N399FE

Part: SENSOR — DIRTY (LE SLAT) · airframe 82,852 hrs · 28,975 cycles

RECEIVED A SLAT DISAGREE ON ARRIVAL. ON ARRIVAL SEA NO FAULTS ON FCC1, FCC 2 OR PSEU. CYCLED FLAPS & ALL SLAT POSITION VALUES CHECKED OK IN FCC SENSOR READOUT. SLATS & FLAPS OPERATE SMOOTH. PERFORMED FLAP TRANSMITTER POSITION CHECK IAW MM 27-50-00-5 ALL INDICATIONS CHECKED GOOD. INSPECTED NR 4 SLAT POSITION SENSOR BOTH WINGS. CLEANED GREASE FROM SENSORS &TARGETS BUT WERE NOT UN NORMALLY DIRTY. INSPECTED CTR ASSESSORY COMPARTMENT SLAT CONTROL MECHANISM FOR MOISTURE OR DAMAGE, NONE FOUND. R & R EPSU PRECAUTIONARY IAW MM 31-71-01-2 CHECKED GOOD. PERFORMED FCC1 & FCC 2 AUTO LAND SYS GND TESTED IAW MM 22-00-00-2-0.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 82,495 hrs · 28,761 cycles

EMERGENCY LIGHT TEST SHOWS "BATT 1 LO". REPLACED BATTERY, IAW MM 33-51-01-4-1. OPS NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 82,025 hrs · 28,515 cycles

ON FINAL, RECEIVED A HEADWINS SHEAR WITH GUIDANCE, WINDS WERE 310/48. WENT AROUND. AIRSPEED FLUCTUATED NOT MORE THAN 5KTS, NO ENGINE EXCEEDENCES, NO ABRUPT ELEVATOR OR FLIGHT CONTROL MANUEVERING. UNEVENTFUL LANDING. FOUND FCC2 SHOWING LAST LEG FAULT "LAT ACC INV" FOR ALL THREE ADIRU. TROUBLESHOT IAW FIM 22-01-22 AND PERFORMED AUTOLAND SYS R-T-S IAW AMM 22-00-00. ALL SYS PASS. PERFORMED FUNCTIONAL TEST OF ADIRU 1, 2, & 3 IAW AMM 34-43-00-5, ALL SYS PASS, ACFT OK. FOR SERVICE. ACFT REMAINS CAT 3.

Part: RELAY — MALFUNCTIONED (EMERGENCY POWER) · airframe 80,853 hrs · 27,850 cycles

ON LEVELOFF AT FL 330, BUSS RT EMERGENCY AC OFF INDICATOR ILLUMINATED WITH ALL ASSOCIATED FAILURES. RAN CHECKLIST, AND DIVERTED IAW GOCC. TROUBLESHOT IAW FIM 24-25-01, FOUND REAC SENSE RELAY/INTFC FAULT CFDS. R & R SENSING RELAY R2-5157 AND RT EMERGENCY AC BUSS RCCB B1-138 IAW 24-50-01-2. R & R TRANSFER RELAY R2-18 IAW 24-25-03-2. PERFORMED EPCU RTS IAW 24-08-02/501 SATISFACTORY. ELECTRICAL EMERGENCY POWER SYS TEST PERFORMED IAW 24-00-00-50, NO DEFECTS NOTED. TRANSFERRED POWER FROM APU TO EXTERNAL POWER AND BACK SEVERAL TIMES NO DEFECTS NOTED. ACFT OK TO CONTINUE.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 80,505 hrs · 27,653 cycles

NO AIRSPEED ON TAKE OFF. LOW SPEED REJECT APPROX 80 KTS. PERFORMED A LOW SPEED ROLLOUT STOP AND WAS NOT A HIGH ENERGY STOP WITH MINIMAL BRAKING.

Part: ELT — NO TEST (CABIN) · airframe 80,130 hrs · 27,451 cycles

DURING "A" CHECK, FOUND ELT INOPERATIVE AND WOULD NOT TEST. T/S IAW FIM 23-25-00-1 AND AMM 23-25-00-4 AND FOUND ON-OFF-ARMED SWITCH ON TRANSMITTER IN THE OFF POSITION. PLACED SWITCH IN THE ARMED POSITION ON TRANSMITTER AND ELT TESTED NORMALY IAW 23-25-00-5-0 AND "A" CHECK STEP 7. G. T/S IAW FIM 23-25-00-1 AND AMM 23-25-00-4 AND FOUND ON-OFF-ARMED SWITCH ON TRANSMITTER IN THE OFF POSITION. PLACED SWITCH IN THE ARMED POSITION ON TRANSMITTER AND ELT TESTED NORMALY IAW 23-25-00-5-0 AND "A" CHECK STEP 7 G.

Part: RETAINER — FAILED (NR 8 BRAKE) · airframe 80,049 hrs · 27,402 cycles

NR 8 BRAKE, 9 ROTOR RETAINERS BROKEN, R & R NR 8 BRAKE ASSY REF AMM 32-43-01-4.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 80,049 hrs · 27,402 cycles

MAIN CARGO DECK AT STA 485 AND RBL 61 CORROSION FOUND IN SEAT TRACK. CUT OUT CORROSION ON SEAT TRACK AT STA 485, RBL REF SRM 53-70-00, FIG 2. PERFORMED PENETRANT INSP OF REPAIR CHANNEL REF DC NDT MANUAL. INSTALLED REPAIR IN SEAT TRACK AT STA 485 AND RBL 61, REF 53-70-00, FIG 2, CATAGORY "A" REPAIR.

Part: FRAME — CRACKED (ZONE 100) · airframe 80,049 hrs · 27,402 cycles

RT FRAME CRACKED AT INBD LEG OF FRAME, STA 1159, L 29R. REPAIRED PER SRM 53-30-00 FIG 7, AND EA 8-5310-150973

Part: LANDING GEAR — MALFUNCTIONED (RIGHT) · airframe 79,480 hrs · 27,122 cycles

AFTER TAKEOFF AND GEAR RETRACTION, RT MAIN GEAR INDICATED UNSAFE ON BOTH GEAR SYNOPTIC AND INDICATOR LIGHTS. COMPLIED WITH CHECKLIST AND GOT NORMAL INDICATIONS. NO FAULTS IN PSEU. PSEU RTS PASSED. CHECKED SENSOR READOUT IN PSEU AND ALL READINGS FOR RT MAIN GEAR ARE NORMAL. INSPECTED RT MAIN GEAR AND NO DEFECTS NOTED. ALL WORK IN REF TO MM 31-71-01-2-0, 32-00-00-00-0 AND 32-30-00-0-0. OK FOR SERVICE. FINAL CLOSED.

Part: BRACKET — BENT (MLG SENSOR) · airframe 77,377 hrs · 26,059 cycles

AFTER T/O RT MAIN GEAR SHOWED NOT RETRACTED RED ON BOTH THE INDICATORS COMPLIED WITH QRH LANDED BACK AT DEPARTURE. DROPPED RT GEAR DOOR TO ACCESS GEAR/ DOOR UP SENSOR. INSPECTED WIRING AND CONDITION OF SENSOR. NO DEFECTS NOTED. NOTICED THAT BOLT THAT ATTACHES SENSOR LEVER LINK TO UPPER SIDE GEAR BRACE WAS BENT. REMOVED BOLT AND FOUND LINK BEARING TO BE DAMAGED CAUSING A 7/16 OF AN INCH PLAY IN THE SENSOR LINKAGE. REMOVED LINKAGE, REPLACED BEARING AND REINSTALLED LINKAGE. CK'D SENSOR TO TARGET GAP, GAP CK'S GOOD. CK'D SAME LINKAGE ON LT GEAR. NO DEFECTS NOTED IAW MM 32-61-15-4.

Part: ROD END — OUT OF ADJUST (ACTUATOR) · airframe 77,362 hrs · 26,048 cycles

ON TAKE OFF RT MLG DID NOT RETRACT. GEAR STATUS CONFIRMED BY BOTH QRH PROCEDURES AND CALL FROM TOWER. COMPLIED WITH QRH. GEAR SUBSEQUENTLY RETRACTED NORMALLY. CHECKED RIG OF MLG MECHANICAL CONTROL PER AMM 32-31-01-5. NO DEFECTS NOTED. REMOVED LOWER ATTACH BOLT FROM MLG RETRACT ACTUATOR AND RAN UP AND DOWN SEVERAL TIMES TO ENSURE ACTUATOR BLED PER AMM 32-33-01-4. ROD END OF RETRACT ACTUATOR REQUIRED ADJUSTMENT PER AMM 32-33-01-4 WHEN REINSTALLING. CYCLED GEAR SEVERAL TIMES PER AMM 32-10-00-5. GEAR RETRACTS COMPLETELY WITH DOOR PINNED OPEN AND OPS NORMAL WITH DOOR ACTIVE.

Part: SENSOR — OUT OF RIG (MLG) · airframe 77,343 hrs · 26,036 cycles

AFTER TAKEOFF RT MAIN GEAR PRIMARY AND SEC GEAR INDICATOR LIGHTS SHOWED GEAR NOT UP AND LOCKED COMPLIED WITH CHECKLIST AND CYCLED GEAR ALL INDICATIONS NORMAL PRIOR TO RECYLING THE GEAR. DID NOT NOTICE ANT ADVERSE YAW OR NOISE INCREASE AS IF A GEAR WAS HANGING. PSEU FAULT HISTORY SHOWS 2 MARGINAL RIG FOR RT UP AND LATCHED SENSOR. FOUND RT UP AND LATCHED SENSOR OUT OF RIG IAW AMM 32-61-15-4. ADJUSTED SENSOR PER SAME. PERFORMED RTS OF PSEU. TEST GOOD. RETRACTED GEAR IAW AMM 32-30-00. ALL INDICATIONS GOOD. REMOVED ACFT FROM JACKS. OK FOR SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 77,283 hrs · 26,011 cycles

MAIN DECK, BELOW FLOOR-CORROSION ALONG BOLT LINE AT STA. 1370 BETWEEN UPRIGHTS R4 AND R9. WHERE THE SLANT PANEL MEETS THE UPPER AFT END OF THE WING BOX. REMOVED AND REPAIRED CORROSION AS REQUIRED, REF SRM 51-21-01 AND E.A. 8-5710-130986 (AFT UPPER SKIN-RT UPPER SURFACE CORROSION REWORK), WORK CARD SEQ. 24.

Part: FITTING — DAMAGED (CABIN FLOOR) · airframe 77,279 hrs · 26,004 cycles

UNDER MAIN CABIN FLOOR, LARGE SECTION OF NR 2 SYS DUCT PUSHED FWD. CAUSE UNKNOWN. FOUND BROKEN FITTING AT STA 735. REMOVED SYS 2 CLAMPS AND DUCTS. INSPECTED DUCTS AND FLANGES FOR CRACKS, FOUND TO BE SERVICEABLE. REINSTALLED DUCTS AND CLAMPS. REPLACED BROKEN FITTING. COMPLIED WITH EA 8-3610-132745 SUPPORT BRACKET AND JOINT REPLACEMENT SB DC-10-36-071. PERFORMED DUCT LEAK CHECK, NO LEAKS NOTED.

Part: THERMOCOUPLE — INOPERATIVE (ENGINE) · airframe 77,067 hrs · 25,903 cycles

DURING CLIMB, ENG CLIMB POWER ENG 1 EGT EXCEEDENCE 993'C MAX. TOTAL EXCEEDENCE TIME APPROX 15 SEC. NO ERRATIC N1, N2, OR F/F. EGT ROSE GRADUALLY & THEN SLOWLY DECLINED AS THROTTLE REDUCED TO IDLE. EGT IN LIMITS WITH THROTTLE REDUCED. NO FIRE WARNINGS. ATB & DECLARED AN EMERGENCY. INTERRIGATED NR 1 & 2 VIA ENG PEAK 992.5, EXCEEDED 925 DEGREES FOR 18.3 SECONDS. N1 104.3, N2 97.1 THE ACARS SYSTEM RECORDED THE EVENT WHICH CLEARLY POINTS TO AN EGT INDICATION PROBLEM & NOT AN ACTUAL PERFORMANCE ISSUE. REPORT SHOWS TEMP INCREASED 110 DEG C IN 1 SEC WITH NO OTHER PARAMETER CHANGES, WHICH IS BEYOND THE INDICATION CAPABILITY. R&R FWD, THERMOCOUPLE & HARNESS IAW AMM 77-21-01-2. PERF HIGH PWR ENG RUN IAW THE JRH AND AMM 72 ALL IND WITHIN LIMITS.

Part: WIRE — CHAFED (ENGINE) · airframe 75,807 hrs · 25,339 cycles

NR 2 ENGINE SHUTDOWN IN FLIGHT. ON CLIMB-OUT PASSING FL 250 HAD A LEVEL 1 NR 2 ENGINE EGT EXCEEDANCE. PER CHECK LIST BROUGHT POWER BACK. TEMP CAME DOWN WITHIN LIMITS BUT SHORTLY CLIMBED BACK ABOVE REDLINE AND HAD A NR 2 EGT HIGH LEVEL 2. SHUT ENGINE DOWN AND RETURNED TO LAND PER CHECKLIST. FOUND WIRES J011-229-20GR AND J011-229-20WH CHAFED THRU SHIELDING AND INTO CONDUCTORS INSIDE OF J BOX, APPROX 6 INCHES BACK FROM PLUG R5-8216. AFTER EA 8-7720-123490, RETERMINATED NR 2 ENG EGT WIRES PER MD10-10 WDM 77-21-01. CONTINUITY CHECK 'OK'. ENG AT MAX ASSURANCE POWER PER MD10-10 JRH ALL PERIMETERS GOOD. OPS CK GOOD.

Part: WIRE — CHAFED (NR 2 ENGINE) · airframe 75,807 hrs · 25,339 cycles

NR 2 ENGINE SHUTDOWN IN FLIGHT. ON CLIMB-OUT PASSING FL 250 HAD A LEVEL 1 NR 2 ENGINE EGT EXCEEDANCE. PER CHECKLIST BROUGHT POWER BACK. TEMP CAME DOWN WITHIN LIMITS BUT SHORTLY CLIMBED BACK ABOVE REDLINE AND HAD A NR 2 EGT HIGH LEVEL 2. SHUT ENGINE DOWN AND RETURNED TO LAND PER CHECKLIST. FOUND WIRES J011-229-20GR AND J011-229-20WH CHAFED THRU SHIELDING AND INTO CONDUCTORS INSIDE OF J BOX , APPROX 6 INCHES BACK FROM PLUG R5-8216. AFTER EA 8-7720-123490, RETERMINATED NR 2 ENG EGT WIRES PER WDM 77-21-01. CONTINUITY CHECK 'OK'. ENG AT MAX. ASSURANCE POWER PER JRH ALL PARAMETERS GOOD OPS CK GOOD.

Part: SKIN — CRACKED (ZONE 300) · corrosion level 2 · airframe 73,998 hrs · 24,502 cycles

LEFT OUTBOARD ELEVATOR UPPER SKIN BULGE/CRACKED AND CORRODED 1.5" FROM INBOARD END AND 2 FEET FROM TRAILING EDGE. REMOVED ENTIRE DAMAGED UPPER SKIN SECTION, APPROXIMATELY 18" TIMES 24", REQUIRED FOR DISCREPANCY CLEAN-UP AND REPAIRED IAW MD/DC10-10 SRM 55-10-00 FIG,8 VOL, 1. CALCULATED NEW WEIGHT AND BALANCE FOR LEFT OUTBOARD ELEVATOR AT 892.77 TAIL HEAVY INCH POUNDS, FOUND TO BE WITHIN LIMITS IAW MD/DC10 SRM 55-20-00 PAGE 1, PARAGRAPH 1A, VOL 11.

Part: FRAME — CORRODED (BS 1401) · corrosion level 3 · airframe 73,998 hrs · 24,502 cycles

CENTER WHEEL WELL SPACE, STA 1401 FWD LWR SIDE OF FRAME FROM L51L - L51R CORROSION REMOVED CORROSION IAW MD/DC10-10 SRM 51-21-01 VOL 2 PG 28. FOUND TO BE OUT OF LIMITS IAW MD/DC10-10 SRM 53-00-01 VOL 1 FIG 1B. REPAIRED FRAME AT STA 1401 IAW MD/DC10-10 SRM 53-00-01 VOL 1 FIG 8. ORIGINAL THICKNESS .080 IAW MD/DC10-10 SRM 53-14-01 VOL 3 FIG 11. REMOVED .043 REMAINING .037.

Part: FRAME — CORRODED (BS 1421) · corrosion level 2 · airframe 73,998 hrs · 24,502 cycles

CENTER WHEEL WELL SPACE-STA 1421, L52L-L51L FRAME (LWR) CORROSION REMOVED CORROSION IAW MD/DC10-10 SRM 51-21-01 VOL 2, PG 28 FOUND TO BE OUT OF LIMITS IAW MD/DC10-10 SRM 53-00-01 VOL 1 FIG 1B. REPAIRED FRAME AT STA 1421 IAW MD/DC 10-10, SRM 53-00-01 VOL 1 FIG 8. ORIGINAL THICKNESS .080 IAW MD/DC10-10 SRM AND 53- 00-01 ORIGINAL THICKNESS .080 IAW MD/DC SRM 53-14-01 VOL 3 FIG 11 REMOVED .029 REMAINING .051

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,998 hrs · 24,502 cycles

FORWARD PIT BILGE STRINGER 52 HAS EXFOLIATED CORROSION IN UPPER CENTER CHANNEL AT BS 824. REMOVED CORRODED SECTION OF LONGERON IAW MD/DC10-10, SRM 53-10-00 FIG 1 VOL 1. INSTALLED NEW SECTION OF LONGERON AND SPLICE REPAIR IAW MD/DC10-10 SRM 53-10-00 FIG, 1 VOL 1, MD/DC10-10 SRM 53-10-00 FIG 2 VOL 1, MD/DC10-10 SRM 51-33-01 PG 1 VOL 11 CAT B REPAIR IAW MD/DC10-10 SRM 53-10-00 FIG 1 AND FIG 2 VOL, 1.

Part: SKIN — DENTED (ZONE 500) · airframe 73,998 hrs · 24,502 cycles

LEFT WING INBOARD FLAP LOWER SKIN HAS SIX DENTS IN SAME AREA XORS299-372. REMOVED AND REPLACED SKIN SECTION AND DOUBLER ON WEDGE IAW MD/DC 10SRM 57-10-00 VOL I FIG 3, AND 51-35-01 VOL II. ALODINED AND PRIMERED IAW MD/DC10 SRM 51-21-01 VOL II.

Part: BEAM — CRACKED (ZONE 100) · airframe 73,998 hrs · 24,502 cycles

MAIN CARGO DOOR SPOOL NR 7, AFT OUTBOARD ATTACH HOLE SHOWS SIGN OF CRACK INDICATION IAW NTSPM 06-10-01.0003 REAMED HOLE UP TO .520 AND ACCOMPLISHED A BHEC INSPECTION. NO CRACK NOTED IAW NTSPM 06-10-01.0003. FABRICATED, INSTALLED AND REAMED TO SIZE REPAIR BUSHING IAW MD/DC 10 SRM 53-50-00 VOLI PG 81.

Part: LONGERON — CRACKED (ZONE 100) · corrosion level 2 · airframe 73,998 hrs · 24,502 cycles

AFT CARGO PIT AT FS 1950 LONGERON 51L IS CORRODED AND CRACKED. [08-29-07] REMOVED CORRODED SHOVEL END FITTING IAW MD/DC10 SRM 51-33-01 PAGE 1 VOL II. DRILLED NEW SHOVEL END FITTING P/N AGA3092-503 TO FIT IAW MD/DC10 SRM 51-31-01 PAGE 7 VOL II. INSTALLED NEW SHOVEL END FITTING IAW MD/DC10 SRM 51-33-01 PAGE 1 VOL II.

Part: SKIN — ACTIVATED (RT ELEVATOR) · airframe 73,998 hrs · 24,502 cycles

RT INBD ELEV LOWER SURFACE PUNCTURED APPROX 5 ' FROM INBD END AND 1' FROM L/E DOT N5102 RPAIRED RT INBOARD ELEVATOR LOWER SURFACE IAW DC/MD 10-10 SRM 55-00-01 VOL 1 PG 9.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 72,427 hrs · 23,821 cycles

HORIZONTAL STAB UPPER LT SKIN PANEL 7439-1 CRACKED 3.5 INCHES. VERIFIED END OF CRACK WITH HI-FREQ E/C. REFERENCE E/A 8-5510-102053 FOR INTERIM REPAIR AND FERRY FLIGHT, AND REFERENCE E/A 8-5510-102054 FOR PERMANENT REPAIR. A/C FERRIED TO LAX FOR PERMANENT REPAIR DOCUMENTED UNDER E/A 8-5510-102054. INTERIM REPAIR ACCOMPLISHED BY IND HVMX DOCUMENTED UNDER E/A 8-5510-102053 PN 299542. REPAIR IS IN WORK AT LAX HVMX. PERFORMED PERMANENT REPAIR PER EA 8-5510-102054.

Part: ENGINE — VIBRATION (NR 1) · airframe 68,861 hrs · 22,415 cycles

AT FL 340 EXPERIENCED NR 1 ENGINE VIBRATION, N1 ROLLED BACK TO 34%, N2 62% FF 690 LBS. EXECUTED ENG FIRE SEVERE DAMAGE CHECKLIST, FUEL DUMP ABOUT 3000 LBS, DECLARED EMERGENCY LANDING 18C. INSPECTED INTAKE AND EXHAUST. NO DEFECTS NOTED. BOROSCOPE INSPECTED NR 1 ENGINE PER W/C 72X3501, NO DEFECTS NOTED, ENGINE OK FOR SERVICE. AFTER BOROSCOPE FOUND LOOSE B-NUT ON CDP LINE AT COMPRESSOR CASE. PERFORMED BOROSCOPE INSPECTION OF NR 1 ENG PER W/C 72X3501. NO DEFECTS NOTED. HOOKED UP VIBE SENSOR AND TACH WIRE ON NR 1 ENG FOR VIBE RUN. PERFORMED VIBE SURVEY PER MD-10-10 AMM 72-00-00-51, INDICATIONS ARE LESS THAN 1.0 MILS AT 3400, 3200 AND 3000 RPM. ENGINE RAN PER JRH.

Part: HINGE — CORRODED (ZONE 500) · airframe 67,538 hrs · 22,002 cycles

COMPLY WITH EA 8-5750-80598, WINGS LT INBD FLAP INBD MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COMPLIED WITH EA 8-5750-80598.

Part: HINGE — GOUGED (ZONE 500) · airframe 67,538 hrs · 22,002 cycles

COMPLY WITH EA 8-5754-80608, WINGS, LEFT INBD FLAP, OUTBD HINGE BRACKET, UPSTOP MOUNT HOLE REPAIR P/N ARC 0154. COMPLIED WITH E.A.8-5754-80608.

Part: HINGE — CORRODED (ZONE 600) · airframe 67,538 hrs · 22,002 cycles

WINGS, RT INBD FLAP AFT HINGE ASSY ARC2512,PIVOT BORE CORROSION. COMPLIED WITH E.A.8-5750-80602.

Part: VANE — CORRODED (LT OB FLAP) · corrosion level 2 · airframe 67,538 hrs · 22,002 cycles

BFM CLOSE R COMPLY WITH EA NR 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK ENT BY: 527637 RPT BY: 527637 FACT 01 SEP04 04:30 BFM U COMPLIED WITH EA 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK RII:497214, ENT BY: 527637 RPT BY: 527637.

Part: PANEL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 67,538 hrs · 22,002 cycles

CTR CARGO SUMP PNL 1741-1721 CRACKED AND CORRODED RT SIDE. REMOVED AND REPLACED IAW DRWG AFA0153 AT MAE.

Part: PANEL — CRACKED (FUSELAGE) · airframe 67,538 hrs · 22,002 cycles

FWD CARGO SUMP PANEL IS CRACKED RT SIDE 960-980. REMOVED AND REPLACED PANEL IAW IAW DRWG ADA0140 AT MAE.

Part: PANEL — CRACKED (CARGO BAY) · corrosion level 2 · airframe 67,538 hrs · 22,002 cycles

FWD CARGO SUMP PANEL CRACKED & CORRODED STA 920 TO 940. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE.

Part: PANEL — CRACKED (CARGO BAY) · corrosion level 2 · airframe 67,538 hrs · 22,002 cycles

FWD CARGO SUMP PNL STA 940-960 CRACKED LT SIDE. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE.

Part: PANEL — CRACKED (CARGO BAY) · corrosion level 2 · airframe 67,538 hrs · 22,002 cycles

FWD CARGO SUMP PNL STA 900-920 IS CRACKED AND CORRODED RT SIDE. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE.

Part: PROXIMITY SENSOR — FAULTY (CARGO DOOR) · airframe 66,994 hrs · 21,820 cycles

ON EXT FINAL TO MEM RECEIVED AN ALERT INDICATING THE MAIN CARGO DOOR WAS OPEN (B-LOOP). DOOR WAS VERIFIED CLOSED BY FIRE/RESCUE PERSONNEL AFTER LANDING. RELEASED FOR SERVICE PER MEL/CDL: 52-40-01-06 CATEGORY: B EXPIRATION: 29MAY04 MEL 52-40-01-06: CARGO DOOR UPPER B ALERT INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT. REPLACED CARGO DOOR PROX SENSOR IAW MM 52-70-06-2. OPS CHECKS GOOD.

Part: FILTER — INOPERATIVE (NR 3 HYD SYS) · airframe 64,866 hrs · 20,834 cycles

AT CRUISE NR 3 HYD WENT TO 0.1 QTY. FOLLOWED PROCEDURE IN QRH - COULD NOT EXT SLATS. EXECUTED A NO SLAT/FLAPS 22 DEG LANDING. CHECKED LT & RH CASE DRAIN & PRESS FILTERS FOR METALLIC RESIDUE. R & R ALL ENGINE HYD FILTERS, R & R NR 3 LOWER ENGINE HYD PUMP PER MM 29-11-01-2 REPLACED UPPER PUMP PER M/M 29-11-01-2.REPL MAIN FILTERS. FILLED SYS. BLED AND RAN ENGINE. FLIGHT CONT LEAK CHECK GOOD. RAN FLT CONT CHECKS PER M/M 27-85-01 RTS PASSED.

Part: SHUTOFF VALVE — FAILED (HYDRAULIC SYS) · airframe 62,578 hrs · 63,255 cycles

AFTER 80 KTS STABILIZER MOTION AURAL WARN ACCOMPANIED RED ANNUNCIATOR ON EAD.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,588 hrs · 19,646 cycles

DURING D-CK, 1 INCH CRACK FOUND AT Y=1386 ON AEA0501-2 KEEL WEB UPPER SPLICE ONLY. REMOVED AND REPLACED TITANIUM REPAIR DOUBLER PER IAW FEDEX EA 8-5314-56044.