N586FE

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 93,365 hrs · 22,321 cycles

DURING EMERGENCY LIGHT PREFLIGHT TEST, LEVEL ONE EMER LT BAT 1 LO MEL 19AUG22 03:20 MEM U RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 29AUG22 "MEL 33-50-04: EMER LIGHTS - INOP." . C/7329674

Part: BOLT — WORN · airframe 92,990 hrs · 22,226 cycles

AFTER TAKEOFF THE LEFT MAIN GEAR INDICATOR WAS RED. WE CHECKED THE CONFIG PAGE WHICH SHOWED RED AS WELL. WE FOLLOWED THE QRH PROCEDURE BUT THE GEAR STILL SHOWED RED ON BOTH INDICATIONS. SHORTLY AFTERWARDS THE GEAR SUDDENLY SHOWED ALL SAFE AND WE CONTINUED THE FLIGHT THIS WAS AT 245 KNOTS INDICATED AND AT FL200 REMOVE AND REPLACED BOLT AND BUSHING IN LEFT M.L.G. DOOR LINK ASSY. AS PER MD-11 M/M 32-34-05-4, TESTED GOOD AS PER MD-11 M/M 32-34-05-5, O.K. FOR SERVICE.

Part: FIRE DETECTOR — BROKEN (A & B SYSTEMS) · airframe 92,143 hrs · 21,996 cycles

1:30 INTO FLIGHT RECEIVED LEVEL 1 FIRE DET 3 FAIL. REMOVED AND REPLACED #3 ENG FDCU, NO HELP ORIGINAL UNIT REINSTALLED. IAW AMM 26-11-02-4. TROIUBLESHOT PER MD11 FIM 26-11-00-2 AND WDM 71-51-11 FOUND LOWER TURBINE 'A' AND 'B' LOOPS RESISTANCE OUT OF LIMITS HIGH. FURTHER TROUBLESHOOTING FOUND BOTH 'A' AND 'B' LOWER TURBINE LOOPS BROKEN. R&R #3 ENG LWR FIRE DETECTOR LOOP ASSY, NEEDS OPS CHECK REF MD11 MM 26-11-03-4-1. ACCOMPLISHED TASK THROUGH STEP 3E(4). CONTINUE AT STEP 3E(5). FACT 04FEB22 22:29 IND U CONTINUED WITH R&R OF #3 ENGINE FIRE LOOP AT STEP 3.E.(5) TO COMPLETION PER MD-11 AMM 26-11-03-4-1 AND 26-11-02-5. OPS CHECK GOOD, NO FURTHER FAULTS NOTED.

Part: NONE — FAILED (N/A) · airframe 92,057 hrs · 21,966 cycles

ABOVE 10 K FEET . RECEIVED A RED U/L REVERSER LIGHT NR 1 ENG. ACCOMPANIED BY SIGNIFICANT VIBRATIONS. SHUTDOWN ENG IAW QRH. ON LANDING, LIGHT TURNED TO AMBER. EMERGENCY DECLARED RTB ON INSPECTION OF # 1 THRUST REVERSER, FOUND O/B CENTER DRIVER UNIT BRAKE HANDLE NOT IN STOWED. STOWED BRAKE HANDLE & CARRIED OUT WINDMILL INSP IAW AMM 72-00-05-200-831. NO DISCREPANCIES NOTED. R & R ENG 1 L/H CDU. RIG/OPS CK OK.

Part: NONE — DELAMINATED (ZONE 300) · airframe 92,043 hrs · 21,958 cycles

REWORK N00507; CORRECTIVE ACTION REQUIRES REPORTABLE DISCREPANCY REPORT (RDR) PER ITEMS 3,5,6 (RDR REVISED 8-23-21) AND SERVICE DIFFICULTY REPORT ITEM 13,14 (GMM REVISION 177) REMOVED AND REPLACED LOWER AFT RUDDER REF AMM 27-20-20-4.

Part: NONE — DELAMINATED (ZONE 300) · airframe 92,043 hrs · 21,958 cycles

REWORK N00508; CORRECTIVE ACTION REQUIRES REPORTABLE DISCREPANCY REPORT (RDR) PER ITEMS 3,5,6 (RDR REVISED 8-23-21) AND SERVICE DIFFICULTY REPORT ITEM 13,14 (GMM REVISION 177) REMOVED AND REPLACED LOWER AFT RUDDER REF AMM 27-20-20-4.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

CTR CARGO, L/H SIDE ROLLER TRAY EXFOLIATED AT APPROX STA. 1600 APPROX LBL 48. REMOVED AND REPLACED CENTER CARGO LEFT HAND ROLLER TRAY STA. 1600, LBL 48. REF MD11 SRM 51-30-01-0G, DWG AFJ7065.

Part: SEAT TRACK — CORRODED (BS 1801) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO COMPARTMENT , CORRODED SEAT TRACK LOBES AT STATION 1801 RBL70 REMOVED AND INSTALLED NEW SEAT TRACK AND SPLICE AT STA 1801 RBL70 MAIN DECK REF SRM 51-41-01-0G FIG.7, SRM 53-00-52-2R FIG. 201, SRM 51-33-01-0G, AND SRM 51-31-01-0G "MAJOR REPAIR"

Part: NONE — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO - STA 1902 R/H SIDE - SIDEWALL PANEL VERTICAL STANCHION HAS CORROSION ON LOWER SECTION I/B SIDE (MARKED) REMOVED AND REPLACE SIDE WALL PANEL VERTICAL STANCHION AT STA 1902 REF SRM 51-31- 01-OG

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO - STA 1781, RBL 107 - SEAT TRACK HAS 2 FLOOR BOARD ATTACH LOBES CORRODED. (VIEWED FROM CENTER CARGO ABOVE CEILING, MARKED) 0005202340 : LEMUS, JOSE H - 14-DEC-2021 17:00 REPAIRED SEAT TRACK PER SRM 53-00-52-2R REPAIR 1 FIG. 201 SHEETS 1-3, SRM 51-33-01-0G, SRM 51-21-01-OG, AND DWG SR10-53-002.SRM 51-41-01-OG.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO - R/H SIDE - SHEAR TIE HAS CORROSION AT STA 1902 BETWEEN LONGERON 42 & 43 REMOVED, FABRICATED AND INSTALLED SHEAR TIE (P/N: AGA7009-7) AT STA 1902 BTWN L-42 AND L-43 RHS REF, DOUGLAS DWG AGA7009 AND MD11 SRM 51-31-01-0G.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 92,043 hrs · 21,958 cycles

RH WING INBD FLAP VANE LOWER SURFACE BETWEEN CTR AND OUTBD TRACK HAS IMPACT DAMAGE REPAIRED R/H WING INBD FLAP VANE LOWER SURFACE, IMPACT DAMAGE REF. SRM 57-50-80-2R REPAIR 2, PER SRM 51-62-01-0G PAR. 10F.

Part: LONGERON — CORRODED (BS 1887 L40R) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO PIT AT STA.1887 RHS LONGERON 40 IS CORRODED BEYOND LIMITS (MARKED) REMOVED CORRODED LONGERON AT STA 1887 RHS L-40 AND REPAIR PER MD11 SRM 53-00-05- 2R 201. AND MD11 SRM 53-00-01-2R FIG 201 SHEET 10. SEE JPF FOR DETAILS. "MAJOR REPAIR"

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CGO COMPARTMENT, STA 1841-STA 1967, RBL20, SEAT TRACK CORROSION ON MULTIPLE AREAS. AFT CARGO STA. 1841-1967 RH REMOVED AND REPLACED SEAT TRACK IAW DOUGLAS DWG. AGA3855.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 92,043 hrs · 21,958 cycles

UPPER MAIN DECK FLOOR BOARD PANEL (271BF)STA. 1321 LBL-50 REQUIRES FABRICATION. REMOVED AND REPLACED MAIN DECK FLOOR BOARD PANEL (271BF) STATION 1321 LBL50 REF FEDEX DWG SRZ-25-005.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO RH STA. 1954 BELOW FLOOR PANEL 187HF OUTBOARD RAIL (REF. AGA3857-508) HAS EXFOLATION CORROSION EXISTS IN 2 LOCATION APROX. 2.00 X 1.00 AND 1.50 X 1.25. REMOVED AND REPLACED FLOOR SUPPORT RAILPER DWG. AGA3857-508

Part: SUPPORT — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO RH STA. 1954 BELOW FLOOR PANEL 187HF OUTBOARD RAIL (REF. AGA3857-508) HAS EXFOLATION CORROSION EXISTS IN 2 LOCATION APROX. 2.00 X 1.00 AND 1.50 X 1.25. REMOVED AND REPLACED FLOOR SUPORT PER DWG AGA 3857

Part: NONE — DELAMINATED (ZONE 600) · airframe 92,043 hrs · 21,958 cycles

R/H WING, UPPER SURFACE, PANEL ARC7163 JUST FWD OF SPOILERS #4  APPEARS TO BE DELAMINATED. BULGING AND SEVERAL FASTENERS PULLING THROUGH PANEL. PERFORMED REPAIR ON ARC7163 FWD OUTBOARD CORNER DELAM AREA PER SRM 51-62-01- 0G PAR 10A, 10F. AND SRM 57-50-80-2R PG 41-42

Part: FLOORBEAM — CORRODED (BS 1741) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STATION 1741, RBL-49 TO RBL-71. REMOVED AND REPLACED SUPPORT AFA3853-20 REF DAC DWG NFA6398 AND SRM 51-31-01-OG. "MAJOR REPAIR"

Part: SEAT TRACK — CORRODED (BS 1675) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO COMPARTMENT, APPROX. STATION 1675, RBL-48 SEAT TRACK FLANGE EXFOLIATING AROUND THE HOLE FOR CLIP-NUT. REPAIR DAMAGED SEAT TRACK REF SRM 53-00-52-2R FIG. 201 REPAIR 5.

Part: FLOORBEAM — CORRODED (BS 1256) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STATION 1256, RBL-90 TO RBL-106. REMOVED AND REPLACED SUPPORT AEA0395-2 REF DAC DWG NEA6398 AND SRM 51-31-01-OG. "MAJOR REPAIR"

Part: FLOORBEAM — CORRODED (BS 1256) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK FLOOR SUPPORT CORRODED AT STATION 1256, RBL-77 TO RBL-86.5 REMOVED AND REPLACED SUPPORT AEA0410-2 REF DAC DWG NEA6398 AND SRM 51-31-01-OG. "MAJOR REPAIR"

Part: SUPPORT — CORRODED (ZONE 600) · airframe 92,043 hrs · 21,958 cycles

R/H WING REAR SPAR SUPPORT-UPPER O/B IDLER, ARB0042-2 IS CORRODED REMOVED AND REPLACED ARB0042-2 SUPPORT PER DAC DWG ARB0042.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO DECK, FLOOR PANEL SUPPORT CORRODED AT STA. 979 BETWEEN RBL 75-107 REMOVED AND REPLACED FLOOR SUPPORT P/N ADA 3615-73 AT STA 979 RBL 90 REF SRM 51- 33-01-OG, DAC DWG ADA 3615

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN STA. 939 LBL "8.00 REFERENCE FLOOR BOARD 245FF, EXFOLIATION CORRISION EXIST APPROX. DIMENSIONS "2.00 X '1.00 ON SEAT TRACK. REMOVED AND INSTALLED SEAT TRACK AND SPLICES PER SRM 51-41-01-0G, FIG 7 SRM 53-00- 52-2R,FIG 201, SRM 51-33-01-0G.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN APPORX. STA 1480-1600, RBL 92 FLOOR BOARD FASTNER GROMMETS CORRODED. FABRICATED NEW MAIN DECK FLOOR PANEL AT STA 1480 - STA 1600 RBL 92 PER FEDEX DRAWING SRZ-25-005.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO DECK, STA 1661 RBL 48-72 FLOOR SUPPORT CORRODED REMOVED AND REPLACED FLOOR SUPPORT AFA3853-24 REF DAC DWG NFA6018 AND SRM 51- 31-01-OG.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING FRAME (BETWEEN PANELS 152LT/152KT) - CRACK STA. 5-113 BTW L28-L29 FABRICATED AND INSTALLED NEW ANGLE REF DWG# A5A7064.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152LT/152KT) - CRACK AT INBD ANGLE STA. 5- 113 BETWEEN L36-L37. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG A5A7064.

Part: SKIN — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

LHS AFT FUSE CANT SKIN AT APPROX STA2128-STA2164, L32L TO L35L HAS EXFOLIATED CORROSION. REPAIRED LHS AFT FUSE CANT SKIN STA 2128-ST A2164 L33L TO L35L PER SRM 53-70-01-2R FIG .202. SHEET 1,2,AND 5

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO AFT DOOR JAMB - STA 1959, STR 40 - INTERCOSTAL CARCKED P/N AGA7211-21 (REMOVAL AND INSTALLATION ON N1196)

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO DOOR JAMB - AFT SIDE STA 1959, BETWEEN L40 - L45 HAS INTEGRANULAR CORROSION IN SEVERAL PLACES ON FWD SIDE OF FRAME INSTALLED NEW FRAME P/N: AGA7202-501 REF MD-11 SRM 51-33-01-0G, SRM 51-35-01-0G, AND DRAWING AGA7202, NGA6084. MAJOR REPAIR.

Part: SUPPORT — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK AT STA 1911 RBL 85-60 FLOOR PANEL SUPPORT BRACKET DAMAGED (MARKED) REMOVED AND REPLACED FLOOR SUPPORT AGA7079-1 REF DAC DWG AGA7127 AND SRM 51-31- 01-OG. "MAJOR REPAIR"

Part: SUPPORT — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN STA 1501 RBL 12 FLOOR SUPPORT HAS CORROSION.(REF NR 572 FOR FABRICATION OF SUPPORT). REMOVED AND REPLACED FLOOR SUPPORT AEA0409-1 REF DAC DWG NEA6018 AND SRM 51-38- 01-OG PARAGRAPH 5B.

Part: SKIN — UNKNOWN (ZONE 500) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: L/H WING, FIXED LEADING EDGE UPPER SURFACE AT STA. XIS 247 HAS AN EXISTING EXTERNAL REPAIR DOUBLER, APPROX. 9"X 11". DOT 52 REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-02 NFIG. 201 REPAIR 8. REFERNCE E.A. 1- 5100-T0363904 "STRUCTURES-REPAIR CATALOG-MD11 REPAIR ID" ATTACHMENT A-1 #52. "MAJOR REPAIR"

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO - CENTER SHEAR-TIE AFT SIDE OF FRAME STA 1967 SHOWS SIGN OF EXFOLIATED CORROSION.(MARKED) REMOVED AND REPLACED SHEAR TIE PER DWG AGA7134 AND SRM51-33-01-OG.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT FUSELAGE (TAIL CONE) BULKHEAD, STA Y 2163, LOWEST STIFFENER CRACKED AT RHS OUTBD EDGE. 0004002951 : RODRIGUEZ, HECTOR - 08-NOV-2021 06:52 INSTALLED STIFFENER AND SUPPORT -19 ON LOWER R/H SIDE OUTBOARD EDGE OF AFT FUSELAGE BULKHEAD (TAIL CONE) AT STA 2163 REF MD-11 SRM 53-80-02-2R FIG 201,SHEET 7.

Part: LONGERON — CORRODED (N/A) · airframe 92,043 hrs · 21,958 cycles

CAC COMPARTMENT LONGERON L51 (PART # AAA7086-1) CORRODED. REMOVE AND REPLACE LONGERON AAA7086-1 REF DWG NAA6754 AND SRM 51-31-01-OG.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO FLOOR PANEL AT STA 759 LBL75-759 IS DAMAGED (MARKED) FABRICATED NEW MAIN CARGO DECK FLOOR PANEL AT STA 759 LBL 75-759 PER FEDEX DRAWING SRZ-25-005

Part: SKIN — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

AFT FUSELAGE - ZONE 312 - UPPER AFT R/H FUSELAGE APROXIMATE STA 2163 TO 2092, STRINGER 11R TO 13R CORROSION PRESENT. AFT FUSELAGE ZONE 312 UPPER AFT R/H FUSELAGE STA 2163.685 TO 2069.440, STRINGER 11R TO 13R CORROSION REPAIR PERFORMED IAW EA 1-5330-T0365138 PART 1 " FUSELAGE-PLATES & SKINS- FUSELAGE AFT BODY SECTION-SKIN PANEL AJC7058-2 - REPAIR" *MAJOR REPAIR* SEE JPF.

Part: SKIN — UNKNOWN (ZONE 300) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: REPAIR DOUBLER FOUND ON RH SIDE UPPER SKIN PANEL OF #2 ENGINE NACELLE. DOT 151 REPAIR WAS PREVIOUSLY INSTALLED PER E.A. 1-5480-T0300648 C "NACELLE /PYLON- FILLET/FAIRINGS-LOWER VERTICAL STAB PANEL" REF. E.A. 1-5100-T0363904 'STRUCTURES- REPAIR CATALOG-MD11 REPAIR IDENTIFICATION" ATTACHMENT A-1 #151. "MAJOR REPAIR"

Part: RUDDER — CORRODED (ZONE 300) · airframe 92,043 hrs · 21,958 cycles

REMOVE UPPER FWD RUDDER F.O.M. 0000575467 : WRAY, BASIL P. B. - 05-JAN-2022 22:23 REMOVED AND INSTALLED SERVICEABLE UPPER FWD RUDDER MPN: NMC6017-529 S/N: 239644 PER AMM 27-20-30-4, 4A-4E, 5A-5H. 0000383059 : FAROOQUI, MOHAMMAD Z - 06-JAN-2022 14:48 VARIFIED ALL ACC COMPLETED WORK ON JPF

Part: RUDDER — CORRODED (ZONE 300) · airframe 92,043 hrs · 21,958 cycles

NEED TO REMOVE UPPER AFT RUDDER FOM. 0000575467 : WRAY, BASIL P. B. - 05-JAN-2022 21:21 REMOVED AND INSTALLED SERVICEABLE UPPER AFT RUDDER MPN: NMC6019-505, S/N: 48406 PER AMM 27-20-30-4 1.A.-3.H.

Part: FRAME — CORRODED (BS 1921-1964) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO - DURING PERFORMING CORROSION REMOVAL OF LWR CLOSE OUT WEB FITTING ABOVE LATCH SPOOLS, FOUND ZEE FRAME P/N AGA7195-3Z HEAVILY CORRODED, REQUIRES NEW ZEE FRAME TO BE FABRICATED FABRICATED NEW ZEE FRAME AGA7195-3 PER DOUGLAS DRAWING AGA7195, MD11 SRM 51-33- 01-0G. INSTALLATION ACCOMPLISHED ON N694. MAJOR REPAIR.

Part: PAINT — DETERIORATED (RT ELEVATOR) · airframe 92,043 hrs · 21,958 cycles

RIGHT OUTBOARD ELEVATOR; UPPER SURFACE PAINT DETERIORATED. PREPPED AND PAINTED R/H O/B ELEVATOR PER SRM 51-21-02-0G

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 92,043 hrs · 21,958 cycles

R/H OUTBOARD ELEVATOR SKIN FOUND TO HAVE DAMAGED/MISSING STATIC MESH AND LAMINATIONS REPAIRED R/H ELEVATOR I.A.W. SRM 51-21-05-2R REPAIR#1 FIG.201 STEPS 1-7.

Part: BRACKET — CORRODED (AFT CARGO) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO AT FWD LWR DOOR CUTOUT LWR JAMB BRACKET IS CORRODED BEYOND LIMITS. INSTALLED NEW BRACKET P/N: AGA7226-1 REF MD-11 SRM 51-33-01-OG, AMM 20-50-02-2 TABLE 204, AND DRWG AGA7226. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 2163-2140) · airframe 92,043 hrs · 21,958 cycles

FUSELAGE: AFT FUSELAGE RH HORIZONTAL CUT-OUT BETWEEN STA 2163 - 2140. FUSELAGE SKIN SHOWING HEAVY CORROSION/EXFOLIATION IN SEVERAL AREAS. WHERE THE LOWER EDGES OF THE FUSELAGE FAIRING ATTACHES TO THE FUSELAGE SKIN. (ABOVE APU EXHAUST) AREA MARKED RED 0000675378 : DUONG, KEVIN - 17-DEC-2021 22:52 REPAIRED PER E.A. 1-5330-T0365166 P1 BY AMT 3748737 0000675378 : DUONG, KEVIN - 17-DEC-2021 23:01 *MAJOR REPAIR* REPAIRED PER E.A. 1-5330-T0365166 P1. FUSELAGE - PLATES & SKIN - FUSELAGE AFT BODY SECTION - SKIN PANEL AJC7060-2 - REPAIR. WORK PERFORMED BY AMT 3748737 0000883981 : SANZ, NELSON D - 17-DEC-2021 23:13 INSPECTED AND ACCEPTED

Part: SKIN — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: LOWER FWD FUSELAGE LH SIDE. EXISTING REPAIR DOUBLER FOUND AT #1 AIR-CONDITIONING EXHAUST VALVE DOOR UPPER AFT CORNER. STA.587. INCORRECT SRM REPAIR INSTALLED. (REF. W.O. 35548, NR N00173). REMOVED AND INSTALLED NEW/FABRICATED REPAIR DOUBLER, TRIPLER AND FILLER AND INTERNAL DOUBLER REF, MD11 SRM 53-20-15-2R FIG 201 REPAIR 3.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN APPROX STA 1520-1530 RBL 48 SEAT TRACK LOBES NICKED/BURRED

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152KT/152JT) - CRACK AT INBD ANGLE STA.5-53 BETWEEN L44-L45. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG A5A7064.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152NT/152LT) - CRACK AT INBD ANGLE STA.1581 L39. CRACK CONFIRMED WITH NDT HFEC. REMOVED AND REPLACED FAIRING SUPPORT RIB PER SRM 51-33-01-0G AND DOUGLAS DWG AFA7769

Part: STRUCTURE — CORRODED (BS 1973-1974) · airframe 92,043 hrs · 21,958 cycles

AFT WASTE TANK AREA AT STA 1976 TO 1964, BOTTOM CENTER FRAME, HAS LARGE CORROSION AREA AROUND BOLT HOLE. (MKD) REMOVED AND REPLACED BOTTOM CENTER FRAME BETWEEN STA 1976 TO STA 1964 REF SRM 51-31-01-0G , DOUGLAS DRAWING AGA7981 AND GMM 7-0-1001 FOR THE IDENTIFICATION. MAJOR REPAIR.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152PT/152NT) - CRACK AT INBD ANGLE STA.1621 L38. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG AFA7769.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152LT/152KT) - CRACK AT INBD ANGLE STA. 5- 113 BETWEEN L43-L44. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG #A5A7064.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152NT/152LT) - CRACK AT INBD ANGLE STA.1581 L34. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG AFA7769.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152NT/152LT) - CRACK AT INBD ANGLE STA.1581 BETWEEN L30-L31. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG 7769.

Part: ANGLE — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

RH WING FILLET FAIRING SUPPORT RIB (PANELS 152NT/152LT) - CRACK AT INBD ANGLE STA.1581 AT L37. CRACK CONFIRMED WITH NDT HFEC. FABRICATED AND INSTALLED NEW ANGLE REF DWG AFA7769

Part: FRAME — CORRODED (BS 1841 S43-48R) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO COMP. FWD FRAME AFT FACE AT STA 1841 & NEAR RBL 43 FUSELAGE FRAME J-CLIP NUTPLATE EXFOLIATED THROUGH THE SKIN (MARKED) IN AFT CARGO COMP. REPAIRED J-CLIP AT STA 1841 & RBL 43 REF SRM 53-00-00-2R FIG 210 "MAJOR REPAIR"

Part: FLOOR PANEL — WORN (MAIN CARGO) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO FLOOR PANEL 241CF HAS A PUNCTURE FABRUCATED NEW MAIN CARGO FLOOR PANEL 241CF PER DRW SRZ-25-005

Part: SUPPORT — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO DECK AT STA 1841 & RBL 100 UNDER FLOOR PANEL 292BF SUPPORT BRACKET DAMAGED (MARKED). REMOVED AND REPLACED SUPPORT PER DWG AGA3814 & SRM 51-31-01-0G

Part: SKIN — CORRODED (BS 2014 S7-8R) · airframe 92,043 hrs · 21,958 cycles

AFT FUSELAGE, ZONE 312 UPPER FWD COMPT STA 2014, RHS BETWEEN STRINGER #10 AND #11, INNER SKIN HAS EXFOLIATED CORROSION AROUND NUTPLATE, MARKED. AFT FUSELAGE, ZONE 312 UPPER FWD COMPT STA2014-1997 STRINGER 10R-11R, CORROSION REPAIR PERFORMED IAW EA 1-5330-T0365138 PART 1 "FUSELAGE - PLANES & SKINS - FUSELAGE AFT BODY SECTION - SKIN PANEL AJC7058-2 REPAIR" *MAJOR REPAIR* SEE JPF.

Part: BEAM — CORRODED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

AFT CARGO AT ABOVE LOWER LATCH SPOOLS-CLOSE OUT WEB FITTING SHOWS EVIDENCE OF EXFOLIATED CORROSION.(AREA MARKED) REMOVED CORROSION ON BEAM P/N: AGA7216-1 REF MD11 SRM 53-00-15-2R PG 22-24 REPAIR 6, DAC DWG AGA7216

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN FLOOR PANEL AT STA 939 RGL 90 HAS PUNCTURE HOLE. FABRICATED A NEW PANEL SRZADA7178-17 IN ACCORDANCE TO FEDEX DRAWING SRZ-25-005.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK AT APROX STA 1661 & RBL 103 FLOOR PANEL 282HF INSERTS DAMAGED/ EXFOLIATED (MARKED) FABRICATED NEW FLOOR PANEL PER FEDEX DWG SRZ-25-005

Part: SKIN — WORN (ZONE 400) · airframe 92,043 hrs · 21,958 cycles

#2 ENG L/H PICKLE BARREL PANEL LWR SIDE WORN THRU BEYOND LIMITS REMOVED AND REPLACED SECTION OF WORN SKIN ON #2 ENGINE LOWER LEFT AFT PICKLE BARREL REF SRM CH 54-20-15, FIG 201 (SHEET 3 OF 6).

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK AT APPROX STA 1661, RBL 36 FLOOR PANEL 283FF INSERTS DAMAGED AND EXFOLIATED. FABRICATED NEW FLOOR PANEL 283FF PER FEDEX DRAWING SRZ-25-005.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK AT APROX STA 775 TO 879 AND RBL 27.50 TO LBL 27.50 CENTER FLOOR PANEL HAS SEVERAL GOUGES/DAMAGES (MARKED). FABRICATED NEW MCD CENTER FLOOR PANEL AT APROX STA 775 TO 879 AND RBL 27.50 TO LBL 27.50 PER FEDEX DRAWING SRZ-25-005.

Part: CONTROL PANEL — DAMAGED (MAIN DECK) · airframe 92,043 hrs · 21,958 cycles

MAIN DECK COURIER AREA (MCD) DOOR CONTROL PANEL IS DAMAGED FABRICATED NEW ABA 8360-13 MCD DOOR PANEL

Part: SUPPORT — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO DECK AT STA 1909 & RBL 45 FLOOR PANEL SUPPORT BRACKET DAMAGED (MARKED) REMOVED AND REPLACED FLOOR SUPPORT AGA7085-501 REF DAC DWG AGA7127 AND SRM 51- 31-01-OG.

Part: NONE — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN STA. 1360 LBL...84-96 FLOOR BOARD BOTTEM SURFACE FASTENER GROMMETS FORMING CORROSION.. REMOVED AND REPLACED FLOOR SUPPORT STA. 1360 LBL 84-96 DAC DWG AEA0394 AND SRM51-35-01-OG AND REMOVED AND REPLACED GROMMETS PER SRM 53-00-50-2R.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO DECK AT STA 1874 & RBL 107 FLOOR PANEL SUPPORT BRACKET DAMAGED (MARKED) REMOVED AND REPLACED SUPPORT IAW DWG AGA7091 AND SRM 51-31-01-0G

Part: SUPPORT — CORRODED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CABIN STA 1480...RBL 72-96..FLOOR SUPPORT STRUCTURE FORMING CORROSION.. REMOVED AND REPLACED FLOOR SUPPORT REF DAC DWG AEA7330 AND SRM 51-31-01-OG.

Part: SKIN — CRACKED (ZONE 600) · airframe 92,043 hrs · 21,958 cycles

R/H LOWER WING, LOWER RE-FUEL DOOR, FWD INBD CORNER HAS A CRACK. (MKD WITH DOT #1) REPAIRED PER SRM 57-40-01,REPAIR 18, FIG 201. (MAJOR REPAIR)

Part: BEAM — CRACKED (ZONE 100) · airframe 92,043 hrs · 21,958 cycles

LWR FWR CARGO COMP. STA. Y595, Z-80. AFT PRESSURE BULKHEAD, LWR HROZ STIFFENER ( NCA6044-29 BEAM ) CRACKED AT LWR FACE NEAR CENTER (MARK 4 PLACES) INSTALLED ALL REPAIR PARTS AT STA 595 Z-80 AFT PRESUSSURE BULKHEAD STIFFNER BEAM NCA 6044-29 REF SRM 53-20-08-2R, SRM 51-31-01-OG, AND SRM 51-33-01-OG MAJOR REPAIR

Part: SKIN — GOUGED (ZONE 500) · airframe 92,043 hrs · 21,958 cycles

L/H WING I/B FLAP LOWER SKIN GOUGED (MARKED) 0005108153 : STOFFLE, JOSHUA - 05-NOV-2021 03:13 REPAIRED L/H WING I/B FLAP LOWER SKIN. REF MD-11 SRM 57-00-00-2R, FIG. 205, SH.1. 0000439384 : KRISHTALL, VLADIMIR - 05-NOV-2021 04:11 BUY BACK 0005108153 : STOFFLE, JOSHUA - 05-NOV-2021 04:29 REPAIRED L/H WING I/B FLAP LOWER SKIN. REF MD-11 SRM 57-00-00-2R, FIG. 205, SH.1. "MAJOR REPAIR" 0000439384 : KRISHTALL, VLADIMIR - 05-NOV-2021 04:39 BUY BACK

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO COMPT, APPROX. STA 1199 X= -107.25 SEAT TRACK 3" SECTION BLENDED BEYOND LIMITS, MARKED. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SEAT TRACK SPLICE AND HAT SPLICES PER SRM 53-00-52, REPAIR-1, FIG.201, DRW# SR10-53-002, SRM 51-33-01. SRM 51-41-01. "MAJOR REPAIR"

Part: TRACK — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

MAIN CARGO COMPT, APPROX. STA 1400 X= -107.25 SEAT TRACK BLENDED BEYOND LIMITS, MARKED. INSTALLED NEW SEAT TRACK SPLICE AND HAT SPLICES FROM STA. 1171-STA.1409 X-107.25. REF SRM 53-00-52-2R FIG 201 REPAIR-1. FDX DRAWING SR10-53-002.

Part: LONGERON — CRACKED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: AT THE TIME OF AGING AIRCRAFT RECORDS REVIEW, A FRAME REPAIR IN THE MAIN CABIN AT STA. 535 LONG. 24L, W.O. 69661 N00385 WAS FOUND. JPF ITEMS ON THE NON ROUTINE THAT SHOULD BE RII ARE MARKED (N/A). MAIN DECK L/H FUSELAGE FRAME AT STATION 535 LOGERON 24L. EXITING REPAIR REMOVED AND REPAIRED ACCOMPLISHED AS PER MD-11 SRM 53-20-07-2R FIG. 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: AT THE TIME OF AGING AIRCRAFT RECORDS REVIEW, A SEAT TRACK REPAIR AT STA. 1269-1329, LBL27 WAS FOUND.(W.O 79052 N00043 AND WRI 25501425 SEQ.173). RII WAS NOT BOUGHT BACK ON NR N00043 AND JPF ITEMS ON SEQ 173 THAT SHOULD BE RII ARE MARKED (N/A). REPAIR REQUIRES REWORK. REMOVED EXISTING SEAT TRACK SPLICE REPAIR AND INSTALLED NEW REPAIR OF SEAT TRACK AT STATION 1269-1329 LBL 27 AS PER MD-11 SRM 53-00-52-2R FIGURE 201/REPAIR 1. "MAJOR REPAIR"

Part: DOUBLER — CRACKED (ZONE 600) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: AT THE TIME OF AGING AIRCRAFT RECORDS REVIEW, A BEADED DOUBLER REPAIR INSIDE R/H WING FIXED LEADING AT STA. XOS 543. W.O 75165 N01071, JPF ITEMS ON THE NON ROUTINE THAT SHOULD BE RII ARE MARKED (N/A). REPAIR REQUIRES REWORK. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 543 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: NONE — NONE (N/A) · airframe 92,043 hrs · 21,958 cycles

REPAIR ASSESSMENT: AT THE TIME OF AGING AIRCRAFT RECORDS REVIEW, A MAJOR REPAIR ON L/H WING FIXED LEADING EDGE AT SLAT TRACK #10 CUTOUT, W.O 75165 N00604, JPF ITEMS REQUIRING RII ARE MARKED (N/A). REPAIR REQUIRES REWORK. MAJOR REPAIR: REMOVED ORIGINAL REPAIR AND REPLACED WITH NEW FABRICATED FILLER AND DOUBLER, REF: SRM 57-40-02-2R REPAIR #7 FIG 201 SHEET 1 AND 2.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 91,848 hrs · 21,878 cycles

10 MIN INTO FLIGHT WE RECIEVED A HYD 1R PUMP OFF ALERT. THE HYD PAGE SHOWED THE RIGHT PUMP OFF WITH A 'T' OVER THE PUMP. ABOUT 3 MINUTES LATER WE SAW THE PRESSURE SPIKE TO 3800 AND WE RECIEVED A HYD 1 OFF ALERT. WITH BOTH PUMPS OFF WE STILL HAD ABOUT 2400 PSI AND A SLOW LEAK DEVELOPED. WHEN THE QUANTITY FELL TO LESS THAN 1 GALLON WE RECIEVED A HYD 1 FAIL ALERT. AMM: 29-11-20-4-1 MD11 FOUND L1 PUMP LEAKING FROM SHAFT SEAL OUT DRAIN MAST. R & R L1 & R1 EDP'S(DUE TO RUN W/O FLUID). CK'D & REPLACED ALL 4 FILTERS. NO CONTAMINATION FOUND. RESERV'D RESV. BLED SYS 1. PUMP/FILTER LK & OPS CK'S OK.

Part: SEAT TRACK — WORN (CABIN) · airframe 90,248 hrs · 21,422 cycles

SEAT TRACK REPAIR AT POSITION 7L/8L ACCOMPLISHED ON SEQ 173 AND WRI 25501425. REPAIRS COMPLETED ON SEQ CARD 173 SEE JPF FOR WORK STEPS NEEDED TO MAKE NR FOR RDR/SDR.

Part: WEB — CRACKED (BS 1372) · airframe 90,248 hrs · 21,422 cycles

RT MLG WHEEL WELL FWD PRESSURE BULKHEAD HAS SUSPECT CRACK AT STIFFENER OUTER END JUST BELOW ACCESS PANEL. MWT REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER, PER EA 1-5310-T0358831 P1.

Part: WIRE — BURNED (BATTERY CHARGER) · airframe 90,238 hrs · 21,417 cycles

BATTERY CHARGER/APU START ELECTRICAL BAY, JUST BELOW POWER CENTER, SMELLED ELECTRICAL BURNING. REMOVED PANEL AND FOUND BURNT WIRING FROM R2-24 POSITION A2 TO B1-114 POSITION A1. WILL INCLUDE PICTURES. PARTS NEEDED. WE NEED WIRE NR C904-26-6 FABRICATED, REF MD-11 WIRING DIAGRAM MANUAL. WIRE LIST SECTION C0900 PAGE 86. WE HAVE RCCB B1-114 CPN 0046345. R & R BAT CH RELAY R2-24, PER AMM 24-34-01. R & R BAT CH RCCB B1-114, PER AMM 24-50-01. REPLACED BUS BAR & BURNED WIRE, PER SWP. BAT CHARGER OPERATIONS TEST, GOOD PER AMM 24-34-03. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED · airframe 89,234 hrs · 21,135 cycles

APPROX 1 SECOND AFTER ADVANCING POWER FOR TAKEOFF RECIEVED LEVEL 1 TIRE DIFF PRESS ALERT. REJECTED TAKEOFF. ALERT CLEARED ITSELF SHORTLY THEREAFTER, ALTHOUGH NR 3 TIRE PRESSURE CONTINUED TO FLUXUATE. ALL TIRE PRESSURES REMAINED IN LIMITS FOR SECOND TAKEOFF. BRAKE TEMP MONITORING, TIRE PRESS INDICATING SYS INOP. ALL TIRE PRESSURES ARE REQD TO BE CHECKED BEFORE THE FIRST FLIGHT OF EACH DAY.

Part: SENSOR — FAILED (BRK TEMP TIRE PR) · airframe 89,234 hrs · 21,135 cycles

APPROX 1 SECOND AFTER ADVANCING POWER FOR TAKEOFF RECIEVED LEVEL 1 TIRE DIFF PRESS ALERT. REJECTED TAKEOFF. ALERT CLEARED ITSELF SHORTLY THEREAFTER, ALTHOUGH NR 3 TIRE PRESSURE CONTINUED TO FLUXUATE. ALL TIRE PRESSURES REMAINED IN LIMMITS FOR SECOND TAKEOFF. ATTEMPT. BRAKE TEMP MONITORING, TIRE PRESS IND ICATING SYS INOP. ALL TIRE PRESSURES ARE REQD TO BE CHECKED BEFORE THE FIRST FLIGHT OF EACH DAY. REMOVED & REPLACED BTM TPI IAW AMM 32-46-02-4. OPS CHECK GOOD. ALL WHEEL PRESSURE AND BRAKE TEMP SHOWING GOOD. OK FOR SERVICE.

Part: FINGER DOUBLER — CRACKED (NR 2 NACELLE) · airframe 88,877 hrs · 21,044 cycles

INNER FINGER DOUBLER ABOVE NUMBER 2 ENGINE AFT MOUNT HAS SMALL CRACK, AND ONE RIVET MISSING. COMPLIED WITH EA #1-5481-T0355009 PART 1. MISSING RIVET AT CRACK DAMAGE LOCATION MOVED TO WRI 54-00/0934

Part: WARNING SYSTEM — FALSE ACTIVATION (EMERGENCY LIGHT) · airframe 88,107 hrs · 20,859 cycles

ON PREFLIGHT, DURING EMERGENCY LIGHT TEST WE GOT A LEVEL ONE ALERT EMER LT BAT 1 LO. RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 15APR20 "MEL 33-50-04: EMER LIGHTS - INOP." PERFORMED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTING BATTERY POWER SUPPLY FOR THREE TIMES REF AMM 33-51-01-5.TEST PASSED. STICKER REMOVED,A/C OK FOR SERVICE.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 500 TO 501.50 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 500 TO 501.50 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 482.15 TO 488.15 CORROSION. LEFT HAND WING - TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 482.15 TO 488.15 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 529.50 TO 531 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 529.50 TO 531 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 675.09 TO 679.87 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 675.09 TO 679.87 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 784 TO 785.50 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 784 TO 785.50 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 791.15 TO 796 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 791.15 TO 796 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 520 TO 521.50 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 520 TO 521.50 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 984.3 TO 992.3 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 984.3 TO 992.3 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 540.2 TO 545.3 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 540.2 TO 545.3 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 969.3 TO 970.8 CORROSION. LEFT HAND WING -TRAILING EDGE REAR SPAR UPPER CAP STATION XORS 969.3 TO 970.8 CORROSION REPAIR CARRIED OUT AS PER EA # 1-5710-T0349970 PART 1, TITLE: WINGS - BASIC WING STRUCTURE - LH WING - REAR SPAR UPPER CAP - CORROSION FOUND ON AFT FLANGE UPPER SURFACE BETWEEN XORS 482 AND XORS 993. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (BS 803-835) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

AFTER REMOVAL OF ADDITIONAL ACCESS FOR SMRM N00877 - CABIN R2 DOOR AFT LOWER CUT OUT AREA FOUND CORROSION . CABIN R2 DOOR AFT LOWER CUT OUT INTERIOR AREA AT RIGHT HAND LONGERON 27 RIGHT , CORROSION REMOVED AND EXCEEDED SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE LIMIT AND COMPLIED WITH EA # : 1-5310-T0350182 P1 TITLE : FUSELAGE - MAIN FRAME - DOOR 2R LOWER SILL 02 EA AREAS CORROSION AT L - 27R . REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100 .

Part: SEAT TRACK — CORRODED (BS 1865-1870) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

AFT LOWER CARGO COMPARTMENT LEFT HAND SEAT TRACK BETWEEN STATION 1865- 1870,X=20 FOUND CORROSION. AFT LOWER CARGO COMPARTMENT LEFT HAND SEAT TRACK BETWEEN STATION 1865 - 1870,X=20 CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REMOVED AND INSTALLED NEW SEAT TRACK FROM STATION 1841 TO STATION 1964 X = 20 AS PER AMM 20- 50-02. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: CARRIAGE — DAMAGED (LT WING TE FLAP) · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD CARRIAGE SPINNER BUSHING REMOVED (REFERENCE: SNRM # N00764) FOUND BORE CENTER SURFACE DAMAGED DAMAGED AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD CARRIAGE SPINNER BORE CENTER SURFACE LOCAL BLEND CARRIED OUT AS PER MD-11 SRM 51-21-01-OG. REPAIR CARRIED OUT AS PER E.A # 1-5750-T0350011 PART 1 TITLE: WINGS - FLIGHT SURFACES - REPAIR FOR LH WING OUTBD FLAP OUTBD CLOSURE RIB HOUSING BORE GOUGE MARK - RSC TRACKING. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BUSHING — MIGRATED (LT WING SLAT) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - #4 SLAT ASSEMBLY OUTBOARD FITTING LOWER BUSHING MIGRATED MIGRATED BUSHING AT LEFT HAND WING - #4 SLAT ASSEMBLY OUTBOARD FITTING LOWER HOLE REMOVED AS PER MD-11 CMM 20-10-7. HOLE MEASURED DIAMETER 1.079" - DIAMETER 1.083" AND FOUND ELONGATED AS PER MD-11 SRM 57-40-02-2R. ELONGATED HOLE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SRM 57-40-02-2R FIG 201. SHOULDER REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER E.A #: 1-5750-T0350181 PART 1 STEP 6A, TITLE: WINGS - FLIGHT SURFACES - LH WING - #4 SLAT ASSY - XOS 659.717 OUTBD SLAT TRACK RIB FOUND WITH EXISTING SPOT-FACE AND DAMAGED HOLE. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 455-480) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND STATION 455 - 480 X = 107.25 SEAT TRACK FOUND CORROSION . CABIN AT LEFT HAND SEAT TRACK STATION 455 - 480 X = 107.25 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATION 392 TO EXISTING SPLICE STATION 484.7 X = 107.25 AS PER SRM 51-31-01-0G . REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100 .

Part: WEB — CRACKED (BS 1841) · airframe 87,323 hrs · 20,619 cycles

AFT LOWER CARGO COMPARTMENT LEFT HAND FLOOR WEB AT STATION 1841,X=39 UNDERNEATH PANEL 187EF FOUND CRACKED. AFT LOWER CARGO COMPARTMENT LEFT HAND FLOOR AT STATION 1841,X=39 UNDERNEATH PANEL 187EF CRACKED WEB REMOVED AND INSTALLED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CORRODED (BS 1841) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

UPON FLOOR SUPPORT REMOVAL FOR REPAIR - LOWER CENTER CARGO AFT BULKHEAD RIGHT HAND WEB FOUND WITH CORROSION AT STATION 1841 X=-20 TO X=-40 . LOWER CENTER CARGO AFT BULKHEAD RIGHT HAND AT STATION 1841,X=-20 TO X=-40 CORROSION WEB REMOVED AS PER SRM 51-21-01-0G AND EXCEEDED LIMIT AS PER SRM 53-00- 00-2R FIGURE 202. CORROSION DAMAGED WEB REMOVED AND INSTALLED WITH FABRICATED WEB AS PER SRM 51-31-01-0G. WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION R . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN RIGHT HAND STATION 475 X = - 27.5 FOUND CORROSION. CABIN AT RIGHT HAND STATION 475 X= - 27.5 SEAT TRACK, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATION 421.5 TO EXISTING SPLICE AT STATION 485 X = - 27.5 AS PER SRM 51-31-01-0G. SEAT TRACK REWORKED BY MACHINING AS PER DRAWING ABA 7684 REVISION G. REFER TO SNRM N01541 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 87,323 hrs · 20,619 cycles

WITH REFERENCE TO WRI : 25509452 - CABIN SEAT TRACK CROWN AT STATION 1281 X = 47.5 FOUND CRACKED OFF. CABIN CRACKED SEAT TRACK AT STATION 1281 X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1311 TO STATION 1229 X = 47.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (LT WING) · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - UPPER INBOARD FIXED LEADING EDGE SURFACE BETWEEN XIS 269.9 AND XIS 276.5 FOUND WITH CHAFFING MARK. LEFT HAND WING - UPPER INBOARD FIXED LEADING EDGE SURFACE BETWEEN XIS 269.9 AND XIS 276.5 CHAFFING MARK REPAIRED PER EA 1-5730-T0349969 P1, TITLE: WINGS - PLATES AND SKINS - LH WING - FIXED LEADING EDGE SKIN FOUND WITH CHAFE DAMAGE BETWEEN XIS 269.900 AND XIS 276.500. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 450 - 480 X=-107.25 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 450 TO STATION 480 X = - 107.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED AT STATION 414 TO EXISTING SPLICE STATION 484 X = - 107.25 AS PER SRM 51-31-01-0G . SEAT TRACK REWORKED BY MACHINING AS PER DOUGLAS DRAWING ABA7681 REVISION J . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN RIGHT HAND SUPPORT AT STATION 395 TO STATION 410 X= -12 FOUND CORROSION. CABIN RIGHT HAND SUPPORT AT STATION 395 TO STATION 410 X = - 12 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE . CORRODED RIGHT HAND SUPPORT AT STATION 395 TO STATION 410 X = - 12 REMOVED AND REPLACED AS PER SRM 51-31-01-0G . SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING ABA 8225 REVISION J . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: ANGLE — CHAFED (BS 535) · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND FRAME STATION 535 9G NET SUPPORT YOKE LONGERON 19 LEFT UPPER EXISTING OUTER REPAIR ANGLE FOUND CHAFFED. CABIN AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT CHAFFED AREA AT EXISTING OUTER REPAIR ANGLE EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE. CHAFFED EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CHAFED (BS 535) · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND FRAME STATION 535 LONGERON 24 LEFT 9G NET SUPPORT YOKE LOWER EXISTING OUTER REPAIR ANGLE FOUND CHAFFED. CABIN AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT CHAFFED AREA AT EXISITNG OUTER REPAIR ANGLE EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIG 205 ALLOWABLE DAMAGE. CHAFFED EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51- 33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CHAFED (BS 535) · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND FRAME STATION 535 LONGERON 24 RIGHT 9G NET SUPPORT YOKE LOWER EXISTING OUTER REPAIR ANGLE FOUND CHAFFED. CABIN AT RIGHT HAND FRAME STATION 535 LONGERON 24 RIGHT CHAFFED AREA AT EXISTING OUTER REPAIR ANGLE EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE. CHAFFED EXISTING OUTER REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CRACKED (LT WING AILERON) · airframe 87,323 hrs · 20,619 cycles

LEFT WING - INBOARD AILERON ASSEMBLY INBOARD HINGE FITTING OUTBOARD EDGE CRACKED. REPAIRED PER EA 1-5750-T0350012 P1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1982) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

BS 1982 RBL 25 FLOOR SUPPORT FOUND CORRODED. FOUND TO EXCEED LIMITS IAW SRM 53-00-00-2R, FIGURE 206, ALLOWABLE DAMAGE . FABRICATED A NEW FLOOR SUPPORT IAW DRAWING AGA 7087, REVISION M. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN BS 1887 TO 2007 IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 1902) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

AFT CARGO COMPARTMENT RIGHT FLOORBEAM AT STATION 1902, BETWEEN X=-20 AND X=-30 FOUND CORRODED. REPAIRED THE FLOORBEAM IAW EA 1-5321-T0349919 A P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (BS 1380) · airframe 87,323 hrs · 20,619 cycles

CENTER LANDING GEAR COMPARTMENT, LEFT WEB DOUBLER AT BS 1380 WAS FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-33-01-0G, A NEW DOUBLER WA FABRICATED IAW DRAWING AEA 0526, REV NC, AND INSTALLED IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT WING, FIXED LEADING COMPARTMENT XOS 666, STRINGER CRACKED. THE STRINGER WAS REPAIRED IAW EA 1-5720-122505 A, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (LT NR 6 SLAT) · airframe 87,323 hrs · 20,619 cycles

LEFT WING NR 6 SLAT ASSEMBLY, INNER NR 3 RIB FROM INBOARD WAS FOUND CRACKED DURING A BORESCOPE INSPECTION. THE NR 3 RIB WAS REPAIRED IAW EA 1-5750-T0350336, P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (RT NR 5 SLAT) · airframe 87,323 hrs · 20,619 cycles

RIGHT WING NR 5 SLAT INNER NR 8 RIB FROM INBOARD WAS FOUND CRACKED, FOUND DURING A BORESCOPE INSPECTION. THE NR 8 RIB WAS REPAIRED IAW EA 1-5750-T0350343 P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — SCRATCHED (BS 869-929) · airframe 87,323 hrs · 20,619 cycles

FUSELAGE SKIN BETWEEN BS 869 TO 929, LONGERON 9 RT WAS FOUND WITH SCRATCHES. THE SCRATCHES WERE REMOVED, 0.048", SKIN ORIGINAL THICKNESS 0.068", REMAINED THICKNESS 0.020" FOUND OUT OF LIMITD IAW SRM 53-00-00-2R, FIGURE 202. SKIN REPAIRED IAW SRM 53-00-01-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 455) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

FORWARD CABIN SEAT TRACK LBL 19, BS 455 WAS FOUND WITH CORROSION ON THE FLANGE. THE CORROSION WAS FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DRAWING SP11530031 REVISION NEW. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (BS 795-849) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

SEAT TRACK, BS 795 - 849, RBL 75.25 WAS FOUND CORRODED. THE CORROSION WAS FOUND TOE EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED BETWEEN BS 869 TO EXISTING SPLICE AT 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 — CORRODED (BS 425-455) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

RIGHT SEAT TRACK AT BS 425 TO 455, RBL 27.5 WAS FOUND CORRODED. FOUND EXFOLIATION EXCEED LIMITS IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE, DAMAGE 1. THE SEAT TRACK WAS REMOVED AND REPLACED FROM BS 421.5 TO EXISTING SPLICE AT BS 485 IAW SRM 51-31-01-0G AND DRAWING ABA 7684 REVISION G . REPAIR CLASSIFIED AS MAJOR IAWGMM 6-2-100 .

Part: SEAT TRACK — CORRODED (BS 785-849) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

BS 795 - 849, RBL 107.25 SEAT TRACK WAS FOUND CORRODED. THE CORROSION WAS FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACEED FROM BS 869 TO EXISTING SPLICE AT 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 — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - SEAT TRACK AT STATION 435 TO STATION 455 X = 0 FOUND CORROSION . CABIN - SEAT TRACK AT STATION 435 TO STATION 455 X = 0 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED FROM STATION 421.5 TO STATION 495 X = 0 AS PER SRM 51-31-01-0G . SEAT TRACK REWORKED BY MACHINING AS PER DOUGLAS DRAWING SP11530031 REVISION NEW . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - SEAT TRACK AT STATION 1871 TO STATION 1881 X = - 47.5 FOUND CORROSION . CABIN AT SEAT TRACK STATION 1871 TO STATION 1881 X = - 47.5 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1831 TO END OF PART STATION 1887 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 (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND SEAT TRACK AT STATION 475 TO STATION 495 X = 27.5 FOUND CORROSION . CABIN AT LEFT HAND SEAT TRACK STATION 475 TO STATION 495 X = 27.5 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED AT EXISTING SPLICES STATION 467 TO STATION 525 X = 27.5 AS PER SRM 51-31-01-0G . SEAT TRACK REWORKED AS PER DOUGLAS DRAWING VZZ 7330 REVISION B . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN LEFT HAND STATION 1965 X = 56 FLOOR SUPPORT FOUND CORROSION . CABIN AT LEFT HAND FLOOR SUPPORT STATION 1965 X = 56 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE . CORRODED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = 56 AS PER SRM 51-31-01-0G . FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA7551 REVISION G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN LEFT HAND SEAT TRACK AT STATION 1721 TO STATION 1731 X = 27.5 FOUND CORROSION . CABIN AT LEFT HAND SEAT TRACK AT STATION 1721 TO STATION 1731 X = 27.5 , CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO EXISTING SPLICE STATION 1711 X = 27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

MAIN DECK - AFT CARGO WASTE COMPARTMENT CEILING FLOOR SUPPORT APPTOXIMATELY AT STATION 1936 TO STATION 2000 X= - 56 FOUND CORROSION . MAIN DECK AT AFT FLOOR SUPPORT STATION 1936 TO STATION 2000 X = - 56 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE . CORRODED AFT FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007 X = - 56 AS PER SRM 51- 31 -01-0G . AFT FLOOR SUPPORT FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA7551 REVISION G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CORRODED (LT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT STATION XW 212. LEFT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION XW212 AREA CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20- 01-1A ALLOWABLE DAMAGE 1 FIGURE101 MATERIAL REMOVED EXCEEDED : 0.100" ,MINIMUM THICKNESS REMAINING 0.048". REPAIR CARRIED OUT AS PER EA 1-5730-T0349794 PART 1 TITLE: WINGS - PLATES AND SKINS - LH WING - CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN STRINGER NO.1 AND INNER REAR SPAR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. LEFT HAND WING REPAIR AREA FUEL LEAK CHECK CARRIED OUT AS PER AMM 12-11-04 FOUND SATISFACTORY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 475 - 485 X = - 36 SEAT TRACK FOUND CORROSION . CABIN AT RIGHT HAND SEAT TRACK STATION 475 TO STATION 485 X = - 36 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED AND REPLACED AT STATION 440 TO STATION 495 X = - 36 AS PER SRM 51-31-01-0G . SEAT TRACK REWORKED AS PER DOUGLAS DRAWING SP11530031 REVISION NEW . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN RIGHT HAND STATION 1581 X = - 8.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1581 X = - 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 1531 TO STATION 1591 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING FIXED LEADING COMPARTMENT STATION XOS 548 DOUBLER FORWARD CUTOUT CRACKED. DOUBLER ON RIGHT HAND WING FIXED LEADING COMPARTMENT AT STATION XOS 548 FORWARD CUTOUT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 2933 REVISION AJ. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (LE SLAT) · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - NUMBER 1 SLAT ASSEMBLY OUTBOARD TRAILING EDGE FOUND WITH CHAFED MARK AT STATION XIS 244. LEFT HAND WING NUMBER 1 SLAT ASSEMBLY REMOVED AND REPLACED AS PER AMM27-80-20-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY PER AMM27-80-20. SLAT RANGE OF MOVEMENT CARRIED OUT FOUND SATISFACTORY PER AMM27-80-00-5. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO WRI#57509644 FOR NUMBER 1 SLAT ASSEMBLY REPLACEMENT WORK DETAILS.

Part: SKIN — CHAFED (LE SLAT) · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - NUMBER 2 SLAT ASSEMBLY INBOARD TRAILING EDGE FOUND WITH CHAFED MARK AT STATION XIS 249. LEFT HAND WING NUMBER 2 SLAT ASSEMBLY INBOARD TRAILING EDGE CHAFED MARK AT STATION XIS 249 REPAIR CARRIED OUT AS PER EA # 1-5750-T0350045 P1, TITLE: WINGS - FLIGHT SURFACES - LT WING #2 SLAT ASSY - CHAFE DAMAGE FOUND ON OUTER SKIN, INNER SURFACE BETWEEN STA XIS 247.028 AND STA XIS 253.212. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND STATION 1219 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND SEAT TRACK STATION 1219 X = 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1209 TO EXISTING SPLICE STATION 1331 X = 8.5. REFER TO SNRM N00869 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STIFFENER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 542 STIFFENER CRACKED. STIFFENER ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 542 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND STATION 1301 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND SEAT TRACK STATION 1301 X= 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1209 TO EXISTING SPLICE STATION 1331 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 1965 X = - 107 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1965 X = - 107, CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1831 TO END OF PART STATION 2007 X = - 107 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 1219 X = - 8.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1219 X = - 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1311 TO STATION 1209 X= - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00868 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 1942 X = - 107 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1942 X = - 107 CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1831 TO END OF PART STATION 2007 X = - 107 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 6. REFER TO SPECIAL / NONROUTINE MAINTENANCE FORM N00861 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING- FIXED LEADING COMPARTMENT STATION XOS 785 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 785 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND STATION 1259 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND SEAT TRACK STATION 1259 X = 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1209 TO EXISTING SPLICE STATION 1331 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00869 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 790 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 790 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 1301 X = - 8.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1301 X = - 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1311 TO STATION 1209 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - RIGHT HAND STATION 1259 X = - 8.5 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1259 X = - 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1311 TO STATION 1209 X = - 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REFER TO SNRM N00868 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT SLAT TRACK) · airframe 87,323 hrs · 20,619 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE AFT INBOARD CORNER OF SLAT TRACK NUMBER 10 CUTOUT AND FOUND CRACK INDICATION APPROXIMATE 1/4 INCHES LENGTH AT STATION XOS 657. REPAIR CARRIED OUT ON LEFT HAND WING FIXED LEADING EDGE AFT INBOARD CORNER OF SLAT TRACK CUTOUT AT STATION XOS 657 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 592 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON LEFT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 592 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

CABIN - LEFT HAND STATION 1861 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND SEAT TRACK STATION 1861 X = 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1771 TO END OF PART STATION 1887 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 87,323 hrs · 20,619 cycles

LEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 906 RIB DOUBLER CRACKED. RIB DOUBLER ON LEFT HAND WING-FIXED LEADING COMPARTMENT AT STATION XOS 906 REMOVED AND REPLACED AS PER SRM 51-31-01-0G . DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 691 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 691 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT STATION YW 467. RIGHT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION YW 467 AREA CORROSION REMOVED FOUND EXCEED LIMIT AS PER SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101, MATERIAL REMOVED EXCEED 0.100", MINIMUM THICKNESS REMAINING = 0.070". CARRIED OUT REPAIR AS PER EA 1-5730-T0349603 P1 TITLE: WINGS - PLATES AND SKINS - RT WING - CORROSION FOUND ON MLG SUPPORT UPPER DOUBLER BETWEEN AUX SPAR AND YW 467. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

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

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 666 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 666 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 739 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 739 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 759 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 759 BEADED DOUBLER 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 87,323 hrs · 20,619 cycles

LEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 993 RIB DOUBLER CRACKED. LEFT WING - FIXED LEADING COMPARTMENT STATION XOS 993 RIB CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G, DOUBLER FABRICATED AS PER DRAWING ARB 1249 REV AA, AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR PER GMM 6- 2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 756 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING FIXED LEADING COMPARTMENT AT STATION XOS 756 BEADED DOUBLER 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 87,323 hrs · 20,619 cycles

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

Part: DOUBLER — CRACKED (RT WING) · airframe 87,323 hrs · 20,619 cycles

RIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 543 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 543 BEADED DOUBLER 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 87,323 hrs · 20,619 cycles

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

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 87,323 hrs · 20,619 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT RIGHT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT RIGHT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR REPAIR CARRIED OUT AS PER EA # 1-5530-T0349889 PART 1 TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LT & RT FWD FLANGES - PSE ALI 55.31.01.1. REPAIR CLASIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 87,323 hrs · 20,619 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT LEFT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR REPAIR CARRIED OUT AS PER EA # 1-5530-T0349889 PART 1 TITLE: STABILIZERS - VERTICAL STABILIZER - CRACK REPAIRS ON VERTICAL STABILIZER REAR SPAR LT & RT FWD FLANGES - PSE ALI 55.31.01.1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 86,709 hrs · 20,403 cycles

#3 PACK BAY CUT-OUT APPEARS TO HAVE A CRACK AT THE UPPER AFT CORNER. COUNTER SUNK HOLES AS REQUIRED IN DOUBLER AND TRIPLER. ALODINED AND PRIMED, IAW MD-11 SRM 53-20-15-2R. AND OK TO INSTALL EXTERNAL ALUMINUM REPAIR DOUBLER AND TRIPLER. SHGN 06JUN19 20:39 MEM INSTALLED DOUBLER AND TRIPLER AT UPPER R/H FWD FUSELAGE #3 PACK DOOR CUTOUT PER EA 1-5300-T0347349 PART 1. OK TO PRIME, EDGE SEAL, AND TOPCOAT. EDGE SEALED DOUBLERS, PRIMED AND PAINTED REF SRM 51-41-01-0G, AND SRM 51-21-01. COMPLIED WITH E.A. # 1-5300-T0347349 PT 1, FUSELAGE - GENERAL - NO. 3 A/C PACK DOOR CUTOUT, UPPER AFT CORNER SKIN CRACK.

Part: SKIN — DENTED (LT WING) · airframe 85,020 hrs · 19,863 cycles

NR 1 SLAT LT WING L/E DENT AT NR 3 SLAT TRACK CUT-OUT COMPLIED WITH EA 1-5730-T0342552 PT1.

Part: SKIN — CRACKED (LT WING) · airframe 84,975 hrs · 19,853 cycles

LT WING L/E SKIN CRACK AT AXIS 247-0280 EA 1-5730-T0342552 CUT OUT DAMAGE AND INSTALLED L/E DOUBLER.

Part: SKIN — CRACKED (LT WING) · airframe 84,975 hrs · 19,853 cycles

L/H WING L/E SKIN CRACK AT AXIS 247-0280 EA 1-5730-T0342552 CUT OUT DAMAGE AND INSTALLED L/E DOUBLER.

Part: TARGET — SHEARED (NLG) · airframe 84,320 hrs · 19,651 cycles

ON RAISING GEAR AFTER TAKEOFF, NOSE GEAR SHOWED AN UNSAFE INDICATION ON PRIMARY AND SECONDARY DISPLAY. FOLLOWED CHECKLIST, VERIFIED GEAR DOWN BY TOWER AND MX, LANDED UNEVENTFULLY. UNSAFE INDICATION PERSISTED AFTER LANDING. INSPECTED NOSE GEAR AND FOUND TARGET FOR DOWN LOCK OF BOTH SENSORS MISSING, TARGET MATERIAL FOR SENSORS CAUSING RED NLG UNSAFE IN BOTH GEAR DOWN AND GEAR UP, IAW AMM 32-22-01-4 PARA 3-A-1-5, PAGE 21, REPLACED THE TARGET ASSY AND PERFORMED A NOSE GEAR OPS IAW 32-61-17-400-801, PERFORMED A NOSE GEAR SWING, ALL CHECKED NORMAL, ACFT OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 84,239 hrs · 19,627 cycles

L1 DOOR SLIDE PUSH TO TEST INOP. REMOVED & REPLACED PTT IND ASSY & OPS NORMAL PER AMM 25-61-04-4. A/C OK FOR SVC.

Part: WIRE HARNESS — DAMAGED (NR 3 ENGINE) · airframe 84,181 hrs · 19,603 cycles

RECEIVED A FIRE LIGHT ON ENGINE 3 AT T/O 3 MIN. CLIMBING THRU 12,000 FT ENGINE WAS SECURED WITH CHECKLIST, FIRE BOTTLE BLOWN. REMOVED AND REPLACED RT NR 2 FIRE EXTINGUISHER BOTTLE UP TO AND INCLUDING STEP 3 G (1)G REF AMM 32-21-01-4. MANIFOLD DISCHARGE PORTS PLUGGED AND FLAGGED FOR PRESSURE/LEAK CHECKS. FOUND NR 3 ENGINE WIRING HARNESS VC4966P WITH HEAT DAMAGE. DUE TO NR 3 ENG R&R, SEE REF WRI 72-00/8408 FOR NR 3 ENG WORK COMPLETION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,915 hrs · 19,523 cycles

DURING A POST FLIGHT INSPECTION, THE L1 DOOR OVERHEAD AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-52-04-2. EMERGENCY LIGHTS TESTED GOOD. OK FOR SERVICE.

Part: IRU — FAILED (BRAKES) · airframe 83,726 hrs · 19,453 cycles

ANTISKID FAIL ALERT AFTER PUT GEAR DOWN, RECYCLED ONCE , STILL FAILED. GO AROUND, 20 MIN FLYING, 3RD GEAR DOWN WITH NO ANTI SKID FAIL. NO WHEEL BRAKES ISSUES NO HOT BRAKES. R & R ANTISKID CONTROL UNIT AS PER AMM 32-45-01-4. OPS TEST CHK'D GOOD. AIRCRAFT OK FOR SERVICE.

Part: PANEL — MISSING (LT ELEVATOR) · airframe 82,183 hrs · 19,039 cycles

LEFT DETACHABLE ELEVATOR PANEL 335AZ FOUND MISSING. REPAIRED IAW EA 1- 5510-T0335323, PT 1. INSTALLED IAW AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PANEL — MISSING (LT ELEVATOR) · airframe 82,183 hrs · 19,039 cycles

LEFT DETACHABLE ELEVATOR PANEL 335HZ FOUND MISSING CARRIED OUT A REPAIR IAW EA 1-5510-T0335323, PT 1. INSTALLED THE PANEL IAW AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: PANEL — MISSING (LT ELEVATOR) · airframe 82,183 hrs · 19,039 cycles

LEFT DETACHABLE ELEVATOR PANEL 335CZ FOUND MISSING. REPAIRED IAW EA 1-5510-T0335323, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C AND STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT UPPER HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2C.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED, AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP INBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335333, PART 1, STEP 3A, AND 3C.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OTBD HINGE ( WING SIDE ) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2B.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE SPOT SURFACE FOUND CORRODED. THE SPOT SURFACE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED THE AREA IAW EA 1-5750-T0335291A, PART 1, STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

THE BORE WAS REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-08. EXISTING HOLE DIA: 0.873", FINAL HOLE DIA: 0.983", MAXIMUM ALLOWABLE HOLE DIA: 0.983". RIGHT WING OUTBD FLAP INBD FWD HINGE REMOVED AND REPLACED AS PER AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2D.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) UPPER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2A.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORRODED., THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2 AND 2A.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE RIGHT WING OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED, AND FOUND OUT OF LIMIT IAW CMM 57-44-08. THE OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2B, AND STEP 2.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OTBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE FWD AND AFT SURFACE FOUND CORRODED. MOUNT BORE, FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C, AND STEP 1.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE FWD AND AFT SURFACE FOUND CORRODED. BORE FWD AND AFT SURFACE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335322, PART 1, STEP 2.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) BARREL NUT HOLE SPOT SURFACE FOUND CORRODED. SURFACE REWORKED IAW CMM 57-44-09. A REPAIR SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1B.

Part: SUPPORT FITTING — CORRODED (LT TE FLAP VANE) · airframe 82,183 hrs · 19,039 cycles

LEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED BUSHING WAS FABRICATED IAW EA1-5750-T0335345, PART 1, STEP 1A. INSTALLED IAW AMM 27-50-32-4. LT WING FLAP VANE ADJUSTEMENT AND TEST CARRIED OUT IAW AMM 27-50-30-5 AND FOUND SATISFACTORY.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING OUTBOARD FLAP VANE NR 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. AN OVERSIZED WAS FABRICATED IAW EA 1-5750-T0335352, PART 1, STEP 3, TEST CARRIED OUT IAW AMM 27- 50-32-5, AND FOUND SATISFACTORY.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

LEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

LEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135691F, PART 5, STEP 2 & 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A NEW REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330927 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330926 B, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 82,183 hrs · 19,039 cycles

RT WING FIXED LEADING EDGE FORMER FOUND CRACK AT STA XOS 584 AS MARKED. REMOVED AND REPLACED WITH NEW FABRICATED FORMER PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NEW FORMER PN: FX ARB2931-14 FABRICATED AS PER DRAWING ARB 2931 REV H.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK R3 DOOR LOWER BEAM FORWARD STOPPER AREA FOUND CRACKED. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,183 hrs · 19,039 cycles

SEAT TRACK AT BS 755, LBL 47.5 FOUND THE CROWN DAMAGED. REPLACED THE SEAT TRACK AT EXISTING SPLICES FROM BS 725 TO 765, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 755) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK CARGO TRACK AT BS 755, LBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED FROM BS 485 TO 745, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ANGLE — DAMAGED (BS 535 FRAME) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK, FUSELAGE FRAME AT BS A 535, LONGERON 24L FOUND A DAMAGED REPAIR ANGLE. THE REPAIR WAS REMOVED AND THE REPAIR REACCOMPLISHED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1681) · airframe 82,183 hrs · 19,039 cycles

SEAT TRACK AT BS 1681, LBL 47.5 FOUND THE CROWN DAMAGED. THE SEAT TRACK WAS REPLACED FROM BS 1631 TO 1731, LBL 47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 47.5 FOUND TO HAVE CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ANGLE — DAMAGED (BS 535 FRAME) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK FUSELAGE FRAME AT BS 535, LONGERON 19L FOUND A DAMAGED REPAIR ANGLE. DAMAGED REPAIR ANGLE REMOVED AND REPAIR REACCOMPLISHED IAW SRM 53-20-07-2R, FIG 202, REPAIR 1.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,183 hrs · 19,039 cycles

SEAT TRACK AT BS 755, RBL 27.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED BETWEEN BS 745 TO 785 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 775) · airframe 82,183 hrs · 19,039 cycles

CARGO TRACK AT BS 775, LBL 75.5 CRACKED. REPLACED THE CARGO TRACK FROM BS 725 TO EXISTING SPLICE AT BS 765, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1681) · airframe 82,183 hrs · 19,039 cycles

SEAT TRACK AT BS 1681, LBL 27.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 1651 TO 1710, LBL 27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 695) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK CARGO TRACK AT BS 695, LBL 27.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED FROM BS 625 TO 745 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100

Part: SEAT TRACK — DAMAGED (BS 998) · airframe 82,183 hrs · 19,039 cycles

SEAT TRACK AT BS 998, LBL 47.5 FOUND WITH CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 949 TO 1029, IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 755) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK CARGO TRACK AT BS 755, RBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED BETWEEN BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 972, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED SEAT TRACK AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CARGO TRACK — CRACKED (BS 638) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK CARGO TRACK AT BS 638, RBL 8.5 FOUND CRACKED. THE CARGO TRACK WAS REPLACED BETWEEN BS 625 TO 705 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (CROWN AREA) · airframe 82,183 hrs · 19,039 cycles

CROWN AREA LONGERON SPLICE AT STA 5-0, LONGERON 4L FOUND CRACKED. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE WAS FABRICATED IAW DWG AEA 7634, REV B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 627 - 628. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 755) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK SEAT TRACK AT BS 755, LBL 27.5 FOUND TO HAVE CROWN DAMAGE. THE SEAT TRACK WAS REPLACED FROM BS 725 TO 765 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 82,183 hrs · 19,039 cycles

LEFT WING DROOPED LEADING EDGE UPPER SKIN FOUND CRACKED AT XDLE 325. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 82,183 hrs · 19,039 cycles

MAIN DECK FLOOR SEAT TRACK AT STA 5-23, X=75.25 FOUND CROWN DAMAGED. REPAIRED SEAT TRACK AT EXISTING SPLICE STA 5-0, X=75.25 TO STA 5-63, X=75.25 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LINK — LACK OF LUBE (NLG STEERING) · airframe 81,376 hrs · 18,799 cycles

HIGH SPEED REJECT DUE TO QUESTIONABLE RUDDER AUTHORITY. REJECTION SPEED 30 KNTS. ON INITAL CONFIGURATION CHECK OF LEFT RUDDER THROW FELT NORMAL WITH GREEN BOXES FOR UPPER AND LOWER RUDDER. RIGHT RUDDER VERY STIFF WITH ONLY TOP RUDDER GREEN BOX. ON SECOND ATTEMPT, RECEIVED A LOWER GREEN BOX FOR LOWER RUDDER. DURING TAKEOFF ROLL, RUDDER SEEMED STIFF AND AS SPEED INCREASED RUDDER SEEMED ABNORMALLY STIFF. ELECTED TO ABORT TAKEOFF. LUBRICATED ALL STEERING LINKS AND COLLARS, CYCLED THE STEERING AND LUBED AGAIN IAW AMM 21-03-3 AND 12-24-06-3.

Part: INDICATION SYS — FALSE ACTIVATION (HYDRAULIC SYS) · airframe 79,457 hrs · 18,232 cycles

HYD 1 FAIL, LEVEL 2 ALERT RT AFTER T/O, IND 23L. REF TO QRH. RAISED GEAR, SLATS CLIMBED TO 230. DECLARED EMERGENCY. PLANNED FOR FLAPS 35/EXT LAND. ALERT CAME ON AFTER GEAR RAISED, PRIOR TO FLAP RETRACTION. REPLACED NR 1 HYD RESEVOIR QTY INDICATION ARM, BOLT, AND NUT REF SMP AND MM 29-12-01-4-0 AND 29-32-02-2. OPS CHECKED SYS AND PERFORMED HSC RTS AND SYS PRESSURE TEST, ALL TESTS PASSED.

Part: HYDRAULIC LINE — RUPTURED (RT MLG) · airframe 78,198 hrs · 17,834 cycles

LANDING GEAR FAILED TO RETRACT. FOUND THE MAIN HYD HOSE RUPTURED & LEAKING AT THE RT GEAR TRIM CYLINDER. ALSO FOUND TRIM CYLINDER INTERLOCK FUSE TRIPPED. INSTALLED FLEX HOSE IAW AMM 20-10-01-2 & 20-40-01-2. RESET TRIM CYLINDER INTERLOCK FUSE IAW AMM 32-37-06-4. PERFORMED ADJUSTMENT TEST ON THE TRUCK BEAM TRIM INTERLOCK CYLINDER IAW AMM 32-37-00-5, TEST CHECKED GOOD. SERVICED NR 3 HYD IAW AMM 12-13-02-3. PERFORMED LEAK CHECK ON THE FLEX HOSE, LEAK CHECKED GOOD. ACFT OK FOR SERVICE. PART NR OF REMOVED HYD HOSE FOR SDR, ACTUAL MPN AE1011181H0342, CPN 3210706, MPN S7928077-8-0342 AR1441-8.

Part: FUEL TANK — CORRODED (BS 1227) · airframe 773 hrs · 17,575 cycles

MAIN DECK CTR WING TANK RIGHT HAND UPPER SURFACE AT BS 1227, BETWEEN X= -8.5 & X= -27.5 FOUND CORRODED. REPAIRED IAW EA 1-5730-T0320743 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (FUEL TANK) · airframe 773 hrs · 17,575 cycles

MAIN DECK CTR WING TANK, LEFT HAND UPPER SURFACE AT BS 1227, BETWEEN X= 8.5 & X= -8.5, FOUND CORRODED. REPAIRED IAW EA 1-5730-T0320743 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 773 hrs · 17,575 cycles

AGEING ACFT, EXISTING REPAIR DOUBLER ON FUSELAGE EXTERIOR SKIN AT CTR CARGO DOOR, LOWER AFT JAMB AT STATION 1781. EXISTING REPAIR CHAFED AT EDGE OF DOUBLERS, CARRIED OUT REPAIR IAW EA 1-5330-T0320626A PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53304421 FOR WORK DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SUPPORT AT BS 1887 - 2007, X= -2, FOUND CORRODED. FLOOR SUPPORT R & R WITH NEW FABRICATED FLOOR SUPPORT IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7080 REV S. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SUPPORT AT BS 1887 - 2007, X= 2 FOUND CORROSION. FLOOR SUPPORT R & R WITH NEW FABRICATED FLOOR SUPPORT IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7081 REV M. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 200) · airframe 773 hrs · 17,575 cycles

MAIN DECK CTR WING TANK, RT UPPER SURFACE AT STRINGER 15, BETWEEN XCW=-27 & X=- 51, FOUND CORRODED. REPAIRED IAW EA 1-5730-T0320742 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 773 hrs · 17,575 cycles

DURING HFEC OPEN HOLE INSPECTION CARRIED OUT ON LT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT, FOUND ONE NR 35 HOLE WITH CRACK INDICATION. REPAIR BUSHING FABRICATED & INSTALLED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 773 hrs · 17,575 cycles

DURING HFEC OPEN HOLE INSPECTION CARRIED OUT ON RT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT, FOUND FOUR EACH, NR 6, 9, 10 & 35 HOLES WITH CRACK INDICATION. NEW REPAIR BUSHINGS FABRICATED & INSTALLED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 773 hrs · 17,575 cycles

AGEING ACFT, EXISTING REPAIR ANGLE ON FRAME AT MAIN DECK CARGO COMPARTMENT, 9G, UPPER YOKE SUPPORT AT STATION 535, LONGERON 19L. EXISTING REPAIR EVALUATED & FOUND REPAIR DOUBLER WITH DEEP CHAFE MARK. EXISTING REPAIR ANGLE R & R WITH NEW REPAIR IAW SRM 53-20-07-2R FIG 202 REPAIR 1 EO 1-5100-7-5001 B6 PT 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 773 hrs · 17,575 cycles

LEFT WING LE LOWER SURFACE NR 11 SLAT TRACK CUT OUT SKIN, FOUND CRACK AT XOS 719.5. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 773 hrs · 17,575 cycles

RIGHT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 627, DURING OTBD SLAT DRIVE CONTROL CABLE INSPECTION.

Part: DOUBLER — CRACKED (LT WING) · airframe 773 hrs · 17,575 cycles

LEFT WING FIXED LE BEADED DOUBLER FOUND CRACK AT XOS 664. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. LT WING NR 5 SLAT CABLE ADJUSTMENT & TEST CARRIED OUT. FOUND SATISFACTORY IAW AMM 27-80-00-5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 773 hrs · 17,575 cycles

LEFT SIDE NLG TRUNNION WEB, CRACK EXTENDED BEYOND THE TRIM OUT AREA, AT BS 595. REPAIRED IAW SRM 53-10-14-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 773 hrs · 17,575 cycles

RIGHT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 613, DURING SLAT DRIVE CONTROL CABLE INSPECTION.

Part: DOUBLER — CRACKED (RT WING) · airframe 773 hrs · 17,575 cycles

RIGHT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 654, DURING OTBD SLAT DRIVE CONTROL CABLE INSPECTION.

Part: TRUNNION — CRACKED (NLG) · airframe 773 hrs · 17,575 cycles

NOSE LANDING GEAR RT TRUNNION WEB CRACKED. AREA TRIMMED OUT & CARRIED OUT REPAIR IAW SRM 53-10-14-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 773 hrs · 17,575 cycles

RIGHT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 650, DURING OTBD SLAT DRIVE CONTROL CABLE INSPECTION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 773 hrs · 17,575 cycles

AGEING ACFT, EXISTING REPAIR DOUBLER ON FUSELAGE EXTERIOR SKIN AT FWD CARGO DOOR CUT OUT, AFT LOWER JAMB AT STATION 1002.3. FOUND REPAIR DOUBLERS DAMAGED AT EDGE. CARRIED OUT REPAIR PER EA 1-5330-T0320747 PT 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: WEB — CRACKED (BS 1250-1256) · airframe 773 hrs · 17,575 cycles

WHILE REMOVING THE L3 DOOR LINERS & DOOR PLUG FOR NDT INSPECTION ACCESS, FOUND MAIN DECK L3 DOOR, FWD JAMB LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26L - 27L, CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1308-1315) · airframe 773 hrs · 17,575 cycles

WHILE REMOVING THE L3 DOOR LINERS & DOOR PLUG FOR NDT INSPECTION ACCESS, FOUND MAIN DECK L3 DOOR, AFT JAMB LOWER WEB BOX AT BS 305.25 - 1315.42, LONGERON 26L - 27L, CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1250-1256) · airframe 773 hrs · 17,575 cycles

WHILE REMOVING THE R3 DOOR LINERS & DOOR PLUG FOR NDT INSPECTION ACCESS, FOUND MAIN DECK R3 DOOR, FWD JAMB LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26R - 27R, CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: WEB — CRACKED (BS 1305-1315) · airframe 773 hrs · 17,575 cycles

WHILE REMOVING THE R3 DOOR LINERS & DOOR PLUG FOR NDT INSPECTION ACCESS, FOUND MAIN DECK R3 DOOR, AFT JAMB LOWER WEB BOX AT BS 1305.25 - 1315.42, LONGERONS 26 - 27R, CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1354, X=75.5 FOUND FLANGE DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1269 - 1391, X =75.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 773, X= 77.5 FOUND CROWN DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 765 TO STA 819 X = 75.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 773 hrs · 17,575 cycles

MAIN DECK CARGO SEAT TRACK AT STATION 1049, X=8.5 FOUND CORROSIONS. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT, FROM STATION 1029 TO 1069, X=8.5 IAW SRM 53-00-52-2R FIG 201REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 1836, X= -8.5 FOUND CORROSION. SEAT TRACK REPLACED FROM STA1791 TO STA 1831 X =-8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1801) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1801, X= -47.5 FOUND CROWN DAMAGED. 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 1538) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SEAT TRACK AT BS 1538, X= 8.5 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 773 hrs · 17,575 cycles

MAIN DECK FLOOR SEAT TRACK AT STATION 5 - 60, X= -27.5 FOUND CROWN DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-43 TO STA 5-123 X = -27.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 773 hrs · 17,575 cycles

RIGHT WING TE LOWER ACCESS PANEL 641JB CUT OUT FWD CHORD LOWER SURFACE FOUND CORROSION. FWD CHORD REMOVED & REPLACED WITH NEW CHORD PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (MCD) · airframe 768 hrs · 17,425 cycles

SEAT TRACK DAMAGED AT POSITION 9L & 10L, JUST OUTBOARD OF ORIGINAL TRACK DAMAGE. REFERENCE WRI 25-50 4035 FOR THE OTHER SEAT TRACK DAMAGE. REMOVED DAMAGED SEAT TRACK, MATCH DRILLED & COUNTERSINK NEW IAW SRM 53-00-52-2R FIG 201. TREATED & PRIMED, INSTALLED NEW SEAT TRACK IAW SRM 53-00-52-2R FIG 201. OK TO CLOSE FLOOR PANELS. INSTALLED FLOORBOARDS & THE LOADING SYSTEM IAW SRM 51-31-01 & AMM 25-59-25-4. REPLACED DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R FIG 201. INSTALLED FLOOR PANELS IAW SRM 51-31-01 & INSTALLED LOADING SYSTEM IAW AMM 25-59-25-4.

Part: SEAT TRACK — WORN (MCD) · airframe 768 hrs · 17,425 cycles

MAIN DECK SEAT TRACK BETWEEN POSITION 9L & 10L IS LOOSE. THE FORWARD SEAT TRACK LOBE IS WORN, WILL NOT HOLD LOCK IN POSITION. NO STRUCTURAL DAMAGE FOUND. LOCK IS R & R IN COAT CLOSET. REPLACED DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R FIG 201. INSTALLED FLOOR PANELS IAW SRM 51-31-01 & INSTALLED LOADING SYSTEM IAW AMM 25-59-25-4.

Part: BUTTON — BROKEN (L1 DOOR) · airframe 768 hrs · 17,408 cycles

DOOR 1 LT RAFT SYS TEST BULB INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-02. 1L DOOR EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. BUTTON IS BROKEN, REPLACED BATTERIES. REPLACED LIGHT CAP ASSEMBLY

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 759 hrs · 17,154 cycles

AIR SYS MANUAL MODE, 2000 AGL NR 3 PACK SHUTDOWN, MANIFOLD NR 3 DEPRESSURIZED. AIR SYS OFF ALERT. ON DECAY CHECK , FOUND PNEUMATIC LEAK FROM RT FWD LOWER CARGO COMPARTMENT, AFT OF NR 3 AC FLOW CONTROL VLV, BETWEEN BULKHEAD. R & R DUCT ASSEMBLY IAW AMM 36-23-01-4. GND OPERATIONS CHECKED NORMAL. NO LEAKS NOTED. DECAY CHECK PASSED.

Part: SKIN — CRACKED (RT WING) · airframe 73,934 hrs · 16,516 cycles

FOUND CRACK ON RT WING AT OTBD SLAT TRACK CUT OUT FOR NR 6 SLAT. VERIFIED BY NDT. REMOVED LWR RT WING PANEL 626EB & PLACED IN COURIER COMPARTMENT. REMOVED DAMAGED SKIN IAW SRM 57-40-02 REPAIR 7 FIGURE 201. PERFORMED HFEC OF CUT OUT AREA IAW NTM PT 6. NO CRACKS NOTED. FABRICATED DOUBLER & FILLER, DRILLED & PRIMED PARTS IAW SRM 57-40-02 REPAIR 7. OK TO INSTALL. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 57-40-02 REPAIR 7. STILL REQUIRES PAINT & PANEL TO BE INSTALLED. APPLIED EXTERIOR PAINT FINISH IAW SRM 51-21-02. INSTALLED REPAIR DOUBLER & FILLER SRM 57-40-02 REPAIR 7. STILL REQUIRES PAINT & PANEL TO BE INSTALLED.

Part: SLIDE RAFT — INOPERATIVE (R1 DOOR) · airframe 72,706 hrs · 16,099 cycles

R1 DOOR SLIDE INFLATION CYLINDER LOW PRESS LIGHT ILLUMINATED. R & R RT EVACUATION SLIDE RAFT CONTAINER IAW MM 25-61-01-4 & ADJUST TEST IAW MM 25-61-01-5.

Part: CARGO TRACK — CORRODED (BS 1411-1491) · corrosion level 2 · airframe 72,685 hrs · 16,095 cycles

MAIN DECK CARGO TRACK AT BS 1411-1491, X=-75.25, FLANGE AREA FOUND CORRODED. CARGO TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1391 - 1531 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,685 hrs · 16,095 cycles

FOUND SEAT TRACK CORRODED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 72,685 hrs · 16,095 cycles

FOUND FLOOR SUPPORT TIE-DOWN INBD AREA WITH CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01, REVISION 53. NEW FLOOR SUPPORT FABRICATED IAW DWG WSP 0668, REVISION B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: LONGERON SPLICE — CRACKED (BS 1651 L44R) · airframe 72,685 hrs · 16,095 cycles

CENTER CARGO LONGERON SPLICE 44R CRACKED AT BS 1651. LONGERON SPLICE FABRICATED IAW DWG AFA7105 REVISION H. REMOVED AND REPLACED WITH NEW IAW SRM 51-33-01, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: LONGERON — CORRODED (BS 1641-1651) · corrosion level 2 · airframe 72,685 hrs · 16,095 cycles

CENTER CARGO LONGERON 44R, FOUND CORRODED AT BS 1641-1651. REPAIRED IAW SRM 53-00-05 FIGURE 201/202, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 72,685 hrs · 16,095 cycles

RIGHT WING L/E SLAT DRIVE MECHANISM ACCESS PANEL 618FB LT FORWARD CUTOUT AREA CRACKED APPROXIMATELY 0.75" AT WS XOS 490. REPAIRED IAW SRM 57-40-02, FIGURE 202, REPAIR 7, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 72,685 hrs · 16,095 cycles

CENTER CARGO, LONGERON SPLICE CRACKED AT BS 5-123, LONGERON 39L. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114, REVISION J. REMOVED AND REPLACED WITH NEW SPLICE IAW SRM 51-33-01, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT BEAM — CRACKED (BS 1746) · airframe 72,685 hrs · 16,095 cycles

CENTER CARGO DOOR ACTUATOR SUPPORT BEAM CRACKED AT BS 1746. REPAIRED IAW SRM 53-50-15 FIGURE 201, REPAIR 2, REVISION 53 AND EA1-5310-T0206160 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118

Part: CARGO TRACK — CORRODED (BS 1942) · corrosion level 2 · airframe 72,685 hrs · 16,095 cycles

MAIN DECK CARGO DOOR FLOOR CARGO TRACK AT BS 1942, LBL 107.25, FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1831 TO 2007 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118

Part: STRUCTURE — DAMAGED (LT WING SLAT) · airframe 69,944 hrs · 15,213 cycles

ON POST FLT INSPECTION, FOUND DAMAGE TO L/E SLATS NR 7 AND NR 8 STAINLESS SHIELD. DAMAGED FITS BETWEEN SLATS. ON FURTHER INSPECTION FOUND MISSING CONNECTING BOLT . DAMAGE TO THE L/E STRUCTURE WHERE SLAT TRACK SLIDES INTO WING. REPAIRED LT WING FIXED LEADING EDGE IAW E.A. 1-5710-163664.

Part: TEE FITTING — CORRODED (AFT BULKHEAD) · airframe 67,863 hrs · 14,636 cycles

AFT WASTE TANK COMPARTMENT AFT PRESSURE BULKHEAD STA 2007, X=-20 (APPROX) FOUND TEE WITH CORROSION.

Part: PANEL — CRACKED (300) · airframe 67,863 hrs · 14,636 cycles

RT AIR INTAKE DUCT REAR CENTER SPAR TO REAR SPAR LOWER PANEL (364RR) FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02 REPAIR 2 FIG.201 REV.48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 113.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 67,863 hrs · 14,636 cycles

LEFT AIR INTAKE DUCT REAR CENTER SPAR TO REAR SPAR LOWER PANEL (363PL) FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02 FIG.201 REPAIR 2 REV.48 REPAIR CLASSIFIED AS MAJOR AS GMM 6-2-100 REVISION 113.

Part: RELIEF VALVE — FAILED (MLG) · airframe 66,865 hrs · 14,393 cycles

ATB LDG GR HANDLE WILL NOT COME UP. FOLLOWED QRH AND ATB. FOUND RELIEF VALVE FOR TRIM CYLINDER HAD COME APART. REPLACED TRIM VALVE IAW MM-32-37-03-4, ON LT MAIN GEAR.

Part: WIRE HARNESS — CHAFED (NR 1 GENERATOR) · airframe 65,398 hrs · 14,008 cycles

NR 1 ENGINE GENERATOR LEADS T2 AND GRD CHAFED AND ARCHED TO COOLING AIRDUCT BRACKET NEAR FWD ENGINE MOUNT. NO RESTRICTION NR1 ENGINE GENERATOR FEEDER CABLE IS DAMAGE DUE TO CHAFE CONDITIONS. INSTRUCTIONS TO MX FOR WRAPPING DAMAGE FEEDER CABLE IAW EA1-2420-146089. COMPLIED WITH PART 1 OF EA 1-2420-146069 , ACFT OK FOR SERVICE. R & R THE NR1 ENGINE IDG FEEDER CABLES REF WD24-21-11 & SMP. ALSO R & R THE NR1 GCU REF 24-21-03-4-0 FOR EPCU RTS FAILING GCU-1, RAN NR1 ENG IAW JRH AND PERFORMED EPCU RTS, ALL TEST PASS. SYS OK FOR SERVICE. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 1841) · corrosion level 2 · airframe 62,395 hrs · 13,288 cycles

CTR CARGO FLOOR PANEL NR 183XB AFT SUPPORT AT STA 1841 FOUND CORRODED. CTR CARGO FLOOR PANEL NR 183XB AFT SUPPORT AT STA 1841 REPAIR CARRIED OUT IAW EA 1-5320-137504. TITLE FUSELAGE LWR CTR CARGO AFT FLOOR PANEL SUPPORT AT STA. = 1841. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 109.

Part: VANE — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT OTBD FLAP VANE NR1 T-FITTING FWD LUG HOLE. REPAIR CARRIED OUT IAW EA 1-5750-137514, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: VANE — CORRODED (TE FLAPS) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT OTBD FLAP VANE NR2 T-FITTING FWD LUG HOLE. REPAIR CARRIED OUT IAW EA NR 1-5750-137515, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: VANE — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT OTBD FLAP VANE NR 5 T-FITTING FWD LUG HOLE. REPAIRED IAW EA 1-5750-137517. REPAIR CLASSIFIED AS MAJOR IAW 6-2-100 REV 109.

Part: VANE — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

RT OTBD FLAP VANE NR 4 T-FITTING FWD LUG HOLE HAS CORROSION. REPAIR CARRIED OUT IAW EA1-5750-137516, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: FRAME — CRACKED (MLG DOOR) · airframe 62,395 hrs · 13,288 cycles

RT MLG WHEEL WELL - RT MLG DOOR FOUND CRACKED NEAR THE DOOR CTR FITTING AREA. REPAIR CARRIED OUT IAW EA NR 1-3210-135697, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: FRAME — CRACKED (LT MLG DOOR) · airframe 62,395 hrs · 13,288 cycles

LT MLG WHEEL WELL - LT MLG DOOR FOUND CRACKED NEAR THE DOOR CTR FITTING AREA. REPAIR CARRIED OUT IAW EA 1-3210-135696, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,395 hrs · 13,288 cycles

MAIN DECK - SEAT TRACK AT STA 635 X = -27 FOUND CRACKED. MAIN DECK - CRACKED SEAT TRACK AT STA 635 X = -27 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665 X = -27 IAW SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,395 hrs · 13,288 cycles

MAIN DECK - SEAT TRACK AT STA 635 X = 47 FOUND CRACKED. CRACKED SEAT TRACK AT STA 635 X = 47 REPAIRED BY SECTIONAL SEAT TRACK. REPLACEMENT FROM STA 625 TO STA 645 X = 47 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,395 hrs · 13,288 cycles

MAIN DECK - SEAT TRACK AT STA 635 X = 8 FOUND CRACKED. MAIN DECK-CRACKED SEAT TRACK AT STA 635 X = 8 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665 X = 8 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 42. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 62,395 hrs · 13,288 cycles

MAIN DECK - SEAT TRACK AT STA 635 X = 27 FOUND CRACKED. MAIN DECK-CRACKED SEAT TRACK AT STA 635 X = 27 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 645 X = 27 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,395 hrs · 13,288 cycles

MAIN DECK CARGO - SEAT TRACK FOUND CORROSION AT STA 1272 TO STA 1304 X = -75. MAIN DECK CARGO - SEAT TRACK CORROSION AT STA 1272 TO STA 1304 X = -75 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1269 TO STA 1391 X = -75 IAW SRM 53-00-52, FIGURE 201 REPAIR 1 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: DOUBLER — CORRODED (RT WING) · airframe 62,395 hrs · 13,288 cycles

RT WING T/E CAVITY LANDING GEAR AREA LOWER WING DOUBLER UPPER SURFACE FOUND CORROSIONS. CORROSION REMOVED AND REPROTECTED AT RT WING T/E CAVITY LANDING GEAR AREA LWR WING DOUBLER UPPER SURFACE IAW SRM 51-21-01 REVISION 42 AND FOUND WITHIN LIMIT SRM 57-10-02 FIGURE 101 REVISION 42. ORIGINAL THICKNESS = 0.085", MATERIAL REMOVED = 0.007" AND REMAINING THICKNESS = 0.078". REPAIR CLASSIFIED AS MINOR GMM 6-2-100 REVISION 109.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING OTBD FLAP INBD HINGE (WING SIDE) LWR MOUNT NR 7 INBD HOLE. REPAIRED IAW EA NR1-5750-135684. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — CRACKED (LT WING) · airframe 62,395 hrs · 13,288 cycles

CRACK AROUND FASTENER HOLES (06 EACH) AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS690 TO XORS700 FOUND DURING HFEC. REPAIR CARRIED OUT IAW EA 1-5710-135699, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.

Part: HINGE BRACKET — WORN (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

WORN - BUSHING AT RT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 OTBD HOLE. REPAIRED IAW EA 1-5750-135689. REPAIR CLASSIFIED AS MAJOR IAW 6-2-100 REV 109.

Part: HINGE BRACKET — WORN (TE FLAPS) · airframe 62,395 hrs · 13,288 cycles

WORN - BUSHING AT LT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 OTBD HOLE. ACTUATOR ATTACHMENT NR 8 OTBD HOLE AT LT WING OTBD FLAP INBD HINGE REPAIRED EA 1-5750-135684. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 OTBD HOLE. REPAIRED IAW EA 1-5750-135688. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 109.

Part: SKIN — CRACKED (RT WING) · airframe 62,395 hrs · 13,288 cycles

CRACK AROUND FASTENER HOLES (04 EACH) AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS690 TO XORS700 FOUND DURING HFEC. REPAIR CARRIED OUT IAW EA NR1-5710-135698, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.

Part: HINGE BRACKET — WORN (TE FLAPS) · airframe 62,395 hrs · 13,288 cycles

BUSHING AT RT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 INBD HOLE. REPAIRED IAW EA 1-5750-135689. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING OTBD FLAP OTBD HINGE (WING SIDE) LWR MOUNT NR 3 OTBD HOLE AFT SURFACE. LOWER MOUNT NR 3 OTBD HOLE AFT SURFACES AT LT WING OTBD FLAP OTBD HINGE REPAIRED IAW EA 1-5750-135683. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORRODED RT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT POINT NR1 INBD HOLE. REPAIRED IAW EA 1-5750-135692. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT POINT NR1 INBD HOLE. REPAIRED IAW EA 1-5750-135691. REPAIR CLASSIIFED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING OTBD FLAP INBD HINGE (WING SIDE) BARREL NUT NR 2B HOLE EXTERIOR SURFACE. BARREL NUT NR 2B HOLE EXTERIOR SURFACE AT LT WING OTBD FLAP INBD HINGE (WING SIDE) REWORKED IAW CMM 20-11-02 REVISION 65 AND FOUND WITHIN LIMIT IAW DWG ARC0502, SHEET 4, REVISION BN LIMITS AND CMM 57-44-08 REVISION 24, FIGURE 604, REWORK LIMIT. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 INBD HOLE.REPAIR CARRIED OUT IAW EA 1-5750-135688, REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT WING OTBD FLAP INBD HINGE (FLAP SIDE) PIVOT POINT NR3 INBD HOLE. REWORKED AND FOUND LIMIT IAW EA 1-5750-135690. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 109.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT POINT NR 1 OTBD HOLE. REPAIRED IAW EA 1-5750-135691. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: ATTACH FITTING — CORRODED (HINGE BRACKET) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 INBD HOLE. ACTUATOR ATTACHMENT NR 8 INBD BORE HOLE AT LT WING OTBD FLAP INBD HINGE (WING SIDE) REPAIRED IAW EA 1-5750-135684. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING OTBD FLAP OTBD HINGE (WING SIDE) BARREL NUT NR 7 HOLE LWR SURFACE. REWORKED FOUND WITHIN LIMIT IAW DWG ARC0503 SHEET 2 REV BG AND CMM 57-44-09 FIG 601 REV 15.

Part: HINGE BRACKET — WORN (TE FLAPS) · airframe 62,395 hrs · 13,288 cycles

WORN BUSHING AT LT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR ATTACHMENT NR 8 INBD HOLE. ACTUATOR ATTACHMENT REPAIRED IAW EA 1-5750-135683. HOLE MEASURED DIA 1.248" MAX DIA 1.220" REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (TE FLAP) · airframe 62,395 hrs · 13,288 cycles

CORROSION - RT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT POINT NR 1 OTBD HOLE. REPAIRED IAW EA 1-5750-135692. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 62,395 hrs · 13,288 cycles

CORROSION - LT WING OTBD FLAP OTBD HINGE (WING SIDE) LWR MOUNT NR 3 INBD HOLE. REPAIRED IAW EA 1-5750-135683. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

EXISTING REPAIR AT MAIN DECK CARGO RT STA 535 FRAME, 9G NET LWR YOKE SUPPORT. EXISTING REPAIR AT MAIN CARGO RT STA 535 9G NET LWR SUPPORT YOKE EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SASCO 304. EXISTING REPAIR AT MAIN DECK CARGO RT STA 535 9G NET LWR SUPPORT YOKE REMOVED AND NEW REPAIR INSTALLED IAW EA 1-5310-137503. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 FRAME, 9G NET UPPER SUPPORT YOKE EVALUATED AND FOUND NOT IAW ANY SRM REPAIR. REPAIR CARRIED OUT IAW EA NR 1-5310-137502, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 FRAME 9G NET UPPER SUPPORT YOKE. EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 9G NET LWR SUPPORT YOKE EVALUATED & FOUND NOT IAW ANY SRM REPAIR . EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 9G NET LWR SUPPORT YOKE REMOVED & NEW REPAIR INSTALLED IAW EA 1-5310-137502. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 109.

Part: RIB — MISREPAIRED (LT WING TE FLAP) · airframe 62,395 hrs · 13,288 cycles

LT WING INBD FLAP OTBD RIB AT STA XIFH 303.445 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP OTBD RIB AT STA XIFH 303.445 EVALUATED AND FOUND NOT IAW SRM 57-00-00 FIGURE 205 REPAIR GENERAL REV 42. EXISTING REPAIR AT LT WING INBD FLAP OTBD RIB AT STA XIFH 303.445 REMOVED AND NEW REPAIR WEB INSTALLED IAW DWG ARC2305 REVISION C. EO NR 1-5100-7-5001 PART 1, TITLE: STRUCTURES -REPAIR ID AND TRACKING REQUIREMENTS 14 CFR 121.707 HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SKIN — MISINSTALLED (ZONE 100) · airframe 62,395 hrs · 13,288 cycles

EXISTING REPAIR - AFT CARGO DOOR MID AFT AREA FOUND EXISTING REPAIR. EXISTING REPAIR AFT CARGO DR MID AFT AREA REMOVED & REPAIRED IAW EA 1-5230- 137513. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109. EO 1-5100-7-5001 A4 PT1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

CABIN - RT STA 1541 TO STA 1561 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 1 REV 42 (MAJOR REAPIR).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

LT STA 1291 TO STA 1311 X = 8.5 SEAT TRACK FOUND CORROSION. CORRODED SEAT TRACK AT LT STA 1291 TO STA 1311 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1229 TO STA 1321 X = 8.5 IAW SRM 53-00- 52 FIGURE 201 REPAIR 1 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

RT STA 6-0 TO STA 6-30 X = -8.5 SEAT TRACK FOUND CORROSION. CORRODED SEAT TRACK AT RT STA 6-0 TO STA 6-30 X = -8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 6-0 TO STA 6-100 IAW SRM 53-00-52, FIGURE 201 REPAIR 1, REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,395 hrs · 13,288 cycles

LWR FUSELAGE EXTERIOR RT STA 755 BETWEEN LONGERON 28, RT AND LONGERON 29 RT, FOUND WITH EXISTING DOUBLER REPAIR. EXISTING REPAIR AT LWR FX EXTERIOR RT SIDE STA 755 L28R TO L29R EVALUATED & FOUND NOT IAW SRM 53-00-01 REPAIR 1 FIG 201 REV 42 SASCO 398. EXISTING REPAIR AT LWR FX EXTERIOR RT SIDE STA 755 L28R TO L29R REMOVED & NEW REPAIR INSTALLED IAW EA 1-5330-137508. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 62,395 hrs · 13,288 cycles

RT WING DROOP L/E INBD LWR CORNER FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING DROOP L/E INBD LWR CORNER EVALUATED AND FOUND NOT IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION 42. REPAIR CARRIED OUT IAW EA NR 1-5750-137511, TITLE: WINGS - FLIGHT SURFACES - RT WING DROOP L/E SKIN REPAIR. EO 1-5100-7-5001 PART 1, TITLE: STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,395 hrs · 13,288 cycles

EXISTING REPAIR - CTR CARGO DOOR FWD LWR CORNER FOUND EXISTING REPAIR. EXISTING REPAIR AT CTR CARGO DOOR FWD LWR CORNER EVALUATED AND FOUND NOT IAW SRM 52-30-10 FIG 201 REPAIR 3 REV 42 SASCO225. EXISTING REPAIR AT CTR CARGO DOOR FWD LWR CORNER REMOVED AND NEW REPAIR INSTALLED IAW SRM 52-30-16 FIG 201. REPAIR 3 REV 42 EO 1-5700-7-5001 A4 PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 62,395 hrs · 13,288 cycles

LT WING INBD FLAP UPPER AFT SKIN AT STA XIFH 190 FOUND WITH EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP UPPER AFT SKIN AT STA XIFH 190 EVALUATED AND FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT IAW EA NR 1-5750-137510, TITLE: WINGS - FLIGHT SURFACES - LT INBD FLAP UPPER SKIN PANEL REPAIR. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 62,395 hrs · 13,288 cycles

CABIN - RT STA 1581 TO STA 1601 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED IAW SRM 53-00-52, FIG 201 REPAIR 1 REV 42 (MAJOR REAPIR).

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,395 hrs · 13,288 cycles

AFT CARGO DOOR FWD LWR CORNER FOUND EXISTING REPAIR. EXISTING REPAIRAT AFT CARGO DOOR FWD LWR CORNER EVALUATED & FOUND NOT IAW ANY SRTM REPAIR SASCO 324. EXISTING REPAIR AT AFT CARGO DOOR FWD LWR CORNER REMOVED AND NEW REPAIR INSTALLED IAW EA 1-5230-137513 TITLE DOORS CARGO DOORS AFT CARGO DOOR OUTER SKIN SLICE REPAIR. EO E1-5100-7-5001 A4 PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 109.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 62,395 hrs · 13,288 cycles

FUSELAGE RT SIDE STA 311 BETWEEN LONGERON 26R AND LONGERON 27R FOUND WITH EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR AT FUSELAGE RT SIDE STA 311 BETWEEN LONGERON 26R AND LONGERON 27R EVALUATED AND FOUND NOT IAW SRM 53-00-01 FIGURE 201, REPAIR 1, REV 42. EXISTING DOUBLER REPAIR AT FUSELAGE RT SIDE STA 311 BETWEEN LONGERON 26R AND LONGERON 27R REMOVED AND NEW REPAIR INSTALLED IAW SRM 53-00-01 FIGURE 201, REPAIR 1,REVISION 42. EO NR 1-5100-7-5001 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.

Part: CONNECTOR — LEAKING (HYD SYSTEM) · airframe 58,368 hrs · 12,317 cycles

AFTER SLAT RETRACTION ON CLIMB OUT, RECEIVED "HYD 3 ELEV OFF" ALERT. APPROX 5 MINUTES LATER, GOT "HYD 3 FAIL" ALERT. COMPLIED WITH QRH. MANUALLY EXTENDED GEAR ON APPROACH. HYD LEAK FROM NR 1 HORIZ STAB TRIM MOTOR BODY. REMOVED AND REPLACED STAB TRIM MOTOR, MM27-43-30-4. DURING OPS CHECK FOR HORIZ STAB HYD OPS SYS, FOUND "HORIZ STAB TRIM RATE CTRL 2" C/B POPPED. TROUBLESHOT AND C/B STAYED IN AFTER DISCON ELEC CON FROM M1-16, BUT IT TRIPS IMMEDIATELY WHEN STATES ABOVE CONNECTOR RECONNECTED. TROUBLESHOT AND FOUND SHORT INSIDE OF DUAL SOLINOID VALVE ON M1-16 TRIM MOT REF WDM 22-22-01 P501. REMOVED AND REPLACED PER MM 27-43-41-4 AND HORIZ STAB HYD OPS NORM WITH NO LEAK PER MM 27-40-00-5.

Part: ACTUATOR — LEAKING (STAB TRIM) · airframe 58,368 hrs · 12,317 cycles

AFTER SLAT RETRACT ON CLIMB-OUT, RECEIVED " HYD 3 ELEV OFF " ALERT. APPROX 5 MINS LATER, GOT "HYD 3 FAIL" ALERT. COMPLIED WITH QRH. MANUALLY EXTENDED GEAR ON APPROACH. HYD LEAK FROM NR 1 HORIZ STAB TRIM MOTOR BODY. R & R STAB TRIM MOTOR, MM 27-43-30-4. DURING OPS CHECK, FOUND "HOR STAB TRIM RATE CTRL 2" C/B POPPED. TROUBLESHOT & C/B STAY IN AFTER DISCON ELEC CON FROM M1-16, BUT TRIPS WHEN STATES ABOVE. CONNECTOR RECONNECTED. TROUBLESHOT & FOUND SHORT INSIDE OF DUAL SOL VALVE ON M1-16 TRIM MOT. REF WDM 22-22-01 P501. R & R PER MM 27-43-41-4 & H-STAB HYD OPS NORM NO LEAKS PER MM 27-40-00-5. FCC-1/-2 AFS RTS PER MM 22-01-01-5 & ALL TESTS PASS. ACFT RTS. PER MM 22-01-01-5 & ALL TESTS PASS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,780 hrs · 12,184 cycles

MID CABIN AFTER REMOVAL OF FLOOR PANELS AT APPROXIMATELY STATION 1540, X = - 75.50, FOUND SEAT TRACK FLANGE CORROSION. CABIN STATION 1540, X = -75.50, SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG 6, VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 57,780 hrs · 12,184 cycles

LEFT WING LEADING EDGE STRINGER AT STATION XOS 672 FOUND CRACKED OFF. REPAIR CARRIED OUT AS PER EA 1-5720-122504, REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MID CABIN AFTER REMOVAL OF FLOOR PANELS AT APPROXIMATELY STATION 5-33, X = - 75.5 FOUND SEAT TRACK FLANGE STRUCTURE CORROSION. SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG.1, VOL.1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · airframe 57,780 hrs · 12,184 cycles

SKIN UNDER RIGHT BODY FAIRING NR 347DF, 01 EACH SURFACE CORROSION FOUND NEAR FASTENER HOLE AT STATION 2155. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. EXCEEDED LIMITS AS PER SRM 53-00-01, FIG. 2, VOL.I. REPAIR CARRIED OUT AS PER SRM 53-20-00, FIG.13, VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STANCHION — CORRODED (ZONE 100) · airframe 57,780 hrs · 12,184 cycles

FORWARD CARGO COMPARTMENT, FOUND COMPARTMENT AFT BULKHEAD LINER SUPPORTING STANCHION CORRODED AT STATION 6-73.5, X = -9". FORWARD CARGO COMPARTMENT AFT BULKHEAD LINER SUPPORTING STANCHION AT STATION 6-73.5, X = -9" CORROSION REMOVED AS PER SRM 51-21-01, VOL.II. MATERIAL REMOVED 0.092", ORIGINAL THICKNESS 0.100", REMAINED THICKNESS 0.008", AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-01, FIG.2, VOL.I. STANCHION REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW STANCHION REWORKED AS PER DRAWING A6A7094. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 57,780 hrs · 12,184 cycles

RIGHT WING LEADING EDGE STRINGER AT XOS 672 FOUND CRACKED OFF. REPAIR CARRIED OUT AS PER EA 1-5720-122505, REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 700) · airframe 57,780 hrs · 12,184 cycles

DURING HFEC INSPECTION, MULTIPLE CRACKS (05 EACH, TOTAL LENGTH APPROX 1.2 INCH) FOUND AT FASTENER HOLE OF LONGERON ADJACENT TO NOSE LANDING GEAR LEFT TRUNNION FITTING. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 57,780 hrs · 12,184 cycles

CENTER LANDING GEAR WHEEL WELL STATION 1391 LEFT WEB CORNER DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON-3 RIGHT FORWARD SECTION EDGE. CRACK LENGTH APPROXIMATELY 0.3 INCH. REPAIR CARRIED OUT AS PER EA 1-5310-122735, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: VANE — DELAMINATED (TE FLAP) · airframe 57,780 hrs · 12,184 cycles

LEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM STATION XIFH 156 TO XIFH 206. LEFT WING INBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-22-5.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 1 O'CLOCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES NR B, NR C AND NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 4 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 57,780 hrs · 12,184 cycles

NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. AREA TRIMMED OUT AND REPAIRED AS PER SRM 53-40-00, FIG.23, VOL.I. PER SRM 53-40-00, FIG.23, VOL.I, OPTION 2: REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 8 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A , NR B , NR C AND NR D (THIRD LAYER). MAIN CARGO DOOR LOWER JAMB, CRACKED NR 6 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 2 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 4 O'CLOCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLE NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D (THIRD LAYER). MAIN CARGO DOOR LOWER JAMB, CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 10 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLE NR C (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 57,780 hrs · 12,184 cycles

02 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122496 PART 1. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A AND NR C (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 57,780 hrs · 12,184 cycles

MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES NR C AND NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. NEW FITTING FABRICATED AS PER EA1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 57,780 hrs · 12,184 cycles

03 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122497 PART 1. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 53,125 hrs · 11,162 cycles

FOUND LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 CORROSION. LT WING, REAR SPAR LOWER CHORD AT STA 1063 - 1075 REPAIRED AS PER FEDEX EA NR 1- 5710- 105615, WINGS, LEFT WING LOWER SPAR CAP AFT FLANGE CORROSION BETWEEN XORS=1063 AND XORS=1075 - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CAP — CORRODED (ZONE 500) · airframe 53,125 hrs · 11,162 cycles

LT WING, REAR SPAR UPPER CHORD AT STA 1035-1043 FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5710-105616, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.

Part: RELAY — BURNED (ZONE 100) · airframe 53,125 hrs · 11,162 cycles

ELECTRICAL ARCING AT NR 1 EPC BAY LT TOP SIDE RELAY R2-53, R2-57, R2-102 AND R2-252 AFFECTED. REMOVED AND REPLACED 4 RELAYS R2-53, R2-57, R2-102 AND R2-252 AS PER STANDARD WIRING PRACTICES MANUAL. WIRINGS SPLICE REPAIRED AS PER STANDARD WIRING PRACTICES MANUAL. WIRINGS CONTINUITY CHECKED AS PER WDM 28-22-01, WDM 28-22-02, WDM 28-22-04 AND WDM 28-22-05, FOUND SATISFACTORY BOOST PUMPS. OPS CHECK CARRIED OUT AS PER AMM 28-22-01-5, FOUND SATIS.

Part: LONGERON — CORRODED (ZONE 100) · airframe 53,125 hrs · 11,162 cycles

FORWARD CARGO COMPARTMENT: BILGE AREA LONGERON 52 AT STA 979 UPPER FLANGE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5330-105625, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 53,125 hrs · 11,162 cycles

WASTE TANK COMPARTMENT, LONGERON 43R END FITTING AT STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 53,125 hrs · 11,162 cycles

AFT CARGO COMPARTMENT, RIGHT TUNNEL AREA LONGERON 38R SPLICE AT STA 1863 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.

Part: LONGERON — CRACKED (ZONE 100) · airframe 53,125 hrs · 11,162 cycles

AFT CARGO COMPARTMENT RT TUNNEL AREA, LONGERON 38R AT STA 1863 FOUND CRACKED. REPAIRED AS PER SRM 53-10-00 VOLUME I, FIGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 53,125 hrs · 11,162 cycles

CENTER CARGO COMPARTMENT, BILGE AREA LONGERON 50L AT FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5310-105620, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · airframe 53,125 hrs · 11,162 cycles

CENTER CARGO COMPARTMENT BILGE AREA LONGERON 52 AT STA 1531 FOUND CORRODED REPAIR CARRIED OUT PER FEDEX EA 1-5310-105623, FUSELAGE, LONGERON L52 AT STA 5-102, SRM SPLICE CLASSIFICATION. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,125 hrs · 11,162 cycles

LOWER FUSELAGE EXTERIOR, NR 1 AIRCON EXHAUST CUTOUT CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-50-00 VOLUME I, FIGURE 16. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 14L (XORS 521), APPROX 13 INCHES LENGTH ON LT WING TANK DURING HFEC INSPECTION. CRACK ON LT WING AT STRINGER END 14L (XORS 521) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. REPAIRED AS PER SRM 57-20-00 VOLUME I, FIGURE 10. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 13 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RT WING AT STRINGER END 11R (XORS 704) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 9R (XORS 819), APPROX 11 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RT WING AT STRINGER END 9R (XORS 819) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 13R (XORS 577), APPROX 13.5 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING AT STRINGER END 13R (XORS 577) REPAIRED AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 14R (XORS 521), APPROX 14.5 INCHES LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING AT STRINGER END 14R (XORS 521) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 13L (XORS 577), APPROX 13 INCHES LENGTH ON LEFT HAND WING TANK DURING HFEC INSPECTION. CRACK ON LT HAND WING AT STRINGER END 13L (XORS 577) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 53,125 hrs · 11,162 cycles

CRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 12 INCHES LENGTH ON LT WING TANK DURING HFEC INSPECTION. CRACK ON LT WING AT STRINGER END 12L (XORS 642) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 54,439 hrs · 11,040 cycles

CRACK FOUND AT STRINGER END 12R (XORS 642), APPROX 13 INCHES LENGTH ON RIGHT HAND WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING (XORS 642) AT STRINGER END 12R REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: UNKNOWN — MALFUNCTIONED · airframe 52,316 hrs · 10,981 cycles

ON APPROACH, BEFORE AND AFTER SLATS EXT, RUDDER PEDALS WERE EXTREMELY LOOSE. TRAVEL BETWEEN PEDALS WAS - 3-4" EACH WITH NO RUDDER MOVEMENT. ALSO NO RESISTANCE IN THE FIRST 3-4" OF PEDAL TRAVEL. VERIFIED 3-4" OF RUDDER PEDAL MOVEMENT BEFORE ANY MOVEMENT OF RUDDER. PER CREW DEBRIEF A/C HAD BEEN IN HEAVY RAIN. MOVED A/C TO HANGER. AFTER A COUPLE OF HOURS LARGE AMOUNT OF WATER DRAINED FROM TAIL AND WHEEL WELLS OF A/C. FOUND CHUNK OF ICE ON INSIDE OF ACCESS DOOR OF TAIL COMP. INSPECTED RUDDER PEDALS, QUADRANTS AND CABLE RUNS, NO DEFECTS NOTED. INSPECTED AND LUBED RUDDER CONTROL MECHANISM PER SMP. NO DEFECTS NOTED. PERFORMED RTS OF FCC 1 AND 2 RUDDER SYSTEM ALL TESTS PASSED. OKAY FOR SERVICE.

Part: WIRE — DAMAGED (FUEL SYSTEM) · airframe 51,510 hrs · 10,799 cycles

FOUND WIRE BUNDLE DAMAGED IN RT AFT SPAR AREA INBD OF RT MAIN GEAR. WIRE NR" SE201-21-16A, E201-22-16B AND E201-23-16C BURNED THRU ABOUT 1 TO 2 FT INBD OF T-STRIP S3-375. WIRES ARE 3 PHASE WIRES FOR R AFT FUEL PUMP M1-1108. PULLED AND COLLARED AFFECTED C/B. TERMINATED 3 NEW PHASE WIRES AT T STRIP S3-375. REPAIRED WIRES E210-21-16A, E201-22-16B, E210-23-16C TO TERM STRIP S3-375 PER SMP CHAP 20. REMOVED AND REPLACED RIGHT AFT RCCB B1-679, CONTROL RELAY R2-59 & NR 3 AFT BOOST PUMP. ALL OPS AND LEAK CK GOOD.

Part: CONTROLLER — MALFUNCTIONED (ENVIRON) · airframe 49,927 hrs · 10,437 cycles

RCVD LEVEL 2 AVIONICS AIR FLOW OFF, THEN AVIONICS FAN O'VRD CAME ON. NO -ESC- CURRENT FAULTS NOTED, -ESC- FAULT REVIEW INDICATES NO FAULTS LAST LEG, -EC- SENSOR READOUTS NORMAL. PERFORMED -ESC- RETURN TO SERVICE CK, SYS PASS. REMOVED AND REPLACED ENV SYSTEM CONTROLLER PER MD11 AMM 21-08-01-4, REMOVED AND REPLACED AIRFLOW SWITCH S1-139 PER MD11 AMM 21-26-05-2. ABLE TO DUPLICATE PROBLEM, WITH A/C PRESSURIZED AT 1.4 DELTA PSI. PRESSURIZED A/C AGAIN AFTER PARTS CHANGED, AND OPERATIONAL CHECK OF AVIONICS COOLING NORMAL, AND NO LEAKS NOTED IN A/C STRUCTURE.

Part: FITTING — CORRODED (ZONE 700) · airframe 48,152 hrs · 10,022 cycles

EVIDENCE OF MINOR SURFACE CORROSION FOUND ON CENTER LANDING GEAR LEFT TRUNNION FITTING LOWER MATING SURFACE AREA. CORROSION MACHINED OFF AND FOUND WITHIN LIMIT AS PER SRM 53-40-00.

Part: FITTING — CORRODED (ZONE 700) · airframe 48,152 hrs · 10,022 cycles

EVIDENCE OF SURFACE CORROSION FOUND ON CENTER LANDING GEAR RIGHT TRUNNION FITTING LOWER MATING SURFACE AREA. SURFACE CORROSION ON CENTER LANDING GEAR RIGHT HAND TRUNNION FITTING LOWER MATING SURFACE AREA REMOVED AS PER SRM 51-21-01 VOLUME II PAGE 27. ORIGINAL THICKNESS = 2.650", MATERIAL REMOVED = 0.011", MATERIAL REMAINING = 2.639" FOUND WITHIN LIMITS AS PER SRM 53-40-00 VOLUME I FIGURE 15. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,152 hrs · 10,022 cycles

CABIN SEAT TRACK AT STATION Y1049, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,152 hrs · 10,022 cycles

MAIN DECK SEAT TRACK AT STATION Y1092, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,152 hrs · 10,022 cycles

MAIN DECK SEAT TRACK AT STATION Y1124, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,152 hrs · 10,022 cycles

CABIN SEAT TRACK AT STATION Y1019, -X8.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I AT STATION Y1009 TO STATION Y1129, -X8.5.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,152 hrs · 10,022 cycles

CABIN SEAT TRACK AT STATION Y1064, -X8.5 FOUND CORRODED. MAIN DECK SEAT TRACK AT STATION Y1009 TO STATION Y1129, -X8.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I. CLASSIFIED REPAIR AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 48,152 hrs · 10,022 cycles

MAIN DECK SEAT TRACK AT STATION Y5-02 TO 5-20, -X8.5 FOUND CORRODED. MAIN DECK SEAT TRACK AT STATION Y5-00 TO STATION Y5-123, -X8.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE I VOLUME I. CLASSIFIED REPAIR AS MAJOR AS PER GMM 6-2-100.

Part: DOOR — CRACKED (ZONE 700) · airframe 48,152 hrs · 10,022 cycles

SNRM N0364: RIGHT HAND MAIN LANDING GEAR FLIPPER DOOR FOUND WITH CRACK AS MARKED. REMOVED AND REPLACED WITH NEW PART AS PER AMM 32-14-10-4. ADJUSTMENT TEST CARRIED OUT AS PER AMM 32-31-00-5, FOUND SATIS.

Part: KEELBEAM — CRACKED (ZONE 700) · airframe 48,152 hrs · 10,022 cycles

CENTER LANDING GEAR FORWARD BULKHEAD, RT KEELBEAM DOUBLER FOUND CRACKED AS MARKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01.

Part: KEELBEAM — CRACKED (ZONE 700) · airframe 48,152 hrs · 10,022 cycles

CENTER LANDING GEAR FORWARD BULKHEAD, LT KEELBEAM DOUBLER FOUND CRACKED AS MARKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01.

Part: SENSOR — MALFUNCTIONED (AOA) · airframe 44,492 hrs · 9,217 cycles

CAPTAINS PLI DROPPED TO FD PITCH BAR WHEN SLATS RETRACTED AND STICK SHAKER ACTUATED CAPTAINS SPEED INDICATOR BECAME RED, ALT MISS COMPARE, W/S DETECT FAIL ILLUMINATED, EVERYTHING WENT NORMAL WHEN SLATS EXTENDED. RETURNED TO MEM. FACT: REPLACED LT AOA SENSOR AFTER INTERROGATING NR 1 FCC SHOWING NR 1 AOA FAULTED FIVE TIMES OUT OF LAST SEVEN FLIGHTS. AFTER REPLACEMENT, REF MM 27-35-02-4, AOA SENSOR PASSED FCC RTS. AOA SENSOR REMOVED WAS NOT SMOOTH IN ITS MOVEMENT, VERY GRITTY.

Part: SPAR — DAMAGED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING - DURING ACCOMPLISHMENT OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGE TENSION STRAP SUPPORT REPLACEMENT, FOUND 2 EACH EXISTING HOLES OVERSIZED. REPAIR CARRIED AT RIGHT WING 2 EA EXISTING OVERSIZED HOLES OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGE TENSION STRAP SUPPORT AS PER EA 1-5750-74333, WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE, TWO OVERSIZED HOLES FOUND.

Part: FRAME — CRACKED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

AFT FUSELAGE COMPARTMENT, UPPER FUSELAGE FRAME CLIP AT CANTED AREA STA 2046 FOUND CRACKED. CRACKED CLIP AT CANTED AREA STA 2046 AT AFT FUSELAGE COMPARTMENT UPPER FUSELAGE FRAME REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. COMPLIED EA 1-5340-75915, FUSELAGE, MAINFRAME OVERSIZED HOLE ON FRAME STATION 2046.00.

Part: FITTING — CORRODED (ZONE 300) · airframe 43,248 hrs · 8,912 cycles

TAIL TANK - NR 14L BARREL NUT BORE FOUND CORRODED AT BEARING SURFACE. NEW NR 14L BARREL NUT BORE FITTING FABRICATED AS PER EA 1-5510-74321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. DAMAGED NR 14L BARREL NUT BORE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: FITTING — CORRODED (ZONE 300) · airframe 43,248 hrs · 8,912 cycles

TAIL TANK - NR 26L BARREL NUT BORE FOUND CORRODED AT BEARING SURFACE. NEW NR 26L BARREL NUT BORE FITTING FABRICATED AS PER EA 1-5510-74321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. DAMAGED 26L BARREL NUT BORE FITTING REMOVED AND REPLACED AS PER SRM 51-33-00 VOL II.

Part: SKIN — CORRODED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

CORROSION AT RT STA 1219 TO 1239 FROM RT X-8.5 - 27 ON CENTER WING UPPER SKIN. CORROSION AREA AS PER EA 1-5710-74330, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 43,248 hrs · 8,912 cycles

TAIL TANK - NR 1L BARREL NUT BORE CORROSION REWORK OUT OF LIMIT. TAIL TANK - NR 1L BARREL NUT BORE CORROSION REMOVED AS PER EA 1-5510- 75912, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - AD 2003-22-08

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

CABIN - INTERCOSTAL CRACKED AT LONGERON 7R, STA RT 1621 TO 1641.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

INTERCOSTAL CRACKED AT LONGERON 7R, STA RT 1581 TO 1601. INTERCOASTAL CRACKED AT LONGERON 7R, STA RT 1581 TO 1601 CARRIED OUT REPAIR IAW SRM 53-00-01 VOL I FIG 5.

Part: STRUCTURE — CORRODED (ZONE 300) · airframe 43,248 hrs · 8,912 cycles

TAIL TANK NR 26R BARREL NUT BORE EXCEEDED LIMIT DURING CORROSION REMOVAL.

Part: SUPPORT BRACKET — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT FOUND SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AS PER SRM 51-31-01, VOL II AND FABRICATED NEW TEE BRACKET AS PER DRAWING ARC0568. INSTALLED NEW TEE BRACKET AT LT WING OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT AS PER SRM 51-35-01 VOL II.

Part: HINGE — CRACKED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) AT HINGE BRACKET AFT SIDE FOUND TEE CHORD CRACKED. REPAIR CARRIED OUT AS PER EA 1-5750-74329, WINGS - FLAP ASSEMBLIES - TEE CHORD FABRICATION.

Part: HINGE — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) NR 3 FRAME AFT FOUND SUPPORT BRACKET CRACKED. FABRICATED NEW TEE AS PER DRAWING NR ARC 0544. LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) 3 FRAME AFT SUPPORT BRACKET REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: STIFFENER — CRACKED (ZONE 700) · airframe 43,248 hrs · 8,912 cycles

LEFT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER HAVE CRACK LINE.COMPLIED FEDEX EA #1-3210-75908, LANDING GEAR - MAIN GEAR AND DOORS - PART FABRICATION. LT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: STIFFENER — CRACKED (ZONE 700) · airframe 43,248 hrs · 8,912 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER HAVE CRACK LINE. COMPLIED FEDEX EA 1-3210-75908, LANDING GEAR - MAIN GEAR AND DOORS - PART FABRICATION. RT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,248 hrs · 8,912 cycles

COCKPIT - ALUMINUM FLOOR BASE (PLATE) LOCATED BELOW FIRST OFFICER RIGHT CONSOLE CORRODED. ALUMINIUM FLOOR BASE (PLATE) LOCATED BELOW FIRST OFFICER RT CONSOLE CORROSION REMOVED BY HAND CLEAN AND REPROTECTED AS PER SRM 51-21- 01 VOL II. REWORK AREA FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I. AREA PAINT TOUCHED UP AS PER SRM 51-21-01 VOL II.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,248 hrs · 8,912 cycles

COCKPIT - ALUMINUM FLOOR BASE (PLATE) LOCATED BELOW CAPTAIN LEFT CONSOLE CORRODED. COCKPIT - ALUMINIUM FLOOR BASE (PLATE) LOCATED BELOW CAPTAIN LT CONSOLE CORROSION REMOVED BY HAND CLEAN AND REPROTECTED AS PER SRM 51-21-01 VOL II. REWORKED AREA FOUND WITHIN LIMITS AS PER SRM 53-00-01 VOL I. AREA PAINT TOUCHED UP AS PER SRM 51-21-01 VOL II.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LT AND RT INBOARD TRAILING EDGE FLAP - HINGE BRACKET CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORROED.

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA #1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY CORROSION.

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC502. COMPLIED AS PER EA 1-5470-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY CORROSION.

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-74322 - WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DWG ARC 0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 0503, SHT 2. COMPLIED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 0503, SHT 2. COMPLIED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION

Part: HINGE — CORRODED (LT WING) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (RT WING) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY CORROSION.

Part: LONGERON — CORRODED (ZONE 100) · airframe 43,248 hrs · 8,912 cycles

AFT CARGO WASTE TANK COMPARTMENT LT STA 1961, LONGERON 36 HAS CORROSION.

Part: STRUCTURE — CORRODED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

CABIN - BASE SECTION OF CHILLER COMPARTMENT AT GALLEY ASSEMBLY BULGING, CORROSION UNDERNEATH.

Part: HINGE — CRACKED (TAIL CONE) · airframe 43,248 hrs · 8,912 cycles

AFT ACCESSORY COMPARTMENT, LT TAIL CONE LOWER HINGE FITTING SUPPORT FOUND CRACKED. AFT ACCESSORY COMPARTMENT, LT TAILCONE LOWER HINGE FITTING SUPPORT REPAIRED AS PER EA 1-5352-57900, FUSELAGE - TAILCONE/ ACTUATION PLATFORM - PART FABRICATION DEVIATION. CRACKED HINGE FITTING SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 43,248 hrs · 8,912 cycles

AFT CARGO WASTE TANK COMPARTMENT LT STA 1961, LONGERON 37 HAS CORROSION.

Part: TRACK — CORRODED (FUSELAGE) · airframe 43,248 hrs · 8,912 cycles

CABIN - FLOOR TRACK AT STA 473 CTR, X = 0, CORRODED. FLOOR TRACK (CORRODED) AT STA 473 CTR X=0 REMOVED AND REPLACED AS PER SRM 51-33-01, VOL.II.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750- 74319, TITLE: WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, - LEFT AND RIGHT OUTBAORD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, TITLE :WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 43,248 hrs · 8,912 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

CABIN FLOOR TRACK CRACKED AT STA 755, LT X = 27.5. FLOOR TRACK CRACKED AT STA 755, LT X = 27.5 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

FLOOR SUPPORT PLATE ASSEMBLY LOCATED BELOW LAVATORY AT STA 427, RT X = 21 CORRODED WITH A THROUGH HOLE. FLOOR SUPPORT AT STA 427, RT X = 21 REMOVED AND REPLACED IAW SRM 51-33-01 VOL II

Part: SKIN — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LT WING NR 2 SLAT CRACK AT 02 PLACES; 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLAT FROM SLAT TRAILING EDGE 3" FROM OUTBD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE 2 INCHES FROM OUTBD EDGE AS PER SRM 51-31-01, VOL.II.

Part: RIB — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LT WING CRACK ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM 51-33-01, VOL.II AND DRAWING ARB2873. COMPLIED WITH EA 1-5750-74325, WINGS - LT SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK.

Part: RIB — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LT WING, CRACK FOUND ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM 51-33-01, VOL.II AND DRAWING ARB2873. COMPLIED WITH EA 1-5750-74325, WINGS - LT SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK.

Part: SKIN — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LEFT WING - NR 2 SLAT WITH CRACK AT 02 PLACES: 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLAT FROM SLAT TRAILING EDGE 3 INCHES FROM OUTBD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE 2 INCHES FROM OUTBD EDGE AS PER SRM 51-31-01, VOL.II.

Part: FITTING — CRACKED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING - LOWER WINGLET AT FORWARD FITTING FOUND CRACKED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

FLOOR SUPPORT PLATE ASSY LOCATED BELOW LAVATORY AT STA 427 RT X=21 WAS CORRODED WITH A THRU HOLE. FLOOR SUPPORT AT STA 427 RT X = 21 REMOVED AND REPLACED IAW SRM 51-33-01 VOL II

Part: FITTING — CRACKED (ZONE 500) · airframe 43,248 hrs · 8,912 cycles

LEFT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. LT WING - OUTBOARD TRAILING EDGE FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: FITTING — CRACKED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING: LOWER WINGLET AT FWD FITTING FOUND CRACKED.

Part: FITTING — CRACKED (ZONE 600) · airframe 43,248 hrs · 8,912 cycles

RIGHT WING : OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. RT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 43,248 hrs · 8,912 cycles

CABIN FLOOR TRACKS CRACKED AT STA 755, LT X=27.5. FLOOR TRACK CRACKED AT STA 755, LT X = 27.5 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1

Part: CONDUIT — OUT OF POSITION (LT MLG) · airframe 38,371 hrs · 7,756 cycles

ON CLIMBOUT FROM ANC "RED UNSAFE" INDICATION ON PRIMARY INDICATING SYSTEM AND "CONFIGURATION PAGE" AS WELL FOR LEFT MAIN GEAR UNSAFE ON RETRACTION. FOUND FWD ANTI SKID CONDUIT LOOSELY ROUTED THROUGH THE FWD HOSE AND CONDUIT GUIDE ASSY SUSPECT UNDER AIR LOAD ANTI SKID CONDUIT WAS STRIKING THE UPLOCK TARGET BRINGING IT OUT OF SENSOR RANGE, REROUTED ANTI SKID CONDUIT AND BRAKE LINES SO THERE WAS CORRECT ROUTING REF MM 32-11-40-4. CHECKED ALL PROXIMITY SENSORS FOR OPERATION AND RIG REF MM 32-61-15-4. ALSO CHANGED WORN PARTS IN MAIN LANDING GEAR LATCH REF IPC 32-34-05-01 ITEMS 80,85,90,95, AND 100.

Part: CONTROL VALVE — FAULTY (MLG) · airframe 38,371 hrs · 7,756 cycles

LEFT MAIN LANDING GEAR UNSAFE ON DEPARTURE. ATTEMPTED PROCEDURES IAW QRH FOR "GEAR PRIMARY OR SECONDARY LIGHTS ILLUMINATED WITH GEAR HANDLE UP" BOTH LIGHTS REMAINED ON . DUMPED 96K FUEL ON RTB LANDING AND ROLLOUT UNEVENTFUL. R&R MLG CONTROL VALVE PER MM 32-31-20-4 OPS LEAK/CHKS GOOD. ADJUSTED MLG GEARWELL DOOR PUSHRODS PER MM 32-31-00-5. DOORS OPS CHECKS GOOD. PERFORMED LANDING GEAR SWING. ALL INDICATIONS /FUNCTIONS NORMAL. A/C OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 37,629 hrs · 7,565 cycles

LEVEL 2 -AIL DEFECT DISAG- ALERT ILLUMINATED DURING FLAP/SLAT RETRACTION ON T/O. RECYCLED FLAPS IAW QRH. ALERT EXTINGUISHED MOMENTARY THEN REAPPEARED AFTER FLAP/SLAT RETRACTION.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,502 hrs · 7,064 cycles

FLT 5155 WRI, NR 1 ALERT TANK 3 TIP FUEL LOW.

Part: WARNING — ACTIVATED (LE SLAT)

AFT SLAT RETRACTION RECEIVED A LEVEL 2. *S/D* REMOVED AND REPLACED R2-5060 RELAY PER SRM. REMOVED AND REPLACED FLAP HANDLE TRANSMITTER PER MM 27-54-03-4 & 27-54-00-5. PERFORMED FCC 1 & 2 SENSOR READOUT ANALOG VALUE EACH DEG ALL READ SAT AND OPS CHECK NORM.

Part: TEE — CRACKED (CTR WING DRAINS)

FUEL FND LEAKING AT RIGHT UPPER AUX TANK PUMP LEFT AND RIGHT FEED THROUGH LINE DURING FUEL DRAIN SHROUD LEAK TEST. LK CK L/FLOAT SW AND CONDUIT RT UPPER AUS TANK PUMP, NO LEAK; LK CK LT UPPER AUX PUMP CONDUIT, NO LEAK. PANEL AND BOTH LWR AUX PUMP WIRES REMOVED. TEE LEFT AND RIGHT REPLACED, WIRING AND LK CK ON TEE ADAPTER AND WIRING CONDUIT CONN.

Part: FIRE WARNING — ACTIVATED (NR 3 ENGINE)

THIS A/C SHUT DOWN THE NR 3 ENGINE ON DESCENT INTO MEMPHIS FOR A ENGINE FIRE ON BOTH A AND B LOOPS. THE CREW BLEW ONE OF THE FIRE BOTTLES.

Part: DRAIN LINE — BROKEN (NR 3 ENGINE)

HYDRAULIC SYSTEM NR 3 OFF ALERT, HYDRAULIC PRESSURE WENT TO ZERO, SYSTEM QUANTITY WAS AT 3.2 GALLONS AND OTHER WARNINGS WERE PRESENT BECAUSE OF HYDRAULIC LOSS. FABRICATED NEW LINE PER EA 1-2910-31452, INSTALLED AND LEAK CHECKED, OPS CHECKED GOOD. NEW LINE TO BE REPLACED AT NEXT B-CHECK PER EA 1-2910-31452.

Part: PANEL — MISSING (LT WING)

REF N0965, LT WING LWR SURFACE SLAT DRIVE ACCESS PNL MISSING AFTER TEST FLIGHT (P/N ARB1268-23) RIPPED OFF. REMOVED REMAINING PIECES, INSPECTED FOR DAMAGE, INSTALLED NEW ARB1268-23 PANEL AND HINGE ASSY, VERIFY LATCH TOLERANCES AND DOCUMENTED ON NRB 6719 TABULATION SHEET. ALSO, VERIFIED AND DOCUMENTED RT WING.

Part: FITTING — CRACKED (NR 2 FUEL TANK)

DISCREPANCY: CENTER FUEL TANK NR 2 RT COMPARTMENT STA XORS 230, 600, RIB REAR SPAR ATTACH FITTING IS CRACKED APPROXIMATELY 1.5 INCHES AT TOP (REF N0432). REMOVED AND REPLACED ARB3216-502 WITH NEW PART PER N/R 0432.

Part: PL1 WASHER — MISINSTALLED (NR 2 FUEL TANK)

DISCREPANCY: WHILE INCREASING MTOGW (SB 57-20) DISCREPANCY WAS FOUND THAT THE PL1-20-1336 WASHER AND PL1-16-1336 WASHERS ON THE UPPER AND LOWER BOLTS (81139-20-99 AND 81139-16-99) HAD BEEN INCORRECTLY INSTALLED PER MM 20-20-01, FIG 201. (ALSO DPS 1.336). PER FIG 201, WASHER INDEX NR 5 BELONGS BEFORE AND AFTER PL1 WASHER WHERE INSTALLED, IN THIS CASE, WASHERS WERE INSTALLED BOTH AFTER PL1 WASHER JUST BEFORE NUT INSTALLED. CORRECTIVE ACTION: BOLTS REMOVED FOR NDT TESTING AND CHECKED GOOD. WASHERS REPLACED AND VERIFIED FOR CORRECT INSTALLATION.