N313FE

Part: MANIFOLD — FAILED (PNEUMATIC SYS) · airframe 68,326 hrs · 24,243 cycles

DURING CLIMBOUT AT 9000FT, LEVEL 3-AIR MANF 2 FAIL - C/W QRH ALERT GONE @ N1 60% DECLARED EMERGENCY. REMOVED AND REPLACED D1-29 #2 MANIFOLD SENSING ELEMENT P/N: 35519-4-310, ANUFACTURER: FENWAL SAFETY SYSTEMS. USED MANIFOLD DETECTION TEST SET, NO FAULTS NOTED, PERFORMED AIR SYS TEST IN SYS 1,2 AND BOTH ALL TESTS PASS. REF: AMM 36-23-02-4 AND FIM: 36-23-00-2. CLEARING MEL, ENGINE RUN FOR CONFIDENCE CHECK ON WRI: 71-01/7841.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 68,325 hrs · 24,241 cycles

FOUND RH INBOARD FLAP DAMAGED DURING WALK AROUND. FABRICATED (PARTS) & REPAIRED RH INBOARD FLAP TO INCLUDE FAIRING USING EA 8-5750-T0362723 AS REFERENCE.

Part: ANTI-SKID VALVE — FAILED (NR 2) · airframe 68,325 hrs · 24,241 cycles

DURING LANDING GOT ANTI SKID FAIL. AFTER LANDING NOTICED #8 BRAKE TEMP HAS AMBER X. REMOVED AND REPLACED #2 ANTI-SKID-RETURN-SHUTOFF (PARKING BRAKE) VALVE PER MD10-30 M.M. 32-45-05-2 STEP 3, PART B, (1) THRU AND INCLUDING (9).

Part: SKIN — CRACKED (LT WING) · airframe 68,280 hrs · 24,223 cycles

LEFT HAND WING - WINGTIP LEADING EDGE ASSEMBLY LOWER SURFACE STATION XW 970.4 FASTENERS AREA FOUND CRACKED. CRACKED SKIN AROUND FASTENERS AREA AT LEFT HAND WING - WINGTIP LEADING EDGE ASSEMBLY LOWER SURFACE STATION XW 970.4 REPAIRED AS PER ENGINEERING AUTHORIZATION # 8-5710-T0361927 PART 1 TITLE " WINGS - BASIC WING STRUCTURE - LH WING - FWD WING TIP ASSY - 02EA CRACKS FOUND ON SKIN LOWER SURFACE AT XW 970.400 " WORK INSTRUCTIONS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CRACKED (BS 547 L33-34L) · airframe 68,280 hrs · 24,223 cycles

LEFT HAND FORWARD FUSELAGE FRAME AT AIRCON PACK #1 COMPARTMENT STATION 547 LONGERON 33 LEFT - LONGERON 34 LEFT FOUND CRACKED. LEFT HAND FORWARD FUSELAGE FRAME AT AIRCON PACK #1 COMPARTMENT STATION 547 LONGERON 33 LEFT - LONGERON 34 LEFT REPAIR CARRIED OUT AS PER E.A.# 8-5310-T0361983 PART 1. TITLE: FUSELAGE - MAINFRAME - REPAIR FOR 2.75 - INCH LONG CRACK FOUND COMMON TO ACA0051-3 FRAME Y = 547.250 AT AIR CONDITIONING COMPARTMENT DOOR CUTOUT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 68,280 hrs · 24,223 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER STATION XOS 667 FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT CRACKED DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME II AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT AT STATION XOS 667 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFID AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (BS 535 L19L) · airframe 68,280 hrs · 24,223 cycles

CABIN - LEFT HAND STATION 535 LONGERON 19 LEFT FRAME FOUND CHAFFED. CABIN - AT LEFT HAND FRAME STATION 535 , LONGERON 19 LEFT CHAFFED MARK REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-10 SRM 53-00-01 FIGURE 1B VOLUME 1. AT LEFT HAND FRAME STATION 535 , LONERON 19 LEFT CHAFFED AREA REPAIR CARRIED OUT AS PER MD-10 SRM 53-30-00 FIGURE 14 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CHAFED (BS 535 L24L) · airframe 68,280 hrs · 24,223 cycles

CABIN - LEFT HAND STATION 535 LONGERON 24 LEFT FRAME FOUND CHAFFED. CABIN - AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT , CHAFFED MARK REMOVED AND FOUND EXCEEDED LIMIT AS PER MD-10 SRM 53-00-01 FIGURE 1B VOLUME1. AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT CHAFFED AREA REPAIRED AS PER MD-10 SRM 53-30- 00 FIGURE 13 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 68,280 hrs · 24,223 cycles

LEFT HAND WING - INBOARD FLAP ASSEMBLY INBOARD MIDDLE SEGMENT UPPER SURFACE STATION XIFH 170 FOUND CRACKED. LEFT HAND WING INBOARD FLAP ASSEMBLY INBOARD MIDDLE SEGMENT UPPER SURFACE STATION XIFH 170 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 85 SHEET 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ENGINEERING AUTHORIZATION # 8-5750- T0361853 PART 1 TITLE " WINGS - FLIGHT SURFACES - ACCOMPLISHED NEW SRM REPAIR ON LHW INBD FLAP ASSEMBLY .

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 68,280 hrs · 24,223 cycles

CABIN - FLOOR PANEL #231HF FOUND DELAMINATED AT STATION 595 - STATION 675. DELAMINATED FLOOR PANEL #231HF AT CABIN STATION 595 - STATION 675 REMOVED AS PER AMM 53-21-08-4. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231HF INSTALLED AS PER AMM 53-21-08-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 68,280 hrs · 24,223 cycles

FORWARD CABIN - FLOOR PANEL #225AF FOUND DELAMINATED AT STATION 459 - STATION 500. DELAMINATED FLOOR PANEL #225AF AT CABIN STATION 459 - STATION 500 REMOVED AS PER AMM 53-21-08-4. FLOOR PANEL #225AF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #225AF INSTALLED AS PER AMM 53-21-08-4. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 68,280 hrs · 24,223 cycles

MAIN DECK CARGO FORWARD COMPARTMENT FLOOR SEAT TRACK SPLICE FITTING FOUND WITH CORROSION X = - 8.5 STATION 645. MAIN DECK CARGO FORWARD COMPARTMENT FLOOR AT SEAT TRACK SPLICE FITTING STATION 645 , X = - 8.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-IO SRM 53-00-01 FIGURE 1A VOLUME 1. CORRODED SEAT TRACK SPLICE FITTING REMOVED AS PER MD-10 SRM 51-31-01 VOLUME 2. SPLICE FITTING FABRICATED AND INSTALLED AT SEAT TRACK STATION 645 , X = - 8.5 AS PER MD-10 SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 68,280 hrs · 24,223 cycles

MAIN DECK CARGO FORWARD COMPARTMENT FLOOR SEAT TRACK SPLICE FITTING FOUND WITH CORROSION X = - 27.5 STATION 645. MAIN DECK CARGO FORWARD COMPARTMENT FLOOR AT SEAT TRACK SPLICE FITTING STATION 645 , X = - 27.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD- 10 SRM 53-00-01 FIGURE 1A VOLUME 1. CORRODED SEAT TRACK SPLICE FITTING REMOVED AS PER MD-10 SRM 51-31-01 VOLUME 2. SPLICE FITTING FABRICATED AND INSTALLED AT SEAT TRACK STATION 645 , X = - 27.5 AS PER MD-10 SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1601 S12L) · airframe 68,280 hrs · 24,223 cycles

CABIN - LEFT HAND STATION 1601 LONGERON 12 LEFT FRAME FOUND DENT. DUPLICATED SDR # 21-1347 WAS RAISED FOR SNRM N01525 WORK ORDER 00079718 WITH SDR # 21-1345 FOR DETAILS.

Part: SKIN — CRACKED (DOOR FRAME) · airframe 68,280 hrs · 24,223 cycles

CABIN - LEFT HAND STATION 1255 L3 DOOR FORWARD LOWER JAMB WEB BETWEEN LONGERON 26 LEFT AND LONGERON 27 LEFT FOUND CRACKED. CABIN - AT LEFT HAND STATION 1255 L3 DOOR FORWARD LOWER JAMB WEB BETWEEN LONGERON 26 LEFT AND 27 LEFT , CRACKED SKIN REPAIRED AS PER MD-10 SRM 53-50-00 FIGURE 19 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 68,280 hrs · 24,223 cycles

MAIN DECK CARGO FORWARD COMPARTMENT FLOOR SEAT TRACK SPLICE FITTING FOUND WITH CORROSION X = - 8.5 STATION 625. MAIN DECK CARGO FORWARD COMPARTMENT FLOOR AT SEAT TRACK SPLICE FITTING STATION 625 , X = - 8.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-10 SRM 53-00-01 FIGURE 1A VOLUME 1. CORRODED SEAT TRACK SPLICE FITTING REMOVED AS PER MD-10 SRM 51-31-01 VOLUME 2. SPLICE FITTING FABRICATED AND INSTALLED AT SEAT TRACK STATION 625 , X = - 8.5 AS PER MD-10 SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 68,280 hrs · 24,223 cycles

CABIN - LEFT HAND STATION 1561 LONGERON 12 LEFT FRAME FOUND DENT. CABIN - AT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT, DENT AREA REPAIRED AS PER MD-10 SRM 53-30-00 FIGURE 4 VOLUME 1. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT BY CLOSE VISUAL OR HIGH FREQUENCY EDDY CURRENT INSPECTION AS PER MD-10 SRM 53-30-00 FIGURE 4 VOLUME 1 AND SRM 53 - DTA TABLE 1 PARAGRAPH 3 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (N/A) · airframe 68,280 hrs · 24,223 cycles

CABIN - LEFT HAND STATION 1601 LONGERON 12 LEFT FRAME FOUND DENT.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · corrosion level 2 · airframe 68,280 hrs · 24,223 cycles

MAIN DECK CARGO FORWARD COMPARTMENT FLOOR SEAT TRACK SPLICE FITTING FOUND WITH CORROSION X = - 27.5 STATION 625. MAIN DECK CARGO FORWARD COMPARTMENT FLOOR AT SEAT TRACK SPLICE FITTING STATION 625 , X = - 27.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD- 10 SRM 53-00-01 FIGURE 1A VOLUME 1. CORRODED SEAT TRACK SPLICE FITTING REMOVED AS PER MD-10 SRM 51-31-01 VOLUME 2. SPLICE FITTING FABRICATED AND INSTALLED AT SEAT TRACK STATION 625 , X = - 27.5 AS PER MD-10 SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 68,280 hrs · 24,223 cycles

DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE SKIN , FOUND CRACK INDICATION AT CORNER # 5 , APPROXIMATE 0.2 " IN LENGTH AT XOS 523. LEFT HAND WING FIXED LEADING EDGE SKIN AT CORNER # 5 AT XOS 523 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 68 SHEET 2 VOLUME I . REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: SKIN — CRACKED (LT WING) · airframe 68,280 hrs · 24,223 cycles

DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE SKIN , FOUND CRACK INDICATION AT CORNER # 11 , APPROXIMATE 0.2 " IN LENGTH AT XOS 610.844. CRACK AT LEFT HAND WING FIXED LEADING EDGE SKIN AT CORNER # 11 AT XOS 610.844 REPAIRED AS PER SRM 57-10-00 FIGURE 107 SHEET 2 VOLUME I. INITIAL INSPECTION TO BE CARRIED OUT AT NEXT C CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTIONS AT EVERY C CHECK NOT EXCEEDING 24 MONTHS AS PER SRM 57-10-00 FIGURE 107 PARAGRAPH 101.D. FOR MAINTENANCE REQUIREMENTS. METHOD : VISUAL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1179-1201) · corrosion level 2 · airframe 68,280 hrs · 24,223 cycles

CABIN - RIGHT HAND STATION 1179 - 1201 X = - 27.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1179 TO STATION 1201 , X = - 27.5 CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-10 SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO EXISTING SPLICE STATION 1129 , X = - 27.5 AS PER MD-10 SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 989-1019) · corrosion level 2 · airframe 68,280 hrs · 24,223 cycles

CABIN - RIGHT HAND STATION 989 - 1019 X = - 27.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 989 TO STATION 1019 X = - 27.5 , CORROSION EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-10 SRM 53-70-00 FIGURE 5 VOLUME 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 969 TO STATION 1069 X = - 27.5 AS PER MD-10 SRM 53-70-00 FIGURE 1 VOLUME 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (LT WING) · airframe 68,280 hrs · 24,223 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT STATION XOS 542 STIFFENER CRACKED. CRACKED STIFFENER REMOVED AS PER SRM 51-31-01 VOLUME II AND FABRICATED STIFFENER AS PER DOUGLAS DRAWING ARB2918 REVISION G. INSTALLED FABRICATED STIFFENER AT LEFT HAND WING LEADING EDGE COMAPARTMENT STATION XOS 542 AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ENGINE — POWER LOSS (NR 1) · airframe 67,869 hrs · 24,043 cycles

ON TAKE OFF ROLL NR 1 ENGINE WAS SLOW TO COME TO TAKEOFF POWER. DURING FLIGHT WITH THROTTLES ALIGNED, NR 1 ENGINE N1 WAS 10% BEHIND THE OTHER ENGINES. ON GROUND AFTER LANDING ENGINE NR 1 WAS 900 LBS FUEL FLOW WHILE ENGINES NR 2 & NR 3 WERE 1300-1500 FUEL FLOW LBS PER HOUR. COMPLETED #1 ENGINE INSTALLATION AND COWLING CLOSED PER WIC 71T0707-1 AND 710000-00-93. IDLE LEAK CHECKED OK, IDLE FUEL FLOW WAS NORMAL AT 1450LBS/HR. PERFORMED MAX POWER ASSURANCE ENG RUN PER JRH ALL NUMBERS WITHIN PARAMETERS, PERFORMED ACCELERATION CHECK ON ENG #1 AND 3 FOR COMPARISON PER JRH CHP 7. CHECKED OK, ALL PARAMETERS FOR BOTH ENGINES MATCH. NO FAULTS NOTED AT THIS TIME.

Part: WINDSHIELD — SPARKS (COCKPIT) · airframe 67,622 hrs · 23,904 cycles

DURING DESCENT, WHEN WINDSHIELD ANTI-ICE TURNED ON, SPARKS & SMOKE CAME FROM RT FORWARD WINDSCREEN AREA. COCKPIT INSPECTION FOUND BURNS ON F/O WINDSCREEN LOWER AFT CORNER. INSPECTED ANTI ICE CONTROLLERS & FOUND NO C/BS TRIPPED IAW FIM 30-41, AND AMM 56-11-00. FOUND WIRE HARNESS GROUNDED OUT & BURNED THROUGH. FOUND WIRES COMING OFF OF R5-1088 BURNED & APPEARED ARCED TO METAL NEAR GLARESHIELD. R & R RT WINDSHIELD CONNECTOR R5-1088, SUPRESSOR E2-8, PN 5D0217-2, AND SURGE FILTER F3-8, PN FLX13 (SN UNK) ALONG WITH ASSOCIATED WIRING BETWEEN R5-1088 & E2-8 TO F3-8, 186R & S3-409, IAW WDM'S 30-41-02, 30-41-02-4, AMM 30-41-02-4, 30-41-03-4 & SWPM. OPS CHECKED GOOD IAW AMM'S 31-41-00-5 AND 30-42-00-5.

Part: WARNING MESSAGE — ILLUMINATED (MANIFOLD) · airframe 67,357 hrs · 23,763 cycles

AT FL 350 WE TURNED ON WING ANTI-ICE. WE THEN RECEIVED A LEVEL 3 AIR MANF 1 FAIL.

Part: SWITCH — FAILED (WING DEICE) · airframe 67,357 hrs · 23,763 cycles

AT FL 350 WE TURNED ON WING ANTI-ICE. WE THEN RECEIVED A LEVEL 3 AIR MANF 1 FAIL. ACCOMPLISHED A DECAY CHECK, IAW AMM 36-00-01-5-0. SYSTEM PASSED DECAY CHECK. INSPECTED PNEUMATIC FAULT MANIFOLD INDICATOR AND FOUND A FAULT BALL FOR THE LT MANIFOLD FAILURE DETECTION SWITCH (SWITCH S1-654). REMOVED AND REPLACED LT MANIFOLD FAILURE DETECTION SWITCH MGF P/N 83165-1 S/N 3253, IAW AMM 36-23-03-4. LEAK CHECK AND OPERATIONS CHECK GOOD. ALSO ACCOMPLISHED AN AIR SYTEM TEST AND RTS OF PSC 1. RAN NR 1 ENGINE, IAW JRH AND OPERATED WING ANTI ICE. NO FAULTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: REGULATOR VALVE — FAILED (CARGO HEAT) · airframe 67,181 hrs · 23,673 cycles

CLIMB POWER CLIMBING THRU 16000 RECEIVED AIR MANF 2 FAIL SYSTEM SELF PROTECTED. RETURNED TO GATE. FOUND AFT CARGO COMPARTMENT HEAT PRESS REG VALVE FAILED IN THE OPEN POSTION. REMOVED AND REPLACED AFT CARGO COMPARTMENT HEAT PRESS REG VALVE IAW AMM 21-41-15-4. OPS AND LEAK CHECKS NORMAL PERFORMED DECAY CHECK AND TEST PASSES.

Part: CONTROLLER — MALFUNCTIONED (MANIFOLD) · airframe 67,173 hrs · 23,668 cycles

PASSING 17,000 FT ON CLIMBOUT RECEIVED A LVL 2 AIR MANF 2 FAIL, FOLLOWED BY THE TRITONE. SYSTEM SELF ISOLATED. RETURNED TO DEPARTURE. TROUBLESHOT IAW FIM 36-23-00-810-801 AND 36-23-810-804. REMOVED AND REPLACED THE MANIFOLD FAILURE DETECTION CONTROLLER IAW AMM 36-21-01-4. OPS CHECKED GOOD. PERFORMED A MANIFOLD DECAY CHECK USING APU IAW AMM 36-00-01-5. TIME FROM 20 PSIG TO 15 PSIG WAS 19 SECONDS. PERFOMED SENSING ELEMENT LOOP TEST WITH TEST BOX 115QE100. NO FAULTS NOTED. PERFOMED MPA RUN FOR 20 MINUTES IAW JRH. NO MANIFOLD FAILURE FAULTS NOTED.

Part: SKIN — CRACKED (ZONE 100) · airframe 67,111 hrs · 23,630 cycles

SUSPECTED CRACK L/H NUMBER 2 PACK UPPER AFT CORNER CRACK WAS REPAIRED IN REF TO SRM 53-50-00 FIG 3A AND EA .8-5350-T0354952

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,111 hrs · 23,630 cycles

SUSPECTED CRACK LT NUMBER2 PAC EXHAUST, UPPER AFT CORNER CRACK WAS REPAIRED IN REF TO SRM 53-50-00 FIG 3A AND EA 8-5350-T0354952.

Part: SKIN — CHAFED (RT WING) · airframe 65,538 hrs · 22,794 cycles

RT WING DROOP L/E OUTBD SKIN SURFACE WORN AREA MARKED DOT 23. DRILLED AND INSTALLED REPAIR PER SRM 57-10-00,FIG 96, V1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 65,538 hrs · 22,794 cycles

[LH O/B FLAP UPR SKIN CRACKED AT FASTENER. MRKD 24 IN. FROM O/B EDGE 24 IN. FROM T/E. REPAIRED THE L/H O/B FLAP O/B ENVELOPE IN REF TO SRM 57-10-00 FIG 65, SHEETS 1 & 2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 65,538 hrs · 22,794 cycles

LH WING OUTBD FLAP UPPER SURFACE - APPROX XOF 740 - CRACK AT FASTENER HOLE. CONFIRMED CRACK USING NDT HFEC. CUTED OUT CRACK L/H WING OUTBD FLAP UPPER SURFACE APPROX XOF 740 FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER REF SRM 57-00-01 VOL I AND 51-3-02 VOL II

Part: FLOOR SUPPORT — CORRODED (BS 1600) · airframe 65,538 hrs · 22,794 cycles

CENTER CARGO AT APPROX STA 1600 ABOUT 17 INCH RIGHT OF CENTER FLOOR SUPPORT IS CORRODED MARKED #65 REMOVED AND REPLACED FLOOR SUPPORT "T" ANGLE PART NUMBER SR84864-17 PER DAC DWG SR84856 , REF SRM 51-31-01 VOL. 2.

Part: WEB — CRACKED (NLG WW) · airframe 65,538 hrs · 22,794 cycles

NLG WHEEL WELL RT UPPER WEB AT STA. 495 HAS A 1.25 IN. CRACK. (ENDS MARKED) REPAIRED WEB AT STATION 495 NOSE LANDING GEAR RT UPPER WHEEL WELL REF. SRM 53-30-00 FIG 6 SHEET 2 VOL.1.

Part: SKIN — WORN (LT WING) · airframe 65,538 hrs · 22,794 cycles

LT WING: DROOP L/E, OUTBD SKIN SURFACE WORN THROUGH AND RIVETS WORN THROUGH. INSTALLED REPAIR FILLER AND DOUBLER IN REF TO SRM 57-10-00 FIG. 96 PAGE 413 VOL. 1

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 65,538 hrs · 22,794 cycles

R/H WING I/B FLAP.. BOTTEM SURFACE..ADJACENT TO I/B SIDE OF FLAP HINGE..FLAP SKIN HAS DEEP DENT.. INSTALLED REPAIR DOUBLER AS REQUIRED REF. SRM 57-00-01 FIG. 4 SHT.2 VOL. 1, REF. E.A. 8- 5750-T0346590.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 65,538 hrs · 22,794 cycles

L/H HORZ STAB UPPER REAR SPAR CAP AFT BARREL NUT HOLE HAS A .200 IN. CRACK AT THE UPPER EDGE OF HOLE AT THE 5 O'CLOCK POSITION. (MARKED) BLENDED OUT CRACK AT AFT BARREL NUT HOLE L/H HORIZ. STAB. PER W/C 55X1203ALI-P4 FIG. 3 BLENDED OUT AREA FOUND TO BE WITHIN LIMITS.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 65,538 hrs · 22,794 cycles

L/H HORZ STAB UPPER REAR SPAR CAP FWD BARREL NUT HOLE HAS A .300 IN. CRACK AT THE OUTBOARD EDGE OF THE PREVIOUS BLEND OUT LOCATION AT THE 6 O'CLOCK POSITION. (MARKED) BLENDED OUT CRACK AT FWD BARREL NUT HOLE L/H HORIZ. STAB. PER W/C 55X1203ALI-P4 FIG. 3 BLENDED OUT AREA FOUND TO BE WITHIN LIMITS.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 65,538 hrs · 22,794 cycles

R/H HORZ STAB UPPER REAR SPAR CAP AFT BARREL NUT HOLE HAS A .300 IN. CRACK AT THE UPPER EDGE OF HOLE AT THE 7 O'CLOCK POSITION. (MARKED) BLENDED OUT CRACK AT AFT BARREL NUT HOLE R/H HORIZ. STAB. PER W/C 55X1203ALI-P4 FIG. 3 BLENDED OUT AREA FOUND TO BE WITHIN LIMITS.

Part: SKIN — DENTED (LT AILERON) · airframe 65,538 hrs · 22,794 cycles

LEFT WING OUTBOARD AILERON EXTERNAL BOTTOM SURFACE APPROXIMATELY AT (XW 779) EXHIBIT AN IMPRESSION DENT (MKD). FABRICATED AND INSTALLED REPAIR DOUBLER REF SRM 57-10-00 PAGE 369 VOL. 1 AND EA # 8-5710-T0346849.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 65,538 hrs · 22,794 cycles

L/H DROOP ELEVATOR UPPER IN/BD SKIN HAS HOLE PUNCHED IN IT, REMOVED & REPAIRED HOLE/CRACK PER SRM 55-10-00 VOL I PG 15.

Part: CONNECTOR — DAMAGED (NR 2 PRV) · airframe 64,640 hrs · 22,306 cycles

DURING CLIMBOUT, A LEVEL 2 AIR SYS 2 PRESSURE LOW LIGHT. RAN QRH STILL NO PRESSURE ON THE NR 2 SYSTEM. AIRCRAFT WAS NOT PRESSURIZING ON SCHEDULE. AT FL260 CABIN ALT. 4000' CLIMBING. FOUND SENSE LINE ON THE NR 2 PRV BROKEN AND PRV CONNECTOR P1-8057 DAMAGED. THE CONNECTOR WAS LOOSE AND COULD MOVE HARNESS AND ACTIVATE SOLENOID. REPLACED THE SENSE LINE AND WRI 36-12/4925. REMOVED AND REPLACED THE NR 2 PRV IAW AMM 36-12-01-4. TESTED GOOD. PRESSURIZED THE ACFT USING NR 2 PNEUMATICS. ACFT PRESSURIZED NORMALLY IAW AMM 21-00-00-5. MANIFOLD PRESSURE SENSOR PM2 CHECKED GOOD.

Part: SLIDE — INOPERATIVE (L1 DOOR) · airframe 64,497 hrs · 22,227 cycles

L1 DOOR TEST LIGHT ILLUMINATED ON PREFLIGHT TWO SLIDES AND / OR RAFTS. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE ASSY AMM 25-61-01-2. OPERATIONAL CHECKS NORMAL. A/C OK FOR SERVICE.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 64,349 hrs · 22,151 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND THE WIRING FROM 1265-20 INTERMITTANT ON WDM 33-52-01. SECURED THE TERMINAL IAW SMP. SYSTEM CHECKED NORMAL IAW AMM 33-50-00.

Part: SENSOR — FAILED (SLATS) · airframe 64,117 hrs · 22,022 cycles

FLAP 22 DEGREES, RETRACTION, LANDING, INTERROGATED THE PSEU AND SENSOR, READOUT SHOWED SENSOR (R2A) FAILED, R & R THE SLAT POSITION SENSOR D1-118 IAW AMM 27-84-02-4. OPS CHECKED SENSOR, STILL SHOWS FAILED IN PSEU, CHECKED WIRING FROM PSEU RACK TO TERMINAL BLOCK FOR SLAT SENSOR R2A, WIRING CHECKED GOOD IAW SWP. REMOVED AND REPLACED R2A SLAT SENSOR AGAIN , OPS CHECKED GOOD , VERIFIED SLAT INDICATION WAS GOOD, COMPLETED WIRING TIES AND CLAMPING OF WIRING FOR SLAT SENSOR. ALSO COMPLETED A PSEU RETURN TO SERVICE, CHECK WAS GOOD.

Part: PROXIMITY SWITCH — FAILED (SLATS) · airframe 64,117 hrs · 22,022 cycles

WHEN EXTENDING SLATS ON APPCH RECEIVED A LEVEL 1 PSEU FAIL R. TO S. TEST, PSEU FAULT, R AND R PSEU IAW AMM 31-71-01-2-0, OPS CHECKS GOOD, ACFT OK FOR SERVICE.

Part: PITOT HEAD — CLOGGED (CAPTAIN'S) · airframe 63,880 hrs · 21,903 cycles

DURING DESCENT, IN HEAVY RAIN, RECEIVED A MISCOMPARE AND SEVERAL ALERTS, SEL ELEV FEEL MAN, SEL FLAP LIM OVRD. DETERMINED THE FIRST OFFICER`S AIRSPEED RELIABLE AFTER RUNNING AIRSPEED UNRELIABLE CHECKLIST. LANDING UNEVENTFUL. FOUND THE CAPTAIN`S PITOT TUBE DRAIN HOLES TOTALLY CLOGGED. REMOVED DEBRIS IAW AMM 34-11-02-6. PUMPED UP CAPTAIN`S AND FIRST OFFICER'S AIRSPEEDS AFTER CLEANING & THEY MATCHED IN FLIGHT DECK. IAW AMM 34-16-00-5. ACFT GOOD FOR SERVICE.

Part: SLIDE — INOPERATIVE (R1 DOOR) · airframe 63,015 hrs · 21,466 cycles

OHMED R1 DOOR SLIDE AND FOUND IT TO BE INOP. REMOVED AND REPLACED R1 DOOR SLIDE REF AMM 25-61-02-4. REMOTE SLIDE PACK PRESSURE INDICATOR DID NOT TEST CORRECTLY. REMOVED AND REPLACED REMOTE SLIDE PRESSURE INDICATOR REF AMM 25-61-03-2. OPS CHECK GOOD.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 62,558 hrs · 21,250 cycles

MAIN DECK SEAT TRACK STA 1510 LBL 8 HAS DAMAGE. REPLACED DAMAGED SEAT TRACK FROM STATION 1491 TO STATION 1531 LBL 8 REF SRM 53-70-00 FIG 1 SHEET 1 VOL 1 AND IN REF TO SR10-53-002 AND IN REF SRM 51-41-01 PAGE 10 VOL 2.

Part: SKIN — CRACKED (LT WING) · airframe 62,558 hrs · 21,250 cycles

LEFT WING SKIN AT THE NR 12 SLAT TRACK CUT OUT OUTBOARD AFT CORNER HAS A .400 INCH CRACK. REPAIRED IAW SRM 57-10-00, FIG 68, PAGE 215, SHEET 1 OF VOL 1.

Part: RIB — CRACKED (LE SLAT) · airframe 62,558 hrs · 21,250 cycles

LT NR 3 SLAT INBOARD RIB HAD APPROXIMATELY 2.5 INCHES CRACKED AT STATION XOS 402.250, YOS 35.5. REPAIRED CRACKED REF SRM 57-00-01 FIG 4 SHEET 2 VOL 1 REF EA 8-5750-T0332627.

Part: SEAT TRACK — DAMAGED (BS 749) · airframe 62,558 hrs · 21,250 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT APPROXIMATELY BS 749 LBL 74. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1, VOL. 1.

Part: SEAT TRACK — DAMAGED (BS 635) · airframe 62,558 hrs · 21,250 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT BS 635, RBL 27. REPLACED THE SEAT TRACK FROM BS 600 TO 650 IAW SRM 53-70-00, FIG 1, SHEET 1, VOL. 1.

Part: SEAT TRACK — DAMAGED (BS 762) · airframe 62,558 hrs · 21,250 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT APPROXIMATELY BS 762, LBL 47. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1, VOL. 1.

Part: SEAT TRACK — DAMAGED (BS 1501-1521) · airframe 62,558 hrs · 21,250 cycles

MAIN CABIN, BS 1501 - 1521, RBL 48 SEAT TRACK LOBES OBLONGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1.

Part: SEAT TRACK — DAMAGED (BS 1500) · airframe 62,558 hrs · 21,250 cycles

MAIN CABIN, BS 1500, LBL 48 SEAT TRACK LOBE DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1.

Part: SEAT TRACK — DAMAGED (BS 879) · airframe 62,558 hrs · 21,250 cycles

MAIN DECK SEAT TRACK RBL 8.5 NEAR BS 879 SHOWS TRACK TOP INNER SURFACE DAMAGED. SUSPECTED CRACK AROUND DAMAGED AREA. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG. 1, SHEET 1 VOL. 1.

Part: SEAT TRACK — DAMAGED (BS 1390-1400) · airframe 62,558 hrs · 21,250 cycles

MAIN CABIN, BS 1390 - 1400, LBL 12 SEAT TRACK LOBE OBLONGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1, PAGE 3, VOL 1.

Part: SKIN PANEL — DAMAGED (NR 2 ENGINE) · airframe 62,558 hrs · 21,250 cycles

NR 2 ENGINE LEFT LOWER FORWARD FAN COWL LAND A/C SIDE. A PREVIOUS REPAIR IS DAMAGED AND COMING APART. REPLACED DAMAGED SKIN PANEL NR 2 ENGINE LEFT LOWER FORWARD FAN COWL LAND PER DAC DWG AJC7415, IAW SRM 51-31-01 FIG 11 VOL 2.

Part: SEAT TRACK — DAMAGED (BS 1390-1400) · airframe 62,558 hrs · 21,250 cycles

BS 1390 - 1400, RBL 48 SEAT TRACK LOBE OBLONGED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, SHEET 1, PAGE 3, VOL. 1.

Part: SEAT TRACK — DAMAGED (BS 1620-1640) · airframe 62,558 hrs · 21,250 cycles

MAIN CABIN BS 1620-1640, RBL 36, SEAT TRACK TOP SURFACE WORN, AND LOBES OBLONGED. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1A, VOL. 1.

Part: SKIN — CRACKED (RT WING) · airframe 62,558 hrs · 21,250 cycles

RIGHT WING SKIN AT THE SLAT DRIVE ACCESS PANEL CUTOUT, INBD FWD CORNER HAS A .700 INCH CRACK. REPAIRED THE SKIN IAW SRM 57-10-00, FIG 68, SHEET 2.

Part: SKIN — CRACKED (RT WING) · airframe 62,558 hrs · 21,250 cycles

RIGHT WING SKIN AT THE FUEL ACCESS PANEL CUT OUT INBOARD FWD CORNER HAS A .500 IN CRACK. REPAIRED IAW SRM 57-10-00, FIG 108, SHEET 2.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 62,205 hrs · 21,094 cycles

L1 DOOR SLIDE PTT LIGHT INOPERATIVE. REMOVED GIRT BAR, SLIDE COVER, AND REPLACED THE INDICATOR LIGHT BATTERIES IAW AMM 25-61-02-5, REINSTALLED THE GIRT BAR AND COVER. OPS CHECKED GOOD IAW AMM 25-61-03-5.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 61,986 hrs · 20,995 cycles

DURING DESCENT, NOTICED ALL FOUR OXYGEN BOTTLES WERE EMPTY, FOUND COURIER O2 MASK NOT PROPERLY STOWED AND LEAKING. REPLACED THE OXYGEN MASK IAW MM 35-13-03-2. OP AND LEAK CHECKED NORMAL IAW AMM 35-11-01-4-0. R & R ALL 4 CREW OXYGEN BOTTLES LEAK & OPS CHECKED GOOD IAW MM 35-11-01-4-0. ACFT OK FOR SERVICE

Part: TRANSMITTER — MALFUNCTIONED (FLAP HANDLE) · airframe 61,969 hrs · 20,987 cycles

REJECTED TAKE OFF AT 95-100 KTS. RECEIVED AN AURAL "FLAP" WARNING. EAD SHOWED A WHITE BOX BUT THE CONFIG PAGE SHOWED ALL GOOD INDICATIONS. REMOVED AND REPLACED THE FLAP HANDLE POSITION TRANSMITTER IAW MM 27-54-03-4. TESTS PASSED.

Part: COALESCER BAG — DIRTY (A/C PACK) · airframe 61,869 hrs · 20,941 cycles

AT ATTITUDE, FL 330, STRONG FUEL ODOR IN COCKPIT, PACKS 1 & 3 RUNNING (2 OFF). SEEMED TO INCREASE WITH INCREASE IN SELECTED TEMP. INSPECTED APU FOR FUEL LEAKS. NO LEAKS NOTED IAW MM 21-54-03-2. REMOVED AND REPLACED NR 1 AND 3 WATER SEPARATOR CONICAL COALESCERS. RAN ALL THREE PACKS FULL HOT WITH NO EVIDENCE OF ANY ODOR. OK FOR SERVICE.

Part: ACTUATOR — ODOR (APU) · airframe 61,874 hrs · 20,943 cycles

DURING PREFLIGHT AFTER APU START, SELECTED APU AIR ON PACKS ON ISOLATION VALVES ON PACKS 1 2 3 ON. STRONG FUEL ODOR IN COCKPIT DISSAPATED AFTER SEVERAL MINUTES. AFTER TALKING WITH THE CREW, THEY SAID THEY SMELLED FUEL WHEN THEY GOT TO THE COCKPIT BEFORE THE APU WAS RUNNING. REMOVED AND REPLACED APU NOZZLE ACTUATOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,874 hrs · 20,943 cycles

DURING TAKEOFF, A HEAVY ODOR OF EXHAUST FUMES. CABIN AIR TEMP FLUCTUATED WITH NO DEMAND FROM CREW. COLD TO HOT ETC. RAN ALL PACKS FULL HOT TO FULL COLD, NO FUMES DETECTED. CLEANED TEMP SENSOR FOR COCKPIT, COURIER AND CABIN AND OPS CHECKED AUTO TRIM SYS IAW AMM 21-60-00-5, ALL ZONES CHECKS OK FOR SERVICE. ACFT IS OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (NR 3 ENGINE) · airframe 60,936 hrs · 20,543 cycles

ON TAKEOFF ROLL AT APPROX 110 KTS MASTER CAUTION LIGHT FLICKERED WITH NO INDICATION. AFTER TAKEOFF LVL 1 ENG 3 EXCEEDANCE WITH 3 EGT SHOWING A TEMP OF 1043 ON THE GAUGE MAKER. ALL OTHER ENG INDICATIONS NORMAL. ON CLIMB OUT NR 3 EGT FLUCTUATION /- 100 OF THE OTHER EGT'S, AFTER LANDING, ALERT CAME BACK AT REVERSE IDLE. R&R ALL EGT HARNESSES AND LEADS REF AMM 77-21-02-2 AND 77-21-01-2. RAN NR 3 ENGINE AT GROUND IDLE FOR 10 MINUTES REF JRH. NO EGT FLUCUATIONS.

Part: VIA — MALFUNCTIONED (NR 1) · airframe 600 hrs · 20,143 cycles

DURING TAKEOFF ROLL, ENGINE FAIL LIGHT AT APPROX 95 KTS. ALL ENGINE PARAMETERS APPEARED NORMAL. SWAPPED THE NR 1 VIA WITH THE NR 3 VIA IAW AMM 31-43-01-4. VIA OP CHECKED NORMAL IAW 31-43-01-5.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (ENGINE) · airframe 600 hrs · 20,144 cycles

REJECTED TAKEOFF AT 80 KTS. ONCE TAKEOFF POWER WAS SET, APPROACHING 80 KTS. THE AUTO THROTTLES PULLED BACK, NR 3 THROTTLE APPROX TWO KNOB WIDTHS. ENG FAIL LIGHT ILLUMINATED. PER CONVERSATION WITH FLIGHT CREW, ALL OTHER ENG INDICATIONS WERE NORMAL, BEFORE & AFTER EVENT. BOTH ATS INOPERATIVE.

Part: CABLE — SHEARED (RIGHT MLG) · airframe 597 hrs · 20,036 cycles

RT MLG WW, NOTED RT GEAR & DOOR EMERGENCY RELEASE CABLE SEPARATED FROM EYEBOLT. CABLE SHEARED. R & R BROKEN CABLE IAW AMM 32-31-01-5, STILL REQUIRES CLEARANCE CHECK OF DOOR LATCH IAW 32-31-01-5. SAFETY ON BOTH ROD END JAM NUTS & EXTENSION & RETRACTION TEST IAW AMM 32-30-00 501. RIGGING & ADJUSTMENT TEST COMPLIED WITH IAW MM 32-31-01-5. ACFT JACKED IAW MM 07-11-00-2. OPERATIONAL CHECK OF ALTERNATE LANDING GEAR CONTROL SYS VERIFIED IAW MM 32-30-00-5-1. ACFT OK FOR SERVICE.

Part: GIRT BAR — DISCONNECTED (L1 DOOR) · airframe 597 hrs · 20,029 cycles

ON ARRIVAL AT ACFT, DOOR L1 GIRT BAR WAS DISCONNECTED ON RT SIDE & HANGING DOWN. REINSTALLED L1 DOOR GIRT BAR IAW MM 25-61-01-2. ACFT OK FOR SERVICE.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 593 hrs · 19,856 cycles

AT 340 NR 1 MANIFOLD FAIL LEVEL 3 ALERT WITH ASSOCIATED HIGH TEMPERATURE. CHECKED FAULT BALLS IN CAC AND NO FAULTS SHOWING OR LATCHED. PERFORMED RTS OFPSC1 AND NO FAULTS. PERFORMED DECAY CHECK PER AMM 36-00-05-5 AND DECAY CHECK GOOD. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE AND SENSE LINE IAW AMM 36-13-04-4. OPS CHECK NORMAL. RAN ENGINE AT HIGH POWER PER JRH AND NO ALERTS ALL INDICATIONS NORMAL. ALL CHECKS GOOD. REMOVED AND REPLACED THE LEFT WING MANIFOLD FAIL DETECTION PRESS SWITCH PER MM 36-23-03-4. LEAK AND OPS CHECK NML.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

MAIN DECK STATION 1059 RT 47.5 SEAT TRACK DAMAGED. REMOVED DAMAGED SEAT TRACK AT STATION 1059 RT 47.50 RBL. IAW 51-31-01. REPLACED DAMAGED SEAT TRACK STATION 985 TO STATION 1065 RT 47.50 IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

MAIN DECK STATION 1060 RT 27.50 SEAT TRACK DAMAGED. REMOVED DAMAGED SECTION OF SEAT TRACK. REPLACED DAMAGED SECTION OF SEAT TRACK ON MAIN DECK AT STATION 1060 RT 27.50 IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

MAIN DECK STATION 915, RT 27.50 SEAT TRACK DAMAGED. REMOVED DAMAGED SECTION OF SEAT TRACK AT STATION 915, RBL 27.5 IAW SRM 53-70-00 FIG 1A. LOCATED, DRILLED & INSTALLED NEW SECTION OF SEAT TRACK AT STATION 915, RBL 27.5 IAW SRM 53-70-00 FIG 1A.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

MAIN DECK STATION 905, RT 27.5 SEAT TRACK DAMAGED. REMOVED DAMAGED SEAT TRACK AT STATION 905, RT 27.50. LOCATED, DRILLED & INSTALLED NEW SECTION OF SEAT TRACK AT STATION 905, RBL 27.50 IAW SRM 53-70-00 FIG 1A.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

MAIN DECK STATION 1027 LT 47.5 SEAT TRACK DAMAGED. REPLACED DAMAGED SEAT TRACK AT STATION 1027 LT SIDE IAW SRM 53-70-00 VOL 1 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

MAIN DECK STATION 1025 LT 47.5 SEAT TRACK DAMAGED. REPLACED DAMAGED SEAT TRACK AT STATION 1025 LT SIDE IAW SRM 53-70-00 VOL 1 FIG 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

AFT FUSELAGE COMPARTMENT RT SIDE, FUSELAGE SKIN HAS CORROSION & EXFOLIATION LOCATED AT STATION 2007 - 2015 BETWEEN LONGERON R12 & R13. FUSELAGE REPAIR DOUBLERS IAW SRM 53-70-01 FIG 201 REPAIR 3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 591 hrs · 19,752 cycles

AFT FUSELAGE RT SIDE, FUSELAGE SKIN FOR HORIZONTAL STAB FAIRING PANEL 347AF DISPLAYS EXTERNAL & INTERNAL CORROSION & OR EXFOLIATION AT STATION 2007 - 2033, LONGERON 5R - 15R. INTERNAL CORROSION CAN BE VIEWED FROM INSIDE RT UPPER AFT FUSELAGE COMPARTMENT ZONE 311. MARKED DOT 2 FUSELAGE SKIN REPAIR DOUBLER IAW SRM 53-70-01 FIG 201 REPAIR 3.

Part: PANEL — DENTED (RT WING) · airframe 591 hrs · 19,752 cycles

RIGHT WING TE INBD, PANEL 641EB HAS SHARP DENT. REPAIRED RT WING PANEL 641EB IAW SRM 51-71-00 VOL II.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 591 hrs · 19,752 cycles

LEFT WING, INBD FLAP HINGE PANEL 541JL HAS DELAMINATION OUTER SURFACE OF PANEL. REPAIR PANEL 541JL IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 591 hrs · 19,752 cycles

LEFT NR 5 SPOILER UPPER SKIN DELAMINATED. REPAIRED LT NR 5 SPOILER AS REQUIRED IAW SRM 57-00-01 FIG 4 SHEET.

Part: SKIN — BULGED (TE FLAP) · airframe 591 hrs · 19,752 cycles

RIGHT INBD FLAP OP LOWER SKIN HAS A BULGE APPR MIDSPAN REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2.

Part: SKIN — CRACKED (RT WING) · airframe 591 hrs · 19,752 cycles

RIGHT WING, PANEL LAND IS CRACKED AT SLAT 8. R & R DOUBLER ARB 2933-48.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 591 hrs · 19,734 cycles

L1 DOOR EMER AIR BOTTLE PRESS IS LOW. SERVICED L1 DOOR EMER AIR BOTTLE.

Part: INDICATOR — INOPERATIVE (R1 DOOR) · airframe 59,005 hrs · 19,683 cycles

DURING PRE-FLIGHT CHECK FOUND R1 DOOR SLIDE PRESS TO TEST INDICATOR INOPERATIVE, NOT TESTING. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C EXPIRATION 01 FEB 15. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01, VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. TROUBLE SHOT IAW FM 25-61 TASK 801. REPLACED BOTH C BATTERIES WITH NIL FIX, REQUIRES MORE TROUBLESHOOTING.

Part: SKIN — CRACKED (LT WING) · airframe 58,420 hrs · 19,423 cycles

FOUND LT WING TAI DUCT CUT OUT INBD UPPER CORNER CRACKED. REPAIRED LT WING TAI DUCT CUT OUT IAW EA 8-5710-T0311682 & SRM 57-40-01 REPAIR 10.

Part: LINE — LEAKING (CSD) · airframe 58,185 hrs · 19,315 cycles

STRONG OIL ODOR IN COCKPIT DURING CLIMB THROUGH 10,000 FEET. CYCLED AIR CONDITIONING PACKS TO TROUBLESHOOT, ODOR GETS STRONGER & CREW NOTICED BURNING EYES & NOSES. CREW DONED OXYGEN MASKS, AND DIVERTED. INSPECTED FOR OIL LEAK IN TAIL AREA FOUND CSD OIL PRESSURE FILL LINE LEAKING AT AFTER ACCY. COMPARMENT, PERFORMED TYPE 2 PERMANENT PIPE REPAIR IAW AMM 20-10-01-2. NO LEAKS NOTED, OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 58,110 hrs · 19,281 cycles

RECEIVED VERY BRIEF CARGO FIRE LEVEL 3 ALERT. ALERT EXTINGUISHED BEFORE WE COULD DETERMINE FWD OR AFT. CHECKED FAULT REVIEW ON MSC LAST LEG AND NO FAULTS FOUND, PERFORMED RTS OF MSC PER MM 31-42-01-5, CHECKED ALL 3 VIA'S AND NO FAULTS LAST LEG, PER RTS ON ALL 3 VIA'S PER MM 31-43-01-5, CHECKED ALL 3 AIU'S AND NO FAULTS LAST LEG, PERFORMED RTS ON ALL 3 AIU'S PER MM 31-43-02-5, ALL TESTS PASSED PERFORMED LOWER CARGO OVERHEAT ADJUSTMENT TEST PER MM 26-14-02-5 AND TEST PASSED SEVERAL TESTS.

Part: TRANSMITTER — LEAKING (BRAKE SYSTEM) · airframe 58,066 hrs · 19,262 cycles

35 MINUTES INTO FLIGHT AT FL 340 LEVEL 1 HYD 1 OFF. HYD 1 QTY 2.6 GALLONS. ONCE SLATS, FLAPS EXTENDED QTY IN HYD 1 DECREASED TO .2 GALLONS WITH LEVEL 2 HYD 1 FAIL ALERT. FOUND NR 1 BRAKE SYS PRESS TRANSMITTER T2-66 LEAKING. R & R NR 1 BRAKE PRESS TRANSMITTER IAW AMM 32-47-01-2 THROUGH PAR 3 B STEP 7 WHICH INCLUDES PRESSURIZING & LEAK CHECK, NO LEAKS FOUND. ALSO CHECKED RT & CTR WW & FOUND NO FURTHER HYD LEAKS. SERVICED NR 1 HYD SYS & CLEANED AREA. NEED TO CONTINUE WITH STEP 8 THRU 10 WHICH INCLUDES BLEEDING THE DUAL BRAKE CONTROL VLV. NR 1 RESERVOIR HAD 2.6 GALLONS QTY AT BLOCK IN. COMPLIED WITH BLEEDING OF DUAL BRAKE CONTROL VLV IAW AMM 32-44-04-2. ACFT OK TO CONTINUE.

Part: O-RING — LEAKING (SPOILER ACT) · airframe 56,942 hrs · 18,786 cycles

THREE HRS INTO FLT, STARTED LOSING HYD FLUID, SHOWED 1.4 GALLONS AFTER LANDING AT SHUTDOWN. FOUND O-RINGS LEAKING AT RT SPOILER SERVO ACTUATOR. REPLACED O-RINGS IAW SMP AND OPS LEAK CHECK IAW MM 27-01-20-04. ALL FAULTS, ALERTS EXTINGUSED. ACFT OK FOR SERVICE. FINAL CLOSED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 55,980 hrs · 18,389 cycles

WINDSHIELD HEAT OFF, IMMEDIATELY CAPTAIN'S CLEARVIEW FRONT WINDOW COMPLETELY CRACKED INTO MANY CRACKS AND ARCING. GOOD FOR EMERGENCY LANDING. RAN QRH DURING DESCENT. WINDSHIELD REPLACED IN REF TO MM 56-11-00-2.

Part: PRESSURE SWITCH — FAILED (NR 1 ENGINE) · airframe 55,849 hrs · 18,336 cycles

NR 1 ENGINE "FUEL FILTER BYPASS" WARNING DURING CRUISE FLT, R & R NR 1 ENGINE DIFFERENTAL PRESSURE SWITCH AND MAIN ENGINE FUEL FILTER IAW 73-34-01-2. LEAK CHECKED GOOD. FILTER LIGHT STILL COMES ON WHEN FUEL LEVER ENGAGED. TROUBLESHOT IAW FIM CODE 73-31-01, FOUND FUEL FILTER DP SWITCH BAD. R & R NR 1 ENGINE FUEL FILTER DP SWITCH IAW MM 73-34-01-2, MM 73-34-01-5. LEAK AND OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 55,624 hrs · 18,236 cycles

DURING CLIMBOUT, RECEIVED IAS, ALT, WINDSHEAR DET, & SEL ELEV FEEL MAN. DURING RETURN TO LAND ALL FLIGHT INSTRUMENTS RETURNED TO NORMAL. AFTER ACFT RETURNED TO GATE, NOTICED SEVERAL RIBBONS OF ICE, AT LEAST AN INCH THICK ON RADOME, ABOVE AND IN FRONT OF PITOT PROBES. SUSPECT POSSIBLE AIRFLOW ISSUES DUE TO ICE BUILDUP. PERFORMED LOW RANGE LEAK AND OPS CK OF CAPT'S, F/O'S, AND STANDBY PITOT STATIC SYS IAW MM34-16-00-5. NO LEAKS OR DEFECTS NOTED. CONFIRMED PITOT PROBE HEATER OPERATION. ACFT IS OK FOR SERVICE.

Part: CONNECTOR — FAILED · airframe 55,262 hrs · 18,085 cycles

ON TAKEOFF ROLL AS POWER SET, NR 2 ENG N1 SURGED, MADE SLIGHT NR 2 THROTTLE REDUCTION AND ADJUSTED, AT THAT TIME ENGINE NR 2 N1 OVERSHOT RED LINE BY A LARGE MARGINE , REJECTED AT 75 KNOTS NO ENGINE POWER SURGED NOTICED. REMOVED & REPLACED CONNECTOR P1-8002 IAW SWPM 20-31-05. PERFORMED POWER ASSURANCE PER JRH. ALL PARAMETERS WITHIN LIMITS.

Part: BEARING — CORRODED (HORIZONTAL STAB) · airframe 53,407 hrs · 17,320 cycles

RT HORIZ STABILIZER CONSTANT SECTION HINGE BEARING MAKING POPPING NOISE. REMOVED BEARING HAS PITTING CORROSION. R & R BEARING REF AMM 55-51-01-2.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 53,407 hrs · 17,320 cycles

MAIN CARGO DOOR NR 7 SPOOL FITTING CRACKED. R & R SUPPORT FITTING REF SRM 51-31-01, VOL II.

Part: CONTROLLER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 53,284 hrs · 17,270 cycles

EMERGENCY LIGHT IN COURIER COMPARTMENT INOPERATIVE ON PRE-FLIGHT CHECK. NO BREAKERS TRIPPED. TRIED NEW EMERGENCY POWER SUPPLY WITH NO HELP. REINSTALLED ORIGINAL IAW AMM 33-51-01-4-0. R & R MISC SYS CONTROLLER IAW MM 31-42-01. OPS CHECKED NORMAL, OK FOR SERVICE.

Part: BEAM — CRACKED (ZONE 200) · airframe 49,838 hrs · 16,020 cycles

CTR CARGO COMPT SUMP AREA FOUND BEAM CRACKED AND BROKEN. REPAIRED AREA IAW SRM 53-60-00 VOL I, FIG 3.

Part: SEAT TRACK — CORRODED (BS 1841-1861) · corrosion level 2 · airframe 49,838 hrs · 16,020 cycles

AFT CARGO COMPT FOUND SEVERE CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 5 VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 49,838 hrs · 16,020 cycles

AIR CONDIT COMPT NR 2 LT/1LT FOUND CRACK ON FWD JAMB FRAME. REPAIRED FRAME IAW SRM 53-00-01 VOL I FIG 8.

Part: FRAME — CRACKED (ZONE 100) · airframe 49,838 hrs · 16,020 cycles

AVIONIC COMPT DURING REMOVAL FRAME WITH OAN J/C SP10530244-7002-5JR FOUND FRAME CRACKED. REPAIRED FRAME IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,838 hrs · 16,020 cycles

MAIN CABIN, CTR WING SECTION, UPPER SKIN SEVERE EXFOLIATION CORROSION ON UPPER SKIN. ACCOMPLISHED EA NR 8-5710-131033.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 49,838 hrs · 16,020 cycles

MAIN CABIN, CTR WING SECTION, UPPER SKIN SEVERE EXFOLIATION CORROSION ON UPPER SKIN. ACCOMPLISHED EA NR 8-5710-131033.

Part: SKIN — CRACKED (RT WING) · airframe 49,838 hrs · 16,020 cycles

DURING INSPECTION RT WING EXT. STRUCTURE L/E FOUND CRACK ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2, VOL I.

Part: WEB — CRACKED (ZONE 800) · airframe 49,838 hrs · 16,020 cycles

DURING INSPECTION AFT PASSENGER DOOR JAMB STRUCTURE FOUND CRACK ON WEB. REPAIRED AREA IAW SRM 53-50-00 FIG 19 SHT 1 VOL I.

Part: WEB — CRACKED (ZONE 800) · airframe 49,838 hrs · 16,020 cycles

DURING INSPECTION ON PASSENGER DOOR JAMB STRUCTURE FOUND CRACK ON WEB. REPAIRED AREA IAW SRM 53-50-00 FIG 19 SHT 2 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 49,838 hrs · 16,020 cycles

DURING INSPECTION LT WING EXT. STRUCTURE L/E FOUND CRACK ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: WEB — CRACKED (ZONE 800) · airframe 49,838 hrs · 16,020 cycles

DURING INSPECTION ON PASSENGER DOOR JAMB STRUCTURE FOUND CRACK ON WEB. REPAIRED AREA IAW SRM 53-50-00 FIG 19 SHT 2 VOL I.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,838 hrs · 16,020 cycles

DURING INSP OF HORIZ STAB CONSTANT AND OUTER SECTIONS SKIN PANEL, FOUND PANEL P/N 7228-1, P/N 7280-2, P/N 7278-2 WITH CRACK, ACCOMPLISHED EA NR 8-5510-129682.

Part: DOUBLER — CRACKED (LT WING STRINGER) · airframe 49,838 hrs · 16,020 cycles

LT WING L/E FOUND STRINGER DOUBLER WITH CRACK. REPAIRED AREA IAW SRM 57-10-00 FIG 49 VOL I.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 49,838 hrs · 16,020 cycles

RT WING, L/E CRACK ON INTERCOSTAL. REPAIRED AREA IAW SRM 57-00-01 FIG 3, SHT 2 VOL I.

Part: FRAME — WORN (ZONE 100) · airframe 49,838 hrs · 16,020 cycles

FWD AVIONIC COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-00-01 FIG 8 VOL I.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 49,838 hrs · 16,020 cycles

LEFT WING L/E FOUND CRACK ON STRINGER DOUBLER. REPAIRED AREA IAW SRM 57-10-00 FIG 49 VOL I.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 49,838 hrs · 16,020 cycles

LT WING OTBD FLAP UPPER SKIN FOUND CRACK ON SKIN. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 49,838 hrs · 16,020 cycles

CTR CARGO COMPT FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-00-01 FIG 10 SHT 5-6 VOL I.

Part: SKIN — DELAMINATED (SPOILER) · airframe 46,847 hrs · 14,640 cycles

LT WING NR 3 SPOILER UPPER SURFACE AREA HAS APPROX 19 INDENTATIONS/PUNCTURES, POSSIBLY LIGHTING STRIKES IN A GROUPED AREA CENTER OF SPOILER. REPAIRED NR 3 SPOILER UPPER SURFACE AREA BY REMOVING DAMAGED SECTION OF SKIN, DOUBLER AND CORE. FABRICATED AND BONDED NEW CORE, DOUBLERS AND SKIN IAW DC/MD 10-30 SRM 51-71-00 VOL II SEALED REPAIR IAW DC 10/MD10-30 SRM 51-71-00 VOL II.

Part: CONTROL VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 46,628 hrs · 14,535 cycles

AFTER TAKEOFF CLIMBING THRU 1000' WITH ENGINE AND WING ANTI-ICE ON THE NR 3 MANIFOLD FAIL LIGHT CAME ON. REMAINED OUT OF ICING. LANDED AT NEAREST SUITABLE AIRFIELD, KSTL. RT WING PRESSURE SWITCH FAULTED IN CAC. DROPPED FLAPS/SLATS AND CHECKED WING ANTI-ICE LINES FOR LEAKS, NONE NOTED. CHECKED FWD CARGO AREA FOR LEAKS, NONE DETECTED. PERFORMED NR 3 SYSTEM DECAY CHECK IAW DC-10 JRH, TEST PASSED. DUE TO PREVIOUS REPORT OF 60 PSIG AND NORMAL DECAY CHECK, CHANGING HIGH PRESSURE BLEED CONTROL VALVE, PRESSURE REGULATING VALVE, RIGHT WING ANTI-ICE VALVE, MANIFOLD FAIL CONTROLLER AND PNEUMATIC CHECK VALVE.

Part: PRESSURE SWITCH — FAILED (NR 3 PNEU SYS) · airframe 46,628 hrs · 14,535 cycles

NR 3 MANIFOLD LT, ILLUMINATED PASSING 3000 WITH FE STANDARD PANEL SETUP. ENGINE WING ANTI-ICE ON PRESSURE WAS 60. FOLLOWED QRH AFTER PHASE ONE PRESSURE, REMAINED AT 40. THROTTLE BROUGHT TO IDLE, PRESS DROPPED TO 20 DURING RTB TO MEM FACT, 11NOV06 20:47 MEM. REMOVED AND REPLACED NR 3 MANIFOLD PRESS SWITCH. LEAKED CHECKED SWITCH ALONG WITH SENSE LINES. LEAKED AND OPS CK GOOD. PERFORMED DECAY CHECK WITH APU AND NR 3 ENGINE. BOTH TEST PASSED. REF DC10 JRH 7-11 AND 7-12. REMOVED AND REPLACED NR 3 ENG PSC, CKS GOOD, REF MM 36-27-01-2. TAXIED ACFT TO HIGH POWER PAD. RAN ENGS IAW JRH PRESSURE. REGULATION CKS GOOD. NR 3 ENG HIGH STAGE VALVE OPERATION CKS GOOD. WING ANT-ICE CKS GOOD REF MM 30-11-00-2.

Part: RELEASE CABLE — DAMAGED (MLG) · airframe 46,017 hrs · 14,310 cycles

DURING GEAR RETRACTION THE RT GEAR INDICATED DOWN (RED LIGHTS) FROM BOTH GEAR POSITION INDICATORS. ALL OTHER GEAR SHOWED UP AND OUT. KEPT A/C AT 230 KNTS AND 5000 FT TO PREFORM QRH PROCEDURES. BOTH LIGHTS WENT OUT BRFORE QRH PROCEDURES WERE PREFORMED, THEN BOTH LIGHTS ILLUMINATED LEADING OUR RETURN. FOUND RT MAIN GEAR ALTERNATE RELEASE CABLE END BENT OB END. REMOVED AND REPLACED CABLE IAW MM. CYCLED MAIN GEAR AND CHECKED EMERGENCY. OK. RETURNED TO SERVICE.

Part: MECHANISM — DIRTY (MLG) · airframe 44,808 hrs · 13,797 cycles

AFTER TAKEOFF FROM SBKP ALL 4 RED GEAR LIGHTS REMAINED ILLUMINATED AT BOTH PILOTS AND FLT ENG POSITIONS. RAN RED TABS, CYCLED GEAR PER CHECKLIST. ALL 4 RED LIGHTS REMAINED ON. SLOWED A/C TO 210 KNOTS (15DEG./EXT) RECYCLED GEAR AGAIN ALL 4 RED LIGHTS EXTINGUISHED. CONTINUED TO MEM. PERFORMED OPS CHECK OF POSITION AND WARNING SYSTEM. GEAR CONTROL HANDLE "STICKY" AND CONTAMINATED WITH DEBRIS. WHEN HANDLE WAS PULLED STRAIGHT OUT INDICATION WOULD NOT CHANGE FROM GREEN TO RED. PERFORMED CLEANING AND LUBE OF LANDING CONTROL MECHANISM DC-10-30 MM 32-31-02-7. PERFORMED OPS CHECK AGAIN. CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (ROLL AXIS) · airframe 44,247 hrs · 13,607 cycles

PDIS - WHILE IN CRUISE FLIGHT AT FL330, LOST NR 1 INU WITH LOSS OF ADI AND HSI, WENT TO ATT REF POS, NO HELP AND THEN WENT TO OFF AND THEN TO ATT REF POS AND GOT ADI AND HSI BACK. DIVERTED TO ATL. REMOVED AND REPLACED NR 2 ROLL AXIS COMPUTER AND NR 1 INU, LOADED DATA BASE.

Part: INSULATION — BURNED (ZONE 100) · airframe 44,088 hrs · 13,531 cycles

IN CENTER ACCESSORY COMPARTMENT RT AND LT SIDE OF FUSELAGE INSULATION BLANKET IS SEVERLY BURNED AROUND 1-2 AND 1-3 SYSTEM PNEUMATIC AIR DUCT. BLANKETS ARE REMOVED FOR BLANKETS MOD WILL BE INSTALLED AND SECURED ON EA 8-2580-86498, SEQ NR 780, EMP.97433, QC.98577.

Part: COLLAR — CRACKED (NLG) · airframe 41,930 hrs · 12,789 cycles

NLG LOWER STEERING SUPPORT COLLAR ASSY CRACKED THROUGH AT FWD SIDE. *S/D* REMOVED AND REPLACED NLG COLLAR ASSY (LOWER COLLAR) WITH NEW PART.

Part: LINE — CRACKED (ZONE 100) · airframe 40,751 hrs · 12,391 cycles

NR 2 ENGINE FIRE-EX MANIFOLD CHECK VALVE FAILED FWD FLOW OPERATIONAL CHECK PER WORK CARD 26C2306. FOUND NR 2 ENGINE FIRE-EX WYE-FIREEX DISCHARGED LINE CRACKED, AND HOLE IN PIPE ASSY FOR OUTBOARD ENGINE FIRE-EX PIPE. REMOVED AND REPLACED P/N AHL7369-1 AND P/N AHL7037-1 WYE FIRE-EX Y-DUCT PER M/M 26-21-04-4, LEAK CHECK GOOD PER STEP 3.

Part: MOUNT — CORRODED (AILERON HINGE) · corrosion level 2 · airframe 40,751 hrs · 12,391 cycles

DURING C-CHECK AT LAX, THE RT OUTBOARD AILERON HINGE 5 MOUNT ASSY P/N ARC1052-02 WAS FOUND WITH THE LUGS CORRODED USED TO ATTACH THE SIDE LOAD STRUT. AFTER CORROSION REMOVAL, THE LUG BORE SIZES WERE INCREASED TO 0.450 INCH. THE ORIGINAL BORE SIZES ARE 0.4057/0.4067. NO REPAIR LIMITS EXIST IN CMM 57-51-02. THIS EA PROVIDES A BOEING APPROVED BUSHING REPAIR EA NR 8-5710-72676, RELEASE DATE: 01/29/2004. REPAIRED 2EA. CORRODED SIDE LOAD STRUT MOUNT LUGS PER EA 8-5710-72676 ON RT OUTBOARD AILERON HINGE 5 MOUNT HOLE. REINSTALLED BRACKET AND TORQUED BOLTS PER M/M 20-50-02-2.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 34,620 hrs · 10,402 cycles

ON T/O FROM ALT RED LIGHT ON LMG STAYED ON. RAN RED TAB PROC, LIGHT STAYED ON. NO FAULT FOUND SWAPPED PILOTS DISPLAY PLUG ON PROX BOX TO ALTERNATE POS, A/C DISPATCH IAW MEL 32-8C.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 34,463 hrs · 10,345 cycles

REJECTED T/O DUE TO NO AIRSPEED ON CAPT SIDE.

Part: SKIN — GOUGED (L/E SLAT) · airframe 34,463 hrs · 10,345 cycles

SEVERAL GOUGES LT WING LWR MIDDLE SURFACE OF SLATS NR 6, 7, 8. ALSO SEVERAL GOUGES ON UPPER SURFACE OF LT WING AT SLATS NR 6, 7, 8. REPAIRED PER EA 8-5750-56805 AND NR N415 UNDER WO 16747.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,463 hrs · 10,345 cycles

BS 1139 X=+6 THERE IS A 2 INCH CRACK IN FLOOR SUPPORT. *S/D* REMOVED, REPLACED AND FAB PER IAW SRM 51-10-01, 51-21-01, 51-31-01.

Part: TURNBUCKLE — BROKEN (LANDING GEAR) · airframe 34,463 hrs · 10,345 cycles

CENTER LAND GEAR LT DOWNLOCK SPRING TURNBUCKLE BROKEN. REMOVED AND REPLACED TURNBUCKLE PER IAW AMM 32-16-01. FUNCTION TEST PERF IN CONJUNCTION WITH 32C3301, TEST GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 34,463 hrs · 10,345 cycles

BS 1984 X=2R, Z=-19 LWR SIDE OF FLOOR SUPPORT HAS LEVEL (2) CORROSION APPROX 3.0 LONG X 2.0 WIDE AROUND MISSING NUT PLATE.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 34,463 hrs · 10,345 cycles

BS 949 RT SIDE OF CENTERLINE TRACK NR 3 UPPER CARGO COMP SEAT TRACK IS DAMAGED APPROX 8 INCHES. *S/D* REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-70-00, 53-42-01.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 34,463 hrs · 10,345 cycles

BS 1050 LT SIDE OF CENTERLINE SEAT TRACK WORN APPROX 6 INCHES. *S/D* REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 34,463 hrs · 10,345 cycles

BS 119 RT SIDE OF CENTERLINE OF UPPER CARGO TRACK NR 3 SEAT TRACK IS DAMAGED APPROX 4 INCHES. *S/D* REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-70-00 & 53-42-01.

Part: STANCHION — CORRODED (FUSELAGE)

AFT FUS WASTE COMP, FS 1967, AT X=23, X=0, X=23 3 EA STANCHIONS THAT RUN VERTICALLY FROM FLOORBOARD LEVEL TO COMP FLOOR HAVE LEVEL 2 EXFOLIATION CORROSION AROUND NUT PLATES.

Part: SKIN — DAMAGED (ELEVATOR)

FOUND CREASE/CRACK/DAMAGED RIGHT O/B ELEVATOR ON WALK-AROUND. REMOVED AND REPLACED PER IAW MM 27-30-02-4. PERFORMED O/B ELEV CHECK PER 27-30-02-6. OPS CHECKS GOOD.

Part: WIRE HARNESS — OUT OF POSITION (LT MLG)

LEFT MAIN GEAR IND (RED) UNSAFE IN THE UP POSITON IN BOTH PILOT AND 2ND OFFICER'S PNL GEAR. *S/D* TENSION OF WIRE BUNDLE ATTACHED TO THE UPLOCK SENSOR FOUND TIGHT. WIRING BUNDLE REROUTED AND LANDING GEAR WARN TEST CARRIED OUT IAW AMM 32-60-00-5. FOUND IND SATISFIED.

Part: BANJO FITTING — CRACKED (HORIZ STAB)

REF EO 8-5510-7-3314 BANJO FITTING LT AFT LOWER HOLE BORE SHOWING 2 CRACK INDICATIONS. *S/D* COMPLIED WITH N/R 854 AND EA 1-5510-32616 REAMED HOLE TO .341 TO ELIMINATE CRACK. FABRICATED FILLER AND BUSHING MANUFACTURED FITTING P/N AJC 7504 PER SRM 55-20-00, FIG 7, DET 7 AND MANUFACTURED DOUBLER PLATE AJC 7504-3 PER SRM 55-20-00, FIG 7, SHT 4, AND EO 8-5510-7-3314 NR 4 BANJO FITTING.

Part: TIRE — FAILED (NLG)

AT LIFT OFF, A LOUD BANG WAS IN THE COCKPIT, AT THE SAME TIME ALL 3 INS UNITS FAILED. DUE TO WEATHER AT NARITA AIRCRAFT WAS DIVERTED TO OSAKA. ON LANDING FOUND RIGHT NOSE GEAR TIRE TREAD HAD COME OFF AND DAMAGED LOWER FUSELAGE AREA. NO INS READINGS DUE TO IN FLIGHT FAILURE. REMOVED AND REPLACED BOTH NOSE TIRE AND WHEEL ASSEMBLIES PER MAINTENANCE MANUAL 32-42-01. REPLACED BENT ROD ASSEMBLY (P/N ACG7177-1), HANDLE (P/N ACG715-1) AND BRACKET (P/N ACG7176-1) ON STEERING BYPASS SYSTEM PER MAINTENANCE MANUAL 32-52-05. ALSO, REPLACED BENT GROUND SENSE ROD AND INSPECTED. INTERIM REPAIRED LOWER FUSELAGE DAMAGE PER ENGINEERING AUTHORIZATION 8-5310-32013.