N308FE

Part: PSEU — MALFUNCTIONED (MLG) · airframe 74,170 hrs · 25,126 cycles

ON FINAL FOR KMEM 18L AT 3000 FT, WE PUT THE GEAR HANDLE DOWN AND RECEIVED 4 RED GEAR UNSAFE INDICATIONS. WE EXECUTED A GO AROUND TO REENTER THE PATTERN AND RAN THE GEAR UNSAFE INDICATION WITH GEAR HANDLE DOWN CHECKLIST. AFTER RUNNING THE CHECKLIST WE WERE ABLE TO GET A 4 GREEN INDICATION. DECLARED EMERGENCY LANDED UNEVENTUALLY. TROUBLESHOOTING PERFORMED REF MD10-30- FIM REF TO 32-30-00-2 FOUND NO CURRENT OR PAST FAULTS ON PSCU. ALSO PERFORMED PIN PROGRAM OPTION PER MD10-30 FIM 32-30-00-2 PER TABLE 202 FOUND NO FAULTS. ALSO NO ISSUES WITH GEAR HANDLE. DID JACK A/C AND PERFORMED NORMAL GEAR OPERATION VARIOUS TIMES PER MD10-30 AMM 32-30-00-5 NO FAULTS NOTED. DID REPLACE A/C PSCU AS AN PERCAUTIONARY REF TO MD10- 30 AMM 31-71-01-2 AND OPS CHECK NORMAL RTS SYSTEM ALSO CHECKS NORMAL THIS TIME. OK FOR SERVICE. ( PSCU , ELDEC CORP P/N 8-946-01 S/N A82).

Part: FITTING — CRACKED (MLG DOOR) · airframe 73,774 hrs · 24,931 cycles

CENTER LANDING GEAR LT AFT DOOR, AFT LOWER SUPPORT WAS CRACKED AT LOWER ATTACH LUG HOLE. REMOVED AND REPLACEED LT MLG DOOR LOWER AFT LINK FITTING IAW DRAWING ABN7451.

Part: HINGE FITTING — CRACKED (NLG DOOR) · airframe 73,774 hrs · 24,931 cycles

CENTER LANDING GEAR LH AFT DOOR IS LOOSE AT FWD AND AFT HINGES. REMOVED AND REPLACED FITTING IAW DAC DWG ANB7451.

Part: VANE — WORN (LT WING TE FLAP) · airframe 73,774 hrs · 24,931 cycles

LEFT WING INBOARD FLAP VANE WORN ON TOP INB INLINE WITH BUB STRIP APPROX. 4 INCHES. REPAIRED WORN AREA ON L/H I/B FLAP VANE AS REQUIRED REF. SRM 57-00-01 VOL.I PG.11 AND SRM 51-71-00 VOL.II.

Part: RIB — CRACKED (CARGO DOOR) · airframe 73,774 hrs · 24,931 cycles

CENTER CARGO DOOR FWD RIB LOWER END IS CRACKED AND PIECE MISSING. REMOVED DAMAGED SECTION OF CENTER CARGO DOOR FWD RIB LOWER END AND INSTALLED REPAIR ANGLE AND FILLER REF. SRM 53-00-01 FIG. 8 VOL. 1.

Part: FLOOR SUPPORT — CORRODED (BS 1845) · airframe 73,774 hrs · 24,931 cycles

MAIN CABIN FLOOR AT STA 1845 RBL 7 UNDER FLOOR BOARD SUPPORT IS CORRODED AT NUT PLATE HOLE. (MKD) REPLACED PER DAC DWG AGA3814

Part: FLOOR SUPPORT — CORRODED (BS 1885) · airframe 73,774 hrs · 24,931 cycles

INSIDE MAIN CABIN, AT BS 1885, LBL 20 UNDER FLOOR PANEL, HAT SECTION SUPPORT IS CORRODED AT NUT PLATE HOLES. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-35-01,V2 AND DWG AGA7559.

Part: FLOOR SUPPORT — CORRODED (BS 1885) · airframe 73,774 hrs · 24,931 cycles

INSIDE MAIN CABIN, AT STA 1885 LBL 44, UNDER FOOL SUPPORT HAT SECTION, IS CORRODED AT NUT PLATE HOLES. (MKD) AT STA. 1885, LBL 44, REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AGA 7559-5 PER DAC. DWG. AGA 7559. INSTALLED FASTENERS PER SRM 51-31-01 VOL 2.

Part: FLOOR SUPPORT — CORRODED (BS 1885) · airframe 73,774 hrs · 24,931 cycles

INSIDE MAIN CABIN, AT BS 1885, RBL 20, UNDER FLOOR PANEL SUPPORT IS CORRODED AT NUT PLATE HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG AGA7091, AND SRM 51-31-01,V2.

Part: FLOOR SUPPORT — CORRODED (BS 1885) · airframe 73,774 hrs · 24,931 cycles

INSIDE MAIN CABIN, AT STA 1885 LBL 36, UNDER FLOOR PANEL SMALL HAT SECTION IS CORRODED AT NUTPLATE HOLE. (MKD) AT STA. 1885, LBL 36, REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AGA 7559-5 PER DAC. DWG. AGA 7559. INSTALLED FASTENERS PER SRM 51-31-01 VOL 2.

Part: FRAME — BENT (FUSELAGE) · airframe 73,774 hrs · 24,931 cycles

MAIN CARGO LT STA 1641 BETWEEN STR L13-L14. FRAME IS BENT. CUT OUT FRAME AND INSTALLED NEW FRAME SECTION PER SRM 53-30-00 FIG05 AND SRM 51- 38-01 VOL II.

Part: SKIN — GOUGED (RT WING LE FLAP) · airframe 73,774 hrs · 24,931 cycles

R/H WING, L/E, I/B FLAP, APPROX. STA. XIFH280 FOUND A GOUGE UNDERNEATH RUB STRIP. INSTALLED REPAIR DOUBLER I.A.W. SRM57-00-01 FIG. 4 SHT.2 VOL. I

Part: FLOOR SUPPORT — CORRODED (BS 1541-1581) · airframe 73,774 hrs · 24,931 cycles

CENTER CARGO COMPARTMENT, FROM STATION 1541 TO STATION 1581, RBL-57 INTERCOSTALS CORRODED. REMOVED AND REPLACED CENTER CARGO COMPARTMENT INTERCOSTALS FROM STA.1541 TO STA. 1581,RBL-57. REF. SRM 51-31-02, VOL II; DAC DWG ACA7049.

Part: SUPPORT — CRACKED (RT WING) · airframe 73,774 hrs · 24,931 cycles

RIGHT WING, LOWER LEADING EDGE WAS CRACKED ON PANEL LAND, AFT OF NR 9 SLAT TRACK. REMOVED AND REPLACED DAMAGED SUPPORT ARB2933-50 IAW DWG ARB2933 AND SRM 51-33-01 V2 AND SRM 51-35-01 V2 REMOVED DAMAGED DOUBLER ARB2933-50. REMOVED DOUBLER ARB2933-50 IAW SRM 51-31-01. MATERIAL VERIFIED MA3941560 7075T6 .090., FABRICATED ARB233-50 IAW DWG ARB 2933. ALODINED AND PRIMED IAW SRM 51-21-01. INSTALLED SUPPORT IAW DWG 2933, SRM 51-33-01, AND SRM 51-35-01.

Part: FLOOR SUPPORT — CORRODED (BS 1747) · airframe 73,774 hrs · 24,931 cycles

MAIN CARGO DECK, STA1747 70RBL FLOOR SUPPORT HAS CORROSION (MARKED) REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH NEW PER DWG AFA 3853 AND SRM 51-31-01,V2.

Part: SEAT TRACK — CORRODED (BS 1975) · airframe 73,774 hrs · 24,931 cycles

MAIN DECK SEAT TRACK BS 1975 RBL 35 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW DWG AGA7091, AND SRM 51-31-01,VOL 2.

Part: SEAT TRACK — CRACKED (BS 1701) · airframe 73,774 hrs · 24,931 cycles

CTR. CARGO COMPT CEILING: STA. 1701 - 27.50 RBL, SEAT TRACK HAT SPLICE CRACKED (VIEWED LOOKING UP FROM CTR. CARGO COMPT.) MRKD. FABRICATED AND INSTALLED -20 SPLICE PLATE, PER DWG SR10-53-010.

Part: FLOORBEAM — CORRODED (BS 1781) · airframe 73,774 hrs · 24,931 cycles

CENTER CARGO COMPT: APPROX STA 1781, X=-16.5 FLOOR BOARD SUPPORT EXTRUSTION. 1 CLIPNUT HOLE SHOWS CORROSION. (UNDERSIDE) MARKED. INSTALLED FLOOR BOARD SUPPORT PER DAC DWG AFA7299.

Part: SUPPORT WEB — CRACKED (BS 1701) · airframe 73,774 hrs · 24,931 cycles

CTR CARGO COMPT: STA 1701 APPROX LONGERON 44L-47L - LOWER SUPPORT WEB CRACKED BELOW ROLLER TRAYS. (MRKD) REMOVED AND REPLACED CRACKED SECTION OF FLOOR BEAM IN CENTER CARGO, STA-1701, REF SRM 53-60-01, PG-7, FIG-3, SHEET-1, VOL-I; SRM 51-33-01, VOL-II; SRM-51-35-01, VOL-II.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,774 hrs · 24,931 cycles

CENTER CARGO COMPT: APPROX STA 1521 X=56.19. RT O/B CARGO RAIL. REF FWD ATTACH FASTENERS. (UNDERSIDE IN CHANNEL) FASTENER NUTS, WASHERS AND STRUCTURE CHANNEL CORRORED. REPAIRED CORRODED CHANNEL REF SRM 53-00-01, VOL I; FIG 7; SHEET 7.

Part: SKIN — GOUGED (LT WING) · airframe 73,774 hrs · 24,931 cycles

LT WING FIXED LEADING EDGE - REPAIR DOUBLER INBD SIDE OF ANTI-ICE DUCT HAS GOUGE CAUSED BY CONTACT WITH SLAT. REPAIRED L/H WING SKIN ATSLAT ANTI-ICE TELESCOPING DUCT CUT OUT REF SRM 57-10-00 FIG. 40 SHEETS 1-3 VOL. 1.

Part: SKIN — CRACKED (LT WING) · airframe 73,774 hrs · 24,931 cycles

LT WING FIXED LEADING EDGE - REPAIR DOUBLER OUTBD SIDE OF ANTI-ICE DUCT HAS GOUGE CAUSED BY CONTACT WITH SLAT. (MARKED) REPAIRED L/H WING SKIN AT SLAT ANTI-CE TELESCOPING DUCT CUT OUT REF SRM 57-10-00 FIG 40 SHEETS 1-3 VOL. 1.

Part: FLOORBEAM — CORRODED (BS 841) · airframe 73,774 hrs · 24,931 cycles

AFT CARGO COMPT: APPROX STA 1841, FLOOR SUPPORT ANGLE HAS CORROSION AT NUT PLATES. (UNDERSIDE OF ANGLE). HEAVY AND LIGHT FROM RIGHT TO LEFT SIDE OF A/C. REMOVED AND REPLACED FLOOR SUPPORT AT STATION 1841 FROM RBL-1 TO RBL-63 REF DAC DWG AGA7170 AND SRM 51-31-01 VOL.2.

Part: FRAME SPLICE — CRACKED (BS 1741) · airframe 73,774 hrs · 24,931 cycles

MAIN DECK STA 1741 FRAME SPLICE DOUBLER CRACKED. MRKD LH SIDEWALL BETWEEN L13L- L14L REMOVED AND REPLACED PER DWG AFA 0018

Part: BULKHEAD — CRACKED (BS 1986) · airframe 73,774 hrs · 24,931 cycles

FUSELAGE AFT PRESSURE BULKHEAD, FWD SIDE, AT UPPER CANTED AREA, PREVIOUS REPAIR BLEND OUT HAS A "1/2" INCH CRACK INDICATION. INSTALLED A REPAIR IAW EA 8-5310-T0348800.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 73,774 hrs · 24,931 cycles

LEFT WING NR 8 SLAT, INBD LOWER SKIN WAS CRACKED. REMOVED AND REPLACED THE LT WING NR 8 SLAT, ADJUSTED AND OPS CHECKED GOOD IAW AMM 27-80-01-4, AND AMM 27-80-00-5.

Part: SKIN — WORN (RT WING) · airframe 73,774 hrs · 24,931 cycles

RT WING DROOP L/E, INBD SIDE OF DROOP L/E SKIN HAS WEAR GROOVE/MARKS (MARKED AND DOT 4) PERFORMED DLE SKIN REPAIR I.A.W. SRM 57-10-00 , PARA. 95 AND FIG. 97 VOL I

Part: FRAME — CRACKED (BS 1501) · airframe 73,774 hrs · 24,931 cycles

LH WHEEL WELL FRAME STA. 1501 APPROX STRINGER 33 - 1 INCH CRACK EMANATING FROM FASTENER HOLE AT FRAME. CRACK WAS CONFIRMED USING NDT HFEC. REPAIRED CRACKED FRAME REF DAC DWG AEA0439 AND SRM51-33-01 VOL. 2, SRM 53-00-01 FIG. 8 VOL. 1.

Part: SEAT TRACK — WORN (BS 1122) · airframe 73,774 hrs · 24,931 cycles

MAIN DECK: SEAT TRACK WORN NEAR STA. 1122 AT RBL X=8.50. AREA MARKED RED REPLACED PER SRM CH 53-70-00,FIG 1,VOL 1.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 73,276 hrs · 24,703 cycles

FUME EVENT. ON TAKEOFF FROM CYMY WITH ENGINES SET TO TAKEOFF POWER AND ABOVE 80KNOTS, BOTH CREW MEMBERS SMELLED A MODERATELY INTENSE BURNED OIL ODOR. THE ODOR DISIPATED DURING CLIMB OUT AND WAS GONE BY 10,00FT MSL. RAN ALL 3 ENGINES AT IDLE PER JRH AND PERFORMED FUNCTIONAL TEST OF ALL 3 A/C PACK IAW AMM 21-00-01-5. NO ODORS NOTICE DURING ANY PACK OPERATION - FUEL USED RECORDED ON FUEL SLIP - AIRCRAFT OK FOR SERVICE.

Part: LANDING GEAR — DAMAGED (CENTER) · airframe 72,982 hrs · 24,580 cycles

AFTER TAKEOFF FROM 36L WITH GEAR HANDLE UP WE RECEIVED A UNSAFE CENTER GEAR INDICATION IN BOTH THE PRIMARY AND SECONDARY INDICATORS. CYCLED GEAR HANDLE PER QRH AND STILL HAD PRIMARY AND SECONDARY CENTER GEAR UNSAFE INDICATION W/GEAR HANDLE UP. GEAR HANDLE DOWN YOU GET ALL FOUR GEAR DOWN AND LOCKED. REMOVED AND REPLACED CENTER LANDING GEAR ASSY AMM 32-15-01-4.

Part: DOOR — INOPERATIVE (L1) · airframe 71,425 hrs · 23,784 cycles

L1 DOOR DID NOT WORK ELECTRICALLY.

Part: PANEL — DELAMINATED (WNG-BDY FAIRING) · airframe 71,035 hrs · 23,583 cycles

RIGHT WING TO FUSELAGE FIXED FAIRING, T/E AT INBD FLAP, PANEL ARC0288-504 R2, PREVIOUS REPAIR HAS COME OFF AND BOTTOM SIDE IS DELAMINATED. REPAIRED.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 71,035 hrs · 23,583 cycles

RIGHT WING NR 1 SPOILER OTBD TOP SECTION HAS A 2.75 X 3.5 INCHES OF DELAMINATION AT XORS 346. REPAIRED THE SPOILER IAW SRM 71-00-01, FIG 4, SHEET 1, VOL I.

Part: DOUBLER — CRACKED (RT WING) · airframe 71,035 hrs · 23,583 cycles

RT WING LE XORS 562 INNER BEADED DOUBLER IS CRACKED. CONDITION CONFIRMED WITH HFEC. REPAIRED PER SRM 57-10-T0335748.

Part: FITTING — CRACKED (CARGO DOOR FRAME) · airframe 71,035 hrs · 23,583 cycles

MAIN CARGO DOOR FRAME NR 7 LATCH SPOOL LOWER SUPPORT FITTING HAS A ONE INCH CRACK EMANATING FROM RETAINER HOLE AT THE FWD INBD SIDE OF FITTING. INSTALLED A NEW SPOOL SUPPORT FITTING IAW SRM 51-33-01, FIG 1, PAGE 1, VOL.2.

Part: FRAME — CRACKED (RT WING) · airframe 71,035 hrs · 23,583 cycles

RT WING LEADING EDGE FRAME ARB1161-15 AT STA XRS 269 IS CRACKED. RT LEADING EDGE FORMER REPAIRED PER EA 8-5710-T0335774.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,035 hrs · 23,583 cycles

AFT WASTE COMPT STA 2007 APPROX 24LBL UNDERSIDE OF FLOOR SUPPORT TRACK CORROSION. REMOVED AND INSTALLED NEW FLOORBOARD SUPPORT BEAM PER DRAWING AGA7087 AND SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 71,035 hrs · 23,583 cycles

UPPER MAIN DECK SEAT TRACK WORN AT RBL 8.50 NEAR STA 675. REMOVED AND INSTALLED DAMAGED SEAT TRACK REF SRM 53-70-00 FIG 11 VOLUME 1.

Part: SEAT TRACK — WORN (BS 615) · airframe 71,035 hrs · 23,583 cycles

UPPER MAIN DECK, TWO SEAT TRACKS WORN AT LBL 47.50 NEAR BS 615. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL I, SRM 51-4-01, VOL II, AND SR10-53-002A. MAJOR REPAIR.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,035 hrs · 23,583 cycles

A/C COMPT PACK BAY NR 1, APPROX STA 553 LONG 36 REF PACK BAY DOOR (113DL). FWD FRAME OF DOOR CUTOUT. THE FRAME IS CRACKED. IT HAS APPROX A 2" CRACK NEAR TOP OF THE FRAME. REPAIRED FRAME PER EA 8-5310-T0335533.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY LIGHTS) · airframe 69,331 hrs · 22,791 cycles

RECIEVED AN EMERGENCY LIGHT BATTERY 1 LOW, ALERT DURING EMERGENCY LIGHT TEST.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 68,855 hrs · 22,590 cycles

DURING HYD LEAK CHECK INSPECTION, OPENED & CLOSED RT MAIN GEAR DOOR. WHEN CLOSING THE RT GEAR DOOR, THE DOOR WOULD NOT STAY UP. TROUBLE SHOT TO THE LATCH ACTUATOR. R & R RT MAIN GEAR DOOR LATCH CYLINDER IAW MM CH 32-34-02-2. OPS & LEAK CHECKED GOOD. RT GEAR DOOR STILL DROPS WHEN HYD TURNED OFF. FOUND LT MAIN GEAR DOOR FRAME CRACKED. EA 8-3210-T0324543 PT 1 COMPLIED WITH. FOUND CRACK ON RT GEAR DOOR, EA 8-3210-T0324543 WAS ACCOMPLISHED. R & R RT MLG DOOR MM IAW 32-14-01-2 D STEP 6. UPDATING FOR RII BUY BACK OF RT MLG DOOR INSTALL WRI 52-80 2674. COMPLETED INSTALLATION, ADJUSTMENT TEST FOR THE RT MLG DOOR IAW AMM 32-14-01-2. OPS CHECKED GOOD.

Part: SKIN — CRACKED (A/C DOOR) · airframe 679 hrs · 22,228 cycles

SIX INCH CRACK ON EXTERNAL SKIN OF NR 3 ACM ACCESS DOOR. REPAIRED THE CRACK SKIN IAW EA 8-5240-T0320735 A.

Part: BULKHEAD — DENTED (FUSELAGE) · 22,228 cycles

CENTER CARGO STATION 1841, RBL 6, BULKHEAD WEB HAS LARGE DENT. REPAIR DOUBLER IAW EA 8-5310-T0320825.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 679 hrs · 22,228 cycles

CENTER CARGO STATION 1841, LBL 6, BULKHEAD WEB HAS LARGE DENT. CUT OUT DENTED WEB AS REQUIRED IAW SRM 51-00-01 FIG 10. INSTALLED REPAIR DOUBLER IAW EA 8-5310-T0320825 PART 1.

Part: WEB — CRACKED (RT MLG WW) · airframe 679 hrs · 22,228 cycles

RIGHT MLG WW NR 3 RESERVOIR, LOWER ATTACH STRUCTURE WEB CRACKED. REMOVED LOWER ATTACH STRUCTURE WEB, RT MLG WW IAW SRM 51-31-01 VOL 2. INSTALLED & FABRICATED STIFFENER PN AEA7035-10 IAW DWG AEA 7035.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 679 hrs · 22,228 cycles

CENTER WING LOWER BARREL, CTR AUXILIARY TANK, CORROSION UNDER RUB STRIPS OF UPPER INBD & OTBD STRIPS. STRUCTURE IS FOR CTR AUXILIARY FUEL TANK COVER. REMOVED LIGHT CORROSION AROUND HOLES IAW SRM 51-00-01 VOL II.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 673 hrs · 21,905 cycles

WHILE PERFORMING PRE-DEPARTURE CHECK RECEIVED, EMER BAT 1 LOW ALERT, WHEN PERFORMING EMER LIGHT TEST. R & R EMER LIGHTING BATTERY POWER SUPPLY IAW MM 33-51-01-4-1. OPERATIONS CHECKED GOOD IAW MM 33-51-01-5. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 65,548 hrs · 21,157 cycles

DURING INSPECTION, THE RT WING FIXED LE FOUND A 1/2 INCH CRACK AT THE NR 2 SLAT TELESCOPING ANTI-ICE DUCT CUT OUT, UPPER OTBD RADIUS. PERFORMED HFEC ON RT WING, AT SUSPECTED CRACK LOCATION TO VERIFY CRACK IAW NTM PT 6. IAW SHEET METAL REQUEST, REMOVED RT WING LOWER LE PANEL JUST OTBD OF TELESCOPING DUCT & REMOVED TELESCOPING DUCT UPPER CUT OUT DOOR IAW SMP. REMOVED DAMAGE AS SHOWN IN FIG 1 IAW EA 8-5710-T0308427 P 1. REQUIRES HFEC TO ENSURE DAMAGE REMOVAL. PERFORMED HFEC INSP IAW NTSPM 06-10-01.001, FOUND NO FURTHER DAMAGE TO CUT OUT AREA.

Part: SKIN — CRACKED (LT WING) · airframe 65,548 hrs · 21,157 cycles

ON WALK AROUND FOUND A CRACK AT LT WING FUELING DOOR INBD SIDE. LT WING LWR LE CRACK VERIFICATION, PERFORMED HFEC OF SUSPECT CRACK AREA, CONFIRMED CRACK. CRACK ENDS AT RIVET HOLE. LT WING REFUEL & DEFUEL PANEL HAS BEEN REMOVED IAW SMP & PLACED IN THE COURIER AREA. EXTERNAL DOUBLER MADE FROM .063" 6AL-4V TITANIUM SHEET MP2358935, FILLER FOR CUT OUT MADE FROM .090" 7075-T6 ALUMINUM SHEET MP1681501. INSTALLED REPAIR PARTS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. AREA STILL REQUIRES CLOSE UP.

Part: ENGINE — OVERTEMP (NR 3) · airframe 65,446 hrs · 21,111 cycles

PASSING 1200 FT, NR 3 ENGINE EGT WENT TO 969 C, PULLED THROTTLE BACK, TEMP STABILIZED, BUT WITHIN MINUTES STARTED FLUCTUATING INTO THE AMBER TOWARDS RED. PULLED THROTTLE TO IDLE & LT RED WITH THROTTLE AT IDLE. NR 3 ENGINE EGT EXCEEDANCE. ACCOMPLISH A BOROSCOPE OF STAGE 1 & 2 HPT BLADES & PERFORM VSV STATIC RIG CHECK WITHIN 10 CYCLES. ACCOMPLISHED GVI OPENED COWLINGS & CORENO DEFECTS NOTED, NO DUCTS DAMAGE & NO AIR LEAKS FOUND. ACFT OK TO CONTINUE.

Part: SKIN — CRACKED (RT WING LE) · airframe 65,393 hrs · 21,089 cycles

DURING WALK AROUND, FOUND ACRACK ON RT WING LE SKIN AT FWD LT CORNER OF FUELING PANEL. PERFORMED HFEC OF SUSPECT AREA, VERIFIED CRACK & IAW NTM PT6 20-30-00. REMOVED CRACK DAMAGE IAW SRM 57-10-00 FIG 68. INSTALLED REPAIR DOUBLER & COMPLIED WITH EA 8-5730-T0307735 MAJOR REPAIR.

Part: DOOR FRAME — DAMAGED (R4 DOORWAY) · airframe 65,220 hrs · 20,998 cycles

R4 DOOR AREA UPPER DOOR FRAME HAS A DEEP GOUGES & CRACKED. REPAIRED IAW EA 8-5310-306410 PART 1

Part: PITOT TUBE — OBSTRUCTED · airframe 64,362 hrs · 20,611 cycles

ABORTED TAKE OFF DUE TO AIRSPEED DISCREPANCY OF 20 KTS, CAPTAIN`S AIRSPEED WAS 60 KNOTS WHEN F/O CALLED 80 KNOTS FOR AIRSPEED CHECK DURING TAKE OFF ROLL. REJECTED TAKE OFF AT 100 KTS HIGHEST BRAKE TEMP NR 2 AT 460 DEG. FOUND EVIDENCE OF INSECT NESTS IN CAPTAIN`S AND FIRST OFFICER'S PITOT PROBES, REMOVED AND REPLACED IAW MM 34-11-02-2.

Part: UNKNOWN — UNKNOWN (DISPLAY) · airframe 64,037 hrs · 20,476 cycles

DURING PREFLIGHT, DISPLAY UNITS 2,4 AND 5 INTERMITTENTLY WENT BLANK. DOWN POWERED ACFT FOR 10 MINS, POWERED ACFT. PERFORMED RTS ON ALL 3 VIA'S ALL TEST PASSED IAW MM 31-43-01-5. TSI ADDED TO REPLACED NR 1 VIA AND PERFORM ADJUSTMENT TEST ON ALL DU SWITCHING.

Part: THROTTLE — FROZEN (NR 2) · airframe 63,960 hrs · 20,441 cycles

NR 2 THROTTLE STUCK AT 87 TO 93 PERCENT. SHUTDOWN ENGINE TO LAND. THROTTLE MOVES FREELY IN CHOCKS. R & R NR 2 ENGINE THROTTLE PUSH-PULL CABLE IAW MM 76-11-01-2 (FOUND WATER IN CABLE, SUSPECT FREEZING IN FLIGHT) OPS CHECKED GOOD, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,202 hrs · 19,717 cycles

DURING INSPECTION, EMERGENCY LIGHTS IN THE FLIGHT DECK AND COURIER AREA CEILING ARE INOPERATIVE. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW MM 33-51-01-4 AND 33-51-01-5.

Part: PANEL — MISSING (NR 3 NACELLE) · airframe 62,199 hrs · 19,715 cycles

DURING WALKAROUND, FOUND NR 3 PYLON MISSING PIE SHAPED PANEL AFT OF ENGINE PYLON. REPLACED SUPPORT ANGLE AUB7036-4 USING SRM. FINAL CLOSED.

Part: LIGHT — SHORTED (CABIN) · airframe 62,198 hrs · 19,714 cycles

DURING PRE-DEPARTURE INSPECTION, WHILE PERFORMING EMERGENCY EXIT POWER LIGHT TEST, ALL CEILING LIGHTS IN FLIGHT DECK AND COURIER AREA INOPERATIVE. TROUBLESHOT SYS AND FOUND POWER BEING DRAWN TO A GROUND FROM POWER SUPPLY NOT PROVIDING ENOUGH VOLTAGE TO LIGHTS. FOUND RT EXIT DOOR AFT EMERGENCY LIGHT ASSY MISSING SCREWS, DROOPING DOWN, AND SHORTING TO METAL FRAMEWORK. RESEATED WITH NEW SCREWS AND EMERGENCY CEILING LIGHTS OPS CHECKED GOOD IAW MM 33-52-04-2.

Part: WIRE HARNESS — FAILED (FIRE DETECTION) · airframe 61,343 hrs · 19,385 cycles

ENG NR3 FIRE INDICATION AT FL 350 INDICATION WENT OUT WHEN THROTTLE PULLED TO IDLE. FOLLOWED CHECKLIST AND SHUTDOWN ENG UNEVENTFUL LANDING. R & R NR 3 ENGINE CORE FIRE DET WIRE HARNESS IAW SMP CHAPTER 20. FDCU OPS CHECKED GOOD IAW MM 26-11-01-5. NR 3 ENG FIRE DET SYSTEMS, OPS CHECKED GOOD IAW MM 26-11-02-5. PERFORMED NR 3 PNEU SYS DECAY, CHECK IAW MM 36-00-04-5, WITH NO DEFECTS. RAN NR 3 ENGINE FOR OVER 10 MINUTES IAW JRH THRU VARIOUS POWER SETTINGS UP TO 90 PERCENT N2, WITH NO DEFECTS NOTED. PERFORMED FIRE DET SYS TEST AFTER ENGINE SHUTDOWN IAW MM 26-11-02-5, WITH NO DEFECTS. ACFT OK FOR SERVICE.

Part: SWITCH — INOPERATIVE (THROTTLE) · airframe 60,788 hrs · 19,154 cycles

DURING T/O ROLL ENGINES WERE SURGE USING MAX POWER AND AUTO THROTTLES. THROTTLES WERE MOVING BACK AND FORTH ABOUT ONE KNOB. ENGINE 2 EXCEEDANCE AT 110 KNOTS 121.3 N1, 109.6 N2. REJECTED TAKEOFF. PERFORMED VISUAL INSPECTION TO ENGINES AS PER MM 72-00-00-6-1. NOT DEFECTS NOTED. ACFT OK FOR SERVICE. REMOVED AND REPLACED THROTTLE SWITCH CAM ASSY. OPS CHECKED SERVICABLE IAW AMM 76-11- 04-2. THRUST CONTROL MODULE TEST PASSED IAW FIM 22-31-01.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 60,609 hrs · 19,082 cycles

ON TAKEOFF ROLL. MAX POWER AT 90KIAS THE ENGINE FAIL LIGHT, ENGINE 2 N1 EXCEEDANCE 120.1 (T/O LIMIT 115.8) REJECTED T/O. PERFORMED FAN (N1) OVERSPEED INSP, FAN ROTOR FREE FOR ROTATION, FIRST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FREE FROM PARTICLES IAW AMM 72-00-00-6-2. ACFT OK FOR SVC. PERFORMED FAN (N1) OVERSPEED INSP, FAN ROTOR FREE FOR ROTATION, 1ST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FREE FROM PARTICLES IAW AMM 72-00-00-6-2. ACFT OK FOR SVC. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,080 hrs · 18,881 cycles

ACFT EMERGENCY LIGHTS SYS INOP. (PLACED ON MEL)

Part: SENSOR — FAILED (LT MLG) · airframe 58,443 hrs · 18,272 cycles

DURING TAKEOFF RETRACTED GEAR RECEIVED A RED UNSAFE INDICATION OF THE LT MAIN GEAR IN BOTH THE PRIMARY AND SECONDARY GEAR POSITION INDICATORS. CYCLED GEAR IAW QRH SAFE DOWN INDICATION, UNSAFE UP. CONTINUED TO DEST AT 250 KNTS. R & R LT MLG POSITION DOWN AND LOCKED SENSOR. ACFT RETURNED TO SERVICE

Part: CYLINDER — FAILED (NLG STEERING) · airframe 55,593 hrs · 17,376 cycles

HEARD THUMP FOLLOWED BY HYD QTY LOW THEN IMMEDIATELY FOLLOWED BY LVL FAIL ALERT JUST PRIOR TO TOUCHDOWN, FOUND LT NWS STEERING ACT HOUSING SHEARED. REPLACED LT NWS STEERING ACT REF AMM 32-52-01-2, OPS CK OK. LEAK CK OK. ALSO INSP NWS STEERING COLLAR AREA AND RT NWS ACT NO DAMAGE FOUND.

Part: FRAME — CRACKED (ZONE 200) · airframe 53,605 hrs · 16,700 cycles

UPPER FUSELAGE ENTRY WAY CRACK ON FITTING SUPPORT (P/N AWE8001-503 ). REPAIRED FRAME IAW SRM 53-30-00 FIG 5 SHT 1 VOL I.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,605 hrs · 16,700 cycles

AFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-70-00 VOL I FIG 13.

Part: WEB — CRACKED (ZONE 100) · airframe 53,605 hrs · 16,700 cycles

LOWER AFT FUSELAGE COMPT CRACK ON WEB, UPPER TORQUE BOX PLANE. REPAIRED WEB IAW SRM 51-40-00 FIG 41 VOL I.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,605 hrs · 16,700 cycles

AFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-70-00 FIG 13 VOL I.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 53,605 hrs · 16,700 cycles

AFTER REMOVAL CEILING PANELS WITH J/C "2552C120-2JR" FWD CARGO COMPT BELOW SEAT TRACK FOUND CRACK. REPAIRED SEAT TRACK IAW SRM 53-70-01 FIG 1 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 53,605 hrs · 16,700 cycles

LOWER EXT FUS FOUND DENT .50" BY .50" DEPTH .04" ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 53,605 hrs · 16,700 cycles

DURING SPAR CAP INSP, FOUND 1 1/2 INCH CRACK. ACCOMPLISHED EA 8-5510-111624.

Part: SKIN — CRACKED (ZONE 300) · airframe 53,605 hrs · 16,700 cycles

DURING INSP OF CONSTANT SECTION UPPER AND LOWER INTERIOR SKIN PANEL FOUND CRACK IN FLYABLE LIMITS.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 51,370 hrs · 15,721 cycles

AFTER T/O, NR 2 HYD LT EDP OVERPRESS, APPROX 4KPSI, PER QRH SHUT OFF THAT PUMP NOTICED NR 2 HYD TEMP WAS HI 70 DEG AND RISING FOLLOWED QRH NO HELP, RECEIVED LT TEMP HI ON NR 2 SYS. FOLLOWED QRH, NO HELP. TEMP KEPT RISING ON NR 2 SYS AT 120 DEG, SHUTDOWN NR 2 ENG. NR 2 ENG HYD PRESS HIGH DURING OP'S. FOUND NR 2 PRESS IND OUT OF TOL. R/R IND NR 2 LT HYD EDP NOT FULLY DEPRESS WHEN SEL'D OFF. R/R`D PUMP FLUID INSP IAW 29-11-01 NO DUCT DMG AND FILTER DELTA P POPPED. ENG RUN, FOUND NR 2 RT EDP NOT CLOSING DURING AUTO SELECTION W/THE LT PUMP FULLY PRESS. R&R R2-5415 AND TESTED PER TAFI, NO HELP. R&R NR 2 LT PRESS SW IAW 29-31-02, NO HELP, LK CKS OK. R/R`D NR 2 RT EDP DEPRESS SOL. R&R TEMP SENSOR CKS OK.

Part: RETAINER — BROKEN (ZONE 600) · airframe 48,225 hrs · 14,663 cycles

AT FL350 WHEN WING ANTI-ICE WAS TURNED ON THE NR 1 PNEU PRESSURE WENT TO FULL SCALE AND BOTH WING ANTI-ICE DISAGREE LIGHTS CAME ON. THE CONFIG WAS NR 1 AND NR 2 PNEU SUPPLIES OPEN 1-3 ISO VALVE OPEN, 1-2 CLOSED AND NR 1 PACK ON. NR 3 PNEU SUPPLY WAS DEFERRED PRIOR TO FLT. ACCOMP CHECK OF NR 1 PSC, NO FAULTS NOTED. FOUND RT OUTBOARD FAULT INDICATOR LOGGED ON PNEU MANIFOLD FAULT INDICATOR. CHECKED WING ANTI -ICE DUCTING AND FOUND RT NR 5 TO NR 6 RETAINER FOR INTERCONNECT JOINT DAMAGED AND INTERCONNECT JOINT NOT CONNECTED TO OUTBOARD ANTI-ICE DUCT. REMOVED AND REPLACED RETAINER AND PERI SEALS FOR INTERCONNECT DUCT. LEAK CHECK NORMAL. RAN NR 1 AND NR 3 ENGS. ALL READINGS NORMAL.

Part: WARNING LIGHT — FALSE INDICATION (MLG) · airframe 47,071 hrs · 14,273 cycles

RT MAIN GEAR LIGHT ON S/O PANEL SHOWED UNSAFE AFTER GEAR RETRACTION. F/O PANEL SHOWED NORMAL. IAW RED TABS RECYCLED LANDING GEAR. LANDING GEAR EXTENDED NORMAL WITH 4 GREEN ON BOTH PANELS. FOLLOWING RETRACTION RT MAIN RED LIGHT ON S/O PANEL STILL STAYED ILLUMINATED. ALL GEAR LIGHTS ON F/O PANEL OUT. APPROX 35 MIN INTO FLIGHT RED LIGHT ON S/O PANEL WENT OUT. ALL LIGHTS TEST NORMAL. BITE CHECK ON PROX BOX, NO FAULTS. MEASURE RT MLG UP LOCKOUT OF LIMITS AND ADJUSTED IAW DC1030AMM 32-34-03-2. OK TO CONTINUE.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 45,018 hrs · 13,640 cycles

IB FLAP TRACK AND DRIVE SUPPORT BORE HAS CORROSION. COMPLIED WITH EA 8-5750-72297. RT WING IB FLAP TRACK AND DRIVE SUPPORT BORE CORROSION.

Part: HINGE — GOUGED (SERVICE DOOR) · airframe 45,018 hrs · 13,640 cycles

COMPLY WITH EA 8-5240-71005. DOORS-SERVICE, TAIL CONE, PATIO DOOR HINGE REPAIR P/N AKC7011-1. CLOSING ACTION ON 09/25/03.ON N/R S00013.COMPLIED WITH EA 8-5240-71005. DOORS SERVICE, TAIL CONE, PATIO DOOR HINGE REPAIR P/N AKC 7011-1.

Part: ADAPTER — CHAFED (ZONE 400) · airframe 45,018 hrs · 13,640 cycles

EXHAUST THRUST REVERSER HAS A CHAFED UPPER ADAPTER. COMPLIED WITH E.A.8-7832-71004.EXHAUST THRUST REVERSER CHAFED UPPER ADAPTER.

Part: CAP — GOUGED (ZONE 500) · airframe 45,018 hrs · 13,640 cycles

COMPLY WITH EA 8-5710-72305. WINGS-MAIN FRAME-GOUGE REPAIR XORS 562.390 (LT) FLAP BULKHEAD LWR CAP. CLOSING ACTION ON 09/26/03. ON N/R S00015. COMPLIED WITH EA 8-5710-72305.WINGS, MAIN FRAME, GOUGE REPAIR STA XORS 562.390.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 41,509 hrs · 12,485 cycles

CAPTAINS FRONT WINDSHIELD (OUTER PANE) CRACKED. REMOVED AND REPLACED NR 1 CAPTAINS WINDSHIELD IAW M/M CHAPTER 56-11-00-2. DUE TO BROKEN WIRE ON TERMINAL BLOCK R5-1071. PERFORM ANTI-ICE/DEFOG TEST IAW M/M CHAPTER 30-42-00 PAGE 201. INSTALLED TERMINAL BLOCK PER S/W/P. ACCOMPLISHED ADJ AND TEST PER MM 30-42-00.

Part: VALVE — FAILED (PNEUMATIC SYS) · airframe 41,502 hrs · 12,482 cycles

ON CLIMB NR 2 PNEU TEMP HI LIGHT ILLUM'D. SHUTDOWN PNEU SUPPLY SEL. PERFORMED RED TAB PROC. REMOVED AND REPLACED THE NR 3 PACK FLOW VALVE AND THE NR 1 PNEU PRESS REGULATOR VALVE. ALL CHECK OK.

Part: FLAP — MALFUNCTIONED (LT WING) · airframe 41,239 hrs · 12,372 cycles

WRI 27-50-7942 WITH FLAPS SEL AT 50 DEG LEFT TAPE IND 45 DEG IN FLT ON GRD FLAP TAPE GO TO 50 DEG. REMOVED AND REPLACED O/B FLAP PER MM 27-50-02-4.

Part: RADAR — FAULTY (WEATHER RADAR) · airframe 39,766 hrs · 11,906 cycles

REPEAT WRITE UP NR 1 RADAR SYS UNSATISFACTORY WITH HEAVY SIDE RETURNS.

Part: ANTENNA — MALFUNCTIONED (WEATHER RADAR) · airframe 39,763 hrs · 11,905 cycles

REPEAT WRITE UP WX RADAR RETURNS BOTH SYS SHOW BLANK AREA IN A SPOKE PATTERN. REMOVED AND REPLACED ANTENNA PER IAW MD DC10-30 AMM 34-41-01-2.

Part: RADAR — MALFUNCTIONED (WEATHER RADAR) · airframe 39,760 hrs · 11,904 cycles

AFT 38 MIN RADAR STARTED SPOKING. REMOVED AND REPLACED RADOME MM 53-51-00-2. REMOVED AND REPLACED WX RADAR ANTENNA PEDESTAL MM 34-41-01-2.

Part: RADAR — MALFUNCTIONED (WEATHER RADAR) · airframe 39,759 hrs · 11,903 cycles

RADAR SPOKING BOTH SYSTEMS ALL RANGES ALL GAINS SETTINGS REPEAT WRITEUP.

Part: ANTENNA — MALFUNCTIONED (WEATHER RADAR) · airframe 39,759 hrs · 11,903 cycles

BOTH CAPT AND F/O RADAR DISPLAY BEGAN TO SPOKE. REMOVED AND REPLACED WEATHER RADAR ANTENNA AND PLATE AS PER MM 34-41-01-2. GROUND CHECK OK.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,795 hrs · 11,616 cycles

AFT FUSELAGE COMPARTMENT ZONE 312 STA Y2046.000 CAN''T TOP ANGLE BRACKET FOUND CRACKED AT BOTH ENDS. *S/D* REMOVED, REPLACED AND FAB PER DRW AJC 7021, SRM 51-31-01 VOL 11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,795 hrs · 11,616 cycles

AFT FUSELAGE COMP ZONE 312 STA Y2069.440 CAN''T TOP ANGLE BRACKET LT CORNER CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW DRW AJC 7029, SRM 51-31-01 VOL 11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,795 hrs · 11,616 cycles

AFT FUSELAGE COMP ZONE 312 STA Y2092.880 CAN''T TOP ANGLE BRACKET FOUND CRACKED AT BOTH ENDS. *S/D* REMOVED, REPLACED AND FAB PER IAW DRW AJC 7028, SRM 51-31-01 VOL 11.

Part: TRIM CYLINDER — MALFUNCTIONED (LANDING GEAR)

99-162 - GEAR HANDLE WOULD NOT RAISE AFT T/O. RED TAB RAN BUT STILL DID NOT WORK. GOOD HYDS ON ALL 3 SYS. NO PINS FND. BLED/RESET TRIM CYLINDER INTERLOCK FUSE PRECAUTIONARY PER DC-10 MM 32-31-06-2. A/C OK FOR RETURN TO SERVICE.

Part: ACTUATOR — FAILED (MLG DOORS)

WHEN LANDING GEAR WAS DEPLOYED FOR LANDING AT PDX, A LOUD AND HEAVY THUMP WAS HEARD AND FELT AS THE CTR. GEAR IMMEDIATELY CAME DOWN. THE REMAINING GEAR SEEMED TO TAKE MORE TIME THAN USUAL. FOUND RETRACT CYLINDER ROD END STRIPPED OUT AND DAMAGED CENTER LANDING GEAR DOORS DAMAGED. AIRCRAFT WAS CONFIGURED PER EA 8-3280-36672 FOR A PERRY PERMIT. PERRY PERMIT NR 27-12 FOR FLIGHT FROM PDX TO LAX FOR PERMANENT REPAIR WAS OBTAINED. *S/D* ENCLOSED COVER SHEET, EA 8-5310-22097, EA 8-5310-22096, SNRM 05, 06, 07, 08, 012, 013, 014, 015, 016, 017, 018, 019, 020, 022, 026, 027, 021, 023, 025.

Part: ENGINE — FLAMED OUT (NR 1)

NR 1 ENGINE FAIL AFTER T/O, HIGH EGT 999+, AFTER THROTTLE RETARD FUEL FLOW AND EGT REMAIN EXCESSIVE. WHILE DUMPING FUEL ENGINE FLAMED OUT. RETURNED TO ANC. *S/D* REMOVED AND REPLACED NR 1 ENG AS PER MM 71-00-00-4 RUN UP LC CK NR 1 ENG. ALL CKS OK TDS 98224.

Part: BRACKET — CRACKED (LT LE SLAT)

LT WING, O/B L/E SLAT DRIVE MECHANISM, OUTER BRACKET ASSY HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. EDDY CURRENT INDICATION.