N919UW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| US AIRWAYS INC | Operator | on 2007-10-28 | Operator named in NTSB report |
Accident & incident history
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.
30 reports on file, 2006-11-27 – 2009-07-14.
Part: RETAINER — CORRODED (GIRT BAR)
PHL - L1 SLIDE TIME CHANGE FOUND GIRT BAR RETAINER PLATE CORRODED. REPLACED GIRT BAR RETAINER.
Part: GIRT BAR — OBSTRUCTED (ZONE 200)
CLT - F/A REPORTS R4 SLIDE WILL NOT ARM. FOUND GIRT BAR JAMMED. CLEARED OBSTRUCTION FROM GIRT, CYCLED DOORS AND SLIDE ARMS & DISARMS NORMALLY.
Part: LANYARD — UNSECURE (EVAC SLIDE)
CLT - THE FORWARD ENTRY DOOR R1 IS DIFFICULT TO ARM. A CORD IS PROTRUDING UNDER THE EMERGENCY ESCAPE SLIDE COMPARTMENT. THE R1 GIRT BAR FLOOR FITTINGS WERE CLEANED AND LUBED. THE R1 DOOR SLIDE LANYARD WAS STOWED. OPERATIONS FOUND NORMAL.
Part: SLAT — CORRODED (WING) · airframe 75,705 hrs · 33,817 cycles
CLT - RON - MAJOR REPAIR - CORROSION ON NR 3 SLAT LEADING EDGE STARTING 51 INCHES FROM INBOARD END & EXTENDING OUTWARD 12 INCHES. REPLACED NR 3 SLAT IAW JOB CARD 19L52027002.
Part: GIRT BAR — BINDING (R1 DOOR)
CLT - THE R1 DOOR EVACUATION SLIDE ARMING LEVER IS BINDING. MAINTENANCE REPOSITIONED THE GIRT BAR LANYARD RING AND CLEANED AND LUBED THE GIRT BAR FLOOR HOLDER.
Earlier reports · 2006–2008 · 25 reports
2008
Part: SLIDE RAFT — OUT OF POSITION (R1 DOOR)
CLT - THE R1 DOOR ESCAPE SLIDE FELL OUT OF CONTAINER. MAINTENANCE REPLACED THE R1 DOOR ESCAPE SLIDE. OK FOR SERVICE.
Part: WEB — CRACKED (L/E SLAT) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT WEB CRACKED, FSS 692. REPAIRED RIGHT WING NR 9 SLAT WEB, FSS 692 IAW USAIRWAYS EA 110393.
Part: WEB — CRACKED (L/E SLAT) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT WEB CRACKED, FSS 599. REPAIRED RIGHT WING 9 SLAT WEB, FSS 599 IAW USAIRWAYS EA 110393.
Part: WEB — CRACKED (L/E SLAT) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING 6 SLAT WEB CRACKED, FSS 550. REPAIRED RIGHT WING 6 SLAT WEB, FSS 550 IAW USAIRWAYS EA 110396.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER, BS 1681, S2L. REPAIRED STRINGER, BS 1681, S2L IAW B737 SRM 53-00-03 FIGURE 201.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER, BS 1681, S2R. REPAIRED STRINGER, BS 1681, S2R IAW B737 SRM 53-00-03 FIGURE 201.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER, BS 1640, S2R. REPAIRED STRINGER, BS 1640, S2R IAW B737 SRM 53-00-03 FIGURE 201.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON STRINGER, BS 440, S29R. REPAIRED STRINGER, BS 440, S29R IAW B737 SRM 53-00-03 FIGURE 201.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, CORROSION ON STRINGER, BS 440, S29R. REPAIRED STRINGER, BS 440, S29R IAW B757 SRM 53-00-03.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, CRACKED STRINGER, BS 1720, S29R. REPAIRED STRINGER, BS 1720, S29R IAW B757 SRM 53-00-03 REPAIR 1.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON SEAT TRACK, BS 1320, RBL 26, WL 208. REPAIRED SEAT TRACK, BS 1320, RBL 26, WL 208 IAW B757 SRM 53-00-052-2R.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON SEAT TRACK, BS 1320 - BS 1340, BL 26, WL 208. REPAIRED SEAT TRACK, BS 1320 - BS 1340, BL 26, WL 208 IAW B757 SRM 53-00-052-2R.
2007
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 1661, BL 0. REPAIRED FLOORBEAM, BS 1661, BL 0 IAW B757 SRM 53-00-51 REPAIR 5.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, R2 DOOR CUTOUT INTERCOSTAL CRACKED, BS 680. REPLACED R2 DOOR CUTOUT INTERCOSTAL CRACKED, BS 680 IAW USAIRWAYS EO 5304R143.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 1260 - BS 1300, LBL 21, WL 208. REPLACED FLOOR SUPPORT, BS 1260 - BS 1300, LBL 21, WL 208 IAW B757 SRM 53-00-04.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 377, LBL 12. REPAIRED FLOORBEAM, BS 377, LBL 12 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, CRACKED FLOORBEAM, BS 1320 - BS 1340, BL 0. REPAIRED FLOORBEAM, BS 1320 - BS 1340, BL 0 IAW B757 SRM 53-00-51.
Part: SKIN — DELAMINATED (T/E FLAP) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEFT WING INBOARD FLAP UPPER SURFACE DELAMINATED. REPAIRED LEFT WING INBOARD FLAP UPPER SURFACE I/A/W USAIRWAYS EA 110418.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION FLOORBEAM, BS 1641, LBL 16. REPAIRED FLOORBEAM, BS 1641, LBL 16 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.
Part: INTERCOSTAL — CRACKED (R2 DOOR) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, THE R2 DOOR HAS A CRACKED INTERCOSTAL, BS 660. REPLACED R2 DOOR INTERCOSTAL, BS 660 IAW USAIRWAYS EO 5304R143.
Part: INTERCOSTAL — CRACKED (R2 DOOR) · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK - THE R2 DOOR HAS A CRACKED INTERCOSTAL, BS 660, AT THE NR 4 DOOR STOP AREA. REPLACED THE R2 DOOR INTERCOSTAL, BS 660, AT THE NR 4 DOOR STOP AREA IAW USAIRWAYS EO 5304R143.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 1661, BL 0 - LBL 58.22. REPAIRED FLOORBEAM, BS 1661, BL 0 - LBL 58.22 IAW B757 SRM 53-00-51 REPAIR 5.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,496 hrs · 32,512 cycles
PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON INTERCOSTAL UPPER CHORD, BS 1661 - BS 1681, RBL 9.2. REPLACED INTERCOSTAL UPPER CHORD, BS 1661 - BS 1681, RBL 9.2 IAW B757 SRM 53-60-61.
Part: DETECTOR — UNKNOWN · airframe 70,782 hrs · 31,750 cycles
FLIGHT 1268, PHL-SJU: ON CLIMBOUT, CREW RECEIVED MASTER WARNING, FIRE WARNING, AND FIRE BELL INTERMITTENTLY. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE NR 1 AND NR 2 TURBINE OVERHEAT DETECTORS ON THE RIGHT ENGINE AND FIRE/OVERHEAT CARD M10426.
2006
Part: WEDGE — DELAMINATED (TE FLAP) · airframe 69,531 hrs · 31,235 cycles
A 3 X 12 INCH AREA OF CORE DAMAGE/DELAMINATION AT RIGHT I/B MID FLAP T/E WEDGE. REMOVED DAMAGED WEDGE AND INSTALLED NEW WEDGE PER BOEING DWG 113N2003.