N435AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,953 hrs · 35,460 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 76,953 hrs · 35,460 cycles

LEFT NUMBER 1 DOOR EMERGENCY FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 76,953 hrs · 35,460 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. RESEATED BATTERY PACK. OPS CHECKS NORMAL.

Part: PERISEAL — LEAKING (ACM) · airframe 76,461 hrs · 35,222 cycles

SAT - INFLIGHT MFE-DFW. CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED SAT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PERI SEALS ON LEFT AIR CYCLE MACHINE AND REPOSITIONED CLAMP ON RIGHT AIR CYCLE MACHINE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 73,461 hrs · 33,739 cycles

STIFFENER AT STATION 1418 IS CRACKED ON AFT SIDE NEXT TO RADIUS BLOCK AT LONGERON 2 LEFT. INSTALLED DOUBLER PER EA MD80-53-013415.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,461 hrs · 33,739 cycles

CRACK IN SHEAR TIE AT STATION 1429 BETWEEN LONGERON 2 LEFT AND LONGERON 3 LEFT. INSTALLED NEW SHEAR TIE PER EA MD80-53-013392.

Part: GCU — INOPERATIVE (ELECTRICAL SYS) · airframe 73,123 hrs · 33,565 cycles

SLC - INFLIGHT SEA-DFW. CREW REPORTED ELECTRICAL POWER INTERRUPTIONS AND AUXILIARY POWER UNIT FAULT LOW OIL PRESSURE. EMERGENCY DECLARED, DIVERTED SLC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,874 hrs · 32,559 cycles

RIGHT AND CENTER EMERGENCY CEILING LIGHTS BETWEEN AFT LAVS INOP. REPLACED BATTERY PACK AND CHARGER.

Part: PAN — CORRODED (ZONE 100) · airframe 69,036 hrs · 31,787 cycles

FORWARD LAV SERVICE PAN HAS LEVEL 1 CORROSION BETWEEN SKIN AND DOUBLER, LOWER CENTER OF DOOR CUTOUT. INSTALLED DOUBLER PER EA MD80-53-005902.

Part: COVER — DAMAGED (TE FLAP) · airframe 69,190 hrs · 31,855 cycles

SCREW MISDRILLED INTO CASTING ON BOTTOM O/B SIDE NIPPLE FLAP HINGE COVER. INSTALLED REPAIR BUSHING PER EA MD8057-005935.

Part: SPLICE — CORRODED (ZONE 100) · airframe 69,036 hrs · 31,787 cycles

LEVEL 1 CORROSION ON TIE DOWN TRACK SPLICE LEFT SIDE STATION 1212-1220. REMOVED AND REPLACED TRACK SPLICE PER SRM 51-30-05.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · airframe 69,036 hrs · 31,787 cycles

LEVEL 1 CORROSION ON RIGHT TIE DOWN TRACK AT MULTIPLE SCREW HOLES AND MOUNTING SCREW HOLES. INSTALLED NEW TIE DOWN TRACK PER SRM 53-30-00.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,036 hrs · 31,787 cycles

LONGERON 7R CRACKED AT STATION 200. REPLACED CRACKED LONGERON WITH NEW LONGERON PER SRM 53-02-00 FIGURE 18.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,036 hrs · 31,787 cycles

LEVEL 1 CORROSION ON SUB FLOOR AREA FROM STATION 164-200. INSTALLED CUSP REPAIR PER AARD 53-20-00-16 AND EA MD80-53-005912.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,036 hrs · 31,787 cycles

LEVEL 1 CORROSION ON RIGHT CUSP STATION 579-598. REPLACED CUSP FROM STATION 502-598 PER SRM 51-01-00.

Part: CUSP WEB — DAMAGED (ZONE 200) · airframe 69,036 hrs · 31,787 cycles

RIGHT CUSP TORN STATION 200-210. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: WEDGE — DAMAGED (RT WING TE FLAP) · airframe 69,036 hrs · 31,787 cycles

RIGHT INBOARD FLAP INBOARD WEDGE HAS A TEMPORARY DOUBLER INSTALLED ON LOWER SIDE. REMOVED TEMPORARY DOUBLER AND INSTALLED A FLUSH DOUBLER PER SRM 57-01-00 FIGURE 5.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,036 hrs · 31,787 cycles

LONGERON 2L CRACKED OUTBOARD SIDE AT STATION 160. INSTALLED NEW LONGERON AND SPLICE PER SRM 53-20-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 69,036 hrs · 31,787 cycles

LEVEL 1 CORROSION ON LEFT CUSP BOTTOM SIDE FROM STATION 522-528. INSTALLED CUSP REPAIR PER AARD 53-20-00-16.

Part: SKIN — DENTED (ZONE 100) · airframe 69,036 hrs · 31,787 cycles

DENTS EXTENDING FORWARD AND AFT FROM UNDER PREVIOUSLY INSTALLED DOUBLER STATION 1250-1280, LONGERON 23R. NEW SHEAR TIE AND REPAIR DOUBLER INSTALLED PER SRM 53-03-00 FIGURE 7 AND SRM 53-04 FIGUE 12B.

Part: CUSP WEB — DAMAGED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

RIGHT CUSP TORN AT STATION 502, RBL 48. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (GALLEY) · airframe 69,036 hrs · 31,787 cycles

LEVEL 1 CORROSION AT OUTBOARD GALLEY MOUNT BOLT HOLE FOR G-2 GALLEY. INSTALLED NEW GALLEY MOUNT FITTING PER SRM 51-01-00.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

2 CRACKS IN LONGERON 4L INBOARD AND OUTBOARD SIDES AT STATION 200. REPLACED LONGERON SECTION PER SRM 53-20-00.

Part: BEAM — CRACKED (ZONE 800) · airframe 69,036 hrs · 31,787 cycles

NR 7 BEAM OF FORWARD PASSENGER DOOR CRACKED. INSTALLED DOUBLER REPAIR ON NR 7 DOOR BEAM PER ESO 80172 AND SRM 52-05-06.

Part: MOUNT — CORRODED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

LEVEL 1 CORROSION ON AFT OUTBOARD NR 1 GALLEY TIE DOWN AT STATION 160, AFT SIDE OF GALLEY DRAIN PAN. REPLACED G1 GALLEY MOUNT PER AARD 51-00-00-012.

Part: RIB — CRACKED (ZONE 500) · airframe 69,190 hrs · 31,855 cycles

NR 5 SLAT CRACKED AT OUTBOARD EAR. REPLACED RIB PER ESO 80117.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

LEFT CUSP CRACKED AT STATION 225. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,036 hrs · 31,787 cycles

CRACK ON BOTTOM SIDE OF MID CARGO DOOR PAN. INSTALLED DOUBLER PER SRM 52-03-00.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 69,033 hrs · 31,786 cycles

LEVEL 1 CORROSION ON BOTTOM SIDE OF LEFT CUSP FROM STATION 275-285. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 69,036 hrs · 31,787 cycles

HFEC INDICATES CRACK ON LEFT WING LEADING EDGE NR 5 SLAT, OUTBOARD TRACK, ON UPPER INBOARD RIB. REMOVED AND REPLACED RIB ASSEMBLY PER SRM 57-50-08.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 69,036 hrs · 31,787 cycles

MID CARGO DOOR STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING PER ESO 80174.

Part: SUPPORT BRACKET — CORRODED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

LEVEL 1 CORROSION ON FORWARD GIRT BAR FITTING AT THE AFT SERVICE DOOR. INSTALLED SERVICEABLE GIRT BAR SUPPORT BRACKET PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

LEVEL 1 CORROSION UNDER FORWARD GIRT BAR BRACKET FITTING AT AFT SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 69,033 hrs · 31,786 cycles

CRACKED CHANNEL IN RIGHT WHEEL WELL, UPPER AFT CORNER. INSTALLED NEW ANGLE PER SRM 51-01-00.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 69,036 hrs · 31,787 cycles

MID CARGO DOOR STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING PER ESO 80174.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

LEVEL 1 CORROSION ON LEFT CUSP FROM STATION 488-496. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 69,036 hrs · 31,787 cycles

FLOORBOARD SUPPORT CRACKED AT STATION 926. REMOVED AND REPLACED SUPPORT PER SRM 51-01.

Part: PAN — CRACKED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

WINDOW PAN CRACKED AT UPPER FORWARD CORNER, BETWEEN STATION 946-965 RIGHT. TRIMMED OUT DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: FITTING — CRACKED (ZONE 800) · airframe 69,036 hrs · 31,787 cycles

CASTING INSIDE OF LARGE ACCESS HOLE OF AFT ENTRY DOOR IS CRACKED ON LT SIDE. REPLACED FITTING IAW ESO 80186.

Part: SKIN — DAMAGED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

DENT IN FUSELAGE SKIN AT STATION 248, LONGERON 15L-16L. COLD AND WORKED AND DYE CHECKED DENT, NO CRACKS, INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIGURE 38 VIEW E.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 69,033 hrs · 31,786 cycles

STIFFENER CRACKED AT STATION 1338 IN RIGHT AFT LAV AREA. REMOVED AND REPLACED STIFFENER PER SRM 51-01.

Part: LINK — STIFF (NOSE GEAR DOOR)

SFO INFLIGHT T562/07OCT - AFTER GEAR RETRACTION CREW REPORTED LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA. CYCLED GEAR THREE TIMES WITH NO IMPROVEMENT. NOISE AND VIBRATION INCREASED WITH AIR SPEED. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE LANDING GEAR DOOR OPEN ON ARRIVAL WITH RIGHT DOOR LINK STIFF. REPLACED RIGHT NOSE LANDING GEAR DOOR LINK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISINSTALLED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT SEAT ROWS 28DEF AND 29DEF OUT OF CONFIGURATION. CORRECTED CONFIGURATION FOR EMERGENCY LIGHTS AT SEAT ROWS 28DEF AND 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT FORWARD GALLEY CEILING AND ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY CEILING AND ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT EXTERIOR OFF WING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT EXTERIOR OFF WING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLADE — FAILED (ENGINE)

MCI - INFLIGHT STL TO SEA. CLIMBING THROUGH FLIGHT LEVEL 280 HEARD LOUD BANG FROM RIGHT HAND ENGINE ACCOMPANIED BY THRUST LOSS. RIGHT HAND ENGINE N1 LESS THAN LEFT HAND ENGINE N1. RIGHT HAND ENGINE SHUT DOWN AND LANDED MCI OVERWEIGHT WITHOUT INCIDENT. RIGHT HAND ENGINE WINDMILLED FOR APPROXIMATELY 15 MINUTES. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. FOUND TURBINE BLADE FAILURE WITHOUT PENETRATION. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACT — DIRTY (BATTERY PACK)

LGA - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. CLEANED CONTACTS FOR FIRST CLASS EMERGENCY BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHTS IN AFT CABIN ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 36 INOPERATIVE. REPLACED BATTERY PACK B5106 FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

LAX EMERGENCY TRACK LIGHTS AT AFT EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY TRACK LIGHTS AT AFT EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: O-RING — CUT (FILTER HOUSING)

STL - INFLIGHT T1986/12 RIGHT ENGINE OIL QUANTITY DECREASED TO ZERO. RIGHT ENGINE LOW PRESSURE LIGHT ILLUMINATED AND PRESSURE DECREASED TOWARDS ZERO. SHUTDOWN RIGHT ENGINE PER QRH PROCEDURE. ENGINE WINDMILLED NORMALLY FOR 15 MINUTES. LANDED STL WITHOUT INCIDENT. FOUND RIGHT OIL FILTER HOUSING O-RING CUT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — MALFUNCTIONED (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, THE SEAT MOUNTED EMERGENCY PATH LIGHTS FROM THE FRONT OF THE AIRCRAFT TO SEAT ROW 19 COME ON WHEN THE FORWARD LIGHT ATTENDANT EMERGENCY LIGHT SWITCH IS PUT IN THE 'ON' POSITION. REPLACED CONTROL MODULE AT STATION 850. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTNANCE, EMERGENCY EXIT LIGHTS 3-19 AND EXIT DOOR INOPERATIVE. REPLACED TWO EMERGENCY EXIT LIGHT BATTERIES. SYTSEM GORND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

AUS - DURING OVERNIGHT MAINTENANCE, L1 DOOR PORTABLE FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY PORTABLE FLASHLIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN NR 2 SEAT TRACK AT APPROX STATION 1304. REMOVED CORRODED AREA AND INSTALLED SEAT TRACK PLUG REPAIR PER 53-20-00-10. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EXTERIOR OVERWING EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

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

Part: FRAME (FS 313)

TUL - FOUND DENT IN TOP FLANGE OF FRAME STATION 313 BETWEEN LONGERON 24L-25L. REPAIRED FRAME PER AARD 53-10-00-17. (M)

Part: DOOR FRAME — DAMAGED (FUSELAGE)

TUL - FOUND DOUBLER IN FORWARD CARGO DOOR CUTOUT AT LOWER FORWARD CORNER NOT PER SRM. REMOVED OLD DOUBLER. INSTALLED DOUBLER PER ESO 80559 DATED 8-13-01. (M)

Part: SKIN — CRACKED (BS 1474)

TUL - FOUND .5 INCH CRACK ON THE RIGHT SIDE OF FUSELAGE AT STATION 1474. INSTALLED DOUBLER REPAIR PER AARP 53-30-00-02. (M)

Part: SKIN — DENTED (FS 1304)

TUL - FOUND DENT IN SKIN AT STATION 1304 LONGERON 19R. INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND INSTALLED SCUFF PLATE PER AARD 53-00-8 FIG 1. (M)

Part: SKIN — CRACKED (FS 1383)

TUL - FOUND CRACK IN SKIN AT FASTENER STATION 1383 JUST ABOVE L14R. STOP DRILLED CRACK AND INSTALLED DOUBLER AT STATION 1383 AOVER 14R IAW SRM 53-01 FIG 2. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND MID CARGO DOOR CUTOUT LOWER BEAM CORRODED STATION 636-693. REMOVED CORROSION, INSTALLED 2 ANGLE DOUBLER PER AARD 53-10-00-3 FIG 2 PAGE 18. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND STATION 446-448, LEFT CUSP CORRODED, TOP SIDE ALSO 1 INCH CRACK IN LEFT CUSP STATION 446-448. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FUSELAGE SKIN STATION 1383 AT FAST ABOVE LONGERON 14L. STOP DRILLED CRACKED INSTALLED DOUBLER REPAIR PER AARD 53-30-00-02. (M)

Part: ATTACH ANGLE — CRACKED (BS 1474)

TUL - FOUND CRACK IN EXTERNAL SURFACE ATTACH ANGLE (LEFT SIDE AT CANTED STATION 1474) FUSELAGE TO VERTICAL STAB JOINER. REPAIRED PER AARD 53-10-00-2 FIG 1 PAGES 1 AND 2. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP AT CLIP STATION 640. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP STATION 558. INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4. (M)

Part: LONGERON — CRACKED (BS 160)

TUL - FOUND CRACK AT FASTENER INBOARD FLANGE OF L4L AT STATION 160. CUT OUT CRACK, INSTALLED LONGERON SPLICE PER AARD 53-00-005 AND NEW END FITTING ON LONGERON. (M)

Part: SEAT TRACK — CORRODED (FS 1304)

TUL - FOUND NR 1 SEAT TRACK CORRODED AT STATION 1304. REMOVED DAMAGED AREA OF NR 3 SEAT TRACK, ALODINED AND PRIMED AND INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: LONGERON — CRACKED (FS 237)

TUL - FOUND LONGERON 17 LEFT CRACKED AT STATION 237 BEHIND FRAME. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR PER SRM 53-02 FIGURE 18. (M)

Part: FIRE DETECTOR — MALFUNCTIONED (RT ENGINE)

LAX - FLT 2710 - ON TAKEOFF ROLL, RIGHT ENGINE FIRE WARNING LOOP B ILLUMINATED. RETURNED AND LANDED LAX WITHOUT INCIDENT. REPLACCED THE LOWER BURN THROUGH BARRIER LOOP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: DOOR — OPEN (NLG)

YYC - FLT 676 - AFTER TAKEOFF, NOSE GEAR DOOR CAUSED VIBRATION. RETURNED AND LANDED YYC WITHOUT INCIDENT. RIGHT NOSE WHEEL WELL DOOR FOUND OPEN. INSPECTED WITH NO DAMAGE FOUND AND SECURED IN UP POSITION. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — NEEDED REPAIRING (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT SECTION OF COACH CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEXT TO RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERHEAD EMERGENCY EXIT LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPAIRED WIRE TO AFT OVERHEAD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR FRAME — MISDRILLED (BS 1174)

TUL - AFT CARGO DOOR LOWER DOOR BEAM AT AFT DOOR STOP, DOOR STOP BOLT HOLE IN SILL FRAME HAS NO EDGE DISTANCE ON OUTBOARD SIDE OF HOLE. INSTALLED DOUBLER ON AFT BOTTOM DOOR STOP BOLT HOLE AND DOOR BEAM PER AARD 53-10-00-16. (M)