N9624T

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 57,316 hrs · 28,699 cycles

FORWARD CABIN PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT IAW AMM 33-53-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: MODULE — MALFUNCTIONED (FUEL SYSTEM) · airframe 56,157 hrs · 27,935 cycles

EMERGENCY DECLARED, DUE TO FUEL IMBALANCE. AIRCRAFT WAS GROUNDED, ACCOMPLISHED FUEL IMBALANCE MCM CARD 28-96-01. REPLACED SEM UNIT IAW MM 28-40-05, OPERATIONS CHECKED NORMAL.

Part: DOUBLER — CORRODED (BS 1302-1310) · corrosion level 2 · airframe 54,977 hrs · 27,174 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON INTERNAL DOUBLER AT AFT LAVATORY SERVICE PAN LOWER FORWARD CORNER. INSTALLED DOUBLER PER E.A.275685 AND SRM 53-34-00-001 FIGURE 3 SHEETS 2 AND 4.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 54,977 hrs · 27,174 cycles

CRACKED SHEAR TIE BS 1380, STRINGER 14R. INSTALLED A DOUBLER IAW 53-10-00-20.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,977 hrs · 27,174 cycles

AIRCRAFT IN BASE MAINTENANCE. FUSELAGE EXTERNAL AFT LAVATORY SERVICE PAN HAS CORROSION AT LOWER FORWARD CORNER. INSTALLED DOUBLER PER EA 275685 AND SRM 53-34-00-001.

Part: HOOK — BENT (L1 DOOR) · airframe 54,876 hrs · 27,110 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR HOLD-OPEN LATCH RELEASE GUST LOCK LATCH PAWL IS BENT DOWNWARD PREVENTING RETRACTION OF THE PAWL WITH DOOR CLOSURE AND WITH DOOR OPENING CAUSES PAWL TO CONTACT THE FUSELAGE. REMOVED AND REPLACED HOLD-OPEN HOOK PER AMM 52-11-04. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,591 hrs · 26,917 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE CEILING LIGHTS FROM FUSELAGE STATION 1130 TO 1300 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-27 (AALA20170910008) AND BATTERY ASSEMBLY B5-107 PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,591 hrs · 26,917 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE CEILING LIGHTS FROM FUSELAGE STATION 1130 TO 1300 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-27 AND BATTERY ASSEMBLY B5-107 (AALA20170910009) PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: WIRE — PULLED (CABIN) · airframe 54,591 hrs · 26,917 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 11D IS INOPERATIVE. TERMINATED PULLED WIRE TO CONNECTOR PER CHP20S 20-20-01. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 54,539 hrs · 26,888 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BY THE L1 DOOR OUTBOARD JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK PER AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,995 hrs · 26,546 cycles

AIRCRAFT WAS NOT GROUNDED. CRACK ON AFT FUSELAGE TAIL SKIN AT STATION 1475. ACCOMPLISHED TEMPORARY REPAIR IAW 53-30-00-4. REINSPECT AND ACCOMPLISH PERMANENT REPAIR WITHIN 50 FLIGHT HOURS. **SUPPLEMENTAL - 06/18/17 - PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-01-00. (CLOSED)

Part: VALVE — FAULTY (ZONE 400) · airframe 53,014 hrs · 25,901 cycles

FLIGHT RETURNED TO DEPARTURE FOR A TAIL COMPARTMENT OVERHEAT INDICATION WARNING. EMERGENCY DECLARED. UNEVENTFUL LANDING. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED RIGHT AUGMENTATION VALVE IAW MCM CARD 5770-20. LEAK CHECK IAW MCM CARD 5770-20 AND MCM CARD 5461. OPERATIONAL CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 53,013 hrs · 25,899 cycles

DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH WARING ILLUMINATED ACCOMPANIED BY FIRE AGENT 2 LOW LIGHT ILLUMINATION. EMERGENCY DECLARED. RETURNED TO FIELD. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED HIGH PRESSURE LEAK CHECK IAW TASK CARD 5461. OPERATIONAL CHECK GOOD. (CLOSED)

Part: SKIN — CRACKED (BS 1474) · airframe 52,987 hrs · 25,882 cycles

AIRCRAFT WAS GROUNDED. FUSELAGE SKIN CRACKED AT BS 1474 AND STRINGER 24 LEFT.REPAIRED SKIN IAW SRM 55-01-00.

Part: WARNING UNIT — FAULTY (ZONE 100) · airframe 52,901 hrs · 25,821 cycles

AIRCRAFT WAS GROUNDED. DURING TAKEOFF ROLL CREW RECEIVED AURAL SLAT OVERSPEED WARNING. TAKE OFF ABORTED AT APPROXIMATELY 80 KNOTS. ACCOMPLISHED CENTRAL AIR DATA COMPUTER BITE CHECK IAW AMM 34-16-00 AND OPERATIONAL CHECK OF SLAT OVERSPEED WARNING IAW AMM 31-51-00. REMOVED AND REPLACED CENTRAL AURAL WARNING UNIT IAW AMM 31-51-02. OPERATIONAL CHECK NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 52,635 hrs · 25,650 cycles

EMERGENCY LIGHTS L2-615 AND L2-671 INOPERATIVE DURING TEST. REMOVED AND REPLACED ASSOCIATED BATTERY ASSEMBLY IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,635 hrs · 25,650 cycles

EMERGENCY LIGHTS 22-615 AND 22-671 INOPERATIVE DURING TEST. REMOVED AND REPLACED ASSOCIATED BATTERY ASSEMBLY IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: BEAM — CRACKED (L1 DOOR) · airframe 52,143 hrs · 25,337 cycles

L1 DOOR NR 6 BEAM CENTER SECTION IS CRACKED AT BOLT HOLE. REPAIRED THE BEAM IAW AARD 52-10-00-3.

Part: OVEN — FAULTY (GALLEY) · airframe 50,689 hrs · 24,481 cycles

AIRCRAFT WAS GNDED. DURING FLIGHT A STRONG ELEC SMELL WAS REPORTED IN THE 1ST CLASS, FWD GALLEY & COCKPIT AREAS. FOUND 1ST CLASS OVEN EMITTING STRONG ELEC ODOR. R & R OVEN IAW AMM 25-39-03. OPERATIONAL CHECKED NORMAL.

Part: WINDOW — LEAKING (COCKPIT) · airframe 50,361 hrs · 24,271 cycles

THE LT AFT COCKPIT WINDOW HAD WATER, BETWEEN THE PANES. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. NO EMER WAS DECLARED. THE ACFT WAS REMOVED FROM SERVICE. REPLACED THE L3 WINDOW IAW AMM 56-10-05.

Part: BALLAST — BURNED (LAVATORY) · airframe 49,654 hrs · 23,826 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. FLIGHT ATTENDANT REPORTED ELEC FUMES SMELL, GENERATING FROM THE LT AFT LAVATORY AREA. FOUND LAVATORY BALLAST BURNED UP. R & R AFT LAVATORY LIGHT BALLAST IAW 33-26-13.

Part: HINGE — WORN (GEAR DOOR) · airframe 49,652 hrs · 23,825 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB VIBRATION WAS FELT IN THE NLG AREA. CONTINUED AROUND THE TRAFFIC PATTERN UNTIL THE NLG WAS LOWERED. POST FLIGHT WALK AROUND REVEALED THAT THE LT GEAR DOOR WAS CLOSED & THE RT GEAR DOOR WAS OPEN. GND CREW REPORTED THAT THE NLG DOOR REMAINED OPEN DURING DEPARTURE. ACCOMPLISHED NOSE GEAR RETRACTION IAW 32-30-00. NOSE GEAR DOORS OPERATED NORMAL. FOUND RT AFT FIXED GEAR DOOR LOOSE. R & R HINGE IAW 32-22-01. BOLTS CHECKED NORMAL.

Part: SKIN — CRACKED (RT WING) · airframe 48,503 hrs · 23,185 cycles

CENTER WING SKIN CAP CRACKED AT FS 826 UNDER SEAT TRACK NR 5 AT WING STATION XCW 42.0. REPAIRED CTR WING SKIN CAP IAW EA 57-038692 DATED 2 20 2015.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

G2 GALLEY ATTACH FITTING IS CORRODED AT STATION 218 INBD OF CTR LINE. INSTALLED NEW G2 GALLEY ATTACH FITTING IAW AARD 51-00-05 & DWG CDK2396.

Part: CASTING — CRACKED (RT SPOILER) · airframe 48,503 hrs · 23,185 cycles

RIGHT WING TE GND SPOILER ACTUATOR CASTING CRACKED AT OTBD FWD SIDE. INSTALLED NEW NT WING GND SPOILER ACTUATOR CASTING IAW SRM 51-01-00-001.

Part: CASTING — CRACKED (LT SPOILER) · airframe 48,503 hrs · 23,185 cycles

LEFT WING TE GND SPOILER ACTUATOR CASTING CRACKED. INSTALLED NEW GND SPOILER ACTUATOR CASTING IAW SRM 51-01-00-001.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CABIN VERTICAL SUPPORT BRACKET CRACKED BELOW SEAT TRACK NR 2 AT STATION 927. R & R VERTICAL SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 3925812.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CABIN VERTICAL SUPPORT BRACKET CRACKED BELOW SEAT TRACK NR 5 AT STATION 905. R & R VERTICAL SUPPORT BRACKET IAW AARD 51-00-05-01 & DWG 9923417.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CABIN VERTICAL SUPPORT BRACKET CRACKED BELOW SEAT TRACK NR 2 AT STATION 905. R &R VERTICAL SUPPORT BRACKET IAW AARD 51-00-05-1, AARD 51-00-00-1 & DWG 9923417.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CABIN VERTICAL SUPPORT BRACKET CRACKED BELOW SEAT TRACK NR 5 AT STATION 927. R & R VERTICAL SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 3925812.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,503 hrs · 23,185 cycles

SEAT TRACK NR 4 CORRODED BETWEEN FS 1291 & 1309. R & R SEAT TRACK IAW SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,503 hrs · 23,185 cycles

RIGHT CUSP CORRODED AT STATION 400. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,503 hrs · 23,185 cycles

RIGHT CUSP HAS CORROSION AT STATION 334. REMOVED CORROSION & FOUND OUT OF LIMITS. INSTALLED DOUBLER IAW SRM 53-05-00-001.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CRACK IN CABIN WINDOW FRAME LOWER AFT CORNER LT STATION 903. TRIMMED OFF CRACKED END, ADDED FILLER & INSTALLED DOUBLER IAW AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CRACK AT RT WINDOW FRAME AROUND UPPER FWD FASTENER AT STATION 888. TRIMMED SMALL CRACK & INSTALLED FILLER & DOUBLER IAW AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,503 hrs · 23,185 cycles

SEAT TRACK NR 6 CORRODED BETWEEN FS 463 & 466. REPAIRED SEAT TRACK IAW SRM 53-05-00.

Part: FORMER — CRACKED (LT WING) · airframe 48,503 hrs · 23,185 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

WINDOW FRAME AT FS 845 & STRINGER 10 LT IS CRACKED AT THE TOP FWD CORNER. REMOVED CRACK & INSTALLED DOUBLE CKD3488 IAW AARD 53-10-00-25.

Part: FORMER — CRACKED (RT WING) · airframe 48,503 hrs · 23,185 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,503 hrs · 23,185 cycles

CRACK IN SKIN AT CUT OUT FOR RT AFT NOSE GEAR DOOR AFT HINGE CUT OUT. INSTALLED DOUBLER IAW SRM 53-05-00-001.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 47,657 hrs · 22,731 cycles

ON APPROACH RECEIVED NO RT MLG GREEN LIGHT. TOWER FLYBY PERFORMED. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. REPLACED LAMPS IN LT, RT & NOSE GEAR MODULES IAW AMM 33-10-00. PERFORMED PROXIMITY SENSOR TESTS FOR ALL LG IAW AMM 32-60-04. NO FAULTS NOTED. INSPECTED LG DOWNLOCK SENSORS IAW AMM 32-60-05. SYSTEM TESTED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,033 hrs · 19,789 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. CLEANED BATTERIES. OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 42,033 hrs · 19,789 cycles

SEAT 8D ESCAPE PATH LIGHT INOPERATIVE. SECURED CONNECTOR FOR SEAT 8D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: BATTERY — DIRTY (CABIN) · airframe 42,033 hrs · 19,789 cycles

FORWARD AND AFT OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. CLEANED BATTERIES. OPS CHECK NORMAL.

Part: O-RING — LEAKING (AC BAY) · airframe 41,762 hrs · 19,650 cycles

DFW - CREW REPORTED ACRID ODOR DURING CLIMBOUT. CREW ACCOMPLISHED QRH PROCEDURE. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED O-RING THAT WAS LEAKING AT VERTICAL CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 41,050 hrs · 19,260 cycles

STL - INFLIGHT ORD-DFW. CREW REPORTED BURNING ODOR ASSOCIATED WITH ELECTRICAL COMPONENTS. FLIGHT ATTENDANTS TURNED OFF POWER TO POWER PORTS AND ODOR DISSIPATED THROUGHOUT CABIN. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. REPLACED BAD POWER PORT POWER SUPPLY AT ROW 8DF. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,923 hrs · 19,191 cycles

STATION 1418, LONGERON 2 RIGHT, FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER AND STRAP REPAIR PER SRM 53-03-00.

Part: INDICATOR — INOPERATIVE (FUEL QTY) · airframe 40,588 hrs · 18,997 cycles

CREW REPORTED FUEL FLOW AND FUEL QUANTITY INDICATION FAILED, SCREEN ONLY SHOWED DASHES. EMERGENCY DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED COCKPIT FUEL QUANTITY INDICATOR AND RIGHT ENGINE FUEL FLOW TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — MALFUNCTIONED (FUEL QYT) · airframe 40,588 hrs · 18,997 cycles

CREW REPORTED FUEL QUANTITY DISPLAYED ALL DASHES ON BOTH A & B CHANNELS. ABNORMAL PROCEDURE NO HELP. FUEL QUANTITY WILL INTERMITTANTLY DISPLAY NORMALLY. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FUEL QUANTITY MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (AC BAY) · airframe 37,347 hrs · 17,371 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING TAKEOFF. QRH PROCEDURES ACCOMPLISHED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT TAIL COMPARTMENT HIGH TEMP SENSORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

CRACK IN RADIUS OF SHEAR TIE, OUTBOARD SIDE STATION 1309 BULKHEAD JUST ABOVE LONGERON 16 LEFT. REMOVED AND REPLACED SHEAR TIE PER EA MD80-53-014345.

Part: SHELF — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

AFT SIDE STATION 1174 SHELF ABOVE CARGO DOOR CUTOUT IS CORRODED. REMOVED AND REPLACED DAMAGED SHELF PER AARD 51-10-00-05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

RIGHT STATION 845 OVERWING FRAME CUSP CUTOUT AFT SIDE 3RD FASTENER HOLE INBOARD FROM OUTBOARD EDGE OF CUSP, WHERE HORSE COLLAR MOUNTS, HOLE IS ELONGATED AND FORWARD EDGE OF HOLE HAS METAL PUSHED DOWN WITH A CRACK IN THE CUSP. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

CRACK IN FUSELAGE SKIN, STATION 1380, JUST ABOVE LONGERON 14 RIGHT. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER AARD 53-30-00-02 AND SRM 53-01-00 FIGURE 4 SHEET 4.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

CORROSION ON FORWARD CARGO LOWER DOOR PAN, STATIONS 389 TO 399 LONGERON 28 RIGHT. PERFORMED DOOR PAN SPLICE REPAIR PER SRM 53-05-00 FIGURE 44 SHEET 12.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

LEFT CUSP CRACKED AT STATION 800 OUTBOARD OF NUMBER 1 SEAT TRACK. INSTALLED LEFT CUSP SHEET AT STATIONS 788 TO 807 PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

CORROSION ON INBOARD FLANGE OF NUMBER 2 SEAT TRACK AT STATION 1174. INSTALLED SEAT TRACK SPLICE REPAIR AT STATIONS 1156 TO 1192 PER SRM 53-05-00 FIGURE 4F.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

FUSELAGE LEFT SIDE, DENT IN FUSELAGE SKIN BETWEEN STATIONS 705 AND 693 AT LONGERON 18 LEFT. INSTALLED PERMANENT CLASS 1 REPAIR DOUBLER PER SRM 53-04-00 FIGURE 12B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

LEFT CUSP STATIONS 1176-1178 HAS CORROSION OUT OF LIMITS PER SRM 51-10-03. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

SEAT TRACK DAMAGED TRACK NUMBER 4 STATIONS 597 TO 598. INSTALLED SPLICE REPAIR AT SEAT TRACK 4 STATIONS 597 TO 598 PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

HEAVY CARGO/FORWARD - CORROSION ON CUSP RIGHT SIDE STATIONS 370 TO 389 ABOVE DOOR. INSTALLED DOUBLER PER IAW AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

AFT CARGO LOWER DOOR BEAM WEB HAS CORROSION FROM STATIONS 1155 TO 1220. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER AARD 53-10-00-24.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

SUBFLOOR STATION 160 JUST INBOARD OF G-1 GALLEY DRAIN HAS CORROSION. INSTALLED REPAIR DOUBLER AND NEW OVERLAY DOUBLER AT STATIONS 160 TO 200 RIGHT BUTTLINES 36 TO 56 PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

G-1 GALLEY FORWARD MID MOUNT HAS CORROSION. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5 AND IPC 53-40-00-08D AND BOEING DRAWING 9936534.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

G-1 GALLEY FORWARD OUTBOARD MOUNT HAS CORROSION. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5 AND IPC 53-40-00-08D AND BOEING DRAWING 9936534.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

CORROSION REMOVAL OUT OF LIMITS ON LEFT HAND CUSP STATIONS 693 TO 712. INSTALLED DOUBLER PER AARD 53-20-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,671 hrs · 17,058 cycles

CORROSION REMOVAL OUT OF LIMITS ON RIGHT CUSP STATION 970. INSTALLED DOUBLER PER ARRD 53-20-00.

Part: SKIN — DENTED (CARGO DOOR) · airframe 36,671 hrs · 17,058 cycles

AFT CARGO DOOR HAS DENT IN SKIN AT LOWER AFT SIDE OF DOOR, MARKED. COLD FORMED SKIN BACK TO CONTOUR AND INSTALLED AN INTERNAL DOUBLER PER SRM 53-04-00-FIGURE 38 CONDITION 2.

Part: SILL — DAMAGED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

MID CARGO PIT HAS DAMAGE TO FORWARD EDGE OF EXTERIOR DOOR SILL 24 INCHES AND 28 INCHES FROM TOP. INSTALLED FILLERS DOUBLER AND TRIPLER AS PER SRM 53-05-00 FIG 80.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

CRACK AT LEFT WINDOW PAN UPPER FORWARD TANG STATION 946. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

CRACK AT LEFT WINDOW PAN UPPER FORWARD TANG STATION 1060. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,671 hrs · 17,058 cycles

CRACK AT LEFT WINDOW PAN UPPER FORWARD TANG STATION 1022. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: RING — CRACKED (WINDOW) · airframe 36,671 hrs · 17,058 cycles

WINDOW RING PANE UPPER AFT TANG CRACKED. REPAIR DOUBLER INSTALLED ALL PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,059 hrs · 16,785 cycles

EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. OPS CHECK NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,098 hrs · 15,451 cycles

FRAME CRACKED AT STATION 1418 AND LONGERON 2 LEFT. INSTALLED DOUBLER AT STATION 1418 FRAME PER EA53-007514.

Part: SPRING — BROKEN (FLAP CONTROL) · airframe 30,320 hrs

DFW - FLAP/SLAT HANDLE WOULD NOT LOCK IN THE UP/RETRACT POSITION. TRIGGER ON LEFT SIDE OF HANDLE WILL NOT GO DOWN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BROKEN SPRING ON LEFT SIDE OF FLAP HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,655 hrs

ABQ INFLIGHT T2457/26JUL DFW TO LAX. CREW REPORTED ELECTRICAL ODOR IN COCKPIT AND FLIGHT ATTENDANTS REPORTED HAZE NEAR AFT GALLEY. LANDED ABQ WITHOUT INCIDENT. COULD NOT DUPLICATE. NO HAZE OR ELECTRICAL ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: START VALVE — INOPERATIVE (LT ENGINE)

LAX INFLIGHT T1928/09MAY - NUMBER ONE ENGINE START VALVE INDICATION ILLUMINATED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED START VALVE FOR NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - LEFT AND RIGHT HAND FORWARD OVERWING EXIT DOOR EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT HAND FORWARD OVERWING EXIT DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT ROWS 18, 20, AND 21 CEILING INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18, 20, AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FUEL CONTROL — INOPERATIVE (ZONE 600)

DFW AT 10,000 FT AS POWER CAME UP THE RIGHT ENG INITIALLY CAME UP THEN DROPPED QUICKLY TO .92 EPR THEN SURGED UP TO ABOUT 1.8 EPR AND THEN IMMEDIATELY DROPPED TO .09 EPR. ENGINE WINDMILLED. RETURNED TO DFW. AIRCRAFT WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE FUEL PUMP AND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,273 hrs · 6,283 cycles

DURING CHECK-C MAINT FOUND CORROSION IN FASTENER HOLES IN LONGITUDINAL FLOOR BEAM 11 INCHES INBD OF DOOR THRESHOLD FROM STA 1155 TO 1211. REPLACED FLOOR BEAM PER SRM 6-70-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,272 hrs · 6,283 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOOR TRACK AT NUT PLATE HOLES FROM STA 1218 TO 1297, RBL 18. LOCATED HOLES AND INSTALLED NEW TRACK PER SRM 6-70-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,272 hrs · 6,283 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT FOUND CORROSION IN CABIN FLOORBEAM, STATION 1155, FROM LBL 22 INCHES TO OTBD. REPLACED PART PER SRM 51-30-0 FASTENER INSTALLATION AND SRM 6-70-01 FOR PART INSTALLATION.

Part: SEPARATOR — CONTAMINATED (A/C BAY) · airframe 8,938 hrs · 4,363 cycles

SMOKE AND ODOR APPEARED IN REAR CABIN. SWITCHED OFF THE LT AIR CONDITIONING PACK. FOUND LT PACK WATER SEPARATORS CONTAMINATED. REPLACED BOTH WATER SEPARATORS. CHECK-C 9-21-00 JFK.

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 6,555 hrs · 3,200 cycles

DURING CHECK-C MAINT, THE LT MLG WHEEL WELL DOOR WAS CRACKED AFT EDGE. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER ILLUSTRATION IN SRM 52-05, FIG 28, SHEET 6.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 5,303 hrs · 2,632 cycles

THE EMERGENCY LIGHT AT THE FORWARD LEFT CABIN DOOR WAS INOPERATIVE. REPLACED THE BATTERY CELLS, (P/N 408822-101) AND THE LAMP, (P/N PR2). CHECK-C 8-21-99 STL.

Part: COVER — MISSING (CABIN)

DURING ROUTINE MAINTENANCE FOUND ESCAPE PATH LIGHT COVERS MISSING. REPLACED MISSING LIGHT COVERS.

Part: POWER SUPPLY — FAILED (EXTERIOR)

FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT POWER SUPPLY.

Part: LINE — LOOSE (RT HYD SYST)

RT HYDRAULIC SYSTEM FAILED. LOST ALL FLUID. NEC TO MANUALLY EXTEND THE LANDING GEAR. FOUND LOOSE HYD LINE IN RT WHEEL WELL. TIGHTENED LINE. ALSO, REPLACED THE RT ENG HYD PUMP AND CASE DRAIN FILTER PRECAUTIONARY.