N589AA

Part: SKIN — DENTED (FUSELAGE) · airframe 66,667 hrs · 28,493 cycles

RIGHT FORWARD FUSELAGE HAS 2 DENTS FROM STATIONS 253 TO 275, LONGERONS 27 TO 28 RIGHT. INSTALLED DOUBLER PER SRM 53-04-3 FIGURE 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,667 hrs · 28,493 cycles

TWO DENTS WITH CRACKS ON LOWER FUSELAGE, FORWARD OF THE FORWARD CARGO DOOR. INSTALLED DOUBLER PER SRM 53-04-03, FIGURE 2.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 66,133 hrs · 28,230 cycles

CEILING EMERGENCY LIGHTS IN ENTRYWAY FORWARD GALLEY ON WITH AIRCRAFT POWERED OFF. RESET AIRCRAFT POWER, OPS CHECK NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 63,449 hrs · 26,897 cycles

RNO - INFLIGHT DFW-SMF. CREW REPORTED LEFT ENGINE OVERTEMP INDICATION FOLLOWED BY AUTO SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT DIVERTED RNO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT RNO ON 11/03/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,881 hrs · 26,097 cycles

CANT FRAME AFT ACCY STATION 1510 CRACKED. INSTALLED DOUBLER PER SRM 53-14-04.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,881 hrs · 26,097 cycles

CRACK IN FRAME STATION 1510. INSTALLED DOUBLER PER SRM 53-01-00.

Part: LAMP — MISSING (CABIN) · airframe 60,950 hrs · 25,670 cycles

ESCAPE PATH LIGHT AT SEAT 11D MISSING LAMP. REPLACED LAMP FOR SEAT 11D ESCAPE PATH LIGHT. OPS CHECK NORMAL

Part: GUARD — MISSING (CABIN) · airframe 60,950 hrs · 25,670 cycles

ESCAPE PATH LIGHT AT SEAT 11D MISSING GUARD. REPLACED GUARD FOR SEAT 11D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 60,950 hrs · 25,670 cycles

ESCAPE PATH LIGHT AT SEAT 11D MISSING LENS. REPLACED LENS FOR SEAT 11D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,900 hrs · 25,179 cycles

FORWARD GALLEY EMERGENCY LIGHT BATTERY DID NOT CHECK OUT ON TEST. REPLACED FORWARD GALLEY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED NORMAL.

Part: GUARD — MISSING (CABIN) · airframe 58,806 hrs · 24,694 cycles

GUARD MISSING ON SEAT 23D ESCAPE PATH LIGHT. REPLACED GUARD FOR SEAT 23D ESCAPE PATH LIGHT. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,806 hrs · 24,694 cycles

SEAT MOUNTED EMERGENCY LIGHTS ROW 20 DEF TO AFT OF AIRCRAFT. REPLACED POWER SUPPLY ABOVE LEFT NUMBER 2 DOOR. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,806 hrs · 24,694 cycles

SEAT MOUNTED EMERGENCY LIGHTS ROW 20 DEF TO AFT OF AIRCRAFT. REPLACED POWER SUPPLY ABOVE 20D. OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 58,806 hrs · 24,694 cycles

ESCAPE PATH LIGHTING AT SEAT 27D MISSING LENS. REPLACED LENS FOR ESCAPE PATH LIGHTING AT SEAT 27D, OPS CHECKED NORMAL.

Part: BOOT — LEAKING (AUXILIARY TANK) · airframe 58,490 hrs · 24,563 cycles

OKC - INFLIGHT DFW-SEA. CREW REPORTED LOUD BANG FROM CABIN THEN LOSS OF PRESSURIZATION. NO MASKS WERE DEPLOYED. EMERGENCY DECLARED DIVERTED OKC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK COMING FROM AFT AUXILIARY TANK BOOT. FLIGHT FERRIED TO TUL TO REPLACE AFT AUXILIARY TANK BOOT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PAN — LOOSE (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

AFT GALLEY DOOR HOLD OPEN PIN LOOSE IN FUSELAGE. REPLACED AFT SERVICE DOOR HOLD OPEN PAN/PIN ASSEMBLY PER AARD53-00-00-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

CORROSION ON RIGHT CUSP AT STATION 218 INBOARD OF SEAT TRACK NUMBER 6. REMOVED AND REPLACED SECTION OF CUSP SHEET FROM STATION 218 TO 237.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

FUSELAGE SKIN CORROSION AT AFT LAVATORY SERVICE PAN BETWEEN SKIN PLIES. REMOVED CORROSION AND INSTALLED TITANIUM DOUBLER.

Part: PAN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

FORWARD CARGO DOOR CUTOUT AT LOWER DOOR FRAME PAN CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

CORROSION AT AFT CARGO DOOR CUTOUT ON LOWER DOOR BEAM AT STATION 1155 TO 1212. INSTALLED DOOR BEAM DOUBLER.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

CORROSION ON AFT CARGO WEB INBOARD OF CARGO DOOR CUTOUT AT STATION 1150 TO 1160. REMOVED AND REPLACED WEB PER SRM 51-30-05.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

CORROSION ON AFT CARGO DOOR BEAM AT STATION 1155 TO 1212. REMOVED CORROSION AND INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

DENT IN SKIN LONGERON 30, STATION 389. ACCOMPLISHED INTERNAL DOUBLER REPAIR UNDER SRM 54-04 FIG 38.

Part: TEE FITTING — CORRODED (BS 168) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

RIGHT CUSP T-ANGLE BLENDED OUT OF LIMITS AT STATION 168 AND AT TANGS 178 TO 180. REMOVED CORROSION AND INSTALLED A TITANIUM DOUBLER.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

FORWARD MOUNT SUBFLOOR CORRODED AT STATION 160 AT G1. REMOVED DAMAGE AND INSTALLED A 4 INCH BY 5 INCH DOUBLER.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

CORROSION ON VERTICAL AND HORIZONTAL LEGS OF MID CARGO DOOR BEAM. REMOVED CORROSION AND INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 58,080 hrs · 24,357 cycles

CRACK IN CUSP AT STATION 1265 RIGHT HAND. REMOVED AND INSTALLED NEW CUSP SHEET FROM STATION 1250 TO 1307.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 58,080 hrs · 24,357 cycles

CORROSION ON CUSP 1174 TO 1176 AT AFT SERVICE DOOR UNDER AFT GIRTBAR FITTING. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD AND EA 008205.

Part: FITTING — CRACKED (SPOILER ACTUATOR) · airframe 58,080 hrs · 24,357 cycles

LEFT GROUND SPOILER ACTUATOR FITTING CRACKED. REMOVED AND REPLACED LEFT GROUND SPOILER ACTUATOR CASTING PER 51-30-2.

Part: SHEAR TIE — DAMAGED (BS 1309) · airframe 58,080 hrs · 24,357 cycles

DING IN SHEAR-TIE AT STATION 1309. CUT AWAY DAMAGE AND INSTALLED DOUBLER PER 53-03-00 FIG 45.

Part: FRAME — CRACKED (BS 1485) · airframe 58,080 hrs · 24,357 cycles

FRAME WEB CRACKED LEFT OF RUDDER PACK AT STATION 1485. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-10-00-32.

Part: CUSP WEB — CRACKED (BS 225) · airframe 58,080 hrs · 24,357 cycles

CRACK IN LEFT HAD CUSP AT STATION 225. ROUTED OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (BS 835-843) · airframe 58,080 hrs · 24,357 cycles

CRACKS FOUND IN RIGHT HAND CUSP AT STA 835 TO 843. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: VANE — CRACKED (TE FLAP) · airframe 58,080 hrs · 24,357 cycles

RIGHT NUMBER 2 FLAP VANE HAS A DENT WITH CRACK ON BOTTOM OF VANE. REMOVED DAMAGE AREA AND INSTALLED HOT BOND DOUBLER PER ESO 80095.

Part: BUMPER BLOCK — DAMAGED (TE FLAP VANE) · airframe 58,080 hrs · 24,357 cycles

LEFT WING NUMBER 1 FLAP VANE HAS DEEP NICK ON RUBBER BUMPER. REMOVED DAMAGE AND INSTALLED HOT BOND REPAIR PER SRM 51-70-02.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 58,080 hrs · 24,357 cycles

CRACKED ANGLE LOWER FORWARD STOP FITTING BOTTOM OF DOOR. REMOVED CRACKED ANGLE INSTALLED NEW ANGLE PER ESO 80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 58,080 hrs · 24,357 cycles

MIDDLE STOP PAD FITTING AFT SIDE CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 58,080 hrs · 24,357 cycles

BOTTOM STOP FITTING FORWARD SIDE CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174

Part: PAN — CRACKED (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

WINDOW PAN CRACKED. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 58,080 hrs · 24,357 cycles

FORWARD CARGO DOOR AFT SIDE OF NUMBER 4 STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Part: PAN — CRACKED (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

WINDOW PAN CRACKED AT STATION 846. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER AARD 53-10-00-025.

Part: PAN — CRACKED (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

WINDOW PAN CRACKED. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25

Part: PAN — CRACKED (FUSELAGE) · airframe 58,080 hrs · 24,357 cycles

WINDOW PAN CRACKED AT STATION 846 LONGERON 12 LEFT. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,502 hrs · 24,116 cycles

EMERGENCY LIGHT BATTERY PACK FOR TAIL CONE WEAK. REMOVED AND INSTALLED NEW BATTERY PACK AS PER MM 33-53-00-06 AND IPC 33-50-00-12D.

Part: ACTUATOR — MALFUNCTIONED (OUTFLOW VALVE) · airframe 57,326 hrs · 24,035 cycles

AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. REPEAT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. FOUND OUTFLOW VALVE ACTUATOR MALFUNCTIONED. REPLACED CABIN PRESSURE OUTFLOW VALVE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 57,326 hrs · 24,035 cycles

AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE PRESSURE CONTROLLER. SYSTEM GROUND CHECKS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 53,870 hrs

ORD - EMERGENCY EXIT SIGN LIGHT AT RT SIDE OF AFT GALLEY EXIT DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN LIGHT AT RT SIDE OF AFT GALLEY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: TURBINE BLADES — FAILED (NR 1 ENGINE) · airframe 53,824 hrs

DFW INFLIGHT T1853/06JUN. CREW REPORTED LOUD NOISE FOLLOWED BY ENGINE GAS TEMPERTURE GOING TO 800 DEGREES. NR ONE ENGINE WAS SHUTDOWN BY CREW. LANDED DFW WITHOUT INCIDENT. SINGLE ENGINE TIME SIX MINUTES. FOUND TURBINE BLADE FAILURE AND METAL IN TAIL PIPE. REPLACED NUMBER ONE ENGINE ON 07JUN AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: STRUT — INOPERATIVE (NLG) · airframe 52,989 hrs

ORD INFLIGHT T1613/22FEB - NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ACCOMPLISHED NOSE LANDING GEAR SHOCK STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 29 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRIM MOTOR — INOPERATIVE

DTW - INFLIGHT AFTER LOC CAP DISCONNECTED AUTOPILOT REALIZED HAD RUNAWAY TRIM. RAN PROCEDURE IN QRH FOR RUNAWAY STABILIZER. PULLED CBS D9-10-11 LOST ALL TRIM, HAD NO ALTERNATE TRIM. DECLARED EMERGENCY DID GO AROUND AND CONFIGURED W .5 NOSE DOWN TRIM. AUTO BRAKES MED. DID HEAT INSPECTION. ALL OK EXCEPT BRAKES HEATED TO 450 DEG. TAXIED SLOWLY TO RAMP AND REQUESTED TUG. FOUND PRIMARY TRIM STOPS MOVING IN SELECTED DIRECTION WITH EITHER CONTROL WHEEL SWITCH ON PEDESTAL HANDLE. ALSO FOUND ALTERNATE LONG. TRIM OPERATE WITH ONLY ONE SWITCH SELECTED. INSPECTED JACKSCREW NO DEFECTS NOTED. REPLACED PRIMARY STABILIZER TRIM MOTOR AND ALTERNATE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT EXIT SIGN AT FORWARD GALLEY DOOR INOPERATIVE. FOUND WIRE BROKEN AT SIGN CONNECTOR. REPINNED CONNECTOR FOR EMERGENCY LIGHT EXIT SIGN AT FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - LEFT AND RIGHT HAND OVERWING EMERGENCY DOOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT OVERWING EMERGENCY DOOR EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

DFW - INFLIGHT T1096/01 LOST PRESSURIZATION AT 31,000 FEET. PERFORMED EMERGENCY DESCENT. RETURNED TO DFW. REPLACED BOTH NUMBER 1 AND NUMBER 2 PRESSURE CONTROLLERS. ACCOMPLISHED COMPLETE SYSTEM TESTS PER MAINTENANCE MANUAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT SERVICE DOOR AND AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK P4010049 (MFR DME CORP) FOR EMERGENCY LIGHTS AT AFT SERVICE DOOR AND BATTERY PACK 60030451 FOR EMERGENCY LIGHTS AT FORWARD AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - EMERGENCY LIGHTS ON CEILING AT ROWS 8 THROUGH 12 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON CEILING AT ROWS 8 THROUGH 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING SEATS 23, 24 AND 26 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTING BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TIRE — FAILED (RT MLG)

BNA - FLT 1307 - EN ROUTE BNA-LAX - TIRE BLEW ON TAKEOFF. RETURNED BNA AND LANDED WITHOUT INCIDENT. REPLACED NR 3 AND 4 MLG TIRE AND WHEEL ASSEMBLY. RIGHT MLG SPRAY DEFLECTOR, RIGHT MLG DOWNLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT AIRSTAIR PANEL LIGHT PULLED OUT. REPLACED FORWARD EMERGENCY EXIT AIRSTAIR PANEL LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION FROM 1160 TO 1207. BLENDED OUT CORROSION PER ESO 80559. (M)

Part: SKIN — DENTED (FUSELAGE) · corrosion level 3

TUL - FOUND SKIN DENTED RIGHT SIDE OF FUSELAGE, JUST AFT OF RADOME AND JUST BELOW SKIN BREAK. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04 PAGE 38. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED AT CLIP NUT HOLE INBOARD LEG STATION 1303. INSTALLED STRAP PER AARD 53-20-00-13. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED, UPPER SURFACE, OUTBOARD LEG AT STATION 1301. INSTALLED STRAP ON SEAT TRACK IAW AARD 53-20-00-13, TREATED AND PRIMED, BLENDED AREA IAW 51-10-3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FLOOR CUSP AT STATION 498 LEFT. ROUTED OUT CRACK, INSTALLED DOUBLER PER SRM 53-00-00. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FLOOR CUSP STATION 218 RIGHT .75 INCH. CUT OUT DAMAGE. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4-3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK UNDER TIE DOWN. CUT OUT CORROSION AREA AND INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1. CUT OUT CORRODED AREA AND INSTALLED PLUG REPAIR PER 53-05 FIG 4A. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS DIM AT ROW 13 THROUGH 16. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — DEFECTIVE (AC BAY)

ICT - FLT 1802 - EN ROUTE LAX-ORD, CREW REPORTS SMOKE IN CABIN. ACCOMPLISHED SMOKE/FIRE CHECKLIST. DIVERTED ICT AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RECIRCULATION FAN. PERFORMED PACK BURNOUT PER THE MM. NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (AFT AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, REAR STAIR EMERGENCY LIGHTS INOPERATIVE. REPAIRED REAR STAIR EMERGENCY LIGHT WIRES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: GASKET — DEFECTIVE (APU)

DFW - FLT 334 - AFTER TAKEOFF DFW, A RUBBER ODOR AND A LIGHT SMOKEY HAZE WAS NOTED BY FLIGHT CREW. FLIGHT AIR INTERRUPTED AND RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU OIL CAP SEAL DAMAGED. REPLACED APU OIL CAP SEAL AND LEAK CHECKED OK. MAINTENANCE PERFORMED PACK BURNOUT. AFTER BURNOUT WAS ACCOMPLISHED, COALESCER BAGS WERE REPLACED AS A PRECAUTIONARY. PACKS WERE OPERATED WITH NO LEAKS, ODOR, OR SMOKE NOTED. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (BS 598-712)

TUL - CUSP MEMBRANE CORRODED RT SIDE. REMOVED CUSP INSTALLED NEW SECTION IAW 51-10, FS 598-712. (M)

Part: WEB — CORRODED (BS 484-503)

TUL - FOUND CORROSION ON CUSP RIGHT SIDE. INSTALLED DOUBLER IAW AARD 53-00-00-02. (M)

Part: WEB — CRACKED (BS 1022)

TUL - FASTENER HOLE IN ORIGINAL CUSP CRACKED. REPAIR IAW AARD 53-00-00-02. (M)

Part: WEB — CORRODED (BS 826-845)

TUL - HOLE AND CORROSION IN AND ON CUSP BETWEEN STATION 826 AND 845. REPAIRED IAW AARD 53-00-00-02. (M)

Part: WEB — CORRODED (BS 772-776)

TUL - FOUND CORROSION ON CUSP STATION 772 AND 776. REPAIRED IAW AARD 53-00-00-02. (M)