N307FE

Part: NONE — NONE (N/A) · airframe 77,898 hrs · 26,982 cycles

LPE ACTIVATED AFTER ROTATION, GO AROUND/TAIL STRIKE LANDING PERFORMANCE ENHANCEMENT FACT 25DEC21 01:19 YYZ U TAIL STRIKE PART A INSPECTION CARRIED OUT I.A.W AMM 05-51-12-6. NO DAMAGE NOTED .A/C OK FOR SERVICE. TALE STRIKE PART A INSPECTION CARRIED OUT I.A.W AMM 05-51-12-6. NO DAMAGE NOTED .A/C OK FOR SERVICE.

Part: PAINT — WORN (RT ELEVATOR) · airframe 77,588 hrs · 26,855 cycles

RH OB ELEVATOR BARE METAL AT LOWER SURFACE AFT OF ACTUATOR FOUND RH OB ELEVATOR LOWER SURFACE AFT OF INB ACTUATOR (PANEL 346BB) HAS MARKED MISSING PAINT, PREPPED AND PAINTED PER MD10-30 SRM 51-21-02 VOL 2 PARAGRAPH 2 STEPS A-J. PERFORMED WEIGHT AND BALANCE CALCULATION PER MD10-30 SRM 55-20-00 VOL 2 PARAGRAPH 2.B. STEPS (1)-(7).

Part: SKIN — DAMAGED (ZONE 600) · airframe 77,588 hrs · 26,855 cycles

NUMBER ONE R/H SLAT HAS SKIN DAMAGED FORWARD SIDE. REPAIRED DAMAGE IN REFERENCE TO MD-10-30 SRM 57-10-00 FIG 43 VOL 1

Part: PANEL — DAMAGED (LT WING TE FLAP) · airframe 77,588 hrs · 26,855 cycles

LEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPMISDRILLED HOLE AT I/B CORNER OF OUTBOARD END. REPAIRED PANEL PER E.A. 8-5710-T0364140(P1)- BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501 (MAJOR REPAIR)

Part: FLOORBOARD — DAMAGED (AFT CARGO) · airframe 77,588 hrs · 26,855 cycles

AFT CARGO COMPARTMENT FLOOR BOARD 187EF DAMAGED FABRICATED NEW FLOOR BOARD SRZAGA3876-3

Part: PANEL — DAMAGED (LT WING TE FLAP) · airframe 77,588 hrs · 26,855 cycles

LEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPS HAS MISDRILLED HOLES. REPAIRED PANEL PER E.A. 8-5710-T0364140 (P1)-BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501(MAJOR REPAIR)

Part: FLOORBOARD — DELAMINATED (N/A) · airframe 77,588 hrs · 26,855 cycles

DELAMINATED FABRICATE NEW AKC7082-3 FLOOR BOARD PER FEDEX DRAWING SRZ-25-005

Part: FLOORBOARD — DELAMINATED · airframe 77,588 hrs · 26,855 cycles

DELAMINATED FABRICATE NEW AKC 7082-19 FLOOR BOARD PER FEDEX DRAWING SRZ-25-005

Part: FLOOR SUPPORT — CORRODED (BS 1581) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK FLOORBOARD SUPPORT ANGLE STA. 1581 LBL=15 EXFOLIATED/CORRODED. REMOVED EXFOLIATED/CORRODED FLOOR SUPPORT ANGLE P/N AFA3853-15 AT STA 1581 LBL 15. FABRICATED , PROCESSED ,TREATED, PRIMED, AND INSTALLATED NEW FABRICATED FLOOR SUPPORT ANGLE. REF. DAC DWG AFA 3853, MD10-30 SRM 51-21-01 VOL 2, MD10-30 SRM 51-33-01 VOL 2.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK FLOOR PANEL SUPPORT ANGLE AT STA 1661 RBL 75 TO 107 CORRODED AROUND SEVERAL CLIPNUTS REMOVED AND REPLACE FLOOR SUPPORT REF DOUGLAS DRAWING AFA-3853.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK FLOORBOARD SUPPORT ANGLE STA. 1661 LBL=107.25 EXFOLIATED/CORRODED. (MRKD) REMOVED AND REPLACED WITH NEW FABRICATED FLOOR BOARD SUPPORT P/N AFA3853-501 REF DAC DWG AFA3853 AND SRM 51-33-01 VOL. 2

Part: FLOORBOARD — DELAMINATED · airframe 77,588 hrs · 26,855 cycles

DELAMINATED FABRICATED NEW ARC7082-55 FLOOR PANEL PER SRZ-25-005

Part: FLOORBEAM — CORRODED (BS 1901 RBL8-27) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK FLOOR SUPPORT ANGLE AT STA 1901 RBL 08 TO RBL 27 CORRORED MAIN DECK FLOOR SUPPORT ANGLE AT STA 1901 RBL 08 TO RBL 27 HAS BEEN REPAIRED PER DWG # AGA7559.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 77,588 hrs · 26,855 cycles

DELAMINATION ON AJC7001-149 STEP FABRICATED NEW AJC7001-149 STEP PER SRZ-25-005

Part: NONE — DAMAGED (ZONE 600) · airframe 77,588 hrs · 26,855 cycles

TEE FITTING HOLES DAMAGED. FABRICATE NEW FITTING PER DWG ARB3280 0000832258 : PUTZ, JARED J - 28-SEP-2021 16:44 FABRICATED TEE-TENSION BEVEL ARB3280-2 REF DWG ARB3280 0000097667 : SEVERJIN, DAVE H - 28-SEP-2021 17:59 C/W.

Part: SKIN — DENTED (CARGO DOOR) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO DOOR OPENING, FWD LOWER CORNER DAMAGE TO SKIN LAYERS (MARKED) 0003882689 : CARREDANO, CHRISTOPHER - 24-SEP-2021 00:24 REPAIRED MAIN CARGO DOOR CORNER REF MD10-30 SRM 53-50-00, VOL I, FIG 26, SHEET 6, PG 178, NOTES 1-14 0000858546 : KAYA, KEVIN P - 24-SEP-2021 00:35 MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO DECK STA.1437 DAMAGED FLOOR BOARD. ON PANEL DOOR #271GF (LH) AREA (MARKED) FABRICATED NEW FLOOR BOARD PANEL PER SRZ-25-005

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK CARGO STA. 1437 DAMAGED FLOOR BOARD. ON PANEL DOOR #271GF LH AREA (MARKED). FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRAWING SRZ-25-005

Part: ANGLE — CRACKED (ZONE 600) · airframe 77,588 hrs · 26,855 cycles

RIGHT WING SLAT #2 OUTBOARD END UNDER STAINLESS SEAL BY DLE HAS CRACKED L-ANGLE MARKED #1 REMOVED AND REPLACED CRACKED ANGLE ARB1647-6 IN REFERENCE TO DOUGLAS DRAWING ARB1647 AND MD-10-30 SRM 51-31-01 VOL2

Part: RUB STRIP — CRACKED (LT WING SLAT) · airframe 77,588 hrs · 26,855 cycles

LH WING: #1 SLAT UPPER SURFACE O/B - T/E RUBSTRIP UNDERSIDE CRACKED. (MRKD) REMOVED AND INSTALLED RUBSTRIP PER E.A 8-5750-T0363959, & REF MD10-30 SRM 51-35-01 VOL II, & REF DAC DWG NRB6224 REF. JPF ITEMS 2,3, AND 4

Part: FLOORBEAM — CRACKED (BS1199 LBL98-104) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1199 AT APPROX. X=98 TO X=104 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2

Part: FLOORBEAM — CRACKED (BS 1481 RBL10-16) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1481 AT APPROX. X=-10 TO X=-16 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2

Part: FLOORBEAM — CRACKED (BS 1461 LBL29-35) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1461 AT APPROX. X=29 TO X=35 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2

Part: FLOORBEAM — CORRODED (BS 1219 LBL89-10) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1219 AT APPROX. X=89 TO X=105 HAS CORROSION REMOVED CORRODED FLOOR BOARD SUPPORT AND FABRICATED NEW FLOOR BOARD SUPPORT P/N AEA0394-501 IAW DOUGLAS DRAWING AEA0394 USING S2929169 EXTRUSION MP5630208 AND INSTALLED REF SRM 51-33-01 VOL 2

Part: FLOORBEAM — CRACKED (BS 1441 LBL10-16) · airframe 77,588 hrs · 26,855 cycles

MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1441 AT APPROX. X=10 TO X=16 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2

Part: BEAM — CRACKED (BS 595 BLKHD) · airframe 77,588 hrs · 26,855 cycles

FOREWARD CARGO AT 595 BULKHEAD LOWER BEAM BEHIND NOSE GEAR P/N NCA6044-29 HAS 4 CRACKS VERIFIED AND MARKED. 0000911637 : STEPHENS, NATHAN M - 09-SEP-2021 19:14 STOP DRILLED ENDS OF CRACKS AND APPLIED DOUBLER REPAIR IAW SRM 53-40-00 V1 FIG36

Part: STIFFENER — CORRODED (ZONE 100) · airframe 77,588 hrs · 26,855 cycles

AFT CARGO COMPARTMENT R/H TUNNEL VERTICAL STIFFNER CORRODED UNDER NUT PLATE ON LOWER AREA AT STA 1841. (DOT 5) 0004092897 : REECE JR., RONALD S - 10-SEP-2021 17:49 WEB ASSEMBLY REPAIRED IAW SRM 53-00-01 GENERAL REPAIR #8 FIGURE 8 SHEETS 1-3 AND DRAWING AGA7171.

Part: FLOORBEAM — CRACKED (BS 1256 LBL 112) · airframe 77,588 hrs · 26,855 cycles

FUSELAGE MAINFRAME OVERWING FLOOR BEAM L/H SIDE AT STA 1256 LBL 112 IS CRACKED APPROX. ONE INCH IN LENGHT. (MKD) REPAIRED FUSELAGE MAINFRAME OVERWING FLOOR BEAM AT STA 1256 LBL112 REF BOEING SERVICE BULLETIN DC10-53-172 FIG 5, DWG SR10530081, EA 8-5310-T0363831 TITLED: FUSELAGE - MAINFRAME- CENTER FUSELAGE FLOOR SUPPORT INSTALLATION, STA 1256

Part: FITTING — CRACKED (BS 595 BULKHEAD) · airframe 77,588 hrs · 26,855 cycles

L/H STA. 595 BULKHEAD TEE CAP VERT LEG AT LONG 43L HAS A .700 IN. CRACK. (MARKED) INSTALLED REPAIR DOUBLERS PER EA8-5310-T0363663

Part: TEE FITTING — CRACKED (FWD CARGO) · airframe 77,588 hrs · 26,855 cycles

FWD CARGO, L/H SIDE "T" CAP CRACKED ON VERTICAL LEG, LOCATED BY STRINGER 45. CORRECTION: LOCATED BY STRINGER 39. INSTALLED REPAIR DOUBLERS PER EA. 8-5310-T0363663

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 77,588 hrs · 26,855 cycles

AFT WASTE COMPT: STA 1967 LBL 107.25 - SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION (VIEWED FROM LH SIDE AFT WASTE COMPT. LOOKING UP). REMOVED AND INSTALLED NEW SEAT TRACK EXTRUSION S4929148 REF SRM 53-70-00 VOL 1 FIG 16, SHEET 1, PG 59 PAR. 1C, SRM 57-70-00 VOL 1, FIG 11 PG 51, SRM 51-33-01 VOL 2, DAC DWG NFA6222 MAJOR REPAIR

Part: FLOORBEAM — CRACKED (BS 1275) · airframe 77,588 hrs · 26,855 cycles

MAIN CABIN OVERWING FLOOR BEAM, R/H SIDE, AT STA 1275 RBL 104, HAS A SEVERED BEAM. (MKD) INSTALLED NEW FABRICTED EXTRUSION SPLICE IAW SRM 51-38-01 PAR 4.D VOL 2 AND DWG VZZ7071(-1) SHEET 2 ZN17 VIEW G-G AND SRM 51-33-01 VOL.2

Part: SKIN — CRACKED (LT WING SLAT) · airframe 77,588 hrs · 26,855 cycles

LH LEADING EDGE, SLAT ANTI ICE TELESCOPING DUCT CUTOUT, PERFORMED NDT HFEC INSP PER NDTSPM PART 6. CRACK INDICATION AT UPPER INBD CORNER APPROX .250 IN LENGTH, MARKED DOT#39 AND RED GREASE PENCIL. NOTE: LOCATION IS CORNER #1 PER SEQ 1015, PG 22, FIG 2. REPAIRED LH LEADING EDGE SLAT ANTI ICE TELESCOPING DUCT CUTOUT AS REQ. PER. SRM 57-10-00 VOL 1 FIG IO3 SH.2-5

Part: DOUBLER — WORN (ZONE 100) · airframe 77,588 hrs · 26,855 cycles

AFT FUSELAGE; 311AB DOOR LAND WORN THRU SKIN @ LH AFT LATCH CONTACT POINT. DOT #11 REPAIRED PER EA 8-5330-T0364309.

Part: SEAT TRACK — WORN (BS 1029) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK: STA 1029 (R) X = -47.50 SEAT TRACK WORN BEYOND (GO-NOGO GAUGE)LIMITS. (MRKD) REMOVED AND REPLACED SEAT TRACK FROM STA 949-1030 RBL 47.50 MAIN DECK MPN S4929405-13500N MP3266343 REF SRM 53-70-00 FIG 1 VOL.1 AND SRM 51-31-01 VOL. 2 "MAJOR REPAIR"

Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 77,588 hrs · 26,855 cycles

MAIN DECK FLOOR PANEL DELAM. FROM STA 1561-1661.BETWN LBL 8.50-27.50 MARKED RED FABRICATED NEW FLOOR BOARD PER FDX DWG SRZ-25-005

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 77,588 hrs · 26,855 cycles

UPPER MAIN CARGO FLOORBOARD 282BF IS MISSING MULTIPLE INSERTS. STA 1561-1661 FABRICATED NEW FLOOR BOARD PER FEDEX DRAWING SRZ-25-005

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,157 hrs · 26,663 cycles

LH UPPER A/C PACK EXHAUST CUTOUT HAS SUSPECTED CRACK IN UPPER AFT CORNER THRU FASTENER HOLE. REPAIRED FUSELAGE SKIN PER MD10-30 SRM 53-50-00 FIG 3A

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 75,980 hrs · 26,070 cycles

DURING AN EMERGENCY LIGHTS TEST, FOUND THE EMERGENCY LIGHTS BATTERY 1 LOW. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01-4-1, AND OPS CHECKED OK. ACFT OK FOR SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,980 hrs · 26,070 cycles

DURING EMERGENCY LIGHTS TEST, FOUND THE BATTERY 1 LOW.

Part: VALVE — FAILED (FUEL SYSTEM) · airframe 75,848 hrs · 25,994 cycles

TNK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN #3 TANK. EMERGENCY DECLARED WITH ATC. IN REF TO FFC ERO 5200247 REMOVED REPLACED AND OPS CHECKED #3 MOTIVE SHUTOFF VALVE IRW FE MD10- 30 AMM 28-21-13-2 AND FE MD10-30 FIM 28-14-00-810-803. OPS CHECKS GOOD. MOTIVE VALVE PART NUMBER 19730-3 SN 0125. MOTIVE VALVE INSTALLED PN 19730-3 SN 4135. NOT TORQUE WRENCH REQUIRED FOR INSTALL. NO SIGNIFICANT TANK ENTRY REQUIRED. CONFIRMED MOTIVE SHUTOFF VALVE FAILED BY FFC CREW PRIOR TO INSTALL.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 75,848 hrs · 25,994 cycles

TANK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN NR 3 TANK. EMERGENCY DECLARED WITH ATC.

Part: FLOAT VALVE — MALFUNCTIONED (FUEL TANK) · airframe 75,782 hrs · 25,960 cycles

AT L/O , FL 360 GOT LVL 1 ALERT FOR " TNK 3 TIP TRAPPED" WITH APPX 8.0 K FUEL IN #3, MEANING WE ONLY HAD 8.0 - 5.8 = 2.2 IN NR 3 TANK , AND INSUFFICIENT FUEL TO MAKE DESTINATION , ALERT WENT AWAY AFTER 2 MIN BUT ON DESCENT, GOT TNK 3 FUEL QTY LO ALERT WITH 6.1 IN TNK 3. QRH SAYS INBD CMPTMT FUEL IS LESS THAN 3.5 K W/ABOUT 100 MILES TO GO DECLARED EMERGENCY AND LANDED, BLOCKED IN WITH 5.8 K IN NR 2. WHILE COMPLYING WITH TSI 28-41 7551 STEP 2 INSPECTION OF GRAVITY TRANSFER SYSTEM TUBING, FOUND BROKEN PRESSURE SENSE LINE ON TRANSFER FLOAT VALVE. REMOVED AND REPLACED TRANSFER FLOAT VALVE PRESSURE SENSE LINE IAW AMM 28-21-10-2. OPS CHECKED GOOD IAW FIM 28-14-00-2, TASK 28-14-00-810-803. ACFT OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (L1 DOOR) · airframe 75,489 hrs · 25,794 cycles

L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS NOT TESTING. REMOVED AND REPLACED REMOTE SLIDE PACK PRESSURE INDICATOR. OPERATIONAL CHECKS GOOD

Part: SPOILER SYS — MALFUNCTIONED · airframe 74,966 hrs · 25,530 cycles

PDIS 307 27-60 6896 28OCT19 PDX FACT U LOGPAGES:3144742 DURING DESCENT WHEN SPOILERS DEPLOYED THE AIRCRAFT HAD A SIGNIFICANT ROLL TO THE RIGHT. FACT 28OCT19 05:05 PDX U C/W FIM 27-60-09-00 . FULLY DEPLOYED SPOILERS AND INSPECTED SURFACES AND EACH SPOILER ACTUATOR, NO DEFECT NOTED. LUBED SPOILER ACTUATORS AND MECHANISM IAW AMM 12-24-08-3. PERFORMED OPERATIONAL CHACK OF THE SPOILER/SPEED BRAKE CONTROL IAW AMM 27-62-00. OPS CHECK NORMAL. COCKPIT INDICATION CORRESPONDS TO SPOILER MOVEMENT.

Part: SKIN — CHAFED (LT WING) · airframe 74,859 hrs · 25,466 cycles

LT WING FIXED L/E UPPER SKIN IS CHAFED UNDER SLAT #1 AND 2 JOINT. CHECK FIT / FAIR GAP CLEARANCE AFTER REPAIR. BLENDED AREA IAW SRM 57-00-01 FIG I. VOL I. REMAINING MAT ON LT WING FIXED L/E UPPER SKIN UNDER SLAT #1 AND 2 JOINT WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 FIG 1B. (VOL I). INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 15A SHEET 1 (VOL I). MAJOR REPAIR. PART MARKED REPAIRED DOUBLER IAW GMM 07-0-1000.

Part: ACCESS PANEL — CORRODED (FUEL TANK) · corrosion level 2 · airframe 74,859 hrs · 25,466 cycles

LWR AUX TANK REAR SPAR ACCESS WEB HAS CORROSION ON BOTH UPPER AND LOWER SURFACES. (PANEL RACK) REMOVED CORR IAW SRM 51-81-00 VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. SH 3 ORIG .190 AFTER REWORK .152 TR# 14401. FABRICATED WEB ON TR # T19/1436040, P/N FX-AYB7081. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,859 hrs · 25,466 cycles

CORROSION UNDER NUT PLATES AFT CARGO FLOOR SUPPORT STA 1907, END TO END. REMOVED & REPLACED NUT PLATES IAW SRM 51-31-01 VOL II, REMOVED CORROSION STA 1902 L- 40 TO R-40 IAW SRM 51-21-01 VOL I. CHECK LIMITS ORIG MAT. .063" MAT. LOSS .026": MAT REM .037", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 VOL I & DWG AGA 3850. TR NO 89336: STA. 1902 LBL 10, FABBED DOUBLER, FILLER & SHIM IAW SRM 53-00-01 VOL I. T19/1438498 IAW SRM 53-00-01 FIG 8 VOL 1: INSTALLED DOUBLER REP. FILLER & SHIM IAW SRM 51-31-01 VOL II. MAJOR REPAIR.

Part: FLOOR PANEL — CORRODED (MAIN DECK) · corrosion level 2 · airframe 74,859 hrs · 25,466 cycles

MAIN DECK FLOOR BOARD LH MOST OUTBD STA 1821-1841 IS CORRODED AND DELAMINATED. REMOVED AND REPLACED CORRODED AND DELAMINATED FLOOR PANEL AT LH SIDE OUTBD STA 1821 - 1841 IAW AMM 53-21-08-4. 100% MATERIAL LOSS ON FLOOR PANEL DUE TO CORROSION OUT OF LIMITS. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 1361-1521) · corrosion level 2 · airframe 74,859 hrs · 25,466 cycles

CORROSION AT CABIN SEAT TRACK FLANGE STA 1361-1521 RBL 76. REMOVED CORROSION FROM SEAT TRACK FLANGE STA 1361-1521 RBL 76 IAW SRM 53-70-00 FIG 5 VOL I. CHECKED LIMITS MINIMUM THICKNESS ALLOWABLE IS 0.060 AFTER REWORK MATERIAL REMAINING IS 0.043 FOUND OUT OF LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. REMOVED AND REPLACED SEAT TRACK BETWEEN STA 1351 TO 1531 RBL 76 IAW SRM 53-70-00 VOL I. MAJOR REPAIR

Part: DOUBLER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 74,859 hrs · 25,466 cycles

LH FWD CENTER CARGO DOOR HAS CORROSION UNDER AFT HINGE ASSY. REMOVED AND REPLACED WEB / DOUBLER IAW DWG ANB7384 AND MD10-30 SRM 51-31-01 VOL II PART . MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 989-1029) · corrosion level 2 · airframe 74,859 hrs · 25,466 cycles

MCD -X8.5 SEAT TRACK BTW STA. 999 -1019 HAS CORROSION. DOT #04573-10. REMOVED CORROSION AT -X8.5 SEAT TRACK UNDER SCALLOP BETWEEN STA. 999 & 1019, CHECKED LIMITS MAX MAT. LOSS IS 0.050" FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 VOL I. REMOVED & REPLACED SEAT TRACK SECTION AT STA 989- 1029, MAT. ID 60-4508 IAW SRM 53-70-00 FIG 1. VOL I. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 74,859 hrs · 25,466 cycles

CABIN LEFT MOST OUTBD FLOOR PANEL HAS HEAT DAMAGE STA 600-660. FABRICATED A NEW FLOOR PANEL IAW DWG ACA3206 AND SRZ- 25-005 MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 74,859 hrs · 25,466 cycles

MAIN DECK LH MOST OUTBD FLOOR PANEL HAS DAMAGE STA -775. FABRICATED FLOOR PANEL IAW DWG ADA8318 AND SRZ- 25-005. MAJOR REPAIR.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 74,552 hrs · 25,306 cycles

DURING DESCENT BELOW 17000 FEET WITH SPEEDBRAKES EXTENDED IN THE 2/3 OR FULL POSITION GOT A RED GEAR UNSAFE LIGHT ON RIGHT MAIN GEAR. ALSO GOT RED LIGHT DURING TURBULANCE WITH SPEEDBRAKE RETARDED. SAME INDICATION ON SYNOPTIC PAGE. NO CURRENT FAULTS ON PSEU. MLG UP/DOOR LATCHED. 04 FLIGHT LEGS OF SENSOR WITH MARGINAL RIGGING. LAST FLIGHT LEG ALSO SHOWED "R GEAR UP AND LATCHED A/B SENSOR DISAGREE" CODE 317074. REF WDM 32-61-03 AND 32-61-04, MEGGED FOR SHORTS TO GND AND TO EACH OTHER WIRING FROM D1-80 TO PSEU. NO FAULTS NOTED.REPLACED R GEAR UP AND LATCHED SENSOR D1-80 REF AMM 32-61-15-4. OPS CHECKED GOOD (GEAR SWING).

Part: CONNECTOR — LOOSE (EGT HARNESS) · airframe 72,992 hrs · 24,456 cycles

PRIOR TO DESCENT, THE NR 1 ENGINE GAUGE WENT BLANK, FOLLOWED BY YELLOW X. WITHIN 10 SECONDS IT CAME BACK ON SHOWING AN EXCEEDANCE OF 955 DEGREES. THEN THE EGT WENT BACK TO NORMAL. FOLLOWED QRH, PULLED THROTTLE TO IDLE. ABOUT TWO MINUTES LATER RECEIVED AN EGT HIGH ALERT, WITH HIGH FUEL FLOW BUMP, EGT WAS AT 1055 DEGREES, FUEL FLOW WENT TO NORMAL. PERFORMED A PRECAUTIONARY IN-FLIGHT SHUTDOWN OF THE NR 1 ENGINE. GAUGE WAS INTERMITTENT THE REMANDER OF FLIGHT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. VIA-1 ENGINE EXCEEDANCES PEAK WAS 1055. FOUND CONNECTOR AT PYLON JUNCTION BOX LOOSE. FOUND FWD EGT LEAD CONNECTOR LOOSE AT PYLON. COULD NOT FULLY TIGHTEN THE CONNECTOR. REMOVED FWD EGT LEAD IAW MM 77-21-02-2. INSPECTED ENGINE FOR INFLIGHT SHUTDOWN IAW MM 72-00-00-6-1. INSTALLED A NEW FWD EGT THERMOCOUPLE HARNESS IAW MM 77-21-02-2. PERFORMED A HIGH POWER ENGINE RUN IAW JRH. ALL PARAMETERS CHECKED GOOD. ACFT OKAY TO CONTINUE.

Part: PITOT TUBE — DAMAGED (FIRST OFFICER'S) · airframe 72,297 hrs · 24,125 cycles

UNRELIABLE AIRSPEED. FIRST OFFICER AIRSPEED GREATER THAN 20 KTS BELOW ACTUAL AIRSPEED. IAS ALERT DISPLAY AT APPROXIMATELY 16000 FT AFTER ENTERING ICING CONDITIONS. ALL OTHER ALERTS ASSOCIATED WITH AIRSPEED UNRELIABLE DISPLAYED FROM THEN ON. INSPECTED THE F/O PITOT PROBE AND FOUND LEADING EDGE DETERIORATED AND PITTED. WHILE REPLACING PITOT PROBE OBSERVED WATER ACCUMULATION IN THE PITOT PROBE AND DRAIN HOLES PLUGGED. PURGED THE PITOT LINE FROM ADM TO REMOVE ALL WATER. REMOVED AND REPLACED F/O'S PITOT PROBE. PERFORMED A LEAK CHECK AND OPS CHECK OF THE SYSTEM, OPS CHECKED GOOD IAW AMM 34-11-02-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,198 hrs · 24,075 cycles

CORROSION FOUND ON MAIN DECK FLOOR SUPPORT AT STA 1361, X = 84. REMOVED AND INSTALLED NEW SUPPORT ASSY REF SRM 51-33-00 VOL II.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 72,198 hrs · 24,075 cycles

LT INBD FLAP ENVELOPE, UPPER SKIN, RT CORNER HAS EDGE SEPARATION. REPAIRED IAW SRM 57-10-00 VOL I FIGURE 86 SHEET 1. CUT OUT DAMAGED SKIN PER SRM 57-10-00 FIG 86 SH 1 VOL I. FABRICATED NEW DOUBLER & SKIN SECTION IAW SRM 57-10-00 FIG 86 VOL I. INSTALLED NEW REPAIR SKIN DOUBLER IAW SRM 57-10-00 VOL I FIG 86.

Part: RUB STRIP — DEBONDED (TE FLAP) · airframe 72,198 hrs · 24,075 cycles

LT INBD FLAP, UPPER SKIN INBD RUB STRIP IS DISBONDED. REPAIRED IAW SRM 57-10-00 VOL I FIGURE 86 SHEET 1. REMOVED BONDED RUB STRIP. FABRICATED NEW SKIN AND DOUBLER IAW SRM 57-10-00 FIG 86 VOL I. INSTALLED NEW REPAIR SKIN DOUBLER IAW SRM 57-10-00 VOL I FIG 86.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,198 hrs · 24,075 cycles

AFT CARGO COMP STA 1841 BELLFRAME WEB LBL 22 HAS IMPACT DAMAGE AND CORROSION. THIS ALSO COVERS NR 394 REMOVED AND REPLACED WEB PER DWG NGA6324 AND SRM 53-16-01 FIG 14.

Part: PAN — CRACKED (RT MLG DOOR) · airframe 72,198 hrs · 24,075 cycles

CENTER LANDING GEAR RT FWD DOOR, INBD FWD LANDING PAN AREA IS CRACKED. REMOVED AND REPLACED DOOR PAN IAW DWG. SE10520012-4

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 72,198 hrs · 24,075 cycles

CENTER CARGO BILGE AREA STA 1735 CENTERLINE INTERIOR ABOVE VHF ANTENNA IT HAS DOME NUTS LOOSE AND CORROSION. REMOVED AND REPLACED VHF ANTENNA SUPPORT BRACKET PER DWG ACA3011-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,198 hrs · 24,075 cycles

MAIN CARGO COURIER AREA FLOOR SUPPORT P/N ABA7333-1 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT P/N ABA7333-1 PER DRAWING ABA 7333 AND NBA 6018.

Part: FRAME ANGLE — CRACKED (BS 2092) · airframe 72,198 hrs · 24,075 cycles

AFT FUSELAGE ZONE 312 UPPER FRAME ANGLE AT BS 2069 CRACKED AT THE SECOND FASTENER FROM THE RT SIDE. REPAIRED THE FRAME ANGLE IAW SRM 53-30-00, VOL I, PG 9, FIG 2. MAJOR REPAIR.

Part: CHANNEL — CHAFED (ZONE 300) · airframe 72,198 hrs · 24,075 cycles

LWR RT NR 2 ENG FAN COWL & IDG SHOW DEEP CHAFED IN STRUCTURE. TAPE/RED MARK REPAIRED AJC7415-6 CHAFED SECTION REF 55-00-01 FIG 7 SH 1-4 PG 25-28 VOL I.

Part: SKIN — DAMAGED (RUDDER) · airframe 72,198 hrs · 24,075 cycles

UPPER AFT RUDDER RT SIDE, UPPER AFT SECTION HAS MATERIAL LOSS EMANATING FROM PLUG FASTENER (POSSIBLE LIGHTNING STRIKE). INSTALLED REPAIR DOUBLER OVER DAMAGED AREA REF SRM 55-00-01 FIG 3 SHEET 2 VOL 1.

Part: FRAME ANGLE — CRACKED (BS 2046) · airframe 72,198 hrs · 24,075 cycles

AFT FUSELAGE VISIBLE IN ZONE 312, FRAME CENTER ANGLE IS CRACKED AT BS 2046, AT THE 12:00 POSITION. REPAIRED THE FRAME ANGLE IAW SRM 53-30-00, PG 9, FIG 2, VOL I. MAJOR REPAIR.

Part: FRAME ANGLE — CRACKED (BS 2092) · airframe 72,198 hrs · 24,075 cycles

AFT FUSELAGE VISIBLE IN ZONE 312, FRAME CENTER ANGLE IS CRACKED AT BS 2092 AT THE 12:00 POSITION. REPAIRED FRAME ANGLE IAW SRM 53-30-00, VOL I, PG 9, FIG 2. MAJOR REPAIR.

Part: DOUBLER — TORN (RUDDER) · airframe 72,198 hrs · 24,075 cycles

UPPER AFT RUDDER RT SIDE, TOP STATIC DISCHARGER WRAP AROUND BASE DOUBLER TORN. REPLACED TORN DOUBLER PER SRM 55-00-01 VOL 1 FIG 3 SHEET 2 PAGE 9 AND DRAWING AMC 7176.

Part: SUPPORT — CORRODED (BS 1967) · corrosion level 2 · airframe 72,198 hrs · 24,075 cycles

AFT FUSELAGE WASTE TANK COMPARTMENT, LT LOWER LINER SUPPORT AT BS 1967 IS CORRODED. REMOVED AND REPLACED THE SUPPORT IAW DRAWING AGA3228-3, INSTALLED IAW SRM 51-31-01, VOL 2.

Part: SPAR CAP — CRACKED (HORIZONAL STAB) · airframe 72,198 hrs · 24,075 cycles

RIGHT HORIZONTAL STAB UPPER, OUTER REAR SPAR CAP HAS A .75 IN CRACK FWD OF THE AFT BARREL NUT HOLE IN THE PREVIOUS BLEND OUT AREA. REPAIRED THE SPAR CAP IAW EA 8-5510-T0334969.

Part: SEAT TRACK — WORN (BS 1396) · airframe 72,198 hrs · 24,075 cycles

MAIN DECK SEAT TRACK AT BS 1396, LBL 8.5 FOUND WORN. REPLACED THE DAMAGED SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL I, SRM 51-31-01, VOL II, 7, AND DWG SR10-53-002. MAJOR REPAIR.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG DOOR) · airframe 71,541 hrs · 23,757 cycles

AFTER TAKEOFF ON GEAR RETRACTION, RECEIVED A RIGHT MAIN GEAR LIGHT INDICATING RED, AND CONFIGURATION CUE RIGHT MAIN GEAR INDICATED RED. FOLLOWED QRH, RECYCLED GEAR DOWN AND BACK UP, SAME INDICATIONS, RIGHT MAIN RED. RETURNED TO DEPARTURE, ALL GEAR INDICATIONS NORMAL FOR LANDING. FOUND DOOR PROXIMITY SENSOR GAP TOO CLOSE, ADJUSTED THE SENSOR GAP IAW MM 32-34-03-2. SWUNG GEAR SEVERAL TIMES, INDICATION CHECKS GOOD.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 71,344 hrs · 23,667 cycles

FUMES WITH APU AIR SUPPLY TO ALL THREE PACKS. VISUALLY CHECKED THE APU BAY, NO FUEL LEAK NOTED. OPERATED ALL THREE PACKS FOR ABOUT HALF AN HOUR, NO FUMES OR FUEL ODOR NOTED IN COCKPIT. ACFT OK FOR SERVICE IAW AMM 21-53-00.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 71,269 hrs · 23,633 cycles

IN FLIGHT SELECT PACK 2 ON & SMOKE COME IN THE COCKPIT. REMOVED AND REPLACED THE COALESCER BAG IAW 21-54-05-2. RAN ALL THREE PACKS WITH APU AS WELL AS NR 2 ENGINE. NO SMOKE IN COCKPIT NOTED. OPS CHECKED GOOD IAW AMM 21-00-00-0.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 70,155 hrs · 23,149 cycles

ERRONEOUS TAKEOFF WARNING, STABILIZER, OCCURRED AT 80 KNOTS, REJECTED TAKEOFF. HAD A GREEN TAKEOFF BOX IN THE EAD. TAKEOFF CONFIG PROPERLY SET FLAPS 10.5, STAB 3.9, FLEX 58, GROSS WEIGHT 450,000 LBS. HIGH PEAK TIRE TEMP 417 DEGREES. RAN CHECKLIST & TOOK OFF 45 MINUTES LATER WITH NO FURTHER PROBLEMS. CHECKED CFDU FOR FAULTS, NO RELATED FAULTS RECORDED. CHECKED STAB TRIM SYS IAW SPM & AMM 27-45-00-0-0, NO FAULTS FOUND. NO RELATED 99 DAY HISTORY. ITEM CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,009 hrs · 23,093 cycles

ON WALK AROUND FOUND CRACK ON AFT TOP CORNER OPENING OF NR 3 PACK DOOR. PERFORMED HFEC INSPECTION OF AREA THAT HAD DAMAGE. REMOVED IAW NTSPM 06-01.010, NO DEFECTS NOTED. DURING INSPECTION FOUND RIVET HOLE IN SKIN JUST BELOW DAMAGE CUT OUT AREA WITH A CRACK STARTING FROM THE RIVET HOLE & PROGRESSING TOWARDS THE SKIN EDGE. HFEC PERFORMED IAW NTSPM 06-10-01.001, DEFECT NOTED. THIS IS A MAJOR REPAIR. REPAIRED IAW EA 8-5300-T0325121.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 69,840 hrs · 23,029 cycles

ON WALK AROUND, FOUND L1 EVACUATION SLIDE PRESS TO TEST LIGHT INOPERATIVE. RELAMPED L1 EVACUATION SLIDE PRESS TO TEST LIGHT IAW SWPM 20-00-00. NO BROKEN WIRES OR OTHER DAMAGE FOUND. TESTED OK FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 69,653 hrs · 22,961 cycles

AFTER ENG START & ADVANCING THROTTLES FOR INITIAL TAXI, WE EXPERIENCED A VERY STRONG FUEL ODOR. ACCOMPLISHED STEP 5 OF TSI PACK BURN OUT REF AMM 21-53-00-7. RAN ENGINES REF JRH AND TAXIED A/C FOR HIGH POWER RUN WITH ALL BLEEDS AND PACKS ON. NO FUEL SMELL WAS NOTED. DURING HIGH POWER RUN, PRESSURIZED A/C TO 4 PSI DP AND ALSO NO FUEL SMELL NOTED A/C OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 69,634 hrs · 22,953 cycles

HAD THE ODOR OF FUEL IN THE COCKPIT DURING PREFLIGHT WITH AP & PACKS RUNNING. THE ODOR WENT AWAY, AND TOOK OFF. PASSING ABOUT FL 230, THE ODOR CAME BACK WITH NO ASSOCIATED INDICATIONS, IT WENT AWAY. THEN PASSING FL 270 THE ODOR CAME BACK BUT STRONGER. CREW WENT ON O2 MASKS & RAN THE CHECKLIST & ODOR WAS CHECKED ABOUT 10,000 ON DESCENT & ODOR WAS GONE AGAIN. DIVERTED BACK, NO INCREASE OF OIL QTY WAS OBSERVED. R & R PACKS 1, 2 & 3 COALESCER BAGS IAW MM 21-54-03-2. RAN ALL 3 ENGINES AT PART POWER, WITH 1 PACK AT A TIME & THEN ALL 3 PACKS FOR APPROX 25 MIN, NO ODORS NOTED AT THIS TIME IAW MM 21-53-00-7.

Part: BATTERY PACK — INOPERATIVE (SLIDE LIGHT) · airframe 69,333 hrs · 22,818 cycles

L1 DOOR SLIDE PRESS LIGHT DOES NOT TEST. R & R REMOTE PRESS INDICATOR BATTERIES IAW FIM 25-61-00-2. PRESS TO TEST OPERATIONS CHECKED NORMAL. OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 69,048 hrs · 22,695 cycles

CREW REPORTS L1 DOOR SLIDE PRESS TO TEST LIGHT WILL NOT TEST. REPLACED REMOTE SLIDE PACK PRESS INDICATOR. SYS OPERATIONS CHECKED NORMAL.

Part: BRACKET — CORRODED (ZONE 100) · airframe 689 hrs · 22,638 cycles

RIGHT WW BRACKETS UNDERNEATH NR 1 HYD AUXILIARY PUMP ARE CORRODED. R & R BRACKETS IAW DWG ANB7189-23.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 689 hrs · 22,638 cycles

RIGHT HORIZONTAL STAB INBD LE SEGMENT, LOWER OTBD T CORD IS CRACKED. STOPPED DRILLED CRACKED & REPAIRED IAW EA 8 5510-T0320356.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 689 hrs · 22,638 cycles

RIGHT HORIZONTAL STAB INBD LE, OTBD FWD RIB IS CRACKED AT UPPER SECTION. REPAIRED RIB IAW SRM 51-31-01 VOL 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 689 hrs · 22,638 cycles

MAIN DECK STATION 1358, RBL 8, SEAT TRACK IS CORRODED THROUGH NUT CLIP HOLE. R & R DAMAGED SECTION OF SEAT TRACK.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 689 hrs · 22,638 cycles

RIGHT WING NR 1 SPOILER PANEL UPPER SKIN INBD SHOWS PREVIOUS REPAIR DOUBLER, DISBONDED & SEPARATED FROM SKIN. REPAIRED RT NR 1 SPOILER UPPER SKIN IAW SRM 51-71-00 VOL II.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 689 hrs · 22,638 cycles

MAIN DECK STATION 1370, RBL 8, SEAT TRACK LUGS OUT OF LIMITS. R & R DAMAGED SEAT TRACK.

Part: CHAIN — BROKEN (L1 DOOR) · airframe 689 hrs · 22,638 cycles

L1 DOOR AFT DRIVE CHAIN BROKEN. REPLACED L1 DOOR AIR MOTOR CHAIN PN SK11863-32 IAW DWG ABA 7941. L1 DOOR AIR MOTOR REPLACED IAW AMM 52-11902-2. L1 DOOR ELEC MOTOR CHAIN DRIVE SPROCKET BEARINGS PN B541DDFS428, TWO REPLACED IAW SOPM 20-10-7. L1 DOOR ELEC ACTUATOR SHAFT PN ABA 7939-501 REPLACED IAW DWG ABA-7941. L1 DOOR ELECTRIC ACTUATOR SHAFT SPACER PN ABA 8014-529 REPLACED IAW DWG ABA-7941. L1 DOOR MAIN DRIVE CHAIN PN SK11863-88 REPLACED IAW AMM 52-11-00-5. OPERATIONAL TEST OF EMER ACTUATION SYS PERFORMED IAW WC 52C1301, CHECKED GOOD.

Part: ACCESS DOOR — MISSING (CARGO DOOR) · airframe 680 hrs · 22,221 cycles

RIGHT LOWER CTR CARGO DOOR ACCESS DOOR 152RT MISSING ON ARRIVAL. FOR ACCESS TO UNLOCK DOOR. INSTALLED NEW ACCESS PANEL ASSEMBLY IAW SMP & AMM 52-32-00-0. OPERATION OF ACCESS PANEL CHECKED GOOD.

Part: BLADE — DAMAGED (NR 3 ENGINE) · airframe 67,884 hrs · 22,150 cycles

DURING BIRD STRIKE INSPECTION, FOUND FOUR FAN BLADES DAMAGED NR 3 ENG. REFERENCE WRI 05-50/1662 FOR PARTS IAW BIRD STRIKE CHECK IAW AMM 05-62-00-6 & AMM 72-00-00-6-1 K. INSPECTED NR 3 ENG CORE INLET FOR EVIDENCE OF FOD INGESTION. NO DEBRIS OR FOD NOTED AT CORE INLET & TURBINE BLADES CHECKED OK. R & R FOUR FAN BLADES & REPAIR T/R BLOCKER DOORS.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 66,655 hrs · 21,623 cycles

EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED. R & R BATTERY PACK IAW MM 33-51-01-4-1. OPS CHECKED NORMAL, OK FOR SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (MANIFOLD) · airframe 65,729 hrs · 21,224 cycles

RECEIVED LEVEL 3 AIR MAINIFOLD FAIL. ACCOMPLISHED CHECKLIST. NO FURTHER ACTION. ALERT EXTINGUISHED 30 MIN LATER. R & R NR 1 SYSTEM FAIL DETECTOR PRESSURE SWITCH IAW MM 36-23-03-4. PERFORMED ADJUSTMENT AND TEST PER MM 36-23-03-5. CHECKED GOOD, OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 65,291 hrs · 21,043 cycles

L1 DOOR SLIDE DEPLOYED INADVERTENTLY AFTER ACFT BLOCKING. R & R SLIDE.

Part: BATTERY — INOPERATIVE (SLIDE LIGHT) · airframe 63,796 hrs · 20,406 cycles

DOOR SLIDE PRESSURE LIGHT TEST INOPERATIVE. SECURED BASE OF LIGHT SOCKET AND REPLACED BATTERIES. OPS CHECK NORMAL. MM 25-61-03-5 & SMP. FINAL CLOSED.

Part: OVERRIDE SWITCH — INOPERATIVE (ENGINE IGNITION) · airframe 63,188 hrs · 20,184 cycles

DURING TEST FLIGHT AT FL250, SHUTDOWN NR 1 ENGINE AND ATTEMPTED MULTIPILE RESTARTS WHICH FAILED, DESCENDED TO 14,000 FT AND ATTEMPTED RESTARTS NOT AVAIL. RETURNED TO DEPARTURE WITH NR 1 ENGINE INOPERATIVE. FOUND ENGINE IGNITION OVERRIDE SWITCH INOP, REPLACED SWITCH S1-9170 IAW SWPM 20-20-02. ENGINE IGNITION AUDIBLE CHECKS GOOD IAW M/M 74-10-01-2.

Part: STOP FITTING — CRACKED (PAX DOOR) · airframe 63,183 hrs · 20,177 cycles

R3 DOOR FOUND FWD SIDE STOP FITTING NR 6 CRACKED. R & R R3 DOOR.

Part: BUSHING — DAMAGED (GENERATOR) · airframe 63,183 hrs · 20,177 cycles

FOUND APU GENERATOR INSTALLATION LOOSE DAMAGED BUSHING ON GENERATOR, DAMAGE TO BUSHING MOUNT ON GEAR BOX ASSY. INSTALLED NEW SERVICABLE APU IAW AMM49-04-01-2-0.

Part: FAIRING — MISSING (CARGO DOOR) · airframe 62,718 hrs · 19,988 cycles

ON ARRIVAL, FOUND THE FAIRING DOOR MISSING, ON THE CENTER CARGO DOOR, THAT COVERS THE VENT LATCH. FURTHER INSP OF DOOR REVEALED A GASH/HOLE APPROX 4-5" IN LENGTH. DOOR AND ASSOCIATED PARTS NOT STOCKED, WILL ORDER AOG. REPAIRING GASH/HOLE DAMAGE, MISSING DOOR IN FAIRING BY FILLING HOLE AND APPLING 3 LAYERS OF FIBERGLASS IN REF TO SRM 51-62-01, VOL II WAITING FOR REPAIR TO CURE/HARDEN. INSTALLED VENT DOOR ASSY REF CHAP 20 SMP AND IPC 53-53-09-01. DOOR OPS CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (BATTERY) · airframe 61,942 hrs · 19,713 cycles

EMERGENCY POWER TEST DID NOT PASS. R & R BATTERY CHARGER.

Part: VALVE — OUT OF ADJUST (NR 3 ENGINE) · airframe 59,818 hrs · 18,907 cycles

WITH MAX T/O POWER NR3 SLOW TO ACCELERATE. ENGAGED A/T AND 1 & 2 DROVE TO T/O SETTING, NR3 STOPPED .1875" SHY OF TARGET N1 WITH 1" KNOB SPLIT BETWEEN 1 & 2 MATCHED AND NR 3. ATTEMPTED MANUAL ADJUSTMENT OF NR 3 TO T/O SETTING. NR3 WAS AT MECHANICAL STOP, STILL .1875" SHY OF TARGET N1. ABORTED TAKEOFF, NR 3 ENG FAILED TO MAKE T/O POWER. FOUND NR 3 ENG VSV CABLE OUT OF RIG, ADJUSTED NR 3 ENG VSV CABLE IAE MD10-30 AMM 73-20-01-2. GROUND FLT IDLE ON NR 3 ENG CHECKED GOOD IAW JRH. DID MPA RUN ON NR 3 ENG IAW JRH OPS CHECK GOOD.

Part: BRAKE — FIRE (MLG) · airframe 59,639 hrs · 18,839 cycles

NORMAL LANDING WITH MEDIUM AUTOBRAKES. AFTER BLOCK IN, MECHANIC REPORTED A FIRE ON BRAKE NR 2. NEVER RECIEVED BRAKE OVERHEAT WARNING AND MAXIMUM BRAKE TEMP WAS 500 DEG C. AFTER BLOCK IN, NOTICED WHEEL ASSY NR 2 WAS SMOKING. WHEN APPROACHED FROM FAR NOTED FLAMES COMING FROM BRAKE BOTTOM REACHING THE TOP BRAKE CYLINDERS. USED DRY CHEMICAL POWDER FIRE EXTINGUISHER (MONO AMMONIA PHOSPHATE POWDER WITH NITROGEN) TO PUT FIRE OUT. WENT TO COCKPIT TO ADVISE FLT CREW. NOTED BRAKE NR 2 TEMP WAS 500 DEG C AND FALLING, USED AVIONICS COOLING UNIT TO COOL DOWN WHEEL & BRAKE ASSY, ALL OTHER BRAKE TEMPS WERE NOT ABOVE 270 DEG C WAITED 60 MINS TO APPROACH TIRES & BRAKES TO PERFORM HIGH ENERGY STOP INSP. INTERROGATED CFDS LAST FLT LEG FAULTS NO ASCU SHOWED, INTERROGATED ASCU NO FAULTS IN HISTORY NOR.

Part: BEAM — CRACKED (ZONE 200) · airframe 55,188 hrs · 17,300 cycles

WHILE PERFORMING J/C 8-2550-7-2354 PT 2 CTR CARGO HANDLING SYSTEM FOUND CRACK ON LOWER FLANGE OF BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 7 VOL I.

Part: SKIN — CRACKED (RUDDER) · airframe 55,188 hrs · 17,300 cycles

DURING RIGGING RUDDER MECHANICAL CTRL ACCIDENTAL DAMAGED ON LOWER AFT RUDDER LT SIDE. REPAIRED SKIN & PAINT AREA IAW SRM 55-10-00 FIG 2 VOL I & DWG D10-11-014.

Part: SKIN — LOOSE (ZONE 600) · airframe 55,188 hrs · 17,300 cycles

RT WING UPPER SURFACE FOUND 8 EA RIVETS LOOSE ON UPPER SKIN OF OUTBD AILERON. REPAIRED AREA IAW SRM 57-10-00 FIG 85 VOL I.

Part: SKIN — WORN (ZONE 600) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E EXT SURFACE FOUND WEAR ON SKIN. REPAIRED L/E WITH DOUBLER IAW SRM 57-10-00 FIG 40 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E INT ZONE FOUND CRACK ON RIB. REPAIRED RIB IAW SRM 57-00-01 FIG 10 VOL I.

Part: SKIN — LOOSE (T/E FLAP) · airframe 55,188 hrs · 17,300 cycles

LT WING OUTBD FLAP LWR SURFACE FOUND 100 LOOSE RIVETS ON SKIN. REPAIRED SKIN LOOSE FASTENERS IAW SRM 57-20-00 FIG 11 VOL I.

Part: SKIN — LOOSE (T/E FLAP) · airframe 55,188 hrs · 17,300 cycles

LT WING OUTBD FLAP UPPER SURFACE FOUND 120 LOOSE FASTENERS ON SKIN. REPAIRED SKIN LOOSE FASTENERS IAW SRM 57-20-00 FIG 11 VOL I.

Part: SKIN — WORN (ZONE 600) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E DROPPED (REMOVED PART) FOUND WEAR ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 39 SHT 2 VOL I.

Part: SKIN — WORN (ZONE 600) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E DROPPED (REMOVED PART) FOUND WEAR ON LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 39 SHT 2 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E INT ZONE FOUND CRACK ON RIB AND MISSING GANG CHANNEL ON RIB. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.

Part: DOUBLER — CRACKED (RT WING) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E INT ZONE FOUND CRACK ON UPPER DOUBLER. REPAIRED IAW SRM 57-10-00 FIG 71 VOL I.

Part: RIB — CRACKED (RT WING) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E INT ZONE FOUND CRACK ON RIB. REPAIRED FORMER IAW SRM 57-00-01 FIG 10 SHT 1 VOL I.

Part: SKIN — CRACKED (RT WING) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E EXT ZONE FOUND CRACKS ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.

Part: STIFFENER — WORN (FUSELAGE) · airframe 55,188 hrs · 17,300 cycles

DURING ACF MODIFICATION AS REQUIRE ON ACF J/C SP10240305-7003-5J, FOUND SEVERE WEARS ON VERTICAL STIFFENERS LT AIR COND COMPT. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 9 SHT 7 VOL I.

Part: SKIN — DENTED (T/E FLAP) · airframe 55,188 hrs · 17,300 cycles

LT WING INBD FLAP UPPER SURFACE FOUND 1 EA DENT ON SKIN. REPAIRED SKIN IAW SRM 51-10-00 PAR 2 VOL II.

Part: TEE FITTING — CRACKED (ZONE 500) · airframe 55,188 hrs · 17,300 cycles

RT WING INT ZONE L/E FOUND CRACK ON FIXED TEE CAP. REPAIRED TEE CAP IAW SRM 57-10-00 VOL I FIG 49.

Part: TEE FITTING — CRACKED (RT WING) · airframe 55,188 hrs · 17,300 cycles

RT WING L/E INT ZONE FOUND CRACK ON FIXED TEE CAP. REPAIRED TEE CAP IAW SRM 57-10-00 VOL I FIG 49.

Part: LUG — DAMAGED (NLG STEERING) · airframe 54,289 hrs · 16,922 cycles

PDIS: CAPT DOES NOT HAVE FULL NOSE WHEEL AUTHORITY TURNING TO THE RIGHT. RETURNED TO RAMP. FOUND NOSE WHEEL STEERING COLLAR RT LUG DAMAGED. REMOVED PISTON AND REMOVED AND REPLACED STEERING COLLAR. REPACKED PISTON AND REINSTALLED PISTON, REF DC-10-30MM 32-21-01-8. REMOVED AND REPLACED RT STEERING CYLINDER REF DC-10-30 MM 32-52-01-2. SERVICED NOSE GEAR STRUT REF DC-10-30 MM 32-21-01-9 2, LEAK CHECKS GOOD. COMPLETED OPS AND LK CK OF STEERING CYLINDER CK'S GOOD REF AMM DC10-32-52-01-2. COMPLETED STEERING CABLE ADJUSTMENT AND SAFETY. COMPLETED STEERING SYSTEM OPS CK, NOW CK'S GOOD WITH TILLER AND RUDDER.

Part: VALVE — MALFUNCTIONED (NR 1 ENG ANTIICE) · airframe 49,163 hrs · 14,935 cycles

ON CLIMBOUT, TURNED ON ANTI-ICE, NR 1 ENG ANTI-ICE DISAGREE LIGHT CAME ON. RAN RED TABS & NO HELP. DISAGREE LIGHT STAYED ON FOR ENTIRE FLT. FOUND SUPPLE DUCT TO ANTI-ICE VALVE BROKEN. REMOVED AND REPLACED NR 1 ENG ANTI-ICE VALVE AND DUCT ASSY REF-30-22-02-2, RAN NR 1 ENG REF-JRH AND ANTI-ICE VALVE CYCLES NORMAL.

Part: ENGINE — DAMAGED (NR 3) · airframe 42,506 hrs · 12,804 cycles

AT 31,000 FT ALT, JUST BEFORE DESCENT NR 3 ENGINE RUMBLED TWICE AND N1 STARTED TO DECREASE. RETARDED THROTTLE TO IDLE AND N1 WAS 38 PERCENT. ADVANCE THROTTLE NO MOVEMENT ON ENGINE WHEN PASSED THROUGH 10,000 FT. ENGINE RUMBLED AND CAME BACK TO NORM. REINSTALLED BORESCOPE PLUGS AND REMOVED TURNING TOOL AND REINSTALLED COVER PLATE. REMOVED AND REPLACED FUEL FLOW TRANSMITTER REF DC-10-30MM 73-31-02-2. LEAK AND OPS CHECKS GOOD ON ENGINE RUN. REMOVED AND REPLACED NR 3 ENGINE PER W/C71T0101-3. PERFORMED ENGINE VIB CHECK PER DC10-30 M/M 72-00-00-5. ENG CHECKED NORMAL PER M/M.

Part: CONTROL HANDLE — LACK OF LUBE (COCKPIT) · airframe 41,243 hrs · 12,408 cycles

WHEN GEAR HANDLE LOWERED FOR LAND AT BOTH PANELS IND. CLEANED AND LUBED GEAR HANDLE PER MM 32-31-02-7, 32-31-02-2. OPS CHECK NORMAL.

Part: PROXIMITY SWITCH — FAULTY (LANDING GEAR) · airframe 41,117 hrs · 12,366 cycles

AFTER LANDING GEAR HANDLE LOWERED HAD NORM GEAR EXT NOISES. REMOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT PER MM 32-61-01-2.

Part: SWITCH — FAILED (THROTTLE)

ON T/O AFT GEAR HANDLE RAISED. UNSAFE GEAR LIGHTS REMAIN ILLUM. REMOVED AND REPLACED S1-341 IN THE THROTTLE SWITCH ASSY NR 2 PER IAW 76-11-04-2 PG 201. OPS CK NORMAL.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 37,003 hrs · 11,178 cycles

UPPER CARGO COMP SEAT TRACK SUPPORT BEAM AT BS 919, 939, 959, 999 & 1019 FOUND TRACK ATTACH HOLES ELONGATED AFT SEAT TRACK REMOVED (LBL 47.5). *S/D* REMOVED AND REPLACED PER EA 8-5310-49609 THRU 49612.

Part: RIB — CRACKED (LE SLAT) · airframe 37,003 hrs · 11,178 cycles

LT WING NR 3 SLAT I/B RIB FOUND CRACKED, LENGTH 6 INCHES.

Part: FRAME — CORRODED (BS 1521)

MAIN CARGO DECK OVER MLG WHEEL WELL AREA, FUSELAGE FRAME AT BS 1521 HAS CORROSION. ** S/D ** REMOVED 3 FLOOR PNL FOR ACCESS TO CTR WHEEL WELL. REMOVED CORROSION, NDT CK HOLES AND THICKNESS. ALODINED AND PAINTED. INSTALLED FASTENERS PER 53-33-00. INSTALLED FLOORBOARDS IAW 53-21-08. LEAK CHECK OK.

Part: DRAIN LINE — OPEN (NR 2 ENGINE)

STA-BKK - IN CRUISE AT FL 330, 2.5 HOURS INTO FLIGHT NUMBER 2 ENGINE OIL PRESS COW LIGHT CAME ON AND OIL QUANTITY WENT TO 0 DID RED TABS PROCEDURE AND SHUT DOWN ENGINE. LANDED BKK WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE OIL MASTER CHIP DETECTOR, NO METAL FOUND. CAPPED OFF LEFT HYDRO PUMP SEAL DRAIN LINE.

Part: VENT DOOR — MISSING (CARGO DOOR)

ON POST FLT INSPECTION, FOUND CTR CARGO DOOR VENT DOOR ACCESS PANEL MISSING FROM CARGO DOOR FAIRING. MADE TEMPORARY REPAIR TO DOOR PER EA 8-5240-33866A TRANSFER TO OIL. REPLACED MISSING VENT DOOR ACCESS PANEL.

Part: WEB — CRACKED (NR 2 PYLON)

N00735 N00736, 2 PYLON AFT LOWER SUPPORT STRUCTURE HAS 3 CRACKED WEBS/STIFFENER, FWD OF THE AFT ENGINE MOUNT AND ABOVE THE AFT ELECTRICAL HARNESS QD, NON ROUTINE. *S/D* REMOVED SUPPORT CAGE, REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-00-01. INSTALLED SUPPORT CAGE PER SRM 53-00-01.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 COWL DUCT)

AFTER TAKEOFF, THE NR 2 ANTI-ICE COWL DUCT FAIL LIGHT ILLUMINATED. A NOTE IN THE MEL FOR THE ANTI-ICE WRITE-UP SAID TO REDUCE NR 2 THROTTLE TO IDLE AND USE ONLY IN EMERGENCY CONDITION. COMPLIED. LIGHT WENT OUT WHEN THROTTLE WAS RETARDED. LIGHT ON APPROXIMATELY 2 MINUTES. REF WRI 30-20/1976 FOR REMOVAL AND REPLACEMENT OF NR 2 ENGINE ANTI-ICE VALVE. NR 2 ENGINE RAN AT TAKEOFF POWER FOR 4 MINUTES PER J.R.H. A/I C.D. FAIL LIGHT REMAINED OUT. CKD NR 2 ANTI-ICE AIR OUTLET SCREEN, FOUND CLEAN. OK FOR SERVICE.

Part: CONTROL HANDLE — LACK OF LUBE (LANDING GEAR)

WHEN GEAR SELECTED DOWN BOTH PILOTS AND S/O PANEL IND FOUND RED LIGHTS. RAN RED TAB PROCEDURE, PER CHECKLIST WHEN ALTERNATE GEAR HANDLE RAISED, GOT FOUR GEAR DOWN GREEN LIGHTS BOTH PANELS. LANDED DOV WITHOUT INCIDENT. MX FOUND LANDING GEAR LEVER NOT RETRACTING CORRECTLY CAUSING SWITCH S1-431 ERRATIC OPERATION. MX CLEANED AND LUBED GEAR SELECTOR CONTROL HANDLE, OPS CHECKED OK.

Part: SELECTOR — MALFUNCTIONED (LANDING GEAR)

LANDING GEAR WON'T COME DOWN, CYCLED GEAR AND STILL NO GEAR DOWN. USED ALTERNATE GEAR HANDLE AND GEAR CAME DOWN AND LOCKED. PRESS OK, QTY OK. REPLACED CENTER GEAR CONTROL VALVE AS PER MM 32-31-04. REPLACED L/GEAR SELECTOR VALVE AS PER MM 32-31-03. PERFORMED EXTENSION AND RETRACTION OF GEAR AS PER MM 32-30-00, CHECKS NORMAL.

Part: CORNER — CRACKED (LT MLG DOOR)

LEFT MAIN LANDING GEAR DOOR - CRACKED AT FWD I/B CORNER. REMOVED AND REPLACED CORNER. REF: SRM 53-00-01.

Part: DOOR FRAME — CRACKED (LT CTR GEAR DOOR)

CENTER LANDING GEAR LT W/W DOOR CRACKED AT FWD I/B CORNER. REF N/R 7003. REMOVED CRACKED FRAME, INSTALLED NEW DOOR FRAME AND INSPECTION PLATES PER DOUGLAS SRM 51-00-00. REINSTALLED DOOR PER MM 32-14-03.

Part: FRAME — CRACKED (CTR GEAR DOOR)

CENTER LANDING GEAR RT W/W DOOR CRACKED AT FWD I/B CORNER REF N/R 7002. REMOVED CRACKED FRAME, INSTALLED NEW DOOR FRAME AND INSPECTION PLATES PER DOUGLAS SRM 51-00-00. RE-INSTALLED DOOR PER M/M 32-14-03 REF C-CK-05 N/R 7002.