N975AS
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.
211 reports on file, 1995-07-01 – 2007-07-11.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,365 hrs · 22,913 cycles
AFT CARGO BAY FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION PER SRM 51-10-4, 51-30-2 AND DAC DWG 9919605.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 44,364 hrs · 22,913 cycles
CABIN FLOOR PANEL HAS DAMAGED INSERTS. FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW SRM 53-05 PG 122B THRU 127 SECTION 44 FIGS 40 THRU 50.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
RIGHT CUSP WEB CORRODED. REMOVED DAMAGED SECTION OF WEB, LOCATED, DRILLED AND INSTALLED A REPLACEMENT CUSP WEB IAW SRM 51-30-2, 51-10-4 AND 51-30-5.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
MID PIT BILGE DRAIN AREA SKIN CORRODED. REMOVED DAMAGED AREA OF SKIN. FABRICATED DOUBLER AND FILLER, INSTALLED IAW SRM 51-10-3 PG 24 AND ASA EA 5330 02220.
Part: FRAME — CORRODED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
AFT CARGO FORMER CORRODED. REMOVED DAMAGED AREA OF FORMER FABRICATED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT FORMER IAW SRM 51-10-3 PG 24.
Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
AFT CARGO RT CARGO TRACK IS CORRODED BETWEEN STA 1148 AND 1155. REMOVED DAMAGED SECTION OF CARGO TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT TRACK SECTION IAW SRM 51-30-1 PG 13 AND 51-30-5 PG 3.
Part: SKIN — GOUGED (T/E FLAP VANE) · airframe 44,364 hrs · 22,913 cycles
RIGHT WING O/B FLAP I/B VANE GOUGED ON LEADING EDGE 7 INCHES FROM I/B END. PREPAIRED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 59.
Part: SKIN — GOUGED (T/E FLAP VANE) · airframe 44,364 hrs · 22,913 cycles
RIGHT WING O/B FLAP I/B VANE GOUGED ON L/E 7 INCHES FROM I/B END. PREPARED DAMAGED AREA. FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 59.
Part: FRAME — CORRODED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
AFT CARGO FRAME CORRODED AT BS 1322 BETWEEN LONG 29R AND LONG 29L. REMOVED DAMAGED AREA OF FRAME, LOCATED, DRILLED AND INSTALLED A REPLACEMENT FRAME AND SPLICE PARTS IAW SRM 53-03 FIG 2A, 51-30-2 PG 1 AND 51-30-5 PG 1.
Part: SKIN — GOUGED (T/E FLAP VANE) · airframe 44,364 hrs · 22,913 cycles
RIGHT WING O/B FLAP O/B VANE GOUGED ON UPPER SURFACE 68 INCHES FROM O/B END. PREPAIRED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-70-2 PG 23 PARA 18B AND 51-70-2 FIG 12.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
AFT CARGO SHEAR TIE CORRODED AT BS 1322 BETWEEN LONG 29R AND LONG 29L. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED, LOCATED, DRILLED AND INSTALLED SHEAR TIE AND REPAIR SPLICES IAW SRM 53-03 PG 4M FIG 3 SRM 51-60-0 PG 5 FIG 1 SHEET 1.
Part: SKIN — DENTED (T/E FLAP VANE) · airframe 44,364 hrs · 22,913 cycles
LT WING I/B FLAP I/B VANE DENTED ON LWR SURFACE NEXT TO PREVIOUS REPAIR EDGE. REMOVED EXISTING REPAIR, PREPAIRED SURFACE, FABRICATED DOUBLER AND INSTALLED IAW SRM 57-03 FIG 9A AND 51-70-2 FIG 12.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
CABIN SEAT TRACK CORRODED. REMOVED DAMAGED AREA OF TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SECTION IAW SRM 53-05 FIG 4A PG 8C AND 8D.
Part: FRAHM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
AFT CARGO FRAME CORRODED AT BS 1287 BETWEEN LONG 29L AND LONG 29R. REMOVED DAMAGED SECTION OF FRAME, LOCATED, DRILLED A REPLACEMENT FRAME IAW SRM 53-3 FIG 2A AND DAC DWG 9957739.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
AFT CARGO SHEAR TIE CORRODED AT BS 1322 BETWEEN LONG 26R AND 25R. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED, LOCATED, DRILLED AND INSTALLED SHEAR TIE AND REPAIR SPLICES IAW SRM 53-03 PG 4M FIG 3, 51-60-0 PG 5 FIG 1 SH 1.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
AFT CARGO FRAME CORRODED AT STA 1250 BETWEEN LONG 29L AND LONG 29R. REMOVED DAMAGED SECTION OF FRAME, LOCATED DRILLED AND INSTALLED A REPLACEMENT FRAME IAW SRM 51-03 FIG 2A AND 51-30-5 PG 12 AND 13.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
AFT CARGO RIGHT ZEE ANGLE CORRODED. REMOVED DAMAGED SECTION OF ZEE, LOCATED DRILLED AND INSTALLED A REPLACEMENT SECTION IAW SRM 51-30-5 PG 3 21 AND 51-30-1 PG 13.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 44,365 hrs · 22,913 cycles
CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWGS 9936549 AND 4932106.
Part: FRAME — CORRODED (BS 1219) · corrosion level 2 · airframe 44,365 hrs · 22,913 cycles
AFT CARGO BAY STUB FRAME FORMER CORRODED ON FORWARD AND AFT SIDES. REPLACED FORMER PER SRM 51-30-2 AND 51-30-5.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
SEAT TRACK HAS DOUBLE DRILLED HOLES. REMOVED DAMAGED SECTION OF TRACK, LOCATED, DRILLED AND INSTALLED A REPLACEMENT TRACK IAW SRM 53-05 PG 11 FIG 4H, 51-10-4 PG 1 AND 51-30-5 PG 1 AND 51-30-1 PG 1.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 44,365 hrs · 22,913 cycles
CABIN FLOORBOARD PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05 AND DAC DWG 99366549.
Part: TAB — DELAMINATED (RUDDER) · airframe 44,365 hrs · 22,913 cycles
RUDDER TAB DELAMINATED AT TRAILING EDGE. REPAIRED WITH GLASS CLOTH AND ASTROSTICKE PER SRM 51-70-1A.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
CABIN RIGHT CUSP WEB CORRODED BETWEEN BS 503 AND BS 541. REMOVED DAMAGED CUSP WEB, LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-10-4 PG 1, 51-30-2 PG 1 AND 51-30-5 PG 1.
Part: FLOOR PANEL — PUNCTURED · airframe 44,365 hrs · 22,913 cycles
COCKPIT FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05.
Part: INTERCOSTAL — CORRODED (BS 1307-1322) · corrosion level 2 · airframe 44,365 hrs · 22,913 cycles
AFT CARGO BAY INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 57-30-2 AND 51-30-5.
Part: TORQUE BOX — CRACKED (BS 209-213) · airframe 44,365 hrs · 22,913 cycles
L1 DOOR CUTOUT TORQUE BOX WEB CRACKED AT AFT SIDE OF LONGERON. INSTALLED DOUBLER AND FILLER PER DWG 65956879 SRM 51-70-4 AND 51-10-3.
Part: ATTACH FITTING — CORRODED (BS 1271) · corrosion level 2 · airframe 44,365 hrs · 22,913 cycles
FRAME ATTACH FITTING HAS EXFOLIATION (CORROSION). REPLACED FITTING PER SRM 51-10-4 AND 51-30-5.
Part: LONGERON — CORRODED (BS 1237-1295) · airframe 44,365 hrs · 22,913 cycles
LONGERON 30 CORRODED INSIDE OF CHANNEL. REPLACED DAMAGED SECTION PER SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-5.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 44,365 hrs · 22,913 cycles
FLOOR TRACK HAS DOUBLE DRILLED HOLES. REPLACED FLOOR TRACK PER SRM 51-10-4 AND 51-30-1.
Part: SEAT TRACK — CORRODED (BS 200-247) · corrosion level 2 · airframe 44,365 hrs · 22,913 cycles
CABIN SEAT TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM 51-10-4, 53-05 AND 51-30-5.
Part: FLOOR PANEL — DAMAGED (BS 946-1003) · airframe 44,365 hrs · 22,913 cycles
CABIN FLOOR PANEL HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.
Part: CUSP WEB — CORRODED (BS 505-508) · corrosion level 2 · airframe 44,365 hrs · 22,913 cycles
FORWARD CARGO BAY LEFTHAND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53-01 AND 51-10-3.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 44,365 hrs · 22,913 cycles
FLOOR TRACK HAS DOUBLE DRILLED HOLES. REPLACED FLOOR TRACK PER SRM 51-10-4 AND 51-30-1.
Part: INTERCOSTAL — CORRODED (BS 842-848) · corrosion level 2 · airframe 44,364 hrs · 22,913 cycles
RIGHT BSTA 845 GUSSET INTERCOSTAL SPLICE AT LONGERON 17R CORRODED. FABRICATED A REPLACEMENT GUSSET, LOCATED DRILLED AND INSTALLED GUSSET IAW SRM 51-30-2 AND 51-30-5.
Part: SKIN — DENTED (FUSELAGE) · airframe 44,364 hrs · 22,913 cycles
RIGHT EXTERNAL FUSELAGE MULITPLE PROTRUDING DENTS. CUT OUT DAMAGED AREA, FABRICATED A REPAIR DOUBLER, STRIP DOUBLER FILLERS AND INSTALLED IAW SRM 53-04 FIG 12B.
Part: CONTROL UNIT — MALFUNCTIONED (TAILCONE JETTISO) · airframe 44,365 hrs · 22,913 cycles
A TEST DEPLOYMENT (PER TASK CARD 28653000) OF THE TAIL CONE EMERGENCY SLIDE FAILED. A SUBSEQUENT TEST PER THE REFERENCE PROCEDURE IN MM 53-53-00 WAS SUCCESSFUL. AN INVESTIGATION HAS BEEN INITIATED TO DETERMINE THE CAUSE OF FAILURE BUT SUBSEQUENTLY CANCELED DUE TO THE MD 80 FLEET BEING RETIRED BEFORE ITS COMPLETION.
Earlier reports · 1995–2006 · 175 reports
2006
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED AND HAS MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED AND HAS DAMAGED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM 51-10-4 , 51-10-3 AND 51-30-1.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM 51-10-4, 51-10-3 AND 51-30-1.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED AND PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,065 hrs · 21,309 cycles
CABIN SEAT TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK WITH INSTALLATION OF TWO REPAIR CHANNELS AND TWO REPAIR PLUGS PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED AND MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL CRACKED. REPLACED FLOOR PANEL.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
CABIN FLOOR PANEL DELAMINATED. REPLACED PANEL PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,065 hrs · 21,309 cycles
COCKPIT FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.
Part: FLOOR PANEL — DELAMINATED (BS 160-200) · airframe 41,065 hrs · 21,309 cycles
FOUND CABIN FLOOR PANEL HAS WATER DAMAGE AND BROKEN INSERTS. REPLACED PANEL PER SRM 53 05.
Part: FLOOR PANEL — DELAMINATED (BS 180-200) · airframe 41,065 hrs · 21,309 cycles
FOUND CABIN FLOOR PANEL DELAMINATED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53 05.
Part: FLOOR PANEL — DELAMINATED (BS 160-180) · airframe 41,065 hrs · 21,309 cycles
FOUND CABIN FLOOR PANEL DELAMINATED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53 05.
Part: FLOOR PANEL — DELAMINATED (BS 200-256) · airframe 41,065 hrs · 21,309 cycles
FOUND CABIN FLOOR PANEL IS DELAMINATED AND HAS PULLED INSERTS. REPLACED PANEL PER SRM 53 05.
Part: FLOOR PANEL — DELAMINATED · airframe 41,065 hrs · 21,309 cycles
FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL PER SRM 53 05.
Part: SEAT TRACK — CORRODED (BS 200-265) · airframe 41,065 hrs · 21,309 cycles
FOUND CABIN SEAT TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05.
2005
Part: ENGINE — SEIZED (RIGHT)
RIGHT ENGINE SEIZED ON FINAL APPROACH. REPLACED ENGINE. TEARDOWN REVEALED INITIAL CAUSE TO BE FAILED COMPRESSOR 8TH STAGE STATOR AT BRAZED WELD REPAIR. CRACK ORIGINATED ON VANE OD T/E AND PROPAGATED INTO HCF.
Part: SPACER — CORRODED (DOOR BEAM)
C-CHECK - AFT CARGO BAY DOOR BEAM SPACER IS CORRODED. REPLACED SPACER. (K)
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 37,036 hrs · 19,290 cycles
C-CHECK, CABIN FLOOR PANEL HAT SECTION IS CRACKED. REPLACED HAT SECTION. (K)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
C-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (K)
Part: FLOORBOARD — CRACKED (FUSELAGE)
C-CHECK - CABIN FLOOR PANEL HAT SECTION IS CRACKED. REPLACED HAT SECTION. (K)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
C-CHECK - INTERCOSTAL CORRODED ON TOP AND BOTTOM FLANGES. REPLACED INTERCOSTAL. (K)
Part: FRAME — CHAFED (FUSELAGE)
C-CHECK, UPPER LT ACCY COMPARTMENT FWD EDGE OF FRAME WEB IS CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLERS AND FILLER. (K)
Part: CUSP WEB — CORRODED (FUSELAGE)
C-CHECK - AFT CABIN UPPER CUSP MEMBRANE IS CORRODED. REMOVED DAMAGED SECTION. INSTALL REPAIR DOUBLER. (K)
Part: CUSP WEB — PUNCTURED (FUSELAGE)
C-CHECK - FWD CARGO BAY CUSP WEB ABOVE DOOR HINGE INS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (K)
Part: SHEAR TIE — CORRODED (FUSELAGE)
C-CHECK - SHEAR TIE CORRODED ON AFT SIDE OF LONGER. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLERS. (K)
Part: VANE — CHAFED (TE FLAP)
C-CHECK, RT WING OB FLAP VANE CHAFED BEHIND IB HINGE FAIRING. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)
Part: VANE — DENTED (RT WING TE FLAP)
C-CHECK - RT WING IB FLAP VANE DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND FILLER. (K)
Part: CUSP WEB — CANNING (FUSELAGE)
C-CHECK - CUSP WEB IS (OIL CANNING). REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER. (K)
2004
Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)
PDX - FOUND DURING CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 26-29. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
DURING FILGHT, FOUND LEFT AFT LAVATORY SMOKE DETECTOR CAUSED FALSE CHIME ALARM. REPLACED DETECTOR. CHECKED OK. (M)
2003
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FLOORBOARD PANEL TORN AND DELAMINATED AT FS 313-389. REMOVED DAMAGED AREA AND REPAIRED WITH FIBERGLASS OVERLAP PER SRM 51-90-0. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
DURING C-CHECK SHEAR TIE FOUND CORRODED AT FS 1212. REMOVED DAMAGED AREA AND INSTALLED DOUBELR PER SRM'S 51-10-2, 51-10-4, 51-30-2, AND 51-30-5. (M)
2002
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - FOUND 30K-CHECK, FOUND FLOORBOARD IS DELAMINATED FORWARD OF FS 617, RBL 36. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, FLOORBOARD HAS NUMEROUS CORRODED INSERTS AND FASTENERS AT FS 160-207, BL 0 TO LBL 60. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - FOUND FLOORBOARD HAS NUMEROUS CORRODED INSERTS AND FASTENERS AT FS 207, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, FLOORBOARD HAS NUMEROUS CORRODED INSERTS AND FASTENERS AT FS 207, LBL 22 TO RBL 22. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — PUNCTURED (FUSELAGE)
OKC - FOUND 30K CHECK, FLOORBOARD IS PUNCTURED AT FS 1117-1174, LBL 22-LBL 44. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - FOUND 30K-CHECK, FLOORBOARD HAS SOFT SPOT AT FS 218 TO 229, BL 0. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: FLOORBOARD — PUNCTURED (FUSELAGE)
OKC - FOUND DURING 30K-CHECK, FLOORBOARD IS PUNCTURED AT FS 256-275, LBL 36. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: SEAT TRACK — GOUGED (FUSELAGE)
OKC - FOUND DURING 30K-CHECK, LEFT INBOARD SEAT TRACK GOUGED AT FS 693, LBL 22. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PART PER SRM 53-05. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - FOUND LONGERON 29R IS CORRODED IN RADIUS AT FS 1180.25-1183. BLENDED AREA PER BAC TLX AOC-OKC-02-0086H AND EA 5310-02134. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K-CHECK, MAIN CABIN FLOOR SUPPORT CORRODED AT FS 195, LBL 44. INSTALLED NEW SUPPORT PER SRM 51-10-2 AND 51-10-4. (M)
Part: FLOORBOARD — DAMAGED (FUSELAGE)
OKC - FOUND 30K-CHECK, FLOORBOARD HAS SOFT SPOT AT FS 1003 TO 1022 AT LBL 22 TO RBL 22. REPLACED FLOORBOARD PER SRM 53-05. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - FOUND DURING 30K-CHECK, FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERON 19L AND 20L. INSTALLED DOUBLER REPAIR PER SRM 53-04. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, LEFT INBOARD SEAT TRACK IS CORRODED AT FS 574-598, LBL 22. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS PER SRM 53-05. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, SHEAR TIE IN AFT CARGO BAY CORRODED IN TWO AREAS AT FS 1287, L29L TO L29R. REMOVED CORROSION AND REPAIRED WITH DOUBLER PER SRM 53-01, 53-03, AND 51-30-2. (M)
Part: SKIN — GOUGED (CARGO DOOR)
OKC - FOUND DURING 30K-CHECK, AFT CARGO BAY DOOR SKIN AND SEAL RETAINER GOUGED AT AFT LOWER CORNER. BLENDED GOUGES PER BAC TLX AOC-OKC-02-00126H AND EA 5230-0-1182. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, UPPER SHEAR TIE CORRODED AT FS 1212, LONGERON 28R. REPLACED SHEAR TIE PER SRM 53-24-0, 51-10-2, 51-10-4, AND 51-30-5. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, FRAME CORRODED ON AFT SIDE AT FS 1060 BETWEEN LONGERON 29L AND 30. CUT OUT DAMAGE AND REPAIRED PER BAC TLX AOC-OKC-02-00095H, EA 5310-02137. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, LONGERON 29R CORRODED IN TWO AREAS AT FS 1212-1231. BLENDED CORROSION AND REPAIRED PER BAC TLX AOC-OKC-02-00090H, EA 5310-02135. (M)
Part: SKIN — GOUGED (RT WING)
OKC - DURING 30K CHECK, FOUND RIGHT WING LOWER LEADING EDGE IS GOUGED AT STATION XFS67. REPAIRED PER BAC TLX AOC-OKC-02-00110H AND EA 5740-01329. (M)
Part: SKIN — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, SKIN CORRODED ON INNER SURFACE AROUND FASTENER HOLES AND SEALANT AT FS 1079-1098, LONGERON 28L-28R. REMOVED CORROSION AND REPAIRED PER BAC TLX AOC-OKC-02-0088H AND EA 5330-01609. (M)
Part: SILL — CRACKED (FUSELAGE)
OKC - FOUND 30K CHECK, R1 DOOR SILL PAN FORWARD EDGE IS CRACKED. WELD REPAIRED PAN EDGE PER EA 53-20-01551. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, LONGERON 30 CORRODED BY FASTENER AT FS 1007-1022. REMOVED CORROSION AND FASTENER. REPAIRED PER BAC TLX AOC-OKC-02-00080H AND EA 5310-02131. (M)
Part: SKIN — GOUGED (RT WING)
OKC - DURING 30K CHECK, FOUND RIGHT WING LOWER LEADING EDGE IS GOUGED AT STATION XFS9. REPAIRED PER BAC TLX AOC-OKC-02-00110H AND EA 5740-01329. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, LONGERON 30 CORRODED ON BOTTOM AND HORIZONTAL LEG AT FS 1237 AND 1245. BLENDED CORROSION AND REPAIRED PER BAC TLX AOC-OKC-02-00083H, EA 5310-02126. (M)
Part: RETAINER — GOUGED (CARGO DOOR)
OKC - FOUND 30K CHECK, MID CARGO BAY DOOR SEAL RETAINERS ARE GOUGED NEAR RADIUS AT FORWARD AND AFT LOWER SEAL RETAINER. BLENDED PER BAC TLX AOC-OKC-02-00125H AND EA 5230-01183. (M)
Part: SKIN — GOUGED (CARGO DOOR)
OKC - FOUND DURING 30K CHECK, MID CARGO BAY DOOR SEAL RETAINERS ARE CHAFED AND SKIN IS GOUGED. BLENDED AND REPAIRED PER BAC TLX AOC-OKC-02-00125H AND EA 5230-01183. (M)
Part: SKIN — GOUGED (LT WING)
OKC - FOUND 30K CHECK, LEFT WING LEADING EDGE UPPER SKIN GOUGED AT STATION XFS 142. CUT OUT DAMAGED AREA AND REPAIRED PER BAC TLX AOC-OKC-02-0081H AND EA 5740-01330. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, LONGERON 30 IS CORRODED AT SPLICE AT FS 1193-1212 ON LOWER SIDE. BLENDED CORROSION, THEN REPAIRED PER BAC TLX AOC-OKC-02-0087H AND EA 5310-02133. (M)
Part: PANEL — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, TRANSITION PANEL INBOARD OF R-1, RIGHT FORWARD SERVICE, DOOR IS CORRODED AT FS 160-200. REPLACED TRANSITION PANEL PER SRM 51-10-5, 51-10-4 AND DAC DWG 9957828. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, FOUND SEAT TRACK CORRODED AT FS 235-237, RBL 44. REMOVED CORRODED SECTION. SPLICED IN REPLACEMENT PER SRM 53-05, FIG 4F. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, SEAT TRACK FOUND CORRODED AT FS 562, RBL 44. REMOVED CORRODED SECTION. SPLICED IN REPLACEMENT SECTION PER SRM 53-05, FIG 4F. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, FRAME WEB CORRODED AT FS 1022 BETWEEN LONGERON 29R AND 30. REPLACED SHEAR CLIP AND REPAIRED PER BAC TLX AOC-OKC-02-0012OH, EA 5310-02138 (AAR EA 13-53-EA078). (M)
Part: SUPPORT ANGLE — BROKEN (FUSELAGE)
OKC - FOUND DURING 30K-CHECK, LONGERON 8R SUPPORT ANGLE FOUND BROKEN AT FS 1415. REPLACED SUPPORT ANGLE PER SRM 51-30-5. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, FRAME CORRODED ON AFT SIDE AT FS 1079 BETWEEN LONGERON 29L AND 29R. REPAIRED WITH SPLICE PER BAC TLX AOC-OKC-02-0091H, EA 5310-01232 (AAR EA 13-53-EA072). (M)
Part: SEAT TRACK — GOUGED (FUSELAGE)
OKC - FOUND DURING 30K-CHECK, SEAT TRACK GOUGED AT FS 257-259, LBL 44. REMOVED GOUGED SECTION. SPLICED IN REPLACEMENT SECTION PER SRM 53-05, FIG 4F. (M)
Part: SKIN — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, SKIN CORRODED ON INNER SURFACE AT FS 1060-1079, LONGERON 29L-29R. REMOVED CORROSION AND REPAIRED PER BAC TLX AOC-OKC-02-0088H AND EA 5330-01609. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, INTERCOSTAL CORRODED AT FS 1155 BETWEEN LONGERON 29R AND 30. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-10-4, 51-30-5, AND DAC DWG 5936071. (M)
Part: WEB — CORRODED (FUSELAGE)
WEB CORRODED IN AFT CARGO BAY AT FUSELAGE STATION 1183-1212. REPLACED WEB SECTION IAW SRM.
Part: WEB — CORRODED (FUSELAGE)
CUSP WEB CORRODED FROM FUSELAGE STATION 1074 TO 1149. REPAIRED CORRODED SECTION IAW SRM.
Part: SEAT TRACK — GOUGED (FUSELAGE)
LEFT INBOARD SEAT TRACK IS GOUGED AT STA 693, LBL 22. REPLACED DAMAGED SECTION OF TRACK IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE)
SEAT TRACK CORRODED AT FUSELAGE STATION 237-240, RBL 22. REPLACED SEAT TRACK IAW SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE)
SHEAR TIE CORRODED IN AFT CARGO BAY AT FUSELAGE STATION 1098, L30-L29R. REPLACED SHEAR TIE IAW SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE)
SHEAR TIE CORRODED IN AFT CARGO BAY AT FUSELAGE STATION 1287, L29L-L29R. REMOVED CORROSION AND INSTALLED DOUBLER IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE)
ANGLE CORRODED AT FUSELAGE STATION 134, CUSP LINE RBL 54. REPLACED ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FLOOR SUPPORT CORRODED AT STA 195, LBL 44. REPLACED FLOOR SUPPORT IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FLOOR SUPPORT CORRODED AT STA 200, BL 0- RBL 60. REPLACED FLOOR SUPPORT IAW SRM.
Part: WEB — CORRODED (FUSELGAE)
LEFT CUSP WEB CORRODED AT FUSELAGE STATION 465-484. REMOVED CORROSION AND REPAIRED IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
FLOOR SUPPORT CORRODED AT STA 160-200, RBL 60. REPLACED FLOOR SUPPORT IAW SRM.
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, AFT CARGO BAY INTERCOSTAL BETWEEN LONGERON 29R AND 30 AT FS 1155 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-5. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, AFT CARGO BAY SHEAR TIE CORRODED TWO PLACES AT FS 1212. REPAIRED SHEAR TIE PER SRM 53-03, FIG 6. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, FUSELAGE SKIN DENTED 50 INCHES AFT OF LEFT FORWARD PASSENGER DOOR, 2 INCHES ABOVE FLOOR LINE BEHIND LOWER SIDEWALL GRILLE. REPAIRED SKIN PER SRM 53-04, FIG 12B, SHEET 4, PG 36. (M)
Part: SKIN — CRACKED (RT WING)
OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE CRACKED .5 INCH ON RIB AT FASTENER HOLES AT WING STATION XRS 69. STOP DRILLED, REMOVED DAMAGE, AND INSTALLED DOUBLER AND SHIM PER SRM 51-10-3. (M)
Part: SKIN — DENTED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, FUSELAGE SKIN DENTED AT FS 208, L16R TO L17R. REPAIRED SKIN PER SRM 53-04, FIG 38. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - FOUND 30K CHECK, AFT CARGO BAY SHEAR TIE FASTENER HOLES (8 EACH) CORRODED AT FS 1212. REPLACED SHEAR TIE PER SRM 51-30-2. (M)
Part: MODULE — INOPERATIVE (CABIN)
SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. REPLACED LIGHT MODULE AND WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 7. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED NORMALLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
OAK - DURING PREFLIGHT CHECK, VARIOUS EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DAMAGED (CABIN)
BUR - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT THE FIRST COUPLE OF ROWS. REPAIRED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — DISCHARGED (CABIN)
PDX - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE AT ROWS 18-22. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SAN - DURING PREFLIGHT CHECK, FOUND 1ST CLASS CABIN EMERGENCY TRACK LIGHTING INOPERATIVE. RESECURED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN FIRST CLASS CABIN. REASSEMBLED (RECONNECTED) TRACK LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 1 THROUGH 7. RECONNECTED TRACK LIGHT MODULE CONNECTORS. LIGHTS THE OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SFO - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LIGHT. LIGHT THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. REATTACHED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - DURING LINE CHECK, FIRST SIX EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE AT ROW 3. RECONNECTED MODULE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING AT ROW 7 'NEEDS A CONNECTOR'. REATTACHED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN 1ST CLASS SECTION. RESECURED CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)
Part: PLUG — OUT OF POSITION (CABIN)
SEA - DURING LINE MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE IN FORWARD CABIN. REINSTALLED PLUG IN TRACK LIGHTING MODULE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING PREFLIGHT CHECK, DISCOVERED EMERGENCY LIGHTING IN FIRST CLASS TO BE INOPERATIVE. RECONNECTED LOOSE SEGMENTS. LIGHT THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING PREFLIGHT CHECK, DISCOVERED EMERGENCY LIGHTING IN FORWARD CABIN TO BE INOPERATIVE. RESECURED ELECTRICAL CONNECTOR. LIGHT THEN OPERATED PROPERLY. (M)
Part: LIGHT — DISCONNECTED (CABIN)
SEA - DURING LINE CHECK, DISCOVERED EMERGENCY TRACK LIGHT AT ROW 25 WAS INOPERATIVE. RECONNECTED LAMP ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)
Part: MECHANISM — LACK OF LUBE (COCKPIT WINDOW)
PDX - DURING PREFLIGHT CHECK, THE FIRST OFFICER'S SLIDING CLEARVIEW WINDOW DIFFICULT TO OPEN. LUBRICATED WINDOW MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - DURING PREFLIGHT CHECK, DISCOVERED 'NUMEROUS EMERGENCY TRACK LIGHTS OUT'. REPLACED WIRE SECTIONS BETWEEN ROW 2 AND 3. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING PREFLIGHT CHECK, DETERMINED THAT THE FIRST CLASS CABIN EMERGENCY TRACK LIGHTING WAS INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SAN - DURING PREFLIGHT CHECK, DETERMINED THAT THE 1ST CLASS CABIN EMERGENCY TRACK LIGHTING WAS INOPERATIVE. RECONNECTED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WINDOW — OUT OF ADJUST (COCKPIT)
SEA - DURING PREFLIGHT CHECK, FOUND IT WAS DETERMINED THAT THE RIGHT SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RE-STOWED WINDOW ALIGNMENT PIN INTOP TRACK. WINDOW THEN OPERATED PROPERLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS AT ROWS 13-21 WERE FOUND TO BE ILLUMINATED EVEN THOUGH POWER WAS TURNED OFF. LIGHTS WERE NOTICEABLY DIMMER THAN NORMAL. REPLACED ASSOCIATED POWER SUPPLIES (BATTERY PACK ASSEMBLIES), LIGHT BULBS (ADVANCED MICRO P/N 7732), AND FIVE CONNECTOR WIRING ASSEMBLIES. LIGHTS THEN OPERATED PROPERLY. (M)
2001
Part: LANYARD — DISCONNECTED (SERVICE DOOR)
LAX - DURING PREFLIGHT CHECK, L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
GEG - DURING PREFLIGHT CHECK, DETERMINED EMERGENCY TRACK LIGHTING TO BE INOPERATIVE FROM ROWS 13 TO 21. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LANYARD — DISCONNECTED (GALLEY DOOR)
SEA - DURING PRE-FLIGHT CHECK, GALLEY SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM THE SLIDE COVER. REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER. (M)
Part: MODULE — DISCONNECTED (CABIN)
SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 7. RECONNECTED LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — DISCONNECTED (CABIN)
SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 7. RECONNECTED LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
LAX - PRIOR TO FLIGHT, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 7. SECURED FLOOR TRACK LIGHTING AT ROW 7. LIGHTS THEN OPERATED NORMALLY. (M)
Part: WINDOW (COCKPIT)
ANC - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. ADJUSTED SLIDER MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
PHX - PRIOR TO FLT 711 - THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 6 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND THE LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SJC - PRIOR TO FLT 319 - THE EMERGENCY FLOOR TRACK LIGHT COVER WAS FOUND TO BE MISSING AND THE LIGHTS INOPERATIVE AT ROW 7. INSTALLED MISSING COVER AND RECONNECTED WIRING TO LAMP MODULE AT ROW 7, LIGHTS THEN OPERATED NORMALLY. (M)
Part: LIGHT — DISCONNECTED (CABIN)
PDX - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING AT ROWS 6 THROUGH 8 WERE DETERMINED TO BE INOPERATIVE. RECONNECTED TRACK LIGHT ASSEMBLIES. TRACK LIGHTS THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)
Part: WIRE — BROKEN (CABIN)
SEA - DURING CRUISE, TRACK LIGHTING CAME ON FOR A MOMENT. A CHECK OF THE EMERGENCY FLOOR TRACK LIGHTS FOUND THE LIGHTS AT ROWS 22 TO 24 INOPERATIVE. REPAIRED BROKEN WIRES. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WINDOW — INOPERATIVE (COCKPIT)
LAX - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO CLOSE. LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (TAILCONE)
SEA - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTING MODULE WAS DETERMINED TO BE BROKEN IN TAILCONE AREA. REPLACED BROKEN EMERGENCY FLOOR TRACK LIGHTING MODULE. LIGHT THEN OPERATED PROPERLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. LIGHT OPERATED PROPERLY. (M)
2000
Part: BATTERY — DISCHARGED (ROW 2)
SEA - DURING MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING AT ROW 2 WAS DETERMINED TO BE INOPERATIVE. REPAIRED WIRING AT ROW 2. LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (AFT CABIN)
DURING MAIN CHECK OVERHEAD EMERGENCY LIGHTS FOUND TO BE INOP BETWEEN AFT LAV. REPLACED NICAD BATTERIES IN BATTERY PACK. OPERATED NORMALLY.
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: HARNESS — DISCONNECTED (CABIN)
SEA - PRIOR TO FLIGHT 660, THE FORWARD 7 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING HARNESS AT ROW 3 AND THE EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SFO - PRIOR TO DEPARTURE OF FLIGHT 391, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
LAX - DURING MAINTENANCE CHECK, 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FIRST CLASS CABIN. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
OAK - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY, RELAY R2-271, AND THE EMERGENCY LGIHT SWITCH AT THE FORWARD FLIGHT ATTENDANT PANEL AND OPERATED NORMALLY. (M)
Part: RELAY — INOPERATIVE (CABIN)
OAK - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY, RELAY R2-271, AND THE EMERGENCY LIGHT SWITCH AT THE FORWARD FLIGHT ATTENDANTS PANEL. OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
OAK - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS ILLUMINATE WHEN ELECTRICAL POWER SWITCHED FROM GROUND POWER TO APU GENERATOR POWER. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: TURBINE — LEAKING (LT ACM)
OAK: FLIGHT DIVERTED DUE TO FUMES IN THE AFT CABIN AFTER TAKEOFF. THE RIGHT AFT LAV SMOKE DETECTOR CHIMES SOUNDED APPROX. TEN TIMES. LANDED WITHOUT INCIDENT, MX FOUND THE LEFT COOLING TURBINE LEAKING OIL. REPLACED COOLING TURBINE. PERFORMED HIGH PRESSURE DUCTING BURNOUT AND AIR QUALITY CHECK; NO ODORS OR DISCREPANCIES NOTED.
Part: WIRE — DISCONNECTED (CABIN) · airframe 21,473 hrs · 11,543 cycles
LAS - FLT 633 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED AND SECURED CONNECTOR AT ROW 2 AND OPERATED NORMALLY. (X)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,412 hrs · 11,513 cycles
SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND WITH BROKEN FASTENERS. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)
Part: WIRE — DISCONNECTED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLT 274, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
ONT - PRIOR TO DEPARTURE OF FLIGHT 447, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)
1999
Part: WIRE — DISCONNECTED (CABIN)
PDX - PRIOR TO DEPARTURE OF FLIGHT 100, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING I NFLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 386, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: SLIDE — WILL NOT TEST (PASSENGER DOOR)
OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)
Part: LAMP — FAILED (ROW 23)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 23 WAS FOUND INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (X)
Part: BATTERY — 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: WIRE — DISCONNECTED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 434, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
LAX - PRIOR TO DEPARTURE OF FLT 559, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLT 444, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
ANC - PRIOR TO DEPARTURE OF FLT 188, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE INOPERATIVE. SECURED CONNECTOR TO LIGHT ASSEMBLY AT ROW 27 AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (ROWS 29-32)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 29 TO 32 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)
Part: BATTERIES — DISCHARGED (ROWS 18-23)
PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 23 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)
Part: WIRE — DISCONNECTED (CABIN)
SMF - AFTER ARRIVAL OF FLIGHT 384, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED WIRING TO LIGHT SOCKET IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLIGHT 463, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 8 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)
Part: BULB — FAILED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT 2 RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE LAMP MODULES AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
PDX - FLT 583 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS IN FIRST CLASS WERE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DAMAGED (CABIN)
SEA - PRIOR TO DEPARTURE OF FLT 264, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)
Part: WIRE — DISCONNECTED (ROW 11)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 9 TO 13 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AT ROW 11 AND OPERATED NORMALLY. (M)
1998
Part: WIRE — DISCONNECTED (CABIN)
PDX - 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: WIRE — DISCONNECTED (ROW 11)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT WERE FOUND INOPERATIVE FROM ROWS 10 THROUGH 13. RECONNECTED WIRING IN FLOOR TRACK AT ROW 11 AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. SECURED CONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: WIRE — LOOSE (CABIN)
SEA - FLT 460 - CREW REPORTED FIRST BANK OF EMEGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
PDX - 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: GUIDE — OUT OF ADJUST (COCKPIT)
SEA - PRIOR TO DEPARTURE OF FLIGHT 198, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WAS BINDING. ADJUSTED WINDOW UPPER GUIDE MECHANISM AND OPERATED NORMALLY. (M)
Part: SLIDE — FAILED (PAX DOOR)
OAK - DURING 15K CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M)
Part: BATTERIES — 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)
1997
Part: WIRE — BROKEN (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 10 TO 13 WERE FOUND INOPERATIVE. REPLACED WIRE SEGMENT IN TRACK ASSEMBLY AND OPERATED NORMALLY. (M)
Part: HOLD OPEN LATCH — LACK OF LUBE (L1 DOOR)
SEA - PRIOR TO DEPARTURE OF FLT 721, CREW REPORTED THE L1 DOOR HOLD OPEN LATCH IS DIFFICULT TO RELEASE. LUBED THE HOLD OPEN LATCH MECHANISM AND OPERATED NORMALLY. (M)
1996
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 10 TO 12 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
1995
Part: EEL ASSY — MALFUNCTIONED (L1 DOOR)
SEA - DURING MAINTENANCE CHECK, THE L1 DOOR PORTABLE EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH UNLESS SWITCH ON LIGHT CYCLED. REPLACED L1 DOOR PORTABLE EMERGENCY EXIT LIGHT AND OPERATED NORMALLY. (W)