N316FE

Part: DOOR SILL — CRACKED (BS 1781) · airframe 64,696 hrs · 24,008 cycles

CENTER CARGO DOOR SILL, LOWER AFT SECTION HAS A CRACK REPAIRED PER SRM MD10 53-00-01 VOL I P40

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK L-1 DOOR AREA FLOOR PANEL, RIGHT NEXT TO MAIN CARGO DOOR CONT, SHOWING SPONGY AND SUSPECTING DELAM. R/R THE FLOOR PANEL#223AF WITH SCREW PER SRM

Part: SKIN — DENTED (LT WING) · airframe 64,696 hrs · 24,008 cycles

REWORK: REFERENCE SNRM 467..L/H WING UPPER SURFACE-L/E SKIN DENTED AT APPROX. STA. XDLE 309,INBD OF #3 SLAT FIXED WING LEADING EDGE IS PRIMARY STRUCTURE. "MAJOR REPAIR" CUTOUT DAMAGED AREA 1IN DIAMETER AND REPAIRED AREA PER. MD10-30 SRM 57-00-01 VOL.1 FIGURE 4 SHEET 2 "MAJOR REPAIR"

Part: FILLET — GOUGED (LT WING SLAT) · airframe 64,696 hrs · 24,008 cycles

LH WING # 1 SLAT FILLET ASSY LOWER SURFACE TRAILING EDGE GOUGE REPAIRED # 1 SLAT FILLET ASSY LOWER SURFACE TRAILING EDGE DAMAGED PER SRM 51-43- 01 VOL 2 PARAGRAPH 11.A STEPS ( 1)-(7)

Part: DOUBLER — DAMAGED (RT WING) · airframe 64,696 hrs · 24,008 cycles

RH WING INTERNAL LE - ABOVE ANTI-ICE TELESCOPE DUCT(ACCESS, PANEL 613AB)- BEADED DOUBLER IS DAMAGED. 0000575467 : WRAY, BASIL P. B. - 03-JUN-2021 13:20 TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR. REFERENCE E.A. 8-5710- T0361809. "WINGS-BASIC WING STRUCTURE-CRACK ON BEADED DOUBLER AT XOS 467 R/H WING LEADING EDGE". "MAJOR REPAIR"

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK FLOOR PANEL FROM STA 1561 TO 1650 AT LBL 107 TO LBL 75 HAS GOUGES IN SEVERAL AREAS (MARKED) FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK FLOOR PANEL FROM STA 1099 TO 1029 AT LBL 107 TO LBL 75 POSSIBLY DELAMED (MARKED) FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 47 TO LBL 75 HAS SEVERAL GOUGES - POSSIBLE DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK: FLOOR PANEL AT APPROX STA 1503 BETWEEN RBL 8 AND LBL 8 IS DAMAGED (MARKED AND DOT 44 IN 2 PLACES) REPAIRED MAIN DECK: FLOOR PANEL AT APPROX STA 1503 BETWEEN RBL 8 AND LBL 8 PER SRM 53-60-00 VOL I PG 6 FIG 6 (MAJOR REPAIR)

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 107 TO 75 DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK FLOOR PANEL FROM APPROX STA 1481-1561 BETWEEN RBL 75-RBL107 IS WORN THROUGH TOP LAYER AT APPROX STA 1511 RBL 75 SIDE (MARKED AND DOT 41) FABRICATED NEW FLOOR PANEL ACA0126-4 FROM STA 1481-1561, RBL 75 TO RBL 107 AS REQ'D REF FEDEX DRAWING SRZ-25-005 (MAJOR REPAIR)

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO PIT FLOOR PANEL 187CF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO PIT FLOOR PANEL 187AF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINAION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO PIT FLOOR PANEL 187GF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO PIT FLOOR PANEL 187BF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DEMLAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005

Part: SKIN — CRACKED (RT WING) · airframe 64,696 hrs · 24,008 cycles

R/H WING ANTI ICE TELESCOPING DUCT CUT OUT, TOP O/B CORNER CRACKED (MARKED) REPAIRED CRACK ON CORNER OF SKIN CUT-OUT FOR ANTI-ICE DUCT PER SRM 57-10-00 VOL.1 FIG. 103 SHEET 5. "MAJOR REPAIR"

Part: SKIN — CRACKED (LT WING TIP) · airframe 64,696 hrs · 24,008 cycles

LH WING TIP LOWER SURFACE, 1" CRACK IN SKIN - APPROX. XW987, OUTBD OF STROBE LIGHT CONTROLLER ACCESS DOOR. REPAIRED WINGTIP SKIN CRACK REF: SRM 57-00-01 VOL 1, FIG 4.

Part: SEAL — CRACKED (RT WING TE FLAP) · airframe 64,696 hrs · 24,008 cycles

RH WING OUTBD FLAP OUTBD HINGE XW638 - METAL SEAL CRACKED AT PANEL 636JL. REMOVED AND INSTALLED NEW METAL SEAL PN ARC2148-9 ON ARC2148-504(636JL)FAIRING REF SRM 51-31-01 VOL 2 AND DWG ARC2148

Part: LONGERON — CORRODED (BS 1854-1864) · airframe 64,696 hrs · 24,008 cycles

AFT CARGO COMPT BILGE STA 1854-1864 CORROSION AT L48R. MRKD 0003884010 : GUTZWEILER, JOHN - 22-MAY-2021 05:37 REMOVED AND REPLACED DISCREPANT LONGERON SPLICE ASSEMBLY AFT CARGO COMPARTMENT BILGE STA 1854 - 1864 LONGERON 48R REF DWG NGA6314.

Part: DOOR FRAME — CHAFED (CARGO DOORWAY) · airframe 64,696 hrs · 24,008 cycles

LOWER CENTER CARGO DOOR, LOWER AFT JAMB EDGE DAMAGED, MARKED. REMOVED DAMAGE AND COMPLIED WITH DOOR JAMB REPAR AT LOWER CENTER CARGO DOOR LOWER AFT EDGE PER MD10-30 SRM 53-53-00 FIG 26 VOL 1.

Part: SKIN — DAMAGED (RT WING SLAT) · airframe 64,696 hrs · 24,008 cycles

RIGHT WING #4 SLAT AFT SIDE HAS MANY DAMAGED, MISSING AND LOOSE RIVETS. 0000435071 : HARPER, RICHARD R - 05-MAY-2021 18:58 REMOVED AND REPLACED FASTNERS ON R/H WING SLAT#4 INNER SKIN PER SRM 57-10-00 PARA.90 PG.387 AND TRACKING EA 8-5750-T0361370

Part: SKIN — DAMAGED (RT WING SLAT) · airframe 64,696 hrs · 24,008 cycles

RIGHT WING #3 SLAT AFT SIDE HAS MANY DAMAGED, MISSING AND LOOSE RIVETS. 0000435071 : HARPER, RICHARD R - 05-MAY-2021 19:03 REMOVED AND REPLACED FASTNERS ON R/H WING SLAT#3 INNER SKIN PER SRM 57-10-00 PARA.90, PG.387 ALSO TRACKING EA 8-5750-T0361351

Part: SEAT TRACK — WORN (MAIN CARGO) · airframe 64,696 hrs · 24,008 cycles

MAIN CARGO COMPT, APPROX STA 1199 X= 47.50, SEAT TRACK WORN. FOUND SEAT TRACK TO BE WORN OUT OF LIMITS. REPLACED SEAT TRACK SECTION AT APPROX STA 1213 TO 1261 X 47.5 PER SRM 53-70-00 FIG 1 VOL 1.

Part: SEAT TRACK — DAMAGED (BS 959-969) · airframe 64,696 hrs · 24,008 cycles

MAIN CARGO COMPT, APPROX STA 959-969 X= -27.50, SEAT TRACK WORN AT TWO LOCATIONS. REMOVED DAMAGE AND INSTALLED PLUG REPAIR. REF. SRM 53-70-00 FIG. 2 VOL.1 "MAJOR REPAIR"

Part: PANEL — CORRODED (LT WING) · airframe 64,696 hrs · 24,008 cycles

L/H WING TRAPERZOID PANEL ARC0269-503 SHOWS SIGNS OF CORROSION AND DELAMINATION PERFORMED REPAIR BONDING ON PNL ARC0269-503 PER SRM 51-71-00 VII PARAGRAPH 18.

Part: SEAT TRACK — WORN (BS 1640) · airframe 64,696 hrs · 24,008 cycles

MAIN DECK SEAT TRACK AT APROX STA 1640 RBL 47.50 WORN (MARKED) REMOVED WORN SEAT TRACK SECTION AND SPLICED IN NEW SECTION OF SEAT TRACK . REF. SRM 53-70-00 FIG. 1 VOL.1 AND FEDEX DRAWING SR10-53-002.

Part: SUPPORT — CORRODED (RT MLG WW) · airframe 64,696 hrs · 24,008 cycles

STRUCTURES - FUSELAGE SEALS AND DRAINS: DURING FUSELAGE PRESSURIZATION, AT R/H MAIN LANDING GEAR WHEEL WELL R/H UPPER T-CORD FWRD BULKKHEAD LEAKING, SHOWING SHOWING WHITE POWDERY SUBSTANCE UNDER 4 EACH CLAMPS/CLIPS & RUB STRIP MIGRATED MIGRATED BETWEEN CLIPS AREA MARKED RED WITH DOT 3 DUE CORROSION, REMOVED AND REPLACED UPPER SUPPORT(AEA7292-2) OUTBD SUPPORT(AEA7291-2) LWR SUPPORT(AEA7284-4) IAW MD10-30 SRM 51-33-01 VOL2 & DRWG AEA7279. REMOVED AND REPLACED 9 INTERMEDIATE PRESSURE PNL CLAMPS AEA7299-3 IAW SRM 51-31- 01 VOL2 & DRWG AEA7294. REINSTALLED RUBSTRIP TO UPPER SUPPORT IAW DRWG AEA7279. FUSELAGE PRESSURIZATION CHK PFM'D IAW MD10 AMM 21-00-00-5, FOUND SATIS.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 64,696 hrs · 24,008 cycles

CENTER LANDING GEAR WHEEL WELL, L/H FWD VERTICAL BULKHEAD, AT TRANSITION HOLE FOR SPOILER/AILERON CONTROL RODS, STA 1381 Z=-76 TO -87. DOUBLER FITTING AEA0486 HAS A FOUR INCH CRACK ALONG THE VERTICAL FASTENER ROW, TOP AREA. (MKD) REMOVE AND REPLACE LONGERON 48R STA 1854 - 1864 BILGE SECTION REF DWG NGA6314, SRM 53-36-01 FIG 1 VOL III, SRM 51-33-01 VOL II, LONGERON ASSEMBLY PART NUMBER AGA7438-1 (2).

Part: LINE — LEAKING (HYD SYSTEM) · airframe 64,446 hrs · 23,893 cycles

PDIS 316 29-02 5970 23FEB21 MEM FACT U "ENROUTE TO KMEM LEVEL 1 "HYD 3 ELEV OFF" ALERT ILLUMINATED. HYD 3 WAS AT 4.3 AT THE TIME. HYD 3 CONTINUED TO DECREASE TO 3.0. GEAR EXTENDED W/GEAR HANDLE AND FLAPS & SLATS DEPLOYED OKAY. MADE FLAPS 35/EXT LANDING KMEM RWY 10C. HYD 3 WENT TO 0.4 AT GEAR EXTENSION WITH LEVEL 3 HYD FAIL ALERT. (D.L.W.)" SHGN 23FEB21 18:03 MEM U ACFT RETRIEVED FROM RWY 18C AND TOWED TO GATE 826. WILL TROUBLESHOOT AFTER OFFLOAD. PRIMARY TRIM CONTROL VALVE. WITH SYSTEM 3 HYD SERVICED, OPERATED HORIZONTAL STABILIZER TRIM REF AMM 27-40-00-2. NOTED LARGE LEAK FROM HYDRAULIC LINE TO UPPER PRIMARY TRIM CONTROL VALVE P/N AJK7004-759. FOUND FITTING 'B'-NUT LESS THAN FINGER TIGHT (ALMOST COMPLETELY DISCONNECTED). DISCONNECTED LINE, INSPECTED 'B'-NUT AS WELL AS MATING SURFACE ON VALVE UNION. NO DISCREPENCIES WERE FOUND. RECONNECTED & RE-TORQUED LINE IAW AMM 20-50-01-2. RE-PREFORMED HORIZ STAB OPS CHECKS REF AMM 27-40-00-2.NO LEAKS NOTED. CLOSED MAIN GEAR DOORS. AIRCRAFT O.K. FOR SERVICE.

Part: TEE FITTING — CRACKED (HYD SYSTEM) · airframe 64,246 hrs · 23,790 cycles

"HYD 3 ELEV OFF" ALERT CAME ON. WE NOTICED HYD 3 QUANTITY SLOWLY DECLINE. WE LATER HAD HYD QUANTITY LOW. WE EXTENDED THE LANDING GEAR NORMALLY. WE THEN HAD HYD 3 FAIL. AFTER BLOCK IN FOUND HYDRAULIC QTY NR 3 SYSTEM AT 3.5 GAL. FOUND HYD LINE CRACKED AT TEE FITTING MPN. AJK7022-509, UPPER HYD. LINE AT HORIZONTAL STAB UPPER PRIMARY CONTROL VALVE. REMOVED AND REPLACED BROKEN HYD LINE, PER 20-10-01-2. SERVICED NR 3 HYD SYSTEM, PER MM 12-13-02-3. LEAK AND OPERATIONS CHECKS NORMAL. OK TO CONTINUE.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE) · airframe 64,083 hrs · 23,698 cycles

MDIS 316 25-60 5669 28NOV20 MEM OPEN U. L1 DOOR SLIDE PRESS TO TEST LIGHT INOPERABLE. RELAMPED AND R & R BATTERIES, PER AMM 25-61-03-2. TROUBLESHOOTING IS REQUIRED PRIOR TO INSTALLING PARTS.

Part: BATTERY PACK — NO TEST (SLIDE LIGHT) · airframe 62,690 hrs · 22,921 cycles

L1 DOOR SLIDE LIGHT WILL NOT TEST. REPLACED SLIDE INDICATOR BATTERIES, OPS CHECKS GOOD. REF MD10MM 25-61-02-2.

Part: ENGINE — FLUCTUATES (NR 3) · airframe 62,143 hrs · 22,618 cycles

CLIMBOUT OUT OFF FL230"ENG 3 EXCEEDANCE"LVL ALERT DISPLAYED.EGT OBSERVERED AT 964 WITH PWR EQUAL OTHER PARAMETERS EQUAL.DURING CRUISE HAD #3 ENG PULLED BACK 10-15% N1 TO KEEP BELOW YELLOW ARC.NOTICED SLOW FLUCTUATIONS FROM 590 EGT TO 800 DURING LVL FLT.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 62,016 hrs · 22,557 cycles

AUX FUEL TANK PANEL AT REAR SPAR HAS CORROSION AT MANY LOCATIONS. FABRICATED FUEL TANK BULKHEAD PANEL ON T19/1410809. REINSTALLED 6EA STIFFNERS IAW SRM 51-31-01. BULKHEAD REMOVED / REPLACED ON WORK CARD 53SI1520-01. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1601-1661) · airframe 62,016 hrs · 22,557 cycles

MAIN DECK SEAT TRACK AT X8.5 STA 1601 TO STA 1661 HAS GOUGES AND SURFACE CORROSION AT 3EA LOCATIONS. REMOVED AND REINSTALLED 2EA FLOOR PANELS FOR ACCESS IAW MD10-30 AMM 53-21-01-2. REPAIRED DAMAGED FLOOR PANELS (2EA) IAW SRM 53-60-00 FIG 6. REMOVED AND INSTALLED NEW SEAT TRACK PN 60-10964 BATCH# 2650682 IAW SRM 53-70-00 FIG 1. MAJOR REPAIR

Part: SWITCH — ACTIVATED (COCKPIT) · airframe 61,529 hrs · 22,277 cycles

AT FL280 ABOUT TO DESCEND INTO ICING WE TURNED ON WING ANTI-ICE. RECEIVED LVL 1 AIR SYS 3 OFF WITH RED MANIFOLD NR 3 INDICATION BOTH ON SCHEMATIC AND AIR SYSTEM CONTROL PANEL BLEED AIR 3 MANIFOLD LIGHT. CONSULTED WITH MOCC DIVERTED TO AVOID KNOWN ICING. REMOVED AND REPLACED NR 3 MANIFOLD FAILURE DETECTION PRESSURE SWITCH PER AMM 36-23-03-4-0.

Part: PROBE — INOPERATIVE (FUEL SYSTEM) · airframe 61,034 hrs · 22,008 cycles

15 MIN ENROUTE. JUST LEVELED AT FL350. GOT LVL 2 FUEL QTY/USED CHK. COMPLIED WITH QRH. TOTAL QTY INDICATED. 9.0 LBS LESS THAN REQUIRED. ( SHOULD OF HAD 57.0, INDICATED 48.0 ) RTB KMEM. POSSIBLE FUEL LEAK. FOUND PROBE NR 3 ON RT INOP, REMOVED AND REPLACED AND OPS CHECK IRW AMM 28-41-01-2 REV 19.16 10/20/16 OPS CHECK GOOD. REMOVED AND REPLACED AND OPS CHECKED NR 2 TANK FEED THRUS R5-9814,R5-9815, R5-9816, R5-9817 AND R5-9818 IRW AMM 28-41-05-4 REV 19.16. INSTALLED TANK NR 2 PROBE PN 020-016-003 SN 197, REMOVED PN 020-016-003 SN 728.

Part: CONTROL MODULE — OUT OF ADJUST (FLAPS/SLATS) · airframe 60,525 hrs · 21,757 cycles

DURING TAKEOFF THE FLAP/SLAT HANDLE WOULD NOT MOVE OUT OF TAKEOFF FLAP SETTING 15.5. INITIALLY COULD NOT MOVE FLAP SELECTOR WHEEL EITHER. EVENTUALLY USED THE FLAP SELECTOR WHEEL TO SELECT FLAPS 24 FOR LANDING, COULD NOT MOVE FLAP HANDLE OR GET SELECTOR TO MOVE UP PAST 15.5. NOTE GROUND PUSH BACK CREW PULLED GROUND POWER PRIOR TO OUR TRANSFER TO APU. INSPECTED AND CLEANED FLAP CONTROL MODULE, CHECKED ALL CABLE RUNS AND PUSH RODS FROM FLAP HANDLE CONTROL MODULE TO CAC, NO DEFECTS NOTED, COMPLETED AN ADJUSTMENT/TEST FLAP CONTROL MODULE IAW AMM 27-51-01-2. NO DEFECTS NOTED AT THIS TIME.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 59,408 hrs · 21,179 cycles

EMERGENCY LIGHTS BATTERY 1 LOW ALERT. FOUND WIRE FOR PIN 8 OF P1-1756A PULLED OUT OF CONTACT. TERMINATED THE WIRE. EMERGENCY LIGHTS OPS CHECKED GOOD. PERFORMED IAW M/M 33-51-01-5 AND WDM 33-51-01.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 58,916 hrs · 20,908 cycles

RIGHT WING, OTBD FLAP INBD HINGE STRESS FITTING FOUND CRACKED. REMOVED AND REPLACED THE FITTING IAW EA 8-5740 -T0331942, AND DWG ARB0029.

Part: SKIN — CRACKED (RT WING) · airframe 58,916 hrs · 20,908 cycles

RT WING, FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACKED .075 LENGTH. REMOVED CRACKED, INSTALLED FILLER AND DOUBLER PER SRM 57-10-00 VOL 1 FIGURE 106 SHEET 2.

Part: SKIN — CRACKED (RT WING) · airframe 58,916 hrs · 20,908 cycles

RT WING, FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACKED .075 LENGTH. REMOVED CRACK AND INSTALLED DOUBLER AND FILLER PER SRM 57-10-00 FIG 106 VOL2 SHEET 2.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,916 hrs · 20,908 cycles

AFT WASTE COMP STA 1967 LOWER CENTER SUPPORT STRUCTURE AFT SIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES . REMOVED AND REPLACED SUPPORT PER DWG AGA 3857-1.

Part: SKIN — CRACKED (TE FLAP VANE) · airframe 58,916 hrs · 20,908 cycles

RT I/B FLAP VANE LOWER SURFACE HAS DEEP DENT, FOUND AN 3/8" CRACK. REPAIRED CRACK IAW SRM 51-71-00 VOL II PAGE 9 PAR 5 (A).

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 58,916 hrs · 20,908 cycles

LEFT OTBD FLAP VANE, RUBSTRIP NR 6 FROM THE INBD END IS DELAMINATED. DELAMINATION FOUND UNDERNEATH RUBSTRIP ON TOP SKIN, 2.75 INCH DIA. REPAIRED THE FLAP VANE RUBSTRIP IAW SRM 51-71-00, VOL 2, FIG 72, PG 154.

Part: SKIN — CRACKED (RT WING) · airframe 58,916 hrs · 20,908 cycles

RIGHT WING FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACK 0.75 IN LENGTH. REPAIRED IAW SRM 57-10-00, FIG 107, SHEET 2.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 58,916 hrs · 20,908 cycles

RIGHT OTBD FLAP VANE SKIN BENEATH NR 6 RUBSTRIP IS DELAMINATED. REPAIRED THE SKIN IAW SRM 51-71-00, VOL II, PAGE 9, PAR 5 (A), PAR 15.

Part: INTERCOSTAL — CORRODED (MLG WW BULKHEAD) · airframe 58,916 hrs · 20,908 cycles

RIGHT WHEEL WELL AFT BULKHEAD TOP INTERCOSTAL CORRODED. REMOVED AND REPLACED THE BULKHEAD INTERCOSTAL IAW DWG AEA0026-6.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,916 hrs · 20,908 cycles

AFT WASTE COMPT: UNDERSIDE OF UPPER CENTER SEAT TRACK SUPPORT HAS MULTIPLE AREAS OF EXFOLIATION CORROSION. INSTALLED CENTER SEAT TRACK SUPPORTS REF DWG AGA7442, SEC JPF STEPS 11 & 12 JPF ATTACH.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 57,490 hrs · 20,241 cycles

ON TAKEOFF ROLL RNWY 18R, AT 80 KNOTS CALL, HUD SHOWED NO AIRSPEED TAPE & 36 KNOTS INDICATED. CAPTAIN'S PFD SHOWED ACCURATE AIRSPEED, BUT NO AIRSPEED TAPE. REJECTED TAKEOFF AT 95 KNOTS. FIRST OFFICERS PFD INDICATIONS ARE NORMAL. PURGED BOTH CAPTAIN`S & FIRST OFFICER`S PITOT, FOUND SOME SMALL FRAGMENTS OF DEBRIS IN BOTH LINES IAW MM 34-11-00-2. PRECAUTIONARY R & R NR 1 AIR DATA MODULE IAW MM 34-16-01-4 & R & R NR 1 ADIRU IAW MM 34-43-03-4. PERFORMED PITOT STATIC SYS LEAK TEST & AIR DATA ADJUSTMENT TEST IAW 34-16-00-5. ALL TESTS PASSED. ALSO CHECKED THE HUD WHILE PERFORMING TESTS & THE SPEED INFO WAS IN VIEW ON HUD DISPLAY. PERFORMED AUTO LAND SYS RETURN TO SERVICE TEST ON EACH FCC 1 & 2 AMM 22-00-00-5.

Part: SKIN — DAMAGED (LT WING) · airframe 57,150 hrs · 20,106 cycles

LEFT WING LIGHTNING STRIKE REPAIR, REF WRI 57-10/0236, WAS ACCOMPLISHED IAW EA 8-5700-T0324518 REV A, WHICH IS CLASSIFIED AS A MAJOR REPAIR. THIS REPAIR WILL REQUIRE AN RII BUYOFF FOR ALL REPAIR STEPS LISTED IN THE EA. COMPLIED WITH EA 8-5700-T0324518 A.

Part: BATTERY — LOW (CABIN) · airframe 56,588 hrs · 19,868 cycles

EMERGENCY LIGHT BATTERY 1 LOW. PERFORMED EMER LIGHT ADJUSTMENT TEST, PASSED IAW AMM 33-51-00-5.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 559 hrs · 19,591 cycles

AFTER LANDING WITH FIRM BRAKE APPLICATION AT APPROX 80KTS, ACFT SHUTTERED FOLLOWED BY UNSAFE GEAR INDICATION ON CTR GEAR & LOSS OF NR 1, 1 & 3 HYD SYS.

Part: FIRE BOTTLE — LOW PRESSURE (NR 1 NACELLE) · airframe 558 hrs · 19,524 cycles

ENGINE FIRE AGENT LOW ALERT ON DEU. TROUBLESHOT IAW FIM 26-21-00-2-0. FOUND NR 1 ENGINE FIRE BOTTLE 1 WITH LOW PRESSURE SWITCH BAD. R & R THE NR 1 ENGINE FIRE BOTTLE IAW AMM 26-21-01-4. OPS CHECKED GOOD IAW 26-21-01-5. ACFT OK FOR SERVICE.

Part: ACCESS PANEL — DAMAGED (LT HORIZ STAB) · airframe 557 hrs · 19,495 cycles

LEFT HORIZONTAL STAB INBD DETACHABLE ELEVATOR ACCESS PANEL 344AT DAMAGED. EXPOSED HONEYCOMB AT OTBD TE AREA. REPAIRED LT HORIZONTAL STATION INBD DETACHABLE ELEVATOR ACCESS PANEL 344AT IAW SRM 51-71-00 & PAINTED IAW SRM 51-21-02 VOL II.

Part: TEE FITTING — CRACKED (RT HORIZ STAB) · airframe 557 hrs · 19,495 cycles

RIGHT LE HORIZONTAL STAB MOST INBD SECTION HAS TWO CRACKS ON STIFFENERS. REMOVED CRACK FROM UPPER HORIZONTAL LE ALC7272-45 IAW SRM 55-00-01 FIG 1A. INSTALLED REPAIR ON LOWER TEE CHORD AT STATION XFS166 IAW EA 8-5510-T0315704.

Part: PANEL — DELAMINATED (LT HORIZ STAB) · airframe 557 hrs · 19,495 cycles

LEFT HORIZONTAL OTBD LOWER HINGE PANEL 334KB HAS DELAMINATION. REPAIRED DELAMINATED PANEL 334KB IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: COWLING — DELAMINATED (NR 2 ENGINE) · airframe 557 hrs · 19,495 cycles

NUMBER 2 ENG LT FAN COWL IS DELAMINATED AT UPPER FWD OUTER SURFACE. REPAIRED NR 2 ENG LT FAN COWL AT UPPER FWD OUTER SURFACE IAW SRM 51-71-00 VOL II, SRM 54-32-01 VOL III. PAINTED IAW SRM 51-21-02 VOL II.

Part: SKIN — CRACKED (LT WING) · airframe 557 hrs · 19,495 cycles

LEFT WING, FWD PANEL LAND IS CRACKED JUST INBD OF PANEL 526FB. FABRICATED REPAIR DOUBLER IAW SRM 57-10-11 VOL 1 FIG 49. INSTALLED FABRICATED REPAIR DOUBLER IAW SRM 57-10-00 VOL 1 FIG 49.

Part: SKIN — CORRODED (BS 1219) · airframe 557 hrs · 19,495 cycles

BS 1219, RBL 48 SKIN PANEL FWD OF CTR WING TANK HAS CORROSION. REPAIRED IAW EA 8-5710-T0315698.

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 557 hrs · 19,495 cycles

RIGHT HORIZONTAL STAB LE PANEL 341 EZ HAS TWO CRACKS ON BULKHEAD OPENING. REMOVED DAMAGED AREA, FABRICATED SPLICE DOUBLERS IAW DWG ALC7222. INSTALLED REPAIR DOUBLERS IAW EA 8-5510-T0315537.

Part: PANEL — CRACKED (ZONE 600) · airframe 557 hrs · 19,495 cycles

RIGHT WING, LOWER SURFACE PANEL LAND IS CRACKED AT AFT INBD OF SLAT TRACK NR 8. R & R THE PANEL IAW SRM 57-21-01 FIG 5 & 51-31-01.

Part: WIRE — DAMAGED (FUEL SYSTEM) · airframe 557 hrs · 19,495 cycles

WIRE NR M1103B20C DAMAGED, RT SIDE ABOVE AUX TANK. REMOVED AND REPLACED WIRE.

Part: LANDING — CRACKED (LE SLAT) · airframe 557 hrs · 19,495 cycles

RIGHT WING, SLAT TRACK NR 7 PANEL LAND CRACKED. R & R IAW SRM 57-00-01, 51-31-01, V2.

Part: SKIN — GOUGED (LE SLAT) · airframe 557 hrs · 19,495 cycles

RIGHT WING NR 5 SLAT HAS A GOUGE ON INNER SECTION OF SKIN. GOUGE IS OUT OF LIMITS. INSTALLED INNER DOUBLERS & FLUSH REPAIR IAW SRM 57-10-00 FIG 11 SH 1.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 54,947 hrs · 19,148 cycles

SMOKE CAME OUT OF OVERHEAD VENT AT REAR OF COCKPIT FOR APPROX 5 SECONDS. JUST TURNED UP COCKPIT & COURIER TEMPS FROM 67 TO 74 DEGREES. DONNED O2 MASKS & TURNED DOWN BOTH TEMPS TO 70 DEGREES. FIRST SMELLED SOMETHING HOT & THAT PROMPTED US TO TURN AROUND. THE SMOKE NEVER CAME FWD TO OUR SEATS & IT WENT AWAY AFTER APPROX 10 SECONDS. RAN NR 1 & 3 PACKS FOR 20 MINUTES & DID NOT NOTICE ANY ODOR OR SMOKE. ALL TEMPS WERE IN LIMITS & CHANGED NR 1 & 3 COALESCER BAGS IAW MM 21-54-03-2. OK FOR SERVICE.

Part: ADIRU — INOPERATIVE (NR 2) · airframe 54,248 hrs · 18,846 cycles

DURING CRUISE, IAS MISCOMPARE ALERT CAME ON BOTH CAP & FO`S PFD. AIRSPEED MISCOMPARE STARTED AT 4 KTS THEN WENT TO APPROX 50 KTS MISCOMPARE BETWEEN BOTH PFD'S, FOLLOWED BY AUTO THROTTLES DISENGAGED, AUTOPILOT DISENGAGED & FLIGHT DIRECTOR DISAPPEARED. ALTITUDE MISCOMPARE BY 450', SEL ELEV FEEL MAN, SEL FLAP LIM OVERRIDE. AFTER TROUBLESHOOTING SYS IAW QRH, DECIDED THAT CADC 2 WAS BAD & USED QRH TO TRANSFER BOTH DISPLAYS TO CADC 1, FD1 & AP2. ALL SYS ON CADC 1 CAME BACK, NO ASSOCIATED PROBLEMS. INSPECTED ALL PITOT & STATIC PORTS. NO BLOCKAGE FOUND. CHECKED & ENSURED ALL AIR DATA MODULE CONNECTIONS WERE SECURED IAW AMM 34-16-01-4. REPLACED NR 2 ADIRU IAW AMM 34-43-03-4, CHECKED SATISFACTORY.

Part: DUCT — BLOWN (BLEED AIR) · airframe 52,569 hrs · 18,126 cycles

AT FL330, LEVEL 2 "AIR SYS NR 1 PRESSURE LOW". SYS SHOWED 11 PSI W/BLEED NR 1 ON. PRESSURE WAS 42 WITH 1-2 ISOL ON. PERFORMED T/S IAW FIM 36-10-32 INTERROGATE CFDS PSC NR 1 FAULT REVIEW AND CURRENT FAULT FOUND PREVIOUS LEGS FAN AIR VALVE TORQUE MOTOR OPEN. CIRCUIT FAULT. DURING ENGINE NR 1 FAN AIR VALVE INSPECTION, FOUND DUCT FLEXIBLE ASSY BLOWN AT FLANGE WELDING PIPE AND DAMAGED FAN AIR VALVE HARNESS BETWEEN ENG NR 1 FIREWALL P1-8028 TO P1-8094 "M1-41" ENG NR 1 FAN AIR VALVE. CARRIED OUT SEVERAL ENGINE VISUAL INSPECTION, NO OTHER DAMAGE FOUND.

Part: LAMP — INOPERATIVE (ESCAPE SLIDE) · airframe 52,235 hrs · 17,986 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WILL NOT TEST, LIGHT INOPERATIVE. REPLACED LAMPS, OPS CHECKED GOOD IAW STANDARD MX PRACTICE.

Part: BATTERY — OVERHEATED (MASTER) · airframe 51,882 hrs · 17,848 cycles

ON INSPECTION OF CAC, FOUND BATTERY SMOKING, OVERHEATED, REMOVED BATTERYS, RINSED AFFECTED AREAS WITH DISTILLED WATER. DRIED, RINSE FLUID AS REQUIRED. VISUAL INSPECTION REVEALED NO DAMAGE. CLEANED IAW THE AMM 24-31-11-04. OK TO CONTINUE.

Part: HINGE — BROKEN (FLAP PANEL) · airframe 51,846 hrs · 17,832 cycles

DISCOVERED DROP PANEL OTBD OF CENTER FLAP FAIRING MISSING. HINGE THAT ATTACHES TO BOTTOM OF WING AND PANEL IS BROKEN AT EVERY LOBE. INSTALLED DOOR PANEL IAW EA 8-5720-164721. ACFT OK FOR SERVICE.

Part: SWITCH — FAILED (E/E BAY DOOR) · airframe 51,842 hrs · 17,831 cycles

AFTER TAKEOFF, MASTER CAUTION ILLUMINATED, WITH LEVEL 1 AVNCS EXT ACC DR ALERT. MISC PAGE WAS CHECKED BEFORE T/O. ALERT WAS NOT DISPLAYED. REMOVED, REPLACED AVIONICS DOOR CLOSE SWITCH IAW MM 52-41-02-2. OP'S CHECK GOOD. FINAL CLOSED.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,777 hrs · 17,804 cycles

DURING GROUND OPS, AFTER SELECTING PACK ONE AND 3 ON (WITH APU RUNNING), COCKPIT FILLED WITH THE ODOR OF RAW JET FUEL. NOT THE ODOR OF JET EXHAUST. PACKS WERE TURNED OFF AND COCKPIT WAS VENTILATED. FOUND APU LEAKING FUEL INTO APU INLET. SHUTDOWN APU AND CONNECTED HUFFER, ODOR WENT AWAY. PACK SYS OPS CHECKS NORMAL.

Part: TERMINAL — BURNED (ZONE 500) · airframe 51,626 hrs · 17,747 cycles

TANK 2L AFT PUMP LO LEVEL 1 ALERT IN CRUISE FLIGHT. COMPLIED WITH LEVL 1 QRH CHECKLIST FUEL PUMP TNK 2, LT C/B (G-17) WAS POPPED BY FUEL PUMP. IN ADDITION, THERE WAS A SIGNIFICANT EVIDENCE OF FLAME/SMOKE/HEAT EXPOSURE TO TERMINAL STRIP S3-372 AND SEVERAL INCHES OF ALL 6 WIRES TERMINATED AT THIS LOCATION. THE 6 WIRES WERE THE 3 PHASES THAT POWERED TANK 2L AFT FUEL PUMP. THE TERMINAL STRIP IS MOUNTED ON THE LEFT WING AFT SPAR CLOSE TO THE PUMP RESET C/B RAN RTS ALL TEST PASSED, DUE TO HISTORY NEED MORE T/S TANK 2L PUMP C/B POPPED. NO REPORTED FAULTS IN MCDU. RESET BREAKER AND PERFORMED FSC R-T-S REF MD-10-30 AMM 28-00-00-5,TEST PASSED. RAN PUMPS IN MANUAL AND COULD NOT DUPLICATE C/B TO TRIP. SUSPECT WIRING ISSUE. ITEM HAS A LONG HISTORY OF C/B POPPED. PULLED AND COLLARED B1-680, OPENED LOWER WING PANEL UNDER NR 2L AFT PUMP, FOUND WIRES AT TERMINAL STRIP S3-372 SHORTED/BURNED REF WDM CH 28-22-02, PG5 SHT 2. STILL EVALUATING THE EXTENT OF DAMAGE AND REPAIR OPTIONS. REPLACED TERMINAL STRIP AT S3-372 THAT WAS BURNED. REF SRM 51-31-01, VOL 2. AVIONICS STILL NEEDS TO TERMINATE WIRING AND OPS CHECK SYS. INSPECTED WIRES, DAMAGED PORTION OF WIRES WAS REMOVED.

Part: PROXIMITY SWITCH — FAILED (SLAT SYSTEM) · airframe 51,190 hrs · 17,570 cycles

AFTER TAKE OFF AND RAISING SLATS, RECEIVED A SLAT DISAGREE LIGHT, SLATS OUT LIGHT WENT OUT, RAN QRH, RETURNED TO DEPARTURE AND LANDED OVERWEIGHT UNEVENTFULLY. INSTALLED PSEU IAW MM 31-71-01-2. COMPLIED WITH RTS OF PSEU IAW MM 31-71-01. RTS PASSED CYCLED FLAPS/SLAT THREW FULL RANGES NO PROBLEMS NOTED OK.

Part: WIRE — DAMAGED (MLG) · airframe 50,361 hrs · 17,246 cycles

LEFT MLG UNSAFE INDICATION. BOTH SYNOPTIC AND PRIMARY AURAL WARNING "LANDING GEAR" CONTINOUS. ALTERNATE GEAR HANDLE REMAINS UP. CENTER GEAR IS STOWED. REPAIRED WIRES TO ELECTRICAL CONNECTOR R5-246 IAW WDM 32-61-11. WIRES CHECKED GOOD. FOUND LT GEAR TARGET ASSY MISSING. REPLACED LT MAIN DOWN LOCK TARGET IAW MM 32-13-01-2. PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST REF 32-30-00-5. ALL INDICATION NORMAL IAW MM 32-60-00-5.

Part: SKIN — MISREPAIRED (RT ELEVATOR) · airframe 49,408 hrs · 16,881 cycles

RT INBD ELEVATOR UPPER SKIN EXISTING REPAIR NOT IN COMPLIANCE IAW ENGINEERING AND WITH SRM. REMOVED DAMAGE PER SRM 51-10-00, FABRICATED REPAIR SKIN. INSTALLED REPAIR IAW SRM 55-10-00, 51-31-01 AND 51-21-02 .

Part: SKIN — DENTED (NR 8 SLAT) · airframe 49,408 hrs · 16,881 cycles

LT WING NR 8 SLAT L/E HAS SEVERAL DENTS. FABRICATED REPAIR PARTS, UPPER AND LOWER DOUBLER, SPLICE PLATE, BAFFLES, UPPER AND LOWER SEAL, AND FILLER. INSTALLED REPAIR PARTS IAW SRM 57-10-00 VOL VI FIG 11. CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1781) · airframe 49,408 hrs · 16,881 cycles

CTR CARGO COMPT BS 1781 FLOORBEAM UPPER CHORD AFT FLANGE LOWER SURFACE CORRODED RBL 26-31. REMOVED FLOORBEAM AND ROLLER TRAYS TO GAIN ACCESS TO DAMAGED AREAS IAW SRM 57-31-01 VII. CLEANED UP CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-21-01 VII. AND 53-00-01 VI. FABRICATED REPAIR PARTS ANGLES AND FILLER IAW SRM 53-00-01 FIG 7 DETAIL 1 VI. TREATED AND PRIMED IAW SRM 51-21-01 V II. REINSTALLED STRUCTURE PREVIOUSLY REMOVED FOR ACCESS IAW SRM 51-31-01 VII.

Part: SEAT TRACK — CORRODED (BS 430) · airframe 49,408 hrs · 16,881 cycles

COURIER AREA SEAT TRACK LBL 8, STA 430 HAS CORROSION. BLENDED CORRSION IAW SRM 51-21-01. ORIGINAL MAT. THICKNESS .090", BLENDED .065". MAT REMAINING .025. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG. 5. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01. CLASSFIED AS A MAJOR REPAIR.

Part: SKIN — CRACKED (BS 500 S37L) · airframe 49,408 hrs · 16,881 cycles

LEFT STA 500, STR 37L, EXTERNAL FUSELAGE HAS DOUBLER NOT IAW SRM OR APPROVED DATA. COMPLIED, REPAIRED IAW EA 8-5330-152407, DATED 6-29-11. LEAK CHECKED IAW AMM21-00-01-5-0, NO LEAKS NOTED.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 49,112 hrs · 16,767 cycles

REJECTED T/O 18R, ENG FAIL LIGHT ON BETWEEN 80 & 90KTS. REJECTED BY 100 KTS. TO GW 377,000. N1 NR2 MORE THAN 11 PERCENT HIGHER THAN NR 3. IAW JRH DECREASED PART POWER TRIM SCREW ON NR 2 ENGINE APPROX .6250 TURN, COUNTERCLOCK WISE DIRECTION JRH SECTION 7, CLOSED AND SECURED NR 2 COWLINGS AND WORK PLATFORM IAW MM 71-10-00, OK FOR SERVICE. CLOSED AND SECURED NR2 ENGINE COWLS AND WORK PLATFORM IAW MM 71-10-00, OK FOR SERVICE.

Part: ACCUMULATOR — LEAKING (HYD SYSTEM) · airframe 47,664 hrs · 16,202 cycles

AT FL 340 LOST HYD SYST 3. COMPLIED WITH QRH. UNEVENTFUL LANDING, LEAK ENDED UP COMING FROM THE UPPER BRAKE PRESSURE ACCUMULATOR IN RT WHEELWELL. REMOVED AND REPLACED PER MM 32-44-01-2. LEAK AND OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 47,651 hrs · 16,196 cycles

DURING TAKEOFF ROLL, WITH AUTOTHROTTLES ENGAGED AT 85 TO 90 KTS A LEVEL 1 ENG 3 EXCEDEANCES ANNUNCIATED. ABORTED TAKEOFF. COMPLIED WITH QRH. N2 NR 3, 109.6 INSPECTED ENGINE EXHAUST FOUND NO PARTICLES PRESENT. NR3 ENGINE, N2 EXCEEDANCE 109.6 REQUIRES BORESCOPE INSP WITHIN 10 CYCLES. INSPECTED NR3 ENGINE EXHAUST AND FOUND NO PARTICLES PRESENT AT THIS TIME. IAW MM 72-00-00-6 1. ACFT WILL NEED BORESCOPE WITHIN 10 CYCLES. BORESCOPED NR 3 ENGINE STAGES 1 & 12 OF HPC AND HPT. NO DAMAGE NOTED. OK TO CLOSE PLUGS. REINSTALLED BORESCOPE PLUGS REF AMM 72-00-00-6-1. TERMINATING ACTION ACCOMPLISHED FOR 72-00-00-6 1 AT 47,650:35 H 16,196 C. COMPLIED WITH DYNAMIC RIG FOR NR 3 ENGINE PER EA 8-7200-142130, ADJUSTMENTS MADE WERE NOTED UNDER WRI 72-00/4385 FOR THE DYNAMIC RIG.

Part: FIRE WARNING — ILLUMINATED · airframe 46,263 hrs · 15,700 cycles

AFTER INS FOR ALIGN - 1 MIN GOT CARGO FIRE FLASHING - PUSHED BUTTON WITH ACW PHASE ONES. REMOVED LARGE(135 LB) CARGO FIRE EXTINGUISHER BOTTLE IAW MM 26-22-01-4 (3 EA) CIRCUIT BREAKERS PULLED AND COLLARED DISCHARGE CARTRIDGES AND DISCHARGE HEADS REMOVED IAW MM. INSTALLED LARGE(135 LB.) CARGO FIRE EXTINGUISHER BOTTLE IAW MM 26-22-01. C/W UP TO AND INCLUDING STEP 3J. STILL REQUIRES CLOSING OF 3 EA CIRCUIT BREAKERS, CONTINUITY TEST AND LOW PRESSURE TEST IAW MM 26-22-01.

Part: ACCESS PANEL — MISSING (CARGO DOOR) · airframe 41,386 hrs · 13,974 cycles

CTR CARGO DOOR ACCESS PANEL FOR VENT DOOR MISSING ON ARRIVAL INTO PDX. OIL: NO RESTRICTION LOWER CENTER CARGO DOOR VENT DOOR MISSING. (OK PER EA 8-5230-113246), (CK AFTER EA FLT) INSPECTED SCRATCH PER SMP 51-80-01 AND DOOR ALL WITHIN LIMITS. COMPLIED WITH PART 1 EA-8-5230-113246. INSTALLED PANEL PER MM. OPS CK OK.

Part: STRUT — DAMAGED (MLG) · airframe 36,264 hrs · 12,272 cycles

ON TAKEOFF FROM MEM, CENTER GEAR INDICATED UNSAFE UP. BOTH DISPLAYS SHOWED UNSAFE UP. COMPLIED WITH ALL CHECKLISTS AND LANDED KMEM 36C. REMOVED CENTER LANDING GEAR SHOCK STRUT, PER FEDEX WORK CARD 32T7101. REMOVED THE CTR LDG AFT W/W LT AND RT GEAR DOORS IN REF TO THE MD-10-30 M/M 32-14-04-2. CLG INST IS HANDLED ON WORKCARD 32T7701 AND IS C/W UP TO AND INCLUDING STEP 8J.COMPLETED FEDEX WORKCARD 32T7701 CENTER LANDING GEAR SHOCK STRUT INST.ALL STEPS COMPLETED ALL OPS CHECKS AND LEAK CHECKS O.K. PER WORKCARD.

Part: SILL — CRACKED (ZONE 600) · airframe 35,912 hrs · 12,115 cycles

FOUND CRACK IN RIGHT WING ISLAND SILL PART ARC7008-2.

Part: SELECTOR VALVE — LEAKING (LANDING GEAR) · airframe 35,596 hrs · 11,992 cycles

SHORTLY AFTER LEVEL OFF GOT LEVEL 1 ALERT HYD 3 ELEV OFF, NOTED THAT HYD 3 QUANTITY WAS DECREASING AT 2.5 GALS. HSC SHUTOFF NR 3 HYD. HYD 3 OFF LEVEL 1 ALERT. AFTER SLATS EXTENDED ON APPROACH, HYD 3 RESTORED. REMAINING FLUID LEAKED OUT, HYD 3 FAILED. GEAR EXTENDED MANUALLY. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE GEAR UP PRESSURE PORT O-RING, PER STD MAINT PRACTICE. NO LEAKS NOTED WITH GEAR HANDLE UP OR DOWN. SERVICED NR 3 HYD SYS TO 7.5 GALS. OK FOR SERVICE.

Part: BLANKET — BURNED (ZONE 100) · airframe 35,321 hrs · 11,892 cycles

IN CENTER ACCESSORY COMPARTMENT AT THE LT AND RT FUSELAGE FEED THROUGH FOR THE PNEUMATIC SUPPLY DUCTS 1-2 AND 1-3 HAVE FUSELAGE INSULATION BLANKETS SEVERELY BURNED AROUND THE DUCT. A/C FUSELAGE WAS INSTALLED WITH OLD TYPE OF INSULATION BLANKET. (P/N 3929452-2) BLANKET WAS NOT SECURED AND LAND ON TOP OF LT AND RT PNEUMATIC DUCTS LOCATED IN CAC AND CAUSED BLANKET TO BURN. CORRECTIVE ACTION: PNEUMATIC DUCTS FOR SYSTEM 1 AND 3 IN CAC INSPECTED FOR ANY KIND OF CRACK AND NO DEFECT IS NOTED. RECOVER DUCTS WITH HEAT RESISTANCE INSULATION BLANKET. OPS. AND LEAK CHECK GOOD PER CMM 20-20-01. EMP 435071, 224967, AND QA144239.

Part: REGULATOR VALVE — INOPERATIVE (TRIM AIR) · airframe 33,462 hrs · 11,184 cycles

SHORTLY AFTER TAKEOFF TRIM AIR OFF LIGHT ILLUMINATED COURIER SUPPLY TEMP INCREASED TO 215 DEG IT THEN DROPPED AND TRIM AIR OFF LIGHT EXTINGUISHED. SUPPLY TEMP ROSE AGAIN, CYCLED REPEATED MULTIPLE TIMES. RETURNED TO BASE. BOTH TRIM AIR PRESSURE REGULATOR VALVES INOP. TRIM AIR SWITCH MUST BE SELECTED.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 32,586 hrs · 10,849 cycles

AFTER TAKEOFF AT 1000 FEET AGL HAD RED MANIFOLD FAIL NR 2, RTB IN ACCORDANCE WITH QRH. RESET MANIFOLD FAILURE DETECTION LOOP NR 2 CIRCUIT BREAKER. PER SMP. PERFORMED AIR TEST, PASSES PER MM 36-23-01-5. RAN NR 2 ENGINE OP'S CHECK NORMAL 181623 PER JRH. REMOVED AND REPLACED NR 1 AVIONICS INTERFACE UNIT PRECAUTIONARY PER MM 31-43-02-4. PERFORMED AIR PREFLIGHT TEST SYSTEM CHECKS NORMAL JRH INTERIOR CHECK.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 32,442 hrs · 10,797 cycles

ON APP AT GEARDOWN 4 GREEN AND FLAPS 35 LVL 2 ALERT SLAT DISAG DURING GO-AROUND AT FLAPS 22 ALERT WENT OUT. CLEANED UP CONFIG AND RECYCLED GEAR AND FLAPS ON DOWNWIND. GEAR FLAPS AND SLATS ALL WORKED NORMAL. FLAPS 50 NORMAL LANDING. PERFORMED FCC RTS WITH NO FAULTS. ALSO, CHECKED FOR CURRENT /FAULT REVIEW IN ALL AIU'S PER FIM. A/C OK FOR SVC.

Part: SKIN — CRACKED (LE SLAT) · airframe 32,332 hrs · 10,735 cycles

COMPLY WITH E.A. 8-5722-70371, WINGS - REPAIR OF MINOR DAMAGE TO LEADING EDGE SLAT SKIN. ACT 07MAY03 06:26 BFM R COMPLIED WITH E/A 8-5755-70371 AT MAE/BFM.

Part: PROXIMITY SWITCH — FAULTY (LANDING GEAR) · airframe 31,122 hrs · 10,251 cycles

ON APPROACH, WHEN LANDING GEAR HANDLE MOVED TO EXTEND, RECEIVED ALL UNSAFE GEAR INDICATIONS ON BOTH LANDING GEAR INDICATORS AND CONFIG PAGE. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT AND TESTED GOOD IAW MD 10-30 AMM 31-71-01-2.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS)

NR 3 HYD QTY LEAK TO A QTY OF .2 GAL CAUSING LVL ALERT OF HYD 3 FAIL. ACCOMPLISH RED TABS INCLUDING ALT GEAR EXT. REMOVED AND REPLACED DAMAGED SECTION OF HYD LINE AND INSTALL NEW PIECE OF TUBING AND SWAGGED PER MM 20-10-01-2. LEAK CK GOOD. REINSTALLED PANELS AND SERVICED NR 3 HYD SYS.

Part: GCU — FAILED (NR 2 ENGINE)

AFTER T/O, NR 2 GEN OFF LIGHT ILLUMINATED FOLLOWED WITH FLAP DISAGREE FLG IN VIEW AND C/B POPS. ALSO, CAN'T PRESS A/C ON LANDING APPROX 1000 FT, NR 2 ISOL, LIGHT ILLUMINATED RED TAB. REMOVED AND REPLACED NR 2 GCU AND BCU PER M/M 24-21-01. GND OPS PER JRH 8-2. RAN ALL THREE ENGS PER JRH 5A.

Part: UPLATCH SENSOR — MALFUNCTION (LT MLG)

UPON GEAR RETRACT, MOMENTARY UNSAFE LEFT GEAR IND IAS 220. LIGHT CAME BACK ON AT TOD (FL190) AND REMAINED ON THROUGH DESCENT. CYCLED GEAR SEVERAL TIMES. LIGHT WILL COME ON WITH APPLICATION OF SPEED BRAKES DURING FLIGHT AS WELL. FOUND LOOSE TERMINAL AT TERMINAL STRIP S3-682 NR 5. TIGHTENED SAME. MX WAS ABLE TO FULLY DUP PROBLEM ON GRD THIS TIME BY MOVING NR 5 TERM AROUND. GEAR IND CKS GOOD ON GRD. JLB 168198 CKD MAIN GEAR DOOR LATCH MECHANISM ON LT MLG PER M/M 32-34-03-2 (CBS 95486) NO DEFECTS NOTED. (JOB PROGRESS STARTED). REMOVED AND REPLACED LT MLG UPLATCH SENSOR IAW M/M 32-61-03, OPS CKS GOOD UPON GEAR RETRACTION ON GND. MAINTENANCE CK FLT UNSAT, WAITING FOR MAXI UPDATE AFTER GOOD CHK FLT.

Part: PROX CNTRL — DIRTY (RT MLG)

WHEN GEAR WERE RAISED AT T/O, THE RT MAIN GEAR INDICATED UNSAFE UP AT BOTH THE FWD AND S/O PANEL RED TABS WERE COMPLETED. PROCEEDED TO DESTINATION AT MAX GEAR EST, SPEED (260 KIAS). DO NOT SUSPECT GEAR IS DOWN. NO CONTROL PROBLEMS. BOTH LIGHTS REMAINED ILLUMINATED ENTIRE FLIGHT TILL GEAR EXTENDED. GEAR INDICATION NORMAL AT GATE. CLEANED RT GEAR PROX SENSOR. REMOVED AND REPLACED GRD PROX CONTROL BOX PER M/M 32-61-03. OK TO CONTINUE. RAMPS CKS NORMAL. FOUND RT UPLOCK SENSOR ARM BINDING, ADJUSTED SENSOR PER M/M 32-61-02.

Part: PROX UNIT — MALFUNCTION (RT MLG)

AFTER T/O GEAR UP, RT MAIN RED LT ON FWD PANEL REMAINED ILLUMINATED. BOTH RED MAIN GEAR LIGHTS ON S/O'S PANEL REMAINED ON. RECYCLED ALL GEAR LIGHTS IN GREEN, GEAR UP SAME RESULTS, 1 RED FWD 2 RED AFT RAN RED TABS STAYED BELOW 260 KTS APPROX 10 MIN INTO FLT RT MAIN RED LT ON S/O'S PANEL WENT OUT APPROX 20 MIN INTO FLT RT MAIN LIGHT ON FWD PANEL WENT OUT LEFT MAIN RED LIGHT ON S/O'S PANEL REMAINED ON. REPLACED RT MAIN GEAR DOOR UP AND LATCHED SENSOR GEAR LIGHT CHECKED GOOD ON RETRACTION TEST. REPLACED PROXIMITY ELECTRONICS UNIT FOR LT GEAR LIGHT PROBLEM. EXTENDED AND RETRACTED GEAR SEVERAL TIMES, ALL LIGHTS CHECK NORMAL.

Part: PROX UNIT — MALFUNCTION (RT MLG)

AFTER T/O, LANDING GEAR HANDLE UP, BOTH RED LIGHTS FOR RIGHT GEAR ILLUMINATED. GEAR HANDLE DOWN, ALL GREEN LIGHTS WENT OUT FOLLOWED BY RT GEAR RED ON FWD PANEL. AFTER ABOUT ONE MIN LIGHT WENT OUT. COMPLIED WITH RED TAB PROCEDURES. *S/D* CK'D ALL SENSORS AND HARNESS, CK'D PROXIMITY ELECTRONICS UNIT HAD A LOGIC FAULT. REMOVED AND REPLACED PROX ELECTRONICS UNIT PER M/M 32-61-01, OPS CK NORMAL NO FAULTS.

Part: GEAR INDICATION — MALFUNCTION (RT MLG)

DEPARTING MEM RETRACTED LANDING GEAR, BOTH FRONT AND REAR PANELS SHOW A RED LIGHT ON RIGHT MAIN GEAR. COMPLIED WITH CHECKLIST. LIGHT WENT OUT PROCEED AT NORMAL SPEED. PERFORMED VISUAL INSPECTION OF RT MAIN LANDING GEAR SENSORS AND ASSOCIATED WIRING CONDUIT ALL APPEARS NORMAL. PERFORMED TEST WITH PROXIMITY ELECTRONICS UNIT ALL GEAR PROX SWITCHES AND LOGIC SYSTEM CK GOOD IAW M/M 32-61-01 PG 202, 203.