N487AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,241 hrs · 40,643 cycles

REFERENCE WORK CARD 0801. EMER LIGHTS ROW 22 - 27 FAILED TO TEST. REPLACED EMER LIGHT BATTERY PACK B5-106 IAW AMM 33-53-00. TESTED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,241 hrs · 40,643 cycles

REFERENCE WORK CARD 0801. EMER LIGHTS ROW 28 - 32 FAILED TO TEST. REPLACED EMER LIGHT BATTERY PACK B5-107 IAW AMM 33-53-00. TESTED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,241 hrs · 40,643 cycles

REFERENCE WORK CARD 0801. EMERGENCY LIGHTS ROW 17 - 21 FAILED TO TEST. REPLACED EMER LIGHT BATTERY PACK B5-104 IAW AMM 33-53-00. TESTED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,241 hrs · 40,643 cycles

REFERENCE WORK CARD 5403, EGRESS POWER SUPPLY AB5-1 FAILS TEST. REPLACED EGRESS LIGHT POWER SUPPLY AB5-1 BATTERY PACK IAW AMM 33-60-98. TESTED OK.

Part: TRANSDUCER — DAMAGED (ZONE 700) · airframe 77,199 hrs · 40,618 cycles

AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL, WHEEL NOT TURNING LIGHT ILLUMINATED. TAKEOFF ABORTED PRIOR TO 80 KNOTS. FOUND BROKEN PINS AT NR 2 WHEEL SPEED TRANSDUCER. R & R TRANSDUCER IAW AMM 32-43-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 76,639 hrs · 40,292 cycles

CRACK IN STATION 1418 FRAME WHERE L2R TERMINATES. R & R AFT STIFFENER AT STATION 1418, L5L TO L5R IAW EA 254341.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,639 hrs · 40,292 cycles

DURING LC21 CHECK, CRACKS WERE FOUND COMMON TO THE 5967113-1 & 5967113-501 FRAME CAPS & THE 5967114-505 FRAME WEB AT FS 1437 COMMON TO THE 4918093 DORSAL FITTINGS AT L2L & L2R. REPAIRED FRAME CAPS & WEB EA 253748. SEE ALSO AALA20150909012 & AALA20150909013.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,639 hrs · 40,292 cycles

DURING LC21 CHECK, CRACKS WERE FOUND COMMON TO THE 5967113-1 & 5967113-501 FRAME CAPS & THE 5967114-505 FRAME WEB AT FUSELAGE 1437 COMMON TO THE 4918093 DORSAL FITTINGS AT L2L & L2R. REPAIRED FRAME CAPS & WEB EA 253748. SEE ALSO AALA20150905002 & AALA20150909013.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,639 hrs · 40,292 cycles

DURING LC21 CHECK, CRACKS WERE FOUND COMMON TO THE 5967113-1 & 5967113-501 FRAME CAPS & THE 5967114-505 FRAME WEB AT FUSELAGE 1437 COMMON TO THE 4918093 DORSAL FITTINGS AT L2L & L2R. REPAIRED FRAME CAPS & WEB EA 253748. SEE ALSO AALA20150905002 & AALA20150909012.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,639 hrs · 40,292 cycles

FUSELAGE SKIN WAS FOUND CRACKED AT TWO LOCATIONS, STATION 1437 ABOVE & BELOW LONGERON 3L. PERFORMED DOUBLER & TRIPLER REPAIR IAW EA 253684.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 76,639 hrs · 40,292 cycles

STOP PAD BRACKET CRACKED ON FWD SIDE OF MID CARGO DOOR AT 2ND FROM BOTTOM OF DOOR. R & R DOOR STOP PAD BRACKET IAW AARD 51-00-05-1 & DWG 5910141.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 76,639 hrs · 40,292 cycles

STOP PAD BRACKET CRACKED ON FWD SIDE OF FWD CARGO DOOR AT CTR OF DOOR. R & R DOOR STOP PAD BRACKET IAW AARD 51-00-05-1 & DWG 5910141.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 76,639 hrs · 40,292 cycles

STOP PAD BRACKET CRACKED ON FWD SIDE OF FWD CARGO DOOR AT UPPER CORNER. R & R DOOR STOP PAD BRACKET IAW AARD 51-00-05-1 & DWG 5910141.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 76,639 hrs · 40,292 cycles

STOP PAD BRACKET CRACKED ON FWD SIDE OF FWD CARGO DOOR AT LOWER CORNER. R & R DOOR STOP PAD BRACKET IAW AARD 51-00-05-1 & DWG 5910141.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,639 hrs · 40,292 cycles

CRACKS IN FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERONS 3R & 4R. INSTALLED DOUBLER REPAIR IAW SRM 53-04-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 75,784 hrs · 39,818 cycles

EMERGENCY TAIL LIGHTS AT TAIL CONE & AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED THE LAMPS FOR BOTH LIGHTS. OPERATIONALLY CHECKED GOOD.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,392 hrs · 39,608 cycles

LONGERON 23 LT IS CRACKED AT FS 200. R & R LONGERON SECTION IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,392 hrs · 39,608 cycles

LONGERON 25 LT IS CRACKED AT FS 200 & 160. R & R LONGERON SECTION IAW SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,392 hrs · 39,608 cycles

LONGERON 24 LT CRACKED AT FS 200. R & R LONGERON SECTION IAW SRM 53-02-00.

Part: RIB — CRACKED (RT WING) · airframe 75,392 hrs · 39,608 cycles

RIGHT WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER IAW EA 57-038624 DATED 16 FEB 2015.

Part: RIB — CRACKED (LT WING) · airframe 75,392 hrs · 39,608 cycles

LEFT WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. INSTALLED REPAIR DOUBLER IAW EA MD80-57-038624 DATED 16 FEB 2015.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 72,951 hrs · 38,171 cycles

LT HAND FWD FLANGES OF VERTICAL STABILIZER & LE SKIN DAMAGED. ACCOMPLISHED REPAIR TO STABILIZER IAW EA MD80 55-033866 & SRM 55-03 FIGURE 29 & 30.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 72,951 hrs · 38,171 cycles

VERTICAL STAB LT HAND HOLE, 4TH HOLE BELOW STATION ZFS 52.267 ELONGATED. INSTALLED BUSHING & STRAP REPAIR IAW DRAWING SG09550005.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 72,951 hrs · 38,171 cycles

AFT ACCESSORY LONGERON 2 LT IS CRACKED AT AFT END OF STATION 1418. REPLACED LONGERON 2 LT & SPLICE IAW SRMS 53-02-00, 53-02-00-001 & DRAWING DDK2782.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 71,996 hrs · 37,621 cycles

LT HAND AFT LAVATORY SMOKE DETECTOR WOULD NOT TEST. INSTALLED NEW SMOKE DETECTOR. OPERATIONS CHECKED NORMAL.

Part: DUCT — LEAKING (AC BAY) · airframe 71,235 hrs · 37,177 cycles

TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED ON CLIMB-OUT. FOUND DUCT LEAKING BETWEEN THE RT PRESSURE REGULATOR VALVE & THE FLOW CONTROL VALVE AT A SENSE LINE UNION. REPLACED DUCT. SYSTEM GROUND CHECKED NORMAL

Part: SWITCH — INOPERATIVE (AC BAY) · airframe 70,051 hrs · 36,530 cycles

LGA - CREW REPORTED LEFT PACK FAILED WITH RIGHT PACK ON MEL. EMERGENCY DECLARED FLIGHT RETURNED LGA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH SINGLE SEGMENT SWITCHES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

ELONGATED HOLE UNDER DOOR GUIDE AT STATION 1212 FROM LONGERONS 25 TO 24 RIGHT. INSTALLED REPAIR DOUBLER ON FRAME STATION 1212 PER EA MD80-53-025872.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,084 hrs · 35,961 cycles

CORROSION ON INTERNAL SKIN FROM STATIONS 750 TO 760 AT LONGERONS 30 TO 29 LEFT AND RIGHT. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 11 SHEET 1 VIEW A.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

CUSP SHEET CRACKED AT FASTENER BETWEEN SEAT TRACKS NUMBERS 1 AND 2. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: PAN — CRACKED (OVERWING EXIT) · airframe 69,084 hrs · 35,961 cycles

LEFT FORWARD OVERWING EXIT DOOR PAN CRACKED AT UPPER AFT CORNER. DYE CHECKED AND STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 52-05-00 FIGURE 51.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

LIGHTNING STRIKE TO FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2 SHEET 3 VIEW C.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

LIGHTNING STRIKE TO FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2 SHEET 3 VIEW C.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

LIGHTNING STRIKE TO FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2 SHEET 3 VIEW C.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

LONGERON 4 LEFT IS CRACKED AT STATION 218 IN THE RADIUS IN THE OUTBOARD LEG. INSTALLED LONGERON AND SPLICE AT LONGERON 4 STATION 218 PER SRM 53-02-00 FIGURE 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

CRACK IN RIGHT FUSELAGE SKIN AT STATION 1310 BETWEEN LONGERONS 6 AND 7 RIGHT. INSTALLED DOUBLER, FILLER AND FINGERS PER SRM 53-04-03 FIGURE 9 AND 51-01-00 PARAGRAPH 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,084 hrs · 35,961 cycles

NUMBER 5 SEAT TRACK AT STATION 200 CORRODED. ACCOMPLISHED STRAP REPAIR PER AARD 53-20-00-13.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,084 hrs · 35,961 cycles

DENT AT LEFT STATION 275 BETWEEN STRINGERS 23 AND 24 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02 FIGURE 02 SHEET 36.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,842 hrs · 35,819 cycles

FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY CHARGER FOR FORWARD EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: APU — MALFUNCTIONED (ZONE 100) · airframe 64,642 hrs · 33,513 cycles

DFW - CREW REPORTED AUXILIARY POWER UNIT FAILED ON TAKEOFF WITH LEFT GENERATOR ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SHUTDOWN AND RESTARTED APU, RAN APU FOR 20 MINUTES NO FAULTS NOTED. REPLACED LEFT GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,538 hrs · 31,873 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,538 hrs · 31,873 cycles

FUSELAGE SKIN CRACKED AT CANT FRAME 1474. INSTALLED DOUBLER PER SRM 53-01-00 ON FUSELAGE AT STATION 1474.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 61,451 hrs · 31,825 cycles

AFTER TAKEOFF FLIGHT ATTENDANTS REPORTED FUMES IN THE CABIN. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE REGULATOR VALVE IN TAIL SECTION.

Part: DETECTOR — INOPERATIVE (NR 2 ENGINE) · airframe 60,642 hrs · 31,372 cycles

AUS - RIGHT ENGINE WARNING INDICATION ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED, RETURNED AUS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE DETECTOR AMPLIFIER AND CAWS COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — ACTIVATED (FUEL SYSTEM)

ATL INFLIGHT T2233/18MAY RSW TO STL. CENTER FORWARD FUEL BOOST PUMP POPPED CIRCUIT BREAKER. LANDED ATL WITHOUT INCIDENT. REPLACED CENTER FORWARD FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,836 hrs

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

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHTS) · airframe 56,836 hrs

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 7 TO 16 INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 7 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DAMAGED (L2 DOOR) · airframe 56,084 hrs

MSP - EMERGENCY SLIDE AT LEFT NUMBER TWO DOOR HANDLE VELCRO MISSING. REPLACED SLIDE AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA - FOUND EMERGENCY LIGHT AT AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT AFT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT LENS AT STAIRWAY MISSING. REPLACED MISSING LIGHT LENS FOR EMERGENCY LIGHT AT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29 INOPERATIVE. REPLACED TWO BATTERY PACKS FOR CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ATL - EMERGENCY LIGHTS FROM 20D TO 31D INOPERATIVE. REPLACED BATTERY PACK AT 20D FOR EMERGENCY LIGHTS FROM 20D TO 31D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS BATTERY PACK B5-105 INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK B5-105 PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, WHEN BATTERY MASTER WAS PLACED IN OFF POSITION OR EMERGENCY LIGHT SWITCH WAS PLACED IN THE ARM POSTION THE COCKPIT, FORWARD ENTRY, SERVICE ENTRY AND STATION 213 EMERGENCY LIGHTS CAME ON. REPLACED BATTEYR PACK AT B5 23. SYSTEM GROUND CHECKED NORMAL OPERAITON. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

SUB FLOOR DIAPHRAGM, CUSP LINE WEB IS CORRODED BELOW G1 GALLEY LINE CONNECTION PAN BETWEEN INBOARD AND AFT DRAIN/SUPPLY LINES BETWEEN STA 148-160. 2 INCH X 2 INCH AREA, .025 INCH DEPTH. REMOVED CORROSION, INSTALLED DOUBLER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND FRAME WITH .25 INCH CRACK ON LEFT, CANT FRAME 1474 6 INCHES FORWARD OF LOUVER BOX DRAIN TUBE FITTING ON FUSELAGE. STOP DRILLED CRACK, MFG AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG NR 2. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACK AT COUNTERSINK RIVET 6 INCHES ABOVE LEFT PYLON. REPAIRED PER SRM 53-01-00 AND AARD 53-30-00-02. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE FLIGHT ATTENDANT FORWARD EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT FLIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY AISLE WALL INOPERATIVE. REPAIRED QUICK DISCONNECT SPLICES AT GALLEY AISLE WALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TERMINAL — BROKEN (TAIL)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT TAIL INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT WIRE TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COOLER — LEAKING (APU OIL SYSTEM)

DFW - FLT 1258 - ON TAKEOFF, CREW REPORTED SMOKE IN CABIN. DECLARED EMERGENCY, RETURNED AND LANDED DFW WITHOUT INCIDENT. REPAIRED OIL LEAK ON OIL COOLER ASSY. CHANGED COALESCER BAGS AND ACCOMPLISHED PACK BURN-OUT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND FUSE SKIN GOUGED FORWARD OF CANT 1431 LONGERON 4R. INSTALLED DOUBLER FORWARD CANT 1431, LONGERON 4R PER SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND 8 INCH SECTION FUSE SKIN HAS MULITPLE DENTS, WRINKLES 1408 STATION LONGERON 2R AND 2L. INSTALLED DOUBLERS ON LEFT AND RIGHT SIDES LONGERONS PER 53-01 FIG 2 SHEET 3. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK AND HOLE IN CUSP AT STATION 183 RIGHT INBOARD OF FORWARD SERVICE DOOR. ROUTED OUT CRACK AND CUTOUT DAMAGED AREA. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: FITTING — CORRODED (HORIZONTAL STAB)

TUL - FOUND RIGHT HORIZ STABILIZER SUPPORT LUG PLATES ON VERTICAL STABILIZER CORRODED BEYOND LIMITS. REMOVED AND REPLACED ALL 4 RIGHT STABILIZER HINGE SUPPORT LUG PLATES SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND TRACK 5 CORRODED STATION 203-204 TOP OUTBOARD FLANGE. INSTALLED A STRAP PER AARD 53-20-00-13. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON UPPER SURFACE OF CUSP FROM STATION 465 TO STATION 483 ON LEFT SIDE. REMOVED DAMAGE, INSTALLED NEW CUSP LEFT STATION 438-503 PER SRM 51-01. (M)

Part: WEB — DENTED (FUSELAGE)

TUL - FOUND DENT IN CUSP FORWARD SIDE STATION 465 LEFT SIDE. REMOVED DAMAGE, INSTALLED NEW CUSP LEFT STATION 438-503 PER SRM 51-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND FASTENER HOLES OF CARGO FLOOR SUPPORT AT STRINGER 29 RIGHT FROM STATION 1155 TO 1211. REMOVED AND REPLACED FLOORBOARD SUPPORT ANGLE 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK CORRODED STATION 200-798. REMOVED AND REPLACED NR 6 SEAT TRACK SRM 51-00-00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP LOWER SIDE CORRODED, SIDE OF LIGHTENING HOLE. INSTALLED CUSP DOUBLER PER SRM 53-01 FIG 4 PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND SEAT TRACK NR 6 IS WORN STATION 826. INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A SHEET 1. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND LEFT WINDOW FRAME CRACKED, FORWARD LOWER CORNER STATION 1250. STOP DRILLED CRACK. INSTALLED DOUBLER AARD 53-10-00-25. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND RIGHT CUSP IS CRACKED STATION 826. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: ANGLE — CORRODED (DOOR FRAME)

TUL - FOUND CORROSION ON ANGLE AT LOWER AFT CORNER OF CARGO DOOR JAMB. INSTALLED NEW ANGLE PER 51-01. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND SHEAR TIE CRACKED AT FS 1437 AT BL 10 LEFT AND RIGHT. REMOVED AND REPLACED BOTH LEFT AND RIGHT SHEAR TIE WITH NEW PARTS SRM 51-01. (M)

Part: ANGLE — CORRODED (DOOR FRAME)

TUL - FOUND CORROSION ON ANGLE AT FORWARD LOWER CORNER OF AFT CARGO DOOR JAMB. REPLACED ANGLE WITH NEW PART PER 51-01. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND SEAT TRACK NR 4 IS WORN STATION 879. ROUTED OUT BLENDED AREA AND INSTALLED SEAT TRACK PLUG PER SRM 53-05. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND TWO DENTS IN FUSELAGE 2 FEET AFT OF FORWARD ENTRY DOOR BETWEEN 17L AND 19L. COLD WORKED DENTS, INSTALLED INTERIOR DOUBLER PER SRM 53-04 FIG 38 SHEET 28 VIEW P AND AARD 53-30-01-01 PAGE 2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK 1 CORRODED AT STATINO 1236. REPAIRED PER AARD 53-20-00-10. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND HOLE IN RIGHT CUSP. FABRICATED DOUBLER INSTALLED PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SENSING ELEMENT — DENTED (FUSELAGE SKIN)

TUL - FOUND SMALL DENT BELOW LEFT FORWARD AUX STATIC PORT. INSTALLED TITANIUM DOUBLER PER SRM 53-04 FIG 38 PER REPAIR. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1 FS 824-826. REMOVED CORROSION CUTOUT DAMAGE AND INSTALLED PLUG PER SRM 53-05 FIG 4B. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SCRATCH WITH DENT IN FUSELAGE SKIN STATION 1309 LONGERON 19R. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: PIN — INSTALLED (NLG)

ABQ - FLT 1284 - AFTER TAKEOFF ABQ EN ROUTE DFW, COULD NOT RETRACT NOSE GEAR. AIR INTERRUPTED AND RETURNED ABQ. LANDED WITHOUT INCIDENT. REMOVED NOSE GEAR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)