N358FE

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,057 hrs · 32,214 cycles

DURING APPCH IN ICING CONDITIONS WITH ENGINE AND AIRFRAME ANTI-ICE ON, RECEIVED LEVEL 3 AIR MANF 3 FAIL ALERT. NR 3 BLEED SYSTEM AUTO PROTECT SHUT OFF NR 3 BLEED SOURCE, CLOSED 1-3 ISOL VALVE, SHUT OFF NR 3 PACK. AIR SYNOPTIC SHOWED THAT AND NR 3 MANIFOLD RED. LVL2 CABIN INFLO LO ALERT - CORRECTED BY TURNING ON NR 2 PACK. WING ANTI-ICE DISAG CORRECTED BY TURNING OFF WING ANTI-ICE. SYNOPTIC TURNED NR 3 MANF BACK TO WHITE IN ABOUT 5 MINUTES. DECLARED EMERGENCY. LANDED KMEM. INTEROGATED CFDS - NO FAULTS FOUND. DECAY CHECK PASSED. PERFORMED R-T-S OF MANIFOLD FAILURE DETECTION CONTROLLER IN REF TO AMM 36-23-01-5 - PASSED. NO FAULT BALLS ON PNEUMATIC MANIFOLD FAULT INDICATOR BOX IN CAC. PRECAUTIONARY REMOVAL AND REPLACEMENT OF MANIFOLD FAILURE DETECTION CONTROLLER IN REF TO AMM 36-23-01-4. NO 30 DAY

Part: TORQUE TUBE — SHEARED (L1 DOOR) · airframe 89,261 hrs · 31,685 cycles

FUELER REPORTED THE L1 DOOR INOPERATIVE. DISCONNECTED THE CABLE FOR RETRACTABLE PANEL 231AC AND DEPRESSURIZED DOOR RESERVOIR IAW AMM 52-11-01-2. PULLED AND TAGGED L1 DOOR CIRCUIT BREAKERS. FOUND THE L1 DOOR POWER DRIVE TORQUE TUBE IS SHEARED AT AFT END ABOVE L1 DOOR. COMPLETED INSTALLATION OF L1 DOOR AFT CABLE DRUM AND SUPPORT ASSY IAW AMM 52-11-09-2. COMPLETED INSTALLATION OF L1 DOOR ELECTRIC ACTUATOR IAW AMM 52-11-01-2. PERFORMED A PNEUMATIC L1 DOOR TEST IAW MM 52-10-01-2. PERFORMED L1 DOOR ADJUSTMENT, TEST, AND RIG IAW AMM 52-11-00-5. ALL OPS CHECKED GOOD.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 88,981 hrs · 31,520 cycles

CRACKS FOUND ON HORIZONTAL STABILIZER COSTANT SKIN PANELS. REPLACED PANELS USING EA 8-5510-T0338233 AS REFERENCE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,684 hrs · 31,364 cycles

CENTER CARGO DOOR FWD LOWER JAMB HAS CORROSION VISIBLE THROUGH LOWER FWD LIGHTENING HOLE. REPAIRED CENTER CARGO DOOR FORWARD LOWER JAMB ANGLE P/N AFA3873-7 REF EA 8-5310-T0336561 P1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,684 hrs · 31,364 cycles

CENTER CARGO STA 1781 AND RBL 48, CORROSION ON FLOOR SUPPORT CAP STRUCTURE. REMOVED DAMAGED CORRODED SECTION OF FLOORBEAM AND SPLICED IN NEW SECTION PER SRM REPAIR 53-60-01 FIG 3 PG 7 & 8.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,684 hrs · 31,364 cycles

CENTER CARGO BILGE STA 1761 I/B OF STRINGER 47R SHEAR TIE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED -33 SHEAR CLIP REF DWG AFA0055.

Part: FRAME — CORRODED (BS 555) · corrosion level 2 · airframe 88,684 hrs · 31,364 cycles

FRAME BS 555, LONGERON 49L HAS SIGNS OF CORROSION. REMOVED AND REPLACED WITH FABRICATED FILLER AND DOUBLER THE FRAME INSTALLATION IAW DRAWING ACA3349 AND SRM 53-30-01, VOL I, FIG 4-4A, FIG. 8.

Part: LONGERON — CORRODED (BS 561-587) · corrosion level 2 · airframe 88,684 hrs · 31,364 cycles

NR 1 ACM BAY LONGERON 49L, BS 561 - 587 CORRODED. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-00-01, VOL I, FIGURE 7, SHEETS 5-7, DETAIL III, AND SRM 51-00-01, VOL II.

Part: SEAT TRACK — WORN (BS 1300) · airframe 88,684 hrs · 31,364 cycles

MAIN DECK, AT BS 1300, RT OTBD SEAT TRACK HAS ELONGATED LOBE. INSTALLED A SEAT TRACK PLUG IAW SRM 53-70-00, FIG 2, SHEET 2.

Part: SEAT TRACK — WORN (BS 1229) · airframe 88,684 hrs · 31,364 cycles

MAIN CABIN SEAT TRACK AT STA 1229, RBL 107 HAS ELONGATED LOBES. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 2.

Part: SHEAR TIE — CRACKED (BS 1761) · airframe 88,684 hrs · 31,364 cycles

CENTER CARGO BILGE BS 1761 INBD OF STRINGER 46R, THE SHEAR TIE HAS A CRACK AND CORRODED. REPAIRED IAW SRM 53-30-00, VOL 1, FIG 9, P 34.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,684 hrs · 31,364 cycles

MAIN DECK, BS 1987, RBL 48, FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW DWG AGA 7091.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

MAIN CARGO COMPT, APPROX STA 740 X= 75.25, SEAT TRACK EXISTING BLENDOUT BEYOND LIMITS, 2017-11-08. REMOVED AND REPLACED SMALL SECTION OF SEAT TRACK (PLUG) IN REF TO SRM 53-70-00 FIG 2 VOL 1 AND DWG SR10-53-010.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,684 hrs · 31,364 cycles

RT WING LE INTERNAL BEADED DOUBLER CRACKS APPROX XORS 518. CONFIRMED WITH NDT HFEC. PRIMARY STRUCTURE, 2017-11-07. REPAIRED THE RT WING L/E BEADED DOUBLER IN REF TO SRM 57-10-00 FIG 71 VOL 1.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,684 hrs · 31,364 cycles

RT WING LE INTERNAL BEADED DOUBLER CRACKS APPROX XORS 570. CONFIRMED WITH NDT HFEC. PRIMARY STRUCTURE 2017-11-07. REPAIRED THE RT WING, L/E INTERNAL BEADED DOUBLER IN REF TO SRM 57-10-00 FIG 71 VOL 1.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 88,684 hrs · 31,364 cycles

LT O/B FLAP I/B HINGE PANEL 535 DR HAS DELAM. REPAIRED LT O/B FLAP I/B HINGE PANEL 535 DR AT THE MARKED DELAMINATED AREA REF SRM 51-71-00 VOL 2 PG 3-47 AND DRAWING ARC2008.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

CTR CARGO BILGE STA 1761 I/B OF STRINGER 47R SHEAR TIE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED -33 SHEAR CLIP REF DWG AFA0055.

Part: FLOOR PANEL — CORRODED (FUSEALGE) · airframe 88,684 hrs · 31,364 cycles

MAIN CARGO LT FLOOR PRESSURE PANEL WSP 0791-901 FWD EDGE AT STA 475 AND X=88 HAS EXFOLIATION CORROSION. INSTALLED NEW PRESSURE PANEL PER EA 8-5321-T0336540 P1. FLOOR PANEL REPLACEMENT, STA Y=475 TO 500 - MINOR ALTERATION.

Part: SKIN PANEL — CHAFED (ZONE 400) · airframe 88,684 hrs · 31,364 cycles

NR 2 ENGINE LT PICKLE BARRELAFT LOWER SKIN WORN. REMOVED AND REPLACED DAMAGED SKIN FOR PANEL ASSY AJC 7415-97. LT SIDE NR 2 ENG LOWER AFT SECTION. REF DRAWING AJC 7415 AND SRM 51-31-01, 51-21-01 AND 514101 VOL II.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

MAIN CARGO DECK STA 475 APPROX 70LBL, AFT OF MAIN CARGO DOOR CONTROL, FLOOR SUPPORT IS CRACKED. REPAIR WAS ACCOMPLISHED IN REF TO EA 8-5310-T0336283, PART 1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

MAIN CARGO DECK STA510 APPROX 60LBL FLOOR SUPPORT IS CRACKED. REPAIRED FLOORBEAM AT STA 515 AND LBL 60 IN REF TO EA 8-5310-T0336284, PART 1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

CTR CARGO STA1781 LONG 46R IS EXFOLIATED/CRACKED. REPAIRED LONGERON REF SRM 53-10-00 FIG 2A, SHEET 4, VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 88,684 hrs · 31,364 cycles

LEFT WING FUELING ACCESS PANEL, BETWEEN THE FUELING PORTS, THE PILLOW DOUBLER HAS 2 CRACKS. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 57-10-00, VOL 2.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,684 hrs · 31,364 cycles

RT WING LE INTERNAL, BEADED DOUBLER CRACKS APPROX, XORS 693. PRIMARY STRUCTURE. REPAIRED THE RT WING BEADED DOUBLER AT STA XORS 693 IN REF TO SRM 57-10-00 FIG 71 PAGE 222 VOL 1.

Part: SEAL — CORRODED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

RT HORIZ STAB TE, INBD AFT FUSELAGE FAIRING LOWER BEAD SEAL AND PAINT BUBBLING. CORROSION EVIDENCE VISIBLE. REPAIRED CORRODED AREA ON RT AFT FUSELAGE, APPROX STA 2190-2163, REF SRM 53-20-00 VOL I FIG 22 PGS 200-205. ALONG WITH JPF ITEMS 3-9 SEE ATTACHMENT FOR JPF MAJOR REPAIR.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,684 hrs · 31,364 cycles

RT WING LE INTERNAL BEADED DOUBLER CRACKED AROUND FASTENER APPROX XORS 490. CONFIRMED WITH NDT HFEC. PRIMARY STRUCTURE. REPAIRED THE RT WING BEADED DOUBLER IN REF TO SRM 57-10-00 FIG 71 VOL 1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

MAIN CARGO COMPT, APPROX STA 635 X= -8.50, SEAT TRACK GOUGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1, SHT 1, VOL 1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 88,684 hrs · 31,364 cycles

MAIN CARGO COMPT, APPROX STA 675 X= -8.50, SEAT TRACK EXISTING BLENDOUT BEYOND LIMITS. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1 SHT 1 VOL 1.

Part: BEARING — MIGRATED (NR 1 PYLON) · airframe 87,891 hrs · 30,863 cycles

DURING COMPLETION OF EA 8-5440-T0321665 REVA PT2, FOUND NR 1 ENG PYLON AFT SPHERICAL BEARING MIGRATION HAS INCREASED PAST ALLOWABLE LIMITS. SPHERICAL BEARING REQUIRES REPLACEMENT, REF EA 8-5440-T0321665 A PART 3 FOR REPLACEMENT. PANELS 437LL AND 438GL ARE REMOVED FROM THE NR 1 ENGINE PYLON TO FOM. REMOVED AND REPLACED AFT BULKHEAD FITTING REF DAC AUB 7025 AND SRM 51-31-01.

Part: THROTTLE — MALFUNCTIONED (NR 2) · airframe 87,773 hrs · 30,797 cycles

DURING DESCENT, THE NR 2 THROTTLE WOULD NOT RETARD FULLY, RESULTING IN A CONFIRM ENGINE OUT MESSAGE. REPEATED SEVERAL TIMES DURING DESCENT AT 10000, N1 46% NR 2 (NR 1 & 3 = 37%). ON DESCENT PAGE IN FMS, SELECTED ANTI-ICE OFF. REDUCED N1 TO NORMAL. NORMAL LANDING. PER FLT CREW DEBREIF A/T ON INITIALLY. A/T THEN SELECTED OFF. THROTTLE WOULD STILL NOT RETARD.TESTED A/T SYS IN FCC1 & FCC-2 AT BLOCK IN. A/T R-T-S PASS.UNABLE TO DUPLICATE AT GATE ENG 2 THROTTLE PULL IN NORM LIMITS.PREFORMED VISUAL INSPECTION OF THE AUTO THROTTLE DRIVE CLUTCH. FOUND WIRE BUNDLE RUBBING ON NR 2 AUTO THROTTLE DRIVE CLUTCH NEAR THE REJECTED TAKE OFF CAM & CABLE SAFTEY WIRE. ADJUSTED WIRE CLIP AND SECURED IN APPROPRIATE LIGHTNIG HOLE IAW AMM 20-30. REMOVED NR 2 ENGINE THROTTLE PUSH PULL CABLE IAW ROUTED SERVICEABLE NR 2 ENGINE THROTTLE PUSH PULL CABLE STILL REQUIRES ALL HOOK UP, CLAMP INSTALL, AND OPS CHECK IAW AMM 76-11-01-2 COMPLETED ROUTING AND INSTALL OF NR 2 THROTTLE CABLE IAW AMM 76-11-01-2. RIG AND PUSH/PULL CHECK GOOD IAW AMM 76-11-01-2. PERFORMED RTS ON FCC 1 AND FCC 2 REF MD10-10 AMM 22-00-00-5, ALL TESTS PASSED.

Part: ENGINE — FAILED (NR 3) · airframe 87,410 hrs · 30,601 cycles

LEVEL FLIGHT, HEARD BOOM NOISE, FELT MOMENTARY HEAVY RUMBLE, AND YAW TO THE RIGHT. NR 3 ENGINE FAILED. COMPLIED WITH QRH. DURING DESCENT, N1-21 EGT-30 N2-10.5 FF - 0 OIL PRESS - 1 OIL TEMP - 60 OIL QTS - 16. FAILED BORESCOPE, REPLACED THE ENGINE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 87,054 hrs · 30,393 cycles

R1 DOOR SLIDE REMOTE PRESSURE INDICATION LIGHT DOES NOT TEST. RELAMPED R1 DOOR SLIDE REMOTE PRESSURE INDICATOR WITH P/N MS25237-338. BULBS INDICATOR OPS CHECK GOOD. ALL WORK DONE IAW AMM 25-61-03-710-801.

Part: LOOP — MALFUNCTIONED (BLEED AIR SYS) · airframe 86,576 hrs · 30,121 cycles

CLIMBING THRU 12,000 FT, LEVEL ONE, AIR SYS 2 OFF, FOLLOWED BY LEVEL 3 ALERT, AIR MANF 2 FAIL. COMPLIED WITH QRH PROCEDURES. R & R LOOP 2 D1-29 IAW AMM 36-23-02-4. OPERATIONS CHECKED GOOD.

Part: SENSOR — INOPERATIVE (BLEED AIR SYS) · airframe 86,519 hrs · 30,095 cycles

AIR MANIFOLD 2 FAIL LVL 3 ALERT ON CLIMB OUT. COMPLIED WITH QRH & RETURNED, UNEVENTFUL RETURN. PERFORMED RTS OF AIU'S TO VERIFY NO FAULTY INFORMATION, AIU CHECKS NORMAL, NO FAULTS NOTED. INTERROGATED AIU FOR COMPONENT CFDS FAULTS. PSC 2 SHOWS FAULT 361022 HI STAGE TEMP SENS OPEN CIRCUIT FAULT.

Part: ACTUATOR — STRIPPED (CARGO DOOR) · airframe 86,240 hrs · 29,960 cycles

WHILE TRYING TO OPEN THE CTR CARGO DOOR, FOUND THE LATCH ACTUATOR INTERNALS STRIPPED & UNABLE TO OPEN MANUALLY. DOOR IS CLOSED, LATCHED & LOCKED. REMOVAL OF CTR CARGO DOOR STARTED DUE TO DAMAGE OF LATCH ACTUATOR MOUNT, CTR CARGO DOOR REMOVAL COMPLETED IAW AMM 52-32-04-2 UP TO STEP 3. 13. FABRICATED DOUBLER, TREATED & PRIMED & OK TO INSTALL. INSTALLED REPAIR PARTS IAW EA 8-5230-T0322601 FIG 1. INSTALLED CTR CARGO DOOR IAW AMM 52-34-04-2. INSTALLED NEW LATCH ACTUATOR IAW MM 52-32-02-2. SERVICED DOOR COUNTER BALANCE MECH IAW MM 52-32-07-2. COMPLETED INSTALLATION OF DOOR IAW MM 52-32-04-2. OPERATED DOOR, OPERATIONS CHECKED GOOD. DOOR LINER INSTALLED.

Part: FITTING — IMPROPER PART (FUEL FILTER) · airframe 860 hrs · 29,875 cycles

ENGINE NR 3 FUEL FILTER ALERT ON TAKEOFF POWER. FOUND ORIFICE TYPE FITTING SWAPPED WITH STRAIGHT FITTING ON FUEL FILTER HOUSING.

Part: MEC — FAILED (NR 3 ENGINE) · airframe 860 hrs · 29,875 cycles

AFTER RE-START AT FL 250, ENG NR 3 WOULD NOT ACCELERATE ABOVE IDLE, THROTTLE MOVEMENT NORMAL. R & R MAIN ENG CONTROL IAW AMM 73-20-01-2.

Part: STRAP — CORRODED (FUSELAGE) · airframe 860 hrs · 29,873 cycles

LOWER FUSELAGE STATION 1590, SURFACE CORROSION INBD OF LOWER RT BEAUTY STRAP. REMOVED CORROSION IAW SRM REF 53-00-01 FIG 1A SH 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 860 hrs · 29,873 cycles

CENTER CARGO COMPARTMENT BILGE STATION 1841, FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT SECTION IAW DWG AGA 7170 & SRM 51-31-01 VOL 2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 860 hrs · 29,873 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1641 LT, X=8.50. REMOVED DAMAGED SEAT TRACK SECTION AT LT X=8.50, BETWEEN STATION 1611 - 1651 IAW SRM 53-70-00 VOL 1. INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-70-00 VOL 1.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 86,053 hrs · 29,873 cycles

LEFT WING LOWER FWD WING LE EXFOLIATION & INTERGRANULAR CORROSION AFT OF FUEL VLV MX PANEL. REMOVED CORROSION IAW SRM 57-10-01 FIG 19C SHEET 6 VOLUME 1. INSTALLED REPAIR DOUBLERS & FILLER IAW SRM 57-10-00 FIGURE 19C VOLUME 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,053 hrs · 29,873 cycles

RIGHT FUSELAGE UPPER AFT CORNER OF NR 3 A/C COMPARTMENT. DOOR CUT OUT HAS A .200 INCH CRACK EXTENDING OUT OF FASTENERS HOLE, END OF CRACKED CRACK, REPAIR COMPLIED WITH IAW SRM 53-50-00 FIG 3 A SHEET 3.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,053 hrs · 29,873 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 750 RT, X=-8.50. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,053 hrs · 29,873 cycles

MAIN DECK SEAT TRACK DAMAGED, LT STATION 750, X=27.50 SPLICED SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 86,053 hrs · 29,873 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1215 RT, X=27.50 SPLICED SEAT TRACK IAW SRM 53-7O-00 VOL 1.

Part: WIRE HARNESS — DAMAGED (ENGINE) · airframe 851 hrs · 29,359 cycles

IN FLIGHT GOT EGT 2 HI 997 DEG ENG 2 EXCEEDANCE. PULLED TO IDLE TEMP DROPPED BELOW LIMITS ON LEVEL OFF WITH THROTTLE AT IDLE. TEMP EXCEEDED LIMITS AGAIN. SHUTDOWN NR 2 ENG & RAN APPROPRIATE CHECKLISTS. REMOVED AND REPLACED BOTTOM LT, BOTTOM RT HARNESSES, AND FWD THERMOCOUPLE LEAD.

Part: INTERCOSTAL — CRACKED (NR 2 NACELLE) · airframe 84,324 hrs · 28,864 cycles

NR 2 ENG INTERCOSTAL FOUND CRACKED UNDER 363GL. INTERCOSTAL PN AJC7644-33. INSTALLED DOUBLER & FILLER IAW SRM 55-0-00 FIG 5 & EA 8-5530-T0309468.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,324 hrs · 28,864 cycles

FUSE UPPER LOBE STATION 1681 FRAME HAS 5 INCH CRACK ABOVE SPLICE AT L13R. REMOVED CRACKED SECTION OF FRAME AND REPAIRED PER SRM 53-30-00 FIG 5 SHEET 1 VOLUME 1.

Part: FITTING — CRACKED (BS 1159 FRAME) · airframe 84,324 hrs · 28,864 cycles

FUSELAGE FRAME FITTING CRACKED BS 1159 WL 20. REPAIRED PER SRM 53-30-00 FIGURE 7 SHEET 2. REPAIRED PER SRM 53-30-00 FIGURE 7 SHEET 2.

Part: STARTER — FAILED (APU) · airframe 84,189 hrs · 28,791 cycles

AFTER APU STARTED ON PREFLIGHT, LEVEL 1 ALERT APU STARTER FAULT. APU INOPERATIVE EXTERNAL POWER REQUIRED FOR ENGINE START. STARTER RELAY WILL NOT DE-ENERGIZE. INSPECTED APU COMPARTMENT NO DAMAGE NOTED OTHER THAN STARTER & LEAD. R & R APU STARTER RELAY IAW WDM 49-44-01, REPLACED APU STARTER IAW 49-44-01-2, REPAIRED STARTER LEAD & REINSTALLED IAW WDM 49-44-01 & SWPM. APU OPS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 83,716 hrs · 28,517 cycles

FLIGHT CREW REPORTED BATTERY 1 LOW MESSAGE, WHEN TESTING EMERGENCY LIGHTS. R & R EMERGENCY LIGHTING BATTERY POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-51-01-4.

Part: GCU — FAILED · airframe 80,125 hrs · 26,606 cycles

AFTER LANDING, ELEC ALERT LEVEL 2 ACCOMPANIED BY NUMEROUS FAILURES. AFTER PARKING ACRID ELECTRICAL BURNING ODOR. DE-POWERED ACFT, NOTIFIED EMERGENCY EQUIPMENT.

Part: ENGINE — FIRE (NR 3) · airframe 79,938 hrs · 26,507 cycles

HAD NO START ON ENG NR 3 RAN QRH ABNORMAL START CHECKLIST. GROUND CREW INFORMED FLT CREW OF TAIL FIRE. AFTER MOTORING ENGINE, STILL HAD FIRE IN ENG NR 3, BLEW FORE BOTTLE INTO NR 3 AND RAN ENGINE FIRE CHECK LIST. INSPECTED NR 3 ENGINE COWLS, PYLON, AND ENGINE. ALSO INSPECTED LOWER WING AREA AND RT GEAR STRUT FOR FIRE DAMAGE. REF MM 72-00-00-6 AND 72-00-00-7. NO CLEANING REQUIRED. REMOVED NR 3 ENG, NR 2 FIRE BOTTLE IAW AMM 26-21-01-4. INSTALLED SERVICEABLE FIRE BOTTLE & SQUIB REF MM 26-21-01-4. PERFORMED ENGINE RUN REFJRH, ENGINE STARTED ON B IGNITION AND ENGINE RUN NORMAL. REF WRI 74-10/8079 FOR NO START A IGNITION.

Part: FUEL CONTROL — FLAMED OUT (NR 1 ENGINE) · airframe 79,569 hrs · 26,323 cycles

NR 1 ENG RPM FLUCTUATED FROM IDLE & 90 % WITH CONCURRENT NR 1 THROTTLE MOVEMENT. NR 2 & 3 ENG VIA AUTOTHROTTLE SYS RESPONDED IN OPPOSITE DIRECTION TO COMPENSATE SPEED ERRORS. AUTOTHROTTLES SWITCHED TO OTHER SYS WITH NO CORRECTION NOTED. AUTOTHROTTLE SYS DISCONNECTED & NR 1 ENG PLACED AT IDLE FOR REST OF FLT. ON FINAL, NR 1 ENG FLAMED OUT. NO INDICATION OF ENG DAMAGE NOTED. ALL FUEL BOOST PUMP PRESSURES GOOD. INSTALLED NR 1 ENG MAIN FUEL PUMP & MEC ASSY REF AMM 73-12-01-2 UP TO STEP 3 B (22). COMPLETED INSTALL & RIG OF NR 1 ENG FCU, PUMP & VSV REF AMM 73-20-01-2 & 73-12-01. PERFORMED ENG TRIM ADJUSTMENT IAW 73-20-01-2. ENG IDLE, FLT IDLE, PART POWER & MAX POWER. OPS CHECK GOOD IAW JRH & MM 73-20-01-2.

Part: PLATE — CRACKED (NR 1 NACELLE) · airframe 79,360 hrs · 26,209 cycles

FOUND 2 EA BOLTS SHEARED AT NR 1 ENG PYLON AT LOWER TOMBSTONE FITTING. R & R LOWER PLUG PLATE, NUT RETAINER AND BOLTS ON THE NR1 ENG. LOWER TOMBSTONE FITTING IAW AMM 54-00-01-4.

Part: FITTING — CRACKED (ZONE 200) · airframe 76,449 hrs · 24,825 cycles

MCD LATCH SPOOL BACK UP FITTING HOLES SHOW DEFECT POS NR 1 HOLE C AND D MARKED IN RED. REPAIRED SPOOL BRACKET HOLES, REPLACED BACK UP FITTING, FABRICATED REPAIR BUSHINGS AND FUNCTIONAL CHECK IAW SRM 53-50-00 VOL 1 FIG 17, MAE TRAVELER T8/752908 AND WORK CARD E-9-5230-7-5000. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — CRACKED (ZONE 200) · airframe 76,449 hrs · 24,825 cycles

MCD LATCH SPOOL BACKUP FITTING HOLES SHOW DEFECT POS NR 7 HOLES A, B, C AND D MARKED IN RED. REPAIRED SPOOL BRACKET HOLES, REPLACED BACK UP FITTING. FABRICATED REPAIR BUSHINGS AND FUNCTIONAL CHECK IAW SRM 53-50-00 VOL 1 FIG 17, MAE TRAVILERT8/752909 AND WORK CARD E 9-5230-7-5000. REPAIRED CLASSIFIED AS A MAJOR REPAIR.

Part: BRAKE ASSY — LOCKED (MLG) · airframe 73,930 hrs · 23,680 cycles

NR 2 AND NR 3 MAIN BRAKES LOCKED UP AT HIGH SPEED LANDING. REMOVED AND REPLACED NR 2 AND NR 3 MAIN BRAKES PER MD10-10 AMM 32-43-01-4. VISUALLY INSPECTED ALL TIRES AND BRAKES, NO DEFECT FOUND.

Part: UNKNOWN — UNKNOWN (SLAT HANDLE) · airframe 73,930 hrs · 23,680 cycles

ON APPROACH TO TJSJ, SLAT HANDLE WOULD NOT MOVE. FLAPS OPERATE NORMAL AFTER FLAP/SLAT HANDLE SEPARATED. MADE NO SLAT WITH FLAPS, 22DEG LANDING. GROSS WT OF 346,00 0 LBS. APPROACH SPEED 198. BRAKE LOCKED AFTER CLEARING RUNWAY,WHILE AWAITING GROUND TUG FOR TOW TO RAMP. AFTER TOW A/C TO FEDEX RAMP. VISUALLY INSPECTED SLAT MECHANISM AT PEDESTAL AND CAC. NO DEFECT FOUND, PERFORMED FLAPS/SLATS OPERATION SEVERAL TIMES, SYS CKS NORMAL AT THIS TIME, AS PRECAUTIONARY LUB SLAT ACTUATOR AT CAC. WORK DONE PER MD10-10 AMM 27-00-00-2.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 71,796 hrs · 22,755 cycles

ON FINAL AT OAK AND SELECTING FLAPS 35 DEGREES, FLAP INDICATION SHOWED 35 DEGREES ON LEFT OUTBOARD AND LEFT INBOARD WHILE RIGHT FLAP INDICATIONS WERE BOTH "X'S". WENT AROUND AND LEFT FLAPS AT 22 DEGREES. RAN FLAP DISAGREE CHECKLIST IN QRH AND CAME IN FOR FLAP 22 / EXT LANDING. FOUND B1-985 C/B "FLAP AOA NR 2" POPPED. SHOOK WIRE HARNESS AT RIB FLAP XMTR & GOT C/B TO POP. CONFIRMED RT INBD FLAP XMTR TO BE CAUSE. ACN RELEASED FOR SERVICE PER "MEL 27-54-01: FLAP POSITION INDICATOR - INOP. REPAIRED WIRES AT R/H I/B FLAP TRANSMITTER PER SWPM. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (PNEUMATIC SYSTEM) · airframe 66,260 hrs · 20,459 cycles

AIR SYS 2 OFF ALERT ILLUMINATED AND WITHIN SECONDS, THE AIR MANF 2 FAIL ALERT ILLUMINATED. RETURNED TO MEMPHIS. NO OTHER SECONDARY INDICATIONS. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 CATEGORY: C EXPIRATION: 18MAY03 MEL 36-23-01-02: NR 2 MANIFOLD FAIL DETECTION LOOP INOP. MX MUST CLEAR ALERT PRIOR TO EACH DISPATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. CATEGORY -C- EXPIRATION DATE 18 MAY 03. *S/D* REPLACED MANIFOLD FAILURE CTRL, ALL LOOPS CHECK GOOD WITH TESTER AMM 36-23-01.