N675AW

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.

166 reports on file, 2005-11-30 – 2017-04-26.

OTHER · 2017-04-26 Matched by certificate designator
ATA 2560

Part: PROXIMITY SWITCH — OUT OF ADJUST (R2 DOOR HANDLE) · airframe 42,292 hrs · 15,590 cycles

R2 DOOR ARM HANDLE DOES NOT INDICATE ARMED IN FLIGHT. PERFORMED ADJUSTMENT OF THE PROXIMITY SWITCH.

Source: SDR AALA201704279005
NO TEST · 2017-04-19 Matched by certificate designator
ATA 3350

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 42,290 hrs · 15,589 cycles

CABIN EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT AT 11WL IAW AMM 33-51-38-400-001A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Source: SDR AALA201704219017
NO TEST · 2017-04-19 Matched by certificate designator
ATA 3350

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 42,290 hrs · 15,589 cycles

CABIN EMERGENCY EXIT LIGHTS FAILED TO TEST. REPLACED EMERGENCY POWER SUPPLY UNIT AT 10WL IAW AMM 33-51-38-400-001A. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Source: SDR AALA201704219016
OTHER · 2017-04-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 42,290 hrs · 15,589 cycles

DELAMINATED RIGHT SIDE SLOPING FLOOR PANEL 132FF IN FORWARD CARGO BAY. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701, REVISION G.

Source: SDR AALA201704199003
OTHER · 2017-03-13 Matched by certificate designator
ATA 3350

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,290 hrs · 15,589 cycles

MISSING EMERGENCY LIGHT LENS 24A, IN PASSENGER CABIN. INSTALLED NEW EMERGENCY LIGHT LENS 24A.

Source: SDR AALA201703149009
OTHER · 2017-03-13 Matched by certificate designator
ATA 3350

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,290 hrs · 15,589 cycles

MISSING EMERGENCY LIGHT LENS 1A, IN PASSENGER CABIN. INSTALLED NEW EMERGENCY LIGHT LENS 1A

Source: SDR AALA201703149011
OTHER · 2017-03-13 Matched by certificate designator
ATA 3350

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 42,290 hrs · 15,589 cycles

MISSING EMERGENCY PATH LIGHT LENS 4A, IN PASSENGER CABIN. INSTALLED NEW EMERGENCY LIGHT LENS 4A

Source: SDR AALA201703149010
OTHER · 2017-03-03 Matched by certificate designator
ATA 5280

Part: HINGE — WORN (NLG DOOR) · airframe 42,290 hrs · 15,589 cycles

WEAR ON RIGHT NOSE LANDING GEAR AFT DOOR HINGES, FORWARD AND AFT POSITION. REPLACED HINGES IAW CMM 52-82-32.

Source: SDR AALA201703059010
OTHER · 2017-03-03 Matched by certificate designator
ATA 5280

Part: HINGE — WORN (NLG DOOR) · airframe 42,290 hrs · 15,589 cycles

WEAR ON LEFT NOSE LANDING GEAR AFT DOOR HINGES, FORWARD AND AFT POSITION. REPLACED THE HINGES IAW CMM 52-82-32.

Source: SDR AALA201703059009
OTHER · 2017-03-02 Matched by certificate designator
ATA 3220

Part: BEARING — MIGRATED (NLG LINK) · airframe 42,290 hrs · 15,589 cycles

MIGRATED BEARING ON LINK AT LOWER POSITION OF NOSE LANDING GEAR. REPLACED LOWER LINK IAW CMM 32-37-02.

Source: SDR AALA201703039004
OTHER · 2017-02-20 Matched by certificate designator
ATA 5340

Part: BUSHING — MIGRATED (FITTING) · airframe 42,290 hrs · 15,589 cycles

MIGRATED BUSHING ON LEFT MAIN LANDING GEAR DOOR ACTUATOR ATTACH POINT KEEL BEAM, IN AFT LUG AT FRAME 42 BETWEEN STRINGER 41 AND 42L. REPLACED FITTING IAW EA 261038.

Source: SDR AALA201703239008
OTHER · 2017-02-20 Matched by certificate designator
ATA 5340

Part: BUSHING — MIGRATED (ATTACH FITTING) · airframe 42,290 hrs · 15,589 cycles

MIGRATED BUSHING ON LEFT MAIN LANDING GEAR DOOR ACTUATOR, UPPER ATTACH POINT ON KEEL BEAM, FORWARD LUG AT FRAME 42 BETWEEN STRINGERS 41 AND 42L. REPLACED FITTING IAW EA 261038.

Source: SDR AALA201703229003
OTHER · 2017-02-18 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

CORROSION ON AFT GALLEY LOWER SUPPORT AT STRINGER 23L BETWEEN FRAMES 66 AND 68. REPLACED THE SUPPORT SRM 51-72-11, AND EA 267408.

Source: SDR AALA201703019017
OTHER · 2017-02-17 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CRACKED (FRAMES 64-66) · airframe 42,290 hrs · 15,589 cycles

CRACK ON AFT GALLEY FLOOR SUPPORT AT -Y254 BETWEEN FRAMES 64 TO 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472040.

Source: SDR AALA201703019015
OTHER · 2017-02-15 Matched by certificate designator
ATA 5530

Part: ATTACH FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER, RUDDER HINGE ARM 5 BEARING. REPLACED HINGE ARM 5 SRM 51-72-11.

Source: SDR AALA201703089004
OTHER · 2017-02-15 Matched by certificate designator
ATA 5530

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON BEARING, HINGE ARM FITTING ASSEMBLY 4 RUDDER AT RIB 6, VERTICAL STABILIZER. REPLACED HINGE ARM FITTING SRM 51-72-11.

Source: SDR AALA201703079041
OTHER · 2017-02-10 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 32-35) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703019019
OTHER · 2017-02-10 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 28-32) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703019023
OTHER · 2017-02-10 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 32-35) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703019018
OTHER · 2017-02-09 Matched by certificate designator
ATA 5320

Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703019014
OTHER · 2017-02-09 Matched by certificate designator
ATA 5530

Part: HINGE FITTING — WORN (VERTICAL STAB) · airframe 42,290 hrs · 15,589 cycles

EXCESSIVE PLAY ON VERTICAL STABILIZER NR 1 HINGE ARM BEARING. REPLACED HINGE ARM FITTING IAW SRM 51-72-11.

Source: SDR AALA201703159011
OTHER · 2017-02-06 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201703159016
OTHER · 2017-02-06 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 36-42) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703019021
OTHER · 2017-02-06 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 51-54) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251FF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201703019016
OTHER · 2017-02-06 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703159019
OTHER · 2017-02-06 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 47-51) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251AF. REPLACED FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201703019024
OTHER · 2017-02-06 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON PASSENGER CABIN FLOOR PANEL 241MF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201703159018
OTHER · 2017-02-05 Matched by certificate designator
ATA 5280

Part: ATTACH FITTING — DAMAGED (MLG DOOR) · airframe 42,290 hrs · 15,589 cycles

ELONGATED HOLE IN RIGHT MLG DOOR FORWARD ATTACHMENT FITTING . REPLACED THE MLG DOOR FITTING EA 267630.

Source: SDR AALA201703159017
INADEQUATE Q C · 2017-02-03 Matched by certificate designator
ATA 5210

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 42,290 hrs · 15,589 cycles

OUT OF ADJUSTMENT DIMENSION A (J2) PASSENGER CREW DOOR 832 BETWEEN FINGER AND STRIKER LEVER DAMPER MECHANISM AT AFT GALLEY AREA. ADJUSTED DIMENSION A (J2) PASSENGER CREW DOOR 832 BETWEEN FINGER AND STRIKER LEVER DAMPER MECHANISM AT AFT GALLEY AREA IAW AMM 52-13-14-820-002-A STEP 4.A ITEM(2).

Source: SDR AALA201702049004
OTHER · 2017-02-03 Matched by certificate designator
ATA 5315

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY INBOARD UPPER FLOORBEAM COUPLING AT -Y1162 AND FR 68. REPLACED COUPLING PER SRM 51-72-11.DRAWING D53472780.

Source: SDR AALA201702139035
OTHER · 2017-02-02 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT GALLEY, SECTION CONNECTING CROSS BEAM AT FR 68 AND STRINGER 23L. REPLACED CONNECTING SECTION PER SRM 51-72-11.

Source: SDR AALA201702239009
OTHER · 2017-02-02 Matched by certificate designator
ATA 5313

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLE IN CARGO COMPARTMENT ON STRINGER 34L AND FR 34 PLUS 14 INCHES. REPAIRED STRINGER PER SRM 53-00-13.

Source: SDR AALA201703079027
OTHER · 2017-02-02 Matched by certificate designator
ATA 5310

Part: PRESSURE PANEL — CRACKED (FRAME 43) · airframe 42,290 hrs · 15,589 cycles

A CRACK INDICATION ON THE LEFT BOX BEAM, PRESSURE PLATE FASTENER HOLE AT FRAME 43 BETWEEN Y1292 AND Y1650. REPLACED PRESSURE PLATE SRM 51-72-11.

Source: SDR AALA201704179004
OTHER · 2017-02-02 Matched by certificate designator
ATA 5210

Part: DAMPENER — OUT OF ADJUST (PAX DOOR) · airframe 42,290 hrs · 15,589 cycles

PASSENGER CREW DOOR BETWEEN FINGER AND STRIKER LEVER DAMPER MECHANISM AT FWD GALLEY AREA OUT OF ADJUSTMENT. ADJUSTED THE PASSENGER CREW DOOR IAW AMM 52-11-14-820-002-A STEP 4.A ITEM 2

Source: SDR AALA201702039013
OTHER · 2017-01-31 Matched by certificate designator
ATA 5320

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SUPPORT FRAME AT STRINGER 23L BETWEEN FR 69 TO FR 70. REPLACED SUPPORT FRAME PER SRM 51-72-11.

Source: SDR AALA201702139043
OTHER · 2017-01-31 Matched by certificate designator
ATA 5320

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SUPPORT FRAME AT STRINGER 23R BETWEEN FR 69 AND FR 70. REPLACED SUPPORT FRAME PER SRM 51-72-11 AND DRAWING D53474180.

Source: SDR AALA201702169013
OTHER · 2017-01-30 Matched by certificate designator
ATA 5755

Part: HINGE PIN — CORRODED (LT SPOILER) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WING SPOILER NR 1 CENTER INBOARD SIDE HINGE PIN. REPLACED HINGE PIN PER AMM 27-64-41-400-001-A.

Source: SDR AALA201702179005
OTHER · 2017-01-30 Matched by certificate designator
ATA 5755

Part: HINGE PIN — CORRODED (LT SPOILER) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING OUTBOARD SIDE SPOILER NR 1 CENTER HINGE PIN THREADS. REPLACED HINGE PIN PER AMM 27-64-41.

Source: SDR AALA201702209020
OTHER · 2017-01-30 Matched by certificate designator
ATA 5751

Part: SUPPORT — CORRODED (LT AILERON) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING AILERON NR 3 SUPPORT ASSEMBLY. REPLACED AILERON NR 3 SUPPORT ASSEMBLY PER AMM 57-51-31-400-001-A.

Source: SDR AALA201702139041
OTHER · 2017-01-27 Matched by certificate designator
ATA 5280

Part: HINGE FITTING — DAMAGED (MLG DOOR) · airframe 42,290 hrs · 15,589 cycles

ELONGATED HOLE ON LEFT FORWARD MLG DOOR HINGE ASSEMBLY BEARING. REPLACED HINGE FITTING ASSEMBLY IAW CMM 52-81-18.

Source: SDR AALA201703159013
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 231 BF. REPLACED FLOOR PANEL 231BF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139029
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 28-31) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703039020
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 231 FF. REPLACED FLOOR PANEL 231FF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702159012
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT GALLEY FLOOR PANEL 221PF. REPLACED FLOOR PANEL PER SRM 53-12-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702169004
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON FORWARD GALLEY FLOOR PANEL 232DF. REPLACED THE FLOOR PANEL IAW SRM 51-72-11 AND DRAWING D53610668 REVISION B.

Source: SDR AALA201702139027
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 232FF. REPLACED FLOOR PANEL 232FF PER SRM 53-12-00 AND IRM 9701 REV G.

Source: SDR AALA201702159008
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: PRESSURE DECK — CORRODED (FRAMES 35-36) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

CORROSION ON FORWARD CARGO BAY PRESSURE DECK UPPER SURFACE AT -Y765 BETWEEN FRAMES 35 AND 36. REPAIRED THE PRESSURE DECK SURFACE IAW EA 267426.

Source: SDR AALA201703159008
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON FLOOR PANEL 231CF. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Source: SDR AALA201702139024
OTHER · 2017-01-25 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON TOP LAYER OF COCKPIT FLOOR PANEL 212CF. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Source: SDR AALA201702139026
OTHER · 2017-01-21 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 252NF. REPLACED FLOOR PANEL 252NF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702219008
OTHER · 2017-01-21 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 58-62) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 251RF. REPLACED FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201703019022
OTHER · 2017-01-19 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 42,290 hrs · 15,589 cycles

CRACK ON PASSENGER CABIN FLOOR PANEL 251LF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Source: SDR AALA201702139025
OTHER · 2017-01-19 Matched by certificate designator
ATA 5530

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON HINGE ARM 3 AT RIB 5 ON VERTICAL STABILIZER. REPLACED HINGE FITTING PER SRM 51-72-11.

Source: SDR AALA201703079032
OTHER · 2017-01-19 Matched by certificate designator
ATA 5320

Part: PROFILE — CRACKED (FRAMES 64-65) · airframe 42,290 hrs · 15,589 cycles

CRACK ON AFT CARGO BAY PROFILE AT STRINGER 44L BETWEEN FRAMES 64 AND 65. REPLACED THE PROFILE IAW SRM 51-72-11 AND DRAWING F53474160.

Source: SDR AALA201703039021
OTHER · 2017-01-19 Matched by certificate designator
ATA 5530

Part: HINGE FITTING — EXCESS PLAY (VERTICAL STAB) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON VERTICAL STABILIZER HINGE ARM 7. REPLACED HINGE ARM 7 FITTING PER SRM 51-72-11.

Source: SDR AALA201703099003
OTHER · 2017-01-19 Matched by certificate designator
ATA 5530

Part: FITTING — WORN (VERTICAL STAB) · airframe 42,290 hrs · 15,589 cycles

EXCESSIVE PLAY ON VERTICAL STABILIZER NR 2 HINGE ARM FITTING. REPLACED HINGE ARM FITTING IAW SRM 51-72-11.

Source: SDR AALA201703159010
OTHER · 2017-01-19 Matched by certificate designator
ATA 5310

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 42,290 hrs · 15,589 cycles

CRACK INDICATION ON THE LEFT PASSENGER CABIN SIDE BOX BEAM FIRST FASTENER HOLE, FORWARD OF FRAME 43 AND Y1650. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Source: SDR AALA201704179003
OTHER · 2017-01-19 Matched by certificate designator
ATA 5310

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 42,290 hrs · 15,589 cycles

A CRACK INDICATION ON THE LEFT PASSENGER CABIN SIDE BOX BEAM SECOND FASTENER HOLE, TWO INCHES FORWARD OF FRAME 43 AND Y1650. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Source: SDR AALA201704179006
OTHER · 2017-01-19 Matched by certificate designator
ATA 5310

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 42,290 hrs · 15,589 cycles

A CRACK INDICATION ON RIGHT PASSENGER CABIN SIDE BOX BEAM, ONE INCH FORWARD OF FRAME 43 AND -Y1650. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Source: SDR AALA201704179005
OTHER · 2017-01-18 Matched by certificate designator
ATA 5320

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY CENTER FITTING AT STRINGER 23L, BETWEEN FR 16 AND FR 20. REPLACED CENTER FITTING PER SRM 51-72-11 AND DRAWING D53112175.

Source: SDR AALA201703079040
OTHER · 2017-01-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK Y1292 BETWEEN FR 64 AND FR 66 PLUS 5 INCHES. REPLACED SEAT TRACK PER SRM 51-72-11 .

Source: SDR AALA201702159009
OTHER · 2017-01-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SEAT TRACK AT Y765 BETWEEN FR 64 TO FR 66 PLUS 5 INCHES. REPLACED SEAT TRACK PER SRM 51-72-11.

Source: SDR AALA201702139040
OTHER · 2017-01-18 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM AT -Y1162 BETWEEN FR 67 PLUS 15 INCHES TO FR 69. REPLACED FLOORBEAM PER SRM 51-72-11.

Source: SDR AALA201702159010
OTHER · 2017-01-18 Matched by certificate designator
ATA 5320

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23R, BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-72-11, DRAWING D53480505 AND EA 267409.

Source: SDR AALA201702239010
OTHER · 2017-01-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY SEAT TRACK AT STRINGER 23R AND FR 20. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53112812 AND D53110876.

Source: SDR AALA201703079039
OTHER · 2017-01-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

CORROSION ON SEAT TRACK, Y1292 BETWEEN FRAMES 36 AND 41. REPLACED THE SEAT TRACK IAW SRM 51-42-11.

Source: SDR AALA201702229008
OTHER · 2017-01-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT RAIL AT -Y1292 BETWEEN FR 64 PLUS 1 INCH. REPLACED SEAT RAIL PER SRM 51-72-11.

Source: SDR AALA201702159011
OTHER · 2017-01-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SEAT RAIL -Y765 BETWEEN FR 64 TO FR 66 PLUS 5 INCHES. REPLACED SEAT RAIL PER SRM 51-72-11.

Source: SDR AALA201702139044
OTHER · 2017-01-18 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201704129001
OTHER · 2017-01-18 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

CORROSION ON AFT GALLEY SHEAR PLATE AT STRINGER 23L BETWEEN FRAMES 69 AND 70. REPLACED SHEAR PLATE IAW SRM A320 51-72-11 AND DRAWING D53474180.

Source: SDR AALA201704129002
OTHER · 2017-01-18 Matched by certificate designator
ATA 5320

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MED DOOR GIRT BAR FITTING AROUND HI-LOCS AT STRINGER 23L BETWEEN FR16 AND FR20. REPLACED FITTING PER SRM 51-72-11.

Source: SDR AALA201703079026
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 252HF. REPLACED FLOOR PANEL 252HF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702219006
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 16-20) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703019020
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY, TOP LAYER OF FLOOR PANEL 222CF. REPLACED FLOOR PANEL 222CF PER AMM 53-12-12-400-001.

Source: SDR AALA201703079031
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FRAMES 36-42) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON FLOOR PANEL BETWEEN Y254 AND -Y254, BETWEEN FRAMES 36 AND 42. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.

Source: SDR AALA201703019025
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON TOP LAYER OF PASSENGER CABIN FLOOR PANEL 241LF. REPLACED FLOOR PANEL 241LF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702219007
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201703159014
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON PASSENGER CABIN TOP LAYER OF FLOOR PANEL 242FF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702229007
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATED TOP LAYER FLOOR PANEL 261AG AT AFT GALLEY AREA. REPLACED FLOOR PANEL 261AG PER SRM 53-02-00.

Source: SDR AALA201702019010
OTHER · 2017-01-17 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON FORWARD GALLEY TOP LAYER FLOOR PANEL 232EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00, AND IRM 9701 REVISION G.

Source: SDR AALA201703159015
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND 9701 REVISON G.

Source: SDR AALA201702039004
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

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

Source: SDR AALA201702039005
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151MF. REPLACED FLOOR PANEL 151MF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139031
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131GF. REPLACED FLOOR PANEL 131GF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139036
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151FF. REPLACED FLOOR PANEL 151FF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139037
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151CF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Source: SDR AALA201703159012
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152EF. REPLACED FLOOR PANEL 152EF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139038
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151EF. REPLACED FLOOR PANEL 151EF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139039
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151RF. REPLACED FLOOR PANEL 151RF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139033
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATED ON AFT CARGO BAY FLOOR PANEL 151DF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND 9701 REVISION G.

Source: SDR AALA201702039007
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151QF. REPLACED FLOOR PANEL 151QF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139032
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 132KF. REPLACED FLOOR PANEL 132KF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139028
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON LEFT HAND SIDE FORWARD CARGO COMPARTMENT FLOOR PANEL 131BF. REPLACED FLOOR PANEL 131BF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139042
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 132 GF. REPLACED FLOOR PANEL 132GF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139034
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131CF. REPLACED FLOOR PANEL 131CF PER SRM 53-02-00 AND IRM 9701 REVISION G.

Source: SDR AALA201702139030
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00.

Source: SDR AALA201702139023
OTHER · 2017-01-12 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 42,290 hrs · 15,589 cycles

DELAMINATED ON AFT CARGO BAY FLOOR PANEL 152MF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND 9701 REVISION G.

Source: SDR AALA201702039006
Earlier reports · 2005–2016 · 69 reports

2016

WARNING INDICATION · 2016-10-30 Matched by certificate designator
ATA 2750

Part: VALVE — FAULTED (FLAPS) · airframe 41,723 hrs · 15,336 cycles

FLIGHT CREW REPORTED RECIEVING A "F/CTL FLAP SYS 1 FAULT" ON FINAL APPROACH, EXECUTED A GO AROUND, RAN NON-NORMAL PROCEDURE DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TSM 27-51-02-810-852-A AND FOUND FLAP VALVE BLOCK 23CV - FOR FLAP SYSTEM 1 BAD AND REPLACED VALVE BLOCK PER AMM 27-54-53-400-001-A. AIRCRAFT WAS GROUNDED.

Source: SDR AALA201610319023
SMOKE/FUMES/ODORS/SPARKS · 2016-10-28 Matched by certificate designator
ATA 2530

Part: OVEN — SMOKE (GALLEY) · airframe 41,720 hrs · 15,335 cycles

AIRCRAFT WAS NOT GROUNDED. OVEN 1 FORWARD GALLEY SMOKING. REMOVED AND REPLACED FWD GALLEY OVEN NR 1 PER AMM 25-35-19-000-001.

Source: SDR AALA201611019012
OTHER · 2016-10-27 Matched by certificate designator
ATA 3350

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 41,713 hrs · 15,332 cycles

EMERGENCY LIGHT LENS MISSING AT 10F. REPLACED THE LENS IAW AMM 33-50-00.

Source: SDR AALA201610289001
NO TEST · 2016-09-17 Matched by certificate designator
ATA 3397

Part: WIRE HARNESS — DEFECTIVE (EMERGENCY LIGHTS) · airframe 41,355 hrs · 15,156 cycles

SEAT ROW ROW 4 EMERGENCY LIGHT INOPERATIVE. REPLACED THE WIRE HARNESS UNDER SEAT AND ACCOMPLISHED A SATISFACTORY OPS CHECKED IAW AMM 33-51-00.

Source: SDR AALA201609199022
NO TEST · 2016-09-17 Matched by certificate designator
ATA 3397

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 41,355 hrs · 15,156 cycles

SEAT ROW 9 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND HARNESS DISCONNECTED UNDER SEAT, CONNECTED AND ACCOMPLISHED A SATISFACTORY OPS CHECKED IAW AMM 33-51-00-710-001.

Source: SDR AALA201609199023
NO TEST · 2016-09-17 Matched by certificate designator
ATA 3397

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 41,355 hrs · 15,156 cycles

SEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT WALL CONNECTOR, CRIMPED NEW PIN, REPLACED BACKSHELL AND ACCOMPLISHED A SATISFACTORY OPS CHECKED IAW AMM 33-51-00-710-001.

Source: SDR AALA201609199021
NO TEST · 2016-06-25 Matched by certificate designator
ATA 3350

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,604 hrs · 14,815 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGNS DO NOT LIGHT UP AT AFT L2 AND R2 DOORS. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-38.

Source: SDR AALA201606269001
FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2016-05-01 Matched by certificate designator
ATA 4920

Part: APU — LEAKING (APU BAY) · airframe 40,211 hrs · 14,648 cycles

AIRCRAFT WAS GNDED. DIRTY SOCK SMELL IN DESCENT OUT OF FL 200. FOUND THE APU LEAKING OIL & REPLACED IT IAW TASK CARD 26L31049005.

Source: SDR AALA201605029014
OTHER · 2016-03-20 Matched by certificate designator
ATA 3350

Part: LIGHT — UNSECURE (CABIN) · airframe 39,882 hrs · 14,515 cycles

AIRCRAFT WAS NOT GNDED, EMER EXIT PATH LIGHT HANGING AT ROW 1C. SECURED LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Source: SDR AALA201603219009
OTHER · 2016-01-21 Matched by certificate designator
ATA 5753

Part: FLAP — DELAMINATED (LT WING) · airframe 39,388 hrs · 14,296 cycles

DURING POST OPEN INSPECTION, FOUND LT OTBD FLAP, TE UPPER ATTACH LEG FOR TE WEDGE BOTTOM SURFACE, DELAMINATED AT ALL ATTACH HOLES. REPAIRED FLAP IAW SRM 57-53-00-201-8E.

Source: SDR AALA201601229008

2015

NO TEST · 2015-07-15 Matched by certificate designator
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 37,717 hrs · 13,609 cycles

FORWARD FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT NOT BLINKING. R & R FLIGHT ATTENDANT FWD FLASHLIGHT BATTERY. OPERATIONS CHECKED GOOD ON GND AT THIS TIME.

Source: SDR AALA201507169005
OTHER · 2015-03-29 Unresolved
ATA 3350

Part: LENS — BROKEN (CABIN) · airframe 36,634 hrs · 13,173 cycles

EMERGENCY EXIT LIGHT LENS ADJACENT L1 DOOR BROKEN. REPLACED EMER EXIT LIGHT LENS.

Source: SDR USAA2015033000006
OTHER · 2015-01-30 Unresolved
ATA 7120

Part: SHEAR PIN — CORRODED (ENGINE MOUNT) · airframe 36,050 hrs · 12,948 cycles

NUMBER 1 ENG AFT MOUNT INBD UPPER INNER SHEAR PIN HAS SLIGHT PITTING ALONG FULL LENGTH OF PIN APPROX 60 DEGREES OF RADIUS. REPLACED NR 1 AFT MOUNT INBD UPPER INNER SHEAR PIN IAW AMM 71-22-11-200-804-A.

Source: SDR USAA2015020200022

2014

OTHER · 2014-12-26 Unresolved
ATA 5320

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,744 hrs · 12,843 cycles

C11 CHECK EIGHT AREAS OF CORROSION AT R1 DOOR SILL PLATE BETWEEN FRAME 16 TO 20, Z-500, -Y1584. REPLACED R1 DOOR SILL PLATE IAW SRM 51-72-11 & DWG D53110339.

Source: SDR USAA2014122900002
SMOKE/FUMES/ODORS/SPARKS · 2014-11-12 Unresolved
ATA 2530

Part: OVEN — FAULTY (GALLEY) · airframe 35,416 hrs · 12,705 cycles

LEFT OVEN SMOKES WHEN TURNED ON SMOKE QUITS WHEN OVEN IS TURNED OFF. REPLACED FWD LT OVEN IAW AMM 25-35-19.

Source: SDR USAA2014111300004
OTHER · 2014-05-23 Unresolved
ATA 3350

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 33,812 hrs · 12,067 cycles

AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY POWER SUPPLY UNIT.

Source: SDR USAA2014052700046
OTHER · 2014-03-17 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 33,171 hrs · 11,842 cycles

DOOR 2L FLOOR LEVEL EMERGENCY EXIT LIGHT MISSING LENS COVER. REPLACED EMERGENCY EXIT LIGHT LENS AT DOOR 2L.

Source: SDR USAA2014031800006

2013

OTHER · 2013-12-22 Unresolved
ATA 3350

Part: LENS — UNSECURE (CABIN) · airframe 32,382 hrs · 11,570 cycles

DOOR R2 LOWER RT EXIT PATH COVER FELL OFF. INSTALLED NEW LENS.

Source: SDR USAA2013122300014
OTHER · 2013-12-07 Unresolved
ATA 3350

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,272 hrs · 11,524 cycles

AFT LT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED AFT LT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT, BATTERY & STRAP AS REQUIRED.

Source: SDR USAA2013120900010
OTHER · 2013-11-08 Unresolved
ATA 3350

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,999 hrs · 11,414 cycles

EMERGENCY EXIT LIGHT ON WHEN SWITCH IS SELECTED TO ARM. REPLACED EMERGENCY EXIT LIGHT SWITCH IAW ESPM 20-45-21, OPS CHECKED GOOD.

Source: SDR USAA2013111100015
OTHER · 2013-10-26 Unresolved
ATA 3350

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,881 hrs · 11,372 cycles

CREW REPORTED THE CABIN LIGHTS ILLUMINATED WITH SWITCH IN THE ARMED POSITION IAW MOC, CREW RESET SYSTEM AND OPERATES NORMAL.

Source: SDR USAA2013102800039
OTHER · 2013-10-16 Unresolved
ATA 3350

Part: SWITCH — INTERMITTENT (EMERGENCY LIGHT) · airframe 31,776 hrs · 11,341 cycles

EMERGENCY EXIT LIGHT SWITCH IN COCKPIT IS INTERMITTENT IN ARMED POSITION, LIGHTS COME ON OCCASIONALLY. EMERGENCY LIGHTS OPS TEST GOOD IAW MM TASK 33-51-00-710-001-A.

Source: SDR USAA2013101700001
OTHER · 2013-04-23 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 29,934 hrs · 10,766 cycles

THE 2R EXIT LIGHT COVER MISSING. REPLACED EXIT LIGHT LENS AT 2R DOOR.

Source: SDR USAA2013042400004

2012

OTHER · 2012-10-24 Unresolved
ATA 2622

Part: EXTINGUISHER — UNSERVICEABLE (COCKPIT) · airframe 28,129 hrs · 10,149 cycles

FLIGHT DECK FIRE EXTINGUISHER SECURITY SEAL BROKEN. REMOVED AND REPLACED FLIGHT DECK FIRE EXTINGUISHER.

Source: SDR USAA2012102500003
OTHER · 2012-09-03 Unresolved
ATA 2560

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 27,657 hrs · 9,989 cycles

FLIGHT ATTENDANT REPORTED FORWARD MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE WITH SERVICEABLE UNIT.

Source: SDR USAA2012090400019
OTHER · 2012-06-11 Unresolved
ATA 2622

Part: FIRE BOTTLE — UNSERVICEABLE (ZONE 200) · airframe 26,727 hrs · 9,701 cycles

SEAL IS BROKEN ON AFT HALON FIRE EXTINGUISHER. REPLACED AFT HALON FIRE EXTINGUISHER BOTTLE AS REQUIRED.

Source: SDR USAA2012061200014
OTHER · 2012-06-09 Unresolved
ATA 3350

Part: CAP — MISSING (CABIN) · airframe 26,709 hrs · 9,693 cycles

ROW 9 A/C RIGHT EMERGENCY EXIT LIGHT MISSING CAP. REPLACED ROW 9 RIGHT EMERGENCY EXIT LIGHT.

Source: SDR USAA2012061100022
OTHER · 2012-05-03 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,303 hrs · 9,568 cycles

FIRST FLIGHT ATTENDANT'S FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND STRAP.

Source: SDR USAA2012050400011
OTHER · 2012-03-02 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 25,670 hrs · 9,338 cycles

SEAT 11F POSITION FLOOR LEVEL EXIT LIGHT LENS COVER MISSING. REPLACED WALL EMERGENCY LIGHT LENS COVER AT SEAT 11F. OPS CHECKED GOOD.

Source: SDR USAA2012030500008

2011

OTHER · 2011-12-12 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 24,840 hrs · 9,067 cycles

EMERGENCY LIGHT LENS COVER MISSING AT R2 DOOR. INSTALLED EMERGENCY LENS COVER.

Source: SDR USAA2011121300005
NO TEST · 2011-11-13 Unresolved
ATA 2420

Part: CONTACTOR — FAULTY (ELECTRICAL SYS) · airframe 24,583 hrs · 8,967 cycles

EMERGENCY GENERATING SYSTEM TEST FAULTED. REMOVED & REPLACED CONTACTOR 3XC IAW AIRBUS MAINTENANCE MANUAL 24-25-55.

Source: SDR USAA2011111400026
OTHER · 2011-11-04 Unresolved
ATA 3350

Part: TERMINAL — MISSING (CABIN) · airframe 24,534 hrs · 8,947 cycles

S1 CHECK - LEFT ROW NR 10 SEAT EMERGENCY LIGHTING WIRE IS MISSING TERMINAL. REPAIRED WIRING HARNESS AT LEFT ROW NR 10 SEAT IAW AIRBUS ESPM 20-43-11.

Source: SDR USAA2011110600001
OTHER · 2011-11-03 Unresolved
ATA 3397

Part: CONNECTOR — MISSING (CABIN) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - LEFT ROW NR 4 SEAT EMERGENCY LIGHT WIRE FROM DADO PANEL MISSING PLUG. INSTALLED PLUG ON LEFT ROW NR 4 SEAT EMERGENCY LIGHT WIRE FROM DADO PANEL IAW A320 AMM TASK 33-51-00-710-001.

Source: SDR USAA2011110500001
OTHER · 2011-10-27 Unresolved
ATA 3220

Part: HINGE PIN — CRACKED (NLG) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - CRACK ON NLG CENTER HINGE PIN AT NLG FR20, CENTER LINE. REPLACED NLG CENTER HINGE PIN AT NLG FR20, CENTER LINE IAW TASK CARD 26C71032007.

Source: SDR USAA2011110600005
OTHER · 2011-10-25 Unresolved
ATA 5240

Part: SHEAR PIN — BROKEN (R2 DOOR) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - R2 DOOR ASSIST BOTTLE SHEAR PIN IS BROKEN. REPLACED R2 DOOR ASSIST BOTTLE SHEAR PIN IAW A320 AMM 52-10-00-610-001.

Source: SDR USAA2011102700005
OTHER · 2011-10-25 Unresolved
ATA 5240

Part: SHEAR PIN — BROKEN (R1 DOOR) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - R1 DOOR ASSIST BOTTLE SHEAR PIN IS BROKEN. REPLACED R1 DOOR ASSIST BOTTLE SHEAR PIN IAW A320 AMM 52-10-00-610-001.

Source: SDR USAA2011102700006
OTHER · 2011-10-19 Unresolved
ATA 5315

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - CRACK ON FLOORBEAM TRACK APPROX 8 INCHES AFT FR23, -Y189. REPLACED FLOORBEAM TRACK APPROX 8 INCHES AFT FR23, -Y189 IAW A320 SRM 51-72-11 & SRM 51-42-11.

Source: SDR USAA2011102700010
OTHER · 2011-10-18 Unresolved
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 221AF BETWEEN FR14 TO FR16, -Z240, BETWEEN Y325 TO -Y18. REPLACED FLOOR PANEL 221AF IAW JOB CARD 26C22053014.

Source: SDR USAA2011102400014
OTHER · 2011-10-17 Unresolved
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66, -Z240, BETWEEN -Y765 TO -Y1704. REPLACED FLOOR PANEL 262BG IAW JOB CARD 26C26053014.

Source: SDR USAA2011102400015
OTHER · 2011-10-14 Unresolved
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 241JF BETWEEN FR42 TO FR47, -Z240 & BETWEEN Y254 TO -Y25. REPLACED FLOOR PANEL 241JF IAW JOB CARD 26C24053002.

Source: SDR USAA2011102400013
OTHER · 2011-10-14 Unresolved
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - DELAMINATED AREA ON FLOOR PANEL 241HF BETWEEN FR36 TO FR42 & BETWEEN Y1292 TO Y1732. REPLACED FLOOR PANEL 241HF. PANEL WILL BE INSTALLED ON JOB CARD 26C24053002.

Source: SDR USAA2011103100015
OTHER · 2011-10-14 Unresolved
ATA 5321

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 24,534 hrs · 8,947 cycles

1S CHECK - DELAMINATION ON FLOOR PANEL 242MF BETWEEN FR42 TO FR47 & BETWEEN -Y1292 TO -Y1732. REPLACED FLOOR PANEL 242MF IAW TASK CARD 26C24053002.

Source: SDR USAA2011102500020
FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2011-10-02 Unresolved
ATA 4990

Part: PACKING — LEAKING (APU) · airframe 24,464 hrs · 8,916 cycles

VERY STRONG DIRTY SOCK ODOR FROM CABIN AIR. MAINTENANCE FOUND OIL LEAK AT COOLING FAN. REPLACED PACKING.

Source: SDR USAA2011100400014
NO TEST · 2011-09-23 Unresolved
ATA 3350

Part: LIGHT — BROKEN (CABIN) · airframe 24,370 hrs · 8,888 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHT ROW 9R BROKEN. MAINTENANCE REPLACED LIGHT ASSEMBLY.

Source: SDR USAA2011092600029
OTHER · 2011-08-18 Unresolved
ATA 3350

Part: LIGHT — DEFECTIVE (CABIN) · airframe 24,011 hrs · 8,775 cycles

EMERGENCY EXIT LIGHT LENS COVER AT 11C IS MISSING. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AT 11C.

Source: SDR USAA2011081900003
NO TEST · 2011-05-21 Unresolved
ATA 3397

Part: CONNECTOR — LOOSE (CABIN) · airframe 23,059 hrs · 8,450 cycles

FLT 121 - ORD - EEL - SEAT 9F EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND CONNECTOR UNDER SEAT LOOSE. RECONNECTED AND OPERATIONAL CHECK GOOD.

Source: SDR USAA2011052391949
OTHER · 2011-03-23 Unresolved
ATA 3397

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 22,422 hrs · 8,218 cycles

PIT - C11/SY6 - WIRE BUNDLE FOR LEFT SEAT ROW 15 EMERGENCY ESCAPE PATH LIGHT HAS BROKEN WIRE. REPLACED WALL SEAT HARNESS. OPS CHECK GOOD PER A320 AMM 33-51-710-001-0.

Source: SDR USAA2011033091284
NO TEST · 2011-03-23 Unresolved
ATA 3350

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 22,422 hrs · 8,218 cycles

PIT - C11/SY6 - ALL 4 EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOP. REPLACED EMERGENCY POWER SUPPLY UNIT AT RIGHT OVERWING EXITS & OPS CHECK GOOD IAW A320 AMM 33-51-38-400-001.

Source: SDR USAA2011032391185
OTHER · 2011-03-12 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1160. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1160 IAW A320 SRM 51-72-11.

Source: SDR USAA2011032391189
OTHER · 2011-03-12 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A320 SRM 51-72-11.

Source: SDR USAA2011032391187
OTHER · 2011-03-12 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A320 SRM 51-72-11.

Source: SDR USAA2011032391192
OTHER · 2011-03-12 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN Y1160 TO Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN Y1160 TO Y1292 IAW A320 SRM 51-72-11.

Source: SDR USAA2011032391190
OTHER · 2011-03-12 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, -Y1292 IAW A320 SRM 51-72-11.

Source: SDR USAA2011032391188
OTHER · 2011-03-12 Unresolved
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE BETWEEN FR69 TO FR70 & BETWEEN S23R TO S24R. REPLACED SHEAR TIE BETWEEN FR69 TO FR70 & BETWEEN S23R TO S24R IAW A320 SRM 51-72-11.

Source: SDR USAA2011032491211
OTHER · 2011-03-12 Unresolved
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,291 hrs · 8,164 cycles

PIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y1292 IAW A320 SRM 51-42-11 & EA 117441.

Source: SDR USAA2011032391186
OTHER · 2011-01-05 Unresolved
ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · airframe 21,841 hrs · 7,997 cycles

PHX - WEEKLY - MAJOR REPAIR - EXFOLIATION CORROSION ON FUSELAGE SKIN AROUND LAVATORY VACUUM VENT EXHAUST AT STA 3354 BETWEEN S31R TO S32R. REPAIRED FUSELAGE SKIN AT STA 3354 BETWEEN S31R TO S32R IAW A320 SRM 53-41-11.

Source: SDR USAA2011010790118

2010

NO TEST · 2010-08-11 Unresolved
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,435 hrs · 7,468 cycles

FLT 174 LAS - EEL - EMERGENCY LIGHTS IN CABIN WILL NOT TEST. MAINTENANCE PERFORMED BITE CHECK / RESET OF CIDS SYSTEM PER AIRBUS MAINTENANCE MANUAL 23-73-00 WITH NO FAULTS NOTED. RE-TESTED EMERGENCY LIGHTS PER AIRBUS MAINTENANCE MANUAL 33-51-00, OPERATIONAL CHECK WAS GOOD.

Source: SDR USAA2010081291657
NO TEST · 2010-07-15 Unresolved
ATA 2560

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,135 hrs · 7,383 cycles

FLT 117 - PHX - EEL - AFT FLIGHT ATTENDANT (L-2) INBOARD EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY IN AFT FLIGHT ATTENDANT FLASHLIGHT.

Source: SDR USAA2010071691435
OTHER · 2010-03-23 Unresolved
ATA 3350

Part: LENS — MISSING (CABIN) · airframe 19,003 hrs · 7,009 cycles

FLT 522 - RNO - EEL - RT FORWARD EMERGENCY EXIT LOWER EMERGENCY LIGHT COVER MISSING. MAINTENANCE INSTALLED LENS COVER.

Source: SDR USAA2010032490636
SMOKE/FUMES/ODORS/SPARKS · 2010-03-08 Unresolved
ATA 2120

Part: FILTER — CONTAMINATED (CABIN) · airframe 18,848 hrs · 6,951 cycles

FLT 259 - PHL - CABIN ODOR - DURING CLIMB HAD "DIRTY SOCK" SMELL IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE O-ZONE FILTER IAW AIRBUS MAINTENANCE MANUAL 21-51-41-400-001-0.

Source: SDR USAA2010030990543

2009

NO TEST · 2009-11-28 Unresolved
ATA 3397

Part: CONNECTOR — REVERSED (EMERGENCY LIGHT) · airframe 17,931 hrs · 6,635 cycles

FLT 17 - PHX - EEL - RED EMERGENCY EXIT SEAT MOUNTED LIGHT AISLE SIDE ROW 11R WILL NOT ILLUMINATE. MAINTENANCE FOUND WIRE CONNECTORS REVERSED - RECONNECTED. OPERATIONAL CHECK WAS GOOD.

Source: SDR USAA2009113093239
OTHER · 2009-06-11 Unresolved
ATA 3350

Part: LIGHT — MISSING (CABIN)

FLT 173 - PHX - EEL - EMERGENCY EXIT ASSEMBLY MISSING SEAT 11D. MAINTENANCE REINSTALLED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 11D.

Source: SDR USAA2009061291463
NO TEST · 2009-01-01 Unresolved
ATA 2560

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 14,602 hrs · 5,516 cycles

FLL - EMERGENCY EQUIPMENT- FLIGHT 531 - NR 8368843, AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT.

Source: SDR USAA2009010290004

2008

WARNING INDICATION · 2008-02-23 Unresolved
ATA 2424

Part: GCU — ODOR (NR 1) · airframe 11,483 hrs · 4,395 cycles

FLT NR 335 - AT CRUISE FLT 340, GOT ELEC NR 1 IDG LO PSI. COMPLIED WITH ECAM ACTIONS. CREW DISCONNECTED GENERATOR & ALSO MENTIONED AN ELECTRICAL ODOR IN COCKPIT. MX CONTROL SUGGESTED CREW TURN OFF NR 1 BLEED & USE APU AS A SECOND BLEED SOURCE. CREW REPORTED FUMES CLEARED, BUT RETURNED 15 MINUTES LATER. ACFT DIVERTED TO STL. NO EMERGENCY DECLARED. MX R & R NR 1 GCU AND NR1 IDG.

Source: SDR USAA920080508
OTHER · 2008-01-29 Unresolved
ATA 5280

Part: HINGE FITTING — CRACKED (NLG DOOR) · airframe 11,316 hrs · 4,339 cycles

SAL - MAJOR REPAIR - BC2 CHECK - NR 6038208, NOSE LANDING GEAR RIGHT DOOR CENTER HINGE FITTING CRACKED. REPLACED THE NOSE LANDING GEAR RIGHT DOOR CENTER HINGE FITTING IAW A320 SRM 51-72-11.

Source: SDR USAA920080343

2006

OTHER · 2006-04-04 Unresolved
ATA 2133

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 3,993 hrs · 1,538 cycles

LAS - CREW REPORTED THAT DURING DESCENT INTO LAS AT APPROX 5,000' THE OUTFLOW VALVE INDICATED FULL OPEN, AMBER, AND THE A/C DEPRESSURIZED. AFTER LANDING CREW REPORTED THAT THE OUTFLOW VALVE INDICATES NORMAL, GREEN. MAINTENANCE REMOVED AND REPLACED THE OUTFLOW VALVE IAW AMERICA WEST AIRLINES T/C R2D21301. ALSO, REMOVED AND REPLACED THE NR 1 AND NR 2 CABIN PRESS CONTROLLERS IAW AIRBUS 320 AMM 21-31-34-401 AND AWA TASK CARD F1B21304.

Source: SDR AWXA200600632
WARNING INDICATION · 2006-01-18 Unresolved
ATA 3231

Part: SAFETY VALVE — MALFUNCTIONED (MLG) · airframe 3,201 hrs · 1,233 cycles

AFTER TAKEOFF CREW REPORTED THAT AFTER GEAR RETRACTION ALL 3 DOORS REMAINED OPEN, HAD THREE GREENS AND THREE REDS. CYCLED GEAR TWICE THEN HAD 3 GREENS BUT GEAR DOORS WERE OPEN. CREW RETURNED TO LAX AND LANDED WITH NO NLG STEERING. MX R & R BOTH LGCIU'S, LANDING GEAR CONTROL LEVER 6GA AND HYDRAULIC CONTROL RELAY 48GA. AIRCRAFT FERRIED TO PHX FOR FURTHER MX. R & R SAFETY VALVE 2630GM AND SELECTOR VALVE MANIFOLD, 2524GM. FOUND BLOCK "A" CONNECTOR ON LGCIU 2 BROKEN. REPLACED BLOCK "A" CONNECTOR ON LGCIU 2 ALONG WITH ALL PINS AND SOCKETS FROM LGCIU 1 AND 2 TO 40GA. PASSED FCF FOR GEAR DOOR DISCREPANCY BUT FAULTED LGCIU 2 AND REVERSER 2. LGCIU 2 WAS REPLACED AND PASSED FCF.

Source: SDR AWXA200600124
WARNING INDICATION · 2006-01-11 Unresolved
ATA 3230

Part: SAFETY VALVE — MALFUNCTIONED (MLG) · airframe 3,137 hrs · 1,204 cycles

CREW REPORTED ALL GEAR WOULD NOT RETRACT. CREW RETURNED TO PHX AND LANDED WITHOUT INCIDENT. CREW TAXIED OFF OF ACTIVE THEN WERE TOWED TO THE GATE. MX R & R LANDING GEAR SAFETY VALVE, 49GA IAW AIRBUS 320 MM 32-31-17-400-001. LEAK CHECK & OPS CHKS GOOD.

Source: SDR AWXA200600051

2005

WARNING INDICATION · 2005-11-30 Unresolved
ATA 3230

Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 2,686 hrs · 1,027 cycles

PHX - AIR TURN BACK - FLT 0081 - DURING CLIMB-OUT OF PHX, CREW REPORTED THAT LANDING GEAR WOULD NOT RETRACT. CREW RETURNED AND LANDED IN PHX WITHOUT FURTHER EVENT. MX CYCLED GEAR NUMEROUS TIMES AND WERE UNABLE TO DUPLICATE DISCREPANCY. PERFORMED MLG HYDRAULIC SAFETY VALVE TEST IAW AMERICA WEST AIRLINES TASK CARD A8M32301, NO FAULTS WERE NOTED. REMOVED AND REPLACED 40GA, LANDING GEAR SELECTOR VALVE, AND 41GA, LANDING GEAR DOOR SELECTOR VALVE, IAW AIRBUS 320 AMM 32-31-12 AND 34. REPLACED FOR PRECAUTIONARY PURPOSES. LEAK CHECKS OF VALVES GOOD. OPERATIONAL TESTS WERE GOOD.

Source: SDR AWXA200501474