N593FE

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING DOUBLER FOUND ON EXTERIOR SKIN LEFT HAND SIDE AT VERTICAL STABILIZER BETWEEN ZFR 293.033 TO ZFR 314.00. EXISTING DOUBLER ON EXTERIOR SKIN LEFT HAND SIDE AT VERTICAL STABILIZER BETWEEN ZFR 293.033 TO ZFR 314.00 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH EA 1- 5530-58209 TITLE : WINGS - R/H LOWER WING SKIN BUSHING REPAIR AT ACCESS HOLE ATTACH POINT . EA 1-5530-58209A P2 TITLE : WINGS - VERTICAL STAB LH SKIN REPAIR .ACCOMPLISHED. EO 1-5100-7-5001B7 PT1 TITLE : STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENT 14CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON EXTERIOR FUSELAGE SKIN AT CENTER CARGO DOOR CUTOUT AFT LOWER JAMB STATION 1781 LONGERON 40 RIGHT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN AT CENTER CARGO DOOR CUTOUT AFT JAMB STATION 1781 LONGERON 40 RIGHT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-15-2R REPAIR 8 FIGURE 202 AND WITH DEEP CHAFFED MARK ON EXISTING REPAIR DOUBLER. EA 1-5330-T0369228 PART 1 TITLE: FUSELAGE - PLATES & SKINS - BLENDOUT ON EXISTING SRM 53-00-15 REPAIR 8 AT CENTER LOWER CARGO DOOR AFT JAMB, STA1781, L-39R TO L-42R ACCOMPLISHED. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON EXTERIOR FUSELAGE SKIN AT CENTER CARGO DOOR CUTOUT AFT JAMB STATION 1781 LONGERON 40 RIGHT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN AT CENTER CARGO DOOR CUTOUT AFT JAMB STATION 1781 LONGERON 40 RIGHT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-15-2R REPAIR 8 FIGURE 202 AND WITH DEEP CHAFFED MARK ON EXISTING REPAIR DOUBLER. EA 1-5330-T0369228 PART 1 TITLE: FUSELAGE - PLATES & SKINS - BLENDOUT ON EXISTING SRM 53-00-15 REPAIR 8 AT CENTER LOWER CARGO DOOR AFT JAMB, STA1781, L-39R TO L-42R ACCOMPLISHED. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - CRUISE PERFORMANCE FILLET ASSEMBLY CRACKED AT STATION XIS 150.7474 LEFT HAND WING - CRUISE PERFORMANCE FILLET ASSEMBLY OUTBOARD RIB AT STATION XIS 150.7474 REPAIR CARRIED OUT AS PER SRM 57-40-71-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TEAR STRAP — OUT OF POSITION (ZONE 100) · airframe 87,265 hrs · 19,523 cycles

WHILE ACCOMPLISHING DOUBLER REPAIR AT FUSELAGE SKIN STATION 675 LONGERON 50 RIGHT HAND, FOUND TEAR STRIP (PART NUMBER: ACA3058-509) AT FORWARD CARGO COMPARTMENT STATION 675 BETWEEN LONGERON 50 RIGHT HAND TO LONGERON 51 RIGHT HAND WITH SHORT EDGE MARGIN FORWARD CARGO COMPARTMENT STATION 675 BETWEEN LONGERON 50 RIGHT HAND TO LONGERON 51 RIGHT HAND TEAR STRIP WITH SHORT EDGE MARGIN CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 53-00-07-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 643 FORMER CRACKED.

Part: SKIN — ABNORMAL (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

DURING HFEC OPEN-HOLE INSPECTION CARRY OUT ON RIGHT HAND WING LOWER SKIN FUEL TANK ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 AND STATION XORS 713.6 , FOUND ADDITIONAL 01 EACH REPAIR BUSHING INSTALLED AT FASTENER HOLE #6 WHICH IS NOT CALLED OUT FOR REPETITIVE INSPECTION FOR N593FE PROJECT. HFEC INSPECTION AND ULTRASONIC INSPECTION CARRIED OUT AS PER DAC NDT SPM PART 06- 10-01.001 AND BOEING DRAWING SN11570000 RESPECTIVELY ON 01 EACH FASTENER HOLE #6 REPAIR BUSHING INSTALLED AREA AND IT'S SURROUNDINGS AS PER STATED IN SRM 57-20-02- 2R TABLE 201,FIGURE 202 REPAIR 5 AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 AND STATION XORS 713.6 AND FOUND NO CRACK EVIDENT .INITIAL INSPECTION CARRIED OUT ON CURRENT CHECK .REPETITVE INSPECTION TO BE CARRY OUT AT EVERY 2000 FC BY ULTRASONIC INSPECTION AND HFEC INSPECTION AS PER SRM 57-20-02-2R REPAIR 5 .TABLE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (AFT BULKHEAD) · airframe 87,265 hrs · 19,523 cycles

EMPENNAGE: AFT FUSELAGE STATION 2164 BULKHEAD THE LOWEST STIFFENER FOUND CRACK APPROXIMATE LENGTH 1 INCH. EMPENNAGE: AFT FUSELAGE STATION 2164 BULKHEAD THE LOWEST AREA CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-33-01-OG. STIFFENER REWORKED AS PER DOUGLAS DRAWING AJC7001 REVISION DT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 87,265 hrs · 19,523 cycles

EMPENNAGE: AFT FUSELAGE RIGHT HAND SKIN AT APU EXHAUST DOOR CUTOUT AREA APPROXIMATELY STATION 2140 LONGERON -36 RIGHT FOUND WITH 1 INCH LENGTH CRACK AS MARKED. EMPENNAGE : AFT FUSELAGE RIGHT HAND SKIN AT APU EXHAUST DOOR CUTOUT AREA APPROXIMATELY STATION 2140 LONGERON 36 RIGHT REPAIR CARRIED OUT AS PER EA # 1-5330- T0369561 P1 TITLE : FUSELAGE - PLATES AND SKINS - TAIL AFT BODY - CRACK ON RH SKIN AT STA 2140,L-36R - CLOSE PROXIMITY TO EXISTING REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR ON FRAME FOUND AT FORWARD AVIONICS COMPARTMENT UNDER RAM AIR DUCTING STATION 469.173 BETWEEN X= 30 TO X= 40. EXISTING REPAIR ON FRAME AT FORWARD AVIONICS COMPARTMENT UNDER RAM AIR DUCTING STATION 469.173 BETWEEN X= 30 TO X= 40 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-07-2R REPAIR 2 FIGURE 201. EXISTING REPAIR CARRIED OUT AS PER EA 1-5310-T0369403 PART 1 TITLE: FUSELAGE - MAINFRAME - FUSELAGE NOSE FRAME REPAIR AT STA 469.173 BETWEEN X=30 AND X=40. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

CABIN - MAIN DECK CARGO COMPARTMENT AFT SEAT TRACK AT STATION 1791 X= 105 FOUND C0RROSION ON FLANGE. CABIN MAIN DECK CARGO COMPARTMENT AFT SEAT TRACK AT STATION 1791 X= 105. C0RROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL EAT TRACK REPLACEMENT AT STATION 1751 TO STATION 1831 X= 105 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SPECIAL / NONROUTINE MAINTENANCE FORM NUMBER: N01356 FOR WORK DETAILS.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

CABIN - MAIN DECK CARGO COMPARTMENT AFT SEAT TRACK AT STATION 1810 X= 105 FOUND C0RROSION ON FLANGE. CABIN MAIN DECK CARGO COMPARTMENT AFT SEAT TRACK AT STATION 1810 X= 105. C0RROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1751 TO STATION 1831 X= 105 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100

Part: SKIN — CHAFED (LT NR 2 SLAT) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - NUMBER 2 SLAT ASSEMBLY INBOARD LOWER EDGE CHAFFING MARK XIS 247.053. LEFT HAND WING NUMBER 2 SLAT ASSEMBLY INBOARD LOWER EDGE CHAFFING MARKED AREA AT XIS 247.053 REPAIR CARRIED OUT AS PER EA : 1-5750-T0369299P1 TITLE: WINGS - FLIGHT SURFACES - LHW #2 SLAT ASSY - CHAFE DAMAGE FOUND ON OUTER SKIN , INNER SURFACE BETWEEN STA 247.028 AND STA XIS 253.212. REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — UNKNOWN (ZONE 100) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON STIFFENER AT AFT CARGO COMPARTMENT STATION 1841 X= -38. EXISTING REPAIR ON STIFFENER AT AFT CARGO COMPARTMENT STATION 1841 X= -38 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-00-00-2R REPAIR GENERAL FIGURE 209 SHEET 1. STIFFENER REMOVED AS PER SRM 51-31-01-0G. STIFFENER FABRICATED AS PER DOUGLAS DRAWING: AGA7170 REVISION: R AND INSTALLED AS PER SRM 51-33-01-0G. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: MOUNT — GOUGED (ZONE 400) · airframe 87,265 hrs · 19,523 cycles

NUMBER 2 ENGINE FORWARD MOUNT HAS GOUGES ON THE AFT LEFT SIDE. REQUIRED REPETITIVE INSPECTION. EA 1-5451-T0369247 PART 1 TITLE: NACELLES / PYLON - TAIL PYLON / STRUT - #2 ENGINE FORWARD MOUNT - SRM BLEND REWORK ON AVB7730-1 SUPPORT - PSE 54.52.03.1 HAS BEEN COMPLIED WITH.

Part: DOUBLER — GOUGED (LT WING) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND AT LEFT HAND WING DROOP LEADING EDGE OUTBOARD SIDE XDLE 309. EXISTING REPAIR DOUBLER AT LEFT HAND WING DROOP LEADING EDGE OUTBOARD SIDE XDLE 309 EVALUATED AND FOUND EXISTING REPAIR DOUBLER WITH DEEP GOUGE MARK AND REMOVED IN ACCORDANCE WITH SRM 51-31-01-0G. DROOP DOUBLER REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 57-40-01-2R REPAIR 15 FIGURE 202. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SKIN — UNKNOWN (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR DOUBLER FOUND ON FUSELAGE SKIN AT STATION 392 LONGERON 25 RIGHT HAND. EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STATION 392 LONGERON 25 RIGHT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 7 FIGURE 201 WITH DEVIATIONS OF FASTENERS. EXISTING REPAIR DOUBLER REMOVED IN ACCORDANCE WITH SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER EA 1-5330-T0369471 PART 1 TITLE: FUSELAGE - PLATES & SKINS - NOSE FUSELAGE - EXISTING REPAIR AT ABA7049-4 RH SKIN BETWEEN STA 383 AND STA 392, BELOW Z= -2.9. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND AT LEFT HAND WING #3 SLAT ASSEMBLY INNER SURFACE STATION XOS 484.511. EXISTING REPAIR AT LEFT HAND WING #3 SLAT ASSEMBLY INNER SURFACE STATION XOS 484.511 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-40-01-2R REPAIR 3 FIGURE 201. REPAIR CARRIED OUT AT LEFT HAND WING #3 SLAT INNER SKIN BETWEEN STATION XOS 455.085 AND STATION XOS 497.924 AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AND EA 1-5750-T0369553 PART 1 TITLE: WINGS - FLIGHT SURFACES - LH WING - #3 SLAT ASSY - INNER SKIN SRM SPLICE REPAIR BETWEEN XOS 455.085 AND XOS 497.924 - RSC TRACKING. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING DROOP LEADING EDGE ASSEMBLY INBOARD EDGE FOUND CHAFFING MARK STATION XDLE 309.934. LEFT HAND WING DROOP LEADING EDGE ASSEMBLY INBOARD EDGE STATION XDLE 309.934 CARRIED OUT REPAIR IN ACCORDANCE WITH SRM 57-40-01-2R REPAIR 15 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR ON FRAME FOUND AT FAC COMPARTMENT UNDER RAM AIR DUCTING STATION 469.173 BETWEEN X=30 TO X=40. EXISTING REPAIR ON FRAME AT FORWARD AVIONICS COMPARTMENT UNDER RAM AIR DUCTING STATION 469.173 BETWEEN X = 30 TO X = 40 EVALUATED AND FOUND NOT REPAIR IAW SRM 53- 00-07-2R REPAIR 2 FIGURE 201. REPAIR CARRIED OUT IAW EA 1-5310-T0369403 PART 1 TITLE : FUSELAGE - MAINFRAME - FUSELAGE NOSE FRAME REPAIR AT STA 489.173 BETWEEN X=30 AND X=40. EO 1-5100-7-5001 B7 P1 TITLE : STRUCTURES - REPAIR CATALOG - MD11 - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DUPLICATED SDR RAISED , REFER TO SNRM N00035 , WORK ORDER 00082944 ,SDR #22-1689 FOR DETAILS

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 553 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 553 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (NONE) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND AT LEFT HAND WING OUTBOARD LEADING EDGE PANEL CUTOUT STATION XOS 906. EXISTING REPAIR AT LEFT HAND WING OUTBOARD LEADING EDGE PANEL CUTOUT STATION XOS 906 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-03-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — NONE (ZONE 100) · airframe 87,265 hrs · 19,523 cycles

EXISTING REPAIR DOUBLER FOUND ON EXTERIOR FUSELAGE SKIN AT STATION 675 LONGERON 50 RIGHT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN AT STATION 675 LONGERON 50 RIGHT HAND EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R REPAIR 8 FIGURE 201 SHEET 5 WITH DEVIATION OF FASTENERS. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER EA 1-5330-T0369415 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 740 FORMER CRACKED LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 740 CRACKED FORMER REMOVED AND FABRICATED PER DOUGLAS DRAWING ARB2923 REVISION D. INSTALLED FABRICATED FORMER AS PER SRM 51-33-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 1025 FORMER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 1025 CRACKED FORMER REMOVED AND FABRICATED FORMER PER DOUGLAS DRAWING ARB2920 REVISION BB. INSTALLED FABRICATED FORMER AS PER SRM 51-33-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 87,265 hrs · 19,523 cycles

CENTRE CARGO COMPARTMENT FOUND BILGE AREA STATION 5-113 TO 1541, LONGERON-52 LONGERON SPLICE SUSPECT CRACKED.

Part: NONE — NONE (N/A) · airframe 87,265 hrs · 19,523 cycles

CENTRE CARGO COMPARTMENT FOUND BILGE AREA STRINGER SPLICE STATION 5-113 TO 1541, LONGERON-50 RIGHT CRACKED.

Part: DOUBLER — CRACKED (ZONE 600 RIB) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING - OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 789 RIB DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 789 CRACKED DOUBLER REMOVED AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AS PER SRM 51-33-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 682 BEADED DOUBLER CRACKED RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 682 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 87,265 hrs · 19,523 cycles

CENTRE CARGO COMPARTMENT FOUND BILGE AREA LONGERON SPLICE STATION 5-113 TO 1541, LONGERON-49 LEFT CRACKED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1371, X= -8.5 FOUND WITH CORROSION. CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1371 X= -8.5 CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1313 TO STATION 1390 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 (N/A) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING DOUBLER FOUND AT UPPER TORQUE BOX WEB STATION 2020 BETWEEN X = - 6.950 TO X = - 15.250.

Part: NONE — NONE (N/A) · airframe 87,265 hrs · 19,523 cycles

CENTRE CARGO COMPARTMENT FOUND BILGE AREA STATION 5-113 TO 1541, LONGERON-43 RIGHT LONGERON SPLICE SUSPECT CRACKED.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 770 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 770 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK FLANGE AT STATION 1301 X= 75.25 FOUND CRACKED. CABIN - MAIN DECK CARGO COMPARTMENT FLOOR CRACKED SEAT TRACK FLANGE AT STATION 1301 X= 75.25 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 1267 TO STATION 1391 X= 75.25 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CORRODED (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

MAIN DECK CARGO AFT COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1871 X=8.5. MAIN DECK CARGO AFT COMPARTMENT FLOOR SEAT TRACK AT STATION 1871 X= 8.5 CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53- 00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1811 TO STATION 1887 X= 8.5 END POINT AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DUPLICATED SDR RAISED, PLEASE REFER TO SNRM N00892. WORK ORDER 00082944. SDR #22- 1520 FOR THE DETAILS.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 730 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 730 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 770 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 770 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING FOUND EXISTING BLEND OUT ON MLG SUPPORT DOUBLER UPPER SURFACE (DIAMOND DOUBLER) BETWWEEN AUX SPAR AND YW467.

Part: SKIN — CRACKED (RT WING) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING - INBOARD FLAP ASSEMBLY UPPER MID SEGMENT SURFACE STATION YIFH 165.300 FOUND CRACKED. CRACK SKIN AT RIGHT HAND WING INBOARD FLAP ASSEMBLY UPPER MID SEGMENT SURFACE STATION YIFH 165.300 REPAIRED AS PER SRM 57-00-01-2R REPAIR 1 FIGURE 201 AND EA 1-5750- T0323138A P2 TITLE : WINGS - FLIGHT SURFACES - EO 1-5100-7-5001 - RH WING - INBD FLAP ASSY - UPPER SKIN PANEL REPAIRS.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 87,265 hrs · 19,523 cycles

MAIN DECK CAGRO AFT COMPARTMENT FLOOR CARGO TRACK FOUND WITH CORROSION AT STATION 1871 X= 8.5. MAIN DECK CARGO AFT COMPARTMENT FLOOR SEAT TRACK AT STATION 1871 X= 8.5 CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53- 00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 1811 TO STATION 1887 X= 8.5 END POINT AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 737 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 737 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 702 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 702 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 760 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 760 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 743 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 743 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 788 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 788 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 762 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 762 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CORRODED (ZONE 200) · airframe 87,265 hrs · 19,523 cycles

MAIN DECK CARGO AFT COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1871 X= -8.5. MAIN DECK CARGO AFT COMPARTMENT FLOOR SEAT TRACK AT STATION 1871 X= -8.5 CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER SRM 53- 00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE STATION 1863 TO STATION 1887 X=-8.5 END POINT AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATELY 0.2 INCH LENGTH AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER AT APPROXIMATELY STATION XOS 486.511. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER AT APPROXIMATELY STATION XOS 486.511 AS PER SRM 57-40-01-2R REPAIR 17 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

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

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 650 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 650 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - OUTBROAD FIXED LEADING EDGE COMPARTMENT STATION XOS 737 BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 737 DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — UNKNOWN (ZONE 600) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING BEADED DOUBLER FOUND AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 667 TO XOS 673. EXISTING BEADED DOUBLER REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 667 TO XOS 673 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — UNKNOWN (RT WING) · airframe 87,265 hrs · 19,523 cycles

AGING AIRCRAFT - EXISTING BEADED DOUBLER FOUND AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 661 TO XOS 667. EXISTING BEADED DOUBLER REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT STATION XOS 661 TO XOS 667 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001 B7 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (LT WING RIB) · airframe 87,265 hrs · 19,523 cycles

LEFT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 789 RIB DOUBLER CRACKED. LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 789 CRACKED DOUBLER REMOVED AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AS PER SRM 51-33-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING LE) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 666 STRINGER CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 666 STRINGER REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: RIB — CRACKED (RT WING) · airframe 87,265 hrs · 19,523 cycles

RIGHT HAND WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 906 RIB DOUBLER CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 906 CRACKED DOUBLER REMOVED AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3594 REVISION K. INSTALLED FABRICATED DOUBLER AS PER SRM 51-33-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FUSE — CRACKED (HYD SYSTEM) · airframe 83,490 hrs · 18,501 cycles

HYD 3 FAIL LEVEL 2 AFTER LANDING. HYD QTY SHOWS ZERO DURING SERVICING OF THE NR 3 HYDRAULIC SYSTEM FOUND THE TRUCK BEAM TRIM CYLINDER INTERLOCK FUSE CASE CRACKED.PN 63602 DATA PLATE MISSING DUE TO THE CRACKED CASE. REPLACED THE TRUCK BEAM TRIM CYLINDER INTERLOCK FUSE, REF MM 32-37-06-4. LEAK CHECK AND OPERATIONS CHECK GOOD. REMOVED AND REPLACED BOTH ENGINE DRIVEN PUMPS ON NR 3 ENGINE, PER MD11 AMM 29-11-20-4-1. DUE TO BEING RAN WITHOUT ANY FLUID. DRY MOTORED NR 3 ENGINE TO OPERATIONS AND LEAK CHECK, BOTH CHECKS GOOD.

Part: WIRE — DAMAGED (LATERAL ROLLERS) · airframe 83,170 hrs · 18,400 cycles

RAMP REPORTED SPARKS UNDER FLOORBOARD AT CENTER CARGO DOOR CUTOUT, WHEN LATERAL ROLLERS ACTUATED. ROLLERS WERE INOPERATIVE. FOUND ROLLER C/B B1-588 TRIPPED. RESET C/B, ACTUATED ROLLERS. C/B TRIPS, NOTICEABLE SPARKS UNDER ROLLER AREA. REMOVED PLUGS P1-993 & P1-992, RESET ALL C/BS. C/BS REMAINED SET. INSPECTED WIRING FROM R5-992 & R5-993 TO C/BS & ALL GOOD. INSPECTED STRUCTURE & SUSPECT WIRING CHAFED STRUCTURE. NO DAMAGE. R & R 24 DAMAGED WIRES & PERFORMED CONTINUITY CHECK OF WIRES, CHECKED GOOD IAW SWPM 20-10-01, 20-20-00, 20-31-00, & WDM 25-52-05, 25-52-06. OPS CHECKED CARGO LOADING SYS, CHECKED NORMAL IAW MM 25-57-00-5, 25-57-10-5, & 25-57-07-5.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 82,903 hrs · 18,331 cycles

PRIOR TO EACH DEPARTURE EVAC DOOR PRESS DORR LIGHT ON L1 INOPERABLE. MEL 09OCT20 09:06 LAX U. RELEASED FOR SERVICE, PER MEL: 25-61-02 CATEGORY: C EXPIRATION: 19OCT20. MEL 25-61-02: L1 EVAC SLIDE REMOTE PRESS INDICATOR-INOPERABLE, PER MEL 25-61-02. VERIFY AND RECORD IN THE AML, EVACUATION SLIDE SYSTEM PRESS ADEQAUTE ONCE EACH FLIGHT DAY." C/7245004 FACT 11OCT20 17:45 MEM. REPOSITIONED PTT BUTTON OPERATIONS CHECKS GOOD. A/C OK FOR SERVICE.

Part: ENGINE — DAMAGED (NR 3) · airframe 82,647 hrs · 18,248 cycles

PDIS 593 72-51 3549 24AUG20 MEM OPEN U LOGPAGES:3355273 PASSING FL 310 FOR 340 ON INITIAL CLIMBOUT, AIRCRAFT SUDDENLY STARTED VIBRATING CONSIDERABLY #3 ENG EVM SHOWED AMBER BOX 5.0 BUT ALL OTHER INDICATIONS NORMAL. REDUCED POWER, VIBRATION INITALLY LESSONED , BUT CAME BACK FAIRLY INTENSELY, UPON BLOCKIN #3 TURBINE APPEARED SEVERELY DAMAGED. REPLACED #3 ENGINE

Part: SUPPORT — CORRODED (ZONE 700) · airframe 82,449 hrs · 18,190 cycles

RIGHT MLG A-FRAME ATTACH HOLES 4EA. AT PN ARB7118 ARE CORRODED. FABRICATED AND INSTALLED 4 EA. REPAIR BUSHINGS AFTER REAMED AND COLD WORK IAW SRM 57-20-14-2R.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 82,449 hrs · 18,190 cycles

MAIN CABIN: FLOOR PANEL DELAMINATED AT LBL 90, STATION 779-839. FABRICATED NEW FLOOR PANEL IN MAIN CABIN AT LBL 90, STATION 779-839 IAW DRAWING SRZ25-005.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK: FLOORBOARD SUPPORT ANGLE AT APPROX STA 435 (INBD OF L1 DOOR) APPROX LBL 74-88 IS CORRODED AND EXFOLIATED. REMOVED AND REPLACED FLOOR SUPPORT ABA8355-1 IN MAIN DECK APPROX STA 435 LBL74-88 REF DWG ABA8355 AND SRM 51-31-01-OG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK: FLOOR BOARD SUPPORT ANGLE AT APPROX STA 435 (INBD OF L1 DOOR) APPROX LBL 74-88 IS CORRODED AND EXFOLIATED (MARKED AND DOT 67). REMOVED AND REPLACED FLOOR SUPPORT ABA8355-1 REF DAC DWG SP11530074 AND SRM 51-31-01-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, STATION 549, RBL -47 FLOOR SUPPORT SHOWS CORROSION. REMOVED AND REPLACED SP11530074-10 FLOOR SUPPORT REF DAC DWG SP11530074 AND SRM 51-31-01-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, STATION 549, RBL -47 FLOOR SUPPORT SHOWS CORROSION. REMOVED AND REPLACED SP11530074-10 FLOOR SUPPORT REF DAC DWG SP11530074 AND SRM 51-31-01-OG. WORK ACCOMPLISHED ON NONROUTINE 1080.

Part: LONGERON SPLICE — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

WASTE TANK, STA 2000, LONGERON SPLICE LT 46 HAS SIGNS OF CORROSION, P/N AJC7675-1. REMOVED AND REPLACED LONGERON AT STA 2000 LT 46 REF SRM 51-33-01-0G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK STATION 421, RBL 27.5 HAS CORROSION. REMOVED AND REPLACED CORRODED SEAT TRACK AS REQUIRED IAW SRM 53-00-52-2R AND SRM 51-31-01-0G.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

COURIER AREA MCD OPENING DOOR JUST AFT FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED ABA8356-1 FLOOR SUPPORT REF DAC DWG ABA8359 AND SRM 51-31-01-OG

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK STA 450 RBL 13 FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED SP11530074-10 FLOOR SUPPORT REF DAC DWG SP11530074 AND SRM 51-31-01-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK STA 450 RBL -13 FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED SP11530074-10 FLOOR SUPPORT REF DAC DWG SP11530074 AND SRM 51-31-01-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK FLOOR SUPPORT STA 421 RBL 30 HAS CORROSION. REMOVED AND REPLACED SP11530074-3 SUPPORT REF DAC DWG SP11530074 AND SRM51-31-01-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK FLOOR SUPPORT AT STA 421 RBL 40 HAS CORROSION. REMOVED AND REPLACED SP11530074-3 SUPPORT REF DAC DWG SP11530074 AND SRM51-31-01-OG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO COMPARTMENT AT STA 1841 AT FLOOR LEVEL HAS CRACKED STIFFENER AT RBL 38. PERFORMED REPAIR TO STIFFENER AT STA 1841, FLOOR LEVEL AND RBL 38 REF SRM 53-00-00-2R SHEET 1 FIG 209.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, HOCKEY STICK (WSP0668-501 SUPPORT) AT STATION 422, RBL-22 SHOWS CORROSION. REMOVED AND REPLACED WSP0668-501 SUPPORT REF DAC DWG SP11530074 AND SRM51-31-01-OG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, STATION 410, RBL-13 FLOOR SUPPORT SHOWS CORROSION. REMOVED AND REPLACED SP11530074-5 SUPPORT REF DAC DWG SP11530074 AND SRM51-31-01-OG.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK LEFT HAND SIDE, FLOOR PANEL DAMAGED (STATION 755-795) LBL100. FABRICATED NEW FLOOR PANEL, MAIN DECK LEFT HAND SIDE STATION 755-795 LBL100 IN REF TO FEDEX DWG SRZ-25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK LEFT HAND SIDE, FLOOR PANEL DAMAGED (STATION 877-999) LBL-100. FABRICATED NEW FLOOR PANEL, MAIN DECK LEFT HAND SIDE STATION 877-999 LBL100 IN REF TO FEDEX DWG SRZ-25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK RIGHT HAND SIDE, FLOOR PANEL DAMAGED (STATION 845-899) RBL-100. FABRICATED NEW FLOOR PANEL, MAIN DECK RIGHT HAND SIDE STATION 845-899 RBL-100 IN REF TO FEDEX DWG SRZ-25-005. THIS N/R IS A DUPLICATE UNDER N/R 189.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, STATION 410, RBL-13 FLOOR SUPPORT SHOWS CORROSION. REMOVED AND REPLACED ABA8225-503 SUPPORT REF DAC DWG SP11530074 AND SRM51-31-01-OG.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK RIGHT HAND SIDE, FLOOR PANEL DAMAGED (STATION 795-845) RBL-100. FABRICATED NEW FLOOR PANEL, MAIN DECK RIGHT HAND SIDE STATION 795-845 RBL-100 IN REF TO SRZ-25-005,

Part: FLOORBOARD — DELAMINATED (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

L/H MAIN CARGO DECK STA 1039 X= 107.25 FOUND FLOOR BOARD AREA DELAM, RED MARK. FABRICATED NEW FLOOR PANEL, MAIN DECK LEFT HAND SIDE STATION 1039 LBL107 IN REF TO FEDEX DWG SRZ-25-005.

Part: COTTER PIN — MISSING (RUDDER TIE ROD) · airframe 82,449 hrs · 18,190 cycles

DURING C-11 CHECK WORKCARD 55C0204-02 FOUND ALL 4EA. LOWER AFT RUDDER TIE RODS MISSING SAFETY COTTER PINS AND NUTS WERE NOT TORQUED. GENERATED NON-ROUTINES N00829, N00830, N00831, N00832 GENERATED MSR REPORT. COMPLIED WITH N00829, N00830, N00831, N00832

Part: COTTER PIN — MISSING (RUDDER) · airframe 82,449 hrs · 18,190 cycles

DURING C-11 CHECK WORKCARD 55C0204-02 FOUND ALL 4EA. LOWER AFT RUDDER TIE RODS MISSING SAFETY COTTER PINS AND NUTS WERE NOT TORQUED. GENERATED NON-ROUTINES N00829, N00830, N00831, N00832

Part: FRAME — CRACKED (FLAP FAIRING) · airframe 82,449 hrs · 18,190 cycles

RIGHTWING OUTBOARD FLAP, INBOARD HINGE FWD FAIRING FRAME IS CRACKED IN HALF A AND HAS ELONGATED RIVET HOLES. MARKED #58. REMOVED AND REPLACED FAIRING FRAME ON RH WING, OB FLAP INBD HINGE PANEL #635 BR PER DAC BLUE PRINT ARCO504.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

CENTER WING LWR FUSELAGE BARREL STRUCT, CRACK ON ATTACH BRACKET AT STA 1278, RT CANTED PANEL. REPLACED CTR WING LWR FUSELAGE BARREL STRUCT, ATTACH BRACKET AT STA 1278 RT REF DAC DRAWING NR AYB7035 AND SRM 51-31-01-0G.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 82,449 hrs · 18,190 cycles

LEFT WING REAR SPAR UPPER CAP, AFT FLANGE UPPER SURFACE HAS CORROSION AT STA XORS 1041. REPAIRED PER EA 1-5710-T0354319 WINGS, BASIC WING STRUCTURE, LT WING REAR SPAR, UPPER CAP, CORROSION AT XORS1042.

Part: COUNTERWEIGHT — CORRODED (RUDDER) · airframe 82,449 hrs · 18,190 cycles

VERTICAL STABILIZER; UPPER RUDDER MID WEIGHT HAS CORROSION ON INTERNAL AFT SECTION. DOT #11 REMOVED AND REPLACED MID SPAN WEIGHT IAW E.A. 1-5540-T0355282 PART 1

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

CENTER CARGO COMPARTMENT, CORROSION ON FRAME, ON BOTTOM SIDE OF THE FLOOR SUPPORT, AT STA 1781 LBL 46 (MARKED NR 8). COMPLETED REPAIR ON FLOORBEAM STA 1781 LBL 46 PER EA 1-5300-T0354162. TITLE, FUSELAGE, GENERAL CORROSION ON FLOORBEAM STA 1781 UPPER CHORD TAB OUT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO AT APPROX STA 1842 FLOORBEAM ON TOP SECTION HAS MINOR SURAFCE CORROSION AT APPROX RBL 50 (MARKED). REMOVED AND REPLACED FLOORBEAM TOP SECTION ( ANGLE SUPPORT ) AT STA APPROX 1842 WITH A NEW PART REF SRM 51-31-01-0G AND DAC DRAWING AGA7170.

Part: LONGERON — CORRODED (BS 1956) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO AT APPROX STA 1956 RBL 45 LONGERON/STRINGER EXFOLIATED (MARKED) REPAIRED LONGERON AGA7038-501 PER EA # 1-5310-T0354242 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO AT APPROX STA 1841 RT SEAT TRACK FWD AREA HAS MINOR SURFACE CORROSION, MARKED. REPLACED SEAT TRACK AT AFT CARGO BETWEEN STA 1841 TO 1942 IAW DAC DRAWING NR AGA 3855 AND SRM 51-31-01-0G.

Part: SKIN — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO WASTE TANK AT APPROX STA 2000 & LBL 46 LWR INTERIOR SURFACE SKIN AREA EXFOLIATED. REPAIRED PER EA 1-5330-T0354479 TITLED: FUSELAGE - PLATES AND SKINS - AFT BODY KEEL PLANK P/N AJC 7164-503 - CORROSION BETWEEN BS 1997 AND BS 2005 AND BETWEEN L-44L AND L-45L.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 82,449 hrs · 18,190 cycles

VERTICAL STABILIZER, UPPER RUDDER MID WEIGHT HAS CORROSION ON INTERNAL AFT SECTION. REMOVED AND REPLACED MID SPAN WEIGHT, IAW EA 1-5540-T0355282 PART 1.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO AT APPROX STA 1956 & RBL 44 LONGERON SUPPORT BRACKET HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED LONGERON SUPPORT BRACKET USING FABRICATED PART REF DAC DRAWING NR NGA6713 AND SRM 51- 31-01-0G.

Part: SKIN — CORRODED (WASTE TANK) · airframe 82,449 hrs · 18,190 cycles

AFT CARGO WASTE TANK AT APPROX STA 2000 & LBL 46 LWR INTERIOR SURFACE SKIN AREA EXFOLIATED, MARKED.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,449 hrs · 18,190 cycles

LT LOWER WING AT ACCESS PANEL AT STA XORS 683.4 TO 713.6 EXISTING REPAIR INTERNAL DOUBLER HAS A .050 INCH CRACK AT HOLE 29 AND .150 IN. CRACK AT HOLE 30. REMOVED AND REPLACED DAMAGED INTERNAL DOUBLER IAW SRM 57-20-02-22 FIG 201 REPAIR 1 SHEET 1.

Part: SKIN — CRACKED (RT WING) · airframe 82,449 hrs · 18,190 cycles

RIGHT WING LEADING EDGE SLAT TRACK #2 CUT OUT HAS A CRACK MARKED #55 TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AT #3 SLAT RH WING LE PER SRM 57-40-02,FIG 202.

Part: FRAME — GOUGED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

FORWARD AVIONICS’ COMPARTMENT, APPROX STA 449, UNDER RAM AIR DUCTING FOR ACM NR 1 (REF BOOT), 1 SCREW NOT SEATED AND 1 SCREW HAS WORN INTO FRAME RADIUS AT FWD INBD POSITION. DAMAGE TRIMMED OUT AND FRAME REPAIRED. REF SRM53-00-07-2R REPAIR NR 2 FIG 201 SHEET 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, APPROX STA 775, X= 75.25, SEAT TRACK BLENDED BEYOND SRM LIMITS, MARKED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK AT STA 775,LBL 75. REF SRM CH 53-70-00, FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, APPROX STA 1531, X= 8.5, SEAT TRACK DAMAGED BEYOND SRM LIMITS. REPLACED DAMAGED SEAT TRACK AT STA. 1531 REF. SRM 53-00-52 R1

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK CARGO R/H SIDE RBL 107 AT APPROX STATION 775 FLOOR PANEL IS DAMAGED THROUGH TOP SURFACE MARKED IN RED. FABRICATED NEW FLOOR PANEL, MAIN DECK STATION 775 RBL-107 IN REF SRZ-25-005.

Part: FLOOR PANEL — WORN (ZONE 200) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK CARGO R/H SIDE RBL 107 AT APPROX STATION 879 FLOOR PANEL IS DAMAGED THROUGH TOP SURFACE MARKED IN RED. FABRICATED NEW FLOOR PANEL, MAIN DECK RIGHT HAND SIDE STATION 845-899 RBL-100 IN REF TO FEDEX DWG SRZ-25-005.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

MAIN DECK, APPROX STA 1271, X= 47.50, SEAT TRACK 7" SECTION HAS BLOWN LOBES AND DEEP GOUGES, MARKED. REPLACED DMAGED SECTION OF SEAT TRACK STA 1271,LBL 47.50. IAW SRM 53-00-52-2R.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 82,449 hrs · 18,190 cycles

CENTER CARGO PANEL 183CB NEEDS INSERTS. REPLACED FLOOR BOARD IAW REPAIR DRAWING SRZ-25-005.

Part: SKIN — CRACKED (RT WING) · airframe 82,449 hrs · 18,190 cycles

R/H LOWER WING SKIN AT #11 SLAT TRACK CUT OUT HAS A .800 IN. CRACK. (END MARKED) TRIMMED OUT CRACKED AREA AND INSTALLED FILLER AND DOUBLER, REFERENCE SRM 57-40- 02 REPAIR 7 FIG 201 SHEETS 1-2.

Part: SKIN — CORRODED (LT WING) · airframe 82,449 hrs · 18,190 cycles

LT WING UPPER SURFACE APPROX XORS 412 REAR SPAR - FILLER DELAMINATED. LEFT WING, UPPER REAR SPAR CAP CORROSION ON UPPER SURFACE BETWEEN XORS 410 AND XORS485; CORROSION REWORK PERFORMED IAW EA 1-5700-T0354331 PART 1 REV/PRINT DATE 02JULY2020. *NOTE: CLASSIFIED AS MINOR REPAIR*

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,449 hrs · 18,190 cycles

PACK #1 EXHAUST EXTERNAL FUSELAGE SKIN - UPPER AFT CORNER - CRACK EMANATING FROM FASTENER HOLE TO CUTOUT. CONFIRMED WITH NDT HFEC. REPAIRED / REMOVED CRACKED SKIN CONDITION. REF: MD-11 SRM 53-20-15-2R REPAIR #3 SHEET 1

Part: FILLER — CORRODED (RT WING) · airframe 82,449 hrs · 18,190 cycles

RT WING UPPER SURFACE APPROX XORS 412 REAR SPAR, FILLER DELAMINATED. CUT AND REMOVED CORRODED SECTION OF FILLER, BLENDED OUT CORROSION ON UPPER SUFACE OF SPAR CAP. FABRICATED AND INSTALLED NEW FILLER SECTION, REFERENCE EA 1-5710-T0354315 WINGS-BASIC WING STRUCTURE-RT WING UPPER SURFACE FILLER.

Part: DOUBLER — DAMAGED (ZONE 100) · airframe 82,449 hrs · 18,190 cycles

CENTER CARGO DOOR LEFT LOWER AFT CORNER PREVIOUS DOUBLER REPAIR DAMAGED. REPLACED DOUBLER PER SRM 53-00-15-2R REPAIR 8

Part: SKIN — CRACKED (LT WING SLAT) · airframe 81,514 hrs · 17,858 cycles

LH WING #8 SLAT CRACKED INNER SKIN COMPLIED WITH E.A. 1-5740-T0348640 "WINGS - ATTACH FITTINGS - CRACK DAMAGE TO INBD SIDE OF LH # 8 SLAT DOUBLER REPAIR"

Part: CONTACTOR — UNKNOWN (BATTERY SYS) · airframe 80,730 hrs · 17,614 cycles

ON CLIMB OUT, LEVEL 1 EMER PWR ON, FOLLOWED QRH, EMER PWR ON REMAINED DISPLAYED DEPLOYED ADG TO CONSERVE BATT DECLARED EMERGENCY, DUMPED FUEL AND LANDED. EPCU CURRENT FAULTS SHOWS " ADG BATT CTL RLY/INTFC" AND "ADG BAT CH EN RLY/INTFC". T/S PER FIM 24-20-00-1 FAULT NOT DUPLICATED, REMOVED AND REPLACED R2-17(L EMER CONT RELAY), R2-5156 (L EMER AC BUS SENSING RELAY), R2-5154 (L EMER DC SENSING RELAY), R2-34 (ADG/BATT CONT RELAY), R2-5411 (EMER PWR RELAY), R2-8927 (R EMER XFR RELAY) PER AMM 24-24-00-4. PERFORMED EMERGENCY PWR SYS TEST OK PER AMM 24-24-00-5 ALSO EPCU RTS PASSED AND EPCU/FCC CAT IIIB TEST PASSED. ALL ENG RAN TEST PER JRH CHAP 3/5, NO DEFECTS FOUND. A/C OK FOR SERVICE.

Part: RELAY — INOPERATIVE (GROUND SERVICE) · airframe 80,609 hrs · 17,586 cycles

EMER PWR ON ALERT ON T/O QRH COMPLIED WITH ; NO EFFECT. MFD'S 1-3 CONTINUALLY FLASHING. ADG DEPLOYED. SHGN 12MAR19 06:15 LAX PREFORMED EMERGENCY POWER TEST PER AMM 24-24-00-5. NO FAULTS FOUND. PREFORMED BATTERY CHARGER TEST PER AMM 24-34-03-5. NO FAULTS FOUND.PREFORMED BATTERY OFF INDICATION TEST PER AMM 24-34-00-5. NO FAULTS FOUND. PREFORMED DC BUS TIE RELAY SENSING TEST PER AMM 24-32-00-5. NO FAULTS FOUND. SHGN 12MAR19 06:40 LAX REPLACED EPCU PER MM 24-08-01-4, RTS TEST GOOD WITH NO FAULTS. REMOVED AND REPLACED THE GROUND SERVICE RELAY PER AMM 24-53-01-4 AMM: 24-53-01-5 RAN ENGINES AT IDLE , REMOVED GROUND POWER , APU POWER , RAN A/C ON ALL THREE ENGINE GENERATORS , NO FAULTS , ALL ENGINE GENERATORS PARALLELED CORRECTLY

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,112 hrs · 17,129 cycles

AT FL 350 IN LEVEL CRUISE .82M RECEIVED FLAP DISAGREE W/FLAPS AT 0 DEGREE/RET9 INDICATING 0 DEGREE/RET ON CONFIG PAGE. UPPER AND LOWER AIRSPEED FEET CAME TOGETHER ON CA SIDE. AP1 WAS ENGAGED. FO SIDE SHOWED NORMAL. THIS OCCURRED SEVERAL TIMES INTERMITTENTLY AND QUICKLY ENOUGH TO NOT BE ABLE TO DETERMINE PROPER SIDE FOR ACCURACY. DECLARED EMERGENCY AND RETURNED TO HNL. INTERROGATED CFDS, FCC NR 1 SHOWS NO CURRENT FAULTS OR PREVIOUS LEG FAULTS. PERFORMED ADJUSTMENT/TEST OF NR 1 CADC REF AMM 34-16-01-4, ALL TESTS PASS. CONSULTED WITH MOCC. PRECAUTIONARY REMOVED AND REPLACED NR 1 CADC REF AMM 34-16-01-4. PERFORMED ADJUSTMENT/TEST ON NR 1 CADC AND PERFORMED AUTOLAND TEST REF AMM 34-16-01-5, ALL TESTS PASS. NO 90-DAY HISTORY. A/C OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,112 hrs · 17,129 cycles

TSI ISSUED FOR MX TO COMPLY WITH FOR FLAP DISAGREE. PERFORMED FLAP POSITION INDICATION SYSTEM ADJUSTMENT TEST REF AMM 27-54-00-5. NO FAULTS FOUND. ALL READINGS WITHIN TOLERANCE. VISUALLY INSPECTED LINKAGE, HARDWARE, WIRE HARNESSES AND CONNECTORS OF EACH INBOARD, OUTBOARD, AND FLAP POSITION TRANSMITTERS. NO DEFECTS NOTED. UNABLE TO ACCOMPLISH FIM 27-50-06 DUE TO NO FAULTS FOUND. REMOVED AND REPLACED NR 2 FCC REF AMM 22-01-03-4, ALL TESTS PASS. PERFORMED AFS TEST REF AMM 22-00-00-5, ALL TESTS PASS. A/C OK FOR SERVICE.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 78,357 hrs · 16,903 cycles

LEVEL ONE EMER POWER ON ALERT 4 HOURS INTO FLIGHT LEVEL CRUISE. REPLACED RELAY R2-5411 PER FIM 24-24-01-00. NO FAULTS NOTED. A/C OK FOR SVC.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK LT FUSELAGE FRAME AT STA 535 L-19L FOUND EXISTING REPAIR DOUBLER CHAFED AS MARKED. REPAIRED AS PER EA 1-5310-138491 B PART 3 TITLE: FUSELAGE - MAIN FRAME - FRAME DAMAGE AT STA 535, BETWEEN L-19L AND L-23L - EXISTING REPAIR. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK LT FUSELAGE FRAME AT STA 535 L-24L FOUND EXISTING REPAIR DOUBLER CHAFED AS MARKED. REPAIRED AS PER EA 1-5310-138491B PART 3 TITLE: FUSELAGE - MAIN FRAME - FRAME DAMAGE AT STA 535, BETWEEN L-19L AND L-23L - EXISTING REPAIR. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 982) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 982, LBL 27.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,847 hrs · 16,753 cycles

LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 732 FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 732 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: BEAM — CRACKED (R3 DOOR) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK R3 DOOR MOST LOWER DOOR BEAM AT FWD STOPPER AREA FOUND CRACKED, AT STA 1262. MAIN DECK R3 DOOR STA1262 CRACKED MOST LOWER DOOR BEAM REMOVED AND REPLACED PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,847 hrs · 16,753 cycles

LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 740 FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 740 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CHAFED (LT WING SLAT) · airframe 77,847 hrs · 16,753 cycles

LEFT WING DROOP LEADING EDGE SLAT OUTBOARD UPPER SURFACE CHAFED XDLE 309. REPAIRED IAW SRM 57-40-01-2R, FIGURE 202, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 5-83, RBL 8.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR NR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1581) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1581 RBL 8.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPLACED BS 1631 TO 1531 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR NR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1793) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1793, RBL 47.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1411) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1411, RBL 8.5 FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. AND THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52- 2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

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

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 47.5, CROWN DAMAGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1641) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1641, LBL 27.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1641) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1641, LBL 8.5 FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR NR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1611) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1611, RBL 8.5 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 1631 TO BS 1531 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR NR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 27.5 CROWN DAMAGED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1711) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1711, LBL 8.5 FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR NR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1831) · corrosion level 2 · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 1831, RBL 8.5 FOUND CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR NR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 77,847 hrs · 16,753 cycles

MAIN DECK SEAT TRACK AT BS 635, LBL 47.5 FOUND CRACKED. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW O2) · airframe 77,684 hrs · 16,694 cycles

LOST ALL OXYGEN SYSTEM PRESSURE IN ALL '3' SYSTEMS AT FL 350. AT A/C BLOCK-IN FOUND ALL O2 BOTTLES READING APPROX 100 PSI. SERVICED ALL O2 BOTTLES PER MM 12-15-01-3. PERFORMED LEAK TEST PER AMM 35-11-01-5. NO LEAKS NOTED. RECHECKED O2 QUANTIY AFTER 30 MN AND O2 QTY HAD NOT DECREASED. A/C OK FOR SERVICE.

Part: SENSOR — MALFUNCTIONED (LE SLAT) · airframe 76,950 hrs · 16,467 cycles

DEPARTED AND SLAT DISAG ALERT DISPLAYED AFTER SELECTING UP/RET RAN QRH, DUMPED FUEL, RETURNED, REMOVED AND REPLACED BOTH PROX SENSORS ON LT WING AND ALSO REPLACED PSEU. ALL TESTS PASS. AIRCRAFT OK FOR SERVICE.

Part: COVER — OUT OF ADJUST (L1 DOOR) · airframe 75,992 hrs · 16,163 cycles

DOORS 1L AND 1R ESCAPE SLIDE DOOR OUT OF PLACE. RE ADJUSTED BOTH SLIDE COVER PLATES, PER SMP.

Part: SOLENOID — MALFUNCTIONED (L1 DOOR) · airframe 74,877 hrs · 15,782 cycles

L1 DOOR DOES NOT OPEN ELECTRICALLY USING EITHER INTERIOR OR EXTERIOR SWITCH. R & R THE L1 DOOR LOCK PIN RELEASE SOLENOID IAW MM 52-10-06-4. OPERATED DOOR SEVERAL TIMES FROM IN/OUTSIDE,ALL CHKD OK.

Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 74,835 hrs · 15,767 cycles

LEFT FORWARD ENTRY DOOR ELECTRIC SWITCH DID NOT OPEN DOOR INITTALLY. CYCLED ARM LEVER A FEW TIMES AND THE DOOR OPENED. REPLACED THE L1 DOOR CONTROL POWER SWITCH S1-1090. IAW SCHEMATIC MANUAL 52-11-0. THE DOOR OPS CHECKED NORMAL.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 74,570 hrs · 15,671 cycles

L1 SLIDE WILL NOT ARM. FOUND GIRT BAR OUT OF ADJUSTMENT ON L1 DOOR...ADJUSTED IAW 52-10-01-2. OPS CHECK NORMAL. ACFT OK TO CONTINUE SERVICE.

Part: TEST SWITCH — DEFECTIVE (EVAC SLIDE) · airframe 74,483 hrs · 15,639 cycles

LEFT CREW DOOR SLIDE INFLATION CYLINDER LOW PRESSURE, LIGHT IS ILLUMINATED. CHECKED SLIDE PRESSURE, REF METHOD B, PRESSURE ON GAUGE IN GREEN BAND. CHECKED SLIDE INFLATION PRESS GAUGE AND FOUND SLIDE ASSY PRESSURE BOTTLE IN GREEN BAND. WHILE CYCLING PTT SWITCH SEVERAL TIMES , FOUND IT WOULD RANDOMLY FLICKER. R&R LIGHT SWITCH PER AMM. OPS CHECKED SWITCH PER TASK 25-61-04-710-801,OPS CHECK GOOD. NO DEFECTS AT THIS TIME.

Part: SWITCH — INTERMITTENT (EVAC SLIDE) · airframe 74,483 hrs · 15,639 cycles

LEFT CREW DOOR SLIDE INFLATION CYLINDER LOW PRESSURE LIGHT IS ILLUMINATED. CHECKED SLIDE INFLATION PRESSURE GAUGE AND FOUND SLIDE ASSY PRESSURE BOTTLE IN GREEN BAND, WHILE CYCLING PTT SWITCH SEVERAL TIMES FOUND IT WOULD RANDOMLY FLICKER. R&R LIGHT SWITCH IAW AMM SMP, OPS CHECKED SWITCH IAW TASK 25-61-04-710-801, OPS CHECK GOOD, NO DEFECTS AT THIS TIME.

Part: BRAKE — FAILED (MLG) · airframe 74,216 hrs · 15,561 cycles

DURING NR 10 TIRE CHANGE, FOUND BRAKE DISKS ARE COMING APART. PREMATURE REMOVAL/INSTALLATION, OFF MPN: 2609472-4, POS: 10, SRL B1471, TAG NR: 1540E0 ON MPN: 2609472-4B, CPN: 3200378, SRL B2599. R & R BRAKE ASSY, REF AMM 32-43-20-4, LEAK AND PRESSURE CHECK GOOD AND ACFT IS OK FOR SERVICE.

Part: FIRE LOOP — FAULTED (NR 3 NACELLE) · airframe 74,189 hrs · 15,550 cycles

PASSING 11,000 FT ON DESCENT, RECEIVED A MOMENTARY FIRE INDICATION ON NR 3 ENGINE LASTED 2 SECONDS AND WENT AWAY. NO OTHER INDICATIONS LEFT ENGINE AT IDLE AND LANDED WITHOUT SHUTTING IT DOWN. PERFORMED FDCU-3 FAULT REVIEW, LOOP B FAULTED, UPPER RIGHT FIRE DETECTOR ASSY A AND LOOP A FAULTED. RETURNED TO SERVICE.

Part: WIRE HARNESS — CHAFED (TAXI LIGHT) · airframe 73,779 hrs · 15,404 cycles

AFTER LANDING TAXI LIGHTS INOPERATIVE. FOUND CB FOR NOSE LANDING TAXI LIGHT LT & RT POPPED. RESET NO HELP. CB POPPED AS SOON AS NOSE TAXI SWITCH TURNED ON. FOUND WIRING HARNESS FOR NOSE TAXI LIGHTS CHAFED THROUGH NEAR UPPER NWS BYPASS ASSEMBLY. NOSE GEAR LT & RT LANDING LIGHT DEFERRED IAW MEL 33-41-01-01-A & DEACTIVATED IAW EA 1-3340-T0325098 A. REPLACED NOSE GEAR LANDING & TAXI LIGHT HARNESS IAW ADM 33-42-01. INSTALLED NEW BULB IAW AMM 33-42-01-2 OPERATIONS CHECKED GOOD IAW WRI'S 33-40 7931, 33-40 8021 & REACTIVATION WRI 33-40 7930 & EA 1-3340-T0325098B P2. PLEASE REFER TO WRI 593 33-40 7931.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 73,302 hrs · 15,243 cycles

AGEING ACFT, EXISTING SKIN REPAIR FOUND ON CTR CARGO DOOR FWD LOWER CORNER. EXISTING SKIN REPAIR EVALUATED & FOUND EXISTING REPAIR DOUBLER CRACKED. CARRIED OUT REPAIR IAW EA 1-5230-T0323286 P1. ACCOMPLISHED REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. REFER WRI 52307661.

Part: DOOR FRAME — DENTED (CARGO DOOR) · airframe 73,302 hrs · 15,243 cycles

FORWARD CARGO DOOR, AFT FRAME FOUND WITH DENT MARK AT STATION 999.5, 25" FROM DOOR LOWER EDGE. REPAIRED IAW EA 1-5230-T0323398 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (NLG TRUNNION) · airframe 73,302 hrs · 15,243 cycles

LEFT NLG TRUNNION FITTING FOUND APPROX 0.25 INCH LENGTH CRACK BS 582. FROM THE PREVIOUSLY SLOT OUT AREA. REPAIRED IAW SRM 53-10-14-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,302 hrs · 15,243 cycles

AGEING ACFT, EXISTING FUSELAGE FRAME REPAIR AT MAIN DECK CARGO, STATION 535 AT LONGERON 19L. EXISTING FUSELAGE FRAME REPAIR EVALUATED & FOUND DAMAGED. CARRIED OUT REPAIR IAW EA 1-5310-138491A P 2. DAMAGE AT STATION 535, BETWEEN LONGERON 19L & L 23, EXISTING REPAIR EO 1-5100-7-5001 B6 PT 1 REPAIR ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,302 hrs · 15,243 cycles

AGEING ACFT, EXISTING FUSELAGE FRAME REPAIR AT MAIN DECK CARGO STATION 535 AT LONGERON -23L. EXISTING FUSELAGE FRAME REPAIR EVALUATED & FOUND DAMAGED. FUSELAGE CARRIED OUT REPAIR IAW EA 1-5310-138491A P 2. MAIN FUSELAGE FRAME DAMAGE AT STATION 535, BETWEEN LONGERON -19L & -23L, EXISTING REPAIR EO 1-5100-7-5001 B6 PT 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — GOUGED (BS 535) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO COMPARTMENT, FRAME FOUND GOUGED AT BS 535, LONGERON 24R. REPAIRED IAW SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — GOUGED (BS 535) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO COMPARTMENT, FRAME FOUND WITH GOUGED AT BS 535, LONGERON 19R. REPAIRED IAW SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CHAFED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE TELESCOPIC DUCT DOOR XOS 464, INBD CUT OUT FOUND CHAFING. CAP REMOVED IAW SRM 51-31-01-0G & FABRICATED A NEW CAP IAW DWG ARB1284 REV AC. INSTALLED NEW CAP IAW SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY XOS 794, FORMER FOUND CRACKED. REPAIRED IAW DWG ARB3954 REV K, AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

DURING HFEC INSPECTION , TWO EACH CRACKS FOUND PROPAGATE FROM THE FWD INBD CORNER OF RT SLAT ACTUATOR. REPAIRED IAW SRM 57-40-01-2R FIG 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PANEL SUPPORT — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY XOS 542, PANEL SUPPORT FOUND CRACKED. REPAIRED IAW SRM 51-33-01-0G, DWG ARB 2933 REV T, AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY, XOS 632, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: ANGLE — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 584, FORMER ANGLE FOUND CRACKED. FORMER ANGLE REPLACED IAW SRM 51-31-01-0G, DWG ARB2931 REV H, AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY, XOS 642, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. A NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, INBD FWD HINGE WING SIDE, PIVOT HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-44-08. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323078 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA 1-5750-67542B P4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING, NR 15 SLAT TRACK CUT OUT, XOS 944, CRACKED. REPAIRED IAW SRM 57-40-02-2R REPAIR 7 FIG 201. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE NR 16, SLAT TRACK CUT OUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7 & EA 1-5730-T0323140 P 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 73,302 hrs · 15,243 cycles

CABIN, X-RAY ON TRANSVERSE SKIN SPLICE, STATION 5 - 123, FOUND LONGERON 6R CTR SPLICE FWD, BETWEEN 1 & 2 FASTENER CRACKED. LONGERON SPLICE R & R IAW SRM 51-33-01-0G. NEW LONGERON SPLICE FABRICATED IAW DWG A5A7112 REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO COMPARTMENT, SEAT TRACK FLANGE CORRODED AT RT STATION 5 - 61, X= -27.5. REPAIRED THE SEAT TRACK 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 73,302 hrs · 15,243 cycles

RIGHT WING, LE NR 15 SLAT TRACK DOOR CUT OUT XOS 947 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY, XOS 542, FORMER FOUND CRACKED. REMOVED, FABRICATED AND INSTALLED NEW FORMER IAW SRM 51-31-01-0G, DWG ARB 2918 REV G, AND SRM 51-33-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1781) · airframe 73,302 hrs · 15,243 cycles

MAIN DECK CARGO TRACK CORRODED, BS 1781, RBL 8.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, INBD FWD HINGE WING SIDE, LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-44-08. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323078 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323026 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1310) · airframe 73,302 hrs · 15,243 cycles

MAIN DECK CARGO TRACK FLANGE CORRODED BS 1310, RBL 75.25. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY, XOS 800, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY, XOS 622, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

LEFT WING INBD FLAP, OTBD AFT HINGE FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. REPAIR ACCOMPLISHED IAW EA 1-5750-67542B P4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING OTBD FLAP, INBD FWD HINGE WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-44-08. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0323078 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1721) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO BAY, CARGO TRACK CORRODED, BS 1721, RBL 8.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

LEFT WING OTBD FLAP, OTBD AFT HINGE FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. REWORKED & FOUND EXCEEDS LIMITS IAW CMM 57-52-04. REPAIR ACCOMPLISHED IAW EA 1-5750-T0323080 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 73,302 hrs · 15,243 cycles

RIGHT WING LE CAVITY, XOS 794, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 873, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, STATION XOS 636, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 674, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 590, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 920, FORMER FOUND CRACKED. REPAIRED IAW SRM 51-31-01-0G, DWG ARB 1164 REV M, AND SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 600, STRINGER FOUND CRACKED. REPAIRED IAW SRM 57-40-03-2R REPAIR 2 FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 901, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40- 02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 604, FWD PANEL SUPPORT DOUBLER, FOUND CRACKED. REPAIRED IAW SRM 51-31-01-0G, DWG ARB 2933 REV, AND SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 654, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 755, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, STATION XOS 624, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 73,302 hrs · 15,243 cycles

LEFT WING LE CAVITY, XOS 664, BEADED DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1279) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO COMPARTMENT, SEAT TRACK CORRODED, AT LT BS 1279, X=8.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1746) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO COMPARTMENT, SEAT TRACK CORRODED, AT RT BS 1746, X= -8.5. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR OTBD HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0322999 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1721) · airframe 73,302 hrs · 15,243 cycles

CABIN MAIN DECK CARGO COMPARTMENT, FRAME WITH DENTED AT RT BS 1721, LONGERON 12R. REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0322999 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 73,302 hrs · 15,243 cycles

LEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUTS HOLE BORE CORRODED. FOUND OUT OF LIMIT IAW CMM 57-44-09. NEW BUSHING FABRICATED & INSTALLED IAW EA 1-5750-T0322999 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 718 hrs · 14,751 cycles

DURING PREFLIGHT CHECK FOUND EMER L1 BAT LO ALERT. R & R EMER EXIT LIGHT POWER SUPPLY. PERFORMED SYS FUNCTIONAL TEST. CHECKED GOOD IAW MM 33-51-01-4.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 714 hrs · 14,605 cycles

DURING PREFLIGHT, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY LOW ALERT. R/R'D EMERGENCY LIGHTS BATTERY POWER SUPPLY IAW MM 33-51-01-4. OPS CHECKED GOOD. OK TO CONTINUE.

Part: SKIN — CRACKED (LT WING) · airframe 68,970 hrs · 13,877 cycles

WHILE ACCOMPLISHING FEA 1-5710-F0308148 FOUND POSSIBLE CRACK ON CORNER OF LT WING REFUEL DOOR PNL 519CB. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. CUT OUT DAMAGE IAW SRM 57-40-02 REPAIR 7, FIG 202. PERFORMED HFEC INSPECTION IAW NTM CHAPTER 20-00-00 PART 6, NO DEFECTS NOTED. FABRICATED & INSTALLED DOUBLER & FILLER IAW SRM 57-40-02 REPAIR 7 FIG 202. NEED COUNTERSINK & PRIMED.

Part: SKIN — CRACKED (LT WING) · airframe 68,966 hrs · 13,875 cycles

WHILE ACCOMPLISHING FEA1-5710-F0308148 FOUND POSSIBLE CRACK ON NR 13 LT WING SLAT TRACK CUT OUT. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. THIS IS AT SLAT TRACK 14 CUT OUT NOT AT 13. NO CRACK AT SLAT TRACK 13 FOUND. REMOVED DAMAGED AREA IAW SRM 57-40-01. COMPLIED WITH HFEC OF THE CUT OUT AREA IAW NDT SMP PT6 NO DAMAGE FOUND IN AREA. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 57-40-02 REPAIR 7.

Part: SKIN — CRACKED (ZONE 600) · airframe 68,966 hrs · 13,875 cycles

RIGHT WING NR 16 SLAT TRACK CUT OUT HAS POSSIBLE CRACK ON LE SKIN. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. VERIFIED CRACK. CUT OUT DAMAGE IAW ERS 14-03138. PERFORMED HFEC INSPECTION OF DAMAGE REMOVAL IAW NTM 20-00-00 PART 6, NO DEFECTS NOTED. REPAIR DOUBLER AND FILLER INSTALLED IAW SRM 57-40-02.

Part: SKIN — CRACKED (ZONE 600) · airframe 68,966 hrs · 13,875 cycles

RIGHT WING PRESSURE REFUEL PANEL 619CB CRACKED. FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. REPAIRED IAW EA 1-5730-T0308294.

Part: SKIN — CRACKED (LT WING LE) · airframe 68,966 hrs · 13,875 cycles

LT WING LE SKIN FWD OF OTBD SIDE OF SLAT DRIVE MECHANISM PANEL FOUND TO BE CRACKED. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F03081 48. CONFIRMED CRACK DURING HFEC INSPECTION IAW NDTSPM PT 6. CRACK EXTENDS FROM CORNER OF CUT OUT TO 1/4 INCH PAST FASTENER. TRIMMED OUT CRACK IAW SRM 57-40-02 FIG 202 REPAIR 7. COMPLY WITH HFEC OF CUT OUT AREA IAW NDTSPM PART 6, 06-00-06. NO INDICATIONS NOTED. FABRICATED DOUBLER & FILLER, TREATED & PRIMED PARTS IAW SRM 57-40-02 FIG 202 REPAIR 7.

Part: SKIN — CRACKED (RT WING) · airframe 68,966 hrs · 13,875 cycles

RIGHT WING NR 10 SLAT TRACK CUT OUT HAS POSSIBLE CRACK ON LE OF WING. CRACK FOUND WHILE ACCOMPLISHING FEA 1-5710-F0308148. VERIFIED CRACK, MARKED END OF CRACK. HFEC IAW NDTSPM PART 6,06-00-06. CUT OUT DAMAGED AREA IAW SRM 57-40-02 REPAIR 7. COMPLIED WITH HFEC IAW NDT STM PT 6 ALL DAMAGED AREA REMOVED. FABRICATED DOUBLER & FILLER IAW SRM 57-40-02 FIG 201 REPAIR 7. INSTALLED DOUBLER IAW SRM 57-40-02 REPAIR 7.

Part: SKIN — CRACKED (LT WING) · airframe 68,332 hrs · 13,685 cycles

LOWER WING SKIN FOUND TO HAVE CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. ACCESS DOOR CUTOUT BETWEEN XORS 683.4 & XORS 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CRACKED (BS 1310) · airframe 68,332 hrs · 13,685 cycles

L3 DOOR AFT FRAME LOWER CUTOUT FOUND CRACKED. BS 1310 CRACKED AREA REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: CARGO TRACK — CORRODED (BS 1219-1239) · corrosion level 2 · airframe 68,332 hrs · 13,685 cycles

MAIN DECK CARGO TRACK FLANGE AT BS 1219 TO 1239, X -75.25 FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CRACKED (BS 1310) · airframe 68,332 hrs · 13,685 cycles

R3 DOOR AFT FRAME LOWER CUTOUT FOUND CRACKED. BS 1310 CRACKED AREA REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CRACKED (BS 1253) · airframe 68,332 hrs · 13,685 cycles

R3 DOOR FWD FRAME LOWER CUTOUT FOUND CRACKED. BS 1253 CRACKED AREA REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CORRODED (BS 2154) · corrosion level 2 · airframe 68,332 hrs · 13,685 cycles

FUSELAGE EXTERIOR APPROXIMATELY BS 2154 RT FOUND SURFACE CORROSION BETWEEN LONGERONS 33 & 35 RT. DAMAGED AREA REPAIRED IAW SRM 53-70-01 REPAIR 3 FIGURE 201 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.

Part: SKIN — CRACKED (BS 1253) · airframe 68,332 hrs · 13,685 cycles

CABIN L3 DOOR FWD FRAME LOWER CUTOUT FOUND CRACKED. CUTOUT CRACKED AREA AT BS 1253 REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.

Part: ECU — FAULTY (NR 3 ENGINE) · airframe 68,287 hrs · 13,671 cycles

AT TOP OF DESCENT ENG 3 FADEC FAULT LEVEL ONE ALERT & ENG 3 FLAMED OUT. RAN CHECKLISTS & RELIT ENG 3. CONTINUE ARRIVAL WITH ALL ENGINES OPERATING, LT IGNITER IN OVERRIDE WITH A & B SELECTED. ENG 3 FADEC FAULT REMAINED ON UNTIL ENG SHUT DOWN NORMALLY ON GROUND. HAD NR 3 ENG FADEC FAULT CODES ON CHANNEL B OF NR 3. R & R NR 3 ECU IAW AMM 73-21-02-04-1. ALL REQUIRED CHECKS WERE GOOD. ACFT OK FOR SERVICE. ACCOMPLISHED HIGH POWER RUN UP PER JRH. BLEEDS OFF ENG PARAMETERS ARE NORMAL.

Part: HMU — INOPERATIVE (NR 1 ENGINE) · airframe 66,480 hrs · 13,103 cycles

ON TAKEOFF WITH MAX POWER SET, NR1 ENGINE NEVER ACHIEVED MAX POWER OF 108.0 PERCENT N1 RPM. NR 2 & NR 3 ENGINE WERE AT 108.0 N1. REJECTED TAKEOFF AT 80 KTS. R & R NR 1 HMU IAW MM 73-21-01-4-1.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,278 hrs · 12,499 cycles

EMERGENCY LIGHT BATTERY 1 LOW. REMOVED & REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT, OPS CHECKED OK PER AMM33-51-01.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,410 hrs · 12,279 cycles

ON REMOVAL OF FLOOR PANEL, MAIN DECK CARGO TRACK FLANGE BETWEEN STA 5-30 AND STA 5-56 X= -77 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. CARGO TRACK REWORKED IAW DWG AFA7740, REV M. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,410 hrs · 12,279 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 281JF AND 291BF SEAT TRACK FLANGE STATION 1665 X= 74 CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REVISION 49. SEAT TRACK REWORKED AS PER DRAWING AFA7740 REVISION M. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 63,410 hrs · 12,279 cycles

CENTER CARGO - DOOR CUT-OUT UPPER DOOR FRAME AROUND ACTUATOR LINK ARM FITTING FOUND CRACKED. REPAIRED IAW EA 1-5310-159832. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 63,410 hrs · 12,279 cycles

ON REMOVAL OF FLOOR PANEL 282GF MAIN DECK CARGO TRACK FLANGE AT BS 1601 X= -77 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REV 49. SEAT TRACK REWORKED IAW DWG AFA7740, REVISION M. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: CARGO TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,410 hrs · 12,279 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANEL 291BF CARGO TRACK FLANGE BETWEEN BS 1775 AND BS 1781 X=102 CORRODED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 5 REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,410 hrs · 12,279 cycles

MAIN DECK CARGO, ON REMOVAL OF FLOOR PANELS 281HF AND 281GF, SEAT TRACK FLANGE BETWEEN BS 1531 AND 1660 X= 75 FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REVISION 49 AND DRAWING AFA7740 REVISION M. REPAIR CLASSIFIED MAJOR AS PER FEDEX GMM 6-2-100 REVISION 114.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,410 hrs · 12,279 cycles

MAIN DECK CARGO TRACK AT BS 1581 X= -8.5 (LT) FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REVISION 49. SEAT TRACK REWORKED IAW DRAWING AFA7792 REVISION C. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 63,410 hrs · 12,279 cycles

RIGHT WING SLAT TRACK NR 12 LOWER CUT OUT CRACKED.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 63,410 hrs · 12,279 cycles

LEFT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R IAW AMM 27-50-22-4, REV 72.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV 72.0. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 600) · airframe 63,410 hrs · 12,279 cycles

NINE FASTENER HOLES FOUND CRACKED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= -683.4 AND STATION XORS= -713.6.

Part: INTERCOSTAL — CRACKED (NR 2 INTAKE) · airframe 63,410 hrs · 12,279 cycles

RT NR 2 ENGINE INTAKE DUCT PANEL NR 364RR ON WIRE CUT-OUT INTERCOSTAL FOUND CRACKED. REPAIRED IAW SRM 55-30-02, FIG 201, REV 49, REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.

Part: SKIN — CRACKED (ZONE 500) · airframe 63,410 hrs · 12,279 cycles

SEVEN FASTENER HOLES FOUND CRACKED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. REPAIRED IAW EA 1-5710-159826 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.

Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR AT LT WING OTBD FLAP INBD HINGE LOWER PIVOT BORE HOLES. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW EA 1-5750-67544 TITLE: WINGS- OTBD T/E FLAPS- LT FLAP - REPAIR OF INBD AND OTBD HINGE. EO 1-5100-7-5001, A4 PART I TITLE: REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

CRACK (4") - LONGERON SPLICE BETWEEN 5-113 TO STA1541 LONGERON 16L MAIN DECK CARGO INTERIOR. MAIN DECK CARGO INTERIOR INTERIOR BETWEEN 5-113 AND STA 1541, LONGERON 16L, CRACKED LONGERON SPLICE R & R IAW SRM 51-33-01 REV 43. NEW LONGERON SPLICE FABRICATED IAW DWG A5A7112 REV D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (RWS 690-700) · airframe 58,016 hrs · 10,979 cycles

CRACK FASTENER HOLE (07 EACH) FOUND BETWEEN XORS 690 TO XORS 700 AT RT WING LOWER SKIN ACCESS DOOR CUTOUT. REPAIR CARRIED OUT IAW EA 5710-140304. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — CRACKED (LT WING) · airframe 58,016 hrs · 10,979 cycles

CRACK FASTENER HOLE (09 EACH) FOUND BETWEEN XORS690 TO XORS700 AT LT WING LOWER SKIN ACCESS DOOR CUTOUT. REPAIR CARRIED-OUT IAW EA 1-5710-140305. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR - LT WING DROOP L/E UPPER SKIN. EXISTING REPAIR AT LT WING DROOP L/E UPPER SKIN FOUND NOT IAW SRM REPAIR. REPAIR AT LT WING DROOP L/E UPPER SKIN CARRIED OUT REPAIR IAW EA 1-5750-138495: REPAIR CLASSIFIED AS MINOR AS GMM 6-2-100, REV 110.

Part: STRUCTURE — MISREPAIRED (ZONE 200) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR - AFT BULKHEAD CHORD, STA 2007, X = -53, FLOOR LEVEL AT MAIN DECK CARGO INTERIOR. EXISTING REPAIR AT BULKHEAD AFT STA 2007 FLOOR LEVEL X= -53 BULKHEAD FOUND REPAIR NOT IAW SRM REPAIR. MAIN DECK INTERIOR AFT BULKHEAD STA 2007 FLOOR LEVEL X= -53 BULKHEAD CHORD CARRIED OUT REPAIR IAW SRM 53-70-08 FIG 201 REPAIR 4 REV 43. EO 1-5100-7-5001 A4 PART I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-110 REV 110.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

CRACKED (APPROX 2 INCH) - SEAT TRACK STA635, X = -8 AT MAIN DECK. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 635 TO STA 665 X= -8 IAW SRM 53-00-52 FIG. 201 REPAIR 1 REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 110.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR DOUBLER FOUND AT RT FUSELAGE SKIN STA 675 LONGERON 50 RT. EXISTING REPAIR DOUBLER AT RT FUSELAGE SKIN STA 675 LONGERON 50 RT, EVALUATED AND FOUND DOES NOT CORRELATE WITH ANY SRM. EXISTING REPAIR DOUBLER R & R IAW SRM 53-00-01, FIG 201, REPAIR 8, REV 43. DUE TO CATEGORY 'B' REPAIR, HFEC METHOD RE-INSP REQUIRED, INITIAL INSP AT 7,500 FLIGHT CYCLES AND REPETITIVE INSP AT 4,750 FLIGHT CYCLES INTERVAL EO 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

CRACKED (APPROX 3 INCH) - SEAT TRACK STA635, X =27.5 AT MAIN DECK CARGO FLOOR. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665 X= 27.5 IAW SRM 53-00-52, FIG 201 REPAIR 1, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 58,016 hrs · 10,979 cycles

CRACK (1") - SEAT TRACK STA 695 X=8 AT MAIN DECK. SEAT TRACK TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 665 TO STA 745 X= 8 IAW SRM 53-00-52 FIG 201, REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.

Part: SKIN — DAMAGED (BS 960-994) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR - STA 960 TO STA 994 APPROX 30 INCH FROM LOWER OF FWD CARGO DOOR EXTERIOR. EXISTING REPAIR ON LOWER FWD CARGO DOOR EXTERNAL SKIN STA 960 TO STA 994. REMOVED AND ACCOMPLISHED IAW EA 1-5230-138490, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CHAFED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR DOUBLER FOUND AT APPROX STA 999 LONGERON 40 RT AT FWD CARGO DOOR JAMB LOWER AFT. EXISTING REPAIR DOUBLER AT STA 999 LONGERON 40 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53-00-15, FIG 202 REPAIR 8, REVISION 43. CHAFED DOUBLER ON STA 999 LONGERON 40 RT REPAIRED SRM 53-00-15, FIG 202, REPAIR 8, REVISION 43. REPETITIVE INSP REQUIRED IAW AIRWORTHINESS LIMITATIONS INSTRUCTIONS PSE NR 53.10.06. INITIAL INSP 12,600 FLIGHT CYCLE AND REPEAT INSP: 6,300 FLIGHT CYCLE. EO 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED, MAJOR IAW GMM 6-2-100, REV 110.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR (2 EACH) FOUND AT MAIN DECK FRAME STA 535 BETWEEN LONGERON 20 LT AND LONGERON 26 LT. EXISTING REPAIR (2 EACH) AT MAIN DECK FRAME STA 535 BETWEEN LONGERON 20 LT AND LONGERON 26 LT EVALUATED AND FOUND NOT IAW SRM. STA 535 MAIN DECK FRAME BETWEEN LONGERON 20 LT AND LONGERON 26 LT REPAIRED IAW EA 1-5310-138491, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SKIN — CHAFED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR DOUBLER FOUND AT STA 2140, LONGERON 41 LT FUSELAGE SKIN. EXISTING REPAIR DOUBLER AT STA 2140 LONGERON 41 LT, FUSELAGE SKIN EVALUATED AND FOUND DOES NOT CORRELATE WITH ANY SRM. EXISTING REPAIR REACCOMPLISHED EA 1-5330-138496, TITLE: FUSELAGE - FUSELAGE SKIN - EXISTING REPAIR DOUBLER ON LT FUSELAGE SKIN AT STA 2103 AND BETWEEN L39L - L42L (NONE - PRESSURIZED SECTION). EO 1-5100-7-5001, A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,016 hrs · 10,979 cycles

EXISTING REPAIR DOUBLER FOUND AT RT FUSELAGE STA 392 LONGERON 25 RT. EXISTING REPAIR DOUBLER AT RT FUSELAGE STA 392 LONGERON 25 RT, EVALUATED AND FOUND DOES NOT CORRELATE WITH ANY SRM. EXISTING REPAIR DOUBLER REMOVED IAW SRM 53-00-01 FIG 201, REV 43. DUE TO CATEGORY 'B' REPAIR, HFEC METHOD RE-INSP REQUIRED, INITIAL INSP AT 8,000 FLIGHT CYCLES AND REPETITIVE INSP AT 4,500 FLIGHT CYCLES INTERVAL EO 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG -REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CORRODED (BS 2007) · airframe 58,016 hrs · 10,979 cycles

CORROSION - CABIN FLOOR SEAT TRACK, STA 2007, X = 47", IN AFT CARGO WASTE TANK COMPARTMENT CEILING. REPAIRED IAW SRM 53-00-52 FIG. 201 REPAIR 1, REV 43 AND EA 1-5310-138498. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: SEAT TRACK — CORRODED (BS 2007) · airframe 58,016 hrs · 10,979 cycles

CORROSION - CABIN FLOOR SEAT TRACK, STA 2007, X = -47", IN AFT CARGO WASTE TANK COMPARTMENT CEILING. REPAIRED AS IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43 AND EA 1-5310-138498. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.

Part: VALVE — FAILED · airframe 55,941 hrs · 10,538 cycles

WHEN WING AND TAIL ANTI-ICE SELECTED RECEIVED BLEED AIR 1 OFF, BLEED AIR 2 OFF, PACK 1 OFF, PACK 2 OFF ALERTS. THEY TRIED ESC IN MAN AND SWAPPING CONTROLLERS - NO HELP. NR 2 BLEED AIR WOULD SHUT DOWN FIRST FOLLOWED BY NR 1 BLEED APPROX 30 SEC LATER. SELECTING TAIL A/I ONLY CAUSED NO ABNORMALITIES. MX INTERROGATED MFC, PSC1, PSC2, ALL ACC'S, AND ESC FOR CURRENT FAULTS AND FAULT HISTORY. ONLY ONE LATCHED FAULT IN PSC1 - TI2 SENS, INTMT AT 19:22, JUST AFTER T/O AT 2500 FT. PERFORMED DECAY CK IAW JRH 8-8 WITH ALL PASSING MIN LIMITS EASILY: NR1 11/7.4, NR2 29/19, NR3 13/9.3. MSC TERMINATED COMMUNICATION SEVERAL TIMES DURING INTERROGATION. T/S CONTINUES. REMOVED AND REPLACED NR 1 ENG HIGH STAGE VALVE REF AMM 36-11-03-4 STILL NEEDS OPS CHECK REF AMM 36-11-03-5, ALSO 6 EA PILOT VALVE HEATERS OPS CHECK NORMAL. REPLACED NR 2 HIGH STAGE VALVE IAW MM 36-11-03-4. RAN ALL 3 ENGS. ALL HI STAGE VALVES CHECKS GOOD IAW MM 36-11-03-5. PREVIOUSLY REPLACED LT WING DP SENSOR OPS CK GOOD IAW MM 30-11-02-5. WING AND TAIL ANTI-ICE SYSTEM OPERATIONAL CK GROUND CK GOOD.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 53,652 hrs · 9,983 cycles

LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNT SURFACE FOUND CORROSION. CORROSIONS REMOVED ON SIDE LOAD MOUNT AT LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER EA 1-5750-122634, REPAIR CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 53,652 hrs · 9,983 cycles

RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNTING SURFACE FOUND CORRODED. CORROSION REMOVED ON SIDE LOAD MOUNTING SURFACE AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS =0.422 INCH, REMAINING THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.017 INCH. SHIM MACHINED AND BONDED AS PER EA 1-5750-122635, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

UPON REMOVAL OF FLOOR PANEL FOR AUX TANK UPPER SURFACE CORROSION REMOVAL ACCESS FOUND SEAT TRACK ATTACHMENT HOLE AT STATION 1219, X=-75 CORRODED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

UPON REMOVAL OF FLOOR PANEL FOR AUX TANK UPPER SURFACE CORROSION REMOVAL ACCESS FOUND SEAT TRACK AT STATION 1184, X=-75 CORRODED.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 53,652 hrs · 9,983 cycles

LEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122631. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. SLAT ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-10-5 FOUND 'SATIS'.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

EMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD AFT SURFACE VERTICAL STIFFENER AT STATION 2007, X=-15.250 FOUND CRACKED AT UPPER CORNER AREA.

Part: SUPPORT FITTING — CRACKED (EMPENNAGE) · airframe 53,652 hrs · 9,983 cycles

EMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD UPPER AFT SURFACE QUANTITY 01 SUPPORT FITTING AT STATION 2007, X=-31.930 FOUND CRACKED.

Part: SKIN — CHAFED (NR 3 SLAT RT) · airframe 53,652 hrs · 9,983 cycles

RIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122632. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. NR 3 SLAT ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-10-5 FOUND SATISFACTORY.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATION AT HOLE C. CARRIED OUT BUSHING REPAIR AS PER SRM 53- 50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES C AND D. CARRIED OUT REPAIR AS PER SRM 53-50-00, VOLUME I, FIGURE 10. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND D. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AT BOLT HOLES AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. BUSHING REPAIR CARRIED OUT AT BOLT HOLES AS PER SRM 53-50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND D. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. BUSHING REPAIR AT BOLT HOLES CARRIED OUT AS PER SRM 53-50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATION AT HOLE D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50- 00, FIGURE 10, VOLUME I. REAPIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 53,652 hrs · 9,983 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES B AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50- 00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: UNKNOWN — UNKNOWN (FIRE LOOP) · airframe 49,395 hrs · 9,050 cycles

AT CRUISE FL340 MOMENTARY ENGINE FIRE INDICATION ON ENGINE ONE. NO OTHER ENGINE INDICATIONS OF FIRE. RETARDED THROTTLE TO IDLE. REMAINED AT IDLE FOR DIVERT TO LAX. CHECKED RESISTANCE FOR LOOP B AND WAS GOOD, IAW FIM 26-11. FOUND SEVERAL CLAMPS WITH OUT FOIL, FOILED CLAMPS, UNABLE TO REPEAT LOOP B FAULT. PERFORMED RTS, RTS PASS.

Part: SKIN — DENTED (TE FLAP) · airframe 49,008 hrs · 8,971 cycles

RIGHT WING I/B FLAP LOWER SURFACE FOUND DENT. REPAIR CARRIED OUT AT RIGHT HAND WING I/B FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,008 hrs · 8,971 cycles

MAIN DECK CARGO, RIGHT FRAME 1661 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1661 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,008 hrs · 8,971 cycles

MAIN DECK CARGO, RIGHT FRAME 1701 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1701 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,008 hrs · 8,971 cycles

MAIN DECK CARGO, RIGHT FRAME 1681 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1681 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,008 hrs · 8,971 cycles

MAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 FOUND DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO, RIGHT FRAME 1641 AT STRINGER L12 AS PER SRM 53-30-00 FIGURE I VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, LT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.666". MAXIMUM HOLE DIAMETER: 1.680". BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIG.16 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, LT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.341"; REWORKED HOLE TO 1.379". MAXIMUM HOLE DIAMETER: 1.385". BUSHING FABRICATED AND INSTALLED AT CLG LT TRUNNION FITTING FWD HOLE AS PER SRM 53-40-00 FIG.16 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2- 100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, RT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, RT TRUNNION FITTING FWD HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112350, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, RT TRUNNION FITTING ALIGNMENT HOLE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. ORIGINAL HOLE DIAMETER: 1.500"; REWORKED HOLE TO 1.6664". MAXIMUM HOLE DIAMETER: 1.680". BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIG.16 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, LT TRUNNION FITTING MATING SURFACE FOUND CORRODED AFTER PILLOW BLOCK REMOVAL. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD SIDE - ORIGINAL THICKNESS: 2.536"; MATERIAL REMOVED: 0.044" REMAINING THICKNESS: 2.492"; MIN. THICKNESS: 2.430". AFT SIDE - ORIGINAL THICKNESS: 2.534"; MAT'L REMOVED: 0.046"; REMAINING THICKNESS: 2.488"; MIN. THICKNESS: 2.430". REWORK AREA REPROTECTED AS PER SRM 51-20-00 VOL.II.REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (LT MLG) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, LT TRUNNION FITTING AFT HOLE FOUND CORRODED. [07-10-07] COMPLIED WITH FEDEX E.A. 1-5310-112351. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CORRODED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

CTR LANDING GEAR, RT TRUNNION FITTING MATING SURFACE FOUND CORRODED. [07-10-07] REMOVED AND FOUND WITHIN LIMITS AS PER SRM 53-40-00 FIG. 16 VOL.I. FWD LUG - ORIGINAL THICKNESS: 2.505"; MATERIAL REMOVED: 0.040" REMAINING THICKNESS: 2.465"; MIN. ALLOWABLE THICKNESS: 2.430". AFT LUG - ORIGINAL THICKNESS: 2.4925"; MAT'L REMOVED: 0.040"; REMAINING THICKNESS: 2.4525"; MIN.ALLOWABLE THICKNESS: 2.430". REWORK AREA REPROTECTED AS PER SRM 51-20- 00 VOL.II.REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 49,008 hrs · 8,971 cycles

LANDING GEAR, LT MLG FLIPPER DOOR, FWD EDGE FOUND CRACKED. [07-13-07] REPAIR CARRIED OUT AT MLG - LT MLG FLIPPER DOOR, FWD EDGE AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 49,008 hrs · 8,971 cycles

LANDING GEAR, NOSE GEAR LT TRUNNION FITTING FOUND CRACKED. [07-06-07] REPAIR CARRIED OUT AT NOSE LANDING GEAR LT TRUNNION FITTING AS PER SRM 53- 40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 500) · airframe 49,008 hrs · 8,971 cycles

LEFT WING ANTI-ICE TELESCOPING DUCT CUT OUT CORNER FOUND CRACKED. [07-13-07] REPAIR CARRIED OUT AT LEFT HAND WING ANTI ICE TELESCOPING DUCT CUT OUT CORNER AS PER FEDEX EA 1-5710-111133, REPAIR CLASSIFIED AS MIN0R AS PER GMM 6-2-100.

Part: DUCT — CRACKED (ZONE 600) · airframe 49,008 hrs · 8,971 cycles

RIGHT WING LEADING EDGE PANEL NEAR TELESCOPING DUCT AREA FOUND CRACKED.

Part: HINGE — CRACKED (MLG DOOR) · airframe 49,008 hrs · 8,971 cycles

LANDING GEAR, FLIPPER DOOR OUTBOARD EDGE ADJACENT TO FORWARD HINGE FOUND CRACKED. [07-16-07] REPAIR CARRIED OUT AT LANDING GEAR - RT FLIPPER DOOR OUTBOARD EDGE ADJACENT TO FORWARD HINGE AS PER SRM 52-10-00 FIGURE 18 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: BUSS — MALFUNCTIONED · airframe 47,829 hrs · 8,690 cycles

WHILE EXPERIENCING DU4,5 &6 INTERMITTENT BLANKING RECIEVED 'BUS R EMER AC OFF' LVL 1 ALERT,THEN 'IRU 2 ON BAT' LVL 1,FINALLY 'IRU2 FAIL' LVL 2 ALERT.LATER RECEIVED 'SELECT FADEC ALTN' LVL 2 ALERT ON ALL ENGINES,'ATC XPNR 1 & 2 'FAIL ALERTS,ETC. DIVERTED CDG PRIOR TO OCEANIC AIRSPACE. PRECAUTIONARY FOR LOSS OF POWER OF RIGHT EMERGENCY AC BUSS, R & R RCCB B1-138, B1-139, R2-18, R2-5157, DU'S 4-5-6, DEU-2, CK S1-281 & ADJUST, B1-139 CHECK GROUNDS AT PINS 5A & 3 PIN 3 VIA CB'S B1-139. INSPECTED BUNDLES AND WIRING. RAN ENGINES 5 MINUETS. ALL TEST OK. TEST FLIGHT WAS PERFORMED FOR ADG FUNCTIONAL TEST. ALL SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL HANDLE — DIRTY (COCKPIT) · airframe 45,501 hrs · 8,148 cycles

LOWERED GEAR AT 1200 FT FOR LANDING, UNSAFE INDICATIONS ALL 4 GEAR BOTH PRIMARY AND SECONDARY. RECYCLED GEAR, GOT SAFE DOWN INDICATIONS. FOUND GEAR HANDLE AND CONTROL MECHANISIM STICKING CAUSING FOUR GEAR UNSAFE INDICATIONS PRIMARY AND SECONDARY. CLEANED AND LUBED SWITCH AND HANDLE CONTROL MECHANISIM AND HANDLE.

Part: STRUCTURE — CORRODED (ZONE 200) · airframe 44,185 hrs · 7,842 cycles

MAIN DECK COMPARTMENT, DURING SLANT PANEL DRAIN INSPECTION FOUND CORROSION, NEAR DRAIN AREA AT LT STA 1361. REMOVED AND FOUND EXCEEDED LIMITS PER SRM 57-20-00 VOLUME I, FIGURE 12. COMPLIED WITH FEDEX EA 1-5710-90740.

Part: NONE — NONE (NONE) · airframe 44,185 hrs · 7,842 cycles

UNABLE TO PERFORM EA 1-5740-90695A PT3, WINGS LEADING EDGE SLATS, LT NR 2 SLAT TRACK WEB AND SUPPORT REPAIR DUE TO LONG LEAD TIME OF NEW WEB PN: ARB2981-5. COMPLIED WITH FEDEX EA 1-5740-90695A

Part: FRAME — DENTED (ZONE 200) · airframe 44,185 hrs · 7,842 cycles

SNRM N00737: CABIN COMPARTMENT LEFT HAND FRAME AT STATION 1681 FOUND WITH DENT BETWEEN STRINGER 10-11. CORRECTIVE ACTION: SNRM N00737: CABIN COMP'T LH FRAME STA 1661 STR 10-11 CARRIED OUT REPAIR AS PER SRM 53-30 -00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. FEDEX EA 1-5330-90741 TITLE: FUSELAGE - FRAME TRACKING SRM FRAME REPAIR AT STA Y=1661 BETWEEN LONGERON 10 & 11 LEFT HAND ISSUED FOR TRACKING REPETITIVE INSPECTION REQUIREMENTS.

Part: FUEL TANK — CRACKED (LT WING) · airframe 44,185 hrs · 7,842 cycles

LEFT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 42 (LOWER STRINGER).

Part: FUEL TANK — CRACKED (RT WING) · airframe 44,185 hrs · 7,842 cycles

RIGHT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 9 (UPPER STRINGER). SLOTTED OUT AND REPAIR CARRIED OUT AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CRACKED (BS 1781) · airframe 44,185 hrs · 7,842 cycles

CENTER CARGO, DOOR ENTRANCE AFT CORNER AT STA 1781 LATERAL FLOORBEAM CHORD FOUND CRACK APPROXIMATELY TWO INCHES LONG. REPAIR CARRIED OUT IAW FEDEX EA 1-5310-90734.

Part: FUEL TANK — CRACKED (LT WING) · airframe 44,185 hrs · 7,842 cycles

LEFT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 12 (UPPER STRINGER).

Part: FUEL TANK — CRACKED (LT WING) · airframe 44,185 hrs · 7,842 cycles

LEFT HAND WING TANK, CRACK FOUND DURING HFEC INSPECTION AT THE END OF STRINGER 43 (LOWER STRINGER). REPAIR CARRIED OUT AS PER SRM 57-20-00.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 43,823 hrs · 7,774 cycles

SLAT DISAGREE AFTER T/O PRIOR TO SLAT RETRACT. NO ROLL MOVEMENT. INDICATION STOPPED AT SLAT RETRACTION ON ARRIVAL SFS SLAT DISAGREE AGAIN. FOLLOWED CHECK LIST. NO SLAT LANDING WAS NORMAL. FOUND DAMAGED L/E STRUCTURE WHERE PULLY FOR NR 1 SLAT EXTEND CABLE IS MOUNTED. REF IPC 27-81 -35-01 PULLY MOUNTED NR 2 SLAT TRACK OUTBOARD WALL CAME OFF WITH PULLY. ABOUT 18" BY 18" OF PART OF WALL CAME WITH PULLY. REPAIR C/O ON LHW NR 2 SLAT TRACK O/B WEB AND SUPPORT AS PER FEDEX EA 1-5740-90695. (TITLE: WINGS-LEADING EDGE SLATS - LT NR 2 SLAT TRACK WEB AND SUPPORT REPAIR AT STATION XIS, = 211.719) SLAT OPS TEST AND ADJ AS PER MM 27-80-00 AND MM 27-80-20 AND FOUND SATISFACTORY.

Part: RELIEF VALVE — LEAKING (TRIM CYLINDER) · airframe 43,753 hrs · 7,754 cycles

AFTER T/O GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. GROUND SENSOR WAS NOT A FACTOR SINCE PRESSURIZATION WAS NORMAL AND A/P ENGAGED. CONSULTED QRH BUT DID NOT USE THE HANDLE RELEASE BUTTON PER MOCC. RETURNED TO DEL. INSPECTION FOUND FLUID DRIPPING FROM TRIM CYLINDER PRESS RELIEF VALVE ON RIGHT L/G. REMOVED AND REPLACED AS PER AMM-32-37-03-4. ADJ/TEST & OPS TEST OF TRUCK BEAM TRIM INTERLOCK CYLINDER C/O SATIS AS PER AMM-32-37-00-5. GEAR HANDLE MOVEMENT CHECKED SATIS VIA USE OF OVERRIDE BUTTON WITH GEAR PINS INSTALLED. SATIS INTERACTION WITH INTERLOCK CYLINDER. HYD SYS NR 3 RESERVICED TO FULL. RETURNED TO SERVICE.

Part: FRAME — DENTED (ZONE 200) · airframe 39,697 hrs · 6,814 cycles

FUSELAGE FRAME AT STA 1601, LT L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1601, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOL I AND INSTALLED AS PER SRM 51-33- 01 VOL II. REFER TO EA 1-5310-79743.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 39,697 hrs · 6,814 cycles

ENGINE NR 3 LT T/R COWL UPPER SLIDER TRACK END FOUND WITH CRACK. REMOVED AND REPLACED AS PER AMM 78-33-01-4 AND REPAIR CARRIED OUT, PLS REFER TO FAA 8130-3 FORM TRACKING NR 5480 FOR FURTHER WORK DETAILS AND INSTALLED AS PER AMM 78-33-01-04 AND FUNCTIONAL TEST CARRIED AS PER AMM 78-30-00, FOUND SATIS.

Part: TRACK — CRACKED (TRUST REVERSER) · airframe 39,697 hrs · 6,814 cycles

ENGINE NR 2, RT, T/R COWL AT UPPER SLIDER TRACK END FOUND WITH CRACK. T/R COWL REMOVED AS PER AMM 78-33-01-4. REPAIR CARRIED OUT, REFER TO FAA 8130-3, FORM TRACKING NO. 5479 RIGHT HAND THRUST REVERSER COWL RE-INSTALLED AS PER AMM 78-33-01-4. ADJUSTMENT AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 78-30-00, FOUND SATIS.

Part: LONGERON — CORRODED (ZONE 100) · airframe 39,697 hrs · 6,814 cycles

CENTER CARGO COMPARTMENT AT BETWEEN STATION 5-73 TO 5-113, LONGERON 52 FOUND CORRODED. CORRODED LONGERON AT CENTER CARGO COMPARTMENT, BETWEEN STATION 5-73 TO STATION 5-113 LONGERON 52 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG 2 VOL I.

Part: PANEL — CORRODED (ZONE 300) · airframe 39,697 hrs · 6,814 cycles

RIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE CORROSION EXCEEDED CONDITION 3 LIMITS. RIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE REPAIRED AS PER EA NR 1-5510-80309 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 22R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 39,697 hrs · 6,814 cycles

RT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II.

Part: STOP FITTING — CRACKED (ZONE 500) · airframe 39,697 hrs · 6,814 cycles

LT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED CRACKED FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,697 hrs · 6,814 cycles

CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 34L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED SPLICE FITTING AND INSTALLED AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,697 hrs · 6,814 cycles

CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 38R SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED SPLICE FITTING AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II.

Part: SPLICE — CRACKED (ZONE 100) · airframe 39,697 hrs · 6,814 cycles

CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 41L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW SPLICE FITTING AS PER SRM 51-33-01 VOL II.

Part: FRAME — DENTED (ZONE 200) · airframe 39,697 hrs · 6,814 cycles

CABIN, FUSELAGE FRAME AT STA 1681, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1681, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5310-79739, FUSELAGE, MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1681, LONGERON 12L, ISSUED FOR TRACKING.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,697 hrs · 6,814 cycles

CABIN - FUSELAGE FRAME AT STA 1721, LEFT HAND, S12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1721, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 53- 30-00 VOLUME II. FEDEX EA 1-5310-79742, FUSELAGE. TRACKING SRM REPAIR ON FRAME AT STATION 1721, LONGERON 12L, ISSUED FOR TRACKING.

Part: FRAME — DENTED (ZONE 200) · airframe 39,697 hrs · 6,814 cycles

CABIN, FUSELAGE FRAME AT STA 1701, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1701, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5310-79741, FUSELAGE, MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1701, LONGERON 12L, ISSUED FOR TRACKING.

Part: RIB — CRACKED (ZONE 500) · airframe 39,697 hrs · 6,814 cycles

LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK AREA AS PER SRM 51-33-01 VOL II.

Part: RIB — CRACKED (ZONE 600) · airframe 39,697 hrs · 6,814 cycles

RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL II.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 35,155 hrs · 5,793 cycles

AT FL 330 .84 MACH, OBJECT HIT WINDSCREEN IN 2 PLACES AND FRACTURED R1 FROM BOTTOM UPWARDS. CONT TO FRACTURE SPREAD ACROSS WINDSHIELD. SPIDER WEB AT LOWER PORTION OF R1 THROUGH TO UPPER PORTION. FACT R/R R1 WINDSHIELD ASSY PER MD-11M/M 56-11-01-4. AFTER R1 FRACTURE RECEIVED MULTIPLE LEVEL 2 ALERTS. ATS DROPPED OFF. FLT DIR BIASED OUT OF VIEW, FLEW A/C MAN. CAP'T AND F/O SPEED DIFFERED BY 30 KNTS+. ALL ALERTS WENT AWAY AND CAME BACK AFTER 30-60 SEC. A/P AND ATS AVAIL DURING INTERIM WHEN ALERTS NOT ILLUM. FACT SUSP ICE INGESTION INTO PITOT SYSTEM. PURGED SAME, NO FOREIGN MATERIAL NOTED. REF MM 34-11-00-2. REMOVED AND REPLACED NR 1 & 2 CADC'S PRECAUTIONARY. REF MM 34-16-01-4. OK FOR SERVICE.

Part: FITTING — CRACKED (O/B FLAP) · airframe 34,449 hrs · 5,627 cycles

LT OB FLAP TRACK FITTING IS CRACKED AT THE UP STOP MOUNT BARREL NUT HOLE. REPAIRED PER EA 1-5750-67543. THIS EA REMOVES THE 3D0011 BARREL NUT ASSY. AND NAS578-8B RETAINER AND INSTALLS A ZERO CLEARANCE FIT PLUG IN PLACE OF THE REMOVED PARTS AND PROVIDES FOR REPETITIVE INSPECTIONS UNTIL REPLACED WITH A NEW PART WHEN AVAILABLE FROM BOEING..

Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 32,788 hrs · 5,228 cycles

AFTER TAKEOFF, BOTH PRIMARY (LIGHT BY HANDLE) AND SECONDARY (SYNOPTIC) SHOWED UNSAFE FOR LEFT MAIN LANDING GEAR WITH GEAR HANDLE UP. CYCLED GEAR, NO HELP. INDICATIONS OK WITH HANDLE DOWN. DUMPED FUEL, RETURNED FOR NORMAL LANDING. REMOVED AND REPLACED LEFT GEAR BRAKE LINE BRACKET SUPPORT ASSY, BOGIE BEAM TRIM ACTUATOR OPS CHECKED IAW MM, OPS NORMAL. PERFORMED OPS EXTENSION RETRACTION TEST ON LEFT MAIN LANDING GEAR IAW MM. OPS, NORMAL. PERFORMED ANTISKID CONTROL UNIT TEST IAW MM. ALL TEST PASS.