N363FE

Part: RELIEF VALVE — FAULTY (FUEL SYSTEM) · airframe 83,208 hrs · 32,163 cycles

AFTER PUSH BACK & STARTED ALL 3 ENGINES, GOT A LEVEL 3 TANK WING OVERFILL. FOLLOWED QRH & FUEL CONTINUED TO VENT OUT OF THE LEFT WING. STARTED WITH 98,400 LBS FUEL & SHUTDOWN WITH 90.8 BURNED ONLY 610 LBS ON THE ENGINES START LEVEL FUEL TANKS 1. R&R VENT OVERFILL RELIEF VALVE IAW AMM 28-12-05-4. OPS CHECKED IAW AMM 28-12-05-5. OPS CHECKED GOOD. R&R NR 3 TIP TANK CLIMB VENT VALVE IAW AMM 28-12-01-4. AFTER FURTHER INSPECTION, FOUND THE NR 3 TANK INBD CLIMB VENT FLOAT VALVE FLAPPER DOOR BROKEN OFF. R&R INBD CLIMB VENT FLOAT VALVE IAW AMM 28-12-01-4. OPS CHECKED GOOD, XFERED FUEL BETWEEN TANKS NO FUEL FROM VENT BOX.

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 82,781 hrs · 31,890 cycles

LOWER FWD FIRE INDICATION. AGENT DISCHARGED. INSTALLED LOWER CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLES 1 AND 2 IAW AMM 26-22-01-4. FAILS STEP 4 ELECTRICAL CONTINUITY TEST, ALSO REQUIRES STEP 5, FIRE EXTINGUISHER DEPLOYMENT LINES ROUTING AND LEAK CHECK. COMPLIED WITH STEP 5 AND 6, FIRE EXTINGUISHER DEPLOYMENT LINES ROUTING AND LEAK CHECK. ROUTING AND LEAK CHECK IS GOOD REF MM 26-22-05-2. R/I CP P1-2288 IAW WDM 26-22-01. ALL OPS CHKS PREVIOUSLY C/W. C/W ELECTRICAL CONTINUITY TEST OF THE LOWER CARGO FIRE EXTINGUISHER CONTAINER DISCHARGE CARTRIDGE AND OPS NORMAL IAW 26-22-01-5 LOWER CARGO FIREX DISCHARGE CIRCUITS - ADJUSTMENT/TEST.

Part: VANE — DENTED (RT WING TE FLAP) · airframe 81,536 hrs · 31,118 cycles

RIGHT INBD FLAP VANE LOWER SURFACE HAS IMPACT DAMAGED .300" X .300" AT THE CENTER TRACK. REPAIRED THE VANE IAW SRM 57-00-01, FIG 4, VOL I, PAGE 11.

Part: SEAT TRACK — CORRODED (BS 1942) · airframe 81,536 hrs · 31,118 cycles

MAIN CABIN, BS 1942, RBL 72, OTBD SEAT TRACK HAS CORROSION UNDERNEATH SPACER. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00, FIG 6.

Part: SKIN — DAMAGED (RT WING) · airframe 81,536 hrs · 31,118 cycles

RIGHT WING LOWER WING ACCESS PANEL CUTOUT AT XORS 683 HAS ONE DAMAGED HOLE AT THE 6 O'CLOCK POSITION AFT. REPAIRED IAW EA 8-5730-T0334612.

Part: SKIN — CRACKED (L1 DOOR) · airframe 81,536 hrs · 31,118 cycles

L1 DOOR HAD STRUCTURAL DAMAGE 4 X 4 AT UPPER AFT CORNER OF EXTERIOR SKIN. REPAIRED THE DOOR SKIN IAW SRM 52-10-00, FIG 12A.

Part: BULKHEAD WEB — CRACKED (BS 595) · airframe 81,536 hrs · 31,118 cycles

BS 595 BULKHEAD WEB AT LONGERON 39L HAS A .5 INCH CRACK AT THE LOWER FASTENER HOLE, PROPAGATING TOWARDS THE EDGE OF THE WEB. REPAIRED THE BULKHEAD WEB IAW SRM 53-40-00, FIG 25, VOL 1.

Part: LONGERON — CORRODED (BS 1967) · airframe 81,536 hrs · 31,118 cycles

AFT CARGO BILGE AREA FOUND SURFACE CORROSION AT BS 1967, LONGERON 48R. REMOVED SURFACE CORROSION IAW SRM 51-21-01 AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-00, VOL 1, FIG 17, SHEET 5.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 81,536 hrs · 31,118 cycles

LEFT INBD FLAP VANE UPPER INBD SURFACE HAS A DEEP SCRATCH 1 X 2.3 INCHES. REPAIRED IAW SRM 51-71-00, VOL II, PAGE 51, PAR 14, REPAIR C.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 81,536 hrs · 31,118 cycles

BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS A 1.8 INCH CRACK EXTENDING INTO RADIUS. REPAIRED THE BULKHEAD TEE CAP IAW EA 8-5310-T0334290 PT.1/PT.2

Part: SKIN — CRACKED (ACM DOOR) · airframe 81,536 hrs · 31,118 cycles

NR 2 ACM BAY ACCESS DOOR SKIN CRACKED 3 INCHES AT UPPER AFT SECTION, CRACK VERIFIED BY HFEC NDI INSPECTION. REPAIRED IAW SRM 52-00-01, FIG 4, SHEET 2, VOLUME 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 81,536 hrs · 31,118 cycles

LEFT WING OUTBOARD OF SLAT TRACK NR 12 INTERNAL BEADED DOUBLER HAS A CRACK. REPAIRED THE DOUBLER IAW SRM 57-10-00, FIG 71, VOL 1.

Part: SKIN — CRACKED (BS 791) · airframe 81,536 hrs · 31,118 cycles

EXTERIOR SKIN SURFACE, BS 859 LONGERON 43R HAS CORROSION AROUND FASTENERS CUT OUT DAMAGED SKIN AND INSTALLED CLASS II REPAIR IAW SRM 53-20-00, FIG 6, SHEETS 16 & 17, & EA 8-5330-T0334722, PT 1

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 81,536 hrs · 31,118 cycles

BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2.0 INCH CRACK EXTENDING INTO RADIUS. REPAIRED THE TEE CAP IAW EA 8-5210-T0334290 PT.1/PT.2.

Part: SKIN — CRACKED (BS 897) · airframe 81,536 hrs · 31,118 cycles

EXTERIOR SKIN SURFACE APPROXIMATELY BS 897, LONGERON 45R HAS A POSSIBLE CRACK. REPAIRED THE SKIN IAW SRM 53-20-00, VOL 1, FIG 6, SHT 17-19.

Part: THROTTLE CABLE — INOPERATIVE (NR 2 ENGINE) · airframe 80,920 hrs · 30,781 cycles

AT TOP OF DESCENT , NR 2 THROTTLE WAS STUCK AT 85% N1. SHUT DOWN NR 2 ENGINE AT 10.000. NORMAL LANDING, WAS ABLE TO MOVE NR 2 THROTTLE TO IDLE DURING TAXI TO CHOCKS. REMOVED AND REPLACED THROTTLE CABLE.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 80,810 hrs · 30,725 cycles

L1 DOOR EMERGENCY SLIDE FALLING OUT. REINSTALLED GIRT BAR IN ATTATCH FITTING IAW AMM 25-61-01-2. ACFT OK FOR SERVICE.

Part: SENSOR — DIRTY (FLAP/SLAT SYS) · airframe 80,684 hrs · 30,663 cycles

DURING APPROACH, WITH SLATS & FLAPS 22'EXT, OBSERVED LEVEL 2 "SLAT DISAGREE". IAW QRH, RETURNED FLAPS/SLATS TO 15'/EXT. OBSERVED INTERMITTENT LEVEL 2 "SLAT DISAGREE". COMPLIED WITH QRH, PERFORMED FLAPS 22' /RET LANDING, EMERGENCY DECLARED. UNEVENTFUL LANDING (NO UNCONTROLABLE ROLL AT ANY TIME. PITCH, POWER, A/S ALL NORMAL DURING ALERT. INSPECTED SENSOR R4B AND FOUND SENSOR AND TARGET VERY DIRTY. CLEANED SENSOR AND TARGET AREA AND SHOOK WIRES, NO ALERTS SHOWN. CYCLED SLATS/FLAPS FULL TRAVEL NUMEROUS TIMES STOPPING AT ALL POSITIONS. ALL INDICATIONS NORMAL ON CONFIG PAGE, PFD'S AND PSEU SENSOR READOUT. PERFORMED SLAT POSITION INDICATION ADJUSTMENT/TEST IAW MM 27-84-00-5. ALL INDICATIONS NORMAL. AIRCRAFT OK FOR SERVICE.

Part: ACTUATOR — FAULTY (L1 DOOR) · airframe 79,914 hrs · 30,258 cycles

L1 DOOR WILL NOT CLOSE. IT IS STUCK IN AN ALMOST CLOSED POSITION. REPLACED ELECTRIC ACTUATOR IAW AMM 52-11-01-2.

Part: RIB — DAMAGED (RT WING) · airframe 787 hrs · 29,653 cycles

RIGHT WING STATION 454.893 HAS A DAMAGED RIB. REPAIRED IAW EA 8-5710-T0319809.

Part: SKIN — CORRODED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

EXTERIOR FUSELAGE STATION 795, LONGERON 47 & 48, SKIN BULGING & RIPPLED. MARKED CUT OUT CORROSION & INSTALLED REPAIR FILLER & DOUBLERS IAW SRM 53-20-00 FIG 6 SHEET 9 VOL I.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 787 hrs · 29,653 cycles

LEFT WING UPPER SURFACE AT WING ROOT, JUST FWD OF THE VISUAL INDICATOR, THERE ARE 2 SMALL AREAS OF SURFACE CORROSION AT XORS 197.2 & XORS 230.6. ACCOMPLISHED EA 8-5730-T0319767 P1.

Part: PANEL — DELAMINATED (NR 2) · airframe 787 hrs · 29,653 cycles

NR 2 ENGINE LEFT RAMP PANEL HAS DELAMINATION. REPAIRED IAW SRM 51-71-00 VOL 2.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 787 hrs · 29,653 cycles

R1 DOOR SLIDE PARTIALLY DEPLOYED IN ERROR. SLIDE NEEDS REPLACED & PNEUMATIC RESERVOIR NEEDS SERVICED. OK TO INSTALL R1 EVAC SLIDE. R & R R1 EVAC SLIDE IAW 10-25-61-01-2. SERVICED R1 DOOR AIR RESERVOIR IAW 10-52-11-07-2.

Part: RIB — CRACKED (RT WING) · airframe 787 hrs · 29,653 cycles

RIGHT WING FIXED LE SUPPORT RIB CRACKED AT OTBD OF FUELING DOOR. REPAIR RIB IAW SRM 57-00-01 FIG 11.

Part: SKIN — CRACKED (RT WING) · airframe 787 hrs · 29,653 cycles

RIGHT WING FIXED LE UPPER INTERIOR SKIN IS CRACKED APPROX XROS 570 BY SLAT TRACK NR 10. INSTALLED FINGER DOUBLER REPAIR IAW SRM 57-10-00 FIG 71.

Part: SKIN — CRACKED (RT WING) · airframe 787 hrs · 29,653 cycles

RIGHT WING, FIXED LE INTERIOR UPPER SKIN IS CRACKED, OTBD OF SLAT TRACK 14, APPROX STATION XROS 810. INSTALLED FINGER DOUBLER PER SRM 57-10-00 FIG 71

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1641, RBL 47. R & R SECTION OF TRACK IAW SRM 53-7000.

Part: STRAP — CRACKED (RT WING) · airframe 787 hrs · 29,653 cycles

RIGHT WING, FIXED LE UPPER INTERIOR SKIN & STRAP ARE CRACKED OTBD OF SLAT TRACK 10, APPROX STATION XROS 570. REMOVED AND REPLACED STRAP SRM 51-31-01, FABRICATED PER SRM 51-10-01 DWG. ARB 1249-12

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN CABIN, APPROX STATION 1381, LBL 7 SEAT TRACK DAMAGED. R & R SECTION OF SEAT TRACK AT STATION 1381, LBL 7 IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK, DAMAGED SEAT TRACK LOBES APPROX STATION 1382, LBL 47. R & R SEAT TRACK SECTION FROM STATION 1350 - 1390, LBL 47 IAW SRM 53-70-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN CABIN, APPROX STATION 1381, RBL 48 SEAT TRACK WORN. R & R SEAT TRACK FROM APPROX STATION 1350 - 1392 IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1391, LBL 75.5. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1375, LBL 8.5. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1385, LBL 45.50. R & R DAMAGED SECTION FROM STATION 1350 - 1390, LBL 45 IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 1390, LBL 45.50. R & R DAMAGED SECTION FROM STATION 1350 - 1390 IAW SRM 53-70-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN CABIN, APPROX STATION 1380, RBL 72 SEAT TRACK WORN. R & R SEAT TRACK FROM APPROX STATION 1350 - 1392 IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1384, X=45.50 RT. R & R SEAT TRACK FROM APPROX STATION 1350 -1392 IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1390 X=45.50 RT. R & R SEAT TRACK FROM APPROX STATION 1350 - 1392 IAW SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN DECK, SEAT TRACK DAMAGED APPROX AT STATION 1384, LBL 75.5. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 787 hrs · 29,653 cycles

MAIN CABIN, APPROX STATION 1381, LBL 72 SEAT TRACK WORN. R & R SECTION OF SEAT TRACK AT STATION 1381, LBL 72 IAW SRM 53-70-00.

Part: CONNECTOR — FAILED (NR 2 ENGINE) · airframe 785 hrs · 29,542 cycles

NR 2 ENGINE LOW N2 RPM ALERT AT 200 AGL AFTER TAKEOFF. R & R CONNECTOR P1-8080IAW SMP & WDM 77-12-01.

Part: SKIN — DAMAGED (RT WING) · airframe 77,451 hrs · 28,910 cycles

RIGHT WING UPPER SURFACE ON THE ISLAND OTBD OF INBD AILERON HAS 7 FASTENERS PULL THRU SKIN ON THE FWD INBD END. REPAIRED UPPER ISLAND SKIN IAW SRM 57-10-00 VOL I FIG 89. VERIFIED THE CUT OUT AREA FREE OF CRACK. COMPLIED WITH HFEC INSPECTION NDT IAW TO CHAPTER 06, FOUND NO CRACK. VERIFIED FILLER PN IS 2024-T3, .060 & DOUBLER IS 2024-T3, .063. INSTALLED FILLER & DOUBLER IAW SRM 57-10-00 VOL 1 FIG 89. PREP & PAINTED TOP COAT ON REPAIRED AREA IAW SRM 51-21-02 VOL II.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,434 hrs · 28,897 cycles

AFT CARGO, 52 LONGERON EXT IS CORRODED BETWEEN STATION 1953 & 1965. R & R LONGERON 52 EXT BETWEEN STATION 1953 & 1965 SRM 51-33-01 VOL II.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,434 hrs · 28,897 cycles

AFT CARGO 51R LONGERON EXT CORRODED BETWEEN STATION 1953 - 1965. R & R LONGERON 51R BETWEEN STATION 1953 - 1965 IAW SRM 51-33-01 VOL II.

Part: SKIN — CRACKED (RT WING) · airframe 77,223 hrs · 28,768 cycles

POSSIBLE CRACK RT WING SLAT CUT OUT SEVEN INCHES FROM WING TIP. VERIFIED CRACK IN RT WING SLAT CUT OUT WITH HFEC IAW NDT SPM PT 6, CRACK APPROX 3/4 INCH LENGTH. CUT OUT CRACK IAW SRM 57-10-00. PERFORMED HFEC INSPECTION TO CUT OUT IAW NDT SPM PT 6, NO DEFECTS NOTED. VERIFIED MATERIALS & FABRICATED DOUBLER & FILLER IAW SRM 57-10-00 FIG 68 PO. TREATED & PRIMED AREA & REPAIR COMPONENTS. INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-10-00 FIG.68.

Part: SKIN — CRACKED (ZONE 600) · airframe 77,093 hrs · 28,698 cycles

DURING WALK AROUND, FOUND LE CRACK AT RT WING FUELING PANEL INBD SIDE. INSTALLED DOUBLER REPAIR IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 76,635 hrs · 28,481 cycles

RIGHT WING, VERTICAL CRACK FOUND AT THE FRONT WING SPAR INBD UPPER CORNER AT FUSELAGE.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,451 hrs · 28,910 cycles

AFT CARGO LONGERON 50R CORRODED BETWEEN STATION 1944 TO 1965. CUT OUT DAMAGED SECTION OF LONGERON 50R STATION 1955 TO 1965 IAW SRM 53-10-00 FIG 2. INSTALLED NEW FABRICATED LONGERON SPLICE AT LONGERON 50R BETWEEN STATION 1955 THRU 1965 IAW SRM 51-33-01 VOL II ABD EA 8-5310-T0305476. FABRICATED TYPE II LONGERON SPLICE MADE OUT OF 7075-T6 IAW SRM 53-10-00. CHECKED FABRICATED PART WITH EDDY CURRENT METHOD FOR DEFECT, NO DEFECT NOTED. RE-INSTALLED PREVIOUSLY REMOVED WEB & FLOOR PANELS FOR ACCESS.

Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 75,886 hrs · 28,062 cycles

FL 380, RECEIVED A HYD 3 OFF LIGHT, PUMPS WENT OFF STAYED THAT WAY UNTIL SLATS OUT, RECEIVED SLAT DISAGREE - PUT SLATS UP SLOWED TO 210 -SLATS EXTENDED BOTH AGREE, PRESSURE CAME BACK ON 3, FLAPS 15 PRESSURE, DROPPED GEAR PRESSURE WENT TO ZERO WITH MAINS DOWN AND LOCKED, NOSE UNSAFE, QRH ALTERNATE HANDLE UP NOSE WHEEL SAFE, PRESSURE ZERO ON 3, ON HYD SYS 2 LT PUMP TEMP OVERTEMP LIGHT FOLLOWED BY RT PUMP LIGHT OFF. HYD SYS 2 FAULT, TEMP 110 DEGREES C PRESSURE GOOD, ALL FAULTS WENT AWAY AFTER TOUCHDOWN. NOSE WHEEL PARTLY, HYD QTY TRANSMITTER CHECKED NORMAL, REF AMM 29-32-02-5. NR 3 HYD SYS TESTS NORMAL, REF FIM 29-10-06. RAN NR 3 ENGINE REF JRH. PREMATURE REMOVAL/INSTALLATION.

Part: UNKNOWN — ODOR (CABIN) · airframe 75,260 hrs · 27,706 cycles

ON ARRIVAL PASSING 7,000' WITH DECK ANGLE 5 DEGREES, F/O'S GOT VERY STRONG FUMES THAT REASSEMBLEED BURNING PLASTICE. HAD A VERY SIMILAR BUT FAINT ODOR UP ON ARRIVAL ON PREVIOUS FLIGHT. SEEM TO BE COMING FORM F/O'S SIDE RATHER THAT CAPTAIN'S SIDE. COULD NOT DUPLICATE WITH APU SOURCE OF AIR OR ENGINE. OPS CHECK GOOD. OK FOR SERVICE. IAW AMM 21-00-00-0 AND IAW JRH.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 74,320 hrs · 27,169 cycles

AFT CARGO, FOUND CORROSION ON THE SHEAR TIE OF THE AFT SIDE OF BS 1975, FRAME BETWEEN LONGERON 50R AND 50L . R & R SHEAR TIE IAW SRM 51-30-01, VOL II.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,320 hrs · 27,169 cycles

AFT CARGO: ANGLE ON THE AFT SIDE OF STA 1966, FRAME BETWEEN RT LONGERON 50 AND LT LONGERON 50 IS CORRDED. REPLACED CORRODED ANGLE WITH NEW ANGLE IAW SRM 51-30-01 VOL.II

Part: BOTTLE — DISCHARGED (DOOR ASSIST) · airframe 73,365 hrs · 26,682 cycles

EMERGENCY ASSIST BOTTLE NEEDS SERVICING. L1 DOOR ASSIST BOTTLE SERVICED IAW MM 52-10-01. OK FOR SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 72,677 hrs · 26,343 cycles

SKIN SHOWS BULGING AT STA 1705, STR 50R. REMOVED CORROSION BY REPLACING SKIN SEC REF EA 8-5330-138730.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,674 hrs · 25,823 cycles

AREA OF BODY STA 878, LOGERON 46R SHOWING CORROSION THROUGH FUSELAGE SKIN. (JUST BELOW OF PREVIOUS DOUBLER REPAIR) CUT OUT CORRODED SECTION OF SKIN AT REF SRM 53-20-01. FABRICATED NEW REPAIR DOUBLER AND INSTALLED THE DOUBLER REF SRM 53-20-00 FIG 6. CUT OUT SECTION OF CORRODED. FABRICATED NEW SECTION OF R47 INSTALLED REF TO SRM 53-10-00. REPAIRED CORROSION REF SRM 53-20-00, FIG 6.

Part: STRUT — CORRODED (RT MLG) · airframe 71,674 hrs · 25,823 cycles

RIGHT MLG SHOCK STRUT (OUTER CYLINDER) LOWER CURCUMFERENTIAL INTERNAL THREADS ARE CORRODED/PITTED. ALSO, THE SHOCK STRUT GLAND NUT THREADS FOR MLG OUTER CYLINDER (SHOCK CYLINDER) ARE CORRODED/PITTED (REF SNRM 872). RIGHT MAIN OUTER CYL.-LOWER CIRCUMFERENTIAL INTERNAL THREAD CORROSION ON MLG CYL. PART IS NOT ACCEPTABLE FOR CONTINUED SERVICE. GEAR REPLACED PER WORKCARD 32T1701-RC, SEQ. 000879.

Part: STRUT — CORRODED (LT MLG) · airframe 71,674 hrs · 25,823 cycles

LEFT MLG SHOCK STRUT (OUTER CYLINDER) LOWER CIRCUMFERENTIAL INTERNAL THREADS ARE CORRODED/PITTED. ALSO, THE SHOCK STRUT GLAND NUT THREADS FOR MLG OUTER CYLINDER (SHOCK STRUT) ARE CORRODED/PITTED. LT MAIN OUTER CYL.-CIRCUMFERENTIAL INTERNAL THREAD CORROSION ON MLG CYL. PART IS NOT ACCEPTABLE FOR CONTINUED SERVICE. GEAR REPLACED PER WORKCARD 32T1701-LC, SEQ. 000878.

Part: BRAKE — FIRE (MLG) · airframe 69,244 hrs · 24,696 cycles

NR 3 BRAKE CAUGHT ON FIRE AT GATE. REMOVE AND REPLACE NR 3 BRAKE IAW MM 32-43-01-4, ALSO INSPECTED ADJACENT AREA FOR DAMAGE AND NO DAMAGE NOTED.

Part: BRAKE — FIRE (NR 3) · airframe 69,244 hrs · 24,696 cycles

NR 3 BRAKE CAUGHT ON FIRE AT GATE. REMOVE AND REPLACE NR 3 BRAKE IAW MD-10 MM 32-43-01-4, ALSO INSPECTED ADJACENT AREA FOR DAMAGE AND NO DAMAGE NOTED.

Part: CYLINDER — DAMAGED (RT MLG) · airframe 69,155 hrs · 24,651 cycles

UPON GEAR RETRACTION HAD RED LIGHT IN PRIMARY RT MAIN INDICATOR. CONFIRMED IN SECONDARY. RAN" GEAR PRIMARY OR SECONDARY LT(S) ILLUMINATE WITH GEAR HANDLE UP" CHECKLIST. RETURN TO KMEM. NO PROBLEMS ON ROLLOUT. REMOVED AND REPLACED RT MLG BUNGEE CYLINDER, ROD END BROKE IN HALF.

Part: CYLINDER — DAMAGED (RT MLG) · airframe 69,155 hrs · 24,651 cycles

UPON GEAR RETRACTION HAD RED LIGHT IN PRIMARY RT MAIN INDICATOR. CONFIRMED IN SECONDARY. RAN GEAR PRIMARY OR SECONDARY LT(S) ILLUMINATE WITH GEAR HANDLE UP CHECKLIST. RETURN TO KMEM. NO PROBLEMS ON ROLLOUT. REMOVED AND REPLACED RT MLG BUNGEE CYLINDER, ROD END BROKE IN HALF.

Part: SUPPORT FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,690 hrs · 24,442 cycles

MCD JAMB SUPPORT FITTING NR 7 HOLES A, B, C AND D ARE CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-31-01. REMOVED SEAT TRACK, ATTACH ANGLE, INTERCOSTAL AND WEB (BY CUTTING) FOR ACCESS IAW SRM 51-31-01. REINSTALLED SEAT TRACK, ATTACH ANGLE, INTERCOSTAL IAW SRM 51-31-01. REINSTALLED AND REPAIRED WEB IAW SRM 51-33-01 AND 51-35-01. INSTALLED NEW FITTING IAW SRM 51-31-01 AND RIGGED ON EA 8-5230-117634 WRI 52-30/5344

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,690 hrs · 24,442 cycles

CENTER CARGO COMPARTMENT DOOR LOWER TORQ BOX AFT LIGHTENING HOLE FWD INBOARD FRAME IS CORRODED REMOVED AND REPLACED FRAME IAW SRM 53-30-00 FIG 2. CUT AND REMOVED FLOORBEAM AND FRAME FOR ACCESS AND REINSTALLED AND REPAIRED IAW SRM 51-33-01 AND 53-30-00.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK LUG CHIPPED AT FS 845 TRACK 75R. BLENDED AREA AND CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 51-31-01 VOL II. REMOVED 3 FLOOR PANELS AND CUT OUT DAMAGE AREA OF SEAT TRACK IAW SRM 51-31-01. NEW TRACK MANUFACTURED ON MAE TRAVELER T8/725393. INSTALLED NEW SEAT TRACK AND 3 EACH FLOOR PANELS IAW SRM 53-31-01 AND 53-21-08-2. FILLED OUT RDR. CLASSIFIED AS A MAJOR REPAIR AND IS RII.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK LUGS WORN AT FS 900, 906 AND 935. TRACK 48L REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVILERS T8/725338 AND T8/725336.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK HAS 2 WORN LUGS AT FS 1631 AND 1636, TRACK LBL 8. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVELERS T8/725335 AND T8/725337 MAJOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK AT STA 755 LBL 48 HAS WORN LUGS REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVELER T8/725392.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK AT FS 755 LBL 8 HAS WORN LUGS. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVELERS, T8/725391 AND T8/725395.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK LUG WORN AT FS 750 TRACK LBL 28. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PART FABRICATED ON TRAVELER, T8/725094.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 68,690 hrs · 24,442 cycles

SEAT TRACK LUG IS CHIPPED AT F/S 635 TRACK RBL 8. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVELERS T8/725394 AND T8/725350. MAJOR REPAIR.

Part: RETRACT CYLINDER — LEAKING (ZONE 700) · airframe 68,580 hrs · 24,399 cycles

HYD SYS QTY SLOW LEAK 0.1 GAL. PER 3 MIN GOT HYD 3 ELEV OFF AND HYD SYS 3 LOW LANDED DEN WITHOUT INCIDENT. RT MAIN GEAR RETRACT CYL LEAKING, SPARES NOT IN PLACE, NEEDS NEW ACTUATOR, OR GEAR DOWN FLT, ACT NIS DEN. REMOVED RETRACT CYLINDER PER MM 32-33-01-4. REPLACED MLG RETRACT CYLINDER PER AMM-32-33-01-4. LEAK CK, OPS CHECK SAME. OK FOR SERVICE.

Part: BLOCKER DOOR — DEBONDED (ZONE 400) · airframe 63,039 hrs · 21,941 cycles

NR 3 ENGINE RIGHT T/R NR 4 BLOCKER DOOR BROKE. REMOVED AND REPLACED NR 3 RIGHT T/R NR 4 BLOCKER DOOR IAW MD-10-10 MM 78-32-06-2.

Part: SKIN — DAMAGED (NR 7 SLAT) · airframe 63,039 hrs · 21,941 cycles

COMPLY WITH EA 8-5710-55426 WINGS - BASIC, LT, LEADING EDGE NR 7 SLAT SKIN REPAIR AT XOS=947.65. COMPLIED WITH EA 8-5710-55426.

Part: SUPPORT — CORRODED (ZONE 600) · airframe 63,039 hrs · 21,941 cycles

COMPLY WITH EA 8-5750-55430 WINGS - FLAP VANE SUPPORT CORROSION REWORK RIGHT O/B FLAP. COMPLIED WITH EA 8-5750-55430.

Part: VANE — BROKEN (ZONE 500) · airframe 61,342 hrs · 21,157 cycles

JUST PRIOR TO PUSHBACK FORT WORTH POLICE DEPT. REPORTED AN A/C PART HAD COME OFF A FEDEX A/C. LOWERED FLAPS AND FOUND LEFT O/B FLAP VANE HAD APPROX 5 FOOT MISSING. HONEYCOMB HAD BROKEN OFF INBOARD END. A/C NOT SAFE FOR FLIGHT. VANE IS IN WORK. INSTALLED LT OUTBOARD FLAP VANE IAW MM 27-50-03-2, AND FLAP VANE OPS CHECKS NORMAL. AS PRECAUTIONARY CHECKED LT OUTBOARD FLAP FOR DAMAGE, NONE FOUND, AND FLAP VANE SPRING FOR SECURITY AND DAMAGE, NONE FOUND. ALSO CHECKED VANE TRACKS AND ROLLERS FOR SECURITY AND OPERATION, NO DEFECTS NOTED. OKAY FOR SERVICE.

Part: SENSOR — ERRATIC (NR 2 ENGINE) · airframe 59,736 hrs · 20,315 cycles

DURING LEVEL CRUISE AT FL 330, CREW OBSERVED A LEVEL 2 ALERT (ENGINE 2 RPM LO) CONSIDERED SEVERE DAMAGE DUE TO NR 1 AND NR 2 RPM SPLIT WITH VERY ERRATIC NR 2 RPM. CREW ACCOMPLISHED SEVERE DAMAGE CHECKLIST IN QRH. PRESHUTDOWN PARAMETERS: NR 1 (94 PERCENT), EGT NORMAL, NR2 (32 PERCENT) PLUS OR MINUS 10 PERCENT AND ERRATIC, FF NORMAL, POST SHUTDOWN PARAMETERS: N1 (0), EGT LOW TEMP, NR 2 (8 PERCENT), FF 0 OIL PRESSURE 6-8 PSI APX. INSPECTED INLET AND EXHAUST; NO DISCREPANCIES FOUND. AFTER C/W MD1010 MM. RAN NR 2 ENG AND DUPLICATED MALFUNCTION. REMOVED AND REPLACED CORE SPEED SENSOR IAW MM. RAN NR 2 ENGINE OPS CHECKED NORMAL.

Part: ODOR — DETECTED (CARGO BAY) · airframe 58,730 hrs · 19,832 cycles

TEN MINUTES AFTER T/O JUMPSEATERS AND F/O SMELLED FUMES IN CARGO COMPARTMENT. RETURNED TO MCO. INSPECTED CARGO COMPARTMENT, OPENED EVERY CONTAINER ON MAIN DECK AND NO FUMES OR PROBLEMS FOUND. RAN ALL 3 PACKS ONE AT A TIME WITH APU AND ENGINE AIR AND NO PROBLEMS FOUND. A/C OK FOR SERVICE IAW M/M 26-15-00-0.

Part: FRAME — FAILED (RT MLG) · airframe 58,064 hrs · 19,485 cycles

RT MLG RETRACT CYLINDER SUPPORT FRAME ASSY FAILURE OCCURRED. REMOVED AND REPLACED STEEL SUPPORT FRAME AND CYLINDER ASSY PER DC10-57-105.

Part: SUPPORT — FAILED (RT MLG) · airframe 58,067 hrs · 19,486 cycles

NR 3 HYDRAULIC SYS AND RT MLG RETRACT ACT FAILED. REMOVED AND REPLACED FRAME SUPPORT.