N597FE

Part: BALANCE WEIGHT — CORRODED (N/A) · airframe 93,236 hrs · 19,777 cycles

R/H O/B AILERON HAS ALL BALANCE WEIGHT CORRODED. REMOVED AND REPLACED 5 BALANCE WEIGHTS ON R/H O/B AILERON.

Part: BALANCE WEIGHT — CORRODED (N/A) · airframe 93,236 hrs · 19,777 cycles

R/H O/B AILERON HAS CORROSION ON BALANCE WEIGHT REMOVED AND REPLACED AILERON INCLUDING ALL BALANCE WEIGHT, INCLUDING N/RS 477, 464, 463

Part: BALANCE WEIGHT — CORRODED (N/A) · airframe 93,236 hrs · 19,777 cycles

L/H AILERON HAS BALANCE WEIGHT CORRODED REMOVED AND REPLACED AILERON INCLUDING WEIGHTS

Part: BALANCE WEIGHT — CORRODED (N/A) · airframe 93,236 hrs · 19,777 cycles

L/H O/B AILERON HAS BALANCE WEIGHT CORRODED. REMOVED AND REPLACED AILERON INCLUDING BALANCE WEIGHT N/R 329,

Part: BALANCE WEIGHT — CORRODED (N/A) · airframe 93,236 hrs · 19,777 cycles

R/H O/B AILERON HAS ALL BALANCE WEIGHT CORRODED. R/H O/B AILERON WAS REPLACED INCLUDING WEIGHTS

Part: SKIN — GOUGED (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

R/H WING LEADING EDGE / BETWEEN I/B SLAT #1 & #2 AT SPLICE FOR TRACK #3 ( ON THE AIRCRAFT ) HAS A DEEP GOUGE ( HIDDEN WHEN SLATS ARE RETRACTED ) BLENDED GOUGE AND REPAIRED AREA ON LEADING EDGE OF RH WING XIS 247 (ABOVE SLAT TRACK 3) PER SRM 57-40-02-2R REP 8 FIG 201 SH 1-2 MAJOR REPAIR

Part: SKIN — CRACKED (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

LH WING, LEADING EDGE, NO. 8 SLAT TRACK CUTOUT, OUTBD EDGE HAS HORIZONTAL CRACK APPROX .500", MARKED ORANGE DOT & RED GREASE PENCIL. REPAIRED PER EA # 1-5730-T0375548 P1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

PANEL 345BB DELAMED. REPAIRED DELAMINTED PANEL 345BB PER SRM 51-62-01-0G PG.44 REPAIR "J" STEP 1-9

Part: STANCHION — CORRODED (ZONE 100) · airframe 93,236 hrs · 19,777 cycles

FWD CARGO COMPT, STA 6-73.5 RBL 9, AFT BULKHEAD, VERTICAL STANSION HAS CORROSION OUT OF LIMITS ON VERTICAL LEG AT NUTPLATE REPAIRED ATANCHION PER EA# 1-5310-T0375475 TITLE: FUSELAGE-FORWARD INTERMEDIATE- FORWARD CARGO COMPARTMENT AFT BULKHEAD, STANCHION AT X=9.050 - CORROSION. "MAJOR REPAIR"

Part: TEE FITTING — CRACKED (ZONE 600) · airframe 93,236 hrs · 19,777 cycles

RIGHTHAND INNER WING; STA. 1481 TRAILING EDGE STRUCTURE HAS CRACKED BRACKET @ HANGAR ASSEMBLY. AS VIEWED FROM WHEELWELL OUTER STRUCTURE NOTE: ARC0250 AND IPC 57-51. REMOVED FABERCATED AND INSTALLED NEW T CLIP ANB7535-127 IAW DWG ANB7535

Part: TEE FITTING — CRACKED (ZONE 500) · airframe 93,236 hrs · 19,777 cycles

LEFTHAND INNER WING; STA. 1481 TRAILING EDGE STRUCTURE HAS CRACKED BRACKET @ HANGAR ASSEMBLY. AS VIEWED FROM WHEELWELL OUTER STRUCTURE NOTE: ARC0250 AND IPC 57-51 REMOVED FABERCATED AND INSTALLES NEW T CLIP ANB7535-127 IAW DWG ANB7535

Part: FLOORBEAM — DAMAGED (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

FWD CARGO PIT FLOOR BEAM AT APPROX STA 6-10 CENTER BUTTLINE HAS AN IMPACT DAMAGE IN WHICH THE VERTICAL LEG WAS DEFORMED BEYOND ALLOWABLE LIMITS. REPAIRED FLOOR BEAM PER SRM 53-00-00-0G FIG 208 MAJOR REPAIR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

DELAMINATION ON RH WING T/E XW899 REPAIRED DELAMINATION ON RH WING T/E XW899 PER SRM 57-00-01-2R REPAIR 2 FIG. 201 SHEET 1

Part: SUPPORT — CORRODED (ZONE 100) · airframe 93,236 hrs · 19,777 cycles

FWD CARGO COMPT, AFT BULKHEAD, LOWER FLOOR BOARD SUPPORT STA RBL 10, HAS CORROSION ON VERTICAL LEG. INSTALLED TEE EXTRUSION AND REPAIR ANGLES AS REQUIRED. REF MD 11 SRM 53-00-00-2R FIGURE 208, SHEET 3, SRM 51-33-01-0G, DAC DWG ADA7667.

Part: PANEL — DELAMINATED (N/A) · airframe 93,236 hrs · 19,777 cycles

PANEL 345BB DELAMED. REPAIRED DELAMINATED PANEL 345BB PER SRM55-20-80-2R PG.25-27

Part: PANEL — DELAMINATED (N/A) · airframe 93,236 hrs · 19,777 cycles

R/H HORIZ PANEL 345BB HAS DELAMINATION. REPAIRED DELAMINATED PANEL 345BB PER SRM55-20-80-2R PG.25-27.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 93,236 hrs · 19,777 cycles

LWR FWD CARGO FLOORBOARD 127EF HAS HOLE DAMAGE AND EDGE DAMAGE FABRICATED FLOORBOARD 127EF REF FEDEX DWG SRZ-25-005 MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 93,236 hrs · 19,777 cycles

LWR FWD CARGO FLOORBOARD 127NF HAS PUNCTURES FABRICATED PANEL REF FEDEX DWG SRZ-25-005 MAJOR REPAIR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

L/H FUSELAGE SKIN AT #1 PACK EXHAUST DOOR UPPER AFT CORNER HAS A .200 IN. CRACK PROPAGATING OUT OF FASTENER HOLE. (MARKED) INSTALLED FILLER, DOUBLER, AND TRIPLER REF MD11 SRM 53-20-15-2R REPAIR 3. MAJOR REPAIR

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

LH WING-BETWEEN UPPER AND LOWER REAR SPAR: ARC7199-529 BRACKET AT XORS 1088 HAS CRACK APROX. 3 INCHES REPAIRED NOTED LH WING-BETWEEN UPPER AND LOWER REAR SPAR: ARC7199-529 BRACKET AT XORS 1088 HAS CRACK APROX. 3 INCHES PER SRM 51-62-01-0G REPAIR"J" PG.44

Part: BRACKET — DAMAGED (N/A) · airframe 93,236 hrs · 19,777 cycles

LEFT WING -- BETWEEN UPPER AND LOWER REAR SPAR - COMPOSITE ANGLE BRACKET AT XORS 1088 HAS 2 DAMAGED HOLES REPAIRED NOTED LEFT WING -- BETWEEN UPPER AND LOWER REAR SPAR - COMPOSITE ANGLE BRACKET AT XORS 1088 HAS 2 DAMAGED HOLES PER SRM 51-62-01-0G REPAIR "A" PG.39-40

Part: SKIN — CORRODED (AFT FUSELAGE) · corrosion level 2 · airframe 93,236 hrs · 19,777 cycles

H AFT FUSELAGE, APPROX STA 2140-2164, BOTTOM EDGE OF FAIRING AJC7897-1, HAS SURFACE CORROSION. REPAIRED LH AFT FUSELAGE BOTTOM EDGE AT APRROX STA 2140-2164, REF SRM 53-70-01 2R REPAIR 3 FIG 201 SHEET 1-5, MD-11 SRM 51-33-01-0G, DAC DWG AJC7059. "MAJOR REPAIR"

Part: CHANNEL — CORRODED (ZONE 100) · airframe 93,236 hrs · 19,777 cycles

FWD CARGO COMPT, STA 6-60 6LBL, CORROSION ON THE CENTER ROLLER TRAY/ FLOOR SUPPORT LAND. REMOVED AND REPLACED A6J7003-1 CHANNEL ASSEMBLY WITH NEWLY FABRICATED A6J7003-1 CHANNEL ASSEMBLY REF DAC DWGS A6J7003, N6J6715, AND NBJ6735 MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 93,236 hrs · 19,777 cycles

CTR CARGO FLOORBOARD 183EB HAS EVIDENCE OF IMPACT DAMAGE FABRICATED FLOORBOARD 183EB REF FEDEX DWG SRZ-25-005 MAJOR REPAIR

Part: SKIN — CRACKED (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

RH AIR COND COMPT OPENING EXTERNAL STRUCTURE - AFT UPPER CORNER - VISUAL INDICATION FROM PAINT OF SKIN CRACK EMINATING THRU 2EA. RIVETS - NDT HFEC INSPECTION CONFIRMED INDICATIONS. REPAIRED AFT UPPER CORNER SKIN AT RH AIR COND COMPT,REF MD-11 SRM 53-20-15-2R SHEET 3 FIG 201 & MD-11 SRM 51-33-01-0G. INSPECTED AND ACCEPTED. MAJOR REPAIR

Part: FRAME — CRACKED (ZONE 300) · airframe 93,236 hrs · 19,777 cycles

TAIL CONE FWD SECTION."FWD END" APPROX. 3-O CLOCK POSITION GUIDE PIN ATTACHING STRUCTURE (FRAME) CRACKED. "MARKED" REPAIRED PER SRM 53-80-07-2R REPAIR 1 FIG 201 SHEET 1.

Part: NOSE COWL — DENTED (ZONE 400) · airframe 93,236 hrs · 19,777 cycles

NO. 2 ENG INLET LEADING EDGE - APPROX 3:00 OCLOCK POSITION (LOOKING FWD)- DENT APPROX 1 INCH DIA. DOT #18 REPAIR NOSE COWL REF. EA # 1-5430-T0375346.

Part: SHIM — DAMAGED (UNKNOWN) · airframe 93,236 hrs · 19,777 cycles

#3 PYLON AFT BULKHEAD TO UPPER SPAR CHORD ANGLE T/E SHIM HAS MIGRATED OUT OF POSITION. (MKD) WORK WITH N/R 641 LOOSE BOLTS NOTE: THESE LOOSE BOLTS MAY REQUIRE REMOVAL FOR NDT CHECK FOR CONDITION OF HOLES PRIOR TO REPLACEMENT. 0000098319 : NAVARRO, ENRIQUE S - 21-JUN-2023 17:33 REMOVED AND REPLACED MIGRATING SHIMS AUB7632-527 IN REFERENCE TO INSTALLATION DRAWING AUB7500 AND REMOVED AND REPLACED DAMAGED DOUBLER AUB7698-1 IN REFERENCE TO INSTALLATION DRAWING AUB7531

Part: FRAME — CRACKED (ZONE 300) · airframe 93,236 hrs · 19,777 cycles

TAIL CONE FWD SECTION. FWD END APPROX 1-0CLOCK POSITION (UPPER R/H) GUIDE PIN LOOSE REPAIRED DAMAGE PER SRM 53-80-07-2R REPAIR 1 FIG 201 SHEET 1.

Part: FRAME — CHAFED (ZONE 300) · airframe 93,236 hrs · 19,777 cycles

TAIL CONE FWD SECTION. FWD L/H UPPER GUIDE PIN LOOSE. REPAIRED DAMAGE PER SRM 53-80-07-2R REPAIR 1 FIG 201 SHEET 1.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 93,236 hrs · 19,777 cycles

LEFT WING -- LOWER REAR SPAR AT XORS 1048 HAS CORROSION REMOVED CORROSION AND REPAIRED LH WING LOWER REAR SPAR AT XORS 1048 PER SRM SRM 57-00-00-2R FIG.202 SHT.3 AND EA T 1-5710-T0374723 WING - BASIC WING STRUCTURE - LH WING REAR SPAR LOWER CAP XORS 1042 TO XORS 1062 - REPAIR MAJOR REPAIR

Part: SKIN — CORRODED (CNTR WING) · airframe 93,236 hrs · 19,777 cycles

MAIN DECK, CENTER TANK, TOP SKIN AT STA 1275 AND RBL 106 HAS CORROSION MARKED #2 BLENDED AND REMOVED CORROSION IAW 51-21-01-0G. APPLIED DOUBLER REPAIR OVER BLEND OUT AREA IAW EA# 1- 5730-T0374766

Part: SPAR — CORRODED (ZONE 500) · airframe 93,236 hrs · 19,777 cycles

LEFT WING REAR SPAR AT APPROX XORS 1042 HAS 3 SPOTS OF CORROSION MARKED #6 #7 #8. BLENDED CORROSION AND REWORKED SPAR REF E.A. #1-5710-T0374802 TITLE: WING-LH OUTER WING-REAR SPAR BETWEEN XORS1030 TO XORS 1045-REWORK.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 93,236 hrs · 19,777 cycles

RIGHTHAND WING; TRAILING EDGE XW=899 OB OF OB AILERON 4" MODERATE CORROSION @ WING EDGE. MARKED REPAIRED TRAILING EDGE XW=899 FOUND APPROX 4" BY 2" AREA OF DELAMINATION AS REQ REF 51-43-01-0G PG 6 PAR 10

Part: BRAKE DISC — DETERIORATED (MLG) · airframe 92,275 hrs · 19,486 cycles

LEVEL 1 BRAKE DIFF TEMP AFTER TAKEOFF. #3 TEMP 59 AND #4 TEMP 395. AFTER LANDING AT THE GATE, MAINTENANCE ADVISED #4 BRAKE GLOWING RED HOT. AIRCRAFT CHOCKED AND BRAKES RELEASED. REMOVED #4 TIRE ,INSPECTED #4 BRAKE FOUND CARBON DISKS DISNITEGRATED AND MELTED THUS LOCKING UP #4 TIRE. REPLACED #4 BRAKE IAWAMM 32-43-20-4 AND REPLACED #4 TIRE ASY PER AMM 32-41-01-04, LEAK AND OPS CKS GOOD PER AMM 32-43-20-6. AC OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 91,825 hrs · 19,367 cycles

UNSAFE CENTER GEAR INDICATION ON BOTH GEAR LIGHTS AND SYNOPTIC ON INITIALLY LOWER THE GEAR. RECYCLED TO GEAR HANDLE AND GOT 4 GREEN ON BOTH SYNOPTIC AND GEAR LIGHTS. REMOVED AND REPLACED CENTER LANDING GEAR DOWNLOCKCYLINDER RESTRICTOR PER MD-11 AMM 32-38-06-4. LEAK CHECK GOOD. GEAR SWING TRANSFERRED TO WRI 32-30/5783 TO BE ACCOMPLISHED ONCE UPPER UNLOCK ACTUATOR LOCK LINK IS REPLACED PERFORMED OPS CHECK AND LANDING GEAR ALTERNATE RELEASE OF CENTER AND ALL GEAR REF MD-11 MM 32-16-02-4. OPS CHECK NORMAL A/C OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 91,525 hrs · 19,288 cycles

HYD 2 FAIL LEVEL 2 ALERT APPROXIMATELY 5:45 INTO FLIGHT. HYDRAULIC SYSTEM 2 QUANTITY DECREASED RAPIDLY TO ZERO. QRH PROCEDURE COMPLETED ***EMERGENCY DECLARED*** FOUND LEAK COMING FROM LINE FROM #2 ENGINE HYD MANIFOLD "PRESS IN LWR PUMP" REPLACED LINE P/N AE708163-3 IAW AMM 29-12-40-2. #2 ENGINE ENGINE RUN ACCOMPLISHED PER JRH. NO LEAKS NOTED, EDP'S OPERATED NORMAL . #2 ENGINE COWLS CLOSED IAW AMM 71-10-00-410-802.

Part: BRAKE ASSY — DELAMINATED (ZONE 700) · airframe 91,058 hrs · 19,140 cycles

MDIS 597 32-40 5376 26JUN22 STN FACT U ON POST FLIGHT INSPECTION FOUND NUMBER 10 BRAKE ASSY FAILED. BRAKE DISCS FAILED (SPLINTERED). R/I 26JUN22 01:47 STN U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2609472-4B POS: 10 SRL: B2783 TAG NBR: 1423H4 ON MPN: 2609472-4B CPN: 3200378 SRL: B0691 TAG NBR: 53G915 FACT 26JUN22 01:47 STN U REMOVED NUMBER 10 BRAKE ASSY MPN 2609472-4B S/N B2783. AND REPLACED WITH SERVICABLE BRAKE ASSY IAW AMM 32-43-20-4 OPS IND OK A/C OK FOR SERVICE

Part: ATTACH FITTING — CRACKED (ZONE 600) · airframe 90,389 hrs · 19,004 cycles

FOUND CRACK 1.75 INCHS LONG ON I/B UPPER WINGLET L/E ATTACH FLANGE ON RIGHT-HAND WING REPAIR IAW EA 1-5750-T0368013 PART 1

Part: FAIRING — CHAFED (ZONE 600) · airframe 90,389 hrs · 19,004 cycles

RH WINGLET LOWER FAIRING 628XW HAS SIGNS OF WIND EROSION 0000355851 : MITROVICH, DAVID T - 14-APR-2022 23:27 REPAIRED R/W WINGLET LOWER PANEL REF: MD11 SRM 51-62-01. REPAIRED METALIZED COATING REF: MD11 SRM 51-43-06-0G. PREPPED & PAINTED REF: MD11 AMM 51-22-00.

Part: FITTING — CORRODED (ZONE 600) · airframe 90,117 hrs · 18,932 cycles

SMIS 597 57-20 5046 05MAR22 MEM FACT U MOD TYPE T MOD NO. 1-5720-T0367318 REV NO. A PS P1 WING - SECONDARY WING STRCT - R/H MLG TRUNNION UPPER / LOWER PAD WHERE A-FRAME COMPLY WITH E..A. 1-5720-T0367318 REV NO. A POS P11 INFO 06MAR22 00:27 ** ATTACHED TO WORK ORDER 00082193 ** FACT 08MAR22 12:51 MEM U 06-MAR-2022 09:30 COMPLIED WITH T1-5720-T0367318P1A THIS ITEM WAS FACTED BY PCS, WO# 00082193, SEQ# 000191, CARD# T1-5720-T0367318P1, CORROSION REPAIRED IN ACCORDANCE WITH E.A. 1-5720-T0367318 A PART 1.

Part: FUEL TANK — CORRODED (BS 1224) · corrosion level 2 · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND CENTRE WING TANK TOP SURFACE AT STATION 1224 , X = 7 TO X = -7 CORRODED. MAIN DECK CARGO COMPARTMENT - CABIN AT CENTER WING TANK TOP SURFACE STATION 1224 , X = 7 TO X = - 7 CORRODED AREA REPAIRED AS PER E.A.#: 1-5730-T0364783 PART 1 , REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 89,281 hrs · 18,689 cycles

WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00328 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 4 TO 5 AND 7 TO 10 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING DOUBLER REMOVED AS PER SRM 51-33-01-0G AT LEFT HAND WING LEADING EDGE AT STATION XOS 789 AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE AT STATION XOS 789 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — NONE (N/A) · airframe 89,281 hrs · 18,689 cycles

WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00331 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 3 TO 4 AND 8 TO 11 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING REPAIR REMOVED AT LEFT HAND WING FIXED LEADING EDGE DOUBLER BETWEEN STATION XOS 653 AND STATION XOS 657 AS PER SRM 51-31-01-0G AND REPAIR DOUBLER CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE BETWEEN STATION XOS 653 AND STATION XOS 657 AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — UNKNOWN (ZONE 500) · airframe 89,281 hrs · 18,689 cycles

WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00585 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 2 TO 6 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. REMOVED EXISTING DOUBLER AT LEFT HAND WING FIXED LEADING EDGE LOWER AT STATION XOS 555 AS PER SRM 51-35-01-0G AND FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING FIXED LEADING EDGE LOWER AT STATION XOS 555 AS PER SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — UNKNOWN (ZONE 230) · airframe 89,281 hrs · 18,689 cycles

WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00518 MAJOR REPAIR, REQUIRED INSPECTION ITEM. JOB PROGRESS FORM ITEMS 5 TO 8 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING SEAT TRACK REPAIR SECTION REMOVED AT EXISTING SPLICES STATION 725 TO STATION 765, X= 47.5 AS PER SRM 51-31-01-0G, AND REPAIRED BY SEAT TRACK SECTION REPLACEMENT AT EXISTING SPLICES STATION 725 TO STATION 765, X= 47.5 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 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR EXTERNAL DOUBLERS AT FUSELAGE SKIN STATION 285 Z=- 33. EXISTING REPAIR EXTERNAL DOUBLERS AT FUSELAGE SKIN STATION 285 Z=-33 RIGHT HAND SIDE EVALUATED AND FOUND REPAIR DEVIATION TO SRM 53-00-01-2R REPAIR 1 FIGURE 201 CLASS II. EA # 1-5330-T0364847 P1 TITLE : FUSELAGE - PLATES & SKINS - NOSE FUSELAGE - EXISTING REPAIR FOUND ON RH SKIN AT STA 285 , Z = -33. ACCOMPLISHED . EO 1-5100-7-5001B6 PT1 TITLE : STRUCTURES - REPAIR CATALOG - MD-11-REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. ACCOMPLISHED. REPAIR CLASSIFED AS MAJOR PER GMM 6-2- 100.

Part: FUEL CELL — CORRODED (BS 1228) · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT FOUND CENTRE WING TANK TOP SURFACE AT STATION 1228 , X = 7 TO X = - 7 CORRODED. MAIN DECK CARGO COMPARTMENT - CABIN AT CENTER WING TANK TOP SURFACE STATION 1228 X = 7 TO X= - 7 CORRODED AREA REPAIRED AS PER E.A.#: 1-5730-T0364783 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON RIGHT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 749 EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 749 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1- 5100-7-5001 B6 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: FORMER — NONE (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON LEFT HAND WING FIXED LEADING EDGE UPPER FORMER AT STATION XOS 584 EXISTING REPAIR ON LEFT HAND WING FIXED LEADING EDGE UPPER FORMER AT STATION XOS 584 EVALUATED AND FOUND FORMER REPLACED BY FABRICATION IAW SRM 51-31-01-0G AND DOUGLAS DRAWING ARB2931 REV H. EO 1-5100-7-5001 B6 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 (N/A) · airframe 89,281 hrs · 18,689 cycles

WHILE PERFORMING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND TRUNNION FITTING EXISTING TRIMMED OUT AREA FOUND NOSE LANDING GEAR RIGHT HAND TRUNNION SUPPORT FITTING ATTACH LONGERON AT APPROX STATION 595 FOUND CRACK. NOSE LANDING GEAR RIGHT HAND TRUNNION SUPPORT FITTING STATION 595 CRACK LONGERON REMOVED AND REPLACED AS PER MD-11 SRM 51-35-01-OG. FABRICATED LONGERON AS PER DOUGLAS DRAWING ACA3796 REVISION A. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 893 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 893 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1- 5100-7-5001 B6 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 (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 555 EXISTING REPAIR ON LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 555 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO 1- 5100-7-5001 B6 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 (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND ON RIGHT HAND WING FIXED LEADING EDGE UPPER FORMER AT STATION XOS 584 EXISTING REPAIR ON RIGHT HAND WING FIXED LEADING EDGE UPPER FORMER AT STATION XOS 584 EVALUATED AND FOUND FORMER REPLACED BY FABRICATION IAW SRM 51-31-01-0G AND DOUGLAS DRAWING ARB2931 REV H. EO 1-5100-7-5001 B6 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 (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT HAND SIDE FRAME STATION 535 LONGERON 24 LEFT. EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT LEFT HAND SIDE FRAME STATION 535 LONGERON 24 LEFT HAND EVALUATED FOUND REPAIRED IN ACCORDANCE WITH SRM 53-20-07- 2R REPAIR 1 FIGURE 201 AND FOUND OUTER REPAIR ANGLE CHAFFED. EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIR CARRIED OUT PER SRM 53-20- 07-2R REPAIR 1 FIGURE 201 LEFT HAND FRAME STATION 535 LONGERON 24 LEFT HAND. EO 1- 5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (600) · airframe 89,281 hrs · 18,689 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 880 FOUND CRACK. RIGHT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 880 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 (500) · airframe 89,281 hrs · 18,689 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 779 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 779 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (BS 2145 L33R) · airframe 89,281 hrs · 18,689 cycles

EMPENNAGE : STATION 2145 LONGERON 33R, RIGHT HAND SIDE AFT FUSELAGE SKIN AREA FOUND CORRODED. EMPENNAGE STATION 2145 LONGERON 33R RIGHT HAND SIDE AFT FUSELAGE SKIN AREA CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-70- 01-2R REPAIR 3 FIGURE 201 AND REPAIR CARRIED OUT PER SRM 53-70-01-2R REPAIR 3 FIGURE 201. REFER TO SNRM N00091 W/O 00080494 FOR REPAIR DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (600) · airframe 89,281 hrs · 18,689 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE STRINGER AT STATION XOS 664 FOUND CRACK. RIGHT WING Ï¿½ FIXED LEADING EDGE STRINGER AT STATION XOS 664 REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (500) · airframe 89,281 hrs · 18,689 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 791 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 791 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 — CRACKED (ZONE 600) · airframe 89,281 hrs · 18,689 cycles

RIGHT WING Ï¿½ TRAILING EDGE REAR SPAR LOWER CAP SILL AT STATION XORS 420 FOUND CRACK. CRACK SILL REMOVED AS PER SRM 51-34-01-OG AND FABRICATED SILL AS PER DOUGLAS DRAWING ARC7008 REVISION C. INSTALLED FABRICATED SILL AT RIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT STATION XORS 420 AS PER SRM 51-34-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (600) · airframe 89,281 hrs · 18,689 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 567 FOUND CRACK. RIGHT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 567 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 (500) · airframe 89,281 hrs · 18,689 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 770 FOUND CRACK. LEFT WING FIXED LEADING EDGE DOUBLER AT STATION XOS 770 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1841) · airframe 89,281 hrs · 18,689 cycles

UPON REMOVAL OF WEB - LOWER CENTER CARGO COMPARTMENT STATION 1841 FLOOR SUPPORT FOUND WITH CORROSION, X= 40 LEFT HAND SIDE. LOWER CENTER CARGO COMPARTMENT STATION 1841 FLOOR SUPPORT CORROSION X= 40 LEFT HAND SIDE REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53- 00-00-2R FIGURE 206 REPAIR GENERAL. DAMAGED SUPPORT REMOVED PER SRM 51-31-01-0G . SUPPORT FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION:R AND INSTALLED AS PER SRM 51-31-01-0G. FRAME EXISTING HOLES PLUG CARRIED OUT REPAIR AS PER EA 1-5310- T0364970 PART 1 TITLE: FUSELAGE- MAINFRAME - PLUG HOLE REPAIRS ON STA1841 RHS FRAME WEB AGA7125-3, X=-50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — CORRODED (N/A) · airframe 89,281 hrs · 18,689 cycles

AFT WASTE TANK COMPARTMENT STATION 1975 BETWEEN LONGERON #46 LEFT HAND AND #47 LEFT HAND TEE FOUND WITH CORROSION. AFT WASTE TANK COMPARTMENT STATION 1975 BETWEEN LONGERON #46 LEFT HAND AND #47 LEFT HAND TEE CORROSION EVALUATED AND FOUND EXFOLIATION CORROSION EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL . DAMAGED TEE REMOVED AND REPLACED WITH NEW TEE AS PER SRM 51-31-01-0G . REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: LONGERON SPLICE — CORRODED (ZONE 100) · airframe 89,281 hrs · 18,689 cycles

LOWER CENTER CARGO COMPARTMENT STATION 5-63 LONGERON 48 LEFT HAND SPLICE FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 5-63 LONGERON 48 LEFT HAND SPLICE CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53- 00-00-2R FIGURE 206 REPAIR GENERAL. DAMAGED SPLICE REMOVED AND INSTALLED WITH FABRICATED SPLICE AS PER SRM 51-33-01-OG. SPLICE FABRICATED AS PER DOUGLAS DRAWING AEA7653 REVISION C . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 89,281 hrs · 18,689 cycles

CENTER UPPER AUXILIARY TANK STRINGER AT LEFT HAND S-52, XCW 48 FOUND CRACK ABOUT 7.5 INCHES IN LENGTH. CENTER UPPER AUXILIARY TANK AT LEFT HAND S-52, XCW 48 CRACK STRINGER REPAIRED AS PER MD-11 SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — NONE (ZONE 500) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING LEADING EDGE DOUBLER AT STATION XOS 789 (DOUBLER REPLACED) EXISTING REPAIR AT LEFT HAND WING LEADING EDGE DOUBLER AT STATION XOS 789 EVALUATED AND FOUND PREVIOUS WORK ORDER 00069707, SPECIAL/NONROUTINE MAINTENANCE FORM N00328 JOB PROGRESS FORM ITEMS 4 TO 5 AND 7 TO 10 DO NOT HAVE REQUIRED INSPECTION ITEMS BLOCK MARKED. EXISTING DOUBLER REMOVED AS PER SRM 51- 33-01-0G AT LEFT HAND WING LEADING EDGE AT STATION XOS 789 AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT HAND WING LEADING EDGE AT STATION XOS 789 AS PER SRM 51-33-01-0G. EO 1-5100-7-5001 B6 PART1, TITLE: STRUCTURES - REPAIR CATALOG-MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM N00920 FOR WORK DETAILS.

Part: TRACK — NONE (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK FROM STATION 725 TO STATION 765 X = 47.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK FROM STATION 725 TO STATION 765 X = 47.5 LEFT HAND SIDE EVALUATED AND FOUND PREVIOUS SPECIAL/NONROUTINE MAINTENANCE FORM N00518 WORK ORDER NUMBER 00069707 JOB PROGRESS FORM ITEMS 5 TO 8 DO NOT HAVE REQUIRED INSPECTION ITEM MARKED. SEAT TRACK REPAIR CARRIED OUT AT EXISTING SPLICES AT STATION 725 TO STATION 765 X=47.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO #1-5100-7-5001 B6 PART1 TITLE:STRUCTURES - REPAIR CATALOG- MD-11- REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. REFER SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00942 WORK OAGING AIRCRAFT - EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK FROM STATION 725 TO STATION 765 X = 47.5 LEFT HAND SIDE EXISTING REPAIR AT MAIN DECK CARGO COMPARTMENT SEAT TRACK FROM STATION 725 TO STATION 765 X = 47.5 LEFT HAND SIDE EVALUATED AND FOUND PREVIOUS SPECIAL/NONROUTINE MAINTENANCE FORM N00518 WORK ORDER NUMBER 00069707 JOB PROGRESS FORM ITEMS 5 TO 8 DO NOT HAVE REQUIRED INSPECTION ITEM MARKED. SEAT TRACK REPAIR CARRIED OUT AT EXISTING SPLICES AT STATION 725 TO STATION 765 X=47.5 IN ACCORDANCE WITH SRM 53-00-52-2R REPAIR 1 FIGURE 201. EO #1-5100-7-5001 B6 PART1 TITLE:STRUCTURES - REPAIR CATALOG- MD-11- REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. REFER SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00942 WORK ORDER NUMBER 00080494 FOR REPAIR DETAILS.ORDER NUMBER 00080494 FOR REPAIR DETAILS.

Part: SKIN — CORRODED (BS 2145 L33R) · corrosion level 2 · airframe 89,281 hrs · 18,689 cycles

EXISTING REPAIR AT AFT FUSELAGE SKIN STATION 2140 LONGERON 33R RIGHT HAND SIDE EXISTING REPAIR AT AFT FUSELAGE SKIN STATION 2140 L33R RIGHT HAND SIDE EVALUATED AND FOUND CORROSION AT STATION 2145 EXCEEDED LIMIT AS PER SRM 53-70-01-2R REPAIR 3 FIGURE 201. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER SRM 53-70-01-2R REPAIR 3 FIGURE 201. EO 1-5100-7-5001 B6 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 — NONE (ZONE 500) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STATION XOS 653 AND STATION XOS 657 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STATION XOS 653 AND STATION XOS 657 EVALUATED AND FOUND PREVIOUS WORK ORDER 00069707, SPECIAL/NONROUTINE MAINTENANCE FORM N00331 JOB PROGRESS FORM ITEMS 3 TO 4 AND 8 TO 11 DO NOT HAVE REQUIRED INSPECTION ITEMS BLOCK MARKED. EXISTING REPAIR REMOVED AS PER SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER SRM 57-40-02- 2R REPAIR 15 FIGURE 203. EO 1-5100-7-5001 B6 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. REFER TO SPECIAL/NONROUTINE MAINTENANCE FORM N00932 FOR WORK DETAILS.

Part: WEB — NONE (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT FLOOR WEB AT STATION 1841, X = 44 EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT FLOOR WEB AT STATION 1841, X = 44 EVALUATED AND FOUND NOT IAW SRM 53-00-00-2R REPAIR GENERAL FIGURE 211. WEB REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REV R. EO 1-5100-7-5001 B6 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: FITTING — CRACKED (N/A) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT NOSE LANDING GEAR TRUNNION FITTING STATION 595 RIGHT HAND SIDE EXISTING REPAIR AT NOSE LANDING GEAR TRUNNION FITTING STATION 595 RIGHT HAND SIDE EVALUATED AND FOUND REPAIRED IAW EA 1-5310-105635 PART 1 TITLE: FUSELAGE - R/H NOSE LANDING TRUNNION WEB CRACK - STOP DRILL DEVIATION FROM SRM AND CURRENT HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK APPROXIMATELY 0.3 INCH AT STATION 583. EXISTING REPAIR REMOVED AS PER SRM 51- 31-01-0G AND REPAIR CARRIED OUT IAW EA 1-5310-T0319974 A PART 3, TITLE: FUSELAGE - MAIN FRAME - RH NLG TRUNION FITTING CRACK INSPECTION. EO 1-5100-7-5001 B6 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — NONE (ZONE 500) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER DOUBLER AT STATION XOS 555 (DOUBLER REPLACED) EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER DOUBLER AT STATION XOS 555 EVALUATED AND FOUND PREVIOUS WORK ORDER NUMBER 00069707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00585 JOB PROGRESS FORM ITEM 2 TO 6 DO NOT HAVE REQUIRED INSPECTION ITEM MARKED. FIXED LEADING EDGE LOWER DOUBLER REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-35-01-0G. FABRICATED DOUBLER AS PER DOUGLAS DRAWING ARB2933 REVISION AJ. EO 1-5100-7-5001 B6 PART1 TITLE:STRUCTURES - REPAIR CATALOG- MD-11- REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. REFER SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00944 WORK ORDER NUMBER 00080494 FOR WORK DETAILS.

Part: WEB — NONE (NA) · airframe 89,281 hrs · 18,689 cycles

AGING AIRCRAFT - EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT FLOOR WEB AT STATION 1841, X = -48 EXISTING REPAIR AT LOWER AFT CARGO COMPARTMENT FLOOR WEB AT STATION 1841, X = -48 EVALUATED AND FOUND NOT IAW SRM 53-00-00-2R REPAIR GENERAL FIGURE 211. WEB REMOVED AND REPLACED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REV R. EO 1-5100-7-5001 B6 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: TRACK — CRACKED (200) · airframe 89,281 hrs · 18,689 cycles

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

Part: TRACK — CRACKED (200) · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 1350 , X = - 75.25 WITH CROWN CRACKED. MAIN DECK CARGO COMPARTMENT - CABIN , CRACKED SEAT TRACK AT STATION 1350 , X = - 75.25 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO EXISTING SPLICE STATION 1269 , X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (200) · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 5-10 , X = 47.5 WITH CROWN CRACKED. MAIN DECK CARGO COMPARTMENT - CABIN , CRACKED SEAT TRACK AT STATION 5-10 , X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 5-63 TO STATION 1531/5-0 , X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (200) · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 1501 , X = 47.5 WITH CROWN CRACKED. MAIN DECK CARGO COMPARTMENT - CABIN , CRACKED SEAT TRACK AT STATION 1501 X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1491 TO EXISTING SPLICE STATION 1531/5-0 , X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK CARGO) · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 1854 , X = 27.5 WITH CORROSION. MAIN DECK CARGO COMPARTMENT - CABIN , AT SEAT TRACK STATION 1854 , X = 27.5 CORROSION EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1811 TO END OF PART STATION 1887 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRACK — CRACKED (200) · airframe 89,281 hrs · 18,689 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 755 , X = 75.25 WITH CROWN CRACKED. MAIN DECK CARGO COMPARTMENT - CABIN , CRACKED SEAT TRCK AT STATION 755 , X = 75.25 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 725 TO EXISTING SPLICE STATION 765 , X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LANDING GEAR — FAILED (LEFT) · airframe 89,041 hrs · 18,626 cycles

RECEIVED UNSAFE INDICATION ON LEFT MAIN GEAR (PRIMARY AND SECONDARY) WHEN GEAR RETRACTED. RECYCLED GEAR AS PER QNH RED (UNSAFE) GEAR INDICATIONS REMAINED. NO SPEED LIMITS EXCEEDED. T/S FOUND CABLE 216A (LH MLG POSITION FOLLOW-UP CABLE) BROKEN OFF. PER MD-11 AMM 32-31-10-4 REMOVED AND INSTALLED 216A AND 216B CABLES. PER MD-11 AMM 32-21-00-5 RIGGED THE CABLES OK. PER MD-11 AMM 07-11-00-2 AND AMM 32-31-00 PERFORMED ALL LDG AND DOORS SWING TEST 4 TIMES WITH NORMAL. A/C OK FOR SERVICE.

Part: CABLE — FAILED (TE FLAPS) · airframe 88,852 hrs · 18,573 cycles

ON FINAL APPROACH, CONFIGURED AT FLAPS 15, SLAT EXT. WHEN ATTEMPTED TO EXTEND FLAPS TO 28, RECEIVED FLAP DISAG ALERT . RECYCLED FLAPS, SAME RESULT RAN QRH FOR FLAP DISAG, LANDED WITH FLAP 15, SLAT EXT CONFIGURATION. INSPECTION FOUND LT I/B FLAP FOLLOW UP CABLE & CABLE PULLY DAMAGED. REMOVED DAMAGED LT FLAP BUSS CABLES IAW MM 27-51-11-4. RIGGED FLAP BUSS CABLES IAW MM 27-50-00-5. REPLACED ONE PULLEY IAW DWG NEH6003. COMPLETED RIG OF FLAP BUSS CABLES. COMPLETED SAFETIES ON ALL TURNBARRELS IAW MM 27-50-00-5 AND ALL OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (SLAT SYSTEM) · airframe 88,825 hrs · 18,567 cycles

DURING FLIGHT WE RECEIVED A LEVEL ONE HYD 1 OFF. FOLLOWED BY HYD 1 QTY LO. 2.3 GALLONS. SERVICES HYD QUANTITY AND REMOVED /REPLACED INBOARD SLAT ACTUATOR AS PER AMM 27- 82-01-4 , OPS AND LEAK CHECK GOOD NO LEAK NOTED.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 87,934 hrs · 18,288 cycles

WHILE REPAIRING DAMAGE TO WEB IN BULK CARGO FLOOR BULKHEAD, FOUND CRACK MEASURING APPROX 5" IN RADIUS OF SUPPORT. REMOVED DAMAGED SECTION OF FLOOR SUPPORT. REQUIRES NDT FOR CRACK REMOVAL CHECK OF UPPER T SUPPORT AREA. PERFORMED HFEC OF UPPER TEE TRIMMED AREA, REF NDTSPM PT6. NO CRACKS NOTED. VERIFIED MATERIAL FOR FILLERS UNDER EXTRUSION REPAIR, PRIMED. INSTALLED ALL REPAIR PARTS REF SRM 53-00-00-2R AND EA 1-5310-T0359958, REV A, PART 2.

Part: BULKHEAD — CRACKED (CENTER CARGO) · airframe 87,934 hrs · 18,288 cycles

RAMP REPORTED DURING OFF LOADING FOUND CRACK MEASURING 2 INCH AT CENTER CARGO ON PARTITION BETWEEN CENTER CARGO AND AFT CARGO. PERFORM HFHC OF DAMAGED CUT OUT FOR CRACK IN PARTITION. DRILLED ALL REPAIR DOUBLERS, EXTERUSION AND FILLERS. INSTALLED WEB DOUBLER, FILLERS & EXTERUSION REPAIR IAW SRM 53-00-00-2R & EA 1-5310-T0359958 A.

Part: BUTTON — FAILED (DOOR SLIDE) · airframe 87,277 hrs · 18,082 cycles

MDIS 597 25-60 3539 30NOV20 MCO OPEN U LEFT ENTRY DOOR EVACUATION SLIDE PRESSURE PRESS TO TEST INDICATION INOP. MEL 30NOV20 23:33 MCO U RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 10DEC20 "MEL 25-61-02: LEFT SIDE___ EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY." REMOVED AND REPLACED PUSH TO TEST SWITCH LIGHT ASSY REF MD11 WDM 25_61_01

Part: TRANSFER VALVE — CONTAMINATED (NR 1 MAIN TANK) · airframe 86,660 hrs · 17,930 cycles

PDIS 597 28-41 3303 18SEP20 MEM OPEN U. APPROX 150 MILES OUT OF KMEM RECEIVED TNK 1 TIP TRAPPED AND TNK 1 FUEL QTY LO LEVEL 1 ALERTS. SHOWED 5700 LBS OF FUEL TRAPPED IN NR 1 TIP TANK. 23.0K TOTAL FUEL. DECLARED EMERGENCY DIRECT TO KMEM. ENROUTE LAT FUEL UNBAL LEVEL 2 ALERT. WENT TO FUEL MANUAL KEPT FUEL IN NR 2 & NR 3 TANKS. INSPECTED NR 1 MAIN TIP TANK AND FOUND DEBRIS IN TRANSFER VALVE, REMOVED DEBRIS. REMOVED AND REPLACED TRANSFER VALVE, PER AMM MD11-28-21-04-4. OPS CK IS GOOD.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 86,124 hrs · 17,787 cycles

GOT A FUEL QTY / USED CHK ALERT AT FL 380. FOLLOWING QRH IT APPEARED THAT WE HAD LOST APPROX 5000 LBS OF FUEL. FOLLOWING CHK IT SEEMED LEAK WAS COMING FROM NR 2 TANK OR ENG. ISOLATED TANK, IT WASNT LEAKING. BURN TO NR 2 WAS MUCH HIGHER THAN NR 1 AND NR 3. CHECK LIST HAD US SHUT DOWN NR 2 ENG. LANDED UNEVENTFULLY. WE WRE NOT MISSING ANY FUEL AND NR 2 TANK HAD INCREASED 1000 TO 5000 LBS THAN WHEN AIRBORNE. MEL 28-01-01-02: TANK NR 2 FUEL TANK SYNOPTIC QTY DISPLAY INOP. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 2 QTY WITH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPERATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LAT TAIL FUEL MGMT INOP.

Part: SEM UNIT — FAILED (FUEL SYSTEM) · airframe 86,124 hrs · 17,787 cycles

GOT A FUEL QTY, USED CHK ALERT AT FL 380 . FOLLOWING QRH IT APPEARED THAT WE HAD LOST APPROX 5000 LBS OF FUEL . FOLLOWING CHK IT SEEMED LEAK WAS COMING FROM NR 2 TANK OR ENG . ISOLATED TANK , IT WASN`T LEAKING . BURN TO NR 2 WAS MUCH HIGHER THAN NR 1, AND 3 . CHECK LIST HAD US SHUT DOWN NR 2 ENG . LANDED UNEVENTFULLY . NOT MISSING ANY FUEL AND NR 2 TANK HAD INCREASED 1000 TO 5000 LBS THAN WHEN AIRBORNE . TANK NR 2 FUEL TANK SYNOPTIC QTY DISPLAY- INOPERATIVE. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 2 QTY WI TH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPE RATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LA T. TAIL FUEL MGMT - INOP." REF TSI 28-41-2974 FOR T/S. REMOVED AND REPLACED SEM IN IAW AMM 28-41-91-4, NO FAULTS AT THIS TIME, OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,610 hrs · 17,665 cycles

ARRIVED AT AIRCRAFT WITH EMER LIGHT SELECTED ON. AFTER RETURNING SWITCH TO NORMAL AND RUNNING EMER LIGHT TEST, EMER 1 BAT LO ANNUNCIATED TROUBLESHOT AND TESTED THE EMERGENCY LIGHTING SYSTEM. TESTS PASSED. AIRCRAFT OK FOR SERVICE.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,769 hrs · 17,415 cycles

RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-09 AND E.A. #: 1-5750-T0351908 PART 1 STEP 1. TITLE: WINGS- FLIGHT SURFACES -EO 1-5750- 7-5002- RH WING- OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) -CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 700) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER AFT HOLE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER AFT HOLE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SRM 57-20-14-2R REPAIR 1. REPAIR BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-20-14-2R REPAIR 1 AND E.A. # : 1-5740-T0350144 PART 1 STEP 7 D(1) AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 7 D(3), TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1- 5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (ZONE 700) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER HOLE SPOT FACE AFT SIDE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER HOLE SPOT FACE AFT SIDE REWORKED AS PER MD-11 SRM 51-21-01-OG. WASHER FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 8A AND STEP 8C, TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (ZONE 700) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER MATING SURFACE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER MATING SURFACE REWORKED BY MACHINING AS PER MD-11 SRM 51-21-01-OG. REPAIR PAD FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 9A AND STEP 10, TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER HOLE SPOT FACE FORWARD SIDE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER HOLE SPOT FACE FORWARD SIDE REWORKED AS PER MD-11 SRM 51-21-01-OG. WASHER FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 8A AND STEP 8C, TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (ZONE 700) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING LOWER SPOT FACE AFT SIDE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING LOWER SPOT FACE AFT SIDE REWORKED AS PER MD- 11 SRM 51-21-01-OG. WASHER FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1- 5740-T0350144 PART 1 STEP 8A AND STEP 8C, TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING STRUCTURE SIDE UPPER FORWARD HOLE FOUND CORROSION. CORROSION AT LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING STRUCTURE SIDE UPPER FORWARD HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-14-2R REPAIR 1. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1-5750-T0350145 P1 STEP 7. TITLE : LANDING GEAR- ANTI- SKID/ PKG BRAKE- REWORK OF THE LH MAIN LANDING GEAR ARB7118-7 FITTING OVERSIZED HOLE- TEMP BOLT BORE REPAIR TRACKING. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 700) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING LOWER MATING SURFACE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING LOWER MATING SURFACE REWORKED BY MACHINING AS PER MD-11 SRM 51-21-01-OG. REPAIR PAD FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 9A AND STEP 10, TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER HOLE FORWARD SIDE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING UPPER HOLE FORWARD SIDE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SRM 57-20-14-2R REPAIR 1. REPAIR BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-20-14-2R REPAIR 1 AND E.A. # : 1-5740-T0350144 PART 1 STEP 7 D(1) AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 7 D(3), TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (LT MLG) · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING LOWER SPOT FACE FORWARD SIDE FOUND CORROSION CORROSION AT LEFT HAND MAIN LANDING GEAR - LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACHMENT FITTING LOWER SPOT FACE FORWARD SIDE REWORKED AS PER MD-11 SRM 51-21-01-OG. WASHER FABRICATED BY MACHINING AND INSTALLED AS PER E.A. # : 1-5740-T0350144 PART 1 STEP 8A AND STEP 8C, TITLE : WINGS- ATTACH FITTINGS- LH MLG RETRACT SUPPORT FRAME ASSY- CORROSION COMMON TO BORE HPLES AND MATING SURFACES. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO E.A. # : 1-5740-T0350144 PART 1 AND SNRM NO. N01298 FOR WORK DETAILS.

Part: FRAME — DAMAGED (BS 535) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , EXISTING REPAIR OUTER ANGLE FOUND DAMAGED . MAIN DECK LEFT HAND FRAME AT STATION 535 LONGERON 24 LEFT , EXISTING DAMAGED OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20- 07-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 84,310 hrs · 17,283 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750- T0330906 A PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE : WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501734 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 392-440) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

UPON REMOVED FWD CABIN FLOOR PANEL # 221FF FOR SEAT TRACK REPAIR ACCESS FOUND FLOOR SUPPORT AT STATION 392 - 440 X = - 12 CORROSION . MAIN DECK FLOOR AT SUPPORT STATION 392 TO STATION 440 X = - 12 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE . CORRODED FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G . FLOOR SUPPORT FABRICATED BY MACHINIG AS PER DOUGLAS DRAWING ABA 8225 REVISION J .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 84,310 hrs · 17,283 cycles

LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750- T0330906 A PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE : WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501734 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · airframe 84,310 hrs · 17,283 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE(#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-07 AND E.A. # : 1-5750-T0330908 A PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE : WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501787 FOR WORK DETAILS.

Part: BRACKET — CORRODED (RT WING) · airframe 84,310 hrs · 17,283 cycles

RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE(#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. # : 1-5750-T0330908 A PART 1 STEP 1 F(1) AND STEP 1 F(3), TITLE : WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501787 FOR WORK DETAILS.

Part: ATTACH FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACH FITTING LOWER AFTER HOLE FOUND CORRODED. CORROSION REWORKED AND FOUND EXCEED TO LIMITS IAW SRM 57-20-14-2R, REPAIR 1. A REPAIR BUSHING WAS FABRICATED IAW SRM 57-20-14-2R, REPAIR 1, AND EA 1-5740-T0350144, PART 1, STEP 7 D(1), AND INSTALLED EA 1-5740-T0350144, PART 1, STEP 7 D(3). THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACH FITTING , LOWER MATING SURFACE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW SRM 57-20-14-2R, REPAIR 1. REPAIRED IAW EA 1-5750-T0350145 P1, STEP 9. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: RIB — CRACKED (LT WING SLAT) · airframe 84,310 hrs · 17,283 cycles

LEFT WING NR 1 LEADING EGE SLAT INBOARD RIB FOUND CRACKED AT XIS 151. REPAIRED THE LEFT WING SLAT INBOARD RIB IAW EA 1-5750-T0350043, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT MAIN LANDING GEAR, RETRACT ACTUATOR UPPER ATTACH FITTING UPPER MATING SURFACE FOUND CORRODED. ATTACH FITTING CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW SRM 57-20-14-2R REPAIR 1. REPAIRED IAW EA 1-5750-T0350145 P1, STEP 9. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CRACKED (BS 1887-2007) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK AFT FLOOR SUPPORT AT STATION 1887 - 2007 X = - 57 FOUND CRACKED . THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 .

Part: RIB — CRACKED (RT WING SLAT) · airframe 84,310 hrs · 17,283 cycles

RIGHT WING NR 1 LEADING EDGE SLAT INBOARD RIB FOUND CRACKED AT XIS 151. REPAIRED THE NR 1 SLAT INBOARD RIB IAW EA 1-5750-T0350046, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT MAIN LANDING GEAR RETRACT ACTUATOR UPPER ATTACH FITTING LOWER FORWARD HOLE FOUND CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW SRM 57-20-14-2R, REPAIR 1. A REPAIR BUSHING WAS FABRICATED IAW SRM 57-20-14-2R, REPAIR 1, AND EA 1-5740-T0350144, PART 1, STEP 7, D(1), AND INSTALLED IAW EA 1-5740-T0350144, PART 1, STEP 7, D(3). THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1305-1315) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STATION 1305.25 TO STATION 1315.42 L-26 LEFT TO L-27 LEFT FOUND CRACKED. REPAIRED AS PER SRM 53-40-15- 2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FLOOR SUPPORT — CORRODED (BS 445) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

FORWARD CABIN FLOOR SUPPORT AT STATION 445, RBL 95 FOUND CORROSION. THE FLOOR SUPPORT WAS FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-00-2R, FIGURE 206 ALLOWABLE DAMAGE. A NEW FLOOR SUPPORT WAS FABRICATED IAW DRAWING ABA 7341, REVISION C . THE FLOOR SUPPORT WAS REMOVED AND RELACED FROM BS 380 TO 459 IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 430) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

FORWARD CABIN SEAT TRACK AT BS 430, RBL 27.5 WAS FOUND WITH CORROSION. THE SEAT TRACK WAS REWORKED IAW DRAWING ABA7684, REVISION G, AND THE CORROSION WAS FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REMOVED AND REPLACED FROM BS 421 TO EXISTING SPLICE BS 485 IAW SRM 51-31-01-0G . THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 695 CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 754 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 5-113 X = 8.5 FOUND WITH CORROSION. FOUND EXFOLIATED AND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 5-83 TO EXISTING SPLICE STATION 5-123 / 1531 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 1541) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 1541, LBL 8.5 FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO EXISTING SPLICE BS 1531 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 1521) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1521, RBL 47.5 WAS FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1511 TO EXISTING SPLICE BS 1531 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 1541) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 1541, LBL 47.5 WAS FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1571 TO EXISTING SPLCE BS 1531 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 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED THE LEFT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 701 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 455) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR CURVED SEAT TRACK AT BS 455, RBL 107.25 FOUND CORRODED. THE SEAT TRACK CORROSION WAS FOUND EXFOLIATED , EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. COMPLIED WITH EA 1-5321-T0350175 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 CRACKED. REPAIRED THE BEADED DOUOBLER IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 544 CRACKED. REPAIRED THE LT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 84,310 hrs · 17,283 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 539 CRACKED. REPAIRED THE LT WING FIXED LEADING EDGE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (MAIN DECK) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 5-60, LBL 47.5 FOUND WITH CROWN DAMAGE. DAMAGE EVALUATED AND FOUND TO EXCEED THE LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1 . THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 5- 63 TO EXISTING SPLICE BS 5-0 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 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 5-113, RBL 8.5 WAS FOUND WITH CORROSION. FOUND EXFOLIATED AND EXCEEDS LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 5-63 TO 5-123 / 1531 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 (MAIN DECK) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 5-60, RBL 7.5 FOUND WITH CROWN DAMAGE. EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 5-43 TO EXISTING SPLICE BS 5-0 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 1282) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 1282 X = 47.5 FOUND CROWN DAMAGED

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1282, LBL 47.5 FOUND CROWN DAMAGED. EVALUATED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1313 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (BS 445) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

FORWARD CABIN FLOOR SEAT TRACK AT STA 445, RBL 35 FOUND CORROSION. CORROSION REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . SEAT TRACK REMOVED AND REPLACED FROM BS 440 TO 495, RBL 35 IAW SRM 51-31-01-0G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — DAMAGED (BS 1282) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 1282, LBL 8.5 WAS FOUND WITH CROWN DAMAGE. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1313 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 755) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 775, X = 75.25 FOUND CROWN DAMAGED. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT, BS 782 TO BS 765 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 755) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 755, RBL 8.5 WAS FOUND WITH CROWN DAMAGE. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE DAMAGED SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 785 TO 745 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 1282) · airframe 84,310 hrs · 17,283 cycles

MAIN DECK SEAT TRACK AT BS 1282, RBL 8.5, WS FOUND WITH CROWN DAMAGE. FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1269 TO 1313 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE SURFACE FOUND CORRODED. CORROSION REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-04 , REPAIR EVALUATED AND FOUND THE LEFT OUTBOARD FLAP AFT INBOARD HINGE PIVOT INBOARD LUG SURFACE REMAINING THICKNESS : 0.406" CORRECT IAW EA 1-5750-T0349971, PART 1, STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0330908 A, PART 1, STEP 1, F(1), AND STEP 1 F(3). THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 84,310 hrs · 17,283 cycles

RIGHT WING FIXED WING LEADING EDGE APPROXIMATELY XOS 593 BEADED DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 84,310 hrs · 17,283 cycles

RIGHT HAND WING FIXED WING LEADING EDGE APPROXIMATELY XOS 528 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE APPROXIMATELY XOS 528 BEADED DOUBLER AREA AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. CORROSION REWORKED AND FOUND WITHIN LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07, AND EA 1-5750-T0330906 A, PART 1, STEP 1, F(1), AND STEP 1 F(3). THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 84,310 hrs · 17,283 cycles

RIGHT WING FIXED WING LEADING EDGE APPROXIMATELY XOS 653, BEADED DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203 REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-04. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-04, AND EA 1-5750-T0349971, PART 1, STEP 1A, AND STEP 1. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORRODED. CORROSION WORKED AND IAW CMM 57-44-08 FOUND TO EXCEED LIMITS. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0349923, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 84,310 hrs · 17,283 cycles

RIGHT HAND WING FIXED LEADING EDGE APPROXIMATELY XOS 538 BEADED DOUBLER FOUND CRACKED REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE APPROXIMATELY XOS 538 BEADED DOUBLER AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A. # : 1-5750-T0325158 B PART 2 STEP 2A AND STEP 2B, TITLE : WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501749 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 52-03 AND E.A. # : 1-5750-T0325158 B PART 2 STEP 2A AND STEP 2B, TITLE : WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501749 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A. # : 1-5750-132310 C PART 2 STEP 2A AND STEP 2B, TITLE : WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501736 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 52-03 AND E.A. # : 1-5750-132310 C PART 2 STEP 2A AND STEP 2B, TITLE : WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 57501736 FOR WORK DETAILS.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PART 1, STEP 3C, AND STEP 3, THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PART 1, STEP 3C, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TOE EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3A, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3C, AND STEP 3. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3A, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3C, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349923, PART 1, STEP 3B, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349923, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349887, PART 1, STEP 3B, AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT, INBOARD BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0349887, PART 1, STEP 3A, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750- T0349884, PART 1, STEP 3A, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. WORKED THE CORROSION AND FOUND EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0349824, PART 1, STEP 3B, AND STEP 3, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, OUTBOARD BORE WAS FOUND CORRODED. THE CORROSION WAS WORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED IAW EA 1-5750-T0349884, PART 1, STEP 3A, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57- 44-09 AND EA 1-5750-T0349824, PART 1, STEP 3A, AND STEP 3. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR, INBOARD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3C, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE BRACKET, OUTBOARD LUG BORE WAS FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PART 1, STEP 3B, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750- T0349824, PART 1, STEP 3, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE LOWER MOUNT, INBOARD BORE SURFACE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PART 1, STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP, OUTBOARD HINGE FITTING OTBD LUG BORE FOUND CORRODED. CORROSION WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349824, PART 1, STEP 3C, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 84,310 hrs · 17,283 cycles

LEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE BRACKET, INBOARD LUG BORE FOUND CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0349884, PART 1, STEP 3B, AND STEP 3. THE REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SENSOR — MALFUNCTIONED (NR 8 BRAKE TEMP) · airframe 84,131 hrs · 17,228 cycles

AFTER LANDING, RECEIVED A BRAKE DIFF TEMP LVL 1 MESSAGE. BRAKE TEMP ON NR 8 WAS ABOUT 200 COOLER THAN ALL OTHER TEMPS. REMOVED AND REPLACED THE NR 8 BRAKE TEMP SENSOR IAW MM 32-46-01-4. PERFORMED A TEST OF THE BRAKE TEMPERATURE MONITOR AND TIRE PRESSURE INDICATING SYSTEM IAW MM 32-46-00-700-804. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (BLEED AIR) · airframe 82,410 hrs · 16,679 cycles

CRUZ FLT FL320.LEVEL THREE ALERT "AIR MANF #2 FAIL. QRH COMPLIED WITH,AIR SYSTEM REMAINED IN AUTO. AIR SYSTEM #2 27PSI #2 BLEED VALVE OPEN PER TECH PILOT CYCLED "PNEUM PRESS REG VLV ENG #2. PRV CYCLED #2 PNEUMATIC SYST PRESSURE LESS THAN 10PSI, LANDED NEAREST SUITABLE FIELD. SHGN 06DEC18 12:16 CAN PERFORMED WIRING CHECK FOUND THE SENSOR D1-117 SHORT TO GROUND PER WDM 36-23-02 ,REMOVED AND REPLACED THE SENSOR PER AMM 36-23-07-4, TURN THE TEST TO NEXT SHIFT. FACT 06DEC18 14:41 CAN PERFORMED FUNCTIONAL TEST OF THE MANIFOLD FAILURE SENSING ELEMENT AS PER AMM 36-23-07-5, TEST NORMAL. PERFORMED MFC RTS TEST PER AMM 36-23-01-5, TEST PASSED. PERFORMED AIR SYSTEM TEST AS PER AMM 36-23-00-5, TEST PASSED. RAN ALL THREE ENGS AS PER MD11 JRH, ALL PARAMETERS NORMAL. DMI CLOSED AND STICKER REMOVER. A/C OK FOR SERVICE.

Part: TRUCK — FAILED (LT MLG) · airframe 81,807 hrs · 16,464 cycles

ON TAXI OUT PVD FELT UNUSUAL VIBRATION WHILE TAXIING. WE SUSPECTED A FLAT TIRE ON THE RIGHT MAIN TRUCK. REMOVED AND REPLACED LT MLG TRUCK ASSEMBLY PER AMM 32-12-20-4.

Part: SLAT TRACK — CRACKED (LE SLAT) · airframe 81,125 hrs · 16,280 cycles

NR 12 RT SLAT TRACK (MOST O/B ON THE NR 5 SLAT) APPEARS TO BE CRACKED FROM L/E OF CUT OUT THROUGH 2 FASTENERS GOING AFT. INSTALLED REPAIR IN REF TO SRM 57-40-02-2R AND PRIMED AND PAINTED REPAIR IN REF TO SRM 51-21-01.

Part: SENSOR — FAILED (BRAKE TEMP) · airframe 80,538 hrs · 16,084 cycles

BRAKE DIFF TEMP, LEVEL ONE ALERT CAME ON DURING CLIMB, TIRE NR 8 WHILE READING QRH IT BECAME A LEVEL TWO BRAKE OVERHEAT WITH A TEMP OF 640 DEGREES AT FL 370. DESCENDED TO FL240, SLOWED AND LOWERED THE GEAR IAW QRH. THE TEMP BEGAN TO DECREASE, BUT THE INDICATION WENT AWAY SHORTLY THEREAFTER. REMOVED AND REPLACED THE NR 8 BRAKE TEMP SENSOR IAW AMM 32-46-01-4. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 80,380 hrs · 16,030 cycles

LVL 2 ANTI SKID L FAIL ON APPROACH, COMPLIED WITH QRH. ANTI-SKID CONTROL VALVE INOP. SYSTEM 1 BRAKE 6 DISABLED. ENSURE PENALIES ARE APPLIED. COMPLIED WITH "M" PROCEDURE. BRAKE INOP KIT INSTALLED ON NR 6 BRAKE.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

LEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 555 FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO SEAT TRACK CROWN AREA DAMAGED AT STA 5-5, RBL 8.5. 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: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 79,426 hrs · 15,721 cycles

EMPENNAGE VERTICAL STAB, UPON REMOVAL FOR ACCESS RT CENTER REAR SPAR TO REAR SPAR INTERCOSTAL AT BS 2164 FOUND CRACKED. REPAIRED AS PER EA 1-5530-T0335514, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

RIGHT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB3954, REVISION K. INSTALLED THE DOUBLER IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (LE SLAT) · airframe 79,426 hrs · 15,721 cycles

DURING BORESCOPE INSPECTION, FOUND THE RT WING NR 8 SLAT INNER RIB, XOS 1092 CRACKED. A NEW RIB WAS FABRICATED IAW DRAWING ARB1928 REVISION G. REMOVED AND REPLACED THE RIB IAW SRM 51-35-01-0G, AND EA 1-5750-T0335496, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DENTED (LT WING SLAT) · airframe 79,426 hrs · 15,721 cycles

LEFT WING NR 3 SLAT FOUND DENTED AT XOS 435.446. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 11, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (LT WING SLAT) · airframe 79,426 hrs · 15,721 cycles

LEFT WING NR 3 SLAT INNER RIB AT XOS 435.446 FOUND CRACKED. REPAIRED THE RIB IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 7, AND EA 1-5750-T0335618, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

DURING HFEC OPEN HOLE INSPECTION ON THE RIGHT WING FUEL TANK LOWER ACCESS PANEL 636AB, FOUND THREE FASTENER HOLES 10, 28 AND 34 CRACKED. REPAIRED IAW SRM 57-20-02-2R, FIGURE 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 79,426 hrs · 15,721 cycles

DURING HFEC INSPECTION AT RT FWD FLANGE LOCATED AT THE UPPER SECTION REAR SPAR CAP OF THE NR 4 BANJO FITTING OF THE VERTICAL STABILIZER, Y=2164 A CRACK WAS FOUND APPROXIMATELY 0.25 INCH LENGTH. REPAIRED IAW EA 1-5530-T0335558, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

RIGHT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 546, FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DRAWING ARB 2933, REVISION AJ, AND INSTALLED IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — CHAFED (BS 535) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 24L. THE REPAIR ANGLE WAS REMOVED IAW SRM 51-33-01-0G. A NEW REPAIR ANGLE WAS FABRICATED IAW SRM 53- 20-07-2R, FIGURE 201, REPAIR 1, AND INSTALLED IAW SRM 53-20-07-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100

Part: FRAME — CHAFED (BS 535) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO, FRAME WITH AN EXISTING REPAIR FOUND CHAFED AT BS 535, LONGERON 19L. REMOVED THE REPAIR IAW SRM 51-33-01-0G. A NEW OUTER REPAIR ANGLE, FABRICATED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE NEW REPAIR ANGLE WAS INSTALLED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

LEFT WING FIXED LEADING EDGE LOWER DOUBLER AT XOS 907 FOUND CRACKED. REPAIRED THE LEADING EDGE LOWER AREA IAW SRM 57-40-03-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 8.5. REPLACED THE SEAT TRACK FROM BS 625 TO 705, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 755) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO TRACK FOUND CRACKED AT BS 755, LBL 49. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 695, RBL 27.5. REPLACED THE SEAT TRACK FROM BS 665 TO 705 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (BS 1721) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO FRAME DENTED AT BS 1721, LONGERON 12L. REPAIRED THE FRAME IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO FLOOR SEAT TRACK FOUND CRACKED AT STA 635 X= -8.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 705, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER SNRM N00528 FOR FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 47. REPLACED THE SEAT TRACK FROM BS 625 TO 665 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 79,426 hrs · 15,721 cycles

MAIN DECK CARGO SEAT TRACK FOUND CRACKED AT BS 635, LBL 27.5. REPLACED THE SEAT TRACK FROM BS 625 TO 665, LBL 27.5 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 79,426 hrs · 15,721 cycles

LEFT HAND WING LEADING BEADED DOUBLER AT STA XOS 789 FOUND CRACKED. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED NEW DOUBLER AT LEFT HAND WING FIXED LEADING EDGE STA XOS 789 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

DURING ACCOMPLISHMENT OF HFEC INSPECTION CARRIED OUT ON LEFT WING FIXED LEADING EDGE CUTOUTS AND ACCESS DOORS. FOUND ONE CRACK, TAI DUCT CUTOUT OTBD CORNER. 0.30 INCH IN LENGTH. REPARIED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

LEFT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 653 XOS 657 FOUND CRACKED. REPAIR CARRIED OUT AT LH WING LEADING EDGE BEADED DOUBLER AT STA XOS 653 - XOS 657 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

LEFT WING LEADING FORMER AT XOS 753 FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW FORMER IAW DRAWING ARB2923, REVISION D, AND INSTALLED IAW SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

DURING ACCOMPLISHMENT OF HFEC INSPECTION CARRIED OUT ON LEFT WING FIXED LEADING EDGE CUTOUTS AND ACCESS DOORS. FOUND ONE CRACK TAI DUCT CUTOUT INBD CORNER, 0.30 INCH IN LENGTH. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

RIGHT HAND WING LEADING DOUBLER AT STA XOS 667 FOUND CRACKED. DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW DOUBLER AS PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED NEW DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE STA XOS 667 AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

RIGHT HAND WING LEADING BEADED DOUBLER AT STA XOS 543 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 543 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

DURING ACCOMPLISHMENT OF HFEC INSPECTION CARRIED OUT ON RIGHT WING FIXED LEADING EDGE CUTOUTS AND ACCESS DOORS. FOUND ONE CRACK TAI DUCT CUTOUT OTBD CORNER (CORNER NR 2) APPROX 0.50 INCH IN LENGTH. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 79,426 hrs · 15,721 cycles

RIGHT HAND WING LEADING BEADED DOUBLER AT STA XOS 643 FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING LEADING EDGE BEADED DOUBLER AT STA XOS 643 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,426 hrs · 15,721 cycles

LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 616 FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT STA XOS 616 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HOSE — FAILED (HYD PUMP) · airframe 79,000 hrs · 15,607 cycles

HYD 3 FAILED WHILE AIRBORNE 1.0 HRS, AT FL360. R & R THE NR 3 ENGINE HYD PUMP. R & R FILTER TO PYLON HOSE ASSY. DRY MOTORED ENGINE. NO LEAKS NOTED ON LT AND RT PUMPS, THE HYD LINE AND ON THE FILTERS. RAN THE NR 3 ENGINE. ALL OPS AND INDICATIONS FOR NR 3 HYD SYSTEM, CHECKED GOOD. NO LEAKS NOTED IAW MM 29-11-20-4-2 AND JRH.

Part: HOSE — CRACKED (HYD SYSTEM) · airframe 79,000 hrs · 15,607 cycles

HYD 3 FAILED WHILE AIRBORNE, 1 HR AT FL360 AT BLOCK IN, FOUND HYD FLUID COMING OUT OF NR 3 ENGINE. OPENED THE NR 3 ENGINE COWLINGS AND THRUST REVERSER IAW AMM 71-10-00-2-1. FOUND LEAK COMING FROM CASE DRAIN FILTER TO PYLON HOSE. FOUND CASE DRAIN HOSE CRACKED ON RIGID END OF LINE AT THE BEND CLOSE TO THE B-NUT. REPLACED THE NR 3 RT ENGINE HYDRAULIC PUMP IAW AMM 29-11-20-4-2. REPLACED THE LT AND RT ENGINE HYD PUMP FILTERS IAW AMM 29-12-41-2. R & R NR 3 ENGINE UPPER ENGINE HYD PUMP. DRY MOTORED ENGINE. NO LEAKS NOTED ON LT AND RT PUMP, ON THE HYD LINE AND ON THE FILTERS. RAN NR 3 ENGINE. ALL OPERATIONS AND INDICATIONS FOR NR 3 HYD SYSTEM CHECKED GOOD. NO LEAKS NOTED IAW MM 29-11-20-4-2 AND JRH.

Part: LAMP — BURNED OUT (ARM INDICATOR) · airframe 78,884 hrs · 15,570 cycles

L1 DOOR ARM & DISARM LIGHT BURNED OUT. COCKPIT INDICATION OF DOOR ARMED STATUS IS WORKING CORRECTLY. REPLACED THE LAMP, OK FOR SERVICE.

Part: INDICATOR — DEFECTIVE (R1 DOOR) · airframe 75,672 hrs · 14,590 cycles

R1 ENTRY DOOR DISARMED LIGHT FALLING APART. RESEATED R1 ENTRY DOOR DISARMED LIGHT AS REQUIRED. ACFT OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,492 hrs · 14,521 cycles

AT 600' AFTER TAKEOFF RECEIVED ENG 1 FIRE INDICATION. COMPLIED WITH QRH, SHUTDOWN ENG, & RETURNED TO BASE. NOTE TO MX, FIRE HANDLE LIGHT & FUEL SWITCH LIGHT WERE NOT ILLUMINATED WHEN COMPLYING WITH QRH PROCEDURES. TROUBLE SHOT UPPER RT FIRE DETECTOR ASSEMBLY & LOOP A & B FAULT IAW FIM 26-11-01 FIG 103. PINS J & K AT FCDU P1-1690B READS 1490 OHMS, PINS J & K AT FCDU P1-1690A READS 1473 OHMS. NO SHORTS, BOTH WITHIN LIMITS. RIGHT UPPER TURB RESPONDER, DH7 READS 10100 OHMS, NO SHORTS, WITHIN LIMITS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 75,224 hrs · 14,421 cycles

FSS DURING PREFLIGHT AT DEPARTURE WAS FULLY OPERATIONAL, AFTER LEVEL OFF IT WAS NOTED THAT POSITION 2, 3, 4, 5, 8, 9 & 11 WERE FAULTED WITH THE MSG ACCESSIBLE DANGEROUS GOODS POSITION INOPERATIVE. WRI 26-24 6635 TO BE FACTED OUT DUE TO SHORT TERM DEACTIVATION OF FSS IAW AMM 26-00-41 & EA 1-2624-T0323054 PART 1. FSS RE-DEFERRED UNDER WRI 26-95 6679. REF EA 1-2624-70323054.

Part: BUSHING — CHAFED (RT PYLON) · airframe 747 hrs · 14,238 cycles

AGEING ACFT, EXISTING REPAIR AT RT WING PYLON AFT BULKHEAD BUSHING ASSEMBLY, PN AUB7175-501, COMMON TO WHERE FORE & OR AFT EDGES OF THE SPHERICAL BEARING AREA, STATION XWN = 332. EVALUATED & FOUND CHAFED. RT WING PYLON AFT BUSHING, ONE EACH, R & R IAW AMM 54-51-02-4, EO 1-5100-7-5001 B6 PT1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: BUSHING — CHAFED (LT PYLON) · airframe 747 hrs · 14,238 cycles

AGEING ACFT, EXISTING REPAIR AT LT WING PYLON AFT BULKHEAD BUSHING ASSEMBLY, PN AUB7175-501, COMMON TO WHERE FORE & OR AFT EDGES OF THE SPHERICAL BEARING AREA, STATION XWN = 332. LT WING PYLON AFT BULKHEAD BUSHING ASSEMBLY EVALUATED & FOUND CHAFED. R & R IAW AMM 54-51-02-4, EO 1-5100-7-5001 B6 PT1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SHEAR TIE — CORRODED (B 1964) · airframe 747 hrs · 14,238 cycles

AFT CARGO BILGE FRAME SHEAR TIE FOUND WITH CORROSIONS AT STATION 1964, LONGERON 50L - 50R. CORROSION REMOVED IAW SRM 51-21-01-0G & FOUND EXCEEDED LIMIT IAW SRM 53-00-00-2R FIG 202 ORIGINAL THICKNESS 0.080", MATERIAL REMOVED 0.060", REMAINED THICKNESS 0.020". DAMAGED SHEAR TIE R & R IAW SRM 51-33-01-0G. NEW SHEAR TIE FABRICATED IAW EA 1-5310-T0321159 PT 1. REFER WRI 53106208 FOR DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, EA 1-5310-T0321159 PT 1.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 747 hrs · 14,238 cycles

CABIN, MAIN DECK CARGO COMPARTMENT AT BS 5-123, LONGERON 6L, CTR SPLICE FWD SIDE FOUND CRACKED ON X-RAY. SPLICE REMOVED IAW SRM 51-31-01-0G. SPLICE FABRICATED IAW DWG A5A7112 REV D, & INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 747 hrs · 14,238 cycles

RIGHT WING FIXED LE COMPARTMENT, BETWEEN STATION XOS 725 & XOS 731, BEADED DOUBLER FOUND CRACKED. RT WING FIXED LE COMPARTMENT CRACKED AREA REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE — WORN (CARGO DOOR) · airframe 747 hrs · 14,238 cycles

CABIN, UPPER CARGO DOOR FWD HINGE LOBES ON ACFT, SIX EACH, FOUND INSIDE DIAMETER WORN, EXCEEDED MAXIMUM PERMITTED LIMIT. CARGO DOOR, FWD HINGE LOBES HOLES REWORKED & FOUND WITHIN LIMITS IAW SRM 52-30-16-1A. EXISTING DIAMETER 0.404", EACH FINAL DIAMETER 0.460" EACH. MAXIMUM ALLOWABLE DIAMETER 0.462. REPAIR BUSHING, SIX EACH FABRICATED BY MACHINING & INSTALLED IAW SRM 52-30-16-1A, UPPER CARGO DOOR FWD HINGE FITTING REMOVED & REINSTALLED IAW AMM 20-50-02. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1300-1361) · airframe 747 hrs · 14,238 cycles

CABIN, MAIN DECK CARGO COMPARTMENT LT BS 1300 - 1361, X= 75.25, SEAT TRACK FOUND CORROSION. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1555) · airframe 747 hrs · 14,238 cycles

CABIN, MAIN DECK CARGO COMPARTMENT RT BS 1555, X= -8.5, SEAT TRACK CROWN AREA FOUND DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 747 hrs · 14,238 cycles

LEFT WING FIXED LE COMPARTMENT, BETWEEN STATION XOS 624 & XOS 629, BEADED DOUBLER FOUND CRACKED. LT WING FIXED LE EDGE COMPARTMENT CRACKED AREAS 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 747 hrs · 14,238 cycles

RIGHT WING FIXED LE COMPARTMENT, BETWEEN XOS 659 & XOS 667, 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: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 747 hrs · 14,238 cycles

DURING ACCOMPLISHMENT OF NDT INSPECTION AT STATION 5-123 TRANSVERSE SKIN, FOUND CRACK ON LONGERON 2R, CTR OF LONGERON SPLICE, BETWEEN 1ST & 2ND FASTENER. CABIN MAIN DECK CARGO COMPARTMENT CTR SPLICE REMOVED IAW SRM 51-31-01-0G. SPLICE FABRICATED BY MACHINING IAW DWG A5A7112 REV D, PN A5A7111-501 & INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 747 hrs · 14,238 cycles

RIGHT WING FIXED LE COMPARTMENT, BETWEEN XOS 765 & XOS 774, 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 747 hrs · 14,238 cycles

RIGHT WING FIXED LE COMPARTMENT, BETWEEN XOS 624 & XOS 630, 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 747 hrs · 14,238 cycles

RIGHT WING FIXED LE COMPARTMENT, BETWEEN XOS 608 & XOS 614, 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 747 hrs · 14,238 cycles

LEFT WING FIXED LE COMPARTMENT, BETWEEN XOS 756 & XOS 765, 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 747 hrs · 14,238 cycles

LEFT WING FIXED LE COMPARTMENT, BETWEEN STATION XOS 726 & XOS 732, BEADED DOUBLER FOUND CRACKED. CRACKED AREAS 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 747 hrs · 14,238 cycles

LEFT WING FIXED LE COMPARTMENT, BETWEEN XOS 682 & XOS 688, 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: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 747 hrs · 14,238 cycles

CABIN MAIN DECK CARGO COMPARTMENT, RT STATION 755, X=-8.5, SEAT TRACK CROWN AREA FOUND DAMAGED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 REPAIR 1 FROM STATION 748 - 815.5, X=- 8.5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 734 hrs · 13,833 cycles

FCC NR 1B DATA FAULT ALERT, NR 1 AUTOPILOT UNAVAILABLE. ACCOMPLISHED QRH AT ARRIVAL DEBRIEFED WITH CREW & FOUND FCC NR 1B STILL IN FAULT, WAS UNABLE TO ACCESS THE NR 1 FCC VIA CFDS. RESET BOTH CB'S OF FCC NR 1 & WAS ABLE TO ACCESS FCC NR 1. CHECKED FCC NR 1 VIA CFDS & FOUND LEG NR 1, 6 FAULTS LOGGED AT ALT 27984 FCC NR 1 AT ALT 27984. R & R FCC NR 1 IAW AMM 22-01-03-4. PERFORMED AUTO FLIGHT ADJUSTMENT TEST IAW AMM 22-00-00-5 ON FCC NR 1. ALL TESTS PASSED & AFTER ALL TESTS, CHECKED FCC NR 1 VIA CFDS & FOUND NO FAULT LOGGED.

Part: ACTUATOR — LEAKING (MLG BRAKE) · airframe 69,958 hrs · 12,806 cycles

DURING TRANSIT CHECK FOUND NR 1 MLG BRAKE OVERHEATED & HYD LEAK FROM THE BRAKE ACTUATOR RESULTED IN SMALL BRAKE FIRE & WAS EXTINGUISHED. PERFORMED THE LT SIDE LG AREA INSPECTION IAW AMM 32-40-00-06, NO ABNORMALITY FOUND. PERFORMED THE BTMTP RT SIDE TEST IAW AMM 32-46-00-5, TESTED NORMAL. R & R THE NR 1 BRAKE ASSEMBLY IAW AMM 32-43-20-4, BTMTP TESTED NORMAL. BRAKE TEMP INDICATED NORMAL R & R NR 1 MAIN TIRE ASSEMBLY IAW AMM 32-41-01-4, TIRE PRESS INDICATED NORMAL. BTMTP TESTED NORMAL, ACFT OK FOR SERVICE.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 69,952 hrs · 12,804 cycles

CABIN UNDER FLOOR AREA STATION 1239, XCW 81 CTR WING FUEL TANK SURFACE FOUND WITH CORROSION AS MARKED. CENTER WING FUEL TANK UPPER SURFACE CORRODED AREA REPAIRED AS PER FEDEX EA 1-5730-T0304398 PART 1. TITLE: WINGS - PLATES AND SKINS - CENTER WING TANK UPPER SKIN CORROSION BLENDOUT AND DOUBLER REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: FORMER — CRACKED (LT WING) · airframe 69,952 hrs · 12,804 cycles

LEFT WING FIXED LE SUPPORT FORMER AT STATION XOS 734 FOUND CRACK DURING OTBD SLAT DRIVE CABLE INSPECTION. FIXED LEADING EDGE CRACKED SUPPORT FORMER AT STATION XOS 734 REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: FORMER — CRACKED (LT WING) · airframe 69,952 hrs · 12,804 cycles

LEFT WING FIXED LE SUPPORT RIB AT STATION XOS 740 FOUND CRACK DURING OTBD SLAT DRIVE CABLE INSPECTION. FIXED LEADING EDGE CRACKED SUPPORT RIB (FORMER) AT STATION XOS 740. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 69,952 hrs · 12,804 cycles

CABIN UNDERFLOOR AREA STATION 1227, XCW 100 CTR WING FUEL TANK SURFACE FOUND WITH CORROSION AS MARKED. CENTER WING FUEL TANK UPPER SURFACE CORRODED AREA REPAIRED AS PER FEDEX EA 1-5730-T0304399 PART 1. WING PLATES AND SKINS, CENTER WING TANK UPPER SKIN CORROSION AT S-15, XCW=100, BLENDOUT AND DOUBLER REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: BUSHING — WORN (FUSEALGE) · airframe 69,952 hrs · 12,804 cycles

CABIN UPPER CARGO DOOR TO REPLACE EXISTING REPAIR BUSHING ON 16 HOLES OF LOWER DOOR JAMB BEAM, QTY 32 BUSHINGS, FITTING NR 1 4 HOLES, FITTING NR 2 3 HOLES, FITTING NR 3 1 HOLE, FITTING NR 4 3 HOLES, FITTING NR 6 2 HOLES, FITTING NR 7 3 HOLES, BUSHING REMOVED FOR NDT HOLES INSPECTION WC E9-5230-7-5000 A3 PT2. BUSHINGS FOUND WORN. INSTALLED WITH NEW REPAIR BUSHINGS (32 EACH) AS PER SRM 53-00-15 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SUPPORT FITTING — DAMAGED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN UPPER CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6, HOLE A, B, C & D DIAMETER OVERSIZED TO 0.520 INCH. REPAIR BUSHINGS FABRICATED AND INSTALLED AT BOLT HOLES 'A', 'B', 'C' AND 'D' AS PER SRM 53-00-15 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SUPPORT FITTING — DAMAGED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN UPPER CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5, HOLE B & C DIAMETER OVERSIZED TO 0.520 INCH. REPAIR BUSHINGS 02 EACH FABRICATED AND INSTALLED AS PER SRM 53-00-15 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CENTER CARGO COMPARTMENT DOOR CUTOUT UPPER JAMB FRAME SUPPORT FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-50-15 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN LT STATION 535 LONGERON 24 LT FRAME EXISTING REPAIR DOUBLER FOUND CHAFFED. DOUBLER REMOVED AND REPAIR CARRIED OUT AS PER SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN RT STATION 1310 LONGERON 26 RT, R3 DOOR AFT JAMB LOWER WEB FOUND CRACKED.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN LT STATION 1259 LONGERON 26 LT, DOOR 3 LT FWD JAMB LOWER WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN RT STATION 1259 LONGERON 26 RT, R3 DOOR FWD JAMB LOWER WEB FOUND CRACKED. WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: FRAME — DENTED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN LT STATION 535 LONGERON 19 LT FRAME FOUND WITH DENT. FRAME REPAIRED AS PER SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100 REVISION 118.

Part: SKIN — CHAFED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CENTER CARGO DOOR FWD CUTOUT STATION 1708 FUSELAGE SKIN BETWEEN LONGERON 40RT & LONGERON 41RT FOUND EXISTING BLEND OUT. FUSELAGE SKIN CARRIED OUT REPAIR AS PER FEDEX EA 1-5330-T0304376 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118. REPETITIVE INSPECTION REQUIRED, INITIAL AT 19,900 FLIGHT CYCLE AND SUBSEQUENT REPETITIVE INSPECTION AT 6,300 FLIGHT CYCLE AS PER SRM 53-00- 15 TABLE 201 REPAIR 8.

Part: FRAME — DENTED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN RT HAND STATION 1641 LONGERON 12 RT FRAME FOUND WITH DENT. FRAME REPAIRED PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPEAT INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES AS PER SRM 53- 00- 07 REPAIR 2 TABLE 201 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: FRAME — DENTED (FUSELAGE) · airframe 69,952 hrs · 12,804 cycles

CABIN RT HAND STATION 1621 LONGERON 12RT FRAME FOUND WITH DENT. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPEAT INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES AS PER SRM 53- 00- 07 REPAIR 2 TABLE 201 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: SKIN — CRACKED (RT WING) · airframe 69,952 hrs · 12,804 cycles

RIGHT WING LE LOWER ACCESS PANEL 619CB, CUTOUT INBD CORNER, FOUND CRACK AT STATION XOS 612 DURING OTBD SLAT DRIVE CABLE INSPECTION. CRACK AT STATION XOS 612 TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.

Part: VANE — DELAMINATED (TE FLAP) · airframe 69,952 hrs · 12,804 cycles

RIGHT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION AT XIFH 160 TO XIFH 187. FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 77.0 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 77.0 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 118.

Part: ENGINE — DAMAGED (LEFT) · airframe 69,280 hrs · 12,562 cycles

DURING CLIMB, EVM GMP AMBER BOX WITH 5.0., PULLED THROTTLE TO IDLE AND COMPLIED WITH QRH. ADVANCED ENG THROTTLE, COULD FEEL AND HEAR A NOTICABLE VIBRATION. RECEIVED AMBER BOX OF 4.0 AT 60 PERCENT N1 LEFT ENGINE AT IDLE FOR APPROACH AND LANDING. DURING TAIL PIPE INSPECTION, MX FOUND NUMEROUS TURBINE BLADES DAMAGED ON NR 3 ENGINE. R & R NR 3 ENGINE IAW WC 29T0303, 71T0003-GE, 71T0903-GE, 79T0203, COMPLETED 80 PERCENT ENGINE RUN AND LEAK CHECKED GOOD, NO LEAK NOTED, OPS CHECKED GOOD.

Part: RELAY — BURNED · airframe 68,968 hrs · 12,457 cycles

JUST PRIOR TO PUSH BACK, APU AUTO SHUTDOWN AND "BUS LT EMER DC OFF" MESSAGE DISPLAYED ON EAD AND SD. INTERROGATED EPCU CURRENT FAULT AND FAULTS REVIEW NO FAULTS NOTED, CHECKED C/B'S AND RCCB FOUND NO FAULTS T/S IAW FIM 24-30-04-00, STEP 1. R & R R2-5154 (CPN:0006974) IAW SWPM, NO HELP.NEED FURTHER T/S IN PROGRESS. FURTHER T/S IAW 24-30-04-00 STEP 2,3,4,5 AND 6 FOUND R2-17 RELAY WAS BURNED (TERMINAL-B2). R & R LT EMERGENCY CONTROL RLY R2-17 THEN EMERGENCY POWER TEST OK AND EPCU RTS TEST PASSED IAW AMM 24-08-01-5. RETURNED ACFT TO SERVICE.

Part: HYDRAULIC SYSTEM — UNKNOWN · airframe 68,666 hrs · 12,371 cycles

AFTER LEVEL OFF, RECEIVED A HYD 3 LEVEL OFF, CHECKED NR 3 HYD FLUID, IT WAS DECREASING RAPIDLY. SHUTOFF NR 3 PUMPS AND RMPS. FLUID KEPT DECREASING TO 0. REPAIRED WIRING INSULATION AS NEEDED IAW SWPM 20-10-01. FINSHED INSTALL OF AC 601 APU IAW WC 49T1901. OPS AND LEAK CHECK GOOD. FIRE WARNING TEST OF APU GOOD.

Part: BRACKET — BROKEN (SLATS) · airframe 68,345 hrs · 12,283 cycles

SLAT DISAGREE, 15,000 FT, SLATS EXTENDED 270 KTS HEARD LOUD BANG ALSO, NO ROLL ISSUES AT ALL AT ANY TIME. COMPLIED WITH QRH, SLAT STOW, FLAPS 0/28. ON INSPECTION, FOUND BRACKET BROKEN. INSTALLED NEW PULLEY BRACKET WITH NEW PULLEYS, ROUTED NR 1 & 2 LT SLAT CABLES AND INSTALLED CABLE KEEPERS IN BRAKE ASSY PER SMP. RECONNECTED NR 1 & 2 LT UPPER DRUM SLAT DRIVE CABLES AND RIGGED PER AMM 27-80-00-5, OPERATED SYSTEM SEVERAL TIMES AND SYSTEM OPERATING NORMALLY, ACFT IS OK FOR SERVICE.

Part: SWITCH — FAILED (L1 DOOR) · airframe 67,109 hrs · 11,930 cycles

L1 DOOR WILL NOT DISARM. R & R S1-1090 DISARM INTERLOCK SWITCH. DOOR OPS CHECKS NORMAL, REF AMM 52-11-02-2. FINAL CLOSED.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 65,136 hrs · 11,385 cycles

PILOT REPORTED EXIT COVER L1 DOOR RETAINER BROKEN , COVER DOESN'T STAY IN PLACE ABOVE THE DOOR. ADJUSTED GUIDE PINS ON LIGHT COVER IAW STANDARD MX PRACTICES, INSTALLED COVER IAW SAME, COVER IS SECURELY IN PLACE AND OPS CHECKED NORMAL THRU SEVERAL CYCLCES OF THE DOOR OPENING AND CLOSING.

Part: SKIN — CRACKED (RT WING) · airframe 64,894 hrs · 11,316 cycles

FOUND CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=713.6 AND XORS=713.6. CARRIED OUT REPAIRED IAW DWG SG1157004, REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: SKIN — CRACKED (LT WING) · airframe 64,894 hrs · 11,316 cycles

LEFT WING L/E SKIN NR 13 SLAT TRACK CUTOUT, FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02, FIG 201 REPAIR 7, REV.48. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 64,894 hrs · 11,316 cycles

BS 405, X 44 UPPER CABIN FLOOR SUPPORT FOUND CRACKED. R & R IAW SRM 51-31-01, REV 48. REPAIR CLASSFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 64,894 hrs · 11,316 cycles

FORWARD CABIN STA Y=415, STA X=52, FLOOR SUPPORT MOUNTING FOUND CRACKED. R & R IAW AMM 20-50-02, REV 70.1 NEW SUPPORT FABRICATED IAW DWG ABA 8303, REV A. REPAIR CLASSIFIED AS MAJOR IAW REV 113.

Part: SKIN — CRACKED (LT WING) · airframe 64,894 hrs · 11,316 cycles

CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTON ON LT WING LOWER SKIN ACCESS DOOR CUTOUT, BETWEEN STA XORS=683.4 AND 713.6. REPAIRED IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 64,894 hrs · 11,316 cycles

RT WING INBD FLAP OTBD SEGMENT INNER SURFACE FOUND DENTED. CARRIED OUT REPAIR IAW SRM 57-50-01, FIG 201, REPAIR 1, REV 48. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 113, AND WORK COMPLIED IAW EA1-5750-154267.

Part: SKIN — CRACKED (RT WING) · airframe 64,894 hrs · 11,316 cycles

FOUND CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT, BETWEEN STA XORS=683.4, AND STA 713.6. CARRIED OUT AND REPAIRED IAW DWG SG1157004, REV A. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100,

Part: SKIN — WORN (RT WING AILERON) · airframe 64,894 hrs · 11,316 cycles

RIGHT WING INBD AILERON SKIN AT LOWER RUB STRIP FOUND WORN. SKIN FABRICATED AND INSTALLED IAW DWG ARC1250 REV D AND IAW EA 1-5750-154260. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: SKIN — CRACKED (RT WING) · airframe 64,894 hrs · 11,316 cycles

RIGHT WING SKIN AT NR 5 SLAT TRACK LOWER CUT OUT FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: SKIN — CHAFED (LEFT WING) · airframe 64,894 hrs · 11,316 cycles

LEFT WING L/E UPPER SKIN, FOUND CHAFED. CARRIED OUT REPAIR IAW SRM 57-40-02, FIG 201, REPAIR 8, REV 48. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.

Part: PITOT TUBE — DIRTY · airframe 63,365 hrs · 10,954 cycles

F/O CADC FAIL LOST AIRSPEED INDICATION F/O SIDE. FOUND F/O'S PITOT TUBE BLOCKED BY UNKNOWN DEBRIS. DISCONNECTED PITOT TUBE AND TRIED PURGING TUBE. DEBRIS WILL NOT DISLODGE. ORDERED NEW TUBE, AWAITING PARTS. F/O'S PITOT TUBE REMOVED IAW AMM 34-11-01-2. R & R F/O'S PITOT TUBE AND PERFORMED A SATISFACTORY OPS CK, REF: AMM 34-11-01.

Part: UNKNOWN — UNKNOWN (FIRE WARNING) · airframe 59,268 hrs · 9,993 cycles

CARGO FIRE FLASHING FWD. FLOW. DISCHARGED AGENT. MASTER WARNING CONTINUED TO FLASH INTERMITTENTLY FOR 3 MINUTES. FOUND NO CURRENT OR FAULT HISTORY IN MSC. REPLACED MSC PRECAUTIONARY. RTS PASSED REF MM 31-42-01-4. NR 1 LOWER CARGO FIRE EXTINGUISHER REMOVED PER MM 26-22-01-4 R & R FWD FIREX CARGO COMPT CANTAINER AND SQUIBBS REF MM 26-22-01-4/5. R & R ALL FIVE SMOKE DETECTORS IN FWD CARGO COMPT REF MM 26-14-01-4. R & R FWD LWR CARGO OVERHEAT DETECTOR REF MM 26-14-02-4. R & R CARGO FIRE CONTROL PANEL AND PERFORMED FUNCTIONAL TEST ON THE CAGO FIRE/CONTROL PANEL AND OPERATIONAL TEST OF LOWER CARGO SMOKE DETECTORS REF MM 26-14-10-4 AND ALL TESTS PASS.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,860 hrs · 9,899 cycles

CTR CARGO DOOR FWD LWR CORNER FOUND WITH LOOSE RIVETS AS MARKED. REPAIRED IAW SRM 52-30-16 REPAIR 3, FIGURE 201, REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

RT INBD FLAP OTBD HINGE (FLAP SIDE) INBD PIVOT HOLE FOUND CORROSION. REWORKED IAW EA NR 1-5750-132282, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: FITTING — CRACKED (LT WING) · airframe 58,860 hrs · 9,899 cycles

LT LWR WINGLET AFT FITTING / SUSPECT CRACK. FITTING REMOVED AND REPLACED IAW SRM 51-33-01, REVISION 42.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP, INBD HINGE (FLAP SIDE), INBD PIVOT HOLE SPOT FACE FOUND CORRODED. REWORKED EA NR 1-5750-132317, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

RT OTBD FLAP, OTBD HINGE ACTUATOR POINT, OTBD BORE CORRODED. REWORKED IAW EA 1-5750-132312, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP, INBD HINGE (FLAP SIDE) PIVOT HOLE INBD FOUND CORRODED. REWORKED EA 1-5750-132317, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — WORN (RT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

RT OTBD FLAP INBD HINGE (WING SIDE) OTBD ACTUATOR HOLE FOUND BUSHING WORN. REWORKED EA NR 1-5750-132306, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — WORN (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP OTBD HINGE (WING SIDE) OTBD ACTUATOR HOLE FOUND BUSHING WORN. REWORKED IAW EA NR 1-5750-132307, REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — WORN (RT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

RT OTBD FLAP, INBD HINGE (WING SIDE), OTBD LWR MOUNT HOLE FOUND BUSHING WORN. REWORKED IAW EA NR 1-5750-132306, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP, OTBD HINGE/ ACTUATOR HOLE INBD BORE CORRODED. REWORKED IAW EA 1-5750-132307, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (NR 5 SLAT) · airframe 58,860 hrs · 9,899 cycles

LT WING NR 5 SLAT ASSY AFT SURFACE FOUND WITH EXISTING REPAIR. LT WING NR 5 SLAT ASSY AFT SURFACE EXISTING REPAIR EVALUATED AND FOUND NOT IAW ANY SRM REPAIR. NR 5 SLAT ASSY AFT SURFACE REPAIRED IAW EA NR 1-5740-132303, TITLE: WINGS - LT WING NR 5 SLAT AFT SKIN - REPAIR. EO NR 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - MD11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP INBD HINGE/ACTUATOR POINT OTBD BORE CORRODED. REWORKED IAW EA NR 1-5750-132308, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — WORN (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP HINGE (WING SIDE) OTBD ACTUATOR HOLE FOUND BUSHING WORN. REWORKED IAW EA NR 1-5750-132307, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP OTBD HINGE/ ACTUATOR HOLE INBD BORE CORRODED. LT WING OTBD FLAP OTBD HINGE/ ACTUATOR HOLE INBD BORE REWORKED IAW EA NR 1-5750-132307. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: FRAME — CHAFED (BS 535) · airframe 58,860 hrs · 9,899 cycles

MAIN DECK CARGO- RT STA 535, 9G NET SAFETY YOKE LWR SIDE FOUND FRAME CHAFED. REPAIR CARRIED OUT IAW EA 1-5310-132299. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 109.

Part: SKIN — MISREPAIRED (300) · airframe 58,860 hrs · 9,899 cycles

FUSELAGE - RT APU EXHAUST CUT-OUT STA 2140, LONGERON 36 RT FOUND WITH EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR AT STA 2140 RT APU EXHAUST CUT-OUT EVALUATED AND FOUND NOT IAW SRM 53-70-01 FIGURE 201 REPAIR 2, REVISION 42. REPAIR CARRIED OUT IAW EA NR 1-5310-132315, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 109.

Part: FLOORBEAM — MISREPAIRED (100) · airframe 58,860 hrs · 9,899 cycles

FWD CARGO COMPARTMENT BILGE AREA, FLOORBEAM UPPER CHORD FOUND WITH STRUCTURE REPAIR AT STA 1059, LBL 20 TO RBL 20. FWD CARGO COMPARTMENT BILGE AREA, FLOORBEAM UPPER CHORD EXISTING REPAIR AT STA 1059, LBL 20 TO RBL 20 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR. FLOORBEAM UPPER CHORD REPAIRED IAW EA NR 1-5310-132313, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (BS 888) · airframe 58,860 hrs · 9,899 cycles

EXISTING REPAIR AT FWD CARGO COMPARTMENT DOOR FWD CUTOUT, STA 888 LONGERON 38 RT TO LONGERON 39 RT. EXISTING REPAIR AT FWD CARGO COMPARTMENT DOOR FWD CUTOUT, STA 888 LONGERON 38 RT TO LONGERON 39 RT, EVALUATED AND FOUND NOT IAW ANY SRM REPAIR. REWORKED CARRIED OUT ON EXISTING REPAIR IAW SRM 53-00-15 FIGURE 202 REPAIR 8, REVISION 42. INITIAL HFEC INSP AT 12,600 FLIGHT CYCLES AND SUBSEQUENT INSP AT 6,300 FLIGHT CYCLES IAW ALI 53.10.06.1, EO 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR ID & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

RT OTBD FLAP HINGE/ ACTUATOR POINT INBD BORE CORRODED. REWORKED IAW EA NR 1-5750-132306. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

LT OTBD FLAP INBD HINGE/ACTUATOR POINT INBD BORE CORRODED. REWORKED IAW EA NR 1-5750-132308, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: FRAME — CHAFED (BS 535) · airframe 58,860 hrs · 9,899 cycles

MAIN DECK CARGO - LT STA 535, 9G NET SAFETY YOKE LWR SIDE FOUND FRAME CHAFED. REPAIR CARRIED OUT IAW EA 1-5310-132298. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 58,860 hrs · 9,899 cycles

LT WING NR 4 SLAT ASSY AFT SURFACE FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT LT WING NR 4 SLAT ASSY AFT SURFACE EVALUATED AND FOUND NOT IAW ANY SRM REPAIR. REWORKED CARRIED OUT IAW EA 1-5740-132302, TITLE: WINGS - LT WING NR 4 SLAT CHAFING AND CRACK -REPAIR. EO NR 1-5100-7-5001 A4 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 58,860 hrs · 9,899 cycles

RT OTBD FLAP INBD HINGE/ PIVOT POINT BORE CORRODED. REWORKED IAW EA NR 1-5750-132306. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: SKIN — MISREPAIRED (BS 1239 S43L) · airframe 58,860 hrs · 9,899 cycles

EXISTING DOUBLER REPAIR FOUND AT CENTER WING LOWER SKIN STA 1239, STRINGER 46, BETWEEN X = 81 AND X = 100. EXISTING DOUBLER REPAIR AT CENTER WING LOWER SKIN STA 1239, STRINGER 46, BETWEEN X = 81 AND X = 100, EVALUATED AND FOUND NOT IAW ANY SRM REPAIR. REWORKED ON EXISTING REPAIR CARRIED OUT AS PER E.A. 1-5710-132316, & E.O. 1-5100-7-5001 A4 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 109.

Part: SEAT TRACK — CORRODED (BS 1219-1259) · airframe 58,860 hrs · 9,899 cycles

MAIN DECK CARGO - APPROX FROM STA 1219-1259 X=-75 OTBD SEAT TRACK FLANGE FOUND SURFACE CORROSION. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 58,860 hrs · 9,899 cycles

MAIN DECK CARGO - R3 DOOR PLUG AFT UPPER STOP FITTING FOUND CRACKED. REPAIRED IAW EA NR 1-5210-132297, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 109.

Part: LONGERON — CORRODED (BS 1219-1429) · airframe 58,860 hrs · 9,899 cycles

UPON REMOVAL OF R3 DOOR SCUFF PLATE FOUND L-28 WITH 3 EA LOCATIONS CORROSION ON FUSELAGE FROM STA 1260-1302. CORRODED LONGERON 28 RT AT STA 1260 TO STA 1302. R & R IAW SRM 51-33-01 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: BRAKE — FIRE (MLG) · airframe 57,684 hrs · 9,621 cycles

NUMBER 10 BRAKE FIRE AT BLOCK.

Part: CABLE — OUT OF ADJUST (MLG) · airframe 57,301 hrs · 9,536 cycles

AFTER T/O MEM RT MAIN GEAR INDICATIONS IN BOTH INDICATORS, GEAR DOWN (RED). RAN QRH WHICH HAD US CYCLE GEAR DOWN THAN UP. GOOD INDICATION, ALL GEAR. PERFORMED RIG/ADJ OF RT MLG POSITION FWD CABLE IAW AMM 32-31-00-5, PERFORMED LANDING GEAR RETRACTION AND EXTENTION IAW TEST 32-31-00-700-804. ACFT RELEASED AND OK FOR SERVICE.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 54,192 hrs · 8,858 cycles

MAIN DECK CARGO AT APPROXIMATELY STATION 1229, X = 75.5 TO X = 107.50, UPPER AUX TANK UPPER SURFACE FOUND CORROSION. MAIN DECK CARGO STATION 1229, X = 75.5 TO X = 107.50, UPPER AUX TANK UPPER SURFACE CORROSION AREA CARRIED OUT REPAIR AS PER EA NR 1-5710-122539 THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. CORROSION REMOVED AS PER SRM 51-21-01, VOL.II. FOUND EXCEEDED LIMIT AS PER SRM 57-20-00, FIG 13, VOL I.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,192 hrs · 8,858 cycles

EMPENNAGE: UNDER RIGHT BODY FAIRING 347DF, SKIN FROM STATION 2150 TO 2164 FOUND SURFACE CORROSION EAR FASTENER HOLES. EMPENNAGE RIGHT HAND BODY FAIRING 347DF STATION 2150 TO STATION 2164 SKIN REPAIRED AS PER SRM 53-20-00, FIG 15 VOL I AND SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIGINAL THICKNESS = 0.100", MATERIAL REMOVED = 0.045", MATERIAL REMAINING = 0.055" AND FOUND EXCEEDED LIMITS AS PER SRM 53-00-01 FIG 2 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 54,192 hrs · 8,858 cycles

LEFT HAND WING NR 14 SLAT TRACK LOWER CUT OUT FOUND CRACKED. SKIN REPAIRED AS PER SRM 57-10-00, FIG 21 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR JAMB NR 1 FITTING REMOVED AND REPLACED AS PER SRM 51-33-01, VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. FITTING AT MAIN CARGO DOOR LOWER JAMB NR 7 REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. MAIN DECK CARGO DOOR LOWER JAMB FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 600) · airframe 54,192 hrs · 8,858 cycles

RIGHT HAND WING LEADING EDGE NR 16 TRACK INBOARD RIB FOUND CRACKED. RIGHT HAND WING LEADING EDGE NR 16 TRACK INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. RIGHT NR 8 SLAT CABLE ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-80-00-5. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES B AND D. HOLES B AND D AT MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 REPAIRED AS PER SRM 53-50-00, FIG 10, VOL I. REPAIR BUSHINGS, FABRICATED AS PER SRM 53-50-00, FIG 10, VOL I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SUPPORT — CRACKED (LT WING TE FLAP) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION, CRACK INDICATION FOUND AT OUTBOARD LOWER FASTENER HOLE COMMON TO ARC4008 AND ARC4009 SUPPORTS OF LEFT HAND SIDE WING OUTBOARD FLAP. LEFT HAND OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-00-830-805.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB NR 2 FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (DOOR FRAME) · airframe 54,192 hrs · 8,858 cycles

DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES B. FITTING AT NR 3 MAIN CARGO DOOR LOWER JAMB REMOVED AND REPLACED AS PER SRM 51-33-01, VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 49,762 hrs · 7,839 cycles

LEFT WING, LEADING EDGE NR 5 SLAT NR 12 TRACK CUT OUT FOUND CRACK. LEFT WING, LEADING EDGE NR 5 SLAT NR 12 TRACK CUT OUT REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT WING, LEADING EDGE NR 4 SLAT NR 10 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 4 SLAT NR 10 TRACK CUT OUT REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT WING, LEADING EDGE NR 7 SLAT NR 14 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 7 SLAT NR 14 TRACK CUT OUT. REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT WING, LEADING EDGE NR 7 SLAT NR 15 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 7 SLAT NR 15 TRACK CUT OUT. REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — GOUGED (ZONE 400) · airframe 49,762 hrs · 7,839 cycles

PYLON NR 3: ABOVE ENGINE DRAIN PAN APPROX STA YN230 RT LOWER PYLON SKIN FOUND WITH SEVERAL GOUGES. COMPLIED WITH FEDEX EA 1-5450-109841, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: SKIN — GOUGED (ZONE 400) · airframe 49,762 hrs · 7,839 cycles

PYLON NR 3: ABOVE ENGINE DRAIN PAN APPROX STA YN=230LH LOWER PYLON SKIN FOUND WITH SEVERAL GOUGES. COMPLIED WITH FEDEX EA 1-5450-109842, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1681 DENTED AT L- 12L. UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1681 AT L-12L REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 031191

Part: SKIN — CORRODED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, CENTER WING TANK UPPER SKIN CORRODED AT STA 1229, RBL 75. COMPLIED WITH FEDEX EA 1-5720-109840, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1701 INNER CHORD DENTED AT L-12R. UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1701 AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED. INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30 -00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311190.

Part: LONGERON — CRACKED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

CTR CARGO BILGE AREA LONGERON 43L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 43L SPLICE AT STA 1531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1701 INNER CHORD DENTED AT L- 12L. UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1701 AT L-12L REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311188.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

CTR CARGO BILGE AREA LONGERON 49R SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 49R SPLICE AT STA 1531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1661 INNER CHORD DENTED AT L- 12R. UPPER CARGO COMPARTMENT, RH SIDEWALL FRAME AT STA 1661 INNER CHORD AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30 -00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NO. 0311189.

Part: FRAME — DENTED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1761 INNER CHORD DENTED AT L-12R. UPPER CARGO COMPARTMENT, RH SIDEWALL FRAME AT STA 1761 INNER CHORD DENTED AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED. INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311193.

Part: LONGERON — CRACKED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

CTR CARGO BILGE AREA LONGERON 44L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 44L SPLICE AT STA 1531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, CENTER WING UPPER SKIN CORRODED AT STA 1229, RBL 98. COMPLIED WITH FEDEX EA 1-5720-109840. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6- 2-100.

Part: FRAME — DENTED (ZONE 200) · airframe 49,762 hrs · 7,839 cycles

FOUND UPPER CARGO COMPARTMENT, LT SIDEWALL FRAME AT STA 1641 INNER CHORD DENTED AT L-12L. UPPER CARGO COMPARTMENT, LH SIDEWALL FRAME AT STA 1641 AT L-12L. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14500 CYCLES AND THEREAFTER 9500 CYCLES, INSPECTION TO BE CARRIED OUT AS PER SRM 53-30 -00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. ITEM TRANSFERRED TO OPEN ITEMS LIST CONTROL NR 0311192.

Part: LONGERON — CRACKED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

CTR CARGO BILGE AREA LONGERON 41L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 41L SPLICE AT STA 1531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

CRACK FOUND AT STRINGER END 20R (XORS 152), APPROX 10" LENGTH ON RT WING TANK, DURING HFEC INSPECTION. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

CENTER CARGO RT TUNNEL AREA, LONGERON 38R SPLICE AT STA 1531 SUSPECTED CRACKED CENTER CARGO RT TUNNEL AREA, LONGERON 38R SPLICE AT STA 1531. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT HAND WING TANK - APPROX 13 INCHES CRACK FOUND AT STRINGER END 13R (XORS 577) DURING HFEC INSPECTION STRINGER END 13R (XORS 577)AT RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: VANE — DELAMINATED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT HAND WING - INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED COMPLIED WITH FEDEX EA 1-5750-109837, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 49,762 hrs · 7,839 cycles

NOSE LANDING GEAR, RT TRUNNION FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5310-105635. STOP DRILL DEVIATION FROM SRM AND SRM 53-40-00 FIG. 22 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT WING TANK, APPROX 3/4 INCHES CRACK FOUND AT STRINGER END 44R (XORS 253) DURING HFEC INSPECTION. REPAIR CARRIED OUT AS PER SRM 57- 20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: VANE — DELAMINATED (TE FLAP) · airframe 52,995 hrs · 10,937 cycles

LEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. (SUPPLEMENTAL 28 MARCH 07) COMPLIED WITH FEDEX EA 1-5750-105636, REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT HAND WING TANK - APPROX 15.5 INCHES LENGTH CRACK FOUND AT STRINGER END 14R (XORS 521) DURING HFEC INSPECTION STRINGER END 14R (XORS 521)AT RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 49,762 hrs · 7,839 cycles

RIGHT HAND WING TANK - APPROX 13 INCHES CRACK FOUND AT STRINGER END 12R (XORS 642) DURING HFEC INSPECTION STRINGER END 12R (XORS 642) RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 49,762 hrs · 7,839 cycles

FOUND CENTER CARGO RT TUNNEL AREA, LONGERON 37R SPLICE AT STA 1531 SUSPECTED CRACKED CENTER CARGO RT TUNNEL AREA LONGERON 37R SPLICE. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 49,762 hrs · 7,839 cycles

LT WING TANK - APPROX 12 INCHES LENGTH CRACK FOUND AT STRINGER END 14L (XORS 521) DURING HFEC INSPECTION STRINGER END 14L (XORS 521) AT LT WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 49,762 hrs · 7,839 cycles

NOSE LANDING GEAR, LT TRUNNION FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5310-105634. STOP DRILL DEVIATION FROM SRM AND SRM 53-40-00 FIG. 22 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 49,762 hrs · 7,839 cycles

LT WING TANK - APPROX NINE (9) INCHES LENGTH CRACK FOUND AT STRINGER END 11L (XORS 704) DURING HFEC INSPECTION STRINGER END 11L (XORS 704)AT LT WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 49,762 hrs · 7,839 cycles

LEFT WING TANK, APPROX 1/2 INCH LENGTH CRACK FOUND AT STRINGER END 40L (XORS 747), DURING HFEC INSPECTION. (SUPPLEMENTAL 28 MARCH 07) STRINGER END 40L (XORS 747) ON LHW TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: FRAME — DENTED (BS 5-0) · airframe 44,493 hrs · 6,626 cycles

MAIN DECK CARGO COMPARTMENT FRAME FOUND DENT AT LEFT STA 5-0, LONGERON 11L. REPAIRED AS PER SRM 53-30-00.

Part: FRAME — DENTED (BS 1661) · airframe 44,493 hrs · 6,626 cycles

MAIN DECK CARGO COMPARTMENT, FRAME FOUND DENT AT LEFT STA 1661, LONGERON 12L. CARRIED OUT REPAIR AS PER SRM 53-30-00.

Part: SKIN — CHAFED (FUSELAGE) · airframe 44,493 hrs · 6,626 cycles

LOWER FUSELAGE, FORWARD CARGO DOOR CUT-OUT AFT LOWER SIDE BETWEEN LONGERON 40R AND 41R, FOUND CHAFED SKIN = ABA7030-1. CARRIED OUT REPAIR AS PER SRM 53-50-00.

Part: STRUCTURE — CRACKED (BS 1721) · airframe 44,493 hrs · 6,626 cycles

CENTER CARGO COMPARTMENT, BILGE AREA AT STA 1721 LONGERON SPLICE 50R FOUND CRACKED. REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 44,493 hrs · 6,626 cycles

MAIN DECK CARGO COMPARTMENT, NR 3 SEAT TRACK COUNTED FROM MOST LEFT, FOUND CRACKED AT STA 635. REPAIRED IAW SRM 53-70-00.

Part: STRUCTURE — CORRODED (BS 1110) · airframe 44,493 hrs · 6,626 cycles

CAC COMPARTMENT INTERIOR, BILGE LOCATION AT STA 1110, LONGERON 51L, FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-10-00.

Part: PSEU — DEFECTIVE (ZONE 700) · airframe 39,918 hrs · 5,593 cycles

GEAR UNSAFE ON PRIMARY AND SECONDARY INDICATIONS WITH LANDING GEAR UP. RIGHT MAIN LANDING GEAR DOOR LINK AND BRACKET ASSEMBLY ADJUSTMENT/TEST CARRIED OUT AS PER AMM 32-34-05-5. PROXIMITY SWITCH ELECTRONICS UNIT REMOVED & REPLACED, OPERATIONAL TEST CARRIED OUT AS PER AMM 31-71-01-2. FOUND SATISFACTORY. LANDING GEAR RETRACTION CARRIED OUT AS PER AMM 32-31-00-5. FOUND SATISFACTORY. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-598-03, POS ONL SRL 42, TAG 578968, ON MFG 8-598-03, SRL C269, TAG 542239.

Part: TARGET — BROKEN (ZONE 700) · airframe 39,915 hrs · 5,591 cycles

RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED PRIMARY AND SECONDARY WITH GEAR UP. PERFORMED QRH PROCEDURE AND RESTRICTED SPEED TO 230 KTS. ON POSTFLIGHT FOUND TARGET BROKEN. REMOVED AND REPLACED RT MLG TARGET AS PER AMM 32-34-05-4. PROXIMITY SENSOR & THE TARGET ASSY ADJUSTMENT CARRIED OUT AS PER AMM 32-61-15-820-001. CARRIED OUT RIGHT MLG DOOR LINK AND BRACKET ASSEMBLY ADJUSTMENT/TEST AS PER AMM 32-34-05-5, FOUND SATISFACTORY. CARRIED OUT LANDING GEAR EXTENSION/RETRACTION ADJUSTMENT/TEST AS PER AMM 34-31-00-5 AND FOUND SATISFACTORY.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 39,913 hrs · 5,589 cycles

TAIL TANK - NR 28L BARREL NUT BORE CORROSION REMOVAL EXCEEDED LIMIT. COMPLIED AS PER FEDEX EA 1-5510-76711 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - AD 2003-22-08.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 39,913 hrs · 5,589 cycles

UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 FOUND DAMAGED. UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 CARRIED OUT REPAIR ON DAMAGED AREA AS PER SRM 53-30-00 VOL I FIG 1. FOR REPETITIVE INSPECTION TRACKING, REFER TO FEDEX EA 1-5310-75963 - FUSELAGE - MAINFRAME - TRACKING OF CATEGORY B REPAIRS ON FRAME.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. ORIGINAL THICKNESS =0.468 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.466 INCH.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2. ORIGINAL THICKNESS =0.430 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.428 INCH.

Part: SEAT TRACK — DENTED (FUSELAGE) · airframe 39,913 hrs · 5,589 cycles

MAIN CARGO DECK STA 810 LEFT HAND SEAT TRACK REF X=27.5 SEAT TRACK DENTED. DENTED SEAT TRACK AT MAIN CARGO DECK STA 810 LEFT HAND SIDE X=27.5 REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR I/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH, AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCH, AND REPAIRED AS PER EA 1-5740-75958 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCH, AND REPAIRED AS PER EA 1-5740-75958 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD O/B FLAP I/B HINGE SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PG 402-407, ORIG THK 0.382 INCH, MATERIAL REMOVED 0.002 INCH, REMAINING THK 0.380 INCH AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR O/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221 INCH, AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: ACTUATOR — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.401, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.400 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: ACTUATOR — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.514, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.513 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH AND REPAIRED AS PER FEDEX EA 1-5740-75955 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.500 MATERIAL REMOVED: 0.008 REMAINING THICKNESS: 0.492 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: ACTUATOR — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. I/B ACTUATOR LUG HOLE REMOVED CORROSION AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: ACTUATOR — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.403 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.003, REMAINING THICKNESS 0.402. REPAIRED AS PER EA 1-5750-75954 - WINGS LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.093 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.094 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.500, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.498 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221, AND REPAIRED AS PER EA 1-5740-75956, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.502 MATERIAL REMOVED: 0.002 REMAINING THICKNESS: 0.500 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHEET 2. ORIGINAL THICKNESS =0.406, MATERIAL REMOVED =0.003, AND REMAINING THICKNESS =0.403.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.223 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.505, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.503 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.487 MATERIAL REMOVED: 0.003 REMAINING THICKNESS: 0.484 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.502, MATERIAL REMOVED 0.004, REMAINING THICKNESS 0.498 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHEET 2. ORIGINAL THICKNESS =0.476, MATERIAL REMOVED =0.002, AND REMAINING THICKNESS =0.474.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE O/B ACTUATOR LUG HOLE CORROSION. REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH AND REPAIRED AS PER FEDEX EA 1-5740-75955 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.127 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.405 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.095 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.397 MATERIAL REMOVED: 0.001 REMAINING THICKNESS: 0.396 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.503 MATERIAL REMOVED: 0.002 REMAINING THICKNESS: 0.501 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.222, AND REPAIRED AS PER EA 1-5740-75956. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2 AND CMM 57-44-09. ORIGINAL THICKNESS =0.446 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.444 INCH.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIG DIA 1.062 INCH, FINAL DIA 1.189 INCH AND REPAIRED AS PER FEDEX EA 1-5750-74315 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 39,913 hrs · 5,589 cycles

LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.391 MATERIAL REMOVED: 0.002 REMAINING THICKNESS: 0.389 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.410 MATERIAL REMOVED: 0.004 REMAINING THICKNESS: 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.405 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,913 hrs · 5,589 cycles

RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.094. REPAIRED AS PER EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: STOP FITTING — CRACKED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

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

Part: STOP FITTING — CRACKED (T/E FLAP) · airframe 39,913 hrs · 5,589 cycles

LT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED DAMAGED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LT WING O/B FLAP AS PER SRM 51-33-01 VOL II.

Part: RIB — CRACKED (LT WING) · airframe 39,913 hrs · 5,589 cycles

LT WING SLAT TRACK 16 I/B RIB FOUND CRACKED. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II & INSTALLED NEW RIB AT LT WING SLAT TRACK NR 16 AS PER SRM 51-33-01 VOL II.

Part: HINGE — CORRODED (ZONE 600) · airframe 39,472 hrs · 5,486 cycles

RIGHT WING OUTBOARD FLAP, INBOARD HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.