N976AS

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,997 hrs · 23,381 cycles

CABIN EMERGENCY LIGHTS JUST FORWARD OF AFT GALLEY COMES ON WHEN BATTERY SWITCH IS TURNED OFF. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD.

Part: SKIN — GOUGED (BS 1309-1322) · airframe 39,203 hrs · 20,184 cycles

OPEN AFT EXTERNAL LAVATORY SERVICE PANEL GOUGED FUSELAGE. BLENDED GOUGES AND INSTALLED REPAIR DOUBLER PER SRM 53 04.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,360 hrs · 19,760 cycles

CUSP WEB IS CORRODED. REPLACED CUSP WEB PER SRM 51-10-4 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

CABIN FLOOR PANEL DELAMINATED WITH CORRODED INSERTS. REPLACED PANEL.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

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

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 38,360 hrs · 19,780 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 38,360 hrs · 19,780 cycles

CABIN FLOOR SEAT TRACK CORRODED. REPLACED TRACK.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

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

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 38,360 hrs · 19,780 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

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

Part: SKIN — DENTED (FUSELAGE) · airframe 38,360 hrs · 19,780 cycles

FUSELAGE SKIN DENTED. COLD FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,360 hrs · 19,780 cycles

CABIN FLOOR PANEL CRACKED. REPLACED FLOOR PANEL PER SRM 53-05 AND DRAWING S4932106.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 38,360 hrs · 19,780 cycles

CABIN FLOOR PANEL IS DELAMINATED AND HAS CORRODED INSERTS. REPLACED PANEL PER SRM 53-05 AND DWG S4932106.

Part: SKIN — GOUGED (FUSELAGE)

FOUND DURING HV CHECK, FUSELAGE SKIN GOUGED ON LT SIDE. REMOVED DAMAGED SECTION. INSTALLED 2 FINGER DOUBLERS AND 1 REPAIR DOUBLER. (M)

Part: WIRE — DISCONNECTED (CABIN)

LAX - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS 'BROKEN' INOPERATIVE AT ROW 3. RECONNECTED WIRE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — LOOSE (EMERGENCY LIGHT)

PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 6. RECONNECTED LOOSE CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

PHX - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FIRST 7 INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR. LIGTHS THEN OPERATED PROPERLY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

SJD - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RESEATED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (EMERGENCY LIGHT)

PHX - FOUND EMEREGNCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: SKIN — GOUGED (VERTICAL STAB)

OKC - DURING HV1-CHECK, FOUND VERTICAL STABILIZER SKIN GOUGED JUST ABOVE HORIZONTAL STABILIZER RIGHT PIVOT POINT. REPLACED SKIN PER SRM 51-30-1 AND 51-30-2. (M)

Part: RELEASE MECH — BROKEN (TAILCONE)

DURING HV1 CHECK, FOUND TAILCONE RELEASE MECHANISM BROKEN. REPLACED MECHANISM PER MM 53-53-02. (M)

Part: SPLICE PLATE — BENT (L/E SLAT)

OKC - DURING HV1 CHECK, FOUND RIGHT WING 0 TO 1 SLAT SPLICE PLATE UPPER END IS BENT. REPLACED SPLICE PLATE PER SRM 51-10-4 AND 57-50-13. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING HV1-CHECK, FOUND INTERCOSTAL CORRODED AT FS 1212-1231. REPLACED INTERCOSTAL PER SRM 51-30-5. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - HV1 CHECK, FOUND CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FS 929-1003. REMOVED DAMAGED SECTION AND REPAIRED WITH FILLER AND SPLICE PER SRM 51-10-4, 53-01, AND 51-30-8. (M)

Part: SKIN — DEBONDED (LT NACELLE)

OKC - HV1 CHECK, FOUND LEFT ENGINE LOWER AFT COWL COMPOSITE MATERIAL IS SEPARATING AT FORWARD ATTACH HOOK. REBONDED COMPOSITE PER EA 7110-01220. (M)

Part: SKIN — CHAFED (CARGO BAY DOOR)

OKC - HV1-CHECK, FOUND FORWARD CARGO BAY DOOR LOWER FORWARD AND AFT CORNERS ARE CHAFED. REMOVED DAMAGED SECTIONS. INSTALLED FILLERS AND DOUBLERS PER EA 5230-01226. (M)

Part: FLOOR PANEL — PUNCTURED (FS)

OKC - HV1 CHECK, FOUND COCKPIT FLOOR PANEL UNDER CAPTAINS SEAT IS PUNCTURED. REMOVED DAMGAED SECTION AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: INSERT — DENTED (FLOOR PANEL)

OKC - HV1-CHECK, FOUND CABIN FLOOR PANEL INSERT DAMAGED AT FS 927-1003. REPLACED FLOOR PANEL INSERT PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS CRACKED AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA PREFLIGHT CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED DURING EXTERIOR CHECK. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING REMAINED ON WITH BATTERY SWITCH OFF. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT WAS FOUND INOPERATIVE AT ROW 31. RESEATED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

THREE TAILCONE PASSAGEWAY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. RESEATED ASSOCIATED POWER SUPPLY. LIGHT THEN OPERATED PROPERLY.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT ANGLE CORRODED AT FS 1214. REPLACED ANGLE PER SRM 51-10-4 AND MD DWG 5936071-507. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK IS CORRODED AT FS 237. REPLACED SEAT TRACK PER SRM 53-05, FIG 4F. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 389-465, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY SHEAR TIE CORRODED AT FS 1174, LONGERON 29L 29R. REPLACED SHEAR TIE PER SRM 53-14-3, 51-10-2 AND 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, DENT IN FUSELAGE SKIN AT STATION 1150 BETWEEN LONGERON 26R-27R. REPAIRED IAW SRM. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK AT RBL 44 AND STATION 287 IS CORRODED. REPAIRED IAW SRM. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD INSERTS CORRODED AT FS 1250-1307. REPLACED 5 FLOORBOARD INSERTS SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, COCKPIT FLOORBOARD DELAMINATED AT AFT CORNER AND 3 INSERTS ARE CORRODED AT FS 148, BL 0. REPLACED FLOORBOARD AND INSERTS PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED 30K CHECK, FOUND FLOORBOARD AT BS 200-256, LEFT BUTTOCK LINE 22, RIGHT BUTTOCK LINE 22 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - FOUND DURING SCHEDULED 30K CHECK, FOUND FLOORBOARD AT BS 160-256, LEFT BUTTOCK LINE 22, LEFT BUTTOCK LINE 44 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, LONGERON 30 CORRODED AT STATION 588. REPAIRED IAW EA. (M)

Part: SKIN — GOUGED (ELEVATOR)

OKC - FOUND DURING 30K CHECK, RIGHT ELEVATOR OUTBOARD LEADING EDGE GOUGED AT TIP MATING SURFACE. REPAIRED IAW EA. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DELAMINATED AT FS 1079-1156, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - FOUND DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 160-200, LEFT BUTTOCK LINE 8, RIGHT BUTTOCK LINE 44 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED 30K CHECK, FOUND FLOORBOARD AT BS 1307-1361, LEFT BUTTOCK LINE 18 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD AT STATION 200-256 RBL 22 TO RBL 44 HAS 18 CORRODED INSERTS. REMOVED AND REPLACED IAW SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, DENT IN FUSELAGE SKIN AT STATION 1340 LONGERON 19R. REPAIRED IAW SRM. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDING AT FS 200-256, RBL 44-54. REPLACED FLOORBOARD WITH FIBERGLASS OVERLAY PER MM 25-00-00, SEC 3E. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD INSERTS CORRODED AT FS 148. REPLACED INSERTS PER SRM 53-05. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DELAMINATED AT FS 579-617, LBL 22 - RBL 22. REPLACED FLOORBOARD WITH FIBERGLASS OVERLAY PER MM 25-00-00, SEC 3E. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 200-256, LBL 14 - RBL 22. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, SEAT TRACK CORRODED AT FS 1122, LBL 22. REPLACED SEAT TRACK PER SRM 53-05, 51-10-4, 51-30-05, AND 51-30-1. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD AT STATION 1156-1250 LBL 22 TO LBL 44 HAS 29 CORRODED INSERTS. REMOVED AND REPLACED IAW SRM. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - FOUND DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 160-200, RIGHT BUTTOCK LINE 44, RIGHT BUTTOCK LINE 54 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED 30K-CHECK, FLOORBOARD AT BS 1117-1174, LEFT BUTTOCK LINE 6, LEFT BUTTOCK LINE 22 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: STIFFENER — CRACKED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD STIFFENER CRACKED AT FS 207-256, LBL 44-54. REPAIRED STIFFENER WITH FIBERGLASS OVERLAY PER MM 25-00-00, PARA 3E, PG 801. (M)

Part: SKIN — GOUGED (LT WING)

OKC - FOUND DURING 30K CHECK, LEFT WIND LEADING EDGE UPPER SURFACE GOUGED AT STATION XFS 624. REPAIRED IAW EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK AT STATION 1229 AND LBL 22 IS CORRODED. REPAIRED IAW SRM. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 160-200, LEFT BUTTOCK LINE 8, LEFT BUTTOCK LINE 44 CORRODED. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - DURING SCHEDULED 30K CHECK, FLOORBOARD AT BS 1079-1117, LEFT BUTTOCK LINE 22, RIGHT BUTTOCK LINE 22 TORN. REMOVED AND REPLACED FLOORBOARD PER MD80 SRM. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 617-693, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: STRAKE — DAMAGED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT STRAKE AFT EDGE IS FLATTENED. REPAIRED IAW EA. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 541-617, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 693-769, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: DOOR — CHAFED (L/E SLAT)

OKC - FOUND DURING 30K CHECK, LEFT WING NR 11 SLAT TRACK DOOR IS CHAFFED AT FORWARD END. REPLACED SLAT TRACK DOOR. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD PUNCTURED AT FS 1250-1307, LBL 22 - LBL 44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 927-1003, LBL 22 - LBL 44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DELAMINATING AT FS 541-579, LBL 22 TO RBL 22. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 889-927, RBL 22 - RBL 44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 807-826, LBL 22 - RBL 22. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY RIGHT TIE-DOWN TRACK FORWARD SPLICE IS CORRODED AT FS 1090. REPLACED SPLICE PER SRM 53-05, FIG 4G, AND 53-24-0, FIG 11. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLIGHT DECK FLOOR PANEL LOWER SURFACE IS SEPARATING FROM CORE AT FS 148.55, RBL 31-44. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: INSERT — CORRODED (FLOORBOARD)

OKC - FOUND DURING 30K CHECK, FLOORBOARD HAS CORRODED INSERTS AT FS 160-200, RBL 8 TO LBL 8. REPLACED INSERTS PER SRM 53-05. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND 30K CHECK, FLOORBOARD DISBONDED AT FS 693-769, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 465-541, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 313-389, LBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 313-389, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K-CHECK, FLOOR SUPPORT CORRODED AT FS 1155, LBL 22-44. REPLACED SUPPORT PER SRM 53-14-1, 51-10-4, AND 51-30-5. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 398-446, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: BRACKET — CRACKED (RT MLG WW)

OKC - FOUND DURING 30K CHECK, HYDRAULIC VALVE BRACKET CRACKED IN RIGHT WHEEL WELL. REPLACED BRACKET PER DAC DWG 7936937, SRM 51-10-2, 51-10-4, AND 51-30-5. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOORBOARD DISBONDED AT FS 465-541, RBL 22-44. REPLACED FLOORBOARD PER SRM 53-05 AND 53-24-0. (M)

Part: DOOR — CHAFED (SLAT TRACK)

OKC - FOUND DURING 30K-CHECK, RIGHT NR 5 SLAT TRACK DOOR CHAFED AT FORWARD END. REPLACED SLAT TRACK DOOR PER MM 27-80-01. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FOUND CUSP WEB CORRODED AT FS 617-712. REPLACED CUSP WEB PER SRM 51-30-2, AND 51-10-4. (M)

Part: SKIN — DENTED (ELEVATOR TAB)

OKC - FOUND DURING 30K CHECK, LEFT ELEVATOR CONTROL TAB DENTED ON LOWER OUTBOARD SURFACE. CUT OFF DAMAGED AREA AND REPAIRED PER SRM 51-70-2. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, CUSP WEB CORRODED AT FS 1239. REPLACED CUSP WEB PER SRM 53-14-3, FIG 12, 51-70-4, 51-30-1 AND 51-30-5. (M)

Part: PANEL — CHAFED (L/E SLAT)

OKC - FOUND DURING 30K CHECK, LEFT NR 3 SLAT TRACK PANEL FORWARD END IS CHAFED AT NOTCH-OUT. REPLACED SLAT TRACK DOOR PER MM 27-80-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR SUPPORT CORRODED AT FS 1212 BETWEEN LONGERON 28L AND 29L. REPLACED SUPPORT PER SRM 53-24-0, FIG 11, AND SRM 51-30-2. (M)

Part: DOUBLER — CRACKED (LT WING)

OKC - FOUND DURING 30K CHECK, LEFT WING LEADING EDGE BUTT SPLICE DOUBLER IS CRACKED 1.25 INCH AT LOWER AFT EDGE. REPLACED SPLICE PER SRM 57-32-1, 51-10-4, AND 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MAIN CABIN FLOOR MEMBRANE (WEB) CORRODED AT FS 200, LBL 10. CUT OUT DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 53-14-1, FIG 11, 51-70-4, FIG 2, AND 51-30-2. (M)

Part: SPLICE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY LEFT TIE DOWN TRACK OUTBOARD FORWARD SPLICE IS CORRODED AT FS 1090. REPLACED TIE DOWN TRACK SPLICE PER SRM 53-24-0, FIG 11, 51-10-2, 51-10-4, 51-10-2, AND 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MAIN CABIN FLOOR MEMBRANE (WEB) CORRODED AT FS 160-200, LBL6-RBL6. CUT OUT DAMAGED SECTION. SPLICED IN NEW SECTION PER SRM 53-14-1, FIG 11, 51-70-4, FIG 2, AND 51-30-2. (M)

Part: DOOR FRAME — CRACKED (L1 DOOR)

OKC - FOUND DURING 30K CHECK, LEFT PAX L1 DOOR INTERNAL FRAME IS CRACKED BEHIND INNER DOOR HANDLE. REPLACED FRAME PER SRM 51-30-2. (M)

Part: STRAP — CRACKED (RT WING)

OKC - FOUND 30K CHECK, RIGHT WING LEADING EDGE SPLICE STRAP IS CRACKED AT STATION XRS 164, XFS 299. REPLACED SPLICE PER SRM 57-32-1, 51-10-4, AND 51-30-2. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SHEAR TIE CORRODED AT FS 1150, LONGERON 29L-29R. REPLACED SHEAR TIE PER SRM 53-14-3 AND 51-30-5. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR MEMBRANE IS CORRODED AT FS 160-200, RBL 10.5-54. REPLACED MEMBRANE PER SRM 53-14-1, FIG 11, 51-10-4, FIG 2, AND 53-30-2. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY SHEAR TIE CORRODED AT FS 1212, LONGERON 28L-28R. REPLACED SHEAR TIE AND PREVIOUS SPLICES PER SRM 53-14-3, FIG 3, 51-10-2, 51-10-4, AND 51-30-5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MAIN CABIN RIGHT SEAT TRACK IS CORRODED AT FS 237, RBL 22. REPLACED TRACK SECTION FROM FS 204 - 245 PER SRM 53-05, FIG 11. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, MAIN CABIN FALSE TRACK IS CORRODED AT FS 160-200, LBL 9. REPLACED FALSE TRACK PER SRM 53-14-1, FIG 11 AND 53-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, RBL 54. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, AND 52-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MAIN CABIN FALSE TRACK CORRODED AT FS 160-200, RBL 9. REPLACED FALSE TRACK PER SRM 53-14-3, FIG 11, AND 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MAIN CABIN FLOOR SUPPORT IS CORRODED AT FS 190, LBL 53. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, LBL 44. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, AND 52-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, MAIN CABIN FLOOR SUPPORT BRACKET IS CORRODED AT FS 170, BL 0. REPLACED SUPPORT BRACKET PER SRM 53-14-1, FIG 11, AND 51-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1250, LONGERON 29L TO 28R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS PER SRM 53-03, FIG 2A. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200, LBL 15. REPLACES SUPPORT PER SRM 53-14-1, FIG 11, AND 51-30-2. (M)

Part: GUSSET — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, MID CARGO BAY GUSSET CORRODED AT FS 636 BETWEEN LONGERON 29R AND 30. REPLACED GUSSET PER SRM 51-10-2, 51-30-5, AND DAC DWG 2913044. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, LBL 54. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, AND 51-30-5. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY RIGHT TIE-DOWN TRACK CORRODED AT FS 1211-1338. REPLACED TIE-DOWN TRACK PER SRM 53-24-0, FIG 11, 51-10-2, 51-10-4, AND 51-30-2. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY LEFT TIE DOWN TRACK CORRODED UNDER CLIPNUTS AT FS 1007-1338. REPLACED TIE-DOWN TRACK PER SRM 53-24-0, FIG 11, 51-10-4, 51-10-2, AND 51-30-2. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, AFT CARGO BAY RIGHT TIE-DOWN TRACK CORRODED AT FS 1007-1155. REPLACED TIE-DOWN TRACK PER SRM 53-24-0, FIG 11, 51-10-2, 51-10-4, 51-10-2, AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 160-200, LBL 56. REPLACED SUPPORT PER SRM 53-14-1, FIG 11, AND 51-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FRAME CORRODED AT FS 1271, LONGERON 29L-29R. REPLACED FRAME PER SRM 53-14-3, FIG 3A, 53-03, FIG 2A, AND 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 165, LBL 53. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1287 BETWEEN LONGERON 29L AND 29R. REPLACED FRAME PER SRM 53-03, FIG 2A. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 204, LBL 9-13. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 200, LBL 15-43. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 160, LBL 5 - RBL 5. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, CUSP WEB CORRODED AT FS 1250-1271, LONGERON 18R. REPAIRED PER SRM 51-70-4, FIG 2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 200, RBL 46-52. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, FLOOR SUPPORT IS CORRODED AT FS 204, LBL 5 - RBL 5. REPLACED SUPPORT PER SRM 53-14-1, FIG 11 AND 53-30-2. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, RIGHT FRAME TO SKIN INBOARD BRACKET CORRODED AT FS 1220, LONGERON 29R. REPLACED BRACKET PER SRM 51-10-2 ND -4, AND DAC DWG 5936064. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, 'J' ANGLE CORRODED AT FS 1212-1219 BETWEEN LONGERON 30-29R. REPLACED 'J' ANGLE PER SRM 51-10-4 AND DAC DWG 5936071-507. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING 30K-CHECK, RIGHT FRAME TO SKIN OUTBOARD BRACKET CORRODED AT FS 1220, LONGERON 29R. REPLACED BRACKET PER SRM 51-10-2 AND -4, AND DAC DWG 5936064. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, RIGHT FRAME TO SKIN BRACKET CORRODED AT FS 1212, LONGERON 29R. REPLACED BRACKET PER SRM 51-10-2 AND -4, AND DAC DWG 5936064. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, LONGERON 29R CORRODED IN AFT PIT FROM STATION 1212-1231. REPLACED SECTION OF LONGERON 29R FROM FS 1117-1250 PER SRM 51-30-5 AND 51-10-4. (M)

Part: PLATE — GOUGED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, AFT CARGO BAY SCUFF PLATE HAS DEEP GOUGES. REPLACED AFT HALF OF SCUFF PLATE PER SRM 51-10-4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, FLOOR SUPPORT ANGLE CORRODED AT FS 1214, LONGERON 29R. REPLACED SUPPORT ANGLE PER SRM 51-10-2 AND -4, AND DAC DWG 5936071-507. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, INTERCOSTAL CORRODED BETWEEN LONGERON 30-29R AT FS 1153. REPLACED INTERCOSTAL PER SRM 51-10-4 AND -30-2, AND DAC DWG 5936071. (M)

Part: PLATE — GOUGED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, AFT CARGO BAY SCUFF PLATE HAS DEEP GOUGES. REPLACED FORWARD HALF OF SCUFF PLATE PER SRM 51-10-4. (M)

Part: BRACKET — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, CENTER CARGO DOOR AFT HOLD-OPEN LATCH SIDE BRACKET CRACKED. REPLACED BRACKET PER SRM 51-10-2, AND DAC DWG 5956028. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - DURING 30K-CHECK, FOUND FALSE SEAT TRACK CORRODED AT FS 1155, BL 0. REPLACED TRACK PER SRM 51-30-1. (M)

Part: BRACKET — CRACKED (HORIZ STAB)

OKC - FOUND DURING 30K-CHECK, LEFT HORIZONTAL STABILIZER REAR SPAR CAP COVER INTERNAL BRACKET IS CRACKED. REPLACED BRACKET PER SRM 51-10-2, AND DOUGLAS DWG 9917401. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

OKC - DURING 30K-CHECK, FOUND GALLEY SUPPORT FLOOR STRUCTURE CORRODED AT FS 175, RBL 26. REPLACED GALLEY SUPPORT FITTING PER SRM 51-10-4 AND 51-30-5. (M)

Part: GUIDE — WORN (THRUST REVERSER)

OKC - DURING 30K CHECK, LEFT ENGINE AFT THRUST REVERSER PANEL AFT MOUNT BOLT GUIDES WORN. REPLACED MOUNT BOLT GUIDE BRACKET PER SRM 51-30-2. (M)

Part: SUPPORT BRACKET — BROKEN (FUSELAGE)

OKC - FOUND 30K CHECK, AFT AIRSTAIR CEILING PANEL SUPPORT BRACKET HAS FASTENER HOLE BROKEN OUT. REPLACED SUPPORT BRACKET ASSEMBLY PER SRM 51-30-1. (M)

Part: BRACKET — CRACKED (FUSELAGE)

OKC - FOUND DURING 30K-CHECK, CENTER CARGO DOOR FORWARD HOLD OPEN LATCH SIDE BRACKET CRACKED .50 INCH. REPLACED BRACKET PER SRM 51-10-2, AND DAC DWG 5956028. (M)

Part: FITTING — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, TIE DOWN FITTING CORRODED IN AFT CARGO BAY FS 1153 BETWEEN LONGERON 30-29R. REPLACED FITTING PER SRM 51-10-3. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY FLOOR SUPPORT AT FS 1150-1212 ABOVE STRINGER 29R CORRODED BEYOND LIMITS. REPLACED FLOOR SUPPORT TEE PER SRM 51-30-5. (M)

Part: BRACKET — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY DOOR JAMB CORNER BRACKET CORRODED AT FS 1155 LONGERON 28R. REPLACED DOOR JAMB BRACKET PER SRM 51-30-2. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, CORROSION AT FS 1212 LONGERON 29L-29R. REPLACED FRAME PER SRM 51-30-2 AND 51-30-5. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, SECTION OF LONGERON 29R CORRODED AT FS 1231-1260. REPLACED CORRODED SECTION PER SRM 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, FLOOR SUPPORT AT FS 1155, LONGERON 28L-29R CORRODED. REPLACED SUPPORT. (M)

Part: STOP FITTING — CRACKED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, AFT CARGO BAY DOOR CRACKED ON AFT TOP SIDE. REPLACED DOOR STOP PER MM 52-31-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED BEYOND LIMITS AT LBL 44 FROM FS 1176-1211. REPLACED SEAT TRACK FROM FS 1155-1231 PER SRM 53-05, FIG 4F. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, CUSP WEB CORRODED AT FS 398, 448, 478, 482, 488, AND 500, BUTTOCK STA'S RBL 44-58. REPLACED CUSP WEB AT FS 389-503 PER SRM 51-30-5 AND 51-30-02. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND CUSP WEB CORRODED AT FS 503-522, 522-541, AND 541-560. REPLACED CUSP WEB AT FS 503-597, RBL 44-58 PER SRM 51-30-5 AND 51-30-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT LBL 22 FROM FS 1122 AND AT 1229. REPLACED SEAT TRACK FROM FS 1085-1310 PER SRM 53-05, FIG 4F. (M)

Part: WEB — CORRODED (FUSELAGE)

OKC - FOUND 30K CHECK, CUSP WEB CORRODED AT FS 602, 614, 617-630, 636-655, AND 655-674 STA'S AT BUTTOCK LINE STA'S RBL 44-58. REPLACED CUSP WEB AT FS 598-712 PER SRM 51-30-5 AND 51-30-02. (M)

Part: BRACKET — CRACKED (CARGO DOOR)

OKC - FOUND DURING 30K CHECK, FORWARD CARGO BAY DOOR AFT SIDE STOP, 2ND FROM TOP, BRACKET CRACKED. REPLACED BRACKET PER SRM 51-10-4, 51-30-1, AND 51-30-5. (M)

Part: BRACKET — CRACKED (CARGO DOOR)

OKC - DURING 30K-CHECK, FOUND AFT CARGO BAY DOOR FORWARD SIDE UPPER STOP BRACKET CRACKED. REPLACED BRACKET PER SRM 51-10-4, 51-30-1, AND 51-30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT STATION 180, RBL 9-43. FABRICATED AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-30-2, 51-10-4 AND 51-10-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K-CHECK, FOUND MAIN CABIN FLOOR SUPPORT CORRODED BEYOND LIMITS AT STATION 180, LBL 25-38. FABRICATED AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-30-2. (M)

Part: STOP FITTING — CRACKED (CARGO DOOR)

OKC - FOUND DURING C-CHECK, FORWARD CARGO BAY DOOR FORWARD SIDE BOTTOM DOOR STOP 3RD FROM TOP, FITTING CRACKED. REPLACED FITTING PER SRM 51-10-4, 51-30-1, AND 51-30-5. (M)

Part: STOP FITTING — CRACKED (CARGO DOOR)

OKC - FOUND DURING 30K-CHECK FORWARD SIDE BOTTOM DOOR STOP FITTING CRACKED. REPLACED FITTING PER SRM 51-10-4, 51-30-1 AND 51-30-5. (M)

Part: STOP FITTING — CRACKED (CARGO DOOR)

OKC - DURING 30K-CHECK, FOUND FORWARD CARGO BAY DOOR FORWARD SIDE TOP DOOR STOP FITTING CRACKED. REPLACED FITTING PER SRM 51-10-4, 51-30-1 AND 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - 30K CHECK, AFT CARGO FRAME CORRODED BEYOND LIMITS AT STATION 1174. REPLACED FRAME AT STATION 1174 LONGERON 28R-27L PER SRM 51-30-5 AND 51-30-2. (M)

Part: BRACKET — CRACKED (FUSELAGE)

OKC - 30K-CHECK, FOUND MID CARGO BAY DOOR FORWARD HOLD-OPEN LATCH SIDE BRACKET (ANGLE) WAS CRACKED. FABRICATED AND INSTALLED REPLACEMENT ANGLE FROM 063 INCH 7075-T6 STOCK PER SRM 51-10-2. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING IN FORWARD CABIN WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED NORMALLY. (M)

Part: SWITCH — LEAKING (APU)

LAX - SMOKE AND FUMES WERE NOTED IN CABIN SHORTLY AFTER TAKEOFF. FIRE ALARMS ANNUNCIATED. REPLACED LEAKING LOP SWITCH ON APU. SUBSEQUENT OPERATION CAUSED NO FUMES OR SMOKE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, FOUND TAILCONE AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: OUTFLOW VALVE — FAILED (AFT FUSELAGE)

EN ROUTE TO SEA FLT 748, AUTO CABIN PRESSURE CONTROL MALFUNCTIONED, WITH CREW PERFORMING EMERGENCY DESCENT FROM 28,000 FEET ALTITUDE TO 10,000. REPLACED OUTFLOW VALVE MOTOR/ACTUATOR ASSEMBLY. SYSTEM THEM OP CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING LINE MAINTENANCE CHECK, THE TAILCONE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - DURING LINE MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING IN ROWS 6 THROUGH 10 WERE FOUND TO BE ON ALL THE TIME. REPLACED BATTERY PACK AT ROW 10. LIGHTS THEN OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (MID CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13 THROUGH 16 WERE FOUND TO BE INOPERATIVE. REPLACED POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE ARMED LIGHT IN THE L1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 3)

PDX - FLT 100 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED WIRING AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (ROW 2) · airframe 18,437 hrs · 9,816 cycles

FAI - FLT 196 - CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 1 THROUGH 3 WERE FOUND INOPERATIVE. SECURED LOOSE CONNECTOR AT ROW 2 AND LIGHTS OPERATED NORMALLY. (X)

Part: PIN — MISALIGNED (COCKPIT WINDOW)

PDX - PRIOR TO DEPARTURE OF FLIGHT 710, CREW REPORTED THE FIRST OFFICERS SLIDING WINDOW GUIDE PIN WAS MISALIGNED. REPLACED UPPER LOCK BAR ON F/O''S WINDOW, ADJUSTED CAM FOLLOWER AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS FOR THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ILLUMINATION WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (ROW 15/28)

ANC - PRIOR TO DEPARTURE OF FLIGHT 190, CREW REPORTED SECTIONS OF THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID AND AFT CABIN WERE INOPERATIVE. SECURED WIRING IN FLOOR TRACK AT ROW 15 AND ROW 28 AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 13 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 9-11)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: MECHANISM — OUT OF ADJUST (PAX DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND STIFF TO OPERATE AND DIFFICULT TO CLOSE. ADJUSTED THE DOOR OPERATING MECHANISM AND OPERATED NORMALLY. (M)

Part: WIRE — FAILED (E/E BAY)

OAK - DURING 15K CHECK, ELECTRICAL POWER WAS TURNED ON AFTER OTHER MAINTENANCE WAS PERFORMED AND SMOKE WAS NOTED EMITTING FROM THE AFT SIDE OF THE LOWER EPC PANEL. INSPECTED THE LOWER AFT EPC PANEL AND FOUND CHAFED AND BURNED WIRES IN THE PANEL NEAR THE RT GEN AC POWER RELAY. REMOVED DAMAGED WIRES AND SPLICED 7 NEW 10AWG WIRES FROM THE RT GEN AC POWER RELAY THROUGH THE EPC PANEL TO THE GEN BUS CIRCUIT BREAKER PANEL PER ASA EA 2400-01045 AND BAC SWPM D6-54446. THE WIRING APPEARED TO HAVE BEEN CHAFING ON THE EPC PANEL STRUCTURE DUE TO WIRES FLEXING EACH TIME THE GENERATOR BUS CIRCUIT BREAKER PANEL WAS OPENED. REPOSITIONED AND RESECURED WIRING IN CLAMPS. (M)

Part: SLIDE — FAILED (TAILCONE)

OAK - DURING 15K CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: SKIN — DENTED (FUSELAGE)

OAK - DURING 15K CHECK DENT WAS FOUND IN FUSELAGE SKIN AFT OF L1 DOOR ABOVE CUSP LINE. REPAIRED WITH DOUBLER IAW ASA EA 5330-01350. (M)

Part: WEB — CORRODED (BS 1160)

OAK - DURING 15K CHECK, FUOND CORROSION ON FLOOR WEB OUTBOARD OF FLOOR PANEL E-14 AT FS 1160. REPAIRED WITH DOUBLER IAW ASA EA 5320-01203. (M)

Part: WEB — CORRODED (BS 1117)

OAK - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR WEB OUTBOARD OF FLOOR PANEL E-13 AT FS 1117. REPAIRED WITH DOUBLER IAW ASA EA 5320-01203. (M)

Part: WIRE — LOOSE (CABIN)

LAX - PRIOR TO DEPARTURE OF FLIGHT 403 - CREW REPORTED THAT THE FORWARD FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING TO THE LAMP MODULE AND THE LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - PRIOR TO DEPARTURE OF FLT 465, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RESEATED FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 305, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RESEATED CONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: CARGO TRACK — CORRODED (BS 1231-1287)

OAK - DURING C-CHECK, FOUND CORROSION ON AFT CARGO TRACK FROM FUSELAGE STATION 1231 TO 1287. REPAIRED CARGO TRACK IAW ASA EA 5320-01309. (M)

Part: ACTUATOR — FAILED (RT MLG)

LAX - AIR TURN BACK OF FLIGHT 557 - CREW REPORTED THE RT MLG UNSAFE LIGHT AND THE GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. ACCOMPLISHED CHECK LIST AND CYCLED GEAR, LIGHTS EXTINGUISHED AFTER APPROXIMATELY 10 MINUTES. LANDED WITHOUT INCIDENT. FOUND RIGHT MLG RETRACT CYLINDER BYPASSING INTERNALLY. REPLACED RT MLG RETRACT CYLINDER. ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M)

Part: SLIDE ASSY — FAILED TEST (TAILCONE)

OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED LIGHT TEST. REMOVED AND REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M)

Part: PORTABLE LIGHT — DIM (CABIN)

PDX- DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LIGHT ASSY — INOPERATIVE (L-1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT AT THE L-1 DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT SIGN LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X)