N368FE

Part: ADIRU — INOPERATIVE (NR 1) · airframe 88,923 hrs · 38,020 cycles

DESCENDING BELOW 24K FEET, RECEIVED AN IAS COMPARATIVE FLAG ON THE PFD. HAD ABOUT A 5-8 KT DIFFERENCE BETWEEN FIRST OFFICER`S AND CAPTAIN'S AIRSPEED. DIFFERENCE WENT AS HIGH AS 30 KTS, BY THE TIME THE AIRSPEED UNREALABLE QRH CHECKLIST WAS COMPLETED. DETERMINED THROUGH STANBY INSTRUMENTS AND QRH CHECKLIST THAT CADC 1 WAS BAD. COULD NOT CONFIRM ANY FAULTS. CAPTAIN`S PITOT TUBE DRAIN HOLES FOUND TO BE CLEAR IAW MM 34-11-02-2. REMOVED AND REPLACED THE NR 1 ADIRU IAW MM 34-43-03-4. REMOVED AND REPLACED THE CAPTAIN'S PITOT AIR DATA MODULE. IAW MM 34-16-01-5. LEAK CHECKED GOOD IAW 34-16-00-5. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 88,765 hrs · 37,913 cycles

IGN OVD ON, ENG ANTI ICE ON, WING ANTI ICE ON, PACKS 1 & 3 ON, PACK 2 OFF. LVL III AIR MANIFOLD 1 FAIL ALERT, WING ANTI ICE 1 ALERT, LVL II AND LVL 1 AIR SYS 1 OFF ALERT. RAN CHECKLIST FOR AIR MANIFOLD 1 ALERT, AND WING ANTI ICE I DISAGREE. ALERTS EXTINGUISHED. PERFORMED PNEU SYSTEM CONTROL BITE TEST IAW MM 36-10-00-2-0, SATISFSACTORY. NO LATCHED FAULTS INDICATED. ACCOMPLISHED MANIFOLD FAIL DETECT SYS TEST IAW MM 36-23-00-2-0. ALL ACCOMPLISHED SATISFACTORY. PERFORMED MANIFOLD DECAY TEST USING THE APU, IAW MM 36-10-00-0-0, TEST PERFROMED SEVERAL TIMES WITH NO DEFECTS NOTED, DECAY TIMES ALL WITHIN LIMITS. NO LATCHED FAULTS IN CFDS AFTER EACH TEST. APU RAN IAW JRH CHAP 6 WITH NO FAULTS. ALL THREE A/C PACKS OPERATED NORMAL. ACFT OK FOR SERVICE.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 88,453 hrs · 37,728 cycles

NR 1 PYLON AFT BULKHEAD FITTING O/B FWD ATTACH HOLE COMMON TO UPPER SPAR WEB CRACKED. REMOVED & REPLACED NR 1 PYLON AFT BULKHEAD FITTING PER DWG AUB7025-13 & SRM 51-35-01 VOL II & EA 8-5450-T0338023.

Part: HINGE — CORRODED (CARGO DOOR) · corrosion level 3 · airframe 88,453 hrs · 37,728 cycles

CENTER CARGO DOOR AFT HINGE HALF SECTION ON DOOR SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED HINGE HALF REF DAC DWG AFA3803 AND EA 8-5230-T0338044.

Part: SEAT TRACK — GOUGED (BS 755) · airframe 88,453 hrs · 37,728 cycles

MAIN DECK SEAT TRACK, BS 755, LBL 47 GOUGED AT TWO PLACES. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1, SRM 51-31-01, VOL. 2, AND SR10-53-002.

Part: BOLT — SHEARED (BS 1370) · airframe 88,453 hrs · 37,728 cycles

LEFT MLG WHEEL WELL, BS 1370, TRAPEZOID PANEL HORIZONTAL STRUCTURE BEAM HAS A SHEARED BOLT.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 88,453 hrs · 37,728 cycles

FWD CARGO DOOR HINGES ARE RUSTY. REMOVED SURFACE RUST, PRIMED AND PAINTED REF SRM 52-10-00 FIG 8 SHEET 1 VOL 2 AND SRM 51-21-02 PAGE 1-9 VOL 2.

Part: SEAT TRACK — GOUGED (BS 615-621) · airframe 88,453 hrs · 37,728 cycles

MAIN CABIN SEAT TRACK GOUGED AT LBL 27.5, BS 615 AND 621 ON THE UPPER SURFACES. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 88,453 hrs · 37,728 cycles

MAIN DECK SEAT TRACK STA 1421, 8.5 LT DAMAGED. REMOVED DAMAGE AND INSTALLED PLUG REF SRM 53-70-00 FIG 2 SHEET 1, VOL 1.

Part: SEAT TRACK — DAMAGED (BS 1129-1149) · airframe 88,453 hrs · 37,728 cycles

MAIN CARGO, BS 1135 - 1139 SEAT-TRACK GOUGED AT RBL 47.5. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1, SRM 51-31-01, VOL 2, AND SR10-53-002

Part: HINGE — CORRODED (CARGO DOOR) · airframe 88,453 hrs · 37,728 cycles

FWD CARGO DOOR, RUST EMANATING FROM HINGE. REMOVED SURFACE RUST, PRIME AND PAINT REF SRM 52-10-00 FIG 8 SHEET 1 VOL 2 AND SRM 51-21-02 PAGE 1-9 VOL 2.

Part: GIRT BAR — DETACHED (L1 DOOR) · airframe 87,569 hrs · 37,220 cycles

FOUND THE L1 GIRT BAR HANGING FROM OPEN DOOR. REINSTALLED GIRT BAR BACK INTO HOLDONG CLIPS ON THE L1 DOOR IAW AMM 25-61-01-2, OK FOR CONTINUED USE AT THIS TIME.

Part: WIRE HARNESS — DAMAGED (LT MLG) · airframe 87,435 hrs · 37,137 cycles

AFTER TAKEOFF, WHEN GEAR HANDLE SELECTED UP. RECEIVED AN UNSAFE LEFT MAIN GEAR ON BOTH PRIMARY & SECONDARY. REVIEWED QRH RESULTING IN PUTTING GEAR HANDLE DOWN AT 210KTS. ALL GEAR SHOWED DOWN & LOCKED. CYCLED HANDLE BACK TO UP, AGAIN SHOWED AN UNSAFE LEFT GEAR. PLACED GEAR HANDLE DOWN WITH 3 GREEN DOWN AND LOCKED INDICATIONS & RETURNED TO DEPARTURE. FOUND WIRE HARNESS FOR L/H MLG DOOR UPLOCK SENSOR HUNG AND NOT ALLOWING THE SENSOR ATTACHMENT LEVER TO MOVE TO THE PROXIMITY POSITION. REPOSITIONED WIRING HARNESS TO ALLOW FULL TRAVEL OF LEVER. ADJUSTED THE DOOR LATCH PROXIMITY SENSOR IAW AMM 32-34-03-2. JACKED ACFT AND SWUNG GEAR SEVERAL TIMES, GEAR INDICATION GOOD UP AND DOWN IAW AMM 32-60-00-5.

Part: DOOR — OUT OF ADJUST (L1) · airframe 87,186 hrs · 36,979 cycles

CANNOT ARM L1 DOOR. PERFORMED ADJUSTMENT TEST OF THE 1L DOOR IAW AMM 25-61-02-5. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — FAILED (ZONE 500) · airframe 86,585 hrs · 36,659 cycles

APPROXIMATELY 2 AT 15 AFTER TAKEOFF FL 350 GOT AIR MFG NR 1 FAIL, LEVEL 3 ALERT. 1 THROTTLE TO IDLE IAW QRH. NR 1 AIR SYSTEM TEMP AND AIR PRESSURE DECREASED, DIVERTED. R&R LT WING MANIFOLD FAIL DETECTION PRESSURE SWITCH.

Part: DOOR — CRACKED (R4) · airframe 85,780 hrs · 36,220 cycles

R4 LOWER CORNER HAS CRACK. REMOVED CRACK & INSTALLED DOUBLER.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 85,780 hrs · 36,220 cycles

STATION 595, BULKHEAD T CAP VERTICAL LEG, AT LONGERON 36L HAS A 1.0 INCH CRACK. REPAIRED IAW EA 8-5310-T0323068.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,780 hrs · 36,220 cycles

DAMAGED SEAT TRACK. REPLACED DAMAGED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 85,780 hrs · 36,220 cycles

DAMAGED SEAT TRACK. REPLACED DAMAGED SEAT TRACK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 85,780 hrs · 36,220 cycles

LEFT SIDE STATION 595, BULKHEAD WEB AT LONGERON 36L HAS A .300 INCH CRACK. NDT AREA FABRICATED & INSTALLED DOUBLERS & FILLER IAW SRM 53-40-00 VOL 1.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 85,780 hrs · 36,220 cycles

LEFT LOWER BS 595, BULKHEAD T CAP VERTICAL LEG AT LONGERON 39L, HAS A TWO INCH CRACK. REPAIRED IAW EA 8-5310-T0323068.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 85,780 hrs · 36,220 cycles

LEFT LOWER BS 595, BULKHEAD TED CAP VERTICAL LEG AT LONGERON 39L, HAS A TWO INCH CRACK. REPAIRED THE TEE IAW EA 8-5310-T0323068.

Part: SKIN — CRACKED (PAX DOOR) · airframe 85,780 hrs · 36,220 cycles

RIGHT AFT PAX DOOR, FWD LOWER CORNER HAS A CRACK INDICATION AT THE LOWER FASTENER IN THE RADIUS. REMOVED CRACK & INSTALLED DOUBLER IAW DWG SR10530084.

Part: SKIN — CRACKED (PAX DOOR) · airframe 85,780 hrs · 36,220 cycles

LEFT FWD PAX DOOR, AFT LOWER CORNER, HAS A CRACK INDICATION AT THE LOWER FASTENER IN THE RADIUS. CUT OUT DAMAGED AREA & INSTALLED THREE DOUBLERS IAW EA 8-5330-T0323541.

Part: CAP — CRACKED (FUSELAGE) · airframe 85,780 hrs · 36,220 cycles

FORWARD CARGO, STATION 595 BULKHEAD T CAP VERTICAL LEG AT LONGERON 39R HAS A .300 INCH CRACK AT THE LOWER FASTENER. REPAIRED T CAP IAW EA 8-5310-T0323071 P1.

Part: BEAM — CRACKED (FUSELAGE) · airframe 85,780 hrs · 36,220 cycles

FORWARD CARGO, STATION 595 BULKHEAD, LOWER HORIZONTAL BEAM Z = -80, UPPER & LOWER SURFACE, CTR AREA, IS CRACKED. INSTALLED REPAIRED DOUBLERS IAW SRM 53-40-00 FIG 36.

Part: SKIN — CRACKED (LT WING) · airframe 85,780 hrs · 36,220 cycles

LEFT WING LE LOWER SURFACE, FUELING PANEL 519CB CUT OUT, FWD INBD CORNER IS CRACKED. REPAIRED REF SRM 57-10-00 VOL 1 REPAIR 100. REPAIR CLASSIFIED AS MAJOR.

Part: HARNESS — FAILED (ENGINE) · airframe 852 hrs · 35,937 cycles

AT CRUISE GOT, ENG 2 EXCEEDANCE, EGT 960. AFTER ENG SHUTDOWN GAUGE FLOATED BETWEEN 0 - 600. COMPLIED WITH TSI 77-20/5735. R&R 4(EA) EGT THERMOCOUPLE LEADS PER MD10-10 AMM 77-21-02-2. R&R BOTH FWD AND AFT HARNESSES PER AMM 77-21-01-2. RAN ENG PER JRH UP TO TAKE-OFF POWER AND ALL INDICATIONS NORMAL.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 851 hrs · 35,861 cycles

L1 DOOR APPEARS TO BIND WHEN CLOSING SHUTTERS & SHAKES. NORMAL OPERATION WHEN OPENING. REMOVED L1 DOOR AFT SPROCKET DRIVE CABLE ASSEMBLY IAW AMM 52-11-09-2. INSTALLED L1 DOOR AFT BRACKET, SPROCKET & DRUM ASSEMBLY IAW AMM 52-11-09-2. ADJUSTED DOOR IAW AMM 52-11-00-5. COMPLETED UP TO 2 A 10U, RESERVOIR NEEDS PRESSURIZED. COMPLETED L1 DOOR ADJUSTMENT TEST IAW AMM 52-11-00-5. REMOVED MEL, OK FOR SERVICE.

Part: INDICATOR — DEFECTIVE (R1 DOOR) · airframe 849 hrs · 35,762 cycles

DOOR 1R PRESS TO TEST LIGHT DOES NOT TEST PROPERLY. AMM 25-61-03-2-0 R & R SLIDE PACK INDICATOR ASSEMBLY. CHECKED OK.

Part: INDICATOR — INOPERATIVE (R1 DOOR) · airframe 849 hrs · 35,757 cycles

DURING PREFLIGHT CHECK R1 DOOR SLIDE DISARM LIGHT INOPERATIVE. REMOVED AND REPLACED SLIDE PACK INDICATOR ASSY. CHECKS OK

Part: SKIN — DAMAGED (LT AILERON) · airframe 83,792 hrs · 35,098 cycles

FLIGHT CONTROLS LT INBD AILERON LOWER SKIN DAMAGE. COMPLY WITH EA 8-2710-T0308548 REV NO POS P3. THIS WRITE UP IS A WORK RELEASE ITEM SEQ 000669 WRI 27104334. NO NON-ROUTINE WAS GENERATED. REPAIRED LT INBD AILERON LOWER SKIN IAW SRM 57-10-00 FIG 85 & EA 2710- T0308548 FLT CTL LT INBD AILERON LOWER SKIN DAMAGE REPAIR EA 8-2710-T0309385 REV NO A POS P1 IS FOR RSC TRACKING. THIS IS A MAJOR REPAIR.

Part: FLAP — CHAFED (RT WING) · airframe 83,792 hrs · 35,098 cycles

RIGHT WING INBD TE FLAP LE ABOVE FLAP FAIRING FWD END HAVE DEEP CHAFED MARK. REPAIRED RT WING INBD TE FLAP LE IAW SRM 57-10-00 FIG 86. TRACKED ON EA 8-5710-T0309738. MAJOR REPAIR.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 83,792 hrs · 35,098 cycles

AFT CARGO DOOR AFT LOWER CUT OUT CORNER WEB SUPPORT ANGLE IS CRACKED. REMOVED & INSTALLED NEW T BRACKET PN AFA 3933-1 BATCH 0002646676 IAW SRM 51-31-01. REMOVED & INSTALLED NEW WEB SUPPORT ANGLE T FABRICATED ON TR T14 1076819 IAW DWG AGA388 & SRM 51-31-01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,792 hrs · 35,098 cycles

AFT CARGO COMPARTMENT BETWEEN STATION 1787 & 1841 SEAT TRACK X= 52.70 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM DC-1053-42-01 & SRM 53-00-01 FIG 1A. MATERIAL LOSS =.030 IN SEVERAL AREAS TOOL USED T14906 DUE DATE 10/31/14. REMOVED SEAT TRACK STATION 1787 - 1841 X=52.70 IAW SRM 51-31-01. FABRICATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01. CATEGORY A MAJOR REPAIR.

Part: ACCESS PANEL — MISSING (NR 1 NACELLE) · airframe 83,662 hrs · 35,035 cycles

DURING WALK AROUND AFTER ACFT ARRIVED, FOUND NR 1 ENGINE PYLON INSPECTION PANEL 437JL BROKEN OFF & MISSING. REPAIRED IAW E.A 8-5480-T0307890 REV.

Part: WIRE — FAILED (FUEL QTY PROBE) · airframe 81,614 hrs · 33,931 cycles

ONE HOUR INTO FLIGHT NOTICED TANK 2 QTY 8000 LBS LESS THAN TANKS 1&3. TROUBLESHOT PER FIM 28-41 AND FOUND NR 2 TANK RT COMPENSATOR PROBE WIRE WAS LOOSE AT RIVET AND WIRE HARNESS HI Z TO SHIELD WAS SHORTED. REPLACED NR 2 TANK RT COMPENSATOR PROBE AND WIRE HARNESS IAW AMM 28-41-01-2 AND WDM 28-41-07. OPS AND LEAK CHECKED NORMAL

Part: FUEL CELL — LEAKING (RT WING) · airframe 81,611 hrs · 33,929 cycles

"TANK 2 PUMP OFF" FOLLOWED BY " NR 2 CROSSFEED" ABOUT 1 HOUR INTO FLIGHT. NR 2 QTY INDICATED ALMOST 5000 POUNDS LESS THAN 1 AND 3. FOLLOWED QRH AND IN MANUAL ALL QUANTITIES DROPPED AT A CONSISTENT RATE. NR 2 QUANTITY VARIED FROM 1,800 TO 10,000. GROUND CREW CONFIRMED LEAK AFTER INSPECTION. FOUND TWO LEAKING FASTNERS AT LOWER SURFACE OF RT WING. CLEANED AND SEALED AREA IN RT TIP FUEL TANK FWD OF AFT SPAR, BOTH SIDES OF RIB IAW AMM 28-11-01-2 LEAK CHECKED GOOD.

Part: SENSOR — OBSTRUCTED (MLG) · airframe 81,466 hrs · 33,856 cycles

UNSAFE UP LEFT GEAR ON BOTH GEAR HANDLE DISPLAY AND ON CONFIGURATION PAGE. SAFE DOWN INDICATION. FOUND CONDUIT FOR THE UP AND LOCKED SENSOR ROUTED INCORRECTLY AND PUTTING SENSOR ACTUATING ARM IN A BIND AND NOT ALLOWING THE SENSOR TO GO INTO CORRECT POSITION WHEN GEAR IS UP AND LOCKED POSITION.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 81,453 hrs · 33,848 cycles

CENTER WHEEL WELL HAS ONE CRACK ON LT SIDEWALL 32" FWD OF STA Y1521 AND 19" DOWN FROM UPPER BULKHEAD. REPAIRED LT WHEEL WELL SIDEWALL IAW EA 8-5310-157347.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 81,453 hrs · 33,848 cycles

CENTER WHEEL WELL HAS THREE CRACKS ON LT SIDEWALL 16" AFT OF STA Y1381 AND 5" DOWN FROM UPPER BULKHEDD. REPAIRED IAW EA 8-5310-157348, SEQ NR 240.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 81,326 hrs · 33,784 cycles

SKIN MISREPAIRED AT BS 1907 BETWEEN LONGERON 19 AND 20 RIGHT. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6, VOL I, REV 98. EO 8-5100-7-5000 A4, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: RAIL — CRACKED (ZONE 100) · airframe 81,326 hrs · 33,784 cycles

RAIL CRACKED. REPAIRED IAW EA 8-5330-159845, PART 1C AND 1D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT OTBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1C, STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,326 hrs · 33,784 cycles

MAIN DECK CARGO DOOR AFT CUT-OUT AT BETWEEN LONGERON 26 LT AND LONGERON 27 LEFT EXTERIOR SKIN FOUND DENTED. CARRIED OUT REPAIR IAW SRM 53-50-00, FIG 26, SHEET 6, VOLUME I. REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615 PART 1 A STEPS 1, 2, 3, 4, 5 AND 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 81,326 hrs · 33,784 cycles

FUSELAGE SKIN BS 1079, LONGERON 52 LEFT MISREPAIRED. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 7, VOL I, REV 98. EO E8-5100-7-5000 A4, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1B, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1A STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 81,326 hrs · 33,784 cycles

FUSELAGE SKIN BS 715 BETWEEN LONGERON 39 AND 40 LT MISREPAIRED. REPAIRED IAW SRM 53-20-00, FIG 6, VOL I, REV 98. EO E8-5100-7-5000 A4, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — WORN (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, INBD AFT HINGE PIVOT HOLE OUTBOARD ATTACHMENT LUG FOUND BUSHING WORN. NEW BUSHING FABRICATED AND INSTALLED IAW EA 8-5750-160618, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

RT WING, OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615, PART 1B STEPS 1, 2, 3, 4 AND 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (BS 879) · airframe 81,326 hrs · 33,784 cycles

CARGO DOOR CUT-OUT FWD SKIN AT STA 879 BETWEEN LONGERON 41 RT AND LONGERON 43 RT MISREPAIRED. CARRIED OUT REPAIR IAW EA 8-5330-160619 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1C STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT MATING SURFACE FOUND WITH CORROSION. REWORK CARRIED OUT IAW CMM 20-11-02 REV 55. FOUND WITHIN LIMIT IAW CMM 57-44-09, REV 55, DWG ARC0503 AND EA 8-5750-160616, PART 1 PAGE 8 OF 10 FIG 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT OTBD MATING SURFACE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1D STEP 1 TO 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE LOWER ATTACHMENT, OTBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1A, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — DAMAGED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

AFTER REMOVAL OF BUSHING ON RT WING, OTBD FLAP, INBD HINGE PIVOT OTBD ATTACHMENT LUG HOLE FOUND OVERSIZED. REPAIR ACCOMPLISHED EA 8-5750-160618, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 81,326 hrs · 33,784 cycles

FUSELAGE SKIN BS 840, LONGERON 43 RT MISREPAIRED. REPAIR CARRIED OUT IAW EA 8-5330-159845, PART 1A AND 1B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT MATING SURFACE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1B, STEP 1 TO 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, OTBD FWD HINGE LOWER ATTACHMENT OTBD BORE FOUND WITH CORROSION. REWORKED CARRIED OUT IAW EA 8-5750-160614 PART 1A STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD, FLAP OTBD, FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORKED CARRIED OUT IAW EA 8-5750-160614, PART 1A STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING. ATTACHMENT FOUND MATING SURFACE WITH CORROSION. REWORK CARRIED OUT IAW CMM 20-11-02, REV 55 FOUND WITHIN LIMIT IAW CMM 57-44-09, REV 55, DWG ARC0503 AND EA 8-5750-160614, PART 1 PAGE 9 OF 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8- 5750-160615 PART 1 B STEPS 1, 2, 3, 4 AND 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — DENTED (ZONE 200) · airframe 81,326 hrs · 33,784 cycles

MAIN DECK CARGO DOOR FORWARD CUT-OUT AT BETWEEN LONGERON 26 LT AND LONGERON 27 LT EXTERIOR SKIN FOUND DENTED. CARRIED OUT REPAIR IAW SRM 53-50-00, FIG 26, SHEET 6, VOLUME I REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160616, PART 1B, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT OTBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615, PART 1 A STEPS 1, 2, 3, 5 AND 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SPAR CAP — CORRODED (ELEVATOR) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

RT DETACHABLE ELEVATOR L/E FRONT SPAR LOWER CAP AREA FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 98. FOUND TO EXCEED LIMITS IAW SRM 55-00-01, FIG 1A VOLUME I REV 98. REPAIR ACCOMPLISHED IAW EA 8-5520-160617 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1A STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 81,326 hrs · 33,784 cycles

LEFT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160613, PART 1A STEP 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, OTBD FORWARD HINGE SIDE LOAD FITTING. ATTACHMENT UPPER BOLT HOLE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160614, PART 1B, STEPS 1 TO 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

RT WING OTBD FLAP, INBD FORWARD HINGE SIDE LOAD FITTING ATTACHMENT FOUND MATING SURFACE WITH CORROSION. REWORK CARRIED OUT IAW CMM 20-11-02, REV 55. FOUND WITHIN CMM 57-44-08, REV 55 AND DWG ARC0502 LIMITS IAW EA 8-5750-160615, PART 1, PAGE 9 OF 11. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

STATION 435, X = 97 MAIN CARGO DOOR CONTROL ACCESS PANEL SUPPORT STRUCTURE FOUND CORROSION. R & R WITH NEW SUPPORT IAW AMM 20-50-02, REV 14.2 AND SRM 51-33-01, VOL II REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RIGHT WING FIXED L/E LOWER SKIN FOUND CRACKED AT OTBD SLAT. REFUELING ACCESS DOOR CUT-OUT INBD FORWARD CORNER APPROX STA XOS 610. REPAIR ACCOMPLISHED IAW SRM 57-10-00, FIG 68, SHEET 2, VOLUME I REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 600) · airframe 81,326 hrs · 33,784 cycles

RT WING AT APPROXIMATELY XOS 906 L/E LOWER SURFACE PANEL ATTACHMENT STRUCTURE FOUND CRACKED. REPAIRED IAW SRM 57-10-00, FIG 49, VOLUME I REVISION 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 81,326 hrs · 33,784 cycles

MAIN DECK CARGO DOOR UPPER AFT HINGE AT BS 735 TO 745 FOUND CORRODED. R & R IAW CMM 52-34-04, REV 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 81,326 hrs · 33,784 cycles

RT INBD DETACHABLE ELEVATOR UPPER SURFACE FOUND PUNCTURED. TRIMMED OUT IAW SRM 55-10-00, VOLUME I, FIG 8, REV 98. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 55-10-00, FIG 8, VOLUME I, REV 98 AND EA NR 8-5520-160617 PART 1. OPS CHECK CARRIED OUT IAW AMM 27-30-01-6, REV 14.2 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (LT WING) · airframe 81,326 hrs · 33,784 cycles

LEFT WING L/E NR 12 SLAT TRACK CUT-OUT FOUND CRACKED. REPAIRED IAW SRM 57-10-00, FIG 68, SHEET 1, VOLUME I, REV 98. REPAIR DOUBLER AND REPAIR FILLER FABRICATED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (RT WING) · airframe 81,326 hrs · 33,784 cycles

RT WING FIXED L/E TELESCOPIC DUCT CUT-OUT INBD EDGE FOUND CRACKED. REPAIRED IAW EA 8-5740-160608 PART 1, REPAIR CLASSIFIED MAJOR IAW GMM-2-100, REV 114.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 80,610 hrs · 33,436 cycles

DOOR SLIDE PRESSURE LIGHT INOP. RELEASED FOR SERVICE IAW MEL: 25-61-01 CATEGORY: C EXPIRATION: 11NOV11 "MEL 25-61-01: EVAC SLIDE REMOTE PRESS INDICATOR - INOP IAW MEL 25-61-01, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY." TRIED NEW BATTERIES, BUT TO NO AVAIL. TROUBLESHOT IAW FIM 25-61-01. REPLACED REMOTE PRESSURE INDICATOR BATTERIES. SLIDE PRESS TO TEST LIGHT OPS CHECKS GOOD, OK FOR SERVICE. CLOSED.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 80,168 hrs · 33,202 cycles

L1 EVAC SLIDE REMOTE PRESSURE INDICATOR INOPERATIVE. REMOVED & REPLACED L1 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR IAW MM 25-61-03-2.OPS CHECK NORMAL.

Part: INDICATOR — INOPERATIVE (SLIDE PRESSURE) · airframe 80,168 hrs · 33,202 cycles

L1 EVACUATION SLIDE REMOTE PRESSURE INDICATOR-INOPERATIVE.

Part: ENGINE — FAILED (NR 3) · airframe 79,143 hrs · 32,668 cycles

ON POWER UP FOR TAKEOFF HEARD 3 TO 4 LOUD THUMPS FROM RIGHT SIDE OF ACFT. IMMEDIATELY REJECTED T/O AT NO MORE THAN 15TO20 KNOTS. NO ABNORMAL ENGINE INDICATIONS NOTED HOWEVER ANOTHER AIRCRAFT REPORTED FLAMES SHOT OUT OF NR 3 ENGINE. CLEARED RWY AND SECURED NR 3 ENGINE.

Part: FRAME — BENT (ZONE 100) · airframe 78,743 hrs · 32,459 cycles

MAIN CARGO COMPARTMENT FRAME BENT AT FRAME 735, LONGERON 12R. REPAIRED FRAME IAW SRM 53-30-00 FIG. 5. CAT. B INSP DUE AT 12,000 AND REPETITIVE INSP DUE AT 8,000. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — GOUGED (ZONE 100) · corrosion level 2 · airframe 78,743 hrs · 32,459 cycles

FWD CARGO AT AFT FUSELAGE CUT OUT LOWER CORNER DOUBLER INSTALLED HAS GOUGE. REPAIRED CORNER IAW SRM 53-50-00. DOUBLER AND TRIPLER, DOUBLER FROM 2024-T3 .071 BATCH 182963, TRIPLER FROM 2024 T3 .080 BATCH 1747937.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,743 hrs · 32,459 cycles

FWS CARGO BILGE AREA AT FR 899 AND STR 52. STRINGER HAS EXFOLIATION CORROSION. REMOVED SPLICE IAW SRM 51-21-01. REMOVED COROOSION IAW SRM 51-21-10. FABRICATED PARTS LONGERON REPAIR AND SPLICE REPAIR ON TRAVELER T10/838926 AND T10/838928. LOCATED AND DRILLED REPAIR PARTS IAW SRM 51-31-01. TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED REPAIR LONGERON AND SPLICE IAW SRM 51-31-01. PAINTED AREA IAW SRM 51-21-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,743 hrs · 32,459 cycles

CTR CARGO BILGE AREA AR FRAME 1761 BETWEEN STRINGER 47R-48R FRAME SUPPORT CLIP HAS CORROSION. R & R WITH NEW SHEAR TIE IAW SRM 51-31-01, 51-21-01, 51-21-02. FABRICATED ON TRAVELER T10/841479.

Part: FITTING — CRACKED (ZONE 200) · airframe 78,743 hrs · 32,459 cycles

LOWER MAIN CARGO DOOR FITTING NR 5 HOLE C-CRACKED. REMOVED CRACKED FITTING AND REPLACED WITH NEW PN AFA7132-1 FITTING IAW SRM 51-31- 01. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 78,743 hrs · 32,459 cycles

RT SIDE UPPER INBD ELEVATOR SKIN HAS 2 EACH AREAS, OTBD TO INBD, AT APPROX 30" AND 60" BULGING UPWARD. FOUND DENTS APPROX 50" FROM OTBD EDGE AND 29" FROM T/E WITHIN LIMIT WITHOUT ANY EVIDENCE OF SKIN BULDGING IAW SRM 51-80-01 PAGE 2, (1) HAS SKIN REPLACEMENT IAW SRM 55-10-00. SPLICED NR2 SKIN IAW SRM 55-10-00, FIG 7 USING 7075-T6 .040 MAT BATCH NR 17243610.016, FILLER BATCH NR 1508112. OTHER DENTS FOUND TO BE WITHIN LIMITS UAW SRM 55-00-01 FIG 1A. DENT DOTS APPLIED AND ENTERED TO DAMAGE FILE IAW GMM 6-3-101. MAJOR REPAIR.

Part: BULKHEAD — CRACKED · airframe 78,743 hrs · 32,459 cycles

STA. 595.00 PRESSURE BULKHEAD CRACKED LT SIDE APROX Z STA. 75.000 CRACK APROX. 0.15 INCHES. COMPLIED WITH E.A. 8-5310-139190 BY REMOVING CRACK USING A 0.25 DIAMETER DRILL, HFEC INSPECTED HOLE, INSTALLED MS20470AD8 RIVET, VERIFIED EXISTING INTERCOSTAL IS 0.050 INCH THICK FABRICATED FROM 7075-T6 AND MATCHED DIMINSIONS IN FIG.2. DISCARDED INCOMING 'REPAIR CLIP" AND PLUGED HOLES USING MS20470AD RIVETS, INSTALLED B/P (NCA 604) FASTENER LOCATIONS THROUGH BULKHEAD WE AND TEE CHORD.

Part: DOOR FRAME — CORRODED (BS 1701) · corrosion level 2 · airframe 78,743 hrs · 32,459 cycles

CENTER CARGO DOOR JAMB STA. 1701, FRAME AT AFT SIDE HAS EXFOLIATED CORROSION. REMOVED DAMAGE, FABRICATED ANGLE ON TRAVELER T10/840028, REPLACED ANGLE P/N AFA3873-3, FABRICATED SPLICE STRAP FROM 7075-T6 .125 BATCH 1788276 AND REPAIRED FRAME IAW SRM 53-50-00 FIG. 1

Part: STIFFENER — CRACKED (BS 595 BULKHEAD) · airframe 78,743 hrs · 32,459 cycles

STIFFENER CRACKED, NR 3 AC BAY AFT PRESSURE BULKHEAD FS 595.0. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 7 CLASSIFIED AS A MAJOR REPAIR.

Part: CHANNEL — CORRODED (BS 1521) · corrosion level 2 · airframe 78,743 hrs · 32,459 cycles

CENTER CARGO UNDERFLOOR AREA AT FR 1521 FWD PRESSURE BULKHEAD ATTACHED "C" CHANNEL SUPPORT FLANGE HAS BLOWN-OUT CORROSION. REPAIRED ATTATCHED "C" CHANNEL AT FRAME 1521 FWD PRESS. BULKHEAD IAW SRM 53-00- 01 FIG. 9 AND SRM 51-31-01. REPLACED TRANSITION PANEL P/N ADJ 7004-505 AND INSTALLED NEW TRANSITION PANEL IAW SRM 51-31-01. REPAIRED ROLLER IAW SRM 53-70-00 FIG. 7 AND SRM 51-31-01 AND INSTALLED SRM 51-31-01.

Part: MEC — FAILED (NR 3 ENGINE) · airframe 78,218 hrs · 32,188 cycles

NR 3 ENGINE LOST POWER AND WAS UNRESPONSIVE. STARTED TO HANG AT RPM, GOT ENG 3 RPM LOW, THEN NR 3 GEN OFF. ENG WAS STILL RUNNING, OIL PRESS WAS LOW, BUT NO LOW OIL PRESS ALERT. PROGRESSIVELY WORSE RESPONSE. ENGINE WAS SHUTDOWN ON APPROACH. R & R OF MEC AND FUEL PUMP ASSEMBLIES IAW MM 73-12-01-2. ADJUSTMENT TEST MEC AFTER ACCOMPLISHMENT OF GROUND IDLE, FLIGHT IDLE AND MAX POWER ASSURANCE RUN IAW MM 71-00-00-5.

Part: ANGLE — CORRODED (MLG) · corrosion level 3 · airframe 76,008 hrs · 31,121 cycles

LT MLG, AUX SPLICE ANGLE FOR THE MLG ATTACH FITTING, P/N ARB0634-1, OUTBOARD OF THE LT MLG FITTING ON THE FWD SIDE OF THE LOWER AUX. SPAR HAS SEVERE EXFOLIATION CORROSION FROM APPROX WING STA XW222.000 TO WING STA XW231.000 RESULTING IN AN APPROX 8 INCH CRACK. REMOVED FITTING ARB0634-1. INSTALLED NEW SPLICE ANGLE ARB0634-1 REF SRM 51-31-01.

Part: RIB — CRACKED (ZONE 500) · airframe 73,556 hrs · 30,034 cycles

WINGS, LT WING LOWER RIB CAP CRACKED AT XORS 402 STGR 35-36 REPAIR: DURING "C" CHECK INSPECTION WHILE ACCOMPLISHING ALI CARD 57X1203ALI-P2 BUTTERFLY CLIPS WERE FOUND TO BE CRACKED AND A 1" CRACK WAS FOUND IN THE SUBJECT ARB2217-2 RIB CAP BETWEEN STRINGER35 AND 36. THE SUBJECT CRACKED CAP LOCATION IS SHOWN IN FIGURE 1. THE 4 BUTTERFLY CLIPS ARE LOCATED AT STA XORS 402 STRINGERS 36L, 36R, AND 37L AND STA XORS 372 STRINGER 43R EA NR 8-5710-102778 HAS BEEN COMPLIED WITH AT TIMCO BY EMPLOYEE NR 7951 ON N/R'S N00809, N00811, N00813, N00827, N00814.

Part: SKIN — DENTED (ZONE 100) · airframe 73,556 hrs · 30,034 cycles

ACCOMPLISH REPAIR AFT OF CENTER CARGO DENT REPAIR CARD T8-5330-106226,W/O35111. C/W EA 8-5330-102770 (FUSELAGE-GROSS WEIGHT DOUBLER DENT AT FUS STA 1850, L39R-40R. REPAIR ON CARD T8-5330-106226-W/035111. MAJOR REPAIR. MECH 1985 QC227 C/W EA 8-5330-106226 FUSELAGE, PLATE/SKIN AFT OF CENTER CARGO DOOR, RT, FS 1850, DENT, INTERIM REPAIR. PERMANENT REPAIR ACCOMPLISHED ON EA 8-5330-102770 ON CARD T 8-5330-106226, W/O35111.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 73,556 hrs · 30,034 cycles

CABIN SEAT TRACK STA 1249, LBL 75 TOPSCALLOPED AREA WORN AND GOUGED, APPROX 3 INCHES. REMOVED AND REPLACED SEAT TRACK STA 1229 TO 1411 IAW DC/MD 10 SRM 53-70-00 PAGE 5, FIG 1 VOL I, MECH 110217, QC002.

Part: ATTACH ANGLE — CHAFED (ZONE 400) · airframe 73,556 hrs · 30,034 cycles

NR 1 PYLON LT ATTACH ANGLE FOR PANEL 488GL CHAFED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW AUB7198 REV AN, DC/MD 10 SRM 51-35-01 VOL II. MECH 2891, QC227.

Part: ATTACH ANGLE — CHAFED (ZONE 400) · airframe 73,556 hrs · 30,034 cycles

NR 1 PYLON ATTACHED ANGLE FOR PANEL 488GL CHAFED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW DAC DRAWING AUB7108 REV AN, AND DC10/MD 10 SRM 51-35-01 VOL II, MECH 2891, QC227.

Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 73,556 hrs · 30,034 cycles

LEFT WING FUEL ACCESS PANEL 534 CT GOUGED ON BOTTOM SIDE. FABRICATED NEW FUEL PANEL IAW DAC DRAWING 0872 REV AP. INSTALLED ON 28C1701-01, MECH 4678 QC 231.

Part: ACCESS PANEL — CORRODED (ZONE 500) · airframe 73,556 hrs · 30,034 cycles

LEFT WING FUEL ACCESS PANEL 535AT PITTED ON BOTTOM SIDE. FABRICATED NEW FUEL PANEL IAW DAC DRAWING ARB0872 REV AP. INSTALLED ON CARD, 28C1701-01. MECH 4678 QC 231.

Part: ACCESS PANEL — CORRODED (ZONE 900) · airframe 73,556 hrs · 30,034 cycles

RIGHT WING FUEL ACCESS PANEL 634CT IS PITTED ON BOTTOM. FABRICATED NEW FUEL ACCESS PANEL 634CT IAW DAC DRAWING ARB0872 REVISION AP. INSTALLED ON CARD 28C1506-01.

Part: WARNING LIGHT — ILLUMINATED (CARGO BAY) · airframe 70,852 hrs · 28,814 cycles

AT FL 320 (SEL CARGO HEAT OFF) ALERT DISPLAYED AND CTR AND AFT CARGO TEMPS WERE 99 DEGRESS. TURNED OF CARGO HEAT AND TEMP REMAINED AT 99 DEGREES. OAT AT FL 320 -8C. BOTH CARGO TEMPS REMAINED AT 99 DEGREES. DECLARED EMERGENCY. LANDED. MEL 17AUG05 00:23 ACN RELEASED FOR SERVICE IAW MEL/CDL: 21-63-02. MEL 21-63-02: LWR CARGO COMPT TEMP INDICATION(S) ( INOP) LOWER CENTER CARGO COMPARTMENT TEMP INDICATIONS INOP. (OPEN)

Part: SKIN PANEL — CRACKED (HORIZONTAL STAB) · airframe 70,753 hrs · 28,748 cycles

DURING MAINTENANCE INSPECTION, FOUND CRACK IN THE UPPER CONSTANT SECTION OF THE HORIZONTAL STABILIZER. THE CRACK WAS IN THE FLYABLE LIMITS. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, IAW EA 8-5510-84843 (REF. NRC N0464).

Part: ENGINE — FAILED (NR 3) · airframe 67,356 hrs · 27,133 cycles

NR 3 ENGINE FAILED APPROX 45 MIN INTO FLIGHT AT FL310 FELT VIBRATION, HEARD NOISE AND MONITORED ALL ENGINE GAUGES WINDING DOWN. NO FIRE LIGHT, FOLLOWED RED TABS AND SHUTDOWN AND FIRED ONE FIRE BOTTLE. COULD NOT DUMP FUEL ( BELOW DUMPABLE LIMIT) SO LANDED OVERWEIGHT 35DEG FLAPS AT 368,000 POUNDS GW. REPLACED THE NR 3 ENGINE

Part: PUMP — FAULTY

02-60 AFTER T/O #3 TANK AFT FUEL PUMP OWR CB POPPED, LIGHT ILLUM. R&R #3 AFT BOOST PUMP PER AMM 28-22-01-2. R&R PUMP HARNESS.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 66,308 hrs · 26,633 cycles

AT CLIMB NR 3 ENG COUGHED AND ROLLED BACK N1 TO 35 PERCENT AND N2 50 PERCENT. EGT BEGAN TO RISE 800 DEG. SHUTDOWN ENG.

Part: INDICATOR — FAULTY (COCKPIT)

ON T/O ROLL PWR COMING UP AT 60 - 70 PERCENT NR 2 EGT WENT OFF SCALE HIGH ON BOTH POINTER AND DIGITAL READOUT. T/O ABORTED AT 15 KTS GROUND SPEED. REMOVED AND REPLACED NR 2 EGT GAUGE AND CB PER MM 77-21-00. OPS GOOD.

Part: TARGET — BROKEN (LT MLG)

LMG WOULD NOT RETRACT, BOTH IND WERE RED. REMOVED AND REPLACED TARGET. OK FOR SERVICE.

Part: STRINGER — CRACKED (WS 130)

DURING AC PF CONVERSION AT OAN, CRACK FOUND ON VERTICAL FLANGE OF STR 34 LT WING STR AT XOR=130. SRM DOES NOT COVER WING STR REPAIRS OF THIS CROSS SECTION AND LOCATION. REPAIR CUT OUT DAMAGE, PERF HFEC INSPECTION, INSTALLED 2 C ANGLES IAW NR 8-5711-44037.

Part: SKIN — CRACKED (CARGO DOOR)

DURING AC PF CONVERSION AT OAN, 2 3/4 CRACKS FOUND ON OUTER SKIN & INTERNAL DOUBLER OF FWD LWR CARGO DOOR. REPAIR INSTALLED INNER AND EXTERNAL DOUBLERS IAW EA NR 8-5210-45542.

Part: FLOORBEAM — CRACKED (BS 1289)

DURING AC PF CONVERSION AT OAN, CRACK FOUND ON FLOORBEAM Y=1289X=107. REMOVED AND REPLACED CRACKED OUTBD AND INSTALLED STAINLESS STEEL REPAIR PARTS IAW EA NR 8-5323-44064.