N983TW

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 51,561 hrs · 26,088 cycles

THE AIRCRAFT WAS GROUNDED. L1 WINDOW IS BUBBLING AND IS VERY HOT. REPLACED L1 WINDSHIELD PER AMM 56-10-02.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 51,452 hrs · 26,013 cycles

AIRCRAFT WAS GROUNDED. FIRST OFFICER WINDSCREEN HAS DELAMINATION IN LEFT LOWER CORNER. REPLACED FIRST OFFICERS WINDSCREEN, TORQUED AND SEALED PER AMM 56-10-02. OPERATIONS CHECK GOOD.

Part: DFGS — MALFUNCTIONED (NR 2) · airframe 50,344 hrs · 25,294 cycles

DURING HEAVY CROSS WINDS, USING THE NR 2 AUTOPILOT, TWO MISSED APPROACHES WERE MADE. DIVERTED AND LANDING WAS UNEVENTFULLY WITH NR 1 AUTOPILOT. PERFORMED A FLIGHT FAULT REVIEW, FIRST APPROACH, AUTOPILOT CAPTURED LOC 2 GLIDESLOOP THEN WENT TO VERT SPEED. RECAPTURED, THEN WENT TO VERT SPEED AND HEADING HOLD. SECOND APPROACH, AUTO PILOT KICKED OFF SWITCHED TO NUMBER 1 FGC AND WORKED FINE NEXT APPROACH. REPLACED THE NR 2 DIGITAL FLIGHT GUIDANCE COMPUTER IAW AMM 22-01-01. THE AIRCRAFT WAS GROUNDED.

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 49,960 hrs · 25,069 cycles

AIRCRAFT WAS GROUNDED. VERY NOTICEABLE RUBBER SMELL THROUGHOUT THE CABIN JUST AFTER TAKE OFF. SMELL DISSIPATED QUICKLY. REPLACED LEFT HAND PACK PRESSURE REGULATING SHUT OFF VALVE PER AMM 21-31-01. (SEE CONTROL AALA201802239017)

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 49,960 hrs · 25,069 cycles

AIRCRAFT WAS GROUNDED. VERY NOTICABLE RUBBER SMELL THROUGHOUT THE CABIN JUST AFTER TAKE OFF. SMELL DISSIPATED QUICKLY. REPLACED RIGHT HAND PACK PRESSURE REGULATING SHUT OFF VALVE PER AMM 21-31-01. (SEE CONTROL AALA201802239016)

Part: LENS — MISSING (CABIN) · airframe 47,939 hrs · 23,780 cycles

EMERGENCY LIGHT LENS MISSING AT STATION 1305, AFT VAULT DOOR. REPLACED EMERGENCY LIGHT LENS, IAW AMM REF 33-53-00. OPERATION NORMAL. THE AIRCRAFT WAS NOT GROUNDED.

Part: LENS — MISSING (CABIN) · airframe 47,939 hrs · 23,780 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT STATION 1305 AFT VAULT DOOR HAS A MISSING LENS COVER. REPLACED LENS COVER IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: DISPLAY — MALFUNCTIONED · airframe 47,775 hrs · 23,684 cycles

ON RUNWAY PRIOR TO ADVANCING THROTTLES, CREW NOTED A 2 TO 3 MILE MISALIGHNMENT BETWEEN AIRCRAFT AND RUNWAY ON NAV DISPLAY. CREW EXITED RUNWAY AND ACCOMPLISHED AN IRS REALIGNMENT, SUBSEQUENT TAKE OFF WAS UNEVENTFULE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 47,263 hrs · 23,351 cycles

L1 DOOR EMERGENCY FLASHLIGHT NR 1 HAS A DISCHARGED BATTERY. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: ANGLE — CORRODED (BS 916) · corrosion level 2 · airframe 47,172 hrs · 23,269 cycles

ANGLE ABOVE LEFT MAIN LANDING GEAR BRAKE ACCUMULATOR IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-30-01-001 AND DRAWING 5935852.

Part: SKIN — CRACKED (BS 83-101) · airframe 47,172 hrs · 23,269 cycles

FUSELAGE SKIN CRACKED AT NOSE LANDING GEAR RIGHT AFT DOOR AFT HINGE CUTOUT. REPAIRED THE SKIN IAW SRM 53-01-00-001.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 46,967 hrs · 23,132 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS BATTERY PACK AB5-1 FAILED WORK CARD 5403. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,967 hrs · 23,132 cycles

EMERGENCY LIGHTS BATTERY ASSEMBLY B5-102 AT ROWS 11-17 FAILED WORK CARD 0801. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 CSD) · airframe 46,474 hrs · 22,827 cycles

DURING CRUISE AT FL 320, NR 2 CSD OIL PRESSURE LIGHT ILLUMINATED WITH NO RISE IN TEMPERATUR, CSD WAS DISCONNECTED. CREW REPORTED AN ELECTRICAL ODOR. EMERGENCY DECLARED, LANDING UNEVENTFUL, AND AIRCRAFT GROUNDED. MAINTENANCE INSPECTED THE NR 2 CSD PRESSURE SWITCH AND WIRING WITH NO DEFECTS NOTED. ACCOMPLISHED AN OPS CHECK OF THE NR 2 CSD WITH NO FAULTS FOUND. REMOVED AND REPLACED NR 2 CSD IAW AMM 24-10-01 AS A PRECAUTION. ACCOMPLISHED MCM CARD 21-96-01 WITH NO ODORS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,824 hrs · 22,439 cycles

AIRCRAFT WAS GNDED. AB5-2 EGRESS LIGHT BATTERY PACK FAILS TO TEST. R & R BATTERY PACK AB5-2 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD.

Part: FITTING — LEAKING (NR 2 OIL) · airframe 45,465 hrs · 22,238 cycles

AT GATE AFTER PAXS DEPLANED, CREW NOTED A BLUE HAZE IN CABIN, ACCOMPANIED BY AN OIL ODOR. ACCOMPLISHED MCM CARD 21-96-01 & NR 2 ENG IGV CASE LEAKING OIL OUT OF FAN INLET SLEEVE. R & R NR 2 ENGINE IAW MCM 71-91-99. ENGINEERING REPORTED OIL LEAK WAS FROM THE SCAVENGE LINE FITTING AT 6:00 POSITION. REMOVED AND REPLACED FAN INLET CASE. AIRCRAFT WAS GROUNDED.

Part: APU — ODOR · airframe 45,460 hrs · 22,234 cycles

AT GATE, PRIOR TO FLIGHT, BOTH PACKS TURNED ON AFTER APU POWERED ON. EGT TOO HOT TURNED OFF RIGHT PACK. FUMES & SMOKE BEGAN FILLING MID TO AFT CABIN, TURNED LT PACK OFF. FOUND APU LEAKING OIL. APU CHANGE PLANNED. ACCOMPLISHED PACK BURNOUT PER WORK CARD 21-92-12.

Part: UFI — TRIPPED (FUEL SYSTEM) · airframe 45,047 hrs · 21,977 cycles

AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB CTR TANK PRESS LOW LIGHT ILLUMINATED. RESET CTR TANK UFIS IAW AMM 28 20 28. TRANSFERRED FUEL TO WING TANKS. OPERATIONAL CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 44,934 hrs · 21,900 cycles

AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE ACFT DE-PRESSURIZED RESULTING IN A CABIN ALT WARNING & CABIN ALT CLIMBING ABOVE 10,000 FEET. DURING DESCENT THE ACFT NOT ONLY PRESSURIZED TO BELOW SEA LEVEL. MANUAL DE-PRESSURIZATION WAS USED TO DESCEND & DE-PRESSURIZE THE ACFT. ACCOMPLISHED BITE OF BOTH CONTROLLERS & OPERATIONAL CHECK WITH NO DEFECTS FOUND. OK FOR SERVICE IAW AMM 21-32-00-101.

Part: CYLINDER — CORRODED (NLG) · corrosion level 2 · airframe 44,619 hrs · 21,725 cycles

SHOP FOUND HEAVY CORROSION & PITTING IN NLG UPPER CYLINDER BORE. PART SCRAPPED AT DIRECTION OF ENGINEERING.

Part: RIB — CRACKED (RT WING) · airframe 43,415 hrs · 21,015 cycles

RIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED. REPAIRED RIB IAW MCM 57-98-06 & EA 251393.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

LEFT ALTERNATE STATIC PORT DOUBLER BETWEEN FS 450 & 460 AT STRINGER 26L IS CORRODED. R & R DOUBLER IAW AARD 53-30-00-07 & EA 251578.

Part: CASTING — CRACKED (RT SPOILER) · airframe 43,415 hrs · 21,015 cycles

RIGHT GND SPOILER ACTUATOR CASTING CRACKED. R & R CASTING IAW AMM 27-62-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,415 hrs · 21,015 cycles

SEAT TRACK NR 6 IS CORRODED BETWEEN FS 216 & 588. R & R SEAT TRACK SECTION IAW AMM 53-40-01-2.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 43,415 hrs · 21,015 cycles

GALLEY TIE DOWN FITTING AT FS 215 & FWD END OF SEAT TRACK 6 IS CORRODED. R & R GALLEY MOUNT IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,415 hrs · 21,015 cycles

SEAT TRACK NR 1 IS CORRODED BETWEEN FS 798 & 1010. R & R SEAT TRACK IAW AARD 51-00-05-01, DWG 5930566 & AMM 53-40-01-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,415 hrs · 21,015 cycles

SEAT TRACK NR 1 IS CORRODED BETWEEN FS 588 & 798. R & R SEAT TRACK IAW AMM 53-40-01-2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

AFT CARGO COMPARTMENT LT TIE DOWN TRACK AT LONGERON 26L IS CORRODED BETWEEN FS 1079 & 1220. R & R TRACK SECTION IAW SRM 51-30-01 & 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · airframe 43,415 hrs · 21,015 cycles

AFT CARGO COMPARTMENT LOWER DOOR BEAM IS CORRODED BETWEEN FS 1155 & 1212. REPAIRED LOWER DOOR BEAM IAW 53-10-00-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

AFT CARGO COMPARTMENT, LT TIE DOWN TRACK AT LONGERON 26L CORRODED BETWEEN FS 1220 & 1309. R & R TRACK IAW SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

FLOORBOARD SUPPORT IS CORRODED AT FS 1155 BETWEEN LONGERONS 28R & 29R. R & R SUPPORT IAW SRM 51-30-05 & 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

FLOORBOARD SUPPORT AT FS 180 IS CORRODED BETWEEN LBL 17 & 39. R & R FLOORBOARD SUPPORT IAW DWG 9936534 & SRM 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

SEAT TRACK NR 4 IS CORRODED BETWEEN FS 1088 & 1307. R & R SEAT TRACK SECTION IAW AMM 53-40-01-2.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

CORROSION IN SUB FLOOR DIAPHRAGM AT BS 186, 7" INBD OF FWD ENTRY DOOR CUT OUT. INSTALLED DOUBLER ON SUB FLOOR AT BS 186 IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

RIGHT CUSP AT STATION 219 - 232 WAS CORRODED. CORRODED SECTION OF CUSP WAS REMOVED FROM STATION 218 - 237 & NEW CUSP SECTION WAS INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

CORROSION ON RT CUSP BETWEEN STATIONS 395 & 396. CORROSION WAS CUT OUT & DOUBLER INSTALLED IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

RIGHT CUSP & SUBFLOOR UNDER NR 6 SEAT TRACK IS CORRODED BETWEEN FS 200 & 218. REPAIRED CUSP IAW 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,415 hrs · 21,015 cycles

SEAT TRACK NR 6 IS CORRODED BETWEEN FS 588 & 797. R & R SECTION OF TRACK IAW SRM 53-05-00-001 FIG 4H & F & AMM 53-40-01-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,397 hrs · 20,445 cycles

EMERGENCY LIGHTS OPERATED BY BATTERY PACK B5-28 INOPERATIVE DURING TEST. R & R BATTERY PACK B5-28. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,397 hrs · 20,445 cycles

EMERGENCY PATH LIGHTS DIM AT SEATS ROW 21 THRU 31 DURING PERFORMANCE OF CARD 5403 STEP 1 A 12. R & R BATTERY PACK AB5-3. SYS CHECKED NORMAL.

Part: FILTER — CLOGGED (RT ENGINE) · airframe 42,206 hrs · 20,349 cycles

RIGHT ENG OIL FILTER CLOGGED LIGHT ILLUMINATED WHEN POWER WAS REDUCED AT TOP OF DESCENT. EMER DECLARED, LANDING UNEVENTFUL, WAS NOT OVERWEIGHT. RAN RT ENG & CHANGED OIL FILTER IAW MM 72-00-02. REPLACED FILTER DIFFERENTIAL PRESS SWITCH IAW MM 79-35-01. ALL CHECKED NORMAL. OK FOR SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 40,676 hrs · 19,551 cycles

LEFT WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED AT BOSS. INSTALLED REPAIR DOUBLER IAW CARD 57-98-05 & EA MD80-57-033976.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 39,850 hrs · 19,146 cycles

ORD CREW REPORTED DC BUS OFF LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RELAYS R2-21 & R2-326. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: VALVE — INOPERATIVE (LT ENGINE) · airframe 39,592 hrs · 18,996 cycles

DFW LT OIL TEMPERATURE ROSE TO 149 DEGREES & FUEL TEMPERATURE ON LT ENG WAS AT 88 DEGREES. FOLLOWED QRH PROCEDURE & SHUT DOWN LT ENG SINGLE ENGINE TIME 18 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED LT ENG FUEL HEAT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: ELECTRONIC UNIT — FAULTED (CARGO BAY) · airframe 38,813 hrs · 18,557 cycles

SMOKE & BURNING SMELL IN FORWARD PART OF CABIN AFTER TAKE-OFF. RECIRCULATION FAN WAS OFF & APU WAS OFF. UPON LANDING FOUND AFT CARGO FIRE DETECTION FAULT LIGHT ON. REPLACED CARGO ELECTRONIC UNIT NR THREE THAT HAD FAULTED. SYSTEM GROUND CHECKED NORMAL.

Part: FAN — MALFUNCTIONED (CARGO BAY) · airframe 38,813 hrs · 18,556 cycles

SMOKE IN CABIN & FUMES IN CABIN. SMOKE DISAPPEARED AFTER RECIRCULATION FAN TURNED OFF. EMERGENCY DECLARED FLIGHT DIVERTED AUS LANDED WITHOUT INCIDENT. REPLACED AFT CARGO RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 38,659 hrs · 18,467 cycles

ROW 28, SEAT EMERGENCY LIGHT INOPERATIVE. REPAIRED CONNECTOR FOR ROW 28 SEAT EMERGENCY LIGHT. OPS CHECK NORMAL

Part: SHROUD — BROKEN (CABIN) · airframe 38,659 hrs · 18,467 cycles

EMERGENCY LIGHT LENS SHROUD BROKEN AT ROW 26. REPLACED LENS SHROUD FOR EMERGENCY LIGHT AT ROW 26. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,659 hrs · 18,467 cycles

OVERWING EMERGENCY EXIT SIGN AND AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK B5-105 FOR OVERWING EMERGENCY EXIT SIGN AND AFT EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 37,711 hrs · 17,968 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. SECURED BATTERY PACK. OPS CHECK NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 37,711 hrs · 17,968 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,711 hrs · 17,968 cycles

ESCAPE PATH LIGHT AT SEAT 28D INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 28D. OPS CHECK NORMAL.

Part: SENSOR — FAULTY (LT MLG DOOR) · airframe 37,711 hrs · 17,968 cycles

ORD - CREW REPORTED AFTER GEAR WAS EXTENDED YELLOW GEAR DOOR OPEN LIGHT STAYED ON. ACCOMPLISHED GO AROUND AND CHECK LIST AND LIGHT STAYED ON. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT MAIN GEAR DOOR SENSOR FAULTY. REPLACED D1-30 SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 36,969 hrs · 17,592 cycles

RDU - INFLIGHT EWR-DFW. CREW REPORTED RIGHT ENGINE INDICATION SYSTEM FAILED. FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MULTIFUNCTION DISPLAY PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

AFT ACCS LONGERON 2 RIGHT CRACKED AFT OF 1418. INSTALLED NEW LONGERON AND SPLICE PLATE PER SRM 53-02-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

FRAME CRACKED 1418 LONGERON 2 RIGHT FORWARD AND AFT SIDES. INSTALLED FORWARD AND AFT SIDE FRAME DOUBLER 1418 2 RIGHT PER SRM 53-03-00 FIGURE 31.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

RIGHT CUSP CRACKED AT STATION 484. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

DENT WITH SCRATCHES AND PLUG RIVET BELOW RIGHT GROUND FLOOD LIGHT AT STATION 558 BELOW LONGERON 21 RIGHT. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER EA MD80-53-016869.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,042 hrs · 15,572 cycles

CORROSION ON BOTTOM OF RIGHT HAND CUSP STATIONS 735. INSTALLED NEW CUSP STATIONS 712 TO 750 PER AARD 51-10-00-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

RIGHT SIDE OF FUSELAGE AT STATION 1380 HAS CRACK IN SKIN IN SHEAR TIE AREA JUST ABOVE PYLON. INSTALLED DOUBLER AND FILLER AT STATION 1380 LONGERON 14 RIGHT PER SRM 53-34-00 AND SRM 53-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,042 hrs · 15,572 cycles

LEFT CUSP STATIONS 1174 TO 1190 CORRODED. INSTALLED DOUBLER STATIONS 1176 TO 1190 PER AARD 53-20-00-16.

Part: BEAM — DAMAGED (CARGO DOOR) · corrosion level 2 · airframe 33,042 hrs · 15,572 cycles

CORROSION ON MID CARGO DOOR BEAM. REMOVED CORROSION AND INSTALLED DOUBLER.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

CUSP ANGLE RIGHT SIDE STATION 883 HAS SMALL NICK ON TOP SIDE. INSTALLED REPAIR ANGLE PER EA MD80-53-016787.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,042 hrs · 15,572 cycles

CORROSION ON BOTTOM OF LEFT CUSP STATIONS 750 TO 769. REMOVED DAMAGED CUSP AND INSTALLED DOUBLER REPAIR AS PER AARD 53-20-00-16.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,042 hrs · 15,572 cycles

AFT CARGO, DOOR JAMB WEB, CORROSION AT NUT PLATE HOLES, STATIONS 1214 TO 1217 BETWEEN LONGERON 28 AND 27 RIGHT. INSTALLED NEW WEB SPLICE PER AARD 53-10-00-24.

Part: SKIN — DENTED (TE FLAP) · airframe 33,042 hrs · 15,572 cycles

LEFT WING FLAPS INBOARD FLAP HAS 2 EACH DENTS WITH SCRATCH IN BOTTOM SKIN CENTER AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED FLUSH REPAIR AT CUT OUT PER SRM 57-01-00 FIGURE 5, SHEET.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,042 hrs · 15,572 cycles

CORROSION ON BOTTOM OF LEFT CUSP STATIONS 638 TO 643. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

LEFT FORWARD FUSELAGE STATION 260 LONGERON 16 LEFT HAS A GOUGE/DENT APPROXIMATELY 2 INCHES LONG. DYE CHECKED GOUGE NO CRACKS FOUND. REMOVED GOUGE PER SRM 53-01-00. INSTALLED DOUBLER PER BOEING REPAIR DRAWING SG09530001 REVISION A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

CRACK ON LEFT FORWARD ENTRY DOOR JAM WEB AT STATION 206 LONGERON 15 LEFT. INSTALLED REPAIR STRAP PER AARD 53-10-00-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,042 hrs · 15,572 cycles

DENT APPROXIMATELY .030 DEEP ON LEFT OF FUSELAGE LOCATED APPROXIMATELY 27 INCHES AFT AND INLINE WITH TOP OF PASSENGER DOOR. INSTALLED DOUBLER PER BOEING DRAWING SG09530001 REVISION A.

Part: BRACKET — CRACKED (LE SLAT) · airframe 33,042 hrs · 15,572 cycles

RIGHT NUMBER 5 SLAT OUTBOARD TRACK BRACKET CRACKED. REPLACED DAMAGED OUTBOARD RIB PER ESO 80117 CHAPTER 27-80-01.

Part: PAN — CRACKED (WINDOW) · airframe 33,042 hrs · 15,572 cycles

WINDOW RING PAN CRACKED, LOWER FORWARD CORNER, RIGHT STATION 984. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: CADC — FAULTY (COCKPIT) · airframe 31,467 hrs · 14,807 cycles

DFW - CREW REPORTED FLIGHT MANAGEMENT ANNUNCIATOR MALFUNCTIONED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE CENTRAL AIR DATA COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,081 hrs · 14,627 cycles

FORWARD CEILING EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN FORWARD CEILING. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,081 hrs · 14,627 cycles

FOUND CEILING EMERGENCY LIGHTS IN ROWS 20 TO 25 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT POSITION B5-106. OPS CHECKED NORMAL.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,302 hrs · 13,812 cycles

INBOARD UPPER TRAPEZOID FITTING ATTACH ANGLE CORRODED OUT OF LIMITS IN RIGHT MAIN WHEEL WELL. REPLACED TRAPEZOID FITTING PER SRM 51-01-00.

Part: CASTING — CRACKED (SPOILER) · airframe 28,232 hrs · 13,340 cycles

LEFT GROUND SPOILER CASTING CRACKED. INSTALLED NEW SPOILER CASTING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,192 hrs · 13,321 cycles

EMERGENCY LIGHT BATTERY PACK WEAK. REPLACED BATTERY PACK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,132 hrs · 13,291 cycles

EMERGENCY OVERHEAD AISLE LIGHTS BETWEEN ROW 18 THRU 21 ARE VERY DIM. REPLACED BATTERY PACK FOR THAT SECTION PER MAINTENANCE MANUAL, OPS CHECKED OK.

Part: PUMP — INOPERATIVE (FUEL BOOST)

DFW - INFLIGHT T2430/06JUN - RIGHT AC BUSS AND AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKERS POPPED IN FLIGHT. RETURNED DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR EVALUATION. REPLACED CENTER BOOST PUMP AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PISTON — INOPERATIVE (NLG)

ORD INFLIGHT T1637/02FEB - RECEIVED UNSAFE NOSE GEAR UP INDICATION. COULD HEAR LOUD NOISE WHEN GEAR WAS RETRACTED. SUSPECTED GEAR DOORS WERE OPEN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT PISTON. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PSEU — INOPERATIVE (NLG)

EWR INFLIGHT T429/30JAN - GEAR UNSAFE LIGHT ILLUMINATED DURING LANDING GEAR RETRACTION. CYCLED GEAR WITH NO HELP. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONIC UNIT FOR NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY EXIT LIGHT ON FORWARD GALLEY WALL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT ON FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - OVERHEAD EMERGENCY LIGHTS AT ROWS 29 TO 32 AND COCKPIT INOPERATIVE. REPLACED BATTERY PACKS AT OVERHEAD ACROSS FROM FIRST CLASS LAVATORY AND B5107 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 29 TO 32 AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY TAIL COMPARTMENT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TIRE — SEPARATED (NR 4)

DFW - RIGHT ENGINE COMPRESSOR STALL ON TAKEOFF DUE TO THREAD SEPARATION OF NUMBER FOUR TIRE RESULTING IN FOD DAMAGE TO RIGHT HAND ENGINE. SHUTDOWN RIGHT ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION AND REPAIRS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 8,353 hrs · 4,612 cycles

DURING CHECK-C FOUND ON THE FWD LT FUSELAGE ALL BLIND FASTENERS IN A LARGE REPAIR AT STA 218, LONGERON 18L TO 19L. REMOVED EXISTING REPAIR. CUTOUT DAMAGED SKIN AND INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 12B, SHEET 34.

Part: DOOR — CRACKED (LT MLG) · airframe 5,898 hrs · 3,150 cycles

DURING CHECK-C MAINT FOUND 2 INCH CRACK IN THE LT MAIN LANDING GEAR DOOR AT AFT OUTBOARD CORNER. LEFT MLG DOOR REPAIRED ON INTERSHOP WORK ORDER 816804 AND INSTALLED PER SRM 51-00 STANDARD PRACTICES. PARTS INSTALLED WET.

Part: BATTERY — DISCHARGED (ROW 21) · airframe 2,454 hrs · 1,369 cycles

THE OVERWING EXIT LIGHTS LT AND RT ABOVE ROW 21 DID NOT ILLUMINATE, AND THE MID CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK FOR THE EMERGENCY LIGHTS, AND SECURED LOOSE WIRE ON EGRESS LIGHTS. NO CHECK-C.