N567AM

Part: TIRE — SEPARATED (MLG) · airframe 67,786 hrs · 29,624 cycles

NUMBER 4 MAIN GEAR TIRE TREAD SEPARATED CAUSING DAMAGE TO INBD FLAP. INSTALLED DOUBLER IAW EA MD80-57-036191 & SRM 57-01-00-001 FIGURE 3.

Part: WEB — CRACKED (NLG WW) · airframe 67,697 hrs · 29,581 cycles

NOSE LANDING GEAR LT SUPPORT WEB CRACKED AT EXISTING DOUBLER. INSTALLED NEW DOUBLER.

Part: WIRE HARNESS — DAMAGED (LT WING) · airframe 67,675 hrs · 29,569 cycles

LIGHTNING STRIKE TO LT WING TIP. REPLACED WIRE HARNESS IN LT WING TIP. OPERATIONS CHECKED NORMAL.

Part: FORMER — CRACKED (LE SLAT TRACK) · airframe 67,564 hrs · 29,497 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER CRACKED. INSTALLED RT WING NR 4 FORMER DOUBLER IAW WORK CARD 57-98-06 & EA M80-57-035589.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 67,541 hrs · 29,476 cycles

PORTABLE LIGHT INOPERATIVE. R & R PORTABLE LIGHT. OPERATIONS CHECKED NORMAL.

Part: RELAY — INOPERATIVE (HORIZ STAB) · airframe 66,300 hrs · 28,827 cycles

DFW CREW REPORTED PRIMARY & ALTERNATE STAB TRIM FAILED IN FLIGHT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HORIZONTAL STABILIZER TRIM DOWN TRIM RELAY R2015. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,399 hrs · 27,319 cycles

LEFT FUSELAGE AFT AREA HAS CRACKED 4 INCHES FOWARD OF EMERGENCY HANDLE. ACCOMPLISHED PERMANENT REPAIR PER SRM 51-92-02.

Part: MOTOR — FAILED (OUTFLOW VALVE) · airframe 61,893 hrs · 26,535 cycles

TUL - INFLIGHT DFW-ORD. CREW REPORTED UNABLE TO PRESSURIZE CABIN. EMERGENCY DECLARED FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 OUTFLOW MOTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOOR — DAMAGED (CABIN) · airframe 61,734 hrs · 26,449 cycles

LEFT NUMBER 1 DOOR DAMAGED IN LOWER FORWARD CORNER. INSTALLED REPAIR DOUBLER PER SRM 52-05-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,394 hrs · 26,267 cycles

ESCAPE PATH LIGHT AT SEAT 11D INOPERATIVE. REPLACED SEAT 11D PROXIMITY LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 61,394 hrs · 26,267 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERY PACK BY ROW 29. OPS CHECK NORMAL.

Part: SHUTOFF VALVE — INOPERATIVE (AC BAY) · airframe 60,565 hrs · 25,846 cycles

ABQ INFLIGHT DFW-LAX. CREW REPORTED LEFT PACK DROPPED OFF LINE DURING FLIGHT AND UNABLE TO REINSTATE. FLIGHT DIVERTED ABQ LANDED WITHOUT INCIDENT. PLACARD LEFT PACK INOPERATIVE PER MEL. FLIGHT CONTINUED ON TO DESTINATION. REPLACED LEFT PACK PRESSURE SHUTOFF VALVE AT DFW ON 01/23/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

DENT AT FRAME STATION 205, LONGERONS 4 TO 5 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-00 FIGURE 38 VIEW P.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

AFT ACCS- 1485 CANT FRAME CRACKED BELOW RIGHT AIRSTAIR ACTUATOR BRACKET. ACCOMPLISHED SPLICE REPAIR AT STATION 1485 RIGHT PER AARD 53-10-00-33.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

AFT ACCS- SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 RIGHT. REMOVED AND REPLACED SHEAR TIE STATION 1451 AFT OF LONGERON 2 RIGHT PER AARD 51-10-00-5.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,658 hrs · 25,398 cycles

AFT CARGO - LEFT TIE-DOWN TRACK CORRODED STATION 1136. CUT OUT SECTION OF TRACK FROM STATIONS 1107 TO 1220 AND SPLICED IN NEW SECTION. ALL WORK ACCOMPLISHED PER SRM 51-10-03, 53-01-00, 51-30-01, 51-30-05 AND 53-05-00 FIGURE 4G SHEET 1.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,658 hrs · 25,398 cycles

RIGHT TIE-DOWN TRACK CORRODED STATIONS 1079 TO 1136. COMPLETED INSTALLATION OF TIEDOWN TRACK AND SPLICE PER AARD 51-10-00-5, SMR 51-30-05 AND SRM 51-30-01.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,658 hrs · 25,398 cycles

CORROSION ON DOOR CUTOUT WEB AT STATION 1212 RIGHT LONGERON 28. CUT OUT SECTION OF WEB FROM STATIONS 1200 TO 1220 AND SPLICED IN NEW SECTION OF WEB PER AARD 53-10-00-24 AND SRM 51-10-03, 51-30-02, 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,658 hrs · 25,398 cycles

SEAT TRACK NUMBER 1 AT STATIONS 790 TO 795 CORROSION BEYOND LIMITS. INSTALLED NEW SEAT TRACK (NUMBER 1) SECTION BETWEEN STATIONS 722 TO 797 PER SRM 53-05-00 FIGURE 4F SHEET 5, 6, 9, 10, 11 AND AARD 53-00-00-012.

Part: PAN — CRACKED (WINDOW) · airframe 59,658 hrs · 25,398 cycles

CRACK IN LEFT WINDOW PAN AFT UPPER STIFFENER AT STA 1003. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

FLOORBEAM SUPPORT CRACKED AT LOWER END, BELOW SEAT TRACK NUMBER 2 STATION 927. INSTALLED NEW FITTING PER AARD 51-10-00-5 AND AARD 51-60-00-08.

Part: PAN — CRACKED (WINDOW) · airframe 59,658 hrs · 25,398 cycles

CRACK IN LEFT WINDOW PAN AT FORWARD UPPER CORNER AT STATION 845. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

CRACK IN TOP LIP OF INTERCOSTAL, BETWEEN FLOORBEAMS, STATIONS 1287 TO 1309. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-05.

Part: MOUNT — DAMAGED (GALLEY) · corrosion level 2 · airframe 59,658 hrs · 25,398 cycles

CORROSION ON GALLEY TIEDOWN STATION 218 RIGHT BUTTLINE 10. INSTALLED GALLEY MOUNT PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,658 hrs · 25,398 cycles

AFT CARGO - BOTTOM OF LEFT CUSP CORRODED AT STATION 1175. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,658 hrs · 25,398 cycles

FLOORBEAM SUPPORT CRACKED AT LOWER END, BELOW SEAT TRACK NUMBER 4, STATION 927. INSTALLED DOUBLE ON FLOORBEAM SUPPORT PER ATTACHED EA MD80-53-019044 DATED 9-7-11.

Part: BOOT — TORN (AC BAY) · airframe 58,930 hrs · 25,006 cycles

OKC - INFLIGHT DFW-YYC. CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED OKC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HOSE TORN BETWEEN AIR SUPPLY AND RIGHT PACK ASSEMBLY 4. PLACARDED RIGHT PACK INOPERATIVE PER MEL. REPLACED RUBBER BOOT FOR RIGHT PACK SYSTEM AT TUL ON 06/03/2011. SYSTEM GROUND CHECK NORMAL OPERATION

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,482 hrs · 24,269 cycles

FOUND THE FORWARD EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

DAMAGED DIAPHRAM AT STATION 164. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

CORROSION ON OUTBOARD GALLEY MOUNT STATION 218. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01-3 SRM 51-30-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

CORROSION FOUND ON RIGHT CUSP STATION 152 AROUND FITTING. REMOVED AND INSTALLED NEW DRAIN PAN SHEET METAL PER SRM 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,818 hrs · 23,465 cycles

CORROSION ON RIGHT SIDE OF CUSP STATIONS 190 TO 200. BLENDED OUT CORROSION PER AARD 53-20-00-14.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

CUSP MEMBRANE BETWEEN STATIONS 218 TO 237 DAMAGED 2 PLACES. REMOVED AND REPLACED DAMAGED CUSP MEMBRANE PER SRM 51-30-03 AND SRM 51-01-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

SEAT TRACK NUMBER 15 CORROSION AT STATIONS 200 TO 218. REMOVED AND SPLICED IN NEW SEAT TRACK PER SRM 53-05-00 FIGURE 4F.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

INBOARD FORWARD GALLEY MOUNT STATION 160 HAS CORROSION. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-30-3 / SRM 51-01-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,818 hrs · 23,465 cycles

STATION 1418 FRAME CRACKED AT LONGERON 2 RIGHT. REPAIRED FRAME PER EA MD-80-53-010008 AT LONGERON 2 RIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,050 hrs · 22,711 cycles

EMERGENCY LIGHT MID AISLE BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK AT MID AISLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,050 hrs · 22,711 cycles

EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED FUNCTIONAL CHECK. REPLACED BATTERY PACK IN CABIN.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,050 hrs · 22,711 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,050 hrs · 22,711 cycles

FORWARD DROP PANEL BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK.

Part: AUGMENT VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 52,539 hrs · 21,990 cycles

ELP - INFLIGHT SJD-DFW. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON FOLLOWED BY ENGINE FIRE BOTTLE AGENT LOW LIGHT. LANDED ELP WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AUGMENTATION VALVE AND LEFT PRESSURE REGULATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WINDOW — DELAMINATED (ZONE 200) · airframe 51,843 hrs

SEA - AIRCRAFT RETURNED TO SEA DUE TO NUMBER THREE WINDOW DELAMINATED AND LEAKING. LANDED WITHOUT INCIDENT. REPLACED NUMBER THREE WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 51,546 hrs

ORD RIGHT HAND SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,546 hrs

LT HAND SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: PAN — CORRODED (FUSELAGE) · airframe 51,286 hrs · 21,457 cycles

DOOR PAN CORRODED AROUND FORWARD STOP STATION 389. REPAIRED PER ESO 80559 DATED 21 OCT 2008.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · airframe 51,286 hrs · 21,457 cycles

SUPPORT AT STATION 1210 IS CORRODED AT AFT CARGO DOOR. REPLACED SUPPORT BRACKET PER SRM 53-01-00 AND 51-01-00.

Part: PROXIMITY SENSOR — INOPERATIVE (RT MLG) · 51,146 cycles

LAX INFLIGHT T1407/29SEP. CREW REPORTED RT RED MAIN LANDING GEAR WARNING REMAINED ON AFTER GEAR EXTENDED. EXTENDED GEAR MANUALLY AND PERFORMED FLY BY. LANDED LAX WITHOUT INCIDENT. REPLACED RT GEAR PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,363 hrs

LGA - EMERGENCY LIGHT AT RT HAND CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT HAND CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,363 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT OVERHEAD SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS EMERGENCY LIGHTS AT LEFT AND RIGHT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AND RIGHT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: DUCT — RUPTURED (ANTI ICE)

MCO - ON CLIMBOUT AT ABOVE 1700 WITH CLIMB POWER, LEFT B-LOOP CAME ON. SHORTLY AFTER LEFT A-LOOP CAME ON. LEFT FIRE WARNING CAME ON IMMEDIATELY. LEVELED OFF AT 18,000 AND PULLED POWER BACK TO 1.40 ENGINE PRESSURE RATIO AND WARNING WENT OUT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. NO FURTHER WARNINGS WERE OBSERVED AT ANYTIME. SHUTDOWN ENGINE AFTER LANDING. REPLACED RUPTURED REAR ANTI ICE DUCT ON LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD CEILING EMERGENCY LIGHTS OVER ROWS 29D AND 28D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS OVER ROWS 29D AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 9D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 8 THROUGH 11. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DEN - AFT EMERGENCY BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TARGET — OUT OF ADJUST (NLG)

LAX - FLT 642 - BUR-DFW, RED NOSE GEAR LIGHT REMAINED ON AFTER LANDING GEAR HANDLE RAISED UP. NO GEAR FAILED TO RETRACT. MAINS OK. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR TARGETS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SCHRADER VALVE — LEAKING (NLG)

LAX - FLT 2430 - EN ROUTE LAX-DFW, AFTER TAKEOFF, UNABLE OT RETRACT NOSE GEAR. RETURNED TO LAX WITHOUT FURTHER INCIDENT. FOUND NOSE GEAR SCHRADER VALVE LEAKING. REPLACED VALVE AND SERVICED NOSE GEAR. ACCOMPLISHED NOSE GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

FOUND CORROSION ON DOOR AFT CARGO JAMB BEAM UPPER AND LOWER LEG OF BEAM VARIOUS PLACES. TREATED, PRIMED, PAINTED AND BLENDED AREA. INSTALLED DOUBLER PER ESO 80559 DATED 3-14-03. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

TUL - FOUND TWO LIGHTNING STRIKES, FS 599 AND 603. REMOVED DAMAGED AREA OF SKIN AND INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND STATION 1309, L18R JUST BELOW RIGHT ENGINE PYLON HAS GOUGE, DENT AND SCRATCH APPROX 6 INCHES LONG, APPEARS PREVIOUSLY WORKED. BLENDED AND INSTALLED TWO ROWS DOBLER PER 53-04-38. (M)

Part: WEB — CRACKED (FUSELAGE)

FOUND RIGHT CUSP WEB CRACKED AT STATION 788-800 AND STATION 804. INTALLED NEW CUSP WEB FROM STATION 788-807 RIGHT PER SRM 53-05-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION BOTTOM NR 3 SEAT TRACK STATION 1177-1178. REMOVED CORRODED SECTION OF TRACK, SPLICED IN NEW SECTION FROM STATION 1174-1309 PER SRM 53-05 FIG 4F. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND HOLE IN CUSP AT STATION 1060 LEFT. CUT OUT DAMAGED SECTION, INSTALL DOUBLER PER AARD 53-00-00-02. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4D INOPERATIVE. INSERTED EMERGENCY EXIT LIGHT PIN IN CONNECTOR ON PLUG TO SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — CORRODED (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS IN FORWARD GALLEY AND FLIGHT DECK INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONNECTIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CLAMP — LOOSE (AC BAY)

SJD - FLT 286 - EN ROUTE SJD-ORD, DETECTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIR INTERRUPTED, RETURNED SJD AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED CLAMP ON LEFT AND RIGHT SIDE PACK. LEAK CHECKED GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (FUSELAGE)

DFW - FLT 1086 - EN ROUTE YVR-DFW, A DISTINCT SMELL OF HOT BURNING PLASTIC WAS DETECTED. SMELL DISSIPATED IN TEN MINUTES. CONTINUED FLIGHT AND LANDED DFW WITHOUT INCIDENT. REPLACED APU AND AIRCRAFT COALESCER WATER SEPARATOR BAGS AND ACCOMPLISHED PACK BURNOUT PER THE MM. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — OUT OF ADJUST (MLG)

ORD - FLT 575 - DURING CLIMB-OUT AT FL 20,000 FT, GEAR DOOR WARNING LIGHT ILLUMINATED. CREW TURNED ENGINE DRIVEN HYDRAULIC PUMPS TO HIGH AND LIGHT EXTINGUISHED. FLT CONTINUED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT MAIN GEAR DOOR SENSOR OUT OF ADJUSTMENT. ADJUSTED RIGHT MAIN GEAR DOOR SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BOOST PUMP — MALFUNCTIONED (CTR FUEL TANK)

SJC - FLT 1226 - AFTER TAKEOFF SJC EN ROUTE TO ORD, AIRCRAFT AIR INTERRUPTED BACK INTO SJC. UNABLE TO OBTAIN FUEL FROM CENTER TANK WITH ALL FUEL PUMPS ON. LANDED OVERWEIGHT WITHOUT INCIDENT INTO SJC. INSPECTED AND THERE WERE NO DISCREPANCIES NOTED. AIRCRAFT INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT SJC TO LAX. FERRY FLIGHT TO LAX FOR FURTHER EVALUATION. COULD NOT DUPLICATE ON GROUND. CENTER TANK BOOST PUMPS OPERATIONS CHECKED NORMAL. (X)