N623FE

Part: SLIDE — FAILED (NOT ENTERED) · airframe 66,511 hrs · 17,301 cycles

L1 DOOR SLIDE PARTIALLY DEPLOYED WHILE TROUBLESHOOTING NR0039 (L1 DOOR INOP). REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY. REF MD11 AMM 25-61-01-4. SEE JPF FOR WORK ACCOMPLISHED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,432 hrs · 16,980 cycles

ON PREFLIGHT OF EMER LTS, GOT LVL 1 ALERT EMER LT BAT 1 LO. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD.

Part: NONE — NONE (N/A) · airframe 65,110 hrs · 16,861 cycles

PDIS 623 28-40 6983 06JUN22 CDG OPEN U LOGPAGES:385994 ON DESCENT FLT 200 RECEIVED LEVEL 2 FUEL QUANTITY FAULT TANK 1/3 FUEL QUANTITY LO - NOW W/ ARRIVED AT CDG DECLARED EMERGENCY FUEL PER QRH ADVISED AS A VALID ALERT. PERFORMED FUEL MIGRATION INSPECTION/CHECK IAW AMM 28-22-00-6.TEST OK, NO MIGRATION FOUND. PERFORMED TEST FQBU IAW 28-41-00-5, FOUND SEM IN FAULT, R&R'D SEM PER AMM 28-41-92-4-0. FQBU TEST PERFORMED FEW TIMES IAW AMM 28-41-00-5 ALL TEST PASSED

Part: HINGE — WORN (ZONE 800) · airframe 64,789 hrs · 16,766 cycles

MAIN DECK CARGO DOOR UPPER EDGE, ATTACHED AFT HINGE FITTING #7 (PART NUMBER:ACA 7223-515) LOBES #12 TO #17 FOUND OUT OF TOLERANCE. MAIN DECK CARGO DOOR UPPER EDGE, ATTACHED AFT HINGE FITTING #7 (PART NUMBER:ACA 7223-515) LOBES #12 TO #17 REWORKED AND FOUND #15 TO #17 LOBES EXCEED LIMIT AS PER MD-11 SRM 52-30-16-1A. ALLOWABLE DAMAGE 2 FIGURE 101 SHEET 3. OVERSIZE REPAIR BUSHINGS 06 EACH FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04 REPAIR- GENERAL, PARAGRAPH 2.Y AND E.A. # 1-5230-T0367842 PART 1 STEP 2 AND STEP 5, TITLE: DOORS- CARGO DOOR/ HYD SYS- MAIN DECK CARGO DOOR- WORN SUPPORT HINGE LOBES (DOOR SIDE). REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — WORN (ZONE 800) · airframe 64,789 hrs · 16,766 cycles

MAIN DECK CARGO DOOR, UPPER EDGE ATTACHED FORWARD (#1) HINGE FITTING (PART NUMBER:ACA 7332-1) ALL 9 LOBES FOUND OUT OF TOLERANCE. MAIN DECK CARGO DOOR, UPPER EDGE ATTACHED FORWARD (#1) HINGE FITTING (PART NUMBER:ACA 7332-1) ALL 9 LOBES REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 52-34-04. OVERSIZE REPAIR BUSHINGS 09 EACH FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04 REPAIR- GENERAL, PARAGRAPH 2.Y AND E.A. # 1-5230-T0367794 PART 1 STEP 2 AND STEP 5, TITLE: DOORS- CARGO DOOR/ HYD SYS- MAIN DECK CARGO DOOR- FORWARD MOST SUPPORT (DOOR SIDE) -HINGE LOBE BORE FOUND WORN. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (CENTER CARGO) · airframe 64,789 hrs · 16,766 cycles

CENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT SUSPECT CRACK. CENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT REPAIR CARRIED OUT AS PER SRM 53-00-05-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — CRACKED (BS 2140) · airframe 64,789 hrs · 16,766 cycles

EMPENNAGE - AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHT FOUND SKIN CRACK 2.2 INCH. EMPENNAGE -AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHT CRACKED SKIN REPAIRED AS PER EA # 1- 5330-T0367785 P1 TITLE : FUSELAGE - PLATES & SKINS - REPAIR PLAN FOR CRACK AJC7060-506 SKIN PANEL AT STA 2140 , L -36R AT THE APU EXHAUST DOOR CUT-OUT EDGE. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1641) · airframe 64,789 hrs · 16,766 cycles

MAIN DECK CARGO COMPARTMENT FLOOR , SEAT TRACK ALONG X = - 8.5 STATION 1641 FOUND WITH CORROSION AT FLANGE. MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK FLANGE AT STATION 1641 X = -8.5 , CORROSION REMOVED AS PER SRM 51-21-01-0G AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1610 TO STATION 1651 X = -8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (MAIN DECK CARGO) · airframe 64,789 hrs · 16,766 cycles

MAIN DECK CARGO COMPARTMENT LEFT HAND STATION 1761 FRAME FLANGE FOUND DENTED AT LONGERON 12 LEFT LOCATION. FRAME FLANGE REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. I

Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT RIGHT HAND WING LEADING EDGE CAVITY STATION XOS= 667.

Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING DOUBLER REPAIR FOUND AT RIGHT HAND WING LOWER SKIN LEADING EDGE CAVITY STATION XOS= 584 TO XOS= 610.

Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS= 789. EVALUATED AND FOUND DOUBLER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51-33-01-0G AND DOUGLAS DRAWING ARB3954 REVISION K. EO 1-5100-7-5001 B7 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS= 667. EVALUATED AND FOUND DOUBLER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51-33-01-0G AND DOUGLAS DRAWING ARB3954 REVISION K. EO 1-5100-7-5001 B7 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: FORMER — UNKNOWN (ZONE 500) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING FORMER REPAIR FOUND AT LEFT HAND WING LEADING EDGE CAVITY STATION XOS= 559. EVALUATED AND FOUND FORMER REPLACED BY FABRICATION IN ACCORDANCE WITH SRM 51- 33-01-0G AND DOUGLAS DRAWING ARB1162 REVISION S. EO 1-5100-7-5001 B7 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING RIB DOUBLER REPAIR FOUND AT RIGHT HAND WING LEADING EDGE CAVITY STATION XOS= 789.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 64,789 hrs · 16,766 cycles

MAIN DECK CARGO COMPARTMENT FLOOR , SEAT TRACK ALONG X = 8.5 CROWN AT STATION 1541 FOUND CRACKED. MAIN DECK CARGO COMPARTMENT FLOOR , CRACKED SEAT TRACK AT STATION 1541 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 5-123 TO STATION 1631 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (ZONE 240) · airframe 64,789 hrs · 16,766 cycles

MAIN DECK CARGO COMPARTMENT FLOOR , SEAT TRACK ALONG X = 47.5 CROWN FOUND CRACKED OFF AT STATION 755. MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 755 X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 725 TO EXISTING SPLICE STATION 765 , X = 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CRACKED (ZONE 200) · airframe 64,789 hrs · 16,766 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO FRAME STATION 1781 LONGERON 12 RIGHT HAND TO 13 RIGHT HAND. EXISTING REPAIR AT MAIN DECK CARGO FRAME AT ACTUAL CORRECT STATION 1781 LONGERON 11 RIGHT HAND TO 14 RIGHT HAND EVALUATED AND FOUND FRAME CRACK APPROXIMATE 4 INCHES. FRAME SPLICE REPAIR AT EXISTING SPLICES STATION 1781 LONGERON 11 RIGHT HAND TO 14 RIGHT HAND CARRIED OUT IN ACCORDANCE WITH SRM 53-00-07-2R REPAIR 4 FIGURE 201. EO 1-5100-7-5001 B7 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 64,789 hrs · 16,766 cycles

RIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 793 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 793 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 64,789 hrs · 16,766 cycles

RIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 696 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 696 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 64,789 hrs · 16,766 cycles

RIGHT HAND WING - LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS = 737 FOUND CRACK. RIGHT HAND WING LEADING EDGE CAVITY DOUBLER AT STATION XOS 737 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: WARNING MESSAGE — FALSE INDICATION (FUEL SYSTEM) · airframe 63,523 hrs · 16,351 cycles

ENROUTE RECEIVED A LEVEL 2 ALERT, FUEL QTY/USED CHK, AND POSSIBLE FUEL LEAK MESSAGE. COMPLIED WITH QRH. WE SHOWED A DISCREPANCY IN FUEL OF 5000 LBS AND WHEN DIVERTED BECAUSE OF POSSIBLE FUEL LEAK IT WAS 7500 LBS DISCREPANCY. IT WAS UNUSUAL THAT FUEL WAS TRANSFERRED UNUSUALLY QUICKLY ON CLIMB OUT TO THE TAIL #7800. THE SAME OCCURRED ON DESCENT. ONCE WE PULLED INTO THE GATE, FUEL BURN AND FOB SYNOPTIC NUMBERS ADDED UP TO EXACTLY WHAT WE TOOK OFF WITH AND NORMAL. WHEN THE TAIL TANK WAS EMPTY ON THE GROUND FUEL BURN AND FOB SHOWED NORMAL. MEL 04SEP21 12:12 IND U RELEASED FOR SERVICE PER MEL : 28-01-03-02 CATEGORY : C EXPIRATION : 14SEP21 "MEL 28-01-03-02: TAIL TANK SYNOPTIC QTY DISPLAY- INOP. AFTER REFUELING, VERIFY BY USING MCDU TAIL TANKLOW FLOAT READOUT OR WITH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML THAT TAIL TANK QTY IS EMPTY. TAIL FUEL MANAGEMENT - INOP.". RELEASED FOR SERVICE PER MEL : 28-01-03-02 CATEGORY : C EXPIRATION : 14SEP21

Part: PROBE — FAILED (TAT) · airframe 62,095 hrs · 15,936 cycles

PASSING FL270, ALL DATA DROPPED OFF PFD (AUTOPILOTS, AUTOTHOTTLES, NAV DATA, FLIGHT DIRECTOR ETC), RAN QRH TO STABILIZE AIRPLANE, PER QRH SWITCHED CADC 1 TO AUX & DATA RETURNED. AIR TURNBACK TO ONT, HAD IDENTICAL FAILURE USING AUX. DATA RETURNED ON ITS OWN A MINUTE LATER. EMERGENCY DECLARED. REMOVED AND REPLACED TAT SENSOR PER AMM 34-16-02-2. OPS CHECK NORMAL. AC OK TO CONTINUE

Part: SUPPORT FITTING — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

FUSELAGE Ï¿½ CENTER STRUCTURE INSTALLATION Ï¿½ WHILE ACCOMPLISHING INSPECT/REPLACE HI-LOKS ON LEFT HAND INBOARD FLAP SUPPORT FITTING AT YIFH 61 FOUND THE EXISTING INSTALLED HI-LOKS EXCEEDS LIMITS AS PER WORKCARD E1-5310-7-5004 PART 5 STEP 13. COMPLIED WITH EA 1 Ï¿½ 5340 Ï¿½ T0308226A PART 2 TITEL: FUSELAGE Ï¿½ ATTACH FITTINGS Ï¿½ LEFT HAND WING INBOARD FLAP SUPPORT FITTING, APPROVAL OF OVERSIZED FASRENERS PER EO 1 Ï¿½ 5310 Ï¿½ 7 Ï¿½ 5004, SERVICE BULLETIN MD11 Ï¿½ 53 Ï¿½ 067 R2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

FUSELAGE Ï¿½ CENTER STRUCTURE INSTALLATION Ï¿½ WHILE ACCOMPLISHING INSPECT/REPLACE HI-LOKS ON RIGHT HAND INBOARD FLAP SUPPORT FITTING AT YIFH 61 FOUND THE EXISTING INSTALLED HI-LOKS EXCEEDS LIMITS AS PER WORKCARD E1-5310-7-5004 PART 6 STEP 13. COMPLIED WITH EA 1 Ï¿½ 5340 Ï¿½ T0308227A PART 2 TITEL: FUSELAGE Ï¿½ ATTACH FITTINGS Ï¿½ RIGHT HAND WING INBOARD FLAP SUPPORT FITTING, APPROVAL OF OVERSIZED FASRENERS PER EO 1 Ï¿½ 5310 Ï¿½ 7 Ï¿½ 5004, SERVICE BULLETIN MD11 Ï¿½ 53 Ï¿½ 067 R2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0353428 PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- LT WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0353493 PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- RT WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0353428 PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- LT WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0353493 PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- RT WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1- 5750-T0353493 PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- RT WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0353428 PART 1 STEP 1F(1) AND STEP 1F(3), TITLE: WINGS- FLIGHT SURFACES- LT WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (AC DOOR) · airframe 59,865 hrs · 15,344 cycles

FUSELAGE - # 2 AIR - CONDITIONING COMPARTMENT DOOR INTERIOR UPPER EDGE FOUND CRACKED BETWEEN STATION YFAD -0.437 AND YFAD -12.422 FUSELAGE - # 2 AIR - CONDITIONING COMPARTMENT DOOR INTERIOR UPPER EDGE CRACKED FRAME BETWEEN STATION YFAD -0.437 AND YFAD -12.422 REPAIRED AS PER E.A # 1-5240- T0353482 P1 TITLE : DOORS - SERVICE - # 2 LH FWD AIR CONDITIONING COMPARTMENT DOOR UPPER EDGE SKIN AND FRAME REPAIR , YFAD -12.42 TO YFAD 12.26 WORK INSTRUCTIONS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE # 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE # 5 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# 1-5750-T0353488 PART 1 STEP 1. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT CORROSION REPAIR. OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00823 ATTACHED E.A. # 1-5750-T0353488 PART 1 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING - OUTBOARD FLAP VANE # 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE # 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND E.A.# 1-5750-T0353488 PART 1 STEP 1. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RH WING- OUTBD FLAP VANE ASSY- TRACK SUPPORT CORROSION REPAIR. OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27- 50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00823 ATTACHED E.A. # 1-5750-T0353488 PART 1 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. SUPPORT FITTING REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201 AND EA 1-5750-T0353488 PART 1 STEP 1. TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING- OUTBD FLAP VANE ASSY TRACK SUPPORT CORROSION REPAIR. OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND PIVOT BORE SPOTFACE REMAINING THICKNESS : 0.423" (OUTBOARD) IS CORRECT AS PER E.A.#: 1-5750-T0353493 PART 1 STEP 1E FIGURE 1, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 764 FOUND BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 764 DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 993 FOUND FORMER CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB 1164 REVISION M. INSTALLED FABRICATED FORMER AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 993 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1025 FOUND FORMER CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED FORMER AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1025 AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CRACKED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1084 FOUND ANGLE CRACKED. CRACKED ANGEL REMOVED AS PER SRM 51-31-01-0G AND FABRICATED ANGLE AS PER DOUGLAS DRAWING ARB 2920 REVISION BB. INSTALLED FABRICATED ANGLE AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1084 AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION CORROSION AT LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND PIVOT BORE SPOTFACE REMAINING THICKNESS : 0.437" (OUTBOARD) IS CORRECT AS PER E.A.#: 1-5750-T0353428 PART 1 STEP 1E FIGURE 2, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 794 FOUND BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 794 DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 59,865 hrs · 15,344 cycles

03EA FASTENER HOLES #30, #31, #32 FOUND WITH CRACK INDICATION DURING ACCOMPLISHMENT OF OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. REPAIR CARRIED OUT AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700 AT HOLES #30, #31, #32 AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AFTER 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES AS PER SRM 57-20-02-2R FIGURE 202 REPAIR 5 TABLE 201 REQUIREMENTS METHOD BY HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORRSION. CORROSION AT LEFT HAND WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-04 AND E.A.#: 1-5750-T0353484 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD AFT HINGE (FLAP SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORRSION. CORROSION AT LEFT HAND WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 04 AND E.A.#: 1-5750-T0353451 PART 1 STEP 1A AND STEP 1, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD AFT HINGE (FLAP SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A.#: 1-5750-149736 A PART 2 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A.#: 1-5750-162328 E PART 3 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57503745 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0353394 PART 1 STEP 3A AND STEP 3, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- RT WING OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-52-03 AND E.A.#: 1-5750-162328 E PART 3 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57503745 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. REPAIR EVALUATED AND FOUND PIVOT INBOARD LUG SURFACE REMAINING THICKNESS: 0.506" (J= LUG THICKNESS) IS CORRECT AS PER E.A.#: 1-5750-162328 E PART 3 STEP 2 FIGURE 2, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57503745 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-52-03 AND E.A.#: 1-5750-149736 A PART 2 STEP 2A AND STEP 2B, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. REPAIR EVALUATED AND FOUND PIVOT OUTBOARD LUG SURFACE REMAINING THICKNESS: 0.530" (E= LUG THICKNESS) IS CORRECT AS PER E.A.#: 1-5750-162328 E PART 3 STEP 2 FIGURE 2, TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57503745 FOR WORK DETAILS.

Part: FRAME — CHAFED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT FOUND EXISTING OUTER REPAIR ANGLE CHAFED MAIN DECK AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT , CHAFED EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-31-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . CHAFED MARKS AT EXISTING OUTER REPAIR ANGLE REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00- 2R FIGURE 205 ALLOWABLE DAMAGE .

Part: FRAME — CHAFED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 19 LEFT FOUND EXISTING OUTER REPAIR ANGLE CHAFED . MAIN DECK AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT , CHAFED EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-31-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 . CHAFED MARKS AT EXISTING OUTER REPAIR ANGLE REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00- 2R FIGURE 205 ALLOWABLE DAMAGE .

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND WITH CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.#: 1-5750-T0353342 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 495 X = -27.5 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 495 X = - 27.5 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 467 TO EXISTING SPLICE STATION 525 X = - 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND WITH CORROSION.

Part: HINGE — CRACKED (RT MLG DOOR) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND MAIN LANDING GEAR DOOR CENTER HINGE AREA FOUND CRACK AT STATION 1440. RIGHT HAND MAIN LANDING GEAR DOOR AT STATION 1440 CRACKED CENTER HINGE REMOVED AND REPLACED AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: DOUBLER — DETACHED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING TRAILING EDGE COMPARTMENT AT APPROXIMATELY STATION XW 375 FOUND FINGER DOUBLER DETACHED. REPAIR CARRIED OUT AT LEFT HAND WING TRAILING EDGE COMPARTMENT AT APPROXIMATELY STATION XW 375 FINGER DOUBLER AS PER SRM 57-50-01-2R FIGURE 202 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A.#: 1-5750-T0353342 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00338 ATTACHED E.A.#: 1-5750-T0353342 PART 1 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 615, FOUND BEADED DOUBLER CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 615 DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-08 AND E.A.#: 1-5750-T0353342 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00338 ATTACHED E.A.#: 1-5750-T0353342 PART 1 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 825 X = - 75.25 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 825 X = - 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 833 TO EXISTING SPLICE STATION 765 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION.

Part: HINGE — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND WIH CORROSION

Part: HINGE — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND WIH CORROSION

Part: HINGE — CORRODED (LT WING) · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE FOUND WITH CORROSION.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND WIH CORROSION CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.#: 1-5750-T0353347 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00280 ATTACHED E.A.#: 1-5750-T0353347 PART 1 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND WIH CORROSION CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A.#: 1- 5750-T0353347 PART 1 STEP 2B AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7- 5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE FOUND WITH CORROSION. CORROSION AT LEFT HAND WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-09 AND E.A.#: 1-5750-T0353347 PART 1 STEP 2A AND STEP 2, TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NUMBER N00280 ATTACHED E.A.#: 1-5750-T0353347 PART 1 FOR WORK DETAILS.

Part: SKIN — CRACKED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING FIXED LEADING EDGE SKIN #14 SLAT TRACK CUTOUT FOUND CRACKED AT XOS 891. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE SKIN #14 SLAT TRACK CUTOUT AT XOS 891 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

WHILE ACCOMPLISHING WORK CARD : 53.10.05.3 FOUND MAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT STATION 1250.75 - STATION 1256.75 LONGERON 26 LEFT - LONGERON 27 LEFT CRACKED. MAIN DECK L3 DOOR FORWARD JAMB LOWER WEB BOX AT STATION 1250.75 TO STATION 1256.75 LONGERON 26 LEFT TO LONGERON 27 LEFT CRACKED SKIN REPAIRED AS PER SRM 53-40-15- 2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1831 X = 27.5 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 1831 X = 27.5 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1811 TO END OF PART STATION 1887 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 775 X = 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 775 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 765 TO STATION 805 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1701 X = 27.5 FOUND CORROSION . MAIN DECK FLOOR SEAT TRACK AT STATION 1701 X = 27.5 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1671 TO STATION 1751 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

WHILE ACCOMPLISHING WORK CARD : 53.10.05.3 FOUND MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 - STA 1315 LONGERON 26 RIGHT - LONGERON 27 RIGHT CRACKED. AT MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 LONGERON 26 RIGHT TO LONGERON 27 RIGHT , CRACKED SKIN REPAIRED AS PER SRM 53-40- 15-2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 586. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT XOS 586 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 668. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT XOS 668 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,865 hrs · 15,344 cycles

RIGHT HAND WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 666. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE DOUBLER AT XOS 666 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = - 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = - 47.5 , EVALUATED DAMAGED CROWN , FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 .CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5- 63 TO EXISTING SPLICE STATION 5-0/1531 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1269 TO STATION 1311 X = - 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1269 TO STATION 1311 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 5-6 X = 47.5 ,DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5- 63 TO EXISTING SPLICE STATION 5-0/1531 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 47.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1269 TO STATION 1311 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 59,865 hrs · 15,344 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 8.5 FOUND CROWN DAMAGED . MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 8.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1269 TO STA 1311 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FMC — MALFUNCTIONED (COCKPIT) · airframe 58,202 hrs · 14,848 cycles

CONFIGURATION FOR TAKEOFF WAS FLAPS 15, ALL INDICATIONS WERE NORMAL UNTIL WE SET TAKEOFF THRUST AND GOT A VERBAL FLAP WARNING AND A WHITE FLAP BOXED WARNING ON THE NUMBER 3 DU. TAKEOFF WAS REJECTED AT 40 KNOTS. REMOVED AND REPLACED STANDARD ELECTRONIC MODULE IAW AMM 28-41-92-4 OPS CHECKED GOOD. REMOVED AND REPLACED BOTH FMC'S IAW AMM 34-63-01-4. GREEN BAND PRESENT AND ALL TAKEOFF WARNING CHECKS OPERATE NORMALLY IAW AMM 27-02-01-5.

Part: FMC — INOPERATIVE · airframe 58,202 hrs · 14,848 cycles

PDIS 623 27-01 3060 13JUN19 MEM FACT U LOGPAGES:2444704 CONFIGURATION FOR TAKEOFF WAS FLAPS 15, ALL INDICATIONS WERE NORMAL UNTIL WE SET TAKEOFF THRUST AND GOT A VERBAL FLAP WARNING AND A WHITE FLAP BOXED WARNING ON THE NUMBER 3 DU. NOTE: TAKEOFF WAS REJECTED AT 40 KNOTS. REMOVED AND REPLACED STANDARD ELECTRONIC MODULE (S.E.M) I.A.W MD-11 AMM 28-41-92-4 OPS CHECK GOOD. REQUIRES FUTHER INSPECTION. CG CALCULATED AFTER SEM UNIT CHANGED, BUT GREEN BAND STILL NOT PRESENT. REMOVED AND REPLACED BOTH FMC'S REF: MD-11 AMM 34-63-01-4. GREEN BAND PRESENT AND ALL TAKEOFF WARNING CHECKS OPERATE NORMALLY. REF: MD-11 AMM 27-02-01-5.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 55,871 hrs · 14,136 cycles

WHILE DOING DELAYED ENGINE START ON ENG 2 (2 START ALL NORMAL) NOTICED ENGINE 3 IDLING HIGHER THAN ENGINE 1. ALL OTHER INDICATIONS ON ENG 3 NORMAL (EGT,FF,ETC.). DECIDED TO SHUT NR 3 DOWN AND RESTART SHUT DOWN NR 3, WAITED UNTIL ALL INDICATIONS WERE ZERO +30 SECONDS. ATTEMPTED RESTART ON NR 3. ALL INDICATIONS NORMAL ON INITIAL START-SHORTLY AFTER F/O RAISED THE FUEL LEVER AT 20% N2, AN AIRCRAFT OVER GROUND CONTROL REPORTED SMOKE/FLAMES COMING OUT OF NR 3 ENGINE. COMPLIED WITH TAILPIPE FIRE PROCEDURES, SHUT OFF FUEL LEVER, MOTORED ENGINE. AIRCRAFT BEHIND US STILL REPORTING SMOKE, FIRED BOTH FIRE BOTTLES. REPLACED NR 3 ENGINE.

Part: SKIN — CRACKED (LT WING) · airframe 55,781 hrs · 14,100 cycles

ONE FASTENER HOLE FOUND CRACKED DURING OPEN-HOLE HFEC INSPECTION ON THE LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5.

Part: SKIN — CRACKED (RT WING) · airframe 55,781 hrs · 14,100 cycles

TWO FASTENER HOLES FOUND CRACKED, DURING OPEN-HOLE HFEC INSPECTION ON THE RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 690 AND 700. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5.

Part: DOUBLER — CRACKED (LT WING) · airframe 55,781 hrs · 14,100 cycles

LT WING BEADED DOUBLER FOUND CRACKED AT STA XOS 702 CRACKED. BEADED DOUBLER AT LT WING STA XOS 702 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,781 hrs · 14,100 cycles

RIGHT WING BEADED DOUBLER FOUND CRACKED AT XOS 766. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: REPAIR — DENTED (FUSELAGE) · airframe 55,781 hrs · 14,100 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND DENTED AT LT STA 1701 LONGERON 12L. DENTED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: DOOR FRAME — CRACKED (L3 DOORWAY) · airframe 55,781 hrs · 14,100 cycles

MAIN DECK L3 DOOR FRAME AFT LOWER FUSELAGE WEB CRACKED AT BS 1310, BETWEEN LONGERONS 26L AND 27L. WEB REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,781 hrs · 14,100 cycles

RIGHT WING BEADED DOUBLER FOUND CRACKED AT XOS 614. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 55,781 hrs · 14,100 cycles

LEFT WING FIXED LEADING EDGE LOWER PANEL CUTOUT CRACKED AT XOS 600 INBD OF FUEL PANEL HINGE DOOR. DOUBLER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB2933, REVISION AJ. INSTALLED THE NEW DOUBLER IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: REPAIR — CHAFED (FUSELAGE) · airframe 55,781 hrs · 14,100 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND EDGE CHAFED AT LT STA 535 LONGERON 24L. EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,781 hrs · 14,100 cycles

RT WING BEADED DOUBLER FOUND CRACKED AT STA XOS 769. CRACKED RT WING BEADED DOUBLER AT STA XOS 769 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,781 hrs · 14,100 cycles

CABIN MAIN DECK CARGO COMPT SEAT TRACK FLANGE CORROSION AT RT STA 1381 TO STA 1481, X= -8.5. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1 AND REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1371 TO STA 1491, X=-8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: REPAIR — CHAFED (FUSELAGE) · airframe 55,781 hrs · 14,100 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND EDGE CHAFED AT LT STA 535 LONGERON 19L. EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 55,781 hrs · 14,100 cycles

LT WING BEADED DOUBLER FOUND CRACKED AT STA XOS 693 CRACKED. LT WING BEADED DOUBLER AT STA XOS 693 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRAKE — FAILED (MLG) · airframe 55,709 hrs · 14,084 cycles

ON T/O GOT LVL 1 BRAKE DIFF TEMP ALERT. NR 1 BRAKE AT 430' F AND INCREASED TO 455' F. LOWERED GEAR AND BRAKE TEMP BEGAN DECREASE. RETRACTED GEAR AT 350'/15000FT AND BRAKE CONTINUED TO COOL DOWN. INSPECTED ALL TIRES AND BRAKES PER AMM 05-56-01-6 AND 05-51-07-6. NR 1 BRAKE DISK BROKEN AND NR 1 MAIN TIRE WORN TO 1ST CORD. REMOVED AND REPLACED NR 1 MAIN TIRE AND NR 1 BRAKE PER AMM 32-41-01-4 AND 32-43-20-4. INSPECTED NR 1 AXLE FOUND NO DAMAGE. PERFORMED OVERSPEED L/G INSPECTION PER AMM 05-51-07-6. NO DAMAGE NOTED.

Part: FIRE LOOP — DEFECTIVE (NR 3 ENGINE) · airframe 51,099 hrs · 12,794 cycles

ENGINE FIRE NR 3 INDICATION AT 10K'. COMPLIED WITH QRH, RETURNED TO LAND. T/S AND CHECKED ALL 6 ENGINE LOOPS WITH THEM DISCONNECTED AT RESPONDERS. FOUND LT CORE LOOPS CLOSEST TO THE RESISTANCE LIMIT IS THE TSM. REMOVED AND REPLACED LT CORE LOOP ASSY, A & B REF AMM 26-11-02-5 AND THEN FOUND TWO ISOLATORS BAD ON THE PYLON LOOPS, WERE TOUCHING METAL CLAMPS. REMOVED AND REPLACED ISOLATORS, ALSO FOUND TWO AIR DUCTS ON THE LT SIDE WITH TIN FOIL MISSING, TIGHTENED THE CLAMPS AND RE-FOILED REF AMM 26-11-03-4-2. OPS CK ENGINE FIRE LOOPS WAS GOOD. COMPLETED A HIGH POWER ENGINE RUN FOR 10 MINUTES AT PART POWER AND TAKEOFF WITH NO FIRE INDICATIONS OR FAULTS REF JRH.

Part: AILERON — DELAMINATED (LT WING) · airframe 50,561 hrs · 12,623 cycles

LEFT WING OTBD AILERON INBD LOWER TE FOUND DELAMINATION, STATION XOA 839 - 849. LT WING OTBD AILERON INBD LOWER TE SURFACE REPAIRED IAW SRM 57-60-80-2R PARA 4A 1A, PERMANENT REPAIR & EA 1-5750-T0325047 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,561 hrs · 12,623 cycles

RIGHT WING OTBD FLAP, INBD LOWER TE FOUND DELAMINATION, BETWEEN STATION XOFH 460 - 469. RT WING OTBD FLAP, INBD LOWER TE REPAIRED & SMOOTHEN IAW SRM 57-50-80 REPAIR 1 PARA 4A 1B. PERMANENT REPAIR & EA 1-5750-T0325048 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DENTED (LE SLAT) · airframe 50,561 hrs · 12,623 cycles

LEFT WING LE NR 8 SLAT EXTERIOR, LE SKIN FOUND WITH MULTIPLE DENTS, STATION XOS 1170. REPAIR CARRIED OUT IAW SRM 57-40-02-2R FIG 201 REPAIR 2 AT XOS 1168 - 1185. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. SRM REPAIR COMPLIED WITH. REFER WRI 57508612 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (RT WING) · airframe 50,561 hrs · 12,623 cycles

RIGHT WING FIXED LE LOWER SKIN DOUBLER FOUND CRACK AT STATION XOS 546. CRACKED DOUBLER REMOVED IAW SRM 51-31-01-0G. FABRICATED NEW DOUBLER IAW DWG ARB2933 REV AJ. INSTALLED NEW DOUBLER IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 50,561 hrs · 12,623 cycles

LEFT WING FIXED LE, LOWER SKIN DOUBLER FOUND CRACKED AT STATION XOS 546. CRACKED DOUBLER REMOVED IAW SRM 51-31-01-0G. FABRICATED NEW DOUBLER IAW DWG ARB2933 REV AJ. INSTALLED NEW DOUBLER AT LT WING FIXED LE LOWER AREA IAW SRM 51-33-01-0G. REPAIR CASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 50,561 hrs · 12,623 cycles

LEFT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 644. REPAIR CARRIED OUT AT LT WING FIXED LE EDGE INTERNAL AREA IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 50,561 hrs · 12,623 cycles

DURING INSPECTION IAW WC E 9-5730-E0317303 A P2 ON RT WING LE AT CORNER 11, FOUND TWO EACH CRACKS, LENGTH APPROX 0.39. REPAIR CARRIED OUT AT RT WING LE CORNER 11 AT XOS 610.844 IAW SRM 57-40-01-2R FIG 201 REPAIR 18. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. INITIAL INSPECTION TO BE CARRIED OUT AT NEXT C CHECK NOT EXCEEDING 24 MONTHS & REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY C CHECK NOT EXCEEDING 24 MONTHS IAW SRM 57-40-01-2R FIG 201 REPAIR 18 TABLE 204.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 50,561 hrs · 12,623 cycles

AGEING ACFT, EXISTING DOUBLER REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT AT RT STATION 775, LONGERON 12R. EXISTING DOUBLER REPAIR EVALUATED & FOUND DAMAGED. CARRIED OUT REPAIR IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. INITIAL INSPECTION REQUIRED AT 14,500 FC. REPETITIVE AT EVERY 9,500 FC IAW SRM 53-00-07-2R TABLE 201 REPAIR 2.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 50,561 hrs · 12,623 cycles

AGEING ACFT, EXISTING DOUBLER REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT, AT RT STATION 1701, LONGERON L12R. EXISTING REPAIR DOUBLER EVALUATED & FOUND DAMAGED. CARRIED OUT REPAIR IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. INITIAL INSPECTION REQUIRED AT 14,500 FC & REPETITIVE INSPECTION REQUIRED AT EVERY 9,500 FC IAW SRM 53-00-07-2R FIG 201 TABLE 201 REPAIR 2.

Part: FRAME — DENTED (FUSELAGE) · airframe 50,561 hrs · 12,623 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME DENTED AT RT STATION 1721, LONGERON 12R. REPAIRED IAW SRM 53-00-00-07-2R FIG 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES & REPETITIVE INSPECTION AT EVERY 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 50,274 hrs · 12,532 cycles

LEFT MLG, RETRACT ACTUATOR UPPER SUPPORT FITTING CORRODED. R & R IAW AMM 20-20-01-2 & CMM 57-11-01.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 50,274 hrs · 12,532 cycles

RIGHT MLG, RETRACT ACTUATOR UPPER SUPPORT FITTING CORRODED. R & R IAW CMM 57-11-01 & AMM 20-20-01-2. MINOR REPAIR.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 50,274 hrs · 12,532 cycles

LEFT MLG, RETRACT ACTUATOR UPPER SUPPORT FITTING ATTACH POINT, UPPER & LOWER BORES CORRODED. REPAIRED IAW SRM 57-20-14-2R. NO CORROSION PRESENT. MINOR REPAIR.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 50,274 hrs · 12,532 cycles

RIGHT MLG, RETRACT ACTUATOR UPPER SUPPORT FITTING ATTACH POINT, UPPER & LOWER BORES CORRODED. REPAIRED IAW SRM 57-20-14-2R. MINOR REPAIR.

Part: FITTING — CORRODED (CLG) · airframe 50,274 hrs · 12,532 cycles

CENTER LG PILLOW BLOCK RT MATTING SURFACE STRUCTURE HAS PITTING CORROSION. REMOVED CORROSION IAW SRM 53-40-14-2R. MINOR REPAIR.

Part: FITTING — GOUGED (CLG) · airframe 50,274 hrs · 12,532 cycles

CENTER LG PILLOW BLOCK, RT MATTING STRUCTURE, FWD & AFT HOLE BORES HAVE GOUGES. REMOVED GOUGES IAW SRM 53-40-14-2R. MINOR REPAIR.

Part: FITTING — CORRODED (LT MLG) · airframe 50,274 hrs · 12,532 cycles

LEFT MLG FIXED BRACE TRAPEZOID FITTING MOUNT PAD HAS PITTING ON LOWER FACE. REPAIRED IAW SRM 57-10-02-2R. MINOR REPAIR.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 50,274 hrs · 12,532 cycles

RIGHT MLG RETRACT ACTUATOR, UPPER SUPPORT FITTING, ATTACH POINT UPPER & LOWER FACE CORRODED. REMOVED CORROSION IAW SRM 57-20-14-2R, NO CORROSION PRESENT. EA 1-5720-T0323766 ACCOMPLISHED ON N00041 TO AUTHORIZE INCREASED SHIM THICKNESS. MINOR REPAIR.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 50,274 hrs · 12,532 cycles

LEFT MLG RETRACT ACTUATOR, UPPER SUPPORT FITTING, ATTACH POINT UPPER & LOWER FACE CORRODED. REMOVED CORROSION IAW SRM 57-20-14-2R. NO CORROSION PRESENT. EA 1-5720-T0323764 ACCOMPLISHED ON N00042 TO AUTHORIZE INCREASED SHIM THICKNESS. MINOR REPAIR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 483 hrs · 11,904 cycles

EMERGENCY LIGHT 1 BATTERY LOW. R & R POWER SUPPLY IAW MM 33-51-01-4-0.

Part: RING — DEFECTIVE (NR 2 ENGINE) · airframe 46,651 hrs · 11,404 cycles

DURING CLIMB OUT RECEIVED ENG 2 FADEC MAINT ALERT. FOLLOWED QRH CHECKED WITH GOC & RETURNED TO ZGGG. REMOVED AND REPLACED NR 2 ENGINE INLET TRANSITION RING PER AMM 71-11-03-4-2. PERFORMED THE ENGINE IDLE TEST PER AMM71-02-06-5-2, NO FAULT NOTED. PERFORMED THE AUTO LAND SYS R-T-S TEST FOR CAT3B PER AMM22-01-01-5, ALL PASSED. OPENED AND CLOSED THE NR 2 ENGINE COWLING DOORS PER AMM71-10-00-2-2.

Part: SUPPORT FITTING — WORN (LT WING) · airframe 45,868 hrs · 11,179 cycles

LEFT WING INBD FLAP INBD SUPPORT STRUCTURE SIX HOLE DIAMETERS FOUND EXCEEDING 0.2815 INCH. REPAIRED IAW EA1-5340-T0308226 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: SUPPORT FITTING — WORN (ZONE 600) · airframe 45,868 hrs · 11,179 cycles

RIGHT WING INBD FLAP INBD SUPPORT STRUCTURE HAS SIX HOLE DIAMETERS FOUND TO EXCEED 0.2815 INCH. REPAIRED IAW EA1-5340-T0308227 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,868 hrs · 11,179 cycles

CARGO BAY UNDER FLOOR AREA RT BS 229 FOUND CORRODED. REPAIRED AS PER EA 1-5750-T0308325 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: SKIN — CRACKED (ZONE 600) · airframe 45,868 hrs · 11,179 cycles

SKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: SKIN — CRACKED (ZONE 500) · airframe 45,868 hrs · 11,179 cycles

SKIN FOUND TO HAVE CRACK INDICATIONS DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS PANEL CUT OUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: DOUBLER — CRACKED (LT WING) · airframe 45,868 hrs · 11,179 cycles

LEFT WING FIXED LE BEADED DOUBLER AT XOS 664 FOUND CRACKED DURING OTBD SLAT DRIVE CABLE INSPECTION. REPAIRED IAW SRM 57-40-02, FIGURE 203, REPAIR 15, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,868 hrs · 11,179 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT STATION 1256, LONGERON 26R FWD R3 DOOR LOWER JAMB, FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 55 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 121

Part: RELAY — FAULTY (ANTI-ICE SYSTEM) · airframe 45,379 hrs · 10,994 cycles

LEVEL 3, ENG 2 ANTI-ICE DUCT, ALERT ON CLIMB OUT AT 5000 FT. FOLLOWED QRH PROCEDURES RETURNED TO PHNL. R&R RELAY R2-5527. HIGH POWER RUN, NO ALERT ILLUMINATED IAW FIM 30-22-05-00 & JRH.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 44,005 hrs · 10,487 cycles

ON DESCENT, LOSS OF NR 2 HYD SYS. IAW CREW DEBRIEF, FLIGHT LASTED 30 MORE MINS AFTER RECEIVING NR 2 HYD SYS FAIL ALERT. HYD FLUID ALL OVER THE TAIL UP TO THE NR 2 ENG COWL. HYD MANIFOLD FILTERS R & R AND LEAK CHECKED OK. LEAK CHECKED OF NEW SECTION OF HYD LINES CHECKED OK. OK FOR SERVICE.

Part: CONTROL PANEL — FAILED · airframe 43,287 hrs · 10,260 cycles

EMERGENCY POWER SWITCH OFF, LIGHTS INOPERATIVE. R & R AIR SYSTEM CONTROL PANEL REF AMM 24-08-02-4. EMERGENCY POWER OFF LIGHT CHECKED GOOD. PERFORMED OPERATIONAL CHECKS IAW AMM 24-08-02-5. CHECKED GOOD EXCEPT FOR SMOKE TEST. RAN ENGINES PER JRH AND PERFORMED SMOKE TEST PER AMM 24-08-02-5.ALL CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: YOKE — DAMAGED (ZONE 200) · airframe 41,230 hrs · 9,657 cycles

LEFT BS 535 LOWER SUPPORT YOKE FOUND DAMAGED. R & R IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: YOKE — DAMAGED (ZONE 200) · airframe 41,230 hrs · 9,657 cycles

LEFT BS 535 UPPER SUPPORT YOKE FOUND DAMAGED. R & R IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: ATTACH FITTING — CORRODED (FLAP HINGE) · airframe 41,230 hrs · 9,657 cycles

RIGHT WING OTBD FLAP, INBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 73. REPAIR ACCOMPLISHED IAW EA 1-5750-162327. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 63,797 hrs · 14,714 cycles

MAIN DECK CARGO TRACK AT STATION 1830, X= 8.5 LT FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,797 hrs · 14,714 cycles

MAIN DECK CARGO - SEAT TRACK AT STATION 1641, X= 8.5 LT FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 63,797 hrs · 14,714 cycles

LT WING INBD FLAP OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 73. REWORKED CARRIED OUT IAW EA 1-5750-162328. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 63,797 hrs · 14,714 cycles

RT WING OTBD FLAP SECONDARY STOP FITTING CRACKED. R & R IAW SRM 51-31-01, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.

Part: ATTACH BRACKET — CORRODED (ZONE 500) · airframe 63,797 hrs · 14,714 cycles

LEFT WING OTBD FLAP, INBD FORWARD BRACKET SIDE ATTACH LOWER HOLE SPOT FACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 73. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08, REV 73. REPAIR EVALUATED AND FOUND SIDE LOAD MATING SURFACE REMAINING THICKNESS UPPER: 0.432"; LOWER: 0.430" WITHIN MINIMUM THICKNESS: 0.3685" BASED ON DIFFERENCE BETWEEN DWG ARCC0502 AND CMM 57-44-08 REV 73, MAXIMUM REWORK LIMIT FOR BARREL NUT HOLE. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 115.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 63,797 hrs · 14,714 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS IAW CMM 57-52-03, REV 73. REWORK CARRIED OUT IAW EA 1-5750-162328. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 35,767 hrs · 8,239 cycles

CTR CARGO BAY BS 1537 LONGERON 44L FOUND LONGERON SPLICE CRACKED. CENTER CARGO COMPARTMENT STA 1537 44L LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINED FABRICATED AS PER DRAWING A5A 7116 REV. D. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: LONGERON SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,767 hrs · 8,239 cycles

CTR. CARGO BAY, STA 1537 L44R FOUND LONGERON SPLICE CORROSION. LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINED FABRICATED AS PER DRAWING A5A7114 REV J. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: FRAME — CHAFED (BS 535) · airframe 35,767 hrs · 8,239 cycles

MAIN DECK CARGO LT FUSELAGE FRAME STA 535 ADJACENT TO SAFETY YOKE UPPER AND LOWER FITTING FOUND EXISTING REPAIR DOUBLER CHAFED. MAIN DECK CARGO LT FUSELAGE FRAME STA 535 ADJACENT TO SAFETY YOKE UPPER AND LOWER FITTINGS EXISTING REPAIR DOUBLER (4EA). R & R IAW SRM 51-31-01, REV 43 AND DWG SG10530002 REV -. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 35,767 hrs · 8,239 cycles

MAIN DECK CARGO STA 5-73 TO 5-93 X=-8 SEAT TRACK BASE FOUND CRACKED. CRACKED SEAT TRACK AT STA 5-73 TO 5-93 X=-8 AREA REMOVED AS PER SRM 51-31-01 REV 43. NEW SEAT TRACK HOLES TRANSFERRED AS PER SRM 51-31-01 REV 43. REPROTECTED AS PER SRM 51-21-01 REV 43. SEAT TRACK INSTALLED AS PER SRM 51-31-01 REV 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: FRAME — DENTED (ZONE 200) · airframe 35,767 hrs · 8,239 cycles

MAIN DECK CARGO - RT STA 775 L-12 FRAME FOUND DENT. MAIN DECK RT STA 775 L12 FRAME DENT TRIMMED OFF AS PER SRM 53-00-07 REPAIR 2 FIG 201 ITEM 1 REV 43. FABRICATED REPAIR DOUBLER AS PER SRM 53-00-07 REPAIR 2 FIG 201 ITEM 1 REV 43 AND HEAT TREATED TO T6 AS PER DPS7.00-1 REV BL AND AVERAGE HARDNESS VALUE TESTED HRB 77.8 AS PER DPS1.05 REV AU. HOLES PICKED UP AS PER SRM 51-31-01 REV 43. PROTECTED AS PER SRM 51-21-01 REV 43. INSTALLED REPAIR DOUBLER AS PER SRM 53-00-07 REPAIR 2 FIG 201 ITEM 1 REV 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 35,767 hrs · 8,239 cycles

CTR CARGO BAY STA 1537 LONGERON SPLICE CRACKED. LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINE FABRICATED AS PER DRAWING A5A7116 REV D. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: FRAME — DENTED (ZONE 200) · airframe 35,767 hrs · 8,239 cycles

MAIN DECK CARGO - RT BS 1701 L12 FRAME FOUND DENT. MAIN DECK RT STA 1701 L12 FRAME DENT EXISTING DOUBLER REMOVED AS PER SRM 51-31-01 REV 43. FABRICATED NEW REPAIR DOUBLER AS PER SRM 53-00-07 REPAIR 2 FIG 201 ITEM 1 REV 43. NEW REPAIR DOUBLER HEAT TREATED TO T6 AS PER DPS7.00-1 REV BL AND AVERAGE HARDNESS VALUE TESTED HRB77.8 AS PER DPS 1.05-3 REV AU. TRANSFERRED HOLES TO NEW REPAIR DOUBLER AS PER SRM 51-31-01 REV 43. REPROTECTED AS PER SRM 51-21-01 REV 43. INSTALLED REPAIR DOUBLER AS PER SRM 53-00-07 REPAIR 2 FIG 201 ITEM 1 REV 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 35,767 hrs · 8,239 cycles

MAIN DECK CARGO STA 5-83 X-=8 SEAT TRACK BASE FOUND CRACKED. CRACKED SEAT TRACK AT STA 5-83 X= 8 AREA REMOVED AS PER SRM 51-31-01 REV 43. NEW SEAT TRACK HOLES TRANSFERRED AS PER SRM 51-31-01 REV 43. PROTECTED AS PER SRM 51-21-01 REV 43. SEAT TRACK INSTALLED AS PER SRM 51-31-01 REV 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 35,767 hrs · 8,239 cycles

CTR CARGO BAY, BS 1537 L45R FOUND LONGERON SPLICE CRACKED. LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE MACHINE FABRICATED AS PER DRAWING A5A7116 REV. D. THIS REPAIR CLASSIFIED AS PER MAJOR AS PER GMM 6-2-100 REV 110.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,767 hrs · 8,239 cycles

DURING WALK AROUND FOUND MAIN DECK FLOOR SUPPORT LOWER SURFACE FROM STA 1887 TO 2007 X=-50 CORROSION AT SEVERAL LOCATIONS. MAIN DECK FLOOR SUPPORT AT STA 1887 TO 2007 X= -50 REMOVED AND REPLACED AS PER SRM 51-31-01 REV 43. MACHINE NEW FLOOR SUPPORT AS PER DRAWING NR AGA7551 REV G. HOLES TRANSFERRED AS PER SRM 51-31-01 REV 43. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 110.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,767 hrs · 8,239 cycles

DURING WALK AROUND FOUND MAIN DECK FLOOR SUPPORT LOWER SURFACE AT STA 1887 X=25 FOUND CRACKED. MAIN DECK FLOOR SUPPORT AT STA 1887 X=25 REMOVED AND REPLACED AS PER SRM 51-31-01 REV 43. MACHINED NEW FLOOR SUPPORT AS PER DRAWING NR AGA 7081 REV. J. HOLES TRANSFERRED AS PER SRM 51-31-01 REV 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: LONGERON SPLICE — CRACKED (BS 1537 L38L) · airframe 35,767 hrs · 8,239 cycles

CTR CARGO COMPARTMENT STA 1537 LONGERON SPLICE FOUND CRACKED AT LONGERON 38L. REMOVED AND REPLACED AS PER SRM 51-33-01 REV 43. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 REV J. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 110.

Part: RIB — CRACKED (NR 16 SLAT TRACK) · airframe 35,767 hrs · 8,239 cycles

RT WING NR 16 L/E SLAT TRACK SUPPORT RIB FOUND SUSPECTED CRACK. CRACKED RIB NR 16 REMOVED AND REPLACED NEW RIB AT RH WING L/EDGE AS PER DOUGLAS DRAWING ARB7565 REV. C. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-10 REV 110. RH WING NR 8 SLAT CABLES ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-00-5 REV 66. FOUND SATISFACETORY. OPERATIONAL TEST OF THE SLAT RANGE OF MOVEMENT CARRIED OUT AS PER AMM 27-80-00-860-801 REV 66.

Part: ACTUATOR — LEAKING (ELEVATOR) · airframe 34,038 hrs · 7,864 cycles

DURING LEVEL FLIGHT, GOT LEVEL 1 ALERT "HYD 1 OFF", QUAN NR 1 2.7 & 520 PSI. TWO MINS LATER, HYD 1 QUAN LO, HYD 1R OFF & HYD PUMP 1L OFF AND "HYD 1 FAIL" ALERT. COMPLIED WITH QUH "HYD 1 OFF" AND "HYD 1 FAIL" CHECK LISTS. EXECUTED "NORMAL" LANDING AT HNL. MX TOWED TO RAMP. REMOVED AND REPLACED LEFT OTBD ELEVATOR ACTUATOR IAW MM 37-33-30-4, ACCOMPLISHED R-T-S OF BOTH FCC'S, ACCOMPLISHED AUTOLAND OPS CHECK, ACCOMPLISHED LEACK CHECK, ALL CHECKS CHECK NORMAL.

Part: SKIN — CHAFED (ZONE 600) · airframe 30,062 hrs · 6,929 cycles

RIGHT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT DOUBLER INBOARD AND OUTBOARD LOWER SECTION FOUND WITH CHAFE MARKS. REPAIR CARRIED OUT AS PER EA NR 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 500) · airframe 30,062 hrs · 6,929 cycles

LEFT WING, LEADING EDGE COMPARTMENT RIB AT XOS 1003 FOUND CRACK. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOOR — CHAFED (TELESCOPIC DUCT) · airframe 30,062 hrs · 6,929 cycles

RIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT LOWER DOOR FWD SECTION FOUND CHAFED. REMOVED AND REPLACED WITH A FABRICATED DOOR AS PER AMM 27-80-30-4. DOOR FABRICATED AS PER EA 1-5740-122550, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ATTACH BRACKET — CRACKED (BS 1259) · airframe 30,062 hrs · 6,929 cycles

MAIN DECK CABIN, 1 OFF FRAME ATTACHMENT BRACKET AT APPROX FRAME STA 1259 LONGERON 15 FOUND CRACKED. NEW FRAME ATTACHMENT BRACKET FABRICATED AS PER EA 1-5740-122552, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 30,062 hrs · 6,929 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLE D. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLE NR D AT NR 4 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 30,062 hrs · 6,929 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLE A. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLE NR A AT NR 2 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 600) · airframe 30,062 hrs · 6,929 cycles

RIGHT WING LEADING EDGE LOWER SECTION AT STA XORS 372, INBOARD OF ANTI-ICE TELESCOPIC DUCT, FOUND WITH CHAFE MARKS. CHAFE MARK SMOOTHED AND REPAIR CARRIED OUT AS PER EA 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CRACKED (MLG DOOR) · airframe 30,062 hrs · 6,929 cycles

RT MAIN LANDING GEAR DOOR UPPER SIDE SURFACE CENTER FRAME CRACKED AT 2 LOCATIONS. REPAIRED AS PER EA 1-5280-123102, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 30,062 hrs · 6,929 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE — CRACKED (RT MLG) · airframe 30,062 hrs · 6,929 cycles

RT MAIN LANDING GEAR DOOR FOUND CRACK ON CENTER HINGE. REMOVED AND REPLACED AS PER SRM 51-31-01.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 30,062 hrs · 6,929 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATION AT HOLES B, C AND D. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLES B, C AND D AT NR 1 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CHAFED (RT NR 3 SLAT) · airframe 30,062 hrs · 6,929 cycles

RIGHT WING NR 3 SLAT ASSY LOWER SECTION TRAILING EDGE FOUND WITH CHAFE MARKS. AREA REPAIRED AS PER EA 1-2780-122549, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CHAFED (RT WING) · airframe 30,062 hrs · 6,929 cycles

RIGHT WING LEADING EDGE LOWER SECTION AT APPROX STA XORS 392, OUTBOARD OF ANTI-ICE TELESCOPIC DUCT, FOUND WITH CHAFE MARKS. REPAIR CARRIED OUT AS PER EA 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 30,062 hrs · 6,929 cycles

RT WING INBOARD FLAP LOWER SKIN CENTER AREA FOUND WITH SEVERAL DENTS. TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 30,062 hrs · 6,929 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES A AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 3 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: PITOT TUBE — OBSTRUCTED · airframe 29,529 hrs · 6,807 cycles

ON TAKEOFF ROLL AIRSPEED INDICATORS DIFFERED BY 20 KNOTS REJECT T/O 04JUL08 09:12 TPE R. PERFORM PITOT TUBE PURGE ON AUX PITOT TUBE FOUND A BIG CLUNK OF MUD BLEW OUT THEN PERFORMED LEAK CHECK NORMAL PER MM 34-11-00-2.

Part: CLAMP — LOOSE (ANTI-ICE DUCT) · airframe 28,007 hrs · 6,479 cycles

NR 2 ENG ANTI ICE DUCT LIGHT, SHUT DOWN NR 2 ENG AS DIRECTED BY CHECKLIST. REMOVED AND REPLACED ENG 2 ANTI-ICE VLV LATCHING (R2-5527) IAW MD-11 SMP. REMOVED AND REPLACED NR 2 ENG COWL ANTI-ICE MANIFOLD FAILURE SENSING ALL 3 LOOPS (D1-89, D1-90, AND D1-91) IAW MD-11 MM 30-22-11-4. HOOKED UP EQUIPMENT FOR THE NR 2 ENG NOSE COWL ANTI-ICE DUCT LEAK CHECK IAW MD-11MM 30-22-09-5. LEAK CHECK C/W SMALL LEAK FOUND AT COUPLING ON DUCT GOING FROM ENGINE THROUGH FIREWALL. RETORQUED CLAMP LEAK CHECKS GOOD. REMOVED EQUIPMENT, REINSTALLED DUCTING CLOSED PANELS. REACTIVATED ANTI ICE VALVE, RAN ENGINE. OPS CHECKS GOOD.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 25,668 hrs · 5,928 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING AFT BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.

Part: STRUT — CORRODED (T/E FLAP) · airframe 25,668 hrs · 5,928 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING AFT STRUT (P/N: ARC2126) FWD AND AFT HOLE FOUND CORRODED. [SUP 05-15-07] COMPLIED WITH FEDEX E.A. 1-5750-111092.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 25,668 hrs · 5,928 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 1 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 25,668 hrs · 5,928 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORRODED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5. COMPLY WITH FEDEX EA 1-5710-111094. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 25,668 hrs · 5,928 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING INBOARD NR 2 BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 25,668 hrs · 5,928 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT SUPPORT FITTING FORWARD BOLT HOLE FOUND CORRODED. REMOVED & REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT & TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094.

Part: HINGE FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 25,668 hrs · 5,928 cycles

LT WING OUTBD FLAP INBD HINGE SUPPORT FITTING OUTBD AND 1 BOLT HOLE FOUND CORROSION. LT WING OUTBD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATIS. FEDEX EA 1-5710-111094 - WINGS, LT WING OUTBD FLAP CONVERSION FROM SR11570026-7001 TO D10-57-010-505SR HAS BEEN COMPLIED WITH. REFER TO SNRM N00732 FOR FURTHER WORK DETAILS.

Part: SKIN — DENTED (ZONE 500) · airframe 25,668 hrs · 5,928 cycles

FOUND LEFT WING, NR 3 SLAT LEADING EDGE FOUND DENT. [SUP 05-15-07] DENT ON NR 3 SLAT LEADING EDGE AT LEFT HAND WING SMOOTHENED OUT AND FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 16 VOLUME I. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-111095, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 25,668 hrs · 5,928 cycles

CRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 25,668 hrs · 5,928 cycles

RIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-09-07] CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 25,668 hrs · 5,928 cycles

CRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 25,668 hrs · 5,928 cycles

CRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 25,668 hrs · 5,928 cycles

CRACK FOUND AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 25,668 hrs · 5,928 cycles

LEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-11-07] CRACK AT LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57- 10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 25,668 hrs · 5,928 cycles

CRACK FOUND AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 25,668 hrs · 5,928 cycles

CRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — PUNCTURED (ZONE 500) · airframe 21,204 hrs · 4,940 cycles

LT WING FIXED LE FOUND PUNCTURED AT XORS 402. PUNCTUREED SKIN ON LT WING FIXED L/E AT XORS402 TRIMMED OUT AND REPAIRED AS PER SRM 57-10-00, FIG 14, VOL 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (OPEN)

Part: PANEL — SEPARATED (ZONE 500) · airframe 21,204 hrs · 4,940 cycles

LOST PANEL L WING COVERS OUTBD SLAT MECHANISM. LT WING PANEL NO.518FB REPLACED AS PER AMM 20-50-02 AND HINGE FILLERS REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK RBL 47 CRACKED AT STA 6-70. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (ZONE 100) · airframe 21,200 hrs · 4,936 cycles

RT OBSERVER SEAT CUT OUT FOUND CRACKED. CRACKED WEB AT COCKPIT FAC CARRIED OUT REPAIR AS PER SRM 53-00-01 VOLUME I, FIGURE 5 AT STA 366. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK LBL 27 CRACKED AT STA 635. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 635. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 755. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK RBL 27 CRACKED AT STA 6-80. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (NR 8 SLAT) · airframe 21,200 hrs · 4,936 cycles

RIGHT WING, NR 8 SLAT MOST OUTBOARD RIB FOUND CRACKED. SLAT REMOVED AND REPLACED AS PER AMM 27-80-30-4. ADJUSTMENT AND OPERATION CHECK CARRIED OUT FOUND SATIS AS PER AMM 27-80-00-5.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK LBL 47 CRACKED AT STA 999. CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 21,200 hrs · 4,936 cycles

CENTER CARGO COMPARTMENT, FOUND RIGHT SIDE LOWER SIDEWALL LOCATION BETWEEN STA 5-113 AND STA 1541 L38R WITH SPLICE FITTING CRACKED. REMOVED AS PER SRM 51-33- 01 VOLUME II. NEW SPLICE FITTING FABRICATED AS PER DRAWING NR A5A7114 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 21,200 hrs · 4,936 cycles

CENTER CARGO COMPARTMENT, FOUND RIGHT SIDE LOWER SIDEWALL LOCATION BETWEEN STA 5-113 AND STA 1541 L41R WITH SPLICE FITTING CRACKED. REMOVED AS PER SRM 51-33- 01 VOLUME II. NEW SPLICE FITTING FABRICATED AS PER DRAWING NR A5A7115 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,200 hrs · 4,936 cycles

MAIN DECK, SEAT TRACK RBL 47 CRACKED AT STA 999 TO STA 929 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RELAY — FAILED (ANTI ICE SYSTEM) · airframe 18,774 hrs · 4,388 cycles

ENG 2 ANTI-ICE OFF LIGHT CAME ON AT TOP OF DESCENT WITH ENG ANTI-ICE SELECTED ON. UNABLE TO DIVERT CLEAR ICING SO SHUT DOWN ENG 2 AS A PRECAUTION. REPLACED RELAY R2-5527. SYSTEM CKS OK PER FIM 30-22-07. RAN NR 2 ENG AND PERFORMED ENGINE NOSE COWL ANTI-ICE SYSTEM CHECK PER JRH, NO DEFECTS NOTED, OK FOR SERVICE.

Part: CLAMP — LOOSE (PNEUMATIC DUCT) · airframe 16,991 hrs · 3,955 cycles

ON CLIMBOUT BETWEEN 5000 FT AND 10,000 FT, NR 2 ENG ANTI-ICE DUCT LEVEL 3 ALERT ILLUMINATED. QRH PROCEDURES FOLLOWED, RETURNED TO KMEM. LEVEL 3 WARNING DISAPPEARS AFTER THROTTLES RETURNED TO IDLE POWER. EMERGENCY EQUIPMENT REQUESTED, LANDING UNEVENTFUL. FOUND TWO VERY LOSE PNEUMATIC DUCT CLAMPS UPSTREAM OF PRSOV, TIGHTENED. OPS CHECKS GOOD PER JRH.

Part: FITTING — SCRATCHED (CARGO DOOR) · airframe 16,697 hrs · 3,882 cycles

CTR CARGO - DOOR SILL BETWEEN NR 1 & NR 2 FROM FWD ROLLER GUIDE FITTING SPOOL SCRATCHED MARKS. FEDEX EA 1-5230-74188 DOOR - CENTER CARGO 104 INCHES DOOR - ALIGNMENT PIN MODIFICATION HAS BEEN COMPLIED WITH & FOUND SATISFACTORY.

Part: FITTING — WORN (NR 3 COWLING) · airframe 16,697 hrs · 3,882 cycles

NR 3 ENG NOSE COWL (FAN COWL) GUIDE FITTING LT & RT FOUND WORN. ACCOMPLISHED AS PER EA 1-7110-74316 ENGINES, ENGINE COWLING - INCORPORATION OF P&W SB 71-120.

Part: FLAP TRACK — WORN (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT I/B FLAP VANE CENTER TRACK WORN. APPLIED A LIGHT COAT OF MIL-G-81322 (MOBILE 28) GREASE TO THE LOWER SURFACE OF CENTRE VANE SUPPORT TRACK OF THE I/B FLAP LT AS PER FEDEX EA 1-5750-74226 PT1. WINGS - TE FLAPS - I/B TE FLAP VANE - CENTRE VANE SUPPORT TRACK - REPAIR.

Part: BRACKET — BROKEN (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING SUPPORT BRACKET BROKEN. RH WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING BROKEN SUPPORT BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 VOL2.

Part: BRACKET — CRACKED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT SUPPORT FOUND CRACKED. LT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT CRACKED SUPPORT REMOVED & FABRICATED AS PER DRWG ARC4230 (REF EARN 46) & INSTALLED AS PER AMM 20-50-02.

Part: BRACKET — CRACKED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT WING O/B FLAP I/B HINGE AFT FAIRING (FLAP SIDE) AFT SUPPORT BRACKET FOUND CRACKED. RT WING O/B FLAP I/B HINGE AFT FAIRING - CRACKED AFT SUPPORT BRACKET REMOVED. FABRICATED AS PER DRWG ARC4230 (REF EARN 047) & INSTALLED AS PER AMM 20-50-02.

Part: FRAME — CHAFED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

AFT TAIL CONE LT FWD FRAME FOUND WITH CHAFED MARK. AFT TAIL CONE LT FWD FRAME REMOVED & REPLACED AS PER SRM 513101 V2.

Part: FRAME — CHAFED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

FWD TAIL CONE AFT LT FRAME FOUND CHAFED MARK. FWD TAIL CONE AFT LH FRAME REPAIR CARRIED OUT AS PER SRM 53-00-01 FIG 9 VOL1.

Part: FAIRING — CRACKED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT WING O/B FLAP I/B HINGE FAIRING FOUND O/B BRACKET CRACKED. LT WING O/B FLAP I/B HINGE FAIRING FWD OUTER CRACKED BRACKET REMOVED, FABRICATED, AS PER DRWG ARC7717 & COMPLIED AS PER EA 1-5750-74228. TE FLAP O/B TE FLAP AFT HINGE BRACKET AERODYNAMIC FAIRINGS FWD SUPPORT BRACKET. FABRICATION, AND INSTALLED AS PER SRM 51-31-01 VOL 2.

Part: FRAME — SCRATCHED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

FWD CABIN RT FRAME SCRATCHED AT STA 695 BETWEEN STR 12 & 13. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229.

Part: FRAME — DENTED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13. CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

FWD CABIN SEAT TRACK CORRODED FROM STA 459 TO 495 -X27.5. FWD CABIN SEAT TRACK CORRODED FROM STA 459 TO 495 -X27.5 CARRIED OUT SECTIONAL REPLACED FROM STA 450 TO 525 -X27.5 AS PER MD11 SRM 53-70-00 FIG1 V1, PERFORMED NDT INSPECTION ON TRIMMED AREA CRACK FREE CONDITION.

Part: FRAME — DENTED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

CABIN LEFT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13. CABIN LT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229.

Part: FRAME — DENTED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

FUSELAGE FRAME DENTED AT STA 5-93 BETWEEN STR 12 & 13. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENTS PER SRM - DTA, EA 1-5310-74229.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

CORROSION ON CABIN SEAT TRACK AT X27.5 STA 459 TO 480. CORROSION ON CABIN SEAT TRACK AT X27.5 STA 459 TO 480 SECTIONAL REPLACED FROM STA 450 TO STA 525 AS PER MD11 SRM 53-70-00 FIG1 VOL1.

Part: FRAME — DENTED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

CABIN G-NET YOKE ASSY ATTACHMENT AT LT SIDE STA 535 DENTED AT UPPER & LOWER LOCATION. CABIN G-NET YOKE ASSY ATTACHMENT AT LT SIDE STA 535 DENTED AT BOTH UPPER & LOWER LOCATION REPAIR CARRIED OUT AS PER DWG NR SRZ-53-503 & PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION .

Part: FRAME — DENTED (ZONE 200) · airframe 16,697 hrs · 3,882 cycles

CABIN LT SIDEWALL FRAME DENTED AT STA 1681 BETWEEN STR 12 & 13. CABIN LT SIDEWALL FRAME DENTED AT STA 1681 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM. DTA, EA 1-5310-74229.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT O/B FLAP O/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP O/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75245 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORRODED. LT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. WINGS - RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT O/B FLAP I/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP I/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT I/B FLAP O/B HINGE O/B STRAP PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE O/B STRAP PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED.

Part: TRACK — CHAFED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B FITTING AND SKIN. LT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B - CHAFE MARK AT I/B & O/B SKIN EDGE TRIMMED 0.080 AS PER SRM 51-21-01 VOL 2 WITHIN LIMIT AS PER SRM 57-00-01 FIG 1A VOL 1 & CHAFE MARK AT FITTING EDGE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-74313 WING - LH LE I/B FLAP VANE SUPPORT - RIB CHAFFED, HFEC CARRIED OUT AT REWORKED AREA & FOUND NO CRACK EVIDENT.

Part: HINGE — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT O/B FLAP I/B HINGE I/B PIVOT HOLE AND LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LH O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 16,697 hrs · 3,882 cycles

LEFT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT I/B FLAP O/B HINGE (FLAP SIDE) O/B STRAP PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (O/B STRAP PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS.

Part: FITTING — CHAFED (ZONE 800) · airframe 16,697 hrs · 3,882 cycles

CTR CARGO - DOOR BETWEEN NR 1 & 2 LATCH FROM FWD GUIDE FITTING CHAFING. FEDEX EA 1-5230-74188 HAS BEEN COMPLIED WITH & FOUND SATISFACTORY.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT I/B FLAP O/B HINGE (FLAP SIDE) I/B STRAP PIVOT HOLE CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREA (STRAP PIVOT HOLE) EXCEED CMM 57-52-03 LIMITATION. R & R WITH NEW HINGE ASSY AS PER DRAWING NRC6060. REF SNRM N0763 FOR JOB DETAILS.

Part: HINGE — CRACKED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT I/B FLAP O/B HINGE FWD UPPER ATTACH FITTING FOUND CRACKED. RT I/B FLAP O/B AFT HINGE ASSY REMOVED & REPLACED AS PER DRAWING NR NRC6060.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS.

Part: HINGE — CORRODED (ZONE 600) · airframe 16,697 hrs · 3,882 cycles

RIGHT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (O/B PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS.

Part: DUCT — FAILED (NR 2 ENGINE) · airframe 11,817 hrs · 2,655 cycles

RECEIVED ENG 2-ICE OFF ALERT, CONSEQUENCE ENG 2A-ICE DUCT FAILED. SHUT DOWN NR 2 ENG IN FLIGHT.

Part: RHEOSTAT — FAULTY (COCKPIT) · airframe 1,412 hrs · 15 cycles

AT CR SMELLED HOT INSULATION ODOR. DISCOVERED POPPED C/B FOR OVERHEAD SWITCH PANEL. MX FOUND OVERHEAD LIGHT RHEOSTAT TRANSFORMER TO BE PRIMARY CAUSE OF ODOR.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 4,363 hrs · 935 cycles

MAIN DECK COMP SEAT TRACK AT BS 635, LBL 3.5 FOUND WITH CRACK APPROX 4 INCHES LONG. * S/D* REMOVED AND REPLACED PER SRM 53-70-00 FIG 1 VOL I.

Part: CONTROL WHEEL — POPPING (LT COCKPIT)

CAPT'S CONTROL WHEEL HAS POPPING SOUND WITH FWD AND AFT MOVEMENT OF CONTROL WHEEL, WITH NO BINDING. REPAIRED IAW EA 1-2700-46588B.