N621FE

Part: POWER UNIT — FAULTED · airframe 74,305 hrs · 19,331 cycles

EMER PWR TST FAIL LEVEL 1 ALERT ILLUMINATED. PER QRH, TURNED EMER PWR SWITCH OFF AND WAITED FOR BAT CHARGING MESSAGE TO GO OUT, THEN TURNED EMER PWR SWITCH ON AND ALL APPEARED NORMAL, UNTIL APU PWR DROPPED OFFLINE AGAIN AND EMER PWR ON LEVEL 1 ALERT ILLUMINATED. T/S PER FIM AND PERFORMED SUCCESSFUL ELEC PWR TEST. ALSO HAD MULTIPLE ISSUES WITH APU PWR REF 49-00-0504

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1330 X = -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1330, 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 AT STATION 1249 TO EXISTING SPLICE STATION 1391, 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: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1029 X = -75.25 FOUND WITH CORROSION. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1029, X = -75.25, CORROSION EVALUATED, FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1009 TO EXISTING SPLICE STATION 1129/6-0, X = -75.25 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 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1015 X = 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1015, 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 AT STATION 1009 TO EXISTING SPLICE STATION 1129/6-0, 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: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 885 X = 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 885, X = 8.5 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 AT STATION 909 TO EXISTING SPLICE STATION 825, X = 8.5 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 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1059 X = 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1059, 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 AT STATION 1009 TO EXISTING SPLICE STATION 1129/6-0, X = 47.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N0065 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. OSD; 1/22/2025

Part: ACCESS DOOR — CRACKED (ZONE 600) · airframe 73,380 hrs · 19,037 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD CORNER #5 FOUND 01 EACH CRACK APPROXIMATELY 0.5 . STATION XOS 490. CRACK AT RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD CORNER #5 STATION XOS 490 CARRIED OUT REPAIR IAW MD-11 SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,380 hrs · 19,037 cycles

AFT FUSELAGE STATION 2140 RIGHT HAND PANEL #347DF CUTOUT SURFACE CORROSION. SURFACE CORROSION AT AFT FUSELAGE - STATION 2140 RIGHT HAND PANEL #347DF CUTOUT PER MD-11 SRM 53-70-01-2R FIGURE 201, REPAIR 3. REPAIR CARRIED OUT PER MD-11 SRM 53-70- 01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. OSD: 1/20/2025

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 73,380 hrs · 19,037 cycles

AFT FUSELAGE LOWER TORQUE BOX UPPER PANEL ON LOWER SURFACE AT ACTUATOR SUPPORT ANGLES AREA CRACKED. (0.5") AT STATION 2122.881, X = - 10. 0.5" CRACK AT STATION 2122.881, X = - 10 AFT FUSELAGE - LOWER TORQUE BOX UPPER PANEL ON LOWER SURFACE AT ACTUATOR ANGLES AREA REPAIRED PER FEDEX DRAWING SR10-53-013. ANGLES 2 EA FABRICATED PER E. A. #: 1-5310-T0381946 P1. TITLE: FUSELAGE - MAINFRAME - AFT BODY - LOWER TORQUE BOX UPPER PANEL AND ANGLES CRACKED AT STA 2122.881, INBD OF X = -10 - ALTERNATE EXTRUSION FOR AJC7496-13 AND AJC7496-15 ANGLES FABRICATION. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755 X= 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X = 8.5 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 AT EXISTING SPLICES STATION 745 TO STATION 785, X = 8.5 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 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541 X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X = -47.5 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 AT STATION 1571 TO EXISTING SPLICE STATION 5-123/1531, 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. OSD: 1/20/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK Ï¿½ CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X= 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ CARGO COMPARTMENT AT SEAT TRACK STATION 1425, 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 AT STATION 1391 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. ORIGNAL SUBMISSION DATE: 1/16/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1411 X= -8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1411, X = -8.5 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 AT STATION 1391 TO STATION 1451, X = -8.5 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 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1431 X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1431, 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 AT STATION 1391 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. ORIGINAL SUBMISSION DATE: 1/16/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X= 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5 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 AT STATION 6-63 TO EXISTING SPLICE STATION 1129 / 6-0, 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. ORIGINAL SUBMISSION DATE: 1/16/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK Ï¿½ CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X= -27.5 FOUND CROWN WORN. MAIN DECK Ï¿½ CARGO COMPARTMENT AT SEAT TRACK STATION 1425, X = -27.5 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 AT STATION 1391 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. ORIGINAL SUBMISSION DATE: 1/16/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1411 X= 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1411, X= 8.5 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 AT STATION 1391 TO STATION 1451, X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIGINAL SUBMISSION DATE: 1/16/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1431 X= 8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1431, X= 8.5 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 AT STATION 1391 TO STATION 1451, X= 8.5 AS PER MD-11 SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00174 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIGINAL SUBMISSION DATE: 1/16/2025

Part: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= -8.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X= -8.5 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 AT EXISTING SPLICES STATION 1531/5-0 TO STATION 5-20, X= -8.5 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 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, 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 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: SEAT TRACK — WORN (ZONE 200) · airframe 73,380 hrs · 19,037 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, 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 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: CONNECTOR — DISCONNECTED (CARGO DOOR) · airframe 72,646 hrs · 18,832 cycles

FWD CARGO DOOR A ALERT ON CLIMB OUT. EMERGENCY DECLARED. FOUND FORWARD CARGO DOOR CLOSED LIMIT WARNING SWITCH CONNECTOR ( P1-1703 ) UNSECURED. SECURED CONNECTOR AND PERFORMED ADJ/TEST OF CARGO DOOR WARNING INDICATION SYSTEM. OPS CHECK GOOD A/C OK FOR SERVICE.

Part: ACTUATOR — UNKNOWN (OUTFLOW VALVE) · airframe 69,897 hrs · 18,045 cycles

CLIMBING THROUGH 4000 FEET CABIN SEL MAN FOLLOWED BY CABIN RATE LEVEL 1. CABIN PRESSURE WOULD NOT STABILIZE INITIALLY IN MANUAL MODE. CABIN WAS INDICATING -5000 FEET . RETURNED TO INDY AND GOT THE CABIN TO STABILIZE ON DOWNWIND MANUALLY. SHGN 12JUL23 04:05 IND U NRR: NO REFERENCE REQUIRED REVIEW OF CFDS SHOWS BOTH CPC'S FAULTING MOTOR/OFV. REMOVED AND REPLACED CABIN OUTFLOW VALVE ACTUATOR IAW AMM 21-31-20-2. OPS CHECK GOOD.

Part: NONE — NONE (NONE) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE SKIN RIGHT HAND SIDE STATION 1082 LONGERON 32 RIGHT. EXISTING REPAIR AT FUSELAGE SKIN RIGHT HAND SIDE STATION 1082 LONGERON 32 RIGHT EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 7 FIGURE 201 SHEET 1. EO #1-5100-7-5001 B7 PART1 TITLE: STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPAIR CLASSIFIED AS CATEGORY B REPAIR. INITIAL INSPECTION CARRIED OUT AT CURRENT CHECK WITH REPETITIVE INSPECTIONS REQUIRED AT EVERY 4,500 FLIGHT CYCLES AS PER SRM 53-00-01-2R TABLE 201 REPAIR 7.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

MAIN DECK CARGO COMPARTMENT , FLOOR PANEL 241DF BS 755 - 795, FOUND DELAMINATED. FLOOR PANEL 241DF AT MAIN DECK CARGO REMOVED IAW AMM 53-21-04. THE NEW FLOOR PANEL WAS FABRICATED IAW DRAWING SRZ-25-005, REVISION R. THE NEW FLOOR PANEL WAS INSTALLED IAW AMM 53-21-04. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FASTENER — MISSING (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

CENTER ACCESSORY COMPARTMENT - BELOW CABIN FLOOR AND LEFT OF FUSELAGE CENTER LINE AT STATION 6-80 TO 6-100, X=8.5 HAS SEVERAL FLOOR PANEL FASTENERS MAKING CONTACT WITH THE SEAT TRACK FLANGE CAUSING DAMAGE. CABIN FLOOR AND LEFT OF FUSELAGE CENTER LINE AT STATION 6-80 TO STATION 6-100 X=8.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 6-0 TO STATION 6-100 X=8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FASTENER — MISSING (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

CENTER ACCESSORY COMPARTMENT - BELOW CABIN FLOOR AND RIGHT OF FUSELAGE CENTER LINE AT STATION 6-80 TO 6-100, X= -8.5 HAS SEVERAL FLOOR PANEL FASTENERS MAKING CONTACT WITH THE SEAT TRACK FLANGE CAUSING DAMAGE. CABIN FLOOR AND RIGHT OF FUSELAGE CENTER LINE AT STATION 6-80 TO STATION 6-100 X=-8.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 6-0 TO STATION 6-100 X=-8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231BF AT STATION 459 - 536 FOUND DAMAGED. DAMAGED FLOOR PANEL 231BF AT MAIN DECK CARGO COMPARTMENT STATION 459 - 536 REMOVED AS PER AMM 53-21-04. FLOOR PANEL 231BF FABRICATED AS PER FEDEX DRAWING SRZ- 25-005 REVISION R. FABRICATED FLOOR PANEL 231BF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. ORIG SUBMISSION DATE: 1/18/2023

Part: SKIN — CRACKED (ZONE 600) · airframe 69,076 hrs · 17,786 cycles

02 EACH FASTENER HOLES NUMBER 10 AND NUMBER 15 FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN - HOLE INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6. 02 EACH CRACKED FASTENER HOLES NUMBER 10 AND NUMBER 15 AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 REPAIRED AS PER SRM 57-20-02-2R REPAIR 5 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLES BY ULTRASONIC AND HIGH FREQUENCY EDDY CURRENT INSPECTION AS PER SRM 57-20-02-2R FIGURE 202 REPAIR 5 TABLE 201 REQUIREMENTS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. OSD: 1/16/2023

Part: RIB — CRACKED (LT NR 7 SLAT) · airframe 69,076 hrs · 17,786 cycles

WHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517) , FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 983.612. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 983.612 AREA REPAIRED AS PER EA# 1-5750-T0372632 A P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT NR 7 SLAT) · airframe 69,076 hrs · 17,786 cycles

WHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517) , FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 963.009. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 963.009 AREA REPAIRED AS PER EA# 1-5750-T0372632 A P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT NR 7 SLAT) · airframe 69,076 hrs · 17,786 cycles

WHILE CARRYING OUT INTERNAL BORESCOPE INSPECTION ON LEFT HAND NUMBER 7 SLAT LOOSE RIVETS AREA (SNRM N00517) , FOUND THE SLAT INTERNAL RIB CRACK AT STATION XOS 968.159. RIB AT LEFT HAND NUMBER 7 SLAT INTERNAL AT STATION XOS 968.159 AREA REPAIRED AS PER EA# 1-5750-T0372632 A P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 69,076 hrs · 17,786 cycles

RIGHT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 704. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 704 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 (RT WING) · airframe 69,076 hrs · 17,786 cycles

RIGHT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 675. RIGHT HAND WING OUTBOARD 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: DOUBLER — CRACKED (LT WING) · airframe 69,076 hrs · 17,786 cycles

LEFT WING OUTBOARD FIXED LEADING EDGE LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 704. LEFT HAND WING OUTBOARD FIXED LEADING EDGE LOWER SKIN DOUBLER AT STATION XOS 704 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1305-1315) · airframe 69,076 hrs · 17,786 cycles

MAIN DECK CARGO L3 DOOR JAMB AFT LOWER CORNER AREA BS 1305.25 - 1315.42 FOUND CRACKED. L3 DOOR JAMB AFT LOWER CORNER AREA STATION 1305.25 TO STATION 1315.42 SKIN CRACKED REPAIRED AS PER SRM 53-40-15-2R REPAIR 3 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = 27.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = 27.5 LEFT HAND SIDE EVALUATED AND FOUND CRACK 1.0" AT SEAT TRACK STATION 635 X = 27.5 LEFT HAND SIDE. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 625 TO STATION 645 X = 27.5 LEFT HAND SIDE AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO # 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES-REPAIR CATALOG-MD11 REPAIR IDENTIFICATION & TRACKING REQUIRMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 1561 LONGERON 12 LEFT EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-07-2R REPAIR 2 FIGURE 201. EO #1-5100-7-5001B7 PT 1 TITLE: STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL INSPECTION CARRIED OUT AT CURRENT CHECK. REPETITIVE INSPECTIONS REQUIRED AT EVERY 9,500 FC AS PER SRM 53-00-07-2R TABLE 201/REPAIR 2. ORIG SUBMISSION DATE: 1/16/2023

Part: FINGER DOUBLER — DEBONDED (LT WING TE) · airframe 69,076 hrs · 17,786 cycles

LEFT WING TRAILING DGE INBOARD ISLAND TOP PANEL LOWER SURFACE FINGER DOUBLER FOUND DISBOND AT STATION XW 375.340 TO XOFH 453.931. LEFT HAND WING TRAILING EDGE INBOARD ISLAND TOP PANEL LOWER SURFACE FINGER DOUBLER AT STATION XW 375.340 TO XOFH 453.931 REPAIR CARRY OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = -8.5 RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = -8.5 RIGHT HAND SIDE EVALUATED AND FOUND CRACK 1.0" AT SEAT TRACK STATION 635 X = -8.5 RIGHT HAND SIDE. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 625 TO STATION 645 X = -8.5 RIGHT HAND SIDE AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO # 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES-REPAIR CATALOG-MD11 REPAIR IDENTIFICATION & TRACKING REQUIRMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 635 X = -47.5 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 635 X = -47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665 X = -47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 695 X = -8 FOUND CRACKED.

Part: SEAT TRACK — CRACKED (BS 745-801 LBL27) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDE EVALUATED AND FOUND CRACK 1.0" AT SEAT TRACK STATION 755 X = 27.5 LEFT HAND SIDE. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDE AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO # 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 715 X = 8.5 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT CRACKED SEAT TRACK AT STATION 715 X= 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 645 TO STATION 745 X= 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 801 X = 27.5 LEFT HAND SIDE

Part: NONE — NONE (NONE) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDE

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = 8.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 625 TO STATION 645 X = 8.5 LEFT HAND SIDE EVALUATED AND FOUND CRACK 1.0" AT SEAT TRACK STATION 635 X = 8.5 LEFT HAND SIDE. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 625 TO STATION 645 X = 8.5 LEFT HAND SIDE AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO # 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES-REPAIR CATALOG-MD11 REPAIR IDENTIFICATION & TRACKING REQUIRMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 695 X = 27.5 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 695 X= 27.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 645 TO STATION 745 X= 27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 635 X = -47.5 FOUND CRACKED.

Part: SEAT TRACK — CRACKED (BS 715) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 715 X = 8 FOUND CRACKED.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 69,076 hrs · 17,786 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 695 X = 27.5 FOUND CRACKED.

Part: SEAT TRACK — CRACKED (BS 745-781 RBL8) · airframe 69,076 hrs · 17,786 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDE EVALUATED AND FOUND CRACK 1.0" AT SEAT TRACK STATION 755 X = -8.5 RIGHT HAND SIDE. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 745 TO STATION 781 X = -8.5 RIGHT HAND SIDE AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO # 1-5100-7-5001 B7 PART 1 TITLE : STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 69,076 hrs · 17,786 cycles

MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 695 X = -8 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK AT STATION 695 X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICES STATION 645 TO STATION 745 X=-8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUBMISSION DATE: 1/27/2023

Part: DOUBLER — DAMAGED (RT WING) · airframe 69,076 hrs · 17,786 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 728 - 734 FOUND WITH CRACK. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT DOUBLER AT APPROXIMATE STATION XOS 728 - 734 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 — DAMAGED (RT WING) · airframe 69,076 hrs · 17,786 cycles

RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 667 - 673 FOUND WITH CRACK. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT DOUBLER AT APPROXIMATE STATION XOS 667 - 673 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,570 hrs · 16,755 cycles

EMERGENCY LIGHT BAT 1 LOW ALERT WHEN EMERGENCY LIGHTS TESTED. EMRG LIGHT TEST CARRIED OUT. FUNCTION CHECKED SATISFACTORY

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN RIGHT STATION 859 X= -8.5 SEAT TRACK CROWN FOUND DAMAGED. CABIN RIGHT STATION 859 X= -8.5 SEAT TRACK CROWN DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 790 TO STATION 871 X= -8.5, AS PER SRM 53- 00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. REFER TO SPECIAL/NON ROUTINE MAINTENANCE FORM NR N00553 FOR WORK DETAILS.

Part: DOUBLER — CHAFED (CARGO DOOR FRAME) · airframe 64,584 hrs · 16,447 cycles

FORWARD CARGO - FORWARD DOOR JAMB EXISTING REPAIR DOUBLERS CHAFFING AT STATION STATION 895 , LONGERON 38 RIGHT TO LONGERON 42 RIGHT. FORWARD CARGO - FORWARD DOOR JAMB AT STATION 895 , LONGERON 38 RIGHT TO LONGERON 42 RIGHT DAMAGED EXISTING REPAIR DOUBLERS REMOVED AND CARRIED OUT REPAIR AS PER SRM 53-00-15-2R FIGURE 202 REPAIR 8 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - LEFT STATION 5-53 X = 8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN - LEFT STATION 5-53 X = 8.5 SEAT TRACK CROWN DAMAGED , REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1530 TO STATION 5-80 X = 8.5 AS PER SRM 53-00-52- 2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CHAFED (BS 535) · airframe 64,584 hrs · 16,447 cycles

CABIN - LEFT STATION 535 SUPPORT YOKE LOWER EXISTING DOUBLER REPAIR FOUND CHAFFED. CABIN - LEFT STATION 535 LOWER FRAME REPAIR CARRIED OUT AS PER MD-11 SRM53-20-07- 2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: DOUBLER — CHAFED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - LEFT STATION 535 SUPPORT YOKE UPPER EXISTING DOUBLER REPAIR FOUND CHAFFED . CABIN - LEFT STATION 535 UPPER FRAME REPAIR CARRIED OUT AS PER MD-11 SRM53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - LEFT STATION 829 X = 8.5 SEAT TRACK CROWN FOUND DAMAGED. CABIN - LEFT STATION 829 X = 8.5 SEAT TRACK CROWN DAMAGED , SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 785 TO STATION 834 X = 8.5 AS PER SRM 53-00-52-2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - RIGHT STATION 1139 X = -47 SEAT TRACK CROWN FOUND DAMAGED . CABIN - RIGHT STATION 1139 X = -47 SEAT TRACK CROWN DAMAGED , SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1120 TO STATION 1170 X = -47 AS PER SRM 53-00-52-2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - LEFT STATION 1301 X = 47 SEAT TRACK CROWN FOUND DAMAGED . CABIN - LEFT STATION 1301 X = 47 SEAT TRACK CROWN DAMAGED , REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1266 TO STATION 1315 X = 47 AS PER SRM 53-00-52- 2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - RIGHT STATION 829 X = -8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN - RIGHT STATION 829 X = -8.5 SEAT TRACK CROWN DAMAGED , SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 790 TO STATION 871 AS PER SRM 53-00-52- 2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN -RIGHT STATION 5-75 , X = -8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN - RIGHT STATION 5-75 X = -8.5 SEAT TRACK CROWN DAMAGED , REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 5-24 TO STATION 5-85 X = -8.5 AS PER SRM 53-00-52- 2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 64,584 hrs · 16,447 cycles

CABIN - LEFT STATION 755 , X = 8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN - LEFT STATION 755 X = 8.5 SEAT TRACK CROWN DAMAGED , SEAT TRACK REPAIRED AT STATION 742 TO STATION 785 X = 8.5 , AS PER SRM 53-00-52-2R . FIGURE 201 . REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: TRUNNION — CRACKED (NLG) · airframe 64,584 hrs · 16,447 cycles

DURING HFEC INSPECTION AT LEFT HAND NOSE LANDING GEAR TRUNNION FITTING CRACK FOUND EXTENDING UPWARD AFTER THE REPAIR FILLER APPROXIMATELY 0.2 INCHES AT APPROXIMATELY STATION 583. LEFT HAND NOSE LANDING GEAR TRUNNION FITTING CRACK 0.2 INCHES EXTENDING UPWARD ON EXISTING REPAIR FILLER AT STATION 583 , STOP DRILL THE END OF CRACK CARRIED OUT AS PER SRM 53-10-14 REPAIR 2 FIGURE 203 . INITIAL INSPECTION TO BE CARRIED OUT EVERY 250 FLIGHT CYCLES AFTER REPAIR AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 250 FLIGHT CYCLES AS PER SRM 53-10-14 TABLE 201 , FIGURE 203 REPAIR 2 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: BRAKE — FAILED (NR 8) · airframe 61,469 hrs · 15,569 cycles

DURING PREFLIGHT, FOUND THE NR 8 BRAKE WITH MULTIPLE PIECES MISSING AND BROKEN. REMOVED AND REPLACED THE NR 8 MAIN BRAKE ASSY IAW 32-43-20-4. ACFT OK FOR SERVICE.

Part: ENGINE — FAILED (NR 3) · airframe 61,366 hrs · 15,527 cycles

PDIS 621 79-01 3323 13SEP19 MEM OPEN U LOGPAGES: 3144515 2 HOURS INTO FLIGHT #3 ENG OIL QTY WENT RAPIDLY TO 4-THEN DECREASED TO 1-OIL PRESS AND TEMP OK. PER MOCC REQUEST WE WENT TO IDLE ON #3 ENG FOR 2 MIN-NO CHANGE-AT 2 HOURS AND 30 MIN-OIL PRESS STARTED TO DECREASE DOWN TO 100 PSI-SHUTDOWN ENG W/ QRH. FACT 15SEP19 21:11 MEM REPLACED #3 ENGINE PER WORK CARDS 71T0903-PW, 7110000-00-99, 71T0101-PW, 54T0203, 7100000-00-99, 29T0303 AND 7110001-00-91.

Part: LINE — FAILED (HYD SYSTEM) · airframe 61,217 hrs · 15,481 cycles

AFTER LANDING GOT "HYD 2 FAIL" PER CREW DEBRIEF LOSS OF FLUID OCCURED WHEN REVERSER WAS DEPLOYED PRESSURE REMAIND GOOD UNTIL ENGINE SHUT DOWN. BLOCK IN HYDRAULIC QTY INDICATING .6 GALLONS. FOUND HYDRAULIC STOW LINE AT THE HCU FAILED AT THE B NUT BRAZED FITTING. REPLACED NBR 2 ENG T/R STOW LINE MPN AJK7552-5658 IAW MM 20-10-01-2 . PERFORMED LEAK CK WHILE ACTUATING T/R AND LINE INSTANTLY BLOW APART. THE LINE AT THE HCU FAILED AT THE B NUT BRAZED FITTING. THIS IS THE SAME THING THAT HAPPENED @ PHX. COMPLIED WITH E..A. 1-7831-T0349005 REV NO. A P2 NO LEAKS NOTED.

Part: HYDRAULIC LINE — LEAKING (ZONE 100) · airframe 60,962 hrs · 15,403 cycles

HYD 2 OFF ALERT AT 1 20 INTO FLIGHT. QUANITY 2.6 GAL REMAINING. DURING CONFIGURATION 3-2 RMP REPRESSURIZED HYD 2 NORMALLY. LANDED WITH 1.6 GAL REMAINING. FOUND #2 SYSTEM PRESSURE "TEST" LINE WITH A PIN HOLE. REMOVED AND REPLACED AYK7550-812 PIPE ASSY. LEAK CHECKS GOOD. SERVICED #2 HYDRAULIC SYSTEM. OK FOR SERVICE.

Part: LINE — LEAKING (MLG BRAKE) · airframe 60,917 hrs · 15,388 cycles

APPROX. 40 MINUITES AFTER T/O GOT LEVEL 1 HYD. 3 ELEV. OFF ALERT. HYD SYS 3 QTY BEGAN DECREASING UNTIL HYD 3 FAIL ALERT. SYS 3 QTY FELL TO ZERO. UPON INSPECTION OF THE BRAKES. FOUND BOTH #5 AND #7 BRAKE SYSTEM 2 LINES WITH SEVERE LEAKS LOCATED UNDER THE SPRINGS. UNDER WRI 32-40/3049: REPLACED #2 HYD SYSTEM BRAKES LINES ON BOTH #5 AND #7 BRAKES. IAW M/M 32-43-00. LEAK CHECKS GOOD.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA.# 1-5750-T0340906 A P1 STEP 1F(1) AND STEP 1F(3). TITLE: WINGS-FLIGHT SURFACES- RT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502236 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA.# 1-5750-T0340906 A P1 STEP 1F(1) AND STEP 1F(3). TITLE: WINGS-FLIGHT SURFACES- RT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502236 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA.# 1-5750-T0340906 A P1 STEP 1F(1) AND STEP 1F(3). TITLE: WINGS-FLIGHT SURFACES- RT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502236 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA.# 1-5750-T0340905 A P1 STEP 1F(1) AND STEP 1F(3). TITLE: WINGS-FLIGHT SURFACES-LT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502241 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA.# 1-5750- T0340905 A P1 STEP 1F(1) AND STEP 1F(3). TITLE: WINGS-FLIGHT SURFACES-LT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502241 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-07 AND EA.# 1-5750-T0340905 A P1 STEP 1F(1) AND STEP 1F(3). TITLE: WINGS-FLIGHT SURFACES-LT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502241 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING ECCENTRIC HOLE: LENGTH 0.881" X WIDTH 0.621", FINAL ECCENTRIC HOLE: LENGTH 0.958" X WIDTH 0.773". MAXIMUM ECCENTRIC REPAIR LIMIT : LENGTH 0.940" X WIDTH 0.670". OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER EA 1-5750-T0344690 PART 1. TITLE: WINGS-FLIGHT SURFACES- RT WING -OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTINGS CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' ECCENTRIC HOLE BORE CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING ECCENTRIC HOLE: LENGTH 0.873" X WIDTH 0.580", FINAL ECCENTRIC HOLE: LENGTH 0.958" X WIDTH 0.678". MAXIMUM ECCENTRIC REPAIR LIMIT : LENGTH 0.940" X WIDTH 0.670". OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER EA 1-5750-T0344707 PART 1 STEP 1.A.. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002- LT WING - OUTBD FLAP VANE ASSY- MISSING ID PLATE AND TRACK SUPPORT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE CORROSION CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING ECCENTRIC HOLE: LENGTH 0.886" X WIDTH 0.633", FINAL ECCENTRIC HOLE: LENGTH 0.964" X 0.700". MAXIMUM ECCENTRIC REPAIR LIMIT : LENGTH 0.940" X WIDTH 0.670". OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER EA 1-5750-T0344690 PART 1. TITLE: WINGS-FLIGHT SURFACES- RT WING -OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTINGS CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA 1-5750-T0344690 P1 AND SNRM NO: N00789 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING ECCENTRIC HOLE: LENGTH 0.865" X WIDTH 0.585", FINAL ECCENTRIC HOLE: LENGTH 1.026" X WIDTH 0.738". MAXIMUM ECCENTRIC REPAIR LIMIT : LENGTH 0.940" X 0.670" WIDTH. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER EA 1-5750-T0344707 PART 1 STEP 1 A. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002- LT WING - OUTBD FLAP VANE ASSY- MISSING ID PLATE AND TRACK SUPPORT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA 1-5750-T0344707 PART 1 AND SNRM NR: N00778 FOR WORK DETAILS.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING ECCENTRIC HOLE: LENGTH 0.885" X WIDTH 0.600", FINAL ECCENTRIC HOLE: LENGTH 0.950" X WIDTH 0.660". MAXIMUM ECCENTRIC REPAIR LIMIT : LENGTH 0.940" X WIDTH 0.670". OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER EA 1-5750-T0344707 PART 1 STEP 1.A.. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002- LT WING - OUTBD FLAP VANE ASSY- MISSING ID PLATE AND TRACK SUPPORT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA 1-5750-T0344707 PART 1 AND SNRM NO: N00778 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE SPOT FACE CORROSION LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. REPAIR EVALUATED AND FOUND PIVOT OUTBOARD LUG SURFACE REMAINING THICKNESS : 0.560" ACCEPTED AS PER EA 1-5750-132737 E PART 5 FIGURE 1. TITLE: WINGS-FLIGHT SURFACES-LT WING -INBD FLAP-OUTBD HINGE (FLAP SIDE) HINGE BRACKET CORROSION-PSE 57-55-01-2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO EA 1-5750-132737 E PART 5 AND SNRM NO: N00747 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03.OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND EA # 1-5750-132737 E PART 5 STEP 2A AND STEP 2B.TITLE: WINGS-FLIGHT SURFACES- LH WING -INBD FLAP-OUTBD HINGE (FLAP SIDE) HINGE BRACKET CORROSION-PSE 57-55-01- 2.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO EA# 1-5750-132737 E PART 5 AND SNRM NO: N00747 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION RIGHT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND EA. 1-5750-132738 D PART 5 STEP 2A AND 2B. TITLE: WINGS-FLIGHT SURFACES-RT WING-INBD FLAP -OUTBD HINGE (FLAP SIDE) HINGE BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO EA. 1-5750-132738 D PART 5 AND SNRM NO: N00744 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE SPOT FACE CORROSION LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE SPOTFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07. REPAIR EVALUATED AND FOUND PIVOT BORE SURFACE REMAINING THICKNESS: INBOARD FACE: 0.471" : OUTBOARD FACE: 0.445" ACCEPTED PER EA. 1-5750-T0340905 A P1 STEP 1 E. TITLE: WINGS- FLIGHT SURFACES-LT WING- INBD FLAP -OUTBD FWD HINGE (WING SIDE) REPAIR-PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 57502241 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION RIGHT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND EA. 1-5750-132738 D PART 5 STEP 2A AND 2B. TITLE: WINGS-FLIGHT SURFACES-RT WING-INBD FLAP -OUTBD HINGE (FLAP SIDE) HINGE BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132737 E PART 5 STEP 2A AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES- LT WING -INBD FLAP-OUTBD HINGE (FLAP SIDE) HINGE BRACKET CORROSION-PSE 57-55-01-2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE CORROSION LEFT HAND WING OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. REPAIR SHIM FABRICATED AND ISTALLED AS PER CMM 57-44-09 AND EA : 1-5750-T0344532 P1 STEP 2. TITLE : WINGS-FLIGHT SURFACES -EO 1-5750-7-5002- LT WING OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO EA. 1-5750-T0344532 P1 AND SNRM NR N00378 FORWORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD FLAP INBOARD FOWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION LEFT HAND WING OUTBOARD FLAP INBOARD FOWARD HINGE (WING SIDE) PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08.OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA.: 1-5750-T0344560 P1 STEP 2. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LT WING-OUTBD FLAP, INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING OUTBOARD FLAP INBOARD FOWARD HINGE (WING SIDE) UPPER MOUNT OUTBOARD HOLE BORE CORROSION RIGHT HAND WING OUTBOARD FLAP INBOARD FOWARD HINGE (WING SIDE) UPPER MOUNT OUTBOARD HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER CMM 57-44-08 AND EA.1-5750-T0344534 P1 STEP 2. TITLE:WINGS-FLIGHT SURFACES-EO 1-5750-7-5002- RT WING-OUTBD FLAP, INBD FWD HINGE(WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE CORROSION LEFT HAND WING OUTBOARD FLAP OUTBOARD FOWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AS PER EA. 1-5750-T0344532 P1 STEP 2 AND ISTALLED AS PER CMM 57-44-09 AND EA : 1-5750-T0344532 P1 STEP 2. TITLE : WINGS-FLIGHT SURFACES -EO 1-5750-7-5002- LT WING OUTBD FLAP, OUTBD FWD HINGE (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — PUNCTURED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATE STATION XIS 159 FOUND SKIN PUNCTURED LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATE STATION XIS 159 SKIN PUNCTURED REPAIRED AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

LOWER AFT CARGO WASTE TANK COMPARTMENT FLOOR SKIN FOUND WITH CORROSION STATION 2000 BETWEEN LONGERON 45 LEFT - 46 LEFT. LOWER AFT CARGO WASTE TANK COMPARTMENT AT STATION 2000 BETWEEN LONGERON 45 LEFT - 46 LEFT FLOOR SKIN CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202. ORIGINAL THICKNESS 0.178 " MATERIAL REMOVED 0.100 " REMAINING THICKNESS 0.078 ". REPAIR CARRIED OUT AS PER EA 1-5330-T0344689 P1 TITLE : FUSELAGE - PLATES & SKINS - AFT BODY - CORROSION FOUND COMMON TO KEEL PLANK SHEET AT STA 2000 , BETWEEN L - 45L AND L - 46L. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — DEBONDED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING FIXED FAIRING ABOVE REAR SPAR UPPER SECTION BETWEEN STATION XW 373 / 486 FOUND FINGER DOUBLER DISBONDED. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED FAIRING ABOVE REAR SPAR UPPER SECTION SKIN BETWEEN STATION XW 373 - XW 486 AS PER SRM 57-50-01-2R FIGURE 202 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 536 - 541 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 536 - XOS 541 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STATION XOS 767 - 772 FOUND WITH CRACK REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT XOS 767 -772 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 615 - 620 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 615 - XOS 620 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 672 - 678 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 672 - XOS 678 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

MAIN DECK CARGO AFT COMPARTMENT FLOOR RIGHT HAND FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1981 X = - 57 MAIN DECK CARGO AFT COMPARTMENT FLOOR, AT RIGHT HAND FLOOR SUPPORT STATION 1981 X = - 57 CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G AT STATION 1887 TO STATION 2007 X = - 57. NEW FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 652 - 657 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 652 - XOS 657 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT STATION XOS 584 - 589 FOUND WITH CRACK REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT XOS 584 - 589 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 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 524 - 530 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 524 - XOS 530 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT WING LEADING EDGE COMPARTMENT AT STATION XOS 993 FOUND FORMER CRACK RT WING LEADING EDGE COMPARTMENT AT STATION XOS 993 CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DRAWING ARB1164 REVISION M AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 783 - 789 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 783 - XOS 789 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STATION XOS 758 - 763 FOUND WITH CRACK REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT XOS 758 - 763 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 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 662 - 667 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 662 - XOS 667 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 578 - 584 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 578 - XOS 584 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

MAIN DECK CARGO AFT COMPARTMENT FLOOR CENTER FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1971 X = - 2. MAIN DECK CARGO AFT COMPARTMENT FLOOR AT CENTER FLOOR SUPPORT STATION 1971 X = -2, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G AT STATION 1887 TO STATION 2007 X = -2. NEW FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA7080 REVISION S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 59,951 hrs · 15,085 cycles

RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STATION XOS 610 - 615 FOUND WITH CRACK REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT XOS 610 - 615 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,951 hrs · 15,085 cycles

MAIN DECK CARGO AFT COMPARTMENT FLOOR CENTER FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1981 X = 2 MAIN DECK CARGO AFT COMPARTMENT FLOOR, AT CENTER FLOOR SUPPORT STATION 1981 X = 2, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206. CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G AT STATION 1887 TO STATION 2007 X = 2. NEW FLOOR SUPPORT FABRICATED BY MACHINING AS PER DRAWING AGA7081 REVISION M. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 642 - 647 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 642 - XOS 647 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,951 hrs · 15,085 cycles

LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 494 - 500 FOUND CRACK LEFT HAND WING OUTBOARD LEADING EDGE BEADED DOUBLER AT APPROXIMATELY STATION XOS 494 - XOS 500 REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT BRACKET — DAMAGED (LT MLG WW) · airframe 59,551 hrs · 14,956 cycles

LT MAIN GEAR WHEEL WELL AFT STRUCTURE SUPPORT NEAR I/B SPOILER, BROKEN REPLACED SUPPORT BRACKET.

Part: SUPPORT — CRACKED (LT MLG WW) · airframe 59,551 hrs · 14,956 cycles

LT MAIN GEAR WHEEL WELL AFT STRUCTURE SUPPORT NEAR I/B SPOILER CRACKED IN WORK.

Part: BRACE — CRACKED (N/A) · airframe 59,551 hrs · 14,956 cycles

L/H MAIN GEAR WHEEL WELL AFT STRUCTURE SUPPORT NEAR I/B SPOILER CRACKED REMOVED AND REPLACED BRACE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 56,380 hrs · 13,991 cycles

DURING A SERVICE CHECK, FOUND EMERGENCY EXIT SIGN LIGHT INOPERATIVE ABOVE L1 ENTRY DOOR MOUNTED ON SLIDING CEILING PANEL. PERFORMED VISUAL INSPECTION OF WIRE B319-15-20 AND B319-16-20 RUN BETWEEN SIGN LIGHT ASSY L2-721 AND TERMINAL BLOCK S3-728. SEVERAL SUSPECT AREAS OF QUESTIONABLE CONDITION WHERE NOTED. NEEDS AVIONICS ASSISTANCE. REPAIRED DAMAGED WIRE IAW WDM 33-52-01, CHECKED NORMALIAW MM 33-27-05-5. REPAIRED DAMAGED WIRE B319-15-20 IAW WDM 33-52-01, CHECKED NORMAL IAW MM 33-27-05-5.

Part: MONITOR — FAILED (ADG POWER) · airframe 55,171 hrs · 13,693 cycles

AFTER DEPLOYING THE ADG, DID NOT PICK UP LT EMERGENCY AC BUSS. DETERMINED BY DISCHARGE GOING FROM -47 TO (-2) TO (0). ADG GROUND TEST CARRIED OUT IAW AMM 24-25-00-700-802, FOUND POWER MONITOR U1-540 FAILED. REMOVED AND REPLACED POWER MONITOR IAW AMM 24-25-06-4. ADG GROUND TEST CARRIED OUT IAW AMM 24-25-00-700-802, FOUND SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 1603) · corrosion level 2 · airframe 55,169 hrs · 13,692 cycles

MAIN DECK FLOOR SEAT TRACK FLANGE FOUND WITH CORROSION AT BS 1603, RBL 8.5. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1780) · corrosion level 2 · airframe 55,169 hrs · 13,692 cycles

MAIN DECK SEAT TRACK FLANGE FOUND WITH CORROSION AT BS 1780, LBL 8.5. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 55,169 hrs · 13,692 cycles

DURING HFEC INSPECTION ON STA 5-123, LONGERON SPLICE 3R FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01-0G, DRAWING A5A7111 REV C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: BEAM — DAMAGED (NR 2) · airframe 55,169 hrs · 13,692 cycles

MAIN DECK CARGO L4 DOOR FWD UPPER BEAM DOOR STOP NR 2 BROKEN. REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1524) · airframe 55,169 hrs · 13,692 cycles

SEAT TRACK CROWN AREA DAMAGED AT BS 1524, LBL 75.25. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1491 - 1531, IAW SRM 53- 00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 55,169 hrs · 13,692 cycles

DURING ACCOMPLISHMENT OF NDT INSPECTION ON THE RT WING LOWER SKIN PANELS, THE OUTER WING ACCESS PANEL CUTOUT AT XORS 696, SIX FASTENER HOLES NR 9, 11, 13, 33, 34, AND 36 WERE FOUND CRACKED. REPAIRED THE SKIN IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 55,169 hrs · 13,692 cycles

DURING ACCOMPLISHMENT OF NDT INSPECTION ON THE LT WING LOWER SKIN PANELS OUTER WING ACCESS PANEL CUTOUT AT XORS 696, ONE FASTENER HOLE NR 6 FOUND CRACKED. REPAIRED THE SKIN IAW SRM 57--20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON — CRACKED (BS 1531) · airframe 55,169 hrs · 13,692 cycles

BS 1531, LONGERON 12R, DURING AN X RAY INSPECTION, A CRACK WAS FOUND ON FWD LONGERON. REPLACED THE LONGERON FROM BS 1511 TO 1531 IAW SRM 53-00-05-2R, FIG 201, REPAIR 1. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1255) · airframe 55,169 hrs · 13,692 cycles

MDCC L3 DOOR FWD LOWER FUSELAGE FRAME WEB CRACKED AT BS 1255 BETWEEN LONGERONS 26-27L. REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR 3. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 55,169 hrs · 13,692 cycles

LEFT WING LEADING EDGE CAVITY AT XOS 669 STRINGER CRACKED. REPAIRED THE STRINGER IAW SRM 57-40-03-02R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 55,169 hrs · 13,692 cycles

LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,169 hrs · 13,692 cycles

RIGHT WING LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 55,169 hrs · 13,692 cycles

RIGHT HAND WING LEADING EDGE CAVITY AT XOS 669 STRINGER CRACKED. REPAIRED THE STRINGER IAW SRM 57-40-03-02R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 54,870 hrs · 13,607 cycles

DURING PREFLIGHT INSPECTION FOUND EMERGENCY LIGHT BATTERY 1 LOW. PERFORMED AN OPS CHECK ON THE EMERGENCY LIGHT SYSTEM IAW AMM 33-50-00-5. TEST PASSED.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE DUCT) · airframe 54,526 hrs · 13,500 cycles

AFTER TAKE OFF AT 1000 FT AGL, RECEIVED A LEVEL 3 ENG 2 ALERT, ICE DUCT. COMPLIED WITH QRH RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-22-05-00. PERFORMED A NR 2 ENGINE ANTI-ICE INSPECTION CHECK IAW AMM 30-22-00-6-2. INSPECTED ENGINE ANTI-ICE DUCTS, DUCT FLANGES, DUCT COUPLINGS, SUPPORT LINKS, NO DISCREPANCIES FOUND. REMOVED AND REPLACED THE NR 2 ENG NOSE COWL ANTI ICE VALVE IAW AMM 30-22-01. R & R THE CONTINIOUS FIRE DETECTOR UNIT (CFD) IAW AMM 30-22-10-4 AND RELAY R2-5527 IAW SMP, CHECKED OK. REMOVED & REPLACED THE NR 2 ENGINE MANIFOLD FAILURE SENSING ELEMENT D1-89, D1-90 AND D1-91 IAW AMM 30-22-11-4. RAN NR 2 ENGINE IAW JRH CHAPTER 5, CHECKED THE ANTI-ICE SYSTEM AND NO DISCREPANCIES NOTED. ACFT OK FOR SERVICE.

Part: SWITCH — INOPERATIVE (L1 DOOR SLIDE) · airframe 54,011 hrs · 13,324 cycles

L1 DOOR EVACUATION SLIDE PRESS TO TEST IS INOPERATIVE.

Part: BRAKE ASSY — DISINTEGRATED (NR 6) · airframe 53,699 hrs · 13,241 cycles

NR 6 BRAKE DISINTEGRATING R & R THE NR 6 BRAKE & TIRE IAW MM 32-43-20-4 & 32-41-01-4.

Part: SENSOR — DEFECTIVE (ANTI-ICE SYS) · airframe 53,669 hrs · 13,233 cycles

ENGINE 2 ANTI-ICE DUCT FAIL, PASSING FL 200 TURNED ON ENGINE ANTI-ICE, RECEIVED NR 2 ENGINE DUCT FAILURE NR 2 ANTI-ICE DISAGREE. QRH INDICATED FAILURE OF NR 2 A/I DUCT. RETURNED TO PAN C WHERE ICING DID NOT EXIST. R & R ALL 3, NR 2 ENGINE COWL ANTI-ICE MANIFOLD FAIL SENSING ELEMENTS REF AMM 30-22-11-4. PERFORMED SATISFACTORY FUNCTIONAL TEST REF AMM 30-22-11-5. PARTS REMOVED ARE ELEMENT, PN 35512-61, AND 2 EA SAFETY SYS, PN 35519-4-310, SN AAC0961 & AAC0955, PARTS INFO PROVIDED REF GMM 12-7-600. OK FOR SERVICE.

Part: HOSE — INOPERATIVE (NR 2 ENGINE) · airframe 515 hrs · 12,603 cycles

LEVEL 1 ENG 2, ANTI-ICE OFF OCCURRED DURING FLIGHT. PERFORMED WING ANTI-ICE TEST & FOUND DP1 SENSOR READOUT 5.33 TOO HIGH. DO LT WING ANTI-ICE SENSE LINE LEAK TEST & FOUND HEAVY AIR LEAKING FROM LOW PORT FITTING OF DP SENSOR. REMOVED THE HOSE FOR CHECK & FOUND THE FITTING & B-NUT BOTH WAS BAD. R & R DP SENSOR & HOSE, LEAK CHECKED & FUNCTION CHECKED, ALL NORMAL IAW AMM 30-11-02-4 & 30-11-00-5. PERFORMED NR 1 PNEUMATIC TEST WITH ENG RUN & FUNCTION NORMAL IAW AMM 36-00-03-5.

Part: STRAP — CRACKED (RT WING) · airframe 505 hrs · 12,288 cycles

RIGHT WING LE LOWER PANEL CUT OUT FWD STRAP AT XOS 550 FOUND CRACKED. REMOVED IAW SRM 51-35-01-0G . FABRICATED IAW DWG ARB2933 REVISION T. INSTALLED IAW SRM 51-35-01-0G . REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 505 hrs · 12,288 cycles

LEFT WING FIXED LE APPROX STATION XOS 623 FOUND BEADED DOUBLER CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1885, X= 8, INBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 REFER TO SNRM N00841 FOR WORK DETAILS REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1871-1887) · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1871 - 1887, X= 47.5, INBD. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1881, X= 27.5, INBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 REFER TO SNRM N00845 FOR WORK DETAILS REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 505 hrs · 12,288 cycles

LEFT WING FIXED LE APPROX STATION XOS 584 FOUND SUPPORT DOUBLER CRACKED. LT WING FIXED LE FABRICATED IAW DWG ARB2931 REVISION H. CRACKED EXISTING DOUBLER, FORMER, R & R WITH NEW FABRICATED DOUBLER, FORMER, IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1853 - 1887, X= 27.5, OTBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1881, X=-8, INBD. SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1855, X= 8, INBD. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1811 TO STA 1887, X= 8 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 505 hrs · 12,288 cycles

MAIN DECK SEAT TRACK FLANGE LOWER SURFACE CORRODED AT STATION 1821 - 1841, X= 27.5, OTBD. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 505 hrs · 12,288 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT STATION 535, LONGERON 24R FRAME FOUND CHAFED. FRAME REPAIRED IAW SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (FUSELAGE) · airframe 505 hrs · 12,288 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT STATION 535, LONGERON 19R FRAME FOUND CHAFED. FRAME REPAIRED IAW SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 505 hrs · 12,288 cycles

RIGHT WING REFUELING PANEL CUT OUT FWD INBD CORNER SUSPECT CRACK AT APPROX STATION XOS 610. CARRIED OUT REPAIR IAW SRM 57-40-01-2R REPAIR 18 FIGURE 201 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 505 hrs · 12,288 cycles

LEFT WING FIXED LE APPROX STATION XORS 633, FOUND BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 505 hrs · 12,288 cycles

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

Part: DOUBLER — CRACKED (RT WING) · airframe 505 hrs · 12,288 cycles

RIGHT WING LE CAVITY AT STATION XOS 789 DOUBLER CRACKED. DOUBLER FABRICATED IAW DWG ARB3954 REVISION K. CRACKED EXISTING DOUBLER R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 505 hrs · 12,288 cycles

RIGHT WING LE CAVITY AT STATION XOS 667 DOUBLER CRACKED. FABRICATED IAW DWG ARB3954 REVISION K. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SENSING ELEMENT — FAULTY (ANTI-ICE SYS) · airframe 48,828 hrs · 11,729 cycles

ON DEPARTURE RECEIVED LVL 3 ENG ANTI-ICE DUCT. QRH COMPLIED WITH. NR 2 ENG SHUTDOWN, RETURNED TO KPHX. REMOVED AND REPLACED NR 2 ENG ANTI ICE MANIFOLD SENSING ELEMENT ON NR 2 BANJO SPAR & SAFETIED. REF MM 30-22-11-4. INSTILATION COMPLETE NEED OPS CHECK.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 47,994 hrs · 11,442 cycles

AT ALTITUDE RECEIVED AIR SYS 2 OFF ALERT WITH RED MANIFOLD PEAK TEMP NOTICED 185. RED MANIFOLD DISPLAY WENT AWAY AFTER A FEW SECONDS. R & R THE MANIFOLD FAILURE CONTROLLER IAW AMM 36-23-01-4. ADJUSTMENT TEST OF NEW MANIFOLD FAILURE CONTROLLER TESTED GOOD IAW AMM 36-23-01-5.

Part: SKIN — CHAFED (ZONE 100) · airframe 46,426 hrs · 10,909 cycles

FWD CARGO DOOR CUT-OUT, FWD SIDE BS 888-895, L41R DOUBLER FOUND CHAFED. REPAIRED IAW SRM 53-00-15, REPAIR 8, FIG 202, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — DAMAGED (RUDDER) · airframe 46,426 hrs · 10,909 cycles

AFT UPPER RUDDER FOUND DAMAGE AT AFT TOP CORNER AND 10 INCHES FROM THE TOP. REPAIRED IAW SRM 55-40-01. REPAIR 4, REV 52 AND EA 1-5540-T0300623, PART 1.

Part: SKIN — CRACKED (RT WING) · airframe 46,426 hrs · 10,909 cycles

EIGHT FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 690 AND XORS 700. HOLES REAMED IAW SRM 57-20-02, FIG 201, REPAIR 5. REPAIR BUSHINGS FABRICATED AND INSTALLED IAW SRM 57-20-02, FIG 201, REPAIR 5, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (LT WING) · airframe 46,426 hrs · 10,909 cycles

SEVEN FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 690 AND XORS 700. REAMED IAW SRM 57-20-02, FIG 201, REPAIR 5. REPAIR BUSHINGS FABRICATED AND INSTALLED IAW SRM 57-20-02, FIG 201, REPAIR 5, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SUPPORT FITTING — WORN (MLG ACTUATOR) · airframe 46,426 hrs · 10,909 cycles

NOSE LANDING GEAR UNLOCK ACTUATOR SUPPORT FITTING UPPER BOLT HOLES, TWO FOUND WORN. REPAIRED IAW EA 1-5310-T0300622. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: FRAME — DEFORMED (CARGO DOOR) · airframe 46,426 hrs · 10,909 cycles

FORWARD CARGO DOOR AFT LOWER FRAME FOUND DEFORMED. REMOVED IAW SRM 51-35-01, REV 52. NEW FRAME FABRICATED IAW ADA7083 REV E AND INSTALLED IAW EA 1-5230-166137, TITLE: DOORS - CARGO DOORS / HYD SYS -FWD LOWER CARGO DOOR -FRAME REPLACEMENT -RSC TRACKING. ADJUSTMENT OF THE FWD LOWER CARGO DOOR LATCHES CARRIED OUT IAW 52-31-04-820-801, REV 76.1 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 46,426 hrs · 10,909 cycles

MAIN CARGO SEAT TRACK FOUND CRACKED AT STATION 755, X= -8.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 745 TO STATION 781, X= -8.5 IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 46,426 hrs · 10,909 cycles

MAIN CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 27.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FRON STATION 625 TO STATION 745, X= -27.5 IAW SRM 53-00-52, FIG 201, REPAIR 1, REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SKIN — CRACKED (ZONE 600) · airframe 46,426 hrs · 10,909 cycles

RT WING T/E LOWER ACCESS PANEL 641JB CUT-OUT FORWARD EDGE LOWER CAP SURFACE, FOUND CRACK ABOUT 2" AT XW 339. REPAIR CARRIED OUT IAW EA 1-5710-166135, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 46,426 hrs · 10,909 cycles

CABIN - R3 DOOR FWD JAMB LOWER WEB BS 1256 FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIGURE 201, REPAIR 3, REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 46,426 hrs · 10,909 cycles

RT WING FIXED L/E BEAD DOUBLER FOUND CRACKED AT XOS 666. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 46,426 hrs · 10,909 cycles

LT WING -T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP LOWER SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5710-166134. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.

Part: SWITCH — UNSECURE (SENSING LIGHT) · airframe 44,494 hrs · 10,365 cycles

RT DOOR PRESSURE SENSING LIGHT INOPERATIVE. SECURED SWITCH BACK TO TEST LIGHT OPS CHECKS GOOD IAW AMM 25-61-04-4 .

Part: ACTUATOR — INOPERATIVE (THRUST REVERSER) · airframe 44,074 hrs · 10,257 cycles

SHORTLY AFTER SETTING TAKEOFF PWR, NR 3 THRUST REVERSER CAME ON. ABORTED TAKEOFF & RETURNED TO RAMP. REMOVED AND REPLACED #3 ENGINE O/B UPPER FEEDBACK ACTUATOR AIW ATA/WRI 78-30/2865 AND ATA/WRI 78-30/2869. A/C OK FOR SERVICE. REMOVED AND REPLACED #3 ENGINE O/B UPPER FEEDBACK ACTUATOR, IAW AMM 78-32- 01-4-2. PERFORMED OPS TEST OF THRUST REVERSER SYS, OPS & LEAK CHECKED GOOD. PERFORMED ENGINE CHECK NR 10 TEST, IAW FIM N72-00-00-1. ALL NR 3 ENG THRUST REVERSER POS VALUES IN EEC3A/B ARE WITHIN LIMITS. TEST PASSED, OPS CHECKED GOOD. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 41,982 hrs · 9,676 cycles

1R DOOR ARMED LIGHT INOPERATIVE. INDICATOR REPLACED , OPS CHECKED IAW MM 52-70-00.

Part: COUPLING — CRACKED (HYD LINE) · airframe 41,734 hrs · 9,608 cycles

AFTER T/O "NR1 HYD LOW" ALERT APPEARED WITH FLUID DECREASING THEN HYD FAIL ALERT IN NR1. FLUID QUANTITY INDICATED 0. FOUND CRACKED UNION NR 1 HYD RETURN LINE, PERFORMED REPAIR IAW AMM 20-10-01. REMOVED AND REPLACED NR 1 ENGINE MANIFOLD FILTERS IAW MM 29-12-41-2. REPLACED NR 1 ENGINE LEFT AND RIGHT HYDRAULIC PUMPS IAW MM 29-11-20-4-2. SERVICED HYDRAULIC SYSTEM IAW MM 29-11-20. BOTH HYDRAULIC PUMPS, FILTER MANIFOLD AND SLAT REPAIR LEAK CHECKED GOOD. INSTALLED SLAT PANEL IAW MM 57-40-01-4. OK FOR SERVICE.

Part: LONGERON — CRACKED (NLG WW) · airframe 40,929 hrs · 9,401 cycles

NLG WHEEL WELL , RT NLG TRUNNION WEB AFTER S/M TRIM OUT ON CRACKED AREA, LONGERON FASTENER HOLE SUSPECT CRACK AS MARKED. LONGERON REMOVED AND REPLACED AS PER SRM 51-31-01 REV 46. FABRICATED LONGERON AS PER DRAWING ACA3796 REV A. CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100 REV 112.

Part: SEAT TRACK — DAMAGED (BS 495) · airframe 40,929 hrs · 9,401 cycles

CABIN - RT STA 495 X=-77.25 SEAT TRACK FOUND DAMAGED. CARRIED OUT REPAIR IAW SRM 53-00-52, REPAIR 4, FIG 201, REV 46. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 112.

Part: TRUNNION — CRACKED (FUSELAGE) · airframe 40,929 hrs · 9,401 cycles

NLG WHEEL WELL, NLG TRUNNION WEB FITTING RT SUSPECT CRACK AS MARKED. CARRIED OUT REPAIR AS PER SRM 53-10-14 FIG 202 REV 46. NLG AND DOORS OPS CHECKED CARRIED OUT AS PER AMM 32-31-00-700-801 REV 70.6 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100 REV 112. INITIAL INSPECTION AT 1500 AND REPETITIVE INSPECTION AT 1500 USING HFEC OR LIQUID PENETRANT.

Part: HINGE — CRACKED (FLIPPER DOOR) · airframe 40,929 hrs · 9,401 cycles

LT MLG WHEEL WELL , FLIPPER DOOR FWD AND AFT HINGE AREA FOUND CRACKED AS MARKED. REPAIRED AS PER SRM 52-82-01 REV 46 AND EA 1-5280-143594. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.

Part: FRAME — DENTED (BS 1721) · airframe 40,929 hrs · 9,401 cycles

CABIN - LT STA 1721 FRAME FOUND DENT. CARRIED OUT REPAIR AS PER SRM 53-00-07 FIG 201 REV 46 REPAIR 2. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.

Part: FRAME — DAMAGED (ZONE 200) · airframe 39,056 hrs · 8,965 cycles

MAIN DECK - WHILE CARRYING OUT EO 1-2620-7-5005C PT1, 3 EACH EXTRA HOLES DRILLED ON FRAME AT STA 1964 BETWEEN LONGERON 2L TO LONGERON 3L. 03 EACH EXTRA HOLES DRILLED AT MAIN DECK WHILE CARRYING OUT EO 1-2620-7-5005 C PT1 AT STA 1964 BETWEEN LONGERON 2L TO 3L REPAIRED IAW SRM 53-00-07, FIG 201, REV 44. CLASSFIED AS MAJOR REPAIR IAW GMM 6-2-100, REV 111.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,221 hrs · 8,086 cycles

CABIN - FLOOR CHANNEL AT RT STA 1985 X= -54 FOUND EXFOLIATION CORROSION. REMOVED AND REPLACED AS PER SRM 51- 31-01 REV. 41. REPAIR CLASSIFED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

FLOOR CHANNNEL AT RT STA 1980 AND STA 1990, X= -27 FOUND EXFOLIATION CORROSION. REMOVED AND REPLACED IAW SRM 51-31-01 REV. 41. NEW FLOOR CHANNEL FABRICATED IAW DWG AGA7087 REV M. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CHAFED (BS 490-505) · airframe 35,221 hrs · 8,086 cycles

CABIN - RT STA 490 TO STA 505, X= -75 SEAT TRACK FOUND CHAFED. COMPLIED WITH EA 1-5310-132281, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 107.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

FLOOR CHANNNEL AT RT STA 1970, X= -5 FOUND EXFOLIATION CORROSION. REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. NEW FLOOR CHANNEL FABRICATED IAW DWG AGA7080 REV. 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: CHANNEL — CORRODED (BS 1990) · airframe 35,221 hrs · 8,086 cycles

CABIN - FLOOR CHANNEL AT R/H STA 1990, X= -19 FOUND CORROSION. REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

FLOOR CHANNEL AT RT STA 1990, X= -60 FOUND CORROSION. REMOVED AND REPLACED IAW SRM 51- 31-01 REV. 41. NEW FLOOR SUPPORT CHANNEL FABRICATED IAW DWG AGA7551 REV G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CABIN - LT STA 415 TO STA 475 X= -107 SEAT TRACK FOUND CORROSION. REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 35,221 hrs · 8,086 cycles

R/H WING INBD TRAILING EDGE OUTBD AFT HINGE INBD PIVOT BORE HOLE FOUND WITH MINOR SURFACE CORROSION. COMPLIED WITH EA 1-5750-132738. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 35,221 hrs · 8,086 cycles

RIGHT WING INBD TRAILING EDGE FLAP OUTBD AFT HINGE OUTBD PIVOT BORE HOLE FOUND WITH MINOR SURFACE CORROSION. COMPLIED WITH EA 1-5750-132738. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 35,221 hrs · 8,086 cycles

LEFT WING INBD TRAILING EDGE OUTBD AFT HINGE OUTBD PIVOT BORE HOLE FOUND WITH MINOR SURFACE CORROSION. COMPLIED WITH EA 1-5750-132737, REPAIR CLASSIFIED AS MAJOR.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 5 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE C. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV.107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 3 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 6 SPOOL SUPPORT FITTING AT HOLE D. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: RIB — CRACKED (LT WING LE) · airframe 35,221 hrs · 8,086 cycles

LEFT WING - LEADING EDGE CAVITY SLAT TRACK NR 16 INBD RIB FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SPOOL SUPPORT FITTING AT HOLE B. COMPLIED WITH EA 1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 107.

Part: WEB — CRACKED (ZONE 200) · airframe 35,221 hrs · 8,086 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" AT MAIN CARGO DOOR NR 7 SUPPORT FITTING HOLE A. COMPLIED WITH EA1-5310-132736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV.107.

Part: SUPPORT — CRACKED (RT WING) · airframe 35,221 hrs · 8,086 cycles

RIGHT WING LEADING EDGE INTERIOR COMPARTMENT NR 16 INBD SLAT TRACK SUPPORT RIB FOUND CRACKED. RT WING L/E INTERIOR COMPARTMENT NR 16 INBD SLAT TRACK SUPPORT RIB REMOVED AND REPLACED IAW SRM 51-31-01 REV 41. NEW RIB SUPPORT FABRICATED IAW DWG ARB2850 REV G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 35,221 hrs · 8,086 cycles

RIGHT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING - INBD FLAP VANE ASSY REMOVED AND REPLACED IAW AMM 27-50-22-4, REV.64. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV. 64.

Part: UNKNOWN — VIBRATION (NR 1 ENGINE) · airframe 33,567 hrs · 7,663 cycles

AFTER TAKEOFF PASSING 13000 FT IN CLIMB PWR NR 1 ENG STARTED VIBRATING. AT LEVEL OFF PULLED NR 1 THROTTLE TO IDLE AND WHEN PASSING BELOW 80 PERCENT N1 VIBRATION WENT DOWN SIGNIFICANTLY AND AT IDLE NO VIBRATION NOTED. KEPT THROTTLE BELOW 80 PERCENT TO REMAINDER OF FLT. EVM'S NORMAL ALL ENGINE READINGS NORMAL. OPENED NR 1 ENG COWLING AND INSPECTED COMPONENTS, INSPECTED TAIL PIPE. REMOVED SPINNER COVER AND FOUND EVERYTHING TO BE NORMAL RAN NR 1 ENG POWER ASSURANCE PER JRH WITH ALL PARAMETERS NORMAL, EPR WAS 1.3 N1 84 PERCENT. RAN NR 3 ENG FOR COMPARISONS AND FOUND ALL TO BE NORMAL. RAN ENG NR 1 TO 1.4 EPR AND STILL FELT NO VIBRATIONS. NO VIBRATIONS FELT IN AIRFRAME OR THROTTLES DURING ENTIRE RUN.

Part: SKIN — DENTED (TE FLAP) · airframe 30,636 hrs · 7,003 cycles

LEFT WING - INBOARD FLAP LOWER SURFACE FOUND SEVERAL DENTS AT XIFH 244. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 30,636 hrs · 7,003 cycles

MAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -8.50" 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: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 30,636 hrs · 7,003 cycles

MAIN DECK COMPARTMENT, STA 1989, X= 55 FLOOR SUPPORT FOUND CRACKED. SUPPORT REMOVED AS PER SRM 51-31-01 VOLUME II. NEW FLOOR SUPPORT MACHINED AS PER DRAWING AGA7551 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DAMAGED (ZONE 200) · airframe 30,636 hrs · 7,003 cycles

MAIN DECK, FRAME DOUBLER AT RIGHT STA 1701 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 30,636 hrs · 7,003 cycles

MAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -27.50 INCH 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: SKIN — DENTED (TE FLAP) · airframe 30,636 hrs · 7,003 cycles

RIGHT WING, INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE FOUND WITH DENT. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT RT WING INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 30,636 hrs · 7,003 cycles

MAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = 47.50" 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: SEAT TRACK — CRACKED (ZONE 200) · airframe 30,636 hrs · 7,003 cycles

MAIN DECK COMPARTMENT, AFTER REMOVAL OF LOWER CARGO CEILING PANEL FOUND SEAT TRACK AT STA 635, X = 8.50 INCH 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: BLOCK — CORRODED (ZONE 700) · airframe 26,045 hrs · 5,927 cycles

CENTER LANDING GEAR, LT PILLOW BLOCK AT FORWARD NUT SIDE FOUND SPOTFACE WITH CORROSION. CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK AT FORWARD NUT SIDE SPOTFACE CORROSION REMOVED AND FOUND WITHIN LIMITS PER SRM 53-40-00 VOLUME I, FIGURE 15. THICKNESS OF FORWARD HOLE SURFACE = 2.478", MATERIAL REMOVED = 0.022", (MINIMUM THICKNESS = 2.430). REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (CENTER LG) · airframe 26,045 hrs · 5,927 cycles

CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK ATTACHMENT FITTING FOUND MATING SURFACE WITH FITTING CORROSION. CENTER LANDING GEAR, LEFT HAND PILLOW BLOCK ATTACHMENT FITTING MATING SURFACE - PITTING CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER 53-40-00 VOLUME I, FIGURE 15. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: TRUNNION — CORRODED (CENTER LG) · airframe 26,045 hrs · 5,927 cycles

CENTER LANDING GEAR, RT TRUNNION AFT HOLE UPPER SURFACE FOUND CORRODED. COMPLIED WITH FEDEX E.A 1-5340-103487, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,045 hrs · 5,927 cycles

MAIN DECK CARGO COMPT, MAIN FRAME AT STA 1581 LONGERON 12L FOUND DENT SNRM NO.: N00660, MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1581 LONGERON 12L REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAT INSPECTION REQUIRED ON THE NEXT 14,500 CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 9,500 CYCLES THEREAFTER AS PER SRM 53-30-00 VOLUME I, FIGURE 1. ITEM TRANSFERRED TO OIL CONTROL NUMBER: 0288129.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,045 hrs · 5,927 cycles

MAIN DECK CARGO COMPT, MAIN FRAME AT STA 1641 LONGERON 12R FOUND DENT SNRM NO.: N00659, MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1641 LONGERON 12R REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAT INSPECTION REQUIRED ON THE NEXT 14,500 CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 9,500 CYCLES THEREAFTER AS PER SRM 53-30-00 VOLUME I, FIGURE 1. ITEM TRANSFERRED TO OIL CONTROL NUMBER: 0288130.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,045 hrs · 5,927 cycles

MAIN DECK CARGO COMPT, MAIN FRAME AT STA 1721 LONGERON 12L FOUND DENT. MAIN DECK CARGO COMPT, DENT MAIN FRAME AT STA 1721 LONGERON 12L REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. INITIAL REPEAT INSPECTION REQUIRED ON THE NEXT 14,500 CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 9,500 CYCLES SUBSEQUENTLY AS PER SRM 53-30-00 VOLUME I, FIGURE 1. ITEM TRANSFERRED TO OIL CONTROL NUMBER: 0288128.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,045 hrs · 5,927 cycles

MAIN DECK CARGO COMPT, MAIN FRAME AT STA 1721 LONGERON 12L FOUND DENT AFA7799-1.

Part: TRUNNION — CRACKED (NLG) · airframe 26,045 hrs · 5,927 cycles

NLG, LT NOSE LANDING GEAR TRUNNION FITTING WEB SUSPECT CRACK.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,045 hrs · 5,927 cycles

MAIN DECK CARGO COMPT, MAIN FRAME AT STA 1641 LONGERON 12R FOUND DENT AFA7817-1.

Part: TRUNNION — CRACKED (NLG) · airframe 26,045 hrs · 5,927 cycles

NOSE LANDING GEAR, LEFT NOSE LANDING GEAR TRUNNION FITTING WEB SUSPECTED CRACKED SNRM NO.: N00556. COMPLIED WITH FEDEX EA NR 1-5310-103482, FUSELAGE, LT NOSE LANDING TRUNNION WEB CRACK. STOP DRILL DEVIATION FROM SRM. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FRAME — DENTED (FUSELAGE) · airframe 26,045 hrs · 5,927 cycles

MAIN DECK CARGO COMPT, MAIN FRAME AT STA 1581 LONGERON 12L FOUND DENT AFA7819-1.

Part: STRINGER — CRACKED (LT WING) · airframe 26,045 hrs · 5,927 cycles

LT WING, CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION AT STRINGER 9 (UPPER STRINGER) WING STA XORS 819 SNRM NO.: N00283, LT WING STA XORS 819 STRINGER 9 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME 1, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 26,045 hrs · 5,927 cycles

FOUND LT WING, CRACK FOUND APPROX 7.5" INCHES IN LENGTH DURING HFEC INSPECTION AT STRINGER 9 (UPPER STRINGER) WING STA XORS 819 (ARB7509).

Part: STRINGER — CRACKED (ZONE 500) · airframe 26,045 hrs · 5,927 cycles

LT WING, CRACK FOUND APPROX 9" INCHES IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 ARB7511.

Part: STRINGER — CRACKED (LT WING) · airframe 26,045 hrs · 5,927 cycles

LT WING, CRACK FOUND APPROX 7.5" IN LENGTH DURING HFEC INSPECTION AT STRINGER 14 (UPPER STRINGER) WING STA XORS 521 SNRM NO.: N00284, LT WING TANK STRINGER 14 AT STA XORS 521 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 26,045 hrs · 5,927 cycles

RT WING, CRACK FOUND APPROX 11" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 SNRM NR N00285, RT WING TANK AT WING STA XORS 704 STRINGER 11, CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 26,045 hrs · 5,927 cycles

RT WING, CRACK FOUND APPROX 11" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704.

Part: STRINGER — CRACKED (LT WING) · airframe 26,045 hrs · 5,927 cycles

LT WING, CRACK FOUND APPROX 7.5" INCHES IN LENGTH DURING HFEC. INSPECTION AT STRINGER 14 (UPPER STRINGER) WING STA XORS 521.

Part: STRINGER — CRACKED (LT WING) · airframe 26,045 hrs · 5,927 cycles

LT WING, CRACK FOUND APPROX 9" IN LENGTH DURING HFEC INSPECTION AT STRINGER 11 (UPPER STRINGER) WING STA XORS 704 SNRM NO.: N00282, LT WING TANK STA XORS 704 STRINGER 11 CARRIED OUT REPAIR AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 26,045 hrs · 5,927 cycles

LEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR, CUTOUT FOUND CRACKED.

Part: SKIN — CRACKED (RT WING) · airframe 26,045 hrs · 5,927 cycles

RIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED. RIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT REPAIR CARRIED OUT PER FEDEX EA NR 1-5730-1013480, WINGS RT WING LEADING EDGE SKIN CRACKS AT TELESCOPING DUCT CUTOUT. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 26,045 hrs · 5,927 cycles

RIGHT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR, CUTOUT FOUND CRACKED.

Part: SKIN — CRACKED (LT WING) · airframe 26,045 hrs · 5,927 cycles

LEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT FOUND CRACKED, SNRM NR N00183. LEFT WING, LEADING EDGE TELESCOPIC ANTI-ICE DUCT UPPER DOOR CUTOUT CRACKED AREA REPAIRED AS PER FEDEX EA NR 1-5730-103497, WINGS, LT WING LEADING EDGE SKIN CRACKS AT TELESCOPIC DUCT CUTOUT. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: PANEL — CORRODED (ZONE 300) · airframe 21,984 hrs · 4,967 cycles

HORIZONTAL STABILIZER RIGHT HAND FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83008.

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 21,984 hrs · 4,967 cycles

HORIZONTAL STABILIZER RIGHT HAND AFT SPAR CAP NR 36R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83007.

Part: PANEL — CORRODED (ZONE 300) · airframe 21,984 hrs · 4,967 cycles

HORIZONTAL STABILIZER RT FORWARD PLANK NR 14R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 21,984 hrs · 4,967 cycles

CENTER CARGO STA 1841 FLOOR AREA BULKHEAD APPROX X= -23 WEB FOUND CRACKED. CRACKED WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= -23 CUT AT STA 1841 X= -23 AND REMOVED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR WEB AND DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,984 hrs · 4,967 cycles

CENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= 3 WEB FOUND CRACKED. CRACKED AREA OF WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= 3 TRIMMED OUT AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 21,984 hrs · 4,967 cycles

CENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= -25 VERTICAL STIFFENER FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW STIFFENER FABRICATED AS PER DRAWING AGA7170 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 21,984 hrs · 4,967 cycles

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

Part: SPLICE — CRACKED (ZONE 100) · airframe 21,984 hrs · 4,967 cycles

CENTER CARGO - RIGHT HAND UTILITY TUNNEL AT STA 1531 L-37 RIGHT HAND LONGERON SPLICE FOUND CRACK. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE FABRICATED AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.

Part: WARNING LIGHT — ILLUMINATED (OVERHEAT SYS) · airframe 20,125 hrs · 4,546 cycles

ON CLIMB-OUT AT 14K MSL ENG 2 A-ICE DUCT LEVEL 3 ALERT WITH AURAL WARNING. FOLLWED QRH CHECKLIST AND SHUTDOWN NR 2 ENGINE RETURN TO ONT. OPENED NR 2 ENGINE COWLS FOR INSPECTION, REMOVED ANTI-ICE VALVE HEAT SHIELD, AND REMOVED TWO DUCT ELBOW JOINT HEAT SHIELD FOR DUCT OVER HEAT AND LEAK CHECK INSP ALL DUCTS AND CLAMPS FOUND NO BLOWN DUCTS AND NO VISUAL LEAKS OR DAMAGED. INSP CONNECTORS ON NR 2 ENGINE COWL A/I VALVE. NO PROBLEMS CHECKED FOR 28V ON P1-8245 PIN A VOLTAGE CHECK GOOD FOUND 28VDC AT PIN A REF WDM 30-22-02 SH 1. NR 2 ANTI-ICE VALVE, AND MONITORING SYSTEM HAS BEEN MEL'ED.

Part: DETECTOR — BURST (NR 2 ENGINE) · airframe 19,369 hrs · 4,368 cycles

ON T/O, PRIOR TO FLAP RET, A/C DISPLAYED A MOMENTARY LVL 3 ENG 2 A-ICE DUCT ALERT. AS THROTTLE WAS BEING MOVED TO IDLE ALERT WENT AWAY. CLIMB TO FL 290 WAS UNEVENTFUL UNTIL 30 MIN INTO FLT WHEN A/C DISP LVL-1 ENG 2 A-ICE OFF ALERT, WITH A CONS OF ENG 2 A-ICE DUCT HAS FAILED. ENG SHUT DOWN IN FLT (QRH) WAS PERF AND APPROX 50K FUEL WAS DUMPED. INSPECTED ANTI-ICE DUCT FROM NR 2 ENG FIREWALL AFT R/R`D SENSING ELEMENTS D89, D90, D91 IAW MD-11 MM 30-22-11-4. REPLACED BURST DETECTION UNIT PER MD11 MM 30-22-10-4. PERF MAX POWER ASSURANCE ON NR 2 ENG AND RAN FOR APPROX 5 MIN WITH NO FAULTS OR ALERTS. NR 2 NOSE COWL ANTI-ICE OPS CHECK NORMAL PER JRH 4-28. A/C OK FOR SVC.

Part: FITTING — SCRATCHED (ZONE 100) · airframe 17,085 hrs · 3,824 cycles

CENTER CARGO DOOR INTERIOR, BETWEEN NR 1 AND NR 2 LATCH, FITTING WITH SCRATCH MARK. FITTING REMOVED AND REPLACED IN ACCORDANCE WITH FEDEX EA 1-5230- 71905 - DOORS - CENTER CARGO 104 INCHES DOOR - ALIGNMENT PIN - MODIFICATION.

Part: FRAME — DENTED (ZONE 200) · airframe 17,085 hrs · 3,824 cycles

CABIN LEFT FRAME STA 1761 BETWEEN STR 12-13 DENTED. CABIN LT FRAME, STA 1761 BETWEEN STR 12-13 LT, CARRIED-OUT REPAIR AS PER SRM 53-30-00 FIG. 1 VOL. I AND COMPLIED WITH FEDEX EA 1-5330-74177 - FUSELAGE- FRAME REPAIR - DTR TRACKING - STATION 1761

Part: FRAME — SCRATCHED (ZONE 200) · airframe 17,085 hrs · 3,824 cycles

FWD TAILCONE, LAST FRAME FOUND WITH SCRATCHES. COMPLIED WITH FEDEX EA 1-5300-74174 - FUSELAGE, EXTENDED TAILCONE, FORWARD SECTION, FRAME REPAIR.

Part: FRAME — DENTED (ZONE 200) · airframe 17,085 hrs · 3,824 cycles

MINOR DENT ON FRAME IN CABIN AT STA 1541 BETWEEN STR 12-13 LEFT.

Part: HINGE — LOOSE (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. LT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES. LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — LOOSE (ZONE 600) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR

Part: BUSHING — LOOSE (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG I/B SIDE BUSHING FOUND LOOSE. COMPLIED WITH FEDEX EA 1-5750-75219 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: BUSHING — LOOSE (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING FOUND LOOSE. LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75221, TITLE : WINGS - TE & TE DEVICES - RT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 17,085 hrs · 3,824 cycles

CTR CARGO - BETWEEN BS 1801-1821, RT 40 LONGERON SPLICE CRACKED. COMPLIED WITH FEDEX EA 1-5310-74180 - FUSELAGE- LONGERON SPLICE AT F.S. 1810, LONGERON 40 RT - CORROSION REPAIR

Part: BUSHING — LOOSE (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR LUG I/B SIDE BUSHING FOUND LOOSE.

Part: BUSHING — LOOSE (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75221, TITLE : WINGS - TE & TE DEVICES - RT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: BUSHING — LOOSE (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

LT WING OB FLAP IB HINGE (FLAP SIDE) ACTUATOR LUG IB SIDE BUSHING FOUND LOOSE. REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TITLE : WINGS - TE & TE DEVICES - LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: HINGE — LOOSE (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING FOUND LOOSE. LT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES. LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: FITTING — CRACKED (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

LEFT WING I/B FLAP I/B SIDE LOAD FITTING FOUND CRACKED. LT WING I/B FLAP I/B SIDE LOAD FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II.

Part: HINGE — CORRODED (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WINGS - TRILAING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR

Part: HINGE — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178, TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR

Part: HINGE — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178, TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR

Part: LONGERON — CRACKED (ZONE 100) · airframe 17,085 hrs · 3,824 cycles

CTR CARGO BAY BETWEEN BS 1513 -1547, LONGERON 45, LONGERON SPLICE CRACKED. SPLICE LONGERON AT BS 5-113 - 1547, 45 RT, REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. NEW SPLICE FABRICATED AS PER DWG A5A7116.

Part: HINGE — CORRODED (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE SURFACE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WINGS - TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR

Part: RIB — CRACKED (ZONE 600) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING LOWER WINGLET FOUND CRACKED. RT WING LOWER WINGLET SUPPORT RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51-33-01 VOL. II.

Part: HINGE — CORRODED (ZONE 600) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WINGS - TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR

Part: FRAME — DENTED (FUSELAGE) · airframe 17,085 hrs · 3,824 cycles

CABIN LEFT 9-G NET YOKE ATTACHMENT FRAME DENTED. NET YOKE ATTACHMENT FRAME DENTED REPAIR CARRIED OUT AS PER DWG SRZ-53-503. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION.

Part: FITTING — CRACKED (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

LEFT WING O/B FLAP (FLAP SIDE) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-74168 - WINGS - OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR

Part: STOP FITTING — CRACKED (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING O/B FLAP (FLAP SIDE) STOP FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-74168 - WINGS - OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR.

Part: FITTING — CRACKED (ZONE 600) · airframe 17,085 hrs · 3,824 cycles

RIGHT WING I/B FLAP SIDE LOAD FITTING FOUND CRACKED. RT WING I/B FLAP SIDE LOAD FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, WINGS - TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR I/B BORE HOLE FOUND CORROSION. CORROSION ON LT WING O/B FLAP OB HINGE (FLAP SIDE) ACTUATOR I/B BORE HOLE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, : TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE FOUND CORROSION. CORROSION ON LT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE SURFACE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES - LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR O/B BORE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, TITLE : TE DEVICES. LT O/B FLAP. O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. CORROSION ON LH WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR.

Part: STRUT — LOOSE (ZONE 100) · airframe 17,085 hrs · 3,824 cycles

INBOARD SLAT MECHANICAL RT STRUT ASSY BEARING FOUND MIGRATED. I/B SLAT MECHANICAL RT STRUT ASSY REMOVED & REPLACED AS PER CMM 27- 03-20.

Part: BRACKET — CRACKED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LEFT WING I/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT BRACKET (TOP OF ACTUATOR) FOUND CRACKED. REMOVED & INSTALLED NEW BRACKET AS PER CMM 20-50-02.

Part: BRACKET — CRACKED (ZONE 500) · airframe 17,085 hrs · 3,824 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) FAIRING SUPPORT FWD I/B BRACKET FOUND CRACKED. REMOVED & REPLACED AS PER AMM 20-50-02.

Part: BRACKET — BROKEN (T/E FLAP) · airframe 17,085 hrs · 3,824 cycles

LEFT WING O/B FLAP I/B HINGE (FLAP LOWER SIDE) FAIRING SUPPORT BRACKET FOUND BROKEN. FLAP I/B HINGE (FLAP LOWER SIDE) FAIRING SUPPORT BRACKET REMOVED AND REPLACED AS PER AMM 20-50-02.

Part: BRACKET — CRACKED (LT WING) · airframe 17,085 hrs · 3,824 cycles

LEFT WING O/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT O/B FWD BRACKET FOUND CRACKED. LT WING O/B FLAP O/B HINGE (WING SIDE) FAIRING SUPPORT O/B FWD BRACKET REMOVED AND REPLACED AS PER AMM 20-50-02.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 12,340 hrs · 2,769 cycles

IN CRUISE GOT HYD 3 ELEV OFF THEN 3-2 NRMP INOPERATIVE LOSS OF NR 3 HYD FLUID, THEN HYD NR 3 FAILED. DUMPED APPROX 50000 LBS OF FUEL AND LANDED AT ORD, DECLARED EMERGENCY AND PULLED CVR. FOUND LOOSE B-NUT AT CHECK VALVE IN AFT ACCESSORY COMP RT SIDE. TIGHTENED SAME.

Part: SEAL — LEAKING (ANTI-ICE DUCT) · airframe 10,323 hrs · 2,297 cycles

NR 2 ENG ANTI-ICE DUCT LEVEL 3 ALERT SHUT DOWN ENG. SECURED LOOSE SEAL & R&R PRESS SWITCH PER PRECAUTION.

Part: CONTROL CABLE — LACK OF LUBE (NLG) · airframe 8,202 hrs · 1,813 cycles

ON T/O AIRCRAFT STARTED TO GO TO RIGHT. LEFT RUDDER COULD NOT CORRECT AND HAD TO USE TILLER. LUBED NLG PER SMP INSP STEERING CABLES PER MM 32-51-00-0 & 32-50-00-5. RESERVICED NLG STRUT PER MM 32-11-01. AC OK FOR SERVICE.