N943AS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ALASKA AIR INC (JSFA) | Operator | on 2007-12-25 | Operator named in NTSB report |
Accident & incident history
Operated by Alaska Airlines, Inc. (per NTSB report)
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.
205 reports on file, 1995-06-16 – 2007-12-15.
Part: HANDLE — OBSTRUCTED (PAX DOOR) · airframe 55,530 hrs · 29,814 cycles
CANNOT OPEN MAIN PAX (L10) DOOR FROM INSIDE, HAD TO OPEN FROM OUTSIDE. REMOVED EXCESS PAINT ON OUTSIDE OF DOOR WHICH PREVENTED OUTSIDE HANDLE FROM MOVING TO OPEN POSITION WHEN ATTEMPTING OPENING FROM INSIDE. INSIDE HANDLE THEN OPENED DOOR PROPERLY.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,542 hrs · 29,304 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND SRM 53-20-01.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,542 hrs · 29,304 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05 AND 53-20-01.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,542 hrs · 29,304 cycles
CABIN FLOOR PANEL DELAMINATED (TOP FIBER LAYER PULLED LOOSE). APPLIED GLASS FABRIC LAYER PER MM 25-00-00 PP 804-805.
Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 54,542 hrs · 29,304 cycles
CABIN FLOOR PANEL IS PUNCTURED. REPAIRED WITH BONDED DOUBLER PER SRM 51-70-02.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,542 hrs · 29,304 cycles
CABIN FLOOR PANEL DELAMINATED (TOP FIBER LAYER PULLED LOOSE). APPLIED GLASS FABRIC LAYER PER MM 25-00-00 PP 804-805.
Part: SKIN — DENTED (T/E FLAP VANE) · airframe 54,542 hrs · 29,304 cycles
LEFTHAND WING OUTBOARD FLAP OUTBOARD VANE IS DENTED ON INBOARD LEADING EDGE. REPAIRED CLUSTER OF DENTS PER SRM 51-60-0, 51-70-2 AND 57-50-14.
Part: SKIN — GOUGED (FUSELAGE) · airframe 54,542 hrs · 29,304 cycles
FUSELAGE SKIN GOUGED AT PREVIOUS BLEND. REMOVED DAMAGED AREA. INSTALLED REPAIR PARTS PER SRM 53-04.
Part: SKIN — DENTED (FUSELAGE) · airframe 54,542 hrs · 29,304 cycles
FUSELAGE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED SKIN FINGER DOUBLERS AND STRAPS PER SRM 53-04.
Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 54,542 hrs · 29,304 cycles
AFT CARGO BAY DOOR FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,542 hrs · 29,304 cycles
CUSP WEB CORRODED. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 51-70-4.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,542 hrs · 29,304 cycles
SEAT TRACK CORRODED. REMOVED DAMAGED SECTION OF TRACK. INSTALLED REPAIR PLUG PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 54,542 hrs · 29,304 cycles
FLOOR PANEL IS DELAMINATED. REPLACED PANEL PER SRM 53-05.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,542 hrs · 29,304 cycles
G3 GALLEY FORWARD INBOARD SEAT TRACK MOUNTING IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED PLUG REPAIR PER SRM 53-05.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,542 hrs · 29,304 cycles
CABIN RIGHTHAND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-70-4.
Earlier reports · 1995–2006 · 190 reports
2006
Part: VANE — GOUGED (TE FLAP) · airframe 50,419 hrs · 27,363 cycles
LEFT WING OUTBOARD FLAP INBOARD VANE IS GOUGED ON LEADING EDGE. REMOVED DAMAGED AREA. INSTALLED A SKIN FILLER AND INTERNAL DOUBLER PER SRM 51 70 2.
Part: LONGERON — CORRODED (BS 1165-1200) · airframe 50,419 hrs · 27,363 cycles
FOUND LONGERON 28L CORRODED. REPLACED DAMAGED SECTION WITH REPAIR SPLICE PER SRM 53 02 FIG 18.
Part: LONGERON — CORRODED (BS 1242-1281) · airframe 50,419 hrs · 27,363 cycles
FOUND LONGERON 30 CORRODED. REPLACED DAMAGED SECTION OF LONGERON PER SRM 51 10 4 51 30 2 AND 51 30 5.
Part: LONGERON — CORRODED (BS 1250-1277) · airframe 50,419 hrs · 27,363 cycles
FOUND LONGERON 29R CORRODED. REPLACED DAMAGED SECTION BY INSTALLING NEW SECTION AND A REPAIR SPLICE PER SRM 53 02 FIG 18.
Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 50,419 hrs · 27,363 cycles
FOUND AFT CARGO BAY FRAME CORRODED. REPLACED DAMAGED SECTION WITH A REPAIR SPLICE PER SRM 53 03 FIG 2A.
Part: SKIN — DENTED (BS 515-525) · airframe 50,419 hrs · 27,363 cycles
FOUND FUSELAGE SKIN DENTED. COLD FORMED TO ORIGINAL CONTOUR AND INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53 04 FIG 38 SHT 21.
Part: STRAP — CORRODED (BS 699-701) · airframe 50,419 hrs · 27,363 cycles
FOUND MID CARGO BAY FRAME STRAP CORRODED. REPLACED STRAP PER SRM 51 10 4 AND 51 30 5.
2005
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - FOUND C-CHECK FUSELAGE SKIN DENTED. REPLACED DAMAGED SECTION. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
OKC - DURING C-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. FIBERGLASS BOND REPAIRED. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FUSELAGE SKIN DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FUSLEAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DENTED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
OKC C-CHECK- PAX CABIN FLOOR PANEL DELAMINATED. FIBERGLASS BOND REPAIRED. (NM02200500846) (K)
Part: SKIN — GOUGED (T/E FLAP) · airframe 46,531 hrs · 25,433 cycles
OKC C-CHECK - LT WING T/E FLAP SKIN GOUGED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)
Part: SPACER — CORRODED (CARGO DOOR) · airframe 46,531 hrs · 25,433 cycles
OKC C-CHECK - AFT CARGO DOOR BEAM VERTICAL SPACER CORRODED. REPLACED BEAM SPACER. (K)
Part: FLOOR PANEL — PEELING (PAX CABIN)
OKC C-CHECK - PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (K)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, FOUND PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (M)
Part: FLOOR PANEL — DAMAGED (CABIN)
OKC C-CHECK- PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (K)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 46,531 hrs · 25,433 cycles
OCK C-CHECK - PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (NM02200500846) (K)
Part: DOOR FRAME — GOUGED (FUSELAGE)
OKC C-CHECK - FWD CARGO DOOR JAMB GOUGED. REPLACED DAMAGED SECTION IAW EA. (K)
Part: FLOOR PANEL — DELAMINATED (FUSELAGE)
OKC C-CHECK, PAX CABIN FLOOR PANEL PEELED AND DELAMINATED. FIBERGLASS BOND REPAIRED. (NM02200500846) (K)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
2004
Part: LATCH — INOPERATIVE (RT WINDOW)
SEA - PREFLIGHT CHECK - RT (F/O) SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPLACED LATCH AND SPRING ASSY. WINDOW THEN OPERATED PROPERLY.
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)
DURING CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS REMAINED ILLUMINATED DURING CYCLE ON/OFF TEST. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
SEA PREFLIGHT CHECK, FOUND AFT SERVICE DOOR L2 EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
2003
Part: SEAT TRACK — GOUGED (FUSELAGE)
DRUING 15K CHECK, FOUND SEAT TRACK GOUGED. REPLACED TRACK PER SRM. (M)
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - DUIRNG 15K CHECK, FOUND CABIN FLOORBOARD IS DELAMINATED AT FS 1193-1250. REPLACED FLOORBOARD PER SRM 53-04. (M)
Part: WEB — CORRODED (FUSELAGE)
FOUND DURING 15K CHECK, CUSP WEB IS CORRODED AT FS 1237. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 53-01 AND 51-10-3. (M)
Part: LONGERON — CORRODED (FUSLEAGE)
OKC - DURING 15K CHECK, FOUND LONGERON CORRODED AT FS 1287. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 53-02 AND 51-10-1. (M)
Part: WEB — CORRODED (FUSLEAGE)
OKC - DURING 15K CHECK, FOUND CUSP WEB IS CORRODED AT FS 560-579. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 53-01 AND 51-10-3. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING 15K CHECK, FUSELAGE SKIN DENTED AT STATION 233. INSTALLED DOUBLER PER SRM 53-04, 51-10-3, AND 51-30-5. (M)
Part: WEB — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CUSP WEB IS CORRODED AT FS 505. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-10-3, 53-14-2, 53-01, 51-70-4, ET AL. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND LONGERON CORRODED AT FS 1218. REMOVED CORROSION. INSTALLED STRAP AND FILLER PER SRM 51-10-3 AND 53-02. (M)
Part: SKIN — DENTED (TE FLAP)
OKC - DURING 15K CHECK, FOUND RIGHT INBOARD FLAP LOWER SURFACE IS DENTED. INSTALLED DOUBLER PER SRM 57-01. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - FOUND SHEAR TIE CORRODED AT FS 655. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 51-10-2, 04, AND 53-03. (M)
Part: SKIN — DENTED (FUSELAGE)
DURING 15K CHECK, FOUND FUSELAGE SKIN DENTED AT STATION 182. INSTALLED DOUBLER PER SRM 53-04, 51-10-3, AND 51-30-2. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT FS 693. REPLACED SHEAR TIE PER SRM 51-10-2, 3, 4, 5. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS EDGE DAMAGE AND INSERTS MISSING AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — DEFECTIVE (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DEBONDED AT FS 160-200. REPLACED FLOORBOARD IAW SRM 53-05. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CORROSION ON BOTTOM OF LONGERON 29L UNDER FRAME AT STATINO 1231. REPAIR IAW SRM. (M)
Part: ATTACH FITTING — GOUGED (TE FLAPS)
OKC - FOUND DURING 15K CHECK, RIGHT WING FLEX JOINT OUTBOARD FLAP ATTACHMENT FITTING GOUGED ON EDGE. REPAIRED IAW EA. (M)
Part: FLOORBOARD — DEBONDED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DISBONDED AT FS 427-446. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FLOORBOARD AT STATION 927 TO 1003 HAS SCREW HOLE BLOWN OUT. REPAIR IAW SRM. (M)
Part: STRINGER — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND STRINGER CORRODED AT FS 1155-1212. REPLACED DAMAGED SECTION PER SRM 51-30-5. (M)
Part: FLOORBOARD — DEBONDED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DISBONDED AT FS 160-200. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — DEBONDED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD UPPER SURFACE IS DISBONDED AT FS 541-579. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: BEAM — CRACKED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FORWARD PAX DOOR UPPER BEAM IS CRACKED AT FORWARD AND AFT CORNERS. REPLACED BEAM IAW SRM 51-30-2. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CORROSION ON INTERCOSTAL AT LONGERON 29L FROM STATION 617-636. REPAIR IAW SRM. (M)
Part: DOUBLER — CRACKED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND LT WING LEADING EDGE SPLICE DOUBLER IS CRACKED AT STATION 120. INSTALLED SPLICE DOUBLER IAW SRM 51-30-2. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND SHEAR TIE CORRODED AT STATION 1212. REPAIR IAW SRM. (M)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
OKC - DURING 15K CHECK, FOUND EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND UPPER FUSELAGE SKIN DENTED AT FS 1437 BETWEEN 2R AND 3R. REPAIRED IAW SRM. (M)
Part: SKIN — GOUGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND AFT FUSELAGE SKIN BETWEEN STATION 1437 AND 1463 GOUGED. REPAIRED IAW SRM. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND DENT IN EXT FUSELAGE AFT OF AFT CARGO DOOR BELOW LONGERON AT 22R. REPAIR IAW SRM. (M)
Part: FLOORBOARD — CRACKED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FLOORBOARD AT STATION 541 TO 617 LBL 44 HAS TWO RIVETS PULLED THROUGH. REPAIR IAW SRM. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND DENT IN LEFT FUSELAGE SKIN AT STATION 214 JUST BELOW LONGERON AT 17. REPAIR IAW SRM. (M)
Part: ARM — GOUGED (AIRSTAIR)
OKC - DURING 15K CHECK, FOUND RIGHT ARM ON AFT AIRSTAIR IS GOUGED. REPAIRED IAW EA. (M)
Part: LONGERON — CORRODED (FUSLEAGE)
OKC - DURING 15K CHECK, FOUND CORROSION AROUND FASTENERS ON LONGERON 29L AT STATION 637. REPAIRED IAW EA. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS FASTENER HOLE BLOWN OUT AT FS 826-926. INSTALLED DOUBLER IAW SRM 53-01. (M)
Part: FLOORBOARD — DEBONDED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD IS DISBONDED AT FS 294-370. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - DURNG 15K CHECK, FOUND CORROSION ON FRAME ANGLE AT STATION 731 ABOVE LONGERON 29L. REPAIR IAW SRM. (M)
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FLOOR PANEL DELAMINATED AT FS 1193. REPAIRED IAW SRM. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS EDGE DAMAGE AT FS 256-313. REPLACED FLOORBOARD IAW SRM 53-05. (M)
Part: INTERCOSTAL — CRACKED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FORWARD PAX DOOR FRAME, INTERCOSTAL HAS .25 INCH CRACK IN RADIUS JUST AFT OF SEAL MECHANISM ADJUSTEMENT LINK. REPALCED INTERCOSTAL PER SRM 51-30-2. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CABIN FLOORBOARD HAS CORRODED INSERTS AT FS 120-160. REPLACED INSERTS IAW SRM 53-05. (M)
Part: STRINGER — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED AT FS 1136-1145. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER IAW SRM 53-02. (M)
Part: SEAT TRACK — GOUGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND RT SEAT TRACK IS GOUGED AT FS 200-275. REPLACED TRACK IAW SRM 53.05. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FRAME CORROSION. INSTALLED REPAIR ANGLE AND STRAP PER EA 5310-02279. (M)
Part: SKIN — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND SKIN CORROSION. INSTALLED REPAIR DOUBLER PER SRM. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - FOUND DURING 15K CHECK, FLOORBOARD EDGE DAMAGE. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND INTERCOSTAL CORROSION. INSTALLED NEW INTERCOSTAL PER SRM. (M)
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FLOORBOARD DELAMINATED. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M)
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FLOORBOARD DELAMINATING. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - FOUND 15K CHECK, FOUND FLOORBOARD INSERTS PULLED THROUGH. REPLACED WITH FLOORBOARD FABRICATED IAW SRM. (M)
Part: BEAM — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND CORROSION ON CARGO DOOR BEAM REPAIR DOUBLER. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR DOUBLER AND TRIPLER PER EA 5310-02278. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND STATION 1079 FRAME HAS PITTING CORROSION. INSTALLED REPAIR STRAP PER SRM. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - DURING 15K CHECK, FOUND FLOORBOARD MISSING INSERTS. FABRICATED AND INSTALLED FLOORBOARD PER SRM. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
SEA PREFLIGHT CHEC, AFT SERVICE R-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
PDX PREFLIGHT CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LIGHT — INOPERATIVE (FWD CABIN)
SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT FORWARD GALLEY. ALSO, THE TRACK COVER WAS MISSING. RECONNECTED WIRING CONNECTOR AND RESECURED COVER. LIGHTS THEN OPERATED PROPERLY. (M)
2002
Part: MODULE — INOPERATIVE (CABIN)
SEA - DURING LINE MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE AT ROW 30. REPLACED EMERGENCY TRACK LIGHT MODULE AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND DISCONNECTED AT ROW 28. RECONNECTED WIRING AT 28. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LONGERON — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 IN AFT CARGO BAY AT FS 1018. REPAIRED LONGERON PER EA 5310-02084. (M)
Part: SKIN — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON SKIN IN MID CARGO BAY AT FS 769. REPAIRED SKIN PER EA 5330-01578. (M)
Part: LONGERON — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 FASTENER HOLE AT FS 781. REPAIRED LONGERON PER EA 5310-02086. (M)
Part: LONGERON — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION AROUND LONGERON 30 FASTENERS AT FS 1029. REPAIRED PER EA 5330-01578. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL IN MID CARGO BAY AT FS 698. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 53-01 AND 51-10-04. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON CARGO BAY LEFT TIEDOWN TRACK AT FS 1007 TO 1220. REPLACED CARGO TRACK PER SRM'S 51-10-3, 51-10-3B, 51-10-4, AND 53-05. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT LONGERON 30 IN MID CARGO BAY AT FS 787. REPLACED SHEAR TIE PER SRM'S 53-01 AND 51-30-02. (M)
Part: FITTING — CRACKED (FUSELAGE)
PAE - DURING C-CHECK, FOUND MID CARGO BAY FITTING CRACKED AT FS 788. REPLACED FITTING PER SRM'S 51-30-5 AND 51-10-4. (M)
Part: SPLICE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 ON SPLICE AT FS 1292. REPLACED SPLICE PER SRM'S 51-30-2 AND 51-30-5. (M)
Part: FRAME — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY FRAME AT FS 1287. REPAIRED FRAME PER SRM 53-03. (M)
Part: FINGER DOUBLER — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON PREVIOUS INTERNAL SKIN REPAIR FINGER DOUBLER AT FS 1287. REPLACED DOUBLER PER SRM'S 51-30-05, 53-01, 53-04, AND 53-10-3. (M)
Part: FRAME — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT FS 1193. REPLACED FRAME PER SRM 51-30-02 AND 51-30-5. (M)
Part: FRAME — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BAY FRAME AT FS 1148. REPLACED FRAME PER SRM'S 51-10-2, 51-10-3, 51-10-4 AND 51-30-5. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND INTERCOSTAL UPPER FLANGE LOWER SURFACE CORRODED IN MID CARGO BAY. REPLACED INTERCOSTAL PER SRM'S 51-10-04, 51-30-02, AND 53-01. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND SHEAR TIE CORRODED AT FS 769. INSTALLED SPLICE REPAIR PER SRM 53-03 AND 51-60. (M)
Part: SKIN — DENTED (E/E BAY DOOR)
PAE - DURING C-CHECK, FOUND E/E BAY DOOR EXTERIOR SKIN DENTED AT FORWARD RIGHT CORNER. REPAIRED DOOR SKIN PER SRM 52-05, FIG 4. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M)
2001
Part: LANYARD — DISCONNECTED (SERVICE DOOR)
SFO - DURING PRE-FLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER. (M)
Part: CONNECTOR — LOOSE (CABIN)
LAX - DURING PREFLIGHT CHECK, TWO EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FORWARD CABIN. RESECURED LOOSE CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (COCKPIT)
SEA - DURING PREFLIGHT CHECK, COCKPIT OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK AT B5-23. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
SEA - DURING FLIGHT, AFT LEFT LAVATORY SMOKE DETECTOR WENT OFF ALTHOUGH NO SMOKE WAS EVIDENT. REPLACED SMOKE DETECTOR. OPS CHECKED OK. (M)
Part: LANYARD — DISCONNECTED (SERVICE DOOR)
SEA - DURING PRE-FLIGHT CHECK, R1 DOOR EMERGENCY SLIDE LANYARD ASSEMBLY LATCH WAS FOUND TO BE DETACHED FROM SLIDE COVER. REINSTALLED LATCH ON COVER. (M)
2000
Part: SIGN — BROKEN (CABIN)
SEA - DURING MAINTENANCE CHECK, FORWARD LEFT OVERWING EXIT IDENTIFIER WAS FOUND TO BE BROKEN (SMASHED). REPLACED EXIT IDENTIFIER ASSEMBLY. OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SAN - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: MODULE — BROKEN (ROW 27)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 27-30 AND AT ROWS 31-33 WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODUEL AT ROW 27 AND BATTERIES IN AFT POWER PACK. ALL LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 31 - 33)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 27-30 AND AT ROWS 31-33 WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODULE AT ROWS 27 AND BATTERIES IN AFT POWER PACK. ALL LIGHTS OPERATED NORMALLY. REF ASAA0080003, (M)
1999
Part: TIE CLIP — CORRODED (BS 1231)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, TOP OF MAIN FRAME TIE CLIP WAS FOUND CORRODED AT STATION 1231, LONGERON 27R-28R. REPAIRED PER SRM 51-31-00. (M)
Part: BRACKET — CORRODED (BS 1220)
PHX - DURING 30K CHECK, FOUND CORROSION AT STATION 1220 BETWEEN LONGERON 28R AND 27R, ON AND AROUND FASTENER COMMON TO CARGO TRACK BRACKET. REPAIRED AND REPLACED DAMAGED BRACKET PER SRM 53-01.. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE LEFT INBOARD TRACK WAS FOUND CORRODED ON THE EDGE AND INSIDE WEB OF THE TRACK AT APPROXIMATELY STATION 1041. REPAIRED AND REPLACED TRACK FROM STATION 1032 TO 1241 WITH SPLICES PER SRM 53-05, FIG 4F. (M)
Part: WEB — CORRODED (BS 478)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 478, LEFT LONGERON 18. REPAIRED AND INSTALLED DOUBLER PER SRM 53-01. (M)
Part: WEB — CORRODED (BS 1150)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1150, LONGERON 18R. REPAIRED AND INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 4. (M)
Part: WEB — CORRODED (BS 545-560)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 545-560, LEFT LONGERON 18. REPAIRED AND INSTALLED DOUBLER PER SRM 53-01. (M)
Part: FRAME — CORRODED (BS 1231)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE FRAME AT STATION 1231, LONGERON 25L ON INTERCOSTAL AT ATTACH FLANGE OF INTERCOSTAL. REPAIRED PER SRM 53-01. (M)
Part: TIE CLIP — CORRODED (BS 1117)
PHX - DURING 30K CHECK, FUOND CORROSION IN THE AFT CARGO COMPARTMENT ON TOP OF THE INTERCOSTAL TIE CLIP, STATION 1117, LONGERON 28R. REPLACED DAMAGED TIE CLIP PER SRM 51-30. (M)
Part: SHEAR TIE — CORRODED (BS 1193)
PHX - DURING 30K CHECK, FOUND CORROSION IN THE AFT CARGO COMPARTMENT AT THE MAIN FRAME SHEAR TIE CLIP, FORWARD AND AFT, STATION 1193, LONGERON 28L-29R. REPAIRED AND REPLACED DAMAGED SHEAR TIE AD CLIP PER SRM 51-30. (M)
Part: LONGERON — CORRODED (BS 598-658)
PHX - DURING 30K CHECK, FOUND CORROSION AROUND FASTENER AT THE MID CARGO BAY, LONGERON 30, FROM STATION 598 TO 658. REPLACED DAMAGED LONGERON SECTION FROM STATION 588 TO 665 AND A SPLICE AT STATION 664.5 PER EA 5310-01764. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM, WAS FOUND CORRODED AT STATION 1007-1222, BL 16L. REPLACED TRACK PER SRM 53-01 AND 53-05, FIG 4G. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE LEFT OUTBOARD TRACK WAS FOUND CORRODED AT STATION 1155. REPAIRED AND REPLACED SEAT TRACK, STATION 1030 TO 1220, LEFT OUTBOARD, PER SRM 53-05, FIG 4. (M)
Part: FLOORBEAM — CORRODED (BS 1338)
PHX - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON TOP SURFACE OF FLOOR STRUCTURE, STATION 1338 RIGHT AT RBL 41 AND RBL 49. REPAIRED FLOORBEAM PER AMS EA 10-5310-0227, ASA EA 5310-01762. (M)
Part: SPLICE — CORRODED (BS 579-598)
PHX - DURNG 30K CHECK, FOUND CORROSION ON LONG SPLICE AT THE MID CARGO BAY, LONGERON 30, FROM STATION 579 TO 598. REPLACED LONG SPLICE PER SRM 51-30. (M)
Part: FRAME — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, MAIN FRAME SPLICE WAS FOUND CORRODED AT STATION 1271, LONGERON 29L-30. REPAIRED PER SRM 51-30. (M)
Part: WEB — CORRODED (BS 665)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 665 TO 674 RIGHT, LONGERON 18. REPAIRED PER SRM 53-01.. (M)
Part: WEB — CORRODED (BS 712-731)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 712 TO 731 RIGHT, LONGERON 18. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 4. (M)
Part: SKIN — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE INTERNAL DOUBLER IN THE CENTER CARGO COMPARTMENT WAS FOUND CORRODED AT STATION 560 BETWEEN LONGERON 29R AND 30. INSTALLED DOUBLER REPAIR PER SRM 51-30. (M)
Part: FITTING — CORRODED (BS 712)
PHX - DURING 30K CHECK, THE FRAME SUPPORT FITTING, RIGHT STATION 712, L18 IS EXFOLIATED. REPAIRED PER SRM 51-30. (M)
Part: WEB — CORRODED (BS 1060-1079)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1060 TO 1079 RIGHT, LONGERON 18. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 4. (M)
Part: SKIN — CRACKED (FUSELAGE)
PHX - DURING 30K CHECK, THE LEFT SIDE OF FUSELAGE SKIN WAS FOUND CRACKED APPROX .20 INCH AT STATION 1401, 4.5 INCH BELOW LONGERON 13L. REPAIRED AND INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 18. (M)
Part: WEB — CORRODED (BS 1098-1117)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1098 TO 1117 RIGHT, LONGERON 18. INSTALLED DOUBLER REPAIR PER SRM 51-01 AND 51-30. (M)
Part: SUPPORT — CORRODED (BS 1287)
PHX - DURING 30K CHECK, FOUND CORROSION ON SUPPORT IN AFT CARGO PIT AT STATION 1287, 28R. REPAIRED AND REPLACED DAMAGED BRACKET PER SRM 51-30-00. (M)
Part: SHEAR TIE — CORRODED (BS 1174)
PHX - DURING 30K CHECK, FOUND CORROSION IN THE AFT CARGO COMPARTMENT AT THE MAIN FRAME SHEAR TIE CLIP, FORWARD AND AFT, STATION 1174, LONGERON 29L-29R. REPAIRED AND REPLACED DAMAGED SHEAR CLIP PER SRM 57-10, 53-14-3 AND 53-30. (M)
Part: DOOR SILL — CORRODED (BS 370-427)
PHX - DURING 30K CHECK, THE FORWARD CARGO COMPARTMENT DOOR CUTOUT, LOWER SILL WAS FOUND CORRODED AROUND RIVET HOLES FROM STATION 370-427 ABOVE LONGERON 28R. REPAIRED PER SRM 53-05, FIG 44. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE PASSENGER CABIN SUBFLOOR WAS FOUND CORRODED AT STATION 180, LBL 5. REPAIRED PER SRM 53-01, FIG 4 SHEET 3. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM, WAS FOUND CORRODED AT STATION 1212-1322, BL 16R. REPLACED TRACK PER SRM 51-31-0. (M)
Part: CHANNEL — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE MID CARGO BAY Z CHANNEL FLOOR SUPPORT FROM STATION 693 TO 731 ABOVE LONGERON 28R WAS FOUND CORRODED. REPAIRED PER SRM 51-10-1. (M)
Part: SHEAR TIE — CORRODED (BS 1041)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, FORWARD SIDE SHEAR TIE CLIP WAS FOUND CORRODED AT STATION 1041, LONGERON 29L-30. REPAIRED AND REPLACED DAMAGED SHEAR TIE PER SRM 53-03, FIG 3. (M)
Part: ANGLE — CORRODED (BS 1022)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, AFT SIDE OF MAIN FRAME WAS FOUND CORRODED AT THE ATTACH ANGLE TO LONGERONS, STATION 1022, LONGERON 30. REPAIRED PER SRM 53-14-3. (M)
Part: INTERCOSTAL — CORRODED (BS 1309-1322)
PHX - DURING 30K CHECK, FOUND CORROSION IN THE AFT CARGO PIT ON THE INTERCOSTAL, STATION 1309 - 1322, LONGERON 28L. REPAIRED PER SRM 53-24-0, FIG 11. (M)
Part: WEB — CORRODED (BS 1183)
PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1183, LEFT LONGERON 18. REPAIRED CORRODED SECTION OF WEB AND SPLICE PER SRM 53-01, FIG 4. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, FORWARD END HAS THREE CORRODED FASTENERS AND NUTPLATES, STATION 1011, BL 6. REPAIRED PER SRM 51-30. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM, WAS FOUND CORRODED AT STATION 1222-1322, BL 16. REPAIRED PER SRM 53-05, FIG 4C AND SRM 53-20-0, FIG 11. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM WAS FOUND CORRODED AT STATION 1007-1155 ABOVE LONGERON 27R. REPAIRED PER SRM 53-01. (M)
Part: FLOOR SUPPORT — PUNCTURED (FUSELAGE)
PHX - DURING 30K CHECK, THE PASSENGER CABIN SUBFLOOR WAS FOUND PUNCTURED AT LBL 7.50, STATION 200. INSTALLED DOUBLER REPAIR PER SRM 53-01. (M)
Part: SKIN — CRACKED (FUSELAGE)
PHX - DURING 30K CHECK, THE RIGHT SIDE OF FUSELAGE SKIN WAS FOUND CRACKED APPROX .25 INCH AT STATION 1401, 4.5 INCH BELOW LONGERON 13R. REPAIRED AND INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 18. (M)
Part: PIN — OUT OF POSITION (SLIDING WINDOW)
PDX - PRIOR TO DEPARTURE OF FLIGHT 304, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. REINSERTED HINGE PIN IN WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (L-1 DOOR)
PDX - FLT 449 - CREW REPORTED L-1 DOOR IS DIFFICULT TO LATCH CLOSED THROUGH THE LAST QUARTER OF THE DOOR HANDLE TRAVEL. FOUND INTERLOCK ARM HITTING LOCKPIN RETAINER. SHIMMED LOCKPIN RETAINER AND ADJUSTED INTERLOCK ARM; DOOR OPERATED NORMALLY. (X)
Part: LIGHT — INOPERATIVE (ROW 22)
SEA - DURING MAINTENANCE CHECK, ONE RED EMERGENCY FLOOR TRACK LIGHT AT ROW 22 WAS FOUND INOPERATIVE. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M)
Part: TUBE — CRACKED (RT LE FLAP)
OAK - DURING C-CHECK, FOUND GOUGE IN RIGHT WING NR 4 LEADING EDGE SLAT TRACK RETRACT TUBE. INSPECTED IAW ASA EA 5740-01167, NO CRACK NOTED. BLENDED GOUGED AREA IAW DC9 SRM 57-01, PAGE 4 FIG 1. (M)
1998
Part: LIGHT — INOPERATIVE (ROW 3)
SEA - PRIOR TO DEPARTURE OF FLIGHT 712, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FORWARD OF ROW 3 WERE INOPERATIVE. RECONNECTED WIRING TO LAMP MODULE AT ROW 3 AND OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN AND TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
ANC - FLT 194 - PRIOR TO DEPARTURE, THE FORWARD FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING IN FORWARD FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - AFTER ARRIVAL OF FLT 104, CREW REPORTED THE OVERHEAD EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: HYDRAULIC PUMP — FAILED (RT MLG WW)
SEA - FLT 570 - PRIOR TO DEPARTURE, CREW REPORTED ODOR AND FUMES IN CABIN. FOUND AUXILIARY HYDRAULIC PUMP LEAKING. REPLACED AUXILIARY HYDRAULIC PUMP, REPLACED RECIRCULATION FAN FILTER, CLEANED LOWER FUSELAGE AND ACCOMPLISHED PNEUMATIC DUCT BURN-OUT PROCEDURE. OPERATED AIR CONDITIONING SYSTEM AND NO ODOR NOTED. PART TC: 9,569. (X)
Part: LINK — BENT (L1 DOOR)
ONT - PRIOR TO DEPARTURE OF FLT 595, CREW REPORTED, THE L1 DOOR WOULD NOT LATCH OPEN. REPLACED THE DOOR HOLD OPEN MECHANISM LINK AND OPERATED NORMALLY. (M)
1997
Part: LAMP — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED 2 LAMP MODULES AND OPERATED NORMALLY. (M)
Part: SKIN — CRACKED (BS 94-110)
SEA - DURING MAINTENANCE CHECK, FOUND CRACK IN SKIN AT NLG DOOR AFT HINGE CUTOUT. STOP DRILLED CRACK IAW ASA EA 5330-01138. (M)
Part: LINK — BENT (L1 DOOR)
SEA - AFTER ARRIVAL OF FLIGHT 379 - CREW REPORTED, THE L1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. REPLACED THE L1 DOOR HOLD OPEN HOOK LINK AND OPERATED NORMALLY. (M)
Part: HOLD OPEN HOOK — OUT OF ADJUST (L1 DOOR)
PDX - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. ADJUSTED THE DOOR HOLD OPEN HOOK PUSHROD AND OPERATED NORMALLY. (M)
Part: LANYARD — DISCONNECTED (TAILCONE)
PDX - DURING INSPECTION OF THE TAILCONE EMERGENC EVACUATION SLIDE THE AUTOMATIC DEPLOY LANYARD WAS FUOND DISCONNECTED FROM THE GIRT TAB. CONNECTED THE AUTOMATIC DEPLOY LANYARD TO THE GIRT TAB. (M)
Part: HOLD OPEN HOOK — OUT OF ADJUST (L1 DOOR)
PDX - AFTER ARRIVAL OF FLT 463, CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. ADJUSTED THE HOLD OPEN HOOK ROD END AND OPERATED NORMALLY. (M)
Part: DOOR HANDLE — BROKEN (L2 DOOR)
SEA - PRIOR TO DEPARTURE OF FLT 700, CREW REPORTED THE L2 DOOR INTERIOR HANDLE BROKEN, HANDLE IS AGAINST BULKHEAD AND DIFFICULT TO GRASP. REPLACED THE HANDLE ASSEMBLY AND OPERATED NORMALLY. (M)
1996
Part: SLIDE LIGHT — FAILED TEST (TAILCONE)
OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M)
Part: SLIDE LIGHT — FAILED TEST (L2 DOOR)
OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHT FAILED TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN AND THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROMROWS 13 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATEDNORMALLY.(M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SFO - DURING MAINTENANCE CHECK, THE AFT TWO OVERHEAD EMERGENCY LIGHTS AND THE OVERHEAD EMERGENCY LIGHT ABOVE THE TAILCONE EMERG EVAC SLIDE WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AND THE OVERHEAD EMERGENCY LIGHTS ROWS 24-27 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: SOCKET — LOOSE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 27 TO 29 FOUND INOPERATIVE. RESET LIGHT SOCKET AT ROW 27 AND OPERATED NORMALLY. (X)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING MAINTENANCE CHECK, EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 24 TO 27 FOUND INOPERATIVE. TIGHTENED LOOSE CONNECTOR AT ROW 24 AND OPERATED NORMALLY. (X)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
1995
Part: EEL WIRING — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMRGENCY FLOOR TRACK LIGHTS FROM ROWS 25 TO 29 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN TRACK AT ROW 25 AND LIGHTS OPERATED NORMALLY. (X)
Part: EEL WIRING — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 25 TO 29 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN TRACK AND LIGHTS OPERATED NORMALLY. (X)
Part: BOLT — BROKEN (L2 DOOR)
PHX - FLT 94 - ON ARRIVAL, CREW REPORTED THE L2 DOOR HANDLE RETAINER BOLT BROKEN. REPLACED BOLT AND OPERATED NORMALLY. (X)
Part: LOCKING MECH — LACK OF LUBE (L1 DOOR)
SEA - ON ARRIVAL OF FLT 595, CREW REPORTED THE L1 DOOR DIFFICULT TO LOCK CLOSED FROM INSIDE. LUBED LOCKING MECHANISM AND OPERATED NORMALLY. (M)
Part: FRAME — CORRODED (Y1287)
PAE - DURING 15K CHECK, FOUND CORROSION ON FRAME AT Y1287, X MINUS 6 TO X MINUS 8, Z-48. REMOVED CORROSION AND INSTALLED NEW PIECES IAW DC-9 SRM 51-20-00, 51-30-02, 53-01 AND 53-03. (M)
Part: SPLICE STRAP — CORRODED (Y1174)
PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME SPLICE STRAP AT Y1174, X PLUS 24, Z-44. REMOVED CORRODED STRAP AND INSTALLED NEW SPLICE STRAP IAW DC-9 SRM 51-01, 51-10-03 AND 51-30-05. (M)
Part: SHEAR TIE — CORRODED (Y1060)
PAE - DURING 15K CHECK, FOUND CORROSION ON SHEAR TIE AT Y1060, X PLUS 4, Z MINUS 47. REMOVED CORROSION AND INSTALLED NEW SHEAR TIE IAW DC-9 SRM 51-10-01, 51-10-03, 51-30-01 AND 53-03. (M)
Part: SKIN — CORRODED (Y1287)
PAE - DURING 15K CHECK, FOUND CORROSION ON SKIN AT Y1287, X MINUS 1 TO X MINUS 6, Z MINUS 47. REMOVED CORRODED AREA OF SKIN AND REPAIRED IAW DC-9 SRM 53-04. (M)
Part: EEL — DEFECTIVE (CABIN)
SEA - ON ARRIVAL OF FLT 467 - CREW REPORTED NUMEROUS EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FORWARD CABIN. REPLACED LIGHT ASSEMBLY AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL TERMINAL — LOOSE (CABIN)
LAX - PRIOR TO DEPARTURE OF FLIGHT 256 - CREW REPORTED THE FORWARD 4 EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. SECURED LOOSE TERMINAL AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT OVERWING EXITS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: PORTABLE EEL — DEFECTIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)