LEADING EDGE SKIN AT XORS 783. A REPAIR WAS INSTALLED IAW SRM 57-10-00, FIGURE 68.
Part: ROD — DISCONNECTED (L3 DOOR)
UNABLE TO ARM L3 DOOR AT DEPARTURE. FOUND ROD AT LOCKING MECHANISM OUT OF PLACE. REINSTALLED ROD AND TIGHTENED HARDWARE.
1998
Part: FAN FRAME — CRACKED (NR 1 ENGINE)
THE NR 1 ENGINE REVERSER SEAL SUPPORT RING, LEFT, WAS FOUND CRACKED AT ALL FIVE FORWARD ATTACH POINTS. THE FLANGE SECTIONS HAD BROKEN COMPLETELY AWAY FROM THE TWO BOLT ATTACHMENTS IN AN ARC THE CRACK PASSING THROUGH THE TOP ROW OF TWO ATTACHMENT RIVETS OF A SUPPORT DOUBLER BRACKET. NO CAUSE HAS BEEN DETERMINED AT THIS TIME. FURTHER INVESTIGATION IS BEING MADE. NO PERIPHERAL DAMAGE IS EVIDENT ON THE RING OR ON THE ADJACENT STRUCTURE. FOUND ON A ROUTINE C-CHECK. ENGINE TT: 64,235 HOURS.
Part: HYD LINE — PUNCTURED (NR 2 HYD SYST)
THE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN HYDRAULIC PRESSURE LINE TO LEFT HYDRAULIC PUMP AND THE RIGHT PUMP WAS LEAKING HYDRAULIC FLUID OUT DRAIN MAST. THE HYDRAULIC LINE AND PUMP WERE REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD.
Part: SMOKE DETECTOR — INOPERATIVE (CARGO COMPT)
THE AFT CARGO FIRE WARNING LIGHT AND SMOKE DETECTOR LIGHT ILLUMINATED WHILE ENROUTE. EMERGENCY PROCEDURES WERE COMPLIED WITH AND THE LIGHTS EXTINGUISHED. BOTH CARGO FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE MASTER WARNING CONTROLLER WAS REMOVED AND REPLACED. THE CARGO FIRE BOTTLES WERE REMOVED AND REPLACED. IN ADDITION, THE AFT CARGO NR 1 SMOKE DETECTOR WAS REMOVED AND REPLACED.