N490AA

Part: RIB — CRACKED (LE SLAT) · airframe 72,737 hrs · 38,171 cycles

LEFT HAND WING NR 4 SLAT RIB CRACKED. INSTALLED DOUBLER REPAIR IAW EA MD80-57-034736.

Part: RIB — CRACKED (LE SLAT) · airframe 72,737 hrs · 38,171 cycles

RIGHT HAND WING NR 4 SLAT RIB CRACKED. INSTALLED DOUBLER REPAIR IAW EA MD80-57-034736.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 71,358 hrs · 37,412 cycles

SAT DURING LANDING GEAR EXTENSION, GREEN NLG DOWN LIGHT DID NOT ILLUMINATE. EMERGENCY DECLARED FLIGHT ACCOMPLISHED GO AROUND & LANDED SAT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR LOCKED PROXIMITY SENSOR D1-32 & CONNECTOR P1-1157. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CSD — OVERSERVICED (RIGHT) · airframe 70,270 hrs · 36,754 cycles

CREW REPORTED, ON CLIMBOUT, RT CONSTANT SPEED DRIVE TEMP HIGH. CREW DISCONNECTED THE CSD. EMERGENCY DECLARED, FLIGHT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RT CSD OVERSERVICED. CONSTANT SPEED DRIVE FLUSHED AND SERVICED. SYS GROUND CHECK NORMAL OPERATION.

Part: WIRE — DAMAGED (CABIN) · airframe 69,383 hrs · 36,244 cycles

AFT AIRSTAIR SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE FOR AFT AIRSTAIR EMERGENCY LIGHTS.

Part: PORTABLE LIGHT — DEFECTIVE (CABIN) · airframe 69,383 hrs · 36,244 cycles

LEFT NUMBER ONE DOOR PORTABLE EMERGENCY LIGHT DIM. REPLACED LEFT NUMBER ONE PORTABLE EMERGEMCY LIGHT. OPS CHECK NORMA.L

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,383 hrs · 36,244 cycles

OVERHEAD EMERGENCY LIGHTS AT ROWS 11 AND 12 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: GENERATOR — MALFUNCTIONED (RIGHT) · airframe 69,355 hrs · 36,229 cycles

DFW - CREW REPORTED EXPERIENCED AC POWER INTERRUPTIONS AND RIGHT CONSTANT SPEED DRIVE OIL PRESSURE LOW LIGHT ILLUMINATED. TRIED TO DISCONNECT RIGHT CSD AND COULD NOT DISCONNECT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT CONSTANT SPEED DRIVE LEAKING. REPLACED GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

LEFT CUSP: CENTER CUSP CRACKED BETWEEN NUMBERS 1 AND 2 SEAT TRACK AT STATION 1250. INSTALLED DOUBLER BETWEEN NUMBERS 1 AND 2 SEAT TRACKS FROM STATIONS 1247 TO 1250 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

LEFT CUSP SHEET FROM STATIONS 1250 TO 1309 CORRODED. INSTALLED LEFT CUSP PER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 69,010 hrs · 36,034 cycles

CRACK INDICATION ON NUMBER 15 SLAT RIB ON NUMBER 5 SLAT LEFT SIDE. REPLACED RIB PER ESO 80117.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

CRACK EXTENDING FROM LIGHTENING HOLE IN LEFT CUSP AT STATION 226. REMOVED DAMAGED LEFT CUSP SHEET STATIONS 218 TO 237. INSTALLED SERVICEABLE LEFT CUSP SHEET FROM STATIONS 218 TO 237 PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,010 hrs · 36,034 cycles

SEAT TRACK NUMBER 6, STATION 1154 CORRODED. ROUTED OUT DAMAGED AREA AND INSTALLED SEAT TRACK PLUG AS PER SRM 53-05-00 FIGURE 4A.

Part: RIB — CRACKED (LE SLAT) · airframe 69,010 hrs · 36,034 cycles

CRACK INDICATION ON NUMBER 15 SLAT RIB ON NUMBER 5 SLAT RIGHT SIDE. INSTALLED NEW SLAT ATTACH FITTING AND LOWER SKIN PER ESO 80177.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

RIGHT CUSP MEMBRANE AT STATION 493 CORRODED. INSTALLED RIGHT CUSP DOUBLER PER AARD 53-2-00-16.

Part: DOUBLER — CRACKED (SERVICE DOOR) · airframe 69,010 hrs · 36,034 cycles

AFT SERVICE DOOR/HOLD OPEN HOOK HOUSING DOUBLER CRACKED. DOUBLER INSTALLED PER SRM 52-05-00 FIGURE 54 AND NEW HOOK HOUSING DRILLED AND INSTALLED PER ESO 80175.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

CABIN HAS A CRACK IN LOWER LEG OF LONGERON 4 LEFT AT STATION 200. INSTALLED LONGERON REPAIR PER AARD 51-00-05-1.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

CORROSION ON DOUBLER BELOW G2 GALLEY FLOOR MOUNT BRACKET STATION 218, 12 INCHES TO RIGHT OF CENTER LINE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 69,010 hrs · 36,034 cycles

CRACK INDICATION AT NUMBER 15 SLAT RIB ON NUMBER 5 SLAT, RIGHT SIDE. REMOVED NUMBER 15 SLAT ATTACH FITTING AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

DENT IN SKIN AT STATION 414 BELOW LONGERON 19 LEFT. INSTALLED INTERNAL DOUBLER, TAPERED SHIMS AND SKIN FILLER PER SRM 53-04-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

TWO CRACKS AT LOWER END OF FLOORBEAM SUPPORT, STATION 927, BELOW SEAT TRACK NUMBER 2. REPLACED SUPPORT PER AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

RIGHT CUSP IS CRACKED FROM STATIONS 1263 TO 1266. CUT OUT DAMAGE AND INSTALLED DOUBLER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

UPPER AFT CORNER OF RIGHT WINDOW PAN CRACKED AT STATION 1098. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

CRACK AT LEFT WINDOW RING PAN AT UPPER AFT CLIP JUST FORWARD OF STATION 1098. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

UPPER AFT CORNER OF RIGHT WINDOW PAN CRACKED AT STATION 1079. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

LOWER FORWARD CORNER OF RIGHT WINDOW PAN CRACKED, STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

LEFT WINDOW PAN CRACKED BETWEEN STATIONS 1041 TO 1060, LOWER FORWARD CORNER. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

CRACK IN LEFT WINDOW RING PAN AT LOWER FORWARD CLIP JUST AFT OF STATION 1060. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

UPPER AFT CORNER OF RIGHT WINDOW PAN CRACKED AT STATION 1193. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

LOWER FORWARD CORNER OF RIGHT WINDOW PAN CRACKED, STATION 1022. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

LEFT WINDOW PAN CRACKED BETWEEN STATIONS 864 TO 845, LOWER FORWARD CORNER. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 69,010 hrs · 36,034 cycles

SCRATCHES/GOUGES IN FUSELAGE SKIN BETWEEN LONGERONS 29 AND 28 RIGHT AT STATION 486. BLENDED GOUGES AND INSTALLED INTERNAL DOUBLER PER SRM 53-04-02

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 66,999 hrs · 34,893 cycles

DFW - CREW REPORTED DURING DESCENT NOSE LANDING GEAR INDICATION SHOWED NOSE GEAR UNSAFE. CYCLED GEAR AND STILL SHOWED RED. ABORTED APPROACH AND ACCOMPLISHED FLYBY TO VERIFY GEAR DOWN. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GEAR INDICATION BULBS THAT WERE BURNED OUT. REPLACED PROXIMITY BOX AS A PRECAUTION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,212 hrs · 31,234 cycles

MID AISLE BATTERY PACK LOW OUTPUT. REPLACED BATTERY PACK IAW MM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,212 hrs · 31,234 cycles

MID AISLE BATTERY PACK HAS LOW OUTPUT. REPLACED BATTERY PACK IN MID AISLE UNDER IAW 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,212 hrs · 31,234 cycles

MID AISLE BATTERY PACK LOW OUTPUT. REPLACED BATTERY PACK IN MID AISLE UNDER MM 33-60-98-4.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,212 hrs · 31,234 cycles

MID AISLE BATTERY PACK LOW OUTPUT. REPLACED BATTERY PACK AT MID AISLE UNDER IAW 33-60-98-4.

Part: SPLICE — DAMAGED (CABIN) · airframe 59,999 hrs · 31,105 cycles

MCI - EMERGENCY LIGHT INOPERATIVE IN REAR AIRSTAIR AREA. REPLACED WIRING SPLICE FOR EMERGENCY LIGHT IN REAR AIRSTAIR AREA.

Part: A/C PACK — SMOKE

MSP INFLIGHT T1037/23JAN - VERY LIGHT SMOKE STARTED TO FLOW THROUGH CABIN. SHUT DOWN RIGHT AIR CONDITIONING PACK AND SMOKE DISSIPATED. CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHTS IN CEILING AT ROWS 29 TO 31 INOPERATIVE. REPLACED BATTERY PACK AT ROW 29 FOR INOPERATIVE EMERGENCY LIGHTS IN CEILING AT ROWS 29 TO 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - CEILING EMERGENCY LIGHTS AT ROWS 13 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT ROW 13 FOR CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - BOTH FORWARD OVERWING EMERGENCY ESCAPE HATCHES EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR BOTH FORWARD OVERWING EMERGENCY ESCAPE HATCHES EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE FUEL)

ABOUT 2000 FT ABOVE GROUND LEVEL ON FINAL APPROACH, GOT LT FUEL INLET LOW LIGHT. SHORTLY AFTER THAT NR 1 ENGINE FAILED. REPLACED LT WING TANK PROBES NUMBER 5 THROUGH 12, LT WING TANK COMPENSATOR, RT WING TANK PROBES NUMBERS 6, 5, 9, 10, AND 11 AND RT WING TANK COMPENSATOR. PERFORMED BIOBORE TO ALL FUEL TANKS AND REPLACED LT ENGINE FUEL CONTROL AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - OVERHEAD EMERGENCY EXIT LIGHTS AT SEATS 28D TO 31D INOPERATIVE. RECHARGED THE EMERGENCY LIGHTS SYSTEM IN THE ARM POSITION FOR THE OVERHEAD EMERGENCY EXIT LIGHTS AT SEATS 28D TO 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: OIL CAP — UNSECURE (APU)

AUS - ON ROTATION BURNING OIL SMELL IN COCKPIT. AT ABOUT 2000 FEET FLIGHT ATTENDANT CALLED TO REPORT SMOKE IN CABIN THAT ALSO SMELLED LIKE BURNING OIL. RETURNED TO AUS AND LANDED WITHOUT INCIDENT. PLACARD APU FOR OIL LEAK. REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT FERRY TO DFW. FOUND OIL CAP NOT SECURE. CLEANED RESIDUE OIL FROM APU AND RAN APU WITH PACKS. NO SMOKE OR OIL SMELL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT SEAT 14D OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 14D OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ABOVE DOORS INOPERATIVE. REPLACED BATTERY PACK B5-105, RESECURED WIRE L799B16N TO TERMINAL 3, AND CORRECTED WIRE CONNECTION L1229F18 FROM TERMINAL 3 TO TERMINAL 5 FOR LEFT HAND AND RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ABOVE DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL MODULE — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT SIGN AT AFT LEFT HAND SERVICE DOOR AT AL2-7 FORWARD OF DOOR NEAR FLOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK CONTROL MODULE AL2-7 AT AFT LEFT HAND SERVICE DOOR FORWARD OF DOOR NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT STATION 1154 INOPERATIVE. FOUND PLASTIC BACK SHELL FOR PLUG FOR BATTERY PACK CONTROL MODULE AB5-4 AT STATION 1154 BROKEN. REPLACED PLASTIC BACK SHELL FOR PLUG FOR EMERGENCY LIGHT BATTERY PACK CONTROL MODULE AB5-4 AT STATION 1154. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT EMERGENCY PATH LIGHT AT ROW 8 INOPERATIVE. REPLACED SOCKET, BULBS, AND LENSE FOR SEAT EMERGENCY PATH LIGHT AT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - RIGHT AND LEFT HAND EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — CORRODED (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN TAIL COMPARTMENT VERY DIM. CLEANED EMERGENCY EXIT LIGHT BATTTERIES FOR TAIL COMPARTMENT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CLAMP — LOOSE (A/C BAY)

LAS - FLT 870 - EN ROUTE LAS-DFW, ON TAKEOFF ABOUT TWO MINUTES INTO FLIGHT THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED, ACCOMPLISHED PROCEDURES AND LIGHT EXTINGUISHED, LIGHT THEN ILLUMINATED ABOUT 30 SECONDS LATER AND FLIGHT ABORTED, RETURNED AND LANDED LAS WITHOUT INCIDENT. READJUSTED THE INBOARD LEFT PRIMARY HEAT EXCHANGER CLAMP, PERFORMED LEAK CHECK WITH THE APU AND THEN WITH BOTH ENGINES AT IDLE. REVEALED NO LEAKS, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BULB — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED LIGHT FROM 3EE-19D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BULB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, FORWARD SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING CONTROL MODULE CONNECTOR BROKEN. REPAIRED FORWARD SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING CONTROL MODUEL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (EMERGENCY LIGHT)

BOS - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT FROM ROW 1-9 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT LIGHTS AT TAIL CONE AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SHEAR TIE — CRACKED (FUSELAGE)

TUL - FOUND CRACK FS 1437. REPLACED SHEAR TIE PER SRM 53-05-00. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK, FS 1380. STOP DRILLED CRACK WITH EXTERNAL DOUBLER PATCH APPLIED PER SRM 51-01-00. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

TUL - FOUND CRACK, FS 1380. STOP DRILLED WITH EXTERNAL DOUBLER PATCH PER SRM 51-01-00. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT SEATS 27, 28, AND 30, INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DIRTY (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 13-16 DIM. CLEANED EMERGENCY EXIT LIGHT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

TUL - FOUND EMERGENCY EXIT LIGHTS IN CEILING AT STATION 1298 AND STATION 1336 INOPERATIVE. INSTALLED SERVICEABLE BATTERY PACK B5-27 AT STATION 1322R PER AMM 33-53-00-4, WORK ACCOMPLISHED ON E584135314. (M)

Part: LIGHT — DEFECTIVE (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY HANDLE RELEASE EXIT LIGHT DIM. REPLACED TAIL CONE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8E TOO BRIGHT. REPLACED EMERGENCY EXIT IGHT AT SEAT 8E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OIL FILTER — LEAKING (NR 2 ENGINE)

EWR - FLT 717 - EN ROUTE LGA-DFW, AT AN ALTITUDE OF 15,000 FEET RIGHT SIDE ENGIEN OIL QUANTITY WENT TO ZERO. RIGHT SIDE ENGINE SHUTDOWN. DIVERTED EWR AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE. REPLACED OIL FILTER, OIL FILTER COVER AND PACKING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 1, STATION 1280. REMOVED CORRODED SECTION OF NR 1 SEAT TRACK, INSTALLED NEW SECTION OF NR 1 SEAT TRACK 1157 TO 1309 PER SRM 51-01. (M)

Part: FRAME — DAMAGED (FUSELAGE)

TUL - FOUND T-FITTING AT BELL FRAME CUT DAMAGED AT BS 636. REMOVED T-FITTING AND REPLACED WITH NEW SRM 51-01. (M)

Part: SPLICE — CRACKED (LONGERON)

TUL - FOUND LONGERON 16 SPLICE CRACKED ABOUT STATION 1427. INSTALLED NEW SPLICE 51-10-1. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON NR 3 SEAT TRACK OUTBOARD FLANGE AROUND SEVERAL FASTENER HOLES STATION 1153 THE 1309. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-10-3 AND ESO80559 DATED 7/26/2000. (M)

Part: SEAT TRACK — CORRODED (GALLEY)

TUL - FOUND GALLEY TIE DOWN SEAT TRACK CORRODED NR 5 TRACK. INSTALLED NEW SECTION NR 5 SEAT/GALLEY TIE DOWN TRACK AARD 51-60 SRM 53-05. (M)

Part: WEB — CORRODED (CABIN)

TUL - FOUND CORROSION ON CUSP AT STATION 1175 JUST INBOARD OF SEAT TRACK NR 1. REMOVED CORROSION BY CUTTING OUT CORRODED AREA OF CUSP. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: STRUCTURE — CORRODED (SUBFLOOR)

TUL - FOUND CORROSION OF SUBFLOOR (CUSP) STATION 209 RIGHT 10 INCHES AFT OF SERVICE DOOR. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - DENT/GOUGE AT UPPER AFT CORNER OF FORWARD CARGO DOOR OPENING DENT OUT OF LIMITS PER SRM 53-04, TABLE C FIG 38, SHEET 12, CONDITION C, D=.875 WIDTH, X=APPROX .156 DEEP. TRIMMED OUT GOUGE PER AARD 53-30-00-6, COLD WORKED DENT AND INSTALLED DOUBLER PER ESO 80559 DATED 7/21/00. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NUMEROUS AREAS OF CORROSION ON NR 2 SEAT TRACK STATION 1193 TO 1235. REMOVED AND REPLACED NR 2 SEAT TRACK WITH NEW STATION 1184 TO STATION 1309 PER SRM 53-05. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON AFT CARGO DOOR JAMB FROM STATION 1158 TO STATION 1209. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 80559 DATED 7/17/2000. (M)

Part: STRUCTURE — DENTED (FUSELAGE)

TUL - FOUND MINOR 2 INCH CIRCULAR DENT AND SURFACE SCATCH 2 FT A HEAD OF AND 1 FT BELOW LEFT PRESSURE RELIEF VALVES. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 20. (M)

Part: FITTING — CORRODED (SUBFLOOR)

TUL - FOUND CORROSION ON SUBFLOOR UNDER G-2 FITTING STATION 218 AND RBL 11. INSTALLED DOUBLER AFTER CUTTING OUT CORROSION DAMAGED PER SRM 51-10-3 AND SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SEVERAL AREAS OF CORROSION ON LEFT CUSP STATION 1022 TO STATION 1079. REMOVED CUSP REPLACED WITH NEW PART PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP, SEVERAL AREAS, STATION 389-408, 408-427, 427-446, 446-465, 465-484, 484 TO 503. INSTALLED NEW CUSP SHEET STATION 389 TO 503 SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORRODED AND PITTED STATION 860. ROUTED OUT DAMAGED AREA. TREATED AND PRIMED AREA ROUTED. INSTALLED SEAT TRACK PLUG IAW SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND SEAT TRACK NR 6 CORRODED AND PITTED STATION 516. ROUTED OUT DAMAGED AREA. TREATED AND PRIMED ROUTED AREA. INSTALLED TRACK PLUG IAW SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 6 SEAT TRACK CORRODED/PITTED STATION 1180. REMOVED DAMAGE AND INSTALLED SEAT TRACK PLUG SEAT TRACK NR 6 STATION 1180 PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 4 SEAT TRACK CORRODED AND PITTED AT STATION 237. ROUTED OUT DAMAGED AREA. TREATED AND PRIMED ROUTED AREA. INSTALLED SEAT TRACK PLUG IAW SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND SEAT TRACK NR 6 CORRODED AND PITTED AT STATION 486. ROUTED OUT DAMAGED AREA. TREATED AND PRIMED AREA ROUTED. INSTALLED SEAT TRACK PLUG IAW SRM 53-05 FIG A. (M)

Part: COALESCER — CONTAMINATED (ACM BAYS)

AMA - FLT 1677 - EN ROUTE DFW/OAK - DURING CRUISE, ELECTRICAL TYPE ODOR NOTED IN CABIN. AIRCRAFT DIVERTED TO AMA AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. REPLACED ALL COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN, OPERATING ALL PACKS WITH NO ODOR NOTED. AIRCRAFT FCF/MAINTENANCE FERRY AMA/DFW WITH NO DEFECTS OR ODOR NOTED. (M)

Part: SILL — CORRODED (CARGO DOOR)

TUL - FOUND CORROSION ON CARGO DOOR LOWER SILL. REPAIRED PER ESO 80559 DATED 9-18-96. (M)