N385FE

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 86,692 hrs · 36,234 cycles

DURING AN EMERGANCY LIGHT TEST, RECEIVED EMERGANCY LGHT BATTERY 1 LOW. REMOVED AND REPLACED THE POWER SUPPLY IAW MM 33-51-01-4. OPS GOOD.

Part: BRAKE — FAILED (NR 8) · airframe 86,428 hrs · 36,079 cycles

ON REMOVAL OF THE NR 8 TIRE, FOUND THE NR 8 BRAKE BEGINING TO DISINTEGRATE. EDGES OF BRAKE STACK FALLING APART AND CRACKED. REMOVED AND REPLACED THE NR 8 BRAKE ASSEMBLY IAW MM 32-43-01-4. OPS AND LEAK CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (L1 DOOR) · airframe 85,849 hrs · 35,747 cycles

CREW REPORTED L1 DOOR WOULD NOT OPEN WITH DOOR SWITCH. REMOVED AND REPLACED L1 DOOR ACTUATOR IAW AMM 52-11-01-2 AND OPS CHECKED IAW AMM 52-11-01-2.

Part: TRACK — UNSECURE (L1 DOOR) · airframe 85,833 hrs · 35,737 cycles

L1 DOOR STUCK HALFWAY OPEN AND WILL NOT MOVE NORMAL OR MANUALLY. DURING INSPECTION OF L1 DOOR, FOUND AFT TRACK WITH LOOSE HARDWARE. TIGHTENED HARDWARE IAW MM 52-10-01-6 AND 20-50-02-2. PERFORMED DOOR WARNING SYS OP CK PER B CHECK WORK CARD 52B7301 AND CHECKED ELECTRICAL INTEGRITY OF CIRCUIT PER WDM 52-11-01, OP CHECK GOOD. NO PARTS CHANGED DOOR OP`S CHECK GOOD AT THIS TIME. OK FOR SERVICE.

Part: DOUBLER — CRACKED (MLG WW) · airframe 85,630 hrs · 35,651 cycles

CENTER LANDING GEAR COMPARTMENT LEFT FORWARD SPOILER MIXER CONTROL ROD ACCESS CUTOUT SUPPORT DOUBLER FOUND CRACKED AT BS 1387. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1902-1947) · corrosion level 2 · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO FLOOR SUPPORT FOUND WITH CORROSION AT AT BS 1902 - 1947, X -2. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1821-1841) · corrosion level 2 · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO TRACK FLANGE FOUND CORRODED AT BS 1821 - 1841, X 27.5. CORROSION REMOVED AND FOUND EXCEEDED LIMITS OF SRM 53-70-00, FIGURE 5, VOLUME I. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1841-1871) · corrosion level 2 · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO TRACK FLANGE FOUND CORRODED AT BS 1841 TO 1871, X -8.5. CORROSION REMOVED AND FOUND EXCEEDED LIMITS OF SRM 53-70-00, FIGURE 5, VOLUME I. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1701-1721) · corrosion level 2 · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO TRACK FLANGE FOUND CORRODED AT BS 1701 - 1721, X 75.25. CORROSION REMOVED AND FOUND EXCEEDED LIMITS OF SRM 53-70-00, FIGURE 5, VOLUME I. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 85,630 hrs · 35,651 cycles

LEFT INBOARD ELEVATOR UPPER SKIN WAS DAMAGED. REPAIRED IAW EA 8-5520-T0329564 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1217) · corrosion level 2 · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO TRACK AT BS 1217, X = 75 FOUND CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-70-00, FIGURE 5, VOLUME I. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 85,630 hrs · 35,651 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT CORNER NR 13 SLAT TRACK. NR 10 CUTOUT, AFT INBOARD CORNER FOUND CRACKED APPROXIMATELY 1/4 INCH LENGTH AT XOS 659. REPAIRED IAW SRM 57-10-00 FIGURE 68 (SHEET 1) VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1626, RBL 27.5 RT, FOUND CORRODED. FOUND OUT OF LIMITS SRM 53-70-00, FIGURE 5, VOLUME I. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1528) · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1528, X -27.5 RT, FOUND WITH CORROSION. FOUND OUT OF LIMITS IAW SRM 53-70-00, FIGURE 5, VOLUME I. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1510) · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO COMPARTMENT CARGO TRACK AT BS 1510, LBL 8.5, FOUND WITH ELONGATED HOLE. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I AND REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 85,630 hrs · 35,651 cycles

MAIN DECK CARGO COMPARTMENT CARGO TRACK AT BS 1510, LBL 27.5 FOUND WITH ELONGATED HOLE. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I AND REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 85,630 hrs · 35,651 cycles

RIGHT WING FLAP OUTBOARD LOWER SURFACE FOUND DENT. REPAIRED IAW EA 8-5750-T0329572 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 85,630 hrs · 35,651 cycles

LEFT WING OUTBOARD FLAP UPPER SURFACE SKIN FOUND CRACKED. REPAIRED IAW EA 8-5750-T0329508 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DENTED (BS 1785) · airframe 85,630 hrs · 35,651 cycles

LOWER FUSELAGE SKIN AT STATION 1785 CENTER CARGO DOOR AFT JAMB 8 INCHES ABOVE SKIN SPLICE WITH DENT AT LONGERON 36 RIGHT. REPAIRED IAW EA 8-5320-T0317635C PART 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: WARNING SYSTEM — FALSE ACTIVATION (FIRE WARNING) · airframe 84,803 hrs · 35,209 cycles

GROUND POWER FAILED ABOUT 1 MINUTE AFTER SWITCHING OVER TO IT. HAD A FLASHING CARGO SWITCH INDICATION, A FIRE IN THE FWD COMPARTMENT. PHASE 1'S WERE DONE, CHECKLIST WAS RAN. ALSO HAD A SMOKE LIGHT ON FOR FWD CARGO COMPARTMENT, NO ODOR OR INDICATION OF A REAL FIRE. FIRE DEPARTMENT WAS CALLED. LOST VIA NR 1 IN THE PROCESS OF THE POWER FLUCTUATION. COMPLETED INSTALLATION & OPERATIONS CHECKS OF LOWER CARGO FIREX CONTAINER 1 IAW AMM 26-22-01-4. OPS CHECKED GOOD.

Part: SPOILER — LACK OF LUBE (WING) · airframe 84,368 hrs · 34,983 cycles

SPEED BRAKE ACTUATION CAUSES 20 DEGREE ROLL TO THE LT DURING DESCENT. NO ABNORMAL FORCES NOTED DURING OPERATION OR SPOILERS WHILE TURNING YOKE LEFT OR RIGHT. WHEN SPOILERS DEPLOYED, ALL DEPLOYED EVENLY. NO SPOILER FLOAT WAS NOTED. LUBRICATED SPOILER SECTORS, CLEANED AND LUBRICATED SPRING CARTRIDGES. ALL OPERATIONAL CHECK GOOD.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 839 hrs · 34,735 cycles

1R CABIN DOOR SLIDE LIGHT ON AT ALL TIMES. R&R R1 SLIDE ASSY REF MD10-10 MM 25-61-01-2. CHECKS OK.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 834 hrs · 34,446 cycles

ON TAKEOFF ROLL, PRIOR TO 60 KTS CABIN SMOKE ILLUMINATED. REF QRH NO SMOKE OR FIRE. NO CAUTION JUST LEVEL THREE OCCUR ON 9 SEPARATE OCCASIONS DURING TAXI IN. PERFORMED A MANUAL TEST OF THE MAIN CABIN SMOKE DETECTORS, OPERATIONS CHECKED GOOD. EXAMINED THE RETURN TO SERVICE, DISCRETE STATUS, INSERT A PAGE FOR VIA UNITS 1, 2, & 3. IAW FIM 26-15-00-2 ALL VIA'S DISCRETE STATUSES AGREE CHECKED GOOD. ACFT HAS DISPLAYED NO FAULTS AFTER BLOCK IN NEXT STEP IN FIM IS TO CHANGE.

Part: BOTTLE — DISCHARGED (PAX DOOR) · airframe 831 hrs · 34,274 cycles

RIGHT MAIN ENTRY DOOR BOTTLE DISCHARGED. SERVICED THE DOOR RESERVOIR IAW MM 52-11-07-2.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 82,847 hrs · 34,126 cycles

RECEIVED A LEVEL 3 ALERT CABIN SMOKE AFTER LANDING & DURING TAXI IN. CHECKED AIR SYNOPTIC & NOTICED 7 SMOKE DETECTORS ACTIVE. RAN EVAC CHECKLIST & BLEW CREW ENTRANCE DOOR 1L & SLIDE, EVACUATED ACFT. SHGN WITH GND POWER ON ACFT ALL UPPER CARGO DECK SMOKE DETECTORS WERE ILLUMINATED ON DU 4 & CABIN SMOKE ON OVERHEAD AIR PANEL WAS ILLUMINATED & CABIN SMOKE LEVEL 3 ALERT ON DU 3. THEN ALL INDICATION WENT NORMAL. CHECKED MSG NO CURRENT FAULTS. CHECKED FAULTS LAST LEG SHOWED 4 FAULTS, 1. CFDIU 2. DEU-1 3. DEU-2 & 4. DEU-3. PERFORMED RTS TEST ON MSC AIR DATA HEATERS, TEST PASSED. PERFORMED CARGO SMOKE TEST IAW MM 26-15-00-0, CHECKED NORMAL, NO FAULTS AT THIS TIME.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 82,842 hrs · 34,124 cycles

CABIN SMOKE ALERT APPEARED 3 TIMES DURING TAXI FOR TAKEOFF. R & R SMOKE DETECTORS AS PRECAUTIONARY. R & R DIODES, THEN RECHECKED DIODES AS REQUIRED FOR REASSURANCE OF PROPER OPERATION IAW AWD 26-15-01, ALL READINGS BETWEEN .506 TO .409. PERFORMED INSOLATION RESISTANCE CHECK FOR SMOKE DETECTOR SIGNAL WIRE FROM DETECTOR TO VIA-1, 2 & 3, ALL CHECKED GOOD. TOOK ACFT FOR A TAXI AROUND TO SIMULATE VIBRATION & TO OPERATIONS CHECK CABIN SMOKE ALERT FAULT. NO FAULTS APPEAR ON EAD OR AIR SYNOPTIC PAGE AT ANY TIME.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,840 hrs · 34,121 cycles

MAIN CABIN, APPROX STATION 1890 TO 2007 LBL 24, FLOOR SUPPORT IS CORRODED. R & R FLOORBEAM, PART WSP0711-556.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 82,840 hrs · 34,121 cycles

MAIN CARGO DECK SEAT TRACK AT BS 755, LBL 27, HAS A WORN LOBE. REPAIRED SEAT TRACK IAW SRM 53-70-00.

Part: HINGE — WORN (CARGO DOOR) · airframe 82,840 hrs · 34,121 cycles

LOWER FWD CARGO DOOR , FWD FUSELAGE HINGE 3 FWD LOBES WORN. INSTALLED THREE EACH, FABRICATED BUSHINGS IN FWD 3 LOBES IAW CMM 52-31-03.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 82,840 hrs · 34,121 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 8 HAS A WORN LUG & LOBE. REPLACED SEAT TRACK SECTION AT STATION 755, RBL 8 WITH NEW SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A VOL II.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 82,840 hrs · 34,121 cycles

MAIN DECK SEAT TRACK AT BS 755 LBL 47 APPROX, HAS A BROKEN LUG. R & R SEAT TRACK AT MAIN DECK BS 755 LBL 47 IAW SRM 53-70-00 FIG 11 VOL I.

Part: INLET — DELAMINATED (NR 2 ENGINE) · airframe 82,840 hrs · 34,121 cycles

NUMBER 2 ENG INLET LT SIDE PANEL 363EL IS DELAMINATED AT FWD & AFT EDGE. PANEL BEYOND REPAIR. REPLACED WITH SERVICEABLE PANEL.

Part: PANEL — DELAMINATED (RT HORIZ STAB) · airframe 82,840 hrs · 34,121 cycles

RIGHT HORIZONTAL PANEL 344EB IS DELAMINATED. REPAIRED RT HORIZONTAL PANEL 344EB IAW SRM 51-71-00 VOL 2.

Part: PANEL — DELAMINATED (WING) · airframe 82,840 hrs · 34,121 cycles

RIGHT HORIZONTAL PANEL 344DB HAS DELAMINATION AT PREVIOUS REPAIR ON CTR SECTION. REPAIRED RT HORIZONTAL PANEL 344DB IAW SRM 51-71-00 VOL II. PREP & PAINTED SRM 51-21-00 VOL II.

Part: PANEL — DAMAGED (RT WING) · airframe 82,840 hrs · 34,121 cycles

RIGHT WW PANEL ARC0280, OTBD OF ACCESS 641 AB, DELAMINATED ON UPPER SURFACE INTERNAL TO WW. PANEL DAMAGED BEYOND ECONOMIC REPAIR, REPLACED WITH SERVICEABLE PANEL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,840 hrs · 34,121 cycles

AFT CGO COMPARTMENT STATION 1950 LT FLOOR LINE ABOVE L48 UNDERSIDE ANGLE HAS EXFOLIATION CORROSION. REMOVED ANGLE FROM AFT CGO COMPARTMENT. FABRICATED ANGLE & INSTALLED ANGLE IAW SRM 51-33-01 VOL 2.

Part: PANEL — DELAMINATED (NR 2 NACELLE) · airframe 82,840 hrs · 34,121 cycles

RAMP PANEL DELAMINATED RT SIDE NR 2 ENG. R & R.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 82,840 hrs · 34,121 cycles

MAIN DECK SEAT TRACK AT BS 755, RBL 8 HAS A WORN LUG & LOBE MARKED DOT 3. REMOVED A SECTION OF SEAT TRACK AT LOBE DAMAGE. REPLACED SEAT TRACK WITH NEW SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A VOL 2.

Part: SKIN — WORN (NR 2 NACELLE) · airframe 82,840 hrs · 34,121 cycles

NUMBER 2 ENG LOWER RT AFT PICKLE BARREL SECTION, PANEL WORN THROUGH AT APPROX 5:30 POSITION, FWD OF CSD, MARKED. REMOVED DAMAGED SKIN SECTION BELOW PREVIOUSLY, ACCOMPLISHED SPLICE REPAIR IAW SRM 51-31-01 VOL 2. FABRICATED REPLACEMENT SKIN SECTION IAW SRM 54-10-00 FIG 20 VOL 1. MATERIAL USED 2024-T3 .063, INSTALLED NEW SKIN IAW SRM 54-10-00 FIG 20 VOL 1 & PAINTED IAW SRM 51-21-01 VOL 2.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 82,840 hrs · 34,121 cycles

LEFT WING OTBD FLAP INBD SIDE PANEL 536DR IS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: SKIN — CRACKED (ZONE 600) · airframe 82,477 hrs · 33,901 cycles

FOUND RT WING FIXED LE CRACKED, ONE INCH INBD OF NR 1 SLAT TRACK COVER. BLEND AREA. CUT OUT DAMAGE & VERIFIED CRACK WAS REMOVED IAW SRM 57-10-00 FIG 68. PERFORMED HFEC OF CUT OUT IAW NTSPM 06-10-01010, NO DEFECTS NOTED. REPAIRED IAW EA 8-5730-T0308722

Part: DOOR — MISSING (NR 1 NACELLE) · airframe 80,497 hrs · 32,807 cycles

NR 1 ENGINE PYLON FORWARD FAIRING INBD AFT BLOWOUT DOOR MISSING. PERFORMED DECAY PRESSURE CHECK IAW MM 36-00-01-5, NO LEAKS OR OTHER DEFECTS NOTES. REPLACED MISSING PRESSURE RELIEF DOOR IN REF SRM 51-30-01 AND COMPLIED WITH EA 8-5410-164823, PART 3 (NO 1 ENG PYLON PRESSURE RELIEF DOOR MISSING) OK FOR SVC. WHILE REPLACING DOOR ADJUSTED BENT CATCH AND CHECKED GOOD.

Part: SPAR — DAMAGED (NR 3 PYLON) · airframe 80,398 hrs · 32,756 cycles

NR 3 ENG PYLON UPPER SPAR WEB HAS NUMEROUS LOOSE HARDWARE ON LT AND RT SIDES FROM STA YN-342 THRU STA YN-417. REF TO DUPLICATED NR 473 AND NR 653: NR 3 ENG PYLON UPR SPAR WEB MISSING/LOOSE HARDWARE(MARK). NR3 ENG PYLON INB'D SIDE UPPER PYLON SPAR CAP ANGLE HAS 13 EA SHEARED FASTENERS. COMPLIED WITH HOLE DIMENSIONS TO 1ST OVERSIZE OF .265 IAW SRM 51-32-01 FIG.2 AND SRM 54-20-00 TABEL 1 SHOWN ON MAPPING SHEET. REPLACED LOOSE BOLTS IAW SRM 54-20-00 & 51-32-01 AS SHOWN ON MAPPING FWD R/H SIDE ALL 7 AND AFT RT SIDE 2 FASTNERS, AFT LT SIDE 9. REPLACED ALL REMAINING LOOSE FASTNERS SHOWN ON MAPPING IAW SRM 54-20-00 & 51-32-01.

Part: SPAR — CRACKED (WING) · airframe 80,398 hrs · 32,756 cycles

FOUND A 2.5 INCH CRACK ON THE WING REAR SPAR TO WW LT BULKHEAD AT ATTACHMENT TEE ANGLE ON THE UPPER END. R & R APB7078-1 FITTING IAW DWG NPB6066 AND SP10570007.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 79,050 hrs · 32,057 cycles

AFTER DEPARTURE, LT MLG RED LIGHTS REMAINED ILLUMINATED, COMPLIED WITH QRH CHECKLIST, WHEN ACFT SLOWED TO 210 KIAS RED LIGHT EXTINGUISHED. ALL OTHER INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. FOUND LEFT MAIN GEAR RETRACT ACTUATOR LEAKING HYD FLUID. REPLACED RETRACT ACTUATOR REF AMM 32-33-01-4. WHILE T/S FOUND LT MLG WHEELS CONTACTING AND BINDING WITH GEAR DOOR AND STOPPING GEAR FROM FULL RETRACTION INTERMITTANTLY, REMOVED AND REPLACED LT MLG DOOR WITH CORRECT CONFIGURED DOOR PER MD10-10 AMM 32-14-01-2. ACCOMPLISHED MLG EXTENSION AND RETRACTION ADJUSTMENT TEST PER AMM 32-30-00-5. NO DEFECTS NOTED. OK FOR SERVICE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 78,261 hrs · 31,647 cycles

LT WHEEL WELL INBD VERTICAL ANGLE AEA0499-1 SHOWS SIGNS OF CORROSION. REMOVED CORROSION ON LT WHEEL WELL INBD VERTICAL ANGLE IAW SRM 51-21-00.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,261 hrs · 31,647 cycles

RT WHEEL WELL REAR SPAR SHOWS CORROSION ON RT END OF APB7080-2 CAP. REPAIRED DAMAGED AREA. REF MD10 SRM VOL I 53-40-00 FIG 11

Part: VERTICAL SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,261 hrs · 31,647 cycles

RT WHEEL WELL FWD BULKHEAD SLANT PANEL VERT FRAME AT THE LOWER OTBD CORNER HAS EVIDENCE OF CORROSION. RT WHEEL WELL FWD BULKHEAD SLANT PANEL VERTICAL FRAME WAS R & R.

Part: SPAR CAP — CORRODED (ZONE 100) · airframe 78,261 hrs · 31,647 cycles

LT WHEEL WEEL REAR SPAR CAP ANGLE SHOWS SIGNS OF CORROSION ON INBD AND OTBD ENDS OF ANGLE, APB7080-1. REMOVED CORROSION ON LT WHEEL WELL REAR SPAR CAP ANGLE IAW SRM 51-21-00.

Part: STRUCTURE — CORRODED (LT MLG WW) · airframe 78,261 hrs · 31,647 cycles

LT MLG WHEEL WELL OTBD VERTICAL TEE, AEA0474-1, SHOW SIGNS OF CORRSION. REMOVED CORROSION ON LT MLG WHEEL WELL OTBD VERTICAL TEE IAW SRM 51-21-00.

Part: SKIN — DENTED (BS 840-859) · airframe 77,776 hrs · 31,410 cycles

LOWER FUSELAGE STA 840 TO STA 859, STR 49L FOUND SKIN DENT. DAMAGED SKIN AREA AT LOWER FUSELAGE STA 840 TO STA 859 TRIMMED AT STA 840 TO STA890 LONG 49L AREA AS PER SRM 53-20-00 FIG 6 VOL I REVISION 96. REPAIRED DOUBLER AND FILLER FABRICATED AND INSTALLED AS PER SRM 53-20-00 FIG 6 VOL I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 77,776 hrs · 31,410 cycles

DURING HFEC OPEN HOLE FOUND 3 EA CRACK INDICATIONS ON RT WING, XORS 345.750. REAR SPAR LOWER CAP. REF TO EO 8-5710-7-5007A, PART 2. CRACKED INDICATION FASTENER HOLES (HOLES 'A', 'B', 'C') REPAIRED AS PER EA 8-5710-143772. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CORRODED (BS 1401 S29L) · airframe 77,776 hrs · 31,410 cycles

LOWER FUSELAGE STA 1401, STR 29L, LONGERON FOUND CORRODED. LOWER FUSELAGE STA 1401, STR 29L LONGERON CORROSION REPAIRED IAW SRM 53-10-10, FIG 2A, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: LONGERON — CORRODED (BS 1341-1381) · airframe 77,776 hrs · 31,410 cycles

LOWER FUSELAGE STA 1341 TO STA 1381, STR 29 LONGERON SEVERAL AREAS FOUND CORRODED. CORROSION REPAIRED AS PER SRM 53-10-00 FIG 2A VOL I REVISION 96. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CORRODED (BS 1370 S31L) · airframe 77,776 hrs · 31,410 cycles

LOWER FUSELAGE STA 1370, STR31L LONGERON SEVERAL AREAS FOUND CORRODED. CORROSION REPAIRED AS PER SRM 53-10-00 FIG 2A VOL I REVISION 96. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (BS 1721-1731) · corrosion level 2 · airframe 77,776 hrs · 31,410 cycles

CABIN LT STA 1721 TO 1731 X=27.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1711 TO STA 1751 X=27.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 111.

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 77,776 hrs · 31,410 cycles

DURING HFEC OPEN HOLE FOUND 1 EACH CRACK INDICATION ON LT WING, XORS 345.750 REAR SPAR LOWER CAP. REF TO EO 8-5710-7-5007A PART 1. EACH CRACK INDICATION ON HOLE 'C' LT WING XORS 345.750 REAR SPAR LOWER CAP. REPAIRED PER EA 8-5710-143775 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — DAMAGED (ZONE 100) · airframe 77,776 hrs · 31,410 cycles

FWD CARGO DOOR JAMB-AFT EDGE FOUND WITH SLIGHT DAMAGE. FORWARD CARGO DOOR JAMB - AFT EDGE FOUND WITH SLIGHT DAMAGE. REPAIRED AS PER SRM 53-50-00 FIG 26 SHEET 1 REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: FLOORBEAM — CORRODED (BS 1841) · airframe 77,776 hrs · 31,410 cycles

AFT CARGO RT FLOOR PANEL SUPPORT AT APPROX STA 1841 SUPPORTING FWD EDGE OF FLOOR PANEL NR 187HF FOUND CORRODED. AFT CARGO RIGHT HAND FLOOR PANEL NUMBER 187HF STA 1841 X=-34 TO X=-90 SUPPORT REPAIRED AND INSTALLED AS PER SRM 53-00-01 FIG 8 VOL I REV 96. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 111.

Part: SKIN — CRACKED (LT WING) · airframe 77,776 hrs · 31,410 cycles

LT WING L/E SLAT TRACK NR 12 LOWER CUTOUT OTBD AREA CRACKED APPROX .5 INCH. 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: LONGERON — CORRODED (BS 1361 L30L) · airframe 77,776 hrs · 31,410 cycles

LOWER FUSELAGE STA 1361, STR 30L, LONGERON FOUND CORROSION. LONGERON TRIMMED IAW SRM 53-10-00, FIG 5, VOL I, REV 96. NEW LONGERON SEGMENT FROM STA 1302 TO STA 1411.5 FABRICATED IAW DWG AEA 0702 REV NC AND INSTALLED IAW SRM 53-10-00, FIG 5, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: LONGERON — CORRODED (BS 1410-1440) · corrosion level 2 · airframe 77,776 hrs · 31,410 cycles

LOWER FUSELAGE STA 1410 TO STA 1440, STR30L, LONGERON FOUND EVIDENCE OF CORROSION (04 EACH). LONGERON REPAIRED AS PER EA 8-5310-143459. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (RT WING) · airframe 77,776 hrs · 31,410 cycles

RT WING NR3 LEADING SLAT ANTI-ICE DUCT UPPER INBD CUTOUT CRACKED APPROX .5 INCH. CRACKED AREA REPAIRED AS PER EA 8-5710-143448. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (RT WING) · airframe 77,776 hrs · 31,410 cycles

RT WING TIP UPPER SURFACE APPROX 13 INCH FROM TIP AND 41 INCH FROM AFT, FOUND CRACKED. SKIN SURFACE TRIMMED AND REPAIR CARRIED OUT AS PER EA 8-5730-143465. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (LT WING) · airframe 77,776 hrs · 31,410 cycles

LT WING NR 3 LEADING SLAT ANTI-ICE DUCT UPPER OTBD CUTOUT CRACKED APPROX .5 INCH. CRACKED AREA TRIMMED AND REPAIR CARRIED OUT AS PER EA 8-5710-143447. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: UNKNOWN — SMOKE (CABIN) · airframe 75,913 hrs · 30,486 cycles

VISIBLE SMOKE ERUPTED FROM THE CABIN VENTILATION SYSTEM AT FL 340, APPROXIMATELY 1 HR. INTO FLIGHT. THE AIR SYNOPTIC INDICATED HIGHER THAN NORMAL TEMP IN THE COURIER DUCT. NO OTHER ABNORMAL INDICATIONS OTHER THAN THE ODOR AND THE SMOKE INSPECTED AND REPLACED NR 1, 2, AND 3 COALESER BAGS PER MM 21-54-03-2, COALESER BAGS WERE NOT CONTAMINATED(NO OIL RESIDUE). CHECKED APU LOAD CONTROL VALVE FOR CONTAMINANTS PER MM49-00-00-2, NO CONTAMINANTS. PERFORMED PACK BURNOUT PROCEDURE PER TAFI 21-50-00"V". RAN ALL THREE PACKS PER DC10-10 MM 21-53-01-2 REF EA 8-2150-61080.ALSO RAN ALL THREE PACKS TOGETHER AND SEPERATELY WITH EACH ENGINE. UNABLE TO DUPLICATE THIS CONDITION AS WRITTEN.

Part: CONTROL UNIT — FAILED (ANTI SKID SYS) · airframe 75,889 hrs · 30,473 cycles

RECEIVED A LEVEL 2 "ANTI SKID FAIL" ALERT FOLLOWING LANDING GEAR EXTENSION. EXECUTED A GO AROUND & COMPLIED WITH QRH. GOT GOOD ANTI-SKID TEST .ON LANDING ROLLOUT THE LEFT BRAKES WERE SENSITIVE & APPEARED TO HAVE LOCKED UP MOMENTARILY. AFTER BLOCK-IN, LEFT BRAKES (NR 1, 2, 5, 6) WAS 292 DEG, 236 DEG, 282 DEG, 279 DEG, RT SIDE IN 170'S INTERROGATED MCDU AND FOUND ASCU FAULTED ON LAST 3FLT LEGS. SUSPECT BAD ASCU.

Part: THROTTLE — BINDING (NR 2) · airframe 75,596 hrs · 30,331 cycles

ON DESCENT NR 2 THROTTLE WAS BINDING AND WOULD NOT RETARD TO IDLE POSITION UNTIL TOUCHDOWN. REMOVED AND REPLACED NR 2 ENGINE THROTTLE PUSH PULL CABLE.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 75,059 hrs · 30,084 cycles

"SLAT DISAG" LEVEL 2 ALERT ON FINAL SELECTING FLAPS 35 DEGREES. WENT AROUND RAN QRH AND ACCOMPLISHED FLAPS 22 LANDING CHECKED FOR PREVIOUS HISTORY OF 99 DAYS FOUND NO INDICATION OF RECURRING PROBLEM. PERFORMED OPERATION AND FUNCTION TEST REF AMM 27-80-00-2. NO DEFECTS WERE NOTED DURING GROUND OPERATION OF FLAP/SLAT SYSTEM RETURNED ACFT TO NORMAL CONFIGURATION ACFT OK TO CONTINUE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 73,266 hrs · 29,289 cycles

ON ARRIVAL IN KAFW, TOOK BIRDSTRIKE IN RT WINDSHIELD, SHATTERED OUTER PANEL. DECLARED EMERGENCY, LANDED UNEVENTFUL AFW FOUND RIGHT WINDSHIELD OUTER PANEL SHATTERED. NEEDS CHANGED OUT. REMOVED AND REPLACED RIGHT WINDSHIELD PER MM 56-11-00-2. SEE OIL 56-10/9049 FOR MISC SEALANT APPLICATION, P/N NBA6045-502.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 72,266 hrs · 28,797 cycles

RT PRIMARY STATIC PORT HAS SKIN MISMATCH GREATER THAN .006 IN 3 EA AREAS OF THE CONTROLLED AREA. MISMATCH MEASUREMENTS WERE .013, .020, .023 REPAIRED AREA IAW SRM 53-20-00 VOL 1 FIGURE 9. ATTENTION RECORDS REPAIR IS A CATEGORY B REPAIR WHICH REQUIRES REPETITIVE INSPECTION AS FOLLOWS DAMAGE CAT B, TOLERANCE INSPECTION REQUIREMENT, INITIAL 34,00, REPETITIVE 23,000 REPLACEMENT N/A.

Part: COMPUTER — MALFUNCTIONED (NR 2 FCC) · airframe 70,272 hrs · 27,933 cycles

ON DESCENT INTO ORD SPOILERS DEPLOYED -HARD RT ROLL- STOWED SPOILERS - CYCLED SPOILERS ROLL WENT - ON APPROACH SELECTED FLAPS 35 GOT SLAT DISAGREE LIGHT AND WHITE SPOILER LIGHT - WENT AROUND - ON LEVEL OFF ON EITHER AP A/C ROLLED HARD RIGHT A/P DISCONNECTED. HAND FLOWN APPROACH CENTRAL FORCES NORMAL. FCC2 FAILED RTS TEST. REPLACED FCC2 PER MD-10-10 M/M 22-01-03-4. FCC2 PASSED RTS. CHECKED OPERATION OF SPOILER POSITION TRANSMITTERS PER MD-10-10 M/M 27-66-01-2. SPOILER INDICATION NORMAL.

Part: SWITCH — FAULTY (COCKPIT) · airframe 67,897 hrs · 26,877 cycles

ON APPROACH TO LAND, LOWERED LANDING GEAR AND DID NOT GET DOWN AND LOCKED ON ANY GEAR JUST 3 RED INDICATIONS. GRABBED GEAR HANDLE AND CHECKED FOR LOCKED DOWN HANDLE, THEN JIGGLE HANDLE, NO HELP. CYCLED LANDING GEAR AND AGAIN GOT 3 RED INDICATIONS. HYDRAULICS WERE GOOD, CHECKED HANDLE FOR SECURITY AND STILL NO GREEN LIGHTS (EITHER SD OR LIGHTS). HIT THE HANDLE HARD WITH FIST AND INSTANTLY GOT 3 GREEN INDICATION. REMOVED AND REPLACED S1-431 LANDING GEAR HANDLE SWITCH, OPS CHECKS OK PER MM 32-31-02-2 AND SUPP 32-60-00-0 PAR 11.

Part: FUEL FILTER — FAILED (APU) · airframe 67,792 hrs · 26,822 cycles

"ENG 1 FUEL FILTER" LEVEL 1 ALERT ILLUMINATED APPROX 1 30 AFTER TAKEOFF. APPROX 40 MIN AFTER "1 ENG FUEL FILTER LIGHT CAME ON, THE LEVEL 2," FUEL CONTAMINATED" ALERT CAME ON , DIVERTED TO STL. REMOVED ALL THREE ENGINE FUEL FILTERS. FOUND ALL CONTAMINATED. REPLACED ALL 3 ENGINE FUEL FILTERS, MEC'S, ENGINE FUEL PUMPS, FUEL DIFFERENTIAL PRESSURE SWITCHES. REPLACED APU FUEL FILTER. DEFUELED AND ENTERED ALL 3 FUEL TANKS. CLEANED SAME. ALL COMPONENTS RIGGED, ADJUSTED AND LEAK CHECKED PER APPROPRIATE MAINTENANCE MANUAL. PERFORMED SATISFACTORY TEST FLIGHT DUE TO ALL THREE ENGINE WORK. RETURNED AIRCRAFT TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (WINDSHEAR) · airframe 67,780 hrs · 26,817 cycles

ON DEPARTURE OUT OF ONT AT APPROX 1000 AGL, GOT A TAIL WINDSHEAR ALERT. WENT TO FIREWALL. NO OVERSPEED. DUMPED FUEL. DIVERTED TO LAX. NO ENGINE EXCEEDANCE'S REPORT ON ACARS NOR AIU'S. PERFORMED POSSIBLE TAIL STRIKE INSPECTION AND FLIGHT CONTROL INSPECTION. PULLED FIGHT RECORDER AND VOICE RECORDER PER FLIGHT SAFTEY. PERFORMED INSPECTION 05-51-12-6 PART 2 A CK AND HARD LANDING SECTION A AND B WITH NO DEFECTS NOTED. FLIGHT CONTROL CK PER MM 27-00-0-2, ALL CK PASSED AS REQUIRED. REMOVED AND REPLACED FLIGHT DATA RECORDER PER FLIGHT SAFETY. SYSTEM OPS CHECK GOOD IAW MD10 MM 31-31-01-2. RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (E/E BAY) · airframe 67,672 hrs · 26,761 cycles

FWD LOWER CARGO SMOKE ALERT DURING FLT, EXTINGUISHED 2 FIRE AGENTS. AFTER 1ST BOTTLE DISCHARGED THE ALERT EXTINGUISHED, DID NOT NOTICE WHICH DETECTOR IN FWD CARGO CAUSED ALERT. IN PROGRESS OF REPLACING BOTH FIRE EXTING BOTTLES AND SQUIBS, ALSO WILL REPLACE ALL 4 FWD CARGO SMOKE DETECTORS. AFTER COMPLETION SYSTEMS NEED TO BE OPS CHECKED PER MM. REMOVED AND REPLACED MSC PRECAUTIONARY OPS CHECKS GOOD PER M/M 31-42-00. REMOVED AND REPLACED NR 2 FIREX BOTTLE AND CARTRIDGE PER M/M 26-22-01-4 AND 26-22-03-4. OPS CHECKS GOOD.

Part: SKIN — GOUGED (ZONE 100) · airframe 64,918 hrs · 26,194 cycles

FORWARD LOWER CARGO COMPARTMENT, AFT LOWER END OF DOOR CUTOUT SKIN IS GOUGED. REMOVED DAMAGED IAW DC10/MD10 SRM 53-50-00 VOL 1, FABRICATED REPAIR IAW DC10/MD10 SRM 53-50-00 VOL 1, INSTALLED REPAIR IAW DC10/MD10 SRM 53-50-00 VOL 1.

Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 67,129 hrs · 26,490 cycles

PERFORMING REPAIR PROVIDED BY SB 55-16, INTERESTED PANEL HAS BEEN CUT OVER THE LAYOUT TRIM LINE REQUIRED. DAMAGED SKIN PANEL PORTION REPLACED AND SPLICED TO EXISTING SKINS IAW FEDEX EA 8-2740-75698 (REF FEDEX NRC N0747, N0940).

Part: RIB — CRACKED (ZONE 500/600) · airframe 67,129 hrs · 26,490 cycles

RIGHT AND LEFT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED, REPAIR ANGLE AND DOUBLER INSTALLED TO RESTORE STRENGTH IAW FEDEX EA 8-5710-75729 (REF FEDEX NRC N0732, N0626).

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 67,129 hrs · 26,490 cycles

CRACK FOUND IN THE LT WING UPPER CAP AT RIB STATION XORS 402. THE CRACK IS ALL WAY THRU THE CAP AND IS LOCATED IMMEDIATELY FORWARD OF STRINGER 15. CRACKS ROUTED AND EXTRUDED REPAIR ANGLE INSTALLED IAW FEDEX EA 8-5710-75730 (REF FEDEX NRC N0625).

Part: SKIN — CRACKED (ZONE 300) · airframe 67,129 hrs · 26,490 cycles

HORIZONTAL STABILIZER CONSTANT SECTION UPPER AND LOWER SKIN CRACKED WITHIN FLYABLE LIMITS. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510- 73244. PARTS AFFECTED: ALC7204-1, ALC7205-1, ALC7441-2.

Part: LINE — DAMAGED (LEFT WING SLAT) · airframe 65,806 hrs · 25,882 cycles

SYSTEM 1 HYD QUANTITY DROPPED BELOW 1 GALLON. NR 1 HYD PRESSURE AND TEMP REMAINED FINE. COMPLETED ACTIONS PER QRH. EVIDENCE OF HYD LEAK AT WINGROOT ON LT WING. MX TO BEGIN T/S. FOUND LEAK ON LEFT WING L/E SLAT PIPING (ITEM 720) REF 27-82-24-02 FIG 2 AT BEND. REMOVED 9 IN PIECE OF PIPING AND REPLACED NEW SECTION PER MM 20-10-01-2, LEAK CHECK GOOD. SERVICED SYS 1 HYD SYS PER 12-13-02-3, OK FOR RETURN TO SERVICE.

Part: CONNECTOR — BURNED (BOOST PUMP) · airframe 64,637 hrs · 25,322 cycles

NR 1 FUEL TANK AFT BOOST PUMP POS, CONNECTOR IS BURNED. R&R WIRE HARNESS & BOOST PUMP HOUSING PER MM 28-22-01-02.

Part: CONNECTOR — BURNED (BOOST PUMP) · airframe 64,637 hrs · 25,322 cycles

NR 1 FUEL TANK AFT BOOST PUMP CONNECTOR IS BURNED. R&R BOOST PUMP PER MM 28-22-01-2, OPS CHECK NORMAL.

Part: WARNING LIGHT — FALSE INDICATION (COCKPIT) · airframe 63,220 hrs · 24,650 cycles

DURING CLIMBOUT AFTER FLAPS/SLAT HANDLE RAISED, DISAGREE LIGHT ILLUMINATED. INSPECTED SLATS/FLAPS, NO DEFECTS FOUND. OK FOR SERVICE.

Part: FUEL CONTROL — SLUGGISH (NR 2 ENGINE)

UPON ROTATION NR 2 FUEL FLOW AROUND 5000. 1 & 3 10000 F/F N1 33 PERCENT, N2 97 PERCENT EGT 700. AC WOULD NOT CLIMB, VERY SLUGGISH.

Part: FITTING — MISSING (LT TE FLAP)

SNRM 764 - LT WING O/B FLAP, I/B OF O/B FLAP VANE ATTACH FITTINGS TO VANE TRACK IS MISS 4 ATTACH BOLTS. REMOVED ALL BOLTS WITH NEW PER MM 27-50-03-2. ENCAPSULATED ALL BOLTS AND NUTS WITH SEALANT PER MM 57-10-00. OK FOR SERVICE.

Part: TARGET — INOP (RT MLG)

WHEN GEAR RAISE AFT TO, RMG REMAIN RED. COMPLIED WITH RED TAB CK LIST RECYCLING GEAR STILL HAD BOTH RT MAIN RED LIGHT WITH GEAR HANDLE UP. REMOVED AND REPLACED TARGET PER MM 32-61-03-2 RF EA 8-3260-47519. AC OK FOR SERVICE.

Part: TARGET — MISSING (LT MLG)

99-122 - AFT T/O DFW LEFT GEAR UNSAFE LIGHTS REMAIN ON BOTH PNLS, RAN RED TABS RETURN DFW. FOUND TARGET MISSING. REPLACED TARGET AND CHECKED REF MM 32-34-03-2 AND EA 8-3260-45056. OPS TEST GOOD. OK FOR SERVICE.

Part: HANDLE — DIRTY (LANDING GEAR)

LANDING GEAR DID NOT COME DOWN WITH THE HANDLE DOWN. WENT AROUND THEN GEAR CAME DOWN (FROM HANDLE DOWN TO GEAR DOWN WAS 3 MIN). PERF A/C GEAR SWING RETRACT AND EXTENSION CKS, GEAR OPS CK OK. A/C GEAR EXTENSION TIME FROM HAND DOWN TO 3 GREEN DOWN AND LOCK 19.85 SEC. CLEAN GEAR HANDLE SLIDE TO PREVENT HANDLE STICK, CAUSING GEAR LIGHT TO STAY RED. GEAR HANDLE OPS CK OK.