N977AS
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.
103 reports on file, 1995-11-24 – 2007-11-18.
Part: SKIN — DENTED (TE FLAP VANE) · airframe 42,705 hrs · 21,774 cycles
RIGHT FLAP I/B SIDE I/B FLAP VANE MULTIPLE DENTS ON LWR. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER, PREPARED AREA BOND AREA AND FASTENER IAW MD80 SRM 51-70-2 PG 11, 23, 43, 45, 59 AND 63.
Part: FRAME — CRACKED (BS 1418 S2L/R) · airframe 42,705 hrs · 21,774 cycles
AFT ACCESSORY COMPT FRAME STA 1418 CRACKED IN RADIUS AT LONG 2R AND LONG 2L. TWO EACH CRACKS PREPARED DAMAGED AREA, STOP DRILLED CRACKS, VERIFIED CRACK TERMINATION IAW MD80 SRM 51-01 PG 9. RECEIVED REPLACEMENT REPAIR PARTS LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 53-03 FIG 31A.
Part: SKIN — DENTED (TE FLAP VANE) · airframe 42,705 hrs · 21,774 cycles
RIGHT WING I/B FLAP O/B VANE MULTIPLE DENTS ON LWR I/B SURFACE. PREPARED DAMAGED AREA IAW MD 80 SRM 51-70-2 PG 11. FABRICATED DOUBLER AND BONDED IAW MD 80 SRM 51-70-2 PGS 23 AND 91.
Part: VANE — DENTED (TE FLAP) · airframe 42,705 hrs · 21,774 cycles
RIGHT I/B FLAP I/B VANE DENTED AT TOP SURFACE IN MIDDLE SECTION OF VANE. REMOVED DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER PREPARED AREA BAND AREA AND FASTENERS IAW MD80 SRM 51-70-2 PGS 11, 23, 43, 45, 59 AND 63.
Part: SKIN — GOUGED (TE FLAP VANE) · airframe 42,705 hrs · 21,774 cycles
RIGHT WING O/B FLAP I/B VANE PREVIOUS REPAIR GOUGED. REMOVED DAMAGED DOUBLER. FABRICATED, LOCATED, DRILLED AND BONDED REPAIR DOUBLER AND FILLER IAW MD80 SRM 51-70-2 PAR 18B AND 57-03 FIG 11 PG 27.
Part: SKIN — DAMAGED (TE FLAP VANE) · airframe 42,705 hrs · 21,774 cycles
LEFT WING O/B FLAP I/B VANE REPAIR DOUBLER GOUGED. REMOVED DAMAGED REPAIR DOUBLER, FABRICATED, LOCATED, DRILLED AND BONDED IAW MD80 SRM 51-70-2 PAR 18B PG 91 AND MD80 SRM 57-03 FIG 11 PG 27.
Part: LONGERON — CRACKED (BS 1418 L2L) · airframe 42,705 hrs · 21,774 cycles
AFT ACCESSORY COMPT LONGERON 2L CRACKED AT AFT SIDE OF FRAME 1418. REMOVED DAMAGED SECTION OF LONGERON LOCATED DRILLED AND INSTALLED REPAIR EXTRUSION AND REPAIR SPLICE IAW MD80 SRM 53-02 FIG 18.
Part: LONGERON — CRACKED (BS 1418 L2R) · airframe 42,705 hrs · 21,774 cycles
AFT ACCESSORY COMPT LONGERON 2R CRACKED AT AFT SIDE OF FRAME STA 1418. REMOVED DAMAGED SECTION OF LONGERON, LOCATED, DRILLED AND INSTALLED REPAIR EXTRUSION AND REPAIR SPLICE IAW MD80 SRM 53-02 FIG 18.
Part: SHEAR TIE — CRACKED (BS 1437) · airframe 42,705 hrs · 21,774 cycles
AFT ACCESSORY COMPT SHEAR TIE CRACKED AT AFT SIDE OF FRAME STA 1437 I/B OF LONGERON 3R. REMOVED DAMAGED SHEAR TIE RECEIVED A REPLACEMENT SHEAR TIE, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 PG 1 AND FIG 3A SHEET 1 AND 51-30-5 PG 12, 13.
Part: SHEAR TIE — CRACKED (BS 1437) · airframe 42,705 hrs · 21,774 cycles
AFT ACCESSORY COMPT SHEAR TIE CRACKED AT AFT SIDE OF FRAME STA 1437 I/B OF LONGERON 3L. REMOVED DAMAGED SHEAR TIE RECEIVED A REPLACEMENT SHEAR TIE LOCATED DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 PG 1 AND FIG 3A SHEET 1 AND 51-30-5 PG 12 AND 13.
Part: FLOOR PANEL — DELAMINATED (BS 826-927) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL PUNCTURED DENTED APPROX IN MIDDLE OF PANEL STA 826 TO STA 927 LBL 44 TO LBL 54. REMOVED DAMAGED AREA, FABRICATED LOCATED DRILLED AND INSTALLED A REPAIR DOUBLER IAW MD80 SRM 53 01 FIG 4 SHEET 4.
Part: FLOOR PANEL — DELAMINATED (BS 866-887) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED AT STA 866 TO STA 887 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
Part: FLOOR PANEL — DELAMINATED (BS 826-866) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED STA 826 TO STA 866 RBL 22 TP RBL 44. FABRICATED A REPLACEMENT PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
Part: FLOOR PANEL — DELAMINATED (BS 826-866) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED STA 826 TO STA 866 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
Part: SKIN — DENTED (LT AILERON) · airframe 42,705 hrs · 21,774 cycles
LEFT AILERON IS DENTED APPROX 2 INCHES FORWARD OF TRIM TAB O/B HINGE LOWER SURFACE. PREPARED DAMAGED AREA IAW MD80 SRM 51-90-0 PG 9, APPLIED LAYER OF MIL C 9084 FIBERGLASS BONDED REPAIR IAW MD80 SRM 51-90-0 PG 44.
Part: FLOOR PANEL — DELAMINATED (BS 887-927) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED STA 887 TO STA 927 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
Part: FLOOR PANEL — DELAMINATED (BS 927-1003) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOORBOARD CRACKED OUT CORNER AND DELAMINATED STA 927 TO STA 1003 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWINGS S4932106.
Part: FLOOR PANEL — DELAMINATED (BS 826-928) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL HAT STIFFENER CREASED ON AFT SIDE AND PANEL HAS 1 INCH CRACK IN CENTER AREA STA 826 TO STA 928 RBL 44 TO RBL 54. REMOVED DAMAGED HAT CHANNEL, INSTALLED A REPLACEMENT CHANNEL IAW MD80 SRM 51-10-4 PG 1 & 51-30-2 PG 1. REPAIRED CRACK IAW MD80 SRM 53-01 PG 12 FIG 2.
Part: FLOOR PANEL — DELAMINATED (BS 927-1003) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED STA 927 TO STA 1003 LBL 22 TO LBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD 80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
Part: FLOOR PANEL — DELAMINATED (BS 769-807) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED STA 769 TO STA 807 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWINGS S4932106.
Part: FLOOR PANEL — DELAMINATED (BS 887-927) · airframe 42,705 hrs · 21,774 cycles
CABIN FLOOR PANEL DELAMINATED STA 887 TO STA 927 RBL 22 TO RBL 44. FABRICATED A REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05 PAGES 251 THRU 257 AND DAC DRAWING S4932106.
Part: SKIN — DENTED (FUSELAGE) · airframe 42,705 hrs · 21,774 cycles
RIGHT EXTERNAL FUSELAGE SKIN DENTED 27 INCHES BELOW PYLON STA 1308 DENT MEASURES .700 DIA DEPTH .032 RATIO OF 21.8 COLD WORKED DENT IAW MD80 SRM 53-04 FIG 38. EDDY CURRENT INSPECTED COLD WORKED AREA NO CRACKS NOTED IAW MD80 NTSPM 06 10 00.001 PROCEDURE 1. FABRICATED INTERNAL DOUBLER COATED DRILLED AND INSTALLED IAW MD80 SRM FIG 38. 53-04.
Part: CSD — OVERTEMP (LT ENGINE) · airframe 40,328 hrs · 20,640 cycles
LEFTHAND ENGINE CSD TEMPERATURE IN RED DURING CLIMB FROM ANC. SHUTDOWN CSD AND DIVERTED TO FAI. REPLACED CSD.
Earlier reports · 1995–2006 · 80 reports
2006
Part: SLIDE — FAILED (L2 DOOR) · airframe 39,471 hrs · 20,237 cycles
DURING CATERING, THE L 2 DOOR SLIDE PACK FELL OUT OF SLIDE CASE AND WOULD NOT DEPLOY. FOR MORE INFO NEED TO NOTIFY INFLT SERVICE FOR DETAILS. CLARIFICATION OF CIRCUMSTANCES SURROUNDING THIS INCIDENT HAS BEEN REQUESTED FROM LINE MAINTENANCE AND IT IS INTENDED TO INCLUDE THAT CLARIFICATION IN THE SUBSEQUENT CLOSED SUPPLEMENT. REPLACED L 2 DOOR EMERGENCY SLIDE. SUBSEQUENT INVESTIGATION REVEALED THAT DEPLOYMENT ATTEMPT WAS CONDUCTED WITH SLIDE OUT OF AIRCRAFT ON CATERING TRUCK PLATFORM. SO EVENT IS NOT CONSIDERED REPORTABLE UNDER FAR 121.703 GUIDELINE.
Part: FLOOR PANEL — DELAMINATED (BS 160-200) · airframe 38,829 hrs · 19,939 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: FLOOR PANEL — DAMAGED (BS 160-200) · airframe 38,829 hrs · 19,939 cycles
FOUND CABIN FLOOR PANEL CORE DAMAGED AT INSERT HOLES. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: SKIN — DENTED (BS 1317-1318) · airframe 38,829 hrs · 19,939 cycles
FOUND FUSELAGE SKIN DENTED. COLD FORMED TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
Part: SKIN — DENTED (BS 229-266) · airframe 38,829 hrs · 19,939 cycles
FOUND FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION PER SRM 53 04.
Part: SKIN — GOUGED (BS 1058 S18-19L) · airframe 38,829 hrs · 19,939 cycles
FOUND FUSELAGE SKIN GOUGED. REMOVED DAMAGED SECTION. INSTALLED FILLER EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER PER SRM 53 04.
Part: FLOOR PANEL — DAMAGED (BS 196-256) · airframe 38,829 hrs · 19,939 cycles
CABIN FLOOR PANEL DAMAGED AT INSERT HOLES. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: FLOOR PANEL — DAMAGED (BS 200-256) · airframe 38,829 hrs · 19,939 cycles
CABIN FLOOR PANEL CORE DAMAGED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: SKIN — CORRODED (BS 1123-1132) · airframe 38,829 hrs · 19,939 cycles
FOUND FUSELAGE SKIN CORRODED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER INTERNAL FINGER DOUBLER AND AN EXTERNAL REPAIR DOUBLER PER ASA EA 5330 02129.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 38,829 hrs · 19,939 cycles
FOUND FORWARD ENTRY DOOR HAS CRACKED INTERCOSTAL BEHIND HANDLE MECHANISM. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.
Part: SKIN — GOUGED (FLAP VANE) · airframe 38,829 hrs · 19,939 cycles
FOUND RIGHT WING OUTBOARD FLAP INBOARD VANE IS GOUGED. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER SRM 51 70 2.
Part: FLOOR PANEL — DELAMINATED (BS 140-160) · airframe 38,829 hrs · 19,939 cycles
FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: FLOOR PANEL — DAMAGED (BS 160-200) · airframe 38,829 hrs · 19,939 cycles
FOUND CABIN FLOOR PANEL CORE DAMAGED AT INSERTS. REPLACED PANEL PER SRM 53 05.
Part: FLOOR PANEL — DELAMINATED (BS 180-200) · airframe 38,829 hrs · 19,939 cycles
CABIN FLOOR PANEL DELAMINATED AND HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: SKIN — GOUGED (FLAP VANE) · airframe 38,829 hrs · 199,939 cycles
FOUND LEFT WING OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR. REMOVED DAMAGED EXISTING REPAIR DOUBLER AND FILLER. INSTALLED REPLACEMENT DOUBLER AND FILLER PER SRM 51 70 2.
Part: FLOOR PANEL — DELAMINATED (BS 140-160) · airframe 38,829 hrs · 19,939 cycles
FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53 05 AND DWG S4932106.
Part: SKIN — DENTED (FLAP VANE) · airframe 38,829 hrs · 19,939 cycles
FOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE DENTED. REMOVED DAMAGED VANE SKIN. INSTALLED SKIN FILLER AND EXTERNAL REPAIR DOUBLER PER SRM 57 03 AND 51 70 2.
Part: BEAM — CORRODED (BS 1117-1250) · corrosion level 2 · airframe 38,829 hrs · 19,939 cycles
AFT CARGO BAY DOOR CUTOUT LOWER BEAM CORRODED. REPLACED BEAM PER SRM 51 10 4 51 30 2 AND 51 30 5.
Part: SKIN — DENTED (BS 1266-1267) · airframe 38,829 hrs · 19,939 cycles
FOUND FUSELAGE SKIN DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
Part: SKIN — DENTED (BS 217-218) · airframe 38,829 hrs · 19,939 cycles
FOUND FUSELAGE SKIN DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04.
Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 1 · airframe 38,829 hrs · 19,939 cycles
AFT CARGO BAY INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51 10 4 51 30 2 AND 51 30 5.
2005
Part: SUPPORT — CRACKED (FS 38-41)
OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL RIGHT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP. (M)
Part: SKIN — DENTED (FS 676)
OKC - DURING C-CHECK, FOUND MID CARGO BAY DOOR SKIN IS DENTED. COLD FORMED SKIN. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FS 1171-1196)
OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED ONE EXTERNAL DOUBLER, TWO INTERNAL DOUBLERS, AND THREE FILLERS. (M)
Part: VANE — CHAFED (TE FLAP)
OKC - FOUND LEFT WING OUTBOARD FLAP INBOARD VANE EXTERNAL DOUBLER IS CHAFED. REMOVED DOUBLER. INSTALLED REPLACEMENT DOUBLER. INSTALLED REPLACEMENT DOUBLER. (M)
Part: SKIN — DENTED (FS 285)
OKC - FOUND DURING C-CHECK, FUSELAGE DENTED. REMOVED DAMAGED AREA. INSTALLED INTERNAL AND EXTERNAL DOUBLERS. (M)
Part: SUPPORT — CRACKED (MLG WW)
OKC - DURING C-CHECK, FOUND NOSE LANDING GEAR WHEELWELL LEFT SUPPORT FRAME UPPER FASTENER CRACKED. STOP DRILLED CRACK. INSTALLED REPAIR ANGLE, SHIM, AND CLIP
Part: SKIN — DENTED (FS 643)
OKC - DURING C-CHECK, FOUND MID CARGO BAY DOOR SKIN IS DENTED. COLD-FORMED SKIN. INSTALLED REPAIR DOUBLER. (M)
Part: LANYARD — DISCONNECTED (L1 DOOR SLIDE)
SEA - PREFLIGHT CHECK, FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
2004
Part: BEAM — CORRODED (FUSELAGE)
OKC - FOUND DURNG C-CHECK, AFT CARGO BAY DOOR JAMB FORWARD BEAM IS CORRODED ON THE INBOARD SLIDE AROUND NUMEROUS RIVETS AT FS 1155 TO 1211. REMOVED DAMAGE AND SPOT FACED AROUND FIVE FASTENERS PER EA 5310-02379. (M)
Part: VANE — GOUGED (TE FLAP)
OKC - DURING C-CHECK, FOUND LEFT WING OUTBOARD T/E FLAP VANE IS GOUGED ON INBOARD L/E. REMOVED DAMAGE. ADDED DOUBLER AND FILLER PER SRM 51-70-2. (M)
Part: VANE — PUNCTURED (TE FLAP)
FOUND DURING C-CHECK, RIGHT OUTBOARD FLAP T/E INBOARD FOREFLAP IS PUNCTURED ON L/E. REMOVED DAMAGED EDGES. ADDED DOUBLER AND FILLER PER SRM 53-03. (M)
Part: COVER — CRACKED (ELEVATOR)
OKC - DURING C-CHECK,FOUND LEFT ELEVATOR INBOARD FAIRING COVER UPPER OUTBOARD FASTENER HOLE IS CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 5520-01193. (M)
Part: INTERCOSTAL — BENT (FUSELAGE)
OKC - DRING C-CHECK, FOUND AFT CARGO BAY INTERCOSTAL IS BENT AND BUCKLED. REPLACED DAMAGED INTERCOSTAL PER SRM 51-10-2. (M)
Part: LIGHT — INOPERATIVE (PAX CABIN)
PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)
2003
Part: LIGHT — INOPERATIVE (PAX CABIN)
PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (L1 DOOR)
LAX - PREFLIGHT CHECK, FOUND FORWARD LEFT PASSENGER L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
SEA - DURING LINE CHECK, FORWARD LEFT L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD PER MM 25-62-00. (M)
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)
SEA - DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE AT ROW 9. REPLACED POEWR SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING PREFLIGHT CHECK, RED EMERGENCY TRACK LIGHTING IN FIRST CLASS WAS FOUND INOPERATIVE. REPLACED HARNESS ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)
PDX - OVERHEAD EMERGENCY SPOT LIGHT FOUND INOPERATIVE AT ROW 8-12. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK, B5-101. LIGHT THEN OPERATED PROPERLY. (M)
2002
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, THE EMERGENCY TRACK LIGHTING AT ROWS 29-33 AND IN THE TAIL SECTION ALONG CATWALK WERE FOUND TO BE INOPERATIVE. REPLACED SHORTED TAILCONE EJECT HANDLE LIGHT ASSEMBLY AND EMERGENCY TRACK LIGHTS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LENS — BROKEN (CABIN)
PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT WHITE LENS BROKEN. REPLACED LENS, A SUB-ASSY OF THE LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE FROM ROW 2 FORWARD. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN, INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY.
Part: WIRE — DISCONNECTED (CABIN)
PHX - DURING PREFLIGHT CHECK, DETERMINED THAT THE EMERGENCY TRACK LIGHTS AT ROW 1 WERE INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS. RECONNECTED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE HARNESS — FAILED (R1 DOOR)
OAK - DURING C-CHECK, FOUND FORWARD SERVICE R1 DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED OK. (M)
2001
Part: MODULE — NOT SEATED (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHT WAS DETERMINED TO BE INOPERATIVE. RESEATED LIGHT MODULE. LIGHT THEN OPERATED PROPERLY. (M)
Part: WINDOW (COCKPIT)
SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. REPOSITIONED UPPER GUIDE PIN. WINDOW THEN OPERATED PROPERLY AND EASILY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROW 8-12 WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES WITHIN ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (GALLEY)
SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPELY. (M)
Part: BATTERY PACK — DISCHARGED (COCKPIT)
SEA - DURING PREFLIGHT, COCKPIT EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REPLACED BATTERY PACK. EXIT LIGHTS OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (COCKPIT)
LAX - DURING LINE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHTS FOUND INOPERATIVE. REINSTALLED BATTERY PACK. EXIT LIGHTS OPERATED PROPERLY. (M)
2000
Part: SLIDE — FAILED (FWD SERVICE DOOR)
DURING C5 MX CHECK, FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FAILED LIGHT TEST.REPLACED SLIDE.
Part: SLIDE — FAILED (AFT SERVICE DOOR)
OAK-DURING C5 MX CHECK, AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE FAILED LIGHT TEST.REPLACED SLIDE.
Part: LANYARD — LOOSE (PAX DOOR SLIDE)
OAK DURING MAINTENANCE CHECK FOUND R1 DOOR EMERGENCY SLIDE LANYARD LATCH PIN, P/N 3961896, LOOSE (COULD BE PUSHED OUT BY HAND). LANYARD ASSEMBLY HAD BEEN PREVIOUSLY MODIFIED PER AD 2000-8-18 AMDT 39-11704. REPLACED ENTIRE LANYARD ASSEMBLY.
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE ARMED LIGHT IN THE L1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M)
Part: WIRE — BROKEN (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 584 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
ONT - PRIOR TO DEPARTURE OF FLIGHT 405, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED LOOSE WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
1999
Part: CONNECTOR — DISCONNECTED (CABIN)
PHX - PRIOR TO DEPARTURE OF FLIGHT 721, CREW REPORTED THE FORWARD 2 EMERGENCY FLOOR TRACK RED LIGHTS WERE INOPERATIVE. SECURED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND RELAMPED AND OPERATED NORMALLY. (X)
Part: CONNECTOR — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. SECURED CONNECTORS TO LIGHT SOCKETS IN FLOOR TRACK AND OPERATED NORMALLY. (X)
Part: POWER SUPPLY — FAILED (ROWS 18-22)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 18 TO 22 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — FAILED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
OAK - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
1998
Part: SLIDE — MALFUNCTIONED (PAX DOOR)
OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)
1997
Part: BAYONET — STUCK (L2 DOOR)
SEA - BEFORE DEPARTURE OF FLIGHT 325, CREW REPORTED THE L2 DOOR WOULD NOT CLOSE. FOUND BAYONET GUIDE ASSEMBLY STUCK IN CLOSED POSITION, CLEANED ROLLER TRACK AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: SWITCH — MALFUNCTION (FLIGHT COMPT)
SEA - AFTER ARRIVAL OF FLT 577, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT. ACCOMPLISHED OPERATIONAL CHECK OF EMERGENCY FLOOR TRACK LIGHTING SYSTEM, UNABLE TO DUPLICATE DISCREPANCY. PRECAUTIONARY REPLACED THE EMERGENCY LIGHTS CONTROL SWITCH S1-177 ON THE OVERHEAD PANEL IN THE FLIGHT COMPARTMENT AND OPERATED NORMALLY. (X)
Part: LIGHT — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSSEMBLY AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CATWALK)
SEA - DURING MAINTENANCE CHECK, NR 1 OVERHEAD EMERGENCY LIGHT IN THE AFT CATWALK AREA WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
1996
Part: HOOK — BENT (L1 DOOR)
PSP - PRIOR TO DEPARTURE OF FLT 481, CREW REPORTED THE L1 DOOR WOULD NOT LATCH IN OPEN POSITION. FOUND THE HOLD OPEN HOOK BENT. STRAIGHTENED AND INSPECTED THE HOOK AND DOOR OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: GUST LOCK MECH — MALFUNCTIONED (L1 DOOR)
SEA - AFTER ARRIVAL OF FLT NR 233 - CREW REPORTED THE L1 DOOR EXTERNAL LATCH WOULD NOT RELEASE. LUBRICATED GUS LOCK MECHANISM AND OPERATED NORMALLY. (M)
1995
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 30 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X)
Part: HANDLE — LACK OF LUBE (L1 DOOR)
LAX - FLT 257 - ON ARRIVAL, CREW REPORTED THE L1 DOOR HANDLE RELEASE STICKS. LUBRICATED HANDLE ASSEMBLY AND OPERATED NORMALLY. (X)