N553AA

Part: POSITION SWITCH — DEFECTIVE (ZONE 200) · airframe 67,966 hrs · 35,503 cycles

DURING TAKEOFF RECEIVED SLAT AUTO FAIL MSG. ABORTED TAKEOFF AT 90. R & R FLAP SLAT HANDLE POSITION SWITCHES & TRANSMITTER IAW MM 27-80-07. ACCOMPLISHED ALL REQUIRED CHECKS. SYS CHECKED NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 67,387 hrs · 35,138 cycles

PORTABLE EMER LIGHT INOPERATIVE. REPLACED PORTABLE EMER LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,059 hrs · 33,746 cycles

FWD CARGO DOOR, DOORSTOP FITTING CRACKED FORWARD CENTER. REMOVED CRACKED DOORSTOP FITTING & INSTALLED SERVICEABLE DOORSTOP FITTING IAW AARD 51-00-05-1.

Part: RIB — CRACKED (LT WING) · airframe 65,059 hrs · 33,746 cycles

LT WING NR 4 SLAT TRACK SUPPORT RIB CRACKED. REMOVED CRACKED LUG & HAND BLENDED REAMED TO COMPLETELY REMOVE THE CRACK FROM THE RIB IAW EA MD80-57-032110.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,526 hrs · 33,414 cycles

ROWS 23 TO 28 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN AFT LAVATORY FOR ROWS 23 TO 28 EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,526 hrs · 33,414 cycles

TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN AFT LAVATORY FOR EMERGENCY LIGHTS IN TAIL CONE. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,526 hrs · 33,414 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACK B5-23. OPERATIONS CHECKED NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,142 hrs · 31,474 cycles

THE 1418 FRAME CRACKED AT LONGERON 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00 FIGURE 31A.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 61,142 hrs · 31,474 cycles

AFT SIDE OF FRAME 1418 AT LONGERON 2 LEFT UPPER OUTBOARD AND INBOARD HOLES ATTACHING FRAME TO LONGERON HATS ARE MISS DRILLED. REPLACED STIFFENER PER AARD 51-10-00-5.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 61,142 hrs · 31,474 cycles

STATION 1418 LONGERON 2 LEFT ATTACH HOLES, AFT SIDE ELONGATED. INSTALLED LONGERON 2 SPLICE REPAIR PER SRM 53-02-00 FIGURE 18 SHEET 1 TO 3 AND EA MD80-53-023674.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

CORROSION ON AFT CARGO DOOR BEAM STATIONS 1160 TO 1206. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

FORWARD LAVATORY SERVICE PANEL HAS CORROSION ON BOTTOM LIP. INSTALLED DOUBLER PER EA-MD80-53-014218.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

CORROSION ON BOTTOM OF CUSP LEFT SIDE AT STATION 1175 BELOW TRACK 2. INSTALLED NEW SECTION OF CUSP STATIONS 1174 TO 1188 PER AARD 53-20-00-16.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

RIGHT TIE DOWN TRACK CORRODED STATIONS 1140 TO 1155. INSTALLED SERVICABLE TRACK PER AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

CRACKED INTERCOSTAL CENTER OF CABIN FLOOR AT STATIONS 1287 TO 1309. INSTALLED INTERCOSTAL CENTER OF CABIN FLOOR AT STATION 1287 TO 1309 PER AARD 51-10-00-5.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

AFT CX - CORROSION ON THE LOWER DOOR FRAME WEB DOUBLER FROM STATIONS 1156 TO 1160 AT LONGERON 28 RIGHT. SPLICED IN NEW SECTION OF WEB PER AARD 53-10-00-24.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

LOWER STOP FITTING IS CRACKED FOR AFT VAULT DOOR. REMOVED AND REPLACED STOP FITTING PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

CRACK ON RIGHT CUSP STATION 1304. INSTALLED NEW CUSP SHEET PER AARD 51-10-00-5 REPAIR 1.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

RIGHT CUSP HAS A PUNCTURE AT STATION 796. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

CABIN, AFT SERVICE AREA, CUSP UNDER AFT GIRT BAR SUPPORT IS CORRODED STATIONS 1170 TO 1174. INSTALLED CUSP REPAIR DOUBLER LEFT SIDE STATIONS 1170 TO 1174 PER AARD 53-20-00-16.

Part: SUPPORT ANGLE — CORRODED (GIRT BAR) · airframe 57,322 hrs · 29,361 cycles

CORROSION ON FORWARD GIRT BAR SUPPORT ANGLE BELOW CUSP SHEET. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

NUMBER 5 SEAT TRACK CORRODED BEYOND MANUAL LIMITS AT STATIONS 200 TO 245. INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE PER SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

CABIN, AFT SERVICE AREA, CUSP UNDER FORWARD GIRT BAR SUPPORT IS CORRODED STATION 1140. INSTALLED DOUBLER REPAIR AT LEFT CUSP STATION 1140 PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

SEAT TRACK 6 BLEND OUT, OUT BEYOND LIMITS STATIONS 616 TO 617. INSTALLED STRAP AND FILLER REPAIR PER AARD 53-20-00-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

SEAT TRACK BLEND OUT, OUT OF LIMITS, TRACK 6 STATIONS 588 TO 589. INSTALLED STRAP AND FILLER REPAIR PER AARD 53-20-00-13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

AFT ACCESSORY 1510 CANT FRAME CRACKED BETWEEN LEFT TAIL CONE LATCHES. INSTALLED DOUBLER PER EA MD80-53-014157 11/19/2010 AND SRM 53-01-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

CUSP SHEET CRACKED JUST AFT OF RIGHT STATION 218 RIGHT BUTTLINE 46. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

CORROSION ON SUBFLOOR BELOW G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

CORROSION ON BOTTOM OF LEFT CUSP STATION 536. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

NUMBER 3 SEAT TRACK VERTICAL UNDER FLOOR SUPPORT CRACKED AT STATION 826 [MKD]. REMOVED CRACKED FITTING, DRILLED UP NEW ONE, AND INSTALLED ALL PER AARD 51-10-00-5.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 57,322 hrs · 29,361 cycles

AFT DOOR JAMB RIGHT UPPER STOP FITTING CRACKED. REMOVED AND REPLACED FITTING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,322 hrs · 29,361 cycles

SEAT TRACK NUMBER 1 HAS CORROSION OUT OF LIMITS AT STATION 898. REMOVED CORROSION AND INSTALLED REPAIR PLUG AT SEAT TRACK NUMBER 1, STATION 898 PER AARD 53-20-00-10.

Part: PAN — CRACKED (WINDOW) · airframe 57,322 hrs · 29,361 cycles

RIGHT WINDOW PAN BETWEEN STATIONS 1060 TO 1079 HAS LOWER FORWARD EAR CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,322 hrs · 29,361 cycles

RIGHT WINDOW PAN BETWEEN STATIONS 1155 TO 1174 HAS LOWER FORWARD EAR CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,322 hrs · 29,361 cycles

RIGHT WINDOW PAN BETWEEN STATIONS 1174 TO 1193 HAS LOWER FORWARD EAR CRACKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,322 hrs · 29,361 cycles

RIGHT WINDOW PAN BETWEEN STATIONS 1041 TO 1060 HAS LOWER FORWARD EAR CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,322 hrs · 29,361 cycles

STATION 1098 LEFT UPPER AFT WINDOW PAN TAB IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,322 hrs · 29,361 cycles

RIGHT WINDOW PAN BETWEEN STATIONS 1022 TO 1041 HAS LOWER FORWARD EAR CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 53,713 hrs · 27,413 cycles

PORTABLE EMERGENCY LIGHT IS DIM. REPLACED EMERGENCY LIGHT IAW MM 33-53-00-5.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,713 hrs · 27,413 cycles

AFT EMERGENCY AISLE LIGHTING BATTERY PACK IS WEAK. REMOVED AND REPLACED WITH SERVICEABLE BATTERY PACK IAW MM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,713 hrs · 27,413 cycles

EMERGENCY AISLE BATTERY PACK IS WEAK. REMOVED AND REPLACED WITH SERVICEABLE BATTERY PACK IAW MM 33-60-98-4.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 53,713 hrs · 27,413 cycles

FORWARD CARGO AFT SECOND FROM INBOARD DOOR STOP CASTING CRACKED. REMOVED AND REPLACED STOP BRACKET UNDER ESO 80174.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 52,573 hrs

LGA FORWARD UPPER EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. REPLACED SAFETY STRAP FOR FORWARD UPPER EMERGENCY FLASHLIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,573 hrs

LGA FORWARD UPPER EMERGENCY FLASHLIGHT BATTERY LOW. REPLACED BATTERY FOR FORWARD UPPER EMERGENCY FLASHLIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,573 hrs

LGA AFT EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK AT AFT EMERGENCY EXIT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,163 hrs

LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,163 hrs

LGA - EMERGENCY LIGHT AT MID CABIN OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,577 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,566 hrs

LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — CHAFED (RUDDER SYS) · airframe 49,375 hrs

PHX INFLIGHT T1658/02DEC PSP-DFW - DURING CLIMB AIRCRAFT EXPERIENCED AN UNCOMMANDED RUDDER INPUT. LANDED PHX WITHOUT INCIDENT. FOUND CHAFED WIRE FOR RIGHT POSITION SENSOR IN AFT TAIL COMPARTMENT. REPAIRED WIRE FOR RIGHT DUEL SERVO RUDDER POSITION SENSOR IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,290 hrs

LGA - EMERGENCY LIGHT AT SEAT 13D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — MISSING (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT 13D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TUBE — LEAKING (LEFT ENGINE)

DFW INFLIGHT T2485/09OCT ORD TO AUS - NUMBER ONE ENGINE HIGH OIL TEMPERATURE INDICATION. ALL OTHER ENGINE INDICATIONS NORMAL. CREW SHUT DOWN NUMBER ONE ENGINE. DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 25 MINUTES. FOUND OIL LEAK FROM COMBUSTION CHAMBER DRAIN TUBE. REPLACED NUMBER ONE ENGINE ON 10 OCT 2007 AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT TAILCONE INOPERATIVE. REPLACED BATTERY PACK AT LEFT AFT LAVATORY OVERHEAD FOR EMERGENCY LIGHTS AT TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAL — DAMAGED (NLG STRUT)

JFK INFLIGHT T1977/15APR NOSE LANDING GEAR WOULD NOT RETRACT. LANDED JFK WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SEALS AND SERVICED NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: COMPRESSOR — STALLED (RIGHT ENGINE)

DFW - ON TAKEOFF ROLL CREW HEARD LOUD BANG AND AIRCRAFT YAWED TO THE RIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 07 DEC 2006 AT DFW DUE TO STEADY STATE COMPRESSOR STALLS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY CEILING LIGHTS AT SERVICE DOOR AND STATIONS 1100 THROUGH 1200 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190R FOR EMERGENCY CEILING LIGHTS AT SERVICE DOOR AND STATIONS 1100 THROUGH 1200. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — NOT SEATED (CABIN)

RDU - OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE AREA INOPERATIVE. RESEATED BATTERY AT POSITION B5-107 FOR OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — MALFUNCTIONED (L2 DOOR)

L2 DOOR SLIDE INADVERTENTLY AND UNSUCCESSFULLY DEPLOYED BY CABIN SERVICE. DRIVER OPENED AFT SERVICE DOOR WHILE SLIDE WAS ARMED. RUG TRUCK PLATFORM PREVENTED FULL DEPLOYEMENT OF SLIDE. REPLACED SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CASTING — GOUGED (RT WING)

TUL - FOUND LEADING EDGE SLAT CABLE PULLEY CUT GROOVE IN NR 1 SLAT CASTING INBOARD SIDE FORWARD SIDE OF CASTING RT WING. BLENDED GOUGE AND INSTALLED DOUBLER PER ESO 80559. (M)

Part: LONGERON — DAMAGED (FUSELAGE)

TUL - FOUND LONGERON DAMAGED 1 INCH AFT OF STATION 1338, STRINGER 17L. INSTALLED LONGERON SPLICE PER SRM 53-02-00 AND AARD 53-00-00-05. (M)

Part: FRAME — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN STATION 1380 FRAME FORWARD SIDE AT STATION 5L. FABRICATED DOUBLER, ALODINED AND PRIMED AND INSTALLED DOUBLER AT STATION 1380 SRM 51-70-4. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME CRACKED IN RADIUS AFT SIDE STATION 1418, LONGERON 2R. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SRM 53-01-0 PAGE 10. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND INTERIM REPAIR ACCOMPLISHED ON AFT CARGO BEAM CORROSION, STATION 1174. REPLACED AFT CARGO DOOR CUT OUT, LOWER BEAM PER SRM 53-01-00. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND 2 GOUGES STATION 231 LEFT BETWEEN LONGERON 17L AND 18L. DYE CHECKED DAMAGE, NO CRACKS. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIG 38. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACK AT FASTENER LONGERON 14L STATION 1380. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-01-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FLOOR WEB AROUND GALLEY TIE DOWN STATION 170 RBL 11. REMOVED DAMAGE. INSTALLED DOUBLER PER SRM 53-01-00 FIG 4 SHEET 3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION 627 LEFT CUSP HAS .5 INCH CRACK EMITTING FROM INBOARD EDGE OF CENTER LIGHTENING HOLE. INSTALLED REPAIR DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION 225-227 LEFT CUSP OUTBOARD OF NR 1 TRACK, CUSP HAS 2 INCH CRACK EMITTING FROM FORWARD SIDE OF LIGHTENING HOLE. STOP DRILLED, DYE CHECKED AND NO CRACKS FOUND. FABRICATED DOUBLER ALODINED, PRIMED AND INSTALLED PER MM 53-10-01. (M)

Part: SEAT TRACK — CRACKED (FUSELAGE)

TUL - FOUND NR 4 SEAT TRACK, LUG CRACKED AT STATION 270. INSTALLED REPAIR PLUG PER AARD 53-20-00-10. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW INNER FRAME CRACKED AT STATION 845 UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 18-21 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (TAIL)

DFW - FLT 369 - EN ROUTE DFW-BOS, SHORTLY AFTER TAKEOFF TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPAIRED TAIL TEMPERATURE SENSOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COALESCER BAG — DIRTY (ACM BAY)

JFK - EN ROUTE LGA-ORD, DETECTED SMOKE AND HAZE IN CABIN AND COCKPIT. DIVERTED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT AND RIGHT SIDE COALESCER BAGS. ACCOMPLISHED HIGH POWER RUN UP. NO SMOKE OR HAZE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (A/C BAY)

MIA - FLT 1304 - EN ROUTE MIA-CLE, DETECTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIR INTERRUPTED, RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE AFT TAIL COMPARTMENT OVERHEAT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUT — LACK OF LUBE (NLG)

DFW - FLT 1314 - AFTER TAKEOFF DURING GEAR RETRACTION, RED NOSE GEAR LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. NOSE GEAR REMAINED EXTENDED. RECYCLED AND GEAR RETRACTED NORMAL. CHECKED SENSORS, LUBRICATED STRUT AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LANDING GEAR — LACK OF LUBE (NOSE)

DFW - FLT 1126 - AFTER TAKEOFF, NOSE WHEEL FAILED TO RETRACT. RECYCLED DOWN THEN UP, RETRACTED NORMAL, CONTINUED AND LANDED DFW WITHOUT INCIDENT. GREASED GEAR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SWITCH — DEFECTIVE (NLG)

LAX - FLT 1258 - AFTER TAKEOFF, RED NOSE GEAR LIGHT WOULD NOT EXTINGUISH WHEN GEAR HANDLE SELECTED UP. RE-CYCLED GEAR, NO HELP. LOUD NOISE HEARD. RETURNED AND LANDED LAX WITHOUT INCIDENT. REPLACED NOSE GEAR UP POSITION PROXIMITY SWITCH. ACCOMPLISHED GEAR SWING, SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (ROWS 19-20)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT ROWS 19-20 INOPERATIVE. TIGHTENED LOOSE CONNECTOR ON EMERGENCY EXIT OVERHEAD LIGHT BATTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FAN — DEFECTIVE (CABIN)

LIT - FLT 791 - EN ROUTE LGA, DFW SMOKE AND ELECTRICAL SMELL DETECTED. AIRCRAFT AIR INTERRUPTED AND LANDED LIT WITHOUT INCIDENT. REPLACED CABIN AIR RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYD PUMP — DEFECTIVE (RT POS)

DTW - FLT 1652 - EN ROUTE DFW/DTW, DURING CRUISE, RIGHT SIDE HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT PROCEEDED TO DTW, LANDING WITHOUT INCIDENT. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND FILTER. SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OUTFLOW VLV ACT — DEFECTIVE (CABIN)

PHX - FLT 1172 - AFTER TAKEOFF PHX DURING CLIMB-OUT, UNABLE TO PRESSURIZE A/C IN EITHER AUTO OR MANUAL MODE. ACCOMP EMERGENCY DESCENT AND ALL PAX OXYGEN MASKS SUCCESSFULLY DEPLOYED. A/C RETURNED TO PHX AND LANDED W/O INCIDENT. REPLACED NR 1 PRESSURIZATION CONTROLLER AND GROUND CONTROL RELAYS R2-4 AND R2-106. SYSTEM GROUND CHECKED NORMAL OPERATION. A/C MAINTENANCE FERRY PHX/TUL. RESTOWED ALL PAX OXYGEN MASKS AND SERVICED PAX OXYGEN SYS. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT AND PRESSURIZATION PROBLEM REPEATED. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPS. ACCOMP FUNCTIONAL CHECK/FERRY FLIGHT WITH NO DEFECTS FOUND. SYS OPS CHECKED NORMAL. (M)

Part: WIRE — SHORTED (LT ACM BAY)

ORD - DURING MAINTENANCE TO REPAIR AN INOPERATIVE LT AIR CYCLE MACHINE COOLING FAN PREVIOUSLY PLACARDED INOP AT DFW/24, FOUND COOLING FAN WIRE BUNDLE SHORTED AND BURNED DUE TO CHAFING AT FIRST CLAMP AND BRACKET. REPLACED LT ACM COOLING FAN, REPLACED ELECTRICAL CONNECTOR AND REPAIRED WIRE BUNDLE BY REPLACING WIRE FROM P1-173 CONNECTOR TO FIRST SPLICE. OPERATED LT ACM WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CLAMP — BROKEN (LT ACM)

DFW - FLT 789 - AFTER TAKEOFF DFW DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND AIRCRAFT RETURNED DFW, LANDING WITHOUT INCIDENT. REPLACED LT AIR CYCLE MACHINE SUPPLY DUCT CLAMP. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (X)