N678AW

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.

151 reports on file, 2007-02-11 – 2017-06-06.

OTHER · 2017-06-06 Matched by certificate designator
ATA 5220

Part: SEAL — TORN (EMERGENCY EXIT) · airframe 42,037 hrs · 15,422 cycles

TORN SEAL AT THE EMERGENCY EXIT DOOR IN PASSENGER CABIN. REPLACED SEAL EMERGENCY EXIT DOOR.

Source: SDR AALA201706099013
OTHER · 2017-06-04 Matched by certificate designator
ATA 1100

Part: PLACARD — DETERIORATED (EMERGENCY EXIT)

DETERIORATED EMERGENCY EXIT DOOR PLACARDS LT AND RT SIDES (PULL TO INFLATE). REPLACED EMERGENCY EXIT DOOR PLACARDS.

Source: SDR AALA201706059008
OTHER · 2017-05-29 Matched by certificate designator
ATA 3350

Part: LENS — BROKEN (EMERGENCY LIGHT)

BROKEN CEILING PANEL EMERGENCY LIGHT LENS IN PASSENGER CABIN. REPLACED THE LENS.

Source: SDR AALA201705309020
OTHER · 2017-05-27 Matched by certificate designator
ATA 5210

Part: SEAL — TORN (PAX DOOR) · airframe 42,037 hrs · 15,422 cycles

TORN PRESSURE SEAL PASSENGER CREW DOOR 832 LT SIDE AT AFT GALLEY AREA.

Source: SDR AALA201705309019
OTHER · 2017-05-24 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY FLOOR SUPPORT -Y81. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11

Source: SDR AALA201706159046
OTHER · 2017-05-24 Matched by certificate designator
ATA 5730

Part: ACCESS PANEL — ELONGATED (RT WING) · airframe 42,037 hrs · 15,422 cycles

ELONGATED HOLE ON RIGHT WING ACCESS PANEL 640JB DOOR ASSEMBLY (TYPE 25) BETWEEN STRINGER 8R AND 11R, BETWEEN RIB 14 AND 15. REPLACED ACCESS PANEL IAW AMM 57-27-11-400-002-A AND SRM 57-27-11.

Source: SDR AALA201706169042
OTHER · 2017-05-18 Matched by certificate designator
ATA 5720

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 42,037 hrs · 15,422 cycles

ELONGATED HOLE ON LEFT WING ACCESS PANEL 540KB DOOR ASSEMBLY (TYPE 25) BETWEEN STRINGER 8L AND 11L, BETWEEN RIB 15 AND 16. REPLACED ACCESS PANEL IAW AMM 57-27-11-400-002-A.

Source: SDR AALA201706169041
OTHER · 2017-05-17 Matched by certificate designator
ATA 2565

Part: SLIDE — CRACKED (PAX DOOR)

CRACKED PASSENGER CREW DOOR SLIDE AT AFT GALEEY AREA. REPLACED THE SLIDE.

Source: SDR AALA201705189003
OTHER · 2017-05-15 Matched by certificate designator
ATA 5340

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 42,037 hrs · 15,422 cycles

CORROSION ON L1 DOOR FITTING LOWER FRAME AT GIRT BAR ATTACH POINTS, FORWARD AND AFT, AT STRINGER 23L BETWEEN FRAMES 16 AND 20. REPLACED FITTING IAW SRM 51-42-11 AND DRAWING D53110339.

Source: SDR AALA201706169031
OTHER · 2017-05-15 Matched by certificate designator
ATA 2560

Part: FITTING — CORRODED (GIRT BAR) · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY R1 DOOR LOWER FRAME LOCK FASTENER FITTINGS AT GIRT BAR ATTACH POINTS STRINGER 23R AND FR 20. REPLACED FITTINGS PER SRM 51-42-11 AND DRAWING D53112806.

Source: SDR AALA201706099032
OTHER · 2017-05-10 Matched by certificate designator
ATA 5530

Part: BEARING — WORN (HINGE ARM) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 7 BEARING. REPLACED FORKED END HINGE FITTING ASSEMBLY IAW SRM 51-72-11.

Source: SDR AALA201706159048
OTHER · 2017-05-10 Matched by certificate designator
ATA 2720

Part: BEARING — WORN (RUDDER HINGE) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON RUDDER HINGE ARM NR 4 BEARING. REPLACED HINGE ARM IAW AMM 55-36-41, AND SRM 51-44-11.

Source: SDR AALA201706029034
OTHER · 2017-05-10 Matched by certificate designator
ATA 5530

Part: HINGE ARM — WORN (VERTICAL STAB) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM #5 BEARING AT RIB 7. REPLACED RUDDER HINGE ARM # 5 PER AMM 55-36-41.

Source: SDR AALA201706099036
OTHER · 2017-05-10 Matched by certificate designator
ATA 5530

Part: HINGE ARM — WORN (VERTICAL STAB) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON VERTICAL STABILIZER BEARING HINGE ARM NR 3. REPLACED RUDDER HINGE ARM IAW SRM 51-72-11-911-001.

Source: SDR AALA201706169034
OTHER · 2017-05-10 Matched by certificate designator
ATA 5320

Part: PRESSURE PANEL — CRACKED (FRAME 43) · airframe 42,037 hrs · 15,422 cycles

CRACK INDICATION ON PASSENGER CABIN PRESSURE PLATE IN OPEN AFT HOLE AT Y1650 AND FRAME 43. REPLACED PRESSURE PLATE IAW SRM 51-72-11 AND EO 5315Y066.

Source: SDR AALA201707109001
OTHER · 2017-05-09 Matched by certificate designator
ATA 2720

Part: BEARING — WORN (HINGE ARM) · airframe 42,037 hrs · 15,422 cycles

AEXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM NR 2 BEARING. REPLACED HINGE ARM IAW SRM 51-40-00.

Source: SDR AALA201706029026
OTHER · 2017-05-08 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON THE RIGHT ELEVATOR REAR SPAR HINGE ARM FITTING NR 6. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705239026
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON ELEVATOR HINGE ARM NR 4. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705199037
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON CARGO BAY FLOOR PANEL 131GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159052
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON LEFT ELEVATOR REAR SPAR HINGE ARM FITTING NR 6. REPLACED HINGE ARM FITTING AMM 55-16-42.

Source: SDR AALA201705239025
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 42,037 hrs · 15,422 cycles

REPAIR DELAMINATED ON FORWARD CARGO COMPARTMENT FLOOR PANEL 132GF. REPLACED FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706029030
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151MF. REPLACED THE FLOOR PANEL IAW 53-02-00-300-011, AND IRM 9701 REVISION G.

Source: SDR AALA201705249028
OTHER · 2017-05-07 Matched by certificate designator
ATA 5312

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 42,037 hrs · 15,422 cycles

CRACK INDICATION ON LEFT SIDE FORWARD CARGO BAY, IN OPEN FASTENER HOLE AT INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 1 INCH INBOARD SIDE TO Y1292. REPAIRED THE PRESSURE PANEL IAW EO 5316Y209.

Source: SDR AALA201706169036
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON THE LEFT ELEVATOR HINGE ARM NR 2. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705199039
OTHER · 2017-05-07 Matched by certificate designator
ATA 5320

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 42,037 hrs · 15,422 cycles

CRACK INDICATION ON LEFT PASSENGER CABIN SIDE BOX BEAM UPPER FLANGE IN OPEN AFT HOLE AT FRAME 43 AND Y1292. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Source: SDR AALA201707109002
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY UPPER SURFACE OF FLOOR PANEL 131KF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706029036
OTHER · 2017-05-07 Matched by certificate designator
ATA 5312

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 42,037 hrs · 15,422 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON LEFT SIDE IN FORWARD CARGO BAY, IN OPEN FASTENER HOLE AT INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 2 INCHES OUTBOARD TO Y1292. REPAIRED PRESSURE PANEL BETWEEN FR 35 AND FR 36 PER EO #5316Y209.

Source: SDR AALA201706169035
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON THE LEFT ELEVATOR REAR SPAR HINGE ARM FITTING NR 5. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705239027
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON RIGHT ELEVATOR REAR SPAR HINGE ARM FITTING NR 1. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705239029
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY UPPER SURFACE OF FLOOR PANEL 131JF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159053
OTHER · 2017-05-07 Matched by certificate designator
ATA 5312

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 42,037 hrs · 15,422 cycles

CRACK INDICATION ON LEFT SIDE FORWARD CARGO BAY IN OPEN FASTENER HOLE, INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 3 INCHES INBOARD SIDE TO Y1292. REPAIRED THE PRESSURE PANEL IAW EO 5316Y209.

Source: SDR AALA201706169037
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY FLOOR PANEL 131CF, LOWER SURFACE. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.

Source: SDR AALA201705249029
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 152QF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706029035
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON THE LEFT ELEVATOR HINGE ARM NR 1. REPLACED HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705199036
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY FLOOR PANEL 132JF AT LOWER SURFACE. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201706169025
OTHER · 2017-05-07 Matched by certificate designator
ATA 5312

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 42,037 hrs · 15,422 cycles

CRACK INDICATION ON LEFT SIDE FORWARD CARGO BAY IN OPEN FASTENER HOLE, INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 3 INCHES OUTBOARD TO Y1292. REPAIRED THE PRESSURE PANEL IAW EO 5316Y209.

Source: SDR AALA201706169038
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON THE RIGHT ELEVATOR REAR SPAR HINGE ARM FITTING NR 5. REPLACED THE HINGE ARM FITTING AMM 55-16-42.

Source: SDR AALA201705239030
OTHER · 2017-05-07 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152FF. REPLACED FLOOR PANEL PER A320 SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201706099035
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (ZONE 300 - STABS) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON RIGHT ELEVATOR HINGE FITTING NR 2. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705199038
OTHER · 2017-05-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

EXCESSIVE PLAY ON THE RIGHT ELEVATOR REAR SPAR HINGE ARM FITTING NR 3. REPLACED THE HINGE ARM FITTING IAW AMM 55-16-42.

Source: SDR AALA201705239028
OTHER · 2017-05-06 Matched by certificate designator
ATA 5521

Part: RIB — CORRODED (LT ELEVATOR) · airframe 42,037 hrs · 15,422 cycles

CORROSION ON THE LEFT ELEVATOR RIB. REPLACED THE RIB ASSEMBLY IAW SRM 51-72-11 AND DRAWING D55281242.

Source: SDR AALA201706169029
OTHER · 2017-05-05 Matched by certificate designator
ATA 5340

Part: COUPLING — ELONGATED (FRAME 68) · airframe 42,037 hrs · 15,422 cycles

ELONGATED HOLE.ON CONNECTING SECTION AT Y1162 AND FRAME 68. REPLACED CONNECTING SECTION IAW SRM 51-72-11 AND DRAWING D53472780.

Source: SDR AALA201705249038
OTHER · 2017-05-05 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY SEAT TRACK AT Y1292 BETWEEN FRAMES 64 AND 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING D53472815.

Source: SDR AALA201705249041
OTHER · 2017-05-05 Matched by certificate designator
ATA 5340

Part: COUPLING — ELONGATED (FRAME 68) · airframe 42,037 hrs · 15,422 cycles

ELONGATED HOLE ON COUPLING AT Y1162 AND FR 68. REPLACED THE COUPLING IAW DRAWING D53472780

Source: SDR AALA201705249039
OTHER · 2017-05-05 Matched by certificate designator
ATA 5751

Part: HINGE PIN — WORN (LT AILERON) · airframe 42,037 hrs · 15,422 cycles

WEAR ON LEFT WING AILERON HINGE PIN NR 1. REPLACED HINGE PIN IAW AMM 27-14-41-400-001-A.

Source: SDR AALA201706029031
OTHER · 2017-05-04 Matched by certificate designator
ATA 3210

Part: PIN — WORN (MLG) · airframe 42,037 hrs · 15,422 cycles

WEAR ON LEFT MAIN LANDING GEAR LOWER TORQUE LINK PIN AT RIB 5. REPLACED LOWER TORQUE LINK PIN IAW AMM 32-11-27.

Source: SDR AALA201706169032
OTHER · 2017-05-04 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66 AND 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG E53474250.

Source: SDR AALA201705189027
OTHER · 2017-05-03 Matched by certificate designator
ATA 5340

Part: FITTING — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY CORNER FITTING AT FRAME 68, STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53480505.

Source: SDR AALA201705249026
OTHER · 2017-05-03 Matched by certificate designator
ATA 5340

Part: FITTING — CRACKED (FRAME 68) · airframe 42,037 hrs · 15,422 cycles

CRACK ON AFT GALLEY CONNECTING SECTION FITTING AT FRAME 68, STRINGER 23L. REPLACED CONNECTING SECTION IAW SRM 51-72-11 AND DRAWING E53474250.

Source: SDR AALA201705249040
OTHER · 2017-04-28 Matched by certificate designator
ATA 5312

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 42,037 hrs · 15,422 cycles

CRACK INDICATION ON RIGHT SIDE FORWARD CARGO COMPARTMENT, INTERNAL STRUCTURE FROM INBOARD HOLE OF LONGITUDINAL BEAM, AT FRAME 36 AND -Y1292. REPAIRED PRESSURE PANEL IAW EO 5316Y209.

Source: SDR AALA201706169039
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 42,037 hrs · 15,422 cycles

MISSING MATERIAL ON PASSENGER CABIN FLOOR PANEL 232DF. REPLACED THE FLOOR PANEL IAW AMM 53-12-12-400-001-A.

Source: SDR AALA201706159043
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 16-21) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221DF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00 AND IRM 9701 REVISION G.

Source: SDR AALA201705199040
OTHER · 2017-04-25 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (FRAME 71) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON INTERNAL ANGLE AT FRAME 71 BETWEEN STRINGER 26R AND 31R. REPLACED THE ANGLE IAW SRM 51-72-11 AND DRAWING D53571510.

Source: SDR AALA201706169040
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD GALLEY TOP LAYER OF FLOOR PANEL 222CF. REPLACED FLOOR PANEL PER AMM 53-12-12-400-001-A.

Source: SDR AALA201706099033
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 20-24) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD GALLEY FLOOR PANEL 231CF, TOP LAYER. REPLACED THE FLOOR PANEL IAW SRM 53-12-00, AND IRM 9701 REVISION G.

Source: SDR AALA201705239032
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: INSERT — DELAMINATED (GALLEY FLOOR) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON THE AFT GALLEY FLOOR PANEL INSERT 261PF. REPLACED FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159051
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 16-20) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221PF, TOP LAYER. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201705239031
OTHER · 2017-04-25 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY CENTER FLOOR SUPPORT FITTING AT STRINGER 23L BETWEEN FRAMES 66 AND 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.

Source: SDR AALA201705189025
OTHER · 2017-04-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT GALLEY FLOOR PANEL 261BG, TOP LAYER. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.

Source: SDR AALA201705249023
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SEAT TRACK AT -Y1292 BETWEEN FRAMES 64 AND 66. REPLACED THE SEAT TRACK SRM 51-72-11, AND DRAWING D53472816.

Source: SDR AALA201705199017
OTHER · 2017-04-21 Matched by certificate designator
ATA 5340

Part: ATTACH FITTING — CORRODED (FRAME 20) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY ATTACH FITTING AT STRINGER 23R, FRAME 20. REPLACED ATTACH FITTING IAW SRM 51-72-11, AND DRAWING D53112789.

Source: SDR AALA201706029032
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY LOWER SUPPORT AT STRINGER 23L, FRAME 66. REPLACED THE SUPPORT IAW SRM 51-72-11, EA 270003, AND DRAWING D53480505.

Source: SDR AALA201706029029
OTHER · 2017-04-21 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOORBEAM AT -Y464.8 AND FRAME 68. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DRAWING D53472816.

Source: SDR AALA201705129016
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY SEAT TRACK -Y1292 AND FR 19 PLUS 5 INCHES. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53112812.

Source: SDR AALA201706169033
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY SEAT TRACK AT -Y765, BETWEEN FRAMES 64 AND 66. REPLACED THE SEAT TRACK IAW SRM SRM 51-72-11, AND DRAWING D53472832.

Source: SDR AALA201705249033
OTHER · 2017-04-21 Matched by certificate designator
ATA 5310

Part: COUPLING — CORRODED (FRAME 66) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY COUPLING AT -Y1292 AND FRAME 66. REPLACED THE COUPLING IAW SRM 51-72-11, AND DRAWING D53472816.

Source: SDR AALA201705199018
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: COVER — CORRODED (FRAME 14) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY DUMMY RAIL COVER AT -Y81 AND FRAME 14. REPLACED THE COVER IAW SRM 51-72-11.

Source: SDR AALA201706029033
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY SEAT TRACK Y765 BETWEEN FRAMES 64 AND 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING D53472815.

Source: SDR AALA201705189015
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY SHEAR PLATE AT STRINGER 23R BETWEEN FRAMES 69 AND 70. REPLACED THE SHEAR PLATE IAW SRM 51-72-11.

Source: SDR AALA201707069003
OTHER · 2017-04-21 Matched by certificate designator
ATA 5310

Part: COUPLING — CORRODED (FRAME 68 - 69) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY COUPLING AT -Y1162 BETWEEN FRAMES 68 AND 69. REPLACED THE COUPLING IAW SRM 51-72-11, AND DRAWING D53472780.

Source: SDR AALA201705249043
OTHER · 2017-04-21 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOORBEAM AT Y765, FRAME 68. REPLACED THE FLOORBEAM IAW SRM 51-72-11.

Source: SDR AALA201705189024
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY FLOOR SUPPORT AT Y503.2 BETWEEN FRAMES 12 AND 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53112825.

Source: SDR AALA201706029024
OTHER · 2017-04-21 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOORBEAM AT Y512 AND FR 68. REPLACED THE FLOORBEAM SRM 51-72-11 AND DRAWING D53472780.

Source: SDR AALA201705129015
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY FLOOR SUPPORT AT -Y1379.5 BETWEEN FRAMES 12 AND 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53112831.

Source: SDR AALA201706159049
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY SEAT TRACK AT Y765 BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Source: SDR AALA201706029023
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT AT -Y1162 BETWEEN FRAMES 68 AND 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Source: SDR AALA201705249042
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY LOWER SUPPORT AT STRINGER 23R, FRAME 68. REPLACED THE SUPPORT IAW SRM 51-72-11, EA 269973, AND DRAWING D53480505.

Source: SDR AALA201706029028
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY SEAT TRACK -Y765, BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING D53112812.

Source: SDR AALA201706159054
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAME 68-69) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT AT Y1162, BETWEEN FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Source: SDR AALA201705249032
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FRAMES 20-23) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY WEB AT STRINGER 23L, -Y1732, BETWEEN FRAMES 20 AND 23. REPLACED THE WEB IAW SRM 51-72-11.

Source: SDR AALA201706099031
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT AT Y1225, BETWEEN FRAMES 66 AND 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Source: SDR AALA201705249034
OTHER · 2017-04-21 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON AFT GALLEY FLOOR SUPPORT AT -Y765, BETWEEN FRAMES 66 TO 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.

Source: SDR AALA201705249027
OTHER · 2017-04-21 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 42,037 hrs · 15,422 cycles

CORROSION ON FORWARD GALLEY SEAT TRACK AT Y1292, FRAME 19. REPLACED SEAT TRACK IAW SRM 51-72-11.

Source: SDR AALA201706029027
OTHER · 2017-04-19 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,036 hrs · 15,421 cycles

DELAMINATION ON PASSENGER CABIN FLOOR PANEL 242LF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.

Source: SDR AALA201705049004
OTHER · 2017-04-19 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,036 hrs · 15,421 cycles

DELAMINATION ON TOP LAYER PASSENGER CABIN FLOOR PANEL 241JF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.

Source: SDR AALA201705049006
OTHER · 2017-04-19 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,036 hrs · 15,421 cycles

DELAMINATION ON PASSENGER CABIN FLOOR PANEL 231KF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.

Source: SDR AALA201705049003
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151DF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159050
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159044
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY FLOOR PANEL 131AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201706169030
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON THE AFT CARGO BAY FLOOR PANEL 151RF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201705189026
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 42,037 hrs · 15,422 cycles

CRACK ON AFT CARGO BAY FLOOR PANEL 151FF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706029025
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131BF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159045
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152NF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201706159047
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

CRACKED AFT CARGO BAY FLOOR PANEL 152EF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201705249031
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201705249030
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY FLOOR PANEL 131GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-11, AND IRM 9701 REVISION G.

Source: SDR AALA201705249025
OTHER · 2017-04-18 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 42,037 hrs · 15,422 cycles

DELAMINATION ON FORWARD CARGO BAY FLOOR PANEL 132FF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201705239033
OTHER · 2017-04-02 Matched by certificate designator
ATA 3350

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 41,984 hrs · 15,400 cycles

EMERGENCY LIGHT COVER BROKEN. REPLACED THE COVER.

Source: SDR AALA201704039003
SMOKE/FUMES/ODORS/SPARKS · 2017-03-30 Matched by certificate designator
ATA 4920

Part: APU — CONTAMINATED · airframe 41,984 hrs · 15,400 cycles

AFTER DEPARTURE, THE CABIN HAD AN ODOR OF DIRTY SOCKS. FOUND APU CONTAMINATED, PERFORMED AN APU WASH, NO ODOR AT THIS TIME. AIRCRAFT WAS GROUNDED.

Source: SDR AALA201703319001
Earlier reports · 2007–2016 · 52 reports

2016

FLUID LOSS; WARNING INDICATION · 2016-12-29 Matched by certificate designator
ATA 2910

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 41,232 hrs · 15,036 cycles

FLIGHT CREW REPORTED THEY LOST THE YELLOW HYDRAULIC SYSTEM ENROUTE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED AND LANDED SAFELY WITHOUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC LINE IAW AMM 29-11-51.

Source: SDR AALA201701039008
OTHER · 2016-08-26 Matched by certificate designator
ATA 3350

Part: LENS — UNSECURE (CABIN) · airframe 40,206 hrs · 14,565 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR LOWER LT EMERGENCY EXIT LIGHT LENS COVER WILL NOT STAY IN PLACE. INSTALLED NEW EMERGENCY EXIT LIGHT LENS COVER AT THE R2 DOOR IAW AMM 33-51-13.

Source: SDR AALA201608279002
OTHER · 2016-03-13 Matched by certificate designator
ATA 2560

Part: RECEPTACLE — LACK OF LUBE (ZONE 800) · airframe 38,733 hrs · 13,927 cycles

AIRCRAFT WAS NOT GNDED. DOOR 2L ARMING LEVER REPORTEDLY STIFF & DIFFICULT TO OPERATE. CLEANED & LUBED GIRT BAR RECEPTACLES & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Source: SDR AALA201603149002
OTHER · 2016-02-29 Matched by certificate designator
ATA 3350

Part: LIGHT — BROKEN (CABIN) · airframe 38,607 hrs · 13,882 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT ASSEMBLY AT SEAT 11C IS BROKEN. R & R LIGHT ASSEMBLY. OPERATIONAL CHECKED NORMAL.

Source: SDR AALA201603019002

2015

NO TEST · 2015-12-22 Matched by certificate designator
ATA 3350

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,035 hrs · 13,634 cycles

AIRCRAFT WAS NOT GNDED. AFT EMER LIGHT BATTERY FAILED TEST. REPLACED AFT EMER LIGHT BATTERY IAW AMM 33-51-38. OPERATIONAL CHECKED GOOD.

Source: SDR AALA201512249005
FALSE WARNING · 2015-10-15 Matched by certificate designator
ATA 2611

Part: AIR FILTER — DEFECTIVE (SMOKE DETECTOR) · airframe 37,418 hrs · 13,390 cycles

MOMENTARY LAVATORY SMOKE WARNING, NO SMOKE NOTED BY FLIGHT ATTENDANTS, WARNING CLEARED ON ITS OWN AFTER A FEW SECONDS. PERFORMED SDCU BITE 26-17-00-710-001A, TEST PASSED. REPLACED ALL SMOKE DETECTOR AIR FILTERS ASSEMBLIES. GOOD FOR SERVICE.

Source: SDR AALA201510169007
WARNING INDICATION; SMOKE/FUMES/ODORS/SPARKS · 2015-09-28 Matched by certificate designator
ATA 2121

Part: FAN — FAILED (ZONE 100) · airframe 37,304 hrs · 13,336 cycles

FLIGHT 430 VENT EXTRACT FAULT ILLUMINATED, FAN HUMMED, GRINDED & SMELLED BEFORE IT FINALLY QUIT. R & R EXTRACT FAN ASSEMBLY IAW AMM 21-26-51-400-001. OPERATIONAL CHECKED NORMAL IAW 21-26-00-710-001.

Source: SDR AALA201509309002
NO TEST · 2015-08-06 Matched by certificate designator
ATA 3350

Part: CHARGER — INOPERATIVE (CABIN) · airframe 36,829 hrs · 13,153 cycles

EMERGENCY LIGHT AFT GALLEY CHARGER WILL NOT TEST, NO LIGHTS ETC. REPLACED CHARGER ASSEMBLY IAW AMM 33-51-38-0401. OPERATIONS CHECKED GOOD.

Source: SDR AALA201508079007
NO TEST · 2015-08-06 Matched by certificate designator
ATA 3350

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,829 hrs · 13,153 cycles

BAD FROM STOCK, FAILED TEST. REPLACED EPSU.

Source: SDR AALA201508079008
OTHER · 2015-04-24 Matched by certificate designator
ATA 2565

Part: SLIDE — OBSTRUCTED (L1 DOOR) · airframe 3,567 hrs · 12,770 cycles

C11 CHECK, L1 DOOR SLIDE MATERIAL COVERING PRESS GAUGE PREVENTING MX FROM READING THE SLIDE PRESS. REPLACED SLIDE IAW TC 26L00025010.

Source: SDR AALA201504249009
OTHER · 2015-04-24 Matched by certificate designator
ATA 2565

Part: GAUGE — OUT OF POSITION (L1 DOOR SLIDE)

L1 SLIDE INFLATION BOTTLE PRESSURE GAUGE IS OBSCURED BY COVER, DIFFICULT TO READ GAUGE THROUGH WINDOW. REPLACED THE L1 DOOR SLIDE.

Source: SDR AALA201504279005
OTHER · 2015-04-10 Matched by certificate designator
ATA 3350

Part: LIGHT — MISSING (CABIN) · airframe 35,703 hrs · 12,752 cycles

7X EMERGNECY EXIT LIGHT MISSING. REPLACED MISSING EMERGENCY LIGHT AS REQUIRED.

Source: SDR AALA201504149004
WARNING INDICATION · 2015-03-06 Unresolved
ATA 7532

Part: ACTUATOR — DEFECTIVE (NR 1 ENGINE) · airframe 35,520 hrs · 12,674 cycles

ENGINE 1 COMPRESSOR VANE FAULT ON TAKEOFF ROLL APPROX 50 KIAS. AVOIDED TAKEOFF & SHUTDOWN ENG 1 IAW ECAM. REPLACED VSV ACTUATOR ON NR 1 ENG IAW AMM 75-32-41 & 71-00-00-710. OPERATIONAL CHECKS ACCOMPLISHED WITH NO DEFECTS NOTED.

Source: SDR USAA2015030900006

2014

OTHER · 2014-12-26 Unresolved
ATA 3350

Part: LIGHT — DISCONNECTED (CABIN) · airframe 34,915 hrs · 12,432 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 11C. RECONNECTED EMER LIGHT AT SEAT 11C. OPERATIONS CHECKED NORMAL IAW AMM 33-00.

Source: SDR USAA2014123000006
OTHER · 2014-11-05 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,462 hrs · 12,245 cycles

FORWARD EMER FLASHLIGHT SHOWS NO CHARGE. REPLACED BATTERY IN FWD EMER FLASHLIGHT. OPERATIONS CHECKED GOOD.

Source: SDR USAA2014110600002
NO TEST · 2014-06-24 Unresolved
ATA 2560

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 33,372 hrs · 11,805 cycles

AFT LT FLIGHT ATTENDANT JUMP SEAT OTBD EMER FLASHLIGHT NOT BLINKING. REPLACED BATTERY PACK, OPERATIONS CHECKED GOOD.

Source: SDR USAA2014062700016
OTHER · 2014-05-13 Unresolved
ATA 3350

Part: LENS — MISSING (EXIT SIGN) · airframe 32,921 hrs · 11,659 cycles

1R EXIT DOOR MISSING PLASTIC COVER AT EXIT SIGN TO THE LT OF THE SLIDE. INSTALLED DOOR R1 EXIT SIGN LENS.

Source: SDR USAA2014051400008
NO TEST · 2014-02-04 Unresolved
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,928 hrs · 11,335 cycles

EMERGENCY POWER SUPPLY UNIT CABIN LT WILL NOT TEST. REPLACED BATTERY PACK OF CABIN MIDDLE LT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.

Source: SDR USAA2014020500004

2013

OTHER · 2013-12-30 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 31,613 hrs · 11,224 cycles

EMERGENCY EXIT SIGN LENS ABOVE DOOR 2L IS MISSING. INSTALLED EMERGENCY EXIT SIGN LENS AT DOOR 2L IAW A320 AMM 33-57-13-400.

Source: SDR USAA2014010200006
NO TEST · 2013-12-01 Unresolved
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,358 hrs · 11,141 cycles

MAINTENANCE REPORTED THE EMERGENCY ROW LIGHT 11C INOPERATIVE. R & R EMERGENCY ROW LIGHT 11C IAW AMM 33-51-19-401, OPERATIONS CHECKED GOOD.

Source: SDR USAA2013120200010
OTHER · 2013-10-24 Unresolved
ATA 3350

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 30,982 hrs · 11,018 cycles

CREW REPORTED THE FLOOR LEVEL EXIT LIGHT LENS MISSING AT 1L DOOR. MAINTENANCE REPLACED LENS AT 1L DOOR.

Source: SDR USAA2013102500006
NO TEST · 2013-10-07 Unresolved
ATA 3350

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,778 hrs · 10,949 cycles

BULBS IN EMERGENCY EXIT SIGN DOOR 1R INOPERATIVE. REPLACED EMERGENCY EXIT SIGN.

Source: SDR USAA2013100800003
OTHER · 2013-08-19 Unresolved
ATA 3350

Part: LIGHT — BROKEN (ZONE 200) · airframe 30,347 hrs · 10,806 cycles

EMERGENCY LIGHT, AISLE SEAT 7C BROKEN, LENS MISSING. REPLACED EMERGENCY LIGHT AT SEAT 7C.

Source: SDR USAA2013082000003
OTHER · 2013-03-25 Unresolved
ATA 3397

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 28,678 hrs · 10,295 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 15 INOPERATIVE. RECONNECTED ELECTRICAL CONNECTOR TO LIGHT ASSEMBLY ON OVERHEAD CEILING MOUNTED EMERGENCY LIGHT PER AIRBUS MAINTENANCE MANUAL 33-51-11. OPERATIONAL CHECK NORMAL.

Source: SDR USAA2013032600008
FLT CONT AFFECTED · 2013-01-09 Unresolved
ATA 2782

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 27,942 hrs · 10,052 cycles

FLIGHT CONTROL SLATS FAULT ECAM MESSAGE ON INITIAL SELECTION OF FLAPS - SLATS DID NOT EXTEND. THIS CREATED A HIGHER APPROACH SPEED SO AN EMERGENCY WAS DECLARED AND CABIN WAS PREPPED AS A PRECAUTION. LANDING SPEED WAS 165 KTS. AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT, (AND NO PASSENGER ISSUES). FOUND LEFT ROTARY ACTUATOR 6029CM TORQUE LIMITER POPPED. REMOVED AND REPLACED B-SLAT ACTUATOR IAW 27-84-49-401.

Source: SDR USAA2013011000017

2012

OTHER · 2012-11-07 Unresolved
ATA 3350

Part: LIGHT — MISSING (CABIN) · airframe 27,375 hrs · 9,847 cycles

EMERGENCY LIGHT AT 11C MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT 11C.

Source: SDR USAA2012110800017
OTHER · 2012-10-25 Unresolved
ATA 3350

Part: LIGHT — DETACHED (CABIN) · airframe 27,267 hrs · 9,803 cycles

EMERGENCY EXIT LIGHT, ROW 1 AIRCRAFT LEFT, DETACHED. RE-ATTACHED EXIT LIGHT ASSEMBLY.

Source: SDR USAA2012102600003
OTHER · 2012-10-03 Unresolved
ATA 3350

Part: FIXTURE — LOOSE (CABIN) · airframe 27,046 hrs · 9,725 cycles

EMERGENCY FLOOR LIGHTING FIXTURE AT 1C LOOSE AND DANGLING. RE-INSTALLED FIXTURE AT SEAT 1C. OPERATIONAL CHECK GOOD.

Source: SDR USAA2012100500033
OTHER · 2012-09-26 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 26,980 hrs · 9,706 cycles

EMERGENCY EXIT LIGHT (RED) AT ROW 9D ON THE SEAT LENS COVER IS MISSING. REMOVED AND REPLACED LAMP ASSEMBLY AT SEAT 9D.

Source: SDR USAA2012092800004
OTHER · 2012-08-15 Unresolved
ATA 3350

Part: LIGHT — MISSING (CABIN) · airframe 26,567 hrs · 9,563 cycles

RED EXIT ROW LIGHTS AT SEAT 1C MISSING FROM WIRES. RE-ATTACHED SEAT 1C EMERGENCY LIGHT AS REQUIRED.

Source: SDR USAA2012081600012
OTHER · 2012-03-01 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 24,836 hrs · 8,988 cycles

THE 16R EMERGENCY EXIT LIGHT COVER MISSING. REPLACED 16R EMERGENCY EXIT LIGHT COVER.

Source: SDR USAA2012030200001

2011

OTHER · 2011-10-23 Unresolved
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,780 hrs · 8,621 cycles

EMERGENCY EXIT LIGHT AT 1C IS INOPERATIVE. RE-INSTALLED EMERGENCY EXIT LIGHT AT 1C. OPS CHECKED GOOD.

Source: SDR USAA2011102400024
SMOKE/FUMES/ODORS/SPARKS · 2011-09-16 Unresolved
ATA 3442

Part: TRANSCEIVER — FAULTY (NR 1 RADAR) · airframe 23,389 hrs · 8,500 cycles

SPECIAL ITEM "SMOKE IN CABIN" JOB CARD 26L00021001 REQUIRED. ACCOMPLISHED JOB CARD # 26L00021001. BASED ON JOB CARD 26L00021001, SOURCE OF ODOR IS THE NR 1 RADAR TRANSCEIVER. LOGPAGE 7565979: RADAR INOPERATIVE. REMOVED AND REPLACED RADAR TRANCEIVER PER AMM 34-41-33. SHOP TEARDOWN REPORT STATES "NO TROUBLE FOUND".

Source: SDR USAA2011110100001
WARNING INDICATION · 2011-06-21 Unresolved
ATA 2915

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 22,473 hrs · 8,184 cycles

SFO-PHL - EL - INFLIGHT LOSS OF GREEN HYDRAULIC PRESSURE. GREEN ENGINE PUMP WAS TURNED OFF WITHIN 30 SECONDS. FOUND LEFT ENGINE HYD PRESSURE SWITCH AT FAULT. REPLACED LEFT ENGINE HYDRAULIC PRESSURE SWITCH PER AMM 29-11-17-400-041. SERVICED HYDRAULIC QUANTITY AS NEEDED, ENGINE RUN-UP AND CHECKED NORMAL.

Source: SDR USAA2011062400007
OTHER · 2011-05-13 Unresolved
ATA 2560

Part: ESCAPE ROPE — MISSING (CABIN) · airframe 22,063 hrs · 8,043 cycles

FLT 174 - PHX-TUS - EMERGENCY EQUIPMENT - LIFE LINE (ESCAPE ROPE) OVERWING AIRCRAFT LEFT MISSING. REPLACED MISSING LIFE LINE (ESCAPE ROPE).

Source: SDR USAA2011051691855
OTHER · 2011-04-24 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,816 hrs · 7,954 cycles

MCN - SY6 CHECK C11 CHECK 2 FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS HAVE LOW BATTERIES. REPLACED FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS BATTERIES 2 EACH AS REQUIRED.

Source: SDR USAA2011042791654
OTHER · 2011-04-22 Unresolved
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON SEAT RAIL BEAM AT FR66, Y1292. REPLACED SEAT RAIL BEAM AT FR66, Y1292 IAW A320 SRM 51-42-11 & AIRBUS DRAWING 18D53472172.

Source: SDR USAA2011050391743
OTHER · 2011-04-22 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, Y1292 IAW A320 SRM 51-42-11 & AIRBUS DRAWING 18D53472209.

Source: SDR USAA2011050391742
OTHER · 2011-04-21 Unresolved
ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON L2 ENTRY SILL FLOOR PANEL BETWEEN FR66 TO FR68, Y1292. REPLACED FLOOR PANEL BETWEEN FR66 TO FR68, Y1292 IAW A320 SRM 51-74-00.

Source: SDR USAA2011050391744
OTHER · 2011-04-21 Unresolved
ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON R2 ENTRY SILL FLOOR PANEL BETWEEN FR66 TO FR68, -Y1292. REPLACED R2 ENTRY SILL FLOOR PANEL BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-74-00.

Source: SDR USAA2011050391745
OTHER · 2011-04-20 Unresolved
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON L-2 DOOR SILL AT FR66, Y1292. REPAIRED L-2 DOOR SILL AT FR66, Y1292 IAW A320 SRM 53-41-14.

Source: SDR USAA2011050291734
OTHER · 2011-04-20 Unresolved
ATA 5320

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL AT FR66, -Y1292. REPAIRED R2 DOOR SILL AT FR66, -Y1292 IAW A320 SRM 53-41-14.

Source: SDR USAA2011050391746
OTHER · 2011-04-19 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - PREVIOUSLY BLENDED EXFOLIATION CORROSION ON FLOORBEAM AT FR64 + 16 INCHES, -Y1732. REPLACED FLOOR BEAM AT FR64 + 16 INCHES, -Y1732 IAW A320 SRM 51-42-11.

Source: SDR USAA2011050291735
OTHER · 2011-04-19 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,926 hrs · 7,995 cycles

MCN - C11 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT 64 + 16 INCHES, Y1732. REPLACED FLOORBEAM AT 64 + 16 INCHES, Y1732 IAW A320 SRM 51-42-11.

Source: SDR USAA2011050391741

2010

NO TEST · 2010-12-13 Unresolved
ATA 3350

Part: EPSU — INOPERATIVE (CABIN) · airframe 20,643 hrs · 7,565 cycles

LOG PAGE 4722412 - FLT 307-LAS - EEL - LEFT EMERGENCY POWER SUPPLY UNIT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED EPSU (11WL) IAW AIRBUS MAINTENANCE MANUAL 33-51-38.

Source: SDR USAA2010121493056
NO TEST · 2010-03-17 Unresolved
ATA 3350

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,002 hrs · 6,660 cycles

FLT 307 LAS - EEL - EMERGENCY EXIT LIGHT TEST FAILS LEFT EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT (L PSU) BATTERY IAW AIRBUS MAINTENANCE MANUAL 33-51-38-401.

Source: SDR USAA2010031890605

2009

NO TEST · 2009-09-07 Unresolved
ATA 3350

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,296 hrs · 6,061 cycles

FLT 230 PHX - EEL - FLASHLIGHT UNDER FORWARD FLIGHT ATTENDANT JUMPSEAT IS NOT SEALED AND NEEDS A NEW BATTERY. MAINTENANCE REPLACED BATTERY AND INSTALLED NEW SECURITY STRAP.

Source: SDR USAA2009090892395

2008

NO TEST · 2008-05-13 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,425 hrs · 4,366 cycles

SAL - EMERGENCY EQUIPMENT - BC2 CHECK - NR 6103162, AFT FLIGHT ATTENDANT SEAT LEFT INBOARD FLASHLIGHT CHARGE INDICATOR NOT BLINKING. REPLACED AFT FLIGHT ATTENDANT SEAT LEFT INBOARD FLASHLIGHT BATTERY.

Source: SDR USAA920081156
NO TEST · 2008-05-13 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,425 hrs · 4,366 cycles

SAL - EMERGENCY EQUIPMENT - BC2 CHECK - NR 6101927, FORWARD FLIGHT ATTENDANT SEAT LEFT FLASHLIGHT CHARGE INDICATOR NOT BLINKING. REPLACED FORWARD FLIGHT ATTENDANT SEAT LEFT FLASHLIGHT BATTERY.

Source: SDR USAA920081157
NO TEST · 2008-05-13 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,425 hrs · 4,366 cycles

SAL - EMERGENCY EQUIPMENT - BC2 CHECK - NR 6103162, AFT FLIGHT ATTENDANT SEAT LEFT OUTBOARD FLASHLIGHT CHARGE INDICATOR NOT BLINKING. REPLACED AFT FLIGHT ATTENDANT SEAT LEFT OUTBOARD FLASHLIGHT BATTERY.

Source: SDR USAA920081155

2007

WARNING INDICATION; SMOKE/FUMES/ODORS/SPARKS · 2007-04-13 Unresolved
ATA 2121

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 7,257 hrs · 2,794 cycles

SJC - BS - CREW REPORTED BLOWER FAIL ECAM MESSAGE ALONG WITH A STRONG ODOR OF AN ELECTRICAL BURNING SMELL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO LAX. MX REPLACED THE BLOWER FAN ASSY, 20QH PER AMM 21-26-51. OPERATIONAL CHECK WAS GOOD.

Source: SDR AWXA200700492
INADEQUATE Q C; FLAME/FIRE · 2007-02-11 Unresolved
ATA 2530

Part: OVEN — FIRE (GALLEY) · airframe 6,599 hrs · 2,535 cycles

OVEN FIRE, F/A REPORTED FIRE IN OVEN NR 4, CARDBOARD FROM FOOD TRAY CAUGHT FIRE. THE F/A EXTINGUISHED WITH PORTABLE HALON FIRE EXTINGUISHER. MX REMOVED AND REPLACED AFT GALLEY HALON EXTINGUISHER AND PLACED THE OVEN ON MEL.

Source: SDR AWXA200700197