N948AS
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.
189 reports on file, 1995-01-03 – 2007-07-25.
Part: WEB — CRACKED · airframe 54,585 hrs · 29,230 cycles
WEB IS CRACKED AT FASTENER HOLE. INSTALLED REPLACEMENT FRAME SECTION AND REPAIR DOUBLERS PER SRM 53 01.
Part: SKIN — DENTED (BS 229-240) · airframe 54,585 hrs · 29,230 cycles
FUSELAGE SKIN DENTED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-04.
Part: SKIN — DENTED (BS 478-528) · airframe 54,585 hrs · 29,230 cycles
FUSELAGE SKIN DENTED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-04.
Part: SKIN — DENTED (BS 579-599) · airframe 54,585 hrs · 29,230 cycles
FUSELAGE SKIN DENTED. REPAIR PER SRM 53-04.
Part: CUSP WEB — CRACKED · airframe 54,585 hrs · 29,230 cycles
CUSP WEB CRACKED. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,585 hrs · 29,230 cycles
CANT REPAIR BRACKET BROKEN. REPLACED EXISTING REPAIR BRACKET PER SRM 51-30-5.
Part: SKIN — BULGED (BS 1231-1250) · airframe 51,585 hrs · 29,230 cycles
FUSELAGE SKIN BULGED. RECONTOURED SKIN AND INSTALLED INTERIOR DOUBLER PER SRM 53-04.
Part: SKIN — BULGED (BS 1190-1210) · airframe 54,585 hrs · 29,230 cycles
FUSELAGE SKIN HAS BULGES. REPLACED PREVIOUSLY INSTALLED EXTERNAL DOUBLER PER ASA EA 5330 02221.
Part: FRAME — CRACKED (FUSLEAGE) · airframe 54,585 hrs · 29,230 cycles
CANT REPAIR (WEB STIFFENER) CRACKED AS FASTENER HOLES. REPLACED WEB STIFFENER PER SRM 51-30-5.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,585 hrs · 29,230 cycles
FRAME ON FRONT LEFTHAND SIDE OF CANT CRACKED AT RADIUS. REPAIRED FRAME PER SRM 51-30-5.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 54,585 hrs · 29,230 cycles
LEFTHAND WING INBOARD FLAP T/E IS DELAMINATED. BONDED DOUBLER IN PLACE PER SRM 51 03.
Part: SKIN — DAMAGED (BS 460-470) · airframe 54,585 hrs · 29,230 cycles
FUSELAGE SKIN CREASED OVER SHEAR TIE. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 53-04.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,585 hrs · 29,230 cycles
RADIO ALTIMETER ANTENNA CUTOUT FLANGE ON FUSELAGE IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-04, 51-30-02 AND 51-30-05.
Part: VANE — DENTED (TE FLAP) · airframe 54,585 hrs · 29,230 cycles
LEFTHAND INBOARD FLAP OUTBOARD VANE HAS DENTS ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR SKIN AND DOUBLER PER SRM 51-70-2.
Part: FLOOR PANEL — CORRODED · airframe 54,585 hrs · 29,230 cycles
CABIN FLOORBOARD CORRODED AT FASTENER HOLES. REPLACED FLOOR PANEL PER SRM 41-30 AND MM 53-20-01.
Part: SKIN — CORRODED (BS 607) · corrosion level 2 · airframe 54,585 hrs · 29,230 cycles
RADIO ALTIMETER ANTENNA CUTOUT AT FLANGE IS CORRODED. REMOVED DAMAGED PIECE. INSTALLED DOUBLER PER SRM 53-04, 51-30-02 AND 51-30-05.
Part: TAB — CRACKED (RUDDER) · airframe 54,585 hrs · 29,230 cycles
RUDDER TAB COATING (FLAME SPRAY) IS CRACKED. BONDED ASTROSTRIKE AL28 AND GLASS CLOTH TO RUDDER PER SRM 51-70.
Part: VANE — DENTED (TE FLAP) · airframe 54,585 hrs · 29,230 cycles
LEFTHAND INBOARD FLAP INBOARD VANE HAS DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA. INSTALLED REPAIR SKIN AND DOUBLER PER SRM 51-70-6.
Part: FLOOR PANEL — BROKEN · airframe 54,585 hrs · 29,230 cycles
CABIN FLOOR PANEL HAS BROKEN END. PREPARED DAMAGED AREA. RE-BONDED PER MM 25-00-00.
Part: SKIN — DENTED (CARGO DOOR) · airframe 54,585 hrs · 29,230 cycles
MID CARGO DOOR SKIN IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FAIRING AND DOUBLER PER SRM 52-05.
Part: FLOOR PANEL — DELAMINATED · airframe 54,585 hrs · 29,230 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05 DAC DWG 9936585 AND DAC DWG S4932106.
Part: MEMBRANE — CRACKED · airframe 54,585 hrs · 29,230 cycles
FORWARD WET AREA MEMBRANE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53-01.
Part: MEMBRANE — CORRODED · corrosion level 2 · airframe 54,585 hrs · 29,230 cycles
FORWARD WEB AREA MEMBRANE IS CORRODED ON UPPER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53-01.
Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,585 hrs · 29,230 cycles
FORWARD WET AREA MEMBRANE IS CORRODED ON UPPER SURFACE. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-01.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 54,585 hrs · 29,230 cycles
CABIN FLOOR PANEL HAS HOLES IN PANEL. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED FLOOR PANEL IAW SRM 53-05 AND DWG 9936585.
Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 54,585 hrs · 29,230 cycles
FLOORBOARD CORRODED AT STA 256 X 22 TO X 44. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05 DWG S4932106.
Earlier reports · 1995–2006 · 163 reports
2006
Part: GLOWSTRIP — MISINSTALLED (CABIN) · airframe 52,126 hrs · 28,060 cycles
PHOTOLUMINESCENT STRIP AT THE RIGHT OVERWING EXIT IS NOT INSTALLED PROPERLY AND COULD INHIBIT EVAC PROCEDURES.
Part: GLOWSTRIP — BROKEN (CABIN) · airframe 52,096 hrs · 28,046 cycles
BREAK IN PHOTOLUMINESCENT STRIP AT RIGHT OVERWING EXIT. CORRECTED BREAK PER EO 3351 01035 AND DWG 335101351 REV B.
Part: FRAME — CHAFED · airframe 50,390 hrs · 27,210 cycles
FOUND FRAME CHAFED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 53 01 FIG. 2.
Part: SKIN — PUNCTURED (LT FLAP VANE) · airframe 50,390 hrs · 27,210 cycles
FOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE IS PUNCTURED ON LOWER SURFACE. REMOVED DAMAGED SECTION. INSTALLED FILLER CORE SKIN FILLER AND REPAIR DOUBLER PER SRM 51 70 2 AND 51 57 03 FIG 9A.
Part: FRAME — CRACKED (FUSELAGE) · airframe 50,390 hrs · 27,210 cycles
FOUND FRAME CRACKED AT FASTENER HOLE. REMOVED DAMAGED SECTION OF FRAME. INSTALLED REPAIR SECTION TWO SPLICE PLATES AND TWO REPAIR ANGLES PER SRM 53 03 FIG 2A.
Part: FITTING — CORRODED (FUSELAGE) · airframe 50,390 hrs · 27,210 cycles
FOUND LONGERON 30 AFT FITTING CORRODED. REPLACED DAMAGED SPLICE FITTING PER SRM 51 10 4 51 30 5 AND 51 30 1.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 50,390 hrs · 27,210 cycles
FOUND RADIO ALTIMETER ANTENNA DOUBLER CORRODED. REPLACED DAMAGED DOUBLER PER SRM 51 10 4 AND 51 30 5.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 50,390 hrs · 27,210 cycles
FOUND RADIO ALTIMETER ANTENNA DOUBLER CORRODED. REPLACED ANTENNA DOUBLER PER SRM 51 10 4 AND 51 30 5.
Part: LONGERON — CORRODED (FUSELAGE)
FOUND LONGERON 30 CORRODED BEYOND LIMITS. BLENDED CORRODED AREA AND INSTALLED REPAIR U CHANNEL PER SRM 53 02.
2005
Part: SKIN — DENTED
LINE CHECK, FUSELAGE DENTED AFT OF L-1 (FWD PAX) DOOR. REMOVED DAMAGED SECTION SECTION. INSTALLED EXTERNAL DOUBLER WITH BLIND RIVETS IAW EA. (K)
Part: SKIN — DAMAGED
SEA LINE CHK, FUSELAGE DAMAGED BY LIGHTNING STRIKE ON LT SIDE. REPAIRED IAW SRM AND EA.(K)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, FOUND PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DEBONDED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS SOFT, DISBONDING SPOT. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
OKC - DURING PAX CABIN FLOOR PANEL HAS TWO CRACKED RIBS. INSTALLED REPAIR HAT CHANNEL AND SPLICE. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS TWO CRACKED RIBS ON BOTTOM SIDE. REMOVED DAMAGED. INSTALLED REPAIR HAT SECTIONS AND SPLICES. (M)
Part: FLOOR PANEL — PUNCTURED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS PUNCTURED AT TWO LOCATIONS. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — PUNCTURED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M)
Part: SKIN — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED AND PITTED ON INSIDE JUST ABOVE LONGERON 3L. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER, DOUBLER, AND FINER DOUBLER. (M)
Part: FLOOR PANEL — PUNCTURED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS PUNCTURED. CORE PLUG REPAIRED. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. REPLACED FLOOR PANEL. (M)
Part: CUSP WEB — CRACKED (FUSELAGE)
OKC - DURING C-CHECK, LONGERON CUSP WEB CRACKED IN MID CARGO BAY. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)
Part: BEAM — CORRODED (CARGO DOOR)
OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR BEAM IS CORRODED. REPLACED BEAM. (M)
Part: WEB — CRACKED (FUSLEAGE)
OKC - FOUND DURING C-CHECK, L1 DOOR CUTOUT INNER WEB IS CRACKED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: RIB — CRACKED (LT WING)
OKC - DURING C-CHECK, LT WING FIXED LEADING EDGE RIB LOWER L-ANGLE IS CRACKED. REPLACED ANGLE. (M)
Part: FLOOR PANEL — BROKEN (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED FLOOR PANEL. (M)
Part: STRINGER SPLICE — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND LONGERON STRINGER SPLICE CORRODED. REPLACED SPLICE. (M)
Part: CUSP WEB — CORRODED (FUSELAGE)
OKC - FOUND DURING C-CHECK, LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M)
Part: WEB — CRACKED (FUSELAGE)
OKC - DURING C-CHECK, LONGERON CUSP WEB CRACKED IN FORWARD CARGO BAY. REPLACED CUSP WEB. (M)
Part: RIB — CRACKED (WING LE)
OKC - DURING C-CHECK, WING LEADING EDGE RIB CRACKED, FROM WS XDS449 TO XDS499. REPLACED RIB. (M)
Part: CUSP WEB — CORRODED (FUSLEAGE)
OKC - DURING C-CHECK, FOUND LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGED. INSTALLED FILLER AND REPAIR DOUBLER. (M)
Part: RIB — CRACKED (RT WING)
OKC - DURING C-CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED. REPLACED DAMAGE. INSTALLED REPAIR ANGLE, SHIM, RADIUS, AND FILLER. (M)
Part: SPLICE — CORRODED (LONGERON)
OKC - DURING C-CHECK, FOUND LONGERON STRINGER SPLICE CORRODED. REPLACED SPLICE. (M)
Part: CUSP WEB — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M)
Part: STRINGER SPLICE — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND LONGERON STRINGER SPLICE CORRODED. REPLACED SPLICE. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. FIBERGLASS BOND REPAIRED. (M)
Part: WEB — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, LONGERON CUSP WEB CORRODED IN MID CARGO BAY. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: SKIN — GOUGED (TE FLAP)
OKC - FOUND DURING C-CHECK, LEFT WING OUTBOARD FLAP VANE HAS GOUGED ON OUTBOARD EDGE. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS ELONGATED HOLE. INSTALLED REPAIR FILLER AND DOUBLER HAT SECTION AND SPLICE. (M)
Part: FLOOR PANEL — DENTED (FUSELAGE)
OKC - C-CHECK, PAX CABIN FLOOR PANEL DENTED, GOUGED, AND DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — BROKEN (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS CORRODED AND BROKEN INSERTS. REPLACED FLOOR PANEL. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS CRACKED, PUNCTURED, CRUSHED, AND DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: SKIN — GOUGED (LT WING)
OKC - DURING C-CHECK, FOUND LEFT WING OUTBOARD FLAP VANE LEADING EDGE IS GOUGED. REMOVED DAMAEGD AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
OKC - FOUND DURING C-CHECK, PAX CABIN FLOOR PANEL IS CRACKED, PUNCTURED, AND DELAMINATED. REPLACED FLOOR PANEL. (M)
Part: SKIN — CRACKED (FUSELAGE)
OKC - FOUND C-CHECK, FOUND L1 DOOR CUTOUT INNER WEB IS CRACKED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - C-CHECK, PAX CABIN FLOOR PANEL HAS PULLED STRANDS OF FIBERGLASS. REPLACED FLOOR PANEL. (M)
Part: WEB — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND LONGERON STRAP (WEB) CORRODED IN AFT CARGO BAY. REMOVED DAMAGE. TREATED/PRIMED PER EA 5310-02444. (M)
2004
Part: LANYARD — DISCONNECTED (L1 DOOR SLIDE)
SEA - PREFLIGHT CHECK, FORWARD PASSENGER L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)
Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)
OAK - DURING PREFLIGHT CHECK, FOUND LAST TWO EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SPACER — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, MID CARGO BAY DOOR BEAM SPACER IS CORRODED AT FASTENER HOLES. REPLACED DAMAGED SPACERS. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M)
Part: FLOORBOARD — DAMAGED (CABIN)
OKC - DURING C-CHECK, CABIN FLOORBOARD HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FUSELAGE SKIN DENTED. RECONTOURED SKIN WITH REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED SKIN WITH REPAIR DOUBLER. (M)
Part: FLOOR PANEL — DAMAGED (CABIN)
OKC - DURING C-CHECK, CABIN FLOORBOARD PANEL HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M)
2003
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 23. RECONNECTED MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SKIN — SCRATCHED (FUSELAGE)
OAK 15K CHECK, FOUND FUSELAGE SKIN HAS THREE SCRATCHES AT 22 INCHES AFT OF L1 DOOR LOWER CORNER. PERFORMED CLASS 1 PERMANENT REPAIR PER SRM 53-04. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND AFT CARGO BAY TIE DOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK EPR SRM 51-30-1. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
OAK 15 CHECK, FOUND AFT CARGO BAY CARGO TRACK IS CORRODED AROUND CLIP NUT HOLES AT FS 1231. REPLACED CARGO TRACK PER SRM 50-31-1. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD END AT FS 237. REPLACED DAMAGED SECTION WITH SPLICE REPAIR PER SRM 53-02. (M)
Part: LONGERON — CORRODED (FUSLEAGE)
OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD AT FS 1041-1060. REPLACED LONGERON SPLICE PER SRM 51-10-3. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD AT FS 1193. REPLACED LONGERON SPLICE PER SRM 51-10-3. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND INTERCOSTAL CORRODED IN AFT CARGO BAY AT FS 1309-1322. REPLACED INTERCOSTAL PER SRM 51-30-5. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND LONGERON L30 CORRODED AT FORWARD END AT FS 1060. REPLACED LONGERON SPLICE PER EA 5310-01717. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND SEAT TRACK IS CORRODED AT FS 1136-1174. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 51-30-5. (M)
Part: SPLICE — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND LONGERON SPLICE CORRODED AT FS 1193-1212. REPLACED LONGERON SPLICE PER SRM 51-10-4 AND 51-30-5. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OAK - DURING 15K CHECK, FLOOR PANEL IS CORRODED AT FS 1155-1174. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-3. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OAK - FOUND DURING 15K CHECK, SEAT TRACK IS CORRODED AT FS 200-220. REMOVED DAMAGED AREA AND SPLICED IN NEW TRACK PER SRM 53-05. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND FLOOR PANEL, MEMBRANE, IS CORRODED AT FS 522. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-10-3. (M)
Part: FITTING — CORRODED (FUSELAGE)
OAK - FOUND 15K CHECK, FRAME TO CUSP FITTING IS CORRODED AT FS 1174. REPLACED FITTING PER SRM 51-10-4 AND 51-30-1. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OAK 15K CHECK, FOUND SEAT TRACK CORRODED AT FS 200-240. REMOVED DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-05. (M)
Part: PANEL — PUNCTURED (LT WING SLAT)
OAK - FOUND 15K CHECK, LEFT WING SLAT NR 1 INBOARD LOWER PANEL IN PUNCTURED. REPLACED SLAT PANEL. (M)
Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)
SEA PREFLIGHT CHECK, FOUND ONE EMERGENCY FLOOR TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED WIRING. LIGHT THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (R1 DOOR SLIDE)
ON PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
PREFLIGHT CHECK, FOUND FIRST FIVE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
PREFLIGHT CHECK, FOUND ONE WHITE EMERGENCY FLOOR TRACK LIGHT INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (ROW 26)
PDX LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FOUND INOPERATIVE AT ROW 26. REPLACED ASSOCIATED BATTERIES. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (ROWS 29 & 30)
SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FOUND INOPERATIVE BETWEEN ROWS 29 AND 33. REPLACED BATTERIES IN AFT RT POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
YVR PREFLIGHT CHECK, FOUND FIRST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
SEA PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 15 FORWARD. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT)
SAN - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS REMAINED ON WITH POWER SWITCH OFF. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)
SEA LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS REMAIN ON IN AFT AND TAIL AREA WITH SWITCH OFF. REPLACED ASSOCIATED POWER SUPPLY. LIGHT THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)
2002
Part: LIGHT — INOPERATIVE (CABIN)
DURING LINE CHECK FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 21-23. REPLACED TWO LIGHTS MODULES. LIGHTS THEN OPERATED PROPERLY.
Part: MODULE — DISCONNECTED (CABIN)
DURING PREFLIGHT CHECK FOUND FIRST TWO EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED MODULE. LIGHTS THEN OPERATED PROPERLY.
Part: BATTERY PACK — DISCHARGED (A/C BAY)
SEA - DURING LINE CHECK, FOUND TAIL CONE AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — DISCHARGED (CABIN)
PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE NEAR AFT LAVATORIES. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
OAK - DURING LINE MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS SECTION. RECONNECTED WIRING TO LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS SECTION. RECONNECTED WIRING TO LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (EVAC SLIDE)
BUR - DURING PREFLIGHT CHECK, THE L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)
Part: CONNECTOR — LOOSE (CABIN)
YVR - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN 1ST CLASS CABIN WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — BROKEN (CABIN)
SEA - DURING LINE CHECK, DISCOVERED EMERGENCY LIGHTING TO BE INOPERATIVE AT ROW 1-3. SPLICED BROKEN WIRE AT SEAT FD3. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - DURING PREFLIGHT CHECK, DISCOVERED 'PART OF EMERGENCY TRACK LIGHTING INOPERATIVE'. REPLACED WIRING AT ROW 1. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — LOOSE (CABIN)
SEA - DURING LINE CHECK, 1ST CLASS EMERGENCY TRACK LIGHTING ROWS 1-4 WERE FOUND TO BE INOPERATIVE. SECURED FIRST CLASS TRACK LIGHTING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — LOOSE (CABIN)
SEA - DURING PREFLIGHT CHECK, FORWARD 1ST CLASS EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. SECURED FIRST CLASS TRACK LIGHTING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: HARNESS — FAILED (PAX DOOR)
OAK - DURING C-CHECK, FOUND TAIL DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED OK. (M)
2001
Part: MODULE — INOPERATIVE (CABIN)
SEA - DURING PRE-FLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED LIGHT MODULE AND RECONNECTED. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED MODULE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE IN 1ST CLASS. RECONNECTED MODULE. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LIGHT — NOT SEATED (CABIN)
SEA - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE AT ROW 1. RESEATED BULB IN SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — DISCONNECTED (CABIN)
SFO - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS FROM ROW 1 TO 3 INOPERATIVE. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED NORMALLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN AT ROW 3. REPLACED SECTION OF TRACK LIGHT WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (ENTRY DOOR)
SEA - DURING PREFLIGHT CHECK, FOUND GIRT BAR LANYARD DETACHED FROM EMERGENCY SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER PER MM 25-62-00. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING PRE-FLIGHT, FOUND SEVEN (3 RED AND 4 WHITE) EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN OVERWING EXIT AREA. REPLACED TRACK LIGHTING LAMPS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (EMERGENCY SLIDE)
ANC - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M)
Part: LANYARD — DISCONNECTED (EVAC SLIDE)
LAX - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGNECY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD BETWEEN GIRT BAR AND SLIDE COVER. (M)
Part: WINDOW — BROKEN (COCKPIT)
LAX - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW LEAKAGE WAS DETERMINED TO BE BROKEN. REINSTALLED HINGE PIN. WINDOW THEN OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
PDX - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT THE AFT GALLEY AND CENTER AISLE WERE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING SERVICE CHECK, OVERHEAD EMERGENCY LIGHTS AT ROWS 21-31 WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACKS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, FIRST FOUR EMERGENCY TRACK LIGHTS IN 1ST CLASS WERE DETERMINED TO BE INOPERATIVE. RECONNECTED TRACK LIGHT WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — DISCONNECTED (CABIN)
PDX - DURING PREFLIGHT CHECK, SECTION OF EMERGENCY FLOOR TRACK LIGHTING IN 1ST CLASS WAS DETERMINED TO BE INOPERATIVE. RECONNECTED LIGHTING SECTION. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (TAILCONE)
PHX - DURING LINE CHECK, TAILCONE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. BURNISHED CONNECTION TO RESTORE ELECTRICAL GROUND. LIGHT THEN OPERATED PROPERLY. (M)
2000
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 13 AND 17 WAS DETERMINED TO BE INOPERATIVE. REPLACED WIRING SPLICE. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LATCH — STUCK (PAX DOOR)
SEA-PRIOR TO FLIGHT 608 THE L-1 DOOR HOLD OPEN LATCH WAS FOUND TO BE STUCK. REPLACED HOOK RELEASE CRANK AND DOOR OPERATED NORMALLY.
Part: BALLAST — BURNED (CABIN)
SMF - DURING FLIGHT 328, THE FLIGHT ATTENDANT REPORTED THE SMELL, AND VISABILITY OF SMOKE IN THE FIRST CLASS CABIN. SMOKE WAS VISABLE FOR APPROXIMATELY 2 MINUTES, THEN DISAPATED. THE AIRCRAFT LANDED IN SMF WITHOUT INCIDENT. SMF MX INSPECTED THE AIRCRAFT AND COULD NOT FIND SOURCE OF SMOKE. THE AIRCRAFT WAS RELEASED FOR FERRY FLIGHT FROM SMF TO AOK FOR FURTHER INSPECTION. OAK MAINTENANCE INSPECTED AND FOUND THAT THE LIGHT BALLAST ABOVE SEAT 1DF HAD CONTACTED AN ADEL CLAMP CREATING AN ARC. REPLACED BALLAST AND REROUTED WRING/ADEL CLAMP, SYSTEM OPERATED NORMALLY. AIRCRAFT RELEASED FOR SERVICE. (M)
Part: HOOK — DEFECTIVE (PAX DOOR)
SEA: CREW REPORTED THE L1 DOOR WAS DIFFICULT TO RELEASE FROM THE LOCKED OPEN POSITION. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATED NORMALLY.
Part: LIGHT — BROKEN (CATWALK)
SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY EXIT LIGHT ASSEMBLIES OVER THE CATWALK WERE FOUND BROKEN. REPLACED LIGHT ASSEMBLIES AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 29 WERE FOUND INOPERATIVE. REPLACED LAMP MODULES AT ROW 29 AND 30 AND OPERATED NORMALLY. (M)
1999
Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)
PDX - DURING MAINTENANCE CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)
Part: SKIN — CORRODED (BS 1126)
OAK - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE SKIN AT ANTENNA MOUNT HOLE AT FS 1126 BETWEEN LONGERON 30 AND LONGERON 29L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW ASA EA 5330-01406. (M)
Part: MOUNT — CORRODED (TE FLAP)
OAK - DURING 30K CHECK, FOUND CORROSION ON RIGHT OUTBOARD FLAP MID HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. REPAIRED IAW ASA EA 2750-01080. (M)
Part: MOUNT — CORRODED (TE FLAP)
OAK - DURING 30K CHECK, FOUND CORROSION ON LEFT OUTBOARD FLAP INBOARD HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. REPAIRED IAW ASA EA 2750-01080. (M)
Part: LONGERON — CORRODED (BS 1006-1022)
OAK - DURING 30K CHECK, FOUND EXFOLIATION ON LONGERON 30 FROM FS 1006 TO 1022. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION IAW ASA EA 5310-01717. (M)
Part: MOUNT — CORRODED (TE FLAP)
OAK - DURING 30K CHECK, FOUND CORROSION ON RIGHT OUTBOARD FLAP INBOARD HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES.. REPAIRED IAW ASA EA 2750-01080. (M)
Part: MOUNT — CORRODED (TE FLAP)
OAK - DURING 30K CHECK, FOUND CORROSION ON LEFT OUTBOARD FLAP MID HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. REPAIRED IAW ASA EA 2750-01080. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERABLE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)
Part: CONNECTOR — LOOSE (CABIN)
PDX - PRIOR TO DEPARTURE OF FLIGHT 102, CREW REPORTED THE FORWARD 2 EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. SECURED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DEFECTIVE (ROW 17)
SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY FLOOR TRACK LIGHTS AT ROW 17 WERE FOUND INOPERATIVE. REPLACED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
1998
Part: HOLD OPEN HOOK — OUT OF ADJUST (GALLEY DOOR)
SEA - DURING MAINTENANCE CEHCK, THE L2 DOOR WOULD NOT LATCH OPEN. ADJUSTED THE DOOR HOLD OPEN LATCH AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 507, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RESEATED CONNECTOR TO LIGHT ASSEMBLY AT ROW 1 AND OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - FLT 414 - PRIOR TO DEPARTURE, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS FROM SEAT 1-D FORWARD WERE INOPERATIVE. REPLACED TWO LAMP MODULES AT SEAT 1-D AND LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — FAILED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPAIRED WIRING TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
1997
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, ALL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AFT OF ROW 29 AND ALL AFT EXIT IDENTIFIER LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACKS AND ALL LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE BETWEEN ROWS 8 AND 12. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M)
Part: MODULE — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD 4 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 2 LAMP MODULES AT ROW 1 AND OPERATED NORMALLY. (M)
Part: INFLATION BOTTLE — LOW PRESSURE (L1 DOOR)
ONT - PRIOR TO DEPARTURE OF FLIGHT 383, CREW REPORTED, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)
Part: LIGHT — DEFECTIVE (CABIN)
LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LGIHT WAS FOUND INOPERATIVE. REPLACED THE ASSEMBLY AND OPERATED NORMALLY. (M)
Part: INFLATION BOTTLE — LOW PRESSURE (DOOR SLIDE)
SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M)
Part: WIRE — BROKEN (CABIN)
SJC - PRIOR TO DEPARTURE OF FLT 419 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING AT FORWARD 2 LIGHT ASSEMBLIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM 29 TO 31 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
1996
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES 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)
1995
Part: SKIN — CORRODED (BS 1164)
PAE - DURING A 15K CHECK, CORROSION WAS FOUND ON SKIN AT Y1164, X3, Z50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA E.A. 5330-01212. TAC: 8795. (X)
Part: INTERCOSTAL — CORRODED (BS 769-786.5)
PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL AT Y769 TO Y786.5, X16, Z46. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-02, SRM 53-10-03, AND SRM 53-01. (X)
Part: SHEAR TIE — CORRODED (BS 1212)
PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1212, X2 TO X7, Z50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-02, SRM 51-10-03, SRM 51-10-04, SRM 51-30-02, AND SRM 53-14-03. TAC: 8795. (X)
Part: SHEAR TIE — CORRODED (BS 1021)
PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1021, X6, Z50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-01 AND SRM 53-03. (X)
Part: INTERCOSTAL — CORRODED (BS 1309-1322)
PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL AT Y1309 TO Y1322, X17, Z42. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, SRM 51-20-00, SRM 51-30-02, SRM 53-24-00, AND SRM 53-01. TAC: 8795. (X)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLT 116, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES, AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERIES AND SIGN OPERATED NORMALLY. (M)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK,THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL — LOOSE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD NR 5200 AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 1 THROUGH 7 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE THREE OVERHEAD EMERGENCY LIGHTS FROM ROW 6 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)
Part: EEL BATTERIES — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROW 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)
Part: COALESCERS — DIRTY (AIR COND SYS)
SEA - FLT 99 - ON ARRIVAL, CREW REPORTED 'DIRTY SOCKS' ODOR IN CABIN OF 10,000 FEET DURING APPROACH. REPLACED COALESCERS AND NO ODORS WERE NOTED. COALESCERS LOOKED AND SMELLED CLEAN. (W)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19 THROUGH 22. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)