N932AS

Part: HOOK — OUT OF ADJ (FWD PAX DOOR)

SEA - PRIOR TO FLT, L-1 DOOR WOULD NOT LATCH OPEN. THE L-1 DOOR HOLD OPEN HOOK WAS FOUND TO BE OT OF ADJUSTMENT. THE DOOR HOLD OPEN HOOK WAS ADJUSTED AND THE DOOR OPERATED NORMALLY. (M)

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB)

OAK - DURING C-CHECK INSPECTION, THE RIGHT HINGE OUTBOARD LUG, INBOARD HINGE PLATE, VERTICAL-TO-HORIZONTAL STABILIZER AFT ATTACH WAS FOUND CORRODED AND PITTED. (M)

Part: PLATE — CORRODED (HORIZONTAL STAB)

OAK - DURING C-CHECK INSPECTION, THE RIGHT HINGE OUTBOARD LUG, INBOARD HINGE PLATE, VERTICAL-TO-HORIZONTAL STABILIZER AFT ATTACH WAS FOUND CORRODED AND PITTED. (M)

Part: SLIDE — WILL NOT TEST (TAIL CONE EXIT) · airframe 45,521 hrs · 29,586 cycles

OAK - DURING C-CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (X)

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,507 hrs · 29,578 cycles

OAK - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 26 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

SEA - AFTER ARRIVAL OF FLT 631, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FLICKERED ON LANDING. ACCOMPLISHED OPERATIONAL CHECK OF THE EMERGENCY LIGHTS SYSTEM. ALL LIGHTS OPERATED NORMALLY WITH THE EXCEPTION OF THE OVERHEAD EMERGENCY LIGHTS AT ROW 15. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

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

Part: BATTERIES — DISCHARGED (CABIN)

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

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS REMAIN ILLUMINATED WITH ELECTRIC POWER OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: RETAINER — CRACKED (CARGO BAY)

LCQ - DURING 15K CHECK, A PREVIOUS REPAIR WELD ON A MID CARGO COMPARTMENT LINER RETAINER WAS FOUND CRACKED. REPAIRED IAW ASA EA 5320-01347. (M)

Part: WEB — GOUGED (CARGO BAY)

LCQ - DURING 15K CHECK, THE FORWARD CARGO COMPARTMENT DOOR JAMB WAS FOUND BENT AND GOUGED. REPAIRED IAW ASA EA 5320-01348. (M)

Part: SKIN — DENTED (L/E SLAT)

LCQ - DURING 15K CHECK, DENTS WERE FOUND ON LEFT WING NR 2 L/E SLAT SKIN. REPAIRED IAW ASA EA 5750-01299. (M)

Part: SKIN — DAMAGED (BS 400-420)

LCQ - DURING 15K CHECK DAMAGE TO FUSELAGE SKIN FROM LIGHTNING STRIKES WERE FOUND FROM STATION 400 TO STATION 420. REPAIRED IAW ASA EA 5330-01352. (M)

Part: SPAR — CORRODED (HORIZONTAL STAB)

LCQ - DURING 15K CHECK, CORROSION FOUND ON HORIZONTAL STABILIZER FORWARD SPAR LOWER CAP AT AFT BARREL NUT CLEARANCE HOLE. REPAIRED IAW ASA EA 5510-01070. (M)

Part: SKIN — GOUGED (L/E SLAT)

LCQ - DURING 15K CHECK, GOUGES WERE FOUND ON RIGHT WING NR 0 L/E SLAT SKIN. REPAIRED IAW ASA EA 5750-01298. (M)

Part: SKIN — DAMAGED (BS 301/313)

LCQ - DURING 15K CHECK, INTERIM REPAIRS TO DAMAGED FUSELAGE SKIN AT STATION 301 AND STATION 313 REQUIRED PERMANENT REPAIR. REPAIRED IAW ASA EA 5330-01347. (M)

Part: SKIN — DAMAGED (SERVICE DOOR)

LCQ - DURING 15K CHECK, FUSELAGE SKIN AT AFT LAVATORY SERVICE DOOR CUT OUT WAS FOUND CHAFED THROUGH. REPAIRED IAW ASA EA 5330-01351. (M)

Part: SLIDE — FAILED (PASSENGER DOOR)

LCQ - DURING 15K CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)

Part: BATTERY — DISCHARGED (ROW 9-10)

LAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 10 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 AFT CABIN AND LOWER TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: LATCH MECHANISM — OUT OF ADJUST (LT COCKPIT)

PDX - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT LT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED THE LT SLIDING WINDOW LATCH MECHANISM AND OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (WS 286)

SEA - DURING MAINTENANCE CHECK, FOUND RIGHT WING LOWER SURFACE SKIN CRACKED AT FORWARD OUTBOARD RADIUS OF FUEL PANEL DOOR CUTOUT. REPAIRED PER ASA EA 5720-01129. (M)

Part: LONGERON — CORRODED (BS 160-208)

OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 30 AT FUSELAGE STATION 176. REMOVED AND REPLACED CORRODED SECTION OF LONGERON 30 FROM FUSELAGE STATION 160 TO 208 IAW DC9 SRM 53-02, PAGE 5. (M)

Part: RIB — CRACKED (WS 189)

OAK - DURING C-CHECK, FOUND CRACK IN THE LEFT WING L/E RIB BETWEEN NR 6 AND NR 7 SLAT TRACKS. REPAIRED PER ASA EA 5710-01039. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: BATTERIES — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE OVERWING EMERGENY EXIT LIGHTS WERE FOUND DIM. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 7 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (X)

Part: SLIDE BOTTLE — LOW PRESS (TAILCONE EXIT)

SEA - FLT NR 242 - CREW REPORTED TAILCONE EMERGENCY EVACUATION SLIDE PRESSURE LOW. REPLACED TAILCONE SLIDE ASSEMBLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (W)

Part: HYD LINE — BROKEN (LT TR UNIT)

PDX - AIR TURN BACK OF FLIGHT 524, CREW REPORTED, THE LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE WARNING LIGHT ILLUMINATED AND LEFT HYDRAULIC QUANTITY DECREASED, SHUT OFF LEFT ENGINE DRIVEN HYDRAULIC PUMP AND HYDRAULIC QUANTITY STABILIZED. LANDED WITHOUT INCIDENT. FOUND HYDRAULIC LINE FROM LEFT ENGINE THRUST REVERSER ACCUMULATOR TO ACCUMULATOR LOW PRESSURE WARNING SWITCH LEAKING. REPLACED HYDRAULIC LINE AND SERVICED HYDRAULIC SYSTEM. (M)

Part: HYD LINE — BROKEN (LT ENGINE TR)

PDX - JUST PRIOR TO PARKING AT GATE OF FLIGHT NR 475, CREW REPORTED SMOKE/FUMES IN CABIN AND LEFT HYDRAULIC QUANTITY DECREASED TO ZERO. SHUTDOWN ENGINES, APU, ELECTRICAL POWER AND OPENED ALL DOORS. PASSENGERS DEPLANED WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE SWITCH BROKEN. REPLACED HYDRAULIC LINE AND SERVICED LEFT HYDRAULIC SYSTEM. (M)

Part: HYD LINE — BROKEN (LT TR UNIT)

SFO - FLT NR 232 - AFTER LANDING, FLIGHT ATTENDANTS REPORTED FUMES/VAPOR IN CABIN. CREW NOTED LEFT HYDRAULIC QUANTITY AT 'O' ENTERING TAXI WAY. ACCOMPLISHED EMERGENCY EVACUATION OF PASSENGERS ON TAXI WAY WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE SWITCH BROKEN. HYDRAULIC FLUID MIGRATED INTO APU INLET CAUSING FUMES/VAPOR IN CABIN. REPLACED HYDRAULIC LINE, HYDRAULIC CASE DRAIN FILTERS AND WATER SEPARATOR COALESCERS, SERVICED AND BLED HYDRAULIC SYSTEM. (M)

Part: PORTABLE — DEFECTIVE (CABIN)

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

Part: EEL GROUND — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 16 WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD B5-102 AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL SOCKET — CORRODED (CABIN)

SEA - ONE CEILING EMERGENCY LIGHT INOP, ROW 24. MAINTENANCE CLEANED SOCKET. (W)

Part: EEL LAMP — FAILED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 24 WAS FOUND INOPERATIVE. RELAMPED AND LIGHT OPERATED NORMALLY. (W)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 14 THROUGH 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W)

Part: MOPSILL — CORRODED (L2 DOOR)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON L2 DOOR MOPSILL BETWEEN GIRT BARS AND FUSELAGE. REMOVED CORRODED MOPSILL CUSP MEMBRANE. INSTALLED NEW MEMBRANE IAW DC-9 SRM 53-05, 51-30-00, 51-30-01, 51-30-02, 51-10-03, TRAMCO EWO 95-8022. (W)

Part: FRAME — CORRODED (BS 1271)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1271 BETWEEN LONGERON 25L AND 27R. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 51-20-00, 51-30-05, 51-10-03, 53-03. (W)

Part: FRAME — CORRODED (BS 1250)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1250 BETWEEN LONGERON 26L AND 29R. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 51-10-03, 51-30-00, 51-30-01, 51-30-02, 51-30-05, 51-30-08, 51-10-03. (W)

Part: FRAME — CORRODED (BS 1155)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1155 BETWEEN LONGERON 29L AND 28R. REPLACED FRAME IAW DC-9 SRM 53-14-03, 51-14-03, 51-30-05, 51-10-02, 51-30-02. (W)

Part: SEAT TRACK — CORRODED (BS 231)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y231, X-45, Z PLUS 0. REMOVED CORRODED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05 PG 8R, 9, 10G AND 10P, 51-10-03 PG 15, 18 AND 21, 51-10-04 PG 1 AND 16, 51-20-00 PG 4A, 7 AND 8, 51-30-01 PG 1 AND 4, 51-30-05 PG 2 AND 7. (W)

Part: FRAME — CORRODED (BS 1231)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1231 BETWEEN LONGERON 26L AND 29R. REPAIRED FRAME IAW DC-9 SRM 53-03, 51-10-03, 53-01, 53-30-20. (W)

Part: FRAME — CORRODED (BS 1326)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1326, Z-42, X PLUS 0. FABRICATED REPAIR SPLICES AND FRAME. CLEANED, TREATED. ALODINED AND PRIMED. INSTALLED REPAIR PARTS AND FASTENERS IAW DC-9 SRM 53-03 FIG 2A 51-30-05 PG 8A, 51-10-03 PG 14, 18A AND 21, 51-30-01 PG 8 AND 14, 51-30-02 PG 1. TOTAL CYCLES 28294. (W)

Part: SKIN DOUBLER — CORRODED (BS 212)

PAE - DURING 30K CHECK CORROSION WAS FOUND ON SKIN DOUBLER AT Y12, X-1, Z-50. REMOVED CORRODED DOUBLER. INSTALLED NEW FINGER DOUBLER LONGERON IAW DC-9 SRM 53-02, 53-14-01, 51-10-03, 51-01, 51-30-02, 51-30-01, 53-34-00. TOTAL CYCLES 20,062. (W)

Part: CARGO TRACK — CORRODED (BS 218-370)

PAE - DURING 30K CHECK CORROSION WAS FOUND AROUND FASTENER HOLES IN CARGO TRACK AT Y300-Y350, X-22, Z-44. REMOVED CORRODED CARGO TRACK. INSTALLED NEW CARGO TRACK IAW DC-9 SRM 53-05, 51-10-03, 51-30-02, 51-30-05. TOTAL CYCLES 20,062. (W)

Part: FRAME — CORRODED (BS 636)

PAE - DURING 30K CHECK, CORROSION WAS FOUND IN FASTENER HOLE AT FRAME AT Y636, X-18, Z-44. REPAIRED FRAME IAW DC-9 SRM 53-01 FIG 2, 51-10-03 PG 15, 51-30-05 PG 1, 2, AND 2A, 51-10-03 PG 3. (W)

Part: ANGLE — CORRODED (BS 1155)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME TO SKIN SUPPORT ANGLE ON FRAME Y1155, X-6, Z-45. REMOVED DAMAGED SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE IAW DC-9 SRM 51-30-05, 51-30-02. (W)

Part: THRESHOLD — CORRODED (CARGO COMPT)

PAE - DURING 30K CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LOWER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1217, LONGERON 29. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01330. (M)