N973AS

Part: LANYARD — DISCONNECTED (R1 DOOR SLIDE)

SEA - PREFLIGHT CHECK, AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,577 hrs · 19,263 cycles

PDX LINE CHK - EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 2 TO 7. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY.

Part: ACCESS PANEL — LEAKING (RT WING)

OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS NR 5 AND NR 7 FROM IB. REMOVED PANEL, ORDERED AND INSTALLED NEW PANEL IAW MM 28-00-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 36,425 hrs · 19,188 cycles

OKC - C-CHECK, AFT PIT STA 1087-1098, LONG 29L HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.

Part: SKIN — CORRODED (FUSELAGE)

OKC - C-CHECK, AFT BELLY SKIN CORRODED STA 1098 TO STA 1110 BETWEEN LONG 29L AND 27L. REMOVED DAMAGE, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 5310-02398 AND EA 10582.

Part: ACCESS PANEL — LEAKING (RT WING)

OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS, NR 5 AND NR 7, FROM IB ENSURED HOLE CLEAN AND ROUND, TOUCH COUNTER SUNK, NDT FOR CRACKS. INSTALLED AD RIVET AND SHAVED BOTH SIDES OF REPAIR IAW EA 5710-01109 AND EA 10575.

Part: LONGERON — CORRODED (FUSELAGE)

OKC- C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.

Part: SKIN — GOUGED (VERTICAL STAB)

OKC - C-CHECK VERTICAL STAB UPPER SKIN GOUGED AROUND BANANA UPPER FAIRING PANEL 3705A ATTACHMENT AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER/SKIN AND DOUBLER, IAW SRM 51-30-1 AND 51-30-2, EA 5530-01108 AND EA 10594.

Part: FRAME — CORRODED (FUSELAGE)

OKC, C-CHECK, AFT CARGO COMPARTMENT FRAME STA 1098 HAS CORROSION ON FORWARD SIDE AND TOP SIDE JUST ABOVE LONGERON 30. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, SPACER AND FILLER IAW SRM.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2

OKC- C-CHECK, LONGERON 29L IS CORRODED FROM STA 1203 TO 1208 ON THE LOWER SURFACE OF THE OB FAIRING. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW SRM 53-02, FIG 18.

Part: VANE — DENTED (RT OB FLAP)

OKC - C-CHECK, RT OB FLAP VANE IB END LOWER SKIN HAS NUMEROUS SMALL DENTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2.

Part: SKIN — DENTED (FLAP)

OKC, C-CHECK, RT WING T/E IB FLAP DENTED AT LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-03, FIG 7.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2

OKC - C-CHECK, AFT BILLIE BATH TUB FITTING TO BULKHEAD STA 1003, LONG 30, HAS AREAS OF CORROSION ON FORWARD INSIDE OF FITTING. REMOVED DAMAGE, SPOT FACED FASTENER HOLES, TREATED AND PRIMED, SEALED AND APPLIED CORROSION INHIBITING COMPOUND IAW EA 5340-01132 AND EA 10588.

Part: DIVERTER — CRAZED (HEAT EXCHANGER)

OKC - C-CHECK, LT PRIMARY HEAT EXCHANGER RAM AIR DIVERTER WORN IN FORWARD LOWER CORNER STOP DRILLED CRACK, FPI FOR CRACK CONTAINMENT AND WELDED CRACK IAW EA 5300-01053 AND EA 10576.

Part: SKIN — CHAFED (LT WING)

OKC - C-CHECK, LT WING L/E UPPER SURFACE CHAFED 25 INCHES OB OF L/E SLAT NR 0, OB TRACK REMOVED DAMAGE. HFEC, NO CRACKS NOTED, TREATED AND PRIMED IAW EA 5740-01411 AND EA 10592.

Part: FAIRING — CRACKED (LT ACM EXHAUST)

OKC- C-CHECK, LT ACM EXHAUST FAIRING IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, WELDED CRACK IAW EA 2120-01087 AND EA 10573.

Part: STRAP — BROKEN (COCKPIT DOOR)

OKC - C-CHECK, COMPLY WITH JOB 062, LOG NR 5784357, COCKPIT DOOR CLOSING STRAP BROKEN OFF. FABRICATED AND INSTALLED PLATE IAW EA 5250-01191 AND EA 10559.

Part: VANE — DAMAGED (RT IB FLAP)

OKC - C-CHECK, RT IB FLAP VANE LOWER SKIN HAS DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC- C-CHECK, CABIN FLOORBOARD STA 180 TO 200 RBL 44 HAS DELAMINATION AND BROKEN EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.

Part: SKIN — DAMAGED (FWD CARGO DOOR)

OKC - C-CHECK, FORWARD CARGO DOOR SKIN ALONG FWD EDGE DINGED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-05, FIG 4.

Part: RADOME — OUT OF ALIGNMENT (FUSELAGE)

OKC - C-CHECK, RADOME FAILED GAP CHECK BETWEEN AFT EDGE OF RADOME AND FUSELAGE SKIN, STEP 17 OF T/C 244530001. RADOME TO FUSELAGE GAP ACCEPTABLE IAW EA 5350-01156.

Part: LONGERON — DAMAGED (FUSELAGE)

OKC - C-CHECK, AFT PIT ON LONG 28L, OTBD LOWER LT SIDE AT STA 1098. REMOVED DAMAGE, FABRICATED REPAIR HAT SECTION IAW SRM 53-02, INSTALLATION TO BE COMPLIED WITH ON MIL-S 4788270.

Part: LONGERON — CORRODED

OKC, C-CHECK, AFT PIT STA 1087-1098, LONG 29L, HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.

Part: SKIN — GOUGED (RT WING)

OKC - C-CHECK, RT WING LOWER IB T/E SKIN GOUGED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-10-4, 57-22-3.

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC, C-CHECK- PAX CABIN GALLEY 2 OB FLOOR ATTACH TRACK HAS CORROSION AT STA 237. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 51-30-5.

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - C-CHECK, CABIN FLOOR PANEL, STA 826-STA 886 DAMAGED AT FWD IB CORNER. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05.

Part: FLOORBOARD — BROKEN (CABIN)

OKC, C-CHECK - CABIN FLOOR PANEL AT STA 864 TO 886 BROKEN AT FWD END. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC- C-CHECK, CABIN FLOOR PANEL AT STA 886 TO 927 IS DAMAGED AT LOWER EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2

OKC, C-CHECK, LONGERON 30 CORRODED BETWEEN STA 1231 AND 1211 IN AFT PIT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02.

Part: FLOORBOARD — CORRODED (CABIN)

OKC - C-CHECK, CABIN FLOORBOARD AT STA 166 AND STA 152 AT RBL 7 HAS 2 EA CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05 PAR 44.

Part: SKIN — CRACKED (FUSELAGE)

OKC C-CHECK - LT NOSE GEAR AFT HINGE CUT OUT IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05, FIG 63.

Part: FLOORBOARD — BROKEN (FUSELAGE)

OKC, C-CHECK - CABIN FLOOR PANEL AT STA 927 TO 1003 BROKEN AT FORWARD CORNER. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.

Part: LONGERON — CORRODED (FUSELAGE)

OKC - C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO 1110 CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19.

Part: BEAM — CORRODED (CARGO DOOR)

OKC, C-CHECK - AFT CARGO DOOR LOWER BEAM CORRODED ON LOWER HORIZONTAL FRAME UNDER REPAIR DOUBLER. REMOVED DAMAGED BEAM, ORDERED AND REPLACED BEAM IAW SRM 51-30-5.

Part: SLAT TRACK — WORN (RT WING) · airframe 36,425 hrs · 19,188 cycles

RT SLAT TRACK NR 3 AFT IB RUB BLOCK FAILS CLEARANCE CHECK AND WORN. REWORKED RUB BLOCK IAW EA 2780-01020.

Part: SEAT TRACK — CORRODED (FUSELAGE)

OKC, C-CHECK- PAX CABIN GALLEY 2 IB FLOOR ATTACH TRACK HAS CORROSION AT STA 237. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 53-05, FIG 4.

Part: SKIN — DENTED (FUSELAGE)

OKC- C-CHECK- LT FUSELAGE SKIN DENTED OVER FRAME AT STA 237, BETWEEN LONG 18L AND 19L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, FINGER DOUBLER, AND STRAP IAW SRM 53-04, FIG 12C.

Part: SEALANT — MISSING (IDLER HINGE)

OKC - C-CHECK-LOG PG 5784367, SEALANT MISSING LT IDLER HINGE. NO ROTATION NOTED, APPLIED SEALANT TO BOTH ENDS OF BOLT IAW EA 5750-01098.

Part: SKIN — DENTED (FUSELAGE)

OKC - C-CHECK - FUSELAGE STATION 160 DENTED BETWEEN LONG 24L AND 25L X= .060 D .75 COLD WORKED SKIN BACK TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38.

Part: VANE — PUNCTURED (RT IB FLAP)

OKC - C-CHECK, RT IB FLAP OB FLAPVANE HAS A PUNCTURE ON THE IB END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2, PARA 18.

Part: SKIN — CHAFED (RT VERT STAB)

OKC - C-CHECK, RT VERTICAL STAB LOWER SURFACE CHAFED IN 5 EA SPOTS INNER BANANA FAIRING PANEL 3802A, ATTACHMENT AREA. REMOVED DAMAGED SKINS, ORDERED AND INSTALLED NEW SKINS IAW SRM 51-30-2.

Part: FLOORBOARD — DELAMINATED (PAX CABIN)

OKC - C-CHECK, FLOORBOARD IN PASSENGER CABIN AT STA 826-864, BETWEEN 22R AND 44R DELAMINATD AND CRACKED. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05.

Part: SKIN — DENTED (FUSELAGE)

OKC- C-CHECK - RT FUSELAGE SKIN DENTED AT STA 223 OVER LONG 4R (WITHIN 1 INCH OF LONG) COLD WORK TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04.

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - C-CHECK, FLOOR PANEL AT STA 826 TO 886 AFT IB CORNER ANGLE IS CRACKED. REMOVED, ORDERED AND REPLACED (W) ANGLE IAW SRM 51-30-8.

Part: FRAME — GOUGED (VERTICAL STAB)

OKC - C-CHECK, VERTICAL STABILIZER PANEL 6308C, CUT OUT JAMB GOUGED AROUND LAND ORDERED AND INSTALLED NEW FRAME IAW SRM 51-30-2.

Part: SKIN — DENTED (AFT CARGO DOOR)

OKC - C-CHECK, AFT CARGO DOOR SKIN DENTED UPPER AFT AREA X=.040, D=.60, FOUND TO BE CONDITION 1B IAW SRM 53-04, FIG 38, D/X=15.

Part: LANYARD — DISCONNECTED (EMERGENCY SLIDE)

FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD.

Part: CONTROL CABLE — WORN (NR 4 SLAT)

OAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M)

Part: FITTING — WORN (NR 4 SLAT)

OAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M)

Part: CONTROL CABLE — WORN (NR 4 SLAT)

OAK LINE CHECK, FOUND LT NR 4 SLAT CABLE FOUND TO BE WEARING INTO WING LEADING EDGE. REPLACED LEADING EDGE STRUCTURE IAW EA 5740-01361. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 25 INOPERATIVE. REINSTALLED, RECONNECTED LIGHT ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — DEFECTIVE (ROW 2)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT MISSING AT ROW 2. REPLACED LIGHT ASSEMBLY, THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY, INCLUDING BATTERY PACK. LIGHT THEN OPERATED NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, DISCOVERED EMERGENCY TRACK LIGHTS AT ROW 21-23 WERE INOPERATIVE. RECONNECTED LIGHTS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: FITTING — CORRODED (CABIN)

PAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR GIRT BAR ATTACH FITTINGS ON FLOORBOARD. REPLACED FITTINGS PER SRM 51-30-1. (M)

Part: WEB — CHAFED (VERTICAL STAB)

PAE - DURING 30K-CHECK, FOUND VERTICAL STABILIZER BULLET FAIRING WEB CHAFED AROUND EDGES WHERE PANEL 6308C TO UPPER TIP BULLET FAIRING IS INSTALLED. REPLACED WEB PER SRM 51-10-4. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON AFT CARGO BAY CLOSEOUT WEB FASTENER HOLES. REPAIRED CLOSEOUT WEB PER EA 5310-02075. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 1022-1041. REPLACED WEB PER SRM 51-30-2. (M)

Part: SKIN — DAMAGED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND FORWARD LOWER CORNER OF R1 DOOR CUTOUT DAMAGE. REPAIRED PER EA 5310-02071. (M)

Part: SKIN — CHAFED (VERTICAL STAB)

PAE - DURING 30K-CHECK, FOUND VERTICAL STABILIZER SKIN CHAFED FROM AFT TO CENTER AREA, WHERE BANANA FAIRING 3804A IS MOUNTED. REPAIRED VERTICAL STABILIZER SKIN PER EA 5530-01089. (M)

Part: SKIN — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON EXTERNAL SKIN AT FS 1122-1128. REPAIRED FUSELAGE SKIN PER EA 5330-01575. (M)

Part: LONGERON — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON LONGERON 28 AT FS 1097 TO 1113. REPAIRED LONGERON 28 PER EA 5310-02078. (M)

Part: PAN — GOUGED (CARGO DOOR)

PAE - DURING 30K-CHECK, FOUND AFT CARGO DOOR JAMB GOUGED AT LOWER FORWARD AND AFT BARRIER DOOR LOCK GUIDE BLOCK LOCATIONS. BLEND REPAIRED DOOR JAMB PER EA 5230-01168. (M)

Part: RETAINER — CORRODED (T/E FLAP)

PAE - DURING 30K-CHECK, FOUND CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING BEARING RETAINER FASTENER HOLES. REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M)

Part: SKIN — PUNCTURED (RT ELEVATOR)

PAE - DURING 30K-CHECK, FOUND HOLE PUNCHED THROUGH RIGHT ELEVATOR LOWER INBOARD END. REPAIRED ELEVATOR LOWER SKIN PER EA 5520-01117. (M)

Part: RETAINER — CORRODED (T/E FLAP)

PAE - DURING 30K-CHECK, FOUND CORROSION ON LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING BEARING RETAINER FASTENER HOLES. REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M)

Part: RETAINER — CORRODED (T/E FLAP)

PAE - DURING 30K-CHECK, FOUND CORROSION ON RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING LOWER BEARING RETAINER FASTENER HOLES. REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M)

Part: RETAINER — CORRODED (T/E FLAP)

PAE - DURING 30K-CHECK, FOUND CORROSION ON RIGHT WING OUTBOARD FLAP CENTER HINGE FITTING BEARING RETAINER FASTENER HOLES. REPAIRED BEARING RETAINER FASTENER HOLES PER EA 5750-01647. (M)

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

PAE - DURING 30K-CHECK, FOUND CORROSION ON RIGHT WIND INBOARD FLAP OUTBOARD HINGE FITTING BEARING BORE. REPAIRED HINGE FITTING BORE PER EA 5750-01645. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND AFT AIRSTAIR LOWER STRAP ASSY FRAME CRACKED JUST ABOVE LEFT WHEEL. REPLACED FRAME PER SRM 51-30-2. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON AFT CARGO DOOR CUTOUT AT STRAP AFT SIDE AT FS 1211. REPLACED STRAP PER SRM 51-30-5. (M)

Part: RECEPTACLE — CRACKED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND LEFT FORWARD OVERWING EXIT JAMB LOWER FORWARD LATCH PIN RECEPTACLE CRACKED AT BOTTOM OF CONE. REPAIRED LATCH PIN RECEPTACLE PER SRM 53-05, FIG 32A. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION FROM STRAP AT AFT GALLEY SERVICE DOOR CUTOUT FORWARD FRAME TO FLOOR JUNCTION. REPLACED STRAP PER SRM 51-30-5. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION FROM STRAP AT AFT GALLEY SERVICE DOOR CUTOUT FORWARD FRAME TO FLOOR JUNCTION. REPLACED STRAP PER SRM 51-30-3, 51-10-04, AND DOUG DWG 5937669. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND FLOOR WEB CORRODED AT FS 1098 TO 1174. REPLACED WEB PER SRM 51-30-1, 51-30-2, 51-10-04, AND 53-1. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND FRAME SHEAR TIE CRACKED IN AIRSTAIR COMPARTMENT AT FS 1437. REPLACED TIE PER SRM 51-10-02, 51-10-4, 51-30-04, AND 53-05. (M)

Part: WEB — CRACKED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND WEB CORRODED AT FS 237-256. REPLACED WEB PER SRM 51-30-2. (M)

Part: WEB — CHAFED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND APU COMPARTMENT CEILING CHAFED AT FS 1368. CUT OUT CHAFED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: DOOR FRAME — DAMAGED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND MECHANICAL DAMAGE ON RIGHT FORWARD SERVICE DOOR CUTOUT FORWARD LOWER CORNER. REPAIRED CUTOUT (JAMB PAN) PER EA 5301-02071. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR CUTOUT (JAMB) AFT EDGE ANGLE AT FLOOR. REPLACED ANGLE PER SRM 51-10-4, 51-30-2, AND 51-30-1. (M)

Part: WEB — CRACKED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND PAX CABIN CUSP WEB CRACKED AT FS 987-999. REPLACED WEB PER SRM 51-30-2, 51-30-5, AND 51-10-4. (M)

Part: SPLICE — DAMAGED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND FRAME TO FLOORBEAM SPLICE AT FS 984 TO HAVE ELONGATED HOLES. REPLACED SPLICE PER MM 20-10-15 AND SRM 53-14-3. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 1193-1231. REPLACED WEB PER SRM 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 984-1003. REPLACED WEB PER SRM 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON FLOORWEB AT FS 1140. REPLACED WEB PER SRM 51-30-2. (M)

Part: RIB — GOUGED (L/E SLAT)

PAE - DURING 30K-CHECK, FOUND LEFT WING NR 1 SLAT INBOARD RIB GOUGED IN INTERCONNECTING PIN BORE. REPLACED INBOARD RIB PER SRM 51-30-2. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR CUTOUT, JAMB, FORWARD EDGE ANGLE AT FLOOR. REPLACED ANGLE PER SRM 51-10-4, 51-30-2, AND 51-30-1. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION IN AFT CARGO BAY ON UPPER SURFACE OF LOWER FLANGE OF FAIL/SAFE ANGLE AT FASTENER HOLES AT FS 1117. REPLACED FAIL/SAFE ANGLE PER SRM 53-01 AND 51-30-02. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 712-731. REPAIRED WEB PER SRM 51-30-2, 53-01 FIG 1, 51-70-4 FIG 2, 51-10-3, AND MM 53-20-01. (M)

Part: SPLICE — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON CARGO TRACK LEFT LOWER SURFACE COMMON TO TRACK SPLICE AT FS 1211-1225. REPLACED SPLICE PER SRM 51-30-5, FIG 1. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND WEB CORRODED AT FS 522-541. REPLACED WEB PER SRM 51-30-02 AND 51-10-4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FS 1174. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION PER SRM 53-05 FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 674-693. REPLACED WEB PER SRM 51-30-2 AND 51-10-4. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON FLOOR WEB AT FS 235-313. INSTALLED NEW WEB PER SRM 51-30-2 AND SRM 52-30-1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FS 235-239. CUT OUT CORRODED LENGTH OF TRACK AND INSTALLED REPLACEMENT SECTION PER SRM 53-05, FIG 4F. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB IN PAX CABIN. INSTALLED NEW WEB PER SRM 53-01 AND 51-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 731-750. REPLACED WEB PER SRM 51-30-2, 51-10-4, AND 51-30-6. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 693-712. REPLACED WEB PER SRM 51-30-2. (M)

Part: WEB — CRACKED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND WEB CRACKED AT FASTENER HOLE AT FS 314. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-70-4. (M)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON FLOOR WEB AT FS 1250-1271. TRIMMED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-70-4 AND SRM 51-30-2. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND SEAT TRACK GOUGED AT FS 547. REMOVED SEAT TRACK SECTION FROM FS 531-550. SPLICED IN NEW SECTION. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CUSP WEB CORRODED AT FS 560-579. REPLACED WEB PER SRM 51-30-2, -1, 2, AND -5. (M)

Part: FITTING — CORRODED (SPOILER)

PAE - DURING 30K-CHECK, FOUND RIGHT WING GROUND SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M)

Part: FITTING — CORRODED (SPOILER)

PAE - DURING 30K CHECK, FOUND LEFT WING OUTBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M)

Part: FITTING — CORRODED (SPOILER)

PAE - DURING 30K CHECK, FOUND RIGHT WING INBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M)

Part: FITTING — CORRODED (SPOILER)

PAE - DURING 30K-CHECK, FOUND LEFT WING GROUND SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M)

Part: FITTING — CORRODED (SPOILER)

PAE - DURING 30K-CHECK, FOUND LEFT WING INBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M)

Part: FITTING — CORRODED (SPOILER)

PAE - DURING 30K-CHECK, FOUND RIGHT WING OUTBOARD FLIGHT SPOILER CENTER HINGE FITTING CORRODED. REPLACED SPOILER HINGE FITTING PER CMM 27-61-10. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CORROSION ON UPPER SURFACE OF INTERCOSTAL IN AFT CARGO BAY AT FS 1309-1322. REPLACED INTERCOSTAL PER SRM 51-30-5 AND 41-30-2. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 828-845. CUT OUT CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-70-4. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING 30K-CHECK, FOUND CORROSION ON TOP OF FRAME IN AFT CARGO BAY. INSTALLED NEW FRAME PER SRM 53-03, FIG 2A. (M)

Part: WIRE — DISCONNECTED (FWD CABIN)

LAS - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES AT ROW 2. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED DAMAGED SECTION OF WIRING AND TWO LENS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING PREFLIGHT CHECK, FORWARD TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPAIRED CONNECTION WIRE AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - DURING LINE MAINTENANCE, THE TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT ROW 22. FOUND WIRE PULLED FROM LIGHT SOCKET. REPLACED MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND FIRST SEVEN EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED. RECONNECTED LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING LINE MAINTENANCE CHECK, AFT EXTERIOR EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROWS 4-12 CABIN INOPERATIVE. REPLACED BATTERIES. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN AFT PAX CABIN INOPERATIVE. REPAIRED WIRING. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS IN AFT PAX CABIN DISCONNECTED. RECONNECTED LIGHTS. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND SEVERAL EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED. RECONNECTED MODULES AND REPLACED LAMP ASSEMBLIES AT ROWS 7 AND 10. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (L1 DOOR)

PDX - DURING PRE-FLIGHT CHECK, L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DISCONNECTED FROM SLIDE COVER AND FROM GIRT BAR. RECONNECTED GIRT BAR TO BOTH THE SLIDE COVER AND GIRT BAR. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTS AT CABIN ROW 33 WERE DETERMINED TO BE INOPERATIVE. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (FWD CABIN) · airframe 24,343 hrs · 13,080 cycles

OAK-DURING HANGAR MAINT CHECK, SECTION OF EMERGENCY TRACK LIGHTING N THE FWD CABIN AREA WAS DETERMINED TO BE INOPERATIVE. REPLACED LAMP MODULE AND ASSOCIATED BATTERY ASSEMBLY, LIGHTS OPERATED NORMALLY.

Part: LIGHT — DAMAGED (FWD CABIN)

DURING MAIN CHECK, FLOOR EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOP AND WITH COVERS MISSING AT FWD GALLEY, AT ROW 6, 10, AND 19.REPLACED BULBS AND COVERS AS REQUIRED. LIGHTS THEN OPERATED NORMALLY.

Part: WIRE — DISCONNECTED (AFT CABIN)

PDX - DURING MAINTENANCE, THE EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. INSPECTED AND FOUND DAMAGED WIRING. REPAIRED WIRING, SYSTEM OPERATES NORMAL. (M)

Part: WIRE — DISCONNECTED (FWD CABIN)

SEA PRIOR TO FLIGHT 328 THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE FOUND TO BE INOPERATIVE. RECONNECTED WITING AND THE LIGHTS OPERATED NORMALLY.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT SHEAR-TIE AT STA 1219, LONGERON 30 TO LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, INTERCOSTAL AT STA 1145 TO STA 1155 BETWEEN LONGERON 29R AND LONGERON 30 WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK THE AFT CARGO COMPARTMENT SHEAR-TIE AT STA 1193, LONGERON 30 TO LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT SHEAR-TIE AT STA 1155, LONGERON 30 TO LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT LONGERON 30 WAS FOUND CORRODED ON THE LOWER SURFACE OF THE FLANGE AT STA 1200. REPAIRED PER EA 5310-01861. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK AFT CARGO COMPARTMENT SHEAR-TIE AT STA 1145, LONGERON 30 TO LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PDX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT SHEAR-TIE AT STA 1174, LONGERON 30 TO LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT SHEAR-TIE AT STA 1231, LONGERON 30 TO LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT LONGERON 29R AT STA 1255 WAS FOUND CORRODED ON THE LOWER SURFACE OF THE UPPER HAT. REPAIRED PER SRM. (X)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 23,642 hrs · 12,714 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT LONGERON 30 AT STA 1240 WAS FOUND CORRODED IN THE LOWER SURFACE. REPAIRED PER SRM. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLIGHT 199, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FIRST CLASS CABIN. RECONNECTED WIRING AND SECURED TRACK, LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 3)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AT ROW 3 AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

SEA - DURING MAINTENANCE CHECK, THE FORWARD CABIN PORTABLE EMERGENCY LIGHT OUTPUT WAS FOUND WEAK. REPLACED BATTERIES AND LIGHT OPERATED NORMALLY. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — DISCHARGED (CABIN) · airframe 21,953 hrs · 11,871 cycles

SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X)

Part: MOTOR — INOPERATIVE (VERTICAL STAB)

RNO: CREW REPORTED THE PRIMARY HORIZONTAL STABILIZER TRIM & ALTERNATE HORIZONTAL STABIL. TRIM INOPERATIVE DURING CLIMBOUT, RET. TO RNO AND LANDED UNEVENTFULLY. REPLACED PRIMARY HORIZONTAL STABILIZER TRIM MOTOR & ALTERNATE HORIZONTAL STABILIZER TRIM MOTOR. REPLACED PRIMARY TRIM BRAKE SWITCH, CAPTAINS RIGH TRIM SWITCH, BOTH OF FIRST OFFICERS TRIM SWITCHES, AND ALTERNATE TRIM CONTROL SWITCH AND OPERATED NORMALLY. THIS REPORT REMAINS OPEN PENDING SHOP FINDINGS ON PRIMARY TRIM MOTOR AND ALTERNATE TRIM MOTOR.

Part: WIRE — DISCONNECTED (CABIN)

SEA - AFTER ARRIVAL OF FLT 395, CREW REPORTED THE FORWARD TWO EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: CONNECTOR — DISCONNECTED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED CONNECTOR TO LIGHT ASSEMBLY IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: SLIDE — WON'T TEST (CABIN)

PHX - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE FOUND INOPERATIVES. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 187, CREW REPORTED THE OVERHEAD EMERGENCY LIGHT IN THE FLIGHT COMPARTMENT WAS INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (ROW 21)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LOCK BAR — DAMAGED (COCKPIT)

SEA - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. REPLACED WINDOW UPPER LOCK BAR AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (ROW 25-27)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 25 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — FAILED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 282, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 534, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

ANC - PRIOR TO DEPARTURE OF FLT 92, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK LIGHTS IN THE FORWARD CABIN AND THEY OPERATED NORMALLY. (M)

Part: SKIN — GOUGED (CARGO DOOR)

OAK - DURING 15K CHECK, GOUGE WAS FOUND IN AFT CARGO COMPARTMENT DOOR EDGE ABOVE AFT UPLOCK LATCH FITTING. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE DOUBLER IAW ASA EA 5210-01070. (M)

Part: SKIN — DENTED (CARGO DOOR)

OAK - DURING 15K CHECK, DENT WAS FOUND IN FORWARD CARGO COMPARTMENT DOOR EDGE INBOARD OF AFT UPLOCK LATCH. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE DOUBLER IAW ASA EA 5210-01070. (M)

Part: BULBS — FAILED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED AFT TRACK SECTION, LAMPS AND LENSES AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

RNO - FLT 613 - AIR TURN BACK, CREW REPORTED, SMOKE/FUMES IN COCKPIT FROM GASPER VENTS AND SLIGHT ODOR NOTED. TURNED OFF AIR CONDITIONING PACKS AND SMOKE DISSIPATED. INSPECTED BOTH ENGINES INLET AND EXHAUST FOR FOD, INSPECTED APU INLETS AND WHEEL WELLS FOR FLUID LEAK, CHECKED BOTH COOLING TURBINES FOR OIL LEVEL AND LEAK, NO DEFECT OR LEAK NOTED. REPLACED BOTH WATER SEPARATOR COALESCERS, NO CONTAMINATION OR ODOR NOTED. ACCOMPLISHED RUN UP OF BOTH ENGINES AND OPERATED BOTH AIR CONDITIONING PACKS, NO SMOKE/FUMES OR ODOR NOTED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: HOLD OPEN HOOK — INOPERATIVE (L-1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE L-1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. REPLACED HOLD OPEN HOOK AND DOOR LATCHED NORMALLY. (M)

Part: STRUT — REQ'D SERVICE (NLG)

LAX - FLT NR 524 - THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR HANDLE WAS RAISED DURING TAKEOFF AT SAN. THE NOSE GEAR INDICATOR PIN IN THE COCKPIT RETRACTED, BUT CONSIDERABLE AIRSTREAM NOISE WAS EVIDENT IN NOSE AREA. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT LOW. INSPECTED NOSE GEAR UP POSITION SENSOR AND FOUND TO BE WITHIN TOLERANCES. SERVICED NOSE GEAR STRUT, PERFORMED GEAR RETRACTION AND SYSTEM OPERATED NORMALLY. (M)

Part: DOWNLOCK SWITCH — DEFECTIVE (NLG)

PDX - FLT 433 - CREW REPORTED, THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GER EXTENDED FOR LANDING. ACCOMPLISHED GEAR UNSAFE LIGHT CHECK LIST AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH S1-412 AND ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M)

Part: PROX SENSOR — OUT OF ADJUST (NLG)

ANC - FLIGHT 113, CREW REPORTED THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENDED FOR LANDING. ACCOMPLISHED GEAR UNSAFE LIGHT CHECK LIST AND LANDED WITHOUT INCIDENT. UNSAFE LIGHT EXTINGUISHED ON TOUCHDOWN. ADJUSTED NOSE LANDING GEAR PROXIMITY SENSOR AND ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M)

Part: PORTABLE LIGHT — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)

Part: SWITCH ASSY — DEFECTIVE (LT THROTTLE)

SEA - CREW REPORTED, THE LANDING GEAR AURAL WARNING SOUNDED AFTER GEAR HANDLE WAS RAISED AND ALL LANDING GEAR UNSAFE LIGHTS REMAINED ON AFTER LANDING GEAR RETRACTED AFTER TAKEOFF. LOWERED LANDING GEAR AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT THROTTLE SWITCH ASSEMBLY AND ACCOMPLISHED LANDING GEAR RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (W)

Part: PORTABLE EEL — DEFECTIVE (CABIN)

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

Part: GUST LOCK — LACK OF LUBE (R1 DOOR)

SEA - AFTER ARRIVAL OF FLT 547 - CREW REPORTED THE R1 DOOR GUST LOCK WOULD NOT ENGAGE PROPERLY. LUBED GUST LOCK MECHANISM AND OPERATED NORMALLY. (M)

Part: EEL PORTABLE — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)

Part: EEL — FAILED (TAILCONE)

OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST, CURRENT LOW. REPLACED THE EVACUATION SLIDE WITH A SERVICEABLE UNIT. (Z)

Part: EEL PORTABLE — DEFECTIVE (CABIN)

OAK - DURING C-CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)

Part: PORT EEL — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FWD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W)