N390FE

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD SYSTEM) · airframe 94,261 hrs · 40,419 cycles

PDIS 390 29-02 9785 03DEC19 DEN FACT U LOGPAGES:3149673 AT FL 340, RECEIVED LEVEL 1 "HYD 3 ELEV OFF". SWITCHED FROM AUTOPILOT 2 TO AUTOPILOT 1. RECEIVED SUBSEQUENT "HYD 3 QTY LO", ACCOMPANIED BY " HYD 3 FAIL". FACT 03DEC19 04:39 DEN U SERVICED #1 AND #3 HYD SYSTEMS REF AMM 12-13-02-3. BLED AIR FROM ALL HYDRAULIC SYSTEMS REF AMM 29-03-00-2. RAN ELEC AND ENGINE HYD PUMPS AND FOUND NO LEAKS. CHECKED TAIL CONE, AFT ACCESSORY COMPT, STAB COMP, CAC, CENTER WHEEL WELL AND BOTH MAIN WHEEL WELLS WITH NO LEAKS NOTED. RAN ALL FLIGHT CONTROLS WITH ELEC AND ENG PUMPS, NO LEAKS NOTED. EXERCISED NOSE WHEEL STEERING, NO LEAKS. RAN ALL 3 ENGINES REF JRH FOR 30 MINS WHILE MOVING FLIGHT CONTROLS. NO LEAKS NOTED. NO DROP IN HYDRAULIC QTY DURING APPROX 3 HOURS OF T/S. A/C OK FOR SERVICE

Part: PROXIMITY SENSOR — OUT OF ALIGNMENT (SLATS) · airframe 93,814 hrs · 40,133 cycles

ON FINAL APP. WITH FLAPS 22*, EXTENDED GEAR AND GOT SLAT DISAG ALERT. PREFORMED GO-AROUND AND RETRACTED GEAR & FLAPS ONLY TO 15*. WENT TO QRH FOR SLAT DISAG. DID FLAP 22* LANDING AND LEFT FLAPS & SLATS IN 22* POSITION ALL THE WAY TO SHUTDOWN. ALERT DID GO AWAY DURING GO AROUND WHEN FLAPS WENT TO 15%. FOUND L4A SENSOR IN PSEU READOUT IN NEED OF ADJUSTMENT, FOUND SLAT TRACK 10 FWD 4 SUPPORT BLOCKS WORN, R & R BLOCKS REF AMM 27-80-04-2, ADJUSTED L4A SENSOR REF 27-84-02-5, OPS CHECKS NORMAL

Part: PSEU — MALFUNCTIONED (N/A) · airframe 92,950 hrs · 39,588 cycles

PDIS 390 27-80 8566 25SEP18 MEM OPEN U "SLAT DISAG" LEVEL 2 ON APPROACH WHEN SELECTING FLAPS 35. NO ROLL NOTED. COMPLIED W/QRH LANDED WITH FLAPS 22/EXT. FACT 25SEP18 18:37 MEM REMOVED AND REPLACED PSEU RE 31-71-01-02. OPS CHECK GOOD OK FOR SERICE

Part: SHEAR TIE — CORRODED (BS 1987) · corrosion level 2 · airframe 92,874 hrs · 39,544 cycles

AFT CARGO BAY, BS 1987, JUST AFT OF THE SERVICE PANEL BETWEEN LONGERONS 51L & 51R CORRODED ON THE AFT SIDE OF FRAME ANGLE. REPAIRED THE SHEAR TIE IAW EA 8-5310-T0341752.

Part: TEE FITTING — CORRODED (RT MLG WW) · corrosion level 2 · airframe 92,874 hrs · 39,544 cycles

CENTER WHEEL WELL AT STA 1521, RT SIDE CORROSION FOUND ON THE UPPER TEE ANGLE. REPAIRED "T" ANGLE PER EA 8-5310-T0341578.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,874 hrs · 39,544 cycles

FWD CARGO COMPT DOOR SILL FWD FLOORBOARD SUPPORT CORRODED UNDER NUTPLATE AT STA 876. CLEANED CORROSION PER SRM 51-21-01 VOL 2.

Part: FLOOR PANEL — CORRODED (BS 495) · airframe 92,874 hrs · 39,544 cycles

MAIN DECK, BS 495 LEFT SIDE FLOOR PANEL UNDER RCB HAD EXTENSIVE EXFOLIATION CORROSON ON THE SURFACE. FABRICATED A NEW FLOOR PANEL IAW DWG WSP0791-1.

Part: SHEAR TIE — CORRODED (BS 1967) · airframe 92,874 hrs · 39,544 cycles

AFT CARGO BAY BILGE SHEAR TIE WAS FOUND CORRODED UNDER THE FRAME BS 1967, LONGERON 50R. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA0021-65.

Part: WEB — CRACKED (MLG WW) · airframe 92,874 hrs · 39,544 cycles

CENTER WHEEL WELL, HAS A CRACK ON RT UPPER SIDE WEB AT APROX STA 1501. INSTALLED REPAIR DOUBLER PER EA 8-5310-T0341389.

Part: FLOOR SUPPORT — CRACKED (BS 1501) · airframe 92,874 hrs · 39,544 cycles

FLOOR SUPPORT BRACKET WAS CRACKED, BS 1501, LONGERON 50R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01, VOL 2.

Part: FITTING — CORRODED (RT MLG TRUNNION) · corrosion level 3 · airframe 92,474 hrs · 39,291 cycles

RIGHT MLG TRUNNION FWD FITTING FWD BEARING INNER DIAMETER SURFACE HAS PITTED CORROSION. COMPLIED WITH EA 8-5740-T0338917 WINGS - ATTACH FITTINGS RT MLG FWD TRUNNION FITTING HOLE CORRODED STEPS 1-8 DATED MAR 20, 2018 MAJOR REPAIR.

Part: SWITCH — MALFUNCTIONED (SPOILER) · airframe 90,955 hrs · 38,367 cycles

UNCOMMANDED GROUND SPOILER DEPLOYMENT DURING TAKEOFF. CHECKED BOTH FCC 1&2 FOR CURRENT OR PREVIOUS FAULTS, NONE FOUND. PERFORMED AGS RTS IN BOTH FCC'S, CHECKED GOOD. INSPECTED AGS ARM SWITCH S1-845 IT APPEARS TO MOVE FREELY AND HAS GOOD AUDIBLE CLICKS. RAN SPOILERS THRU MANUALLY AND CHECK REJECTED TAKE OFF WITH THRUST REVERSERS DEPLOYED AND ALSO KNOCK DOWN CHECKED GOOD. NO DEFECTS FOUND. INSTALLED NEW SUBPEDESTAL THROTTLE SWITCHES. REF MD10-10 AMM76-11-04-2. LAND TEST PERFORMED ON WRI 22-10-6879. SPOILER QUADRANT LIGHT REINSTALLED OPS CK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 90,224 hrs · 37,990 cycles

RIGHT STA 595 BULKHEAD WEB LOWER FASTENER HOLE AT LONGERON 43R HAS A CRACK INDICATION. OPENED CRACK HOLE ON THE LOWER WEB TO .247 FOR NDT. PERFORMED OPEN HOLE HFEC. NO INDICATION FOUND IAW NDTSPM 93K0393. EA 8-5310-T0326599 FOR MORE INFORMATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 90,224 hrs · 37,990 cycles

RIGHT STA 595 FUSELAGE SKIN COMMON TO THE TEE CAP AT LONGERON 38R HAVE 2 EA. FASTENER HOLES WITH CRACK INDICATIONS. SAME HOLE LOCATIONS AS TEE CAP CRACK, OPENED FWD HOLE TO .247 AND AFT HOLE .262 AT LONGERON 38R ON THE FUSELAGE SKIN FOR NDT. PEFORMED OPEN HOLES HFEC. NO INDICATION FOUND IAW NDTSPM 93K0393. EA NR 8-5310-T0326599 FOR MORE INFORMATION.

Part: FRAME — CORRODED (BS 449) · airframe 90,224 hrs · 37,990 cycles

FWD AVIONICS AREA THROUGH OPENING IN NLG WHEEL WELL UNDER SYSTEM NR 1 RAM AIR DUCT, FRAME AT BS 449, LBL 30 HAS DAMAGE AND SIGNS OF CORROSION. REMOVED LIGHT CORROSION IAW SRM 51-21-01VOL 2.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,224 hrs · 37,990 cycles

CENTER CARGO COMPARTMENT, FWD BULKHEAD LOWER WEB HAS EXFOLIATION CORROSION AT 42R, STA 1521, FOUND UNDER ROLLER TRAY. MARKED, 2016-07-30. R & R SMALL SECTION OF ANGLE WITH PN S2929469, S2933839 & S4931827 IN REF TO SRM 53-00-01, FIG 9, VOL 1.

Part: SKIN — CRACKED (BS 535) · airframe 90,224 hrs · 37,990 cycles

NR 3 AIR CONDITIONING DOOR AFT UPPER CUT OUT CORNER HAS A .100 INCH CRACK. REPAIRED IAW SRM 53-50-00 FIG 3A VOL I.

Part: ANGLE — CORRODED (ZONE 100) · airframe 90,224 hrs · 37,990 cycles

CENTER CARGO COMPARTMENT, AFT BULKHEAD LOWER WEB CORRODED. FOUND AT BS 1781, UNDER THE AFT END OF THE ENTRY WAY OMNI ROLLER TRAY. REMOVED AND REPLACED CORRODED ANGULAR SUPPORT BRACKET IAW SRM VOLUME 2 51-31-01,V2.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 90,224 hrs · 37,990 cycles

RIGHT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A 1.75" CRACK AT LONGERON 39R, MARKED.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 90,224 hrs · 37,990 cycles

RIGHT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A 1.5" CRACK AT LONGERON 43R, MARKED.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 90,224 hrs · 37,990 cycles

RT STA 595 BULKHEAD TEE CAP HAS A CRACK BETWEEN LONGERON 37R AND 38R ON THE VERTICAL AND FORWARD HORIZONTAL LEG EXTENDING THROUGH THE RADIUS, MARKED.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 90,224 hrs · 37,990 cycles

RIGHT STA 595, BULKHEAD TEE CAP VERTICAL LEG HAS A 1.75" CRACK AT LONGERON 39R, MARKED.

Part: SWITCH — MALFUNCTIONED (BLEED AIR SYS) · airframe 892 hrs · 37,470 cycles

ON CLIMB OUT, SELECT ENG & WING ANTI-ICE ON, AS SOON AS WING ANTI-ICE SELECTED, GOT AIR SYS 3 OFF WITH BLEED AIR 3 VLV & PACK 3 BEING TURNED OFF AUTOMATICALLY. R & R NR 3 SYS MANIFOLD FAILURE DETECTION SWITCH IAW AMM.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 890 hrs · 37,391 cycles

SEAT TRACK LUG BROKEN, BETWEEN POS 2L & 3L LOCK ID IS Q758. REPAIRED DAMAGED SEAT TRACK IAW SRM 53-70-00 & SR 10-53-002. THIS IS A MAJOR REPAIR. REPLACED SEAT TRACK SEGMENT ONLY, PN 4929150-12000N. INSTALLED FLOORBOARDS & ROLLER SYS.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 886 hrs · 37,114 cycles

IN CRUISE AT FLIGHT 350, AIR SYS SMELLS LIKE A GYM ROOM OR DIRTY SOCKS. PERFORMED REPLACEMENT OF PACK SYS 1, 2, & 3 CONICAL COALESCER BAGS. ODOR CLEARED UP & PACKS OPERATIONS CHECK GOOD. ACFT GOOD FOR SERVICE.

Part: CABLE — FRAYED (L1 DOOR) · airframe 881 hrs · 36,871 cycles

DURING SERVICE CHECK, FOUND L1 DOOR AFT UPPER DRIVE CABLE FRAYED. R & R L1 DOOR AFT UPPER DRIVE CABLE. RIG & OPS CHECKED OK.

Part: DUMP VALVE — FAILED (FUEL SYSTEM) · airframe 87,541 hrs · 36,568 cycles

RIGHT WING DUMP VLV FAILED TO CLOSE AFTER DUMP TERMINATION. RIGHT FUEL DUMP VLV SYS WIRING CHECKED FROM RT FUEL DUMP VLV M1-89 TO FUEL SYS CONTROLLER. RT FUEL DUMP VLV TO FUEL SYS CONTROLLER, RT FUEL DUMP VLV TO 1, 2, 3 VIA CONTINUITY & INSULATION CHECKED NORMAL IAW WDM 28-31-02. R & R RT WING DUMP VLV. REMOVED AVIONIC COMPARTMENT LT SIDE COOLING RACK DUCT. INSTALLED AVIONICS COOLING DUCT IN FWD AV COMPARTMENT AS REQUIRED, OPERATIONS CHECK REQUIRED. R & R RT WING DUMP VLV. OPERATIONS CHECKED RT WING DUMP VLV IAW MM. DUMP VLV ACCESS PANEL INSTALLED & SEALED.

Part: DUCT — CRACKED (NR 2) · airframe 87,531 hrs · 36,560 cycles

NR 2 NOSE COWL INLET DUCT, CRACKED THROUGHOUT CIRCUMFERENCE. R & R WITH NEW NOSE COWL ASSEMBLY IAW AMM 54-22-01-2.

Part: SKIN — CRACKED (TE FLAP) · airframe 87,531 hrs · 36,560 cycles

LEFT OTBD FLAP UPPER SURFACE 2 CRACKS ON THE SKIN .120 TO .250 INCHES IN LENGTH APPROX XOF 560. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.

Part: FLOORBEAM — MECHANIC ERROR (FUSELAGE) · airframe 87,531 hrs · 36,560 cycles

AFT CARGO COMPARTMENT STATION 1868 LT X=36.00 FLOOR LINE, FLOORBEAM HAS MULTIPLE HOLES WITH UNACCEPTABLE SPACING BETWEEN HOLES. FABRICATED & INSTALLED REPAIR ANGLE IAW SRM 53-00-01 FIG 9 SHT 7.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,531 hrs · 36,560 cycles

MAIN DECK STATION 1390 LT 75.5 SEAT TRACK IS DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 87,531 hrs · 36,560 cycles

MAIN DECK SEAT TRACK AT STATION 1381 LT 75.5 IS DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: DOOR — CRACKED (LT MLG) · airframe 87,531 hrs · 36,560 cycles

LEFT MLG DOOR, CRACK EXISTS AT THE UPPER CTR HINGE PORTION OF THE DOOR. REMOVED DOOR AND REPLACED WITH NEW MLG DOOR IAW MM 32-14-01-2

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 86,501 hrs · 36,008 cycles

TWO INCH CRACK LT MLG WW INBD BULKHEAD 30 INCHES FWD OF AFT BULKHEAD AND THREE INCHES DOWN FROM UPPER BULKHEAD. MARKED CRACK END HFEC. REPAIRED DAMAGED AREA, CRACK, REF SRM 53-00-01.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 85,364 hrs · 35,350 cycles

RECEIVED LEVEL 1 "HYD 3 ELEV OFF" ALERT. NR 3 SYS INDICATED 4.4 GALLONS AND OVER A 10 MIN PERIOD DECREASED TO 4.0, DIVERTED. DURING GEAR EXTENSION, NR 3 QTY DECREASED TO 1.7 GALLONS WITH "HYD 3 QTY LO". AFTER LT TURN OFF RUNWAY, MX TOW IN. FOUND O-RING TO HYD PRESSURE TRANSDUCER IN RT WHEEL WELL AT NR 3 SYS MANIFOLD BLOWN OUT. R & R O-RING ON TRANSDUCER REF AMM 29-12-46-2 AND SERVICED HYD TO PROPER QTY REF AMM 12-13-02. PRESSURE AND LEAK CHECKS GOOD.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,054 hrs · 34,105 cycles

LT WHEEL WELL SLANT PANEL INBD VERTICAL "L" ANGLE IS CORRODED AT LWR EDGE. R & R "L" ANGLE, REF SRM 51-35-01.

Part: ANGLE — CORRODED (MLG WW BULKHEAD) · corrosion level 2 · airframe 83,054 hrs · 34,105 cycles

LT MAIN WHEEL WELL, FWD BULKHEAD, CORROSION LOCATED AT OTBD LOWER CORNER OF SLANT PANEL. R & R ANGLE. REF DWG NPB6072 AND DPS 4.708.

Part: PANEL — CORRODED (LT MLG WW) · corrosion level 2 · airframe 83,054 hrs · 34,105 cycles

LT WHEEL WELL SLANT PANEL HAS SURFACE CORROSION ALONG THE LOWER EDGE IN SEVERAL AREAS. R & R LOWER SECTION OF SEAL RETAINER, REF SRM 51-35-01 AND 51-33-01.

Part: WEB — CRACKED (ZONE 100) · airframe 83,054 hrs · 34,105 cycles

SEVERAL CRACKS FOUND AT STA 1406 IN LT WHEEL WELL ON THE UNDERWING BARREL KEEL STRUCTURE. REPAIRED WEB AT STA 1406 IN LT WHEEL WELL ON THE UNDERWING KEEL STRUCTURE IAW EA 8-5310-148486.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,054 hrs · 34,105 cycles

LT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR END. R & R VERTICAL TEE SECTION.

Part: ANGLE — CORRODED (MLG WW) · corrosion level 3 · airframe 83,054 hrs · 34,105 cycles

RT MAIN WHEEL WELL REAR SPAR CAP ANGLE (APB7080-2) HAS 2 CRACKS (2' CRACK INDICATION AFTER BLEND OUT) REMOVED AND INSTALLED REPAIR ANGLE. SRM 53-40-00, FIG 11.

Part: TEE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 83,054 hrs · 34,105 cycles

RT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR CORNER. REMOVED CORROSION. REF EA 8-5340-148481.

Part: FLOOR SUPPORT — CORRODED (BS 1801) · corrosion level 2 · airframe 82,577 hrs · 33,866 cycles

AFT CARGO COMPARTMENT BILGE STA 1801 BETWEEN LONGERON 51 RIGHT AND LONGERON 52 FLOOR SUPPORT FRAME CLIP FOUND CORROSION. NEW SHEAR CLIP FABRICATED AS PER DOUGLAS DRAWING AFA0053, REVISION N. CORRODED SHEAR CLIP AT AFT CARGO COMPARTMENT BILGE STA 1801 BETWEEN LONGERON 51 RIGHT AND LONGERON 52, FLOOR SUPPORT FRAME AREA REMOVED AND REPLACED AS PER SRM 51- 31-01, VOLUME II, REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.

Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 82,577 hrs · 33,866 cycles

FORWARD DOOR CUTOUT FUSELAGE JAMB AFT BETWEEN LONGERON 39 AND LONGERON 42 DOUBLER REPAIR FOUND WITH EDGE DAMAGED. R & R IAW SRM 53-50-00, FIG 26, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 51. FOUND WITHIN DAC DWG ARC0503, SHEET 2, REV BG LIMIT AND CMM 57-44-09, REV 51, TABLE 601 IN-SERVICE REWORK LIMIT. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-09, REV 51. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAPS) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SPAR CAP — DAMAGED (ZONE 600) · airframe 82,577 hrs · 33,866 cycles

DURING HFEC OPEN HOLE CARRY OUT FOUND 01EA DAMAGE HOLE ON RT WING XORS 345.750 REAR SPAR LOWER CAP AS MARKED. REPAIRED IAW EA 8-5710-143766, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT BEARING HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143446, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — WORN (RT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) BARREL NUT HOLE BUSHING FOUND WORN. REPAIR CARRIED OUT IAW EA 8-5750-143446, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) BARREL NUT HOLE / SURFACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143446, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SPAR CAP — CRACKED (RT WING) · airframe 82,577 hrs · 33,866 cycles

DURING HFEC OPEN HOLE CARRY OUT FOUND 2EA HOLES CRACK INDICATION ON RT WING XORS 345.750 REAR SPAR LOWER CAP AS MARKED. REPAIRED IAW EA 8-5710-143766, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. REPAIR CARRIED OUT IAW EA 8-5750-143445, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT FOUND INBOARD BUSHING WORN. REPAIR CARRIED OUT IAW EA 8-5750-143762, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT LOWER HOLE FOUND CORROSION AFTER BUSHING WAS REMOVED. REPAIR CARRIED OUT IAW EA 8-5750-143762, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — DAMAGED (RT WING) · airframe 82,577 hrs · 33,866 cycles

RIGHT WING - DURING REMOVAL OF FASTENERS FOR NDT INSPECTION AS PER E.O. 8-5710-7-5007 P2, FOUND 01 EACH FASTENER HOLE SIZE EXCEED HOLE SIZE LIMIT. REPAIRED IAW EA 8-5710-143766, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 82,577 hrs · 33,866 cycles

DURING HFEC OPEN HOLE INSPECTION CARRIED OUT , FOUND 02 EACH HOLES CRACK INDICATION ON THE RT WING XORS 345.750 REAR SPAR LOWER CAP. REPAIRED AS IAW EA 8-5710-143766, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT UPPER HOLE FOUND CORROSION AFTER BUSHING WAS REMOVED. REPAIR CARRIED OUT IAW EA 8-5750-143762, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. REWORK CARRIED OUT IAW EA 8-5750-143762, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

L/H WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FORWARD AND AFT FACE FOUND CORROSION. REWORKED CARRIED OUT IAW EA NR8-5750-143762, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143762, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 82,577 hrs · 33,866 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE FOUND CORROSION AFTER BUSHING WAS REMOVED. REPAIR CARRIED OUT IAW EA 8-5750-143445, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,577 hrs · 33,866 cycles

LT WING LEADING EDGE XOS 789, FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED. R & R IAW SRM 51-31-01, VOL II REV 96. NEW RIB DOUBLER FABRICATED AS IAW DWG ARB1249, REV AA. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — DELAMINATED (NR 4 SPOILER) · airframe 82,577 hrs · 33,866 cycles

LT WING, NR 4 SPOILER UPPER SKIN AREA FOUND DELAMINATION. REMOVED, REPLACED AND OPS CHECK CARRIED OUT IAW AMM 27-60-01-4, REV 10 FOUND SATISFACTORY. LT WING NR 4 SPOILER CLEARANCE CHECK CARRIED OUT IAW AMM 27-60-01-6 REV 10, FOUND SATISFACTORY.

Part: SKIN — CRACKED (LT WING) · airframe 82,577 hrs · 33,866 cycles

LT WING NR 4 SLAT, OUTBOARD SLAT TRACK CUTOUT FOUND CRACKED. TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 68, REV 96, VOLUME I. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (LT WING) · airframe 82,577 hrs · 33,866 cycles

LT WING - OUTBOARD OF PYLON, SLAT MECHANISM PANEL, INBOARD FORWARD CUTOUT FOUND CRACKED. TRIMMED AND REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 68, VOL I, REV 96. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 82,577 hrs · 33,866 cycles

RT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. CARRIED OUT IAW EA NR8-5710-143754, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 82,577 hrs · 33,866 cycles

LT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACK AT 2 LOCATIONS. TRIMMED AND REPAIR CARRIED OUT IAW EA 8-5710-143751, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 81,273 hrs · 33,208 cycles

AFTER T/O GR HNDL UP, BOTH LT MAIN GR INDICTATORS WERE RED. CHECKED VIEWING PORT AND DID NOT HAVE GOOD UPLOCK INDICATIONS. REMOVED AND REPLACED LT MLG UP AND LATCHED PROX SENSOR. AWAITING AVIONICS TO RUN WIRES. STILL NEEDS ADJ/TEST AND GEAR SWING DUE TO DICREPANCY. CONNECTED WIRES IAW REQUST ON LT MGD UP LATCH IAW SENSOR IAW AMM CH. 32-61-15-4 AND 32-61-15-5. CHECKS GOOD. CLEANED VISUAL WINDOW TO SEE UPLOCK. PERFORMED GEAR SWING. CHECKS GOOD. ALL INDICATIONS GOOD.

Part: SUPPORT BRACKET — CRACKED (HORIZONTAL STAB) · airframe 79,683 hrs · 32,434 cycles

LEFT HORIZONTAL STAB INBD L/E REMOVED SECTION, MOST INBD, HAS A CRACKED OTBD LOWER SUPPORT BRACKET. REMOVED TEE CAP IAW SRM 51-35-01. LOCATED, DRILLED & DEBURRED IAW DWG ALC 7273 ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED NEW TEE CAP IAW SRM 51-35-01 & EA 8-5510-123667.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 79,683 hrs · 32,434 cycles

PANEL NR 151ET SUPPORT CRACKED IN HALF, STA 1241, TOP OF LT WING. REMOVED CRACKED ANGLE IAW MD/DC 10 SRM 51-31-01 VOL II. MAT ID FOR ANGLE 7075-0 .063 PO NR 629531.1 AND FABRICATED IAW DAC DWG NR ANB 7051 REV C. ALODINED AND PRIMED IAW MD/DC 10 SRM 51-21-01 VOL II PG 21-24. INSTALLED IAW DAC DWG ANB7051 REV C AND MD/DC 10 SRM 51-31-01 VOL II.

Part: PANEL — WORN (ZONE 400) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON PANEL 487 ER IS WORN. NR 3 PYLON PANEL 487ER WAS WORN BEYOND ALLOWABLE LIMITS IAW SRM 54-00-01 VOL I PG 5. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 54-00-01 VOL I PG 11. ALODINED AND PRIMED DOUBLER AND FILLER IAW SRM 51-21-01 VOL II. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-31-01 VOL II.

Part: PANEL — CHAFED (ZONE 500) · airframe 79,683 hrs · 32,434 cycles

LEFT WING INBD L/E PANEL 516 HB IS CHAFED. BLENDED AREA IAW SRM 57-00-01 VOL I, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS, ORIG THICKNESS .090 BLEND LIMITS 20 PERCENT OR .072 WAS .067 IAW SRM 51-31- 01 VOL II FIG 1. FABRICATED DOUBLER IAW SRM 57-00-01 VOL I FIG 4 PG 12. ALODINED AND PRIMED IAW SRM 51-21-01 VOL II. INSTALLED DOUBLER IAW SRM 57-00-01 VOL I FIG 4 PG 12.

Part: PANEL — CHAFED (NR 3 PYLON) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON PANEL 487 EL IS CHAFED AT THE FWD END. BLENDED CHAFED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED IAW SRM 51-21-01. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-01.

Part: SKIN — DENTED (NR 2 NACELLE) · airframe 79,683 hrs · 32,434 cycles

NR 2 ENGINE FAN COWL EXTERIOR SURFACE DENTED APPROX 10 INCH FROM THE L/E; 3' FROM THE TOP. EVAULATED THE DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01. DENTED AREA IS DELAMINATED. REPAIRED DELAMINATED AREA BY REMOVING DAMAGE, FABRICATED DETAILS, PREPPED AND CLEANED FOR BOND, LAYED UP, VAC BAGGED CURED REPAIR, SANDED FLUSH, ALODINED, SEALED, PRIMED AND PAINTED REPAIR AREA IAW SRM 54-00-01, 51-71-00 AND SRM 54-32-01.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 79,683 hrs · 32,434 cycles

RIGHT HORIZONTAL STAB UPPER SURFACE HAS A DENT. CHECKED THE DEPTH OF THE DENT. FOUND TO BE 0.059 DEEP WITH NO CRACKS. DENT IS IN LIMITS PER SRM 51-80-01; PG 2; PARA 1; VOL II. ALODINED, PRIMED AND PAINTED PER SRM 51-21-01, PGS 21-24, VOL II AND SRM 51-21-02, PG 8, VOL II.

Part: PANEL — CHAFED (NR 1 NACELLE) · airframe 79,683 hrs · 32,434 cycles

NR 1 PYLON PANEL 437 FR IS CHAFED. BLENDED AREA IAW SRM 54-00-01. BOTH FOUND TO BE OUT OF LIMITS IAW 54-00-01 & DWG 7108. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-01 & 51-41-01.

Part: PANEL — CHAFED (NR 3 NACELLE) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON PANEL 488 GL IS CHAFED IN SEVERAL AREAS. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED REPAIR DOUBLERS IAW SRM 54-00-01. TREATED & PRIMED REPAIR DOUBLERS IAW SRM 51-21-01. INSTALLED REPAIR DOUBLERS IAW SRM 51-31-01.

Part: BLADE — DAMAGED (ZONE 400) · airframe 79,683 hrs · 32,434 cycles

NR 3 ENGINE S/N 451539 10TH STAGE COMPRESSOR BLADE T/E TIP AREA HAS A DING 0.036 INCH WITH 0.020 TEAR ON THE CONVEX SIDE. BLENDED BLADE TIP AND REMOVED THE DAMAGED AREAS AND PERFORMED AN INSPECTION TO ENSURE DEFECTS HAVE BEEN REMOVED IAW MD-10-10 AMM 72-36-00-2.

Part: FRAME — CRACKED (TAILCONE) · airframe 79,683 hrs · 32,434 cycles

TAIL CONE RIGHT FRAME HAS A CRACK WITH A PREVIOUS STOP DRILL HOLE AT STA 2199 AT THE UPPER LONGERON. FORMED ANGLE PER SRM 53-30-00. FABBED, LOCATED, & DRILLED HOLES PER SRM 53-30-00. ALODINED & PRIMED PER SRM 51-21-01. INSTALLED PER SRM 51-35-01.

Part: FRAME — GOUGED (TAIL CONE) · airframe 79,683 hrs · 32,434 cycles

TAIL CONE RIGHT UPPER FRAME IS GOUGED, 3 PLACES. REMOVED RIGHT UPPER SUPPORT PER DC/MD-10 SRM 51-35-01; VOL II. FABRICATED, LOCATED AND DRILLED HOLES PER DAC DWG AKC7068; REV "T". INSTALLED SUPPORT PER DC/MD-10 SRM 51-33-01; VOL II AND DC/MD-10 SRM 51-35-01, VOL II.

Part: FRAME — DAMAGED (ZONE 100) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR AREA AT STA 663.542, LONGERON 28, UPON SPOOL BACK UP FITTING REMOVAL, REPAIR BUSHINGS WERE FOUND IN FRAME P/N ACA 7230-6 AND ANGLE P/N ACA 7230-8. REPAIRED FRAME, ANGLE AND SHEAR TIE IAW FEDEX EA 8-5310-123514 TITLE "FUSELAGE STA 663.542 MCD SILL REAME OVERSIZE HOLES - REPAIR".

Part: BULKHEAD — CRACKED (NR 3 NACELLE) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON AFT MOUNT BY THE "V" BLOCK, THERE IS A SHEARED FASTENER AND LOOSE FASTENERS ALONG THE AFT ROW. REMOVED BOLTS IN REF TO DC/MD-10 SRM 51-31-01; VOL II. ACCOMPLISHED BHEC INSPECTION OF THE HOLES AFT ROW AT THE AFT MOUNT V-BLOCK IAW NDTSPM 60-10-01.003 USING TWS 8209A. CRACKS WERE INDICATED IN 4 HOLES. REAMED 4 HOLES, INDICATED HOLES IN REF TO DC/MD-10 SRM 54-20-00; FIG 27; VOL I. ACCOMPLISHED BHEC OF REAMED HOLES IAW NDTSPM 60-10-01.003 USING TOOL NR TWS 8209A; NO CRACK NOTED. INSTALLED BUSHINGS IN 4 HOLES IN REF TO DC/MD-10 SRM 54-20-00; PARA 2; VOL I. INSTALLED BOLTS IN ALL HOLES IN REF TO DAC DWG AUB 7025; REV "AS".

Part: SKIN — CHAFED (LT AILERON) · airframe 79,683 hrs · 32,434 cycles

LT WING INBD AILERON INBD LOWER NOSE PANEL IS CHAFED. BLENDED OUT DAMAGE. FOUND OUT OF LIMITS IAW SRM 57-00-01. FABRICATED NEW SKIN PANEL IAW IAW DWG ARC 1316. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-01. INSTALLED IAW DWG ARC 1316 & SRM 51-35-01. PART MARKED IAW GMM 7-0-1000.

Part: SHEAR TIE — CORRODED (BS 1501) · airframe 79,683 hrs · 32,434 cycles

THE CENTER LANDING GEAR SPACE, SHEAR TIE AT FRAME 1501, RIGHT SIDE IS CORRODED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED DAMAGED SHEAR TIE SECTION IAW SRM 53-30-00. FABBED SHEAR TIE & SPLICE IAW SRM 53-30-00 & DWG AEA 0273. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED SHEAR TIE & SPLICE IAW SRM 51-33-01.

Part: SKIN — CORRODED (BS 1501-1521) · airframe 79,683 hrs · 32,434 cycles

THE CENTER LANDING GEAR SPACE, BELLY SKIN, RIGHT SIDE FROM STA 1501 TO 1521 IS CORRODED. REMOVED CORROSION AND FOUND SKIN TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRED DAMAGED SKIN IAW EA 8-5330-123511.

Part: ATTACH FITTING — CORRODED (BS 1521) · airframe 79,683 hrs · 32,434 cycles

THE INTERCOSTAL ATTACH FITTING FWD OF BS 1521 IN THE RIGHT WHEEL WELL, OTBD SIDE IS CORRODED ON THE BACK SIDE. REMOVED ATTACH FITTING IAW SRM 51-35-01. REMOVED CORROSION IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. FABBED IAW DWG NEA 6081. ALODINED & PRIMIED IAW SRM 51-21-01. INSTALLED IAW SRM 51-33-01.

Part: SHEAR TIE — CORRODED (BS 1481) · airframe 79,683 hrs · 32,434 cycles

THE CENTER LANDING GEAR SPACE, RIGHT SIDE BELLY AT STA 1481, FROM SHEAR TIE IS CORRODED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED DAMAGED SHEAR TIE SECTION IAW SRM 53-30-00. FABBED SHEAR TIE & SPLICE IAW SRM 53-30-00 & DWG AEA 0273. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED SHEAR TIE & SPLICE IAW SRM 51-33-01.

Part: FITTING — CORRODED (BS 1501-1521) · airframe 79,683 hrs · 32,434 cycles

THE CENTER LANDING GEAR SPAC, LONGERON FITTING, RIGHT SIDE FROM STA 1501 TO 1521 IS CORRODED. REMOVED FITTINGS IAW SRM 51-33-01. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED CORROSION & FOUND OUT OF LIMITS IAW SRM 53-00-01. MACHINED FITTING IAW DWG AYB7020. REMOVED CORRODED SECTION, FABBED NEW LONGERON SECTION & REPAIR SPLICES IAW DWG AYB 7013 & SRM 53-00-01. INSTALLED LONGERON SECTION, REPAIR SPLICES & END FITTINGS IAW SRM 53-00-01 & 51-31-01.

Part: STRINGER — CRACKED (RT WING) · airframe 79,683 hrs · 32,434 cycles

RIGHT WING UPPER STRINGER 8 AT COMP PROBE LAND IS CRACKED. REPLACED COMP. PROBE DOUBLER IAW EA 8-5720-123508.

Part: FITTING — WORN (ZONE 200) · airframe 79,683 hrs · 32,434 cycles

MAIN CABIN RIGID BARRIER FITTING NR 7 IS WORN. REPLACED IAW EA 8-5340-123670.

Part: FITTING — WORN (ZONE 200) · airframe 79,683 hrs · 32,434 cycles

MAIN CABIN RIGID BARRIER FITTING NR 6 IS WORN. REPAIRED IAW EA 8-5340-123670.

Part: BRACKET — BROKEN (THRUST REVERSER) · airframe 79,683 hrs · 32,434 cycles

NR 1 ENGINE INBD T/R UPPER FWD STOP BRACKET IS BROKEN. REMOVED BUMPER & BRACKET IAW CF-6 ENGINE MANUAL 78-32-03; PG 409; 405. LOCATED & DRILLED UP BUMPER P/N 3111M84P001A & P/N 3110M30P001A IAW ENGINE MANUAL 78- 32-03; FIG 405; PG 409. INSTALLED BUMPER & BRACKET IAW ENGINE MANUAL 78-32- 03; FIG 405; PG 409.

Part: SEAT TRACK — GOUGED (BS 1239) · airframe 79,683 hrs · 32,434 cycles

MAIN CABIN SEAT TRACK, STA 1239; BUTT LINE, 48R "2" GOUGES. DAMAGE OUT OF LIMITS. REMOVED DAMAGED SECTION IAW SRM 53-70-00. FABRICATED REPAIR PARTS IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED REPAIR PART IAW SRM 53-70-00.

Part: SKIN — CHAFED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING, OUTBD LOWER L/E NOSE PANELS ARE CHAFED ON THE INBD EDGE FROM 34 INCHES OUTBD. FOUND OUT OF LIMITS. REMOVED PANEL IAW SRM 51-35-01 & SRM 51-33-01. FABRICATED A NEW PANEL IAW TPS 1003. LOCATED & DRILLED HOLES IAW DWG ARC 1109-37. ALODINED & PRIMED IAW SRM 51-21-01. PART MARKED IAW GMM 7-0-1000. INSTALLED IAW DWG ARC 1109 & SRM 51-35-01 & SRM 51-33-01. PAINTED IAW SRM 51-21-02.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 7 SPOOL BACK UP FITTING HOLES "A"; "B"; "C" AND "D" HAVE CRACK INDICATIONS. REPAIRED MAIN CARGO DOOR SPOOL FITTING IAW SRM 53-50-00.

Part: PANEL — CHAFED (RT WING TE FLAP) · airframe 79,683 hrs · 32,434 cycles

RIGHT WING INBD T/E FLAP PANEL 641 BR IS CHAFED. REPAIRED TWO AREAS OF CHAFING BY REMOVING DAMAGED AREAS & FABRICATING & BONDING A FILLER & DOUBLERS IAW SRM 51-71-00. REMOVED CAM LOCKS TO FACILITATE REPAIR & RE-INSTALLED IAW SRM 51-31-01. ALODINED, PRIMED, & SEALED THE REPAIRS IAW SRM 51-21-01 & 51-41-01.

Part: COWLING — GOUGED (NR 1 NACELLE) · airframe 79,683 hrs · 32,434 cycles

1 ENGINE INBD FAN COWL IS GOUGED ABOVE THE MID LATCH. CLEANED UP DAMAGE, CHECKED LIMITS, REQUIRES REPAIR. REMOVED SURFACE FINISH, FABBED DOUBLER, ALODINED & PRIMED AREA IAW SRM 51-71-00. SEALED DOUBLER EDGES BOND LINE IAW SRM 51-71-00.

Part: SUPPORT — CRACKED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING T/E VERTICAL ATTACH SUPPORT IS CRACKED AT THE UPPER PART OF FRAME 33, OUTBD OF THE INBD EDGE. REMOVED & REPLACED POST IAW DWG 3 ARC0295 & SRM 51-33-01.

Part: PANEL — CHAFED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING INBD LOWER T/E PANEL 541 KB IS CHAFED. REPAIRED PANEL BY BONDING A DOUBLER IAW SRM 51-71-00. REMOVED & RE-INSTALLED PANEL IAW SRM 51-31-01.

Part: FITTING — DAMAGED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 1 SPOOL BACK UP FITTING HOLES "A"; "B" AND "C" HAVE CRACK INDICATIONS.

Part: SKIN — DENTED (BS 690 S50) · airframe 79,683 hrs · 32,434 cycles

FOUND 2 DENTS ON THE LOWER FUSELAGE AT STA 690, STRINGER 50.

Part: PANEL — CHAFED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING INBD LOWER T/E PANEL 541 FB IS CHAFED. REPAIRED CHAFED AREAS BY BLENDING AND FOUND OUT IF LIMITS. FABRICATED REPAIR DOUBLER & BONDED IAW SRM 51-71-00, 51-21-01 & 51-31-01. ALODINED, PRIMED & SEALED IAW SRM 51-21-01. RE-INSTALLED HINGE REMOVED TO F.O.M. IAW SRM 51-31-01. REMOVED & RE-INSTALLED PANEL IAW SRM 51-31-01.

Part: ATTACH ANGLE — CRACKED (NR 3 PYLON) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON L/E HEAT EXCHANGER ACCESS AREA FWD ATTACH ANGLE IS CRACKED. REMOVED & INSTALLED PANEL IN REF TO SRM 51-31-01. REMOVED & INSTALLED ANGLE IN REF TO SRM 51-35-01. FABRICATED ANGLE IN REF SRM 51-21-01. PART MARKED FX AUB 7083-13 IN REF TO GMM 7-01000.

Part: CHANNEL — CRACKED (LT WING TE FLAP) · airframe 77,338 hrs · 28,921 cycles

LEFT WING INBD FLAP OUT HINGE AFT FAIRING STRUCTURE ATTACH CHANNEL IS CRACKED AT THE UPPER INBD BOLT. REMOVED CRACKED CHANNEL REF SRM 51-33-01. FORMED, LOCATED & DRILLED CHANNEL REF DWG ARC 2594 & SRM 51-33-01. ALODINED, PRIMED & APPLIED TOP COAT REF SRM 51-21-01. INSTALLED CHANNEL REF SRM 51-33-01. PART MARKED PER GMM 7-0-1001.

Part: SLAT TRACK — GOUGED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING NR 18 SLAT TRACK UPPER CLOSE OUT PANEL IS GOUGED. REMOVED AND INSTALLED DOOR ASSY IAW SRM 51-31-01. CLEANED, WELDED & INSPECTED REF. DPS 10.225. ALODINED & PRIMED IAW SRM 51-21-01.

Part: WEB — CRACKED (NR 3 PYLON) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON L/E WEB BETWEEN PANELS 487 DL AND 487 DR IS CRACKED. REMOVED & INSTALLED WEB IAW SRM 51-31-01, 51-33-01 & 51-35-01. CUT OUT DAMAGE, FABRICATED DOUBLER & INSTALLED DOUBLER IAW SRM 54-00-01. ALODINED & PRIMED IAW SRM 51-21-01.

Part: PANEL — CRACKED (THRUST REVERSER) · airframe 79,683 hrs · 32,434 cycles

NR 3 ENGINE RIGHT T/R UPPER HINGE CLOSE OUT PANEL IS CRACKED AT THE HINGE RELIEF. REPLACED DAMAGED HINGE ACCESS PANEL WITH A NEW PANEL IAW SRM 51-31-01.

Part: RIB — WORN (NR 3 PYLON) · airframe 79,683 hrs · 32,434 cycles

NR 3 PYLON PANEL 489 AL HAS A WORN RIB. REMOVED & REPLACED RIB IN REF TO DAC DWG AUB 7107; REV " P '.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 3 SPOOL BACK UP FITTING HOLES "A"; "C" AND "D" HAVE CRACK INDICATIONS. REPAIRED FITTING HOLES IAW SRM 53-50-00.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 5 SPOOL BACK UP FITTING HOLES "A" AND "C" HAVE CRACK INDICATIONS, BACK UP FITTING REQUIRES REPLACEMENT. WORK ACCOMPLISHED ON W/C E9-5230-7-5000. REPAIRED MCD. UPPER & LOWER BEAMS IAW SRM 53-50-00. REMOVED REPLACED FITTING IAW DWG NCA 6084 & SRM 51-33-01.

Part: BRACKET — CRACKED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING FUEL PRESSURE SWITCH BRACKET IS CRACKED INBD OF THE NR 15 SLAT TRACK. REMOVED CRACKED BRACKET IAW SRM 51-33-01. FORMED, LOCATED & DRILLED NEW BRACKET IAW DWG ARB 0177. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED BRACKET IAW DWG ARB 0177 & SRM 51-33-01. REMOVED & RE-INSTALLED LEFT PRECHECK VALVE REF AMM 28-21-17-2. LEAK CHECKED GOOD.

Part: BRACE — CRACKED (LT WING AILERON) · airframe 79,683 hrs · 32,434 cycles

LEFT WING INBD AILERON BAY, VERTICAL TEE BRACE LOCATED AT XW 373 AND 22 INCHES AFT OF THE REAR SPAR HAS A CRACK TO THE BOTTOM OF THE TEE ANGLE. REMOVED CRACKED TEE ANGLE IAW SRM 51-33-01. LOCATED & DRILLED HOLES IN NEW ANGLE & INSTALLED IAW DWG ARC 0472 & SRM 51-33-01.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 6 SPOOL BACK UP FITTING HOLES "B" AND "D" HAVE CRACK INDICATIONS. REPAIRED MAIN CARGO DOOR SPOOL BACK UP FITTING HOLES " B " & " D " IAW SRM 53-50-00.

Part: ATTACH ANGLE — CRACKED (LT WING TE FLAP) · airframe 79,683 hrs · 32,434 cycles

LEFT WING INBD FLAP OTBD HINGE FAIRING STRUCTURE, FWD ATTACH ANGLE IS CRACKED FROM THE BOLT HOLES RUNNING TO THE OUTER EDGE. REMOVED ATTACH ANGLE REF SRM 51-33-01. FORMED, LOCATED & DRILLED NEW ATTACH ANGLE REF DWG ARC 2568. ALODINED & PRIMED ANGLE REF SRM 51-21-01. INSTALLED ANGLE REF SRM 51-33-01. REMOVED TO F.O.M. & INSTALLED ACCESS PANEL REF SRM 51-31-01. PART MARKED IAW GMM 7-0-1001.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 4 SPOOL BACK UP FITTING HOLES "A" AND "C" HAVE CRACK INDICATIONS, BACK UP FITTING REQUIRES REPLACEMENT. REWORK OF BOLT BORES ACCOMPLISHED ON WC E9-5230-7-5000. REPAIRED MCD JAMB UPPER & LOWER BEAMS IAW SRM 53-50-00. REMOVED & REPLACED NR 4 SPOOL BACK UP FITTING IAW DWG NCA6084 & SRM 51-33-01.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 79,683 hrs · 32,434 cycles

LEFT WING OTBD FLAP, INBD HINGE, AFT LOWER FAIRING IS CRACKED. REMOVED PANEL 535 JL IAW SRM 51-31-01. PANEL 535JL WAS CRACKED; WELDED PANEL 535JL IAW RS DPS 10.301 & DWG ARC 2147; REV " M ". WELS WAS CHECKED IAW DWG ARC 2147; REV " M " & DPS 4.707, NO CRACKS NOTED. ALODINED & PRIMED IAW SRM 51-21-01. RE-INSTALLED PANEL 535 JL IAW SRM 51-31-01.

Part: PANEL — CHAFED (RT WING) · airframe 79,683 hrs · 32,434 cycles

RIGHT WING INBD LOWER T/E PANEL 641 KB IS CHAFED. REPAIRED RT WING INBD LOWER T/E PANEL 641 KB BY FABRICATING A DOUBLER & BONDING IT TO THE PANEL. SEALING & RESTORING THE FINISH IAW 51-71-00.

Part: ATTACH BRACKET — CHAFED (NR 1 NACELLE) · airframe 79,683 hrs · 32,434 cycles

NR 1 ENGINE PYLON, FWD APRON PANEL ATTACHING BRACKET AT STA YN 281 HAS A 1/2 INCH CHAFED HOLE ON THE EDGE. REMOVED & REPLACED FAIRING SUPPORT PER DWG AUB 7083; REV " K " & SRM 51-31-01; VOL II.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,683 hrs · 32,434 cycles

MAIN CARGO DOOR NR 3 SPOOL FITTING, INBD END HOLE HAS A CRACK EXTENDING AFT. REMOVED & REPLACED SPOOLBACK UP FITTING & CENTERLINE GUIDE AFT BACK UP FITTING IAW DWG NCA 6084.

Part: PANEL — CRACKED (RT WING) · airframe 79,683 hrs · 32,434 cycles

RIGHT WING LOWER T/E PANEL 641 GB IS CRACKED. FABRICATED PANEL IAW DWG ARC 0389. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED PANEL IAW SRM 51-21-02. PART MARKED PANEL AMM 7-0-1000.

Part: STIFFENER — CRACKED (LT WING) · airframe 79,683 hrs · 32,434 cycles

LEFT WING UPPER L/E PANEL 516 DT HAS A CRACKED ANGLE. REMOVED BROKEN STIFFENER IAW SRM 51-31-01. FABRICATED NEW STIFFENER IAW DWG ARB 1261 REV NC. HEAT TREATED NEW STIFFENER IAW TPS 1003 REV A, ARB 78/80 HT 102308-2. NEW STIFFENER REQUIRES ALODINE & PRIMED IAW SRM 51-21-01 VOL II. PART MARKED IAW GMM 7-0-1001. INSTALLED STIFFENER IAW SRM 51-31-01 & DWG ARB 1261 REV NC.

Part: ANGLE — CORRODED (ZONE 400) · corrosion level 2 · airframe 79,683 hrs · 32,434 cycles

RT SIDE OF NR 2 ENG INLET STRUCTURE APPROX STA YID 328.413 UPPER FRAME CAP HAS CORROSION AND NUTPLATES CORRODED, APPROX MIDWAY BETWEEN FRONT CENTER SPAR AND REAR CENTER SPAR BENEATH PANEL NR 364JR. REMOVED CORRODED CAP ANGLE PER SRM 51-31-01 VOL II. CAP ANGLE CORROSION FOUND TO BE OUT OF LIMITS. TOTAL MATERIAL LOSS, IAW MD/DC 10 SRM 54-00-01 VOL I. FORMED AND FABRICATED NEW CAP ANGLE P/N AJC7286-8 PER DAC DWG AJC7286 REV F. INSTALLED NEW CAP ANGLE PER DAC DWG AJC7286 REV F AND MD/DC 10-10 SRM 51-35-01 PG 5 VOL II.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 79,683 hrs · 32,434 cycles

NR 1 PYLON PANEL 438 CR IS CRACKED AT THE WELD. FABRICATED REPAIR DOUBLER IAW SRM 54-00-01. INSTALLED REPAIR DOUBLER IAW SRM 54-00-01 & SRM 51-35-01.

Part: RIB — CRACKED (ZONE 500) · airframe 79,683 hrs · 32,434 cycles

LEFT WING UPPER L/E PANEL 517 CT HAS 2 CRACKED RIBS. REMOVED 2EA CRACKED RIBS IAW SRM 51-35-01 & SRM 51-33-01; VOL II. & FABRICATED IAW DWG ARB 2407; REV "G". ALODINED & PRIMED IAW SRM 51-21-01; PGS 21 - 24; VOL II. INSTALED IAW DWG ARB 2407; REV "G"; SRM 51-35-10 & 51-33-01; VOL II.

Part: INTERCOSTAL — CORRODED (RT WING WW) · airframe 79,683 hrs · 32,434 cycles

RIGHT WHEEL WELL FWD OF STA 1521, THE OTBD INTERCOSTAL IS CORRODED. REMOVED INTERCOSTAL IAW SRM 51-35-01. FOUND CORRODED TEE CAP. UPON REMOVAL OF THE INTERCOSTAL. REMOVED CORROSION & WORKED AREA IAW SRM 53-40-00 & E.A. 8-5310-123513. FABRICATED INTERCOSTAL IAW DWG AEA 0026. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-01. INSTALLED IAW DWG AEA 0026.

Part: ATTACH FITTING — GOUGED (DOOR) · airframe 79,683 hrs · 32,434 cycles

RIGHT PATIO DOOR FWD END ATTACH CLIP IS GOUGED. REMOVED OLD STIFFENER (ATTACH CLIP) IAW DC/MD-10 SRM 51-35-01 VOL II. FORMED NEW STIFFENER PER FEDEX GMM 7-0-1001 SECTION 7 ITEM C & IAW DC/MD-10 SRM 51-10-00 VOL II. HEAT TREATED IAW TPS 1003 REV "A". HRB 62/63 HT 102608-1. LOCATED; DRILLED & DEBURRED PER FEDEX GMM 7-0-1001 SECTION 7 ITEM C & IAW DC/MD-10 SRM 51-31-01 VOL II. ALODINED & PRIMED IAW DC/MD-10 SRM 51-21-01 VOL II. INSTALLED STIFFENER IAW DC/MD-10 SRM 51-35-01 VOL II.

Part: STRUCTURE — CRACKED (FUSLEAGE) · airframe 77,227 hrs · 31,266 cycles

DURING LAX "C" CHECK VISIT W.O 36243; RH OB FLAP - IB FWD HINGE ASSEMBLY 3 STRUCTURAL CRACKS WERE DISCOVERED. ARB2431-2 (OB SIDE OF ASSEMBLY )1.25" CRACK FROM 1ST TO 2ND FASTENER. 1.25" CRACK FROM 5TH TO 6TH FASTENER. NON-ROTINE N01103 ARB2431-502 (IB SIDE OF ASSEMBLY) 1.00" CRACK FROM 10TH TOWARD 11TH FASTENER. EA 8-5710-105699 WAS CREATED. BOEING HAS DETERMINED THAT THE CRACK (S) CONDITION IS STRUCTURALLY ACCEPTABLE FOR CONTINUED SERVICE. E.A. 8-5710-105699 REQUIRES AN INSPECTION AT EACH "B" CHECK UNTIL THE HINGE SUPPORTS ARE REPLACED AT NO LATER THAN THE NEXT "C" CHECK OR 24 MONTHS. THE HINGE SUPPORT FITTINGS WILL BE REPLACED WITH IMPROVED PARTS.

Part: BOLT — CORRODED (ZONE 700) · airframe 77,227 hrs · 31,266 cycles

DURING RT MLG REMOVAL, THE FWD RT TRUNNION BOLT (P/N: ARG7557-501) WAS FOUND TO BE SEVERELY CORRODED. ALSO, THE RT MLG TRUNNION BOLT INNER SLEEVE (P/N: ARG7653- 3), SPIRAL LUBE HOLES WERE NOT DRILLED OUT TO THE PROPER SIZE PER DOUGLAS B/P: ARG7653 REPLACED CORRODED TRUNNION BOLT AND SLEEVE WITH SERVICEABLE PARTS ON SEQ 801, W/C32T1701-R DURING "C" CHECK, W/O36243 AT LAX HVMX GEAR CHANGE REF ITEM NR 3A, SEQ 801, S801, ITEM 4K7-14.

Part: BOLT — CORRODED (ZONE 700) · airframe 77,227 hrs · 31,266 cycles

DURING LT MLG REMOVAL, THE LT MLG FWD TRUNNION BOLT (P/N:ARG7557-501) WAS FOUND TO BE CORRODED. ALSO LT MLG FWD TRUNNION BOLT SPACER (P/N:ARG7653-3) SPIRAL GROOVE LUBE HOLES WERE NOT DRILLED OUT TO PROPER SIZE PER DOUGLAS B/P: ARG7653. REPLACED CORRODED TRUNNION BOLT AND SLEEVE WITH SERVICEABLE PARTS ON SEQ 800, W/C 32T1701-L DURING "C" CHECK, W/O 36243 AT LAX HVMX GEAR CHANGE. REF ITEM NR 3A, SEQ 800 S800, ITEM 4K7-14.

Part: BOLT — SHEARED (ZONE 400) · airframe 74,767 hrs · 30,186 cycles

NR 1 PYLON, UPPER PLUG LOCKING BOLT HEAD SHEARED OFF DURING REMOVAL. REF BOLT P/N AUB7227-1. INSTALLED NR 1 PYLON UPPER PLUG LOCKING BOLT. REF M/M 54-00-01-4

Part: VENT — LOOSE (CARGO DOOR) · airframe 73,003 hrs · 29,435 cycles

UNABLE TO PRESSURIZE A/C. RETURNED TO PDX. FOUND HARDWARE DAMAGED AND LOOSE ON MAIN CARGO VENT DOOR. INSPECTED DOOR NO DAMAGED. REPLACED HARDWARE PER SMP. PERFORMED PRESSURIZATION CHECK. OPS CHECK NORMAL.

Part: CONNECTOR — MISPINNED (COCKPIT) · airframe 72,928 hrs · 29,397 cycles

ON ARRIVAL AT KMEM SELECTED GEAR DOWN, GOT LEVEL 2 ANTI-SKID FAIL ALERT. MISSED APPROACH, RAN CHECKLIST, STILL GOT SAME ALERT. LANDED UNEVENTFULLY WITH ANTI-SKID FAIL LIGHT ILLUMINATED. SELECTED ANTI-SKID OFF CLEARING RUNWAY IAW CHECKLIST. T/S FOUND A "G" ON INSERT B PIN F8 ON ALL 3 VIA'S PER TSM THIS SHOULD BE A "O". INTERMITTENT "G" ON PIN 8G OF INSERT B. ONLY ON VIA-1. VIA'S 2&3 INDICATE NORMAL. THIS FAULT INDICATES A WIRE FROM TERM BLOCK S3-90 IS BAD OR A BAD VIA-1. R/R'D VIA 1 & VIA 2 IAW MD10-10 M/M. ALL CHECKS NORMAL IAW RTS. RETESTED ANTI SKID PER FIM. ALL TEST PASSED AS REQUIRED IN FIM. OK FOR SVC AT THIS TIME.

Part: CABLE — BROKEN (NLG) · airframe 71,123 hrs · 28,610 cycles

AT LIFTOFF AFTER GEAR RETRACTION TOWER INFORMED CREW, NOSE GEAR WAS DOWN. RECEIVED A RED NOSE GEAR LIGHT AND ELECTED TO EXTEND GEAR, NORMAL GEAR INDICATION (3 GREEN). DURING TAXI FELT SLIGHT RIGHT PULL BUT NO OTHER ABNORMALITIES. AFTER LANDING FOUND RIGHT STEERING CABLE BROKEN. REMOVED AND REPLACED BOTH LEFT AND RIGHT LOWER STEERING CABLES AND RIGGED PER DC-10 M/M 32-51-00-2. PERFORMED GEAR RETRACTION OF NOSE GEAR ASSY, GEAR RETRACTED NORMAL. OK FOR SERVICE.

Part: SMOKE DETECTOR — FAULTY (CABIN) · airframe 68,168 hrs · 27,393 cycles

NR 12 CABIN CARGO SMOKE DETECTOR LIGHT CAME ON. R&R NR 12 SMOKE DETECTOR PER MM 26-18-01-2.

Part: SPLICE — CRACKED (RT WING)

FWD RT WING ROOT, SPLICE FITTING AT FUSELAGE TO WING FRONT SPAR LWR CHORD IS CRACKED BETWEEN TWO FASTENER HOLES. NDT VERIFIED STA 1156 XCW 118. REMOVED AND REPLACED DOUBLER PER EA 58-5710-59060.

Part: ARM — CRACKED (RUDDER PEDAL) · airframe 67,632 hrs · 27,100 cycles

CAPT'S RUDDER PEDAL LT SIDE ARM ASSY IS CRACKED AT LINK ATTACH POINT. REMOVED AND REPLACED ARM ASSY PER CMM 27-21-02.

Part: UNKNOWN — ODOR (CABIN) · airframe 73,161 hrs · 29,001 cycles

DURING CLIMBOUT NOTICED ACRID FUMES EMANATING FROM AIR CONDITION SYS, PROCEED TO COMPLY WITH EMERGENCY CKLIST AND RETURN TO DEP AIRPORT.

Part: FLAP — FAULTY (WINGS) · airframe 67,124 hrs · 26,862 cycles

LAND PHASE, SEL FLAPS 15 DEG, RT FLAPS TRACKED TO 15 DEG, LEFT FLAP TAPE IND ONLY 5 DEG. CREW RAN NO FLAPS/ASYM FLAPS WITH SLATS EMERGENCY CKLIST. FLAP OVRD GUARD HANDLE NEEDS NEW SAFETY WIRE. DURING SPLIT FLAP IND, NO ADVERSE FLT CHARACTERISTICS.

Part: VALVE — DAMAGED (NR 2 ENGINE)

SMOKE IN COCKPIT & CABIN USING BLD 2 & 3 & PACK 1. SWITCH TO PACK 3 WITH SAME SMOKE & SMELL. RED TAB RUN. REMOVED AND REPLACED NR 2 ENG PRESS REG VLV PER IAW DC10 AMM 36-12-01. OK FOR SERVICE.

Part: BRACKET — DAMAGED (RT TE FLAP)

RT WING O/B FLAP POS XMITTER CABLE PULLEY BRACKET IS SAWED-OFF AT XORS 405, FWD OF I/B AILERON O/B HINGE ATTACH AND GUIDE PULLEY PIN MISSING. REMOVED AND REPLACED IAW AMM 27-51-07.