N381FE

Part: SENSOR — MALFUNCTIONED (NR 3 ENGINE) · airframe 97,807 hrs · 41,586 cycles

DURING THE NR 3 ENGINE SHUTDOWN AND RELIGHT WHILE AIRBORNE, THE ENGINE STARTED OK, BUT WOULD NOT EXCELLERATE OFF IDLE. IDLE. R & R OF C.I.T. SENSOR AND LEAK CHECKED GOOD IAW AMM 73-20-02-2.

Part: SEAT TRACK — CORRODED (BS 1980) · corrosion level 3 · airframe 97,795 hrs · 41,578 cycles

VIEW FROM AFT CARGO WASTE TANK BAY, BS 1980, RBL 80, LOOKING AT UNDERSIDE OF SEAT TRACK WAS EXFOLIATION BY THE NUTPLATE. REPLACED THE SEAT TRACK BETWEEN BS 1887 - 1997 IAW DWG SR10-53-002, AND DWG SP10510261.

Part: TEE FITTING — CRACKED (BS 1462-1505) · airframe 97,795 hrs · 41,578 cycles

LEFT MLG WHEEL WELL, OTBD WEB WAS CRACKED AT PREVIOUS REPAIR LOWER STIFFENER CHANNEL. REMOVED AND REPLACED THE TEE FITTING ANB7203-151, IAW DRAWING ANB7203, AND SRM 51-33-01, VOL 2.

Part: SKIN — DENTED (BS 967) · airframe 97,795 hrs · 41,578 cycles

FUSELAGE SKIN, BS 967, LONGERON 41R, THERE WAS TWO DENTS WITHIN THREE INCHES OF EACH OTHER. FWD DENT IS .080 INCH DEEP, AFT DENT IS .100 INCH DEEP. THE DAMAGE WAS OUT OF LIMITS IAW SRM 53-20-00, VOL I, REPAIRED THE DOUBLERS IAW EA 8-5310-T0341447.

Part: STIFFENER — CRACKED (NR 2 ENGINE) · airframe 97,795 hrs · 41,578 cycles

NR 2 ENGINE INLET, RT SIDE STIFFNER, BEHIND PANEL 364NR WAS CRACKED. REPAIRED THE STIFFENER IAW SRM 55-20-00, VOL I, FIG 1, SHEET 4, AND DRAWING AJC7402.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 97,795 hrs · 41,578 cycles

MAIN CABIN SEAT TRACK STA 1005-1020 LBL48 SEAT TRACK WORN/DAMAGED. REPLACED DAMAGED SEAT TRACK FROM STA 989 TO 1029 REF SRM 53-70-00 FIG 1 VOL 1 & SRM 51-31-01 VOL 2 & SR10-53-002 DWG & SRM 51-41-01 VOL 2.

Part: FRAME — CRACKED (BS 615) · airframe 97,795 hrs · 41,578 cycles

FWD CARGO BAY BS 615 LONGERON 48R, FRAME WAS CRACKED. REPAIRED THE FRAME IAW SRM 53-00-01, FIG 8, VOL 1. AND DWG ACA0036. SEALED THE REPAIR IAW SRM 51-41-01 VOL. 2.

Part: LONGERON — CORRODED (BS 826) · airframe 97,795 hrs · 41,578 cycles

FWD CARGO BAY, BS 826, LONGERON 51L HAD CORROSION. REPAIRED IAW SRM 3-10-00, FIG 2, SH 1.

Part: FINGER DOUBLER — CORRODED (BS 1680-1701) · airframe 97,795 hrs · 41,578 cycles

CENTER CARGO BAY, BS 1680 - 1701, BETWEEN STRINGERS 51L & 51R FINGER DOUBLERS HAD SURFACE CORROSION. REMOVED THE SURFACE CORROSION, CLEAN THE AREA, ALODINE, PRIMED, AND PAINTED IAW SRM 51-21-01, VOL 2.

Part: DOUBLER — DAMAGED (BS 1632-1672) · airframe 97,795 hrs · 41,578 cycles

FUSELAGE SKIN DOUBLER AT BS 1632 - 1672, LONGERON 48L HAS POPPED FASTENERS & DEFORMED BEAUTY STRIP. POSSIBLE INTERGRANULAR CORROSION UNDER PRODUCTION SPLICE DOUBLER. REPAIRED IAW EA 8- 5330-T0341638.

Part: FASTENER — MISSING (DOOR FRAME) · airframe 97,795 hrs · 41,578 cycles

AFT CARGO BAY, BS 1785 CENTER CARGO DOOR FRAME HAD SEVERAL OPEN FASTENER HOLES, BETWEEN LONGERON 37R AND 38R. INSTALLED THE FASTENERS IAW EA 8-5310-T0341819.

Part: FORMER — CRACKED (LT WING) · airframe 97,795 hrs · 41,578 cycles

LEFT WING LEADING EDGE, XORS 491 UPPER STRUCTURE HAD A 6 INCH CRACK ON THE FORMER. ACCOMPLISHED A REPAIR IAW EA T 8-5710-T0341645 P1. MAJOR REPAIR.

Part: DOUBLER — CRACKED (BS 1374-1379) · airframe 97,795 hrs · 41,578 cycles

LT KEEL BEAM MACHINED DOUBLER AFT ANGLE HAD A CRACK BETWEEN TWO FASTENERS. REPLACED THE MACHINED DOUBLER IAW SRM 51-31-01, VOL 2, AND DWG NEA6078.

Part: DOUBLER — CRACKED (BS 1374-1379) · airframe 97,795 hrs · 41,578 cycles

RT KEEL BEAM MACHINED DOUBLER AFT ANGLE HAD A CRACK BETWEEN FIVE FASTENERS. REPLACED MACHINED DOUBLER IAW ARM 51-31-01, VOL 2, AND DWG NEA6078.

Part: RIB — WORN (AFT FUSELAGE) · airframe 97,795 hrs · 41,578 cycles

AFT FUSELAGE BULKHEAD, LEFT SIDE BELOW THE UPPER LIGHT ASSEMBLY, HORIZONTAL RIB HAD DEEP WEAR. REPAIRED THE DAMAGED RIB IAW EA 8-5310-TO341640.

Part: SEAT TRACK — CORRODED (BS 1129-1131) · corrosion level 2 · airframe 97,795 hrs · 41,578 cycles

MAIN CABIN SEAT TRACKS, BETWEEN BS 1160 TO 1260 LBL 75, HAD LIGHT CORROSION. REPLACED THE DAMAGED SEAT TRACK IAW SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II, SRM 51-41-01 VOLUME II

Part: DOUBLER — CRACKED (LT WING) · airframe 97,795 hrs · 41,578 cycles

LT LEADING EDGE STA XORS = 562 UPPER STRUCTURE HAS 5.25" CRACK ADJACENT TO FORMER (WEB). VIEW THROUGH SLAT CABLES BOTTOM PANELS SLAT TRACK 10 AREA REMOVED AND REPLACED NEW -11 DOUBLER REF DAC DWG ARB1249.

Part: DOUBLER — CRACKED (LT WING) · airframe 97,795 hrs · 41,578 cycles

LT LEADING EDGE STA 775 UPPER STRUCTURE HAS 5.25" CRACK ADJACENT TO FORMER (WEB). VIEW THROUGH SLAT CABLES BOTTOM PANELS SLAT TRACK 12 AREA REMOVED CRACKED ARB1249-9 DOUBLER AND REPLACED WITH NEW IAW DRAWING ARB1249.

Part: DOUBLER — CRACKED (LT WING) · airframe 97,795 hrs · 41,578 cycles

LT LEADING EDGE STA XORS 562 UPPER STRUCTURE INNER BEADED DOUBLER HAS 3 CRACKS .250" - 1.0". VIEW THROUGH SLAT CABLES BOTTOM PANELS SLAT TRACK 10 AREA. INSTALLED REPAIR DOUBLER REF SRM 57-10-00 FIG 71 VOL I 07/26/18. INSTALLED DOUBLER REF SRM 57-10-00 FIG 71 VOL I ITEM 4. FABRICATED DOUBLER REF SRM 57-10-00 FIG 71 VOL I.

Part: SKIN — CRACKED (RT WING) · airframe 97,795 hrs · 41,578 cycles

RIGHT WING SKIN AT THE SLAT ANTI-ICE TELESCOPING DUCT CUTOUT HAS A .600 INCH CRACK AT THE UPPER OUTBOARD CORNER AND ONE .200 INCH AND TWO .600 INCH CRACKS AT THE UPPER INBOARD CORNER. RIGHT WING SKIN WAS REPAIRED IAW SRM 57-10-00, FIG 103, SHEET 2, VOLUME 1.

Part: SKIN — CRACKED (LT WING) · airframe 97,795 hrs · 41,578 cycles

LT WING SKIN AT THE SLAT ANTI-ICE TELESCOPING DUCT CUTOUT HAS A .600 INCH CRACK AT THE UPPER INBOARD CORNER AND A .500 INCH CRACK AT THE UPPER OUTBOARD CORNER WITH AN EXISTING STOP DRILL. REPAIRED LT WING SLAT ANTI-ICE TELESCOPING DUCT CUT OUT IAW SRM 57-10-00 VOL1 FIG 102 PG 479-484.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 96,446 hrs · 40,808 cycles

SMOKE IN COCKPIT DURING CLIMB OUT. DUCT TEMP WENT BOXED AMBER 225 DEGREES. FOLLOWED QRH PROCEDURE. AIR TURN BACK TO DEPARTURE. INSTALLED NEW DRAIN LINE FOR #1 PACK WATER SEPARATOR. RAN PACK IAW AMM 21-00-01-5, LINE LEAK CHECKED GOOD. REMOVED AND REPLACED THE NR 1, 2 AND 3 WATER COALESCER BAGS IAW AMM 21-54-03-2. ACCOMPLISHED AN A/C PACK AND DUCT ODOR CLEANING IAW AMM 21-53-00-7. AFTER BURNOUT, REMOVED AND REPLACED ALL THREE SYSTEMS COALESCER BAGS IAW AMM 21-54-03-2.

Part: ROD END — DAMAGED (RT DOOR) · airframe 96,394 hrs · 40,774 cycles

RIGHT CABIN DOOR ARMING LEVER DOESN'T STAY IN HORIZONTAL POSITION WHEN DOOR IS ARMED. CAUSES OCCASIONAL CABIN DOOR FWD RT ALERT. COMPLETED INSTALLATION OF THE RT FWD PASSENGER DOOR INTERIOR CONTROL MECHANISM AND PERFORMED RIG AND AJDUSMENT IAW AMM 52-11-06-2, AND 52-11-00/501. OPS CHECKED NORMAL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 95,812 hrs · 40,464 cycles

HYD 1 FAILED ON APPROACH. ACFT RECEIVED A HYD 1 OFF LIGHT WHEN QTY WENT 2.7 GALLONS. WHEN CREW WENT TO CONFIGURE FOR LANDING HYD QTY WENT TO .5 GALLONS. AND GOT HYD FAIL. HYD LEAK IN L/H WHEEL WELL PIPE ASSY IS APK7002-1 INSTALLED SEALS AND 18" FLEX LINE PER MM 20-10-01-2.SERVICED #1 HYDRAULIC SYSTEM PER MM 12-13-02-3.LEAK AND OPS CHECK NORMAL

Part: SHAFT — WORN (L1 DOOR) · airframe 95,785 hrs · 40,449 cycles

FOUND L-1 DOOR AIR MOTOR SPROCKET SHAFT WORN AND CHAIN SKIPPING ON SPROCKET. REMOVED AND REPLACED SPLINE SHAFT ASSY AND CHAIN ASSY CONNECTING AIR MOTOR TO ELECTRIC ACTUATOR..ALL DOOR OPS CHECKS ARE GOOD.

Part: ACTUATOR — FAILED (L1 DOOR) · airframe 95,758 hrs · 40,437 cycles

L1 DOOR SWITCH INTERMITTENT. R & R THE L1 ELECTRIC DOOR ACTUATOR IAW AMM 52-11-01-2. MOTOR AND SWITCHES OPS NORMAL.

Part: PROXIMITY SENSOR — FAILED (LE SLAT) · airframe 95,427 hrs · 40,281 cycles

PSEU FAIL LEVEL 1 ALERT 1000FT, 250 KTS LEVEL. ELECT PROX SWITCHING MPN: 8-946-01 CPN: 3110976. CFDS FAULT PSEU. CURRENT FAULTS 317097 RIGHT SLAT OUTBD SENSOR B FAULT. REF TSM TASK 27-80-00-810-804. SENSOR READOUT R4B SLAT SENSOR FAIL. NEED PSEU. R&R NR 2 B RT SLAT INDB SENSOR AND NR 4B RT OUTBD SENSOR REF FIM 27-80-00-2, SWPM 20-20-03. OPS CHECKS OK, REF MM 217-84-02-4.

Part: SPRING — FAILED (LT MLG) · airframe 95,228 hrs · 40,171 cycles

LEFT MAIN GEAR INDICATED UNSAFE UPON RETRACTION. ACCOMPLISHED CHECKLIST, RETURNED GEAR TO SAFE DOWN INDICATIONS, UNEVENTFUL LANDING. IDENTIFIED PARTS LANDING GEAR EXTENSION. FOUND LT MLG UPLOCK CRANK EXTENSION SPRING BROKEN, REF IPC 32-34-02-01, FIG. 1, ITEM 091. REPLACED SPRING REF MD10 IPC 32-34-02-01, FIG. 1, ITEM 091. PERFORMED MAIN LANDING GEAR EXTENSION/RETRACTION TEST (4 CYCLES) IAW AMM 32-30-00-5 - SATISFACTORY. BOTH PRIMARY AND SECONDARY LANDING GEAR INDICATIONS NORMAL . OK FOR SERVICE.

Part: HINGE — CRACKED (PANEL) · airframe 95,094 hrs · 40,103 cycles

PANEL 361DL LT PICKLE BARREL PANEL UPPER HINGE HAS BROKEN LOBE AT STA 2020-2022. R & R DAMAGED HINGE SECTION IAW EA 8-5450-T0326629.

Part: CAP — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

LEFT STA 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS 2" CRACKS EXTENDING THROUGHOUT BOTH FASTENER HOLES AND INTO THE RADIUS. INSTALLED NEW T-CAP FROM LONGERON 37L TO 44L IAW EA.

Part: CAP — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

LEFT STA 595 BULKHEAD TEE CAP VERTICLE LEG AT LONGERON 41L HAS 1.25 IN CRACK EXTENDING THROUGHOUT THE LOWER FASTENER HOLE. INSTALLED NEW T-CAP BETWEEN LONGERON 37L AND 44L IAW EA.

Part: DOWEL PIN — GOUGED (ZONE 600) · airframe 95,094 hrs · 40,103 cycles

NR 3 ENGINE NOSE COWL INNER BARREL ACCOUSTIC PANEL REPAIR DOUBLER AT 6:00 AFT OF LIP. REPAIR FASTENERS ARE NOT FLUSH. R & R DOUBLER AND INSTALLED WITH FLUSH FASTENERS IAW SRM 54-11-00, FIG C.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

ACM COMPARTMENT AT STA 595, LONG 44L INTERCOSTAL HAS CRACK PROPAGATING FROM REPAIR DOUBLER. R & R WEB ACA 3816-503 IAW SRM 51-33-01, VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,094 hrs · 40,103 cycles

MAIN CABIN, APPROXIMATELY STA 1901, RBL 48, FLOOR SUPPORT IS CORRODED. R & R FLOOR SUPPORT, PN WSP 0711-554 IN REF TO SRM 51-35-01, FIG 2, VOL 2.

Part: BRACKET — WORN (R1 DOOR) · airframe 95,094 hrs · 40,103 cycles

R1 DOOR EVACUATION SLIDE BOTH FWD AND AFT ATTACH BRACKETS WORN. R & R BRACKETS IAW SRM 51-35-01, DWG ABA 8216-2.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

CENTER CARGO BILGE AREA BETWEEN STA 1561 TO STA 1521, LONGERON 49R AS CORROSION BEYOND SERVICEABLE LIMITS, REQ R & R OF PN AEA 0451-1. R & R LONGERON 49R FROM STA 1561 TO STA 1521, REF DWG AEA 0451 AND SRM 51-00-00, VOL 1.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

RIGHT STA 595, BULKHEAD T-CAP FWD LEG JUST BELOW LONGERON 37R HAS A .5" CRACK EXTENDING FROM THE RADIUS TO THE FWD FASTENER HOLE. REPAIRED IAW EA 8-5310T0325916 SPLICED T-CORD AND INSTALLED NEW SECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

NR 3 A/C COMPARTMENT CUTOUT AFT UPPER CORNER SKIN HAS A .75" CRACK FROM SKIN EDGE THRU 1 FASTENER. REPAIRED A/C COMPARTMENT IAW SRM 53-50-00, FIG 3A, VOL 1.

Part: DOUBLER — DAMAGED (LT WING) · airframe 95,094 hrs · 40,103 cycles

LEFT WING OTBD WING TIP UPPER SURFACE APPROXIMATELY STA XW 927 HAS AN EXISTING REPAIR. DOUBLER DAMAGED. R & R DOUBLER IAW SRM 57-00-01, VOL 1.

Part: CAP — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

LEFT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS A 2.00" CRACK EXTENDING THROUGH BOTH FASTENER HOLES AND INTO THE RADIUS. INSTALLED NEW TEE CAP FROM LONGERON 37L TO 44L PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

NLG EXTERIOR SKIN RT FWD CORNER AT STA 306 HAS A CRACK. REPAIRED DAMAGED IAW SRM 53-50-00, FIG 25, SHEET 3.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,094 hrs · 40,103 cycles

FWD LOWER CARGO STA 960 BETWEEN STR 50 LT- STR 50 RT. J CAP FORMING MILD CORROSION. CORROSION R & R IAW SRM REF 53-30- 00, FIG 5, SH 1.

Part: CAP — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

LEFT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 41L HAS A 1.25" CRACK EXTENDING THROUGH THE LOWER FASTENER HOLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

MAIN CABIN, APPROXIMATELY STA 1987, RBL 8, FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT IAW DWG WSP 0711.

Part: STOP — CRACKED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

NR 3 AIR CONDITIONING COMPARTMENT UPPER AFT CORNER DOOR STOP ACA3852-4 CRACKED THROUGH FASTENER HOLE. R & R STOP ACA3852-4, REF SRM 51-35-01, VOL II.

Part: SKIN — DAMAGED (LE SLAT) · airframe 95,094 hrs · 40,103 cycles

RIGHT WING, NR 2 SLAT XORS 264, UPPER SURFACE REPAIR DOUBLER. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

MAIN CABIN SEAT TRACK DAMAGED AT STA 1381, LBL 75. REPLACED SEAT TRACK SECTION IAW SRM 53-70-00 V1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

SEAT TRACK DAMAGED AT STA 1383, LBL 27. REPLACED SEAT TRACK SECTION WITH PN S4929147 IAW SRM 53-70-00, FIG 1, VOL 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 95,094 hrs · 40,103 cycles

MAIN CABIN, APPROXIMATELY STA 1920 THRU STA 2007, RBL 60, FLOOR SUPPORT IS CORRODED. R & R FLOOR SUPPORT IAW DWG WSP0711.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 94,722 hrs · 39,918 cycles

FUME EVENT ON DESCENT FROM 16,000 FT UNTIL 5,000 FT. HEAVY MUSTY DIRTY SOCK SMELL. PACK 2 WAS OF, PACK 1/2 ON. PERFORMED PACK & DISTRIBUTION DUCT ODOR CLEANING PROCEDURE IAW AMM 21-53-00-7. R & R THE NR 1 & 3 PACK COALESCE SOCKS IAW AMM 21-54-03-2. AFTER ABOVE PROCEDURES NO ODOR FOUND DURING PACK 1 & 3 OPERATION. NO HISTORY LAST 30 DAYS.

Part: ARMING LEVER — MALFUNCTIONED (L1 DOOR) · airframe 94,716 hrs · 39,916 cycles

L1 DOOR WILL NOT OPEN ELECTRICALLY. RESET SLIDE ARMING HANDLE IAW AMM 52-10-01-5. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 94,722 hrs · 39,918 cycles

FUME EVENT ON DESCENT FROM 16,000 FT UNTIL 5,000 FT. HEAVY MUSTY DIRTY SOCK SMELL. PACK 2 WAS OFF, PACK 1/2 ON. PERFORMED PACK & DISTRIBUTION DUCT ODOR CLEANING PROCEDURE IAW AMM 21-53-00-7. R & R THE NR 1 & 3 PACK COALESCE SOCKS IAW AMM 21-54-03-2. AFTER ABOVE PROCEDURES NO ODOR FOUND DURING PACK 1 & 3 OPERATION. NO HISTORY LAST 30 DAYS.

Part: CABLE — LOOSE (L1 DOOR) · airframe 940 hrs · 39,563 cycles

DURING CLOSE L1 DOOR WAS FOUND UPPER AFT DOOR CABLE BRACKET BOLT LOOSE WHEN DOOR CLOSE OR RETRACT OPEN. NOTE DOOR OPERATES NORMAL. EXTENDED OVERWATER OPERATIONS REQUIRES TWO SLIDES & OR RAFTS. INSPECTION CABLE & BRACKETS BOTH APPEAR NORMAL. CABLE FOR TOP SLIDING COVER OF DOOR APPEARS LOOSE DUE TO COILING OF CABLE, BUT CABLE IS SECURE IAW AMM 52-10-02-2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 940 hrs · 39,527 cycles

EMERGENCY EXIT LIGHTS, RT & LT SIDE ON BULKHEADS FWD OF L1 & R1 DOORS INOPERATIVE. R & R EMER LIGHTING POWER SUPPLY IAW AMM 33-51-01-4, NO HELP. THE TWO LIGHTS WITH THREE BULBS ARE BOTH VERY DIM, TO THE POINT WHERE THEY APPEAR TO BE INOPERATIVE WITH THE COVERS ON. REMOVED AND REPLACED L-1 DOOR EXIT SIGN AND LAMPS IAW MM 33-00-00-2 AND WDM 33-52-01.OPS CHECKED NORMAL IAW MM 33-50-00-5. ACFT OK TO CONTINUE.

Part: WINDOW — UNSECURE (COCKPIT) · airframe 936 hrs · 39,292 cycles

CAPTAIN`S WINDOW NOT LATCHED AIRBORNE. VERIFIED CAPTAIN`S WINDOW CLOSED PROPERLY SEVERAL TIMES.

Part: CRANK ASSY — DISCONNECTED (L1 DOOR) · airframe 932 hrs · 39,063 cycles

FOUND L1 ENTRY DOOR UPPER AFT CRANK ARM DISCONNECTED FROM BOGIE ASSEMBLY. REMOVED AND REPLACED L1 DOOR AFT UPPER BOGIE CRANK ASSY. AND ATTACHING HARDWARE, REMOVED AND REPLACED L1 DOOR AFT SWITCH ACTUATOR ASSY IAW MM 52-11-03-2. L-1 DOOR OPS NORMAL.

Part: SKIN — CRACKED (RT WING) · airframe 92,346 hrs · 38,552 cycles

CRACK IN RT WING SKIN BETWEEN SLAT 5 & 6 AT SLAT TRACK 12. PERFORMED HFEC INSPECTION. HFEC SHOWS POSITIVE INDICATION IAW 20-30-00 PART 6. INSTALLED DOUBLER AND FILLER IAW SRM 57-10-00 FIG 68.

Part: SKIN — CRACKED (RT WING) · airframe 92,346 hrs · 38,552 cycles

RIGHT WING LE IS CRACKED BETWEEN NR 4 & NR 5 LE SLATS. REMOVED ACCESS PNL AFT OF CRACK. PNL IN COURIER AREA. REMOVED EXISTING FASTENERS & CUT OUT DAMAGE AREA IAW SRM 57-10-00 FIG 68 SHEET 1. COMPLIED WITH HFEC OF CUT OUT AREA IAW NDT SPM PART 6 20-30-00, NO DEFECTS NOTED. FABRICATE DOUBLER AS .063 TITANIUM & MATERIAL FOR FILLER AS 7075-T6 .090, VERIFIED MATERIAL. REPAIR DOUBLER & FILLER, OK TO INSTALL IAW SRM 57-10-00. INSTALLED REPAIR IAW SRM 57-10-00 FIGURE 68 SHEET 1 & SRM 51-38-01 FOR ONE ALTERNATE FASTENER. REQUIRES PRIME & PAINT. PRIMED & PAINTED REPAIR DOUBLER IAW DC-10 SRM 51-21-02 VOL.2. EL REMOVED TO FOM FOR REPAIR NEEDS TO BE INSTALLED.

Part: WARNING MESSAGE — FALSE INDICATION (MLG) · airframe 92,122 hrs · 38,421 cycles

DURING VISUAL APPROACH, LANDING GEAR WAS SELECTED DOWN & RECEIVED THREE RED ON PRIMARY & SECONDARY DISPLAYS. CYCLED GEAR & RECEIVED SAME RESULT. BOTH TIMES FELT GEAR EXTEND, PERFORMED A LOW APPROACH & TOWER CONFIRMED GEAR WAS DOWN. AT 1000 FT THEN FINALLY RECEIVED THREE GREEN ON BOTH DISPLAYS, RAN QRH & LANDED. CHECKED PSEU SENSOR READOUT FOR POWER INPUTS & DISCRETE INPUTS. ALL READINGS NORMAL. CHECKED GEAR HANDLE & LANDING GEAR ALTERNATE EXTENSION HANDLE SWITCH. BOTH CHECKED GOOD. ADJUST SELECTOR VALVE ASSEMBLY. CLEANED & LUBED LANDING GEAR HANDLE CABLES IAW SMP. PERFORMED GEAR SWING OF ALL 3 LG. OPS CHECKED GOOD IAW AMM 32-30-00-5.

Part: MEC — INOPERATIVE (NR 2 ENGINE) · airframe 91,207 hrs · 37,944 cycles

CLIMBING OUT AT 15,000 FT NR 2 ENGINE SPOOLED DOWN TO INOPERATIVE. DID ENGINE SHUTDOWN PROCEDURES AND RETURNED FOR LANDING. REPLACED MEC AND FUEL PUMP, ACCOMPLSIHED HIGH POWER RUNS, ALL CHECKED GOOD. COMPLETED INSTALLATION OF MEC AND FUEL PUMP PERFORMED A THROTTLE RIG CHECK AND A VSV RIG OF THE NE 2 ENGINE MEC STILL REQUIRES IDLE LEAK CHECKS AND POWER RUNS. REF. MD-10 AMM 73-20-01-2. PERFORMED WET/DRY MOTOR AND GROUND IDLE AND FLT IDLE CHECKS IAW JRH. NO LEAKS NOTED DURING ENGINE RUN AND ALL PARAMETERS WITHIN LIMITS OUTLINED IN JRH. STILL NEEDS MAX POWER ASSURANCE RUN AND FINAL RII BUY BACK. PERFORMED HIGH POWER ASSURANCE RUN ON NR 2 ENGINE. REF JRH 7-31. ALL PARAMETERS WITHIN LIMITS.

Part: BOLT — CORRODED (RT MLG TRUNNION) · airframe 90,000 hrs · 37,293 cycles

RIGHT MLG FWD UPPER TRUNNION BOLT CORRODED. REPLACED RT MLG FWD TRUNNION BOLT PER EO 8-3210-7-5004B PT2, ACCOMPLISHED CHECK.

Part: TRUNNION — CORRODED (LT MLG) · airframe 90,000 hrs · 37,293 cycles

LEFT MLG STRUT FWD TRUNNION LUG IS CORRODED, MISSING. REMOVED AND REPACED LT MAIN LANDING GEAR.

Part: BOLT — CORRODED (RT MLG TRUNNION) · airframe 90,000 hrs · 37,293 cycles

RIGHT MLG FWD UPPER TRUNNION BOLT CORRODED. REPLACED RT MLG FWD TRUNNION BOLT PER EO 8-3210-7-5004B PT2, SEQ 207, ACCOMPLISHED CHECK.

Part: SHEAR TIE — CORRODED (BS 1701) · corrosion level 2 · airframe 90,000 hrs · 37,293 cycles

CENTER CARGO BAY, FOUND TWO SHEAR TIES EXFOLIATED AT BS 1701 BETWEEN LONGERON 51 LEFT AND RIGHT. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-33-01 VOL II.

Part: THROTTLE CABLE — WORN (NR 2 ENGINE) · airframe 89,514 hrs · 37,030 cycles

NR 2 THROTTLE WOULD NOT GO PAST, RETARD PAST 70 PERCENT AT ALT, 60 PERCENT AT 5000'. NR 2 ENG WINDMILLED APPROX 10 MINS. THROTTLE SYS APPEARED TO BE PHYSICALLY FROZEN, THROTTLE DID PHYSICALLY RETARD COMPLETELY AFTER A FEW MINUTES OF ACFT BLOCKING IN (ENG NOT RUNNING). CREW SHUTDOWN ENGINE FOR THIS REASON. R & R AFT ENGINE THROTTTLE PUSH-PULL CABLE IAW MM 76-11-01-2. OPS CHECKED GOOD, OK FOR SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 89,302 hrs · 36,927 cycles

LEVEL 3 CABIN ALTITUDE ALERT WHILE PASSING 17,000 ON DEPARTURE. CABIN ALTITUDE UP TO 11,700 BEFORE DESCENT BELOW 10,000. LEVEL 1 CABIN DOOR FWD RT ALERT BELOW 10,000. LANDED WITHOUT INCIDENT. REPLACED OUTFLOW VALVE. REF 21-31-20. TESTED NORMAL, NO FAULTS NOTED. R & R NR 2 CABIN PRESSURE CONTROLLER REF MM 21-31-04-4-0. R & R RELAYS R2-5019, R2-5009 & R2-5744. REF IPC 24-51-51-01, 24-51-52-01 & 24-51-51-01. RTS ON BOTH CABIN CONTROLLERS GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 89,248 hrs · 36,897 cycles

ON ARRIVAL, EMERGENCY LIGHT TEST FAILED WITH "ALERT BATTERY LT 1 LO". EMERGENCY LIGHTS TESTED THREE TIMES WITHOUT FAILURE IAW WRI 33-50-1205.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,781 hrs · 36,644 cycles

ON COCKPIT PREFLIGHT, RECEIVED ALERT "EMERGENCY LIGHT BATTERY 1 LOW". PREMATURE REMOVAL /INSTALLATION. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-4. OPS CKS GOOD.

Part: SEAL — FAILED (COCKPIT WINDOW) · airframe 86,296 hrs · 35,358 cycles

COPILOT SLIDING WINDOW SEAL FAILED ON TAKEOFF AND INITIAL CLIMBOUT. FOUND COPILOTS WINDOW WAS NOT FULLY CLOSED. LATCH WAS IN CLOSED POSITION BUT LOCKS WERE NOT FULLY ENGAGED. OPENED AND CLOSED WINDOW AND LOCKED, LATCHES FULLY ENGAGED. PRESSURIZED ACFT TO 2 PSI, NO LEAKS OR SQUEELING NOTED AT COPILOTS WINDOW, WINDOW OK FOR SERVICE, REF AMM 56-12-00-5.

Part: B-NUT — LEAKING (DOOR CYLINDER) · airframe 85,671 hrs · 35,054 cycles

FL 350 1 HR INTO FLIGHT GOT LVL 1 ALERT "HYD 3 ELEV OFF". HYD SYNOPTIC SHOWED 3.5 GAL REMAINING AND SLOWLY DECREASING. ELECTED TO LOWER THE GEAR CONVENTIONALLY BEFORE WE LOST ALL HYD 3 QUANTITY. CONTINUED TO DESTINATION 100 MILES AHEAD. OVER NEXT 20 MINUTES SYS 3 QUANTITY DECREASED TO .5 GAL REMAINING RESULTING IN LVL 2 ALERT "HYD SYS 3 FAIL" LANDED WITHOUT FURTHER PROBLEMS. FOUND LEAK AT INBD B-NUT ON RT MLG DOOR LATCH CYLINDER. PERFORMED PERMANENT REPAIR PER MM 20-10-01 -2 USING RYNGLOK P/N R82101T04.

Part: HANDLE — UNSECURE (L1 DOOR) · airframe 85,353 hrs · 34,919 cycles

INADVERTANT EMERGENCY DOOR HANDLE (DOOR L1) MOVED TO DEPLOY POSITION AFTER BLOCK IN. NO SLIDE DEPLOYMENT. INSTALLED SLIDE ASSEMBLY PER MM 25-61-01-2. OPERATIONAL CHECK NORMAL SLIDE PREVIOUSLY REMOVED CPN INSTALLED 2500311 MPN AWD7274-1L.

Part: SKIN PANEL — CRACKED (HORIZONTAL STAB) · airframe 84,840 hrs · 34,683 cycles

THE HORIZONTAL STABILIZER, LT OUTER SECTION SKIN PANEL NR 7439-1, TOP SIDE JUST OUTBOARD OF FAIRING AND FORWARD OF REAR SPAR IS A 1.750 INCH CRACK. VERIFIED BY HFEC EDGES MARKED. APPROXIMATE LOCATION XE 67.333 STRINGER NR 1 INSTALLED REPAIR PER EA 8-5510-121560.

Part: UPLOCK SENSOR — OUT OF ADJUST (RT MLG) · airframe 84,051 hrs · 34,314 cycles

UNSAFE RIGHT MAIN GEAR AFTER TAKEOFF WITH GEAR HANDLE IN "UP" POSITION, BOTH INDICATIONS. VISUAL INSPECTION INDICATED UP AND DOOR CLOSED. FOUND RT MAIN LANDING GEAR PROX UPLOCK SENSOR OUT OF ADJUSTMENT. SHIMMED IAW MM 32-61-15-4. PERFORMED RTS IAW AMM 32-61-15-4. SYSTEM OP CK'D NORMAL.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 82,518 hrs · 33,594 cycles

NUMBER 2 ENGINE SHUT DOWN WHEN IT WOULD NOT RESPOND TO THROTTLE MOVEMENTS. NO PARAMETERS EXCEEDED. NORMAL LANDING ACCOMPLISHED PER CREW DEBRIEF THROTTLES WERE NEVER STIFF AND ENGINE WAS SHUT DOWN ABOUT 30 MINUTES IN FLIGHT. NR 2 ENG AND MOVED THROTTLE LEVER IN COCKPIT TO VERIFY MOVEMENT AT FUEL CONTROL. FUEL CONTROL LEVER MOVED ACCORDINGLY. STARTED ENG WITH THROTTLE AT IDLE. NR 2 ENG SPOOLED UP PAST FLIGHT IDLE DURING START. SUSPECT MEC, IAW MD10.

Part: LONGERON SPLICE — CRACKED (BS 1139 S16R) · airframe 82,228 hrs · 33,464 cycles

RT FUSELAGE AT BS 1139 LONGERON SPLICE 16R CRACKED. REMOVED CRACKED LONGERON SPLICE. FABRICATED LONGERON SPLICE PER DAC DRAWING ADA0179. LOCATED NEW STRINGER SPLICE AT BS 1139 L16R. INSTALLED SPLICE PER SRM 53-10-00 AND DAC DRAWINF ADA0179

Part: LONGERON SPLICE — CRACKED (BS 1139 S17R) · airframe 82,228 hrs · 33,464 cycles

RT FUSELAGE AT STA 1139 LONGERON SPLICE 17R CRACKED. REMOVED CRACKED LONGERON SPLICE. FABRICATED LONGERON SPLICE PER DAC DRAWING ADA0179. LOCATED NEW STRINGER SPLICE AT STA 1139 I-17R. OK TO INSTALL. PENETRANT INSPECTION REQUIRERD PER DAC DRAWING ADA 0179. OK TO INSTALL. INSTALLED SPLICE PER SRM53-10-00 ADA 0179.

Part: INSULATOR — OUT OF POSITION (BLEED AIR SYS) · airframe 80,219 hrs · 32,618 cycles

JUST AFTER T/O AIR SYS 2 OFF WITH FLICKERING MANIFOLD FAIL LIGHT. POWER BACK FOR DESCENT AND FLICKERING MANIFOLD LIGHT WENT AWAY. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 NR 2 MANIFOLD FAIL DETECTION LOOP INOP. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. T/S IAW FIM FAULT CODE 36-23-09. AT MFDC CONNECTOR PIN -E- TO GRD SHOWS 128 OHMS. FOUND LOOPS D1-28B AND D1-28 CONN HAD LOOSE INSULATOR CAUSING SHORT. REPOSITIONED INSULATOR, STRAIGHTEN PIN. SYSTEM RESISTANCE OPEN ON PINS E, F AND -X- OF MFDC CONN AIU 2 RTS PASSED IAW MM 31-43-02. REMOVED AND REPLACED LOOP D1-28B PER MD10 AMM 36-23-02-4. TEST OF NR 2 ENG PNEU SYSTEM MM 36-00-03-5. TEST CHECKED GOOD.

Part: WEB — CRACKED (ZONE 400) · airframe 79,356 hrs · 32,223 cycles

CRACK 1.5 INCH ON PYLON NR 1 UPPER VERTICAL WEB AT STA YN268. REPAIR IAW 54-00-01 FIG 3 VOL I.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,356 hrs · 32,223 cycles

ONE CRACK 4 INCHES LONG ON LONGERON INSIDE APU COMPT RT SIDE STA 2050. REPAIRED CRACK PER SRM 53-17-01 VOL 3 FIG 4, SRM 54-00-01 FIG 2B VOL 1, SRM 51-35-01 PG 1-13 VOL 2.

Part: STRUCTURE — UNKNOWN (VERTICAL STAB) · airframe 79,356 hrs · 32,223 cycles

VERTICAL STABILIZER RT SIDE OLD REPAIR AT XAR=417.800. REPAIR IAW SRM 55-00-01 FIG 3 VOL 1.

Part: TEE FITTING — CRACKED (ZONE 100) · airframe 79,356 hrs · 32,223 cycles

AT STA Y=1156 ON TEE CAP INTERNAL RT SIDE BETWEEN LONGERONS 39-40 FOUND CRACK 3 INCHES LONG. REMOVED TEE ANGLE AND INTERNAL DOUBLER IAW SRM 53-40-00 FIG 8 VOL 1. PERFORMED NDT INSPECTION FOUND CRACK 4.3 INCHES LONG. REPAIRED PER SRM 53-40-00 FIG 8 VOL 1.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 79,356 hrs · 32,223 cycles

ONE CRACK 2 INCHES LONG INSIDE TRACK AND FORMED PART AT STA 1019 X=-27 MAIN CABIN FLOOR PANEL. REPAIR SEAT TRACK PER SRM 53-70-00 FIG 1 VOL 1.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 79,356 hrs · 32,223 cycles

INTERNAL LOWER FUSELAGE CAC BULKHEAD RT SIDE FOUND 1 EACH CRACK 6 INCHES LONG ON VERTICAL STIFFENER STA 1159 X=-81 Z=-29. PERFORMED REPAIR IAW SRM 57-00-01 FIG 11 VOL 1.

Part: STRUCTURE — UNKNOWN (RT WING) · airframe 79,356 hrs · 32,223 cycles

RIGHT WING TIP AT STA YW=756 LOWER SURFACE FOUND DOUBLER REPAIR. REMOVED REPAIRED WING TIP IAW AMM 57-23-01-2 DWG ARB2208 ARB2209 AND SRM 51-30-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 79,356 hrs · 32,223 cycles

AIR CONDITIONING COMPT LT TEE ANGLE WITH CORROSION ON INTERNAL LOWER STRUT FROM STA 560 TO STA 580. INSTALLED NEW SECTION OF LONGERONS AND SPLICE REPAIR PER SRM 53-10-00 FIG 7 VOL 1.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 79,356 hrs · 32,223 cycles

WING LT LOWER SIDE AT XORS=391 TO XORS=433 OLD REPAIR QTY 3 EACH DOUBLER. ACCOMPLISH FEDEX EA 8-5710-84114.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 79,356 hrs · 32,223 cycles

LOWER FUSELAGE EXTERNAL DOUBLER STA 1210 LONG 52 DAMAGED. REPAIRED IAW SRM 53-40-00 FIGURE 20 VOL 1.

Part: FRAME — CRACKED (LT WING) · airframe 79,356 hrs · 32,223 cycles

ONE EACH CRACK .5 INCH LONG, ON LEADING EDGE FRAME LT WING AT XORS 372. REPAIR IAW SRM 57-20-00 FIG 1 VOL 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,356 hrs · 32,223 cycles

RIGHT AIR CONDITIONING COMPT LOWER BULKHEAD FOUND 1 EACH CRACK 0.5 INCH LONG ON WEB AT STA 540. REPAIR PER SRM 53-00-01 FIG 7-9 VOL 1.

Part: WEB — CRACKED (APU BAY) · airframe 79,356 hrs · 32,223 cycles

ONE CRACK 1 INCH LONG ON WEB INSIDE APU COMPT STA 2033. REPAIR CRACK IAW SRM 53-17-01 VOL 3 FIG 4, SRM 54-00-01 FIG 2B VOL 2, SRM 51-35-01 PG 1-13 VOL 2.

Part: LONGERON — CRACKED (FUSLEAGE) · airframe 79,356 hrs · 32,223 cycles

ONE CRACK 1 INCH LONG ON LONGERON INSIDE APU COMPT STA 2050. REPAIRED CRACK PER SRM 53-17-01 FIG 4 VOL 3, SRM 54-00-01 FIG 2B VOL 1, SRM 51-35-01 PG 1-13 VOL 2.

Part: FRAME — CRACKED (RT WING) · airframe 79,356 hrs · 32,223 cycles

ONE CRACK 0.5 INCH LONG ON FRAME SIDE RT WING AT STA XORS 623. REPAIRED CRACK IAW SRM 57-20-00 FIG 1 VOL 1.

Part: SKIN — CRACKED (NR 3 NACELLE) · airframe 79,356 hrs · 32,223 cycles

ONE EACH CRACK 1 INCH LONG ON EXTERNAL CORE COWL SKIN RIGHT SIDE ENGINE NR 3. REPAIR IAW SRM 54-10-00 FIG 16 VOL 1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,356 hrs · 32,223 cycles

AIR CONDITIONING COMPT RIGHT SIDE FOUND 6 EACH CRACKS 0.5 INCH LONG ON BULKHEAD SKIN STA 500. REPAIR PER SRM 53-30-00 FIG 6 VOL 1.

Part: FRAME — CRACKED (LT WING) · airframe 79,356 hrs · 32,223 cycles

ONE CRACK 0.25 INCH LONG INSIDE FRAME LEADING EDGE LT WING AT XORS 368. REPAIR CRACK IAW SRM 57-20-00 FIG 1 VOL 1.

Part: SKIN — CRACKED (ZONE 100) · airframe 76,885 hrs · 30,969 cycles

NR S 14 COMPLY WITH EA 8-5330-70980 FUSELAGE - PLATES AND SKIN - NEA6013 SKIN CRACK REPAIR AT STA 1154, LONGERON 38R. CLOSING ACTION ON 07/28/03 COMPLIED WITH EA 8-5330-70980.

Part: CLIP — CRACKED (ZONE 100) · airframe 76,885 hrs · 30,969 cycles

NR 359 LT FUSELAGE UPPER WING TO BODY SUPPORT RIB ATTACH ANGLES 2EA CRACKED AT STA 1361. CLOSING ACTION ON 07/20/03 REMOVED AND REPLACED BODY SUPPORT ATTACH ANGLES IAW SRM 53-31-01.

Part: CAP — CRACKED (FUSELAGE) · airframe 76,885 hrs · 30,969 cycles

COMPLY WITH EA 8-5310-70981. FUSELAGE MAINFRAME STA 595 TEE CAP CRACK REPAIR L39 LEFT AND RIGHT P/N NCA6044. CLOSING ACTION ON 07/28/03 COMPLIED WITH EA 8-5310-70981.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 76,885 hrs · 30,969 cycles

MAIN CARGO DECK SEAT TRACK LBL 48 STA 1441 TO 1541 HAS 7 EACH GOUGED AREAS. CLOSING ACTION ON 07/16/03 BLENDED OUT AREAS AND FOUND OUT OF LIMITS IAW SRM 53-70-00. REMOVED DAMAGED TRACK AND INSTALLED NEW TRACK IAW SRM 53-70-00. PARTS FAB ON TRAVELERS T2/348607, T2/348609, T2/348608.

Part: BRACKET — CRACKED (ZONE 600) · airframe 76,885 hrs · 30,969 cycles

NR 1010 RIGHT WING LOWER SPAR-TO-RIB FITTING IS CRACKED AT STA XORS 402 LWR SPAR S36. CLOSING ACTION ON 07/23/03, REMOVED BUTTERFLY BRACKET IAW SRM 51-33-01, INSTALLED NEW BRACKET IAW SRM 51-33- 01. TORQUE HI-LOCKS IAW SRM 51-31-01. SEALED IAW SRM 51-41-01.

Part: FLAP TRACK — CORRODED (ZONE 500) · airframe 76,885 hrs · 30,969 cycles

NR S 21 COMPLY WITH E.A.8-5750-70986A. WINGS-INBOARD FLAP-INBOARD TRACK SUPPORT BRACKETS CORROSION REPAIR. CLOSING ACTION ON 07/22/03 COMPLIED WITH EA 8-5750-70986A.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 76,885 hrs · 30,969 cycles

NR S-16 COMPLY WITH E.A.8-5750-70983. WINGS LEADING EDGE SLAT-NO-S SLAT TRAILING EDGE CRACK REPAIR. CLOSING ACTION ON 07/22/03 COMPLIED WITH E.A.8-5750-70983.

Part: SUPPORT — CORRODED (T/E FLAP) · airframe 76,885 hrs · 30,969 cycles

WINGS- LEFT OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM ARC2177. CLOSING ACTION ON 07/22/03. COMPLIED WITH EA 8-5740-70985. WINGS- LEFT OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 76,885 hrs · 30,969 cycles

MAIN CARGO DECK SEAT TRACK LBL 48 STA 1129 TO 1219 HAS 3EA GOUGED AREAS. CLOSING ACTION ON 07/20/03, REMOVED AND REPLACED SEAT TRACK 53-70-00. PARTS FAB ON TRAVELERS 348514,T2/348516,T2/348515.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,885 hrs · 30,969 cycles

MAIN CARGO DECK SEAT TRACK RBL 48 STA 1341 TO 1361 HAS CORROSION AROUND FASTENERS. CLOSING ACTION ON 07/16/03 REMOVED AND REPLACED SEAT TRACK AT RBL 48 STA 1341 TO 1361. PARTS FAB ON TRAVELER T2/348647, T2/348645, T2/348646. PARTS INSTALLED IAW SRM 53-70-00 AND M/M 53- 21-08-2.

Part: FLAP — DELAMINATED (RT WING) · airframe 76,885 hrs · 30,969 cycles

RIGHT INBOARD FLAP T/E DELAMINATED AS MARKED. CLOSING ACTION ON 07/20/03 REMOVED 4 EACH SECTIONS OF TRAILING EDGE IAW M/M 51-31-01. FABRICATED 4 EACH SECTIONS OF T/E ON TRAVELERS T2/347267, T2/347290, T2/347288. FABRICATED Z-ANGLE ON TRAVELER T2/347381. INSTALLED FOUR EACH SECTIONS OF T/E AND Z-ANGLE IAW SRM 57-20-00, PAINTED AREA IAW SRM 51-21-02.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 76,885 hrs · 30,969 cycles

COMPLY WITH EA 8-5750-70992. RT INBD FLAP UPPER SKIN REPAIR AT XIFH 279.360. CLOSING ACTION ON 07-23-03 COMPLIED WITH EA 8-5750-70992.

Part: SPLICE — DAMAGED (SEAT TRACK) · airframe 76,885 hrs · 30,969 cycles

NR S- 23 COMPLY WITH EA 8-5310-70987. FUSELAGE - MAINFRAME, MINOR DEVIATION TO SEAT TRACK SPLICE. CLOSING ACTION ON 07-23-03 COMPLIED WITH EA 8-5310-70987.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 76,885 hrs · 30,969 cycles

FORWARD PIT FLOOR PANEL DELEMINATED WITH CORROSION. RECEIVED PANEL AND FAB ON TRAVELER T2/351475 IAW DWG SRZ 25-005.

Part: CLIP — CRACKED (LT WING) · airframe 76,885 hrs · 30,969 cycles

LEFT WING LWR SPAR-TO-RIB FITTING IS CRACKED AT STA XORS 402 LWR SPAR S37. REMOVED CRACKED BUTTERFLY CLIP STA XORS 402 LWR SPAR S37 IAW SRM 51-33-01. INSTALLED NEW CLIP IAW SRM 51-33-01 SEALED IAW SRM 51-41-01.

Part: FITTING — CORRODED (ZONE 600) · airframe 76,885 hrs · 30,969 cycles

COMPLY WITH EA 8-5750-70979. WINGS - RT OUTBOARD FLAP - INBOARD HINGE LUG CORROSION REPAIR (P/N ARC19840 ENT BY: 60601C RPT BY: 60601C PLND: MECH:02 SPAN:0 D 02:00 PARTS: ENT BY:402783 17JUL03 14:38:47 S=S FACT 18JUL03 11:47 BFM U COMPLIED WITH EA 8-5750-70979 WINGS - RT OUTBOARD FLAP-INB'D HINGE LUG CORROSION REPAIR (P/N ARC 1984) ENT BY: 39017C RPT BY: 39017C CLOSED ON 07/18/2003 ON FEDEX NR S00012 ACCOMPLISHED AT MAE UNDER W/O NR 13414.

Part: HINGE — DAMAGED (TE FLAP) · airframe 76,885 hrs · 30,969 cycles

COMPLY WITH EA 8-5740-70982 LEFT I/B FLAP-HINGE ASSY ATTACHING LUG REWORK. CLOSING ACTION ON 07/17/03, ON N/R S00017. COMPLIED WITH EA NR 8-5740-70982, LEFT I/B FLAP-HINGE ASSY ATTACHING LUG REWORK.

Part: RIB — CRACKED (ZONE 300) · airframe 76,885 hrs · 30,969 cycles

TAILCONE , LT SIDE- INTERNAL RIB IS CRACKED, FWD END AT NR 2 RIB: 24 INCHES BELOW MAINT PLATFORM. ACCOMPLISHED AT MAE UNDER W/O NO.13414. FABRICATED REPAIR AND INSTALLED REPAIR IAW/SRM 53-00-01 FIG 10 REPAIR PARTS FABRICATED ON MAE TRAVELLER NO. T2/347292

Part: UNKNOWN — ODOR (COCKPIT)

CREW MADE AIR TURNBACK INTO MEM DUE TO ODORS AND OR FUMES. ALL HAZARDOUS MATERIALS REMOVED. INSP AC IN REF TO PART 1 SERVICE CK. RAN APU AND PACKS FOR 30 MIN. ALL PARAMETERS NORM. NO SIGN OF ODORS, FUMES OR SMOKE. OK FOR SERVICE.

Part: FITTING — WORN (NR 2 ENGINE) · airframe 71,874 hrs · 28,511 cycles

DURING A/C P-F CONV AT AERO WEAR WAS FOUND ON UPPER PORTION OF THRUST FITTING. PROBABLY CAUSED BY CONTACT WITH NR 2 ENG PRE-COOLER. THE AMOUNT OF WEAR IS NOT COVERED BY SRM 54-00. REPAIR REQUIRES INSTALL OF TWO NESTED REPAIR ANGLES FROM 0.063 THICK 6AL-4V ANNEALED TITANIUM AS PER FEDEX EA NR 8-5412-47997.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 71,874 hrs · 28,511 cycles

DURING A/C P-F CONV AT AERO CORROSION WAS FOUND ON UPPER SURFACE OF LWR DOOR JAMB CHORD, BS 1708. AMOUNT OF MATERIAL REMOVED IS NOT COVERED BY DC10 SRM 53-00-01 FIG 1A. REPAIR REQUIRES INSTALLATION OF RESTORATIVE STRENGTH INTERNAL ANGLE AS PER FEDEX EA NR 8-5315-47995.

Part: SKIN — GOUGED (LT WING) · airframe 71,874 hrs · 28,511 cycles

DURING A/C P-F CONV AT AERONAVALI SEVERAL GAUGES WERE FOUND ON LEFT LWR WING SKIN PNLS. AFT GOUGES WERE REMOVED BY BLENDING PER DC10 SRM 57-10-00, FIG 59 & 82. MANY IND WERE NO LONGER COVERED BY THE SRM LIMITS. REPAIR REQUIRES INSTALL OF TWO INTERNAL STRAPS COMMON TO WING STR 39 AS PER FEDEX EA NR 8-5730-47989.