N980TW

Part: WINDSHIELD — DAMAGED (FIRST OFFICER'S) · airframe 52,067 hrs · 26,677 cycles

FOUND A SCRATCH AND CRACK ON THE FIRST OFFICER`S WINDSHIELD. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE FIRST OFFICER`S WINDSHIELD IAW MM 56-10-02, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 51,981 hrs · 26,617 cycles

FORWARD PORTABLE EMERGENCY LIGHT DID NOT OPERATE NORMALLY. MAINTENANCE REPLACED EMERGENCY LIGHT AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-53-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,494 hrs · 26,293 cycles

DFW - THE AIRCRAFT WAS GROUNDED. CEILING EMERGENCY LIGHTS AT AFT SERVICE DOOR AND ROWS 28-30 INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK B5-107 OPS CHECKS GOOD REF WDW 33-51-12. (SEE ALSO SDR AALA201809149024).

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,494 hrs · 26,293 cycles

DFW - THE AIRCRAFT WAS GROUNDED. REPLACED BATTERY PACK FOR ITEM 2 BS-107. SUSPECT BAD FROM STOCK. BATTERY PACK WAS REPLACED. (SEE ALSO SDR AALA201809149023)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,407 hrs · 26,240 cycles

SEAT 4E FORWARD EMERGENCY LIGHT LENS WAS MISSING. REPLACED THE LENS IAW MM 33-53-00. OPS CHECKED OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,407 hrs · 26,240 cycles

LEFT CEILING EMERGENCY LIGHT AT ROW 23 WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY PACK B5-106 IAW MM 33-53-00. OPS CHECKED OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 51,407 hrs · 26,240 cycles

LEFT CEILING EMERGENCY LIGHT AT ROW 25 WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY PACK B5-106 IAW MM 33-53-00. OPS CHECKED OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 51,407 hrs · 26,240 cycles

LEFT CEILING EMERGENCY LIGHT AT ROW 27 WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY PACK B5-106 IAW AMM 33-53-00. OPS CHECKED OK.

Part: GENERATOR — FAILED (LEFT) · airframe 51,307 hrs · 26,169 cycles

CLIMBING THORUGH FLIGHT 280, THE ELECTRICAL SYSTEM STARTED FLASHING ON AND OFF. ALL THE CAPTAINS INSTRUMENTS BEGAN FLASHING. AUTOPILOT AND AUTO THROTTLE DISCONNECTED. LEFT GENERATOR FAIL LIGHT CAME ILLUMINATED. CENTER FUEL PRESSURE LOW LIGHT. DID NOT GET AC X TIE LIGHT. THE AIRCRAFT WAS GROUNDED. REPLACED LT ENGINE GENERATOR PER AMM 24-10-01. OPERATIONS AND LEAK CHECKS GOOD.

Part: CSD — FAILED (LEFT) · airframe 51,307 hrs · 26,169 cycles

THE AIRCRAFT WAS GROUNDED. CLIMBING THORUGH FLIGHT 280, THE ELECTRICAL SYSTEM STARTED FLASHING ON AND OFF. ALL THE CAPTAINS INSTRUMENTS BEGAN FLASHING. AUTOPILOT AND AUTO THROTTLE DISCONNECTED. LEFT GENERATOR FAIL LIGHT CAME ILLUMINATED. CENTER FUEL PRESSURE LOW LIGHT. DID NOT GET AC X TIE LIGHT. REPLACED THE LT CSD.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,178 hrs · 26,095 cycles

FORWARD EMERGENCY EXIT LIGHTS BALLAST WAS INOPERATIVE. COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BALLAST IAW MM 33-53-00. OPS CHECKED GOOD.

Part: HANDLE — OUT OF ADJUST (STERN DOOR) · airframe 51,009 hrs · 25,974 cycles

AFT TAILCONE EMERGENCY EXIT DOOR HANDLE COVER WILL NOT LATCH UP IN THE DISARM POSITION. MAINTENANCE ADJUSTED THE AFT TAILCONE DOOR EXIT HANDLE LATCH AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 50,999 hrs · 25,961 cycles

NOTIFIED BY THE CREW, THE L1 DOOR SLIDE WAS NOT ENGAGED. INSTALLED THE L1 DOOR SLIDE IAW AMM 25-62-00.

Part: PLACARD — PEELING (CABIN) · airframe 50,654 hrs · 25,710 cycles

LEFT FORWARD LOWER LIGHT EMERGENCY EXIT STICKER PEELING FROM OVERING EXIT. REPLACED ESCAPE PATH EXIT SIGN MARKER.

Part: PLACARD — PEELING (CABIN) · airframe 50,654 hrs · 25,710 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT STICKER PEELING. REPLACED THE STICKER.

Part: PLACARD — PEELING (CABIN) · airframe 50,654 hrs · 25,710 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT EXIT STICKER PEELING. REPLACED THE STICKER.

Part: PLACARD — PEELING (CABIN) · airframe 50,654 hrs · 25,710 cycles

LEFT AFT OVERWING EXIT EMERGENCY LIGHT EXIT STICKER PEELING. REPLACED THE PLACARD.

Part: BRACKET — CRACKED (MID CARGO DOOR) · airframe 50,459 hrs · 25,583 cycles

MID CARGO DOOR FORWARD EDGE STOP BRACKET CRACKED. INSTALLED A NEW STOP PAD BRACKET IAW 51-00-05-1 AND DRAWING 5910141.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,459 hrs · 25,583 cycles

VISUAL INDICATION OF A CRACK IN FUSELAGE SKIN AT LEFT NLG, AFT FOLLOW-UP DOOR, AFT HINGE AT PREVIOUS ROUT-OUT. INSTALLED A DOUBLER IAW SRM 53-05-00.

Part: SKIN — CRACKED (BS 89-101) · airframe 50,459 hrs · 25,583 cycles

CRACKED FUSELAGE SKIN AT LEFT NOSE LANDING GEAR, AFT FOLLOW-UP DOOR, AFT HINGE AT PREVIOUS ROUT-OUT. INSTALLED REPAIR DOUBLER PER SRM 53-05-00-001, FIGURE 158.

Part: BATTERY PACK — WEAK (CABIN) · airframe 50,459 hrs · 25,583 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. EMERGENCY LIGHT PACK B5-107 WEAK. REPLACED BATTERY PACK PER AMM 33-53-00.

Part: PLACARD — BROKEN (GALLEY DOOR) · airframe 50,373 hrs · 25,525 cycles

SELF ILLUMINATING EXIT PLACARD WAS FOUND BROKEN ABOVE FORWARD GALLEY SERVICE DOOR. REPLACED SELF ILLUMINATING EXIT PLACARD IAW AMM 11-00-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,821 hrs · 24,527 cycles

EMERGENCY LIGHT BY THE R1 DOOR HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-53-01. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 48,728 hrs · 24,474 cycles

THE AIRCRAFT WAS NOT GROUNDED. FA REPORTED AFT FLASHLIGHT INOP. CHECKED AND REPLACED AFT (FWD) BATTERY PACK FOR FLASHLIGHT PER AMM 25-60-00, AND OPS CKS NORMAL PER 25-60-00, INSTALLED NEW TAMPER STRAP.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 48,667 hrs · 24,431 cycles

THE AIRCRAFT WAS NOT GROUNDED. ON FINAL APPROACH GEAR HANDLE POSITIONED TO DOWN. RIGHT MAIN GEAR NOT GREEN. OTHER GEAR DOWN AND LOCKED. GEAR DOOR OPEN LIGHT NOT ON. NO OTHER RED LIGHT ILLUMINATED. TOWER FLYBY CONFIRMED GEAR DOWN. AN EMERGENCY WAS DECLARED AND THE QRH WAS COMPLIED WITH. LANDED RWY 31R UNEVENTFUL MAINTENANCE PINNED ALL 3 GEAR AT RUNWAY. REMOVED AND REPLACED 4 EA BULBS PER M/M 32-60-03. OPS CK GOOD. REMOVED GEAR PINS AND STOWED IN A/C.

Part: PIN — SHEARED (SERVICE DOOR) · airframe 48,547 hrs · 24,358 cycles

THE AIRCRAFT WAS GROUNDED. AFT SVC DOOR HANDLE RETAINING PIN SHEARED OFF. REMOVED AND REPLACED AFT SERVICE DOOR SHAFT HANDLE ASSEMBLY IAW CMM 52-40-03.

Part: SLIDE — DEFECTIVE (SERVICE DOOR) · airframe 48,376 hrs · 24,253 cycles

CREW REPORTS FWD SERVICE DOOR GIRT BAR LOOSE. FOUND SERVICE DOOR RESTING ON CATERING TRUCK WITH SLIDE PACK LOOSE. APPEARS SLIDE PACKING PIN HAS PULLED LOOSE. REPLACED R1 DOOR SLIDE AS REQ USING MCM CARD 25-94-20. THE AIRCRAFT WAS GROUNDED.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 47,914 hrs · 23,942 cycles

EMERGENCY EXIT SIGN NEAR FLOOR ADJACENT TO THE FORWARD LAVATORY IS DETACHED. INSTALLED LIGHT ASSEMBLY IAW AMM 33-53-01. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 47,218 hrs · 23,496 cycles

LEFT MAIN LANDING GEAR WHEEL WELL INTERCOSTAL CRACKED AT AFT END OF KEEL BEAM. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-60-00 AND DRAWING 5936395.

Part: GUSSET — CRACKED (LT MLG WW) · airframe 47,218 hrs · 23,496 cycles

LEFT MAIN LANDING GEAR WHEEL WELL INTERCOSTAL GUSSET CRACKED AT AFT END OF KEEL BEAM. REMOVED AND REPLACED GUSSET IAW SRM 51-60-00 AND DRAWING 5936395.

Part: COMPUTER — FAULTY · airframe 47,114 hrs · 23,424 cycles

DURING TAKE OFF ROLL NR 2 ENGINE EPR INDICATION LAGGED SIGNIFICALLY BEHIND NR 1 ENGINE. N1, EGT AND N2 MATCHED. REMOVED AND REPLACED THE NR 2 ENGINE EPR COMPUTER IAW AMM 77-11-02. AIRCRAFT WAS GROUNDED.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 46,635 hrs · 23,134 cycles

R1 DOOR SLIDE BOTTLE PRESSURE READS OUTSIDE OF THE GREEN BAND. REMOVED AND REPLACED R1 DOOR SLIDE IAW IAW WORK CARD 25-94-20.

Part: COOLING FAN — BURNED (ZONE 200) · airframe 45,860 hrs · 22,670 cycles

AIRCRAFT WAS GNDED. DURING PAX BOARDING, EXTERNAL POWER WAS DISCONNECTED. APU OVER TEMP WITH BOTH PACKS OPERATING. SHUT OFF LT PACK. AFTER 10 MINUTES RT PACK SHOWED FLOW LOSS. SHUTOFF RT PACK & RESTARTED LT PACK. A BURNING SMELL & SMOKE REPORTED IN CABIN. APU, BOTH PACKS & RECIRCULATION FAN SHUTOFF. PAXS DEPLANED. MAINTENANCE FOUND LEFT GROUND COOLING FAN AND CONNECTOR P1-173 BURNED. REMOVED AND REPLACED COOLING FAN IAW AMM 21-20-06 AND CONNECTOR IAW SWPM 20-31-00, WDM 21-22-00 AND EA 259619. SEE ALSO AALA20160411002. SUPPLEMENTAL (CLOSED)

Part: CONNECTOR — BURNED (ZONE 200) · airframe 45,860 hrs · 22,670 cycles

AIRCRAFT WAS GNDED. DURING BOARDING EXTERNAL POWER WAS DISCONNECTED. APU OVER TEMPED WITH BOTH PACKS OPERATING. LT PACK OFF, AFTER 10 MINS RT PACK FLOW LOSS, RT PACK OFF, LT PACK ON. BURNING SMELL & SMOKE REPORTED IN CABIN.. APU, PACKS & RECIRCULATION FAN SHUT OFF. PAXS DEPLANED. FOUND LT GND COOLING FAN & CONNECTOR P1-173 BURNED. R & R COOLING FAN IAW AMM 21-20-06 & CONNECTOR IAW SWPM 20-31-00, WDM 21-22-00 & EA 259619. SEE ALSO AALA 20160408005.

Part: ACM — LEAKING (AC BAY) · airframe 45,850 hrs · 22,664 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, FLIGHT ATTENDANT REPORTED SMOKE FROM TAIL CONE AREA. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING CARD MCM 21-96-01 & FOUND LT AIR CYCLE MACHINE LEAKING OIL. R & R AIR CYCLE MACHINE IAW MCM 21-94-01.

Part: HYDRAULIC LINE — BROKEN (HYDRAULIC SYS) · airframe 45,483 hrs · 22,435 cycles

AT CRUISE, JUST PRIOR TO DESCENT, LT HYD LOW PRESS LIGHT CAME ON. LT HYD QTY WENT TO 5. CREW TURNED THE HYD PUMP OFF. AN EMER WAS DECLARED. UPON LANDING, QTY WENT TO 1. LT T/R DEPLOYED BUT DID NOT STOW. REPLACED LT PRESS FILTER INBD HYD LINE & UNION IAW PP GPM, NO LEAKS NOTED. THE ACFT WAS GNDED.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 45,474 hrs · 22,429 cycles

THE ANNUNCIATOR TEST SWITCH WAS ACCIDENTALLY CONTACTED DURING FLIGHT. ANNUNCIATOR TEST SWITCH STUCK IN TEST MODE & WOULD NOT DISENGAGE. ALL ANNUNCIATOR & WARNING LIGHTS REMAINED ON FOR THE DURATION OF THE FLIGHT. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. R & R SWITCH S1-134 TEST SWITCH IAW WDM 33-17-02 & AMM 33-10-00. OPERATIONALLY CHECKED OK. THE ACFT WAS GNDED.

Part: TARGET — OUT OF ADJUST (CARGO DOOR) · airframe 45,465 hrs · 22,424 cycles

AIRCRAFT WAS GNDED. FWD CARGO DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 100 KNOTS. CLEANED DEBRIS FROM DOOR OPENING & ADJUSTED TARGET GAP IAW 52-70-02. OPERATIONAL CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 44,831 hrs · 22,025 cycles

DURING TAKEOFF ROLL KNOTS THE FWD CARGO DOOR WARNING LIGHT ILLUMINATED. TAKEOFF WAS REJECTED AT 70 KNOTS. ADJUSTED THE TARGET SENOR GAP & PERFORMED OPERATIONAL CHECK OF CARGO DOOR IAW AMM 52-70-02. SYS CHECKED NORMAL.

Part: TRANSDUCER — BROKEN (MLG) · airframe 43,825 hrs · 21,392 cycles

DURING TAKEOFF, WHEEL NOT TURNING, LIGHT ILLUMINATED AT 90 KNOTS, TAKEOFF ABORTED. LIGHT EXTINGUISHED AS POWER REDUCED. FOUND NR 1 MAIN WHEEL SPEED TRANSDUCER MISSING BOTH PINS. R & R TRANSDUCER IAW AMM 32-43-02.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

DEEP BLEND OUT IN SEAT TRACK NR 2 BETWEEN FS 1100 & 1102. R & R SECTION OF NR 2 SEAT TRACK BETWEEN FS 1088 & 1183 IAW AMM 53-40-01.

Part: RIB — CRACKED (LT WING) · airframe 43,619 hrs · 21,275 cycles

LEFT WING NR 4 SLAT INBD LE RIB, MACHINED AREA FOR RIBLET REPAIR SHOWS CRACK INDICATION AT THE AFT SIDE. R & R RIB IAW SRM 51-30-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

FUSELAGE SKIN CRACKED AT NLG DOOR AFT HINGE CUT OUT, FS 110 & LONGERON 28R. REPAIRED SKIN IAW EA 250976 & SRM 53-05-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

AFT CARGO COMPARTMENT RT TIE DOWN TRACK AT STRINGER 26R IS CORRODED BETWEEN FS 1212 & 1320. R & R TRACK IAW SRM 51-30-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

AFT CARGO COMPARTMENT LT AFT TIE DOWN TRACK CORRODED BETWEEN FS 1220 & 1309 AT LONGERON 26L. R & R TRACK IAW SRM 51-30-01 & 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

CABIN SEAT TRACK NR 4 CORRODED BETWEEN FS 1088 & 1309. R & R SEAT TRACK IAW SRM 53-05-00-001 FIG 4F & AMM 53-40-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

AFT CARGO LT CTR TIE DOWN TRACK CORRODED BETWEEN FS 1107 & 1220 AT LONGERON 26L. R & R TRACK IAW SRM 51-30-01 & 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

RIGHT CUSP SHEET CORRODED BETWEEN FS 788 & 807. R & R CUSP SHEET IAW SRM 53-14-02-001, DWG EDK3238, DWG 9930538, DWG 53630 & 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

RIGHT CUSP SHEET CORRODED BETWEEN FS 712 & 788. R & R CUSP SHEET IAW SRM 53-14-02-001, DWG FDK3241, DWG 9930538, DWG 53630 & 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

LEFT CUSP SHEET CORRODED BETWEEN FS 1174 & 1178. REPAIRED CUSP SHEET IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

CABIN G2 GALLEY INBD MOUNT AT FS 218 & RBL 10 IS CORRODED. R & R MOUNT IAW SRM 51-00-05-1, DWG CDK-2396, DWG 9936535 & DWG 53630.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

EXISTING LT CUSP SHEET SPLICE DOUBLER REPAIR AT FS 1162 TO 1174 HAS CRACKED TAB AT STATION 1174. REMOVED EXISTING DOUBLER, REPAIRED CUSP SHEET IAW SRM 53-05-00 FIG 131A-21 & AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

SEAT TRACK NR 4 CORRODED BETWEEN FS 264 & 265. INSTALLED SEAT TRACK PLUG IAW SRM 53-05-00-001.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

CRACK IN INTERCOSTAL STIFFENER BETWEEN FS 1463 & 1485 AT L19L. R & R STIFFENER IAW PRINT 9911946 & SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

CABIN SEAT TRACK NR 4 CORRODED OUT OF LIMITS BETWEEN FS 1012 TO 1088. R & R SEAT TRACK NR 4 FROM STATION 1012 - 1088 IAW SRM 53-05-00-001.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

FASTENER HOLE OUT OF ROUND IN INBD SIDE OF HAT CHANNEL AT FS 179 RT. REPAIRED CHANNEL IAW AARD 53-20-00.

Part: KEELBEAM — CRACKED (BS 965-984) · airframe 43,619 hrs · 21,275 cycles

RIGHT WW KEEL BEAM WEBBING CRACKED ABOVE GEAR DOOR HINGE, 12" FROM AFT END. INSTALLED DOUBLER IAW SRM 53-01-00 FIG 4 & SRM 51-30-02-001.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

FORWARD CABIN WEB TAB IS CRACKED AT STATION 202 & L11L. REPAIRED IAW AARD 53-10-00-11 & SRM 51-30.

Part: HINGE FITTING — CRACKED (BS 83.5) · airframe 43,619 hrs · 21,275 cycles

NOSE WW SUPPORT BEAM CRACKED AT LT AFT HINGE OF FWD DOOR. INSTALLED 8130 HINGE SUPPORT IAW AARD 51-00-05-1 & DWG 9957851.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

AFT CARGO, CORROSION ON BOTTOM SIDE OF WEB FROM STATION 1203 TO 1218 ABOVE LONGERON 27R - 28R. REPAIRED WEB IAW 53-10-00-24.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,619 hrs · 21,275 cycles

FORWARD CABIN WEB TAB IS CRACKED AT STATION 202 & L15L. REPAIRED IAW AARD 53-10-00-11 & SRM 51-30.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

AFT CARGO DOOR CUT OUT, CORROSION EMITTING FROM BELOW DOUBLER ON LOWER FRAME BETWEEN STATIONS 1169 - 1190 AT LONGERON 27R. REMOVED DOOR BEAM DOUBLER, REMOVED CORROSION FROM DOOR BEAM, INSTALLED DOOR BEAM DOUBLER IAW AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,619 hrs · 21,275 cycles

LOWER SIDE OF LEFT CUSP IS CORRODED BETWEEN STATIONS 693 & 712. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: RIB — CRACKED (RT WING) · airframe 43,619 hrs · 21,275 cycles

RIGHT WING NR 4 SLAT TRACK INBD SUPPORT RIB IS CRACKED AT XIS 134.546. REPAIRED RIB IAW EA 250763 DATED 5 7 2015.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 41,024 hrs · 19,882 cycles

TOP HOLE IN LOWER WRAP AROUND LT SIDE MARKED NR 13 IS WORN. ACCOMPLISHED REPAIR IAW EA MD80-55-034804.

Part: SUPPORT BEAM — CRACKED (NLG WW) · airframe 40,036 hrs · 19,398 cycles

NOSE WW SUPPORT BEAM CRACKED ABOVE AFT HINGE ON FWD LT HAND NOSE GEAR DOOR. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA MD80-53-033084.

Part: CLAMP — LOOSE (AC BAY) · airframe 39,364 hrs · 19,004 cycles

ORD CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LT HAND PACK HEAT EXCHANGER OUTLET DUCT CLAMP LOOSE. ADJUSTED BOOT & TIGHTENED CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 39,256 hrs · 18,949 cycles

SAT INFLIGHT DFW-MTY CREW REPORTED CABIN PRESSURIZATION FLOW LIGHT ILLUMINATED. FLIGHT DIVERTED SAT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR & NR 2 CABIN PRESSURE CONTROLLERS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: SENSOR — FAULTY (AC BAY) · airframe 39,179 hrs · 18,905 cycles

DFW CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT & RT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: DUCT — LEAKING (AC BAY) · airframe 38,982 hrs · 18,795 cycles

TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMB-OUT. REPLACED LEAKING RT HEAT EXCHANGER DUCT & LT CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL.

Part: CLAMP — LEAKING (AC BAY) · airframe 38,972 hrs · 18,789 cycles

TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB OUT. QRH PROCEDURES ACCOMPLISHED & LIGHT WENT OUT. FOUND RT PACK CLAMP BETWEEN AIR CYCLE MACHINE & PRIMARY HEAT EXCHANGER LEAKING. INSTALLED 2 SHIMS & TORQUED CLAMP. SYSTEM GROUND CHECKED NORMAL.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 37,847 hrs · 18,182 cycles

PUB - INFLIGHT DEN-DFW. CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT AND CABIN. EMERGENCY DECLARED FLIGHT DIVERTED PUB LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH COALESCER BAGS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 34,763 hrs · 16,614 cycles

CORROSION ON FORWARD RIGHT SUBFLOOR STATION 199 INBOARD OF FIBERGLASS HAT CHANNEL. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 34,749 hrs · 16,607 cycles

CORROSION ON AFT DOOR JAMB WEB UNDER RIGHT TIE-DOWN TRACK, STATIONS 1215 LONGERON 28 RIGHT. REMOVED AND REPLACED WEB SECTION PER AARD 53-10-00-24.

Part: BEAM — CORRODED (FUSELAGE) · airframe 34,733 hrs · 16,601 cycles

CORROSION ON LOWER DOOR BEAM LONGERON 28 RIGHT AT STATION 1163. INSTALLED FULL LENGTH DOOR BEAM REPAIR DOUBLER PER AARD 51-10-00-3 AND EA MD80-53-021252.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,733 hrs · 16,601 cycles

CORROSION ON LEFT CUSP 1309, INBOARD SIDE OF NUMBER 1 SEAT TRACK. INSTALLED NEW CUSP SHEET FROM STATIONS 1250 TO 1309 PER AARD 51-10-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,489 hrs · 16,001 cycles

DENT IN FUSELAGE AT STATION 255 BELOW LONGERON 22 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-04-03 AND DRAWING SG09530002 ZONE 179 THROUGH ZONE 185.

Part: CLAMP — LOOSE (AC BAY) · airframe 32,983 hrs · 15,739 cycles

DFW - CREW REPORTED DURING TAKEOFF TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LOOSE CLAMP ON AUGMENTATION VALVE TO PNEUMATIC DUCT. TORQUED CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 32,978 hrs · 15,735 cycles

AFT CARGO CORROSION ON FORWARD LOWER DOOR JAM SUPPORT ANGLE. REMOVED AND REPLACED BRACKET PER AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,978 hrs · 15,735 cycles

AFT CARGO CENTER INTERCOSTAL CRACKED 5 PLACES STATIONS 1287 TO 1309. INSTALLED INTERCOSTAL STATIONS 1287 TO 1309 PER AARD 51-10-00-5.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 32,978 hrs · 15,735 cycles

SCRATCH IN FUSELAGE SKIN STATION 244. INSTALLED EXTERNAL DOUBLER, SKIN PLUG, INTERNAL REPAIR DOUBLER, INTERNAL FILLER, AND INTERNAL REPAIR DOUBLER PER SRM 53-04-00 FIGURE 38.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,978 hrs · 15,735 cycles

FUSELAGE SKIN CRACK AT STATION 796 ON LONGERON RIGHT NUMBER 4. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04-02 AND DRAWING SG09530001 VIEW G2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,978 hrs · 15,735 cycles

RIGHT SIDE 10 INCHES ABOVE CUSP LINE STATION 446 DAMAGED. INSTALLED PERMANENT INTERNAL REPAIR DOUBLER PER SRM 53-04-02 AND BOEING DRAWING SG09530001.

Part: AUGMENT VALVE — INOPERATIVE (AC BAY) · airframe 32,970 hrs · 15,730 cycles

LAX - CREW REPORTED DURING CLIMBOUT SMOKE IN THE AFT CABIN AREA. AFTER CAPTAIN RESTARTED THE APU THERE WAS VISIBLE SMOKE IN THE COCKPIT AS WELL. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT AUGMENTATION VALVE AND LEFT PACK PRESSURE REGULATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,385 hrs · 15,423 cycles

CRACK IN SUB WEBBING OUTBOARD OF NUMBER 2 SEAT TRACK AT STATION 218. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 32,385 hrs · 15,423 cycles

AFT CARGO DOOR BEAM HAS LIGHT CORROSION STATIONS 1160 TO 1198. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,385 hrs · 15,423 cycles

AFT CARGO RIGHT FLOORBOARD SUPPORT STATIONS 1150 TO 1155 CORRODED. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-30-01 AND AARD 51-10-00-5.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 32,385 hrs · 15,423 cycles

LEFT WHEEL WELL CORROSION ON ANGLE ABOVE BRAKE ACCUMULATOR. INSTALLED NEW ANGLE IAW AARD 51-10-00-5. INSTALLED CONNECTORS.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 32,385 hrs · 15,423 cycles

RIGHT WHEEL WELL CHORD ANGLE ABOVE BRAKE ACCUMULATOR CORRODED. INSTALLED NEW CORD ANGLE IAW AARD 51-10-00-5 AND SRM 51-30-1.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 32,385 hrs · 15,423 cycles

RIGHT WHEEL WELL CHORD ANGLE ABOVE BRAKE ACCUMULATOR CORRODED. INSTALLED NEW CORD ANGLE IAW AARD 51-10-00-5 AND SRM 51-30-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,385 hrs · 15,423 cycles

CORROSION BEYOND MANUAL LIMITS ON CUSP SECTION AT LEFT STATIONS 503 TO 579. REMOVED AND REPLACED CUSP WHOLE SECTION FROM LEFT STATIONS 503 TO 579.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,385 hrs · 15,423 cycles

CORROSION ON AFT SIDE OF FRAME AND SHEAR TIES AT STATION 1287, LONGERON 29 LEFT TO LONGERON 29 RIGHT IN THE AFT CARGO. INSTALLED SHEAR TIE ON AFT SIDE OF FRAME, STATION 1287, LONGERON 29 LEFT TO LONGERON 29 RIGHT PER SRM 51-30-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,385 hrs · 15,423 cycles

DENT IN FUSELAGE SKIN BELOW LONGERON 18 LEFT AT STATION 218. INSTALLED REPAIR DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: JOINT — WORN (LE SLAT) · airframe 32,385 hrs · 15,423 cycles

LEFT WING KNUCKLE JOINT WORN OUTBOARD END OF NUMBER 4 SLAT. REPLACED WORN OUTBOARD KNUCKLE JOINT RIB NUMBER 4 LEFT SLAT PER ESO 80117.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,385 hrs · 15,423 cycles

TIE DOWN FOR FORWARD GALLEY HAS CORROSION INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED SERVICEABLE GALLEY MOUNT TIE DOWN PER AARD 51-10-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 32,385 hrs · 15,423 cycles

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

Part: PAN — CRACKED (WINDOW) · airframe 32,385 hrs · 15,423 cycles

CABIN UPPER FORWARD CORNER OF WINDOW PAN CRACKED AT STATIONS 927 TP 946 LONGERON 12 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 32,385 hrs · 15,423 cycles

UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATIONS 1003 TO 1022 LONGERON 15 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 32,385 hrs · 15,423 cycles

LOWER AFT CORNER OF WINDOW PAN CRACKED AT STATIONS 1212 TO 1231 LONGERON 15 RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-5.

Part: PAN — CRACKED (WINDOW) · airframe 32,385 hrs · 15,423 cycles

UPPER AFT CORNER OF WINDOW PAN CRACKED AT STATIONS 1022 TO 1041 LONGERON 15 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-5.

Part: LIGHT — SHORTED (CABIN) · airframe 31,090 hrs · 14,771 cycles

MLI - INFLIGHT MCI-ORD. FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR IN MID CABIN. EMERGENCY DECLARED, DIVERTED MLI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND READING LIGHT AT 22D WITH BLOWN LIGHT BULB. REPLACED LAMP FOR SEAT 22D READING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,879 hrs · 13,737 cycles

CORROSION ON LONGERON 25 RIGHT AT LOWER FASTENER HOLE TO PRIMARY STATIC PORT PLATE. REMOVED CORROSION AND REPAIRED WITH LONGERON SPLICE AND FILLER PER SRM 53-02-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,879 hrs · 13,737 cycles

FRAME CRACKED AT STATION 1418 AT LONGERON 2 RIGHT. INSTALLED DOUBLER PER ENGINEERING AUTHORITY MD80-53-007708 DATED 10-8-09.

Part: DOUBLER — WORN (TE FLAP VANE) · airframe 28,818 hrs · 13,715 cycles

FOUND TWO WEAR GOUGES IN LEADING EDGE OF FLAP-VANE AT INBOARD END OF OUTBOARD FLAP ABOVE INBOARD HINGE OF OUTBOARD FLAP. REMOVED WORN DOUBLER AND INSTALLED NEW HOT-BONDED DOUBLER PER ESO-80096.

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 28,879 hrs · 13,737 cycles

CRACK EXTENDING FROM FASTENER HOLE IN RIGHT NOSE LANDING GEAR DOOR JAMB BEAM AT STATION 48. REPAIRED CRACK PER AARD 53-10-00-4.

Part: BATTERY PACK — WEAK (CABIN) · airframe 28,818 hrs · 13,715 cycles

EMERGENCY LIGHT BATTERY PACK WEAK AT STATION 1057. REMOVED BATTERY PACK AT STATION 1057.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

AFT CARGO DOOR FORWARD SIDE LOWER STOP PAD FITTING CRACKED. REPLACED LOWER FORWARD STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

AFT CARGO DOOR FORWARD SIDE LOWER STOP PAD FITTING CRACKED. REPLACED LOWER FORWARD STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

AFT CARGO DOOR FORWARD SIDE LOWER STOP PAD FITTING CRACKED. REPLACED LOWER FORWARD STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 28,818 hrs · 13,715 cycles

STOP FITTING CRACKED. REPLACED WITH NEW STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (DOOR) · airframe 28,818 hrs · 13,715 cycles

STOP FITTING CRACKED. REPLACED WITH NEW STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

FORWARD SIDE OF DOOR TOP STOP-FITTING CRACKED. REPLACED FORWARD SIDE UPPER STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

FORWARD CARGO DOOR FORWARD SIDE LOWER STOP-PAD FITTING IS CRACKED. REPLACED FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

FORWARD CARGO DOOR FORWARD SIDE THIRD FROM BOTTOM STOP-PAD FITTING CRACKED. REPLACED FITTING PER ESO 80174.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 28,818 hrs · 13,715 cycles

AFT SIDE OF DOOR TOP FITTING CRACKED. REPLACED FITTING PER ESO 80174.

Part: SENSOR — FAULTY (OVERHEAT SYS) · airframe 28,637 hrs · 13,637 cycles

TAIL HIGH TEMPERATURE WARNING INDICATION LIGHT ILLUMINATED. RETURNED BNA AND LANDED WITHOUT INCIDENT. REPLACED LEFT TAIL TEMPERATURE SENSOR.

Part: SENSOR — FAULTY (A/C BAY) · airframe 28,631 hrs · 13,633 cycles

CREW REPORTED TAIL COMPARTMENT OVER TEMP INDICATION AT 18,000 FEET AND DID NOT EXTINGUISH. RETURNED TO SEA AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT TEMPERATURE SENSOR.

Part: ELECTRONIC UNIT — FAULTY (CARGO BAY) · airframe 28,144 hrs · 13,429 cycles

AFT CARGO FIRE INDICATIONS AT 20,000 OUT OF DFW. LEVELED AT 21,000, RETURNED TO DFW BOTH FIRE BOTTLES DISCHARGED. EVEN AFTER BOTTLES DISCHARGED, HAD INTERMITTENT AFT CARGO FIRE INDICATIONS. REPLACED CARGO ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GCU — INOPERATIVE (LEFT)

PDX INFLIGHT T9663/04OCT SEA TO SFO - LEFT GENERATOR FAILED AND RIGHT GENERATOR ON MEL. ONLY AUXILIARY POWER UNIT GENERATOR OPERATING. LANDED PDX WITHOUT INCIDENT. REPLACED LEFT GENERATOR CONTROL UNIT BUS CONTROL UNIT AND LEFT BUS POWER RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (RT ENGINE)

DFW INFLIGHT T2320/15SEP - DURING CLIMB NUMBER TWO ENGINE OIL PRESSURE BEGAN TO DROP. DROPPED RAPIDLY THEN CAME BACK TO NORMAL WHEN THROTTLES BROUGHT BACK TO IDLE. OIL TEMPERATURE INDICATED HIGH. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE OIL PUMP AND CHECKED OIL FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DISLODGED (R1 DOOR)

OKC RIGHT NUMBER ONE DOOR SLIDE DISLODGED FROM DOOR AND FELL TO RAMP. SLIDE WAS NOT ARMED. SLIDE BOTTLE PRESSURE SHOWS ZERO. REPLACED RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DENTED (LT WING) · airframe 8,063 hrs · 4,422 cycles

DURING CHECK-C MAINT THE LT WING FIXED LE 15 INCHES AND 19 INCHES OTBD FROM 0 SLAT OTBD TRACK, FOUND DENT IN LE. INSTALLED REPAIR PER SRM 57-06B, FIG 14.

Part: DUCT — WORN (HEAT EXCHANGER) · airframe 8,063 hrs · 4,422 cycles

DURING CHECK-C MAINT THE FUSELAGE RT SIDE OVERBOARD DUCT FOR THE HEAT EXCHANGER WAS WORN THIN. REPAIRED PER SSRM 53-30-101. REPLACED DUCT PER SPM 6-70-01.

Part: DUCT — WORN (HEAT EXCHANGER) · airframe 8,063 hrs · 4,422 cycles

DURING CHECK-C MAINT THE FUSELAGE LT SIDE OVERBOARD DUCT FOR THE HEAT EXCHANGER WAS WORN THIN. REPAIRED DAMAGE PER SSRM 53-30-101 PAGE 202. REPAIRED AND REPLACED DUCT PER SPM 6-70-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,404 hrs · 4,011 cycles

THE FUSELAGE SKIN WAS DAMAGED AT 6 O'CLOCK, STATION 110 TO 113. TRIMMED OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FIG 12B, SHEET 22.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 7,404 hrs · 4,011 cycles

THE FWD BULKHEAD SUPPORT ANGLE WAS DAMAGED AT STA 110, LBL 2. REPAIRED PER ARA 18260.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 7,404 hrs · 4,011 cycles

THE FORWARD BULKHEAD SUPPORT ANGLE WAS DAMAGED AT STA 110, RBL 2. REPAIRED PER ARA 18260.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,404 hrs · 4,011 cycles

THE FUSELAGE SKIN WAS DAMAGED UNDER THE FWD DRAIN MAST. REPAIRED DAMAGED SKIN UNDER THE FWD DRAIN MAST PER ARA 18254 AND SRM 53-04, FIG 12B.

Part: STRUCTURE — BENT (FUSELAGE) · airframe 7,404 hrs · 4,011 cycles

THE Y-CHORD WAS BENT AT STA 110, LONGERON 28L TO 28R. INSTALLED NEW Y-CHORD PER ARA 18257, BETWEEN LONGERON 26L AND 26R.

Part: FAN BLADE — FOD (NR 2 ENGINE) · airframe 2,153 hrs · 1,202 cycles

THE RT ENGINE HAD STRONG COMPRESSOR STALLS AFTER TAKEOFF. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO STL. FOUND FOREIGN OBJECT DAMAGE TO THE FAN CASE AND FAN BLADES. THE FOREIGN OBJECT WAS NOT IDENTIFIED. REPLACED TWO SETS OF BLADES, (P/N A03779-4), AND THE FAN CASE, (P/N 799482). NO CHECK-C.