N677AW
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.
101 reports on file, 2006-11-19 – 2016-05-12.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. EMER POWER SUPPLY 10WL FAILED FUNCTIONAL TEST. REPLACED POWER SUPPLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400-001-A.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. EMER POWER SUPPLY 12WL FAILED FUNCTIONAL TEST. REPLACED POWER SUPPLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400-001-A.
Part: LENS — BROKEN (CABIN)
AIRCRAFT IS IN BASE MX. CABIN FWD LT PARTITION EMER EXIT LIGHT HAS A BROKEN LENS. R & R LENS LIGHT IAW AMM 33-51-18-400-001-A. PROCEDURE 8 STEP C.
Part: LENS — BROKEN (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. RT SIDE EMER EXIT LENS MISSING AT EXIT DOOR SIDEWALL PANEL BROKEN. REPLACED LENS IAW AMM 33-51-13-400-001-A.
Part: LENS — BROKEN (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. LT SIDE EMER EXIT LENS MISSING AT EXIT DOOR SIDEWALL PANEL BROKEN. REPLACED LENS IAW AMM 33-51-13-400-001-A.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 131 AF IN FWD CARGO COMPARTMENT, BETWEEN FRAME 24 & 28, AT -Y765 & Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 PARA 8 H FIG 209 & IRM 9701 REV G.
Part: SPRING — WORN (ZONE 800) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. PAX & CREW DOOR 831 GIRT BAR FITTING SPRING & PIN ASSEMBLY WORN. REPLACED SPRING & PIN ASSEMBLY IAW AMM 52-11-31-400-003-A.
Part: SPRING — WORN (ZONE 800) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. PAX & CREW DOOR 841 GIRT BAR FITTING SPRING & PIN ASSEMBLY WORN. REPLACED SPRING & PIN ASSEMBLY IAW AMM 52-11-31-400-003-A.
Part: SPRING — WORN (ZONE 800) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. PAX & CREW DOOR 842 GIRT BAR FITTING SPRING & PIN ASSEMBLY WORN. REPLACED SPRING & PIN ASSEMBLY IAW AMM 52-11-31-400-003-A.
Part: SPRING — WORN (ZONE 800) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. PAX & CREW DOOR 832 GIRT BAR FITTING SPRING & PIN ASSEMBLY WORN. REPLACED SPRING & PIN ASSEMBLY IAW AMM 52-11-31-400-003-A.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 251 RF IN PAX CABIN, BETWEEN FRAME 58 & 62 AT -Y254 & Y254. REPLACED FLOOR PANEL 251 RF IAW SRM 53-02-00-201 PAR 8H FIG 209 IRM 9701.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 252SF IN PAX CABIN, BETWEEN FRAME 58 & 62 AT -Y765 TO -Y254. REPLACED FLOOR PANEL 252SF IAW SRM 53-02-00-201 PAR 8H FIG 209 IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 251 LF, BETWEEN FRAME 54 & 58 AT -Y254 & Y254. REPLACED FLOOR PANEL 251 LF IAW SRM 53-02-00-201 PAR 8H FIG 209 IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 231RF IN PAX CABIN, BETWEEN FRAME 28 & 32 AT -Y254 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 PAR 8H FIG.209 & IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FWD GALLEY FLOOR PANEL 222EF, BETWEEN FRAME 13 & 20, AT -Y765 & Y254. REPLACED FLOOR PANEL IAW SRM 53-12-00-201 PAR 5F FIGURE 206 IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 231WF IN PAX CABIN, BETWEEN FRAME 32 & 35, AT Y765 & Y1292. REPLACED FLOOR PANEL 231WF IAW SRM 53-02-00-201 PAR 8H FIG 209 & IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 231KF IN PAX CABIN, BETWEEN FRAME 24 & 28 AT -Y254 & Y254. REPLACED FLOOR PANEL 231KF IAW SRM 53-02-00 PAR 8H FIG 209 IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 221EF IN FWD GALLEY AREA, BETWEEN FRAME 20 & 24 AT -Y254 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-12-00-201 PAR 5F FIGURE 206 & IRM 9701 REVISION G.
Part: FITTING — CORRODED (RT MLG DOOR) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON RT MLG DOOR FWD ATTACH POINT FITTING ON KEEL BEAM, BETWEEN FRAME 42 & 43 AT RT STRINGER 41 & 42. REPLACED FITTING IAW SRM A320 51-72-11 & DWG D53370600.
Part: ATTACH FITTING — CORRODED (LT MLG DOOR) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON LT MLG DOOR FWD ATTACH FITTING ON KEEL BEAM, BETWEEN FRAME 43 - 42, AT LT STRINGER 41 - 42. REPLACED FITTING IAW SRM 51-72-11 & DWG D53370600.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY CTR FITTING STRINGER 23, BETWEEN FRAME 66 & 68 AT Y1732. REPLACED FITTING IAW SRM 51-72-11 & DWG D53480505.
Part: HINGE PIN — CORRODED (LT SPOILER) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON LT WING NR 3 SPOILER HINGE PIN, OTBD SIDE. REPLACED HINGE PIN IAW AMM 27-64-43-400-001-A STEP 4B 3.
Part: HINGE PIN — CORRODED (LT SPOILER) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON LT WING NR 4 SPOILER HINGE PIN, BETWEEN WS 9235 & 9704. REPLACED LT WING NR 4 SPOILER HINGE PIN IAW AMM 27-64-44.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. FLOOR PANEL 261PF HAS DELAMINATION, BETWEEN FRAME 68 & 70 AT -Y1292 - Y1292. FLOOR PANEL REPLACED IAW SRM 53-02-00 PARA 8H FIG 209 & IRM 9701 REV G.
Part: HINGE PIN — CORRODED (LT SPOILER) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON LT WING NR 3 SPOILER HINGE PIN, BETWEEN WS 7792 & 8268. REPLACED LT WING NR 3 SPOILER HINGE PIN IAW AMM 27-64-43.
Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON COUPLING IN THE AFT GALLEY, BETWEEN FRAME 66 & 68 AT -Y1450. REPLACED COUPLING IAW SRM 51-42-11 & DWG D53480505.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY FLOORBEAM, BETWEEN FRAME 67+15 & 69 AT -Y1162. REPLACED FLOORBEAM IAW SRM 51-72-11 & DWG D53472780.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON RT SHEAR PLATE, BETWEEN FRAME 69 & 70 AT STRINGER 23 RT. REPLACED SHEAR PLATE IAW SRM 51-72-11, DWG D53474180 & EA 104986.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY SEAT RAIL, BETWEEN FRAME 64 & 66, AT -Y1292. SEAT RAIL REPLACED IAW SRM 51-72-11 & DWG D53472816.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON FWD GALLEY FLOORBEAM, BETWEEN FRAME 12 & 20 AT Y765. REPLACED FLOORBEAM IAW SRM 51-72-11 & DWG D53112812.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY FLOORBEAM, BETWEEN FRAME 66+5 & 70 AT Y765. REPLACED BEAM IAW SRM 51-72-11 & DWG D53472780.
Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY FLOORBEAM COUPLING, BETWEEN FRAME 64 & 66 AT -Y1292. REPLACED COUPLING IAW SRM 51-72-11 & DWG D53472816.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY DOOR SILL, BETWEEN FRAME 66 & 68 AT -Y1450. REPLACED DOOR SILL IAW SRM 51-72-11 & DWG D53480505.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON L2 DOOR CUT OUT LOWER SILL PLATE, AT FRAME 68 & STRINGER 23L. REPAIRED SILL PLATE IAW SRM 53-41-14 FIG 201 SHEET 4 REPAIR PRINCIPLE 7.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT GALLEY FLOOR BEAM, BETWEEN FRAME 66 +5 & 70, AT -Y765. REPLACED FLOORBEAM IAW SRM 51-72-11 & DWG 53472040.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 12 & 24, AT Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53110984.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. CORROSION ON AFT CARGO COMPARTMENT DOOR SILL, BETWEEN FRAME 60 & 62 AT STRINGER 38R. REPAIRED DOOR SILL IAW SRM A320 53-41-49-201 PARAGRAPH 5C FIG 203 SHEET 1.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 131G, BETWEEN FRAME 28 & 30, AT Y970.80 & Y1353. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 PAR 8H FIG 209 & IRM 9701 REV G.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,541 hrs · 14,239 cycles
AIRCRAFT IN BASE MX. DELAMINATION ON FUSELAGE FLOOR PANEL 132JF, BETWEEN FRAME 30 & 34, BETWEEN Y -765 & Y-970.8. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 PAR 8H FIG 209 IRM 9701 REV G.
Earlier reports · 2006–2015 · 62 reports
2015
Part: LIGHT — MISSING (CABIN) · airframe 39,135 hrs · 14,066 cycles
AIRCRAFT WAS GNDED. ROW 11 EMER CAP LIGHT MISSING. INSTALLED NEW EMER LIGHT ASSEMBLY AT ROW 11. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-19.
Part: LIGHT — DETACHED (CABIN) · airframe 38,792 hrs · 13,923 cycles
SEAT 1C EMER AISLE LIGHT, TORN AWAY FROM SEAT ASSEMBLY.
Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 37,793 hrs · 13,497 cycles
FLIGHT 660 EN-ROUTE, SHORTLY AFTER TAKEOFF AFT GALLEY ODOR OF BURNING ELEC COMPONENTS, THEN ALL THINGS TURNED OFF IN GALLEY, ODOR NO LONGER PRESENT. MOST NOTICEABLE IN AREA OF COFFEE MAKERS. R & R AFT GALLEY COFFEE MAKERS 1, 2 & 3 IAW AMM 25-35-15. CHECKED GOOD, NO DEFECTS NOTED.
2014
Part: SLIDE — FAULTY (R1 DOOR) · airframe 35,562 hrs · 12,647 cycles
EMERGENCY LIGHT TEST THROUGH PTP PANEL FAILS AT FWD LT LOCATION STEP 14F ON WEEKLY CHECK. FLASHING FAULT LIGHTS ON INTERIOR LIGHTS FAULT & EXTERIOR LIGHTS FAULT ON EMER POWER SUPPLY UNIT. REPLACED R1 DOOR SLIDE ASSEMBLY IAW JOB CARD 26L0025010. EMER LIGHT TEST OPERATIONS CHECKED GOOD.
Part: POWER SUPPLY — FAULTED (CABIN) · airframe 35,562 hrs · 12,647 cycles
EMERGENCY LIGHT TEST THROUGH PTP PANEL FAILS AT FWD LT LOCATION STEP 14F ON WEEKLY CHECK. FLASHING FAULT LIGHTS ON INTERIOR LIGHTS FAULT & EXTERIOR LIGHTS FAULT ON EMER POWER SUPPLY UNIT. R & R FWD LT EMER LIGHT POWER SUPPLY UNIT IAW AMM 33-51-00.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 35,446 hrs · 12,597 cycles
RON VISIT FLOOR PANEL 261LG HAS CORROSION ON INBD END SCREW HOLES & AFT OTBD EDGE. REPLACED FLOOR PANEL 261LG IAW AMM 53-32-12-400.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 35,446 hrs · 12,597 cycles
RON VISIT CORROSION ON SHEAR FRAME PLATE BETWEEN FRAME 69 TO 70, STRINGER 23L. REPLACED SHEAR FRAME PLATE BETWEEN FRAME 69 TO 70, STRINGER 23L IAW SRM 51-42-11.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,446 hrs · 12,597 cycles
RON VISIT CORROSION ON SUPPORT FRAME INTERCOSTAL BETWEEN FRAME 69 TO 70, STRINGER 23L. REPLACED SUPPORT FRAME INTERCOSTAL BETWEEN FRAME 69 TO 70, STRINGER 23L IAW SRM 51-42-11.
Part: APU — FIRE (ZONE 200) · airframe 35,367 hrs · 12,564 cycles
ON TAXI OUT HAD 3 DIFFERENT ACFT SAY WE HAD FLAMES COMING OUT APU EXHAUST. PUSHED APU FIRE SWITCH & DISCHARGED THE FIRE AGENT. FIRE FROM TAILPIPE WENT OUT. RETURNED TO GATE WITH EMER EQUIPMENT FOLLOWING. INSPECTED APU IAW AMM 49-00-00-200-001-A. INSPECTION COMPLIED WITH, NO DEFECTS NOTED.
Part: LIGHT — UNSECURE (CABIN) · airframe 35,139 hrs · 12,452 cycles
THE EMER LIGHT ON SEAT 3C CAME LOOSE. SECURED EMER LIGHT ON SEAT 3C IAW CMM 25-20-76. OPERATIONS CHECKED GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,544 hrs · 12,225 cycles
CEILING EMER LIGHTS AT ROWS 1 & 8 INOPERATIVE. REPLACED EMER POWER SUPPLY UNIT 10WL IAW AMM 33-51-38.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,337 hrs · 12,141 cycles
90WL2, 90WL1 & SEAT 4C EMER EXIT LIGHTS INOPERATIVE. REPLACED EMER POWER SUPPLY UNIT 10WL IAW AMM 33-51-38-400-001-A.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,121 hrs · 12,066 cycles
EMERGENCY LIGHTS WILL NOT TEST. REPLACED FWD EMER POWER SUPPLY UNIT. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.
Part: COVER — UNSECURE (CABIN) · airframe 33,894 hrs · 11,986 cycles
THE EMERGENCY PATH LIGHT AT ROW 4 LT IS HANGING OUT OF SEAT. R & R ROW 4 LT EMERGENCY PATH LIGHT HOUSING COVER IAW AMM 33-51-19. OPERATIONS CHECKED GOOD.
Part: STATOR VANE — MALFUNCTIONED (NR 2 ENGINE) · airframe 33,243 hrs · 11,749 cycles
ABORTED TAKEOFF FOR ENG 2 COMPRESSOR VANE FAULT AT 60KTS. RTO & RETURNED TO GATE. REPLACED ACTUATOR VARIABLE STATOR VANE IAW JOB CARDS 26P32075006 & 26P32075009.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 33,243 hrs · 11,749 cycles
ABORTED TAKEOFF, ENG NR 2 COMPRESSOR VAIN FAULT OCCURRED ON TAKEOFF. ABORTED TAKEOFF AT 80 KNOTS. ACCOMPLISHED TSM 75-30-00-810-844-A01, TSM 75-30-00-810-846A01 & VSV ACTUATOR CHANNEL A & B TEST IAW AMM 71-00-00-710-013-C HIGH POWER ASSURANCE TEST. ENG NR 2 & RELATED TESTS OK. ACFT OK FOR SERVICE.
2013
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 32,109 hrs · 11,372 cycles
CARGO FLOOR PANEL DELAMINATED BETWEEN FRAMES 56 AND 58. R & R FLOOR PANEL IAW AMM 53-42-14-400-001-A.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 32,109 hrs · 11,372 cycles
CARGO FLOOR PANEL DELAMINATED BETWEEN FRAMES 50 AND 52. R & R FLOOR PANEL IAW AMM 53-42-14-400.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 32,109 hrs · 11,372 cycles
CARGO FLOOR PANEL DELAMINATED BETWEEN FRAMES 53 AND 56. R & R FLOOR PANEL IAW AMM 53-42-14-400-001-A.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 32,109 hrs · 11,372 cycles
CARGO FLOOR PANEL 151DF DELAMINATED. R & R FLOOR PANEL IAW AMM 53-42-14.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 32,109 hrs · 11,372 cycles
CARGO FLOOR PANEL 151LF DELAMINATED. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-42-14.
Part: FILTER — DIRTY (LAVATORY) · airframe 31,953 hrs · 11,326 cycles
SMOKE ECAM APPEARED ALARM (2-3 SECONDS) THEN DISAPPEARED AFTER INSPECTION ALL APPEARED NORMAL. MAINTENANCE CLEANED FILTER IN AFT LAV, LEFT. BITE TEST GOOD.
Part: BUFFER — OUT OF ADJUST (R1 GUST LOCK) · airframe 31,298 hrs · 11,114 cycles
CABIN DOOR R1 GUST LATCH INOPERATIVE. ADJUSTED BUMPER, BUFFER FOR R1 DOOR ASSY, GUST LOCK OPERATES NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,447 hrs · 10,870 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 24C-INOPERATIVE. R & R SEAT MOUNTED EMERGENCY LIGHT ASSY AT 24C IAW MM 33-51-18.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,316 hrs · 10,833 cycles
EMERGENCY LIGHT 22E OUT. REPLACED LIGHT ASSY AT ROW 22E IAW AMM 33-51-19-400-001-A.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,242 hrs · 10,813 cycles
EMERGENCY LIGHT ON SEAT 22C-INOPERATIVE. R & R LIGHT ASSY ON SEAT 22C.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,876 hrs · 10,691 cycles
FLIGHT ATTENDANT REPORTS AFT GALLEY FORWARD FACING JUMPSEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT PER AIRBUS MAINTENANCE MANUAL 25-65-53.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,655 hrs · 10,611 cycles
EMERGENCY EXIT LIGHT ON SEAT 11C INOPERATIVE. REPLACED EMERGENCY LIGHT AT 11C, OPERATIONAL CHECK GOOD.
2012
Part: COVER — MISSING (CABIN) · airframe 28,499 hrs · 10,233 cycles
GOGO MOD - LEFT SEAT ROW 22 MISSING EMERGENCY LIGHT COVER. REPLACED EMERGENCY LIGHT ASSY AT LEFT SEAT ROW 22. OPS CHECK GOOD.
Part: LIGHT — MISSING (CABIN) · airframe 27,698 hrs · 9,959 cycles
EMERGENCY EXIT LIGHT (RED - SEAT MOUNTED) AT 11R MISSING. INSTALLED EMERGENCY EXIT LIGHT ASSEMBLY AT 11R IAW AIRBUS MAINTENANCE MANUAL 33-51-18-400-001.
Part: LENS — UNSECURE (EXIT SIGN) · airframe 27,271 hrs · 9,818 cycles
EXIT SIGN LENS COVER FELL OFF 2R DOOR. RE-ATTACHED EXIT SIGN LENS COVER AT 2R DOOR AS REQUIRED.
Part: EXTINGUISHER — UNSERVICEABLE (CABIN) · airframe 26,641 hrs · 9,625 cycles
AFT RIGHT H2O FIRE EXTINGUISHER BRACKET BROKEN. BRACKET FOUND TO BE SERVICEABLE. REPLACED H2O FIRE EXTINGUISHER DUE TO BROKEN SEAL.
Part: LIGHT — MISSING (ZONE 200) · airframe 25,894 hrs · 9,388 cycles
SEAT ROW 11 DEF MISSING EMERGENCY EXIT LIGHT. REPLACED EXIT LIGHT ASSEMBLY ON SEAT ROW 11 DEF.
2011
Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 24,994 hrs · 9,056 cycles
1S CHECK - RIGHT SIDE OFF WING ESCAPE SLIDE INFLATION RESERVOIR HAS A LOW CHARGE. REPLACED RIGHT SIDE OFF WING ESCAPE SLIDE INFLATION RESERVOIR. PERFORMED FUNCTIONAL TEST & INFLATION RESERVOIR MONITORING IAW A320 AMM 25-62-46-000-001 & 25-62-46-400-001.
Part: LENS — CRACKED (CABIN) · airframe 24,994 hrs · 9,056 cycles
1S CHECK - LEFT WING AFT EMERGENCY OVERWING LIGHT HAS CRACKED LENS. REPLACED THE LEFT WING AFT EMERGENCY OVERWING LIGHT LENS IAW A320 SRM 51-42-11.
Part: LENS — BROKEN (CABIN) · airframe 24,939 hrs · 9,038 cycles
THE 2R DOOR EMERGENCY EXIT LIGHT COVER BROKEN OFF. MAINTENANCE INSTALLED NEW EMERGENCY EXIT LIGHT COVER AT DOOR 2R.
Part: BATTERY — DISCHARGED (CABIN) · airframe 23,153 hrs · 8,427 cycles
PHX - EEL - BATTERY ON EMERGENCY POWER SUPPLY UNIT UNDER AFT LEFT OVERWING DOOR IS DEAD. MAINTENANCE REPLACED EPSU BATTERY.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR TIE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR TIE BETWEEN FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11 & TYPICAL REPAIR A320-2528-10-0011A.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-72-11, EA 117648, AIRBUS DRAWING D53472816 & D53472780.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A320 SRM 51-72-11, EA 117648 & AIRBUS DRAWING D53472780.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A320 SRM 51-72-11 & EA 117648.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816 & D53472780.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 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.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR TIE BETWEEN FR69 TO FR70, Y1732. REPLACED SHEAR TIE BETWEEN FR69 TO FR70, Y1732 IAW A320 SRM 51-72-11 & TYPICAL REPAIR A320-2528-10-0011A.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR68, Y1292. REPLACED FLOORBEAM AT FR68, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y254 IAW A320 SRM 51-72-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR17, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR17, Y1292 IAW AIRBUS DRAWING D53110920.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y1292. REPLACED FLOORBEAM AT FR16, -Y1292 IAW A320 SRM 51-72-11, 51-40-00 & 51-43-00.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,383 hrs · 8,161 cycles
PIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, -Y254 IAW A320 SRM 51-72-11.
2010
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,584 hrs · 7,868 cycles
FLT 612 - ATL - EEL - FORWARD GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY.
Part: FIRE — DETECTED (NR 2 ENGINE) · airframe 21,022 hrs · 7,648 cycles
FLT 498 - DEN - POSSIBLE FIRE / TORCHING NEAR NUMBER 2 ENGINE REPORTED BY PASSENGER. CREW REPORTED ALL ENGINE PARAMETERS WERE NORMAL. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUN WITH NO FAULTS OR LEAKS FOUND.
Part: SEAL — MALFUNCTIONED (LT ENGINE) · airframe 18,795 hrs · 6,868 cycles
FLT 495 LAS-PHX - FUMES - TOXIC SMELL OF BURNT PLASTIC COMING FROM CABIN / COCKPIT AIR CONDITIONING BLEEDS. TURNING OFF NR 1 PACK SEEMS TO CLEAR ODOR OUT. MAINTENANCE FOUND NR 1 ENGINE TO BE THE SOURCE OF THE ODOR. REMOVED AND REPLACED NR 1 ENGINE. VENDOR TEARDOWN INDICATES NR 3 CARBON SEAL WORN BEYOND LIMITS.
2009
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,540 hrs · 6,413 cycles
FLT 504 - PHX - EEL - FORWARD FLIGHT ATTENDANT'S FLASHLIGHT INOP. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,376 hrs · 6,357 cycles
FLT 504 - PHX - EEL - FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY.
Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 17,035 hrs · 6,240 cycles
FLT 302 PHX-CLT - RETURN TO FIELD / EMERGENCY LANDING - BLUE SYSTEM LOSS & LOW LEVEL WARNING. CREW DECLARED AN EMERGENCY, RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BLUE RESERVOIR DRAIN VALVE LEAKING. REPLACED DRAIN VALVE 2264GM IAW MM 29-12-35-401.
Part: PIN — BACKED OUT (CONNECTOR) · airframe 16,688 hrs · 6,130 cycles
FLT 123 - PHX - EEL - EMERGENCY LIGHT 22L WILL NOT ILLUMINATE. MAINTENANCE FOUND PIN 1 ON CONNECTOR 7680VC8 RECEDED - PUSHED PIN IN POSITION. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.
Part: WIRE — DISCONNECTED (CABIN) · airframe 16,040 hrs · 5,923 cycles
FLT 430 - LAS - EEL - ESCAPE PATH LIGHT RT AFT OVERWING EXIT INOPERATIVE. MAINTENANCE RECONNECTED WIRES AT ESCAPE PATH LIGHT RT AFT OVERWING EXIT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,733 hrs · 5,813 cycles
FLT 319 LAS - EEL - AISLE EMERGENCY LIGHT AT 22L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT 22L. OPERATIONAL CHECK GOOD.
2008
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,890 hrs · 5,168 cycles
LOGPAGE 4452017 FLT NR 143 CMH-PHX EMERGENCY EQUIPMENT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT ON AND NOT INSTALLED CORRECTLY. MX R&R THE AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY AND INSTALLED FLASHLIGHT CORRECTLY. OPS CHECK GOOD.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 13,363 hrs · 4,986 cycles
AFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT F/A FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (K)
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 11,594 hrs · 4,397 cycles
SAL - EEL - C3 CHECK - LEFT HAND AFT FLIGHT ATTENDANTS FLASHLIGHT HAS A LOW BATTERY. REMOVED AND REPLACED THE LEFT HAND AFT FLIGHT ATTENDANTS FLASHLIGHT BATTERY.
2006
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 6,248 hrs · 2,367 cycles
PHX - EEL - EMERGENCY ROW LIGHT AT SEAT 1B INOP DURING STEP 6B3 OF CARD I8M05333. MAINTENANCE REPLACED FWD CABIN POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD.