N972AS

Part: SUPPORT ANGLE — CRACKED (NLG WW) · airframe 45,132 hrs · 23,404 cycles

NLG WHEEL WELL FORWARD BULKHEAD SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-30-02 AND 51-10-02.

Part: VANE — DENTED (T/E FLAP) · airframe 45,132 hrs · 23,404 cycles

LEFTHAND OUTBOARD CENTER FLAP VANE DENTED. COMPOSITE REPAIRED PER SRM 51-70-2.

Part: LONGERON — CRACKED · airframe 45,132 hrs · 23,404 cycles

LONGERON CRACKED. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 53-02.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

LONGERON REPAIR SPLICE CORRODED. REMOVED EXISTING REPAIR SPLICE AND INSTALLED REPLACEMENT SPLICE PER SRM 53-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,132 hrs · 23,404 cycles

INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-4 AND 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

FUSELAGE DENTED. RECONTOURED SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-04.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

AFT ACCESSORY COMPARTMENT FRAME PUNCTURED. REPLACED DAMAGED SECTION OF FRAME WITH REPAIR DOUBLER PER SRM 51-70-4 AND 53-14.

Part: FRAME — CHAFED (BS 1361) · airframe 45,132 hrs · 23,404 cycles

FRAME CHAFED. REMOVED DAMAGED AREA. INSTALLED REPAIR ANGLE FILLER AND REPAIR PLATE PER SRM 53-03.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

AFT ACCESSORY COMPARTMENT FRAME TO SKIN ATTACH ANGLE CRACKED. REPLACED DAMAGED ANGLE PER SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

AFT ACCESSORY COMPARTMENT FRAME CRACKED. STOP DRILLED CRACKED AND REPAIRED PER SRM 53-03.

Part: SUPPORT ANGLE — CRACKED (NLG WW) · airframe 45,132 hrs · 23,404 cycles

NLG WHEEL WELL FORWARD BULKHEAD SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-30-02 AND 51-10-02.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

LONGERON CORRODED. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 53-02.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,132 hrs · 23,404 cycles

LONGERON SPLICE CORRODED. REPLACED SPLICE PER SRM 51-10-4 AND 51-30-5.

Part: VANE — DENTED (TE FLAP) · airframe 45,132 hrs · 23,404 cycles

LEFTHAND INBOARD FLAP VANE DENTED. BONDED REPAIR DOUBLER IN DAMAGED AREA PER SRM 51-70-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 45,132 hrs · 23,404 cycles

AFT CARGO DOOR DENTED AT PREVIOUS REPAIR. REMOVED DAMAGED SECTION AND INSTALLED FILLERS FINGER DOUBLERS AND INTERNAL DOUBLER PER ASA EA5230 01382.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

ACCESSORY COMPARTMENT FRAME TO SKIN ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-11, 51-30-02 AND 51-30-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

FUSELAGE DENTED. COLD WORKED DENT AND INSTALLED INTERNAL DOUBLER PER SRM 53-04.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,132 hrs · 23,404 cycles

INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 53 01 51 10 04 AND 51 30 05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

RIGHTHAND CUSP WEB CORRODED. REPLACED DAMAGED SECTION WITH DOUBLER PER SRM 53-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,132 hrs · 23,404 cycles

RIGHTHAND CARGO TRACK CORRODED. REPLACED TRACK PER SRM 51-10-4 AND 51-30-01.

Part: VANE — DENTED (T/E FLAP) · airframe 45,132 hrs · 23,404 cycles

LEFTHAND INBOARD FLAP VANE HAS MULTIPLE DENTS. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER PER SRM 51-70-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

CARGO BAY STUB FRAME CLIP CORRODED. REPLACED CLIP PER SRM 51-10-3 AND DAC DWG 5936064.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

FUSELAGE SKIN DENTED. COLD FORMED SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 45,132 hrs · 23,404 cycles

CARGO TRACK CORRODED. REPLACED TRACK PER SRM 51-30-02 AND 51-30-01.

Part: LONGERON — CRACKED (BS 1415-1430) · airframe 45,132 hrs · 23,404 cycles

LONGERON IS CRACKED. REPLACED DAMAGED SECTION WITH SPLICE PER SRM 53-02.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 45,132 hrs · 23,404 cycles

TEMPORARY FUSELAGE SKIN REPAIR GOUGED IN AFT LAVATORY SERVICE DOOR AREA. REPLACED EXISTING REPAIR DOUBLER PER ASA ER 5330 02233.

Part: LONGERON — DENTED (BS 246 L17L) · airframe 45,132 hrs · 23,404 cycles

LONGERON DENTED. REPLACED DAMAGED SECTION WITH SPLICES PER SRM 53-02.

Part: INTERCOSTAL — CORRODED (BS 1215) · airframe 45,132 hrs · 23,404 cycles

INTERCOSTAL CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-5 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 1287-1309) · airframe 45,132 hrs · 23,404 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51-30-1 AND 51-30-5.

Part: SHEAR TIE — CORRODED (BS 1211) · airframe 45,132 hrs · 23,404 cycles

SHEAR TIE CORRODED. REPLACED SHEAR TIE PER SRM 53-03.

Part: FRAME — CORRODED (BS 1287) · airframe 45,132 hrs · 23,404 cycles

FRAME CORRODED. REPLACED FRAME PER SRM 53-03.

Part: SKIN — GOUGED (LAV SERVICE) · airframe 44,212 hrs · 22,988 cycles

SMALL GOUGE FOUND AT 2 O'CLOCK POSITION ON LAVATORY AFTER SERVICE DOOR. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER EA 5330 02208.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 43,041 hrs · 22,439 cycles

DAMAGE FOUND AFT OF L1 DOOR AT STA 238 TO 240. DENT AND GOUGE ON EXISTING REPAIR DOUBLER. INSTALLED NEW EXTERNAL REPAIR DOUBLER PER SRM 53-04 FIG 12B.

Part: FLOOR PANEL — DELAMINATED (BS 313-389) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.

Part: CHANNEL — CORRODED (BS 807-927) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL HAT CHANNEL CORRODED AT HOLE. REPLACED HAT CHANNEL PER DAC DRAWING 9957921.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 41,474 hrs · 21,683 cycles

AFT CARGO BAY DOOR CREASED JUST BELOW HANDLE. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER FILLER AND SHIMS PER ASA EA 5230 01321.

Part: FLOOR PANEL — CHAFED (BS 826-927) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL CHAFED. REPLACED FLOOR PANEL PER SRM 51-30-2.

Part: FLOOR PANEL — DELAMINATED (BS 636-) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL DELAMINATED. BOND REPAIRED DAMAGED AREA PER SRM 51-70-3.

Part: FLOORBEAM — CORRODED (BS 1155) · corrosion level 1 · airframe 41,474 hrs · 21,683 cycles

CABIN FLOORBEAM CORRODED. REPLACED SUPPORT PER SRM 51-30-2.

Part: FLOOR PANEL — DELAMINATED (BS 580) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL DELAMINATED. BOND REPAIRED DAMAGED AREA PER SRM 51-70-3.

Part: FLOOR PANEL — DELAMINATED (BS 612) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL DELAMINATED. BOND REPAIRED DAMAGED AREA PER SRM 51-70-3.

Part: VANE — GOUGED (TE FLAP) · airframe 41,474 hrs · 21,683 cycles

RT WING OUTBOARD FLAP INBOARD VANE GOUGED ON LEADING EDGE. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2.

Part: FITTING — CORRODED (BS 218) · corrosion level 1 · airframe 41,474 hrs · 21,683 cycles

GALLEY MOUNT FITTING CORRODED. REPLACED FITTING PER SRM 51-10-4 AND 51-30-5.

Part: FLOOR PANEL — CORRODED (BS 1117-1174) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL CORRODED. REPLACED FLOOR PANEL PER SRM 53-05.

Part: FLOOR PANEL — CORRODED (BS 1117-1174) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL CORRODED AT INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.

Part: DUMMY RAIL — CORRODED (BS 1098-1212) · corrosion level 1 · airframe 41,474 hrs · 21,683 cycles

FALSE TRACK CORRODED. REPLACED FALSE TRACK PER SRM 51-30-1.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL Z-ANGLE SUPPORT CORRODED. REPLACED Z-ANGLE SUPPORT PER SRM 51-30-2.

Part: CUSP WEB — CORRODED · airframe 41,474 hrs · 21,683 cycles

CUSP WEB CORRODED. REMOVED CORROSION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 53-01 AND 51-70-4.

Part: INSERT — PULLED (FLOOR PANEL) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL HAS PULLED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.

Part: INSERT — PULLED (FLOOR PANEL) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL INSERTS PULLED. REPLACED FLOOR PANEL PER SRM 53-05.

Part: SUPPORT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 41,474 hrs · 21,683 cycles

R1 DOOR GIRT BAR SUPPORT CORRODED. REPLACED SUPPORT PER SRM 51-10-4.

Part: SEAT TRACK — CORRODED (BS 200-281) · corrosion level 1 · airframe 41,474 hrs · 21,683 cycles

SEAT TRACK CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR SECTION PER SRM 53-05.

Part: FLOOR PANEL — CORRODED (BS 1174-1250) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05.

Part: SKIN — DENTED (BS 240-248) · airframe 41,474 hrs · 21,683 cycles

FUSELAGE DENTED. RECONTOURED SKIN. INSTALLED DOUBLER PER SRM 53-04.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,474 hrs · 21,683 cycles

R1 DOOR AREA WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. INSTALLED FILLER AND DOUBLER PER SRM 51-70-04.

Part: FLOOR PANEL — DAMAGED (BS 389-465) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL CREASED. REPLACED FLOOR PANEL PER SRM 53-05.

Part: SEAT TRACK — CORRODED (BS 200-281) · corrosion level 1 · airframe 41,474 hrs · 21,683 cycles

CABIN SEAT TRACK CORRODED. REPLACED DAMAGED SECTION. INSTALLED REPAIR DOUBLER PER SRM 53 05.

Part: FLOOR PANEL — DELAMINATED (BS 788-826) · airframe 41,474 hrs · 21,683 cycles

CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05.

Part: PRESSURE SWITCH — DEFECTIVE (RT ENG OIL PRESS) · airframe 41,177 hrs · 21,542 cycles

DIV (TO PDX) RT ENG OIL FILTER CLOG ANNUNICATION IN CRUISE. SHUT DOWN ENG IN FLIGHT. REPLACED OIL FILTER DIFF PRESSURE SWITCH. OP CHECKED OK. NO FILTER CLOGGING CONTAMINATION WAS FOUND.

Part: SKIN — GOUGED (L1 DOOR)

FOUND DURING HV CHECK, FORWARD PAX (L-1) DOOR SKIN GOUGED AND BENT AT BOTTOM FORWARD EDGE. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: SKIN — CHAFED (CARGO BAY DOOR)

DURING HV-CHECK, FOUND AFT CARGO BAY DOOR FORWARD EDGE CHAFED AT UPLATCH HOOK. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — CHAFED (FLAP VANE)

FOUND RT OUTBOARD FLAP VANE CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)

Part: DOOR FRAME — CORRODED (AFT CARGO BAY)

FOUND HV CHECK, AFT CARGO BAY DOOR JAMB BEAM CORRODED. REPLACED BEAM. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING INSPECTION, FOUND CABIN FLOOR PANEL FOR STATION 693-769 BETWEEN RBL 44 AND RBL 54 HAT CHANNEL ON UNDERSIDE IS CRACKED. REPAIRED IAW MD80 SRM 51-70-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING INSPECTION, FOUND MAIN CABIN STATION 628 X= -44 CORROSION ON SEAT TRACK. REPAIRED BY REMOVING DAMAGED SECTION. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK AND TWO SPLICES IAW MD80 SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT ANGLE EXFOLIATED STATION 1212 BETWEEN 28R AND 27R. REPAIRED BY REMOVING DAMAGED SUPPORT AND INSTALLED NEW SUPPORT IAW MD80 SRM 51-30-4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT STATION 1080 HAS EXFOLIATION ON UNDERSIDE AT NUTPLATES ABOVE LONGERON 30 TO 28L. REPAIRED BY REMOVING EXFOLIATED PART AND INSTALLED NEW PART PER MD80 SRM 51-10-4. (M)

Part: FLOORBOARD — DELAMINATED (FS)

DURING INSPECTION FOUND FLOORBOARD STATION 769 TO 826, LBL 22-44 HAS SEVERAL AREAS OF EDGE DAMAGE. REPAIRED BY FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING INSPECTION, FOUND CORROSION ON AFT SIDE OF FRAME AT STATION 1271 AND LONGERON 30. REPAIRED BY REMOVING DAMAGE. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW MD80 SRM 53-03. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING INSPECTION, FOUND SKIN CRACKED AT FORWARD HINGE RIGHT AFT NOSE GEAR DOOR EMINATING FROM RIVET HOLE FORWARD OF FORWARD HINGE CUTOUT. REPAIRED IAW SRM 51-10-2, 51-10-4 AND 51-30-2. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING INSPECTION, FOUND MID CARGO PIT STATION 598-617 LONGERON 30 CORRODED AROUND FASTENERS. REPAIRED BY REMOVING CORROSION, SPOT FACED AREA, IAW EA 5310-02311 AND AAR EA 10234. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 175-196. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: WEB — CRACKED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND RIGHT CUSP WEB IS CRACKED AT FS 1204. REPLACED CRACKED SECTION, AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 826-864. REPLACED CHANNEL PER SRM 53-05. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 927-1003. INSTALLED FASTENER TO PLUG PUNCTURE PER SRM 53-01. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS SHREDDING AT FS 946-1003. REPLACED CHANNEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AROUND THREADED FASTENERS AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M0

Part: SEAT TRACK — GOUGED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND SEAT TRACK GOUGED AT FS 1145-1222. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-2. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE DAMAGE, UNSPECIFIED AT FS 148-160. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL CRACKED AT FS 617-693. REPLACED CHANNEL PER SRM 51-10-4 AND 51-10-3. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL CRACKED IN HAT CHANNELS AT FS 796-826. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAS CRACKED INSERT AT FS 196-256. REPLACED CHANNEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS CRACKED ON UNDERSIDE AT FS 674-693. REPLACED CHANNEL PER SRM 53-05. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 807-826. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC 0 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL SURFACE IS DISBONDED AT FS 864-886. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS DISBONDING AND HAS CORRODED FASTENERS AT FS 196-256. REPLACED CHANNEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL CORNER IS CRACKED AT FS 886-927. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FS)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 826-864. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: CHANNEL — CHAFED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED FLOOR PANEL HAT CHANNEL PER SRM 51-30-2, 51-10-4, AND 51-10-3. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS CORRODED AT FS 1003-1079. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL SURFACE IS SHREDDING. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: LINKAGE — OUT OF ADJUST (COCKPIT WINDOW)

SEA - DURING PREFLIGHT CHECK, FOUND RIGHT SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED UPPER LOCK BAR LINKAGE. WINDOW THEN OPERATED PROPERLY. (M)

Part: WINDOW — STUCK (COCKPIT)

LAX - DURING PREFLIGHT CHECK, THE FIRST OFFICERS SLIDING CLEARVIEW WINDOW WAS FOUND TO BE DIFFICULT TO OPEN. LUBRICATED WINDOW. WINDOW THEN OPERATED PROPERLY. (M)

Part: BATTERY — INOPERATIVE (FWD CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN FIRST CLASS WAS FOUND INOPERATIVE. REPLACED BATTERY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: FLOOR PANEL — PUNCTURED (CABIN)

FOUND DURING 30K CHECK, FORWARD CARGO BAY FLOOR PANEL IS PUNCTURED AND FS 330-370. REPLACED SECTION OF FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FS 180-200)

FOUND DURING 30K CHECK, FALSE TRACK CORRODED AT FLOORBOARD FASTENER HOLES AT FS 180-200. REPLACED FALSE TRACK PER SRM 51-10-4 AND 51-30-1. (M)

Part: MOUNT — CORRODED (ANTENNA)

OKC - FOUND DURING 30K CHECK, ANTENNA MOUNTING CORRODED AND PITTED AT FS 1127. BLENDED CORROSION. ALTHOUGH BEYOND LIMITS, WAS ACCEPTED PER EA 5330-01612 AND BAC TLX AOC-OKC-02-00166H. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LONGERON 30 SPLICE IS CORRODED AT FS 1201. BLENDED SPLICE PER EA 5310-02153 AND BAC TLX AOC-OKC-02-00159H. (M)

Part: PAN — CHAFED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY DOOR PAN CHAFED AT FORWARD AND AFT LOWER RUB BLOCKS. BLENDED DAMAGED AREAS PER EA 5230-01187 AND BAC TLX AOC-OKC-02-00125H AND -00126H. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LONGERON SPLICE HAS CORRODED FASTENERS AT FS 1201. REPAIRED DAMAGED AREA PER SRM 53-01. (M)

Part: SUPPORT — CRACKED (PNEUMATIC SYS)

OKC - FOUND DURING 30K CHECK, PNEUMATIC DUCT ANGLE SUPPORT CRACKED AT AFT END OF WHEELWELL IN KEEL BEAM. REPLACED ANGLE PER SRM 51-10-2 AND 51-10-4. (M)

Part: RUB STRIP — WORN (T/E FLAP)

OKC - FOUND DURING 30K CHECK, LEFT WING FLAP FLEX JOINT UPPER PANEL CHAFE STRIPS WORN. REPLACED RUB STRIP PER SRM 51-10-2 AND 51-10-4. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL HAS DAMAGED EDGE. REPLACED PANEL PER SRM 53-05 AND 51-10-4. (M)

Part: DOOR — CRACKED (L/E SLAT)

OKC - FOUND DURING 30K CHECK, RIGHT NR 5 SLAT NR 13 TRACK DOOR IS CRACKED. REPLACED TRACK DOOR PER BAC DWG 9937467. (M)

Part: FITTING — GOUGED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, LEFT WING OUTBOARD FLAP MID FITTING HAS TOOLING MARKS AND GOUGES, TWO PLACES. REPAIRED PER EA 5750-01759. (M)

Part: RETAINER — CHAFED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY DOOR LOWER SEAL RETAINER IS CHAFED AT FORWARD AND AFT CORNERS. REPLACED SEAL RETAINER PER SRM 51-10-2. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL HAS DAMAGED EDGE. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL UPPER SKIN IS DISBONDED. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL IS CORRODED. REPLACED PANEL IS SRM 51-10-4. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY FLOOR PANEL PUNCTURED AT FS 427-465. REPLACED PANEL PER SRM 53-05. (M)

Part: ACCESS PANEL — GOUGED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING FLAP FLEX JOINT UPPER ACCESS PANEL UPPER SURFACE IS GOUGED. REPAIRED PANEL PER SRM 51-70-1. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL HAS DAMAGED EDGE. REPLACED PANEL PER SRM 53-05. (M)

Part: HINGE — CRACKED (BARRIER DOOR)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY BARRIER DOOR HINGE IS CRACKED. REPLACED HINGE PER SRM 51-30-2. (M)

Part: RUB STRIP — WORN (T/E FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING FLAP FLEX JOINT UPPER PANEL CHAFE STRIPS WORN IN SEVERAL AREA. REPLACED RUB STRIP PER SRM 51-10-2. (M)

Part: PANEL — DAMAGED (RT WING)

OKC - FOUND DURING 30K CHECK, RIGHT WING LOWER PANEL 1219C COUNTERSINK HOLES ARE ELONGATED. INSTALLED DOUBLER PER SRM 57-06A. (M)

Part: CHANNEL — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, DOOR FRAME CHANNEL CRACKED IN FORWARD CABIN AREA. REPAIRED CHANNEL PER SRM 51-70-5. (M)

Part: ACCESS PANEL — CHAFED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, LEFT WING FLAP LOWER FLEX JOINT ACCESS PANEL IS CHAFED IN SEVERAL PLACES. REPLACED PANEL PER SRM 51-10-4. (M)

Part: RUB STRIP — CHAFED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, MID CARGO DOOR LOWER PAN FORE AND AFT RUB BLOCKS ARE CHAFED. REPAIRED PAN PER EA 5230-01185. (M)

Part: PANEL — DAMAGED (RT WING)

OKC - FOUND DURING 30K CHECK, RIGHT WING LOWER LEADING EDGE PANEL 1248C HAS 3 ELONGATED HOLES. INSTALLED DOUBLERS PER SRM 51-07. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 1174-1250. REPLACED CUSP WEB PER SRM 51-30-2 AND 51-30-5. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL IS PUNCTURED. REPLACED PANEL PER SRM 53-05. (M)

Part: ACCESS PANEL — CRACKED (RT SPOILER)

OKC - FOUND DURING 30K CHECK, RIGHT OUTBOARD FLIGHT SPOILER ACCESS PANEL 1625A IS CRACKED. REPLACED PANEL PER SRM 51-10-2. (M)

Part: FITTING — WORN (RT WING FLAP)

OKC - FOUND DURING 30K CHECK, RT WING OUTBOARD FLAP VANE NR 4 FITTING IS WORN. REPLACED FITTING PER CMM 27-50-02. (M)

Part: STRUCTURE — CHAFED (RT SPOILER)

OKC - FOUND DURING 30K CHECK, RIGHT GROUND SPOILER IS CHAFED ON BOTTOM INBOARD TRAILING EDGE. REPAIRED DAMAGED AREA PER SRM 51-70-1B. (M)

Part: SKIN — GOUGED (RT WING LE)

OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE PANEL 1263 SKIN GOUGED AT SCREW HOLES. INSTALLED DOUBLER PER SRM 57-06A. (M)

Part: FITTING — WORN (RT WING TE FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP VANE NR 5 FITTING IS WORN. REPLACED FITTING PER CMM 27-50-02. (M)

Part: FITTING — WORN (RT WING TE FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP VANE NR 6 FITTING IS WORN. REPLACED FITTING PER CMM 27-50-02. (M)

Part: BRACKET — CHAFED (RT WING)

OKC - FOUND DURING 30K CHECK, RIGHT WING LEADING EDGE PANEL 1248C BRACKET IS CHAFED. REPLACED CHAFED AREAS OF BRACKET PER SRM 51-10-2 AND 51-30-2. (M)

Part: ACCESS PANEL — CRACKED (RT SPOILER)

OKC - FOUND DURING 30K CHECK, RIGHT INBOARD FLIGHT SPOILER ACCESS PANEL 1626A IS CRACKED. REPLACED PANEL. (M)

Part: FITTING — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, G-1 GALLEY LOWER INBOARD MOUNT FITTING IS CORRODED. REPLACED FITTING PER SRM 51-30-2. (M)

Part: FITTING — CORRODED (FWD ENTRY)

OKC - FOUND DURING 30K CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE GIRT BAR ATTACH FITTING IS CORRODED. REPLACED FITTING PER SRM 51-30-1. (M)

Part: STRUCTURE — CHAFED (RT SPOILER)

OKC - FOUND DURING 30K CHECK, RT OUTBOARD FLIGHT SPOILER IS CHAFED ON TRAILING EDGE UPPER SIDE OUTBOARD OF ACTUATOR MOUNT. REPAIRED DAMAGED AREA PER SRM 51-70-1B. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, INTERCOSTAL IS CORRODED AT FS 541, 29R. CUT OUT AND REPLACED CORRODED SECTION WITH FILLER AND DOUBLER PER SRM 51-70-5. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SHEAR TIE CORRODED AT FS 1174. REPLACED SHEAR TIE PER SRM 51-10-2. (M)

Part: ACCESS PANEL — CRACKED (RT WING)

OKC - FOUND DURING 30K CHECK, RIGHT GROUND SPOILER ACCESS PANEL 1627A IS CRACKED. REPLACED PANEL PER SRM 51-10-2. (M)

Part: GUIDE — GOUGED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, MID CARGO DOOR FORWARD AND AFT UPLOCK GUIDE ANGLES ARE GOUGED. REPLACED GUIDE ANGLES PER MM 20-30-01. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, COCKPIT LEFT SIDE FORWARD FLOOR PANEL IS CRACKED. REPAIRED CRACK PER MM 25-00-00, 3E. (M)

Part: INTERCOSTAL — GOUGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, INTERCOSTAL GOUGED AT FS 1322-1338. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-10-4, 51-30-2 AND DAC DWG 5936667. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LONGERON SPLICE CORRODED AT FS 1201. REPLACED DAMAGED SPLICE PER SRM 51-10-2, 51-10-4, AND 53-02. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR PANEL IN PUNCTURED AT FS 1117-1155. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — TORN (CABIN)

OKC - FOUND DURING 30K CHECK, FLOORBOARD TORN AT FOUR FASTENER HOLES AT FS 886-927. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY TRACK CORRODED/GOUGED AT FS 1130-1322. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-5. (M)

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL EDGE DAMAGED AT FS 636-693. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY FLOOR PANEL EDGE DAMAGED AT FS 693-730. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY TRACK CORRODED AT CLIP NUT HOLES AT FS 525-785. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-5, AND 51-10-4. (M)

Part: VANE — DENTED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP VANE GOUGED ON LEADING EDGE. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-60-0, 51-70-2, AND 50-14. (M)

Part: SUPPORT — CRACKED (RT WING)

OKC - FOUND DURING 30K CHECK, RIGHT WING TRAILING EDGE INNER SUPPORT FORMER CRACKED AT FORWARD EDGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-10-2, 51-10-4, AND 51-30-2. (M)

Part: BRACE — CRACKED (AFT AIRSTAIR)

OKC - FOUND DURING 30K CHECK, AFT AIRSTAIR LEFT SIDE BRACE CRACKED AT LOWER FORWARD END. STOP DRILLED CRACK AND INSTALLED ANGLE DOUBLER PER SRM 51-10-2, 51-10-4, 51-30-2, AND 52-01. (M)

Part: ANGLE — CORRODED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, AFT CARGO DOOR VERTICAL ANGLE BEAM IS LOWER PAN AND FASTENERS ARE CORRODED. REPLACED CORRODED PARTS PER SRM 51-30-2. (M)

Part: HINGE FITTING — CORRODED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING HARDWARE AND BEARING BOLT HOLES CORRODED. REMOVED CORROSION AND REPAIRED BOLT HOLES BY INSTALLING BUSHINGS PER EA 5750-01756. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FUSELAGE SKIN DENTED AT FS 1124. INSTALLED INTERNAL DOUBLER OVER DENT PER SRM 53-04. (M)

Part: HINGE — CORRODED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING OUTBOARD FLAP CENTER HINGE BEARING BOLT HOLES CORRODED. REMOVED CORROSION AND INSTALLED BUSHINGS IN BOLT HOLES PER EA 5750-01756. (M)

Part: SKIN — CRACKED (AFT AIRSTAIRS)

OKC - FOUND DURING 30K CHECK, AFT AIRSTAIR SKIN CRACKED AND GOUGED ON RIGHT SIDE. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-10-2, 51-10-4, 51-30-2, 52-03 AND 52-60-0. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY TRACK CORRODED AT FS 1212-1322. REPLACED TRACK PER SRM 51-30-01. (M)

Part: BRACE — CRACKED (AFT AIRSTAIR)

OKC - FOUND DURING 30K CHECK, AFT AIRSTAIR LOWER SECTION RIGHT SIDE BRACE CRACKED. STOP DRILLED CRACK AND INSTALLED ANGLE DOBLER PER SRM 51-30-2, 51-10-2, 51-10-4, AND 52-01. (M)

Part: CLIP — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, THRESHOLD PLATE FORWARD RADIUS CLIP CORRODED IN AFT CARGO BAY. REPLACED PLATE PER SRM 51-30-5. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, EXTERNAL ATTACH ANGLE CRACKED AT FS 807. REPLACED ATTACH ANGLE PER SRM 51-10-2, 51-10-4, 51-30-2, 51-30-5, AND DAC DWG 991252. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 1250. REPLACED CUSP WEB PER SRM 51-30-2 AND 51-30-5. (M)

Part: STEP — GOUGED (AIRSTAIRS)

OKC - FOUND DURING 30K CHECK, STAIRCASE GOUGED TOP FORWARD. INSTALLED DOUBLER PER SRM 52-01. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FORMER IS CORRODED AT FS 1271. REPLACED DAMAGED SECTION OF FORMER PER SRM 53-14-3, 53-03, 51-30-2, AND 51-30-5. (M)

Part: CLIP — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, TEE CLIP ON EXTERNAL KEEP PLANK CRACKED AT FS 875. REPLACED TEE CLIP PER SRM 51-30-5. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, BULKHEAD SUPPORT CRACKED IN MID CARGO BAY AT FS 529. REPLACED BULKHEAD PER SRM 51-10-4 AND 51-30-2. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY THRESHOLD CORRODED ON UNDERSIDE AT FS 1155. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SILL — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT SERVICE (L-2) DOOR SILL PAN IS CORRODED. REPLACED SILL PER SRM 51-30-2 AND 51-30-5. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, INTERCOSTAL CRACKED BETWEEN FLOORBEAMS AT FS 1287-1309. REPLACED INTERCOSTAL PER 51-10-1, 51-10-2, 51-10-4, 51-30-5, AND DAC DWG 9936580. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FRAME ASSEMBLY CORRODED AT FS 1211. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M)

Part: STRAP — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT SERVICE (L-2) DOOR SCUFF PLATE STRAP WAS CORRODED. REPLACED STRAP PER SRM 51-10-2, 51-10-4, 51-30-1, AND DAC DWG 993654. (M)

Part: FRAME — CHAFED (VERTICAL STAB)

OKC - FOUND DURING 30K CHECK, JACKSCREW ACCESS PANEL ON THE VERTICAL STABILIZER HAS CHAFED FRAME MATING FACE. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M)

Part: DOOR — GOUGED (L/E SLAT)

OKC - FOUND DURING 30K CHECK, NR 3 LEFT SLAT TRACK DOOR NR 9 IS GOUGED/CHAFED ON TOP EDGE. REPLACED SLAT TRACK DOOR PER SRM 51-10-4 AND 51-30-8. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE GIRT BAR FITTING INSERTS ARE CORRODED. REPLACED FOUR INSERTS PER SRM 51-30-1. (M)

Part: INSERT — CORRODED (FLOOR PANEL)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 200-256. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)

Part: FITTING — CORRODED (CABIN)

OKC - FOUND DURING 30K CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE GIRT BAR FLOOR FITTING IS CORRODED AT FS 160. REPLACED FITTING PER SRM 51-30-1. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 180-192. REPLACED FLOOR SUPPORT PER SRM 51-10-2, 51-10-4, 51-30-1, 51-30-2, AND DAC DWG 9936534. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 180-200. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 160-180. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)

Part: RIB — CRACKED (FLOOR PANEL)

OKC - FOUND 30K CHECK, FLOOR PANEL HAS A CRACKED RIB AT FS 465-541. CUT OUT AND REPLACED DAMAGED SECTION PER SRM 51-70-5, 53-24-0, AND 51-60-0. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 160-200. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)

Part: INSERT — CORRODED (FLOOR PANEL)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL DELAMINATED AT FS 1146-1250. REPLACED FLOOR PANEL PER SRM 53-24-0 AND 53-05. (M)

Part: INSERT — CORRODED (FLOOR PANEL)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS CORRODED INSERTS AT FS 1071-1155. REPLACED FLOOR PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)

Part: RIB — WORN (FLOOR PANEL)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL RIB WORN IN 6 PLACES AT FS 1003-1098. REPLACED DAMAGED SECTION PER SRM 51-70-5, 53-24-0, AND 51-60-0. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 1022-1071. REPLACED CUSP SECTION AND INSTALLED DOUBLER PER SRM 51-30-2, 51-30-5, AND 51-70-4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 1148-1164. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-05, 51-10-4, 51-30-1, 51-30-2 AND 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1155, LONGERON 27L-27R. REPLACED FRAME PER SRM 51-30-5. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SIX CLIP NUT HOLES ARE CORRODED ON MID CARGO BAY TRACK AT FS 522-561. REPLACED DAMAGED SECTION PER SRM 53-24-0 AND 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING 20K CHECK, FLOOR PANEL CRACKED AT OUTBOARD SIDE FS 465-541. REPLACED FLOOR PANEL PER SRM 51-70-5, 51-60-0 AND 53-24-0. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS ONE PUNCTURE, 50 DENTS, AND DISBONDING AT BOTH ENDS OF LOWER STIFFENERS AT FS 825. INSTALLED DOUBLERS ON LOWER STIFFENER PER SRM 51-70-2 AND 53-05. (M)

Part: ACCESS PANEL — CRACKED (SPOILER)

OKC - FOUND DURING 30K CHECK, LEFT INBOARD FLIGHT SPOILER ACCESS PANEL 1526 IS CRACKED. REPLACED PANEL PER SRM 51-30-1. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 313-370. INSTALLED DOUBLER ON WEB PER SRM 53-14-2, 53-01, 51-70-4, AND 51-30-1. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - FOUND DURING 20K CHECK, FLOORBOARD HAS TORN METAL AT 'W' SANDWICH EXTRUSION AT FS 826-886. REPLACED SUPPORT SECTION PER SRM 51-30-8, 51-20-0, AND 51-10-4. (M)

Part: PANEL — CHAFED (LT WING)

OKC - FOUND DURING 30K CHECK, LEFT WING FORWARD ROCK DEFLECTOR PANEL IS WORN/CHAFED AT EDGES. REPAIRED WITH DOUBLER PER SRM 51-30-2 AND 51-70-4. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR PANEL IS PUNCTURED AT FS 1003-1071. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS ONE PUNCTURE, ONE DENT, AND DISBONDING AT ENDS OF LOWER STIFFENER AT FS 826-927. INSTALLED DOUBLERS ON LOWER STIFFENER AND REBONDED ENDS PER SRM 51-70-2 AND 53-05. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS TORN METAL AT 'W' SANDWICH EXTRUSION AT FS 886-946. REPLACED SUPPORT SECTION PER SRM 51-30-8, 51-20-0, AND 51-10-4. (M)

Part: INTERCOSTAL — GOUGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, INTERCOSTAL BETWEEN LONGERON 26L-27L GOUGED AT FS 1322. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-10-4, 51-30-2, AND DAC DWG 5936667. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SHEAR TIE FRAME CORRODED AT FS 1155. REPLACED FRAME PER SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED IN CABIN AT FS 200. REPLACED SUPPORT PER SRM 53-14-1, 51-10-2, 51-10-4, AND 51-30-2. (M)

Part: ATTACH FITTING — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, UPPER LEFT TAILCONE ATTACH BRACKETS TWO CRACKED. REPLACED BRACKETS PER SRM 51-10-2, 51-10-4, 51-30-1, AND DAC DWG 9911957. (M)

Part: BRACKET — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, BRACKET BELOW 'Y' DUCT IN ACCY COMPARTMENT IS CRACKED. REPLACED BRACKET PER SRM 51-10-3, 51-30-1 AND DAC DWG 5937954. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD SKIN CRACKED AT FS 212. REPLACED FLOORBOARD SECTION PER SRM 53-05. (M)

Part: ROD — CRACKED (BARRIER DOOR)

OKC - FOUND DURING 30K CHECK, AFT CARGO COMPARTMENT BARRIER DOOR ASSEMBLY AFT HOLDUP SPEAR IS CRACKED. REPLACED SPEAR PER SRM 51-30-2. (M)

Part: WEB — CRACKED (L1 DOOR)

OKC - DURING 30K CHECK, FOUND LEFT FRONT (L1)DOOR INNER WEB IS CRACKED AT RADIUS AT HANDLE AREA. REPLACED INNER WEB PER SRM 51-30-2 AND 51-30-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 624. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 826. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 275. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 275. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M)

Part: STOP FITTING — CRACKED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY DOOR ADJUSTMENT SCREW STOP PLATE FITTING IS CRACKED JUST ABOVE DOOR SWITCH TARGET. REPLACED STOP PLATE FITTING PER SRM 51-30-5. (M)

Part: RUB STRIP — GOUGED (T/E FLAP)

OKC - FOUND DURING 30K CHECK, RIGHT WING FLAP FLEX JOINT RUB STRIP IS GOUGED IN 3 AREAS. REPLACED FLAP FLEX JOINT FAIRING PER 51-10-2, 51-10-4, 51-30-2 AND DAC DWG 5935920. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD IS DISBONDED AT ONE END AND CREASED/CRACKED ACROSS ENTIRE WIDTH OF BOARD AT FS 927-1003. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: PANEL — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, TRANSITION PANEL IS CORRODED AT FS 148-169 AND 196-200. REPLACED SECTION OF TRANSITION PANEL PER SRM 51-10-2, 51-10-4, 51-30-1 AND DAC DWG 9959828. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FASTENER HOLES AT FS 200. REPLACED FLOOR SUPPORT PER SRM 53-14-1, 51-10-2, 51-10-4, AND 51-30-2. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD CORRODED AT 4 FASTENER HOLES AT FS 886-927. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FALSE TRACK CORRODED AT FS 149-200. REPLACED TRACK PER SRM 53-14-1, 51-10-2, 51-10-4, AND 51-30-1. (M)

Part: CHANNEL — WORN (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FORWARD RIGHT MLG WHEELWELL DOOR FORMER HAS 3 WORN AREAS. REPLACED MLG DOOR CHANNEL AT FORWARD EDGE OF DOOR CUTOUT PER SRM 51-3-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 180. REPLACED FLOOR SUPPORT PER SRM 53-14-1, 51-10-2, 51-10-4, 51-30-5, AND 51-30-2. (M)

Part: ROD — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY BARRIER DOOR FORWARD HOLD UP ROD IS CRACKED. REPLACED HOLD-UP ROD PER SRM 51-30-2. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS CORRODED INSERTS AT FS 160-200 NEAR L1 ENTRY DOOR. REPLACED FLOORBOARD SECTION PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 408-503. REPLACED DAMAGED WEB SECTION PER SRM 51-30-1 AND -5. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 712-769. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICED IN WEB REPAIR PER SRM 51-70-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB IS CORRODED AT FS 522-598. REPLACED DAMAGED WEB SECTION PER SRM 51-30-1 AND -5. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 509. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICED IN WEB REPAIR PER SRM 51-70-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 294-313. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-70-4. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD NR 5 HAS 6 CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD NR 5 PER SRM 53-05. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND 30K CHECK, FLOORBOARD NR 8 HAS 8 CORRODED INSERTS AT FS 200-256. REPLACED FLOORBOARD NR 8 PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 522-579. INSTALLED DOUBLERS AT FS 518-529 AND 566-574 PER SRM 51-70-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB IS CORRODED AT FS 408-503. REPLACED DAMAGED WEB SECTION PER SRM 51-30-1 AND -5. (M)

Part: FLOORBOARD — DENTED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS TWO DENTS AT FS 927-1003. REPLACED FLOORBOARD SECTION PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LEFT CUSP WEB IS CORRODED AT FS 598-693. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-30-2 AND -5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200. REPLACED FLOOR SUPPORT PER SRM 51-10-2, -4, AND 51-30-2. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HONEYCOMB DAMAGED AT FS 408-446. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND 30K CHECK, FOUND FLOORBOARD NR 3 HAS 16 CORRODED INSERTS AT FS 160-200. REPLACED FLOORBOARD NR 3 PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB IS CORRODED AT FS 598-712. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM 51-30-5 AND -2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200. REPLACED FLOOR SUPPORT PER SRM 53-14-1, 51-10-2, 51-10-4, AND 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB CORRODED AT FS 845-886. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICED IN WEB REPAIR PER SRM 51-70-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, RIGHT CUSP WEB CORRODED AT FS 218-256. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICED IN WEB REPAIR AT FS 250-256 PER SRM 51-70-4. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT CUSP WEB CORRODED AT FS 370-389. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, AND SPLICED IN WEB REPAIR PER SRM 51-70-4. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

OKC - FOUND 30K CHECK, LONGERON 18R EXTERNAL ATTACH ANGLE IS CRACKED AT FS 788. REPLACED ATTACH ANGLE PER SRM 51-10-2, 51-30-2, 51-30-5, AND DAC DWG 9936527. (M)

Part: STRAP — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, L-2 AFT GALLEY SERVICE DOOR SILL PLATE BACKING STRAPS ARE CORRODED. REMOVED CORROSION FROM 7 STRAP AND REPLACED 9 STRAP PER SRM 51-10-2, 51-10-4, 51-30-2 AND DAC DWG 5936084. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

OKC - FOUND 30K-CHECK, AFT CARGO BAY FORWARD BULKHEAD SUPPORT IS CRACKED AT FS 1007. REPLACED SUPPORT PER SRM 53-24-0, 51-10-2, 51-10-4 AND 51-30-2. (M)

Part: PANEL — CORRODED (T/E FLAP)

OKC - FOUND 30K CHECK, LEFT WING FLAP EXPANSION JOINT PANEL NR 1531A HAS FRETTING CORROSION. REPLACED EXPANSION JOINT PANEL PER SRM 57-50-14, 51-10-2, 51-10-4, AND 51-10-3. (M)

Part: LATCH — CRACKED (CARGO DOOR)

OKC - FOUND 30K CHECK, MID CARGO BAY DOOR HOLD-OPEN LATCHES AND CORNER BRACKET CRACKED AT FORWARD END. REPLACED HOLD-OPEN LATCHES AND BRACKET PER SRM 51-10-2, 51-10-4, 51-30-3 AND DAC DWG 5956273. (M)

Part: CONNECTOR — LOOSE (CABIN)

SJC - DURING PREFLIGHT CHECK, FIRST COUPLE OF FEET OF EMERGENCY FLOOR TRACK LIGHTS IN FIRST CLASS CABIN WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

BUR - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 3. RECONNECTED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: FAIRING — DAMAGED (HORIZ STAB)

OAK - RIGHT HORIZONTAL STABILIZER UPPER FAIRING WAS DAMAGED DURING LINE MAINTENANCE. TEMP REPAIRED FAIRING WITH CUT OUT PIECE FROM ANOTHER FAIRING AND SPEED TAPE PER EA 5510-01157. (M)

Part: ENGINE — FAILED (RIGHT)

SEA - DURING CLIMB, EXPERIENCED RIGHT ENGINE INTERNAL FAILURE, SUSPECT BIRD STRIKE. FIRST INDICATION JOLT OCCURRED AT 200 FT, WITH OBVIOUS FAILURE OCCURRING AT 29,000 FT. PERFORMED AIR TURNBACK, RETURNING TO SEA. REPLACED ENGINE. (M)

Part: BATTERY — DISCHARGED (CABIN)

PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT BATTERY. OPS TESTED OK. (M)

Part: BATTERY — INOPERATIVE (FWD PAX ENTRANCE)

PDX - DURNG LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT BATTERY, OP TESTED OK. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND DISCONNECTED EMERGENCY TRACK LIGHTS IN THE 1ST CLASS CABIN. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND LONGERON 29R IN AFT CARGO BAY TO HAVE CORROSION AROUND FASTENER HOLES AT FS 1022-1025. INSTALLED U-CHANNEL REPAIR PER EA 5310-012066. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CRACK DAMAGE AT THE LEFT LOWER CORNER OF THE FORWARD BULKHEAD AT FS 110 SITUATED IN THE NLG WHEEL WELL. INSTALLED REPAIR DOUBLER PER EA 5310-02068. (M)

Part: FRAME — CORRODED (FUSELAGE)

OAK - DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF CIRCUMFERENTIAL FRAME AT FS 1250 FROM LONGERON 29R-28L. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING LINE CHECK, WITH SWITCH OFF, EMERGENCY TRACK LIGHTS AT ROWS 8 AND 9 TURNED ON WHEN EXTERNAL POWER WAS REMOVED FROM THE AIRCRAFT. REPLACED ASSOCIATED BATTERY POWER SUPPLY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS ON BOTH SIDES OF AIRCRAFT WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS IN FORWARD CABIN TO BE INOPERATIVE. REPLACED DISCHARGED BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: SOCKET — DEFECTIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FIRST FIVE EMERGENCY FLOOR TRACK LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED DEFECTIVE LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — LOOSE (CABIN)

SEA - DURING SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE AT SEAT 1 IN 1ST CLASS. RECONNECTED LOOSE LIGHT MODULE. LIGHT THEN OPERATED PROPERLY. (M)

Part: WINDOW — OUT OF ADJ (COCKPIT)

SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW COULD NOT BE OPENED. ADJUSTED WINDOW CAM FOLLOWER PER MM 56-10-03. WINDOW THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

LAX - DURING PRE-FLIGHT CHECK, FOUND FIRST SIX EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

LAX - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 3 FORWARD. RECONNECTED LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WINDOW (COCKPIT)

SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS DETERMINED TO BE DIFFICULT TO OPEN. CLEANED AND LUBRICATED WINDOW SLIDING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PRE-FLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 1ST CLASS. RECONNECTED LIGHT MODULE SOCKET. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND 1ST CLASS EMERGENCY TRACK LIGHTING TO BE INOPERATIVE. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN WERE DETERMINED TO BE INOPERATIVE. RESEATED LIGHT MODULES AND COVER. LIGHTS THEN OPERATED NORMALLY. (M)

Part: WINDOW (COCKPIT)

SEA - DURING PREFLIGHT CHECK, CAPTAINS SLIDING CLEARVIEW WINDOW WAS DETERMINED TO BE DIFFICULT TO OPEN. LUBRICATED WINDOW SLIDING MECHANISM. WINDOW THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING PRE-FLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 6 FORWARD. RESEATED TRACK LIGHTING MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING PRE-FLIGHT CHECK, FOUND FIRST FOUR EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

ANC - DURING PRE-FLIGHT CHECK, FOUND FIRST SIX EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

ANC - DURING PRE-FLIGHT CHECK, FOUND FORWARD STRIP OF EMERGENCY TRACK LIGHTING TO BE INOPERATIVE. RECONNECTED LOOSE TRACK LIGHT MODULE CONNECTOR AT FOURTH LIGHT. LIGHTS THEN OPERATED NORMALLY. (M)

Part: CONNECTOR — DAMAGED (CABIN)

PDX - DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS. REPAIRED CONNECTION. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING PRE-FLIGHT CHECK, FOUND AN EMERGENCY FLOOR TRACK LIGHT WIRING EXPOSED, DISCONNECTED IN 1ST CLASS CABIN. RECONNECTED FLOOR TRACK LIGHT WIRING. TRACK LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY — DISCHARGED (MID CABIN)

DURING MAINTENANCE CHECK THE FLOOR EMERGENCY TRACK LIGHTS AT ROWS 6-12 WAS FOUND TO BE INOP. REPLACED THE EMERGENCY BATTERIES AND THE LIGHTS OPERATED NORMALLY.

Part: LATCH — FAILED (PAX DOOR) · airframe 23,626 hrs · 12,710 cycles

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN RELEASE LATCH WAS STIFF TO OPERATE. LUBRICATED AND ADJUSTED, HOLD OPEN LATCH OPERATED NORMALLY. (X)

Part: POWER SUPPLY — DISCHARGED (AFT CARGO COMPT)

SEA - DURING MAINTENANCE CHECK, BOTH EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY IN THE AFT CARGO COMPARTMENT AND THE LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INTERMITTENT (CABIN)

SEA - DURING MAINTENANCE CHECK, GHE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT, STARTS OUT DIM, THEN GOES TO BRIGHT. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (COCKPIT)

SEA - DURING MAINTENANCE CHECK, THE COCKPIT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DAMAGED (CABIN)

FAI - PRIOR TO DEPARTURE OF FLIGHT 92, CREW REPORTED THE EMERGENCY FLOOR TRACK RED LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,824 hrs · 11,834 cycles

SEA - FLT 137 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTING IN FIRST CLASS, WAS FOUND INOPERATIVE. REPLACED BROKEN TRACK LIGHT SECTION AND LIGHTS OPERATED NORMALLY. (X)

Part: MODULE — BROKEN (CABIN) · airframe 21,808 hrs · 11,827 cycles

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 2 FORWARD. REPLACED BROKEN LIGHT MODULE AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,704 hrs · 11,778 cycles

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE IN THE AFT GALLEY AREA. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN) · airframe 21,447 hrs · 11,655 cycles

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 20 TO 22 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: TURBINE — FAILED (LT ENGINE)

SFO - AIR TURNBACK OF FLT 289, TOWER REPORTED SPARKS COMING FROM LEFT ENGINE ON TAKEOFF. ALL ENGINE INDICATIONS WERE NORMAL. RETURNED TO SFO AND LANDED UNEVENTFULLY. REPLACED THE LEFT ENGINE. SHOP TEARDOWN REVEALED 8TH STAGE STATOR VANE FAILURE, TWO VANES FRACTURED AT THE SHROUD AND CAUSED DOWNSTREAM DAMAGE. PRATT AND WHITNEY IS CONDUCTING FURTHER ANALYSIS OF THE HARDWARE TO DETERMINE THE CAUSE OF THE STATOR VANE FAILURE. (M)

Part: PIN — CONTAMINATED (SERVICE DOOR)

PDX - DURING MAINTENANCE CHECK, THE R1 DOOR WOLD NOT LATCH OPEN. FOUND GUST LOCK CATCH PIN COVERED WITH SEALANT, REMOVED SEALANT AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: SPRING — MISSING (TAILCONE)

PHX - DURING C-CHECK, THE TAILCONE DID NTO RELEASE DURING PERFORMANCE OF TAILCONE RELEASE TEST. FOUND AFT CABIN ENTRY DOOR PUSH-PULL CABLE INTERNAL RELEASE SPRING MISSING. INSTALLED SPRING AND ADJUSTED TAILCONE RELEASE MECHANISM, TAILCONE RELEASE OPERATED NORMALLY. (M)

Part: GUIDE PIN — OUT OF POSITION (RT COCKPIT)

SEA - FLT 417 - AFTER ARRIVAL, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED GUIDE PIN ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (X)

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. (X)

Part: CONNECTOR — DISCONNECTED (CABIN)

ANC - AFTER ARRIVAL OF FLT 127 - CREW REPORTED THE EMERGENCY LIGHTS FLASHED ON. THEN OFF, DURING CRUISE EN ROUTE SEA/ANC. INSPECTED EMERGENCY LIGHTS SYSTEM AND FOUND EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 11 TO 14 INOPERATIVE. RE-CONNECTED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS DIFFICULT TO CLOSE. RE-RIGGED THE L1 DOOR VERTICAL ADJUSTMENT IAW DC9 MM AND OPERATED NORMALLY. (X)

Part: POWER SUPPLY — INOPERATIVE (EMER EXIT)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (ROW 12)

SEA - DURING MAINTENANCE CHECK, ONE WHITE EMERGENCY FLOOR TRACK LIGHT AT ROW 12 WAS FOUND INOPERATIVE. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERTED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LAMP — DEFECTIVE (ROW 28)

SEA - AFTER ARRIVAL OF FLIGHT 251, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS ILLUMINATE BRIEFLY WHEN THE AUXILIARY HYDRAULIC PUMP IS TURNED ON. REPLACED DEFECTIVE LAMP MODULE AT ROW 28 AND SECURED LOOSE CONNECTIONS IN FLOOR TRACK FROM ROWS 24 AND 28 AND OPERATED NORMALLY. (M)

Part: LATCH — BINDING (COCKPIT WINDOW)

ANC - AFTER ARRIVAL OF FLT 90, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOLD NOT OPEN. LUBRICATED UPPER WINDOW LATCH MECHANISM AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: HOLD OPEN HOOK — BENT (PAX DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT LATCH OPEN. FOUND DOOR HOLD OPEN HOOK PIVOT LINK BENT. REPLACED LINK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FOWARD 6 SETS OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODULE AND OPERATED NORMALLY. (X)

Part: HOOK — BENT (PAX DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOOK WAS FOUND TO BE BENT AND WOULD NOT RETRACT FROM THE LOCKED POSITION. REPLACED HOOK ASSY, BURNISHED MINOR GOUGE, AND ADJUSTED HOLD OPEN HOOK. DOOR OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 718, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RESEATED CONNECTOR TO LIGHT ASSY AT ROW 1 AND OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (BS 229)

OAK - DURING 15K CHECK, GOUGE AND CRACK WAS FOUND IN FUSELAGE SKIN AT STATION 229, LONGERON 18L. INSTALLED FLUSH DOUBLER IAW DC9 SRM 53-04 FIG 47. (M)

Part: SKIN — DENTED (BS 219)

OAK - DURING 15K CHECK, DENT WAS FOUND IN FUSELAGE SKIN AT STATION 219 BETWEEN LONGERON 17L AND CUSP. REMOVED DAMAGED AND INSTALLED FLUSH REPAIR DOUBLER IAW ASA EA 5330-01326. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 21 TO 28 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: SWITCH — FAILED (FLIGHT COMPT)

SEA - AFTER ARRIVAL OF FLT 231, CREW REPORTED THE EMERGENCY LIGHTS AND FLOOR TRACK LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT. ACCOMPLISHED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, UNABLE TO DUPLICATE DISCREPANCY. PRECAUTIONARY REPLACED THE EMERGENCY LIGHTS CONTROL SWITCH S1-177 ON THE OVERHEAD PANEL IN THE FLIGHT COMPARTMENT AND THE EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER B1-41 AND OPERATED NORMALLY. (X)

Part: INFLATION BOTTLE — LOW PRESSURE (L2 DOOR)

PDX - DURING MAINTENANCE CEHCK, THE L2 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: CARGO TRACK — CORRODED (BS 1218-1322)

OAK - DURING C-CHECK, FOUND CORROSION ON AFT CARGO TRACK FROM FUSELAGE STATION 1218 TO 1322. REPAIRED CARGO TRACK IAW ASA EA 5320-01311. (M)

Part: FRAME — CORRODED (BS 1250)

OAK - DURING C-CHECK, FOUND CORROSION ON FUSELAGE FRAME AT STATION 1250 FROM LONGERON 27L TO 27R. REPLACE FRAME IAW DC9SRM 53-03, PAGE 4E, FIG 2A. (M)

Part: CARGO TRACK — CORRODED (BS 1079-1218)

OAK - DURING C-CHECK, FOUND CORROSION ON AFT CARGO TRACK FROM FUSELAGE STATION 1079 TO 1218. REPLACED CARGO TRACK IAW DC9 SRM. (M)

Part: HOLD OPEN HOOK — OUT OF ADJUST (L1 DOOR)

PDX - AFTER ARRIVAL OF FLT 343, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO LATCH AND UNLATCH IN THE OPEN POSITION. ADJUSTED THE HOLD OPEN HOOK ROD END AND OPERATED NORMALLY. (M)

Part: HOOK — OUT OF ADJUST (L-1 DOOR)

PDX - AFTER ARRIVAL OF FLT 383, CREW REPORTED THE L-1 DOOR STICKS IN THE OPEN POSITION. ADJUSTED THE HOLD OPEN HOOK AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY FLOOR TRACKLIGHTS WERE FOUND INOPERATIVE. REPLACED DEFECTIVE LIGHT ASSEMBLY ANDOPERATED NORMALLY.(M)

Part: HOLD OPEN HOOK — OUT OF ADJUST (L2 DOOR)

LAX - DURING MAINTENACNE CHECK, THE L2 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE IN LATCH. ADJUSTED HOLD OPEN HOOK MECHANISM AND OPERATED NORMALLY. (M)

Part: EMERG EVAC SLIDE — FAILED LIGHT TES (L1 DOOR)

OAK - DURING C-CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. (M)

Part: LINKAGE — BROKEN (L-1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR GUST LOCK WAS FOUND INOPERATIVE. REPLACED BROKEN GUST LOCK LINKAGE, ADJUSTED AND LOCK OPERATED NORMALLY. (W)