N931AS

Part: TIRE — FAILED (MLG)

DURING LANDING ROLL, BOTH LT MLG TIRES RUPTURED. THE MLG STRUT DID NOT COLLAPSE, BUT SOME FUSELAGE DAMAGE WAS CAUSED BY FLYING PIECES OF TIRE MATERIAL. (AN O-53 FLIGHT IRREGULARITY/HAZARD REPORT HAS BEEN FILED AS HAS A PRELIMINARY ENGINEERING REPORT). THE POS-1 TIRE HAD BEN RETREAD 3 TIMES, POS-2 TIRE, 1 TIME. AIRCRAFT DAMAGE WAS REPAIRED AS REQUIRED. PIECES HAVE BEEN SENT TO MFG FOR ANALYSIS. (K)

Part: SKIN — DENTED (LT NR 5 SLAT)

OKC - DURING C-CHECK, FOUND LEFT WING NR 5 SLAT IS DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER SRM 57-03. (M)

Part: FRAME — CRACKED (FUSELAGE)

OKC - FOUND DURING C-CHECK, RIGHT MLG FORWARD INBOARD CORNER FRAME CHANNEL CRACKED. REPLACED FRAME PER SRM 51-10-4. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT ROWS 20 AND 21. REBONDED PANELS PER MM 25-00-00. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT CLASS DIVIDERS. REBONDED PANELS PER MM 25-00-00. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT G-3 AND G-4 GALLEYS. REBONDED PANELS PER MM 25-00-00. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - FOUND DURING C-CHECK, FLOOR PANEL DELAMINATED AT CABIN ROW 11. REBONDED PANEL PER MM 25-00-00. (M)

Part: FRAME — CRACKED (FUSELAGE)

OKC- DURING C-CHECK, FOUND RIGHT MLG AFT OUTBOARD CORNER FRAME CHANNEL REPAIR T-CRACKED. REPLACED PREVIOUS REPAIR PER SRM 53-05. (M)

Part: LIGHT — INOPERATIVE (CABIN)

OKC - FOUND DURING HV CHECK, PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M)

Part: SLIDE — FAILED (L-2 DOOR)

OKC - C-CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE FAILED TO INFLATE FULLY DURING DEPLOYMENT TEST IAW WK CARD 28525002. SLIDE ASSY WAS REPLACED INSP OF THE REMOVED ASSY REVEALED A DENTED ASPIRATOR. ASSY WAS OVERHAULED, INCLUDED REPLACEMENT OF ASPIRATOR, POWER UNIT, CYLINDER SLING, GIRT, AND GIRT ATTACHMENT. MOST PROBABLE CAUSE OF FAILURE WAS OBSTRUCTION OF THE ASPIRATOR PORT BY BUBBLEWRAP SECURED TO FUSELAGE TO PROTECT AC FROM IMPACT BY DEPLOYING SLIDE. MFG HAS DEVELOPED PROTECTIVE PADDING KIT: 1) CUSHIONED PAD TO PROTECT AC FROM IMPACT BY DEPLOYING SLIDE. 2) LARGE GROUND COVER TO PROTECT SLIDE FROM CONTAMINATION AND DAMAGE. SLIDE DEPLOYMENT TEST WK CARDS BEING REVISED TO SPECIFY USE OF KIT. (REV 3)

Part: LIGHT — INOPERATIVE (FWD CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 4. SPLICED BROKEN WIRE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LIGHT — INOPERATIVE (ROW 9)

SEA PREFLIGHT CHECK, FOUND EMEREGNCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 9 FORWARD. REPAIRED ASSOCIATED JUMPER WIRE TO BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

SEA LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE, BATTERY PACK DISCHARGED. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

SEA LINE CHECK, RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (ROW 29)

EMERGENCY TRACK LIGHTING INOPERATIVE AT ROW 29. REPLACED LIGHT MODULE (HOLDER AND LAMP). LIGHTS THEN OPERATED PROPERLY. (M)

Part: VANE — DELAMINATED (TE FLAP)

OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP, INBOARD VANE BONDED REPAIR HAS DELAMINATED LOWER SURFACE. REPAIRED PER SRM. (M)

Part: VANE — PUNCTURED (TE FLAP)

OKC - DURING 30K CHECK, FOUND RIGHT INBOARD FLAP, OUTBOARD VANE PUNCTURED LOWER SKIN AT INBOARD END. REPAIRED PER SRM. (M)

Part: SKIN — DENTED (RUDDER)

OKC - DURING 30K CHECK, FOUND RUDDER HAS DENT ON LEFT SIDE. REMOVED DAMAGE AND HOT BONDED .012 7075-T6 REPAIR DOUBELR TO RUDDER PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FORWARD FLIGHT ATTENDANT SEAT INBOARD FLOOR ATTACH ANGLE CORRODED. REPAIRED PER SRM. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURNG 30K CHECK, FOUND LONGERON 28L CORRODED IN FORWARD CARGO BAY AT FS 231. REPLACED DAMAGED SECTION PER SRM 53-02. (M)

Part: FLOORBOARD — CRACKED (FUSLEAGE)

OKC - DURING 30K CHECK, FOUND CABIN FLOORBOARD CRACKED. REPAIRED FLOORBOARD PER SRM. (M)

Part: MOUNT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND GALLEY MOUNT CORRODED. REPLACED MOUNT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 218. REPLACED SUPPORT PER SRM 51-10-3 AND 4. (M)

Part: SKIN — DENTED (CONTROL TAB)

OKC - DURING 30K CHECK, FOUND LEFT ELEVATOR CONTROL TAB HAS SHARP DENT ON LOWER SURFACE INBOARD SIDE. REPAIRED PER SRM. (M)

Part: SKIN — DENTED (RUDDER)

OKC - DURING 30K CHECK, FOUND RUDDER HAD DENT JUST ABOVE LOWER HINGE. REMOVED DAMAGED AND HOT BONDED REPAIR DOUBLER PER SRM. (M)

Part: TRACK — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FALSE TRACK CORRODED FROM STATION 160-200. REPLACED FALSE TRACK PER SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL CENTER POST HAS CORROSION JUST BELOW FLOOR LEVEL AT STRINGER 30L. REPAIRED PER SRM. (M)

Part: FITTING — CORRODED (CARGO DOOR)

OKC - DURING 30K CHECK, FOUND CORROSION ON CARGO DOOR BEAM TEE FITTING. REPLACED TEE FITTING PER SRM. (M)

Part: SKIN — DAMAGED (TE FLAP)

OKC - DURING 30K CHECK, FOUND RIGHT OUTBOARD FLAP TRAILING EDGE CREASED. REPAIRED FLAP TRAILING EDGE PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSLEAGE)

OKC - DURING 30K CHECK, FOUND SHEAR TIE AT FRAME 712 BETWEEN L30 AND L29. REPLACED SHEAR TIE PER SRM. (M)

Part: BULKHEAD — CRACKED (CRACKED)

OKC - DURING 30K CHECK, FOUND AFT PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT OP MOST RIVETS. REPLACED WEB AT BL 0 PER SRM 51-30-5. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT CARGO TRACKS BETWEEN L27R AND L28R ARE CORRODED. INSTALLED REPAIR DOUBLER PER SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT INTERCOSTAL BETWEEN 1287 AND 1309 HAS THREE CRACKS IN RADIUS. REPAIRED PER SRM. (M)

Part: RETAINER — CRACKED (FLOORBOARD)

OKC - DURING 30K CHECK, FOUND FLOORBOARD CENTER STATION 886-946 RETAINER CRACKED AROUND FASTENER. REPAIRED PER SRM. (M)

Part: BULKHEAD — GOUGED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND RIGHT MLG WHEEL WELL AFT PRESSURE BULKHEAD IS GOUGED AT FS 1003. REPLACED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 51-70-4. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND MID CARGO AREA INTERCOSTAL BETWEEN STRINGER L30 AND L29 IS CORRODED. REPLACED INTERCOSTAL PER SRM. (M)

Part: FLOORBOARD — PUNCTURED (FUSLEAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD HAS TWO PUNCTURES. REPLACED FLOORBOARD PER SRM. (M)

Part: FITTING — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND MID CARGO BAY LOWER DOOR JAMB FITTING IS CORRODED AT FS 636-644. REPLACED DAMAGED FITTING, SUPPORT PER SRM 51-10-2, 4, AND 5. (M)

Part: MOUNT — CORRODED (GALLEY)

OKC - DURING 30K CHECK, FOUND GALLEY MOUNT CORRODED. REPLACED MOUNT. (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND AFT CARGO AREA ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE PER SRM. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FORWARD PIT STATION 523, BULKHEAD SUPPORT ANGLE CORRODED. REPLACED SUPPORT ANGLE PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 160. REPLACED DAMAGED SUPPORT PER SRM 51-10-3. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT IN AFT CARGO BAY AT FS 1156 IS CORRODED. REPLACED SUPPORT PER SRM 51-10-4. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT CORRODED AT FS 196. REPLACED DAMAGED SUPPORT PER SRM 51-10-4. (M)

Part: FITTING — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FUSELAGE STATION 200 LBL 8 FITTING CORRODED. REPLACED FITTING PER SRM. (M)

Part: VANE CAP — CRACKED (LT ENG COWL)

OKC - DURING 30K CHECK, FOUND RIGHT OUTBOARD FLAP NR 3 VANE CAP CRACKED ON UPPER SURFACE. REPLACED VANE CAP PER SRM 51-30-1 AND 2. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING 30K CHECK, FUSELAGE DENTED AND GOUGED AT FS 1190. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: FLOORBOARD — GOUGED (FUSLEAGE)

OKC - DURNG 30K CHECK, FOUND FLOORBOARD STATION 811 RBL 22-43 LOWER SKIN CORNER GOUGED. REPAIRED PER SRM. (M)

Part: TIE — CRACKED (MLG DOOR)

OKC - DURING 30K CHECK, FOUND LT MLG DOOR FRAME TIE CRACKED INTERNAL STRUCTURE JUST BELOW GEAR BUMPER. REPAIRED PER SRM. (M)

Part: STIFFENER — CRACKED (NR 1 NACELLE)

OKC - DURING 30K CHECK, FOUND NR 1 ENGINE NOSE COWL TWO STIFFENERS CRACKED AFT SIDE OF FORWARD BULKHEAD AT 6 O'CLOCK POSITION. REPAIRED PER SRM. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD LOWER SURFACE CORNER IS CRACKED. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: ANGLE — CRACKED (LT WING)

OKC - DURING 30K CHECK, FOUND LEFT WING LEADING EDGE FRAME TIE IS CRACKED AT UPPER AFT END. REPLACED ANGLE PER SRM 51-10-2. (M)

Part: SHEAR TIE — CRACKED (RT WING)

OKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2, AND 30-5. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOOR SUPPORT EXFOLIATED AT FS 200. REPLACED SUPPORT PER SRM 51-10-3 AND 10-4. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD MISSING RIVETS AND IS DELAMINATED AT FS 200-237. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SHEAR TIE — CRACKED (RT WING)

OKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2 AND 30-5. (M)

Part: PRESSURE PANEL — CRACKED (MLG WW)

OKC - DURING 30K CHECK, FOUND OVERHEAD PRESSURE WEB CRACKED IN RIGHT MLG WHEEL WELL AT FS 995. CUT OUT DAMAGED SECTION AND REPLACED WITH DOUBLER PER SRM 53-04. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - DURING 30K CHECK, FOUND FLOORBOARD INSERTS MISSING AT FS 150-200. REPLACED FLOORBOARD PER SRM 53-05. (M)

Part: SHEAR TIE — CRACKED (RT WING)

OKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2, AND 30-5. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 3. REPLACED LIGHT MODULE (LENS/BULB). RESECURED COVER. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - FORWARD PASSENGER ENTRY L-1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M)

Part: WIRE HARNESS — FAILED (SERVICE DOOR)

OAK - DURING C-CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING LINE CHECK, THREE CABIN OVERHEAD EMERGENCY LIGHTS CAME ON WHEN AIRCRAFT BATTERY WAS SWITCHED OFF. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PACK AT B5-107. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — DEFECTIVE (CABIN)

SFO - DURING LINE CHECK, EMERGENCY LIGHTS IN TAIL AREA WERE DETERMINED TO BE INOPERATIVE. REPLACED DEFECTIVE BATTERY PACK ASSEMBLY. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (L1 DOOR)

SEA - DURING PRE-FLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM SLIDE COVER LATCH. REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER LATCH. (M)

Part: LAMP — BROKEN (CABIN ROW 7) · airframe 48,409 hrs · 30,908 cycles

PHX-DURING LINE CHECK, A SECTION OF EMERGENCY TRACK LIGHTING AT CABIN ROW 7 WAS DETERMINED TO BE INOPERATIVE. REPLACED LAMP MODULE, LIGHTS OPERATED NORMALLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING PREFLIGHT CHECK PRIOR TO FLIGHT 628, EMERGENCY TRACK LIGHTING AT ROW 10 WAS DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY ASSEMBLY. LIGHTS THEN OPERATED NORMALLY. (M)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE MID-CARGO COMPARTMENT LONGERON 28L WAS FOUND CORRODED AT STA 570 TO STA 579. REPAIRED PER EA 5310-01854. (X)

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT LONGERON 29R, STA 1260 TO STA 1280 WAS FOUND CORRODED AT THE UPPER FLANGE AT THE SPLICE. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE SHEAR TIE AT STA 1307, LONGERON 26L TO LONGERON 30 WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, AT THE AFT CARGO COMPARTMENT STA 1200, OUTBOARD LEG, LONGERON 28L, BOTTOM SIDE CORRODED AROUND FASTENERS. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT SHEAR TIE AT STA 1218 BETWEEN LONGERONS 29L AND 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE SHEAR TIE AT STA 1287, LONGERON 27L TO LONGERON 27R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT FRAME AT STA 1250 LONGERON 29R WAS FOUND CRACKED. REPAIRED PER SRM. (X)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE MID-CARGO COMPARTMENT INTERCOSTAL TO SKIN FASTENERS AT STA 693 TO STA 712, LONGERON 29L WERE FOUND CORRODED. REPAIRED PER SRM. (X)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE MID-CARGO COMPARTMENT STA 579, LONGERON 28R WAS FOUND CORRODED. REPAIRED PER EA 5310-01859. (X)

Part: FRAME — CORRODED (FUSELAGE)

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT FRAME WAS FOUND CORRODED AT STA 1322, LONGERON 30 UNDER THE VERTICAL SUPPORT. REPAIRED PER SRM. (X)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE MID-CARGO COMPARTMENT LONGERON 29L AT STA 579 TO STA 570 WAS FOUND CORRODED. REPAIRED PER EA 5310-01858. (X)

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT BEAM FROM STA 1212 TO STA 1220 AT LONGERON 29R WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT STA 1200 TO 1208, OUTBOARD LEG BOTTOM SIDE OF LONGERON 29L WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: SPLICE — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, AFT CARGO COMPARTMENT STA 1146, LONGERON 28R SPLICE WAS FOUND CORRODED. REPAIRED PER SRM. (X)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE LEFT TIE-DOWN TRACK AT STA 1212 TO STA 1232 SCREW HOLES WERE FOUND CORRODED. REPAIRED PER SRM. (X)

Part: STRUCTURE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE AFT CARGO COMPARTMENT STA 1075, LONGERON 28R, BOTTOM SIDE WAS FOUND CORRODED. REPAIRED PER EA 5310-01856. (X)

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 47,526 hrs · 30,468 cycles

PHX - DURING SCHEDULED C-CHECK, THE MID-CARGO COMPARTMENT RIGHT CARGO TRACK INTERCOSTAL CORRODED AT STA 769 TO STA 786, LONGERON 28R TO LONGERON 29R. REPAIRED PER SRM. (X)

Part: BATTERY — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 21 AND AT THE FORWARD OVERWING EMERGENCY EXITS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLYS AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: POWER SUPPLY — DEFECTIVE (CABIN)

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

Part: FITTING — CORRODED (BS 208-218)

PHX - DURING 15K CHECK, FOUND CORROSION ON LEFT LOWER FRAME FITTINGS AT FS 208 AND 218. REMOVED DAMAGED FITTINGS AND INSTALLED NEW FITTINGS IAW DC9 SRM 51-30-01 AND 51-30-05. (M)

Part: FLOORBEAM — CORRODED (BS 1338)

PHX - DURING 15K CHECK, FOUND CORROSION ON FLOORBEAM CAP, LBL 42 AT FS 1338. BLENDED DAMAGED AREA AND INSTALLED DOUBLER ANGLE AND WEAR STRIP IAW DC9 SRM 53-05, FIG 20A. (M)

Part: ANGLE — CORRODED (BS 208)

PHX - DURING 15K CHECK, FOUND CORROSION ON R1 DOOR LOWER CUSP ANGLE AT FS 208. REPAIRED IAW ASA EA 5310-01675 AND DC9 SRM 53-05, FIG 55. (M)

Part: FRAME — CORRODED (CARGO DOORWAY)

PHX - DURING 15K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER FRAME ON INBOARD SIDE. REPLACED BEAM IAW DC9 SRM 51-30-05 AND 53-05, FIG 63. (M)

Part: FITTING — CORRODED (BS 218)

PHX - DURING 15K CHECK, FOUND CORROSION ON THE LEFT FRAME SUPPORT FITTING AT FS 218. REMOVED DAMAGED SECTION OF FITTING AND INSTALLED REPAIR ANGLE AND DOUBLER IAW ASA EA 5310-01672. (M)

Part: WEB — CORRODED (BS 208-218)

PHX - DURING 15K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 208 TO 218. REPAIRED IAW ASA EA 5310-01679. (M)

Part: LONGERON — CORRODED (BS 1309)

PHX - DURING 15K CHECK, FOUND CORROSION ON LONGERON 29L AT FS 1309. REMOVED DAMAGED AREA AND SPLICED IN NEW SECTION IAW DC9 SRM 53-02, FIG 18. (M)

Part: LONGERON — CORRODED (BS 1231-1251)

PHX - DURING 15K CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 1231 TO 1251. REMOVED DAMAGED AREA AND SPLICED IN NEW SECTION IAW DC9 SRM 53-02, FIG 18. (M)

Part: FITTING — CORRODED (BS 1287)

PHX - DURING 15K CHECK, FOUND CRACK AND CORROSION ON LEFT FLOOR TRACK LOWER SUPPORT ANGLE FITTING BETWEEN LONGERONS 27L AND 28L AT FS 1287. REPLACED FITTING IAW DC9 SRM 51-30-00. (M)

Part: SEAT TRACK — CORRODED (BS 1092-1183)

PHX - DURING 15K CHECK, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK FROM FS 1092 TO 1183. REMOVED DAMAGED TRACK AND INSTALLED NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 630, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED THE WIRING AND LAMP MODULES IN THE FORWARD CABIN AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 630, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED THE WIRING AND LAMP MODULES IN THE FORWARD CABIN AND OPERATED NORMALLY. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRED WIRING TO THE LIGHT ASSEMBLY 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 OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (OVERWING EXIT)

SEA - DURING MAINTENANCE CHECK, THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: SLIDE — MALFUNCTIONED (PAX DOOR)

OAK - DURING CK CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: PIN — OUT OF TRACK (COCKPIT)

OAK - AFTER ARRIVAL OF FLIGHT 456, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDOW AFT HINGE PIN MIGRATED OUT OF POSITION. REPOSITIONED PIN INTO HINGE AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 9 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - FLT 231 - PRIOR TO DEPARTURE, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTING HAS LOOSE WIRING AND IS MISSING A LAMP AT ROW 2. REPLACED LAMP MODULE AND SECURED WIRING AT ROW 2, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT FROM ROWS 19 TO 22 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 88, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. ADJUSTED VERTICAL POSITION OF DOOR AND OPERATED NORMALLY. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - AFTER ARRIVAL OF FLIGHT 559, CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. ADJUSTED THE L1 DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 472, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. ADJUSTED THE L1 DOOR MECHANISM AND OPERATED NORMALLY. (M)

Part: SKIN — DENTED (RT LE SLAT)

FAI - AFTER ARRIVAL OF FLT 191; CREW REPORTED BIRD STRIKE DURING APPROACH. ACCOMPLISHED BIRD STRIKE INSPECTION AND FOUND RT WING NR 1 L/E SLAT DENTED. FERRIED AIRCRAFT TO SEA, REPAIRED AND INSTALLED DOUBLER IAW ASA EA 5750-01258. TT: 37,613 HOURS. TC: 25,343. (X)

Part: SEAL — OUT OF POSITION (L1 DOOR)

LAX - AFTER ARRIVAL OF FLT 253 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. REPOSITIONED THE L1 DOOR UPPR SEAL AND OPERATED NORMALLY. (M)

Part: SPRING — MISSING (L2 DOOR)

PDX - AFTER ARRIVAL OF FLT 530 - CREW REPORTED THE L2 DOOR WAS DIFFICULT TO OPEN. REPLACED THE L2 DOOR HANDLE ASSIST SPRING, REPOSITIONED LOWER HINGE SNUBBER BEARING, CLEANED AND LUBED SPRING GUIDE SHAFT AND OPERATED NORMALLY. (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: WINDOW — LACK OF LUBE (LT COCKPIT)

PDX - AFTER ARRIVAL OF FLT 592 - CREW REPORTED, THE CAPTAINS SLIDING WINDOW WAS DIFFICULT TO OPEN. LUBRICATED THE WINDOW UPPER SLIDE TRACK AND OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (RT WING)

SEA - RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5730-010151. (M)

Part: STOP PINS — OUT OF ADJUST (L1 DOOR)

SEA - AFTER ARRIVAL OF FLIGHT 621, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. ADJUSTED THE DOOR STOP PINS AND OPERATED NORMALLY. (M)

Part: SEAL — STICKING (L1 DOOR)

SEA - AFTER ARRIVAL OF FLT 365, CREW REPORTED THE L1 DOOR HANDLE STICKS AND DIFFICULT TO OPEN. LUBRICATED DOOR UPPER TRIM SEAL. CHECKED HANDLE PULL FORCE AND FOUND TO BE WITHIN MM LIMITS. OPERATED DOOR AND OPERATED NORMALLY. (M)

Part: LIGHTS — FAILED TEST (R1 DOOR)

OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M)

Part: DOOR — OUT OF ADJUST (L1 DOOR)

SEA - AFTER ARRIVAL OF FLIGHT 367 - CREW REPORTED, THE L1 DOOR CATCHES DURING OPENING. ADJUSTED L1 DOOR AND OPERATED NORMALLY. (M)

Part: LATCH MECHANISM — LACK OF LUBE (L1 DOOR)

ANC - AFTER ARRIVAL OF FLT 112, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED LATCH MECHANISM AND DOOR OPERATED NORMALLY. (M)

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

LAS - PRIOR TO DEPARTURE OF FLT 627 - CREW REPORTED, THE L1 DOOR WOULD NOT LOCK CLOSED. ADJUSTED THE HOLD OPEN HOOK AND DOOR OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 22 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: SNUBBER — LACK OF LUBE (L-2 DOOR)

ANC - FLT 181 - CREW REPORTED, LEFT AFT SERVICE DOOR DIFFICULT TO CLOSE. CLEANED AND LUBED DOOR SNUBBER, DOOR 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: POWER SUPPLY — INOPERATIVE (CABIN)

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

Part: TURNBUCKLE — OUT OF ADJUST (PAX DOOR)

PDX - AFTER ARRIVAL OF FLT 485, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN FROM INSIDE. ADJUSTED TURNBUCKLE FOR UPPER DOOR RELIEF GATE AND DOOR OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (X)

Part: HYD LINE — BROKEN (LT MLG)

PDX - FLT 427 - AFTER ARRIVAL, CREW REPORTED THAT 3 MINUTES AFTER REACHING CRUISE AT FL 350 DEPARTING OAK, LOST RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE. LANDED WITHOUT INCIDENT. FOUND GOOSE STUCK IN LT MLG STRUT ASSY AND BROKEN HYDRAULIC LINE TO THE LT MLG DOWNLOCK CYLINDER. REPLACED LINE AND SERVICED HYDRAULIC RESERVOIR. (X)

Part: DOOR — OUT OF ADJUST (L1 DOOR)

PDX - AFTER ARRIVAL OF FLIGHT 481, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. FOUND BOTTOM OF DOOR DRAGGING ON LOWER SILL. ADJUSTED DOOR PER MM AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD ONE-THIRD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, LIGHTS OPERATED NORMALLY. (M)

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD ONE-THIRD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, LIGHTS OPERATED NORMALLY. REFERENCE NR ASAA9580247.

Part: EEL SOCKET — SHORTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 2 SHORTED LAMP SOCKETS AND REPLACED F1 FUSE IN POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRE — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK THE L-2 DOOR EXIT IDENTIFIER LIGHT WAS FOUND INOPERATIVE. SECURED LOOSE GROUND WIRE AND LIGHT OPERATED NORMALLY. (W)

Part: EEL WIRE — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT AT ROW 14 WAS FOUND INOPERATIVE. SECURED LOOSE GROUND WIRE AND LIGHT OPERATED NORMALLY. (W)

Part: SEAT TRACK — CORRODED (BS 210)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK Y210, X-45, Z PLUS 1. REMOVED CORRODED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05 PG 10, 51-10-03 PG 18, 51-10-04 PG 16, 51-20-00 PGS 1 AND 7, 51-30-01 PGS 1 AND 4, 51-30-02 PG 1, 51-30-05 PGS 1, 4, 4A 6 AND 7. (W)

Part: FRAME — CORRODED (BS 1233)

PAE - DURING 30 K CHECK, CORROSION WAS FOUND ON FRAME AT Y1233, X PLUS 12 TO X-8 AND AFT SIDE OF FRAME. REMOVED CORROSION, FRAME OUT OF LIMITS. REMOVED DAMAGED SECTION AND REPAIRED FRAME IAW DC-9 SRM 53-03, 53-01, 53-14-03, 51-30-05. (W)

Part: MEMBRANE — CORRODED (BS 1142)

PAE - DURING 30K CHECK CORROSION WAS FOUND ON CEILING WEB IN LEFT TUNNEL OF AFT CARGO COMPARTMENT AT Y1142, Z PLUS 52, Z PLUS 0. REMOVED MEMBRANE. INSTALLED NEW MEMBRANE WET WITH SEAL AT FUS STATION 984-1338, X PLUS 52, Z PLUS 0 IAW DOUGLAS AIRCRAFT DRAWING NR 9930612. (W)

Part: FRAME — CORRODED (BS 1311)

PAE - DURING 30 K CHECK, CORROSION WAS FOUND ON FRAME AT Y1311, Z-43, X PLUS 0. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 53-14-03 PGS 24-26, 51-10-01 PG 50, 53-03 PG 1, 51-10-03 PGS 15 AND 18. (W)

Part: INTERLOCK — OUT OF ADJUST (FWD ENTRY DOOR)

LAX - DURING MAINTENANCE THE FWD ENTRY DOOR WOULD NOT LATCH PROPERLY. ADJUSTED DOOR INTERLOCK MECHANISM AND OPERATED NORMALLY. (W)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 18 TO 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W)

Part: FAIRING — OUT OF ADJUST (LT TE FLAP)

SEA - DURING SERVICE CHECK, THE LEFT INBOARD FLAP FAIRING WAS FOUND TO BE OUT OF ADJUSTMENT. WITH THE FLAPS RETRACTED, THE LEFT MLG DOOR WOULD NOT OPEN DUE TO INTERFERENCE FROM FLAP FAIRING. ADJUSTED THE FLAP FAIRING PER MM 27-51-0 AND MLG DOOR OPERATED NORMALLY. (W)

Part: INTERLOCK SPRING — BROKEN (L2 DOOR)

PDX - DURING SERVICING THE L2 SERVICE DOOR WOULD NOT LOCK OPEN OR CLOSED NORMALLY. REPLACED THE DOOR INTERLOCK SPRING AND CAM FOLLOWER AND DOOR OPERATED NORMALLY. (Z)

Part: CAM FOLLOWER — DEFECTIVE (L2 DOOR)

PDX - DURING SERVICING THE L2 SERVICE DOOR WOULD NOT LOCK OPEN OR CLOSE NORMALLY. REPLACED THE DOOR INTERLOCK SPRING AND CAM FOLLOWER AND DOOR OPERATED NORMALLY. REFERENCE ASAA9580003.

Part: DOOR HANDLE — OUT OF SEQUENCE (FWD ENTRY DOOR)

ONT - PRIOR TO DEPARTURE OF FLIGHT 383 CREW REPORTED THE FORWARD ENTRY DOOR WOULD NOT LATCH PROPERLY. CYCLED DOOR HANDLE AND OPERATED NORMALLY. (Z)

Part: DOOR — OUT OF ADJUST (FWD ENTRY DOOR)

PDX - DURING MAINTENANCE, THE FORWARD ENTRY DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. ADJUSTED THE HORIZONTAL RIG AND DOOR OPERATED NORMALLY. (Z)

Part: DOOR — DIFF TO CLOSE (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED DOOR AND OPERATED NORMALLY. (Z)

Part: EEL WIRING — LOOSE (CABIN)

SEA - DURING CHECK, CEILING EMERGENCY LIGHTS AT ROWS 6 TO 9, 15 TO 18 AND 26 TO 29 INOP. MAINTENANCE ATTACHED LOOSE GROUND WIRES TO GROUND STUDS. OPS CHECKED NORMAL. (W)

Part: EEL BATTERY PACK — DISCHARGED (EXTERIOR)

SEA - DURING CHECK, EXTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK. (W)

Part: SKIN — DENTED (MID CARGO DOOR)

PAE - DURING 30K CHECK, A DENT WAS FOUND IN MID-CARGO COMPARTMENT DOOR. REMOVED DAMAGED AREA. FABRICATED DOUBLER, FILLER AND SHIMS. INSTALLED REPAIR WITH SEALANT AND SECURED WITH FASTENERS IAW SRM 52-05, FIGURE 3 AND 5-10-03, PGS 15 AND 18. (X)

Part: SEAT TRACK — CORROSION (CABIN)

PAE - DURING 30K CHECK CORROSION WAS FOUND ON SEAT TRACK FROM Y1098 TO Y1212, X-0, Z-0. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-10-03, 51-10-04, 51-20-00, 51-30-01, 51-30-02 AND 53-14-03. (Z)

Part: MOPSILL — CORROSION (R1 DOOR)

PAE - DURING 30K CHECK CORROSION WAS FOUND ALONG MOPSILL AT R1 DOOR. REMOVED CORODED MOPSILL WEB Y160 TO Y184, X-53 TO X-57.5, Z PLUS 1. FABRICATED NEW WEB. ALODINED, PRIMED, PAINTED AND INSTALLED IAW SRM 51-30-01, 51-30-02, 53-01 AND 53-20-01. (Z)

Part: SEAT TRACK — CORROSION (CABIN)

PAE - DURING 30K CHECK CORROSION WAS FOUND ON SEAT TRACK FROM Y201 TO Y225, X PLUS 22, Z PLUS 1. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-20-00, PGS 1-15, 51-30-01, PGS 1-8, 51-30-05, PGS 1-10, AND 53-03, PG 10. (Z)