N935AS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ALASKA AIR INC (JSFA) | Operator | on 2002-03-17 | 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.
245 reports on file, 1995-02-06 – 2005-08-08.
Part: SKIN — DENTED (FS 503-522)
OKC - FOUND FUSELAGE SKIN IS DENTED. RECON TOURED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FS 636)
OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED SUPPORT. (M)
Part: CLIP — CORRODED (FS 1287)
OKC - DURING C-CHECK, FOUND CARGO TRACK-TO-FRAME TIE DOWN CLIP CORRODED. REPLACED CLIP. (M)
Part: WEB — CORRODED (FS 1155-1211)
OKC - DURING C-CHECK, FOUND AFT CARGO BAY THRESHOLD WEB CORRODED. REPLACED WEB. (M)
Part: SKIN — DENTED (FS 254)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD-WORKED DENT. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FS 1234-1244)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. COLD WORKED DENT. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FS 1271)
OKC - FOUND DURING C-CHECK, FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FS 427)
OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED SUPPORT. (M)
Part: SKIN — DENTED (FS 1322)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: SPACER — CORRODED (FS 375-427)
OKC - DURING C-CHECK, MID CARGO BAY DOOR SILL JAMB BEAM DOUBLER, SPACER, CORRODED. REPLACED SPACER. (M)
Part: SUPPORT — CORRODED (FS 1145)
OKC - DURING C-CHECK, FOUND SUPPORT STRAP CORRODED. REPLACED STRAP. (M)
Part: SKIN — DENTED (FS 1295)
OKC - FOUND DURING C-CHECK, FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: SKIN — DENTED (FS 522-541)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER AND STRAPS. (M)
Part: FLOOR SUPPORT — CORRODED (FS 696)
OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT FITTING CORRODED AND CRACKED. REPLACED SUPPORT FITTING. (M)
Part: SKIN — CANNING (FS 1290)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS `OIL CANNED`. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: SUPPORT BEAM — CORRODED (FS 1155-1212)
OKC - DURING C-CHECK, FOUND AFT CARGO BAY DOOR SUPPORT BEAM CORRODED. REPLACED BEAM. (M)
Part: SKIN — DAMAGED (TE FLAP)
OKC - FOUND DURING C-CHECK, LEFT WING OUTBOARD FLAP T/E OUTER SECTION DAMAGED, DENTED. BOND REPAIRED. (M)
Part: VANE — GOUGED (TE FLAP)
OKC - DURING C-CHECK, FOUND LEFT INBOARD FLAP VANE GOUGED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER AND FILLER. (M)
Part: SKIN — DENTED (FS 1254)
OKC - DURING C-CHECK, FOUND FUSELAGE SKIN IS DENTED. COLD-WORKED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)
Part: FLOOR SUPPORT — CORRODED (FS 617-712)
OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT CORRODED. REPLACED SUPPORT. (M)
Part: ATTACH ANGLE — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND AFT CARGO BAY FRAME ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE. (M)
Part: LONGERON — CORRODED (FS 207-218)
OKC - DURING C-CHECK INSPECTION, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M)
Part: INTERCOSTAL — CORRODED (FS 1164)
OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: INTERCOSTAL — CORRODED (FS 1309-1320)
OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: LONGERON — CORRODED (FS 465-495)
OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REPLACED DAMAGED SECTION. (M)
Part: LONGERON — CORRODED (FS 322-325)
OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M)
Part: LONGERON — CORRODED (FS 207-218)
OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M)
Part: INTERCOSTAL — CORRODED (FS 693-712)
OKC - DURING C-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: LONGERON — CORRODED (FS 294-313)
OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M)
Part: SHEAR TIE — CORRODED (FS 1231)
OKC - DURING C-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M)
Part: LONGERON — CORRODED (FS 729-733)
OKC - DURING C-CHECK, FOUND LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER STRAP AND SHIM. (M)
Part: LONGERON — CORRODED (FS 712)
OKC - FOUND DURING C-CHECK, LONGERON CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR CHANNEL. (M)
Part: ANGLE — CORRODED (FS 1115-1211)
OKC - FOUND DURING C-CHECK, T-ANGLE CHORD ON SUPPORT BEAM CORRODED. REPLAED T-ANGLE. (M)
Part: INTERCOSTAL — CORRODED (FS 1003-1022)
OKC - DURING C-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)
Part: FRAME — CORRODED (FS 1322)
OKC - DURING C-CHECK, FOUND FRAME CORRODED. REPLACED DAMAGED FRAME SECTION. (M)
Part: COALESCER BAG — FAILED (RT A/C PACK)
ATB - FAILED RIGHT AIR CONDITIONING SYSTEM WATER SEPARATOR CAUSED CABIN TO FILL WITH SMOKE. REPLACED WATER SEPARATOR, AND PERFORMED PNEUMATIC DUCTS BURN OUT PROCEDURE. (M)
Earlier reports · 1995–2004 · 209 reports
2004
Part: FLOORBOARD — DELAMINATED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FLOORBOARD IS DELAMINATED AT FS 693-750. REPAIR IAW SRM. (M)
Part: BEAM — CORRODED (CARGO DOOR)
OKC - DURING C-CHECK, FOUND AFT CARGO LOWER DOOR BEAM CORRODED AROUND FORWARD DOOR STOP FITTINGS. REPAIR IAW EA. (M)
Part: LONGERON — CHAFED (FUSELAGE)
OKC - DURING C-CHECK, FOUND RIGHT STATION 1380 LONGERON 17-19R FRAME CHAFED UNDER TUBE CLAMP. REPAIR IAW SRM. (M)
Part: MOUNT — CRACKED (ANTENNA)
OKC - DURING C-CHECK, FOUND .5 INCH CRACK ON MOUNT AREA OF FEED ASSEMBLY RIGHT SIDE OF TAIL CONE. REPAIR IAW EA. (M)
Part: STRUCTURE — BENT (L1 DOOR)
OKC - DURING C-CHECK, FOUND LOWER LEFT EDGE OF L1 DOOR BENT INWARD. REPAIR IAW SRM. (M)
Part: FRAME — DAMAGED (FUSELAGE)
OKC - DURING C-CHECK, FOUND TEMP REPAIR INSTALLED ON FORWARD FRAME AT FS 811. REPAIR IAW SRM. (M)
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)
SEA - DURING LINE CHECK, FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT BOTH LEFT AND RIGHT OVERWING EXITS. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — BROKEN (EMERGENCY LIGHT)
SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE UP TO ROW 7. REPAIRED SHORTED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)
LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 16. REPLACED MISSING MODULE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 1. REPLACED LIGHT MODULE CONNECTOR SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)
2003
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)
OAK LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROWS 19 AND 24. CLEANED ELECTRICAL CONNECTOR IN THE AREA. LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)
SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. SPLICED IN NEW CONNECTOR WIRE AT ROW 1. ALSO, REPLACED BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)
PDX PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)
SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 19. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LANYARD — DISCONNECTED (L1 DOOR SLIDE)
PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: LINE — BLOCKED (NR 1 FIRE BOTTLE)
PDX LINE CHECK, NR 1 FIRE BOTTLE WAS DISCHARGED TO EXTINGUISH APU FIRE. DISCOVERED LINE WAS PARTIALLY BLOCKED WITH DISCHARGE HEAD SHRAPNEL. REPLACED FLEX LINE. (M)
Part: STARTER — FAILED (APU)
PDX - NOTICED SMOKE COMING FROM APU COMPARTMENT. OPENED COMPARTMENT LEFT DOOR AND OBSERVED FLAMES. ACTIVATED BOTH NR 1 AND NR 2 FIRE BOTTLES. SUBMITTERS STATES, THERE WAS DEFINITELY SMOKE, BUT WHETHER THERE WERE ACTUALLY FLAMES IS SOMEWHAT PROBLEMATIC. ENGINEERING SUGGESTS THAT THERE WAS PROBABLY ONLY SMOKE, AND THAT IT WAS DUE TO VAPORIZATION OF THE COIL AND ARMATURE COATINGS, NOT TO FIRE. SUBSEQUENT SHOP INVESTIGATION/REPAIR REVEALED THAT ALL DAMAGE WAS WITHIN THE APU STARTER MOTOR. THE ELECTRICAL LEADS TO THE STARTER WERE NOT DAMAGED, AS WAS FIRST SUSPECTED. THE STARTER MOTOR WAS REPAIRED BY REPLACING THE COIL AND ARMATURE, AND THE UNIT RETURN TO SEVICEABLE SPARES. (M)
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
PREFLIGHT CHECK, FORWARD RIGHT SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)
AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND LONGERON 28L IS CORRODED AT FLANGE OF REPAIR SPLICE. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM. (M)
Part: INTERCOSTAL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND L1 DOOR HANDLE SUPPORT BOX AFT INTERCOSTAL CRACKED. REPLACED DAMAGED INTERCOSTAL PER SRM. (M)
Part: SEAT TRACK — WORN (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FIRST OFFICER UPPER SEAT TRACKS WORN. REPLACED SEAT TRACKS PER SRM. (M)
Part: FRAME — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FRAME AT FS 83.5 CRACKED AT RBL 9. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CORROSION ON CENTER PANEL MOUNTING SUPPORT. REPLACED FLOOR PANEL MOUNTING SUPPORT. (M)
Part: SUPPORT — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND TAIL CONE RELEASE PANEL SUPPORT ARM CRACKED. APPLIED FIBERGLASS OVERLAY TO SUPPORT ARM PER SRM. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO TRACK CORROSION AT FASTENER HOLES. REPLACED DAMAGED TRACK PER SRM. (M)
Part: ANGLE — CORRODED (GIRT BAR)
OKC - DURING 30K CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR ESCAPE SLIDE GIRT BAR FITTING FORWARD MOUTN ATTACH ANGLE. REPLACED ATTACH ANGLE PER SRM. (M)
Part: FLOORBOARD — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND MID CARGO FLOORBOARD PUNCTURED AND CORRODED AT FASTENER HOLES. REPLACED FLOOR PANEL PER SRM. (M)
Part: ATTACH FITTING — GOUGED (LT TE FLAP)
OKC - FOUND DURING 30K CHECK, LEFT OUTBOARD FLAP HINGE ATTACH LUG IS GOUGED. BLENDED PER ASA EA 5750-01803. (M)
Part: FRAME — DAMAGED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FRAME FLANGE HAS TOOL DAMAGE AT FASTENER HOLES. REPLACED DAMAGED FRAME PER SRM. (M)
Part: CAP — GOUGED (RT WING LE)
OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE END CAP GOUGED. BLENDED, PERFORMED WELD REPAIR PER EA 5740-01344. (M)
Part: CARGO TRACK — DAMAGED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND MID CARGO TRACK LEFT SIDE LOWER SURFACE HAS FASTENER WITH SHORT EDGE MARINE. INSTALLED SPLICE PLATE ON CARGO TRACK. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND SHEAR TIE CORRODED. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR SPLICE PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CENTER FLOOR PANEL SUPPORT CORROSOIN. REPLACED SUPPORT PER SRM. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN SEAT TRACK CORROSION AT FASTENERS. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM. (M)
Part: SKIN — DAMAGED (FUSELAGE)
OKC - DUIRNG 30K CHECK, FOUND FUSELAGE SKIN DAMAGED BETWEEN LONGERONS 19R AND 20R AT STATION 365. INSTALLED REPAIR DOUBLER PER SRM. (M)
Part: VANE — DENTED (LE FLAP)
OKC - DURING 30K CHECK, FOUND RIGHT FLAP VANE DENTED ON LEADING EDGE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM. (M)
Part: INTERCOSTAL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO AREA INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL PER SRM. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR SUPPORT CRACKED. REPLACED DAMAGED CABIN FLOOR SUPPORT PER SRM. (M)
Part: CHANNEL — CRACKED (SUBFLOOR)
OKC - DURING 30K CHECK, FOUND RIGHT SUB FLOOR U-CHANNEL IS CRACKED. FABRICATED AND REPLACED U-CHANNEL PER SRM. (M)
Part: VANE — DENTED (TE FLAP)
OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP VANE DENTS ON INBOARD END. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER SRM. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO AREA LONGERON 30 CORRODED ON UNDERSIDE OF FLANGE. REPAIRED LONGERON 30 PER SRM. (M)
Part: ANGLE — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FORWARD CARGO DOOR FORWARD ANGLE IN CENTER FORWARD EDGE IS CRACKED. REMOVED AND REPLACED DAMAGED ANGLE PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, AFT CARGO AREA HAS CORRODED SHEAR TIE. REPLACED SECTION OF DAMAGED SHEAR TIE PER SRM. (M)
Part: STEP — CRACKED (AIRSTAIR)
OKC - FOUND DURING 30K CHECK, AFT ENTRY STAIRS HAVE CRACK ON LOWER STEP. BLENDED OUT CRACKS PER SRM. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND LONGERON AND 29R AFT OF STATION 579 HAVE CORROSION AROUND FASTENERS. REMOVED DAMAGED DOUBLER. INSTALLED NEW REPAIR DOUBLER AND STRAP PER ASA EA 5330-01195. (M)
Part: VANE — DENTED (RT TE FLAP)
OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP VANE DENTED ON OUTBOARD END LOWER SURFACE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM. (M)
Part: FRAME — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO AREA HAS FRAME CORRODED. REMOVED FRAME CORROSION AND INSTALLED REPAIR ANGLES PER SRM. (M)
Part: SKIN — GOUGED (VERTICAL STAB)
OKC - DURING 30K CHECK, FOUND RUDDER LEADING EDGE UPPER SKIN GOUGED AND CREASED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM. (M)
Part: GUARD — CRACKED (LT MLG)
OKC - DURING 30K CHECK, FOUND LEFT MLG SPLASH GUARD CRACKED AT WELD. REPLACED WELDED AREA PER MM PROCEDURES. (M)
Part: HINGE FITTING — CORRODED (RT TE FLAP)
OKC - DURING 30K CHECK, FOUND RIGHT WING FLAP HOLE FOR BEARING ASSEMBLY IS CORRODED. REMOVED CORROSION. INSTALLED REPAIR SLEEVE AND BUSHING PER EA 5750-01796. (M)
Part: PANEL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND RIGHT FUSELGAE AFT PANEL NR 2207 IS CRACKED AT THE FORWARD END. REPAIRED PANEL WITH BONDED FIBERGLASS OVERLAY PER SRM. (M)
Part: WEB — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FORWARD CARGO AREA LEFT CUSP WEB CRACKED. REPLACED CUSP WEB PER SRM. (M)
Part: MOUNT — GOUGED (PANEL)
OKC - FOUND DURING 30K CHECK, RIGHT WING NR 1 INBOARD SLAT CLOSE OUT MOUNT BROKEN. REPLACED BRACKET PER SRM. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, STATION 1015 LONGERON 30 CORROSION AT FASTENER HOLES. SPOT FACED CORROSION PER EA 5310-02158. (M)
Part: CHANNEL — PUNCTURED (HORIZONTAL STAB)
OKC - DURING 30K CHECK, FOUND RIGHT HORIZONTAL STABILIZER AFT SPAR HINGE CHANNEL SUPPORT PUNCTURED. REPLACED DAMAGED CHANNEL PER SRM. (M)
Part: FLOOR PANEL — BROKEN (FS)
OKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS BROKEN END AT FS 924-1004. BONDED DAMAGED AREA WITH FIBERGLASS CLOTH AND EPON 828 RESIN PER SRM 51-70-3. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CENTER FLOOR SUPPORT CORRODED AT FS 200. REPLACED SUPPORT PER SRM 53-01. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, RIGHT FORWARD FLOOR PANEL SUPPORT IS CORRODED AT FS 180. REPLACED SUPPORT TRACK PER SRM 51-30-2 AND 30-5. (M)
Part: ATTACH ANGLE — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND GILLINER ATTACH ANGLE IS CRACKED AT FS 617. REPAIRED CRACKED ANGLE WITH COLD BOND FIBERGLASS OVERLAY PER SRM 51-70-1. (M)
Part: CHANNEL — CHAFED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND APU SHROUD RIGHT AFT HAT CHANNEL FRETTING AT FS 1361-1390. REMOVED DAMAGED SECTION AND REPAIRED WITH FILLER AND DOUBLER PER SRM 51-70-5. (M)
Part: PANEL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND RIGHT FUSELAGE AFT PANEL 2207 IS CRACKED AT THE FORWARD END. REPAIRED PANEL WITH FIBERGLASS OVERLAY PER SRM 51-70-1. (M)
Part: DOOR — CORRODED (MLG)
OKC - OFUND DURING 30K CHECK, LEFT MLG STRUT DOOR IS CORRODED ON LOWER OUTER SURFACE. REMOVED DAMAGED SECTION AND INSTALLED BONDED ALUMINUM FILLER AND DOUBLER PER EA 3110-01126. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO BAY TRACK CORRODED AT FS 1007-1155. REPLACED TRACK PER SRM 51-30-1. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200. REPLACED SUPPORT PER SRM 53-01. (M)
Part: CARGO TRACK — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND MID CARGO BAY TRACK IS CORRODED AT FS 588-636. REPLACED DAMAGED SECTION OF TRAKC PER SRM 53-05. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, RIGHT FORWARD FLOOR PANEL SUPPORT CORRODED AT FS 200. REPLACED SUPPORT PER SRM 53-01. (M)
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS SEVERAL LOOSE OR MISSING INSERTS AT FS 1155-1250. REPLACED PANEL PER SRM 53-05. (M)
Part: FLOOR PANEL — CRUSHED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS CRUSHED AREA AT FS 259-313. REPLACED PANEL PER SRM 53-05. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FLOOR PANEL IS CORRODED AT FS 148-200. REPLACED PANEL PER SRM 53-01. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, FORWARD FLOOR SUPPORT CORRODED AT FS 160-200. REPLACED SUPPORT PER SRM 53-01. (M)
Part: FITTING — CORRODED (GIRT BAR)
OKC - DURING 30K CHECK, LEFT FORWARD PASSENGER L-1 DOOR EMERGENCY SLIDE GIRT BAR AFT FLOOR FITTING IS CORRODED AT FS 180. REPLACED FITTING PER SRM 53-01. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FLOOR PANEL MOUNTING SUPPORT TRACK IS CORRODED AT FS 160-200. REPLACED SUPPORT TRACK PER SRM 53-01. (M)
Part: STRUCTURE — CHAFED (TE FLAP)
OKC - DURING 30K CHECK, FOUND LEFT FLAP MID VANE OUTBOARD UPPER TRAILING EDGE CHAFED. REPAIRED CHAFED AREA PER SRM 51-70-2. (M)
Part: STRAP — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FRAME SUPPORT (STRAP) IS CORRODED AT FS 1127. REPLACED FRAME PER SRM 51-10-4 AND 30-5. (M)
Part: BRACKET — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT SERVICE (L-2) DOOR EMERGENCY SLIDE AFT GIRT BAR FLOOR BRACKET IS CORRODED. REPLACED BRACKET PER SRM 53-01. (M)
Part: DOOR FRAME — GOUGED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, AFT PASSENGER DOOR LOWER FRAME HAS GOUGES. REPLACED FRAME PER SRM 52-01. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND MID CARGO BAY CENTER FLOOR PANEL ATTACH ANGLE IS CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-2 AND 30-2. (M)
Part: FRAME — WORN (FUSELAGE)
OKC - FOUND DURING 30K CHECK, FRAME SEVERLY WORN AT FS 636. INSTALLED FILLER, ANGLE, AND PLATE ON FRAME PER SRM 53-03. (M)
Part: SKIN — DEBONDED (SPOILER)
OKC - DURING 30K CHECK, FOUND RIGHT WING GROUND SPOILER IS DISBONDED. REMOVED DAMAGED AREA AND REBONDED WITH FIBERGLASS PER SRM 51-70-1B. (M)
Part: FITTING — BROKEN (FUSELAGE)
OKC - FOUND DURING 30K CHECK, LEFT OVERHEAD STOWAGE BIN MOUNT FITTING IS BROKEN. REPLACED MOUNT FITTING PER MM 20-10-12 AND 30-01. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, FORWARD CENTER FLOOR PANEL MOUNTING SUPPORT IS CORRODED AT FS 200. REPLACED SUPPORT PER SRM 51-30-5. (M)
Part: SKIN — CRACKED (LT WING LE)
OKC - DURING 30K CHECK, FOUND LEFT WING LEADING EDGE CRACKED JUST OUTBOARD OF VORTILON. INSTALLED SPLICE PER SRM 51-10-2, 10-4, 30-2 AND 30-5. (M0
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND SEAT TRACK UPPER SURFACE INCLUDING INBOARD AND OUTBOARD FLANGES ARE CORRODED. REPLACED DAMAGED TRACK SECTION PER SRM 53-05. (M)
Part: FLOOR PANEL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FLOOR PANEL IS CRACKED AT FS 731-786.5. REPLACED PANEL PER SRM 51-10-2, 10-3, AND 10-4. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS CORRODED INSERTS AT FS 1079-1117. REPLACED PANEL PER SRM 53-05. (M)
Part: FLOOR PANEL — DEBONDED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL IS MISSING SEVERAL INSERTS REPLACED PANEL PER SRM 53-05. (M)
Part: FLOOR PANEL — BROKEN (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FLOOR PANEL HAS BROKEN INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53-05. (M)
Part: DOOR — CRACKED (CARGO BARRIER)
OKC - DURING 30K CHECK, FOUND FORWARD CARGO BAY BARRIER DOOR IS CRACKED. REPAIRED CRACKS WITH BONDED 7075-T6 FILLER AND DOUBLER PER SRM 51-70-2. (M)
Part: SUPPORT ANGLE — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO BAY SUPPORT ANGLE CORRODED AT FS 1218. REPLACED ANGLE PER SRM 51-30-5 AND 53-14-3. (M)
Part: PANEL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND COCKPIT LT SIDE PANEL IS CRACKED. REINFORCED PANEL WITH BONDED FIBERGLASS DOUBLER PER MM 25-00-00. (M)
Part: DOOR — PUNCTURED (CARGO BARRIER)
OKC - DURING 30K CHECK, FOUND MID CARGO BAY BARRIER DOOR IS PUNCTURED ON INNER FACE. REPAIRED WITH BONDED 7075-T6 FILLER AND DOUBLER PER SRM 51-70-2. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, FLOOR PANEL IS CORRODED ON UPPER SURFACE AT FS 1022. REMOVED CORROSION AND INSTALLED DOUBLER AND HAT CHANNEL PER SRM 51-30-2 AND 53-05. (M)
Part: FLOOR PANEL — WORN (FUSELAGE)
OKC - DURING 30K CHECK, FOUND RIGHT FLOOR PANEL UPPER SURFACE IS WORN TO METAL. REPLACED PANEL PER SRM 53-05. (M)
Part: SKIN — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND RIGHT FLOOR PANEL UPPER SKIN IS CRACKED AT AFT FASTENER HOLE. INSTALLED DOUBLER PER SRM 53-05. (M)
Part: FLOOR PANEL — GOUGED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND MID CARGO BAY FLOOR PANEL IS GOUGED IN SEVERAL PLACES ALONG EDGE. REPLACED PANEL PER SRM 51-10-2 AND 10-4. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO BAY FLOOR PANEL IS DELAMINATED, PUNCTURED, AND CORRODED ON TOP AND BOTTOM SIDES. REPLACED PANEL PER SRM 51-10-2, 10-3, AND 10-4. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL SUPPORT HAT CHANNEL IS CORRODED AT FS 1098-1211. REPLACED SUPPORT PER SRM 51-10-2, 10-3, 10-4 AND 30-1. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN PANEL HAS CORRODED/MISSING INSERTS AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05 AND 53-24-0. (M)
Part: BRACKET — CRACKED (FLOOR SUPPORT)
OKC - DURING 30K CHECK, FOUND CABIN FLOORBEAM STIFFENER BRACKET IS CRACKED AT CUSP LINE AT FS 503. REPLACED STIFFENER, ANGLE, PER SRM 51-10-4 AND 30-5. (M)
Part: ATTACH ANGLE — CRACKED (FS)
OKC - DURING 30K CHECK, FOUND FORWARD CARGO BAY BULKHEAD LOWER GILINER ATTACH ANGLE IS CRACKED AT FS 218. STOP DRILLED CRACK AND INSTALLED STACKED DOUBLER AND TRIPLER PER SRM 53-01. (M)
Part: WEB — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, RIGHT CUSP WEB IS CRACKED AT FS 218. REPLACED CUSP WEB PER SRM 51-10-2, 10-4, 30-2, AND 30-5. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL SUPPORT IS CORRODED AROUND FASTENER HOLES AT FS 237. REPLACED SUPPORT PER SRM 51-10-2, 10-3, 10-4, AND 30-5. (M)
Part: FLOOR PANEL — PUNCTURED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND LEFT FLOOR PANEL SURFACE IS PUNCTURED AT FS 408. REPLACED FLOOR PANEL PER SRM 53-20-1, AND 53-05. (M)
Part: WEB — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND LEFT CUSP WEB UPPER SURFACE CORRODED AT FS 1250. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4. (M)
Part: SKIN — SCRATCHED (NR 1 SLAT)
OKC - DURING 30K CHECK, FOUND RIGHT NR 1 SLAT LEADING EDGE IS SCRATCHED. REMOVED SCRATCHES AND INSTALLED DOUBLER PER SRM 57-09. (M)
Part: FRAME — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FRAME CRACKED AT FS 83.5. STOP DRILLED CRACK, AND INSTALLED DOUBLER PER SRM 53-03. (M)
Part: WEB — CHAFED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND WEB IS CHAFED AT AFT END OF RIGHT NLG DOOR. MATERIAL LOSS IS IN EXCESS OF 20 PERCENT. REPLACED NLG DOOR JAMB GUSSET PER SRM 51-10-2, 10-4, 30-2, AND 30-5. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, LEFT FORWARD FLOOR SUPPORT CORRODED. REPLACED DAMAGED FLOOR SUPPORT PER SRM 51-10-2, 10-3, 30-2 AND 53-14-1. (M)
Part: FRAME — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FRAME CRACKED IN FIVE PLACES AT FS 83. REPLACED FRAME PER SRM 51-10-4, 30-2, AND 30-5. (M)
Part: FLOOR PANEL — BROKEN (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED DAMAGED FLOOR PANEL PER SRM 53-05. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, SEAT TRACK SECTION IS CORRODED. REPLACED DAMAGED SECTION PER SRM 53-05. (M)
Part: SUPPORT BRACKET — CRACKED (MLG WW)
OKC - FOUND DURING 30K CHECK, LEFT MLG WHEEL WELL HYDRAULIC LINE SUPPORT BRACKET CRACKED. REPLACED BRACKET PER MM 20-30-01. (M)
Part: PANEL — CRACKED (AILERON HINGE)
OKC - FOUND DURING 30K CHECK, RIGHT AILERON HINGE PANEL NR 3 IS CRACKED AT DRAIN HOLE. STOP DRILLED CRACK AND VERIFIED CONTAINMENT BY EDDY CURRENT INSPECTION PER SRM 51-01. (M)
Part: SUPPORT FITTING — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND AFT CARGO BAY BARRIER DOOR AFT NET SUPPORT FITTING IS CRACKED. REPLACED SUPPORT FITTING PER SRM 51-10-4 AND 51-30-1. (M)
Part: DOOR — CRACKED (MLG)
OKC - FOUND DURING 30K CHECK, LEFT MLG DOOR AFT OUTBOARD CORNER WAS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. (M)
Part: SUPPORT — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, RIGHT MLG DOOR WHEEL BUMPER SUPPORT CRACKED. REPLACED BUMPER SUPPORT PER MD-80 SB 32-197. (M)
Part: WEB — CHAFED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND WEB IS CHAFED AT AFT END OF LEFT NLG DOOR. MATERIAL LOSS IS IN EXCESS OF 20 PERCENT. REPLACED NLG DOOR JAMB GUSSET PER SRM 51-10-2, 10-4, 30-2 AND 30-5. (M)
Part: INTERCOSTAL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND FORWARD LEFT PAX ENTRANCE INTERCOSTAL CRACKED INBOARD OF HOLD-OPEN HANDLE RELEASE. REPLACED RELEASE (CLIP) PER SRM 51-30-2 AND 51-30-5. (M)
Part: DOOR — CRACKED (MLG)
OKC - DURING 30K CHECK, RIGHT MLG DOOR AFT OUTBOARD CORNER CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05. (M)
Part: SILL — CRACKED (FUSELAGE)
OKC - DURING 30K CHECK, FORWARD CARGO BAY DOOR JAMB SILL PLATE EDGE CRACKED. STOP DRILLED CRACK AND INSTALLED PLUG RIVET PER SRM 51-01. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, CABIN FLOOR PANEL TO HAVE 16 CORRODED INSERTS FROM FS 160-180. REPLACED FLOOR PANEL PER SRM 53-05. (M)
Part: LONGERON — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, SECTION ON LONGERON CORRODED IN AFT CARGO BAY AT FS 1255. REPLACED DAMAGED SECTION OF LONGEORN PER SRM 51-30-5 AND 53-02. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - DURING 30K CHECK, FOUND CABIN FLOOR PANEL FOND TO HAVE 4 CORRODED INSERTS FROM FS 110-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, SEAT TRACK CORROSION AT FS 200-255. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-05. (M)
Part: FLOOR PANEL — CORRODED (FUSELAGE)
OKC - FOUND DURING 30K CHECK, CABIN FLOOR PANEL TO HAVE 16 CORRODED INSERTS FROM FS 160 TO 200. REPLACED FLOOR PANEL PER SRM 53-05. (M)
Part: BRACKET — CRACKED (FUSELAGE FRAME)
OAK - FOUND DURING C-CHECK, FORWARD SERVICE DOOR FORWARD UPPER CORNER FRAME SUPPORT BRACKET CRACKED. FABRICATED AND REPLACED BRACKET PER SRM 51-30-5, 51-10-3, AND DAC DWG 9911579. (M)
Part: BRACKET — CRACKED (FUSELAGE FRAME)
OAK - FOUND DURING C-CHECK, FORWARD SERVICE DOOR AFT UPPER CORNER FRAME SUPPORT BRACKET CORRODED. FABRICATED AND REPLACED BRACKET PER SRM 51-30-5, 51-10-3, AND DAC DWG 9911579. (M)
Part: RETAINER — CRACKED (DOOR SEAL)
OAK - DURING C-CHECK, AFT CARGO DOOR FORWARD SEAL RETAINER AT CAM IS CRACKED. FABRICATED AND REPLACED RETAINER PER SRM 51-30-5, 51-10-2, AND 51-10-3. (M)
Part: SKIN — GOUGED (FUSELAGE)
OAK - DURING C-CHECK, FOUND FUSELAGE SKIN CREASED/GOUGED AT FS 1485-1497. BLENDED CREASED/GOUGED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M)
Part: PANEL — CHAFED (MLG WW)
OAK - FOUND DURING C-CHECK, MLG WHEELWELL CUTOUT OUTBOARD AFT PANEL IS CHAFED BEYOND LIMITS. INSTALLED 7075-T6 DOUBLER PER SRM 57-01. (M)
2002
Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)
DURING PREFLIGHT CHECK, L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD.
Part: BATTERY PACK — DISCHARGED (CABIN)
SAN - DURING PREFLIGHT CHECK, FOUND THAT EXTERNAL EMERGENCY LIGHTS INOPERATIVE FORWARD OF ROW 10. REPLACED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M)
Part: WIRE — DAMAGED (CABIN)
RNO - DURING PREFLIGHT CHECK, ONE EMERGENCY TRACK LIGHT AT ROW 6 WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: SLIDE — FAILED (TAILCONE)
OAK - DURING LINE CHECK, THE TAILCONE WAS INADVERTENTLY RELEASED, AND WAS DAMAGED AS A RESULT OF THE FALL. THE AFT EMERGENCY ESCAPE SLIDE, RIGGED TO AUTOMATICALLY DEPLOY UPON TAILCONE RELEASE, DID NOT DEPLOY. INSPECTION OF THE ESCAPE SLIDE PACK AND ITS RIGGING REVEALED NO ANOMALIES WHICH MIGHT ACCOUNT FOR THE NON-DEPLOYMENT. THE DAMAGED TAILCONE WAS REPLACED AND THE SLIDE RE-RIGGED. THE SLIDE WAS SUBSEQUENTLY REMOVED FOR OVERHAUL ON NOV 12. (M)
2001
Part: WIRE — BROKEN (CABIN)
LAX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING AT ROW 9 WAS DETERMINED TO BE INOPERATIVE. REPAIRED BROKEN CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)
Part: MODULE — DAMAGED (CABIN)
SEA - DURING PRE-FLIGHT CHECK, ROW 6 TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED MODULE AT ROW 6. LIGHTS THEN OPERATED PROPERLY. (M)
Part: HARNESS — FAILED (EVAC SLIDE)
OAK - DURING C-CHECK, AFT (REAR) DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED OK. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING LINE CHECK, ROW 1-3 TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M)
Part: WINDOW (COCKPIT)
SEA - DURING PREFLIGHT CHECK, FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS DIFFICULT TO OPEN. TIGHTENED LOOSE SLIDE AT UPPE AFT LOCATION. WINDOW THEN OPERATED PROPERLY. (M)
Part: LANYARD — DETACHED (SERVICE DOOR)
PHX - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM DOOR. REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER. (M)
Part: DOOR — OUT OF ADJ (ENTRANCE)
SEA - DURING LINE CHECK, FORWARD ENTRY L1 DOOR WAS DETERMINED TO BE HARD TO CLOSE WITH EXTERIOR HANDLE. REMOVED CENTER LINER. ADJUSTED DOOR PER MM 52-11-00. REINSTALLED LINER. DOOR LEAKED CHECKED OK. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING LINE CHECK, PORTABLE EMERGENCY LIGHT WAS DETERMINED TO BROKEN. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M)
2000
Part: BATTERY PACK — DISCHARGED (COCKPIT)
SEA - DURING PREFLIGHT, COCKPIT OVERHEAD EMERGENCY LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED BATTERY ASSEMBLIES. LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING LINE CHECK, 1ST CLASS CABIN EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY ASSEMBLIES. LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, INTERIOR EMERGENCY OVERHEAD LIGHTS AT AFT GALLEY AND AT SEAT ROW 30 WERE DETERMINED TO BE INOPERATIVE. REPLACED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE MIDDLE EMERGENCY LIGHT OVER THE TAILCONE CATWALK WAS FOND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M)
Part: SEAL — CONTAMINATED (L1 DOOR)
SEA-THE L1 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. INSPECTED THE L1 DOOR AND CLEANED THE LOWER SEAL AREA. TEH DOOR OPERATED NORMALLY.
Part: BATTERY — DISCHARGED (ROW 1 - 17)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 1-7 AND 13-17 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERIES AT AFFECTED LOCATIONS AND ALL LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
OAK - DURING C-CHECK, THE OVERHEAD EMERGENCY LIGHT IN THE FLIGHT COMPARTMENT WAS FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLYS AND OPERATED NORMALLY. (M)
Part: DOOR FRAME — MISREPAIRED (SERVICE DOOR)
OAK - DURING C-CHECK, THE L2 DOOR WAS DIFFICULT TO LOCK CLOSED. REMOVED EXCESS AERODYNAMIC FILLER FROM DOOR FRAME AND OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - AFTER ARRIVAL OF FLIGHT 557 - CREW REPORTED THE OVERHEAD EMERGENCY LIGHT IN THE FLIGHT COMPARTMENT WAS INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: WINDOW — STUCK (COCKPIT)
SEA - FLT 9300 - CREW REPORTED CAPTAINS SLIDING WINDOW DIFFICULT TO OPERATE. ADJUSTED SLIDING WINDOW PER THE MM AND OPERATED NORMALLY. (M)
Part: BRACKET — OUT OF POSITION (RUDDER)
SEA - DURING INSPECTION WHEN THE BELLOWS WERE EXTENDED AND THE RUDDER LIMITER HOOK ROTATED INTO THE HIGH-SPEED RUDDER LIMIT POSITION, THE PROX SENSOR SUPPORT BRACKET MOVED VERY CLOSE TO THE BELLOWS PUSHROD. REWORKED SURFACE OF CORNER SUPPORT BRACKET AND REPAIRED PER EA 2720-01034. (M)
Part: SKIN — GOUGED (VERTICAL STAB)
SEA - DURING INSPECTION, A GOUGE DAMAGE WAS NOTED ON THE LEFT SKIN OF THE VERTICAL STABILIZER TIP. REPAIRED SKIN PER EA 5530-01055. (M)
Part: BEARING — WORN (ELEVATOR)
SEA - DURING INSPECTION, THE LEFT GEARED TAB HINGE FITTING BEARINGS WERE FOUND TO BE WORN. REPLACED HINGE FITTINGS PER EA 5520-01077. (M)
Part: SUPPORT BRACKET — CRACKED (FAIRING)
SEA - DURING INSPECTION, THE RIGHT HORIZONTAL FAIRING SUPPORT WAS FOUND WITH A SMALL CRACK EMANATING FROM AN ELONGATED NUTPLATE HOLE ON THE UPPER SECTION OF THE SUPPORT. REPAIRED PER EA 5510-01094. (M)
Part: PLATE — LOOSE (TAIL CONE)
SEA - DURING INSPECTION, THE SHEAR PIN PLATE ATTAHED TO THE RADIAL FRAME OF THE TAILCONE WAS FOUND LOOSE AT THE 10 O''CLOCK POSITION. UPON REMOVAL OF THE PLATE, MAINTENANCE FOUND THE TWO ATTACHING HOLES ON BOTH SIDES OF THE MAIN ALIGNMENT PIN HOLE WERE ELONGATED. REPAIRED PER EA 5350-01067. (M)
Part: SUPPORT BRACKET — DAMAGED (HORIZONTAL STAB)
SEA - DURING MAINTENANCE INSPECTION, THE RIGHT SUPPORT FOR THE HORIZONTAL STABILIZER FAIRING WAS FOUND WITH AN OBLONG HOLE AT THE NUTPLATE. REPAIRED PER EA 5510-01094. (M)
1999
Part: MECHANISM — LACK OF LUBE (L1 DOOR)
SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO BE VERY HARD TO CLOSE AND LATCH FROM THE OUTSIDE. LUBRICATED AND DOOR OPERATED NORMALLY. (M)
Part: HINGE PIN — LOOSE (LT COCKPIT)
PDX - AFTER ARRIVAL OF FLT 711 - CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM CAME APART. REINSERTED THE WINDOW MECHANISM HINGE PIN AND OPERATED NORMALLY. (M)
Part: TRACK — LOOSE (LT COCKPIT)
SEA - AFTER ARRIVAL OF FLIGHT 223, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WS DIFFICULT TO OPEN. TIGHTENED THE UPPER WINDOW TRACK SCREWS AND SECURED THE AFT WINDOW MOLDING AND OPERATED NORMALLY. (M)
Part: MECHANISM — LACK OF LUBE (L1 DOOR)
SEA - AFTER ARRIVAL OF FLIGHT 160, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. CLEANED AND LUBRICATED DOOR BAYONET CAM AND FOLLOWER ASSEMBLY AND OPERATED NORMALLY. (M)
Part: FAN — FAILED (CARGO COMPT)
LAX - AIR TURN BACK OF FLIGHT 559, FLIGHT ATTENDANT REPORTED SMOKE/ODOR IN THE REAR OF THE CABIN ON TAKEOFF. FOUND THE AIR CONDITIONING RECIRCULATION FAN CIRCUIT BREAKERS POPPED. REPLACED THE FAN AND FILTER AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (L1 DOOR)
SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT CLOSE FROM OUTSIDE. RERIGGED THE L1 DOOR IAW DC9 MM AND OPERATED NORMALLY. (M)
Part: SKIN — DENTED (FUSELAGE)
LCQ - DURING 15K CHECK, DENT WAS FOUND IN FUSELAGE SKIN AT FS 229. REPAIRED IAW ASA EA 5330-01363. (M)
1998
Part: HOLD OPEN HOOK — MALFUNCTIONED (L1 DOOR)
SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS DIFFICULT TO UNLATCH FROM THE FULL OPEN POSITION. ADJUSTED THE DOOR HOLD OPEN MECHANISM AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (L1 DOOR)
PDX - DURING MAINTENANCE CHECK, THE L1 DOOR BAYONET DID NOT LOCK THE HINGE FROM ROTATING. ADJUSTED THE L1 DOOR ROTATION ROD AND OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (LT COCKPIT)
SEA - AFTER ARRIVAL OF FLT 92, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WAS DIFFICULT TO OPEN. ADJUSTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM, REPOSITIONED SIDEWALL PANEL AND WINDOW TRIM AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (LT COCKPIT)
SEAT - PRIOR TO DEPARTURE OF FLT, 539, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WAS DIFFICULT TO OPEN. ADJUSTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (LT COCKPIT)
SFO - PRIOR TO DEPARTURE OF FLT 349, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. LUBRICATED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M)
Part: MECHANISM — OUT OF ADJUST (LT COCKPIT)
SEA - AFTER ARRIVAL OF FLT 349, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M)
Part: TRIM — OUT OF ADJUST (L1 DOOR)
SEA - AFTER ARRIVAL OF FLT 196, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. TRIMMED FORWARD UPPER CORNER OF DOOR TRIM AND OPERATED NORMALLY. (M)
1997
Part: MECHANISM — OUT OF ADJUST (L1 DOOR)
SEA - AFTER ARRIVAL OF FLIGHT 442, CREW REPORTED THE L1 DOOR HANDLE DOES NOT OPERATE SMOOTHLY FROM INSIDE. ADJUSTED VERTICAL POSITION OF DOOR AND OPERATED NORMALLY. (M)
Part: BAYONET — BINDING (L1 DOOR)
SEA - AFTER ARRIVAL OF FLT 88; CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. REPLACED THE L1 DOOR BAYONET OPERATING CRANK ASSEMBLY, CLEANED SEALS, AND LUBRICATED DOOR MECHANISM, OPERATED NORMALLY. TT: 35,641 HOURS. TC: 23, 295. (X)
Part: CABIN — INOPERATIVE (CABIN)
LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
Part: LATCH MECHANISM — OUT OF ADJUST (LT COCKPIT)
SEA - PRIOR TO DEPARTURE OF FLT 501 - CREW REPORTED THE FLT COMPARTMENT LT SLIDING WINDOW WOULD NOT LATCH CLOSED. ADJUSTED THE LT SLIDING WINDOW LATCH MECHANISM AND OPERATED NORMALLY. (M)
Part: DOOR MECHANISM — OUT OF ADJUST (L1 DOOR)
SEA - FLT 451 - CREW REPORTED L1 DOOR WAS DIFFICULT TO OPEN. RIGGED L1 DOOR AND DOOR OPERATED NORMALLY. (M)
Part: ROLLERS — REQ'D LUBE (L1 DOOR)
PDX - AFTER ARRIVAL OF FLIGHT 561, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. LUBED DOOR ROLLERS AND OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM THE CLASS DIVIDER TO ROW 9 WERE FOUND INOPERATIVE. REPAIRED WIRING AND TRACK AT THE CLASS DIVIDER AND LIGHTS OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)
1996
Part: SKIN — OVERSIZED (L1 DOOR)
PDX - AFTER ARRIVAL OF FLT 482 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND L1 DOOR OUTER SKIN CONTACTING DOOR FRAME. TRIMMED DOOR SKIN AND OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)
Part: WIRE — BROKEN (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 6 AND OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (X)
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: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)
1995
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X)
Part: BRAKE ASSY — WORN (NR 1 MLG WHEEL)
LAX - FLT 256 - AFTER ARRIVAL, CREW REPORTED THE BRAKES FADED DURING LANDING ROLL-OUT AND TAXI. REPLACED NR 1 AND NR 3 BRAKE ASSEMBLIES AND BLED NR 2 AND NR 4 BRAKE HYDRAULIC SYSTEMS. TAC: 06465. REFERENCE, OPERATOR CONTROL NR 95ZZZX6425A. (X)
Part: BRAKE ASSY — WORN (NR 3 MLG WHEEL)
LAX - FLT 256 - AFTER ARRIVAL, CREW REPORTED THE BRAKES FADED DURING LANDING ROLL-OUT AND TAXI. REPLACED NR 1 AND NR 3 BRAKE ASSEMBLIES AND BLED NR 2 AND NR 4 BRAKE HYDRAULIC SYSTEMS. TAC: 02066. REFERENCE, OPERATOR CONTROL NR ASAA9580270. (X)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS 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 LIGHTS OPERATED NORMALLY. (M)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL BATTERIES — DISCHARGED (CABIN)
PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND DIM. REPLACED THE FORWARD AND AFT BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL BATTERIES — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY AND FORWARD GALLEY AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL PORTABLE — DEFECTIVE (CABIN)
PAE - DURING 30K CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)
Part: CARGO TRACK — CORRODED (BS 218-370)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y218 TO Y370, X-14, Z-44. REPLACED CARGO TRACK IAW DC-9 SRM 53-05. (M)
Part: LONGERON — CORRODED (BS 692-694)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29L AT Y692 TO Y694, X PLUS 7, Z MINUS 49. REMOVED CORROSION AND INSTALLED REPAIR IAW DC-9 SRM 53-01, 51-10-03, 51-10-01, 53-14-02, 53-02. (M)
Part: CARGO TRACK — CORRODED (BS 1007-1155)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1007 TO Y1155, X-15, Z-45. REPLACED CARGO TRACK IAW DC-9 SRM 51-10-03, 51-30-02, 51-30-01. (M)
Part: FITTING — CORRODED (BS 1214-1216)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON MOUNT BRACKET AT Y1214 TO Y1216, X-4. REPLACED BRACKET IAW DC-9 SRM 51-10-01 AND 51-30-01. (M)
Part: FRAME — CORRODED (BS 1250)
PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1250, X-7 TO X PLUS 16, Z-45. REPLACED FRAME IAW DC-9 SRM 51-10-03 AND 53-03. (M)
Part: MECHANISM — OUT OF ADJUST (L-1 DOOR)
SEA - FLT 477 - CREW REPORTED L-1 DOOR DIFFICULT TO OPEN. ADJUSTED DOOR PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M)
Part: EEL BATT PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)