N618FE

Part: POWER UNIT — FAILED (HUD) · airframe 84,963 hrs · 20,742 cycles

DURING PREFLIGHT , A STRONG ACRID SMELL WAS EVIDENT IN THE COCKPIT. TURNING ON PACKS DID NOT CHANGE THE SMELL. REMOVED AND REPLACED THE HUD OPU IAW AMM :31-82-02-4.COMPLIED WITH E..A. 1-3182- T0381273 REV NO. POS. P2. AND ALL C/B'S CLOSED. PERFORMED HUD TEST PASSED IAW AMM : 31-82-01-5. OIL TRACKING CLOSED. OK FOR SVC.

Part: DOUBLER — CHAFED (ZONE 100) · airframe 84,860 hrs · 20,728 cycles

FORWARD CARGO DOOR AFT JAMB EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION 1002.3, LONGERON -39 RIGHT TO LONGERON -44 RIGHT. FORWARD CARGO DOOR AFT JAMB AT STATION 1002.3, LONGERON -39 RIGHT TO LONGERON -44 RIGHT CHAFFED EXISTING REPAIR DOUBLER REPAIRED AS PER EA# 1-5330-T0313873 B P4 TITLE: FUSELAGE - PLATES & SKINS - FWD CARGO DOOR CUTOUT, AFT JAMB SRM REPAIR - DTA INSPECTIONS PER ALI/PSE. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600 FLAP) · airframe 84,860 hrs · 20,728 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) 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 EA # 1-5750- T0331061 D PART 3 STEP 1.G, TITLE : WINGS - FLIGHT SURFACES - RH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57503911 FOR DETAILS.

Part: HINGE BRACKET — CORRODED (ZONE 500 FLAP) · airframe 84,860 hrs · 20,728 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE #3) 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 EA # 1-5750- T0331060 C PART 3 STEP 1.G, TITLE : WINGS - FLIGHT SURFACES - LH WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57503912 FOR DETAILS.

Part: DOUBLER — CHAFED (ZONE 100) · airframe 84,860 hrs · 20,728 cycles

FORWARD CARGO DOOR FORWARD JAMB EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION 895.7, LONGERON -40 RIGHT TO LONGERON -41 RIGHT. FORWARD CARGO DOOR FORWARD JAMB AT STATION 895.7, LONGERON -40 RIGHT TO LONGERON -41 RIGHT CHAFFED EXISTING REPAIR DOUBLER REPAIRED AS PER EA# 1-5330-T0313T28 B P5 TITLE: FUSELAGE - PLATES & SKINS - FWD CARGO DOOR FWD JAMB, EXISTING SRM REPAIR - SRM 53-00-15 REPAIR 8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CHAFED (ZONE 100) · airframe 84,860 hrs · 20,728 cycles

CENTER CARGO DOOR - AFT DOOR JAMB EXISTING REPAIR DOUBLER FOUND CHAFFED AT STATION 1781, LONGERON -39 RIGHT TO LONGERON -42 RIGHT. CENTER CARGO DOOR - AFT DOOR JAMB AT STATION 1781, LONGERON -39 RIGHT TO LONGERON -42 RIGHT CHAFFED EXISTING REPAIR DOUBLER REPAIRED AS PER EA# 1-5330-T0313845 B P5 TITLE: FUSELAGE - PLATES & SKINS - BLENDOUT ON EXISTING SRM 53-00-15 REPAIR 8 AT CENTER LOWER CARGO DOOR AFT JAMB, STA 1781, L-39R TO L-42R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

AFT CARGO - STATION 1841 TO STATION 1967 X= -21 FLOOR SUPPORT TRACK FOUND CORROSION. AFT CARGO STATION 1841 TO STATION 1967 X= -21 FLOOR SUPPORT TRACK CORROSION REMOVED AS PER MD-11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00- 52-1A ALLOWABLE DAMAGE 1 FIGURE 101 SHEET 1. CORRODED FLOOR SUPPORT TRACK REMOVED AND REPLACED WITH NEW FLOOR SUPPORT TRACK AS PER AMM 20-50-02 AT AFT CARGO STATION 1841 TO STATION 1967 X= -21. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 795 X= -8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 795 X = -8.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 745 TO STATION 816 X = -8.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 84,860 hrs · 20,728 cycles

LEFT WING - NUMBER 12 SLAT TRACK CUTOUT OUTBOARD LOWER CORNER AT STATION XOS 777 FOUND CRACK. REPAIR CARRIED OUT AT LEFT WING - NUMBER 12 SLAT TRACK CUTOUT OUTBOARD LOWER CORNER AT STATION XOS 777 AS PER MD-11 SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1281 X=47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1281 X=47.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1247 TO STATION 1313 X=47.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1281 X=8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1281 X=8.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1265 TO STATION 1351 X=8.5 EXISTING SPLICE AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 755 X=27.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755 X=27.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 745 TO STATION 816 X=27.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1560 X= -47.5 FOUND CORRODED. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1560 X = -47.5 CORROSION FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 5-123 TO STATION 1571 X = -47.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X=47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X=47.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 6-0 TO STATION 6-60 X=47.5 AS PER MD11 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X=8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X=8.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 6-0 TO STATION 6-60 X=8.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 84,860 hrs · 20,728 cycles

LEFT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK ABOUT 2". CRACKED RIB DOUBLER AT LEFT WING - FIXED LEADING EDGE STATION XOS 789 REMOVED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING: ARB3954 REVISION K AND INSTALLED AS PER MD-11 SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 84,860 hrs · 20,728 cycles

MAIN DECK - CARGO COMPARTMENT SEAT TRACK AT STATION 1541 X=47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541 X = 47.5 CROWN WORN ON EDGE AREA REMOVED AS PER MD11 SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 5-123 TO STATION 1571 X = 47.5 AS PER MD11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600 LE) · airframe 84,860 hrs · 20,728 cycles

RIGHT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 1" INCH. CRACKED RIB DOUBLER AT RIGHT WING - FIXED LEADING EDGE STATION XOS 667 REMOVED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING: ARB3954 REVISION K AND INSTALLED AS PER MD-11 SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 600 LE) · airframe 84,860 hrs · 20,728 cycles

RIGHT WING - FIXED LEADING EDGE LOWER STIFFENER AT STATION XOS 542 FOUND CRACK ABOUT 1" INCH. CRACKED STIFFENER AT RIGHT WING - FIXED LEADING EDGE LOWER STATION XOS 542 REMOVED AS PER MD-11 SRM 51-31-01-0G. STIFFENER FABRICATED AS PER DOUGLAS DRAWING: ARB2918 REVISION G AND INSTALLED AS PER MD-11 SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CONTROL UNIT — FALSE ACTIVATION (NR 1) · airframe 84,504 hrs · 20,600 cycles

ON DEPARTURE AFTER APPROXIMATELY 5 MINUTES OF FLIGHT, RECEIVED #1 ENGINE FIRE LIGHTS AND BELL. NO OTHER FIRE INDICATIONS WERE PRESENT. AFTER RETARDING #1 THROTTLE TO IDLE (AS PER QRH), FIRE WARNINGS WENT AWAY AND DID NOT RETURN. FIRE SYSTEM TESTED AFTER EVENT AND TESTED GOOD. ENGINE WAS RETURNED TO FULL POWER WITH NO ADDITIONAL EVENTS. MEL 30JUL24 08:02 OAK RELEASED FOR SERVICE PER MEL : 26-11-01 CATEGORY : C EXPIRATION : 09AUG24 "MEL 26-11-01: ENG NO. 1 FIRE DETECTION LOOP A - INOP." RTS PASSED. REMOVED AND REPLACED #1 FDCU REF AMM 26-11-02-4. OPS CHECK GOOD.

Part: LAMP — NO TEST (R1 DOOR) · airframe 83,719 hrs · 20,411 cycles

R1 SLIDE PRESS TO TEST INOPERATIVE. RELEASED FOR SERVICE PER MEL : 25-61-02. R1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY." VERIFIED PRESSURE IS ADEQUATE. IDENTIFIED PARTS MD-11 SLIDE REMOTE PRESSURE. RELAMPED LENS AND NOW OP CKS NML.

Part: DOOR — UNKNOWN (UNKNOWN) · airframe 81,486 hrs · 19,859 cycles

RAMP REPORTED DAMAGE TO C-3 LOWER AFT EDGE OF OF CARGO DOOR AFTER LOADING. DAMAGE TO BOTTOM EDGE OF DOOR APPROX. 8 INCHES FWD OF AFT EDGE OF DOOR. APPROX .800 WIDE X .300 DEEP X .300 TEAR OUT DISPLACEMENT. SHGN 16MAY23 03:28 PDX U EA: 1-5330-T0374418 (PART 2) COMPLIED WITH EA REF ABOVE. INFO 16MAY23 12:11 MC1 R FERRY PERMIT 23-0015 ISSUED. EXPIRATION DATE: 05/18/23 KRIS ROUX/MOC UPDT 17MAY23 20:09 LAX U NRR: NO REFERENCE REQUIRED AIRCRAFT ARRIVED AT LAX/HVMX IS A SAFE SERVICEABLE CONDITION. REPAIRED DAMAGE IN REF MD11 SRM 52-30-16-2R FIG 201 REPAIR 3 AND EA# 1-5230-T0374504

Part: DOOR — DAMAGED (DOUG) · airframe 81,486 hrs · 19,859 cycles

MDIS 618 53-30 2587 14MAY23 PDX OPEN U RAMP REPORTED CENTER CARGO DOOR LOWER FOWARD DOOR EDGE DAMAGE AFTER LOADING AIRCRAFT. DAMAGE WITH TEAR OUT APPROX .700 WIDE X.300 DEEP X .300 PULL OUT GOUGE AT FWD LOWER RADIUS OF DOOR EDGE SHGN 16MAY23 03:22 PDX U EA: 1-5330-T0374418 (PART 1) COMPLIED WITH EA REF ABOVE. INFO 16MAY23 12:11 MC1 R FERRY PERMIT 23-0015 ISSUED. EXPIRATION DATE: 05/18/23 KRIS ROUX/MOC INFO 17MAY23 20:14 ** ATTACHED TO WORK ORDER 00086187 ** INFO 17MAY23 22:37 ** DETACHED FROM WORK ORDER 00086187 ** ADDED IN ERROR INFO 17MAY23 22:38 ** ATTACHED TO WORK ORDER 00086187 ** REPAIRED DAMAGE IN REFERENCE TO MD11 SRM 52-30-16-2R REPAIR 3 FIG 201. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 80,471 hrs · 19,571 cycles

FLOORBEAM BS 1887 CORRODED X- 47.5 TO X- 75.5. FOUND OUT OF LIMITS IAW SRM 53-00-00-2R FIGURE 202 SHEET 1 REPAIR GENERAL . FLOORBEAM REMOVED AND REPLACED IAW SRM 51-35-01-0G . FLOORBEAM FABRICATED IAW DRAWING AGA 7091 REVISION AL . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 80,471 hrs · 19,571 cycles

LEFT WING OUTBOARD LEADING EDGE COMPARTMENT ACCESS PANEL FORWARD CUTOUT DOUBLER FOUND CRACK AT APPROXIMATELY STATION XOS 787. CRACK AT LEFT WING OTRD LE COMPARTMENT ACCESS PANEL FORWARD CUTOUT DOUBLER APPROX XOS 787. CARRIED OUT REPAIR IAW SRM 57-4-01-2R, REPAIR 9, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 80,471 hrs · 19,571 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN SUSPECT CRACK AROUND THE FASTENER AT APPROXIMATELY STATION XOS 787. CRACK AT LEFT WING OTBD FIXED LE LOWER SKIN AROUND THE FASTENER APPROX XOS 787 CARRIED OUT REPAIR IAW SRM 57-40-01-2R, REPAIR 9 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (BS 1258) · airframe 80,471 hrs · 19,571 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE OVERWING FLOOR BEAM UPPER FLANGE AT STATION Y = 1258 X =111 FOUND CRACK INDICATION APPROXIMATELY 0.6" . FLOORBEAM REPAIRED IAW EA # 1-5310-T0371793 PART 1 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (BS 1275) · airframe 80,471 hrs · 19,571 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE OVERWING FLOORBEAM WEB AT STATION Y=1275 BETWEEN X=115 AND X = 116 FOUND CRACK INDICATION. FLOORBEAM REPAIRED IAW EA 1-5310-T0371857 PART 1 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1671 L52) · airframe 80,471 hrs · 19,571 cycles

LOWER CENTER CARGO BILGE AREA L52L FOUND WITH CORROSION AT BS 1671. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 205, SHEET 1. REPAIR CARRIED OUT IAW EA 1-5310-T0371796, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SPAR — CRACKED (TAIL NACELLE) · airframe 80,471 hrs · 19,571 cycles

ULTRASONIC INSPECTION CARRIED OUT ON RIGHT HAND SIDE UPPER SPAR ASSEMBLY OF THE TAIL PYLON AND FOUND 01 EACH CRACK INDICATION ON RADIUS AT PYLON UPPER CAP VERTICAL FLANGE STATION YID = 408.500 PROPAGATING FROM EDGE TOWARDS AFT DIRECTION APPROXIMATE 1/4 INCHES LENGTH. REPAIRED IAW EA 1-5451-T0371714, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — BROKEN (MAIN DECK CARGO) · airframe 80,471 hrs · 19,571 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 775 X = 75.5 CROWN FOUND BROKEN . MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 775 X = 75.5 BROKEN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A FIGURE 101 SHEET 1 ALLOWABLE DAMAGE 1 . SEAT TRACK REPAIR CARRIED OUT AT EXISTING SPLICE STATION 765 TO STATION 785 X = 75.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 11/16/2022

Part: SKIN — CRACKED (LT WING) · airframe 80,471 hrs · 19,571 cycles

03 EACH FASTENER HOLES #6 , #10 , #28 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 AND STATION XORS = 713.6. BUSHING REPAIR CARRIED OUT ON 03 EACH CRACKED FASTENER HOLES #6 , #10 , #28 AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 AS PER SRM 57-20-02-2R REPAIR 5 FIGURE 201 SHEET 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — BROKEN (BS 755) · airframe 80,471 hrs · 19,571 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 755 X = 75.5 CROWN FOUND BROKEN. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 80,471 hrs · 19,571 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 647 - 652 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER APPROXIMATE STATION XOS 647 - 652 AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — BROKEN (BS 775) · airframe 80,471 hrs · 19,571 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 775 X = 75.5 CROWN FOUND BROKEN. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 80,471 hrs · 19,571 cycles

RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN AT AROUND THE MOST OUTBOARD FASTENER HOLE AREA SUSPECT CRACK. REPAIR CARRIED OUT AT RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN AROUND THE MOST OUTBOARD FASTENER HOLE AREA AT XDLE = 325.114 AS PER SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 80,471 hrs · 19,571 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT SKIN DOUBLER AT APPROXIMATE STATION XOS 789 FOUND CRACKED. REMOVED AS PER SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DRAWING ARB3954 REVISION K AND INSTALLED AT RIGHT WING LEADING EDGE COMPARTMENT SKIN APPROXIMATE STATION XOS 789 SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — BROKEN (BS 755) · airframe 80,471 hrs · 19,571 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 755 X = -8.5 CROWN FOUND BROKEN. MAIN DECK CARGO COMPARTMENT FLOOR BROKEN SEAT TRACK CROWN AT STATION 755 X= - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT IN ACCORDANCE WITH SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101 SHEET 1. SEAT TRACK REPAIR CARRIED OUT AT EXISTING SPLICES AT STATION 745 TO STATION 785 X = -8.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 SHEET 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — BROKEN (BS 755) · airframe 80,471 hrs · 19,571 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 755 X = 27.5 CROWN FOUND BROKEN. MAIN DECK CARGO COMPARTMENT FLOOR BROKEN SEAT TRACK CROWN AT STATION 755 X = 27.5 EVALUATED AND FOUND EXCEEDED LIMIIT IN ACCORDANCE WITH SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101 SHEET 1.SEAT TRACK REPAIR CARRIED OUT AT EXISTING SPLICES STATION 745 TO STATION 825 X = 27.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201 SHEET 1 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 80,471 hrs · 19,571 cycles

02 EACH FASTENER HOLES #16 , #34 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. BUSHING REPAIR CARRIED OUT ON 02 EACH CRACKED FASTENER HOLES #16 , #34 AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 AS PER SRM 57-20-02-2R REPAIR 5 FIGURE 201 SHEET 3. INITIAL REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 80,471 hrs · 19,571 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 652-657 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER APPROXIMATE STATION XOS 652 - 657 AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 80,471 hrs · 19,571 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 789-795 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER APPROXIMATE STATION XOS 789 - 795 AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 80,471 hrs · 19,571 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELYSTATION XOS 901-906 FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER APPROXIMATE STATION XOS 901-906 AS PER SRM 57-40-01-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (BS 535 L33R) · airframe 80,471 hrs · 19,571 cycles

RIGHT HAND AIRCON COMPARTMENT SERVICE DOOR CUTOUT UPPER AFT CORNER FOUND CRACKED AT STATION 535 LONGERON 33 RIGHT. SKIN REPAIRED AS PER SRM 53-20-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (LT MLG) · airframe 80,471 hrs · 19,571 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AND FOUND 02EACH CRACK PROPAGATED FROM NOSE LANDING GEAR WHEEL WELL LEFT HAND TRUNNION FITTING LOWER AREA STATION 585 EXISTING TRIMMED OUT AREA APPROXIMATELY 0.2" AND 0.3. REPAIRED AS PER SRM 53-10-14-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CONTROL VALVE — MALFUNCTIONED (TE FLAPS) · airframe 79,279 hrs · 19,249 cycles

AFTER TAKE-OFF RECEIVED LVL 2 FLAP DISAG APPX 20 SECONDS AFTER THE FLAP HANDLE MOVED TO 0 DETENT POSITION. THERE WAS NO ROLLING MOTION & CONFIGURATION PAGE SHOWED FLAPS SYMMETRICAL & EXTENDED AT 17 DEGREES. IAW QRH PROCEDURE MATCHED FLAP HANDLE WITH THE INDICATED FLAP POSITION AS FLAPS CONTINUED TO RETRACT UNCOMMANDED WITH NORMAL HYD SYSTEMS. EVENTUALLY FLAPS RETURNED TO FLAPS UP POSITION UNCOMMANDED AND MATCHED THAT POSITION WITH THE FLAP HANDLE. ON LANDING WITH HANDLE IN THE FULL UP POSITION, FLAPS BEGAN AN UNCOMMANDED EXTENSION OVER A 15 MIN PERIOD TO 10 DEGREES WITH NORMAL HYD SYSTEMS. R & R INBD FLAP CONTROL VALVE IAW AMM 27-52-03-4. OPS CHECK GOOD IAW MM 27-50-00-5 TEST NR 11.

Part: SEAT TRACK — WORN (BS 740-770 LBL7) · airframe 77,300 hrs · 18,684 cycles

MAIN CABIN, FOUND DAMAGED SEAT -TRACK AT LBL 7 FROM STA. 740 TO 770 REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

MAIN DECK, CENTER OVER WING AT STATION BETWEEN 1219-1239, BETWEEN X=75.25- X=107.25 FOUND CORROSION. MAIN DECK, CENTER OVER WING AT STATION BETWEEN 1219-1239 BETWEEN X=75.25-X=107.25. CORROSION REMOVED AND REPAIRED, AS PER EA: 1-5730-T0357856 PART 1. TITLE: WINGS-PLATES AND SKINS-CORROSION FOUND ON CENTER WING UPPER FORWARD AND CENTER SKIN AT MULTIPLE LOCATIONS. REPAIR CLASSIFIED AS MINOR, PER GMM 6-2-100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM: N00994 FOR EA ATTACHED SIGNED OFF WORK DETAILS.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

MAIN DECK, CENTER OVERWING SKIN AT STATION BETWEEN 1219-1239, BETWEEN X= -75.25 TO X= -107.25 FOUND CORROSION. MAIN DECK, CENTER OVERWING SKIN AT STATION BETWEEN 1219-1239 BETWEEN X= -75.25 TO X= -107.25. CORROSION REMOVED AND REPAIRED, AS PER EA: 1-5730-T0357856 PART 1. TITLE: WINGS-PLATES AND SKINS-CORROSION FOUND ON CENTER WING UPPER FORWARD AND CENTER SKIN AT MULTIPLE LOCATIONS. REPAIR CLASSIFIED AS MINOR, PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 75,595 hrs · 18,230 cycles

06 EA FASTENER HOLES (NR 6, 9, 10, 11, 12 AND 36) FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6. RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6, 06 EA CRACK INDICATION FASTENER HOLES (NR 6, 9, 10, 11, 12 AND 36) BUSHING REPAIR CARRIED OUT, AS PER MD-11 SRM 57-20-02-2R, FIG 201 REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES BY HFEC INSPECTION, PER MD-11 SRM 57-20-02-2R FIG 202/REPAIR 5 TABLE 201. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 75,595 hrs · 18,230 cycles

06 EACH FASTENER HOLES (NR 6, 9, 10, 11, 12 AND 36) 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. RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=683.4 AND STATION XORS=713.6. 06 EACH CRACK INDICATION FASTENER HOLES (NR 6, 9, 10, 11, 12 AND 36). BUSHING REPAIR CARRIED OUT AS PER MD-11, SRM 57-20-02-2R, FIGURE 201, REPAIR 5. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT INSPECTION, PER MD-11, SRM 57-20-02-2R FIGURE 202/REPAIR 5, TABLE 201. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 75,595 hrs · 18,230 cycles

UNABLE TO DETERMINE THE CRACK END FOUND PROPAGATE ON THIRD FASTENERS FROM BELOW TOWARDS FIRST FASTENER AT STATION 2164 ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP DUE TO WEB BLOCKAGE. VERTICAL STABILIZER RIGHT HAND REAR SPAR FORWARD AND AFT FLANGE AT STATION 2164. REPAIR CARRIED OUT, AS PER EA 1-5530-T0357925 PART 1 TITLE: STABILIZERS-VERTICAL STABILIZER-CRACK FOUND AT REAR SPAR RT FWD FLANGE AT EXISTING SRM REPAIR AREA. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. REFER TO WRI: 55309651 FOR WORK DETAILS.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 75,595 hrs · 18,230 cycles

MAIN DECK, DURING OPEN UP ON FLOOR PANEL 272HF AT STATION 1481 TO STATION 5-32/5-53 RIGHT HAND FOUND EDGE DELAMINATED. DELAMINATED FLOOR PANEL 272HF AT MAIN DECK RIGHT HAND STATION 1481 TO STATION 5-32/5-53 REMOVED, AS PER AMM 53-21-09-4. FLOOR PANEL 272HF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 272HF INSTALLED, AS PER AMM 53-21-09-4. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 75,595 hrs · 18,230 cycles

EMPENNAGE, UPON REMOVAL FOR RIGHT HAND BANJO FITTING ACCESS REFERENCE (SPECIAL/NONROUTINE MAINTENANCE FORM N00613). FOUND LEFT HAND SIDE NUMBER 4 BANJO FITTING AT STATION 2164 LOWER VERTICAL STABILIZER FORWARD FLANGE CRACKED. LEFT HAND NUMBER 4 BANJO FITTING LOWER VERTICAL STABILIZER FORWARD FLANGE UPPER SPAR CAP STATION 2164 CRACKED APPROXIMATELY 3.50 INCHES TRIMMED, AS PER SRM 55-30-02-2R FIGURE 201 SHEET 2 REPAIR 5. REPAIR CARRIED OUT, AS PER SRM 55-30-02-2R FIGURE 204 REPAIR 5. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 5400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2700 FLIGHT CYCLES, AS PER SRM 55-30-02-2R TABLE 203 FIGURE 204 REPAIR 5. REQUIREMENT METHOD BY ULTRASONIC AND HIGH FREQUENCY EDDY CURRENT, PER SN10550000 REQUIREMENTS.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 75,595 hrs · 18,230 cycles

EMPENNAGE, UPON REMOVAL FOR BANJO FITTING REPAIR ACCESS, RIGHT HAND SIDE LOWER WEB PANEL FOUND WITH A CRACK LINE FROM CORNER EDGE AT STATION Y=2164. VERTICAL STABILIZER LOWER PYLON CARRY THRU REAR CENTER SPAR TO REAR SPAR RIGHT HAND SIDE LOWER WEB PANEL REPAIR CARRIED OUT, AS PER EA 1-5530-T0357937 PART1. TITLE: STABILIZERS-VERTICAL STABILIZER-FASTENER DEVIATION TO SRM 55-30-02 REPAIR 6-LOWER PYLON RT CARRY THRU REAR CENTER SPAR TO REAR SPAR WEB REPAIR. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 75,595 hrs · 18,230 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT STATION XOS 756. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT STATION XOS 756 REPAIR CARRIED OUT, AS PER MD11, SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — WORN (CABIN) · airframe 75,595 hrs · 18,230 cycles

CABIN RIGHT HAND STATION 6-10 X=27.5 SEAT TRACK CROWN FOUND WORN. CABIN, MAIN DECK AT RIGHT HAND SEAT TRACK STATION 6-10, X= -27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. WORN CROWN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 6-0 TO EXISTING SPLICES STATION 6-20, X= -27.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 75,595 hrs · 18,230 cycles

LEFT HAND FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT STATION XOS 757.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 75,595 hrs · 18,230 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT STATION XOS 862.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

CABIN RIGHT HAND STATION 1678 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN, MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1678, X= -8.5 CORROSION EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1671 TO STATION 1711, X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

MAIN DECK SEAT TRACK AT STATION 5-43 X= -8.5 FOUND CORROSION. CABIN, MAIN DECK AT SEAT TRACK STATION 5-43, X= -8.5 CORROSION EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 1531 TO STATION 1594, X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 75,595 hrs · 18,230 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT STATION XOS 586. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT STATION XOS 586 REPAIR CARRIED OUT, AS PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 75,595 hrs · 18,230 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT STATION XOS 669. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT STATION XOS 669 REPAIR CARRIED OUT, AS PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

CABIN LEFT HAND STATION 5-10 X=27.5 SEAT TRACK FOUND CORROSION. CABIN, MAIN DECK AT LEFT HAND SEAT TRACK STATION 5-10, X=27.5 CORROSION EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-0 TO EXISTING SPLICES STATION 5-40, X=27.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

MAIN DECK SEAT TRACK AT STATION 1386 X=8.5 FOUND CORROSION. CABIN, MAIN DECK AT SEAT TRACK STATION 1386, X=8.5 CORROSION EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1351 TO STATION 1431, X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 75,595 hrs · 18,230 cycles

MAIN DECK, FLOOR PANEL 281EF AT STATION 1741 TO STATION 1821 LEFT HAND FOUND DELAMINATED. DELAMINATED FLOOR PANEL 281EF AT MAIN DECK LEFT HAND STATION 1741 TO STATION 1821 REMOVED, AS PER AMM 53-21-09-4. FLOOR PANEL 281EF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRICATED FLOOR PANEL 281EF INSTALLED, AS PER AMM 53-21-09-4. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 75,595 hrs · 18,230 cycles

CABIN RIGHT HAND STATION 1438 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN, MAIN DECK AT RIGHT HAND SEAT TRACK STATION 1438, X= -8.5 CORROSION. EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1411 TO STATION 1451, X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK) · airframe 75,595 hrs · 18,230 cycles

MAIN DECK SEAT TRACK AT RIGHT HAND STATION 959 X= -8.5 FOUND CROWN WORN. CABIN, MAIN DECK AT RIGHT HAND SEAT TRACK STATION 959, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. WORN CROWN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 949 TO EXISTING SPLICES STATION 1029, X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 75,595 hrs · 18,230 cycles

CABIN LEFT HAND STATION 1468 X=8.5 SEAT TRACK FOUND CORROSION. CABIN, MAIN DECK AT LEFT HAND SEAT TRACK STATION 1468, X=8.5 CORROSION EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1431 TO EXISTING SPLICE STATION 1531, X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: WIRE HARNESS — FAILED · airframe 74,696 hrs · 18,011 cycles

AFTER TAKEOFF APPROXIMATELY 200 FT, ENGINE 2 ANTI ICE DUCT ILLUMINATED, FOLLOWED QRH & SHUTDOWN NR 2 ENG. RETURNED TO LAND. PERFORMED LEAK CHECK OF NR 2 ENG ANTI-ICE DUCT IAW AMM 30-22-09-5. NO LEAKS FOUND, PRESSURE HELD WITH NO LOSS. COMPLIED WITH FIM 30-22-07-00. ALL RESISTANCE CHECKS OVER DUCT LOOPS CHECKED GOOD. NO HIGH VOLTAGE FOUND ON PIN 5. R & R CFD CONTROLLER IAW AMM 30-22-10. INSTALLED NR 2 ENGINE CORE COMP. ELEC. CTL. HARNESS IAW AMM 71-50-04-4-1. OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (ENGINE ANTI ICE) · airframe 71,258 hrs · 17,031 cycles

PDIS 618 30-20 7669 16MAR19 MCI OPEN U PREVIOUS WRITEUP FOR "ENG 2 A-ICE DISAG", SHOULD HAVE BEEN "ENG 2 A-ICE OFF". THE DISAG LIGHT ON THE ENG 2 ANTI-ICE SWITCH ILLUMINATED AS A RESULT OF THE "OFF" ACTION DUE TO THE AIRCRAFT DETECTING A LEAK IN THE ENGINE 2 ANTI-ICE DUCT. SINCE THE MEL ACTION WIRED THE ANTI-ICE VALVE OPEN, THERE WAS NO WAY FOR THE AIRCRAFT TO PROTECT ITSELF. AFTER DISCUSSING WITH MOCC & GOCC, THE DECISION WAS MADE TO SHUTDOWN #2 ENGINE (WINDMILL FOR 25 MINUTES, AFTER 10 MINUTES AT IDLE) AND DIVERT TO KMCI. REMOVED AND REPLACED THE #2 ENGINE ANTI-ICE DUCT BURST DETECTION UNIT REFERENCE BOEING MD-11 AMM 30-22-10-4. FUNCTIONAL TEST OF THE #2 ENGINE COWL ANTI-ICE MANIFOLD FAILURE SENSING ELEMENT REFERENCE BOEING MD-11 AMM 30-22-11-720-801 GOOD.

Part: ANTI-ICE SYSTEM — UNKNOWN · airframe 71,258 hrs · 17,031 cycles

PDIS 618 30-20 7669 16MAR19 MCI OPEN U LOGPAGES:2999060 PREVIOUS WRITEUP FOR "ENG 2 A-ICE DISAG", SHOULD HAVE BEEN "ENG 2 A-ICE OFF". THE DISAG LIGHT ON THE ENG 2 ANTI-ICE SWITCH ILLUMINATED AS A RESULT OF THE "OFF" ACTION DUE TO THE AIRCRAFT DETECTING A LEAK IN THE ENGINE 2 ANTI-ICE DUCT. SINCE THE MEL ACTION WIRED THE ANTI-ICE VALVE OPEN, THERE WAS NO WAY FOR THE AIRCRAFT TO PROTECT ITSELF. AFTER DISCUSSING WITH MOCC & GOCC, THE DECISION WAS MADE TO SHUTDOWN #2 ENGINE (WINDMILL FOR 25 MINUTES, AFTER 10 MINUTES AT IDLE) AND DIVERT TO KMCI.

Part: LAMP — INOPERATIVE (PRESS TO TEST) · airframe 71,011 hrs · 16,945 cycles

PREFLT, RIGHT (R1) EVAC SLIDE REMOTE PRESS TO TEST INDICATING SYSTEM INOP. RELAMPED R1 DOOR EVAC SLIDE REMOTE PRESSURE TEST LIGHT IAW AMM 25-61-04-4. OPS CHECKS NORMAL.

Part: ENGINE — LEAKING (NR 2) · airframe 70,606 hrs · 16,835 cycles

PDIS 618 79-20 7309 05DEC18 SIN OPEN U LOGPAGES:1957706 # 2 LOW OIL QTY. WENT TO 1, SHUT DOWN #2 ENG RTN TO SINGAPORE . DECLARE EMERGENCY . AUTOLAND RWY 02C , CLR WIND 0.5007 KTS. INSTALLED #2 ENGINE PER W/C 71T0902-GE FACT 11DEC18 23:06 SIN COMPLIED WITH W/C 29T0302, W/C 7110000-00-90, W/C 7110000-00-91, W/C 7110000-10-99, W/C 79T0202, W/C 71T0101-GE. ENGINE RUN PERFORMED BY 244510 AS PER MD-11 JRH. OPS TEST PER AMM 71-00-00-700-809 FOUND SATIS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. BARREL NUT SURFACE REWORKED AS PER CMM 57-44-08 AND FOUND EXCEED LIMIT PER EA 1-5750-T0343585 P1 FIGURE 2. SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343585 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FINGER DOUBLER — DETACHED (RT WING) · airframe 70,605 hrs · 16,834 cycles

RIGHT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT ON STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — DETACHED (LT WING) · airframe 70,605 hrs · 16,834 cycles

LEFT WING FINGER DOUBLER FOUND DETACHED AT ISLAND UPPER SKIN OUTBOARD OF INBOARD AILERON AT STATION XW 375 AND E 65.00. REPAIR CARRIED OUT AT STATION XW 375, E 65.00 TO E 70.00 AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (TE FLAP) · corrosion level 2 · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE CORROSION. TEE FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343646 P1 STEP 1B. TRACK SUPPORT CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (TE FLAP) · corrosion level 2 · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE CORROSION. TEE FITTING 'E' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343646 P1 STEP 1A. TRACK SUPPORT CORROSION REPAIR AND INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (BS 383-420) · airframe 70,605 hrs · 16,834 cycles

FUSELAGE : FORWARD AVIONICS COMPARTMENT APPROXIMATELY STATION 383-420, X=90, MAIN DECK FLOOR STRUCTURE SUSPECTED CRACKED. FUSELAGE FORWARD AVIONICS COMPARTMENT APPROXIMATELY STATION 383 - 420 , X= 90 , MAIN DECK FLOOR SUPPORT REMOVED AND REPLACED AS PER MD 11 STRUCTURE REPAIR MANUAL 51-31-01-0G AND STRUCTURE REPAIR MANUAL 51-33-01-0G, FLOOR SUPPORT PART NUMBER : ABA 8304-501 FABRICATED BY MACHINING AS PER DOUGLAS DRAWING ABA 8304 REV B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. HOLE BORE (HOLE 3) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA #: 1-5750-T0331061 A P1 STEP 1F(1) AND STEP 1F(3) TITLE: WINGS - FLIGHT SURFACES - RT WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57506803 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE ( WING SIDE ) PIVOT HOLE BORE CORROSION. CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA # 1-5750-T0331060 A P1 STEP 1F(1) AND STEP 1F(3) TITLE: WINGS - FLIGHT SURFACES - LT WING - INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR - PSE 57.55.01.1 - ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57506788 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 1897) · corrosion level 2 · airframe 70,605 hrs · 16,834 cycles

MAIN DECK CARGO COMPARTMENT AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STATION 1897 X = 58. MAIN DECK CARGO AFT FLOOR PANEL SUPPORT AT STATION 1897, X = 58. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R, FIGURE 206. FLOOR PANEL SUPPORT AT STATION 1887 TO STATION 2007, X = 58 REMOVED AND REPLACED AS PER AMM 20- 50-02, FLOOR PANEL SUPPORT PART NUMBER : AGA 7551-503 FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA 7551 REV G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343585 P1 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE B AND A) 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 EA # 1-5750-128597 E PART 4 STEPS 2A AND 2B TITLE: WINGS - FLIGHT SURFACES - RH WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) REPAIR - PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57507289 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343585 P1 STEP 1C AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP INBOARD FOWARD HINGE (WING SIDE) PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 08.OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 08 AND EA.# 1-5750-T0343585 P1 STEP 1A AND STEP 1.TITLE: WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP INBOARD FOWARD HINGE (WING SIDE) FORWARD MOUNT INBOARD HOLE BORE (#6 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 EA.# 1-5750-T0343585 P1 STEP 1B AND STEP 1.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP INBD HINGE (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO EA.# 1-5750-T0343585 P1 AND SNRM N00396 FOR WORK DETAILS.

Part: BRACKET — CORRODED (TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT WING INBOARD FLAP DRIVE LINK IDLER BRACKET BORE FOUND CORROSION. IDLER BRACKET BORE REWORKED AS PER CMM 57-52-03 AND LOCAL BLEND AT 9' CLOCK POSITION INSIDE THE BORE HOLE FOUND EXCEED LIMIT AS PER BLUEPRINT LIMIT IN ACCORDANCE WITH EA 1-5750-T0343644 P1 FIGURE 1. REPLACEMENT BUSHINGS ARC3086-1 AND ARC3087-1 FABRICATED AND INSTALLED AS PER EA 1-5750-T0343644 P1 STEP 1, 2 AND STEP 5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) 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 EA # 1-5750-128597 E PART 4 STEPS 2A AND 2B TITLE: WINGS - FLIGHT SURFACES - RH WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) REPAIR - PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REFER TO WRI: 57507289 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE COROSION CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE B AND A) 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 EA # 1-5750-128598 C PART 5 STEP 2A AND STEP 2B TITLE: WINGS - FLIGHT SURFACES - LH WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) REPAIR - PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57507288 FOR WORK DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REOWRKED 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 EA # 1-5750-128598 C PART 5 STEP 2A AND STEP 2B TITLE: WINGS - FLIGHT SURFACES - LH WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) REPAIR - PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57507288 FOR WORK DEATILS.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 70,605 hrs · 16,834 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT RIGHT HAND STATION 6-05, X = - 47.5. DAMAGED CROWN EDGE SMOOTHEN OUT AND FOUND EXCEED LIMIT PER STRUCTURE REPAIR MANUAL 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 6-20 TO EXISTING SPLICE STATION 6-0, X= -47.5 PER STRUCTURE REPAIR MANUAL 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 70,605 hrs · 16,834 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 5-05, X = 47.5. SEAT TRACK DAMAGED CROWN EDGE SMOOTHED OUT AND FOUND EXCEED LIMIT PER STRUCTURE REPAIR MANUAL 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACMENT FROM STATION 5-20 TO EXISTING SPLICE STATION 5-0, X = 47.5 PER STRUCTURAL REPAIR MANUAL 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) PIVOT HOLE BORE (#4 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 EA.# 1-5750-128595 A P2 STEP 2B AND STEP 2.TITLE: WINGS- FLIGHT SURFACES- EO 1- 5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE CORROSION. CORROSION AT RIGHT OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND EA #: 1- 5750-128596 B P2 STEP 1 TITLE: WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750- 7-5002 - RH WING - OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-128596 B P2 AND SNRM N00328 FOR WORK DETAILS.

Part: REPAIR — DENTED (FUSELAGE) · airframe 70,605 hrs · 16,834 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT RIGHT HAND STATION 1681, LONGERON 12R. FRAME EXISTING REPAIR DENTED AT RIGHT HAND STATION 1681, LONGERON 12 RIGHT. CARRIED OUT REPAIR AS PER STRUCTURE REPAIR MANUAL 53-00-07-2R FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE (#7 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 EA # 1-5750-128596 B P2 STEP 1 TITLE: WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-128596 B P2 AND SNRM N00328 FOR WORK DETAILS.

Part: REPAIR — DENTED (FUSELAGE) · airframe 70,605 hrs · 16,834 cycles

CABIN- MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT LEFT HAND STATION 1701 , LONGERON 12 LEFT. CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT LEFT HAND STATION 1701, LONGERON 12 LEFT, CARRIED OUT REPAIR AS PER MD11 STRUCTURE REPAIR MANUAL 53-00-07-2R FIGURE 201 REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 14,500 FC AFTER REPAIR COMPLETION AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 9,500 FC AS PER STRUCTURE REPAIR MANUAL 53-00-07-2R TABLE 201/REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE (#7 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 EA #: 1-5750-128596 B P2 STEP 1 TITLE: WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-128596 B P2 AND SNRM N00328 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (#3 BORE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND EA #: 1-5750-128596 B P2 STEP 1 TITLE: WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-128596 B P2 AND SNRM N00328 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE CORROSION. CORROSION AT RIGHT OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM 57-44-09 AND EA #: 1- 5750-128596 B P2 STEP 1 TITLE: WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750- 7-5002 - RH WING - OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750-128596 B P2 AND SNRM N00328 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-09 AND EA #: 1-5750-128596 B P2 STEP 1 TITLE: WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-08 AND EA #: 1-5750-T0343637 P1 STEP 2A AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1- 5750-7-5002 - RH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

RIGHT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (#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 EA #: 1-5750-T0343637 P1 STEP 2B AND STEP 2 TITLE: WINGS - FLIGHT SURFACES - EO 1-5750-7-5002 - RH WING - OUTBD FLAP, INBD FWD HINGE (WING SIDE) - CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA #: 1-5750- T0343637 P1 AND SNRM N00283 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMM 57-44-09.SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-09 AND EA.# 1-5750-128595 A P2 STEP 2A AND STEP 2.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) - CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO EA.# 1-5750- 128595 A P2 AND SNRM N00344 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT LEFT HAND OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE (#7 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 EA.# 1-5750-128595 A P2 STEP 2C AND STEP 2.TITLE: WINGS- FLIGHT SURFACES- EO 1-5750-7-5002- LH WING- OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO EA.# 1-5750-128595 A P2 AND SNRM N00344 FOR WORK DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND WING LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 789 -795 FOUND CRACK. REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 789 - 795 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 70,605 hrs · 16,834 cycles

LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 661- 667 FOUND CRACK. REPAIR CARRIED OUT ON LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 661 - 667 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 70,605 hrs · 16,834 cycles

LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 495 - 500 FOUND CRACKED AS MARKED. REPAIR CARRIED OUT ON LEFT HAND WING OUTBOARD LEADIING EDGE SKIN BEADED DOUBLER AT STATION XOS 495 - STATION XOS 500 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 70,605 hrs · 16,834 cycles

LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 728 - 734 FOUND CRACK AS MARKED. REPAIR CARRIED OUT ON LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 728 - 734 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (TE FLAP) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. STOP FITTING ON LEFT HAND WING OUTBOARD FLAP AT STATION XOVH 537 REMOVED AND REPLACED AS PER MD11 SRM 51-33-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 70,605 hrs · 16,834 cycles

LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 615-625 FOUND CRACK. REPAIR CARRIED OUT ON LEFT HAND WING OUTBOARD LEADING EDGE SKIN BEADED DOUBLER AT STATION XOS 615 - 625 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,293 hrs · 16,748 cycles

FUSELAGE SKIN CORROSION AT STA 2122-2163 LONGERON 33R-35. COMPLY WITH EA 1-5310-T0342510 REV NR POS P1. COMPLIED WITH T1-5310-T0342510P1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,293 hrs · 16,748 cycles

MDIS 618 53-30 7104 20SEP18 MEM FACT U DURING WALK AROUND FOUND POSSIBLE CRACK IN THE NR 1 PACK BAY CUT OUT ON UPPER AFT CORNER. INFO 20SEP18 21:14 FACT 25SEP18 07:14 MEM U COMPLETED REPAIR OF NR 1 PACK DOOR IN REF TO SRM 53-20-15-2R. COMPLIED WITH EA 1-5330-T0342533 PART 1 FOR TRACKING ONLY. REPAIRED REF SRM 53-20-15 2R FIG 201 REPAIR 3.

Part: DOOR — CRACKED (AIR CON BAY) · airframe 70,293 hrs · 16,748 cycles

DURING WALK AROUND FOUND POSSIBLE CRACK IN THE #1 PACK BAY CUT OUT ON UPPER AFT CORNER. INFO 20SEP18 21:14 COMPLETED REPAIR OF #1 PACK DOOR IN REF TO MD11 SRM 53-20-15-2R. COMPLIED WITH EA# 1-5330-T0342533 PART 1 FOR TRACKING ONLY. REPAIRED REF MD11 SRM 53-20-15 2R FIG 201 REPAIR 3.

Part: CYLINDER — INOPERATIVE (MLG HANDLE) · airframe 69,980 hrs · 16,684 cycles

LANDING GEAR HANDLE WOULD NOT RETRACT AFTER TAKE-OFF. RAN QRH CHECKLIST, PROBLEM REMAINED. RETURNED TO DEPARTURE, LANDING UNEVENTFUL. R & R THE TRUCK BEAM TRIM CYLINDER FUSE IAW AMM 32-37-06-4-0. OPS CHECKED NORMAL IAW AMM 32-37-00-5. NO LEAKS NOTED. GEAR HANDLE MOVES TO UP POSITION.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 69,087 hrs · 16,417 cycles

L1 DOOR PRESSURE LOW, SERVICED THE DOOR IAW 12-25-04-3. OK FOR CONTINUE SERVICE.

Part: CONNECTOR — BROKEN · airframe 69,064 hrs · 16,405 cycles

FIRST OFFICER`S WINDSHIELD FOGGED UP AND ICED UP. UNABLE TO WIPEOUT. FOUND THE SUPRESSOR PIG TAIL BROKEN AT TERMINAL AT LOWER R CORNER OF WINDSHIELD. DISCONNECTED THE BROKEN SUPRESSOR AND CONNECTED A NEW SUPRESSOR IAW AMM 30-41-02-4-0.

Part: HINGE — DAMAGED (DOOR) · airframe 68,701 hrs · 16,306 cycles

FOUND MC DOOR HINGES TO HAVE WEAR ON HINGE LUGS AND PITTING BEYOND SRM LIMITS 51-31-01. REPLACED MCD HINGE SECTIONS IAW SRM 51-31-01. REPLACED MCD HINGE SECTIONS AS PER SRM 51-31-01 ALL REPAIRS COMPLIED WITH HINGE SECTIONS PAINTED IAW SRM 51-21-02. ALL INSPECTIONS OF REPAIR COMPLIED WITH IAW QC.

Part: DOOR SILL — WORN (N/A) · airframe 68,701 hrs · 16,306 cycles

SMIS 618 53-10 6121 18FEB18 MEM OPEN U MOD TYPE T MOD NO. 1-5310-T0338478 REV NO. PS P1 FUSELAGE - MAIN DECK CARGO DOOR JAMB WORN HOLES ON MAIN DECK CARGO DOOR FOR COMPLY WITH E..A. 1-5310-T0338478 REV NO. POS. P1 REAMED HOLE ON THE FIRST TWO LUGS ON THE FWD A/C FUSELAGE SIDE HINGE FITTING OVER THE CMM REPAIR LIMITS OF .462. NE DIAMETER OF LUGS BORE IS .470, AND BUSHED BACK DOWN TO FACTORY DIMENSION. PER FEDEX E.A. 1- 531-T0338478 P1.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 68,701 hrs · 16,306 cycles

MAIN DECK CARGO DOOR JAMB WORN HOLES ON MAIN DECK CARGO DOOR FOR COMPLY WITH EA 1-5310-T0338478 REV NO. POS P1. REAMED HOLE ON THE FIRST TWO LUGS ON THE FWD A/C FUSELAGE SIDE HINGE FITTING OVER THE CMM REPAIR LIMITS OF .462. NE DIAMETER OF LUGS BORE IS .470, AND BUSHED BACK DOWN TO FACTORY DIMENSION PER EA 1- 531-T0338478 P1.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 68,354 hrs · 16,206 cycles

L1 DOOR PRESSURE GAUGE READING LOW. SERVICED L1 DOOR PNEUMATIC BOTTLE IAW AMM 12-25-04-3.

Part: DISPLAY — DAMAGED · airframe 68,220 hrs · 16,165 cycles

CAPT MCDU LOSE POWER WITH ASSOCIATED SMOKE IN COCKPIT. SMOKE DISAPPEARED AFTER ABOUT 5 MINS. MCDU POWER SELF RESTORED APPROXIMATELY 20 MINS AFTER INITIAL POWER LOSS. MCDU LOST POWER APPROXIMATELY 3 MORE TIMES UNTIL PARKED AT THE GATE. INSPECTED ELECTRICAL COMPT AREA, CENTER PEDESTAL AREA AND COCKPIT AREA AND ALSO,ALL ELECTRICAL WIRE WERE NORMAL , NO FIRE EVIDENCE AND NO C/B POPPED OUT. R/R'D CAPT MCDU AND TEST PASSED PER AMM 31-65-01-4. PERFOREMD RTS OF A/T AND PASSED PER AMM 22-00-07-5. E/E COMPT COOLING SYSTEM AND ESC TEST PASSED PER AMM 21-08-01-5. A/C OK FOR SERVCIE. PART NAME : MCDU MANUFACTURER : HONEYWELL P/N : 4059051-904 S/N : 98041004

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 67,366 hrs · 15,927 cycles

EMERGENCY LIGHT TEST FAILED WITH EMERGENCY LIGHT BATTERY 1 LOW. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4, TESTED OK IAW AMM 33-50-00-5. ACFT OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 66,150 hrs · 15,525 cycles

1L ACCUMULATOR BOTTLE LOW ON PREFLIGHT. SERVICED L1 DOOR ACCUMULATOR IAW AMM 12-25-04-3.

Part: WASHER — MISSING (TAILCONE LATCH) · airframe 65,911 hrs · 15,460 cycles

WHILE IN A TURN TO FINAL APPROACH, HAD A LEVEL 2 TAILCONE UNLOCK ALERT. LASTED A FEW SECONDS AND THEN EXTINGUISHED FOR THE REMAINDER OF THE FLIGHT. INSPECTED RIGHT TAILCONE LATCH CAM FOLLOWER ASSY. FOUND THE INSTALLATION HAD MISSING WASHERS. THE CAM ARM HAS THE SAME LATERAL PLAY AT THE LEFT SIDE. REASSEMBLED LEFT AND RIGHT CAM ASSEMBLIES IAW AMM 53-52-01-5. PERFORMED TAILCONE LATCH ADJUSTMENT IAW AMM 53-52-01-5. CLOSED TAILCONE IAW AMM 53-52-01-2. TAILCONE NOW FULLY SEATS ON LEFT AND RIGHT SIDE OF FUSELAGE. TAILCONE UNLOCK ALERT EXTINGUISHED.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · airframe 65,752 hrs · 15,406 cycles

CORROSION ON HORIZONTAL STAB BARREL NUT HOLE AT LOWER CAP HSS 44.56. ACCOMPLISHED A REPAIR IAW EA 1-5510-T0330176 PT1.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED IN THREE BAYS AT XOS 632 - 639. NDT VERIFIED A CRACK AT LT WING FIXED L/E BEADED DOUBLER. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-40-02-2R, FIG 203.

Part: DOUBLER — CORRODED (BS 1305) · airframe 65,752 hrs · 15,406 cycles

MAIN CARGO BAY, L3 DOOR, AFT LWR CUTOUT DOUBLER HAS CORROSION. REMOVED CORROSION AT BS 1305 IAW SRM 53-40-15-2R, FIG 201, SHEET 3. REPAIRED AREA IAW EA 1-5330-T0330025 P1.

Part: ATTACH FITTING — CORRODED (LT AILERON) · airframe 65,752 hrs · 15,406 cycles

AFTER REMOVING BALANCE WEIGHTS FROM LT AILERON FOUND NUMEROUS WEIGHT ATTACH FITTINGS WITH CORROSION/PITTING. REMOVED UNSERVICEABLE LT O/B AILERON AND INSTALLED SERVICEABLE LT O/B AILERON IN REF TO AMM 27-10-30-4 AND PERFORMED OPERATIONAL TEST AND RANGE OF MOVEMENT OF LT AILERON IN REF TO AMM 27-10-00-710-802, OPERATIONAL TEST AND RANGE MOVEMENT GOOD.

Part: FLOORBOARD — CANNING (CARGO BAY) · airframe 65,752 hrs · 15,406 cycles

OIL CAN EFFECT (OIL CANNING) ON UPPER DECK CARGO BAY FLOOR PANEL LOCATED JUST AFT OF R4 DOOR PLUG. REMOVED FLOOR PANEL 292EF IN REF AMM 53-21-04-4. FABRICATED FLOOR PANEL 292EF IN REFERENCE DWG SRZ-25-005. INSTALLED FLOOR PANEL 292EF IN REF AMM 53-21-04-4.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,752 hrs · 15,406 cycles

MAIN CARGO COMPARTMENT L3 DOOR JAMB, AFT LWR TORSION BOX HAS WEB CRACKED. REPAIRED MAIN COMPARTMENT L3 DOOR JAMB PER SRM 53-40-15-2R, FIG 201, REPAIR 3.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,752 hrs · 15,406 cycles

MAIN CARGO COMPARTMENT R3 DOOR JAMB, AFT LWR TORSION BOX HAS WEB CRACKED, AS MARKED. REPAIRED MAIN CARGO COMPARTMENT R3 DOOR JAMB PER SRM 53-40-15-2R, FIG 210, REPAIR 3.

Part: SKIN SPLICE — CRACKED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RT WING FIXED L/E SKIN SPLICE ANGLE IS CRACKED AT XOS 584. REMOVED AND REPLACED RT WING FIXED L/E SKIN SPLICE ANGLE AT XOS 584 IAW SRM 51-33-01-0G, 51-35-01-0G, 51-31-01-OG.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LT O/B WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACK IN 2EA BAYS AT APPX XOS STA 650- XOS 654. REPAIRED LT O/B WING FIXED L/E COMPARTMENT BEADED DOUBLER BETWEEN XOS STA 650- XOS 654 PER SRM 57-40-02-2R, REPAIR 15, FIG 203, 51-21-01-0G, 51-35-01-0G.

Part: SUPPORT — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LT O/B WING FIXED L/E COMPARTMENT SUPPORT STRUCTURE CRACKED AT APPX XOS STA 1024. DISCONNECTED LT WING L/E 8 EXTEND SLAT DRIVE CABLE AT STA XOS 1024 PER AMM 20-20-05-2, AMM 91-11-05-2 FOR ACCESS, REPLACED SUPPORT P/N ARB2920U13 PER SRM 51-31-01-0G, RECONNECTED AND TENSIONED 8 SLAT DRIVE CABLE AT STA XOS 1024 PER AMM 20-20-05-2.

Part: SPAR CAP — CORRODED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RT WING UPPER REAR SPAR, UPPER SURFACE OF SPAR CAP REAR FLANGE, XORS 1030- XORS 1042 HAS CORROSION 4EA AREAS, MARKED IN RED 77-38. ACCOMPLISHED REPAIR IN REFERENCE EA 1-5710-T0330116 AT RT WING UPPER REAR SPAR, UPPER SURFACE OF SPAR CAP REAR FLANGE, XORS 1030- XORS 1042.

Part: SUPPORT — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LT O/B WING FIXED L/E COMPARTMENT RIB CHORD SUPPORT CRACK AT APPROX XOS STA 666. REPAIR RIB CHORD SUPPORT ON LT O/B WING FIXED L/E COMPARTMENT CRACK AT APPROX XOS STA 666 IAW MD-11 SRM 57-40-03-2R.

Part: SKIN SPLICE — CRACKED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RT WING FIXED L/E SKIN SPLICE ANGLE IS CRACKED AT XOS 584. REMOVED AND REPLACED RT WING FIXED L/E SKIN SPLICE ANGLE AT XOS 584 IAW SRM 51-33-01-0G, 51-35-01-0G , 51-31-01-OG.

Part: SUPPORT — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LEFT WING INBD FIXED L/E COMPARTMENT, PANEL LANDING SUPPORT IS CRACK ON THE I/B SIDE OF THE PYLON. REMOVED AND REPLACED THE SUPPORT IAW DWG ARB1161, AND SRM 51-31-01-0G.

Part: FRAME — CRACKED (BS 469) · airframe 65,752 hrs · 15,406 cycles

FRAME IS CRACKED INSIDE FWD AVIONICS BAY AT BS 469.173 . REPAIRED IAW SRM 53-10-07-2R FIG 210.

Part: SUPPORT — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LEFT WING FIXED L/E PANEL SUPPORT CRACKED AT XOS 540. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-33-01-0G AND SRM 51-35-01.

Part: STRINGER — CRACKED (RT WING LE) · airframe 65,752 hrs · 15,406 cycles

RIGHT WING FIXED L/E STRINGER IS CRACKED BETWEEN XOS 661 - 661. REPAIRED THE STRINGER IAW SRM 57-40-03-2R.

Part: FRAME — CRACKED (BS 469) · airframe 65,752 hrs · 15,406 cycles

FRAME IS CRACKED INSIDE FWD AVIONICS BAY AT BS 469.173. REPAIRED IAW SRM 53-10-07-2R, FIG 201.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 65,752 hrs · 15,406 cycles

LEFT INBD FLAP VANE, UPPER T/E SURFACE CHAFED AT INBD END. REPAIRED AND APPLIED EXTERIOR COATINGS IAW SRM 57-50-80. REPAIR 2, PARA 2.

Part: DOUBLER — CRACKED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 493- 500. REPAIRED IAW SRM 57-40-02-2R, FIG 203.

Part: DOUBLER — CRACKED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RIGHT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 560. REPAIRED IAW SRM 57-40-02-2R.

Part: DOOR FRAME — CRACKED (BS 1250-1256) · airframe 65,752 hrs · 15,406 cycles

R3 DOOR FRAME FWD UPPER WEB IS CRACKED ON THE AFT END, ACCOMPLISHED REPAIR ON R3 DOOR JAMB FWD UPPER WEB IAW EA 1-5310-T329909 P1.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED AT XOS 587. REPAIRED IAW SRM 57-40-02-2R, FIG 203.

Part: DOUBLER — CRACKED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RIGHT WING FIXED L/E BEADED DOUBLER AT XOS 648 - 703 HAS NUMEROUS CRACKS, REPAIRED IAW SRM 57-40-02-2R, FIG 203.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,752 hrs · 15,406 cycles

LEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED AT XOS 544. REPAIRED IAW SRM 57-40-02-2R, FIG 203.

Part: DOUBLER — CRACKED (RT WING) · airframe 65,752 hrs · 15,406 cycles

RIGHT WING FIXED L/E BEADED DOUBLER IS CRACKED AROUND FOUR FASTENERS BETWEEN XOS 62 5- 629. REPAIRED IAW SRM 57-40-02-2R, REP 15, FIG 203.

Part: WEB — CRACKED (DOOR FRAME) · airframe 65,752 hrs · 15,406 cycles

MAIN CARGO BAY L3 DOOR FRAME LOWER TORSION BOX HASA WEB CRACKED, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-40-15-2R, FIG 201.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 64,543 hrs · 15,021 cycles

ON TOUCH DOWN WHEN AUTO BRAKE ENGAGED, ACFT PULLED TO THE LT. MANUALLY DISCONNECTED AUTO BRAKE & MANUALLY BRAKED TO TURNOFF SPEED. UPON ARRIVAL AT GATE THE NR 8 BRAKE INDICATED A HYD LEAK. R & R HYD LINE FOR NR 8 BRAKE ASSEMBLY IAW AMM 20-40-01-2.

Part: SWITCH — BROKEN (EVAC SLIDE) · airframe 63,907 hrs · 14,823 cycles

PRIOR DEPARTURE, FOUND R1 EVAC SLIDE PTT SWITCH BROKEN. R1 DOOR OPERATES NORMAL. REPLACED PTT SWITCH IAW MM 25-61-04-4. ACFT OK FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (ANTI-ICE SYS) · airframe 628 hrs · 14,498 cycles

AT FL 320, 2 30 HRS INTO FLIGHT, RECEIVED LEVEL 1 ALERT. ENG 2 ANTI-ICE OFF. CONSULTED QRH, REFERENCING EXISTING MEL 30-22-02-03-A. WE WERE CONCERNED WITH POSSIBLE LIKELY DUCK LEAK. LANDED AT NEAREST SUITABLE AIRPORT. TROUBLE SHOT IAW FIM 30-22-07-00. REPLACED NR 2 ANTI-ICE SOV IAW AMM 30-22-01-4-1. RAN NR 2 ENG IAW JRH, SYS CHECKED OK. OPENED & CLOSED NR 2 ENG & COWLS IAW MM 71-10-00-2-1 & 52-46-01-2 & NR 2 ENG COWLS.

Part: ENGINE — FAILED (NR 3) · airframe 625 hrs · 14,414 cycles

CLIMBING TO FL 350 AT APPROX FL 250 AT CLIMB POWER, HAD A NR 3 ENG EVM COMPUTER AMBER BOX 5.0. ALL OTHER ENG PARAMETERS NORMAL., HAD AIRFRAME VIBRATION WITH THROTTLE OUT OF IDLE. CLIMB POWER N1 WAS 105. RAN QRH & CALLED MX, RECOMMENDED RTB. TURBINE FAILURE ENG APPROVED FOR ENG CHANGE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 625 hrs · 14,413 cycles

EMERGENCY LIGHT TEST HAS, BATT 1 LO, ALERT. FAULT WAS AT POWER UP AFTER LAYOVER. AFTER 2 HOURS ALLOWED TO CHARGE, FAULT CONTINUES. R & R BATTERY & CHARGER PACK.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 621 hrs · 14,316 cycles

L1 DOOR ARMING HANDLE SAFETY BUTTON WILL NOT STAY IN THE SAFE POSITION. FOUND HARDWARE LOOSE ON ARMING HANDLE. SECURED HARDWARE, BUTTON NOW STAYS IN THE SAFE POSITION.

Part: SIGN — UNSECURE (CABIN) · airframe 615 hrs · 14,103 cycles

EXIT SIGN OVER DOOR R1 FELL OFF. SECURED DOOR R1 EXIT LIGHT COVER IAW AMM SMP. ACFT OK FOR SERVICE.

Part: HINGE — WORN (CARGO DOOR) · airframe 60,980 hrs · 13,965 cycles

MAIN DECK CARGO DOOR HINGE, DOOR SIDE, FOUND 8 EACH HINGE LOBES EXCEED WEAR LIMITS.

Part: SUPPORT ANGLE — CRACKED (NR 2 SLAT) · airframe 60,980 hrs · 13,965 cycles

LEFT WING NR 2 SLAT OTBD EDGE SUPPORT ANGLE FOUND CRACK AT STATION XDLE 328. ANGLE REMOVED IAW SRM 51-35-01, A NEW SUPPORT ANGLE WAS FABRICATED IAW DRAWING ARB1647 REVISION C, AND INSTALLED IAW SRM 51-35-01 AND EA 1-5750-T0313966 PART 1 STEP 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (NR 2 SLAT) · airframe 60,980 hrs · 13,965 cycles

LEFT WING NR 2 SLAT RIB AT STATION XIS 342 FOUND CRACKED. RIB REMOVED IAW SRM 51-35-01, A NEW RIB FABRICATED IAW DRAWING ARB1629 AND INSTALLED IAW SRM 51-35-01 AND EA 1-5750-T0313966 PART 1 STEP 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 60,980 hrs · 13,965 cycles

RIGHT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 613.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 60,980 hrs · 13,965 cycles

RIGHT WING OTBD FLAP TE WEDGE INBD EDGE FOUND DELAMINATION 6 INCHES X 12 INCHES.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 58,452 hrs · 13,157 cycles

DURING SLAT EXTENSION, THE SLATS REMAINED RETRACTED. RAN QRH AND MADE A SLATS RET 28 FLAP LANDING. PERFORMED OPS CHECK OF SLATS REF AMM 27-80-01-5. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (TAIL) · airframe 57,149 hrs · 12,741 cycles

ON BLOCK IN, VISUALLY FOUND TAIL STRIKE. MULTIPLE AREA OF DAMAGE TO TAIL SECTION BELLY SKIN AND STRUCTURE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 56,359 hrs · 12,500 cycles

PREFLT CHECK FOUND LEVEL 1 "EMER LT BAT LO" R & R EMERGENCY EXIT LIGHTS BATTERY IAW MM 33-51-01-4,CARRIED OUT OPS TEST IAW MM 33-51-01-05.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 56,344 hrs · 12,492 cycles

RT WING T/E LOWER ACCESS PANEL NR 641JB CUT-OUT FORWARD TEE FITTING, FOUND CORROSION. TEE FITTING REPAIRED IAW EA 1-5710-163502. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.

Part: LONGERON — CRACKED (MLG TRUNNION) · airframe 56,344 hrs · 12,492 cycles

BS 595, LONGERON 49 RT FASTENER HOLE COMMON TO RT NLG TRUNNION FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. NEW LONGERON FABRICATED AND REWORKED AS PER DRAWING ACA3796 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,344 hrs · 12,492 cycles

OVERWING TANK PANEL BS 1234, "X" = 0, FOUND CORRODED. EXFOLIATION CORROSION REMOVED IAW SRM 51-21-01 REVISION 50. FOUND ACCEPTABLE AS PER EA 1-5730-163505, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 56,344 hrs · 12,492 cycles

RT WING FIXED L/E LOWER SURFACE AT STATION XOS 775 (NR 12 SLAT TRACK LOWER CUTOUT) FOUND CRACKED. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 56,344 hrs · 12,492 cycles

LT WING - L/E LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBOARD CORNER AS PER SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 56,344 hrs · 12,492 cycles

RT WING L/E LOWER SURFACE ACCESS PANEL 619AB CUTOUT, FORWARD EDGE FOUND CRACKED AT STA XOS 608. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 56,344 hrs · 12,492 cycles

RT WING LOWER FIXED L/E AT XOS 612 INBD REFUELING PANEL CUTOUT FWD CORNER, FOUND CRACKED.SRM 51-31-01 REVISION 50. NEW DOUBLER FABRICATED AS PER DRAWING ARB2933 REVISION AJ AND INSTALLED AS PER SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 56,344 hrs · 12,492 cycles

RT WING REFUELING ACCESS DOOR COMPARTMENT UPPER BEADED DOUBLER CRACKED BETWEEN XOS 640 AND XOS 648. REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: SKIN — CHAFED (ZONE 100) · airframe 56,344 hrs · 12,492 cycles

FORWARD CARGO DOOR FORWARD LOWER CUTOUT FOUND EDGE CHAFED. TRIMMED OUT AND REPAIR CARRY-OUT AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: TEE FITTING — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 56,344 hrs · 12,492 cycles

LT WING T/E LOWER ACCESS PANEL 541JB CUTOUT FORWARD TEE FOUND CORRODED AT XW317. CUTOUT FORWARD AREA REMOVED AS PER SRM 51-31-01 REVISION 50 AND REPLACED WITH NEW TEE AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: TRUNNION — CRACKED (ZONE 200) · airframe 56,344 hrs · 12,492 cycles

NLG WHEEL WELL LT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50 AND REPAIR PARTS INSTALLED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: TRUNNION — CRACKED (ZONE 200) · airframe 56,344 hrs · 12,492 cycles

NLG WHEEL WELL, RT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 55,238 hrs · 12,205 cycles

DURING POST FLT CHECK, FOUND L1 DOOR PNEUMATIC PRESSURE LOW. SERVICED PASSENGER DOOR PNEUMATIC STORAGE BOTTLE. PRESSURE AND LEAK CHECKED GOOD.

Part: VALVE — FAILED (R1 DOOR SLIDE) · airframe 54,001 hrs · 11,900 cycles

R1 DOOR ESCAPE SLIDE PNEUMATIC ACCUMULATOR PRESSURE GAUGE READS BELOW GREEN BAND. SERVICED R1 DOOR PNEUMATIC STORAGE IAW MM 12-25-04-3-0. REF ITEM 52-10/7162 R & R R1 BOTTLE RECHARGE VALVE.

Part: RESERVOIR — DISCHARGED (R1 DOOR) · airframe 52,522 hrs · 11,527 cycles

DURING TRANSIT CHECK, FOUND R1 DOOR PNEUMATIC STORAGE RESERVOIR PRESSURE BELOW GREEN BAND. SERVICED R1 DOOR IAW AMM 12-25-04-3, ACFT OK TO CONTINUE SERVICE. FINAL CLOSED.

Part: BOTTLE — UNDERSERVICED (PAX DOOR ASSIST) · airframe 51,839 hrs · 11,355 cycles

R1 DOOR ASSIST BOTTLE NEEDS SERVICE. SERVICED R1 DOOR ASSIST BOTTLE IAW MM 12-25-04-0. FINAL CLOSED.

Part: MOTOR — LEAKING (H/S TRIM) · airframe 51,324 hrs · 11,244 cycles

HYD 3 FAIL, HYD 3 QTY DECREASED TO 0 (ZERO). FUEL DUMPED AND EMERGENCY GEAR EXTENSION IAW JQH. R & R NR 3 UPPER AND LOWER HYD EDP IAW AMM 29-11-20-4. TURN OVER TO NEXT SHIFT FOR LEAK CHECK AND TEST. CHECK FOUND HYD LEAKED FROM THE CASING OF NR 3 HYD HORIZ STAB TRIM MOTOR. R & R MOTOR IAW AMM27-43-30-4. TURNOVER TRIM MOTOR BLEED HORIZ STAB TEST AND LEAK CHECK TO NEXT SHIFT.

Part: FRAME — DEFORMED (ZONE 200) · airframe 50,715 hrs · 11,115 cycles

MAIN DECK CARGO - FRAME AT STA 1721, LONGERON 12 LT FOUND DEFORMED. MAIN DECK CARGO STATION 1721 LONGERON 12LH FRAME AREA CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 50,715 hrs · 11,115 cycles

LWR VERTICAL STABILIZER FOUND RT SIDE BANJO FITTING FWD CRACK. REPAIR CARRIED OUT AS PER SRM 55-30-02 REPAIR 3 REVISION 44 AND EA 1-5530-143476: REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 50,715 hrs · 11,115 cycles

10 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA XORS 713.6. REPAIR CARRIED OUT AT R/H WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6 AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (LT WING) · airframe 50,715 hrs · 11,115 cycles

08 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA 713.6.

Part: LONGERON — CRACKED (ZONE 100) · airframe 50,715 hrs · 11,115 cycles

CTR CARGO COMPARTMENT RT TUNNEL STRUCTURE FOUND LONGERON L-29 CRACKED AT STA 1676. LONGERON AT STATION 1676 L-29RH CENTER CARGO COMPARTMENT TUNNEL TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-00-05 FIGURE 202 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REVISION 111.

Part: HEAT EXCHANGER — FAILED · airframe 50,118 hrs · 10,984 cycles

PASSING FL200, RECEIVED LEVEL 2 "ENG 1 OIL TEMP HI" FOLLOWED BY DECREASING OIL QUANTITY AND DECREASING PRESSURE. NR1 ENGINE WAS SHUTDOWN IAW CHECKLIST AFTER OIL QUANTITY REACHED ZERO. OIL TEMP PEAKED AT 167 DEG. AFTER SHUTDOWN NOTICED OIL QUANTITY INCREASING FROM 0 TO 19 OVER A 20 MINUTE PERIOD. ELECTED TO RESTART ENGINE AFTER DUMPING FUEL AND NR1 ENGINE OPERATED NORMALLY THEREAFTER. R & R FUEL/OIL HEAT EXCHANGER IAW MM 79 -21-02-4. PERFORMED NR1 ENG SPECIAL INSP, NO-OIL-PRESSURE INSP, A AND D SUMP VENT INSP, OIL SYS CONTAMINATION INSP & ENGINE POST-WINDMILLING INSP SATIS IAW AMM 72-00-05-6 1. PERFORMED NR1 ENG DRY & WET MOTOR, MIN IDLE LEAK CHECK OK IAW JRH. LATCHED NR1 ENG COWLING IAW AMM 71-10-00-21. RAN NR1 ENG FOR MIN/APPR IDLE IAW JRH, FOUND ALL PARAMETER NORMAL. RECHECKED OIL TANK WITH NO FUEL CONTAMINATED.

Part: SKIN — CORRODED (WING BOX) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -25. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CORRODED (WING BOX) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -54. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (WING BOX) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -56. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (WING BOX) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = 0. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (WING BOX) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -70. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CHAFED (BS 1009 S39R) · airframe 45,145 hrs · 9,911 cycles

FORWARD CARGO DOOR CUT-OUT AFT EDGE, APPROX STA 1009, LONGERON 39-R FOUND CHAFED SKIN ADA7030-1. CARRIED OUT REPAIR AS PER SRM 53-50-01 FIG. 17 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK, 1 RT DOOR WAY FLOOR EXTENDED SEAT TRACK STA 436 TO STA 446 X= -88 FOUND CORROSION. COMPLIED WITH EA 1-5320-128592, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (ZONE 500) · airframe 45,145 hrs · 9,911 cycles

LEFT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-128598. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 45,145 hrs · 9,911 cycles

LEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE FOUND CORRODED HINGE FITTING. COMPLIED WITH EA 1-5750-128595. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 45,145 hrs · 9,911 cycles

RIGHT WING, FLAP SIDE INBOARD FLAP OOUTBOARD HINGE PIVOT HOLE FOUND CORRODED HINGE FITTING. COMPLIED WITH E.A. 1-5750-128597. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 45,145 hrs · 9,911 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP LOWER BARREL NUT HOLE FOUND CORRODED HINGE FITTING ARC0503-12. COMPLIED WITH E.A. 1-5750-128596. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 45,145 hrs · 9,911 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER BARREL NUT HOLE FOUND CORRODED HINGE FITTING ARC0503-12. COMPLIED WITH E.A. 1-5750-128596. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 480-485) · airframe 45,145 hrs · 9,911 cycles

FORWARD CABIN, FLOOR SEAT TRACK BASE STA 480 TO 485, X = 27.50. FOUND CORRODED SEAT TRACK ACA7106-505. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 436-446) · airframe 45,145 hrs · 9,911 cycles

MAIN DECK, NR 1 RIGHT DOOR WAY FLOOR EXTENDED SEAT TRACKS STA 436 TO STA 446, X = -88 FOUND CORRODED SEAT TRACK ABA7681-503. COMPLIED WITH EA 1-5320-128592. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 45,145 hrs · 9,911 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT FORWARD AND AFT SURFACE FOUND WITH CORROSION HINGE FITTING ARC0503-12. COMPLIED WITH FEDEX EA 1-5750-128596. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 45,145 hrs · 9,911 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE FOUND WITH CORROSION HINGE FITTING. COMPLIED WITH EA 1-5750-128596. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 45,145 hrs · 9,911 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE FOUND WITH CORROSION HINGE FITTING ARC0503-12. COMPLIED WITH E.A. 1-5750-128596. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES NR B, NR C AND NR D, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES NR A, B AND C CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES NR B, NR C AND NR D, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES NR A, B, C AND D, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 45,145 hrs · 9,911 cycles

CABIN, SEAT TRACK AT APPROX STA 755, X = 8.5, FOUND CRACK SEAT TRACK ADA8390-1. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,145 hrs · 9,911 cycles

MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES NR A, NR B, NR C AND NR D, CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES SUPPORT FITTING AFA7132-1. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: LINK — OUT OF TOLERANCE (MLG DOOR) · airframe 41,570 hrs · 9,163 cycles

RIGHT MLG TO 90 SEC TO 2 MIN TO COMPLETE RETRACTION CYCLE. RED IN TRANSIT LIGHT ON BOTH PRIMARY AND SECONDARY SYSTEMS. FOUND RIGHT GEAR DOOR LINK ASSY CLEARANCE TO BE OUT OF TOLERANCE. INSTALLED SHIM AND ADJUSTED IAW MD11 MM 32-34-05-5. COMPLIED WITH GEAR SWING TO VERIFY GOOD INDICATION. OPS CHECKS GOOD, REF MD11 MM 32-31-00-5 STEP 10.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 41,346 hrs · 9,114 cycles

AFTER TAKEOFF GEAR LEVER RAISED AND RED LIGHT REMAINED ON IN RT MAIN INDICATOR (BOTH) PER QRH, REMAINED BELOW 230 KNOTS, EXTENDED GEAR RAISED GEAR AND ALL RED LIGHTS EXTINGUISHED. CONTINUED TO DESTINATION NO PROBLEM. T/S IAW FIM 32-30-03 AND 31-71-04-00. NOTHING FOUND A/C OK TO CONTINUE.

Part: TEE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 40,106 hrs · 8,872 cycles

AFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4.

Part: TEE FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 40,106 hrs · 8,872 cycles

AFTER BUSHING REMOVAL, RIGHT WING INBOARD FLAP VANE OUTBOARD TEE FITTING BORE FOUND CORRODED. RIGHT WING INBOARD FLAP VANE OUTBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27-50-22-4.

Part: TEE FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 40,106 hrs · 8,872 cycles

AFTER BUSHING REMOVAL, LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING BORE FOUND CORRODED. LEFT HAND WING INBOARD FLAP VANE INBOARD TEE FITTING REMOVED AND REPLACED AS PER AMM 27- 50-22-4. FLAP OPERATION TEST CARRIED OUT AS PER AMM 27-50-00-860-801.

Part: LONGERON — CRACKED (ZONE 100) · airframe 40,106 hrs · 8,872 cycles

CENTER CARGO, STATION 1710 (TRANSVERSE SKIN SPLICE AREA), LONGERON 49L FOUND CRACKED. 09-24-07 CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5310-113188. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CHAFED (FUSELAGE) · airframe 40,106 hrs · 8,872 cycles

FUSELAGE EXTERIOR, FORWARD CARGO DOOR CUTOUT AFT LOWER AREA FOUND CHAFED. 09-21-07 FUSELAGE EXTERIOR, FORWARD CARGO DOOR CUTOUT AFT LOWER CHAFFED AREA REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 100) · airframe 35,494 hrs · 7,877 cycles

CTR CARGO DOOR CUTOUT AT AFT LOWER SIDE FOUND CHAFED. REPAIR CARRIED OUT AT CTR CARGO DOOR CUTOUT AFT LWR SIDE CHAFED AS PER SRM 53-50-00 VOLUME I FIGURE 16. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUT — CORRODED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

LT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 2 BOLT HOLE FOUND WITH CORROSION. REPAIR CARRIED OUT AT LT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 2 BOLT HOLE AS PER FEDEX EA NR 1-5750-97750, TITLE: "WINGS - OUTBOARD TRAILING EDGE FLAP, LT I/B SUPPORT STRUT, CORROSION REPAIR". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRUT — CORRODED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

LT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 1 BOLT HOLE FOUND WITH CORROSION. REPAIR CARRIED OUT AT LT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 1 BOLT HOLE AS PER FEDEX EA NR 1-5750-97750, TITLE: "WINGS, OUTBOARD TRAILING EDGE FLAP, LT I/B SUPPORT STRUT CORROSION REPAIR". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (ZONE 600) · airframe 35,494 hrs · 7,877 cycles

RIGHT WING O/B FLAP I/B HINGE SUPPORT FITTING (P/N ARC4008) O/B NR 2 BOLT HOLE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EO 1-5750-7-5008. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DOOR — CRACKED (ZONE 700) · airframe 35,494 hrs · 7,877 cycles

RIGHT MAIN LANDING GEAR FLIPPER DOOR ASSY FOUND CRACK AT AFT OF FWD EDGE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR FLIPPER DOOR ASSY AS PER AMM 32-14-10. PERFORMED RIGHT MLG FLIPPER DOOR ADJUSTMENT AND TEST AS PER AMM 32-31-00, FOUND SATISFACTORY.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 35,494 hrs · 7,877 cycles

M/D CARGO SEAT TRACK (STA 1501-1510, LT X=27.5) FOUND EDGE BROKEN.

Part: SKIN — CHAFED (ZONE 100) · airframe 35,494 hrs · 7,877 cycles

CTR CARGO DOOR CUTOUT AT AFT LWR SIDE FOUND CHAFED. REPAIR CARRIED OUT AT CTR CARGO DOOR CUTOUT AFT LWR SIDE CHAFFED AS PER SRM 53-50-00 VOLUME I FIGURE 16. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 100) · airframe 35,494 hrs · 7,877 cycles

FWD CARGO DOOR CUTOUT AT FWD LWR SIDE FOUND CHAFED. DOOR CUTOUT AT FWD LWR SIDE CHAFE SMOOTHENED AS PER SRM 53-50-00 VOLUME I FIGURE 16. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

LEFT WING O/B FLAP I/B HINGE SUPPORT FITTING (P/N ARC4009) O/B NR 3 BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED WITH A NEW FLAP AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

LT WING FIXED LEADING EDGE STA XOS 698 TO STA XOS 703 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW FEDEX EA 1-5730-97748.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

LEFT WING FIXED LEADING EDGE STA XOS 625 TO STA XOS 629 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-97746.

Part: STRINGER — CRACKED (LT WING) · airframe 35,494 hrs · 7,877 cycles

HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 42 LT WING. REPAIR CARRIED OUT AS PER FEDEX EA 1-5720-97744.

Part: STRINGER — CRACKED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 16 LT WING. REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRINGER — CRACKED (LT WING) · airframe 35,494 hrs · 7,877 cycles

SNRM N00398: HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 38 LT WING. REPAIRED WITH REPAIR ANGLES AS PER SRM 57-20 -00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 35,494 hrs · 7,877 cycles

RIGHT WING FIXED L/E INNER BEADED DOUBLER FOUND CRACKED AT XOS 643 - 647. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-97747.

Part: STRINGER — CRACKED (RT WING) · airframe 35,494 hrs · 7,877 cycles

HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 42 RT WING. REPAIRED AS PER SRM 57-20-00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 35,494 hrs · 7,877 cycles

HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 12 LT WING. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 35,494 hrs · 7,877 cycles

SNRM N00399: HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 9 RT WING. REPAIR CARRIED OUT AT STR 9 RT WING AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 35,494 hrs · 7,877 cycles

SNRM N00405: HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 16 RT WING. REPAIRED WITH REPAIR ANGLES AND FABRICATED CLIP AS PER SRM 57-20-00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2- 100. COMPLIED WITH FEDEX EA 1-5720-97738 - TITLE: WINGS - STRINGER REPAIR PER SRM VOL.I 57-20-00 FIG. 10 - FX ARB3397 CLIP.

Part: STRINGER — CRACKED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

HFEC INSPECTION CARRIED OUT FOUND CRACK AT STR 14 LT WING. CRACK ON LH WING STRINGER 14 END REPAIRED WITH REPAIR SPLICE AS PER SRM 57- 20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 35,494 hrs · 7,877 cycles

LT WING FIXED L/EDGE TELESCOPIC DUCT CUT-OUT UPPER SURFACE INBD AND OUTBD CORNER FOUND CRACKED. LT WING FIXED L/EDGE TELESCOPIC DUCT CUT-OUT UPPER SURFACE INBD AND OUTBD CORNER CRACKED AREA REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5730-97743, TITLE: "WINGS LT WING LEADING EDGE SKIN CRACKS AT TELESCOPING DUCT CUTOUT". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 35,494 hrs · 7,877 cycles

RT WING FIXED L/EDGE TELESCOPIC DUCT CUT-OUT I/B AND O/B UPPER CORNER FOUND CRACKED. RT WING FIXED L/EDGE TELESCOPIC DUCT CUT-OUT UPPER SURFACE INBD AND OUTBD CORNER CRACKED AREA REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5730-97742, TITLE: "WINGS, RT WING LEADING EDGE SKIN CRACKS AT TELESCOPING DUCT CUTOUT". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 600) · airframe 35,494 hrs · 7,877 cycles

RT WING I/B FLAP LOWER SURFACE FOUND SURFACE CORROSION. CLEANED AS PER AMM 12-26-02 AND TREATED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FLAP — CORRODED (LT WING) · airframe 35,494 hrs · 7,877 cycles

LT WING IB FLAP LOWER SURFACE FOUND SURFACE CORROSION. CORROSION CLEANED AS PER AMM 12-26-02 AND TREATED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: LINE — LEAKING (NR 3 ENGINE) · airframe 31,023 hrs · 6,896 cycles

ENG - 3 A-ICE DISAG, ILLUMINATED WITH SWITCH OFF. TURNED SWITCH ON, DISAG LT STILL ON. TURNED A/I OFF, DISAG LT STAYED ON FOR APPROX 15 MINUTES THEN WENT OUT. MEL 24JAN05 RELEASED FOR SERVICE PER MEL/CDL: 30-22-01-02-A CATEGORY: C EXPIRATION: 03FEB05 ENG NR 3 ANTI-ICE VALVE INOP. FOUND NR 3 ENG AI VALVE MUSCLE AIR LINE LEAKING. REMOVED AND REPLACED LINE IAW SMP RAN ENG PER JRH AND A/I VALVE OPS CHECKS GOOD.

Part: DOUBLER — CRACKED (LANDING GEAR WW) · airframe 30,530 hrs · 6,792 cycles

CENTER LANDING GEAR WHEEL WELL RT STA Y= 1381, DOUBLER FOUND CRACKED AT LOCATION ADJACENT TO RT SPOILER MIXER. DOUBLER FABRICATED PER DOUGLAS DRAWING NR AEA0526 AND PART MARKED PER GMM 7-0-1001. CRACKED DOUBLER AT CENTER LANDING GEAR WHEEL WELL RT STA Y= 1381 ADJACENT TO RT SPOILER MIXER. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.

Part: BATTERY — FAILED (NR 1 & 2) · airframe 30,530 hrs · 6,792 cycles

"EMERGENCY POWER TEST FAIL" ALERT DISPLAY. TWO (2) EACH MAIN BATTERY (P/N: 31433-001) REMOVED AND REPLACED PER AMM 24-34-02-4. OPERATIONAL TEST OF THE MAIN BATTERY CARRIED OUT PER AMM 24-34-02-5. FOUND SATISFACTORY. POSITION 1, S/N OFF: 10101125, S/N ON:10201519, SERVICEABLE TAG NO.: 684804 POSITION 2, S/N OFF: 10201514, S/N ON:10200188, SERVICEABLE TAG NO.: 684803.

Part: FITTING — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 3L EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 3L REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR.

Part: FITTING — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 35R EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 35R, REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR.

Part: FITTING — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 26L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 26L, REMOVED AND REPLACED PER SRM 51-33-01 VOLUME 2.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 34R. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 28L. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789.

Part: FITTING — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 30L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE NR 30L REPAIRED PER FEDEX EA 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000.

Part: FITTING — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 14L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 14L, REMOVED AND REPLACED PER SRM 51-33-01 VOLUME 2.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK SEAT TRACK AT STA Y= 635, X= -8 FOUND WITH APPROXIMATELY FOUR (4) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP. MAIN DECK SEAT TRACK AT STA Y= 625 TO Y= 655, X= -8 CUT AND REMOVED PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 32L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 15R EXCEEDED LIMITS. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT NR 15R REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR - 1-5510-7-5000.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 20L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 21R EXCEEDED LIMITS. REF TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 21R. REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE, REWORK/REPAIR, 1-5510-7-5000.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 24L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 1R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 17R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 16L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789, HORIZONTAL STABILIZERS BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000

Part: STRUCTURE — CORRODED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 2L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON BARREL NUT BORE NR 7R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK SEAT TRACK FOUND WITH THREE (3) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP AT STA Y= 635, X= -8. CUT AND REMOVED AT STA Y= 625 TO Y= 655, X= 8 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 16R, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: FRAME — CHAFED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO COMPARTMENT, RT STA 535 FRAME FOUND CHAFED AT UPPER AND LOWER YOKE MOUNTING AREA. TRIMMED OUT AND REPAIRED PER FEDEX DRAWING SRZ-53-503 AND SRM 51-31-01 VOLUME I.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 24R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 36R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 27L. AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 23L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 25L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 19L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789.

Part: TRACK — CRACKED (TRUST REVERSER) · airframe 30,530 hrs · 6,792 cycles

NR 1 ENGINE, RT TRUST REVERSER UPPER SLIDER TRACK CRACKED. R / R PER WORK CARD 78T3901-R.

Part: STRUCTURE — CORRODED (ZONE 400) · airframe 30,530 hrs · 6,792 cycles

BARREL NUT BORE NR 20 RT, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789.

Part: LONGERON — DENTED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO, LONGERON FOUND DENT AT RT STA Y= 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND.

Part: STRINGER — CRACKED (ZONE 600) · airframe 30,530 hrs · 6,792 cycles

BOOSTER PROGRAM, RT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACK AS VIEWED FROM ACCESS PANEL NR 636AB. ARB751-1. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.

Part: CONTROL VALVE — CRACKED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

HFEC INSPECTION CARRIED OUT ON HORIZONTAL STABILIZER TRIM CONTROL VALVE AND CRACK FOUND AT UPPER CONTROL VALVE BORE APPROXIMATELY 0.25 INCH LENGTH FROM PRESSURE PASSAGE BORE. REMOVED AND REPLACED PER AMM 27-43-42-4. OPERATION CHECK CARRIED-OUT PER AMM 27-40-00-5. P/N ON: AJG7041-5545, S/N ON: RON549, FEDEX SERVICEABLE TAG NR: 629223.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED (P/N ALC8107Y2) PER SRM 51-33-01 VOLUME II.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 30,530 hrs · 6,792 cycles

CORROSION REMOVED ON NR 14 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REMOVED AND REPLACED (P/N ALC8106Y2) PER SRM 51-33-01 VOLUME II.

Part: LONGERON — DENTED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA Y= 1681, LONGERON 12R FOUND WITH DENT/CHAFFED. REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1 AND SRM 51-33-01 VOLUME II. RE-INSPECTION TO BE ACCOMPLISHED AT 16,292 FLIGHT CYCLES WITH REPETITIVE INSPECTION THEREAFTER OF EVERY 9,500 FLIGHT CYCLES. REFER TO FEDEX EA 1-5310-79793, FUSELAGE - MAIN FRAME - TRACKING OF CATEGORY B REPAIRS ON FRAME.

Part: STRINGER — CRACKED (ZONE 500) · airframe 30,530 hrs · 6,792 cycles

LT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACKED AS VIEWED FROM ACCESS PANEL NR 536AB. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.

Part: BRACKET — CRACKED (ZONE 500) · airframe 30,530 hrs · 6,792 cycles

LT WING OUTBOARD FLAP HINGE FWD FAIRING SUPPORT BRACKET FOUND CRACKED AT INBOARD LOWER. BRACKET REMOVED AND REPLACED PER SRM 51-05-01 VOLUME II.

Part: SKIN — DAMAGED (ZONE 500) · airframe 30,530 hrs · 6,792 cycles

LT WING UPPER SURFACE STA XOS=772, ON PREVIOUS METAL FILLER REPAIR FOUND EXISTING BLENDOUT EXCEEDED SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET. NR 2 LIMITS. BLENDOUT DIMENSION: LENGTH=1.5 INCH, WIDTH= 1.25 INCH, DEPTH=0.0052 INCH; ORIGINAL THICKNESS= 0.312 INCH, REMAINING=0.262 INCH. L/H WING, TAPERED UPPER CENTER, OUTER SKIN PANEL SURFACE LOCATED AT STA XROS= 772, FRONT SPAR LINE - EXISTING BLENDOUT REPAIR CARRIED OUT PER SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET 2 AND 9. COMPLIED WITH FEDEX EA 1-5720-77972, WINGS - LT HAND TAPERED UPPER / CENTER OUTER SKIN PANEL - REWORK

Part: FRAME — DENTED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA 1681, LONGERON 12. FOUND WITH DENT/CHAFFED. REMOVED PER SRM 51-33-01 VOLUME II. REPAIR DOUBLER FABRICATED PER SRM. REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II. REFER TO EA 1-5310-79792, FUSELAGE MAINFRAME TRACKING OF CATEGORY B REPAIRS ON FRAME. NEXT INSPECTION IS SET TO 16,292 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES THEREAFTER.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK, L1 DOOR WAY SEAT TRACK FOUND CORROSION BETWEEN STA 425 - 445. REMOVED PER SRM 51-31-01 VOLUME II. SEAT TRACK P/N ABA760-505 FABRICATED PER DOUGLAS DRAWING ABA7680 AND SRM 51-35-01 USING ABA760-5070 RAW MATERIAL. FABRICATED SEAT TRACK INSTALLED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO, SEAT TRACK FOUND WORN AT LT STA 752 - 760, X= 25. REMOVED FROM L/H STA Y= 745 - Y= 815, X= 25 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND INSTALLED PER SRM 51-31-01 VOLUME II.

Part: LONGERON — DENTED (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO, LONGERON FOUND DENT AT RT STA 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 30,530 hrs · 6,792 cycles

MAIN DECK CARGO, SEAT TRACK FOUND WORN AT RT STA 999, X= - 8. TRIMMED OUT PER MD-11 SRM 53-70-00 VOLUME I FIGURE 1. REPAIR PARTS FABRICATED AND INSTALLED PER MD-11 SRM 53-70-00 VOLUME I FIGURE1.

Part: ACTUATOR — INOPERATIVE (FLAPS) · airframe 26,255 hrs · 5,854 cycles

ON DEPARTURE FLAPS NO RETRACT PLEASE. REMOVED AND REPLACED FLAP LIMITER DUPLEX ACTUATOR IAW MM 27-56-01-0 4. PERFORMED ADJUSTMENT OF FLAP LIMITER ACTUATOR IAW MM 27-50-00-5, ALSO PERFORMED FUNCTIONAL TEST OF THE FLAP LIMITER ACTUATOR IAW MM 27-50-00-5, CHECKED GOOD. REMOVED AND REPLACED FLAP CONTROL VALVE (INBOUND) IAW MM 27-52-03-4 . PERFORMED TEST OF FLAP SYS OPERATION / RANGE MOVEMENT IAW MM 27-50-00-5, CHECKED GOOD. LEAK OPS CHECK OK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,718 hrs · 5,742 cycles

CENTER CARGO DOOR CUT OUT LOWER AFT CORNER FOUND ROLLER TRAY SUPPORT CHORD CRACK. ***** S/D COMING ****

Part: ATTACH FITTING — CORRODED (ZONE 500) · airframe 25,718 hrs · 5,742 cycles

LT WING OUTBD FLAP OUTBD HINGE ( A/C SIDE ) LOWER OUTBD ATTACH POINT ( TO AFT SPAR ) HOLE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71841 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKETS LOWER OUTBOARD ATTACHMENT BORE COMMON TO THE REAR SPAR LOWER CAP.

Part: SKIN — CORRODED (RT WING) · airframe 25,718 hrs · 5,742 cycles

RT WING UPPER SURFACE FOUND CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL. RT WING UPPER SURFACE CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL REPAIR CARRIED AS PER FEDEX EA 1-5720-69365 WINGS OUTER WING / RT OUTER AFT SKIN PANEL - CORROSION REWORK.

Part: PIVOT — CORRODED (ZONE 500) · airframe 25,718 hrs · 5,742 cycles

LT INBD FLAP OUTBD HINGE (FLAP SIDE ) OUTBD PIVOT BORE CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. 2 AND FEDEX EA - 1-5750-71842 WINGS - TRAILING EDGE FLAPS - INBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKET CORROSION REPAIRED.

Part: RIB — CRACKED (ZONE 500) · airframe 25,718 hrs · 5,742 cycles

LEFT OUTBOARD FLAP, FOUND 01 EACH CRACK ON NOSE RIB SUPPORT ISLAND, APPROX 0.25 INCH IN LENGTH. REPAIR CARRIED OUT AS PER EA 1-5750-71833 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR.

Part: RIB — CRACKED (ZONE 600) · airframe 25,718 hrs · 5,742 cycles

RIGHT OUTBOARD FLAP, FOUND 01 EACH CRACK ON NOSE RIB SUPPORT ISLAND, APPROX. 0.25 INCH IN LENGTH. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-71833 WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAP - SECONDARY UP STOP - REPAIR.

Part: PIVOT — CORRODED (ZONE 500) · airframe 25,718 hrs · 5,742 cycles

LT INBD FLAP,OUTBOARD HINGE (FLAP SIDE ) INBD AND OUTBOARD PIVOT BORES CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. 2 AND FEDEX EA - 1-5750-71842 WINGS - TRAILING EDGE FLAPS - INBOARD TRAILING EDGE FLAP - OUTBOARD FLAP HINGE BRACKET CORROSION REPAIRED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 25,718 hrs · 5,742 cycles

FORWARD CABIN - R1 DOOR ENTRANCE TRACK FOUND CORRODED AT STA 430. CORROSION BLENDED CARRIED OUT FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,718 hrs · 5,742 cycles

FORWARD CABIN - L1 DOOR ENTRANCE TRACK FOUND CORRODED AT STA 420 - 457. CORROSION BLENDED CARRIED OUT FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 25,718 hrs · 5,742 cycles

MAIN DECK CARGO FLOOR SEAT TRACK CRACKED AT STA 695, LBL 27.5. REPAIR CARRIED-OUT AT MAIN DECK CARGO FLOOR SEAT TRACK BETWEEN STA 680 AND STA 745 IAW SRM 53-70-00 FIG 1 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 25,718 hrs · 5,742 cycles

RIGHT WING, LEADING EDGE RIB CRACK INBOARD OF NR 16 SLAT TRACK. RIGHT WING, LEADING EDGE RIB INBOARD OF NR 16 SLAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2.

Part: RIB — CRACKED (LT WING) · airframe 25,718 hrs · 5,742 cycles

LEFT WING, LEADING EDGE RIB CRACK INBOARD OF NR 16 SLAT TRACK. LEFT WING, LEADING EDGE RIB CRACK INBOARD OF NR 16 SLAT TRACK REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.

Part: ELECTRICAL SYS — FAILED (AC SYS)

GOT LEVEL ONE ALERT BUS R EMERGENCY AC OFF LOST ALL ASSOC DISPLAYS & RADIUS. REMOVED AND REPLACED R2-5157 PER SMP.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 17,012 hrs · 3,839 cycles

A 12.75 CRACK FOUND ON NR 4 SEAT TRACK BETWEEN BS 781-800 AT MAIN CARGO COMPT. *S/D* REMOVED AND REPLACED BETWEEN STA 745-816+27 PER IAW SRM 53-70-00 VOL 1.

Part: CLAMP — DAMAGED (NR 1 ENGINE)

00-11- NR 1 FIRE WARN AFT LVL OFF. THROTTLE IDLE EXTING THE LIGHT. REPEAT WRITE UP. RETIGHTENED CLAMPS, REPLACED DAMAGED DUCT METAL SEALS PN 144OM41P01 FOR 14TH STAGE DUCT. PRECAUTION REPLACED U/P RT TURBINE DET ASSY AND FDCU1 RTS PASS PER MM 26-11-02-700-801. NR 1 ENG FIRE DET LOOP B INOP. C/W MX P26-1.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 1 ENGINE)

00-10 - DURING CRUISE FIRE DETECT 1 FAIL LEVEL 1 ALERT CAME ON AND OFF SEVERAL TIMES. NR 1 ENG CK FIRE SENSORS AND HARNESS NORM. PNEUMATIC DUCT LEAK CK. NO LEAK FOUND. NR 1 ENG COWLING CLOSED PER MM 71-10-00-2-1. FOUND NORMAL.

Part: SEAT TRACK — CRACKED (BS 635)

SNRM 403,0404, 467 - MAIN DECK CARGO COMP BS 635, LBL 47 CRACK IN LWR -403, MAIN DECK CARGO COMP BS 635, RBL 8.5 CRACK IN LWR -404, MAIN DECK CARGO COMP BS 635, LBL 27 CRACK IN LWR - 467. SEAT TRACKS REPAIRED PER SRM 53-70-00 FIG VOL 1.

Part: ENGINE — BIRD STRIKE (NR 3 ENGINE)

99-200 - ON T/O A LARGE BIRD STRUCK THE RT SIDE OF THE A/C. ENG MADE LOUD NOISE PWR REDUCED, VIB WENT AWAY, AND RETURN FOR LAND. FAN BLADES REPLACED SEE WRI 72-10/4339 AND 72-10/4336. REVERSER TRANSLATING COWL REPLACED PER 78-30/4338. PERF TRIM BALANCE ON NR 3 ENG PER MD11 MM 72-30-00. PERF BIRD STRIKE INSP IAW MD11 MM 05-52-01-6 AND 72-00-02-200-801.

Part: POWER RELAY — FAILED (RT COCKPIT)

SFS - APPROXIMATELY 25 MINUTES INTO FLIGHT, THE FIRST OFFICER LOST ALL DISPLAYED INSTRUMENTATION. AIR TURNBACK TO SFS, CURRENTLY BEING T/S. REMOVED AND REPLACED THE NR 3 AUXILIARY POWER RELAY. RAN ENGINE, POWER TRANSFER OK.