N979TW

Part: SUPPORT — CRACKED (LT WING) · airframe 52,709 hrs · 26,978 cycles

LEFT WING GROUND SPOILER ACTUATOR SUPPORT WAS FOUND CRACKED. REPLACED THE SUPPORT IAW SRM 51-30-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,709 hrs · 26,978 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SKIN AT STATION 1380 L14R. REPLACED SKIN DOUBLER PER 53-30-00-02 AND SRM 53-34-00-001.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 52,636 hrs · 26,929 cycles

L2 DOOR SLIDE PRESSURE WAS LOW. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED L2 SLIDE IAW 25-94-17.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 52,035 hrs · 26,551 cycles

LEFT LOWER, EMERGENCY LIGHT HAS A BROKEN WIRE. INSTALLED A NEW CONNECTOR. OPS CHECKED OK IAW MM 20-31-01.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 52,004 hrs · 26,531 cycles

AIRCRAFT WAS GROUNDED. CHECK FIRST OFFICERS WINDSHIELD FOR DELAMINATION. R1 WINDOW WAS REPLACED. REFERENCE DATED FOR 7/11/18 FOR ALL REFERENCES AND SIGNATURES OF WORK PERFORMED.

Part: RELAY — BURNED (CABIN LIGHTS) · airframe 50,769 hrs · 25,734 cycles

NR 1 FA REPORTED A BURNING ELECTRICAL ODOR AT THE SAME TIME THE AFT CABIN LIGHTS WOULD NOT COME ON. AFTER LANDING AND AT THE GATE, THE LIGHT CAME ON WITH NO ELECTRICAL ODOR. THE AIRCRAFT WAS GROUNDED. INSTALLED A NEW RELAY FOR THE AFT UPPER LIGHTING IAW WDM 33-22-02. OPS CHECKED GOOD IAW 33-21-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,875 hrs · 25,156 cycles

CRACK ON FUSELAGE SKIN BETWEEN BS 37 AND 110, RIGHT NOSE LANDING GEAR ABOVE AFT STRUT DOOR HINGE BEYOND STOP DRILL. REPAIRED IAW SRM 53-05-00-001.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 49,875 hrs · 25,156 cycles

CORROSION ON LEFT WING OUTBOARD FORWARD FLAP CENTER HINGE FITTING AT LOWER OUTBOARD STUD ATTACH POINT. REMOVED AND REPLACED HINGE FITTING IAW AMM 57-40-01-201

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,875 hrs · 25,156 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON RIGHT MAIN LANDING GEAR WHEEL WELL LOWER SIDE OF TRAPEZOID ANGLE ABOVE THE BRAKE ACCUMULATOR. REMOVED AND REPLACED ANGLE PER SRM 57-01-00, AARD 51-00-05-1, AND DRAWING 5930516.

Part: ANGLE — CORRODED (LT MLG WW) · corrosion level 2 · airframe 49,875 hrs · 25,156 cycles

CORROSION ON LEFT MAIN LANDING GEAR WHEEL WELL LOWER SIDE OF TRAPEZOID ANGLE ABOVE THE BRAKE ACCUMULATOR. REMOVED AND REPLACED ANGLE IAW SRM 51-30-02-001.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 49,875 hrs · 25,156 cycles

CORROSION ON RIGHT WING OUTBOARD FLAP CENTER HINGE FITTING AT UPPER AND LOWER STUDS. REMOVED AND REPLACED HINGE FITTING PER AMM 57-40-01-201

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,875 hrs · 25,156 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK ON FORWARD CARGO DOOR AFT BOTTOM STOP PAD FITTING (BRACKET). REMOVED AND REPLACED STOP PAD FITTING PER AARD 51-00-05-1 AND DRAWING 5910141.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 49,202 hrs · 24,725 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 49,131 hrs · 24,679 cycles

FORWARD ENTRY EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED THE BATTERIES IN FLASHLIGHT IN FC AND SECURITY STRAP IAW MM 25-60-00 OK FOR SERVICE.

Part: LEVER — OBSTRUCTED (GIRT BAR) · airframe 48,293 hrs · 24,167 cycles

R1 EMERGENCY DOOR GIRT BAR IS DIFFICULT TO REMOVE FROM ARMED POSITION ON THE FLOOR. CLEANED DEBRIS FROM GIRT BAR LEVER. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 48,266 hrs · 24,150 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT GALLEY SERVICE BAR IS DISCHARGED. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,416 hrs · 23,613 cycles

WHILE ACCOMPLISHING WORK CARD 5403, EMERGENCY POWER SUPPLY BATTERY AB5-1 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPS CHECKED NORMAL

Part: DUCT — LOOSE (AC BAY) · airframe 46,462 hrs · 23,034 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, ACFT WOULD NOT PRESSURIZE. FOUND RUBBER DUCT CAME LOOSE ON LT PACK. SECURED DUCT ON LT PACK & ACCOMPLISHED LEAK & OPERATIONAL CHECK IAW AMM 21-00-00-501.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,219 hrs · 22,882 cycles

CRACK IN WEB SKIN OTBD OF STIFFENER OF 1463 CANT FRAME INSIDE LT LOUVER BOX ASSEMBLY. INSTALLED DOUBLER REPAIR IAW SRM 53-03-00 FIGURE 38 & EA 258286. ACFT IN BASE MX.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,219 hrs · 22,882 cycles

RIGHT AFT TIE DOWN TRACK IN AFT CARGO HAS CORROSION. REPLACED TIE DOWN TRACK IAW SRM 51-01-00. ACFT IN BASE MX.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,219 hrs · 22,882 cycles

AFT CARGO CORROSION AT RT TIE DOWN TRACK, STATION 1117 - 1155. REPLACED CARGO TIE DOWN TRACK IAW SRM 51-01-00. ACFT IN BASE MX.

Part: BULKHEAD — DENTED (NLG WW) · airframe 46,219 hrs · 22,882 cycles

NOSE LANDING GEAR AFT BULKHEAD, STATION 110, HAS DENT IN LOWER LT SIDE. COMPLETED REPAIR DOUBLER INSTALLATION IAW SRM 51-70-04-001. ACFT IN BASE MX.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,219 hrs · 22,882 cycles

COCKPIT FIRST OFFICERS OTBD SEAT TRACK IS CORRODED. R & R FIRST OFFICERS OTBD SEAT TRACK IAW AARD 51-00-05-1. ACFT IN BASE MX.

Part: STRUT — CORRODED (ZONE 700) · corrosion level 2 · airframe 46,219 hrs · 22,882 cycles

BORE G2 MACHINED TO 1.685 INCH TO REMOVE CORROSION, MAX REWORK DIMENSION 1.597 INCH. PART SCRAPPED. DOES NOT MEET ULTIMATE STRENGTH LIMITS IAW ENGINEERING. COMPONENT IN SHOP MX.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 45,990 hrs · 22,734 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB RECEIVED A PRESS FLOW LIGHT INDICATION. ACCOMPLISHED BY SOUND OF RUSHING AIR. THE LIGHT EXTINGUISHED, BUT THE CABIN WOULD NOT PRESSURIZE. ACCOMPLISHED TROUBLESHOOTING PROCEDURE IAW AMM 21-32-00 WITH NO FAULTS FOUND. R & R NR 2 PRESS CONTROLLER, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 45,981 hrs · 227,428 cycles

AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT AFT GALLEY POSITION EMER FLASHLIGHT BATTERY IS INOPERATIVE. R & R BATTERY PACK. OPERATIONAL CHECKED GOOD IAW AMM 25-60-00.

Part: TUBE — CORRODED (ZONE 700) · corrosion level 2 · airframe 45,913 hrs · 22,690 cycles

LANDING GEAR SHOP REPORTS TUBE OD HAS EXCESSIVE CORROSION AROUND PIN BORE. ADDITIONAL MACHINING WILL BRING MAX REWORK BELOW LIMITS. PART SCRAPPED & DESTROYED.

Part: BATTERY PACK — CREW ERROR (EMERGENCY LIGHTS) · airframe 43,728 hrs · 21,419 cycles

DURING PREFLIGHT CREW NOTED EMERGENCY LIGHTS INOPERATIVE. BATTERY SWITCH WAS LEFT ON. BATTERY PACKS WERE DRAINED. REPLACED BATTERY PACK IAW AMM 33-53-00. SYSTEM CHECKED NORMAL.

Part: SELECTOR — FAULTY (CABIN PRESSURE) · airframe 43,693 hrs · 21,396 cycles

AIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB CREW REPORT UNABLE TO PRESSURIZE AIRPLANE & PRESSURIZATION FLOW LIGHT ILLUMINATED. PERFORMED BITE CHECK OF CABIN PRESS CONTROLLERS 1 & 2 WITH CABIN PRESSURIZATION SELECTOR FAULT INDICATED. R & R SELECTOR & PERFORMED OPERATIONAL CHECK IAW AMM 21-32-10. SYS CHECKED NORMAL.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 42,652 hrs · 20,864 cycles

FORWARD ENTRY DOOR NR 6 BEAM CRACKED CTR SECTION. INSTALLED DOUBLER IAW 52-10-00-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,652 hrs · 20,864 cycles

FUSELAGE SKIN CRACKED PAST STOP DRILL AT LT NLG STRUT DOOR AFT HINGE. INSTALLED DOUBLER IAW SRM 53-05-00-001.

Part: RIB — CRACKED (RT WING) · airframe 42,515 hrs · 20,790 cycles

RIGHT WING NR 4 SLAT RIB FOUND CRACKED. INSTALLED REPAIR DOUBLER.

Part: RIB — CRACKED (LT WING) · airframe 42,515 hrs · 20,790 cycles

LEFT WING NR 4 SLAT RIB FOUND CRACKED. INSTALLED REPAIR DOUBLER.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 40,281 hrs · 19,634 cycles

OVERHEAD ESCAPE PATH LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY B5-101. OPERATIONS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 40,281 hrs · 19,634 cycles

OVERHEAD ESCAPE PATH LIGHT AT ROW 9 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY B5-101. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 40,281 hrs · 19,634 cycles

EMERGENCY LIGHT WIRE BROKEN AT CONNECTOR. REPLACED CONNECTOR IN AFT STAIRCASE FOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,518 hrs · 19,213 cycles

FS SKIN DAMAGE AT STATION 247 AT STRINGER 26 LT. INSTALLED DOUBLER REPAIR IAW SRM 53-04-03-001.

Part: REGULATOR — LEAKING (COCKPIT) · airframe 38,057 hrs · 18,419 cycles

ELP - INFLIGHT DFW-SJD. CREW REPORTED CREW OXYGEN LEAK. EMERGENCY DECLARED FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DISCOVERED CAPTAINS OXYGEN REGULATOR LEAKING. SWAPPED WITH OBSERVERS REGULATOR AND PLACARD OBSERVERS REGULATOR PER MEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MOTOR — INOPERATIVE (STAB TRIM) · airframe 36,197 hrs · 17,464 cycles

DFW - CREW REPORTED STAB TRIM FAILED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED STAB TRIM MOTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

DENT IN SKIN AT STATION 200 BETWEEN LONGERON 4 TO 5 LEFT. INSTALLED INTERNAL DOUBLER PER BOEING DRAWING SG095530001.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

ELONGATED HOLE IN RIGHT FRAME STRAP STATION 1220. INSTALLED NEW STRAP.

Part: CUSP WEB — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

RIGHT CUSP AT ABOUT STATION 294 HAS A DEEP GOUGE. ACCOMPLISHED CUSP REPAIR PER EA MD80-53-020619.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

DENT IN SKIN AT STATION 199 BETWEEN LONGERONS 4 TO 5 LEFT. ACCOMPLISHED REPAIR PER BOEING DRAWING SG09530001.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

CUSP SHEET ON STATIONS 1184 TO 1206 RIGHT SIDE. INSTALLED CUSP SHEET RIGHT STATIONS 1174 TO 1250.

Part: STRUCTURE — CRACKED (SERVICE DOOR) · airframe 35,196 hrs · 16,917 cycles

AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA COMP-52-020541.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

CORROSION ON RIGHT CUSP MEMBRANE AT STATION 579 UNDER NUMBER 6 SEAT TRACK. INSTALLED NEW RIGHT CUSP SHEET AT STATIONS 579 TO 598 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

RIGHT CUSP SHEET AT STATIONS 1184 TO 1206 CORRODED. INSTALLED NEW RIGHT CUSP SHEET AT STATIONS 1174 TO 1250.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

G2 GALLEY FORWARD OUTBOARD MOUNT, STATION 215 ON FORWARD END OF NUMBER 6 SEAT TRACK IS CORRODED. INSTALLED NEW MOUNT PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

SEAT TRACK NUMBER 6 FROM STATIONS 205 TO 580 CORRODED. INSTALLED NEW SEAT TRACK PER AARD 51-10-00-5.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

MID CARGO LOWER DOOR BEAM HAS AREAS OF CORROSION FROM STATIONS 636 TO 693. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: STRAP — CRACKED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

PASSENGER DOOR JAMB INNER SKIN TONGUE CRACKED STATION 208 LONGERON 15 LEFT. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-11.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: SKIN — CANNING (ENTRY DOOR) · airframe 35,196 hrs · 16,917 cycles

FORWARD ENTRY DOOR, OIL-CANNING AND WAVINESS ON BOTTOM SKIN STATIONS 164 TO 198. ACCOMPLISHED REPAIR PER SHOP ESO 80172.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

RIGHT CUSP SHEET HAS CORROSION AT STATIONS 380 TO 389 ON OUTBOARD EDGE. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

CUSP SHEET AT STATION 886 RIGHT SIDE HAS ELONGATED FASTENER HOLE. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

CORROSION ON BOTTOM OF WEB AT STATIONS 1212 TO 1215 LONGERON 28 RIGHT. INSTALLED WEB SPLICE PER AARD 53-10-00-24.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

CORROSION ON MEMBRANE STATIONS 1145 TO 1175 AT AFT SERVICE DOOR THRESHOLD AREA UNDER AND AROUND FIBERGLASS SUPPORT ANGLE. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

LEFT CUSP STATIONS 503 TO 522 CORRODED. ACCOMPLISHED CUSP REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

SEVERAL AREAS OF CORROSION ON RIGHT CUSP MEMBRANE FROM STATIONS 455 TO 500. ACCOMPLISHED REPAIR OF CUSP PER BOEING DRAWING SG09530019.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

CORROSION ON BOTTOM OF LEFT CUSP, BETWEEN STATIONS 731 TO 750. ACCOMPLISHED CUSP REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

CORROSION ON TOP OUTBOARD SIDE CUSP STATION 608 AND LONGERON 18 RIGHT. ACCOMPLISHED CUSP REPAIR PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

H-FITTING LEFT STATIONS 1170 TO 1174 AT AFT SERVICE DOOR CUTOUT AT FLOORLINE CORRODED. INSTALLED NEW H-FITTING STRAP PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

RIGHT CUSP SHEET HAS CORROSION AT STATIONS 389 TO 408 ON OUTBOARD EDGE. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

HOLE IN FORWARD SUBFLOOR, STATION 198, LEFT BUTTLINE 44, BELOW FORWARD END OF NUMBER 2 SEAT TRACK. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,196 hrs · 16,917 cycles

SUBFLOOR CORRODED 10 INCHES INBOARD OF FORWARD SERVICE DOOR STATION 160. REPAIRED SUBFLOOR PER AARD 53-20-00-16.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

FASTENER HOLE ELONGATED IN FITTING BELOW CUSP STATION 446. INSTALLED NEW FITTING PER AARD 51-10-00-5.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

FASTENER HOLE ELONGATED IN FITTING BELOW CUSP STATION 332. INSTALLED NEW FITTING PER AARD 51-10-00-5.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

HORSE COLLAR RIGHT STATION 886 DAMAGED. INSTALLED NEW HORSE COLLAR PER AARD 51-10-00-5.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,196 hrs · 16,917 cycles

WINDOW FRAME, BETWEEN STATIONS 946 AND 965, RIGHT SIDE OF CABIN, TOP FOWARD CORNER HAS CRACK. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: SELECTOR PANEL — DEFECTIVE (CABIN PRESSURE) · airframe 33,762 hrs · 16,161 cycles

MCI - CREW REPORTED AIRCRAFT LOST CABIN PRESSURIZATION. ACCOMPLISHED EMERGENCY DESCENT. MASKS WERE NOT DEPLOYED. EMERGENCY DECLARED FLIGHT LANDED MCI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED OVERHEAD PRESSURIZATION SELECTOR PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN PRESSURE) · airframe 33,335 hrs · 15,941 cycles

CLE - INFLIGHT DFW-EWR. CREW REPORTED PRESSURIZATION ISSUES DURING FLIGHT. RIGHT PACK INOPERATIVE AND LEFT PACK FAILED TO HOLD PRESSURIZATION. EMERGENCY DESCENT TO 10,000 FT. EMERGENCY DECLARED FLIGHT DIVERTED CLE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARD LEFT AND RIGHT PACKS FOR FERRY FLIGHT TO ORD FOR REPAIRS. RESECURED CONNECTOR P1-450 THAT WAS LOOSE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,303 hrs · 15,924 cycles

AFT ACCS SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT. INSTALLED SHEAR TIE PER AARD 51-10-00-5.

Part: VANE — WORN (TE FLAP) · airframe 31,231 hrs · 14,950 cycles

LEFT WING DEEP WEAR IN NUMBER 3 FLAP VANE LEADING EDGE ABOVE OUTBOARD FLAP INBOARD HINGE. INSTALLED BONDED REPAIR DOUBLER PER SRM 51-70-02.

Part: DUCT — BROKEN (NR 2 ENGINE) · airframe 28,108 hrs · 13,533 cycles

IAD - INFLIGHT DCA-DFW. THE CREW REPORTED AIRCRAFT HAD A RIGHT ENGINE FIRE INDICATION. EMERGENCY DECLARED, LANDED IAD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 2 ENGINE COWL ANTI-ICE DUCT BROKEN AND UPPER COWL DAMAGED. REPLACED NUMBER 2 ENGINE UPPER COWL AND ANTI-ICE DUCT.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 27,030 hrs · 13,023 cycles

AMA INFLIGHT SAN ORD - CREW REPORTED NUMBER ONE ENGINE OIL PRESSURE LOSS. CREW SHUT DOWN NUMBER ONE ENGINE. SINGLE ENGINE TIME 17 MINUTES. LANDED AMA WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE DUE TO OIL PRESSURE LOSS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 60,255 hrs · 31,693 cycles

FORWARD CARGO DOOR, FORWARD STOP CASTING CRACKED, SECOND CASTING FROM BOTTOM. REMOVED AND REPLACED STOP CASTING PER SHOP ESO 80174.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 60,255 hrs · 31,693 cycles

STOP PAD CRACKED. REMOVED AND REPLACED CASTING, PER ESO80174.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 60,255 hrs · 31,693 cycles

STOP PAD BRACKET CRACKED. REMOVED AND REPLACED CASTING PER ESO 80174.

Part: CASTING — CRACKED (FUSELAGE) · airframe 60,255 hrs · 31,693 cycles

BRACKET CASTING CRACKED. REMOVED AND REPLACED CASTING PER ESO 80174.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,255 hrs · 31,693 cycles

EMERGENCY BATTERY PACK WEAK BS-1. INSTALLED A SERVICEABLE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,255 hrs · 31,693 cycles

EMERGENCY LIGHT BATTERY PACK WEAK BS-101. INSTALLED A SERVICEABLE BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT AFT EXIT SIGNS LEFT AND RIGHT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT EXIT SIGNS LEFT AND RIGHT OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG)

ORD INFLIGHT T309/03FEB - NOSE GEAR WOULD NOT RETRACT. RECEIVED RED LIGHT INDICATION AND HEARD NOISE. CYCLED GEAR WITH SAME RESULTS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 9,520 hrs · 5,317 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROW 11 TO 14, AND THE EGRESS LIGHT LENS WAS MISSING AT THE LEFT SIDE NUMBER 2 CABIN DOOR. REPLACED LAMP MODULE P/N 7732 AT ROW 10, AND REPLACED THE MISSING LENS P/N 0105607-301. CHECK-C 10-11-02 STL.

Part: LAMP · airframe 9,280 hrs · 5,184 cycles

THE EGRESS LIGHT AT THE RH OVERWING EXIT AND AT THE AFT GALLEY EXIT, WERE INOPERATIVE. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 10-11-02 STL. --CLOSED--

Part: BATTERY PACK (FWD OVERWING) · airframe 5,335 hrs · 2,890 cycles

THE FWD OVERWING EMERGENCY LIGHTS DID NOT ILLUMINATE WITH THE SWITCH ON. REPLACED THE BATTERY PACK. CHECK-C 11-8-00. --CLOSED--

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 3,803 hrs · 2,087 cycles

AT THE FWD OVERWING EMERGENCY EXITS, THE LT AND RT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE B5-103 POWER SUPPLY. CHECK-C 11-8-00 STL.

Part: BULB — FAILED (MLG INDICATOR) · airframe 2,396 hrs · 1,328 cycles

ON GEAR EXTENSION THE RT LANDING GEAR DOWN LIGHT FAILED TO ILLUMINATE. VISUALLY CHECKED GEAR DOWN AND DIVERTED FROM LGA TO JFK FOR LANDING. REPLACED LAMP. NO CHECK-C.