N955U

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,886 hrs · 41,587 cycles

AFT CARGO, CORROSION EMITTING FROM BELOW STAINLESS DOUBLER ON LOWER DOOR BEAM STATION 1160-1200. REMOVED DOUBLER & CLEANED UP CORROSION, MANUFACTURED FILLERS & REINSTALLED DOUBLER IAW AARD 53-10-00-3 & EA 256278.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,886 hrs · 41,587 cycles

FORWARD CARGO COMPARTMENT DOOR FWD SIDE, LOWER DOOR STOP CASTING IS CRACKED. INSTALLED NEW DOOR STOP CASTING, FITTING, IAW AARD 51-00-50-1, DWG 4920233, & DWG CD K2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,886 hrs · 41,587 cycles

MID CARGO COMPARTMENT DOOR AFT SIDE SECOND FROM BOTTOM DOOR STOP CASTING IS CRACKED. INSTALLED NEW DOOR STOP CASTING, FITTING, IAW AARD 51-00-05-1, DWG 4920233 & DWG CDK 2345.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,886 hrs · 41,587 cycles

FORWARD CARGO COMPARTMENT DOOR, FWD SIDE, UPPER DOOR STOP CASTING IS CRACKED. INSTALLED NEW DOOR STOP CASTING, FITTING, IAW AARD 51-00-50-1, DWG 4920233 & DWG CD K2345.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,886 hrs · 41,587 cycles

FUSELAGE DENT IN SKIN AT STATION 1351 AT L6L. HFEC REVEALED CRACK, EXTERNAL DOUBLER INSTALLED IAW SRM 53-01-00-001.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 76,886 hrs · 41,587 cycles

AFT CARGO DOOR FWD STOP FITTING CRACKED. R & R STOP BRACKET IAW AARD 51-00-05-1.

Part: COMPRESSOR BLADE — DAMAGED (RT ENGINE) · airframe 75,774 hrs · 40,893 cycles

AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CREW REPORTS A COMPRESSOR STALL ON RT ENG FOLLOWED BY A REDUCTION IN EPR & INCREASE IN EGT. ACCOMPLISHED CARD 72-96-12 71-91-12 & BORESCOPE WITH A DETAILED VISUAL INSPECTION OF RT ENG COMPRESSOR & TURBINE. BORESCOPE IDENTIFIED DAMAGE TO STAGE 12 & 13 COMPRESSOR BLADES. REPLACED THE RT ENG IAW MCM 71-91-03 & 71-91-09.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,146 hrs · 39,885 cycles

GOUGE AT STATION 200 AT LT LONGERON 200. INSTALLED DOUBLER IAW SRM 53-04-02-001 FIGURE 2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,146 hrs · 39,885 cycles

CRACK IN LONGERON 24 LT AT STATION 200. SPLICED IN LONGERON REPAIR IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,146 hrs · 39,885 cycles

CRACK IN LONGERON 23 LT AT STATION 200. SPLICED IN LONGERON REPAIR IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 74,146 hrs · 39,885 cycles

CRACK IN LONGERON 25 LT AT STATION 160. SPLICED IN LONGERON REPAIR IAW SRM 53-02-00-001.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 74,146 hrs · 39,885 cycles

OUT OF ROUND HOLE AT THE VERTICAL 503 BAND LABELED 24. INSTALLED PLUG IAW SRM 55-03-00.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 74,146 hrs · 39,885 cycles

OUT OF ROUND HOLE AT THE VERTICAL 503 BAND LABELED 22. INSTALLED PLUG IAW SRM 55-03-00.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 74,146 hrs · 39,885 cycles

OUT OF ROUND HOLE AT THE VERTICAL 503 BAND LABELED 21. INSTALLED PLUG IAW SRM 55-03-00.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 74,146 hrs · 39,885 cycles

OUT OF ROUND HOLE AT THE VERTICAL 503 BAND LABELED 38. INSTALLED PLUG IAW SRM 55-03-00.

Part: SWITCH — INOPERATIVE (AC BAY) · airframe 73,251 hrs · 39,358 cycles

CREW REPORTED DIRTY SOCK SMELL & SOON AFTER LOSS OF BOTH AIR CONDITIONING PACKS. ANNUNCIATOR LIGHT PRESSURIZATION FLOW ALSO ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED BOTH SINGLE SECOND SEGMENT CLIMB SWITCHES & BOTH COLESCER BAGS. SYS GROUND CHECK NORMAL OPERATION CLOSED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,239 hrs · 39,347 cycles

EMERGENCY CEILING LIGHTS ABOVE SEATS 12 TO 16 ARE INOPERATIVE. REPLACED BATTERY B5-102. OPERATIONS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,239 hrs · 39,347 cycles

FOUND CRACK IN SKIN AT STATION 1510. INSTALLED DOUBLER IAW SRM 53-01-00-001.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 73,239 hrs · 39,347 cycles

MID CARGO DOOR AFT STOP CRACKED. R & R AFT STOP IAW AARD 51-00-05-1.

Part: FORMER — CRACKED (SLAT TRACK) · airframe 73,102 hrs · 39,264 cycles

LEFT HAND WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT HAND WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05 & EA MD80-57-034864.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 71,650 hrs · 38,373 cycles

BHM CREW REPORTED ON CLIMB OUT, RT HAND ENG ENCOUNTERED 2 SUCCESSIVE COMPRESSOR STALLS. EMERGENCY DECLARED FLIGHT RETURNED BHM LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR REPAIR. REPLACED RT HAND ENGINE AT BHM ON 10/04/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: ADC — INOPERATIVE (NR 1) · airframe 71,602 hrs · 38,346 cycles

DFW CREW REPORTED ON TAKEOFF ROLL CAPTAIN LOST AIRSPEED, ALTITUDE, & VERTICAL SPEED INDICATOR. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,344 hrs · 38,192 cycles

FORWARD INTERIOR OVERWING EXIT LIGHT WILL NOT STAY OFF WHEN POWER REMOVED FROM AIRCRAFT. REPLACED B5-103 EMERGENCY LIGHT BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 71,344 hrs · 38,192 cycles

LT NR 1 DOOR PORTABLE EMERGENCY LIGHT FAILED TEST. REPLACE LT NR 1 DOOR PORTABLE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,344 hrs · 38,192 cycles

AFT INTERIOR EMERGENCY LIGHT FAILED TEST. REPLACED B5-105 EMERGENCY LIGHT BATTERY PACK. OPERATIONS CHECKED NORMAL.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 70,848 hrs · 37,893 cycles

CREW REPORTED RT GENERATOR FAILED WITH APU ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENGINE CONSTANT SPEED DRIVE AND GENERATOR. SYS GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

DENT WITH GOUGE IN FUSELAGE SKIN AT STATION 1304 LONGERON 19 RIGHT. INSTALLED DOUBLER PER SRM 53-04-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

GRIND MARKS IN SKIN FROM STATIONS 1363 TO 1367 ABOVE LONGERON 4 LEFT. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 4.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

LONGERON 4 LEFT CRACKED FROM STATIONS 160 AND 200. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

DAMAGE TO STATION 400 AT LONGERON 19 LEFT. INSTALLED DOUBLER AND SHIMS PER SRM 53-04-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

DAMAGE TO SKIN FROM STATIONS 503 TO 512, LONGERON 22 TO 23 RIGHT. INSTALLED DOUBLER PER SRM 53-04-03.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

WEB IS CRACKED AT STATION 208 AT LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,648 hrs · 37,180 cycles

BOTTOM OF RIGHT CUSP AT STATION 702 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

STATIONS 1271 TO 1287, CABIN FLOORBOARD INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED DAMAGED INTERCOSTAL AND INSTALLED SERVICEABLE INTERCOSTAL FROM STATIONS 1271 TO 1287 AS PER AARD 51-00-05-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

FORWARD FUSELAGE HAS CRACK AND LOOSE FASTENERS IN SKIN, AFT OF LEFT AFT CORNER OF NOSE LANDING GEAR CUTOUT. INSTALLED DOUBLER REPAIR PER SRM 53-01-00 FIGURE 2 AND AARD 53-30-01-2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

GRIND MARKS IN SKIN FROM STATIONS 1200 TO 1204 BETWEEN LONGERONS 4 AND 5 RIGHT. INSTALLED DOUBLER PER SRM 53-04-03 FIGURE 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

DENT AT STATION 201 BETWEEN LONGERONS 4 AND 5 LEFT. INSTALLED DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

CRACK IN TOP OF VERTICAL STIFFENER BELOW LONG 1 AT STATION 1338. REPLACED STIFFENER PER AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,648 hrs · 37,180 cycles

SEAT TRACK NUMBER 2.5 CORRODED AT STATIONS 1120 TO 1136. INSTALLED SERVICEABLE SEAT TRACK FROM STATIONS 1098 TO 1136 PER AARD 51-00-05-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,648 hrs · 37,180 cycles

TOP OF CENTER FUEL TANK HAS VERTICAL ANGLE CRACKED AT LOWER END AT STATION 905 AND JUST BELOW NUMBER 5 SEAT TRACK. REMOVED CRACKED FITTING AND INSTALLED SERVICEABLE FITTING AS PER AARD 51-00-05-1 AND BOEING INSTALLATION DRAWING 9936637-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,580 hrs · 36,553 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 26D. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 68,580 hrs · 36,553 cycles

TAIL COMPARTMENT LIGHTS ABOVE CATWALK INOPERATIVE. RESEATED THE BATTERIES IN THE POWER SUPPLY FOR THE TAIL COMPARTMENT LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 68,580 hrs · 36,553 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 27 INOPERATIVE. RESEATED THE BATTERIES AT ROW 24 FOR CEILING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 67,322 hrs · 35,802 cycles

TUL - CREW REPORTED LOSS OF PRESSURIZATION DURING FCF. EMERGENCY DECLARED FLIGHT LANDED TUL WITHOUT INCIDENT. REPLACED OUTFLOW VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 67,319 hrs · 35,800 cycles

ELP - INFLIGHT DFW-SAN. CREW REPORTED BOTH AUTO PRESSURE CONTROLLERS FAILED AND CABIN LOST PRESSURIZATION SUDDENLY. MASK WERE DEPLOYED IN CABIN. EMERGENCY DECLARED FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH CABIN PRESSURE CONTOLLERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOWNLOCK SENSOR — FAULTY (LANDING GEAR) · airframe 66,590 hrs · 35,390 cycles

DFW - CREW REPORTED UNSAFE LANDING GEAR INDICATION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT MAIN DOWNLOCK INDICATING LOCKED. REPLACED DOWN LOCK SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 66,341 hrs · 35,237 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL, CORROSION ON BOTTOM OF ANGLE JUST ABOVE ACCUMULATOR. INSTALLED NEW CHORD ANGLE PER SRM 51-30-01 AND AARD 51-10-00-5.

Part: ANGLE — DAMAGED (RT MLG WW) · airframe 66,341 hrs · 35,237 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL HAS CORROSION ON BOTTOM OF ANGLE JUST ABOVE ACCUMULATOR. INSTALLED NEW CHORD ANGLE PER SRM 51-30-01 AND AARD 51-10-00-5.

Part: FITTING — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 66,341 hrs · 35,237 cycles

CORROSION ON FITTING AT FORWARD END OF THRESHOLD. REPLACED FITTING.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,341 hrs · 35,237 cycles

DENTS WITH GOUGES IN FUSELAGE SKIN STATION 237 LONGERONS 17 TO 18 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 38 SHEET 30 VIEW P.

Part: TURBINE BLADES — DAMAGED (LT ENGINE) · airframe 64,106 hrs · 33,944 cycles

DFW - CREW REPORTED LOUD BANG, VIBRATION AND RISE IN ENGINE GAS TEMPERATURE. LEFT ENGINE FAILED. AFTER ENGINE SHUTDOWN CREW REPORTED BANK ANGLE AUDIBLE WARNING EVEN THOUGH WINGS LEVEL. SINGLE ENGINE TIME 10 MINUTES. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND TURBINE BLADE DAMAGE. REPLACED LEFT ENGINE AT DFW ON 05/20/2010. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,741 hrs · 33,735 cycles

EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,741 hrs · 33,735 cycles

EMERGENCY LIGHT ON ROW 8 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ON ROW 8. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,477 hrs

LGA - LEFT AND RIGHT EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT EXTERIOR FUSELAGE EMERGENCY LIGHTS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,738 hrs

LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT MISSING LENS AT SEAT 4E. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (ZONE 200) · airframe 59,738 hrs

LGA - FORWARD AND AFT SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 6E INOPERATIVE. RESET CONNECTOR AT SEAT 6E FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 59,738 hrs

LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT HAS DAMAGED SHROUD AT SEAT 6E. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,738 hrs

LGA - EMERGENCY LIGHT AT AFT TAIL COMPARTMENT WALK WAY MISSING LENS. REPLACED LENS FOR THE AFT EMERGENCY LIGHT AT AFT TAIL COMPARTMENT WALK WAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — INCORRECT (EMERGENCY LIGHT) · airframe 59,738 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD OF RIGHT LAVATORY HAS INCORRECT LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD FORWARD OF RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 59,738 hrs

LGA - EMERGENCY FLASHLIGHT STRAP BROKEN AT FORWARD GALLEY. REPLACED FLASHLIGHT STRAP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 59,738 hrs

LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT MISSING LAMPS AT SEAT 4E. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT) · airframe 59,738 hrs

LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT MISSING SHROUD AT SEAT 4E. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (ZONE 200) · airframe 59,738 hrs

LGA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. RESET CONNECTOR AT SEAT 29D FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL PANEL — FAILED (FIRE DETECTION) · airframe 59,072 hrs

ORD FORWARD COMPARTMENT BOTTLE NR 2 SQUIB FAILED DURING TEST OF CARGO FIRE SUPPRESSION. REPLACED CARGO FIRE SUPPRESSION CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 29 FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 29D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — FOD (LEFT ENGINE) · airframe 57,430 hrs

ORD INFLIGHT - NUMBER ONE ENGINE LOST POWER DURING CLIMB. CREW HEARD LOUD POPS. PULLED THROTTLE TO IDLE AND LEFT NUMBER ONE ENGINE AT IDLE FOR LANDING. NUMBER ONE ENGINE PARAMETERS WERE NORMAL. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE AND ISOLATORS ON 22 NOV AT ORD DUE TO COMPRESSOR STALL DUE TO FAN FOREIGN OBJECT DAMAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 57,377 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 8 INOPERATIVE. SECURED LOOSE BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (CABIN)

LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY INOPERATIVE. SECURED LOOSE BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - OVERHEAD EMERGENCY LIGHTS AT ROWS 29 TO 32 INOPERATIVE. REPLACED BATTERY PACK AT ROW 29 FOR INOPERATIVE OVERHEAD EMERGENCY LIGHTS AT ROWS 29 TO 32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (BRAKE)

ORD - INFLIGHT T730/28SEPT, DURING TAKEOFF ROLL WHEEL NOT TURNING LIGHT ILLUMINATED. ABORTED TAKEOFF. SPEED LESS THAN 10 KNOTS. FOUND NO ELECTRICAL OUTPUT FROM NUMBER 3 TRANSDUCER. REPLACED NR 3 TRANSDUCER AND REPLACED ANTI-SKID CONTROL BOX AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROWS 27 AND 28 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 27 AND 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - TWO EACH AFT TAIL CONE EMERGENCY LIGHTS AND AFT CATWALK OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR TWO EACH AFT TAIL CONE EMERGENCY LIGHTS AND AFT CATWALK OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — CONTAMINATED (CABIN) · airframe 42,454 hrs · 21,637 cycles

THE EMERGENCY EGRESS LIGHTS BETWEEN ROWS 15 AND 22 ILLUMINATED WITH THE SWITCH ARMED. REMOVED WATER FROM THE ELECTRICAL CONNECTORS. CHECK-C 2-13-01 STL.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,448 hrs · 19,949 cycles

EVIDENCE OF CORROSION AT STA 1320 FORMER RING AND STR 30 INTERCONNECT. REPLACED 21 INCH LONG SECTION OF FORMER PER MD80 SRM 53-03 PG 4. CK C28C 04/14/00 JFK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT)

FOUND THE OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-19-99 STL.

Part: SKIN — DENTED (BS 69)

MCI - DURING OVERNIGHT MAINTENANCE CHECK, FOUND SKIN AND FORMER DENTED AT STATION 69.5 ON RT SIDE BELOW PRESS DUCT, .5 INCH WIDE BY 7 INCH LONG BY 5/8 INCH DEEP. NDT INSPECTION OF SKIN SHOWED NO CRACK OR CORROSION. REPLACED FORMER PER SRM 51-01, PAGE 1 ITEM C. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

MCI - DURING OVERNIGHT MAINTENANCE FOUND CRACK MIGRATING OUT OF FASTENER HOLE RT SIDE VERTICAL STABILIZER ATTACH ANGLE, FS 1388. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PER SRM 51-10-0 AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACFT TT: 33,526 HOURS. ACFT TC: 16,902. (X)

Part: ANGLE — CRACKED (VERTICAL STAB)

MCI - DURING OVERNIGHT MAINTENANCE, FOUND LOWER ATTACH ANGLE FOR WRAP AROUND FAIRING AT VERTICAL STABILIZER CRACKED THROUGH FASTENER HOLE, 7 IN FORWARD OF PRODUCTION BREAK, LT SIDE FS 1421. REMOVED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE PER SRM 51-10-0 AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACFT TT: 33,526 HOURS. ACFT TC: 16,902. (X)

Part: ANGLE — CRACKED (VERTICAL STAB)

MCI - DURING OVERNIGHT MAINTENANCE, FOUND LOWER ATTACH ANGLE FOR WRAP AROUND FAIRING AT VERTICAL STABILIZER CRACKED THROUGH FASTENER HOLE, 7 IN FORWARD OF PRODUCTION BREAK, RT SIDE FS 1421. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PER SRM 51-10-0, AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACFT TT: 33,526 HOURS. ACFT TC: 16,902. (X)

Part: SWITCH — LOOSE (COCKPIT)

PBI - FLT 268 - DURING PREFLIGHT, WHEN PA BUTTON IN COCKPIT WAS PUSHED THE BUTTON ARCED AND SPARKED. SECURED LOOSE SWITCH. (M)

Part: PACK — OVERHEATED (RIGHT)

SNA - FLT 176 - DURING PRE-FLIGHT, THE RT PACK OVERHEATED SENDING WHITE SMOKE INTO THE CABIN. CLEARED SMOKE AND CLEANED SENSOR. MFG NR B7110. CK-C 2D 2-3-97 MCI. (X)

Part: AIR DISTRIBUTION — ODOR (CABIN)

JFK - FLT 783 - DURING PRE-FLIGHT WHEN CREW TURNED ON AIR CONDITIONING, THEY REPORTED SMOKE IN THE CABIN. OPERATED LT AND RT AIR CONDITIONING PACKS FULL HOT AND COLD USING APU AND ENGINE AIR. UNABLE TO DUPLICATE. SUSPECT DE-ICING FLUID INJESTION. CHECK-C 2D. 02-13-97. JFK. (X)

Part: POWER STRIP — DAMAGED (CABIN)

STL - FLT 32 - EGRESS LIGHTS INOPERABLE. F/C FOUND ON PRE-FLIGHT. REPLACED POWER STRIP, LAMP BAR, AND RACK COVER. CK-C 2-3-97 - JFK. (X)

Part: ACARS PRINTER — FAILED (COCKPIT)

STL - FLT 360 - DURING CRUISE, ACARS PRINTER SHOCKED THE FIRST OFFICER. FLIGHT CREW THEN PULLED THE CIRCUIT BREAKER. SECURED ACARS PRINGER CASE GROUND. (M)

Part: COALESCER BAG — CONTAMINATED (CABIN)

STL - FLT 99 - DURING APPROACH, SMOKE EMITTED INTO AFT CABIN AND COCKPIT. FOUND LEFT AND RIGHT COALESCER ELEMENTS, MFG PN 179460-8-1, CONTAMINATED. REPLACED LEFT AND RIGHT COALESCER ELEMENTS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-2D - 10-17-95 - MCI.

Part: TARGET ASSY — LOOSE (RT MLG)

STL - FLT 159 - AFTER TAKEOFF, THE RT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION. FOUND RT GEAR TARGET ASSEMBLY LOOSE. SECURED TARGET ASSEMBLY WITH BELT, MFG PN NAS6203-2H. PERFORMED MM SENSOR CHECK, OPERATIONAL CHECK NORMAL. CHECK C-2D - 10-17-95 - MCI.

Part: CONTROL CABLE — FAILED (ROW 15-19)

STL - FLT 202 - A CHECK OF THE EGRESS LIGHTS REVEALED ROW 15 TO ROW 19 INOPERATIVE. REMOVED AND REPLACED FEEDER LINE FLEX CABLE, MFG PN 5853-1. OPERATIONAL CHECK OF THE EGRESS LIGHT SYSTEM WAS NORMAL. CHECK C-2D - 10-17-95 - MCI.