N677AW

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.

101 reports on file, 2006-11-19 – 2016-05-12.

NO TEST · 2016-05-12 Matched by certificate designator
ATA 3350

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.

Source: SDR AALA201605139015
NO TEST · 2016-05-12 Matched by certificate designator
ATA 3350

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.

Source: SDR AALA201605139014
OTHER · 2016-05-10 Matched by certificate designator
ATA 3350

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.

Source: SDR AALA201605119003
OTHER · 2016-04-10 Matched by certificate designator
ATA 3350

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.

Source: SDR AALA201604119010
OTHER · 2016-04-10 Matched by certificate designator
ATA 3350

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.

Source: SDR AALA201604119009
OTHER · 2016-03-21 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201604049004
OTHER · 2016-03-19 Matched by certificate designator
ATA 2560

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.

Source: SDR AALA201603219014
OTHER · 2016-03-19 Matched by certificate designator
ATA 2560

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.

Source: SDR AALA201603219017
OTHER · 2016-03-19 Matched by certificate designator
ATA 2560

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.

Source: SDR AALA201603219016
OTHER · 2016-03-19 Matched by certificate designator
ATA 2560

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.

Source: SDR AALA201603219015
OTHER · 2016-03-11 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249010
OTHER · 2016-03-11 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249015
OTHER · 2016-03-11 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249011
OTHER · 2016-03-10 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249017
OTHER · 2016-03-10 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249014
OTHER · 2016-03-10 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249009
OTHER · 2016-03-10 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249018
OTHER · 2016-03-10 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603249016
OTHER · 2016-03-07 Matched by certificate designator
ATA 5280

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.

Source: SDR AALA201604049002
OTHER · 2016-03-07 Matched by certificate designator
ATA 5280

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.

Source: SDR AALA201604049003
OTHER · 2016-03-04 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201603249004
OTHER · 2016-03-01 Matched by certificate designator
ATA 5755

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.

Source: SDR AALA201603239015
OTHER · 2016-03-01 Matched by certificate designator
ATA 5755

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.

Source: SDR AALA201603249005
OTHER · 2016-03-01 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603219021
OTHER · 2016-03-01 Matched by certificate designator
ATA 5755

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.

Source: SDR AALA201603249012
OTHER · 2016-02-25 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201603249002
OTHER · 2016-02-25 Matched by certificate designator
ATA 5315

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.

Source: SDR AALA201603239014
OTHER · 2016-02-25 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201605169007
OTHER · 2016-02-25 Matched by certificate designator
ATA 5347

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.

Source: SDR AALA201603249007
OTHER · 2016-02-25 Matched by certificate designator
ATA 5315

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.

Source: SDR AALA201603249003
OTHER · 2016-02-25 Matched by certificate designator
ATA 5315

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.

Source: SDR AALA201603249013
OTHER · 2016-02-25 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201603249008
OTHER · 2016-02-25 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201603249001
OTHER · 2016-02-25 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201603189009
OTHER · 2016-02-25 Matched by certificate designator
ATA 5315

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.

Source: SDR AALA201603219019
OTHER · 2016-02-25 Matched by certificate designator
ATA 5347

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.

Source: SDR AALA201603179012
OTHER · 2016-02-23 Matched by certificate designator
ATA 5320

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.

Source: SDR AALA201603249006
OTHER · 2016-02-21 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603219020
OTHER · 2016-02-21 Matched by certificate designator
ATA 5321

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.

Source: SDR AALA201603219018
Earlier reports · 2006–2015 · 62 reports

2015

OTHER · 2015-12-30 Matched by certificate designator
ATA 3350

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.

Source: SDR AALA201512319003
OTHER · 2015-11-14 Matched by certificate designator
ATA 3350

Part: LIGHT — DETACHED (CABIN) · airframe 38,792 hrs · 13,923 cycles

SEAT 1C EMER AISLE LIGHT, TORN AWAY FROM SEAT ASSEMBLY.

Source: SDR AALA201511159007
SMOKE/FUMES/ODORS/SPARKS · 2015-07-22 Matched by certificate designator
ATA 2530

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.

Source: SDR AALA201507249002

2014

OTHER · 2014-11-19 Unresolved
ATA 2565

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.

Source: SDR USAA2014112000006
OTHER · 2014-11-19 Unresolved
ATA 3350

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.

Source: SDR USAA2014112000003
OTHER · 2014-11-01 Unresolved
ATA 5321

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.

Source: SDR USAA2014110300020
OTHER · 2014-10-31 Unresolved
ATA 5320

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.

Source: SDR USAA2014110300011
OTHER · 2014-10-31 Unresolved
ATA 5320

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.

Source: SDR USAA2014110300019
FLAME/FIRE · 2014-10-20 Unresolved
ATA 4920

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.

Source: SDR USAA2014102100005
OTHER · 2014-09-25 Unresolved
ATA 3350

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.

Source: SDR USAA2014092600006
NO TEST · 2014-07-22 Unresolved
ATA 3350

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.

Source: SDR USAA2014072300004
NO TEST · 2014-06-30 Unresolved
ATA 3350

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.

Source: SDR USAA2014070100009
NO TEST · 2014-06-09 Unresolved
ATA 3350

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.

Source: SDR USAA2014061000002
OTHER · 2014-05-14 Unresolved
ATA 3350

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.

Source: SDR USAA2014051500021
OTHER · 2014-03-10 Unresolved
ATA 7530

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.

Source: SDR USAA2014031100003
FALSE WARNING · 2014-03-08 Unresolved
ATA 7700

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.

Source: SDR USAA2014031000030

2013

OTHER · 2013-11-10 Unresolved
ATA 5321

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.

Source: SDR USAA2013111100032
OTHER · 2013-11-10 Unresolved
ATA 5321

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.

Source: SDR USAA2013111100030
OTHER · 2013-11-10 Unresolved
ATA 5321

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.

Source: SDR USAA2013111100031
OTHER · 2013-11-10 Unresolved
ATA 5321

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.

Source: SDR USAA2013111200006
OTHER · 2013-11-10 Unresolved
ATA 5321

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.

Source: SDR USAA2013111200007
WARNING INDICATION · 2013-10-25 Unresolved
ATA 2120

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.

Source: SDR USAA2013102800020
OTHER · 2013-08-20 Unresolved
ATA 5210

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.

Source: SDR USAA2013082100005
OTHER · 2013-06-13 Unresolved
ATA 3350

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.

Source: SDR USAA2013061400004
OTHER · 2013-06-03 Unresolved
ATA 3350

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.

Source: SDR USAA2013060400004
OTHER · 2013-05-28 Unresolved
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,242 hrs · 10,813 cycles

EMERGENCY LIGHT ON SEAT 22C-INOPERATIVE. R & R LIGHT ASSY ON SEAT 22C.

Source: SDR USAA2013052900008
OTHER · 2013-04-21 Unresolved
ATA 2560

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.

Source: SDR USAA2013042300014
OTHER · 2013-03-28 Unresolved
ATA 3350

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.

Source: SDR USAA2013032900026

2012

OTHER · 2012-12-12 Unresolved
ATA 3350

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.

Source: SDR USAA2012121700016
OTHER · 2012-09-16 Unresolved
ATA 3350

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.

Source: SDR USAA2012091700009
OTHER · 2012-08-05 Unresolved
ATA 3350

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.

Source: SDR USAA2012080600057
OTHER · 2012-06-10 Unresolved
ATA 2622

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.

Source: SDR USAA2012061100029
OTHER · 2012-04-04 Unresolved
ATA 3350

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.

Source: SDR USAA2012040500005

2011

OTHER · 2011-12-27 Unresolved
ATA 2565

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.

Source: SDR USAA2011122800003
OTHER · 2011-12-20 Unresolved
ATA 3350

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.

Source: SDR USAA2011122300022
OTHER · 2011-12-02 Unresolved
ATA 3350

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.

Source: SDR USAA2011120600023
NO TEST · 2011-06-09 Unresolved
ATA 3350

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.

Source: SDR USAA2011061000017
OTHER · 2011-04-09 Unresolved
ATA 5322

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.

Source: SDR USAA2011041991527
OTHER · 2011-04-09 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991533
OTHER · 2011-04-09 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991532
OTHER · 2011-04-09 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991535
OTHER · 2011-04-09 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991536
OTHER · 2011-04-09 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991534
OTHER · 2011-04-09 Unresolved
ATA 5322

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.

Source: SDR USAA2011041991526
OTHER · 2011-04-09 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991537
OTHER · 2011-04-08 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991528
OTHER · 2011-04-08 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991530
OTHER · 2011-04-08 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991529
OTHER · 2011-04-08 Unresolved
ATA 5315

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.

Source: SDR USAA2011041991531

2010

NO TEST · 2010-12-28 Unresolved
ATA 2560

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.

Source: SDR USAA2010122893256
FLAME/FIRE · 2010-10-25 Unresolved
ATA 7200

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.

Source: SDR USAA2010102692408
SMOKE/FUMES/ODORS/SPARKS · 2010-03-17 Unresolved
ATA 7200

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.

Source: SDR USAA2010031890607

2009

OTHER · 2009-10-26 Unresolved
ATA 2560

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.

Source: SDR USAA2009102792881
OTHER · 2009-10-07 Unresolved
ATA 2560

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.

Source: SDR USAA2009100892736
WARNING INDICATION · 2009-08-31 Unresolved
ATA 2930

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.

Source: SDR USAA2009090192303
NO TEST · 2009-07-30 Unresolved
ATA 3397

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.

Source: SDR USAA2009073091948
NO TEST · 2009-06-01 Unresolved
ATA 3397

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.

Source: SDR USAA2009060291375
NO TEST · 2009-05-04 Unresolved
ATA 3350

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.

Source: SDR USAA2009050591083

2008

NO TEST · 2008-11-07 Unresolved
ATA 2560

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.

Source: SDR USAA920082017
NO TEST · 2008-09-12 Unresolved
ATA 2560

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)

Source: SDR USAA920081679
NO TEST · 2008-04-02 Unresolved
ATA 2560

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.

Source: SDR USAA920080761

2006

NO TEST · 2006-11-19 Unresolved
ATA 3350

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.

Source: SDR AWXA200601951