N303FE

Part: O-RING — DAMAGED (FUEL PUMP) · airframe 98,122 hrs · 32,925 cycles

PDIS 303 28-40 7724 21AUG21 IND OPEN U APPROXIMATELY 30 MIN INTO CRUISE TNK 1 FUEL QTY LO, TNK 1 TIP TRAPPED ALERTS ILLUMINATED. APPROXIMATELY 7700 LBS OF FUEL ACROSS EACH TANK.. TANK 1 STOPPED FEEDING AT 7500. SELECTED MANUAL, THEN AUTO, NO HELP. IN STEEP DESCENT WITH SPOILERS FULLY DEPLOYED. ALERTS EXTINGUISHED AND FUEL CONTINUED ON SCHEDULE. EMERGENCY DECLARED. SHGN 21AUG21 02:23 IND U PERFORMED FUEL QUANTITY TEST, TEST PASSED NO FAULT NOTE REF AMM 28-41-00-5-0. ALSO PERFORMED FSC TEST REF AMM 28-08-01-5 NO FAULT NOTED. MCDU SHOWN NO FAULT HISTORY, NEED MORE TRUBLESHOOTING. RNR O RING ON FUEL PUMP PRESSURE LINE FROM INBD FLOAT VALVE TO OUTBRD TRANSFER VALVE IN #1 MAIN TANK REF MD10AMM 28-00-01-2 OPS CHECK GOOD NO FUEL TRAPPED IN #1 TIP TANK. WORK PERFORMED BY STS TANK TIGERS INC WO#12144R668

Part: CONNECTOR — DAMAGED (APU FIRE WARNING) · airframe 97,401 hrs · 32,595 cycles

DURING COCKPIT SET UP/PREFLIGHT & AFTER APU STARTED RECIEVED FIRE WARNING TONE, LWR CARGO FIRE, FLASHING DISCHARGE LIGHTS, PUSHED DISCHARGE, AFTER 2 MIN, STILL FLASHING, PUSH 2ND BOTTLE, CALLED FIRE& MX. EXITED AIRCRAFT. AFTER REPLACEMENT OF BOTTLES FOUND CONNECTOR PLUGS FOR BOTH 1 & 2 BOTTLES FOR FWD AND AFT DISCHARGE CONNECTOR PLUGS WERE SWAPPED ( FWD BUTTON WAS PRESSED BUT AFT SQUIB WAS DISCHARGED) REF WRI 26-97/7185 FOR CORRECTIVE WIRING ACTION. WORK CONTINUES. PERFORMED CARGO COMPARTMENT FIRE EXTINGUISHING DEPLOYMENT LINES ROUTING AND LEAK CHECK PER AMM CHPT 26-22-05-5,DEPLOYMENT LINES LEAK CK'S SAT. OK FOR SERVICE.

Part: VIA — FAILED (COCKPIT) · airframe 96,578 hrs · 32,152 cycles

ON TAKE OFF ROLL AT APPROX 120 KTS ALL DISPLAYS (DV'S) STARTED FLASHING EXCEPT FOR DV NR 1 (CAPTS ). TAKEOFF WAS CONTINUED & WE HAD NUMEROUS ALERTS THAT FLASHED (CAC DOOR OPEN, A LIST OF YAW ALERTS) DURING OUR RETURN TO THE FIELD. THE FLASHING DISPLAYS CONINUED, & DU NR 6 (FOS) WAS COMPLETELY BLANK. CONSANTLY GOT INTERMITING "PACK 2 OFF" & "ANTI-SKID NO TEST" ALERTS. ON BASE TO FINAL FO SELECTED HIS EIS SOURCE TO AUX & ALL DISPLAYS CAME BACKON NORMALLY & FLASHING STOPPED. REPLACED VIA NR 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

SEAT TRACK AT 1290 LBL100 HAS CORROSION REQ REPAIR. REPLACED CORRODED SEAT TRACK AT STA 1290 LBL 100 REF SRM 53-70-00 FIG 1 VOL 1.

Part: STRUCTURE — DAMAGED (PYLON) · airframe 96,360 hrs · 32,018 cycles

DURING BOAT TAIL INSTALLATION, AFT SLING ATTACHMENT TO SKIN FAIRING CAP IS DAMAGED. REPAIRED DAMAGED AREA REFERENCE SRM 54-00-01 FIG. 11 SHT.1 VOL. 1 AND SRM 54-00-01 FIG. 13 SHT. 1 VOL. 1.

Part: FLOORBOARD — GOUGED (ZONE 200) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO - FLOOR BOARD 233FF - GOUGE. REPAIRED FLOOR BOARD 233 FF. REF. FEDEX DRAWING SRZ-25-005

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO -SEAT TRACK DAMAGED AT STA. 798 LBL 8. PERFORMED REPAIR TO SEAT TRACK REF. SRM 53-70-00 FIG. 1 SHEET 1 .VOL.1 FOR DAMAGED LOCATED AT STA 798 LBL 8 MAIN DECK.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO DECK, STA 1241 102LBL TO 110LBL, CENTER WING UPPER SKIN CORROSION CENTRE WING TOP SKIN AT STRINGER 13, BETWEEN XCW 102 TO XCW110, CORROSION REWORK PERFORMED IAW EA 8-5710-T0353142 PART 1.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 96,360 hrs · 32,018 cycles

SMIS 303 57-30 6346 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353174 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, FWD AND CENTER SKIN PANELS, STR 15, X COMPLY WITH E..A. 8-5730-T0353174 REV NO. POS. P1 INFO 26MAR20 11:54 ** ATTACHED TO WORK ORDER 00076323 ** CTR WING TOP SKIN, STA 1228, ABOVE CTR OF STRINGER 15, XCW -6 TO 20 SKIN EDGE(S) CORROSION REWORK PERFORMED IAW EA# 8-5730-T0353174 PART 1.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 96,360 hrs · 32,018 cycles

SMIS 303 57-30 6345 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353169 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, CENTER SKIN PANEL, STR 14 TO STR 15, COMPLY WITH E..A. 8-5730-T0353169 REV NO. POS. P1 INFO 25MAR20 14:44 ** ATTACHED TO WORK ORDER 00076323 ** CTR WING, TOP SKIN, STA 1232, XCW 19, CORROSIONREWORK PERFORMED IAW EA # 8-5730- T0353169 PART 1.

Part: SKIN — CRACKED (RT CLG DOOR) · airframe 96,360 hrs · 32,018 cycles

RIGHT CENTER LANDING GEAR DOOR AFT DOOR HAS INNER SKIN CRACK APPROX .5" JUST FWD OF THE FWD HINGE. NDT VERIFIED AND MARKED END OF THE CRACK. REMOVED AND REPLACED FRAME SECTION PER DWG ANB7378 AND SRM 51-31-01,V2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO DECK, CENTER WING UPPER SKIN, STA 1229 100RBL HAS CORROSION ALONG EDGE (MARKED) CENTRE WING UPPER SKIN, STRINGER 15, XCW -89 TO XCW -105, CORROSION AT SKIN EDGES REWORKED IAW EA 8-5710-T0353281 PART 2

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO DECK, CENTER WING UPPER SKIN, STA1229 88RBL TO 100RBL HAS CORROSION AROUND MARKED FASTENERS CENTRE WING UPPER SKIN, STRINGER 15, XCW -89 TO XCW -105, CORROSION AT MARKED FASTENER AREAS REWORKED IAW EA 8-5710-T0353281 PART 2.

Part: CAP — CORRODED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO AFT PRESSURE BULKHEAD TEE CAP HAS A CONFIRMED CRACKED ON RADIOUS STA 2007 APPROX BETWEEN X23-X25 REMOVED AND REPLACED DAMAGED SECTION OF TEE CAP REF. REPAIR SRM 53-40-00 VOL 1 FIG. 16, SRM 51-33-01 VOL 2.

Part: FITTING — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

NLG WW RH SIDE BLKHD FITTING PN# ACA3837-2 REQUIRES FABRICATION DUE TO SHEET METAL REPAIR. REF NR# (225). INSTALLED ACA3837-2 FITTING I.A.W DWG. ACA3837. REF. N00225.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

AVIONICS COMPARTMENT AT STA 464 LBL 28. LONGITUDIONAL STIFENNER, AND WEB AATACH ANGLE CORRODED (MARKED) FABRICATED AND INSTALLED -59 INTERCOSTAL PER DWG NBA6074 AND SRM 51-31-01 VOL. 2. WORK ACCOMPLISHED ON N/R 507.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO DECK, STA1227 83LBL TO 94LBL, CENTER UPPER WING SKIN HAS CORROSION (MARKED) CENTRE WING UPPER SKIN CORROSION AT STRINGER 15 BETWEEN XCW 83 TO XCW 94, REWORK PERFORMED IAW EA 8-5710-T0353281 PART 1

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

AFT AVIONIC COMPARTMENT, STA.475, LOOKING IN THRU REFRIGERATOR DOOR, L/H BILGE AREA FLOOR SUPPORT ANGLE SHOWING CORROSION.(MARKED) FABRICATED AND INSTALLED -59 INTERCOSTAL PER DWG NBA6074 AND SRM 51-31-01 VOL. 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO COMPARTMENT UNDER FLOOR AREA, FLOOR SUPPORT BEAM CORRODED AT STATION 2006 RBL 23, VIEWED FROM AFT WASTE TANK COMPARTMENT. MARKED DOT #1. REAMOVED AND REPLACED WITH NEW FLOOR SUPPORT BEAM AGA 7087-506 REF. DWG AGA 7087, SRM 51-31-01 VOL 2.

Part: ATTACH FITTING — CHAFED (LE SLAT) · airframe 96,360 hrs · 32,018 cycles

R/H WING OUTBD SLAT #6 SLAT TRACK INBD ATTACHED FITTING IS WORN DUE TO EXCESSIVE CHAFING OF SLAT TRACK LOWER INBD RAIL. REPAIRED DAMAGED AREA BY BLENDING OUT AREA, ALODINED AND PRIMED AREA REFERENCE E.A. 8-5710-TT0353271 P1 " WINGS RH WING SLAT TRACK #6 SUPPORT OUTBD RIB AT STA. XOS429- GOUGE"

Part: WEB — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

L/H NLG WHEEL WELL WEB HAS 2 EA. CRACKS AT FASTENER HOLES AT STA. 495 AND Z= -73. (MARKED) INSTALLED REPAIR DOUBLERS, FILLERS I.A.W SRM 53-30-00 FIG. 6.

Part: WEB — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

L/H NLG WHEEL WELL WEB HAS 2 EA. CRACKS AT FASTENER HOLES AT STA. 495 AND Z= -73. (MARKED) REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046.

Part: SUPPORT BRACKET — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

NOSE LANDING GEAR L/H RETRACT SUPPORT BRACKET LUG CRACKED. REMOVED AND REPLACED ACA007-1 FITTING REF. DAC DWG NCA6044 AND EO 8-5340-7-5000 D PT2.

Part: SEAT TRACK — DAMAGED (BS 1661 LBL106) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO - SEAT TRACK DAMAGED AT STA.1661 LBL 106. REPAIRED SEAT TRACK DAMAGE REF: SRM 53-70-00 FIG.1 SHT.1 PG.3

Part: BULKHEAD — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

NOSE LANDING GEAR WHEELWELL; X= -24 Y= 486 Z= -48 2" CRACK ON BULKHEAD. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046. INSTALLED REPAIR DOUBLERS I.A.W SRM 53-30-00 FIG. 6. REF. N00225.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

MAIN CARGO - SEAT TRACK DAMAGED AT STA.1661 LBL 106. REPAIRED SEAT TRACK DAMAGE REF: SRM 53-70-00 FIG.1 SHT.1 PG.3

Part: BULKHEAD — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

NOSE LANDING GEAR WHEELWELL; X= -24 Y= 494 Z= -58 HAS 2EA. 1" CRACKS @ ADJACENT FASTENERS ON BULKHEAD. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046. INSTALLED REPAIR DOUBLERS I.A.W SRM 53-30-00 FIG. 6. REF NON-ROUTINE N00225.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 96,360 hrs · 32,018 cycles

NLG WHEEL WELL RH BULKHEAD -Y= 24, APPROX STA. 470 AND 476, -X= 41. TWO 6" INCH CRACKS. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1. AND DAC DWG NCA6046. INSTALLED REPAIR DOUBLER I.A.W SRM 53-30-00 FIG. 6.

Part: WEB — CORRODED (LT MLG WW) · airframe 96,360 hrs · 32,018 cycles

LH WHEEL WELL - WEB (P/N AEA0026-5) BETWEEN STA 1501 - 1521 IS CORRODED. (AREA MARKED) REMOVED AND REPLACED WITH FABRICATED PART FX AEA0026-5 PER DWG AEA0026 AND SRM 51-30-00 V.2

Part: STIFFENER — CRACKED (TAILCONE) · airframe 96,360 hrs · 32,018 cycles

AFT BULKHEAD TAIL CONE AT UPPER R/H SUPPORT STIFFNER (3RD FROM THE TOP, MARKED IN RED) O/B IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR HAT CHANNEL PER E.A. 8-5310- T0353336 AND SRM 51-31-01 VOL. 1.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 96,360 hrs · 32,018 cycles

FWD CARGO CUT-OUT - LOWER AFT CORNER - DOUBLER/TRIPLER GOUGED. REMOVED DAMAGED DOUBLERS AND REPLACED WITH NEW DOUBLERS,REF SRM 53-50- 00,FIG26.

Part: VALVE — MALFUNCTIONED (FUEL TRANSFER) · airframe 96,181 hrs · 31,911 cycles

PDIS 303 28-43 6202 25JAN20 LIT OPEN U LOGPAGES:3213631 "TNK 1 TIP TRAPPED" AT FL350 FOR 3 MINUTS. ALERT CLEARED ITSELF, THEN RETURNED CAUSING DIVERT INTO KLIT MEL 25JAN20 16:55 LIT U RELEASED FOR SERVICE PER MEL : 28-43-04-A CATEGORY : C EXPIRATION : 04FEB20 "MEL 28-43-04-A: NO. (IDENTIFY) _1_ TIP TANK FLOAT SWITCH(ES) - INOP. NO. (IDENTIFY) _1__ TIP TANK GRAVITY XFER SYS - INOP CLOSED. ADD MEL PENALTY FUEL." TNK 1 TIP TRAPPED: "MEL 28-43-04-A #1 TIP TANK FLOAT SWITCH-INOP. NO. 1 TIP TANK GRAVITY XFER SYS INOP CLOSED. ADD MEL PENALTY FUEL." CAT C EXP 04 FEB20. FACT 03FEB20 19:51 MEM ALL WORK COMPLETED BY FFC. WO# 3200060. ALL OPS CK AND LK CK C/W. A/C OK FOR SERVICE.

Part: SWITCH — DEFECTIVE (R1 DOOR) · airframe 95,825 hrs · 31,737 cycles

IN CLT DURING TAXI "DOOR DISARMED" LIGHT ON PANEL TO THE RIGHT SIDE OF THE R1 DOOR ILLUMINATED. ALL DOORS SHOWED CLOSED IN COCKPIT, AND DOOR LEVER WAS IN THE "SLIDE AREMED" POSITION PDM-CONTROL NUMBER 7205681 - VERIFIED MEL 52-10-03: MAIN ENTRY DOOR OR SLIDE RAFT - CABIN DOORS 1L OR 1R - EXP 9NOV19 CAT C MEL 30OCT19 00:00 CLT U RELEASED FOR SERVICE PER MEL : 52-10-03 CATEGORY : C EXPIRATION : 09NOV19 "MEL 52-10-03: R1 MAIN ENTRY DOOR - INOP - EXTENDED OVERWATER OPS REQUIRES TWO SLIDES AND/OR RAFTS." INFO NOTED BY MEM MX C/7205681 PART 30OCT19 06:12 MC1 U IDENTIFIED PARTS FLAP LIMIT MPN: H20-28B CPN: 0029452 QTY: 1 FOUND R1 DOOR CONTROL POWER INTERLOCK SWITCH S1-1091 STICKING, REMOVED AND REPLACED SAME. OPS CHECKS GOOD. REF IPC 52-11-70 AND AMM 52-11-00. SWITCH P/N H20-24B, S/N BAN7024-1 MANUFACTURER- EATON.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 95,820 hrs · 31,733 cycles

AIRCRAFT FUSELAGE STRUCK BY CONTAINER DURING STORM, LEAVING HOLE IN SKIN JUST FORWARD AND BELOW BULK CARGO DOOR. INSTALLED REPAIR REF MD-10 SRM 53-20-00 FIG 6 AND E.A. 8-5330-T0350329 P1 FUSELAGE - PLATES & SKINS - CONTAINER STRIKE LWR AFT L/H FUSELAGE - REPAIR. OK TO EDGE SEAL AND PAINT, EDGE SEALED AND PAINTED REPAIR REF MD-10 SRM 51-41-01 AND SRM 51-21-01.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 95,528 hrs · 31,575 cycles

PDIS 303 21-10 5616 25JUL19 MCI OPEN U LOGPAGES:3142593 TURNED ON #2 PACK IN CRUISE. GOT SMOKE IN COCKPIT ONLY, TURNED #2 PACK OFF SMOKE DISSIPATED. MEL 26JUL19 00:32 MCI U RELEASED FOR SERVICE PER MEL : 21-51-01-A CATEGORY : C EXPIRATION : 04AUG19 "MEL 21-51-01-A: NR 2 PACK - INOP." RAN #2 ENG PER JRH AND PERFORMED #2 PACK OPS CK PER AMM REF 21-54-03 WITH #2 ENG AIR AND APU AIR. RAN ALL THREE PACKS AND COULD NOT DUPLICATE SMOKE OR ODOR. PLACED #2 PACK ON MEL. INFO 26JUL19 01:30 MEM ***MOCC UPDATE**** PLEASE WORK IN CONJUNCTION WITH TSI: 21-54/5617.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 95,515 hrs · 31,569 cycles

MDIS 303 33-50 5599 21JUL19 JFK OPEN U ON PRE-FLIGHT CHKS "EMER LT BAT 1 LO" DISPLAYED DURING EMERGENCY LIGHT TEST. MEL 21JUL19 10:27 JFK U RELEASED FOR SERVICE PER MEL : 33-50-02 CATEGORY : C EXPIRATION : 31JUL19 "MEL 33-50-02: EMER LIGHTS - INOP." PART 21JUL19 10:51 MC1 U IDENTIFIED PARTS EMERG EXIT LIGHTS MPN: 60-4411-5 CPN: 3300197 QTY: 1 FACT 22JUL19 05:00 PDX REPLACED EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECK GOOD. SDR PARTS INFO: MANUFACTURER P/N 60-4411-5, S/N OFF 0016, S/N ON 0402.

Part: HINGE — CRACKED (RT MLG DOOR) · airframe 95,041 hrs · 31,292 cycles

RIGHT MAIN GEAR DOOR CENTER HINGE CRACKED. REMOVED AND RE3PLACED DOOR HINGE AND INTERNAL TEE FITTINGS AND INSTALLED GEAR DOOR PAN REPAIR UISNG REF MD10 SRM 52-10-00 FIG 5 AND REINSTALLED ACCESS PANEL UISNG REF SRM MD10 51-35-02.

Part: WIRE — DAMAGED (CABIN) · airframe 94,064 hrs · 30,775 cycles

EMER LIGHTS BAT 1 LO ALERT. FOUND DAMAGED WIRE AT P1-1756A PIN 1 GND CAUSING ONLY 64 VAC TO PIN 6 CHARGING POWER. REPAIRED WIRE GND AT PIN 1 CKS GOOD AS WELL AS 115 VAC AT PIN 6 C/W EMER LIGHT TEST. OPS TESTS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 93,965 hrs · 30,713 cycles

EMERGENCY LIGHT BATTERY 1 LOW ALERT. REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 93,892 hrs · 30,673 cycles

LEFT INBD UPPER SURFACE CRACKED ON OTBD TRIM AT XIFH 310. REMOVED AND REPLACED THE SKIN IAW DWG ARC 2443, ZONE 8.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 93,892 hrs · 30,673 cycles

LEFT INBD FLAP UPPER SKIN CRACKED ON OUTBD TRIM AT XIFH 310. REMOVED & INSTALLED A FABRICATED OUTBD TRIM SKIN IAW SRM 57-52-01, FIG 1, PAGE 1 VOL I, DRAWINGS ARC3098 AND ARC2258.

Part: SEAT TRACK — CORRODED (BS 1738) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK, BS 1738, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICE IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL 2, AND SRM 51-41-01, VOL 2.

Part: SEAT TRACK — CORRODED (BS 1751-1711) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK BS 1753, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICES IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL II, SRM 51-41-01, VOL II, AND EA 8-5310-TO339630.

Part: SEAT TRACK — CORRODED (BS 1759) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK, BS 1759, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICE IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL 2, AND SRM 51-41-01, VOL 2.

Part: SEAT TRACK — CORRODED (BS 1681) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK, BS 1681, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICES IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL 2, AND SRM 51-41-01, VOL 2.

Part: STOP FITTING — CRACKED (ACM DOOR FRAME) · airframe 93,892 hrs · 30,673 cycles

NR 3 ACM DOOR FRAME STOP FITTING HAS A .250 INCH CRACK. REPAIRED STOP FITTING IAW SRM 53-00-01, FIG 2, SHEET 2, VOL 1, AND EA.

Part: SHEAR TIE — CORRODED (BS 1964) · airframe 93,892 hrs · 30,673 cycles

AFT CARGO BAY, BS 1967, LONGERON 48L SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA7058.

Part: HINGE — CRACKED (ZONE 100) · airframe 93,892 hrs · 30,673 cycles

NR 3 PACK DOOR AFT HINGE CRACKED. REPAIRED IAW SRM 53-00-01, FIG 2, PAGE 15, VOL 1, AND EA.

Part: FLOOR SUPPORT — CORRODED (BS 1741-1761) · airframe 93,892 hrs · 30,673 cycles

MAIN CABIN BS 1761 - 1741 BETWEEN RBL 74 TO 106 . CORROSION FOUND ON THE FLOOR SUPPORT LOWER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG AFA7435

Part: SEAT TRACK — CORRODED (BS 1761-1741) · airframe 93,892 hrs · 30,673 cycles

MAIN CABIN BS 1761 - 1741 BETWEEN RBL 47 - 74, CORROSION FOUND ON THE SEAT TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00, VOL 1, FIG 1, PAGE 3.

Part: LONGERON — CORRODED (BS 1967) · airframe 93,892 hrs · 30,673 cycles

AFT CARGO BAY BS 1967, LONGERON 48L CORRODED. REPLACED THE SECTION OF THE LONGERON BS 1959 - 1994 IAW EA 8-5310-T0339590.

Part: FLOOR SUPPORT — CORRODED (BS 1967) · airframe 93,892 hrs · 30,673 cycles

AFT CARGO, BS 1967, RBL 48 FLOOR SUPPORT HAS CORROSION ON LOWER FWD CORNER. FABRICATED A NEW FLOOR SUPPORT AND INSTALLED IAW DWG AGA3225

Part: FLOOR SUPPORT — CORRODED (BS 1741-1761) · airframe 93,892 hrs · 30,673 cycles

MAIN CABIN BS 1761 - 1741 BETWEEN RBL 74 TO 106, CORROSION AT FLOOR SUPPORT AND TRACK. LOWER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG # AFA7435

Part: SHEAR TIE — CORRODED (BS 1964) · airframe 93,892 hrs · 30,673 cycles

AFT CARGO BAY, BS 1967, LONGERON 48R SHEAR TIE TO WEB HAS EXFOLIATION CORROSION, AFT SIDE OF FRAME. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA7058

Part: BRACKET — CRACKED (LT WING) · airframe 93,892 hrs · 30,673 cycles

LT WING LE ACCESS THROUGH PANEL 561BB (FIRE BOTTLE AREA) - FWD OUTBD CORNER OF BOX STRUCTURE JOIN BRACKET CRACKED LOWER CORNER. INSTALLED NEW ANGLE CLIP PART ARB0116-21 IAW DWG ARB0116 SRM 51-33-01 VOL II.

Part: SHEAR TIE — CORRODED (BS 1964) · airframe 93,892 hrs · 30,673 cycles

AFT CARGO BAY, BS 1967, LONGERON 48R SHEAR TIE TO WEB HAS EXFOLIATION CORROSION, AFT SIDE OF FRAME. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA7058.

Part: SKIN — CRACKED (BS 620) · airframe 93,892 hrs · 30,673 cycles

MAIN CARGO DOOR OPENING FWD LOWER CORNER SKIN DAMAGED. REPAIRED IAW SRM 53-50-00, FIG 26.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 93,892 hrs · 30,673 cycles

LH INBD FLAP UPPER SURFACE-TWO CRACKS EMANATING FROM FASTENERS AT APPROX XIFH 177. CONFIRMED WITH NDT HFEC. REPAIRED PER MD10 SRM 57-00-01, FIG. 4, SHEET 2, VOL 1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 93,892 hrs · 30,673 cycles

LEFT INBD FLAP UPPER SURFACE CRACKED, EMANATING FROM FASTENER AT XIFH 171. CONFIRMED WITH NDT HFEC. REPAIRED IAW SRM 57-00-01, FIG 4, PG 12, VOL I.

Part: SUPPORT — CRACKED (BS 1381) · airframe 93,892 hrs · 30,673 cycles

SUPPORT CRACKED. REMOVED AND REPLACED THE DAMAGED SUPPORT.

Part: SUPPORT — CORRODED (BS 2007) · airframe 93,892 hrs · 30,673 cycles

AFT FUSELAGE TANK COMPARTMENT, BS 2007, LT LOWER BULKHEAD TRANSVERSE SUPPORT HAS CORROSION. REMOVED AND REPLACED THE TRANSVERSE SUPPORT IAW DWG NJC6040, SRM 51-35-01,V2, AND SRM 51-33-01,V2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK SEAT TRACK DAMAGED AT STATION 2007,LBL 27. REPAIRED SEAT TRACK REF SRM 53-70-00 FIG 18 SHEET1,2,3 VOL 1 AND REF SRM 51-31-01 VOL 2.

Part: ANGLE — CRACKED (RT NR 3 LE SLAT) · airframe 93,892 hrs · 30,673 cycles

RIGHT NR 3 SLAT INTERNAL ANGLE IS CRACKED BEYOND LIMITS. REMOVED AND REPLACED THE ANGLE IAW DWG ARB1679, AND SRM 51-31-01, VOL 2.

Part: SKIN — CRACKED (LE SLAT) · airframe 93,892 hrs · 30,673 cycles

RT WING NR 1 SLAT AFT/LWR SURFACE HAS 2 EA CRACKS NEAR I/B L/E. REPAIRED NR 1 SLAT AFT/LOWER SURFACE CRACKS NEAR I/B L/E REF SRM57-10-00 VOL I P 64 FIG 18A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO COMP FLOOR SUPPORT BRACKET HAS EXFOLIATION ON TOP SURFACE LOCATED AT STA 1701 RBL 36-48. REMOVED, FABRICATED AND INSTALLED SUPPORT PER B/P AFA3865.

Part: SEAT TRACK — DAMAGED (BS 2007) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK SEAT TRACK DAMAGED AT BS 2007, LBL 27. REPAIRED THE SEAT TRACK IAW SRM 53-70-00 FIG. 18, SHEETS 1, 2, 3 VOL. 1. AND SRM 51-31-01 VOL. 2.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 93,892 hrs · 30,673 cycles

RIGHT OTBD FLAP VANE HAS DELAMINATION BELOW THE NR 5 RUBSTRIP. REPAIRED THE FLAP VANE IAW SRM 51-71-00, VOL II.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 93,892 hrs · 30,673 cycles

RIGHT INBD FLAP VANE LOWER SURFACE REPAIR DOUBLER IS MISSING, XIFH 199. REPAIRED THE FLAP VANE IAW SRM 57-53-01, FIGURE 1, VOL 3, AND INSTALLED A NEW DOUBLER AND BONDED IAW SRM 51-71-00, VOL II, PG 64.

Part: BRACKET — CRACKED (BS 1709) · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO, BS 1709, NEAR FWD LOWER CORNER OF DOOR, END OF FRAME, HAD A CRACKED BRACKET. REMOVED & REPLACED THE BRACKET IAW DWG AFA3170, & SRM 51-31-01, VOL II.

Part: DOOR FRAME — CORRODED (BS 1701) · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO DOOR BS 1701 FWD FRAME CORRODED. REPAIR IAW EA 8-5310-T0338873.

Part: CHANNEL — CORRODED (BS 1521-1610) · airframe 93,892 hrs · 30,673 cycles

CTR CARGO BAY ZEE CHANNEL HAS CORROSION UNDER NUTPLATES, THE FULL SPAN LENGTH FROM BS 1521 - 1696, RBL 64. FABRICATED A NEW CHANNEL IAW DRAWING ADJ7004

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT STA 522 LBL 48. REPAIRED DAMAGED SEAT TRACK IAW SRM 53-70-00 FIG 2 VOL1.

Part: SEAT TRACK — DAMAGED (BS 475) · airframe 93,892 hrs · 30,673 cycles

MAIN CABIN: BS 475, LBL 107.25, OTBD SEAT TRACK. ONE INCH LONG GOUGE. REPAIRED THE SEAT TRACK IAW SRM 53-70-00 FIG. 1 VOL. 1.

Part: FRAME — CORRODED (BS 1781) · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO BAY FRAME FLANGE HAS CORROSION AT BS 1781, BETWEEN LONGERONS 50L AND 50R. INSTALLED A CHANNEL SPLICE AND FILLER IAW SRM 53-30-00, VOL 1, PAGE 15, FIG 5. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1781) · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO BAY FRAME FLANGE HAS CORROSION AT BS 1781, BETWEEN LONGERONS 50L AND 50R. REMOVED THE SECTION OF THE FRAME FLANGE, FABRICATED A REPAIR AND INSTALLED IAW SRM 53-30-00, FIG 5, VOL 1, & DWG AFA3907.

Part: FRAME — CORRODED (BS 1967) · corrosion level 2 · airframe 93,892 hrs · 30,673 cycles

AFT CARGO BAY, BS 1967, ADJACENT TO AFT BULKHEAD. BETWEEN STRINGERS 49L & 49 R. MILD SURFACE CORROSION AND METAL DISCOLORATION FORMING ON THE J-CAP. REMOVED THE CORROSION IAW SRM 51-21-01, V2. AND INSTALLED A REPAIR IAW SRM 51-30-00, V1, PG 31, AND SRM 51-30-00, V2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK, SEAT TRACK NEAR STATION 735, RBL 27.50 CORROSION BEYOND LIMITS. REPLACED DAMAGED SEAT TRACK FROM STATION 725 TO STATION 765, RBL-27.50 PER SRM 53-70-00 FIG 1 VOL. 1, SRM 51-31-01 VOL 2 AND SR10-53-002.

Part: TEE FITTING — CORRODED (BS 1521) · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO BAY FWD BULKHEAD, BS 1521, BETWEEN LONGERONS 51L AND 52L TEE FITTING SHOWS CORROSSION. BLENDED OUT CORROSION IAW SRM 51-21-01, VOL 2.

Part: FRAME — CHAFED (BS 588) · airframe 93,892 hrs · 30,673 cycles

A/C BAY NR 1 PACK. BS 588. JUST BELOW AND AFT OF PACK BAY DOOR. THE PACK SHUT OFF VALVE CABLE FOUND WORN ON TOP OF FRAME. REMOVED THE DAMAGED SECTION OF THE FRAME AND REPAIRED IAW SRM 53-00-01, FIG 8, VOL 1, AND DWG ACA0050.

Part: FRAME — CORRODED (BS 959) · airframe 93,892 hrs · 30,673 cycles

LOWER FUSELAGE , FWD CARGO BAY, AT BS 959, LONGERON 52, CORRODED ON THE FRAME LOWER J CHANNEL. REMOVED AND REPAIRED IAW SRM 53-30-00, FIG 5.

Part: DOOR SILL — CORRODED (BS 1721) · corrosion level 2 · airframe 93,892 hrs · 30,673 cycles

LOWER CENTER CARGO BAY, BS 1721 AT DOOR SILL CORNER HAD EXFOLIATION. REPAIRED IAW DWG AFA0416, AND EA 8-5310-T0338873, P2.

Part: FRAME ANGLE — CORRODED (BS 1521) · corrosion level 2 · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO BAY, BS 1521, FWD BULKHEAD. LONGITUDINAL STRUCTRUAL BEAM, LONGERON 44L CORRODED. REMOVED AND REPLACED THE FRAME ANGLE IAW EA 8-5310-25134, REV A, PART 2.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 93,892 hrs · 30,673 cycles

CENTER CARGO COMPT STA 1521 FWD BULKHEAD BWTN STRINGERS 47 & 48 LT. MINOR SURFACE CORROSION FORMING ADJACENT THREE EACH 1/4 FASTENERS. REMOVED MINOR SURFACE CORROSION AT CENTER CARGO COMPARTMENT STA 1521 FWD BULKHEAD BETWEEN STRINGERS 47 & 48L IN REF TO SRM 51-21-01 VOL II.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK SEAT TRACK WORN RBL X= 47.50 NEAR STA 898. REPLACED DAMAGED SEAT TRACK FROM STATION 858 TO STATION 898, RBL-47.50 REF SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — WORN (BS 1125) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK SEAT TRACK WORN LBL 8.5 NEAR BS 1125. REPLACED THE SEAT TRACK BETWEEN BS 1125 TO 1145 IAW SRM 53-70-00, FIG 1, VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 93,892 hrs · 30,673 cycles

MAIN DECK, SEAT TRACK WORN RBL X= 27.50 NEAR STA 1119. REPLACED DAMAGED SEAT TRACK FROM STATION 1125 TO STATION 1145, RBL-27.50 REF SRM 53-70-00 FIG1 VOL 1.

Part: SKIN — DAMAGED (BS 1721) · airframe 93,892 hrs · 30,673 cycles

CTR CARGO BAY DOOR OPENING, FWD LOWER EDGE SKIN DAMAGE. REPAIRED IAW EA 8-5310-T0338873, P 3.

Part: RIB — CRACKED (RT WING) · airframe 93,892 hrs · 30,673 cycles

RIGHT WING NR 3 SLAT INBD FACING EDGE CRACKED. REMOVED AND REPLACED THE RIB IAW DWG NRB6027.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,673 hrs · 30,564 cycles

EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED DURING PREFLIGHT TEST. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4. OPS TESTED GOOD IAW AMM 33-51-01-5.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 93,485 hrs · 30,479 cycles

EMER LT BAT 1 LO DURING PREFLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTING BATTERY POWER SUPPLY IAW AMM 33_51_01_4. OPS CHECK GOOD. A/C OK FOR SERVICE. POWER SUPPLY PN 60-4411-5 SN 0299.

Part: INDICATOR — DEFECTIVE (ZONE 200) · airframe 93,232 hrs · 30,347 cycles

DURING PREFLIGHT INSPECTION DISCOVERED R1 DOOR ESCAPE SLIDE PUSH TEST LIGHT WOULD NOT ILLUMINATE. RELAMPED LIGHT ASSY WITH CORRECT 368 BULBS. LIGHT CHECKS NORMAL

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 93,063 hrs · 30,248 cycles

RIGHT MAIN ENTRY DOOR EMERGENCY SLIDE TEST LIGHT WOULD NOT TEST. REMOVED AND REPLACED THE BATTERIES. REMOVED AND REPLACED THE BULBS. PRESS TO TEST, OPS CHECKED NORMAL IAW MM 25-61-03-5.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 92,695 hrs · 30,053 cycles

EMER LT BATT 1 LOW DURING EMER LIGHT TEST, TEST FAILED. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY PER AMM 33-51-01-4. OPS CHECKED GOOD. A/C OK FOR SERVICE.

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 92,225 hrs · 29,848 cycles

FLAP DISAGREE LEVEL 3 ALERT OCCURED DURING APPROACH. RAN QRH TO END UP WITH 15 DEGREE EXT CONFIGURATION. DECLARED EMERGENCY AND LANDED. REPLACED RT NBOARD FLAP POISITION TRANSMITTER IAW AMM 27-54-04-4.

Part: TRANSDUCER — INOPERATIVE (NR 2 BRAKE) · airframe 91,809 hrs · 29,656 cycles

DURING APPROACH, PUT GEAR DOWN AND RECEIVED A LEVEL 2 ANTI-SKID LT FAILED ALERT. COMPLIED WITH QRH CHECKLIST PROCEDURE. ANTI-SKID SYSTEM WHEEL SPEED TRANSDUCERS (OUTPUT TO ANTI-SKID CONTROL UNIT) NR 2 BRAKE INOPERATIVE.

Part: INDICATOR — INOPERATIVE (R1 DOOR) · airframe 91,111 hrs · 29,341 cycles

R1 PRESS TO TEST PRESS INDICATOR LAMP OUT. RELEASED FOR SERVICE IAW MEL 25-61-01, CATEGORY C, EXPIRATION 08JUN16. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01, VERIFY & RECORD IN THE AML. EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

RIGHT STATION 1156 BULKHEAD T CAP VERTICAL LEG HAS A CRACKED INDICATION AT THE 2ND FASTENER HOLE FROM THE TOP ON THE OTBD SIDE OF THE BULKHEAD STIFFENER AT X= -72.5 & LONGERON 40R, 2016-04-19. SDR 16-1192 CORRECTIVE ACTION WRITTEN IN ERROR, IT SHOULD BE REPAIRED IAW EA 8-5310-T0324803, NOT EA 8-5310-T0324511.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

LEFT STATION 1156, PRESS BULKHEAD T CAP AT LONGERON 37L, HAS A CRACK INDICATION AT THE NR 1 AFT HOLE ON THE HORIZONTAL LEG UNDER THE SPLICE PLATE. REPAIR IAW SRM 53-40-00 FIG 24 VOL 2.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 90,918 hrs · 29,271 cycles

CENTER WW RT BULKHEAD CRACKED. R & R FACTORY DOUBLER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

CENTER WW LT FWD BULKHEAD CRACKED. R & R FACTORY DOUBLER.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

SEAT TRACK AT POSITION 8R, DAMAGED SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 90,918 hrs · 29,271 cycles

LEFT VERTICAL TO EXT FUSE DRAG ANGLE HAS 2.5 IN CRACK. MARKED BELOW NR 2 BANJO FITTING. REPAIRED CRACKED ANGLE LT VERTICAL BELOW NR 2 BANJO FITTING IAW SRM 55-20-00 V I FIGURE 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

JPF STEP 6, SKIN AT LONGERON 39R HAS A 3 INCH CRACK ABOVE SKIN SPLICE. REPAIRED IAW EA 8-5310-T0324511.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

FT WASTE COMPARTMENT. LT FLOOR SUPPORT UNDERSIDE, LBL 75 - 107, BETWEEN STATION 1964 - 1975, DELAMINATED & CORRODED. R & R LT FLOOR SUPPORT IAW DWG AGA3810 & SRM 51-31-01 VOL 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

STATION 1841, CORROSION ON FLOORBEAM. CLEANED CORROSION & REPAIRED FLOORBEAM.

Part: SKIN — GOUGED (LT WING) · airframe 90,918 hrs · 29,271 cycles

LEFT LOWER CTR WING SKIN, UPPER SURFACE HAS NUMEROUS GOUGES FROM FASTENER. REMOVAL OF THE SPLICE ANGLE, BETWEEN XCW=95 & XCW=99, BETWEEN THE FRONT SPAR & STRINGER 49. REPAIRED IAW EA 8-5710-T0324689.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

FLOORBOARD SUPPORT AT STATION 1561, BETWEEN 48L & 72L HAS CORROSION. FABRICATED NEW SUPPORT IAW DWG AEA7326 & SRM 51-35-01 VOL 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

MAIN CABIN, STATION 1821, LBL 57, FLOOR SUPPORT CORRODED. FABRICATED FLOOR SUPPORT IAW BP AGA 7510. INSTALLED IAW SRM 51-31-01 VOL 2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

RIGHT STATION 1156, BULKHEAD T CAP HORIZONTAL LEG HAS A CRACK INDICATION, BETWEEN TWO FASTENER HOLES, JUST ABOVE LONGERON 39R, BELOW THE SPLICE PLATE. REPAIRED IAW SRM 53-40-00 FIG.24 VOL 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

LEFT STATION 1156, FUSELAGE SKIN LAYER HAS ONE EACH FASTENER HOLE WITH A CRACK INDICATION AT LONGERON 39L. REPAIRED IAW EA 8-5310-T0324512.

Part: SKIN — CRACKED (LT WING) · airframe 90,918 hrs · 29,271 cycles

LEFT LOWER WING SKIN OTBD AFT CORNER OF SLAT TRACK 10 HAS .200 IN CRACK. TRIMMED OUT CRACK & INSTALLED FILLER & DOUBLER.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

UPPER MAIN CABIN COMPARTMENT SEAT TRACK DAMAGED AT STATION 910, LBL 48. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

RIGHT STATION 1156 BULKHEAD T CAP, VERTICAL LEG HAS A CRACK INDICATION, AT THE 2ND FASTENER HOLE FROM THE TOP, ON THE OTBD SIDE OF THE BULKHEAD STIFFENER, AT X= -72.5 & LONGERON 40R. REPAIRED IAW EA 8-5310--T0324511.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

MAIN DECK, SEAT TRACK IS SHOWN DAMAGED FROM STATION 830 - 840, LBL 8. INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

MAIN DECK STATION 162, LBL 48 SEAT TRACK WORN. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

MAIN DECK, STATION 1621, LBL 48 SEAT TRACK DAMAGED. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

WHEEL WELL, RT SIDE PRESS BULKHEAD, JUST AFT OF STATION 1368, STRINGER IS CRACKED. ACCESS THROUGH OPENING, JUST BELOW KEEL BEAM OF RT MLG. INSTALLED SPLICE ANGLE AS REQUIRED IAW SRM 51-33-01 VOL II. REMOVED CTR WW DOOR FWD HINGE FITTINGS FOR ACCESS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

LEFT STATION 1156, PRESS BULKHEAD T CAP AT LONGERON 37L, HAS A CRACK INDICATION AT THE NR 1 AFT HOLE ON THE HORIZONTAL LEG, UNDER THE SPLICE PLATE. REPAIRED IAW EA 8-5310-T0324309.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 90,918 hrs · 29,271 cycles

RIGHT VERTICAL TO FUSE EXT DRAG ANGLE HAS 1 INCH CRACK. MARKED AREA BELOW NR 2 BANJO FITTING. REPAIRED IAW SRM 55-20-00 FIG 3 SHEET 1-3.

Part: PANEL — GOUGED (RUDDER) · airframe 90,918 hrs · 29,271 cycles

UPPER AFT RUDDER LT SIDE, FWD WRAP AROUND PANEL 378GL & RUDDER FITTING GOUGED, APPROX 1/4" DEEP. INSPECTED UPPER AFT RUDDER & ATTACH HARDWARE ON FWD RUDDER AFT SPAR & FOUND NO OTHER STRUCTURAL DAMAGE IAW MM 27-20-00-6. UPPER AFT RUDDER PANEL 378GL REPAIRED & FITTING REPLACED & INSPECTED. TRIMMED SMOOTH EDGE OF PANEL 375 DL IAW SRM 55-00-01 FIG 1A SHT 2. INSTALLED NEW AFT RUDDER BRACKET IAW AMM 20-20-01-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

AFT CARGO COMPARTMENT, STATION 1921 - 1942, LBL 75 - 107, CEILING ABOVE DOOR ENTRANCE, FLOOR SUPPORT CORRODED. REPAIRED IAW SRM 53-70-00 FIG 18 & EA 8-5321-T0324514.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 90,918 hrs · 29,271 cycles

UPPER MAIN CARGO COMPARTMENT, SEAT TRACK DAMAGED AT 655 LBL 48. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: CABLE — BROKEN (L1 DOOR) · airframe 900 hrs · 28,889 cycles

ON POST FLIGHT FOUND L1 DOOR LOWER DRIVE CABLE BROKEN. REMOVED CABLE, CYCLED DOOR SEVERAL TIMES & DOOR WORKS PROPERLY ELECTRICALLY. MAIN ENTRY DOOR INOPERATIVE. EXTENDED OVERWATER OPERATIONS REQUIRES TWO SLIDES & OR RAFTS. TROUBLESHOOTING IS REQUIRED PRIOR TO INSTALLING PARTS. INSTALLED L1 DOOR LOWER AFT DRIVE CABLE IAW AMM 52-10-02-2, OPERATIONS CHECKED GOOD. THE CORRECT PN`S ARE AS FOLLOWS, NAS4903DU18 & AN320D3.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 898 hrs · 28,808 cycles

DURING EMER LIGHT TEST REVEALED LEVEL 1 ALERT EMER POWER BATT 1 LOW. R & R EMER EXIT LIGHTS POWER SUPPLY IAW AMM 33-51-01-4-1. OPERATIONS CHECK IAW 33-51-01-5 NORMAL.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 898 hrs · 28,765 cycles

RAMP REPORTED LOOSE LOCK RESTRAINT ID H1388 BETWEEN 7L & 8L. PERFORMED SEAT TRACK REPAIR ON DAMAGED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1. CAT A MAJOR REPAIR.

Part: EXTINGUISHER — UNWANTED DEPLOY (CARGO BAY) · airframe 896 hrs · 28,693 cycles

ON ACFT POWER UP THE FWD LOWER CARGO NR 1 FIRE COMPARTMENT EXTINGUISHER NR 1 CYLINDER DISCHARGED. REMOVED FWD CARGO FIRE EXT CONTAINER NR 1 IAW MM 26-22-01-4-1.

Part: ACCESS DOOR — MISSING (CARGO DOOR) · airframe 892 hrs · 28,540 cycles

ON WALK AROUND CTR CARGO DOOR VENT ACCESS DOOR MISSING. REPLACED CTR CARGO DOOR FAIRING FILLET DOOR. DOOR OPERATIONS CHECKED SATISFACTORY.

Part: MANIFOLD — RUPTURED (NR 3 ENGINE) · airframe 892 hrs · 28,540 cycles

AT APPROX 1000 FEET ON STABLE FLAPS 35 DEGREES APPROACH, THE NR 3 ENG FLAMED OUT. IAW CREW, N2 INDICATION ROLLED BACK & AFTER TOUCHED DOWN, NR 3 ENGINE WAS SHUTDOWN. LT FUEL MANIFOLD FOUND RUPTURED, R & R.

Part: KEYPAD — UNKNOWN (COCKPIT DOOR) · airframe 892 hrs · 28,513 cycles

COCKPIT DOOR CHIME DOES NOT WORK WITH CODE 1 ENTERED, WHEN EMERGENCY CODE 112 ENTERED, CHIME BEEPS WHEN IT SHOULD BE A STEADY TONE FOR 30 SEC. REPROGRAMMED IRCD PER AMM 52-54-01-5-0. 1 ENT NOW CHIMES CREW AND ALL EMERGENCY CODES ARE ACTIVE AND FUNCTION PROPERLY.

Part: SENSOR — FAILED (OIL TEMP) · airframe 89,029 hrs · 28,437 cycles

LEVEL 2 OIL TEMP HIGH. OIL TEMP 203 ABOVE RED LINE. NR 2 ENGINE SHUTDOWN. SPIKING AFTER SHUTDOWN AT GATE. TROUBLESHOT IAW FIM 79-32-00/201. REMOVED AND REPLACED THE NR 2 ENGINE OIL TEMP SENSOR IAW MM 79-32-01-2. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (EVAC SLIDE) · airframe 88,874 hrs · 28,366 cycles

RIGHT EVACUATION SLIDE REMOTE PRESS TO TEST INOPERATIVE. R & R REMOTE SLIDE PACK PRESS INDICATOR IAW MM 25-61-03-2. OPERATIONS CHECKED GOOD.

Part: CONTROL CABLE — BROKEN (AILERON) · airframe 88,415 hrs · 28,163 cycles

CAC COMPARTMENT SLAT TO AILERON LOCK OUT CONTROL CABLE BROKEN. R & R SLAT TO AILERON LOCKOUT CONTROL CABLE IAW MM 27-11-04-2. ADJUSTED AILERON LOCKOUT & OPERATIONS CHECKED GOOD IAW AMM 27-10-00-5.

Part: BOLT — BROKEN (LE SLAT TRACK) · airframe 88,415 hrs · 28,163 cycles

LEFT WING NR 8 SLAT, TRACK 19, LOWER FWD BOLT ROLLER INBD PIECE & NUT MISSING & BOLT BROKEN. FABRICATED BOLT IAW DWG ARB0132. R & R LT WING NR 8 SLAT TRACK LOWER FWD BOLT ROLLER IAW IPC 57-44-42-01 & MM 20-50-02. BOLT FABRICATED IAW EA 8-5740-T0310598.

Part: BOLT — SHEARED (RT WING) · airframe 88,415 hrs · 28,163 cycles

SHEARED BOLT AT RT WING AFT SPAR XCW -118. REMOVED BOLT RT WING AFT SPAR XCW -118. CLEANED CORROSION, INSTALLED BUSHING IAW EA 8-5710-T0310659 INSTALLED NEW SERVICABLE ANB7277-501 BOLT.

Part: CONTROLLER — FAILED (AIR MANIFOLD) · airframe 88,182 hrs · 28,057 cycles

AIR MANIFOLD NR 3 FAILED, AFTER WING ANTI-ICE SELECTED. R & R MANIFOLD FAIL DETECTION CONTROLLER IAW AMM 36-23-01-4. SYS OPS CHECKED NORMAL. RAN NR 3 ENGINE IAW JRH & CHECKED WING ANTI-ICE SYS.

Part: SKIN — CRACKED (RT WING) · airframe 88,415 hrs · 28,163 cycles

RIGHT WING XOS -464 CORNER OF ANTI-ICE TUBE CUT OUT UPPER INBD HAS A .5 INCH CRACK TRAVELS FROM CORNER TO SCREW, VERIFIED END OF CRACK. REPAIRED ANTI-ICE TUBE CUT OUT ON LE OF RT WING IAW SRM 57-40-01. REFER TO EA 8-5720-T0308578 PART 1.

Part: SKIN — CRACKED (ZONE 500) · airframe 88,141 hrs · 28,038 cycles

FOUND POSSIBLE CRACK ON LT INBD FUELING PANEL. COMPLIED WITH HFEC OF ABOVE NOTED AREA, IAW 06-10-01.001. CRACK NOTED RUNNING FROM INBD CORNER RADIUS TO FIRST FASTENER. INSTALLED REPAIR DOUBLER AND RIBS IAW EA 8-5710-T0308138 PT1.

Part: SKIN — CRACKED (LT WING) · airframe 88,141 hrs · 28,038 cycles

FOUND POSSIBLE CRACK ON LT INBD FUELING PANEL. COMPLIED WITH HFEC OF ABOVE NOTED AREA IAW 06-10-01.001. CRACK NOTED RUNNING FROM INBD CORNER RADIUS TO FIRST FASTENER. INSTALLED REPAIR DOUBLER AND RIBS IAW EA 8-5710-T0308138 PT1.

Part: SKIN — CRACKED (LT WING) · airframe 88,141 hrs · 28,038 cycles

FOUND POSSIBLE CRACK ON LT INBD FUELING PANEL. COMPLIED WITH HFEC OF ABOVE NOTED AREA IAW 06-10-01.001. CRACK NOTED RUNNING FROM INBD CORNER RADIUS TO FIRST FASTENER. INSTALLED REPAIR DOUBLER AND RIBS IAW EA8-5710-T0308138 PT1.

Part: CONNECTOR — DAMAGED (BRAKE SYSTEM) · airframe 86,644 hrs · 27,373 cycles

RECEIVED LEVEL 2 ALERT. "BRAKE OVERHEAT". CONFIG PAGE SHOWED NR 3 BRAKE AT 731 DEG. DESCENDED TO FL250 FROM FL350, EXTENDED LANDING GEAR IAW QRH. TEMP IMMEDIATELY WENT DOWN TO 124 DEG AFTER A FEW MINUTES TEMP MATCHED OTHER BRAKES. LANDING GEAR WAS RETRACTED AND CLIMBED TO FL350. INSPECTED NR 3 MAIN LANDING GEAR BRAKE ASSEMBLY, FOUND BRAKE TEMP SENSOR HARNESS BROKEN AT BACKSHELL OF CONNECTOR EXPOSING WIRING. AIU-2 FLAGGED R FWD INBD BRAKE TEMP OUT OF RANGE. BRAKE TEMP SENSOR. FOUND THAT THERE WAS ENOUGH OF A SERVICE LOOP IN WIRE TO RETERMINATE. REF SMP AND WDM 32-46-01, REMOVED DAMAGED SECTION OF WIRING AND RETERMINATED WIRING, ALSO, REMOVED AND REPLACED DAMAGED ELBOW AS WELL AS CONNECTOR P1-2335. BRAKE TEMPERATURE MONITOR SYSTEM CHECKS NORMAL IAW AMM 32-46-02-2. ACFT OK FOR SEVICE.

Part: CONTROL UNIT — INOPERATIVE · airframe 85,922 hrs · 27,053 cycles

ON CLIMBOUT, GOT LEVEL 2 ELEC ALERTS, AND LEVEL 1 SEL ELEC SYS MAN ON ELEC SYNOPTIC, DC TIE 3 INDICATION. GONE & AC TIE 3 GONE. NO INDICATION OF GEN 3 AT ALL ON ELEC SYNOPTIC. R & R EPCU.

Part: PANEL — WORN (NR 2 PYLON) · airframe 85,148 hrs · 26,738 cycles

NR 2 PYLON CUT-OUT FOR PANEL 457CL EDGE IN CONTACT WITH LATCHES ARE WORN OUT. REPAIRED NR 2 PYLON LT ACCESS DOOR LANDING OF 457CL IAW EA 8-5450-162534, REPAIR CLASSIFED AS MAJOR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 85,148 hrs · 26,738 cycles

UPPER CARGO SEAT TRACK RBL 28, FS 1471 HAS 2 WORN LOBES. REPAIRED SEAT TRACK AT BS 1411 -1531, RBL 28 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 85,148 hrs · 26,738 cycles

UPPER CARGO SEAT TRACK RBL48, BS 1591 - 1599 HAS 3 WORN LOBES. REPAIRED SEAT TRACK AT BS 1561 -1611, RBL 48 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 85,148 hrs · 26,738 cycles

UPPER CARGO TRACK , FS 1381 HAS ONE WORN LOBE. BLENDED LOBE, OUT OF LIMITS IAW SRM 53-70-00 FIG 5, SH 1, FABRICATED SEAT TRACK AND REPAIRED AT STA 1351-1381, RBL 75 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 85,148 hrs · 26,738 cycles

UPPER CARGO TRACK 48L, FS 1510 TO 1491 HAS THREE WORN LOBES. REPAIRED IAW SRM 53-70-00 FIG.1. MAJOR REPAIR.

Part: CARGO TRACK — WORN (ZONE 200) · airframe 85,148 hrs · 26,738 cycles

UPPER CARGO TRACK 48L, FS 1381 TO 1391 HAS NINE WORN LOBES. BLENDED DAMAGED AREA MAT.= .225, MAT. LOSS=.003" MAT. REMAINING= 0.222 FOUND TO BE IN LIMITS & LOBES WERE OUT OF LIMITS WITH REMAINING OF .240" IAW SRM 53-70-00 FIG 5, SHEET 1. REMOVED SEAT TRACK FROM FS 1371 - 1391 IAW SRM 51-31-01, FABRICATED SEAT TRACK, LOCATED & DRILLED IAW SRM 51-31-01, LOCATED & DRILLED SPLICE IAW SRM 51-31-01. TREATED & PRIMED SEAT TRACK, SPLICE HAT & SPLICE PLATE IAW SRM 51-21-01. INSTALLED SEAT TRACK, SPLICE HAT & SPLICE PLATE IAW SRM 53-70-00 FIG 5, PAINTED SEAT TRACK IAW SRM 51-21-02. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 85,148 hrs · 26,738 cycles

SKIN AT BS 1900, L52L MISREPAIRED. FABRICATED NEW DOUBLER & TRIPLER IAW SRM 53-20-00. INSTALLED NEW DOUBLER & TRIPLER IAW SRM 51-31-01. MAJOR REPAIR.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 85,148 hrs · 26,738 cycles

RT WING INBD FLAP HAS PUNCTURE ON T/E 3' OTBD OF SPRING CARTRIDGE. REMOVED DAMAGE IAW SRM 57-10-00, FIG 85. FABRICATED DOUBLER LOCATED AND DRILLED FASTENER HOLES IAW SRM 51-31-01. INSTALLED DOUBLER IAW SRM 51-31-01. TREATED AND PRIMED IAW SRM 57-21-01. PAINTED IAW SRM 51-21-02. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1920 L44L) · airframe 85,148 hrs · 26,738 cycles

SKIN AT BS 1920 L44L MISREPAIRED. REPAIRED IAW CURRENT SRM 53-20-00 FIG. 6 VOL. I. MAJOR REPAIR

Part: O-RING — FAILED (SHUTOFF VALVE) · airframe 85,116 hrs · 26,722 cycles

HYD 1 FAILED. FOUND O-RING BLOWN ON 3-1 RMP NR 1 SYS S/O VALVE. R & R O-RING REF MM 29-22-02-2. LEAK CHECKED GOOD. SERVICED NR 1 SYSTEM TO 6.5 GAL. CYCLED ALL FLT CONTROLS NUMEROUS TIMES. SYS QTY NEVER BELOW 1.3 GALS. ACFT OK FOR SERVICE.

Part: UNKNOWN — SMOKE (APU BAY) · airframe 84,945 hrs · 26,648 cycles

FIVE MINUTES AFTER NORMAL APU START & RUN, APU FAIL ALERT & AUTO SHUTDOWN TOOK PLACE. ONE MINUTE LATER, SMOKE & FUMES NOTICED FROM APU AREA. APU FIRE HANDLE PULLED & AGENT DISCHARGED. INSPECTED APU BAY FOR LEAKS AND OBVIOUS DAMAGE, NO DEFECTS NOTED REF MM 49-00-00. STARTED APU TWICE IAW JRH WITH NO ANOMOLIES DURING START. NO FAULTS INDICATED IN AIU 1, 2, 3. LOADED APU WITH PNEUMATICS AND ELECTRICAL APU OPERATED NORMALLY. PERFOMED OPS CHECK OF APU IAW AMM 49-00-00-5 OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 84,130 hrs · 26,309 cycles

AIR BOTTLE ON L1 DOOR HAS LOW PRESSURE. SERVICED L1 DOOR ASSIST BOTTLE REF MM 52-10-01-5. OK TO CONTINUE.

Part: DOWNLOCK SENSOR — MALFUNCTIONED (MLG) · airframe 83,788 hrs · 26,190 cycles

ON CONFIGURING FOR LANDING, LT MAIN GEAR INDICATED UNSAFE ON BOTH GEAR INDICATOR LIGHT AND CONFIG SYNOPTIC PAGE. COMPLIED WITH QRH "GEAR UNSAFE INDICATION WITH HANDLE DOWN" TO INCLUDE AN ALTERNATE GEAR EXTENSION. CFDS FAULTS LT GEAR DOWN AND LOCKED SENSOR A. R & R LT MLG DOWNLOCK SENSORS A & B, OPS CHECKED NORMAL REF MM 32-61-15-4, AND WDM 32-61-04, 32-61-03. ACCOMPLISHED RTS OF PSEU IAW MM 31-7101-2 WITH NORMAL RESULTS.

Part: LAMP — INOPERATIVE (SLIDE) · airframe 83,525 hrs · 26,092 cycles

DURING PRE-FLIGHT EVACUATION SLIDE "PRESS TO TEST" WOULD NOT WORK (TEST). RELAMPED PRESS TO TEST SWITCH, OPS CHECKED NORMAL IAW MM 25-61-03-5-0.

Part: LAMP — INOPERATIVE (RT DOOR) · airframe 83,265 hrs · 25,992 cycles

RT DOOR PRESSURE CHECK LIGHT DOES NOT DISPLAY ON PREFLIGHT. RELAMPED PUSH TO TEST BOTTON WITH CORRECT LAMPS OP'S CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 82,474 hrs · 25,680 cycles

L1 DOOR PRESS TO TEST LIGHT DOES NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL: 52-10-03, L1 MAIN ENTRY SLIDE/RAFT INOP, R & R L1 DOOR SLIDE RAFT PRESS TO TEST BATTERIES IAW SMP. PRESSURE PRESS TO TEST LIGHT, OPS CHECKS NORMAL IAW MM 25-61-03-5. ACFT OK FOR SERVICE.

Part: TRANSDUCER — FAILED (LT MLG) · airframe 81,463 hrs · 25,291 cycles

LEFT MLG - NR 5 & 6 TRANSDUCER HARNESSES HAVE SPIRAL WRAP COMPLETELY MELTED ONTO HARNESS ALONG ENTIRE LENGTH OF AXLE. MELTED SPIRAL (WRAP REMOVED FROM BEHIND NR 5 & 6 WHEEL SPEED TRANSDUCERS. WIRE CASING DAMAGE REPAIRED WITH TEFLON TAPE. CONNECTORS WRAPPED AND TIED AND NEW TEFLON SPIRAL WRAP INSTALLED. WHEEL TRANSDUCER INSTALLED IAW MM 32-45-03-2. SPIN TEST SATISFACTORY IAW M.M. 32-45-03-2.

Part: WIRE HARNESS — MELTED (RT MLG) · airframe 81,463 hrs · 25,291 cycles

RT MLG NR 7 & 8 TRANSDUCER HARNESSES HAVE SPIRAL WRAP COMPLETELY MELTED ONTO HARNESS ALONG ENTIRE LENGTH OF AXLE. REMOVED MELTED SPIRAL WRAP FROM AFT WIRE HARNESS (7&8 WHEELS) REPAIRED DAMAGED WIRE COATING WITH DM52186 TYPE 1 TAPE FOR HIGH TEMP & REPLACED MELTED SPIRAL WRAP WITH DMS1973 HIGH TEMP SPIRAL WRAP AS REQUIRED MM 20-30-01-2 CARBON BRAKE EO.8-3243-7-5000 .

Part: WIRE HARNESS — MELTED (LT MLG) · airframe 81,463 hrs · 25,291 cycles

LEFT MLG- NR 1 & 2 TRANSDUCER HARNESSES HAVE SPIRAL WRAP COMPLETELY MELTED ONTO HARNESS ALONG ENTIRE LENGTH OF AXLE. REMOVED MELTED SPIRAL WRAP FROM ANTI-SKID HARNESS & REPLACED IT WITH NEW HIGH TEMP SPIRAL WRAP (DMS 1973-375) PER REV C DWG SR10320028 SHEET 8 EMP-235856 EMP-235856 QC97667

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 81,463 hrs · 25,291 cycles

NR 3 TRANSDUCER WIRE HARNESS - SPIRAL WRAP COMPLETELY MELTED ONTO HARNESS ALONG ENTIRE LENGTH OF AXLE. REFER TO: LEVEL 2 ALERT"ANTI-SKID R FAIL" AFTER PRESSING ANTI-SKID TEST BUTTON. REMOVED JUMPER WIRE FROM NR 3 BRAKE ASSY. PER AMM 32-43-01-04. INSTALLED NEW SPIRAL ON NR 3&4 WIRE HARNESS ON RT GEAR PER DWG SR10320028. REPLACE FWD ANTI-SKID WIRE ASSY.PER AMM 32-11-01-04. PERFORMED CONTINUTITY CHECK. PER WDM 32-45-02. REPLACED NR 3 TRANSDUCER PER AMM 32-45-03-2, REINSTALLED NR 4 TRANSDUCER PER AMM 32-45-03-02. INSTALLED NR 3&4 HUB CAPS PER AMM 32-41-02-2. PERFORMED WHEEL SPIN TEST PER AMM 32-45-03-2. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER 32-45-01-4. PERFORMED ANTISKID TEST PER 32-45-00-05. ALL TESTS AND OPS CHECK GOOD.

Part: SKIN — DAMAGED (TAILCONE) · airframe 81,320 hrs · 25,244 cycles

DURING WALKAROUND FOUND NR 2 ENGINE PATIO ACCESS DOOR MISSING. CALLED MOCC AND UPLOAD PICTURES. SKIN HAS A HOLE WITH THIS MEASURES 2 INCHES LONG 1.5 INCH WIDE. TAILCONE ASSY TO BE REPLACED TAILCONE ASSY REMOVED PER MM 53-52-00-2. INSTALLED TAILCONE IAW AMM 53-52-00-2. COMPLETED ADJUSTMENT CHECK FOR TAIL CONE ASSY PER MM REF 53-52-00-2.NO ADJUSTMENT NEEDED.STOWED TAILCONE PER SAME MM REF. ACFT OK FOR SERVICE.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (ENGINE) · airframe 78,608 hrs · 24,378 cycles

REJECTED T/O WITH ENG FAIL LIGHT AT 87 KTS RWY 18R KMEM OAT 19C, GW 398,000, RW WET. AUTOTHROTTLES ON ENG NR 2 INITIALLY OVERSHOT MAX POWER AND THEN (MANUALLY LIMITED FURTHER INCREASE) RETARDED NR 2 BELOW MAX PWR GIVING >11 PERCENT DIFFERENCE ON POWER SETTINGS IN POWER. NO ENGINE EXCEEDANCE OCCURRED. ACFT RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-B. FOUND NO FAULTS IN FCC-1 OR FCC-2. THRUST CONTROL MODULE RTS IN BOTH FCC'S, PASSED. A/T SYSTEM OPS NORMAL. A/C REMAINS CAT 2.

Part: SKIN — CHAFED (ZONE 200) · airframe 76,919 hrs · 23,751 cycles

FUSELAGE SKIN CHAFED BELOW UPPER CARGO DOOR. BLENDED 22 AREAS AND CHECKED LIMITS FOUND TO BE SERV IAW SRM 53-00-01. CHECKED 7 AREAS FOUND OUT OF LIMITS. FABRICATED DOUBLERS AND FILLERS, TREATED AND PRIMED AND INSTALLED PARTS ALL IAW SRM 53-50-00. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, IS RDR, IS SDR AND IS RII.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 76,919 hrs · 23,751 cycles

MAIN CARGO, LUGS ON SEAT TRACK ARE WORN AT FOUR PLACES BETWEEN FS 1249 - 1319 LBL 8. INSPECTED FOUND AREAS TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW TRACK AND SPLICE HAT/PLATE AND INSTALLED ALL REPAIR PARTS ALL ON MAE TRAVILERS T8/748406, T8/748404 AND SRM 53-70-00 FIG 1 AND FIG 5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS REPORTABLE AND IS RII.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,919 hrs · 23,751 cycles

MCD FLOOR PANEL IS CRACKED AT STA 1891 LBL 59. REMOVED FLOOR PANEL AND FOUND CRACKED FLOOR SUPPORT WITH LOOSE FASTENERS. FABRICATED NEW FLOOR SUPPORT AND NEW FLOOR PANEL, INSTALLED NEW SUPPORT AND PANEL, TIGHTENED FASTENERS IAW MAE TRAVELERS T8/747683,T8/750032, SRM 51-31-01, 51-21-01 AND AMM 12-22-01-7. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 76,919 hrs · 23,751 cycles

MAIN CARGO, LUGS ON SEAT TRACK WORN AT FS 1279 LBL 47. REMOVED DAMAGED SECTION, FABRICATED NEW SECTION, FABRICATED SPLICE HAT/PLATE AND INSTALLED ALL REPAIR PARTS ON MAE TRAVELERS T8/748246 AND T8/748248 IAW SRM 53-70-00. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 76,919 hrs · 23,751 cycles

MAIN CABIN SEAT TRACK IS DAMAGED AT SEVERAL AREAS FROM STATION 1629 TO 1661 AT RBL 27 BLENDED SEAT TRACK AT STATIONS 1629 - 1651 RBL 27 FOUND TO BE IN LIMITS (ORIGINAL THICKNESS .145, AFTER REWORK .140) IAW SRM 53-70-00 FIG 5. BLENDED SEAT TRACK AT 1661 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. CUT OUT DAMAGED SECTION, FABRICATED NEW SEAT TRACK SECTION, SPLICE HAT/PLATE. INSTALLED NEW TRACK AND REPAIR PARTS REMOVED AND REINSTALLED FLOOR PANELS ALL IAW TRAVELERS T8/748751, T8/748710, T8/749337, SRM 53-70-00 FIG 1 AND SRM 51-31-01. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 76,919 hrs · 23,751 cycles

MAIN CABIN SEAT TRACK IS DAMAGED AT SEVERAL AREAS FROM STATION 1079 TO STATION 1179 RBL 47. BLENDED AREAS FOUND OUT OF LIMITS. REMOVED DAMAGE AREA OF SEAT TRACK. FABRICATED NEW SECTION AND SPLICE HAT/PLATE INSTALLED NEW PARTS IAW TRAVELERS T8/748481 AND T8/748484, SRM 53-70-00. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 76,919 hrs · 23,751 cycles

MCD SEAT TRACK IS GOUGED AT RBL 7 STATION 635. BLENDED AREA FOUND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW TRACK AND INSTALLED NEW SEAT TRACK ON MAE TRAVELER T8/747973 AND IAW SRM 53-70-00 FIG 1 AND FIG 5. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 76,919 hrs · 23,751 cycles

MAIN CARGO, LUGS ON SEAT TRACK WORN AT FS 1406 LBL 47. REMOVED SEAT TRACK SECTION, FABRICATED NEW SECTION AND SPLICES INSTALLED NEW SECTION IAW SRM 53-70-00 ON TRAVELER T8/748310. MAJOR REPAIR.

Part: PUMP — INOPERATIVE (NR 1) · airframe 73,680 hrs · 22,594 cycles

ON CLIMB-OUT PASSING 16,000', GOT HYD LEVEL 1 ALERT WITH HYD NR 1, NR 2, NR 3 PUMPS OFF. FOUND C/B POPPED. RESET AND IT POPPED AGAIN. RETURNED TO BASE(SJU) MEL 10JAN07. ACN RELEASED FOR SERVICE PER MEL/CDL: 29-11-01 CATEGORY: C EXPIRATION: 20JAN07 "MEL 29-11-01: ENG NR 1 HYD PUMP - INOP. PUMP REMOVED."

Part: FITTING — FAILED (NR 2 PYLON) · airframe 71,042 hrs · 21,803 cycles

REMOVED NR 2 ENG REF W/C 71T1101 WHILE LOWERING ENGINE AFT LT MOUNT BROKE, TEARING WEB AND CRACKED ANGLES ALSO BOTH T/R HALVES DAMAGED. TURNED OVER TO DAY SHIFT FOR FURTHER EVALUATION. REPLACED WEB AND FITTINGS AS REQUIRED REF DWG AVB7318 AND SRM 51-00-01 RII:271980.

Part: PRESSURE SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 70,386 hrs · 21,559 cycles

EN ROUTE AT FL 350, IN AND OUT OF POSSIBLE ICING CONDITIONS, WHEN INITIATING WING A/I ON, RECEIVED AIR SYS 3 OFF (LEVEL 1) ANNUNCIATED, WITH NR 3 BLEED (AMBER) AND NR 3 MANF (RED) LIGHTS ILLUMINATED. QRH PROCEDURES FOLLOWED. DIVERTED INTO TO KDEN. RED MANF LIGHT EXTINGUISHED APPROX 10 MIN FROM LANDING MEL: RELEASED FOR SERVICE PER MEL/CDL: 30-11-01 CATEGORY: C EXPIRATION: 27AUG05 WING A/I SHUTOFF VALVES, INOP. DO NOT OPERATE A/C IN ICING." PERFORMED LEAK DECAY CHECK FOR NR 3 MANIFOLD OK. CHECKED MANIFOLD FAIL DETECTOR UNIT FOR FAULTS. REPLACED NR 3 MAN FAIL DETECTOR PRESS SWITCH AND TESTED OK TO CONTINUE.

Part: BRACKET — CORRODED (NR 1 SPOILER) · airframe 69,975 hrs · 21,379 cycles

COMPLY WITH EA 8-5740-55486, WINGS, NR 1 SPOILER ACTUATOR MOUNT HOLD-DOWN BRACKET CORROSION. COMPLIED WITH EA 8-5740-55486, WINGS NR 1 SPOILER ACTUATOR MOUNT/HOLD-DOWN BRACKET CORROSION.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 69,532 hrs · 21,220 cycles

CRG FIRE LWR AFT ALERT ON DESCENT. CREW FIRED 1 BOTTLE AND DECLARED EMERGENCY, NO EVIDENCE OF ANY FIRE IN AFT OR CENTER CARGO COMPART OR CONTAINERS AS THEY WERE OFF LOADED. REMOVED AND REPLACED LWR FWD CARGO FIRE EXT IAW M/M 26-22-01-4. REMOVED AND REPLACED MSC IAW M/M 31-12-01-4, OPS CHECK NORMAL. INSPECTED WIRING IN AFT LWR CARGO PER REF TO MD-10 FIM 26-14-02, NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED BOTH SMOKE DET IN CENTER CARGO COMP AND BOTH DET IN AFT CARGO COMP PER MM 26-14-01-4 AND PERFORMED ADJ/TEST OF LOWER CARGO COMP FIRE/SMOKE DETECTION SYSTEM PER MM 26-14-01-5. NO DEFECTS NOTED. OK FOR SERVICE.

Part: HANDLE — MISSING (CARGO DOOR) · airframe 67,407 hrs · 20,372 cycles

UPON A/C ARRIVAL FOUND COVER DOOR TO CENTER CARGO DOOR LOCKING HANDLE MISSING. ALSO MISSING HINGE ASSY. CENTER CARGO DOOR LOCK HANDLE COVER TEMP REPAIR PER EA LIMITED TO 2 FLT CYCLES COMPLIED WITH PART 1 OF EA 8-5350-76446. DOOR REPLACED.

Part: CHIP DETECTOR — CONTAMINATED (NR 2 ENGINE) · airframe 65,002 hrs · 19,404 cycles

ENGINE NR 2 OIL FILTER LEVEL 2 ALERT, CAME ON AT TOP OF CLIMB. THROTTLE WAS RETARDED TO IDLE BUT ALERT STAYED ON. ENGINE NR 2 WAS SHUT DOWN IAW THE CHECKLIST. ENGINE FAN COWLS WERE OPENED AND THE MASTER CHIP DETECTOR WAS PULLED, FERROUS METAL STRANDS WERE COVERING THE END. THE LUBE SUPPLY FILTER AND SCAVENGE OIL FILTER WAS REMOVED AND SAMPLES WERE PLACED IN SAMPLE BAGS & TAGGED. MEM PP ENGINE WAS NOTIFIED THAT A FINE FERROUS CONTAMINANT GOLD IN COLOR, WAS PRESENT. PULLED SCAVENGE PUMP FILTER SCREENS AND FOUND METAL IN THE B SCAVENGE IN FILTER.

Part: CONTROL HANDLE — DIRTY (COCKPIT) · airframe 64,901 hrs · 19,364 cycles

ON GEAR EXTENSION DURING FINAL APPROACH ALL FOUR L/G INDICATORS STAYED RED, SYSTEM DISPLAY SHOWED ALL RED ALSO. RECYCLED GEAR HANDLE - NORMAL EXTENSION. FOUND THAT WHEN LANDING GEAR HANDLE IS PULLED OUT THAT THE HANDLE WILL NOT FULLY RETURN TO THE STOWED POSITION REMAINING IN THE TEST POSITION. A SLIGHT TAP ON THE GEAR HANDLE EXTINGUISHES ALL OF THE GEAR INDICATION LIGHTS. CLEANED DUST AND LINT FROM GEAR HANDLE SLIDE AND GEAR HANDLE SWITCH S1-431 PER SMP. GEAR HANDLE NOW OPERATES SMOOTHLY AND STOWS FULLY EACH TIME. TESTS NORMAL IAW M/M 32-60-00-5.

Part: SLAT — CRACKED (RT WING) · airframe 63,802 hrs · 18,881 cycles

NR 1 SLAT RT WING CRACKED AT LIGHTNING HOLE AT I/B END AT XFS 145. REMOVED AND REPLACED DOUBLER PER SRM 57-00-01 VOL 1 FIG 4.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,802 hrs · 18,881 cycles

CORRODED LONGERON 18 LEFT AT BS 1215. REMOVED AND REPLACED LONGERON PER SRM 53-10-00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,801 hrs · 18,881 cycles

AFT CARGO TUNNEL BS 1847-1857, STR 28R INTERCOSTAL PANEL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,801 hrs · 18,881 cycles

AFT CARGO TUNNEL BS 1897-1902, STR 27R INTERCOSTAL PANEL CORRODED. REMOVED AND REPLACED WEB AND CHANNEL PER SRM 51-00-00, 51-21-01, 51-35-01 & 51-33-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,802 hrs · 18,881 cycles

AFT FUSELAGE WASTE TANK COMP BS 1967, STR 47L & 47R Z-ANGLE SIDEWALL PNL SUPPORT CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 53-16-01 & 51-35-01.

Part: STANCHION — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,802 hrs · 18,881 cycles

AFT FUSELAGE BS 1967, STR 50R CORRODED STANCHION SUPPORT. REMOVED AND REPLACED STANCHION PER SRM 51-35-01.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,802 hrs · 18,881 cycles

UPPER CARGO SEAT TRACK AT BS 595 TO 765 HAS CRACK AT 655. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 & 51-21-01.

Part: GUIDE — CORRODED (CARGO BAY) · airframe 63,802 hrs · 18,881 cycles

N 56 LEVEL CORROSION IN FWD CARGO PIT ON LEFT HAND CARGO GUIDE RAIL.

Part: SLAT — FAILED (WING)

DURING SLAT EXT BEFORE LAND SLAT DISAGREE STAY ILLUMINATED. RED TAB WERE ACCOMPLISH AND A NO SLAT WITH FLAPS LAND WAS ACCOMPLISH. REMOVED AND REPLACED S1-379 PER MM 27-84-02-2 PG 201. FUNCTIONAL CK GOOD PER PARAGRAPH 3. ACFT OK FOR CONT SERVICE.

Part: SLAT — MALFUNCTIONED (WING)

SLATS WOULD NOT EXTEND WHEN SEL FOR LAND. LAND WITH FLAPS BUT NO SLATS. TROUBLESHOT SYS PER DC-10-30 TAFT 27-80-00 PG 119. OPS CK NORMAL, NO DEFECTS NOTED.

Part: PROXIMITY SWITCH — MALFUNCTIONED (AVIONICS BAY) · airframe 61,510 hrs · 18,169 cycles

AFT RAISING LAND GEAR, LIGHT ON PILOTS LAND GEAR LIGHT PANEL REMAINED ILLUM. TROUBLESHOOTING PER TAFI 32-30-00 FAULT CODE AF, NO FAULT FOUND. PRECAUTIONARY REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT PER DC 10-30 MM 32-61-01-2. OK FOR SERVICE.

Part: BLOCK — CORRODED (LT MLG) · airframe 60,761 hrs · 17,914 cycles

LT MAIN LANDING GEAR FIXED BRACE PILLOW BLOCK HAS CORROSION IN I/B & O/B HOLES ON TRAPEZOIDAL FITTING. REMOVED AND REPLACED CORROSION PER SRM 57-20-003 EA 8-5710-49631.

Part: BLOCK — CORRODED (RT MLG)

RT GEAR FIXED BRACE PILLOW BLOCK I/B HOLE CORRODED. *S/D* REMOVED CORROSION PER SRM 57-20-003 EA 8-5710-49631.

Part: FIRE BOTTLE — DISCHARGED (NR 2 ENGINE)

NR 2 ENGINE SHOWING LOW PRESSURE ON FIRE BOTTLE. (PER CREW DEBRIEF - AGENT NR 2). REMOVED AND REPLACED NR 2 ENGINE FIRE BOTTLE IAW 26-21-02-2.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT)

ON TAKEOFF, PNEUMATIC TEMP HI LIGHT FLICKERED INTERM ON PILOT ANNUNCIATOR PANEL. REMOVED AND REPLACED OVERHEAD WARN AND CAUTION ANNUN, SYS LOGIC CONTROLLER UNIT, UNIT PER MM 33-15-03-2. OPS CK GOOD.

Part: TAIL CONE — DAMAGED (AFT FUSELAGE)

IN FLT HAD LOUD BANG FOLLOWED BY AIRFRAME VIBRATIONS. ON POST FLT PATIO DOORS UNDER NR 2 ENGINE HAD OPENED IN FLT. *S/D* REMOVED AND REPLACED LT AND RT DROOP ELEVATORS AND TAIL CONE ASSY PER MM 27-30-03-4, MM 53-52-00. REPAIRED TAIL MISMATCH COVER ON EA 8-5310-35203.

Part: PROXIMITY UNIT — FAILED (RT MLG)

RIGHT MAIN LANDING GEAR LIGHT REMAINED ON RED AFTER GEAR RETRACTION ON TAKEOFF, F/O PANEL ONLY. GEAR WAS CYCLED DOWN AT BACK UP AND ALL INDICATIONS WERE NORMAL WITH RIGHT MAIN RED LIGHT OUT. REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT AS PER TAFI 32-30-00, OPS CHECK NORMAL.

Part: PROX CONTROL — MALFUNCTIONED (RT MLG)

ON TAKEOFF, AFTER GEAR UP RIGHT MAIN GEAR RED LIGHT ILLUMINATED ON BOTH FRONT AND S/O PANEL RECYCLED GEAR AND LIGHT WENT OUT ON APPROACH TO ATL BEFORE GEAR DOWN RIGHT MAIN GEAR LIGHT AGAIN ILLUMNA, ON FRONT PANEL ONLY S/O PANEL NO LIGHT FACT 11SEP96 22:30 ATL U REPLACED PROXIMITY SWITCH CONTROL UNIT MM 32-61-01.

Part: GROUND PROX BOX — DEFECTIVE (E/E COMPT)

ALL FOUR GEAR LIGHTS ILLUM WITH HANDLE UP, NO OTHER WARNINGS. RECYCLED GEAR IAW RED TAB PROCEDURES, GOT 4 GREEN ON BOTH PANELS WITH GEAR EXTENDED. AFTER THE GEAR WAS RETRACTED, THE FOUR RED LIGHTS REILLUMINATED, NO HORN. REMOVED AND REPLACED GROUND PROX BOX AS PER MM 32-61-01, OPS CHECK OK.

Part: FITTING — CORRODED (BS 1790)

INSIDE AFT CARGO COMPT - FWD LOWER CORNER OF DOOR SILL - LONGERON 41 - END FITTING AT STA 1790 IS CORRODED - LEVEL 2. INSTALLED NEW FITTING.

Part: ANGLE — CORRODED (BS 1795-1835)

INSIDE AFT CARGO COMPT STA 1795-1835, LONGERON 44L, NESTING ANGLE AND ATTACHING WEB TO CARGO DOOR LOWER TORQUE BOX HAS CORROSION - LEVEL 2. REMOVED AND REPLACED NESTING ANGLE AND ATTACH WEB.

Part: LONGERON — CORROSION (BS 152-154)

RUSTY FASTENERS IN LWR CENTER CARGO COMPT UNDER FLOOR SPACE AT FS 152-154L, LONGERONS 45-47L. REMOVED FASTENERS, BURNISHED OUT CORROSION, FABRICATED ANGLE AND INSTALLED IAW EO 8-5310-25134.

Part: T ANGLE — CRACKED (LT HORIZ STAB)

LEFT STAB L/E 2ND RIB, REMOVED SECTION O/B WEB UPPER T-CHORD IS CRACKED ON INSIDE. REMOVED T-CHORD, INSTALLED NEW T-CHORD P/N ALC-7502-11, PER SRM 51-00-01.

Part: T ANGLE — CRACKED (RT HORIZ STAB)

RT STAB L/E 2ND RIB, O/B SECTION UPPER WEB T-CHORD IS CRACKED, ENTIRE LENGTH INSIDE. REMOVED T-ANGLE, INSTALLED NEW PART ALC7502-12, FEDEX SRM 51-00-01.

Part: BULKHEAD — CORRODED (BS 1156)

WING CTR SECT FUEL TANK BLKHD STA 1156 HAS INTERGRANULAR CORROSION AT VERTICAL STIFFENER O/B OF OPENING PNL143CZ, FWD FACE, LWR AREA. REMOVED CORROSION FROM AFFECTED AREA IAW DC10 SRM 51-21-01. THICKNESS LIMIT CK'D OK. ALONDINED AND PAINTED AFFECTED AREA IAW DC10 SRM 51-21-01.

Part: T-CHORD — CRACKED (LT HORIZ STAB)

LT/STAB L/E 2ND REMOVED SECTION O/B WEB LWR T-CHORD IS CRACKED ON INSIDE 6. STOP DRILLED CRACK, FABRICATED SHIMS AND REPAIRED ANGLE AS PER EA 8-5510-25132.

Part: BRACKET — CRACKED (RT LE SLAT)

RIGHT WING O/B SLAT DRIVE OUTER BRACKET CRACKED, LOWER FWD FLANGE RADIUS. REMOVED AND REPLACED BRACKET WITH NEW BRACKET MODIFIED TO EO 8-2780-7-2319C SPEC. MM 27-83-02 (REF TO CONTROL ITEM 4, PART NR 4).