N595FE

Part: BATTERY — INOPERATIVE (ZONE 800) · airframe 98,725 hrs · 21,079 cycles

L1 PRESS TO TEST REMOTE SLIDE LIGHT IS INOP. REPLACED BATTERIES & BULBS, PREFORMED SLIDE FUNCTIONAL TEST IAW MM 25-61-05-01, OPS CHECKED GOOD, A/C OK FOR FLIGHT.

Part: ENGINE — FAILED (NR 3) · airframe 98,409 hrs · 20,988 cycles

PDIS 595 79-36 8740 30MAR25 02:47 NRT OPEN ENG 3 OIL FILTER LEVEL 2 ALERT @FL350. AIRFRAME VIBRATION STARTED JUST PRIOR TO ALERT AND CONTINUED UNTIL THROTTLE AT IDLE. ENGINE PARAMETERS NORMAL. CONSULTED QRH. SHUT DOWN #3 ENGINE AS ALERT WOULD NOT CLEAR WITH THROTTLE AT IDLE. ***EMERGENCY DECLARED***

Part: BULB — WRONG PART (ZONE 200) · airframe 98,018 hrs · 20,881 cycles

1L ESCAPE SLIDE BOTTLE PRESSURE LIGHT WILL NOT ILLUMINATE UPON TESTING. AMM: 25-61-04-5 T/S AND FOUND WRONG BULBS INSTALLED IN LIGHT ASSY. RELAMPED WITH PROPER 368 BULBS NOW L1 DOOR SLIDE REMOTE PRESSURE INDICATOR OPS CHECKS NORMAL REF MM 25-61-04-5. ACFT OK FOR SERVICE. OSD: 1/31/2025

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

FLIGHT COMPARTMENT FLOOR PANEL #215BF FOUND DELAMINATED STATION 335. FLIGHT COMPARTMENT STATION 335 DELAMINATED FLOOR PANEL #215BF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-02-4. FLOOR PANEL #215BF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

FLIGHT COMPARTMENT FLOOR PANEL #215DF FOUND DELAMINATED STATION 350. FLIGHT COMPARTMENT, STATION 350 DELAMINATED FLOOR PANEL #215DF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-02-4. FLOOR PANEL #215DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

FLIGHT COMPARTMENT FLOOR PANEL #216AF FOUND DELAMINATED STATION 330. FLIGHT COMPARTMENT STATION 330 DELAMINATED FLOOR PANEL #216AF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-02-4. FLOOR PANEL #216AF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 100) · airframe 97,301 hrs · 20,676 cycles

FUSELAGE SKIN STATION 585 #1 AIRCON PACK EXHAUST OUTLET CUTOUT SUSPECT CRACK. CRACKED FUSELAGE SKIN STATION 585 #1 AIRCON PACK EXHAUST OUTLET CUTOUT, REPAIR ACCOMPLISHED PER E.A.#: 1-5320-T0380781 P1. TITLE: FUSELAGE AUXILIARY STRUCTURE REPAIR FOR CRACKED SKIN LAYER ACA3354-501 EDGE AT STA 586, L-48L AT THE AIRCON DOOR JAMB AREA. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TEE ANGLE — NONE (ZONE 100) · airframe 97,301 hrs · 20,676 cycles

AFT CARGO / WASTE TANK COMPARTMENT - EXISTING REPAIR FOUND AT THE PRESSURE BULKHEAD UPPER TEE STATION 2007, X = -41 REQUIRES EVALUATION FOR CONFORMITY TO APPROVED DATA EXISTING REPAIR AT AFT CARGO / WASTE TANK COMPARTMENT PRESSURE BULKHEAD UPPER TEE STATION 2007, X = -41 EVALUATED AND FOUND REPAIRED IAW SRM 53-70-08-2R REPAIR 4 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TEE ANGLE — NONE (ZONE 100) · airframe 97,301 hrs · 20,676 cycles

AFT CARGO / WASTE TANK COMPARTMENT - EXISTING REPAIR FOUND AT THE PRESSURE BULKHEAD UPPER TEE STATION 2007, X = 34 REQUIRES EVALUATION FOR CONFORMITY TO APPROVED DATA EXISTING REPAIR AT AFT CARGO / WASTE TANK COMPARTMENT PRESSURE BULKHEAD UPPER TEE STATION 2007, X = 34 EVALUATED AND FOUND REPAIRED IAW SRM 53-70-08-2R REPAIR 4 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231EF DELAM. CABIN - MAIN DECK CARGO COMPARTMENT DELAMINATED FLOOR PANEL #231EF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. FLOOR PANEL #231 EF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231GF DELAM. CABIN - MAIN DECK CARGO COMPARTMENT, DELAMINATED FLOOR PANEL #231GF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. FLOOR PANEL #231GF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF DELAM. CABIN - MAIN DECK CARGO COMPARTMENT, DELAMINATED FLOOR PANEL #231HF REMOVED AND REPLACED AS PER MD-11 AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200)

MAIN DECK CARGO COMPARTMENT DENT FOUND ON FUSELAGE FRAME AT STATION 1641 LONGERON 12 RIGHT. MAIN DECK CARGO COMPARTMENT - DENT ON FUSELAGE RIGHT HAND FRAME STATION 1641 LONGERON 12 RIGHT REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER MD-11 SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200)

MAIN DECK CARGO COMPARTMENT DENT FOUND ON FUSELAGE FRAME AT STATION 1761 LONGERON 12 RIGHT. MAIN DECK CARGO COMPARTMENT - DENT ON FUSELAGE RIGHT HAND FRAME STATION 1761 LONGERON 12 RIGHT REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER MD-11 SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200)

MAIN DECK CARGO COMPARTMENT Ï¿½ SEAT TRACK CROWN FOUND WORN AT STATION 1291, X = 47.5. MAIN DECK CARGO COMPARTMENT - AT SEAT TRACK STATION 1291, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1229 TO STATION 1331, X = 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING LEADING EDGE LOWER ACCESS PANEL #618GB ATTACHMENT DOUBLER FOUND CRACKED AT STATION XOS 488. RIGHT HAND WING LEADING EDGE LOWER ACCESS PANEL #618GB ATTACHMENT CRACKED DOUBLER AT STATION XOS 488 AREA REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 2933 REVISION AJ. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 97,301 hrs · 20,676 cycles

CENTER WING UPPER AUXILIARY TANK RIGHT HAND COMPARTMENT STRINGER 47 FOUND CRACKED AT STATION XCW -17 APPROXIMATELY 3.55 . CENTER WING UPPER AUXILIARY TANK RIGHT HAND COMPARTMENT STRINGER 47 AT STATION XCW -17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (FUEL TANK) · airframe 97,301 hrs · 20,676 cycles

CENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 FOUND CRACKED AT STATION XCW 46.5. CENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 AT STATION XCW 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (FUEL TANK) · airframe 97,301 hrs · 20,676 cycles

CENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 FOUND CRACKED AT STATION XCW 17 APPROXIMATELY 4.75 . CENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 AT STATION XCW 17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 97,301 hrs · 20,676 cycles

LEFT HAND WING LEADING EDGE LOWER ACCESS PANEL #519AB ATTACHMENT DOUBLER FOUND CRACKED AT STATION XOS 604. LEFT HAND WING LEADING EDGE LOWER ACCESS PANEL #519AB ATTACHMENT CRACKED DOUBLER AT STATION XOS 604 AREA REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 2933 REVISION AJ. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 678. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 678 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 636. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 636 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1426, X = - 47.5Ï¿½ FOUND CROWN DAMAGED. CABIN - AT SEAT TRACK STATION 1426, X = - 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1411 TO STATION 1451, X = - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 97,301 hrs · 20,676 cycles

LEFT HAND WING TRAILING EDGE LOWER SPAR CAP FOUND WITH CORROSION AT STATION XORS 1070. LEFT HAND WING TRAILING EDGE LOWER SPAR CAP CORROSION AT STATION XORS 1070 REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-00-10-1A ALLOWABLE DAMAGE 1. CORRODED LOWER SPAR CAP AT STATION XORS 1070 REPAIR CARRIED OUT AS PER E.A.#: 1-5710- T0380742 PART 1. TITLE: WING BASIC WING STRUCTURE LH WING LOWER REAR SPAR CAP AFT FLANGE CORROSION REPAIR, XORS 1067 TO XORS 1074. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X = 47.5 FOUND CROWN DAMAGED. CABIN - AT SEAT TRACK STATION 5-10, X = 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 5-63 TO EXISTING SPLICE STATION 1531/5-0, X = 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 614 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 880. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 880 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 903. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 903 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — NO DISCREPANCY (ZONE 500) · airframe 97,301 hrs · 20,676 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER STATION XOS 663 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER STATION XOS 663 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001 B7 PART 1 TITLE STRUCTURES - REPAIR CATALOG - MD- 11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN Ï¿½ MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X = - 47.5Ï¿½ FOUND CROWN DAMAGED. CABIN - AT SEAT TRACK STATION 1541, X = - 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1571 TO EXISTING SPLICE STATION 1531/5-123, X= - 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 97,301 hrs · 20,676 cycles

RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 651. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 651 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1426, X = - 27.5 FOUND CROWN DAMAGED. CABIN - AT SEAT TRACK STATION 1426, X = - 27.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1411 TO STATION 1451, X = - 27.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN BS 1571 TO 1691 X = 8.5 LT SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 1571 TO STATION 1691 X = 8.5 LEFT HAND SIDE EVALUATED AND FOUND CROWN DAMAGED (WORN) AT STATION 1581 EXCEEDED LIMIT IAW SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. DAMAGED (WORN) SEAT TRACK REPAIRED BY REPLACEMENT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B7 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 97,301 hrs · 20,676 cycles

EXISTING REPAIR AT MAIN DECK CARGO TRACK BETWEEN STATION 1531 TO STATION 1631 X = -8.5 RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 1531 TO STATION 1631 X = -8.5 RIGHT HAND SIDE EVALUATED AND FOUND CROWN DAMAGED (WORN) AT STATION 1541 EXCEEDED LIMIT IAW SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101. DAMAGED (WORN) SEAT TRACK REPAIRED BY REPLACEMENT IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. EO 1-5100-7-5001 B7 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — NO DISCREPANCY (ZONE 100) · airframe 97,301 hrs · 20,676 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT STATION 5-73, LONGERON 12 RIGHT (FRAME) EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT STATION 5-73 LONGERON 12 RIGHT HAND SIDE (FRAME) EVALUATED AND FOUND REPAIRED IAW SRM 53-00-07- 2R REPAIR 2 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 100) · airframe 97,301 hrs · 20,676 cycles

FOUND CRACK INDICATION DURING HFEC INSPECTION, APPROXIMATELY 0.25 INCH IN LENGTH, AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING LOWER SECTION STATION Y=595 ON EXISTING SLOT OUT AREA. CRACK AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING LOWER SECTION STATION Y=595 ON EXISTING SLOT OUT AREA, REPAIR ACCOMPLISHED PER E.A.#:1-5310-T0380699 P1 AND MD-11 SRM 53-10-14 REPAIR 2, FIGURE 202. TITLE: FUSELAGE MAINFRAME CRACK REPAIR ON LH NOSE LANDING GEAR TRUNNION FITTING, STA 595. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SWITCH — FAILED (UNKNOWN) · airframe 96,962 hrs · 20,563 cycles

CABIN RATE ALERT ON CLIMB OUT. CYCLED CONTOLLERS WITH NO CHANGE. LEVELED OFF AT 11,000 THEN DESCENDED DOWN TO 9,000 WITH CABIN ALT ALERT. AIR TURN BACK TO KIND. FOUND MIAN CARGO DOOR VENT DOOR OPEN. FLIGHT CREW SAID THEY NEVER HAD A DOOR OPEN INDICATION. OPENED & CLOSED DOOR SEVERAL TIMES. LIGHT WAS OUT INITIALLY BUT INDICATION DID RETURN TO NORMAL. SUSPECT SWITCH IS INTERMITTENT. DOOR LATCH IS SERVICEABLE AND LATCHES SECURELY. CARGO DOOR UPR A ALERT - INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT.REMOVED AND REPLACED VENT DOOR WARNING SWITCH (S1-1346), REF SSM 52-34-0. TESTS NORMAL IAW AMM 52-70-00-5.

Part: TIRE — LEAKING (NLG) · airframe 96,745 hrs · 20,504 cycles

3 HRS 46 MINS INTO THE FLIGHT RECEIVED A LEVEL 1 TIRE PRESSURE LOW. THE LEFT NOSE WHEEL SHOWED 132 PSI, THE RIGHT SHOWED 178 PSI. DURING THE REMAINDER OF THE FLIGHT THE PRESSURE DROPPED DROPPED TO 88 PSI FOR THE LEFT AND 160 FOR THE RIGHT NOSEWHEEL. AFTER LANDING TAXI AND BLOCK IN THE LEFT PSI CAME UP TO 111, THE RIGHT TO 221. VERIFIED TIRE PRESSURE INDICATION, REPLACED LH NLG TIRE PER ABOVE REF, TIRES SVC'D TO NORMAL LIMITS, OPS CHK GOOD

Part: SKIN — CRACKED (ZONE 500) · airframe 93,768 hrs · 19,718 cycles

LEFT HAND WING #8 LEADING EDGE SLAT LOWER SKIN SURFACE (COVE PANEL) FOUND CRACK AT STATION XOS 1146.814 LEFT HAND WING #8 LEADING EDGE SLAT LOWER SKIN SURFACE (COVE PANEL) CRACK AT STATION XOS 1146.814 REPAIRED AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AND EA 1-5750-T0339798 A P2 TITLE : WINGS - FLIGHT SURFACES - LH WING SLAT NO. 8, INNER SKIN SPLICE REPAIRS AT STA XOS 1028 - 1058, STA XOS 1089 - 1105, STA XOS 1144 - 1158 - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 93,768 hrs · 19,718 cycles

LEFT HAND WING #8 LEADING EDGE SLAT LOWER SURFACE (COVE PANEL) FOUND CRACK AT STATION XOS 1030.567 LEFT HAND WING #8 LEADING EDGE SLAT LOWER SURFACE (COVE PANEL) CRACK AT STATION XOS 1030.567 REPAIRED AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AND EA 1-5750-T0339798 A P2 TITLE : WINGS - FLIGHT SURFACES - LH WING SLAT NO. 8, INNER SKIN SPLICE REPAIRS AT STA XOS 1028 - 1058, STA XOS 1089 - 1105, STA XOS 1144 - 1158 - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

AFT CARGO - FLOOR PANEL SUPPORT AFT UPPER CHORD STATION 1841 X = -26.5 FOUND CORROSION AFT CARGO - FLOOR PANEL SUPPORT AFT UPPER CHORD STATION 1841 X = -26.5 CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS PER SRM 53-00- 00-2R REPAIR GENERAL FIGURE 202. FLOOR PANEL SUPPORT REMOVED AND REPLACED WITH REWORKED SUPPORT AS PER SRM 51-31-01-0G. FLOOR PANEL SUPPORT REWORKED FROM S2505014 EXTRUSION AS PER DOUGLAS DRAWING AGA7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 46 LEFT SPLICE SUSPECT CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 46 LEFT REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 1701 - 1721 LONGERON 51 LEFT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 1701 - 1721 LONGERON 51 LEFT REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING AFA 7102 REVISION E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 52 SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 52 REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 51 RIGHT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 51 RIGHT REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A 7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

AFT CARGO - STATION 1841 RIGHT HAND WEB FOUND CRACKED. CRACKED WEB AT AFT CARGO - STATION 1841 RIGHT HAND REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 44 LEFT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 44 LEFT REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 51 LEFT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 5-113 TO 1541 LONGERON 51 LEFT REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - BILGE STATION 1701 - 1721 LONGERON 49 LEFT SPLICE FOUND CRACKED. CRACKED SPLICE AT CENTER CARGO - BILGE STATION 1701 - 1721 LONGERON 49 LEFT REMOVED AND REPLACED WITH FABRICATED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED AS PER DOUGLAS DRAWING AFA 7102 REVISION E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 93,768 hrs · 19,718 cycles

CENTER CARGO - FLOOR PANEL SUPPORT FORWARD CHORD STATION 1841 X = 7 TO -44 FOUND CORROSION CENTER CARGO - FLOOR PANEL SUPPORT FORWARD CHORD STATION 1841 X = 7 TO -44 CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED ALLOWABLE LIMITS PER SRM 53-00-00-2R REPAIR GENERAL FIGURE 202. FLOOR PANEL SUPPORT REMOVED AND REPLACED WITH REWORKED SUPPORT AS PER SRM 51-31-01-0G. FLOOR PANEL SUPPORT REWORKED FROM S2932021 EXTRUSION AS PER DOUGLAS DRAWING AGA7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 93,768 hrs · 19,718 cycles

RIGHT HAND WING FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 906 RIGHT HAND WING FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 906 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 93,768 hrs · 19,718 cycles

LEFT HAND WING FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 635. LEFT HAND WING FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 635 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 93,768 hrs · 19,718 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FIXED LEADING EDGE SKIN CORNER 13 AT STATION XOS 657 ( SLAT TRACK #10 CUTOUT , AFT INBOARD CORNER ) FOUND CRACK APPROXIMATE 0.15 " RIGHT HAND FIXED LEADING EDGE SKIN CORNER 13 AT STATION XOS 657 (SLAT TRACK #10 CUTOUT, AFT INBOARD CORNER ) REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 93,768 hrs · 19,718 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FIXED LEADING EDGE SKIN CORNER 11 AT STATION XOS 610 (FUEL ACCESS DOOR FORWARD INBOARD CORNER) FOUND CRACK APPROXIMATE 0.8 ". CRACK AREA ON LEFT HAND FIXED LEADING EDGE SKIN CORNER 11 AT STATION XOS 610 (FUEL ACCESS DOOR FORWARD INBOARD CORNER) REPAIRED AS PER SRM 57-40-01-2R REPAIR 18 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT NEXT C CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION AT EVERY C CHECK NOT EXCEEDING 24 MONTHS BY VISUAL METHOD AS PER SRM 57-40-01-2R FIGURE 201 TABLE 204 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 93,768 hrs · 19,718 cycles

LEFT HAND WING FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 675. LEFT HAND WING FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 675 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (ZONE 100) · airframe 93,005 hrs · 19,521 cycles

PDIS 595 24-40 5629 19MAR22 ANC FACT U ON SHUTDOWN, WHILE TRANSFERRING TO EXTERNAL POWER, DEU 3,4,AND 5 WENT BLANK, MCDU 2 AND 3 WENT BLANK CIRCUIT BREAKERS STANDBY ALTIMETER VIBRATOR, AVIONICS COMPARTMENT EXHAUST FAN, CAC FAN 1,2, AND 3, AVIONICS RACK FAN 2, AND AVIONICS COMPARTMENT COOLING FAN ALL POPPED. WE SMELLED SMOKE AND REMOVED ALL POWER FROM AIRCRAFT. FACT 19MAR22 22:31 ANC U REPLACED EXTERNAL POWER RELAY REF M/M 24-41-01-4.

Part: NONE — CORRODED (ZONE 700) · airframe 91,822 hrs · 19,192 cycles

LH MLG SUPPORT FAYING SURFACE REWORK AND POSTPONE OF ATTACH HOLE COLD WORK COMPLIED IAW E.A.#1-5740-T0364727 BLEND THE UPPER AND LOWER MLG SUPPORT FAYING SURFACES,LOWER FAYING SURFACE FELL OUT OF S.R.M.. LIMITS,

Part: PIN — FAILED (STAB CONTROL) · airframe 89,063 hrs · 18,467 cycles

AFTER TAKEOFF AND AFTER FLAP RETRACTION WITH AUTOPILOT ON GOT A LEVEL 1 "STAB OUT OF TRIM". AUTOPILOT DISCONNECTED AND WE WERE UNABLE TO MOVE STAB TRIM EITHER WITH TRIM SWITCHES OR MANUAL HANDLES. FLEW WITH AUTOPILOT OFF AND DUMPED 100K POUNDS OF FUEL. MADE MANUAL LANDING. TRIM NEVER MOVED FROM TAKEOFF POSITION OF 8.4. REMOVED HORIZONTAL STAB CHAIN DRIVE UNIT, PER AMM 27-44-06-4. FOUND FUSE PIN SHEARED. REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: AJH7337-507 POS: ONL SRL: DCA-415 ON MPN: AJH7337-507 CPN: 2710948 SRL: FX0002.

Part: RELAY — FAILED (BATTERY) · airframe 89,059 hrs · 18,465 cycles

REPEAT WRITEUP, AT TOC FL 331 STARTED SETTING BAT DISCHARGING ALERT INTERMITTENTLY COMING ON, SOMETIMES LASTING 15-20 SECONDS APPROXIMATELY SMOOTH AIR. BATTERY VOLTAGE ON SYNOPTIC WAS NEVER BELOW 29 VOLTS. FOUND RELAY R2-5142 INTERMITTENTLY NO OUT PUT, RELAY R2-5145 NO ACTIVATION WITH POWER ON, PIN A2/A3 STUCK ON. REPLACED BOTH RELAYS, PER WDM 24-62-11 AND TEST NORMAL, PER AMM 24-32-00-5. REMOVED AND REPLACED THE GROUND SERVICE RELAY R2-15, PER AMM 24-53-01-4. PERFORMED RETURN-TO-SERVICE TEST OF EPCU, PER AMM 24-08-01-5, TEST PASSED. PERFORMED OPERATIONAL TEST OF THE BATTERY, PER AMM 24-34-02-5, TEST NORMAL. PERFORMED OPERATIONAL TEST OF THE BATTERY CHARGER RELAY R2-24, PER AMM 24-34-01-2, TEST NORMAL.PERFORMED OPERATIONAL TEST OF THE BATTERY CHARGER, PER AMM 24-34-03-4, TEST NORMAL.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 88,326 hrs · 18,273 cycles

CENTER CARGO - DOOR FORWARD BOTTOM CORNER BETWEEN XIFH 1708 - 1717 FOUND CHAFFING. CENTER CARGO DOOR FORWARD BOTTOM CORNER BETWEEN XIFH 1708 - 1717 REPAIR CARRIED OUT AS PER EA #1-5230-T0355307 PART 1, TITLE: DOORS - CARGO DOOR - DEVIATION TO SRM 52-30-16 REPAIR 3 - CENTER LOWER CARGO DOOR OUTER SKIN, FORWARD LOWER CORNER XIFH 1708-1717. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 88,326 hrs · 18,273 cycles

CENTER CARGO - DOOR FORWARD BOTTOM CORNER BETWEEN XIFH 1708 - 1717 FOUND CHAFFING. CENTER CARGO DOOR FORWARD BOTTOM CORNER BETWEEN XIFH 1708 - 1717 REPAIR CARRIED OUT AS PER EA #1-5230-T0355307 PART 1, TITLE: DOORS - CARGO DOOR - DEVIATION TO SRM 52-30-16 REPAIR 3 - CENTER LOWER CARGO DOOR OUTER SKIN, FORWARD LOWER CORNER XIFH 1708-1717. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — CORRODED (BS 1959) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

AFT CARGO - DOORWAY AFT JAMB FRAME SURFACE, LEFT HAND STATION 1959 X=32 TO 55 FOUND CORROSION. AFT CARGO DOORWAY AFT JAMB FRAME SURFACE LEFT HAND STATION 1959 X=32 TO 55 CORROSION REMOVED AND FOUND X=34 TO 55 WITHIN LIMIT AS PER SRM 53-00-00-2R FIGURE 205 AND X=32 TO 33 EXCEEDED LIMIT AREA REPAIR CARRIED OUT PER EA 1-5310-T0355300 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1940) · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO, FOUND THE FLOOR SUPPORT AT BS 1940, X - 57 TO BE CORRODED.

Part: SEAT TRACK — CORRODED (BS 1671) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT, FOUND THE SEAT TRACK FLANGE CORRODED AT BS 1671, X 8.5. CORROSION REMOVED AND FOUND EXCEEDED LIMIT SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BETWEEN BS 1691 TO 1571 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT — CORRODED (BS 1940) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00-2R, FIGURE 206, ALLOWABLE DAMAGE. THE FLOOR SUPPORT WAS REMOVED AND REPLACED BETWEEN BS 1887 - 2007 IAW SRM 51-31-01-0G. CLASSIFIED AS MAJOR IAW GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (BS 1246.5) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1246.5 , RBL 75.25 FLANGE WAS CORRODED. THE CORROSION WAS REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1601) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT , FOUND SEAT TRACK CORRODED AT STATION 1601 , X 8.5 . MAIN DECK CARGO COMPARTMENT AT SEAT TRACK BS 1601, X 8.5, CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1691 TO EXISTING SPLICE 1571 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1784) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT , FOUND SEAT TRACK AT BS 1784 , X - 8.5 CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1751 TO 1811 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1254) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT , FOUND SEAT TRACK AT STATION 1254 , X = - 75.25 FLANGE CORRODED . MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1254 , X = - 75.25 CORROSION REMOVED 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 1209 TO STATION 1269 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REFER TO SNRM N00830 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100 .

Part: CAP — CORRODED (BS 1841) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

CENTER CARGO - STATION 1841 X = 56 LEFT HAND BILGE AREA CAP FOUND CORROSION. CENTER CARGO - STATION 1841 X = 56 LEFT HAND BILGE AREA AT CAP CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-2R FIGURE 205 . CAP REMOVED AS PER SRM 51-31-01-0G . CAP FABRICATED AS PER DOUGLAS DRAWING AGA 7098 REVISION H AND INSTALLED AS PER SRM 51-31-01-0G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (BS 1225) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT FOUND SEAT TRACK AT BS 1225 RBL 75.25 FLANGE CORRODED. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1252) · corrosion level 2 · airframe 88,326 hrs · 18,273 cycles

MAIN DECK CARGO COMPARTMENT , FOUND SEAT TRACK AT STATION 1252 , X = - 75.25 FLANGE CORRODED . MAIN DECK CARGO COMPARTMENT AT SEAT TRACK FLANGE STATION 1252 , X= - 75.25 CORROSION REMOVED 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 1209 TO STATION 1269 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REFER TO SNRM N00830 FOR WORK DETAILS . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: TRUNNION — CRACKED (BS 583) · airframe 88,326 hrs · 18,273 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON EXISTING TRIMMED OUT AREA X= -24, BS 583 OF NOSE LANDING GEAR RIGHT TRUNNION FITTING, FOUND CRACKED APPROXIMATE 0.8". THE NLG TRUNNION FITTING WAS REPAIRED IAW SRM 53-10-14-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CRACKED (BS 583) · airframe 88,326 hrs · 18,273 cycles

DURING ACCOMPLISHMENT OF SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER: N00325, HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING STATION 583 AND FOUND LONGERON IN THE TRIMMED AREA WITH CRACK INDICATION PROPAGATE FROM THE LOWER FASTENER HOLE APPROXIMATELY 0.250 INCHES LENGTH. NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION 583 X = - 24 ATTACH AREA CRACKED LONGERON REMOVED AND REPLACED WITH NEW LONGERON AS PER SRM 51-31-01- 0G . REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 .

Part: DOUBLER — CRACKED (LT WING) · airframe 88,326 hrs · 18,273 cycles

LEFT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT XOS 908. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,326 hrs · 18,273 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS695.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,326 hrs · 18,273 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS695. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 695 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LE SLAT) · airframe 88,326 hrs · 18,273 cycles

LEFT HAND WING NUMBER 1 SLAT CRUISE PERFORMANCE FILLET RIB AT ALIGNMENT PIN AREA FOUND CRACK.

Part: RIB — CRACKED (RT WING) · airframe 88,326 hrs · 18,273 cycles

LEFT HAND WING NUMBER 1 SLAT CRUISE PERFORMANCE FILLET RIB AT XIS 150.7474 ALIGNMENT PIN AREA FOUND CRACK. LEFT HAND WING NUMBER 1 SLAT CRUISE PERFORMANCE FILLET RIB AT XIS 150.7474 REPAIR CARRIED OUT IN ACCORDANCE WITH EA 1-5750-T0355185 P1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 88,326 hrs · 18,273 cycles

LEFT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKED AT XOS 755. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,326 hrs · 18,273 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACK A AT STATION XOS731. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 731 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,326 hrs · 18,273 cycles

RIGHT HAND FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACK AT STATION XOS731.

Part: DOUBLER — CRACKED (RT WING) · airframe 88,326 hrs · 18,273 cycles

RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS682.

Part: DOUBLER — CRACKED (LT WING) · airframe 88,326 hrs · 18,273 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS908.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 88,326 hrs · 18,273 cycles

RIGHT WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS682. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 682 REPAIR CARRIED OUT 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 88,326 hrs · 18,273 cycles

LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS755.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,965 hrs · 18,194 cycles

DURING PREFLIGHT, CREW REPORTED WHEN TESTING EMERGENCY LIGHTS EIS MESSAGE SHOWED EMERGENCY LIGHTS BATTERY LOW. EMERGENCY LIGHTS OPERATIONS CHECK 'SATIS' IAW AMM 33-52-01-5, PLACARD REMOVED.

Part: TIRE — FAILED (LT MLG) · airframe 87,778 hrs · 18,157 cycles

LEVEL 2 "TIRE FAILURE" ON #5 TIRE ON SHORT FINAL. R & R # 5 MLG TIRE ASSY. INSPECTED AREA OF LT MLG, CHECK GOOD. REF MM 32-41-01-4.

Part: RELAY — UNKNOWN (ZONE 100) · airframe 86,141 hrs · 17,654 cycles

LEVEL 1 EMERGENCY PWR ON IN FLIGHT, COMPLIED WITH QRH, ALERT REMAINED ON. DEPLOYED ADG PER QRH WITH MOCC CONCURRENCE CHECKED ASSOCIATED WIRING FROM OVERHEAD ELECTRICAL PANEL TO EPCU AND FROM R2-17 TO R2-5411. NO DEFECTS NOTED. REPLACED R2-17 AND R2-5411. PERFORMED EMERGENCY POWER TEST. ALL TEST PASSED.

Part: TRANSDUCER — FAILED (WHEEL SPEED) · airframe 83,871 hrs · 16,909 cycles

PDIS 595 32-42 1218 22SEP18 LAX FACT U LOGPAGES:2871877 BEFORE TAKEOFF RECEIVED LEVEL 2 "TIRE FAIL" ALERT. #9 TIRE DISPLAY LOST - RETURNED TO GATE. REMOVED & REPLACED WHEEL SPEED TRANSDUCER IAW MM 32-45-03-4 & 32-45-03-5 OPS CHECK NORMAL.

Part: TRANSDUCER — FAILED (MLG) · airframe 83,255 hrs · 16,734 cycles

TIRE FAIL ABNORMAL ALERT DISPLAYED INFLIGHT. CONFIG PAGE SHOWED TIRE NR 5 AND 6 AT 80 PSI. SUBSEQUENTLY ALERT WENT AWAY AND PRESSURE WAS NORMAL ON CONFIG. CFDS FAULTS LAST FLIGHT CONFIRMED NR 5 TIRE PRESSURE TRANSDUCER FAILED. INSTALLED SERVICEABLE NR 5 WHEEL TIRE PRESSURE TRANSDUCER REF AMM 32-46-03-4. INDICATION OPERATES NORMAL

Part: SKIN — CRACKED (A/C BAY DOOR) · airframe 82,815 hrs · 16,600 cycles

NR 2 AIR CON COMPARTMENT DOOR SKIN AND FRAME FOUND CRACKED.

Part: SKIN — BULGED (BS 2033) · airframe 82,815 hrs · 16,600 cycles

BS 2033 EMPENNAGE APU CUTOUT FWD LT SIDE FOUND SKIN BULGE.

Part: INTERCOSTAL — CRACKED (EMPENNAGE) · airframe 82,815 hrs · 16,600 cycles

RIGHT REAR CENTER EMPENNAGE SPAR TO REAR SPAR INTERCOSTAL FOUND CRACKED.

Part: FLOOR SUPPORT — CRACKED (BS 1887-2007) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK AFT FLOOR SUPPORT AT BS 1887 - 2007 FOUND CRACKED AT FWD END AREA.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,815 hrs · 16,600 cycles

RIGHT WING FIXED L/E LOWER CAVITY FOUND BEADED DOUBLER CRACKED, XOS 655.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,815 hrs · 16,600 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 731 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 82,815 hrs · 16,600 cycles

LEFT WING LEADING EDGE NR 12 SLAT TRACK CUTOUT, LOWER OTBD CORNER SKIN CRACKED AT XOS 776. REPAIRED IAW SRM 57-40-02-2R, FIGURE 201, REPAIR 7. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,815 hrs · 16,600 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 646 FOUND CRACKED. REPAIRED THE LEFT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STIFFENER — CRACKED (RT WING) · airframe 82,815 hrs · 16,600 cycles

RIGHT WING FIXED L/E LOWER CAVITY FOUND RIB STIFFENER CRACKED, XOS 669.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,815 hrs · 16,600 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 881 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,815 hrs · 16,600 cycles

RIGHT WING FIXED L/E LOWER CAVITY BEADED DOUBLER CRACKED, XOS 675.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,815 hrs · 16,600 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 655 FOUND CRACKED. REPAIRED THE LEFT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 82,815 hrs · 16,600 cycles

LEFT WING NR 8 L/E SLAT LOWER SURFACE SKIN FOUND CRACKED ABOUT 2 INCHES IN LENGTH AT XOS 1055.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,815 hrs · 16,600 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 613 FOUND CRACKED. REPAIRED THE LEFT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (BS 535) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK, FRAME, BS 535, LONGERON 24R FOUND DAMAGED.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 82,815 hrs · 16,600 cycles

DURING HFEC INSPECTION, THE NR 4 BANJO FITTING OF THE LOWER VERTICAL STABILIZER, RT REAR SPAR CAP FWD FLANGE AT THE UPPER SECTION, VSS 2164, FOUND ONE CRACK ALONG THE RADIUS AT THE LOWEST FASTENER, APPROX 1.377 INCHES IN LENGTH.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 82,815 hrs · 16,600 cycles

DURING HFEC INSPECTION ON THE NR 4 BANJO FITTING OF THE LOWER VERTICAL STABILIZER, THE LT REAR SPAR CAP FWD FLANGE AT THE UPPER SECTION, VSS 2164, FOUND ONE CRACK ALONG THE RADIUS AT THE LOWEST TWO FASTENER. APPROX 2.244 INCHES IN LENGTH.

Part: SEAT TRACK — GOUGED (BS 1281) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK SEAT TRACK AT BS 1281, RBL 8.5, CROWN GOUGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (BS 1541) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1541, X=47.5, FOUND CROWN DAMAGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK SEAT TRACK AT BS 5-10, RBL 8.5 FOUND CROWN DAMAGED. OUT OF LIMITS IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 5-10, X-47.5 FOUND CROWN DAMAGED.

Part: FRAME — CRACKED (BS 555) · airframe 82,815 hrs · 16,600 cycles

NR 1 AIR CONDITIONING COMPARTMENT BS 555 FRAME FOUND CRACKED.

Part: SEAT TRACK — CHAFED (COCKPIT) · airframe 82,815 hrs · 16,600 cycles

RT OBSERVER`S SEAT TRACK FOUND CHAFED.

Part: SEAT TRACK — GOUGED (BS 1281) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK SEAT TRACK AT BS 1281, LBL 8.5, FOUND CROWN GOUGED. THE SEAT TRACK WAS REPLACEMED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 5-10, X=27.5 FOUND CROWN DAMAGED.

Part: SEAT TRACK — GOUGED (BS 1281) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK SEAT TRACK AT BS 1281, RBL 47.5, CROWN GOUGED.

Part: SEAT TRACK — GOUGED (BS 1541) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK SEAT TRACK AT BS 1541, LBL 8.5, FOUND CROWN DAMAGED.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 82,815 hrs · 16,600 cycles

MAIN DECK SEAT TRACK AT BS 6-50, RBL 27.5, FOUND CROWN DAMAGE. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TIRE — FAILED (LT CNTR MLG) · airframe 82,684 hrs · 16,557 cycles

DURING CLIMBOUT, PASSING APPROXIMATELY 15,000 FT, RECEIVED A LVL 1 TIRE PRESSURE LOW ALERT. CALLED UP CONFIG SYNOPTIC AND OBSERVED LEFT CENTER TIRE PRESSURE FALLING RAPIDLY FROM APPROX 100 - 120 TO 0. LVL 2 TIRE FAIL ALERT WITH PRESSURE PASSING APPROXIMATELY 30. CHECKED QRH 13-03-09 AND SIMULTANEOUSLY NOTED BRAKE TEMP CTR LT, RISING RAPIDLY. RECEIVED A LVL 2 BRAKE OVERHEAT. STARTED DESCENT AND SLOWED TO LOWER GEAR. MAX TEMP OBSERVED 550 DEGREE. KEPT GEAR DOWN UNTIL TEMP REACHED APPROXIMATELY 250 DEGREES, TRIED RAISING GEAR, TEMP IMMEDIATELY STARTED TO RISE. LOWERED THE GEAR AND COOLED BRAKE TO APPROXIMATELY 100 DEGREES. RAISED GEAR AGAIN, MAX BRAKE TEMP THEN AT 120 DEGREES. UNEVENFULL LANDING. NO APPARENT DAMAGE TO THE TIRE, TIRE FLAT.

Part: LAMP — INOPERATIVE (PSI INDICATOR) · airframe 82,634 hrs · 16,543 cycles

DURING A POST FLIGHT INSPECTION. FOUND THE L1 DOOR SLIDE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 25-61-03-5

Part: PUSHROD — OUT OF POSITION (SHUTOFF VALVE) · airframe 81,978 hrs · 16,360 cycles

DURING PREFLIGHT NOTICED #2 FIRE HANDLE SLIGHTLY OUT OF NORM POSITION. PUSHED HANDLE INTO NORM, NO ABNORMAL INDICATIONS. AFTER TAKEOFF GOT LEVEL 1 GEN 2 OFF ALERT ACCOMPANIED WITH FIRE IND IN #2 FIRE HANDLE, NO OTHER INDICATIONS OR WARNINGS. NOTICED FIRE HANDLE NOT FULLY IN NORM & BUMPED IT INTO NORM. BOTH WARNINGS WENT AWAY & RESULTED IN EGPS FAIL. CHECKED #2 FIRE HANDLE RIGGING PER AMM 76-20-01-5 & FOUND #2 FIRE HANDLE WAS OUT OF LIMIT. FURTHER T/SHOT & FOUND #2 HYD FIRE S/O VALVE PUSH ROD INTERFERED WITH VALVE DRAIN HOSE ON #2 HYD RESERVOIR. REROUTE HOSE RESET #2 GEN AFTER #2 FIRE HANDLE OPS CK IN RAN EPCU RTS TEST PER AMM 24-08-01-5,EPCU RTS PASSED. RAN #2 ENG IAW JRH & #2 GEN OPS NORMAL OK FOR SVC.

Part: HANDLE — OBSTRUCTED (FIRE) · airframe 81,986 hrs · 16,362 cycles

ON PREFLT NOTICED THAT THE NR 2 ENGINE FIRE HANDLE WAS OUT THE NORMAL POSITION, SLIGHTLY DOWN. ATTEMPTED TO RETURN TO NORMAL WITHOUT LUCK, 19 MINUTES AFTER TAKEOFF APPROACHED A LEVEL ONE GENERATOR 2 OFF ALERT ACCOMPANIED WITH THE NR 2 FUEL LEVER ENGINE FIRE INDICATION. CONSULTED QRH. NO RELIEF, PUSHED THE NR 2 FIRE HANDLE BACK TO NORMAL POSITION GEN 2 OFF ALERT DISAPPEARED ALONG WITH THE ABSENCE OF THE FIRE INDICATION IN THE NR 2 FUEL LEVER, GEN RESET. FOLLOWED BY A EPGS FAULT LEVEL ONE. CHECKED THE NR 2 FIRE HANDLE RIGGING AND FOUND THE NR 2 FIRE HANDLE POSITION WAS OUT OF LIMITS. SHOULD BE IN PLUS/MINUS 0.15" AT NORMAL POSITION BUT IT WAS APPROX 1" BELOW THE NORMAL POSITION AND EPCU CURRENT FAULT SHOWED FIRE SWITCH 2 ACT/INTFC. FOUND THE NR 2 HYD FIRE SHUTOFF VALVE PUSH ROD WAS INTERFERRING WITH THE VALVE DRAIN HOSE ON NR 2 HYD RESERVOIR. REROUTED THE HOSE AND NR 2 FIRE HANDLE OPS CHECKED NORMAL. HANDLE POSITION WITHIN LIMITS. RESET NR 2 GENERATOR. RAN EPCU RTS TEST, EPCU RTS PASSED. RAN NR 2 ENGINEAND NR 2 GENERATOR OPS NORMAL. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 81,864 hrs · 16,334 cycles

ON SHORT FINAL TO VOBL RWY 9 WITH A/P DISCONNECTED HAD MULTIPLE LEVEL 2 WARNING FLASH 2 TO 3 TIME. USE MANUAL SPOILERS AUTOBRAKES INOP WERE 2 THAT STOOD OUT. ATC REPORTED A 100 DIFFERENCT IN ALT REPORTED AND WHAT WAS INDICATED IN COCKPIT. NIL CURRENT FAULTS AND FAULT REVIEW, PERFORMED AUTO FLIGHT RETURN TO SERVICE TESTS ON BOTH FCC 1 & FCC 2 IAW MD-11 AMM 22-00-00-5 AND OPS CHECKS GOOD. ALL TEST PASSED. T/S AS PER FIM 34-12-02 FOR ALTITUDE DIFFERENCE. NIL FAULTS REF AMM 34-16-14-5. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 79,651 hrs · 15,646 cycles

REMOTE BOTTLE LIGHT INOPERATIVE ON THE R1 DOOR.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 79,651 hrs · 15,646 cycles

REMOTE BOTTLE LIGHT INOPERATIVE ON THE R1 DOOR.

Part: ACTUATOR — FAILED (CARGO DOOR) · airframe 79,056 hrs · 15,486 cycles

AFT LOWER CARGO DOOR WILL NOT CLOSE. INSTALLED ACTUATOR, AFT-LOWER-CARGO DOOR. OPS CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (FUEL SYSTEM) · airframe 78,985 hrs · 15,465 cycles

RECEIVED A LAT FUEL IMBAL WARING AFTER 35 MIN OF FLIGHT. FUEL SYSTEM IN MANUAL AND PROPERLY CONFIGURED. RIGHT 17.8, CENTER 14.8, LEFT 20.2. QRH COMPLIED WITH TO CORRECT IMBALANCE. CREW VERBAL AFTER FUEL WAS BALANCED AND MESSAGE CLEARED. RECEIVED LAT FUEL IMBALANCE A SECOND TIME AND NOTIED FUEL QTY WAS INCREASING IN TANK NR 1, WHILE NR 2 AND 3 DECREASED. ENGINE FUEL BURN WAS EQUAL ACROSS ALL THREE ENGINES. R&R THE FUEL SHUTOFF VALVE CONTROLLER PER MD-11 M/M 28-21-02-4. REPLACED THE LEFT WING REFUEL/DEFUEL MANIFOLD ASSY PER MD-11 M/M 28-00-00-4. ALL PARTS WERE LEAK CHECKED AND OPS CHECKED GOOD.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION AT RT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.368", LOWER 0.365". MATERIAL REMOVED: UPPER 0.0101", LOWER 0.010", REMAINING THICKNESS: UPPER 0.358", LOWER 0.355". REPAIR SHIM FABRICATED AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1. TITLE: WINGS, FLIGHT SURFACES EO1-5750-7-5002, RT WING-OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS, HOLE SURFACE CORROSION. CORROSION AT LT WING, OTBD FLAP 11B, FWD HINGE, WING SIDE, BARREL NUT, HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.371", LOWER: 0.3955", MATERIAL REMOVED; UPPER 0.008", LOWER: 0.008", REMAINING THICKNESS UPPER; 0.363", LOWER: 0.3875". REPAIRED SHIM, FABRICATED AND INSTALLED IAW EA 1-5750-T0325375, PART 1, STEP 1. TITLE: WINGS, FLIGHT SURFACES E01-5750-7-5002, LT WING, OTBD FLAP, INBD HINGE, WING SIDE, CORROSION REPAIR. REFER TO WRI: 57507886 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CHAFED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE SKIN, INSPECTION CARRIED OUT IAW WRI 57307476 & FOUND EXISTING REPAIR DOUBLER WITH CHAFED MARK AT STATION XOS 906. CHAFED DAMAGE HAS BEEN REMOVED & NEW REPAIR DOUBLER REPAIR ACCOMPLISHED IAW EA 1-5710-79779C P 2. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. REFER TO WRI 57107894 FOR WORK DETAILS.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING LE SLAT EXTERIOR SKIN TE FOUND CRACK AT STATION XOS 816. TRIMMED OUT & DOUBLER REPAIR CARRIED OUT IAW EA 1-5750-T0325443 PART 1 P1. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100. REFER TO WRI 57507879 FOR WORK DETAILS. REPAIR IS A CATEGORY B WITH INITIAL INSPECTION AT NEXT AT C CHECK, NOT TO EXCEED 24 MONTHS & INSPECTION INTERVAL AT EVERY C CHECK NOT TO EXCEED 24 MONTHS.

Part: DOUBLER — CORRODED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE LOWER SKIN ATTACHMENT, DOUBLER FOUND CRACK AT STATION XOS 993. ACCOMPLISHED REPAIR IAW SRM 57-40-03-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER 1.226 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICATED & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1C. REFER TO WRI 57507886 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.665 INCHES, FINAL DIAMETER 0.677 INCHES & MAX ALLOWABLE DIAMETER 0.667 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325372 PART 1 STEP 1E. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08, EXISTING DIAMETER 0.627 INCHES, FINAL DIAMETER 0.629 INCHES & MAX ALLOWABLE DIAMETER 0.621 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-TO325375 PART 1 STEP 1D. REFER TO WRI 57507886 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.251 INCH, FINAL DIAMETER 1.254 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH;. REPAIRED BUSHING, FABRICATED & INSTALLED IAW EA 1-5750-T0325374 PART 1 STEP 1D. REFER TO WRI 57507887 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.727 INCHES, FINAL DIAMETER 0.731 INCHES & MAX ALLOWABLE DIAMETER 0.709 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1B. REFER TO WRI 57507886 FOR WORK DETAILS. REFER CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.282", FINAL DIA: 1.315", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325473, PART 1, STEP 1A AND 1C. TITLE: WINGS, FLIGHT SURFACES, EO1-5750-7-5003, RT WING, INBD FLAP, OTBD HINGE BRACKET ASSY. CORROSION REPAIR-PSE 57.55.01.2 REFER TO WRI: 57507900 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325374 PART 1 STEP 1B. REFER TO WRI 57507887 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIRED BUSHING, FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325372 PART 1 STEP 1C. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.582 INCH, FINAL DIAMETER 0.597 INCHES. MAX ALLOWABLE DIAMETER 0.584 INCHES. SHOULDER BUSHINGS, TWO EACH, FABRICATED BY MACHINING & INSTALLED AT LOWER MOUNT INBD & OTBD BORE IAW EA 1-5750-T0325372 PART 1 STEP 1A. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 6 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.2805 INCH, FINAL DIAMETER 1.284 INCH & MAX ALLOWABLE DIAMETER 1.254 INCH. REPAIRED BUSHINGS, FABRICATED & INSTALLED IAW EA 1-5750-T0325372 PART 1 STEP 1B. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.256 INCH, FINAL DIAMETER 1.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHINGS, FABRICATED & INSTALLED IAW EA 1-5750-T0325372 PART 1 STEP 1D. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA : 0.709". SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1B. TITLE: WINGS, FLIGHT SURFACES EO1-5750-7-5002. RT WING-OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER HOLE BORE CORROSION. CORROSION HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAX ALLOWABLE DIAMETER 0.391 INCH. REPAIRED BUSHING, FABRICATED & INSTALLED IAW EA 1-5750-T0325374 PART 1 STEP 1C. REFER TO WRI 57507887 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING, OTBD FLAP VANE HORN FITTING D FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.858", WIDTH: 0.598", FINAL SIZE: LENGTH 0.9495", WIDTH: 0.649", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940", WIDTH: 0.670". REPAIR BUSHING FABRICATED IAW EA 1-5750-T0325479, PART 1, STEP 2C, TITLE: WINGS, FLIGHT SURFACES EO1-5750-7-5002, LT WING, OTBD FLAP, VANE ASSY-TRACK SUPPORT REWORK AND REFER TO WRI: 57507896 FOR WORK DETAILS. BUSHING INSTALLED IAW AMM 27-50-32-4. FITTING REMOVED AND INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.708", FINAL DIA: 0.722". MAXIMUM ALLOWABLE DIA: 0.709". SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1B. TITLE: WINGS, FLIGHT SURFACES-EO1-5750-7-5002. RT WING, OTBD FLAP, INBD HINGE, WING SIDE CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION AT HOLE 3 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.598 INCHES, FINAL DIAMETER 0.604 INCHES, MAX ALLOWABLE DIAMETER 0.584 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325374 PART 1 STEP 1B. REFER TO WRI 57507887 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.390 INCHES, FINAL DIAMETER 0.407 INCHES, MAX ALLOWABLE DIAMETER 0.391 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325372 PART 1 STEP 1C. LIGHT SURFACES E01-5750-7-5002 LT WING OTBD FLAP, OTBD HINGE, WING SIDE, CORROSION REPAIR. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW MM 6-2-100

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.382 INCH, FINAL DIAMETER 0.410 INCH & MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. REPAIRED BUSHING, FABRICATED & INSTALLED IAW EA 1-5750-T0325374 PART 1 STEP 1C. REFER TO WRI 57507887 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION AT HOLE INBD BORE REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.2235 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICATED & INSTALLED IAW EA1-5750-T0325470 PART 1 STEP 1A & 1C. REFER TO WRI 57507895 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE. BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 1.255 INCH & MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING & FABRICATED & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1C. REFER TO WRI 57507886 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.222 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325470 PART 1 STEP 1A & 1C. REFER TO WRI 57507895 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.282", FINAL DIA: 1.288", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1C. TITLE: WINGS, FLIGHT SURFACES EO1-5750-7-5002-RT WING-OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE BORE CORROSION. CORROSION HOLE NR 2 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 0.944 INCHES, FINAL DIAMETER 0.951 INCHES, MAX ALLOWABLE DIAMETER 0.944 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325374 PART 1 STEP 1A. REFER TO WRI 57507887 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 1.250", FINAL DIA: 1.254", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1C. TITLE: WINGS-FLIGHT SURFACES EO1-5750-7-5002 RT WING-OTBD FLAP INBD HINGE, WING SIDE, CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING DIAMETER 1.252 INCH, FINAL DIAMETER 01.259 INCH, MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHINGS, FABRICATED & INSTALLED IAW EA 1-5750-T0325372 PART 1 STEP 1D. REFER TO WRI 57507888 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING, OTBD FLAP VANE HORN FITTING B FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.915", WIDTH: 0.621". FINAL SIZE: LENGTH 1.0395", WIDTH: 0.7395", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940", WIDTH: 0.670". REPAIR BUSHING FABRICATED IAW EA 1-5750-T0325479, PART 1, STEP 2A. TITLE: WINGS-FLIGHT SURFACES EO1-5750-7-5002 LT WING, OTBD FLAP VANE ASSY, TRACK SUPPORT REWORK AND REFER TO WRI: 57507896 FOR WORK DETAILS, BUSHING INSTALLED IAW AMM 27-50-32-4. FITTING REMOVED AND INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE SURFACE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING THICKNESS 0.437 INCHES, MATERIAL REMOVED FWD SIDE 0.006 INCHES, AFT SIDE 0.016 INCHES, REMAINING THICKNESS 0.415 INCHES, MIN ALLOWABLE THICKNESS 0.423 INCHES. REPAIR SHIM FABRICATED & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1. CORROSION REPAIR REFER TO WRI 57507886 FOR WORK DETAILS. REFER CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-48-08. EXISTING DIAMETER 0.708 INCHES, FINAL DIAMETER 0.731 INCHES, MAX ALLOWABLE DIAMETER 0.709 INCHES. REPAIR BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1B. REFER TO WRI 57507886 FOR WORK DETAILS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIA: 0.943", FINAL DIA: 0.953". MAXIMUM ALLOWABLE DIA: 0.944". REPAIRED BUSHING, FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0325475, PART 1, STEP 1A. TITLE: WINGS, FLIGHT SURFACES EO1-5750-7-5002, RT WING, OTBD FLAP INBD HINGE, WING SIDE CORROSION REPAIR. REFER TO WRI: 57507889 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING, OTBD FLAP VANE HORN FITTING C FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.918", WIDTH: 0.653". FINAL SIZE: LENGTH 1.019", WIDTH: 0.718", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940", WIDTH 0.670". REPAIR BUSHING, FABRICATED IAW EA 1-5750-T0325479, PART 1, STEP 2B, TITLE: WINGS, FLIGHT SURFACES-EO1-5750-7-5002-LT WING-OTBD FLAP VANE ASSY, TRACK SUPPORT REWORK AND REFER TO WRI: 57507896 FOR WORK DETAILS BUSHING INSTALLED IAW AMM 27-50-32-4. FITTING REMOVED AND INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.283", FINAL DIA: 1.315". MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0325473, PART 1, STEP 1A AND 1C. TITLE: WINGS, FLIGHT SURFACES EO1-5750-7-5003 RT WING, INBD FLAP, OTBD HINGE BRACKET ASSY, CORROSION REPAIR-PSE 57.55.01.2. REFER TO WRI: 57507900 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, UPPER MOUNT HOLE OTBD BORE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 0.942 INCHES, FINAL DIAMETER 0.950 INCHES & MAX ALLOWABLE DIAMETER 0.944 INCHES. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0325375 PART 1 STEP 1A. REFER TO WRI 57507886 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SUPPORT — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING OTBD LE SKIN INTERNAL SUPPORT FORMER ASSEMBLY, FOUND CRACK AT STATION XOS 585. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G. NEW FORMER FABRICATED IAW DWG ARB 2931 REV H & PROTECTED IAW SRM 51-21-01-0G. NEW FORMER INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 785. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT RT STATION 1681, LONGERON 12R. EXISTING REPAIR REMOVED IAW SRM 51-33-01-0G & REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES & REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE LOWER SUPPORT DOUBLER FOUND CRACK AT STATION XOS 505. CRACKED DOUBLER REMOVED IAW SRM 51-31-01-OG & FABRICATED NEW DOUBLER IAW DWG ARB 2933 REV A. INSTALLED NEW DOUBLER AT RT WING FIXED LE LOWER AREA AT XOS 505 IAW SRM 51-33-01-OG. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN FLOOR SEAT TRACK FOUND CRACKED AT RT STATION 635, X=-8.5. CRACKED SEAT TRACK REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT RT STATION 1661, LONGERON 12R. EXISTING REPAIR REMOVED IAW SRM 51-33-01-0G & REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES & REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 639. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 631. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,413 hrs · 15,285 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSIONS, AT RT STATION 1556, X=-27.5. CORRODED SEAT TRACK REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 655. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR DENTED AT RT STATION 1701, LONGERON 12R. EXISTING REPAIR REMOVED IAW 51-33-01-0G & REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES & REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R TABLE 201 REPAIR 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 765. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 664. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE COMPARTMENT FORMER FOUND CRACKED, AT STATION XOS 560. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G. NEW FORMER FABRICATED IAW DWG ARB 1162 REV S & PROTECTIVE TREATMENT CARRIED OUT IAW SRM 51-21-01-0G. NEW FORMER INSTALLED IAW SRM 51-34-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 761. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE SKIN SUPPORT FRAME, FORMER, FOUND CRACK AT STATION XOS 584. CRACKED SUPPORT FRAME, FORMER, REMOVED IAW SRM 51-31-01-OG & FABRICATED NEW FORMER IAW DWG ARB 2931 REV H. INSTALLED NEW FORMER AT RT WING FIXED LE SKIN IAW SRM 51-33-01-OG AT XOS 584. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN FLOOR SEAT TRACK FOUND CRACKED AT LT STATION 635, X= 8.5. CRACKED SEAT TRACK REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 711. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 695. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 626. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 738. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING LE COMPARTMENT, FIXED LE SKIN SUPPORT FRAME INTERNAL DOUBLER FOUND CRACKED, AT STATION XOS 667. CRACKED DOUBLER REMOVED IAW SRM 51-31-01-0G & FABRICATED DWG ARB3954 REV K. INSTALLED NEW DOUBLER IAW SRM 51-31-01-06. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING TE LOWER SPAR CAP STRAP FOUND CRACKED, AT STATION XORS 422. CRACKED STRAP SILL REMOVED IAW SRM 51-31-01-0G. NEW STRAP SILL FABRICATED IAW DWG ARC 7008 REV C & PROTECTIVE TREATED IAW SRM 51-21-01-0G. NEW STRAP SILL INSTALLED IAW SRM 51-34-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,413 hrs · 15,285 cycles

LEFT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 587. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN MAIN DECK CARGO COMPARTMENT. FRAME EXISTING REPAIR DENTED AT LT STATION 1701, LONGERON 12L. EXISTING DAMAGED REPAIR ANGLE REMOVED & REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES & REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES TO BE CARRIED OUT IAW SRM 53-00-07-2R TABLE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN FLOOR SEAT TRACK FOUND CRACKED AT RT STATION 63, X= -27.5. CRACKED SEAT TRACK REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 639. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSIONS, AT RT STATION 1661, X=-27.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 78,413 hrs · 15,285 cycles

RIGHT WING FIXED LE INTERNAL BEADED DOUBLER FOUND CRACKED, AT STATION XOS 700. ACCOMPLISHED REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 78,413 hrs · 15,285 cycles

DURING ACCOMPLISHMENT OF NDT INSPECTION AT TRANSVERSE SKIN SPLICE AT STATION 5 - 0, FOUND CRACK ON LONGERON 11R, CTR SPLICE AFT, BETWEEN 4TH & 5TH FASTENERS. R & R IAW SRM 51-33-01-0G. NEW LONGERON SPLICE PN AEA7633-509, FABRICATED BY MACHINING IAW DWG AEA 7633 REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TEST SWITCH — STUCK (EMERGENCY LIGHTS) · airframe 77,496 hrs · 14,948 cycles

ON CAPTAINS PREFLIGHT, EMER LIGHT TEST DOES NOT SHOW ON ND. POST-FLIGHT CHECK; FOUND "EMER LITE BAT 1 LO" ALERT ON EAD. FOUND EMER LITE TEST SWITCH, S1-402, IS STUCK IN THE TEST POSITION CAUSING EMER LITES TO ILLUMINATE CONTINUOUSLY WHILE ARMED. R&R TEST SWITCH IAW MD11 ELEC SMP. EMER LITE OPS CHECK SATISFACTORY REF MD11 AMM 33-50-00-5. MEL CLEARED.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 757 hrs · 14,418 cycles

L1 DOOR ASSIST BOTTLE HAS LOW PRESSURE.

Part: RESERVOIR — INOPERATIVE (L1 DOOR ASSIST) · airframe 757 hrs · 14,412 cycles

L1 DOOR EMERGENCY BOTTLE HAS LOW PRESSURE. R & R L1 DOOR PNEUMATIC STORAGE RESERVOIR IAW AMM 52-11-04-4. CHECKED GOOD. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 756 hrs · 14,379 cycles

FOUND L1 DOOR ASSIST BOTTLE PRESS LOW. SERVICED L1 DOOR BOTTLE IAW AMM 12-25-04-3.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 755 hrs · 14,360 cycles

L1 DOOR PRESS GAUGE 0 PSI. SERVICED L1 DOOR PRESS IAW MM 12-25-04-3.

Part: PRESSURE SYSTEM — DEFECTIVE (R1 DOOR) · airframe 74,040 hrs · 13,863 cycles

R1 DOOR EMER SLIDE REMOTE PRESS TO TEST BUTTON INOPERATIVE. R&R REMOTE PRESSURE ASSY PER M/M 25-61-04-4, 25-61-04-5 .

Part: SKIN — CRACKED (ZONE 500) · airframe 73,500 hrs · 13,704 cycles

LEFT WING SLAT TRACK NR 11 CUT OUT OTBD CORNER STATION XOS 720 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: SEAT TRACK — CRACKED (BS 1861) · airframe 73,500 hrs · 13,704 cycles

RIGHT BS 1861 RBL 27.5 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 73,500 hrs · 13,704 cycles

RT INBD FLAP DAMAGED. REPAIRED IAW EA 1-5750-T0308747 PART 1.

Part: UNKNOWN — ODOR (CABIN) · airframe 71,702 hrs · 13,151 cycles

DURING DESCENT, APPROXIMATELY 10.000 FT, A BURNING ODOR WAS DETECTED IN COCKPIT. ODOR SUBSIDED AFTER ABOUT ONE MINUTE. INSPECTED AIRCRAFT, COULD NOT DUPLICATE.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

SKIN AT CENTER CARGO DOOR AFT LOWER CUTOUT AREA MISREPAIRED. REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8 REV. 50

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 68,564 hrs · 12,263 cycles

RT WING INBD FLAP LOWER SKIN MISREPAIRED. REPAIRED IAW EA 1-5750-160994. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — CRACKED (ZONE 600) · airframe 68,564 hrs · 12,263 cycles

RT WING OTBD FIXED L/E AT XOS 906 FOUND CRACKED. REPAIRED AS PER SRM 57-40- 01 FIGURE201 REPAIR 9 REV.50.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 68,564 hrs · 12,263 cycles

RT WING INBD FLAP UPPER SKIN MISREPAIRED. REPAIRED IAW EA 1-5750-160994. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (BS 495-515) · airframe 68,564 hrs · 12,263 cycles

SKIN BS 495 TO 515 BETWEEN LONGERON 45 TO 46 LT MISREPAIRED. REPAIRED AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 REV. 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (LT WING) · airframe 68,564 hrs · 12,263 cycles

LT WING L/E TELSCOPIC DUCT CUTOUT MISREPAIRED. REPAIRED AS PER SRM 57- 40-01 REPAIR 10 FIGURE 201 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

CENTER CARGO BETWEEN STA 5-113 AND STA 1561, LONGERON 37 RT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7114 REVISION: E. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

CENTER CARGO BETWEEN BS 5-113 AND 1561 LONGERON 41 RT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50 NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7115 REVISION: D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

CENTER CARGO BETWEEN STA 5-113 AND STA 1561 LONGERON 43 LT SPLICE END, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE100) · airframe 68,564 hrs · 12,263 cycles

CENTER CARGO BETWEEN STA 5-113 AND STA 1561 LONGERON 47 LT SPLICE END, SUSPECTED CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. NEW SPLICE FABRICATED BY MACHINING AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

CENTER CARGO LONGERON 38 LT BETWEEN STA 5-113 AND STA 1561 , FOUND LONGERON SPLICE CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 68,564 hrs · 12,263 cycles

RT FUSELAGE SKIN FROM STA 2027 TO 2024 (BENEATH FAIRING NR 341CF), FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, REV 50 ORIGINAL THICKNESS: 0.095 INCH, MATERIAL REMOVED: 0.085 INCH, REMAINING THICKNESS : 0.010 INCH AND FOUND EXCEEDED LIMIT IAW SRM 53-70-01, FIG 201, REPAIR 3, REV 50. REPAIR CARRIED OUT IAW SRM 53-70-01, FIG 201, REPAIR 3, REV 50. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

AGING AIRCRAFT - EXISTING REPAIR AT RT FUSELAGE SKIN AT STA 1830 BETWEEN LONGERONS 37 AND 38 MISREPAIRED. REPAIRED IAW EA 1-5330-160992. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 68,564 hrs · 12,263 cycles

LEFT WING L/E NR 8 SLAT LOWER SURFACE MID AREA FOUND CRACKED. REPAIRED AS PER SRM 57-40-01 FIGURE 201 REPAIR 3 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: CARGO TRACK — DAMAGED (BS 1421) · airframe 68,564 hrs · 12,263 cycles

MAIN DECK CARGO TRACK AT BS 1421, X=8 FOUND CROWN WITH A HOLE ELONGATED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM BS 1411 TO 1471 X =8 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.

Part: FRAME — DENTED (BS 1701 L12R) · airframe 68,564 hrs · 12,263 cycles

FRAME BS 1701, LONGERON 12R FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.

Part: FRAME — MISREPAIRED (BS 535) · airframe 68,564 hrs · 12,263 cycles

BS 535 LONGERON 25LT FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201. REPAIR 1, REVISION 50 EO 1-5100-7-5001B PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.

Part: SKIN — CRACKED (RT WING) · airframe 68,564 hrs · 12,263 cycles

RIGHT WING OTBD L/E PANEL NR 619CB CUTOUT OTBD FORWARD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING OUTBOARD LEADING EDGE PANEL 619CB CUTOUT OUTBOARD FORWARD CORNER AS PER SRM 57-40-02 REPAIR 7 FIGURE 201 REVISION 50 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: FRAME — DENTED (BS 1641 L12L) · airframe 68,564 hrs · 12,263 cycles

FRAME BS 1641, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 68,564 hrs · 12,263 cycles

AGING AIRCRAFT -EXISTING REPAIR AT RT FUSELAGE SKIN AT BS 488 BETWEEN LONGERONS 28 AND 29 MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 7, REV 50 EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR AS GMM 6-2-100, REV 115.

Part: FRAME — DENTED (BS 1721 L12L) · airframe 68,564 hrs · 12,263 cycles

FRAME BS 1721, LONGERON 12L FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100, REVISION 115.

Part: TRUNNION — CRACKED (NLG) · airframe 68,564 hrs · 12,263 cycles

NLG RT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115

Part: TRUNNION — CRACKED (NLG) · airframe 68,564 hrs · 12,263 cycles

NOSE LANDING GEAR LT TRUNNION FITTING CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-14, FIGURE 202, REPAIR 2, REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115

Part: SEAT TRACK — DAMAGED (BS 1541) · airframe 68,564 hrs · 12,263 cycles

MAIN DECK CARGO TRACK AT BS 1541, X=-8 FOUND CROWN HAS A HOLE ELONGATED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM BS 1531 TO 1571 X =-8 AS PER SRM 53-00-52 FIGURE 201, REPAIR 1 REVISION 50. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.

Part: STRINGER — MISREPAIRED (BS 535) · airframe 68,564 hrs · 12,263 cycles

BS 535, LONGERON 21L MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 50 EO 1-5100-7-5001B, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 68,564 hrs · 12,263 cycles

LT WING INBD FLAP VANE LOWER SURFACES BETWEEN INBD AND MID TRACKS, FOUND DELAMINATED. REMOVED AND REPLACED LEFT HAND WING INBOARD FLAP VANE AS PER AMM 27-50-22-4 REVISION 72.0. FLAP VANE ADJUSTMENTS AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 72.0. FOUND SATISFACTORY. FLAPS OPERATION CHECK CARRIED OUT AS PER AMM 27-00-00-860-801 REVISION 72.0 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 115.

Part: HOLDER — OUT OF POSITION (SLIDE PRESSURE) · airframe 68,216 hrs · 12,179 cycles

FOUND 1R DOOR EVACUATION SLIDE REMOTE PUSH TO TEST SWITCH INOPERATIVE. FOUND PRESSURE INDICATOR LIGHT HOLDER WAS OUT OF POSITION. INSTALLED LIGHT HOLDER AND OPS CHECKED NORMAL IAW MM 25-61-04-4, ACFT OK FOR SERVICE.

Part: CONTROL PANEL — ODOR (COCKPIT LIGHTS) · airframe 63,153 hrs · 10,928 cycles

PROIR TO STARTUP F/O AND CAPT HEARD WHAT SOUNDED LIKE ELECTRICAL ARCING AND SPARKING. THEN SMELLED ELECTRICAL SMOKE IN THE COCKPIT. OVERHEAD SWITCH ONLY LIGHTING / CIRCUIT BREAKER WAS POPPED. RESET OVERHEAD PANEL LIGHTING CIRCUIT BREAKER. NO FAULTS NOTED OR ABNORMAL ODORS . ACFT OK FOR SERVICE ALSO, TSI 33-10/0262 WRITTEN & C/W. ALSO, EA 1-3310-144184 WAS WRITTEN AND C/W TO PULL AND COLLAR CB C-13 (B1-539).

Part: FRAME — CRACKED (ZONE 300) · airframe 62,964 hrs · 10,889 cycles

UPPER AFT FUSELAGE FRAME CLIP AT CANT STATION Y = 2069.44, CRACKED APPROX 1 INCH IN LENGTH. R & R IAW SRM 51-31-01, REV 44. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 62,964 hrs · 10,889 cycles

LOWER VERTICAL STABILIZER AT PANEL NR 363QL INTERIOR AREA, WEB FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-30-02 FIGURE 201 REPAIR 2, REVISION 44 AND EA 1-5530-143725, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 100) · airframe 62,964 hrs · 10,889 cycles

FUSELAGE EXTERIOR SKIN CUTOUT AROUND APU EXHAUST DOOR ACTUATOR FOUND CRACK ABOUT 0.5 INCH. FUSELAGE EXTERIOR SKIN CUTOUT AROUND APU EXHAUST DOOR ACTUATOR, WELDING REPAIR CARRIED OUT AS PER E.A. 1-5330-143414. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 62,964 hrs · 10,889 cycles

LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, 18 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION. LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, 18 EACH FASTENER HOLES CARRIED OUT REPAIR AS PER E.A. 1-5710-143727. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 62,964 hrs · 10,889 cycles

LEFT WING OUTBOARD FLAP TRAILING EDGE WEDGE INBOARD EDGE LOWER SURFACE. FOUND DELAMINATION. REPAIRED AS PER E.A. 1-5750-132474. REPAIR CLASSISIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 62,964 hrs · 10,889 cycles

RIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6, 24 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION. CARRIED OUT REPAIR AS PER E.A. 1-5710-143728. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,964 hrs · 10,889 cycles

MAIN DECK CARGO - SEAT TRACK FROM STA 5-53 TO STA 5-73, "X" =8 FOUND SEVERAL LOCATIONS CORRODED. MAIN DECK CARGO - CORRODED SEAT TRACK FROM STA 5-53 TO STA 5-73, "X" =8 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 5-123, "X" =8, AS PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 44. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 110.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 62,964 hrs · 10,889 cycles

RT WING - INBD FLAP LOWER SURFACE FOUND DENT AT XIFH 198. DENT AREA TRIMMED OUT AND FABRICATED NEW SKIN AND DOUBLER AS PER SRM 57-50-01, FIGURE 201 REPAIR 2, REVISION 44. NEW SKIN AND DOUBLER INSTALLED AS PER SRM 57-50-01 FIGURE 201, REVISION 44. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 62,964 hrs · 10,889 cycles

RIGHT WING - NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUT-OUT INBOARD CORNER UPPER EXTERIOR SKIN FOUND CRACKED AT XOS 464. RIGHT HAND WING - NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUT-OUT INBOARD CORNER, CRACKED UPPER EXTERIOR SKIN AT XOS 464 TRIMMED OUT AS PER SRM 57-40-01 FIGURE 201, REVISION 44. REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED AS PER SRM 57-40-01 FIGURE 201, REPAIR 10, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 60,621 hrs · 10,340 cycles

RT MAIN GEAR UNSAFE ON PRIMARY INDICATOR AFTER GEAR DOWN ON APPROACH AT MEM SECONDARY INDICATOR WAS GREEN. WENT MISSED APPROACH LEAVING GEAR DOWN AND RAN THE GEAR UNSAFE INDICATION WITH GEAR HANDLE DOWN, FOLLOWED BY NORMAL LANDING MEM RWY 36R. REMOVED AND REPLACED PSEU NO HELP THEN REMOVED AND REPLACED RT MLG PRIMARY DOWN AND LOCKED SENSOR IAW WDM 32-61-02 OPS CHECK NORMAL, OK FOR RETURN TO SERVICE.

Part: FUEL TANK — CORRODED (CENTER) · airframe 58,052 hrs · 9,717 cycles

MAIN DECK, CENTER WING TANK AT STA 1230 X = -65 FOUND CORROSION. REPAIRED AS PER E.A. 1-5710-127758, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — DAMAGED (BS 759-799) · airframe 58,052 hrs · 9,717 cycles

LEFT LOWER FUSELAGE EXTERIOR SKIN AT STA 759 TO STA 799, BETWEEN LONGERON 42L TO LONGERON 46L FOUND LIGHTNING STRIKE MARK. AREA REWORKED AND FOUND 2 CRACKS EVIDENT AFTER FPI CARRIED OUT. REPAIR CARRIED OUT AT CRACKED SKIN AS PER SRM 53-20-20-00 FIG.2 SHT 21 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FUEL TANK — CORRODED (CENTER) · airframe 58,052 hrs · 9,717 cycles

MAIN DECK, CENTER WING TANK AT STA 1230 X = -79 FOUND CORROSION. REPAIRED AS PER E.A.1-5710-127758, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (BS 735-759) · airframe 58,052 hrs · 9,717 cycles

LEFT LOWER FUSELAGE EXTERIOR SKIN AT STA 735 TO STA 759, BETWEEN LONGERON 42L TO LONGERON 46L FOUND LIGHTNING STRIKE MARK. AREA FOUND CRACKED AFTER FPI WAS CARRIED OUT. REPAIR CARRIED OUT AT CRACKED SKIN AS PER SRM 53-20-00 FIGURE 2 SHEET 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FUEL TANK — CORRODED (CENTER) · airframe 58,052 hrs · 9,717 cycles

MAIN DECK, CENTER WING TANK AT STA 1230 X = -100 FOUND CORROSION. REPAIRED AS PER E.A. 1-5710-127758, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 100) · airframe 58,052 hrs · 9,717 cycles

FORWARD CARGO, DOOR CUT-OUT SKIN AT STA 888, LONGERON 40R FOUND CHAFED. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 17 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — DELAMINATED (RT WING AILERON) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, OUTBOARD AILERON TRAILING EDGE MIDDLE SECTION FOUND DELAMINATION. REPAIRED AS PER DRAWING SG11570003. WEIGHT AND BALANCE CARRIED OUT, ACTUAL = 31.00 IN-LBS, AS PER CMM 57-51-03. REFER TO WORKCARD 27C1306 FOR OPERATIONAL CHECK. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (BS 1681 L12R) · airframe 58,052 hrs · 9,717 cycles

MAIN DECK, FRAME AT RIGHT STA 1681 LONGERON 12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, INBOARD FLAP VANE LOWER SURFACE INBOARD SIDE FOUND DELAMINATION. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5 FOUND SATISFACTORY.

Part: FRAME — DENTED (BS 1661 L12R) · airframe 58,052 hrs · 9,717 cycles

MAIN DECK, FRAME AT RIGHT STA 1661 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIG.1 VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES AS PER SRM 53-30-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 58,052 hrs · 9,717 cycles

CABIN, SEAT TRACK AT STA 635 X = 27.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665, X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

CABIN, SEAT TRACK AT STA 635 X = 47.5 FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STANCHION — CORRODED (AFT BULKHEAD) · airframe 58,052 hrs · 9,717 cycles

FORWARD CARGO (UPON OPEN UP FOR THRUST REVERSER MODIFICATION) FOUND STA 6-70 X = 57, AFT BULKHEAD STANCHION LOWER SECTION CORRODED AROUND ANCHOR NUT. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW STANCHION REWORKED AS PER DRAWING A6A7094. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127439, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127442, THIS REPAIR IS CLASSIFIED MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT INBOARD HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127438, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127439, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127438, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT FORWARD MOUNTING SURFACE FOUND CORROSION. REWORKED AS PER CMM 57-44-08 REPAIR 1-1. WITHIN DRAWING ARC0502 BLUE PRINT TOLERANCE = 0.436", 0.060" & - 0.015". NEW SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08 REPAIR 1-1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REPAIR 1-1. NEW BUSHING FABRICATED AND INSTALLED ON INBOARD ACTUATOR HOLE AS PER EA 1-5750-127440, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127444, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127443, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE LOWER BARREL NUT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127444, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127443, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127439, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127444, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127438, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

RIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127440, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,052 hrs · 9,717 cycles

LEFT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA 1-5750-127442, REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

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

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

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

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

CRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE A, FIRST LAYER SKIN. REPAIRED AS PER EA 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

CRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE A, SECOND LAYER SKIN. REPAIRED AS PER EA 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 58,052 hrs · 9,717 cycles

CRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE D, SECOND LAYER SKIN. CRACK INDICATION AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE D, SECOND LAYER SKIN REPAIRED AS PER E.A. 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — DENTED (ZONE 100) · airframe 58,052 hrs · 9,717 cycles

LOWER FUSELAGE AT STA 515 BETWEEN LONGERON 45L AND LONGERON 46L SKIN PANELS EXTERIOR SURFACE FOUND WITH DENT PREVIOUSLY BLENDED OUT. FOUND WITH OIL CANNING CONDITION. REPAIR CARRIED OUT AS PER E.A. 1-5310-127759, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 500) · airframe 58,052 hrs · 9,717 cycles

LEFT WING LEADING EDGE COMPARTMENT CEILING UPPER SUPPORT RIB FOUND CRACKED AT APPROXIMATELY XORS 634 NEAR TO OUTBOARD SIDE OF NR 11 SLAT TRACK. REMOVED AS PER SRM 51-31-01 VOLUME II. RIB FABRICATED AS PER DRAWING ARB2923 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

CRACK INDICATION STILL EXIST DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.520 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLE B, SECOND LAYER SKIN. REPAIRED AS PER EA 1-5310-127754, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 58,052 hrs · 9,717 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON DIAMETER 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLE C AND D. REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RECTIFIER — INOPERATIVE · airframe 56,791 hrs · 9,430 cycles

EMERGENCY PWR ON ALERT INFLIGHT. WHEN SELECTED OFF, DC3 DID NOT APPEAR POWERED. EMERGENCY PWR ARM AND ALERT STAYED ON. ADG DEPLOYED. ON SHORT FINAL DC3 UNPOWERED WITH LOSS OF ADG POWER RESULTING IN LOSS OF ASSOCIATED SYSTEMS. FLIGHT DIVERTED DFW AND LANDED WITHOUT INCIDENT. INTERROGATED EPCU FOUND TR-3/INTFC FAULT, ALSO WHEN DEBRIEFED CREW THEY HAVE LOST NR 3 DC BUS, WORK ACCOMPLISHED PER AMM AND TSM 24-30-00/24-31-01-2. REMOVED AND REPLACED NR 3 TR PER AMM 24-31-01. PILOTS AND ENGINEERING, ALONG WITH ACCOMPLISHMENT OF MTSI 24-30/8002. ACFT RELEASED FOR SERVICE.

Part: RECTIFIER — MALFUNCTIONED · airframe 56,791 hrs · 9,430 cycles

EMERGENCY PWR ON ALERT INFLIGHT. WHEN SELECTED OFF, DC3 DID NOT APPEAR POWERED. EMERGENCY PWR ARM AND ALERT STAYED ON. ADG DEPLOYED. ON SHORT FINAL DC3 UNPOWERED WITH LOSS OF ADG POWER RESULTING IN LOSS OF ASSOCIATED SYSTEMS. FLIGHT DIVERTED DFW AND LANDED WITHOUT INCIDENT. INTEREGATED EPCU FOUND TR-3/INTFC FAULT. WORK ACCOMPLISHED PER AMM &TSM 24-30-00/24-31-01-2. REMOVED & REPLACED NR 3 TR PER AMM 24-31-01. ACFT RELEASED FOR SERVICE.

Part: LANDING GEAR — CRACKED (ZONE 700) · airframe 55,740 hrs · 9,198 cycles

FOUND CTR LANDING GEAR SHOCK STRUT CYLINDER CRACK FROM TOP DOWN ABOUT 33 INCHES. REMOVED AND REPLACE CENTER MAIN LANDING GEAR AND PERFORMED MLG RETRACTION TEST.

Part: BULKHEAD — CORRODED (ZONE 400) · corrosion level 2 · airframe 53,354 hrs · 8,663 cycles

REFERENCE TO SNRM N00486, CORROSION WAS DETECTED AFTER REMOVAL OF NR 3 PYLON AFT MOUNTING BEARING. COMPLIED WITH FEDEX EA NR 1-5410-112388, TITLE: NACELLES AND PYLONS, NR 3 PYLON AFT MOUNT BEARING HOUSING BORE, INTERIM (24 MONTHS) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BEARING RACE — MIGRATED (NR 3 PYLON) · airframe 53,354 hrs · 8,663 cycles

NR 3 PYLON AFT MOUNT BEARING AFT FACE OUTER RACE FOUND MIGRATED. 08-31-07 REMOVED AND REPLACED AS PER FEDEX E.A. 1-5410-112388. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (BS 1956) · airframe 53,354 hrs · 8,663 cycles

AFT CARGO, LONGERON 51L SPLICE END AROUND STA 1956 FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (BS 1521) · airframe 53,354 hrs · 8,663 cycles

FUSELAGE, LEFT EXTERIOR SURFACE LONGERON END CAP FITTING AT STA 1521 LONGERON 30L FOUND CRACKED. 08/31/07 REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE END CAP FITTING FABRICATED AS PER DOUGLAS DRAWING AEA7643 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 53,354 hrs · 8,663 cycles

LEFT WING FIXED LEADING EDGE SLAT TRACK COVER CUTOUT OUTBOARD CORNER AT STA XOS = 832, FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE STA XOS = 889 SLAT TRACK COVER CUTOUT AREA AS PER SRM 57-100-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6 -2-100.

Part: STRUCTURE — NONE (ZONE 600) · airframe 53,354 hrs · 8,663 cycles

RIGHT WING NR 7 SLAT FOUND WITH DENTS. CARRIED OUT AS PER DAC NDT SPM REV. 13 06- 10-01.001 AND FOUND NO CRACKS ON DENTS. ALL DENT MARKS MEASURED AND FOUND WITHIN LIMIT AS PER SRM 57-10-00 FIGURE 16 VOLUME I. REWORKED AREA PROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — DENTED (ZONE 600) · airframe 53,354 hrs · 8,663 cycles

RIGHT WING NR 6 SLAT FOUND WITH DENTS. 08-31-07 MEASURED AND FOUND 4 AREAS EXCEEDED LIMIT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 16 VOLUME I. ALL DENT AREAS REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 600) · airframe 53,354 hrs · 8,663 cycles

RIGHT WING SLAT TRACK NR 16 RIB FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51- 35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 53,354 hrs · 8,663 cycles

LEFT WING FIXED LEADING EDGE SLAT COVER CUTOUT OUTBOARD CORNER AT STA XOS = 774 FOUND CRACKED. 08-31-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: CONTROL VALVE — UNKNOWN (TE FLAPS) · airframe 51,958 hrs · 8,346 cycles

PDIS: FLAPS FROZE AT 22-23 DEG ON RETRACTION, RETURN FLAP HANDLE TO 25DEG FLAPS EXTENDED BACK TO 25 DEG, NO ASYMMETRY NOTED, ON 2ND ATTEMPT TO RETRACT FLAPS, FLAPS MOVED SLOWER THAN NORMAL AND FLAPS FULLY RETRACTED. ON LANDING FLAPS EXTEND NORMALLY. AFTER LANDING LOB FLAP MOVES SLOWER THAN OTHERS. NO DEFECTS NOTED ON GROUND OPERATIONAL CHECK. PRECAUTIONARY REPLACED INBD, CENTER AND OUTBD WING FLAP CONTROL VALVES AND RESTRICTORS. OPERATIONAL TEST CARRIED OUT, OPERATION NORMAL. A/C OK FOR SERVICE.

Part: COMPUTER — FAILED (FLT CONTROL) · airframe 51,958 hrs · 8,346 cycles

PDIS : FLAPS DID NOT RETRACT WHEN FLAP HANDLE RAISED AFTER T/O, PER QRH, MATCHED FLAP HANDLE TO INDICATED POSITION (15DEG) BUT FLAP INDICATION SHOWED FLAPS CONTINUING TO COME UP. EVENTUALLY INDICATED "0", MATCHED FLAP HANDLE AGAIN. RTB WITH NO PROBLEM ON FLAP EXTENSION AND NORMAL LANDING. PERFORMED INSPECTION OF FLAPS AND CONTROLS, NO OBVIOUS DISCREPANCY FOUND. PERFORMED FCC RTS, FCC1 FAILS. CYCLED FLAPS FROM UP POSITION TO 50 DEG POSITION, OPERATIONS AND INDICATIONS NORMAL, SENSOR READ OUT INDICATIONS WITHIN LIMITS. INITIAL FCC RTS SHOWED FAULT CODE N124.12, N124.13,N124.14, ON FCC1. REMOVED AND REPLACED FCC1. PERFORMED RTS ON FCC1 AND FLAP OPERATIONAL, FLAP OPERATION AND INDICATIONS NORMAL.

Part: TIRE — DAMAGED (NR 9) · airframe 51,925 hrs · 8,337 cycles

NR 9 TIRE FAIL ALERT ON LNDG ROLLOUT CDG. NO OTHER INDICATIONS. FOUND NR 9 TIRE EXPOSED. FOUND BRAKE NR 10 HYD PRESS LINE CUT, AND BRAKE NR 9 HID FITTING BENT, NEED TO REPLACE NR 9 BRAKE. REMOVED AND REPLACED BRAKE NR 10 HYD PRESS LINE AS PER SUMP. LEAK TEST OK. REMOVED AND REPLACED MAIN TIRE NR 10 AS PER MM 32-41-01-4. CHECKED CONTINUITY TEST BETWEEN ANTI-SKID CONTROL UNIT AND WHEEL SPEED TRANSDUCER NR 9 AND 10. CHECKED WIRING CONTINUITY BETWEEN ANTI SKID MANIFOLD CTR GEAR AND ASCU, PRECAUTIONARY CHANGED ASCU AS PER MM 32-45-01-4. PERFORMED ANTI-SKID TEST AS PER MM 32-41-01-5, ALL TEST PASSED. REMOVED AND REPLACED NR 9 BRAKE ASSY AS PER MM 32-43-20-4. LEAK CHECK OK. REMOVED AND REPLACED NR 9 WHEEL

Part: FRAME — DENTED (ZONE 200) · airframe 48,724 hrs · 7,607 cycles

FOUND MAIN DECK CARGO AT STA 1681 LT, FRAME HAS DING. REPAIR CARRIED OUT AT MAIN DECK CARGO STA 1681 LT FRAME DING AREA AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR REQUIRE REPETITIVE INSPECTION AS PER FEDEX EA NR 1-5330-95672, TITLE: "FUSELAGE - FRAME, TRACKING SRM FRAME REPAIR AT STA Y=1681 AT LONGERON 12 LEFT AND 13 LEFT".

Part: FRAME — DENTED (ZONE 200) · airframe 48,724 hrs · 7,607 cycles

FOUND MAIN DECK CARGO AT STA 1661 LT FRAME HAS A DING. REPAIR CARRIED OUT AT MAIN DECK CARGO STA 1661 LT FRAME DING AREA AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR REQUIRE REPETITIVE INSPECTION AS PER FEDEX EA NR 1-5330-95671, TITLE: "FUSELAGE - FRAME - TRACKING SRM FRAME REPAIR AT STA Y=1661 AT LONGERON 12 LEFT".

Part: FRAME — DENTED (ZONE 200) · airframe 48,724 hrs · 7,607 cycles

FOUND MAIN DECK CARGO, AT STA 1721 RT FRAME, HAS A DING. REPAIR CARRIED OUT AT MAIN DECK CARGO STA 1721 RT FRAME DING AREA AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR REQUIRE REPETITIVE INSPECTION AS PER FEDEX EA NR 1-5330-95673, TITLE: "FUSELAGE - FRAME - TRACKING SRM FRAME REPAIR AT STA Y=1721 AT LONGERON 12 RIGHT".

Part: FITTING — CRACKED (ZONE 600) · airframe 48,724 hrs · 7,607 cycles

RT WING O/B FLAP SECONDARY UP STOP SUSPECT CRACK. RT WING O/B FLAP SECONDARY UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

LEFT WING OUTBOARD AILERON TRAILING EDGE INBOARD UPPER SURFACE FOUND DELAMINATED. LEFT WING OUTBOARD AILERON TRAILING EDGE INBOARD UPPER SURFACE REPAIRED AS PER FEDEX EA NR 1-5790-95674, TITLE: WINGS, OUTBOARD AILERON, REPAIR LEFT OUTBOARD AILERON DELAMINATION. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

FOUND CORROSION LT WING O/B FLAP I/B HINGE FITTING (ARC1984) O/B NR 3 BOLT HOLE . CORROSION AT LT WING O/B FLAP I/B HINGE FITTING (ARC1984) O/B NR 3 BOLT HOLE. REPAIRED AS PER FEDEX EA NR 1-5750-95810, TITLE: "WINGS - LT OUTBOARD TRAILING EDGE FLAP, I/B BRACKET AFT O/B ATTACHMENT BORE, CORROSION REPAIR". REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

LT WING O/B FLAP I/B HINGE SUPPORT FITTING (ARC4009) O/B NR 3 BOLT HOLE FOUND CORROSION. LT WING O/B FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30- 4. OPERATIONAL CHECK AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.

Part: SKIN — CRACKED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

LT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACKED. CRACK AT LT WING FIXED L/E TELESCOPING DUCT CUTOUT REPAIRED AS PER FEDEX EA NR 1-5730-95669, TITLE: "WINGS - STRUCTURE. LEFT LEADING EDGE SKIN CRACKS AT ANTI-ICE TELESCOPING DUCT CUTOUT". REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,724 hrs · 7,607 cycles

HFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER-14 END. RIGHT WING STRINGER 14 END CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

CRACK FOUND IN LEFT WING TANK AT END OF STRINGER 13 DURING HFEC INSPECTION. LEFT WING TANK AT THE END OF STRINGER 13 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

CRACK FOUND IN LEFT WING TANK AT END OF STRINGER 14 DURING HFEC INSPECTION. LEFT WING AT THE END OF STRINGER 14 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,724 hrs · 7,607 cycles

HFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER-12 END. RIGHT WING STRINGER 12 END CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 48,724 hrs · 7,607 cycles

HFEC INSPECTION CARRIED OUT, FOUND CRACK ON END OF LEFT HAND WING STRINGER 10. LEFT HAND WING TANK AT THE END OF STRINGER 10 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 48,724 hrs · 7,607 cycles

HFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER-13 END. RIGHT WING STRINGER 13 END CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HYDROMECH UNIT — FAILED (FUEL SYSTEM) · airframe 43,881 hrs · 6,487 cycles

"ENG 3 RPM LOW" ALERT RECEIVED AT START OF DESCENT FROM FL330. EGY NR 3 APPROX 50, FUEL FLOW APPROX 700. NO INDICATEIONS OF ENGINE DAMAGED. COMPLIED WITH QRH PROCEDURES FOR ENG RPM LOW AND ENG RESTART INFLIGHT. ENGINE RESTARTED NORMALLY AND OPERATED NORMALLY FOR REMAINDER FO FLIGHT. (OPEN)

Part: STRINGER — CRACKED (ZONE 600) · airframe 43,814 hrs · 6,470 cycles

RIGHT HAND WING LEADING EDGE STRINGER AT STA XORS 799 FOUND CRACKED. RIGHT HAND WING LEADING EDGE STRINGER AT STA XORS 799 CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 18, VOLUME I.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 43,814 hrs · 6,470 cycles

MAIN CARGO DECK LT STA 1701 TRANSVERSE FRAME DAMAGED BETWEEN LONGERON 11 AND LONGERON 12. MAIN CARGO DECK LT STA 1701 TRANSVERSE FRAME BETWEEN LONGERON 11 AND LONGERON 12, DAMAGED AREA TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG 1 VOLUME I. REFER TO FEDEX EA 1-5310-79787, TITLE: FUSELAGE, MAIN FRAME TRACKING SRM REPAIR ON FRAME AT STATION 1701.

Part: YOKE — DAMAGED (ZONE 200) · airframe 43,814 hrs · 6,470 cycles

MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY HAS DAMAGE, TRANSVERSE FRAME. MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY ATTACHED TRANSVERSE FRAME, FLANGE DAMAGED AREAS AT 02 LOCATIONS, TRIMMED AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,814 hrs · 6,470 cycles

MAIN CARGO DECK STA Y= 132 RT SEAT TRACK X= -47.5 SEAT TRACK DAMAGED. MAIN CARGO DECK STA Y= 1321 RT SEAT TRACK X= -47.5 SEAT TRACK DAMAGED AREA, SECTIONAL CUT-OUT OF SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I BETWEEN STA 1321 AND STA 1361 OF RBL 47.5.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,923 hrs · 8,465 cycles

MAIN CARGO DECK STA 810 LEFT REFERENCE X= 47.5 SEAT TRACK DAMAGED. MAIN CARGO DECK STA 810 LEFT REFERENCE X= 47.5 DAMAGED SEAT TRACK SECTIONAL CUT-OUT AND REMOVED BETWEEN STA 765 AND STA 825 AND SECTIONAL REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-70-00 FIGURE 1 VOLUME I.

Part: SKIN PANEL — CRACKED (ZONE 600) · airframe 43,814 hrs · 6,470 cycles

RT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 FOUND WITH APPROXIMATELY 13 INCH CRACKED. RIGHT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 CRACKED . REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-79779, TITLE: WINGS, BASIC WING STRUCTURE, RIGHT LEADING EDGE SKIN CRACK BY SLAT NR 7.

Part: DEU — FAULTY (NR 1) · airframe 43,281 hrs · 6,355 cycles

ON DEPARTURE CLIMBING THROUGH 800 FEET, DEU 1,2,3 SHOWED RED(X) ACCOMPANIED BY MASTER WARNING LIGHT AND BELL, MASTER CAUTION LIGHT, AND ALL ALERTS INDICATING ON EAD. COULD NOT SILENCE WARNING HORN. INTERROGATED CFDS AND FOUND NR 1 DEU FAULTY. REMOVED AND REPLACED NR 1 DEU IAW MM 31-61-02-4, RTS PASSED.

Part: DUCT — FAILED (NR 1 ENGINE) · airframe 42,913 hrs · 6,260 cycles

FIVE MINUTES AFTER T/O RECEIVED HYD PUMP 1R OFF ALERT. HYD SYS SNOPSIS SHOWED -T- OVER 1R PUMP, 1 MINUTE LATER HYD SYSTEM FAILED, PRESSURE WENT TO -0-. ALSO NOTED AMBER -T- OVER LEFT PUMP PRIOR TO HYD 1 SYS OFF. REPLACED NR 1 ENG LOW PRESS TURBINE SUPPLY AIR DUCT AT THE 11 O`CLOCK POSITION. REMOVED AND REPLACED LT EDP NR 1 ENGINE IAW MD-11AMM 29-11-20-41. LEAK CHECKS GOOD.

Part: LINE — CONTAMINATED (CDP) · airframe 41,810 hrs · 6,010 cycles

DURING DESCENT AT 6000 MSL, 250 KIAS IDLE THRUST ENG 2 RPM LO ALERT, FOLLOWED BY FLAMEOUT, EGT 75 DEG WITH IGNITION OVERRIDE ENGINE ACCELERATED TO NORMAL IDLE. ENGINE OPERATION DURING APPROACH, LANDING AND ROLLOUT WAS NORMAL. INSPECTED NR 2 ENG OIL MASTER CHIP DETECTOR IAW MM 79-36-01-61, NO CONTAMINATION FOUND. SYS AND FOUND CDP LINE FROM COMPRESSOR SECTION TO NR 2 ECU HAS WATER INSIDE, AND DRAIN PORT AT LOW POINT PLUGGED. OPENED CDP LINE AT ECU AND AT ENG AND BLEW DRY NIT THRU LINE TO CLEAN WATER AND DEBRIS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 39,199 hrs · 5,395 cycles

CAPT'S WINDSHIELD CRACKED. 15JUN03 09:03 SIN R, CAPT'S WINDSHIELD REMOVED AND REPLACED AS PER AMM 56-11-01. WINDSHIELD ANTI-ICE SYSTEM OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 30-41-00. WINDSHIELD DEFOG SYSTEM OPERATION TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 30-42-00. R/I 15JUN03 09:04 SIN R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 39,199 hrs · 5,395 cycles

CAPT'S WINDSHIELD CRACKED.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,197 hrs · 5,391 cycles

SNRM N0938 - RT HORZ STAB BARREL NUT BORE NR 35 CORROSION BLEND OUT, OUT OF LIMIT. CORRECTIVE ACTION: SNRM N0938: RH HORIZONTAL STABILIZER BARREL NUT BORE NR 35 CORROSION BLEND OUT AREA CARRIED-OUT REPAIR AS IAW EA 1-5510-71716 - STABILIZER - HORIZONTAL STABILIZER - REWORK OF HOLE 35R, REFERENCE EO 1-5510-7-5000.

Part: BUSHING — LOOSE (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

SNRM N0860 - LT WING - OUTBOARD TRAILING EDGE FLAP - OUTBOARD AFT FLAP-HINGE FOUND PIVOT BEARING HOLES LT AND RT WITH BUSHINGS LOOSE (FLAP SIDE). SNRM N0860: LOOSE BUSHINGS LT AND RT OF PIVOT BEARING HOLES REPLACED WITH OVERSIZED BUSHINGS IAW EA 1-5750-69348 - WINGS - LT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE — LOOSE (ZONE 600) · airframe 39,197 hrs · 5,391 cycles

RT WING - OUTBOARD TRAILING EDGE FLAP, AFT INBOARD FLAP-HINGE ASSEMBLY FOUND PIVOT BEARING, INBOARD MOUNT HOLE WITH BUSHING LOOSE (FLAP SIDE). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69346 - WINGS - RT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: BUSHING — LOOSE (TE FLAP HINGE) · airframe 39,197 hrs · 5,391 cycles

LEFT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD AFT FLAP - HINGE FOUND HYDRAULIC ACTUATOR ROD-END MOUNT HOLES BUSHINGS LT AND RT LOOSE. LOOSE BUSHINGS AT LT AND RT OF ACTUATOR MOUNT HOLES REPLACED WITH OVERSIZED BUSHINGS AS PER FEDEX EA 1-5750-69348 - WINGS - LEFT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: BUSHING — LOOSE (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

SNRM N0875: RT WING - OUTBOARD TRAILING EDGE FLAP, AFT OUTBOARD FLAP-HINGE ASSEMBLY FOUND PIVOT MOUNT, OUTBOARD HOLE WITH BUSHING LOOSE. SNRM N0875 - LOOSE BUSHINGS AT PIVOT MOUNT OUTBOARD HOLE REPLACED WITH OVERSIZED BUSHING AS PER FEDEX EA 1-5750-69255 - WINGS - RT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE — LOOSE (ZONE 500) · airframe 39,197 hrs · 5,391 cycles

LT WING - OUTBOARD TRAILING EDGE FLAP, AFT INBOARD FLAP-HINGE FITTING FOUND PIVOT BEARING, INBOARD HOLE BUSHING LOOSE, WORN (FLAP SIDE). REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69347 - WINGS - LT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE — LOOSE (ZONE 500) · airframe 39,197 hrs · 5,391 cycles

LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD AFT FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR ROD-END HOLES, LT AND RT BUSHINGS LOOSE, WORN (FLAP SIDE). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69347 - WINGS - LT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - INBOARD TRAILING EDGE FLAP, OUTBOARD AFT FLAP -HINGE FITTING FOUND LT AND RT PIVOT BEARING BORE HOLES WITH CORROSION (FLAP SIDE). REPAIR CARRIED-OUT AS PER CMM 57-52-03 AND FEDEX EA 1-5750-69351 - WINGS - RT INBOARD FLAP OUTBOARD HINGE CORROSION - REPAIR.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 39,197 hrs · 5,391 cycles

SNRM N0746: RT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP-HINGE FWD FITTING FOUND INBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0746: REPAIR CARRIED-OUT AS PER CMM 57-44-08 AND FEDEX EA 1-5740-68424 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP - HINGE AFT FITTING FOUND INBOARD ACTUATOR BORE WITH MINOR CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69255 - WINGS - RIGHT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP HINGE AFT FITTING FOUND OUTBOARD PIVOT BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69346 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 39,197 hrs · 5,391 cycles

SNRM N0767: LT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FWD FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR'S UPPER LT AND RT MOUNT HOLES WITH CORROSION (WING SIDE FITTING). SNRM N0767: REPAIR CARRIED-OUT IAW CMM 57-44-08 AND EA 1-5740-71706 WINGS - LEFT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 39,197 hrs · 5,391 cycles

SNRM N0769: LT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FWD FLAP-HINGE FITTING FOUND HYDRAULIC ACTUATOR'S UPPER LUG MOUNT HOLES, LT AND RT WITH BORE SURFACE CORROSION (WING SIDE FITTING). SNRM N0769: REPAIR CARRIED-OUT AS PER CMM 57-44-09 AND FEDEX EA 1-5740-71707 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP - HINGE AFT FITTING FOUND OUTBOARD ACTUATOR BORE WITH MINOR CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69346 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP - HINGE AFT FITTING FOUND INBOARD PIVOT BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69255 - WINGS - RIGHT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP - HINGE AFT FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69255 - WINGS - RIGHT OUTBOARD FLAP OUTBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 39,197 hrs · 5,391 cycles

SNRM N0750: RT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP-HINGE FWD FITTING FOUND INBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0750: REPAIR CARRIED-OUT IAW CMM 57-44-09 AND EA 1-5740-71708 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP-HINGE FWD FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. REPAIR CARRIED-OUT AS PER CMM 57-44-08 AND FEDEX EA 1-5740-68424 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

LEFT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP - HINGE ASSY FOUND PIVOT BEARING OUTBOARD BORE HOLE WITH MINOR CORROSION (ON FLAP SIDE). REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69347 - WINGS - LEFT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 39,197 hrs · 5,391 cycles

SNRM N0748: RT WING - OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP-HINGE FWD FITTING FOUND OUTBOARD ACTUATOR BORE WITH PITTING CORROSION. SNRM N0748: REPAIR CARRIED-OUT IAW CMM 57-44-09 AND EA 1-5740-71708 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSY. FOR ACTUATOR INSTALLATION CORRODED.

Part: HINGE FITTING — CORRODED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

RIGHT WING - OUTBOARD TRAILING EDGE FLAP, INBOARD FLAP - HINGE AFT FITTING FOUND INBOARD ACTUATOR BORE WITH MINOR CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL II AND FEDEX EA 1-5750-69346 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE ACTUATOR AND PIVOT MOUNT - REPAIR.

Part: RIB — CHAFED (T/E FLAP) · airframe 39,197 hrs · 5,391 cycles

LEFT WING - INBOARD TRAILING EDGE FLAP, NR 2 VANE TRACK CUTOUT FOUND RIB STRUCTURE WITH CHAFING MARK NEAR ROLLER AREA. WORK CARRIED OUT IN ACCORDANCE WITH FEDEX EA 1-5750-69350 - WINGS - LEFT INBOARD FLAP NUMBER 2 FLAP VANE TRACK RIB WORN LUG - REPAIR.

Part: SUPPORT — CORRODED (ZONE 500) · airframe 39,197 hrs · 5,391 cycles

LT WING - OUTBOARD TRAILING EDGE FLAP VANE ASSY FOUND NR 3 VANE TRACK SUPPORT'S FWD MOST MOUNT HOLE WITH CORROSION IN BORE SURFACE (NUMBERED FROM INBOARD). REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-71714 - WINGS - LEFT OUTBOARD FLAP VANE - NR 3 VANE TO TRACK SUPPORT CORRODED.

Part: SUPPORT — CORRODED (T/E FLAP VANE) · airframe 39,197 hrs · 5,391 cycles

LEFT WING - OUTBOARD TRAILING EDGE FLAP VANE FOUND NR 1 VANE TRACK SUPPORT FWD MOST MOUNT HOLE BORE SURFACE CORRODED. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-71713 - WINGS - LEFT OUTBOARD FLAP VANE - NR 1 VANE TO TRACK SUPPORT CORRODED.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 39,197 hrs · 5,391 cycles

LT WING: LEADING EDGE RIB AT SLAT TRACK NR 16 FOUND WITH HAIRLINE CRACK. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II AND DRAWING ARB2850.