N7520A

Part: CYLINDER — CORRODED (RT MLG) · airframe 72,039 hrs · 38,149 cycles

AIRCRAFT WAS GNDED. FOUND CORROSION ON RT MLG STRUT CYLINDER WHILE REMOVING GEAR INSPECTION PATCH. ACCOMPLISHED STEP B THROUGH STEP H OF AARD 32-10-00-4 IAW EA 256707 FOR TIME LIMITED REPAIR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,015 hrs · 38,132 cycles

MOD VISIT 27, FLIGHT DECK EMER LIGHTS FOUND INOPERATIVE. R & R BATTERY PACK IAW AMM 33-53-00.

Part: ACCUMULATOR — FAULTY (THRUST REVERSER) · airframe 70,476 hrs · 37,197 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT, RT THRUST REVERSER ACCUMULATOR LOW PRESS LIGHT ILLUMINATED. RAN QRH, LIGHT REMAINED ON. LIGHT EXTINGUISHED ON REVERSER EXTENSION. R & R RT THRUST REVERSER ACCUMULATOR IAW AMM 78-31-01. PERFORMED LEAK CHECK. SYS CHECKED NORMAL.

Part: SKIN — CRACKED (BS 1380) · airframe 70,239 hrs · 37,064 cycles

FUSELAGE SKIN CRACKED AT STATION 1380 L14R. INSTALLED DOUBLER REPAIR IAW SRM 53-01-00-001 & SRM 53-30-00-02.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 70,239 hrs · 37,064 cycles

MID CARGO DOOR, THIRD FROM BOTTOM FWD STOP PAD FITTING IS CRACKED. R & R TOP PAD FITTING IAW AARD 51-00-05-1 & DWG 5910141.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,238 hrs · 36,478 cycles

AFT EMER PATH LIGHTING FAILED CHECK. R & R AFT BATTERY PACK.

Part: OVERHEAT SENSOR — FAULTY (AC BAY) · airframe 68,743 hrs · 36,160 cycles

TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMB OUT. FOLLOWED THE QRH PROCEDURE & THE LIGHT EXTINGUISHED. EMER DECLARED FLIGHT RETURNED. ACFT REMOVED FROM SERVICE. REPLACED LT & RT TAIL COMPARTMENT OVERHEAT SENSORS & PERI SEALS.

Part: WEB — DAMAGED (NLG WW) · airframe 66,926 hrs · 35,090 cycles

RT NLG WW WEB DAMAGED FROM CONTACT WITH STEERING ACT. INSTALLED REPAIR DOUBLER IAW SRM 53-05-00 FIGURE 36 & EA MD80-53-033037.

Part: FITTING — WORN (LE SLAT) · airframe 66,924 hrs · 35,088 cycles

RT HAND WING NR 12 SLAT TRACK KNUCKLE WORN. INSTALLED NEW SERVICEABLE KNUCKLE AT RT HAND NR 12 SLAT TRACK.

Part: FITTING — WORN (LE SLAT) · airframe 66,924 hrs · 35,088 cycles

RT HAND NR 4 SLAT OTBD END KNUCKLE WORN. INSTALLED NEW SERVICEABLE RT HAND NR 4 SLAT OTBD END KNUCKLE.

Part: FORMER — CRACKED (LE SLAT) · airframe 66,924 hrs · 35,088 cycles

RT HAND LE SLAT, NR 4 SLAT TRACK INBD FORMER CRACKED. INSTALLED REPAIR DOUBLER IAW EA MD80-57-032663.

Part: FORMER — CRACKED (LE SLAT) · airframe 66,924 hrs · 35,088 cycles

LT HAND LE NR 4 SLAT TRACK INBD FORMER CRACKED. ACCOMPLISHED DOUBLER REPAIR IAW EA MD80-57-032663.

Part: RIB — WORN (LT WING) · airframe 66,924 hrs · 35,088 cycles

LT HAND NR 15 SLAT TRACK OTBD RIB CASTING WORN OUT. INSTALLED NEW SERVICEABLE RIB CASTING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

AFT ACCESS CANT FRAME 1485 RT HAS CRACK OTBD OF STAIR ACTUATOR LOWER MOUNT. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-33.

Part: FRAME — WORN (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

WEAR TO FWD SIDE 1361 FRAME AT LONGERON 2 RT. INSTALLED DOUBLER IAW SRM 51-70-02 PAGES 2 & 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CORROSION AROUND SPLICE FASTENER FROM STATIONS 797 TO 1031. PERFORMED SEAT TRACK SPLICE REPAIR IAW SRM 53-05-00 FIGURE 4H.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

FIRST OFFICERS, AFT OTBD SEAT TRACK HAS CORROSION ON FWD END OF ASSEMBLY. REMOVED FIRST OFFICERS AFT OTBD SEAT TRACK ASSEMBLY & INSTALLED A SERVICEABLE SEAT TRACK ASSEMBLY.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CRACK IN RT HAND CUSP MEMBRANE AT STATION 814, OTBD NR 6 SEAT TRACK. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16, SRM 53-14-03, FIGURE 10, SHEET 1 & AA DRAWING FDK3239.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON RT HAND CUSP AT STATION 398, OTBD NR 6 SEAT TRACK. INSTALLED DOUBLER FROM STATIONS 396 TO 400 IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

AFT CARGO HAS CORROSION ON CUSP IN RT HAND TUNNEL AT STATION 1300. INSTALLED NEW RT HAND CUSP SHEET FROM STATIONS 1250 TO 1309 IAW AARD 51-00-05-1 & DRAWING 9930612.

Part: PAN — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CRACK AT RT HAND WINDOW PAN, UPPER FWD CLIP AT STATION 886. INSTALLED REPAIR ANGLE ON UPPER FWD CLIP OF RT HAND WINDOW PAN AT STATION 886 IAW AARD 53-10-00-25.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CRACK IN LT HAND CUSP AT STATION 225 OTBD OF NR 1 SEAT TRACK. R & R CUSP SHEET IAW AARD 53-20-00-16 & SRM 51-30.

Part: DIAPHRAGM — DENTED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

DENT & TOOLING MARK ON COCKPIT SUBFLOOR STATION 140 & RBL 39, JUST FWD OF FLOORBOARD SUPPORT. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

ENTRY DOOR SURROUND, WEB TEE CRACKED AT STATION 210 & LONGERON 15 LT. INSTALLED DOUBLER REPAIR ON WEB TEE AT STATION 210 IAW AARD 53-10-00-11.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CRACK IN LT HAND CUSP AT STATION 1012 OTBD OF NR 1 SEAT TRACK. INSTALLED LT HAND CUSP SHEET FROM STATIONS 1006 TO 1012 IAW AARD 51-00-05-1 & 53-20-00-16 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION FROM STATIONS 365 TO 369 OTBD OF NR 6 SEAT TRACK. INSTALLED PLUG & CHANNEL IAW AARD 53-20-00-10 SRM 53-05-00 FIGURE 4A SHEET 1.

Part: CUSP WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CRACK IN RT HAND CUSP AT STATION 885 BETWEEN INBD FASTENER HOLES FOR NR 6 SEAT TRACK. INSTALLED DOUBLER AT RT HAND STATION 885 IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CRACK AT LT HAND WINDOW PAN, LOWER AFT CLIP AT STATION 905. INSTALLED NEW CLIP ON LT HAND WINDOW PAN, LOWER AFT CLIP, AT STATION 905 IAW AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

LT HAND CUSP CORRODED FROM STATIONS 958 TO 961. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CRACK AT LT HAND WINDOW PAN, UPPER FWD CLIP AT STATION 886. INSTALLED NEW UPPER FWD CLIP ON LT HAND WINDOW PAN AT STATION 886 IAW AARD 53-10-00-25.

Part: PAN — GOUGED (SERVICE DOOR) · airframe 66,924 hrs · 35,088 cycles

FWD SERVICE DOOR, LOWER PAN AREA HAS GOUGE IN PAN FROM SCREW AT CORE BOLT. INSTALLED DOUBLER IAW SRM 52-01-00 FIGURE 2 SHEET 3 & EA COMP-52032744 REVISION B.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

AFT CARGO, CORROSION ON RT HAND TIE DOWN TRACKS AROUND FASTENER HOLES FROM STATIONS 1155 TO 1007. INSTALLED RT HAND TIE DOWN IAW SRM 51-30-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON RT HAND TIE AFT DOWN TRACK IN AFT CARGO FROM STATIONS 1212 TO 1322. INSTALLED NEW TRACK IAW AARD 51-00-05-1 & SRM 51-30-01.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON G 2 GALLEY MOUNT FITTING. INSTALLED G 2 GALLEY MOUNT FITTING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON AFT LOWER LEG OF SHEAR TIE AT STATION 1136 BETWEEN LONGERONS 28 & 27 RT. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA MD80-53-032852.

Part: FRAME — WORN (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

DEEP WEAR ON THE FWD SIDE OF THE FUSELAGE FRAME AT STATION 1361 & LONGERON 2 RT. INSTALLED DOUBLER IAW SRM 51-70-02 PAGES 2 & 4.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

GOUGE IN UPPER FLANGE OF NR 1 SEAT TRACK AT STATION 1121. INSTALLED SEAT TRACK PLUG IAW SRM 53-05-00 FIGURE 4A.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON SUBFLOOR FROM STATIONS 185 TO 200 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON G 2 GALLEY MOUNT. INSTALLED G 2 INBD FWD GALLEY MOUNT.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CABIN VAULT DOOR LT HAND JAMB, STIFFENER IS CRACKED AT LOWER FWD FASTENER 19 INCHES ABOVE FLOOR. INSTALLED SERVICEABLE STIFFENER AT LT HAND VAULT DOOR JAMB 19 INCHES ABOVE FLOOR.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION ON AFT INBD GALLEY MOUNT FITTING. INSTALLED GALLEY MOUNT FITTING.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,924 hrs · 35,088 cycles

CORROSION UNDER G1 GALLEY DRAIN PAN AT STATION 148 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

CABIN VAULT DOOR RT HAND JAMB, STIFFENER IS CRACKED AT LOWER FWD FASTENER 17 INCHES ABOVE FLOOR. INSTALLED SERVICEABLE STIFFENER AT RT HAND VAULT DOOR JAMB 17 INCHES ABOVE FLOOR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

GOUGE IN UPPER FLANGE OF NR 1 SEAT TRACK AT STATION 1121. INSTALLED SEAT TRACK PLUG IAW SRM 53-05-00 FIGURE 4A.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 66,924 hrs · 35,088 cycles

FASTENERS ARE RUSTY ON VERTICAL LEG OF LOWER DOOR BEAM BETWEEN STATIONS 1155 TO 1212. REPLACED 28 FASTENERS ON INBD ROW LOWER LEG OF DOOR BEAM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,122 hrs · 34,617 cycles

AFT TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-28 FOR AFT TAIL CONE EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: MODULE — INOPERATIVE (ZONE 100) · airframe 64,737 hrs · 33,830 cycles

DFW - CREW REPORTED INTERMITTANT FAULTS: TAS INPUT FAIL, HDG INPUT FAIL, ALT INPUT FAIL SYNCHRO INPUT FAIL. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NPU CONFIGURATION MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW O2) · airframe 64,045 hrs · 33,445 cycles

BNA - INFLIGHT BWI-DFW. CREW REPORTED FLIGHT DECK CREW O2 LOW PRESSURE. EMERGENCY DECLARED FLIGHT DIVERTED BNA LANDED WITHOUT INCIDENT. REPLACED FLIGHT DECK CREW O2 BOTTLE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SEAL — DEFECTIVE (NLG STRUT) · airframe 63,596 hrs · 33,173 cycles

MTY - CREW REPORTED NOSE LANDING GEAR WOULD NOT RETRACT. NOSE GEAR RED LIGHT REMAINS ON WITH GEAR HANDLE UP / RETRACTED. EMERGENCY DECLARED FLIGHT RETURNED MTY LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR SHOCK STRUT SEAL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — OUT OF ADJUST (CABIN) · airframe 62,595 hrs · 32,597 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 6 INOPERATIVE. RE-ADJUSTED BATTERY PACK, OPS CHECKS NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 62,595 hrs · 32,597 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.

Part: BATTERY PACK — OUT OF ADJUST (CABIN) · airframe 62,595 hrs · 32,597 cycles

LEFT FORWARD AND AFT OVERWING DOOR UPPER EXIT SIGNS DIM. RE-ADJUSTED BATTERY PACK, OPS CHECK NORMAL.

Part: CONTROL BOX — INOPERATIVE (ANTI-SKID SYS) · airframe 61,234 hrs · 31,830 cycles

ORD - CREW REPORTED LEFT AND RIGHT INBOARD AND OUTBOARD ANTI SKID LIGHTS ILLUMINATED WITH LANDING GEAR EXTENSION. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ANTI-SKID CONTROL BOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,783 hrs · 31,574 cycles

AIRCRAFT DAMAGED BY ELECTRICAL CART. A 12 INCH HOLE IN FUSELAGE SKIN, FORWARD OF LEFT WING ROOT STATIONS 577 TO 597. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-04-00, 12C AND EA MD80-53-018160.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 59,510 hrs · 30,894 cycles

DFW - CREW REPORTED LOSS OF RIGHT HYDRAULIC PRESSURE AND FLUID ON DESCENT. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK ON THE RIGHT ENGINE HYDRAULIC PRESSURE LINE THAT GOES INTO THE FILTER HOUSING. REPLACED LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

AFT ACCESSORY WEB IS CRACKED AT TAIL CONE ALIGNMENT PIN, JUST ABOVE LOWER LEFT HAND TAIL CONE LATCH. REPAIRED UNDER SRM 51-70-05 FIGURE 1 SHEET 3.

Part: CAP — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

CAP IS CRACKED AT VERTICAL FLANGE STATION 846 BELOW NUMBER 5 SEAT TRACK. REPAIRED UNDER EA MD80 57-007195.

Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

CUSP SUPPORT ANGLE BRACKET AT STATION 824 DAMAGED DURING REMOVAL. REPAIRED UNDER EA MD80 53-007229.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

AFT CARGO DOORWAY FORWARD INBOARD CORNER FITTING IS CORRODED BEYOND LIMITS. REPLACED FITTING UNDER AARD 51-00-00-012.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

SEAT TRACK NUMBER 2 STATION 1198-1201 OUT OF LIMITS DUE TO CORROSION. REPLACED SEAT TRACK UNDER SRM 53-05 FIG 4F.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

CRACK AT TOP OF VERTICAL STIFFENER TOP CENTER OF AFT BULKHEAD. STOP DRILLED CRACK AND INSTALLED DOUBLER UNDER AARD 53-10-00-15.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

CUSP AT STATION 815 IS CRACKED. REPAIRED UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

RIGHT CUSP AT STATION 469 CORROSION IS OUT OF LIMITS. REPAIRED UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

LEFT CUSP STATION 527 CORROSION. INSTALLED REPAIR UNDER AARD 53-20-00-16.

Part: CAP — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

STATION 826 RIGHT UPPER SKIN CAP CRACKED AT FORWARD END OF INTERCOSTAL BELOW NUMBER 5 SEAT TRACK. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE UNDER EA MD80 57-007195 DATED 8/20/09.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

CORROSION ON SUBFLOOR AT RIGHT STATION 218 UNDERNEATH GALLEY MOUNT FITTING, OUT OF LIMITS. INSTALLED REPAIR DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

CORROSION ON CUSP BELOW AFT SERVICE DOOR FORWARD GIRT BAR FITTING. INSTALLED DOUBLER UNDER AARD 53-20-00-16.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

TEMPORARY DOUBLER INSTALLED ON FUSELAGE STAION 522. INSTALLED PERMANENT REPAIR UNDER SRM 53-04 FIG 12B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

CUSP LEFT STATION CORRODED OUT OF LIMITS. INSTALLED REPAIR DOUBLER UNDER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

CUSP IS CRACKED BETWEEN LIGHTENING HOLES RIGHT STATION 220-222. REPLACED CUSP UNDER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,945 hrs · 28,938 cycles

LEFT CUSP CORRODED OUT OF LIMITS AT STATION 670. INSTALLED REPAIR DOUBLER UNDER AARD 53-20-00-16.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 55,945 hrs · 28,938 cycles

RIGHT WHEEL WELL UPPER PRESSURE DECK IS CRACKED AT FUEL SHROUD SUPPORT AT STATION 997. REPAIRED UNDER SRM 53-01-00 FIG 2.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

WINDOW PAN CRACKED AT STATION 1041. INSTALLED REPAIR ANGLE UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

WINDOW PAN CRACKED AT STATION 1098. INSTALLED REPAIR ANGLE UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

WINDOW PAN CRACKED AT STATION 826. INSTALLED REPAIR ANGLE UNDER AARD 53-10-00-25.

Part: PAN — CRACKED (FUSELAGE) · airframe 55,945 hrs · 28,938 cycles

FORWARD LOWER WINDOW PAN TAB CRACKED RIGHT SIDE AT STATION 826. INSTALLED REPAIR ANGLE UNDER AARD 53-10-00-25.

Part: BEARING — FAILED (NLG) · airframe 54,124 hrs

ORD INFLIGHT - CREW REPORTED UNABLE TO RETRACT NOSE GEAR. PLACED GEAR DOWN AND GREEN LOCKED LIGHT ILLUMINATED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED TURNING TUBE THRUST BEARING AND REPACKED NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 54,097 hrs

LGA - EMERGENCY LIGHT AT SEAT ROWS 1 TO 20 INOPERATIVE. REPAIRED BROKEN WIRE UNDER SEAT 1DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DIRTY (CABIN) · airframe 52,860 hrs

LGA - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. CLEANED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,509 hrs · 27,065 cycles

TUL BATTERY PACK AT OVERHEAD SEAT 25DEF FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,509 hrs · 27,065 cycles

TUL BATTERY PACK AT OVERHEAD SEAT 29DEF FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,891 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,891 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 22 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 22. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOOK AND LOOP — INOPERATIVE (L2 DOOR SLIDE)

MSP - EMERGENCY DOOR SLIDE AT LEFT NUMBER TWO DOOR GIRT BAR HOOK AND LOOP INOPERATIVE. REPLACED EMERGENCY DOOR SLIDE AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DAMAGED

MSP - EMERGENCY SLIDE GIRT BAR VELCRO INOPERATIVE AND MANUAL DEPLOY HANDLE RING CORRODED AT RIGHT NUMBER ONE DOOR. REPLACED EMERGENCY SLIDE AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOOK AND LOOP — INOPERATIVE (L2 DOOR)

ORD - L2 DOOR SLIDE GIRT BAR HOOK AND LOOP STRIP IS DIRTY AND WILL NOT HOLD. REPLACED LEFT NUMBER TWO DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL VALVE — STUCK (A/C BAY)

ORD - AFTER TAKEOFF SAW AND SMELLED SMOKE AND FUMES IN COCPIT AND CABIN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND LEFT HAND PACK TEMPERATURE VALVE STUCK OPEN. REPLACED LEFT TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - CEILING EMERGENCY LIGHTS AT ROWS 17 TO 23 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 17 TO 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5107 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY LIGHT ON LOWER WALL ACROSS FROM FORWARD LAVATORY IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON LOWER WALL ACROSS FROM FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY PACK AT B5-28 FOR EMERGENCY LIGHTS IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW FORWARD SEAT MOUNTED EMERGENCY LIGHTS AT 27D INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: DUCT — DAMAGED (A/C BAY)

SLC - FLT 360 - EN ROUTE SLC-DFW, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED SOON AFTER TAKEOFF ROTATION. ANTI-ICE NOT ON. CLOSED CROSSFEED AND SE PACK TO HIGH PRESSURE BLEED OFF, BUT LIGHT REMAINED ILLUMINATED. FLIGHT ATTENDANTS REPORTED BURNING SMELL. RETURNED SLC, WITH POWER REDUCED TO IDLE, TEMPERATURE HIGH LIGHT EXTINGUISHED AND PRESSURIZATION FLOW LIGHT ILLUMINATED. LANDED WITHOUT INCIDENT. REPLACED ELBOW DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HORN — DAMAGED (L/E SLAT)

TUL - FOUND NR 0 RIGHT INBOARD SLAT HORN HAS DAMAGE ON INBOARD SIDE LOWER. STRAIGHTENED DENTED AREA PER ESO 80559. REFORMED AND DYE CHECKED. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

TUL - FOUND SEAT TRACK NR 6 DAMAGED AT 730. REPLACED SEAT TRACK NR 6 FROM STATION 718 TO 793 PER SRM 53-05 FIG 4F. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

TUL - FOUND MOST OUTBOARD SEAT TRACK ON LEFT SIDE OF A/C AT STATION 250 IS DAMAGED OUT ON LOWER SIDE. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STATION 218 TO STATION 265 AS PER SRM 53-05 SEAT TRACK SPLICE. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP DAMAGED AROUND RIVET HEAD, CRACKED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-00-00-02. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND .5 INCH HOLE IN CUSP, OUTBOARD OF SEAT TRACK NR 5 STATION 736. REMOVED DAMAGE, DYE CHECKED, NO CRACKS. INSTALLED DOUBLER REPAIR PER AARD 53-00-00-02 AND SRM 53-01 FIG. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LEFT CUSP SEVERAL PLACES BETWEEN STATION 693 AND 712. CUTOUT CORRODED AREA AND INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01. ALSO, INCORPORATED ESO 80559. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

NR 4 SEAT TRACK, STATION 236, CORRODED. REMOVED CORRODED SEAT TRACK. INSTALLED NEW TRACK SECTION FROM STATION 200 TO 265 PER SRM 53-05 FIG 4B. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP OF SEAT TRACK STATION 1175 TO 1179. INSTALLED NEW SEAT TRACK FROM STATION 1173 TO 1307 SRM 53-05. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN SKIN AT STATION 349 LONGERON 29L. REMOVED DAMAGED AREA OF FUSELAGE SKIN AND INSTALLED REPAIR PER SRM 53-04 FIG 38 SHEET 24. (M)

Part: SEAT TRACK — WORN (FUSELAGE)

TUL - FOUND WORN AREA ON SEAT TRACK NR 5 AT STATION 200. REPLACED SECTION OF NR 5 SEAT TRACK FROM STATION 200 TO 246 AS PER SRM 53-05. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND FLOOR SUPPORT CORRODED, STATION 148, RBL 6 INCHES. REMOVED AND REPLACED FLOORBOARD SUPPORT WITH NEW SUPPORT SRM 51-01. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND WINDOW PANEL CRACKED AT TOP AFT CORNER FASTENER HOLE STATION 1022 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND STATION 1260-1309, OUTBOARD SEAT TRACK NR 2 HAS CORROSION AROUND TOPS BOTTOM OF BOLT ACCESS HOLES. HEAVY CORROSION OF TOP OF SEAT TRACK STATION 1299 TO 1309. INSTALLED NEW SEAT TRACK SPLICE FOR NR 2 TRACK, STATION 1260-1309 PER SRM 53-05-00. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DEEP DENT IN FUSELAGE SKIN APPROX STATION 305 ABOVE LONGERON 24L. REMOVED DAMAGED PART OF SKIN. INSTALLED DOUBLER PER SRM 53-04-00. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION STATION 1155 TO 1212. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION SEAT TRACK NR 3 STATION 1165-1307. REMOVED AND INSTALLED NEW SEAT TRACK STATION 1165-1307 SRM 53-05. (M)

Part: WEB — DENTED (FUSELAGE)

TUL - FOUND CUSP DENTED STATION 1077 LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - WINDOW PANEL CRACKED TOP FORWARD CORNER LEFT WINDOW PANEL STATION 946. STOP DRILLED AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND LOWER FLANGE OF FLOORBEAM WORN STATION 389 RBL 1. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-21. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP HAS CORROSION STATION 598-617. REMOVED CORRODED AREA THAT WAS BEYOND LIMITS BY CUTTING OUT. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: GEAR HANDLE — LACK OF LUBE (COCKPIT)

DFW - FLT 0899 - DURING APPROACH AFTER GEAR EXTENSION, ONLY THREE RED LIGHTS ILLUMINATED. ACCOMPLISHED EMERGENCY EXTENSION CHECKLIST, GAVE THREE GREEN LIGHTS AND GEAR DOOR LIGHT EXTINGUISHED WHEN HANDLE WAS STOWED. LANDED DFW WITHOUT FURTHER INCIDENT. LUBRICATED GEAR HANDLE AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: VALVE — DEFECTIVE (RT ACM)

IAH - FLT 616 - ON APPROACH TO IAH FROM DFW, SMOKE DETECTED IN CABIN. RIGHT AIR CONDITIONING PACK WAS SHUT DOWN AND PULLED J-7 CIRCUIT BREAKER. LANDED IAH WITHOUT INCIDENT. REPLACED RIGHT AIR CONDITIONING PACK TEMPERATURE CONTROL VALVE. ALSO, REPLACED LEFT AND RIGHT COALESCER BAGS. PERFORMED AIR CONDITIONING PACK BURN-OUT PER MM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR EMERGENCY WALK AROUND LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR EMERGENCY WALK AROUND LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)