N505AA

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 70,929 hrs · 37,209 cycles

MID CARGO DOOR LOWER FWD STOP PAD FITTING CRACKED. R & R FITTING.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 70,905 hrs · 37,191 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05 & EA MD80-57-034432.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 70,905 hrs · 37,191 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMED IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06 & EA MD80-57-034432.

Part: SCHRADER VALVE — FAULTY (NLG) · airframe 69,830 hrs · 36,585 cycles

LAX CREW REPORTED NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SHRAEDER VLV & REPACKED LOWER STRUT PISTON WITH NEW SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CADC — INOPERATIVE (NR 2) · airframe 68,696 hrs · 35,926 cycles

NR 2 CENTRAL AIR DATA COMPUTER, ALTITUDE ALERT & AUTO PILOT FAILED AFTER TAKE OFF. EMERGENCY DECLARED FLIGHT RETURNED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 2 CENTRAL AIR DATA COMPUTER SYSTEM. GROUND CHECKED NORMAL OPERATION.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,977 hrs · 34,990 cycles

HEAVY CORROSION ON UNDER SIDE OF CUSP T FROM STATIONS 148 TO 160, RIGHT BUTTLINE 57. REPLACED CUSP ANGLE PER EA MD80-53-026762.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CORROSION ON SUBFLOOR FROM STATIONS 160 TO 200, RIGHT BUTTLINE 44 TO 57. INSTALLED SUBFLOOR DOUBLER FROM STATIONS 160 TO 200 RIGHT AND SUBFLOOR OVERLAY/DOUBLER FROM STATIONS 160 TO 184 RIGHT PER AARD 53-20-00-16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CRACKED ANGLE LOWER OUTBOARD END OF STIFFENER ON FORWARD SIDE OF STATION 1338 BULKHEAD NEXT TO LONGERON 15 RIGHT. INSTALLED CLIP PER AARD 51-00-05-1.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

FASTENER AT STATION 1437 BETWEEN LONGERONS 2 AND 3 LEFT CRACKED. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CRACKED ANGLE UPPER OUTBOARD END OF STIFFENER ON FORWARD SIDE OF STATION 1338 BULKHEAD NEXT TO LONGERON 14 RIGHT. INSTALLED NEW OUTBOARD ANGLE PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CRACKED ANGLE LOWER OUTBOARD END OF STIFFENER ON FORWARD SIDE OF STATION 1338 BULKHEAD NEXT TO LONGERON 14 RIGHT. INSTALLED NEW OUTBOARD ANGLE PER AARD 51-00-05-1.

Part: BEAM — GOUGED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

AFT CARGO HAS DEEP GOUGE IN CEILING BEAM AT STATION 1174, INBOARD OF DOOR OPENING. BLENDED GOUGE AND INSTALLED REPAIR ANGLE ON CEILING BEAM PER AARD 53-20-00-21.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 66,977 hrs · 34,990 cycles

MID CARGO DOOR OUTER SKIN IS DAMAGED. INSTALLED NEW EXTERIOR SKIN PER ESO 80174.

Part: SKIN — BENT (CARGO DOOR) · airframe 66,977 hrs · 34,990 cycles

FORWARD CARGO DOOR, EXTERIOR SKIN LOWER SECTION, EDGE OF SKIN BENT TO RIVETS. INSTALLED REPAIR LOWER SECTION OF SKIN PER ESO 80174.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

FUSELAGE SKIN CRACKED AT STATIONS 1309, LONGERON 7 RIGHT. INSTALLED DOUBLER, DOUBLER FILLER, AND FINGERS PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CRACK IN RIGHT CUSP, STATION 807, AREA WHERE SEAT TRACK SPLICE FASTENERS ATTACH. INSTALLED NEW CUSP SHEET FROM STATIONS 788 TO 807 PER AARD 51-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CRACK IN LONGERON 4 LEFT OUTBOARD FLANGE AT STATION 160. REMOVED DAMAGED PORTION OF LONGERON AND INSTALLED NEW LONGERON SECTION PER AARD 51-00-05-1.

Part: RIB — CRACKED (LE SLAT) · airframe 66,977 hrs · 34,990 cycles

LEFT WING NUMBER 5 SLAT, NUMBER 15 SLAT RIB HAS CRACK INDICATION. REPLACED NUMBER 15 RIB ON SLAT NUMBER 5 PER ESO 80117.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

FUSELAGE SKIN CRACKED AT STATION 1309, LONGERON 7 LEFT. INSTALLED DOUBLER, DOUBLER FILLER, AND FINGERS PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,977 hrs · 34,990 cycles

CRACK ON RIGHT CUSP FROM STATIONS 724 TO 726. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,977 hrs · 34,990 cycles

AFT CARGO HAS CORROSION ON CUSP ABOVE DOOR OPENING FROM STATIONS 1174 TO 1193. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SWITCH — FAILED (COCKPIT) · airframe 65,832 hrs · 34,316 cycles

DFW - CREW REPORTED SLAT AURAL WARNING AND SLAT DISAGREE LIGHT ON. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP HANDLE SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL UNIT — UNKNOWN (ELECTRICAL SYS) · airframe 65,605 hrs · 34,189 cycles

ONT - CREW REPORTED DURING CLIMBOUT RIGHT GENERATOR WAS CYCLING CAUSING RELAY CHATTER AND ALL LIGHTS AND GAUGES TO FLICKER. EMERGENCY DECLARED FLIGHT RETURNED ONT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT BUS CONTROL UNIT AND GENERATOR CONTROL UNIT (MPN-947F9453). SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE HARNESS — SHORTED (CABIN) · airframe 63,826 hrs · 33,203 cycles

FOUND POWER PORT UNIT AT SEAT 12D HAD SHORTED OUT. REPLACED POWER SUPPLY J BOX AND POWER PORT HARNESS FOR 12DEF. OPS CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 63,529 hrs · 33,055 cycles

ROW 7 EGRESS LIGHT LAMP BROKEN. REPLACED LAMP FOR ROW 7 EMERGENCY EGRESS LIGHT. OPS CHECK NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 63,529 hrs · 33,055 cycles

ROW 7 EGRESS LIGHT SHROUD LENS KNOCKED OFF. REPLACED LENS FOR ROW 7 EMERGENCY EGRESS LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 63,529 hrs · 33,055 cycles

TAIL CONE JETTISON INTERIOR CATWALK HANDLE EMERGENCY ILLUMINATOR LIGHT INOPERATIVE. RE-SEATED BATTERY PACK. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 63,529 hrs · 33,055 cycles

OVERHEAD CATWALK EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK FOR OVERHEAD CATWALK EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,529 hrs · 33,055 cycles

AFT CABIN OVERHEAD EMERGENCY LIGHT BY AFT LAVS AND BULKHEAD DOOR INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN OVERHEAD EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,538 hrs · 32,497 cycles

FOUND AFT ACCESSORY COMPARTMENT OVERHEAD CATWALK EMERGENCY LIGHT INOPERATIVE. RE-SEATED BATTERY PACK FOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,538 hrs · 32,497 cycles

FOUND AFT ACCESSORY AFT RIGHT OVERHEAD EMERGENCY LIGHT INOPERATIVE. RE-SEATED ASSOCIATED BATTERY PACK BATTERY. OPS CHECK NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 60,152 hrs · 31,191 cycles

LONGERON 2 RIGHT CRACKED AT STATION 1418. REMOVED DAMAGE INSTALLED SPLICE REPAIR PER AARD 53-30-00-2.

Part: CHARGER — FAILED (MAIN BATTERY) · airframe 58,624 hrs · 30,342 cycles

BNA - INFLIGHT DCA-DFW. BATTERY CHARGER ILLUMINATED INFLIGHT. EMERGENCY DECLARED, LANDED AT BNA WITHOUT INCIDENT. REMOVED AND REPLACED BATTERY CHARGER BREAKER AND BOTH BATTERIES IN ACCORDANCE WITH MD80 AMM 24-30-01-4 AND 30-02-2. OPS CHECK GOOD OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW- COCKPIT EMERGENCY LIGHTS STAYS ON WITH POWER OFF. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COCKPIT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - BATTERY PACK AT B5 28 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 28 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,864 hrs

LGA - BATTERY PACK AT B5 23 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 23 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,864 hrs

LGA - BATTERY PACK AT B5 1 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 1 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,864 hrs

LGA - BATTERY PACK AT B5 105 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 105 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,864 hrs

LGA - BATTERY PACK AT B5 100 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 100 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,864 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,864 hrs

LGA - BATTERY PACK AT B5 101 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 101 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,864 hrs

LGA - BATTERY PACK AT B5 3 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 3 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 10 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 10. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT OVERHEAD MAIN ENTRY DOOR TO SEAT ROW 3 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD MAIN ENTRY DOOR TO SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: LENS — BROKEN (CABIN)

DFW - EMERGENCY LIGHT AT SEAT ROW 15DEF HAS CRACKED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RADOME — DAMAGED (FUSELAGE)

BNA - ON POST FLIGHT FOUND BIRD STRIKE ON RADOME. RADOME PUNCTURED AND RADAR ANTENNA DENTED. REPLACED RADOME AND RADAR ANTENNA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - FORWARD DOOR OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD DOOR OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — DAMAGED (RIGHT)

EN ROUTE PHL-DFW, COMPRESSOR STALL ON RIGHT ENGINE AFTER TAKEOFF. POWER WAS REDUCED AND STALLS CLEARED. ALL ENGINE INDICATIONS REMAINED IN NORMAL RANGE. RIGHT ENGINE KEPT RUNNING FOR APPROACH. LANDED PHL WITHOUT INCIDENT. REPLACED NUMBER 2 ENGINE DUE TO FOD DAMAGE INCURRED OVERTEMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - EMERGENCY LIGHTS AT UPPER OVERHEAD IN FORWARD CABIN LOCATION B5-100 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT UPPER OVERHEAD IN FORWARD CABIN AT LOCATION B5-100. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN)

DFW - EXIT IDENTIFIER BETWEEN 1ST CLASS AND FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EXIT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN CEILING OF ENTIRE AIRCRAFT INOPERATIVE. PERFORMED BATTERY TRICKLE CHARGE FOR 6 HOURS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

BOS - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT PORTABLE ASSEMBLY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT PORTABLE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3, 7, 9, 10, 13, 16, 18, 19, 21, 22, 23, 25, 26 THROUGH 31 DIM. REPLACED EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED, 1 INCH, AT FASTENER STATION 1381 LONGERON 14L ABOVE NR 1 ENGINE PYLON. ROUTED OUT LENGTH OF CRACK AND INSTALLED DOUBLER AT STATION 1381 LONGERON 14L PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED .5 INCH AT FASTENER STATION 1381 LONGERON 14L ABOVE NR 1 ENGINE PYLON. ROUTED OUT CRACK AND INSTALLED DOUBLER AT STATION 1381 LONGERON 4L PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND STATION 838 CORRODED ON RIGHT CUSP, 2 INCHES BY 2 INCHES, AROUND LIGHTENING HOLE TOP AND BOTTOM SIDE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP SHEET SEVERAL PLACES. REPLACED CUSP SHEET FROM STATION 598-712 LEFT SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP SHEET CORRODED 2 INCHES BY 2 INCHES, SEVERAL PLACES STATION 712 TO STATION 788. REMOVED CUSP SHEET, INSTALLED NEW CUSP SHEET 51-01. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION 797 CUSP CRACKED 1 INCH AT NR 2 SEAT TRACK SPLICES. REPLACED CUSP SHEET FROM STATION 788-807 LEFT SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND SEAT TRACK CORRODED FROM STATION 1164 TO 1309, SEAT TRACK NR 2. REMOVED AND REPLACED SEAT TRACK SRM 53-05 PART 1 FIG 4. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND DEEP GOUGE AND DENT AT STATION 117 BETWEEN 27R AND 28R IN FUSELAGE SKIN. INSTALLED NEW DOUBLER PER ESO 80559, DATED 11/3/2000. (M)

Part: FRAME — CRACKED (CABIN WINDOW)

TUL - FOUND UPPER AFT CORNER OF WINDOW FRAME CRACKED .2 INCH, AT APPROX STATION 1060, LEFT SIDE. STOP DRILLED CRACK, DYE CHECKED TO CONFIRM, VERIFIED MATERIAL AND INSTALLED REPAIR PER AARD 53-10-00-25.L (M)

Part: FRAME — CRACKED (CABIN WINDOW)

TUL - FOUND UPPER AFT CORNER OF WINDOW FRAME CRACKED .25 INCH AT APPROX STATION1041 LEFT SIDE. TRIMMED OUT CRACK, DYE CHECKED TO CONFIRM, VERIFIED MATERIAL AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

TUL - FOUND CRACK .25 INCH IN UPPER FLANGE OF INTERCOSTAL STATION 1271-1287 BL 0. INSTALLED NEW INTERCOSTAL SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1193-1208. INSTALLED NEW SEAT TRACK NR 1 FROM STATION 1174-1309 PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED, .040 INCH BY 3 INCH AND .020 INCH DEEP, STATION 826. INSTALLED NEW SEAT TRACK FROM STATION 798-1031 PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED, 1 INCH BY 1 INCH AND .030 DEEP, AT STATION 1262. INSTALLED NEW SEAT TRACK NR 1 FROM STATION 1174-1309, PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - NR 1 SEAT TRACK CORRODED STATION 1211-1223. INSTALLED NEW SEAT TRACK FROM STATION 1174-1309 PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED AT STATION 1235. INSTALLED NEW SEAT TRACK NR 1 FROM STATION 1174-1309 PER SRM 51-01. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK WORN BEYOND LIMITS. ROUTED WORN AREA AND INSTALLED PLUG PER SRM 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED 3 INCHES BY 2 INCHES, ON LUGS AT STATION 865. INSTALLED NEW TRACK SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT SIDE OF CABIN UPPER SURFACE OF CUSP CORRODED 3 INCHES BY 4 INCHES, STATION 610-614. INSTALLED CUSP DOUBLER PER SRM 53-01 FIG 4. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

TUL - FOUND CRACK, .75 INCH, IN AFT FLANGE OF INTERCOSTAL STATION 1041. INSTALLED NEW INTERCOSTAL PER SRM 51-01 STATION 1022-1041 BL 0. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED, .25 INCH, IN RADIUS AT STATION 154. INSTALLED SPLICE IN LONGERON PER SRM 53-02. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SCRAPE AND DENT IN FUSELAGE SKIN AT L28R STATION 539. COLD WORKED DENT TO WITHIN LIMITS AND INSTALLED INTERNAL 2024T3-032 DOUBLE 11-4-00 PER SRM 53-04 FIG 38. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND DENT AND GOUGE ON LEFT FUSELAGE 8 INCHES AFT OF LOWER EDGE OF FORWARD LAVATORY SERVICE DOOR BETWEEN STRINGERS. DYE CHECKED AREA AFTER COLD WORKING, NO CRACK. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1 INCH BY 3 INCHES, NR 5 SEAT TRACK AROUND CLIP NUT HOLES. INSTALLED SEAT TRACK SPLICE REPAIR PER SRM 51-01, NR 5 FROM STATION 200 TO 265 PER SRM 53-05 PART 1. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1 INCH BY 12 INCHES, NR 3 SEAT TRACK STATION 1197-1209. INSTALLED NEW TRACK SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND AREA OF CORROSION ON LEFT CUSP AROUND FITTING LIGHTENING HOLE FORWARD OF STATION 617. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER FORWARD OF STATION 617 SRM 53-01 FIG 4-3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED, 1 INCH BY 4 INCHES, STATION 1246-1250. INSTALLED SEAT TRACK PLUG PER SRM 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1 INCH BY 2 INCHES, NR 3 SEAT TRACK STATION 1302. INSTALLED NEW TRACK SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1 INCH BY 15 INCHES, ON NR 3 SEAT TRACK STATION 1279. INSTALLED NEW TRACK SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 5 SEAT TRACK STATION 236. INSTALLED SEAT TRACK SPLICE REPAIR ON TRACK PER 51-01 FROM STATION 200 TO 265 PER SRM 53-05 PART 2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION, 1 INCH BY 3 INCHES, ON SEAT TRACK NR 1 STATION 1022 TO 1025. INSTALLED NEW TRACK SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 6 SEAT TRACK, STATION 1150. ROUTED CORRODED AREA AND INSTALLED PLUG PER SRM 53-20-00-10. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND DENT AT STATION 230 BETWEEN LONGERON 19L AND 20L. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORRODED, 1 INCH BY 3 INCHES, AT STATION 826. INSTALLED NEW TRACK SRM 51-01. (M)

Part: BEAM — CORRODED (CARGO DOORWAY)

TUL - FOUND CORROSION, 1 INCH BY 6 INCHES, ON AFT CARGO DOOR JAMB BEAM STATION 1155 TO STATION 1212. INSTALLED DOUBLER REPAIRS PER AARD 53-10-00 AND ESO 80559 11/7/2000. (M)

Part: DOOR FRAME — CRACKED (RT MLG DOOR)

TUL - FOUND RIGHT MAIN GEAR DOOR CUTOUT JAMB FORWARD OUTBOARD SECTION CRACKED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-10. (M)

Part: ENGINE — LEAKING (NR 2)

GDL - FLT 1276 - AFTER ROTATION FLIGHT ATTENDANT REPORTED AIR CONDITIONING SMOKE IN CABIN. RETURNED AND LANDED GDL WITHOUT INCIDENT. OIL LEAK FROM BREATHER. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (COCKPIT)

SAT - FLT 1463 - ON APPROACH, SLAT DISAGREE LIGHT ILLUMINATED. DECLARED EMEGENCY AND LANDED SAT WITHOUT INCIDENT. INSPECTED AND CYCLED FLAPS SEVERAL TIMES. REPLACED FLAT/SLAT HANDLE POSITION SWITCH ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: SPLICES — CORRODED (CABIN)

PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDEWALL LIGHTS AND EXIT SIGN LIGHTS INOPERATIVE. REPLACED WIRE SPLICES TO EMERGENCY EXIT SIDEWALL LIGHTS AND EXIT SIGN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COMPRESSOR — FAILED (NR 1 ENGINE)

ORD - FLT 1063 - EN ROUTE ORD-DEN AT 27,000 FT CREW NOTICED SMOKE IN AFT SECTION OF CABIN. ACCOMPLISHED CHECKLIST FOR SMOKE AND FUMES IN CABIN, LOWERED PACK TEMPERATURE, SMOKE BEGAN TO DISSIPATE. WHILE CLIMBING THROUGH 6300 FEET A LOUD EXPLOSION WAS HEARD. LEFT ENGINE BEGAN WINDING DOWN AND AIRCRAFT BEGAN VIBRATING. LEFT ENGINE SEIZED UP WITHIN SECONDS OF FAILURE. AIR INTERRUPTED AND RETURNED TO ORD. LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE AND PERFORMED COALESCER BAGS RIGHT AND LEFT PACKS PER MM PERFORMED PACK BURN OUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION. DISASSEMBLY REVEALED HEAVY DAMAGE TO THE HIGH PRESSURE COMPRESSOR (HPC) AS WELL AS THE LOW PRESSURE TURBINES. DAMAGE TO

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LGHTS BETWEEN ROW 16 AND 20 IS INTERMITTENT. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT ROW 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: KEEL BEAM — CRACKED (BS 927)

TUL - FORWARD END OF KEEL BEAM CRACKED. REPAIRED IAW SRM AARD 53-10-00-6, AARD 53-10-00-1. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, LOWER EMERGENCY EXIT SIGN AT RIGHT ENTRY DOOR INOPERATIVE. REPAIRED BROKEN WIRE BEHIND WALL TO RIGHT ENTRY DOOR LOWER EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PASSENGER SEAT ROW 21 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 21. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)