N585FE

Part: CONTROL PANEL — SHORTED (APU FIRE DETECT) · airframe 93,883 hrs · 21,827 cycles

DESCENDING THROUGH 15,000 FEET ON ARRIVAL INTO MEMPHIS LEVEL THREE APU FIRE MESSAGE. FOLLOWED QRH, PULLED APU AGENT DISCHARGE HANDLE, DISPENSING BOTH FIRE BOTTLES IN ACCORDANCE WITH CHECKLIST. APU FIRE MESSAGE STAYED ON. DECLARED AN EMERGENCY WITH ATC AND SPOKE WITH CFR ON RWY 27 AFTER LANDING. NEVER HAD ANY INDICATION OF SMOKE OR FUMES AND CFR HAD NO INDICATION THAT THERE WAS A FIRE IN THE TAILCONE AREA. EMERGENCY DECLARED, FOUND APU FIRE WARNING LIGHTS L2-130 ON APU GROUND CONTROL PANEL SHORTED TO GROUND AND REPLACED L2-130 IAW 26-21-10-4 AND SWPM AND WDM 26-12-01 PAGE 4 SHEET 1. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 93,525 hrs · 21,719 cycles

EMERGENCY EXIT SIGN ABOVE R1 DOOR INOP. RELAMPED-NO HELP. REMOVED AND REPLACED POWER SUPPLY NO JOY. IN REF. TO AMM 33-51-01-4 REMAINS ON MEL FACT 07OCT22 08:47 ANC U REPAIRED BROKEN WIRE B370-17-20 IN REF TO SWPM 20-10-03. EMERGENCY LIGHTS OP TEST GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 93,525 hrs · 21,719 cycles

EMERGENCY EXIT SIGN ABOVE R1 DOOR INOP. RELAMPED-NO HELP. REMOVED AND REPLACED POWER SUPPLY, NO FIX. IAW AMM 33-51-01-4 REMAINS ON MEL. REPAIRED A BROKEN WIRE B370-17-20 IAW SWPM 20-10-03. EMERGENCY LIGHTS OP TEST GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG TIRE) · airframe 93,227 hrs · 21,633 cycles

PDIS 585 32-41 1079 27AUG22 ANC OPEN U TIRE PRESSURE LO IN CRUISE. CONTINUAL DECREASE IN PRESSURE LEFT NOSE TIRE. LOW OF 83 PSI AT LANDING. TIRE PRESS DIFF ALERT ON ROLLOUT. INSPECTION OF TIRE INDICATED NORMAL. ***EMERGENCY DECLARED*** FACT 27AUG22 13:32 ANC REMOVED AND REPLACED LH NOSE TIRE REF AMM 32-42-010-4 VERIFIED TIRE PRESS INDICATION. OK FOR SVC 8/29/2022

Part: TIRE — LEAKING (NLG LEFT) · airframe 93,227 hrs · 21,633 cycles

PDIS 585 32-41 1079 27AUG22 ANC FACT U TIRE PRESSURE LO IN CRUISE. CONTINUAL DECREASE IN PRESSURE LEFT NOSE TIRE. LOW OF 83 PSI AT LANDING. TIRE PRESS DIFF ALERT ON ROLLOUT. INSPECTION OF TIRE INDICATED NORMAL. ***EMERGENCY DECLARED*** R/I 27AUG22 13:32 ANC U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: ACG7453-1 POS: 1 SRL: FEB91-0345 ON MPN: ACG7453-1 CPN: 3210443 SRL: NOV90-0316 TAG NBR: 97G961 FACT 27AUG22 13:32 ANC U REMOVED AND REPLACED LH NOSE TIRE REF AMM 32-42-010-4 VERIFIED TIRE PRESS INDICATION. OK FOR SVC

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 93,214 hrs · 21,630 cycles

DURING HIGH FREQUENCY EDDY CURRENT ON LEFT HAND OVERWING FLOOR BEAM AND THE UPPER AND LOWER FLANGES AT X = 90 TO X = 116 STATION Y = 1305, FOUND 02 EACH CRACK AT UPPER FLANGE 2ND FASTENER FROM INBOARD NEAR X = 116 AFT SIDE APPROXIMATELY CRACK 1.3Ï¿½ AND FORWARD SIDE APPROXIMATELY 2.0Ï¿½ LENGTH. LEFT HAND OVER WING FLOOR BEAM AT STATION Y = 1305 BETWEEN X = 90 TO X = 116 02 EACH CRACK AT UPPER FLANGE 2ND FASTENER FROM INBOARD NEAR X = 116 REPAIR CARRIED OUT AS PER EA: #1-5310-T0369942 PART 1 TITLE: FUSELAGE Ï¿½ MAINFRAME Ï¿½ MAIN DECK CARGO OVERWING FLOOR BEAM AT STA1305.250 CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (RT NR 6 SLAT) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ NUMBER 6 SLAT INNER RIB AT STATION XOS 863.325 FOUND CRACK AFTER SKIN REMOVAL. RIGHT WING NUMBER 6 SLAT INNER RIB AT STATION XOS 863.325 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1828 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 93,214 hrs · 21,630 cycles

LOWER AFT CARGO COMPARTMENT STATION 1841, X 32 TO X-30 FLOOR SUPPORT FOUND WITH CORROSION. CORROSION AT LOWER AFT CARGO COMPARTMENT STATION 1841, X 32 TO X-30 FLOOR SUPPORT REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53-00-00- 2R REPAIR GENERAL FIGURE 206. CORRODED SUPPORT REMOVED AS PER SRM 51-31-01-OG. SUPPORT REWORKED AS PER DOUGLAS DRAWING: AGA 7170 REVISION R AND INSTALLED AT LOWER AFT CARGO COMPARTMENT STATION 1841 X 60 TO X Ï¿½ 60 AS PER SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (RT NR6 SLAT) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ NUMBER 6 SLAT INNER RIB AT STATION XOS 868.476 FOUND CRACK AFTER SKIN REMOVAL. RIGHT WING NUMBER 6 SLAT INNER RIB AT STATION XOS 868.476 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB 1828 REVISION B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 500) · airframe 93,214 hrs · 21,630 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD TRAILING EDGE BETWEEN XIFH 247.32 AND XIFH 251.32 EXISITING REPAIR DOUBLER UNABLE TO COMPLY WITH E.A. # : 1-5750-T0357767 B P2 WORK STEP 1. LEFT HAND WING INBOARD FLAP OUTBOARD TRAILING EDGE BETWEEN XIFH 247.32 AND XIFH 251.32 EXISITING REPAIR DOUBLER REMOVED AS PER SRM 51-35-02-OG AND CARRIED OUT REPAIR AS PER EA # 1-5750-T0357767 C PART 2 TITLE: WINGS Ï¿½ FLIGHT SURFACES Ï¿½ LH WING Ï¿½ INBD FLAP ASSY Ï¿½ AFT SEGMENT LOWER SKIN DAMAGE AT XIFH 249.500 Ï¿½ RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57500585 FOR WORK DETAILS.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 93,214 hrs · 21,630 cycles

CABIN - STATION 508, X = 8.5 SEAT TRACK CROWN FOUND DAMAGE. CABIN - AT SEAT TRACK STATION 508 X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED 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 465 TO STATION 525 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 93,214 hrs · 21,630 cycles

CABIN - STATION 508, X = 27.5 SEAT TRACK CROWN FOUND DAMAGED. CABIN - AT SEAT TRACK STATION 508 , X = 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED 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 465 TO STATION 525 , X = 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (FWD CARGO) · airframe 93,214 hrs · 21,630 cycles

LOWER FORWARD CARGO COMPARTMENT BILGE UNDER FLOOR STATION 6-55, LONGERON 48 RIGHT HAND FOUND WITH CORROSION. CORROSION AT LOWER FORWARD CARGO COMPARTMENT BILGE UNDER FLOOR STATION 6-55, LONGERON 48 RIGHT HAND REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R REPAIR GENERAL FIGURE 205. SECTIONAL REPAIR CARRIED OUT AT LOWER FORWARD CARGO COMPARTMENT BILGE UNDER FLOOR FROM STATION 6-40 TO STATION 6-60 EXISTING SPLICE LONGERON 48 RIGHT HAND AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (RT WING) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING - NUMBER 6 SLAT INNER RIB AT STATION XOS 858.175 FOUND CRACK. RIGHT WING NUMBER 6 SLAT AT STATION XOS 858.175 CRACKED INNER RIB REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB FABRICATED AS PER DOUGLAS DRAWING ARB1827 REVISION C. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 93,214 hrs · 21,630 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 545 FOUND CRACK. LEFT WING FIXED LEADING EDGE AT STATION XOS 545 CRACKED BEADED DOUBLER 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 500) · airframe 93,214 hrs · 21,630 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK. LEFT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CORRODED (AFT CARGO) · corrosion level 2 · airframe 93,214 hrs · 21,630 cycles

LOWER AFT CARGO COMPARTMENT STATION 1923 X 29.31 SEAT TRACK FOUND WITH SURFACE CORROSION. CORROSION AT LOWER AFT CARGO COMPARTMENT STATION 1923 X 30 SEAT TRACK REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER ALLOWABLE DAMAGE 1 FIGURE 101. CORRODED SEAT TRACK REMOVED AS PER AMM 20-50-02. TRACK REWORKED AS PER DOULAS DRAWING: AGA7191 REVISION C AND INSTALLED AT LOWER AFT CARGO COMPARTMENT STATION 1921 TO STATION 1959, X 29.31 AS PER AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CHAFED (ZONE 600) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE FORWARD SURFACE REPAIR DOUBLER AT STATION XOS 767 FOUND CHAFFED. RIGHT WING FIXED LEADING EDGE FORWARD SURFACE AT STATION XOS 767 CHAFFED REPAIR DOUBLER REMOVED AS PER SRM 51-31-01-OG AND CARRIED OUT REPAIR AS PER SRM 57-40-02- 2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK. RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 93,214 hrs · 21,630 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. LEFT WING FIXED LEADING EDGE AT STATION XOS 655 CRACKED BEADED DOUBLER 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 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 711 FOUND CRACK. RIGHT WING FIXED LEADING EDGE AT STATION XOS 711 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 500) · airframe 93,214 hrs · 21,630 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE UPPER FORMER FOUND CRACK AT STATION XOS 584. LEFT WING FIXED LEADING EDGE AT STATION XOS 584 CRACKED UPPER FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 93,214 hrs · 21,630 cycles

CABIN Ï¿½ STATION 1249, X = - 27.5 SEAT TRACK CROWN FOUND DAMAGED. CABIN - AT SEAT TRACK STATION 1249 , X = - 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED 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 1229 TO STATION 1269 , X = - 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 600) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE LOWER STIFFENER FOUND CRACK AT STATION XOS 542. RIGHT WING FIXED LEADING EDGE LOWER CRACKED STIFFENER AT STATION XOS 542 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB2918 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 600) · airframe 93,214 hrs · 21,630 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE UPPER FORMER FOUND CRACK AT STATION XOS 584. RIGHT WING FIXED LEADING EDGE AT STATION XOS 584 CRACKED UPPER FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISION H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 100) · airframe 93,214 hrs · 21,630 cycles

DURING HIGH FRIQUENCY EDDY CURRENT SURFACE INSPECTION ON THE RIGHT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATELY 0.2Ï¿½. RIGHT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA CRACK AT STATION Y = 595 REPAIR CARRIED OUT AS PER MD-11 SRM 53-10-14-2R FIGURE 202 REPAIR 2. REPETITIVE INSPECTION REQUIREMENT INITIAL INSPECTION AT 1500 FLIGHT CYCLE, REPETITIVE AT 1500 FLIGHT CYCLE METHOD: HIGH FREQUENCY EDDY CURRENT (NDT SPM) PART 6. PER SRM 53-10-14-2R TABLE 201 / FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 93,214 hrs · 21,630 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER FOUND CRACK AT STATION XOS 667. LEFT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 667 REMOVED AND REPLACED AS PER SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (LT MLG) · airframe 93,214 hrs · 21,630 cycles

DURING HIGH FRIQUENCY EDDY CURRENT SURFACE INSPECTION ON THE LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACKS WITH LENGTH APPROXIMATELY 0.4Ï¿½.

Part: SWITCH — FAILED (N/A) · airframe 92,064 hrs · 21,312 cycles

PDIS 585 52-30 0345 02FEB22 IUD OPEN U AIR TURN BACK AFTER TAKEOFF FROM OTBH. MAIN CARGO VENT DOOR OPEN, NO ALERTS. DUMPED APPROXIMATELY 58K BEFORE LANDING. INSPECT VENT DOOR. PART 02FEB22 04:51 MC1 U IDENTIFIED PARTS SWITCH 27/32/52 MPN: H20-24B CPN: 0030004 QTY: 1 MEL 02FEB22 05:01 IUD U RELEASED FOR SERVICE PER MEL : 52-40-01-06 CATEGORY : B EXPIRATION : 05FEB22 "MEL 52-40-01-06: CARGO DOOR UPR A ALERT - INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TOBLOCK-OUT." MAIN CARGO DOOR "A" INDICATION INOP C/7303873 FACT 03FEB22 11:38 MEM RESTORED AIRCRAFT TO NORMAL CONFIGURATION PER MEL 52-40-01-06 .REPLACED MAIN CARGO DOOR VENT PROX IMITY SWITCH PER AMM MD-11 AMM 52-70-00-5. PERFORMED OPERATIONAL TEST PER AMM 52-70-00-5. OPS CHECK GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 91,095 hrs · 21,003 cycles

EMERGENCY LIGHT TEST FAIL DURING PREFLIGHT WITH EMER LT BATT 1 LO (LEVEL 1 ALERT). PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM REF AMM 33-50-00-5. NO FURTHER FAULTS FOUND.OPS CHECK GOOD AT THIS TIME.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1- 5750- T0338727 B PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507899 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1- 5750- T0338727 B PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507899 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1- 5750- T0338727 B PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507899 FOR WORK DETAILS.

Part: LUG — CORRODED (FLAP ACTUATOR) · airframe 88,429 hrs · 20,269 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1- 5750- T0338726 B PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507937 FOR WORK DETAILS.

Part: LUG — CORRODED (TE FLAP ACTUATOR) · airframe 88,429 hrs · 20,269 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1- 5750- T0338726 B PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507937 FOR WORK DETAILS.

Part: BEAM — CRACKED (L3 DOOR) · airframe 88,429 hrs · 20,269 cycles

CABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR NUMBER 1 (UPPER) BEAM AFT DOOR STOP NUMBER 1 FOUND CRACKED AT STATION 838.330, Z=51.367. CABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR NUMBER 1 (UPPER) BEAM AFT DOOR STOP NUMBER 1 STATION 838.330, Z=51.367. REMOVED AND REPLACED, AS PER MD-11 SRM 51- 31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 88,429 hrs · 20,269 cycles

CABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR NR 1 (UPPER) BEAM AFT DOOR STOP NR1 FOUND CRACKED AT STATION 838.330 , Z= - 51.367. CABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR NR 1 (UPPER) BEAM AFT DOOR STOP NR 1 STATION 838.330, Z= -51.367. REMOVED AND REPLACED PER MD-11 SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — OUT OF LIMITS (CARGO DOOR) · airframe 88,429 hrs · 20,269 cycles

MAIN DECK - UPPER CARGO DOOR SIDE FORWARD HINGES ( PART NUMBER ACA 7332-1) FOUND 8 LOBES OUT OF LIMITS. MAIN DECK, UPPER CARGO DOOR SIDE FORWARD HINGES (P/N ACA 7332-1) 9 LOBES, REWORKED AS PER MD-11 SRM 51-21-01-0G. REPAIR BUSHINGS (09EA) FABRICATED BY MACHINING AND INSPECTED, AS PER MD-11 CMM 52-34-04 AND EA NR 1-5230-162590 A PART 2 STEPS 2 AND 5. TITLE: DOORS-CARGO DOORS-MAIN DECK CARGO DOOR FORWARD HINGE LOBES ELONGATED: STA 636. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 88,429 hrs · 20,269 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN DAMAGED AT BS 755 , LBL 27.5. DAMAGE REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-00-52-1A. FIGURE 101. ALLOWABLE DAMAGE 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: VANE — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LEFT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE WAS FOUND CORRODED.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND E.A. NR 1-5750-T0355814 PART 1 STEP 1 A. 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: SUPPORT — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND E.A. NR 1-5750-T0355814 PART 1 STEP 1 B. 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. REFER TO SNRM N00665 ATTACHED E.A. NR 1- 5750- T0355814 PART 1 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

LT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND E.A. NR 1-5750 T0355812 PART 1 STEP 2 A. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LT 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: SUPPORT FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

LT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5 AND E.A. NR 1-5750-T0355812 PART 1 STEP 2 B. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LT WING-OUTBD FLAP VANE ASSY-TRACK SUPPORT CORROSION REPAIR. OVERSIZED ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4, REFER TO SNRM N00661 ATTACHED E.A. NR 1- 5750- T0355812 PART 1 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.

Part: FLOORBEAM — CORRODED (BS 420) · airframe 88,429 hrs · 20,269 cycles

UPON REMOVAL OF LAVATORY MODULE IN THE CABIN, RIGHT. BS 420, X -20 - X -27, THE FLOORBEAM STRUCTURE WAS FOUND CORRODED. FLOOR SUPPORT REMOVE AND REPLACED BY FABRICATION PER DOUGLAS DRAWING # WSP0668 REVISION 'B' AND INSTALLED PER MD - 11 AMM 20-50-02 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (MAIN DECK CARGO) · airframe 88,429 hrs · 20,269 cycles

FOWARD CABIN MAIN DECK CARGO FLOOR PANEL EDGE FOUND CORRODED BETWEEN 475 - 503 ,X = -28 TO X = -35. REMOVE AND REPLACED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR , PER GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (MAIN DECK CARGO) · airframe 88,429 hrs · 20,269 cycles

FORWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORROSION AT BS 475 - 503 , X -74.5 TO X -94. REMOVE AND REPLACED AS PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (MAIN DECK CARGO) · airframe 88,429 hrs · 20,269 cycles

FORWARD MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND WITH CORROSION AT RIGHT, BS 475 - 503 ,X -37 TO X -46.5. REMOVED AND REPLACED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (MAIN DECK CARGO) · airframe 88,429 hrs · 20,269 cycles

FORWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORRODED AT LEFT, BS 475 -503 , X 1 TO X 8. REMOVE AND REPLACED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — CORRODED (MAIN DECK CARGO) · airframe 88,429 hrs · 20,269 cycles

FORWARD MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND WITH CORROSION AT LEFT BS 475 - 503 , X 19.5 TO X 26.5. REMOVE AND REPLACED AS PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION.

Part: BRACKET — CORRODED (RT FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE. REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND UPPER BARREL NUT FACE EXCEEDS LIMIT BASED THE DIFFERENCE BETWEEN DRAWING LIMITS AND CMM MAXIMUM. REWORK LIMITS FOR BARREL NUT HOLE. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-08 AND E.A. NR 1-5750-T0355552 PART 1 STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING- OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NO. N00427 ATTACHED E.A. NR 1-5750-T0355552 PART 1 FOR WORK DETAILS.

Part: STOP FITTING — CRACKED (R3 DOOR FRAME) · airframe 88,429 hrs · 20,269 cycles

MAIN DECK CARGO COMPARTMENT R3 DOOR, NR 5 BEAM, FORWARD DOOR STOP NR 5 WAS FOUND CRACKED.

Part: BEAM — CRACKED (BS 794) · airframe 88,429 hrs · 20,269 cycles

CABIN - MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR # 5 BEAM FORWARD DOOR STOP # 5 FOUND CRACKED . AT STATION 793.670 , Z = -9.702 . CABIN - MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR # 5 BEAM FOWARD DOOR STOP # 5 , AT STATION 793.670 , Z = -9.702 . REMOVE AND REPLACED BY FABRICATION PER DOUGLAS DRAWING # ADA3752 . REVISION ' E ' AND FEDEX E.A. # 1-5230-T0355710. P1 . TITTLE : DOORS - CARGO DOOR - ALTERNATE MATERIAL FABRICATION FOR MAIN DECK PASSENGER DOOR 3 RIGHT - STOP # 5 BEAM . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LEFT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # 1- 5750- T0338726 B PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507937 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORRODED. 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 DATA FOR THE PIVOT BORE SHOWN IN FIGURE 2 IS CORRECT AS PER E.A. # 1- 5750- T0338727 B PART 1 STEP 1 E, TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI :57507899 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS. 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. NR 1-5750-T0322886 C PART 3 STEP 2. TITLE: WINGS-FLIGHT SURFACES-FLIGHT SURFACES-LT 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: 57507967 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.

Part: FUEL TANK — CORRODED (CENTER) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

MAIN DECK CENTER WING TANK AT S-13, BETWEEN XCW = - 104 AND XCW = -110 AREA FOUND CORROSION. MAIN DECK CENTER WING TANK AT STRINGER - 13, BETWEEN XCW = -104 AND XCW = - 110. REPAIR CARRIED OUT PER FEDEX E.A. # 1-5730-T0355693 P1. TITTLE :- WINGS - PLATES AND SKINS - CORROSION FOUND ON CENTER WING UPPER CENTER SKIN PANEL AT STRINGER -13, BETWEEN XCW = - 104 AND XCW = - 110. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - FIXED LEADING EDGE AT STATION XOS 1191 FOUND CRACK AS MARKED . RIGHT WING - FIXED LEADING EDGE AT STATION XOS 1191 SKIN REPAIR CARRIED OUT AS PER MD - 11 SRM 57-40-01-2R, FIGURE 201, REPAIR 16 . REPAIR CLASSIFIED AS MAJOR PER GMM 6 - 2 - 100 .

Part: FUEL TANK — CORRODED (CENTER) · airframe 88,429 hrs · 20,269 cycles

MAIN DECK - CENTER WING TANK AT STATION 1244 X= - 105 AREA FOUND CORROSION.

Part: BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

LT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE). REWORKED AND FOUND EXCEEDS 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. NR 1-5750-T0322886 C PART 3 STEP 2. TITLE: WINGS-FLIGHT SURFACES-FLIGHT SURFACES-LT 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: 57507967 FOR WORK DETAILS.

Part: FLOOR PANEL — CORRODED (MAIN DECK) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

FOWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORROSION AT STATION 475 TO STA 503 , BETWEEN X = 37 TO 46.5 . FORWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL AT STATION 475 - STATION 503, BETWEEN X = 37 TO X = 46.5 , CORROSION BLENDED OUT PER EA 1-5321-T0355727 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - FIXED LEADING EDGE AT STATION XOS 1191 FOUND CRACKED.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE). REWORKED AND FOUND EXCEEDS 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. NR 1-5750-T0322914 C PART 3 STEP 2A AND STEP 2. TITLE: WINGS-FLIGHT SURFACES-RT 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: 57507893 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING FLAP) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE). REWORKED AND FOUND EXCEEDS 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. NR 1-5750-T0322914 C PART 3 STEP 2A AND STEP 2. TITLE: WINGS-FLIGHT SURFACES-RT 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: 57507893 FOR WORK DETAILS.

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 88,429 hrs · 20,269 cycles

FOWARD CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL EDGE FOUND CORROSION AT STATION 475 TO STA 503 , BETWEEN X = 37 TO 46.5 .

Part: DOUBLER — CRACKED (LT WING LE) · airframe 88,429 hrs · 20,269 cycles

LEFT WING - FIXED LEADING EDGE CAVITY BEADED DOUBLER BETWEEN XFS 990 - XFS 1005 , NEAR SLAT #7 OUTBOARD TRACK FOUND CRACK AS MARK . LEFT WING - FIXED LEADING EDGE CAVITY BEADED DOUBLER BETWEEN XFS 990 - XFS 1005 , NEAR SLAT #7 OUTBOARD TRACK REPAIR CARRIED OUT AS PER MD - 11 SRM 57-40-02-2R . FIGURE 203 . REPAIR 15 . REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100 .

Part: FRAME — DENTED (BS 1721) · airframe 88,429 hrs · 20,269 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND DENTED AT LEFT STATION 1721 , LONGERON 12 L . REPAIR CARRIED OUT PER MD - 11 SRM 53-00-07-2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - UPPER WING SURFACE FOUND CORROSION AT XORS 355 . REPAIR CARRIED OUT, AS PER FEDEX E.A. NR 1-5730-T0355660, P1. TITTLE:WINGS-PLATES AND SKINS-CORROSION BLENDOUT REPAIRS ON RT OUTER WING, UPPER AFT SKIN PANEL, XORS 345-385 STRINGER 1 TO 4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - UPPER WING SURFACE FOUND CORROSION AT XORS 323, STRINGER 1R. REPAIR CARRIED OUT AS PER FEDEX E.A. # 1-5730-T0355660. P1 . TITTLE : WINGS - PLATES AND SKINS - CORROSION BLENDOUT REPAIRS ON RIGHT OUTER WING , UPPER AFT SKIN PANEL , XORS 345 - 385. STRINGER 1 TO 4 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1661) · airframe 88,429 hrs · 20,269 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR FOUND DENTED AT LEFT STATION 1661 , LONGERON 12 L . REPAIR CARRIED OUT PER MD - 11 SRM 53-00-07 -2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1321) · airframe 88,429 hrs · 20,269 cycles

MAIN DECK - SEAT TRACK AT STATION 1321 X = - 107.25 FOUND DAMAGED. REPAIR CARRIED OUT PER MD-11 SRM 53-00-52-2R . REPAIR 3 . FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SKIN — CORRODED (RT WING) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - UPPER WING SURFACE FOUND CORROSION AT XORS 327, STRINGER 4R. REPAIR CARRIED OUT AS PER FEDEX E.A. # 1-5730-T0355660. P1 . TITTLE : WINGS - PLATES AND SKINS - CORROSION BLENDOUT REPAIRS ON RIGHT OUTER WING , UPPER AFT SKIN PANEL , XORS 345 - 385. STRINGER 1 TO 4 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE FOUND CORROSIONS. CORROSIONS AT LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. REPAIR. EVALUATED AND FOUND DIMENSIONS SHOWN IN FIGURE 1 ARE CORRECT AS PER E.A. # 1-5750-T0355621 PART 1 STEP 2; TITLE: WINGS-FLIGHT SURFACES- EO 1-5750-7-5002-LT WING OUTBD FLAP, INBD AFT HINGE (FLAP SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NO. N00582 ATTACHED E.A. NR 1-5750-T0355621 PART 1 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT 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. NR 1-5750-T0355621 PART 1 STEP 2B AND STEP 2; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LT WING OUTBD FLAP, INBD AFT HINGE (FLAP SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · airframe 88,429 hrs · 20,269 cycles

LELEFT WING - UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER SUSPECTED CORROSION NEAR INBOARD EDGE . STA XW 212.2972. LEFT HAND WING UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER NEAR INBOARD EDGE STATION XW 212.2972 CORROSION REMOVED FOUND EXCEED LIMIT AS 0.100 INCH MAXIMUM MATERIAL REMOVAL FOR GENERAL CORROSION PER SRM 57-20-01-1A . AND REPAIRED AS PER EA # 1-5730-T0355553 P1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE. 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. NR 1-5750-T0355552 PART 1 STEP 1C AND STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REFER TO SNRM NO. N00427 ATTACHED E.A. NR 1-5750- T0355552 PART 1 FOR WORK DETAILS.

Part: BRACKET — CORRODED (FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (NR 3 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. NR 1-5750-T0355484 PART 1 STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1- 5750-7-5002-RT WING-OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REFER TO SNRM NO. N00375 ATTACHED E.A. NR 1-5750-T0355484 PART 1 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 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. NR 1-5750-T0355552 PART 1 STEP 1A AND STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REFER TO SNRM NO. N00427 ATTACHED E.A. NR 1-5750-T0355552 PART 1 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.

Part: BRACKET — CORRODED (RT FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. NR 1-5750-T0355484 PART 1 STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REFER TO SNRM NO. N00375 ATTACHED E.A. NR 1-5750-T0355484 PART 1 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 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. NR 1-5750-T0355552 PART 1 STEP 1A AND STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (RT FLAP HINGE) · corrosion level 2 · airframe 88,429 hrs · 20,269 cycles

RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. NR 1-5750-T0355484 PART 1 STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-RT WING-OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 88,429 hrs · 20,269 cycles

LT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. NR 1-5750-162588 A PART 3 STEP 2A AND STEP 2; TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002-LT WING-OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 88,429 hrs · 20,269 cycles

LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (NR 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. NR 1- 5750-T0355425 PART 1 STEP 1A AND STEP 1; TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7- 5002-LT WING-OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NO. N00333 ATTACHED E.A. NR 1-5750- T0355425 PART 1 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND E.A. NR 1-5750-162588 A PART 3 STEP 2A AND STEP 2; TITLE: WINGS-FLIGHT SURFACES- EO 1-5750-7-5002-LT WING-OUTBD FLAP, OUTBD FWD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REFER TO SNRM NO. N00291 ATTACHED E.A. NR 1-5750-162588 A PART 3 FOR WORK DETAILS.

Part: SEAT TRACK — DAMAGED (MAIN DECK CARGO) · airframe 88,429 hrs · 20,269 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK TOP SURFACE CORROSION AT BS 1114 - 6.0 , LBL 8.5. REPAIR CARRIED OUT PER SRM 53-00-52-2R . REPAIR 1 . FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (NR 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. NR 1-5750-T0355425 PART 1 STEP 1B AND STEP 1; TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002-LT WING-OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM NO. N00333 ATTACHED E.A. NR 1-5750-T0355425 PART 1 FOR WORK DETAILS.

Part: BULKHEAD — CRACKED (BS 1382) · airframe 88,429 hrs · 20,269 cycles

CENTER LANDING GEAR COMPARTMENT DOUBLER, ADJACENT TO SPOILER FEED THRU ROD BS 1382 FORWARD BULKHEAD RIGHT CORNER FOUND CRACKED. CENTER LANDING GEAR COMPARTMENT / DOUBLER ADJACENT TO SPOILER FEED THROUGH ROD STATION 1382 . X = -31.50 FORWARD BULKHEAD RIGHT CORNER , CRACKED DOUBLER REMOVEDAND REPLACED BY FABRICATION PER DOUGLAS DRAWING # AEA0526 . REVISION ' NC ' AND INSTALLED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 88,429 hrs · 20,269 cycles

LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 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. NR 1-5750-T0355425 ART 1 STEP 1C AND STEP 1; TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002-LT WING-OUTBD FLAP INBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (BS 1382 BULKHEAD) · airframe 88,429 hrs · 20,269 cycles

CENTER LANDING GEAR COMPARTMENT, DOUBLER ADJACENT TO SPOILER FEED THRU ROD BS 1382, FORWARD BULKHEAD LEFT CORNER FOUND CRACKED. ENTER LANDING GEAR COMPARTMENT / DOUBLER ADJACENT TO SPOILER FEED THROUGH ROD STATION 1382 . X = -31.50 FORWARD BULKHEAD LEFT CORNER , CRACKED DOUBLER REMOVEDAND REPLACED BY FABRICATION PER DOUGLAS DRAWING # AEA0526 . REVISION ' NC ' AND INSTALLED PER SRM 51-31-01-OG . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 88,429 hrs · 20,269 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT BS 6-03 , RBL 47.5. REPAIRED IAW SRM 53-00-52-2R, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 88,429 hrs · 20,269 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT FIXED LEADING EDGE SKIN ADJACENT TO CORNER SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD APPROX 1.5 INCHES AS MARK. AT XOS 490.850 . RIGHT WING FIXED LEADING EDGE SKIN ADJACENT TO CORNER SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD STATION XOS 490.850 SKIN REPAIR CARRIED OUT AS PER MD - 11 SRM 57-40-01-2R . FIGURE 201. REPAIR 17 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SKIN — CRACKED (LT WING LE) · airframe 88,429 hrs · 20,269 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT FIXED LEADING EDGE SKIN ADJACENT TO CORNER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD APPROX 1.5 INCHES AS MARK.

Part: SKIN — CRACKED (RT WING LE) · airframe 88,429 hrs · 20,269 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT FIXED LEADING EDGE SKIN ADJACENT TO CORNER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD APPROX 1.5 INCHES AS MARK.

Part: CONTROL UNIT — INOPERATIVE (ANTI-SKID SYS) · airframe 83,545 hrs · 18,807 cycles

"ANTI-SKID FAIL" AFTER GEAR EXTENSION ON APPROACH. WENT AROUND COMPLIED WITH QRH. LANDED UNEVENTFUL AT PHX. MULTIPLE A/S CONTROL UNIT FAULTS LAST LEG. REMOVE AND REPLACED ANTISKID CONTROL UNIT AS PER MM 32-45-01-4, WILL REQUIRE OPERATIONAL TEST AS PER MM 32-45-01-5.

Part: FLOORBEAM — CRACKED (BS 475) · airframe 83,516 hrs · 18,801 cycles

ON REMOVAL OF THE FLOOR PANEL, LT BS 475, LBL 77.5 - 87.5 FLOORBEAM AT LBL 68 WAS FOUND DAMAGED. REPAIRED IAW EA 1- 5321-T0341774, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 83,516 hrs · 18,801 cycles

LEFT WING FIXED LEADING EDGE SKIN ALONG XOS 578 AND XOS=584 , NR 4 SLAT SKIN AREA CRACKED. REPAIRED IAW EA 1-5730-T0341646, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 83,516 hrs · 18,801 cycles

VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR INTERCOSTAL LT SIDE, AFT END, WAS CRACKED AT VSS 2164. REPAIRED IAW EA 1-5530-T0341716, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 83,516 hrs · 18,801 cycles

DURING AN HFEC INSPECTION IN THE REAR SPAR CAP LT FORWARD FLANGE, LOCATED IN THE UPPER SECTION, FOUND A CRACK INDICATION AT THE RADIUS, AT BS 2164 , ZID 54.5. REPAIRED IAW EA 1-5530-T0341644, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RH WING LEADING EDGE STRINGER, XOS 667 WAS FOUND CRACKED. REPAIRED IAW EA 1-5710- 115147 A, PART 2.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 83,516 hrs · 18,801 cycles

VERT STAB REAR CENTER SPAR TO REAR SPAR INTERCOSTAL RIGHT SIDE AFT END WAS FOUND CRACKED AT VSS 2164. REPAIRED IAW EA 1-5530-T0341715, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 83,516 hrs · 18,801 cycles

DURING AN HFEC INSPECTION IN THE REAR SPAR CAP RT FORWARD FLANGE, AT THE UPPER SECTION, FOUND A CRACK INDICATION AT THE RADIUS AT STATION 2164 , ZID 54.5. REPAIRED IAW EA 1-5530-T0341680A, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 765) · airframe 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 765, LBL 75.25, FOUND THE CROWN DAMAGED. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 765 TO 785 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 83,516 hrs · 18,801 cycles

MAIN DECK SEAT TRACK AT BS 755, LBL 47.5 WAS FOUND CRACKED. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 755) · airframe 83,516 hrs · 18,801 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 8.5 WAS FOUND CRACKED. REPLACED THE SEAT TRACK FROM BS 745 TO 785, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER, AT XOS 729 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT XOS 783, WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT XOS 678, WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT XOS 587, WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LEFT WING ALONG XOS 584, ALONG THE NR 4 SLAT, THE LT L/E PLATING FORMER WAS CRACKED. THE FORMER WAS FABRICATED IAW DRAWING ARB2931, REV H. THE FORMER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT XOS 680 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT XOS 703 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER, AT XOS 878 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 6-30 X= 8.5 FOUND CORROSION. SEAT TRACK CORROSION FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-0 TO STA 6-60, X= 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1284 X=-47.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGE FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1265 TO STA 1391, X=- 47.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 666, ALONG NR 5 SLAT LOCATION, LT L/E PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED 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 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1284 X= 8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGE FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1229 TO STA 1351, X= 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 627, ALONG NR 4 SLAT LOCATION, LT LEADING EDGE PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 557, ALONG NR 4 SLAT LOCATION, LT LEADING EDGE PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED 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 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1284, X=-8.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGE FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1265 TO STA 1331, X=- 8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 83,516 hrs · 18,801 cycles

EXISTING REPAIR AT MAIN DECK CARGO SEAT TRACK STA 605 TO STA 645, X= -8 R.SEAT TRACK EVALUATED AND FOUND SEAT TRACK FLANGE CRACKED AT STA 635, X= -8 R. REPAIR CARRIED AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO 1-5100-7- 5001 B6 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 634, ALONG NR 4 SLAT LOCATION, LT L/E PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED 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 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1069 X=-47.5 FOUND CROWN DAMAGED. SEAT TRACK DAMAGE FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1049 TO STA 1129 (STA 6-0), X=-47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 83,516 hrs · 18,801 cycles

RT WING LEADING EDGE BEADED DOUBLER AT STA XOS 544 FOUND CRACK. BEADED DOUBLER REPAIRED 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 83,516 hrs · 18,801 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1079 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK AT STA 1079 X= 47.5 FOUND CROWN DAMAGED FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1049 TO STA 1129 (STA 6-0), X= 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 739, ALONG NR 5 SLAT LOCATION, LT LEADING EDGE PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 620, ALONG NR 4 SLAT LOCATION, LT L/E PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 83,516 hrs · 18,801 cycles

LT WING, ALONG STA XOS 766, ALONG NR 5 SLAT LOCATION, LT LEADING EDGE PLATING BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 83,516 hrs · 18,801 cycles

EXISTING REPAIR AT MAIN DECK CARGO FLOOR SEAT TRACK STA 5-0 TO STA 5-43 X= 47.5 L. EXISTING REPAIR AT MAIN DECK CARGO FLOOR SEAT TRACK EVALUATED AND FOUND DAMAGED WITH CHAFING MARK AT STA 5-11, X= 47.5 L AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. FLOOR SEAT TRACK, CARRIED OUT REPAIR AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201, EO 1-5100-7-5001 B6. ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HELICOIL — BACKED OUT (NR 3 HMU) · airframe 82,953 hrs · 18,620 cycles

ABOUT AN HOUR INTO FLIGHT AT FL370, A LEVEL 2 FUEL QTY/USED CHECK. RAN QRH AND LEAK WAS FROM THE NR 3 ENGINE. DIVERTED AND DECLARED AN EMERGENCY. TOW DRIVER STATED FUEL WAS LEAKING FROM THE NR 3 ENGINE EVEN AFTER SHUTDOWN. PULLED THE FIRE HANDLE AND THE LEAK STOPPED. VISUALLY INSPECTED THE NR 3 ENGINE AND FOUND A HELICOIL BACKED OUT OF THE HMU FEED LINE.

Part: TUBE — LEAKING (FUEL DIST) · airframe 82,951 hrs · 18,619 cycles

RECEIVED A LEVEL 2 FUEL QTY/USED CHK CAUTION, 1 HOUR INTO FLIGHT DESCENDING THROUGH FL340, ON ARRIVAL. COMPLIED WITH QRH, DECLARED EMERGENCY AND LANDED. CONFIRMED A FUEL LEAK FROM THE NR 1 ENGINE. FUEL SOV CLOSED ON THE NR 3 ENG AFTER SHUTDOWN. R & R THE PUMP TO FUEL CONTROL TUBE AND GASKETS IAW MM 73-12-01-4-1. LEAK CHECKED GOOD. OK FOR SERVICE.

Part: CONTROL UNIT — INOPERATIVE (ANTI SKID SYS) · airframe 81,885 hrs · 18,247 cycles

RTO AT 65KTS FOR AN ANTI-SKID FAIL LIGHT. COMPLIED WITH QRH. TROUBLESHOT IAW FIM 32-40-12-00, FIG 110. FOUND SEVERAL INSTANCES OF ASCU FAULTING. R & R THE ASCU IAW AMM 32-45-01-4. OPS CHECKED IAW AMM 32-45-01-5. OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 81,824 hrs · 18,231 cycles

EMERGENCY LIGHTS WILL NOT PASS TEST. LEVEL 1 ALERT FOR THE BATTERY LOW OCCURS DURING TEST. REMOVED AND REPLACED THE BATTERY POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED NORMAL.

Part: CONTROL HANDLE — LACK OF LUBE (MLG) · airframe 80,896 hrs · 17,953 cycles

ON APPROACH, ALL FOUR LANDING GEAR UNSAFE LIGHTS REMAINED ON. QRH CLEARED, ALL GREEN DOWN AND LOCK LIGHTS AFTER QRH. TROUBLESHOT IAW FIM 32-30-05-01, NO DEFECTS NOTED. NO CURRENT FAULTS DETECTED, THE PSEU TESTED OK, CLEANED AND LUBRICATED THE LANDING CONTROL MECHANISM IAW AMM 32-31-00-7. OK FOR SERVICE.

Part: CONTROLLER — FAILED (WINDSHIELD) · airframe 78,990 hrs · 17,379 cycles

COCKPIT WINDOW FOGGED AND BECAME UNUSABLE, AIRCRAFT HAD TO STOP TAXI UNTIL WINDSCREEN COULD BE WIPED REPEATEDLY. TROUBLESHOT IAW FIM 30-42 AND MM 30-42-00-5. ALL SIX CONTROLS WERE TESTED. LT AFT CONTROLLER FAILED TESTS. R & R THE CONTROLLER IAW MM 30-42-01-4 AND TESTED IAW MM 30-42-00-5, TEST PASSED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

WHILE ACCOMPLISHING W/C 25C2206, FOUND CORROSION ON MAIN DECK FLOOR SEAT TRACK FLANGE LOWER AT STA 1643-1680, X=75, INBD. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1611 TO STA 1751, X =75 IAW SRM 53-00-52-2R, FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,752 hrs · 17,319 cycles

WHILE ACCOMPLISHING W/C 25C2206 FOUND CORROSION ON MAIN DECK FLOOR SEAT TRACK FLANGE LOWER AT STA 1541-STA 1580, X=75, INBD. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1531 TO STA 1611 X=75 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) · airframe 78,752 hrs · 17,319 cycles

WHILE ACCOMPLISHING W/C 25C2206 MAIN DECK SEAT TRACK FLANGE LOWER FOUND CORROSION AT STA 5-90 TO 5-113, X =-75, INBD. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-83 TO STA 5-123, X =-75 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

WHILE ACCOMPLISHING W/C 25C2206, FOUND CORROSION ON MAIN DECK FLOOR SEAT TRACK, FLANGE LOWER AT STA 1641, X= -8, OTBD. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1651 X = -8 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

WHILE ACCOMPLISHING W/C 25C2206 FOUND CORROSION ON MAIN DECK FLOOR SEAT TRACK. FLANGE LOWER AT STA 1561 TO STA 1604, X = -8, OTBD. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1651, X = -8 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

MAIN DECK CARGO BAY CARGO TRACK CROWN AREA DAMAGED BS 5-32, X -47.5. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63, X = -47.5 AND FABRICATED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (MLG WW) · airframe 78,752 hrs · 17,319 cycles

CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD, LEFT SPOILER MIXER FEED THROUGH CUTOUT FOUND DOUBLER CRACKED AT STA X=31.5, Y=1381. R & R IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

MAIN DECK CARGO BAY CORROSION ON CARGO TRACK FLANGE BS 1681 - 1701, X 75.25. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1611-STA 1751, X =75.25 AND FABRICATED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

MAIN DECK CARGO TRACK CROWN DAMAGED BS 1681, RBL 47.5. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1671 TO STA 1711 X = - 47.5 AND FABRICATED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

MAIN DECK CARGO BAY L3 DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255 BETWEEN LONGERONS 26 - 27L. WEB REPAIRED AND FABRICATED AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 78,752 hrs · 17,319 cycles

FOUND CRACK INDICATIONS DURING HFEC INSPECTION ON RIGHT WING LOWER SKIN ACCESS CUTOUT BETWEEN XORS 683.4 AND 713.65. REPAIR CARRIED OUT IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. REPAIR IS A CATEGORY B REPAIR WITH INITIAL INSPECTION 2000 CYCLES AFTER COMPLETION OF THIS REPAIR AND REPETITIVE 2000 CYCLES IAW PSE 57.23.01.2 IAW SRM 57-20-02-2R, FIG 202, REPAIR 5.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

MAIN DECK CARGO BAY R3 DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED BS 1255 BETWEEN LONGERONS 26 - 27R. WEB REPAIRED AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 78,752 hrs · 17,319 cycles

MAIN DECK CARGO BAY R3 DOOR AFT LOWER FRAME WEB CRACKED BS 1310 BETWEEN LONGERONS 26 - 27R. WEB REPAIRED AND FABRICATED 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 78,752 hrs · 17,319 cycles

MAIN DECK CARGO BAY, CORROSION ON SEAT TRACK FLANGE ATBS 1461, RBL 8.5. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1451-STA 1491, X = -8.5 AND FABRICATED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (S47) · airframe 766 hrs · 16,670 cycles

LOWER CTR WING STRINGERS CRACKED AT STRINGER 47, XCW 46, 17, 17, 46 & 81. STRINGER 45 CRACKED AT XCW 81,17 & 17, STRINGER 45 CRACKED AT XCW 81. REPAIRED IAW DWG 201501160111.

Part: BUTTON — INOPERATIVE (L1 DOOR) · airframe 759 hrs · 16,481 cycles

SLIDE LIGHT ON 1L WILL NOT TEST. R & R L1 DOOR PRESS TO TEST PUSH BUTTON IAW AMM 25-61-04.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT FIXED LE SUPPORT RIB OTBD ATTACHED ANGLE AT XOS 584 FOUND CRACKED. REMOVED IAW SRM 51-31-01 REVISION 56. NEW ANGLE FABRICATED IAW DRAWING ARB2931 REVISION H. ANGLE INSTALLED IAW SRM 51-33-01 REVISION 56. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT FIXED LE SUPPORT RIB AT XOS 584 FOUND CRACKED. REMOVED AND REPLACED IAWSRM 51-31-01 REVISION 56, DWG ARB2931 REVISION H, AND SRM 51-33-01 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: FLOOR SUPPORT — CORRODED (BS 420) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

FORWARD CABIN FLOOR SUPPORT FOUND CORRODED BS 420 X= -27. FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 56.

Part: FLOOR SUPPORT — CORRODED (BS 420) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

FORWARD CABIN FLOOR SUPPORT FOUND CORRODED BS 420 LBL 47. FLOOR SUPPORT REMOVED AND REPLACED IAW AMM 20-50-02 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FWD CABIN FLOOR METAL PANEL 231VF FOUND CORRODED RCB PANEL. REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: SEAT TRACK — CORRODED (BS 1761-1841) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

FOUND CORROSION ON CABIN SEAT TRACK FLANGE LOWER SURFACE FROM BS 1761 TO 1841, LBL 75. REPAIRED IAW EA1-5321-T0309846 PART1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CARGO FLOOR PANEL 232BF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

RIGID CARGO BARRIER METAL FLOOR PANEL 233PF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 233SF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL FABRICATED PER DWG WSP0785 REVISION B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: REPAIR — DAMAGED (TE FLAP) · airframe 73,769 hrs · 15,814 cycles

EXSITING REPAIR FOUND AT RIGHT WING INBOARD FLAP OUTBOARD WEB AT APPROXIMATELY XIFH 133.9. EXISTING REPAIR EVALUATED AND FOUND DAMAGED. REPAIR REMOVED AND REPLACED AS PER DRAWING NR ARC2305 REVISION C AND SRM 51-35-01 REVISION 56. EO 1-5100-7-5001 B4 PART 1 TITLE: "STRUCTURE- REPAIR CATALOG - MD11- REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 233UF FOUND CORRODED. REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL 233UF FABRICATED PER DRAWING WSP0785 REVISION B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CABIN - UPON REMOVAL OF RIGID CARGO BARIER METAL FLOOR PANEL 232PF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL FABRICATED PER DRAWING WSP0790 REVISION A. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 231BF FOUND CORRODED. REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FLOOR PANEL — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CARGO METAL FLOOR PANEL 231AF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FORWARD CABIN FLOOR METAL PANEL 232VF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-21-10-2 REVISION 79.1. NEW METAL FLOOR PANEL FABRICATED PER DRAWING WSP0785 REVISION B. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FLOOR PANEL — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CARGO METAL FLOOR PANEL 231PF FOUND CORRODED. FLOOR PANEL REMOVED AND REPLACED IAW AMM 53-21-10-2 REVISION 79.1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CABIN SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1841 - 1887, X=-8. CABIN AT STATION 1841 - 1887 X= -8 CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 56. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CABIN SEAT TRACK FLANGE LOWER SURFACE FOUND CORRODED AT STATION 1841 - 1887, X=75.25. REPAIRED IAW EA1-5321-T0309846 PART 1 TITLE FUSELAGE CARGO COMPARTMENT FLOORS, SEAT TRACK CORROSION PTF VARIATION DWG SRM SPLICE REPAIR. REFER TO WRI 53219487 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

CABIN DURING CONTROL CABLES INSPECTION IN CTR CARGO FOUND CORROSION ON CABIN SEAT TRACK FLANGE LOWER SURFACE AT STATION 1621 X=8. SEAT TRACK REPAIRED PER SRM 53-00-52 FIGURE 201. REPAIR 1 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FRAME — DENTED (FUSELAGE) · airframe 73,769 hrs · 15,814 cycles

CABIN RT STATION 1721 LONGERON 12 FRAME FOUND DENTED. FRAME REPAIRED PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 56 REPETITIVE INSPECTION REQUIRED-INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00- 07 REPAIR 2 TABLE 201 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: SKIN — DAMAGED (RT WING) · airframe 73,769 hrs · 15,814 cycles

EXISTING REPAIR FOUND AT RIGHT WING NR 4 SLAT LOWER SKIN AT STATION XOS 608 TO STATION XOS 612. EXISTING REPAIR EVALUATED AND FOUND DAMAGED. SLAT LOWER SKIN REPAIRED PER SRM 57-40-01 FIGURE 201 REPAIR 3 REVISION 56 AND EA 1- 5750-T0309965 PART1 TITLE: WINGS-FLIGHT SURFACES-RTW NR 4 SLAT ASSY SEVERAL EXISTING REPAIRS REPLACED WITH AN SRM SKIN SPLICE REPAIR-RSC TRACKING. EO 1-5100- 7-5001 B4 PART 1 TITLE:"STRUCTURE- REPAIR CATALOG - MD11- REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. EA#1-5750-T0309965 PART1 ISSUED FOR RSC TRACKING AND ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2- 100 REVISION 122.

Part: STRAP — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING OTBD FLAP INBD FWD HINGE, OTBD TENSION STRAP FOUND CRACK AS MARKED. TENSION STRAP REMOVED AND REPLACED WITH NEW TENSION STRAP AS PER SRM 51-33-01 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: SKIN — DAMAGED (RT WING) · airframe 73,769 hrs · 15,814 cycles

REPAIR FOUND AT RIGHT HAND WING INBOARD UPPER FIXED LEADING EDGE XIS 247. EXISTING REPAIR EVALUATED AND FOUND DAMAGED. RIGHT HAND WING INBOARD UPPER FIXED LEADING EDGE XIS 247 REPAIRED PER EA 1-5730-T0309906 PART1 TITLE: WINGS-PLATES AND SKINS-EO 1-5100-7-5001-RT WING-EXISTING REPAIR ON LEADING EDGE SKIN UPPER SURFACE BETWEEN XIS 243 TO XIS 250. EO 1-5100-7- 5001 B4 PART 1 TITLE:"STRUCTURE- REPAIR CATALOG - MD11- REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122. REFER TO WRI 57309494 FOR DETAILS

Part: FRAME — DENTED (FUSELAGE) · airframe 73,769 hrs · 15,814 cycles

CABIN RT STATION 1721 LONGERON 12 FRAME FOUND DENT. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 56 REPETITIVE INSPECTION REQUIRED-INITIAL AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00- 07 REPAIR 2 TABLE 201 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: SKIN — DAMAGED (RT WING) · airframe 73,769 hrs · 15,814 cycles

EXISTING REPAIR FOUND AT RIGHT HAND WING INBOARD FIXED LEADING EDGE XIS 195 -220. EXISTING REPAIR EVALUATED AND FOUND DAMAGED. RIGHT HAND WING INBOARD FIXED LEADING EDGE XIS 195 -220 REPAIRED PER EA 1-5730-T0309875A PART1 TITLE: WINGS-PLATES AND SKINS-EO 1-5100-7-5001-RT WING-EXISTING REPAIR ON LEADING EDGE SKIN LOWER SURFACE BETWEEN XIS 195 TO XIS 220. EO 1-5100-7- 5001 B4 PART 1 TITLE:"STRUCTURE- REPAIR CATALOG - MD11- REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122. REFER TO WRI #57309504 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 768 - 772 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER AREA REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 73,769 hrs · 15,814 cycles

FORWARD CABIN FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X=27 AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 6-80 TO 6-90 X=8.5 AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,769 hrs · 15,814 cycles

MAIN DECK CARGO FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1139 - 1149 X=8.5 AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: DOUBLER — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STA XOS 698 - 703 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 73,769 hrs · 15,814 cycles

FORWARD CABIN FLOOR SEAT TRACK FOUND CRACKED AT STATION 635 X= -8.50 AS MARKED. SEAT TRACK REPAIRED PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: DOUBLER — CRACKED (LT WING) · airframe 73,769 hrs · 15,814 cycles

LEFT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 753 - 759. FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56 REPAIR. CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 653 - 657 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER AREA REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: DOUBLER — CRACKED (LT WING) · airframe 73,769 hrs · 15,814 cycles

LEFT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 728 - 734. FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: DOUBLER — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 625-629 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER AREA REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: DOUBLER — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 661 - 667 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER AREA REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: DOUBLER — CRACKED (RT WING) · airframe 73,769 hrs · 15,814 cycles

RIGHT WING LE COMPARTMENT BEADED DOUBLER AT STATION XOS 633 - 636 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION & TENSION CHECK. CRACKED BEADED DOUBLER AREA REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 56. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122

Part: FIRE WARNING — FALSE ACTIVATION (NR 3 ENGINE) · airframe 71,454 hrs · 15,090 cycles

AT TAKE OFF, APROX 110 KTS. RECEIVED RED MASTER WARNING AND LEVEL 3 NR 3 ENG FIRE ALERT. REJECTED TAKEOFF AT POWER REDUCTION ON REJECT ALERT WENT AWAY. NO FIRE BELL. MAX PWR TAKEOFF.

Part: WIRE HARNESS — DAMAGED (NR 3 NACELLE) · airframe 71,293 hrs · 15,028 cycles

ON DEPARTURE, RECEIVED A LEVEL 3 "ENG 3 FIRE" ALERT. APPEARED FOR APPROX 30 SECONDS THEN WENT OUT, THEN ONE MINUTE LATER RETURNED. SHUTDOWN ENGINE IAW QRH. FIRE WARNING CAME ON THREE MORE TIMES. FIRED SECOND BOTTLE, DECLARED EMERGENCY. R & R BOTH LOOPS A & B WIRE HARNESSES ON NR 3 ENG REF AMM 71-50-04-4-1. NR 3 ENG FIRE DETECTION SYS OPS CHECKED NORMAL IAW AMM 26-11-02-5.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 69,556 hrs · 14,428 cycles

CENTER GEAR LIGHT DID NOT ILLUMINATE WITH GEAR DOWN. SECONDARY SHOWED DOWN AND LOCKED. RECYLED & LIGHT ILLUMINATED. PSCU HAS NO FAULT MEMORY STORED. FOLLOWED FIM 31-71-04-00 AND VISUALLY INSPECTION ALSO CLEANED CLG LOCKED SENSOR, NO DEFECT FOUND. THEN CLG GEAR POSITION INDICATION OPS TEST IAW MM 32-61-16-5, CLG POSITION INDICATION NORMAL ON THE GROUND. ACFT OK SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 1922-1976) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

MAIN DECK FLOOR SUPPORT FOUND WITH CORROSION AT BS 1922, 1937 AND 1976, X= -58.5. REMOVED AND REPLACED AS PER AMM 20-50-02-4 REVISION 72.1. FLOOR SUPPORT MACHINED AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100 REVISION 115.

Part: HINGE — WORN (MAIN CARGO DOOR) · airframe 69,546 hrs · 14,423 cycles

MAIN DECK UPPER CARGO DOOR HINGE LOBES 04 PLACES WORN FORWARD HINGE AREA. REPAIRED IAW CMM 52-34-04 REVISION 74. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,546 hrs · 14,423 cycles

DURING X-RAY INSP AT CABIN STATION 5-0, LONGERON 2R STRINGER FORWARD SECTION OTBD ROW FROM EDGE CRACK INDICATION FOUND APPROX .3750" IN LENGTH. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,546 hrs · 14,423 cycles

DURING X-RAY INSPECTION, AT CABIN STATION 5-0, LONGERON 1R, FORWARD SECTION INBD ROW FROM EDGE TO NR 2 HOLE HAS A CRACK INDICATION APPROX 2.25" IN LENGTH. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,546 hrs · 14,423 cycles

DURING X-RAY INSPECTION AT CABIN STATION 5-0, LONGERON 2L, FORWARD SECTION INBD ROW FROM EDGE CRACK INDICATION FOUND APPROX .3750" IN LENGTH. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: HINGE — DAMAGED (RT WING TE FLAP) · airframe 69,546 hrs · 14,423 cycles

DURING FPI ON RT INBD FLAP, OTBD HINGE (FLAP SIDE) PIVOT INBD HOLE FOUND DAMAGED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 REVISION 74. REPAIRED IAW EA 1-5750-162593 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: BUSHING — WORN (LT WING TE FLAP) · airframe 69,546 hrs · 14,423 cycles

LEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.254", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-162592 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: HINGE — CORRODED (WING SIDE) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

RT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162587 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115

Part: BUSHING — WORN (RT WING TE FLAP) · airframe 69,546 hrs · 14,423 cycles

RT INBD FLAP OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07 REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03 REV 74. EXISTING HOLE DIAMETER 1.255", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-162593 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 69,546 hrs · 14,423 cycles

LEFT OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 74. EXISTING DIAMETER 1.228", FINAL DIAMETER 1.232", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162589. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: HINGE — CORRODED (WING SIDE) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

LEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: BUSHING — WORN (LT WING TE FLAP`) · airframe 69,546 hrs · 14,423 cycles

LEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED AS PER CMM 20-20-07 REVISION 74. FOUND EXCEED LIMITS AS PER CMM 57-52-03 REVISION 74. NEW BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-162592 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: BUSHING — WORN (RT WING TE FLAP) · airframe 69,546 hrs · 14,423 cycles

RIGHT INBD FLAP, OTBD AFT (FLAP SIDE) PIVOT OTBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.258", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-162593, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 115.

Part: HINGE — CORRODED (WING SIDE) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

LEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

RT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR, INBD HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER 1.249", FINAL HOLE DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED AS PER E.A. 1-5750-162587 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 69,546 hrs · 14,423 cycles

CENTER CARGO COMPARTMENT LONGERON SPLICE AT 43RH BETWEEN STA 5-113 TO STA 1541 FOUND CRACKED. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION E. INSTALLED AS PER SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 69,546 hrs · 14,423 cycles

LONGERON SPLICE, 47L, CRACKED AT BS 5-113 TO 1541. LONGERON SPLICE REMOVED AS PER SRM 51-31-01 REVISION 50. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114 REVISION E AND INSTALLED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: HINGE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

RT OTD FLAP, OTBD FORWARD WING HINGE ACTUATOR OTBD HOLE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 74 EXISTING HOLE DIAMETER 1.215", FINAL DIAMETER 1.221", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162586, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.

Part: LONGERON SPLICE — CRACKED (BS 1541 L49L) · airframe 69,546 hrs · 14,423 cycles

CENTER CARGO COMPARTMENT LONGERON SPLICE CRACKED AT LONGERON 49L BETWEEN BS 5-113 TO 1541. REMOVED AND REPLACED SPLICE IAW SRM 51-31-01 REVISION 50.

Part: BEAM — CRACKED (BS 1746-1750) · airframe 69,546 hrs · 14,423 cycles

CENTER CARGO DOOR ACTUATOR MOUNTING BEAM FOUND CRACKED AT BS 1746 TO 1750. REPAIRED AS PER EA 1-5310-162594. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 69,546 hrs · 14,423 cycles

RT OTBD FLAP, OTBD FORWARD WING HINGE ACTUATOR INBD HOLE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09 REV 74. EXISTING HOLE DIAMETER 1.249", FINAL DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162586 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

CENTER CARGO COMPARTMENT LONGERON 49 LEFT CORRODED AT BS 1531 TO 1541. REPAIRED IAW EA 1-5310-162591. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: ATTACH FITTING — CORRODED (ZONE 500) · airframe 69,546 hrs · 14,423 cycles

LEFT WING PANEL ATTACHMENTS FOUND CORROSION. REPAIRED IAW EA 1-5710-162381. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: ATTACH FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 69,546 hrs · 14,423 cycles

RT WING T/E PANEL NR 641JB SUPPORT ATTACHMENT FOUND CORRODED. REPAIRED IAW EA1-5710-162382. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: TEE FITTING — CRACKED (MLG WW BULKHEAD) · airframe 69,546 hrs · 14,423 cycles

CENTER LANDING GEAR COMPARTMENT LT BULKHEAD TEE FITTING FOUND CRACKED. TEE FITTING REMOVED IAW SRM 51-31-01, REV 50. TEE FITTINGFABRICATED BY MACHINING IAW DWG APB7158 REV C AND INSTALLED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: DOUBLER — CRACKED (MLG WW) · airframe 69,546 hrs · 14,423 cycles

CENTER LANDING GEAR COMPARTMENT LT BULKHEAD SPOILER CONTROL ROD CUTOUT SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-31-01, REV 50. NEW DOUBLER FABRICATED BY MACHINING IAW DWG AEA0526 REVISION D AND INSTALLED IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: TEE FITTING — CRACKED (MLG WW BULKHEAD) · airframe 69,546 hrs · 14,423 cycles

CENTER LANDING GEAR WW RT FORWARD BULKHEAD TEE FITTING CRACKED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — DAMAGED (ZONE 100) · airframe 69,546 hrs · 14,423 cycles

CENTER CARGO DOOR CUT-OUT FORWARD JAMB DOUBLER REPAIR EDGE FOUND BLENDED BY ABOUT .5" AT LONGERON 40RT. R & R IAW SRM 53-00-15, FIG 202, REPAIR 8, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.

Part: SKIN — DENTED (NR 8 SLAT) · airframe 69,546 hrs · 14,423 cycles

LT OTBD SLAT NR 8 SKIN DENTED. R & R NR 8 SLAT ASSY ON LT WING IAW AMM 27-80-30-4, REV 74.0. CARRIED OUT ADJUSTMENT & TEST AND SLAT RANGE OF MOVEMENT IAW 27-80-30-5, REV 74.0 AND AMM 27-80-00-5, REV 74.0 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 115.

Part: LANDING GEAR — MALFUNCTIONED · airframe 69,093 hrs · 14,304 cycles

AFTER TAKE OFF, RETRACTED LANDING GEAR, CENTER GEAR CUBE FLASHED RED (UNSAFE) RAN QRH CONFIG SYNOPTIC SHOWED CTR GEAR SAFE. FLASHING CENTER GEAR LIGHT APPROXIMATELY 25 MIN THEN STOPPED. NO FURTHER INDICATION PROBLEMS. ON EXTENSION OF GEAR FOR LANDING. THRU ROLLOUT AND TAXI, ALL INDICATIONS NORMAL. PERFORMED VISUAL CHECK OF WIRING HARNESS AND TARGETS FOR SECURITY AS A PERCAUTION. NO EVIDENCE OF VISUAL DAMAGE TO WIRING AND TARGETS FIRMLY SECURED. PERFORMED CENTER LANDING GEAR PROXIMITY SENSOR TEST IAW MM 32-61-16-5. INDICATIONS WERE NORMAL IAW SUB TASK 32-61-16-741-006. ACFT OK TO CONTINUE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 64,986 hrs · 13,219 cycles

UNSAFE LT MAIN GEAR UP ON DEPARTURE, COMPLIED WITH QRH AND COMFIRMED INDICATION WITH CONFIG PAGE. ALL MLG DOOR CLOSED ON ARRIVAL. PERFORMED T/S IAW FIM 32-30, PAGE 121. PERFORMED SELF TEST ON PSEU MM 31-71-01-2, NO FAULT. PERFORMED VISUAL INSP, NO DEFFECT, AND NO LEAKS FOUND. INSPECT DOOR LATCH INSTALLATION IAW MM 32-34-03. NO DAMAGE FOUND. PERFORMED MLG DOOR ACTUATION IAW MM 32-34-00-2 , THE DOOR OPENED AND CLOSED NORMALLY, ALL INDICATION NORMAL. CHECK HYD SUPPLY ON MAIN LT LANDING DOWN LOCK CYLINDER DURING GEAR DOOR SIMULATION, FOUND HYD PRESSURE, NO TIME FOR MORE T/S. ADJUSTED LT MLG DOOR PROXIMITY SENSOR. FINAL CLOSED.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 64,577 hrs · 13,130 cycles

R1 DOOR PRESS TO TEST LIGHT DOESN'T WORK. RELEASED FOR SERVICE IAW MEL: 25-61-02, R & R REMOTE PRESSURE INDICATOR PER MM 25-61-04-4-0 , OPS CHECKED OK.

Part: SKIN — CRACKED (ZONE 600) · airframe 63,767 hrs · 12,936 cycles

03 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS=713.6. REPAIR CARRIED OUT AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS=713.6 AS PER DRAWING 11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE AT STA 5-0 X= -8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK R & R IAW SRM 51-33-01, REV 44. NEW SEAT TRACK FABRICATED IAW DWG A5A7082-1 REV B EXISITING SPLICE REMOVED AND RE-ISTALLED IAW SRM 51-33-01, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 63,767 hrs · 12,936 cycles

06 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 TO STATION XORS= 713.6. REPAIR CARRIED OUT AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS= 683.4 AND STATION XORS=713.6 AS PER BOEING DRAWING SG11570004 REVISION A. THIS REPAIR IS CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CRACKED (BS 1521) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1521 X=75 FOUND CRACKED. TRIMMED OUT IAW SRM 53-00-52, FIG 201, REVISION 44. CRACK SEAT TRACK REMOVED IAW SRM 51-33-01 REV 44. REPAIR SEAT TRACK AND SPLICE FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE AT STA 5-53 TO STA 5-83 X= -8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK R & R IAW SRM 51-33-01, REV 44. NEW SEAT TRACK FABRICATED IAW DWG A5A7082-1, REV B. EXISTING SPLICE REMOVED AND RE-INSTALLED IAW SRM 51-33-01, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 44. NEW SEAT TRACK FABRICATED AS PER DWG A5A7082-1 REVISON B. EXISTING SPLICE REMOVED AND RE-INSTALLED AS PER SRM 51- 33-01 REVISION 44. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE AT STATION 5-0 TO STATION 5-53 X= 8.5 FOUND WITH SURFACE CORROSION. SEAT TRACK REMOVED AND AND NEW SEAT TRACK INSTALLED IAW SRM 51-33-01 REV 44. NEW SEAT TRACK FABRICATED IAW DWG REV B. EXISTING SPLICE REMOVED AND RE-INSTALLED IAW SRM 51-33-01, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 44. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CRACKED (BS 1982 L47L) · airframe 63,767 hrs · 12,936 cycles

WASTE TANK COMPARTMENT BILGE AREA STATION 1982 LONGERON L-47L CRACKED. REPAIRED IAW SRM 53-00-05 FIGURE 202, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (LT WING) · airframe 63,767 hrs · 12,936 cycles

LEFT WING LEADING EDGE CUTOUT AT SLAT TRACK NR 14 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING LEADING EDGE LOWER CUTOUT AT SLAT TRACK NR 14 AS PER SRM 57-40-02 FIGURE 201 REVISION 44. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: FRAME — DEFORMED (BS 1641) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - FRAME AT STATION 1641 LONGERON 12R FOUND DEFORMED. TRIMMED OUT IAW SRM 53-00-07, FIG 201 REV 44. REPAIR ANGLE FABRICATED AND INSTALLED IAW SRM 53-00-07, FIG 201, REV 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: FRAME — DEFORMED (BS 1661 L12R) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - FRAME AT STATION 1661 LONGERON 12R FOUND DEFORMED. TRIMMED OUT IAW SRM 53-00-07, FIG 201 REVISION 44. REPAIR ANGLE FABRICATED AND INSTALLED IAW SRM 53-00-07, FIG 201 REVISION 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 63,767 hrs · 12,936 cycles

RIGHT WING LEADING EDGE LOWER CUTOUT AT SLAT TRACK NR 14 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER CUTOUT AT SLAT TRACK NR 14 AREA AS PER SRM 57-40-02 FIGURE 201 REVISION 44 REPAIR 7. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: FRAME — DEFORMED (BS 1701 L12R) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - FRAME AT STATION 1701 LONGERON 12R FOUND DEFORMED. REPAIR ANGLE REMOVED AND NEW REPAIR ANGLE INSTALLED AS PER SRM 51-33-01 REVISION 44. NEW REPAIR ANGLE FABRICATED AS PER SRM 53-00-07 FIGURE 201 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FRAME — DAMAGED (BS 1681 L12L) · airframe 63,767 hrs · 12,936 cycles

FRAME AT STATION 1681 LONGERON 12L FOUND DEFORMED AT EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR REMOVED AND NEW REPAIR ANGLE INSTALLED AS PER SRM 51-33-01 REVISION 44. NEW REPAIR ANGLE FABRICATED AS PER SRM 53-00-07 FIGURE 201 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FRAME — DEFORMED (BS 1741 L12L) · airframe 63,767 hrs · 12,936 cycles

MAIN DECK CARGO - FRAME AT STATION 1741 LONGERON 12LH FOUND DEFORMED. TRIMMED OUT IAW SRM 53-00-07, FIG 201, REVISION 44. REPAIR ANGLE FABRICATED AND INSTALLED IAW SRM 53-00-07, FIG 201 REVISION 44. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: VALVE — FAILED (TRIM AIR VALVE) · airframe 61,765 hrs · 12,441 cycles

ON CLIMB OUT RECEIVED LVL 2 ALERT TRIM AIR OFF TEMP REACHED 225 F. COCKPIT TEMP 99 F COULD NOT CONTROL TEMP IN AUTO WITH QRH OR MANUAL. TEMP LOWERED TO 190F AND REMAINED THERE UNTIL DECENT. FOUND FD TRIM AIR VALVE STUCK OPEN. PN 398398-3 CURRENTLY NIS ANC. CPN 2100193 QTY 1 VALVE MSN 1160678 R & R FWD TRIM AIR VALVE IAW REF TO MM 21-61-12-4. ALL TESTS AND CHECKS PASSED. SYS OK FOR SERVICE.

Part: DIMMER — FAILED (COCKPIT LIGHTS) · airframe 61,744 hrs · 12,437 cycles

500 HRS INTO FLT AT CRUISE FL 360. CREW HEARD AN ARCING SOUND BY THE RT OBSERVERS POSITION, LIGHT SMOKE AND AN ACRID SMELL WERE ALSO NOTED. THE OVER-HEAD SWITCH PANEL LTG (C-30) CIRCUIT BREAKER POPPED AND SMOKE AND FUMES DISAPATED. OVERHEAD PANEL LIGHTS WERE OUT THE REMAINDER OF FLIGHT. NO OTHER MALFUNCTIONS ON AC BUS 3 NOTED. T/S IAW FIM 33-11, FOUND OVERHEAD LAMP DIMMER (U1-13 0) R & R O/H LAMP DIMMER IAW MM 33-11-03-2. ACFT OK FOR SERVICE, CLEARS PIREP. PREMATURE REMOVAL/INSTALLATION.

Part: WIRE HARNESS — SHORTED · airframe 61,581 hrs · 12,393 cycles

HAD A TANK 2L AFT PUMP LO ALERT, LEVEL 1 AFTER TAKE OFF FOR ENTIRE FLIGHT. CIRCUIT BREAKER WAS POPPED. FOLLOWED QRH AND KEPT CB OUT. WIRES RUNNING UNDER FLOOR PANELS SHOW SHORT. DISCOVERED DAMAGED AND MELTED WIRE HARNESS UNDER FLOOR PANEL 272CF. ROUTED NEW WIRES FROM OVERHEAD AT S9-124 DOWN TO FLOOR SECURED HARNESS AT TOP OF CONDUIT AND AT BOTTOM. WIRES STILL NEED ROUTED AND CLAMPED UNDER FLOOR, SECURED ON TOP AND AND SPLICED AT BOTH ENDS. CLEANED AND INSPECTED CONTROL CABLES IAW MM 20 20-06-2 NO DAMAGE FOUND. REAPPLIED CORROSION PREVENTION COMPOUND TO CABLES. COMPLETED INSTALLATION OF WIRING FROM PRODUCTION SPLICES S9-124 TO REPAIR SPLICES AT LOCATION X=-57/Y=1399/Z=-20 IAW SWPM 20-10-03 AND WDM 28-22-02. UN-DOCUMENTED REPAIRS WERE FOUND IN DAMAGED AREA, CUT OUT OF HARNESS. INSPECTED ENTIRE WIRE RUN FOR ADDITIONAL UN-DOCUMENTED SPLICES AND FOUND NONE. INSULATION BLANKETS, REINSTALLED SAME NR2 L AFT FUEL BOOST PUMP IAW MM 28-22-01-4, PUMP OPS CHECK NORMAL, REINSTALLED SIDEWALL PREVIOUSLY REMOVED FOR MAINT., INSTALLED MISSING NUTCLIPS . INSTALLED PREVIOUSLY REMOVED FLOOR PANELS IAW MM 53-21-01-4. REINSTALLED REMOVED CARGO FLOOR LOCKS IAW ACFT PLACARDING. OK FOR SERVICE.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT WING NR 4 SLAT INNER SURFACE FOUND 03 EACH EXISTING REPAIRED PATCH AT APPROXIMATELY XORS 538. RIGHT WING NR 4 SLAT INNER SURFACE 03 EACH EXISTING DOUBLERS EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. EXISTING DOUBLERS 03 EACH REMOVED AND REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 57-00-01 FIGURE 8, VOLUME 1. EO NR 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES, REPAIR CATALOG, MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 58,726 hrs · 11,729 cycles

FUSELAGE SKIN EXTERNAL FOUND WITH EXISTING DOUBLER REPAIRS AT STA 1896 LONGERON 42 LT. REPAIR DOUBLER EVALUATED AND FOUND NOT IAW SRM 53-20-00 VOLUME I. EXISTING REPAIR DOUBLERS REMOVED AND NEW REPAIR CARRIED OUT AS PER SRM 53-20-00 FIGURE 2, VOLUME IEO NR 1-5100-7-5001 A4 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 58,726 hrs · 11,729 cycles

FUSELAGE SKIN EXTERNAL FOUND WITH EXISTING DOUBLER REPAIRS AT STA 1801 LONGERON 37 RIGHT. FUSELAGE SKIN REPAIR AT STA 1801 LONGERON 37 RIGHT EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-20-00 FIGURE 2 VOLUME I. EXISTING DOUBLER REPAIR AT FUSELAGE SKIN EXTERNAL STA 1801, LONGERON 37 RIGHT REMOVED AND REPAIR CARRIED OUT AS PER SRM 53-20-00 FIGURE 2, VOLUME I, EO NR 1-5100-7-5001 A4 PART 1, TITLE, STRUCTURES, REPAIR CATALOG, MD11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: PANEL — CORRODED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

LEFT STA 1229, XCW = 8 TO 20 CENTER WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (BS 1229) · airframe 58,726 hrs · 11,729 cycles

RIGHT STA 1229, XCW = -46 TO -48 CENTER WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA. NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (WING BOX) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, CENTER WING UPPER SKIN PANEL STA 1229 X = -80 TO X = -100 FOUND WITH CORROSION AROUND FASTENER HEAD. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (WING BOX) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, CENTER WING UPPER SKIN PANEL STA 1229, X = - 50 TO X = - 80 FOUND WITH CORROSION AROUND FASTENER HEAD. REPAIRED AS PER E.A. NO. 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

RIGHT STA 1229, XCW = -8 CENTER WING UPPER PANEL FOUND CORROSION. REPAIRED AS PER EA NR 1-5710-127459, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

17 FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT- OUT BETWEEN XORS 690 AND XORS 700. COMPLIED WITH EA 1-5710-127455, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 58,726 hrs · 11,729 cycles

09 FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT- OUT BETWEEN XORS 690 TO XORS 700. REAMED AND REPAIR CARRIED OUT AS PER EA 1-5710-127454, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE NR A. REPAIRED AS PER EA 1-5310-127450, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT WING UPPER SURFACE REAR SPAR CAP AT APPROXIMATELY XORS 1042 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT ON REWORK AREA AS PER EA NR 1-5710-128576. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT WING UPPER SURFACE TRAILING EDGE REAR SPAR AREA APPROXIMATELY XORS 981 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT ON REWORK AREA AS PER EA 1-5710-128576, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 58,726 hrs · 11,729 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT INBOARD LUG BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127449, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, FUSELAGE RIGHT MAIN FRAME STA 1681 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 58,726 hrs · 11,729 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT OUTBOARD LUG BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127449, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 300) · airframe 58,726 hrs · 11,729 cycles

RIGHT HORIZONTAL STABILIZER BODY FAIRING ENCLOSED AREA AT STA 2164 FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. REPAIR CARRIED OUT AS PER SRM 53-20-00 VOLUME I FIGURE 13. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, FUSELAGE LEFT LONGERON SPLICE AT STA 1651 LONGERON 13 FOUND CRACKED APPROXIMATELY 3 INCHES. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DRAWING AFA7181. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLE NR D.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 58,726 hrs · 11,729 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT LOWER SPOT FACE FOUND CORROSION. REWORKED AS PER SOPM 20-11-02. FOUND WITHIN LIMIT AS PER DRAWING NR ARC0502 AND CMM 57-44-08 FIGURE 604 REWORK LIMITS MINIMUM THICKNESS. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 58,726 hrs · 11,729 cycles

LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT LOWER SPOT FACE FOUND CORROSION. REWORKED AS PER SOPM 20-11-02. FOUND WITHIN LIMIT AS PER DRAWING NR ARC0503 AND CMM 57-44-09 FIGURE 601 REWORK LIMITS. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG INBOARD BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127448, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND ON FIRST AND SECOND LAYER WEB FROM TOP DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE NR D. REPAIRED AS PER EA 1-5310-127450, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, FUSELAGE RIGHT MAIN FRAME STA 1741 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) SIDE LINK ATTACHMENT SPOT FACE FOUND CORROSION. REWORKED AS PER SOPM 20-11-02. FOUND WITHIN LIMIT AS PER DRAWING ARC0502 AND CMM 57-44-08 FIGURE 604 REWORK LIMIT. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 58,726 hrs · 11,729 cycles

LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG INBOARD, BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127447, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1341, X = 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG OUTBOARD, BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127446, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1079, X = -8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 58,726 hrs · 11,729 cycles

RIGHT WING INBOARD FLAP, FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM CENTER TO OUTBOARD VANE TRACK. REMOVED AND REPLACED AS PER AMM 27-50-22-4. RT WING INBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND STISFACTORY.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES NR B AND NR C. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 5-65, X = -27.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 1661) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 1661, X = -47.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA 5-65, X = 27.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1, VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 58,726 hrs · 11,729 cycles

RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) ACTUATOR ATTACHMENT LUG INBOARD, BORE FOUND CORROSION. REWORKED AS PER EA 1-5750-127446, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,726 hrs · 11,729 cycles

CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES NR B AND NR C. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: RETAINER — CRACKED (EMERGENCY EXIT) · airframe 57,514 hrs · 11,472 cycles

LEFT FWD EMERGENCY EXIT HATCH, SEAL RETAINERS, TWO RETAINERS CRACKED REPLACED LOWER AFT AND LOWER FWD SEAL RETAINERS ON LT FWD EMERGENCY EXIT HATCH REF DWG 50-7978 AND SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR.

Part: LONGERON — CORRODED (WING TO BODY) · airframe 53,523 hrs · 10,632 cycles

RIGHT WING TO FUSELAGE BODY FAIRING LONGERON 27, STA 1305 FOUND WITH CORROSION. 09-11-07 RIGHT HAND WING TO FUSELAGE BODY FAIRING LONGERON REMOVED & REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — DAMAGED (LT WING) · airframe 53,523 hrs · 10,632 cycles

AFTER LEFT WING UPPER FUELTANK PANEL NR 531AT CUTOUT RUBSTRIP REMOVED. FOUND SKIN CUTOUT WITH 02 EACH DOUBLE HOLES. 09-11-07 COMPLIED WITH FEDEX E.A. 1-5710-115177, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: VANE — CORRODED (TE FLAP) · airframe 53,523 hrs · 10,632 cycles

LEFT WING, OUTBOARD FLAP VANE INSIDE OF LEADING EDGE ACCESS HOLE FOUND CORRODED. 09-11-07 REMOVED AND REPLACED AS PER AMM 27-50-32-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-32-5 FOUND SATISFACTORY. LH WING OUTBOARD FLAP OPERATION CHECK CARRIED OUT AS PER AMM 27-50-00-2 FOUND SATISFACTORY.

Part: STRAP — CRACKED (TE FLAP HINGE) · airframe 53,523 hrs · 10,632 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER FEDEX E.O. 1-5750-7-5004 PT1, REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRUCTURE — CHAFED (RT WING) · airframe 53,523 hrs · 10,632 cycles

RT WING FIXED LEADING EDGE BETWEEN XOS 680 TO XOS 717 FOUND CHAFING MARK. 09-11-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.15 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: LONGERON — CRACKED (FUSLEAGE) · airframe 53,523 hrs · 10,632 cycles

HFEC INSPECTION CARRIED OUT FOUND 01 EACH LOWER FASTENER HOLE ON THE LONGERON WITH CRACK INDICATION LOCATED NEAR THE RIGHT NOSE LANDING GEAR TRUNNION FITTING, APPROX TOTAL LENGTH OF 3/8 INCH LENGTH. 09-12-07 LONGERON LOCATED NEAR THE RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6 -2-100.

Part: STRUCTURE — CHAFED (RT WING) · airframe 53,523 hrs · 10,632 cycles

RIGHT WING FIXED LEADING EDGE XOS 717 TO XOS 774 FOUND CHAFED MARK. 09-11-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG.15 VOL. I.REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 53,523 hrs · 10,632 cycles

LEFT WING, NR 5 SLAT LEADING EDGE AREA FOUND WITH DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 5 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · airframe 53,523 hrs · 10,632 cycles

LEFT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STATION XORS 1042 FOUND CORRODED. COMPLIED WITH FEDEX E.A. 1-5710-115175, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,523 hrs · 10,632 cycles

HFEC INSPECTION CARRIED OUT FOUND 01 EACH LOWER FASTENER HOLE ON THE LONGERON WITH CRACK INDICATION LOCATED NEAR THE LEFT NOSE LANDING GEAR TRUNNION FITTING, APPROX TOTAL LENGTH OF 1/2 INCH LENGTH. 09-12-07 COMPLIED WITH FEDEX E.A. 1-5310-115173, REPAIR AND SRM 51-31-01 VOL.II. CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: FITTING — CRACKED (LT WING LE FLAP) · airframe 53,523 hrs · 10,632 cycles

LEFT WING, OUTBOARD FLAP LEADING EDGE STOP BOLT FITTING FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: DOUBLER — CRACKED (BS 1341) · airframe 53,523 hrs · 10,632 cycles

CENTER LANDING GEAR STATION 1341.0 RIGHT DOUBLER FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: DOUBLER — CRACKED (BS 1341) · airframe 53,523 hrs · 10,632 cycles

CENTER LANDING GEAR STATION 1341.0 LEFT DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SLAT TRACK — CRACKED (LT WING) · airframe 53,523 hrs · 10,632 cycles

LEFT WING, FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER FOUND CRACKED. 09-11-07 REPAIR CARRIED OUT AT LEFT HAND WING : FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER AREA AS PER SRM 57-10-00 FIG. 21 VOL I. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 53,523 hrs · 10,632 cycles

RIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 789 FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5710-115149, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CRACKED (FUSELAGE) · airframe 53,523 hrs · 10,632 cycles

NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. 09-11-07 NOSE LANDING GEAR LEFT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53-40- 00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG BAY) · airframe 53,523 hrs · 10,632 cycles

NOSE LANDING GEAR RIGHT TRUNNION FITTING SUSPECT CRACKED. 09-11-07 NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING REPAIR CARRIED OUT AS PER SRM 53- 40-00 FIG. 23 VOL I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 53,523 hrs · 10,632 cycles

RIGHT WING LEADING EDGE CAVITY STRINGER AT XOS 667 FOUND CRACKED. COMPLIED WITH FEDEX E.A. 1-5710-115147, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 53,523 hrs · 10,632 cycles

LEFT WING LEADING EDGE CAVITY AREA STRINGER AT STATION XOS 790 FOUND CRACKED. 09-11-07 COMPLIED WITH FEDEX EA. 1-5710-115148, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: ELEMENT — FAILED (APU COMPARTMENT) · airframe 51,845 hrs · 10,243 cycles

APU FIRE ALARM AND LIGHT CAME ON WITH APU FIRE LEVEL 3 ALERT AT 12000 FEET DESCENT ONTO FINAL APPROACH PULLED APU FIRE HANDLE AND DISCHARGED FIRE BOTTLE LIGHT WENT OUT AFTER 30 SECONDS BLEED AIR NR 2 AND NR 2 PACK AUTO SHUT DOWN. APU COMPARTMENT INSPECTION REVEALED NO SIGNS OF FIRE OR HOT AIR LEAK. APU WAS NOT RUNNING DURING OCCURRENCE. MAINTENANCE REPLACED NR 2 FIRE EXTINGUISHER BOTTLE AND APU FIRE DETECT ELEMENT LOOP B.

Part: WIRE — BURNED (ELECTRICAL) · airframe 50,381 hrs · 9,909 cycles

LEVEL-1 ALERT TANK 2L AFT PUMP LOW. TANK 2L LT AFT CB POPPED. REPLACED NR 2 L PUMP IAW MM 28-22-01-4 NO HELP. REMOVED ELC TERMINAL FROM R2-56 2X AND CB STAYED IN. REINSTALLED ORIGINAL NR 2 L PUMP IAW MM 28-22-01-4. FOUND ELECTRICAL WIRES BURNED UNDER THE FLOOR AT STA ABOUT 1 401. REPAIRED ELECTRICAL WIRES AND FSC R-T-S TEST PASSED IAW MM20-30-01-2 AND MM28-08-01-5. A/C OK FOR SVC.

Part: CADC — MALFUNCTIONED (NR 1) · airframe 48,744 hrs · 9,553 cycles

LOSS OF CADC 1 AFTER V1. RAN CLIST AND RETURN TO WSSS. REMOVED AND REPLACED NR 1 CADC AS PER MM 34-16-01-4, PERFORMED CADC NR 1 OPS TEST & CAT III RTS AS PER MM 34-16-01-5. PITOT STATIC TEST AS PER MM 34-11-00-2 CHK SATIS. A/C OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG 4059060-901.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 48,738 hrs · 9,547 cycles

CENTER LANDING GEAR LEFT AFT MOUNTING HOLE FOUND WITH CORROSION AFTER LANDING GEAR REMOVAL. COMPLIED WITH FEDEX EA 1-5340-94620, FUSELAGE ATTACH FITTINGS CTR. LANDING GEAR TRUNNION SUPPORT FITTING CORROSION REWORK. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 48,738 hrs · 9,547 cycles

FOUND CENTER LANDING GEAR LEFT AFT MOUNTING HOLE FOUND WITH CORROSION AFTER LANDING GEAR REMOVAL. COMPLIED WITH FEDEX EA 1-5340-94620, FUSELAGE - ATTACH FITTINGS CTR. LANDING GEAR TRUNNION SUPPORT FITTING CORROSION REWORK. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · corrosion level 2 · airframe 48,738 hrs · 9,547 cycles

CENTER LANDING GEAR LEFT MOUNTING AREA LOWER SURFACE FOUND WITH SURFACE CORROSION AFTER LANDING GEAR REMOVAL. COMPLIED WITH FEDEX EA 1-5340-94620 FUSELAGE ATTACH FITTINGS CTR. LANDING GEAR TRUNNION SUPPORT FITTING CORROSION REWORK. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: ROLLER — GOUGED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LEFT HAND WING, INBOARD FLAP AFT UPPER ROLLER FITTING FOUND WITH GOUGED MARK AFTER REMOVAL FOR ROLLER REPLACEMENT. GOUGED MARK ON LEFT HAND WING, INBOARD FLAP AFT UPPER ROLLER FITTING REMOVED AND NEW SHOULDER BUSHING FABRICATED AND INSTALLED PER FEDEX EA 1- 5750-94614, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - UPPER AFT ROLLER FITTING REPAIR. ORIGINAL HOLE DIAMETER = 0.937", REWORKED HOLE DIAMETER = 1.025". REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 300) · airframe 48,738 hrs · 9,547 cycles

LEFT HAND HORIZONTAL STABILIZER, CENTER PLANK UPPER SKIN AT STA XE=51.000 STRINGER 6, FOUND HOLE ELONGATED. COMPLIED WITH STEP 47 OF FEDEX EA 1-5510-94597.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,738 hrs · 9,547 cycles

FORWARD CARGO COMPARTMENT CEILING PANEL AREA, MAIN DECK SEAT TRACK AT STA 695.0, X= 27 SUSPECTED CRACKED. MAIN DECK SEAT TRACK AT STA 665.00 AND STA 745.00, X= 27 REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LEFT INBOARD TRAILING EDGE FLAP LOWER SURFACE FOUND WITH DENTS AT OUTBOARD MID AREA. REPAIRED AS PER SRM 57-10-00 VOLUME I, FIGURE 2. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT HAND WING NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING CUTOUT AREA UPPER CORNER CRACKED. CURRENT SRM REPAIR IS ONLY APPLICABLE FOR LOWER SURFACE AREA OF THE WING FIXED LEADING EDGE CUTOUT AREAS. COMPLIED WITH FEDEX EA 1-5740-94606.

Part: RIB — CRACKED (ZONE 300) · airframe 48,738 hrs · 9,547 cycles

WITH REFERENCE TO FEDEX EA 1-5510-94597, LEFT HAND HORIZONTAL STABILIZER FORWARD UPPER RIB CAP AT STA XE = 51.00 FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5510-94611.

Part: HINGE BRACKET — CORRODED (ZONE 300) · airframe 48,738 hrs · 9,547 cycles

INSTRUCTED TO REMOVE AND REPLACE INBOARD TRAILING EDGE FLAP OUTBOARD HINGE BRACKET WITH P/N: ARC2512-501 BUT ITEM CAME WITH P/N: ARC2512-1. REVISION B REVISES FEDEX EA 1-5750-79754A P2 BY DELETING REMOVAL AND REPLACEMENT REQUIREMENT, SCHEDULING PART II AND PART III WORK INSTRUCTIONS. REVISION WAS DUE TO BOEING COMMERCIAL AIRPLANE COMPANY PROVIDING DAMAGE TOLERANCE ANALYSIS APPROVING CONTINUED SERVICE OF EXISTING HINGES WITH INSPECTIONS PER AIRCRAFT AIRWORTHINESS LIMITATION INSPECTION. INITIAL INSPECTION REQUIRED AT 19,900 FC AND REPETITIVE INSPECTION AT 10,000 FC CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 48,738 hrs · 9,547 cycles

LEFT HAND WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER CRACKED. COMPLIED WITH FEDEX EA 1-5740-94607. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 300) · airframe 48,738 hrs · 9,547 cycles

EMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE FOUND CRACKED CORRECTIVE ACTION: SNRM NO.: N00958 - EMPENNAGE, FORWARD UPPER DOG HOUSE ENTRANCE, CUT OUT EDGE CRACKED AREA REPAIRED AS PER SRM 53-00-01 VOLUME I, FIGURE 5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RT WING, OB FLAP IB HINGE FITTING AT MOST OB LOWER BOLT HOLE FOUND WITH CRACK INDICATION. REPLACED AS PER AMM 27-50-30-4. OTBD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.

Part: DOOR — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RT WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER WITH APPROXIMATELY ONE (1) INCH CRACKED. COMPLIED WITH FEDEX EA 1-5740-94606.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,738 hrs · 9,547 cycles

FORWARD CARGO COMPARTMENT CEILING AREA, MAIN DECK SEAT TRACK STA 635, X = 8, FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,738 hrs · 9,547 cycles

FORWARD CARGO COMPARTMENT CEILING AREA, MAIN DECK SEAT TRACK STA 635, X = 27 FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,738 hrs · 9,547 cycles

FORWARD CARGO COMPARTMENT CEILING AREA, MAIN DECK SEAT TRACK STA 635, X = -8 FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CRACKED (LT WING) · airframe 48,738 hrs · 9,547 cycles

LEFT HAND WING, OUTBOARD FLAP INBOARD HINGE AT MOST OUTBOARD LOWER BOLT HOLE FOUND WITH CRACK INDICATION. COMPLIED WITH FEDEX EA 1-5750-94604.

Part: BRACKET — CRACKED (LT WING) · airframe 48,738 hrs · 9,547 cycles

LEFT HAND WING, LEADING EDGE RIB BRACKET LOWER AREA, STA XORS 538, OUTBOARD SIDE OF REFUEL ACCESS 519CB CUTOUT AREA FOUND CRACKED ARB1187-15. REMOVED AND REPLACED AS PER SRM 51-31- 01 VOLUME II. NEW FORMER FABRICATED AS PER DWG ARB2917. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: SKIN — UNKNOWN (HORIZ STAB) · airframe 48,738 hrs · 9,547 cycles

LEFT HAND HORIZONTAL STABILIZER, BARREL NUT AFT SKIN PLANK REPLACEMENT - TO COMPLY WITH FEDEX EA 1-5510-94597, SR11550010-77 STRINGER PANEL ASSY. COMPLIED WITH FEDEX EA 1-5510-94597.

Part: SKIN — UNKNOWN (HORIZ STAB) · airframe 48,738 hrs · 9,547 cycles

RIGHT HAND HORIZONTAL STABILIZER, BARREL NUT AFT SKIN PLANK REPLACEMENT - TO COMPLY WITH FEDEX EA 1-5510-94598 SR11550010-78 STRINGER PANEL ASSY. COMPLIED WITH FEDEX EA 1-5510-94598.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 44 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT WING TANK, APPROXIMATELY TEN (10) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 10 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LT WING TANK, APPROXIMATELY 10.5 INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 9 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LEFT WING TANK, APPROXIMATELY 2.5 INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 43 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LT WING TANK, APPROXIMATELY TEN (10) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 10 DURING HFEC INSPECTION. REPAIRED AS PER 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

FOUND LEFT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 16 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT WING TANK, APPROXIMATELY NINE (9) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 13 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT WING TANK, APPROXIMATELY TEN (10) INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 12 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LEFT WING TANK, APPROXIMATELY 10.5 INCHES LONG CRACK FOUND ON OUTBOARD END OF STRINGER 12 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,738 hrs · 9,547 cycles

LEFT WING TANK, APPROXIMATELY NINE (9) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 11 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 1A. CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 42 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,738 hrs · 9,547 cycles

RIGHT WING TANK, APPROXIMATELY ONE (1) INCH LONG CRACK FOUND ON OUTBOARD END OF STRINGER 43 DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 48,738 hrs · 9,547 cycles

FOUND UPPER CARGO COMPARTMENT, SEAT TRACK AT STA 775, X = 47 CRACKED. REPAIR CARRIED OUT BETWEEN STA 725 TO STA 755, X = 47 AS PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRACKET — MISALIGNED (ZONE 200) · airframe 43,871 hrs · 8,451 cycles

MAIN DECK, NEW ANGLE BRACKET P/N ADA3548-1 FOR INTERCOSTAL ADA8392-1 INSTALLATION AT STA Y= 775 TO STA Y= 791.75 LONGERON 7L FOUND MISALIGNED WITH FUSELAGE TRANSVERSE FRAME EXISTING HOLE. NEW ANGLE BRACKET FABRICATED PER DAC DWG ADA3852 AND PART MARKED P/N FX ADA3852-3 PER FEDEX GMM 7-0-1000. NEW ANGLE BRACKET INSTALLED PER FEDEX EO 1-5310-7-5002 REV 02 PART 2, FUSELAGE - MAINFRAME - INTERCOSTAL INSTALLATION INSPECTION/ PASSENGER TO FREIGHTER CONFIGURARTION DISCREPANCIES. COMPLIED WITH FEDEX EA 1-5310-74761, FUSELAGE - MAINFRAME - DEVIATION TO EO 1-5310-7- 5002.

Part: RELAY — DEFECTIVE (ZONE 200) · airframe 43,871 hrs · 8,451 cycles

CABIN EMERGENCY LIGHTING NOT ILLUMINATED WHEN SWITCHED (ON). CABIN EMERGENCY LIGHTING TROUBLESHOOTING CARRIED OUT IAW FIM 33-51-00. FOUND RELAY R2-5700 AT FAULT. REMOVED AND REPLACED RELAY R2-5700 IAW STANDARD WIRING PRACTICES. OPERATIONAL CHECK CARRIED OUT IAW AMM 33-52-01.

Part: SEGMENT — CORRODED (ZONE 400) · airframe 43,871 hrs · 8,451 cycles

ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE FOUND WITH CORROSION. ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE CORROSION REPAIR CARRIED OUT.

Part: STRUCTURE — CRACKED (TE FLAPS) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, INBOARD AFT HINGE LOCATION MID ATTACHMENT FITTING SUSPECTED CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30.

Part: LINE — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

CENTER CARGO COMPARTMENT, LT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, A CRACKED OF 1.1/8 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, 1 1/8 INCH CRACKED AT THE FUEL SHROUD LINE. REPAIRED PER FEDEX EA #1-2822-79763, FUEL SYSTEMS, FUEL SHROUDS AND DRAINS, CRACK REPAIR ON TUBE FOR TAIL TANK.

Part: LINE — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, A CRACKED OF 1 1/4 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, 1 1/4 INCH CRACKED AT THE FUEL SHROUD LINE REPAIRED PER FEDEX EA NR 1-2822-79763, FUEL SYSTEMS, FUEL SHROUDS AND DRAINS. CRACK REPAIR ON TUBE FOR TAIL TANK.

Part: LONGERON — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

CENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902 FOUND WITH CORROSION CRACK. CENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902. REMOVED PER SRM 53-10-00 VOLUME I. NEW LONGERON FABRICATED PER DRAWING NR: AFA7093. REPAIR SPLICE REWORKED PER SRM 51-31-01 VOLUME II. FABRICATED LONGERON AND REPAIR SPLICE. INSTALLED PER SRM 53-10-00 VOLUME I.

Part: FRAME — DENTED (ZONE 200) · airframe 43,871 hrs · 8,451 cycles

TRANSVERSE FRAME AT LT STA Y= 1721 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 FLIGHT CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-DTA.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.289, FINAL DIAMETER= 1.291. COMPLIED WITH FEDEX EA 1-5750-79749

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.251, FINAL DIAMETER= 1.314. COMPLIED WITH FEDEX EA 1-5750-79749,

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.

Part: HINGE — CORRODED (TE FLAP) · airframe 43,871 hrs · 8,451 cycles

RT WING, IB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER = 1.249, FINAL DIAMETER = 1.257. COMPLIED WITH FEDEX EA 1-5750-79749,

Part: FRAME — DENTED (ZONE 200) · airframe 43,871 hrs · 8,451 cycles

TRANSVERSE FRAME AT LT STA Y= 1701 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-DTA.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, IB FLAP, OB AFT HINGE PIVOT HOLE OB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03 PAGES 442 TO 443.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.403 INCH, REMAINING THICKNESS=0.400 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.190 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.504 INCH, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.006 INCH, AND REPAIRED AS PER EANR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: STOP FITTING — CRACKED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING FOUND CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, OB FLAP, IB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OB FLAP, OB AFT HINGE, IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.509 INCH, REMAINING THICKNESS=0.504 INCH, MATERIAL REMOVED=0.005 INCH, AND REPAIRED AS PER EA NR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.408 INCH, REMAINING THICKNESS=0.401 INCH, MATERIAL REMOVED=0.007 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

SNRM NR N0488- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA1-5750-79749.

Part: SPLICE — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 CRACKED. CRACKED AREA AT CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 TRIMMED OUT AS PER SRM 53-00-01 VOL I AND EA NR 1-5310-77963 FIGURE 2. REPAIR STRAP FABRICATED AND INSTALLED AS PER EA NR 1-5310-77963, TITLE: FUSELAGE, MAIN FRAME, CAC COMPARTMENT BODY STATION 6-100, LONGERON 38 (RT) SPLICE REPAIR.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.501 INCH, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

SNRM NR N0483 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: STRINGER — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

AFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L SPLICE FITTING. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

SNRM NR N0484 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, OB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

SNRM NR N0486- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA#1-5750-79749.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.405 INCH, REMAINING THICKNESS=0.402 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.505 INCH, REMAINING THICKNESS=0.502 INCH, MATERIAL REMOVED=0.003 INCG, AND REPAIRED AS PER EA NR 1-5750- 79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.188 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.405 INCH, REMAINING THICKNESS=0.396 INCH, MATERIAL REMOVED=0.009 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.400 INCH, REMAINING THICKNESS=0.391 INCH, MATERIAL REMOVED=0.009 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, IB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.095 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.503 INCH, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.005 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600)

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.089 INCH, FINAL DIAMETER=1.091 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 43,871 hrs · 8,451 cycles

LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.079 INCH, FINAL DIAMETER=1.081 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED.

Part: SPLICE — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

AFT CARGO, WASTE TANK LEFT AT STAY = 1988, STRINGER END NR 8 FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK LEFT AT STAY = 1988, STRINGER END NR 8 SPLICE FITTING REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

AFT CARGO, RT LONGERON SPLICE AT STA Y= 1855 TO Y= 1870, STRINGER 38R FOUND CRACKED. AFT CARGO, CRACKED RT LONGERON SPLICE AT STA Y= 1855 TO Y= 1870, STRINGER 38R REMOVED PER SRM 51-31-01 VOLUME I. SPLICE MACHINE, FABRICATED PER SRM 31-10-00 VOLUME I FIGURE 2. REPAIR SPLICE INSTALLED PER SRM 51-31-01 VOLUME II.

Part: LONGERON — CRACKED (ZONE 100) · airframe 43,871 hrs · 8,451 cycles

AFT CARGO, RT LONGERON 38R AT STA Y= 1860 FOUND CORRODED AND CRACKED. AFT CARGO, CORRODED AND CRACKED RT LONGERON 38R BETWEEN STA Y= 1787 AND Y= 1890, REMOVED PER SRM 51-31-01 VOLUME II. NEW LONGERON FABRICATED PER DWG AFA7093 AND PAINTED PER SRM 51-21-01 VOLUME II. FABRICATED LONGERON AND REPAIR PARTS INSTALLED PER SRM 51-31-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,871 hrs · 8,451 cycles

MAIN DECK, SEAT TRACK AT STA Y= 715, X= -7.5 FOUND BASE DAMAGED. MAIN DECK, DAMAGED SEAT TRACK REMOVED FROM STA Y= 655 TO STA Y= 735 X= -7.5 PER SRM 51-31-01. SEAT TRACK FABRICATED PER SRM 50-70-00 VOLUME I, FIGURE 1. SEAT TRACK INSTALLED PER SRM 51-31-01.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 43,871 hrs · 8,451 cycles

RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING CRACKED. RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING REMOVED AND REPLACED PER SRM 51-31-01 VOLUME 1.

Part: PUMP — INOPERATIVE (NR 3 HYD SYSTEM) · airframe 41,977 hrs · 8,015 cycles

IN CLIMB AT FL 350 HYD PUMP 3L OFF, ALERT ILLUMINATED FOLLOWED BY HYD PUMP 3R FAULT. ALERT WITH TEMP AMBER AT 97 DEG AND AMBER -T- ILLUMINATED ON BOTH PUMPS. BOTH PUMPS HAD OVERTEMPED. RELEASED FOR SERVICE PER MEL/CDL: 29-11-01-A, MEL 29-11-01-A: ENG NR 3 HYD PUMP INOP. PUMP REMOVED, RNR ENG NR 3 UPPER LEFT EDP PER MM REF 29-11-20-4-1.

Part: BULKHEAD — DAMAGED (NR 1 PYLON) · airframe 40,595 hrs · 7,719 cycles

MX REPORTED FINDING HYDRAULIC FLUID ACCUMULATED INSIDE OF THE NR 1 ENGINE PYLON DUE TO THE LEAK AT AUK7617-5001 HYDRAULIC LINE. HYDRAULIC LEAK WAS FIXED AND PYLON VISUALLY INSPECTED FOR INTEGRITY/SECURITY PRIOR TO ANC/LAX LEG. A FOLLOW UP CONDITIONAL INSPECTION FOR SUSPECTED TITANIUM MEMBERS THAT MIGHT HAVE OR WOULD MORE THAN LIKELY BECOME HYDROGEN EMBRITTLED DUE TO HOT HYDRAULIC FLUID CONTAMINATION WAS REQUESTED PER EA 1-5450-74134. REMOVED AND REPLACED NR 1 ENG PYLON BULKHEADS (4 EA) EA 1-5450-74184 STEPS 1 THRU 11. AIRCRAFT RELEASED FOR REVENUE SERVICE.

Part: WIRE HARNESS — BURNED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

HORIZONTAL STABILIZER CENTER SECTION TOP- WIRE BUNDLE AT THE RT INBOARD SIDE, INSIDE THE AFT FUSELAGE COMPT, FOUND BURNED AND DAMAGED DURING FSC RETURN-TO-SERVICE TEST.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 11R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 12R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 19R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: BRACKET — CORRODED (ZONE 500) · airframe 38,793 hrs · 7,292 cycles

LT WING O/B FLAP O/B HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLES 2EA CORRODED.O/B HINGE. LEFT O/B FLAP- O/B HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORROSION HOLES REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1- 5740-68587.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 34R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 29R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 25R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 3R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 22R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 9R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 21R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 18R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 38,793 hrs · 7,292 cycles

RT WING, O/B FLAP, I/B HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLES 2 EACH CORRODED. WINGS - RIGHT O/B FLAP, I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORROSION REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740- 68589.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 5R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 2R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 35R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 13R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 31R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 10R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 36R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 8R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 20R FOUND CORRODED AT THE BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 6R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 17R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 24R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 33R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 15R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 7R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 30R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 26R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 14R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: BRACKET — CORRODED (ZONE 500) · airframe 38,793 hrs · 7,292 cycles

LT WING OUTBOARD FLAP INBOARD HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLE AND LUG CORRODED. WINGS- LEFT O/B FLAP- I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED HOLE REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740-68588.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 28R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.COMPLIED WITH FEDEX EA 1-5510-67579.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 4R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 23R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 32R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 16R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 27R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 13L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 14L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 9L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 1R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 5L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 7L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 12L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: SKIN — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 17L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. SNRM N0676 - COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 31L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 6L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 10L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 34L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR30L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 15L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 4L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 3L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 8L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,793 hrs · 7,292 cycles

RTWING O/B FLAP I/B HINGE O/B LUG HOLE CORRODED. RIGHT O/B FLAP- I/B HINGE AFT SUPPORT BORE CORROSION REMOVED AND BUSHING REPAIRED AS PER FEDEX EA 1-5750-66818.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 36L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 28L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: HINGE — CORRODED (LT WING) · airframe 38,793 hrs · 7,292 cycles

LT WING O/B FLAP O/B HINGE I/B LUG HOLE (FLAP SIDE) CORRODED.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 11L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: HINGE — CORRODED (RT WING) · airframe 38,793 hrs · 7,292 cycles

RT WING FOUND OUTBOARD HINGE OUTBOARD HOLE CORRODED AFTER BUSHING REMOVAL.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 2L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 32L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,793 hrs · 7,292 cycles

LT WING O/B FLAP I/B HINGE (FLAP SIDE) O/B LUG HOLE CORRODED. LEFT O/B FLAP- I/B HINGE AFT SUPPORT BORE CORROSION REMOVED AND BUSHING REPAIRED AS PER FEDEX EA 1-5750-68586.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 16L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES. COMPLIED WITH FEDEX EA 1-5510-67579 STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 33L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: NUT — CORRODED (ZONE 300) · airframe 38,793 hrs · 7,292 cycles

LT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE, NR 29L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.

Part: STRUCTURE — CORRODED (ZONE 600) · airframe 38,793 hrs · 7,292 cycles

RT WING I/B FLAP O/B HINGE PIVOT HOLE LUG CORRODED. SNRM N0582 - RT WING I/B FLAP O/B HINGE PIVOT HOLE LUG HOLE OVERSIZED TO 1.250 INCH AS PER SRM 51-31-01 VOL II AND REPROTECTED AS PER SRM 51-21-01 VOL II. COMPLIED WITH FEDEX EA 1-5750-68593 WINGS- RIGHT INBOARD TRAILING EDGE FLAP- HINGE BRACKET CORRODED.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 38,793 hrs · 7,292 cycles

RT WING INBOARD FLAP TRACK AFT ATTACH POINT WITH 1 EA HOLE CORRODED.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 38,793 hrs · 7,292 cycles

RT WING INBOARD FLAP TRACK ATTACH POINTS 2 EA FOUND WITH CORROSION.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 38,793 hrs · 7,292 cycles

LT WING INBOARD FLAP TRACK 3 EA ATTACH POINTS FOUND WITH CORROSION.

Part: STRUCTURE — CORRODED (LT WING TE FLAP) · airframe 38,793 hrs · 7,292 cycles

FOUND LT WING OUTBOARD HINGE FLAP SIDE PIVOT HOLE CORRODED, AFTER REMOVAL OF BUSHINGS.

Part: HINGE — CORRODED (TE FLAP) · airframe 38,793 hrs · 7,292 cycles

LT WING OUTBOARD HINGE, FLAP SIDE PIVOT HOLE CORRODED AFTER REMOVAL OF BUSHINGS.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 38,793 hrs · 7,292 cycles

LT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE FOUND CRACKED, APPROXIMATELY 1 INCH IN LENGTH. LT WING L/E SLAT TRACK NR 16 RIB SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: SUPPORT — CRACKED (ZONE 600) · airframe 38,793 hrs · 7,292 cycles

RT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE, FOUND WITH CRACK APPROXIMATELY 1 INCH IN LENGTH.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,339 hrs · 6,243 cycles

RIGHT FUSELAGE BS 1841, S-39 TO 2-41 EXTERIOR SKIN DENTED. REMOVED AND REPLACED SKIN PER SRM 53-20-00 FIG 2.

Part: MANIFOLD — FAILED (BLEED AIR)

NR 2 MANIFOLD FAIL LEVEL 3 ALERT CAME ON. *S/D* COMING

Part: MANIFOLD — INOPERATIVE (NLG)

AFTER T/O, RETRACTED GEAR, NOSE WHEEL INDICATION WENT RED. GEAR WAS NOT UP. CYCLED GEAR WITH SAME RESULTS. THEN RETURNED TO SUBIC, GEAR SHOWED UNSAFE ON BOTH PRIMARY AND SECONDARY INDICATIONS. *S/D* REMOVED AND REPLACED NOSE LAND GEAR UNLOCK CYLINDER AND STEERING MANIFOLD PER IAW MM 32-35-06-4, 32-35-05-4.

Part: PACKING — LEAKING (ELEVATOR)

00-119 DURING CRUISE FLIGHT, RECEIVED HYD NR 2 OFF LEVEL 1 ALERT. R&R BOTH UPPER & LOWER ACCESS PANELS TO GAIN ACCESS TO LEFT INBD ELEVATOR ACTUATOR DUE TO LEAK. REPLACED WORN O RING PACKING (PN NAS1612-12 & BACK UP RING PN MS28774-119) LEAK CHECK. OPS CK OK REF MM 27-33-20.

Part: RETRACT MECH — LACK OF LUBE (NLG)

RETRACT LANDING GEAR ON CLIMBOUT, BOTH PRIMARY GEAR SHOW NOSE GEAR UNSAFE (RED). LUBED NOSE GEAR PER 12-21-03-3. JACKED MLG AND CYCLED 15 TIMES, 7 SEC TO RETRACT, 17 SEC TO EXTEND. WITHIN LIMITS PER 32-30-17-02.

Part: BUSHING — OVERSIZE (VERT STAB)

RT BANJO NR 4 FITTING AFT LWR FASTENER'S HOLE FOUND INSTALL WITH BUSHING OF DIAMETER 0.593 IN EXCEED MAX REWORK DIAMETER OF HOLE SIZE 0.450. REPAIRED FITTING AS PER EA 1-5530-47413 & EA 1-5530-47414.

Part: SEAT TRACK — CRACKED (BS 635)

MAIN DECK UPPER FUSELAGE, SEAT TRACK FOUND CRACK AT BS 635 X = 8.5 RT. CRACK LENGTH APPROX 3.4 IN. *S/D* REPAIRED AND INSTALLED PARTS, FABRICATED PER SRM 53-70-00 FIG 1 VOL.