N320FE

Part: WARNING MESSAGE — ILLUMINATED (BLEED SYSTEM) · airframe 104,239 hrs · 31,665 cycles

LEVEL 1 AIR SYS 3 OFF ILLUMINATED FOURTEEN MINUTES INTO FLIGHT AT FL 280. ASSOCIATED BLEED (3) AND PACK (3) OFF. RED DUCT LINE ILLUMINATED ON AIR SYNOPTIC. COMPLIED WITH QRH. REF MM 36-00-01-5, PERFORMED DECAY CHECK OF #3 PNEUMATIC SYSTEM, DECAY CHECK PASSED AT 14 SECONDS FROM 20 PSI TO 15 PSI. MANIFOLD DETECTION CONTROL UNIT INDICATED NO WHITE BIT BALLS. PSC 3, MSC, AIU'S, VIA'S INDICATED NO CURRENT FAULTS SHOWED FOR CURRENT FLIGHT LEG. DUE TO HISTORY, IAW FIM 36-23-00-2-0. REMOVED AND REPLACED NR 3 AIU AS PRECAUTION. RTS PASSED ALONG WITH AIR SYSTEM TEST. NO FURTHER FAULTS FOUND. AIRCRAFT OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 3 AIR SYSTEM) · airframe 104,148 hrs · 31,618 cycles

LVL 1 AIR SYS OFF ALERT. AIR SYS AUTOMATICALLY SHUT OFF NR 3 BLEED AND NR 3 PACK. NR 3 DUCT WENT MOMENTARILY RED PRIOR TO AUTO SHUTDOWN OF NR 3 AIR SYS. CHECKED PNEUMATIC MANIFOLD FAULT INDICATOR IN CAC. NO FAULT BALLS ARE ILLUMINATED. CHECKED AIU'S, PSC'S AND THE MSC. THERE WERE NO FAULTS PERTAINING TO THE NR 3 PNUEMATIC SYS. PERFORMED DECAY CHECK WITH APU IAW AMM 36-00-01, DECAY CHECK PASSED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 104,078 hrs · 31,580 cycles

EMER LT BAT 1 LOW ON PREFLIGHT PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MD-10-30 AMM 33-50-00-5-0. OPS CHECK GOOD; OK FOR SERVICE.

Part: BATTERY — LOW VOLTAGE (NR 1) · airframe 104,078 hrs · 31,580 cycles

EMER LIGHT BAT 1 LOW ON PREFLIGHT.

Part: CONTROL MODULE — FAILED (TE FLAPS) · airframe 104,059 hrs · 31,570 cycles

ON APPROACH SLATS EXTENDED, FLAPS WOULD NOT MOVE, HANDLE STUCK. EXECUTED A GO AROUND. SPENT SOME TIME WIGGLING THE HANDLE AND DIAL- AND-FLAP AND FINALLY GOT THEM TO MOVE. AFTER LANDING CLEANED UP THE WING AND ATTEMPTED TO EXTENDED FLAPS AGAIN . HANDLE STUCK ONCE AGAIN. PERFORMED FUNCTIONAL TEST OF FLAP/SLAT CONTROL MODULE IAW AMM 27-51-01-2-0. INSPECTED THE FLAP MECHANICAL CONTROL CABLES FOR DEBRIS OR ANY TYPE OF OBSTRUCTION, NO DEFECTS FOUND IAW AMM 27-51-00-6. ACFT OK TO CONTINUE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,318 hrs · 31,184 cycles

CORROSION ON NUT PLATES FOR FLOOR ATTACHMENTS, AFT CARGO COMPARTMENT AT STA 1902. REMOVED CORROSION IAW SRM 53-00-01 VOL II. ORIG THICKNESS 0.063". AFTER REWORK 0.045". OUT OF LIMITS. FABRICATED ANGLE ON T19/1450803. INSTALLED ANGLE IAW SRM 51-31-01 VOL I. REPAIRED BEAM IAW SRM 53-00-01 VOL II FIG 9. MAJOR REPAIR.

Part: STOP — WORN (ACCESS PANEL) · airframe 103,318 hrs · 31,184 cycles

LATCH STOPS WORN ACCESS PANEL 311AB RH SIDE. TITLE: FUSELAGE - PLATES AND SKINS - 311AB ACCESS DOOR CUTOUT LANDING SKIN RH FWD DAMAGE REPAIR WAS ACCOMPLISHED ON EA 8-5310-T0350318. MAJOR REPAIR

Part: LANDING — CRACKED (HORIZONTAL STAB) · airframe 103,318 hrs · 31,184 cycles

H-STAB ACCESS PANEL 311AB LANDING ON LH HAS A CRACK REMOVED DAMAGE IAW SRM 53-00-01 FIG 4 SHT 2. PERFORMED HFEC IAW SOPM 06-10-01-001. NO FURTHER CRACKS REMAIN. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO 8- 5310-T0350635 PT1 TITLE: FUSELAGE - MAIN FRAME - 311AB ACCESS DOOR CUTOUT LANDING CRACKED LH AFT FWD OF STA 2033. MAJOR REPAIR

Part: NUT PLATE — DAMAGED (TE FLAP) · airframe 103,318 hrs · 31,184 cycles

LT I/B FLAP INBOARD HOIST FITTING HAS 2 EACH NUT PLATES STRIPPED OUT. REMOVED AND REPLACED 2 EA NUT PLATES ON LT I/B FLAP I/B HOIST FITTING IAW DWG ARC2369 AND SRM 51-31-01 VOL II. SKIN SPLICE REPAIR IAW SRM 57-10-00 FIG 86 VOL I. RSC TRACKING ON EA T8-5750-T0350532 WINGS AND FLIGHT SURFACES. LT I/B FLAP SRM REPAIR WING ST XFTH 132-152. (MAJOR REPAIR)

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 103,318 hrs · 31,184 cycles

MAIN CARGO FLOOR PANEL BWTWEEN STA 595 AND STA 675 BETWEEN -X75.5 AND -X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 595-675 AND BETWEEN -X75.5 AND -X107.5 FABRICATED ON MAE TRAVELER T19/1448049 IAW SRZ 25-005. CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 103,318 hrs · 31,184 cycles

MAIN CARGO FLOOR PANEL BETWEEN STA 595 AND STA 675 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 595 TO STA 675 BETWEEN X27.5 AND X47.5 FABRICATED ON VTMAE TRAVELERR T19/1448546 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 103,318 hrs · 31,184 cycles

MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 495 AND STA 595 BETWEEN X27.5 AND X47.5 FABRICATED ON VTMAE TRAVELER T19/1448544 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 103,318 hrs · 31,184 cycles

MAIN CARGO FLOOR PANEL BETWEEN STA 675 AND STA 735 BETWEEN X27.5 AND X47.5 IS DAMAGED. MAIN CARGO FLOOR PANEL AT STA 675 - STA 735 BETWEEN X27.5 TO X47.5 FABRICATED ON VTMAE TRAVELER T19/1448545 IAW SRZ-25-005 CAT "A" MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 103,318 hrs · 31,184 cycles

MAIN CARGO FLOOR PANEL BETWEEN STA 765 AND STA 795 BETWEEN X91.5 AND X107.5 IS DAMAGED. MAIN CARGO FLOOR PANEL BETWEEN STA 765 TO 795 BEWTEEN X91.5 AND X107.5 FABRICATED ON VTMAE TRAVELER T19/1448549 IAW SRZ-25-005 CAT "A" MAJOR REPAIR

Part: LIGHT — MALFUNCTIONED (POWER SWITCH) · airframe 101,699 hrs · 30,326 cycles

DURING PREFLIGHT, WHEN SELECTING EMERGENCY PWR SWITCH TO ARM, THE ON LIGHT REMAINED ILLUMINATED. RESET FUEL LEVERS. ACFT HAD POWER DROP OFF DURING PREFLIGHT. COMPLIED WITH AN OPS TEST IAW AMM 24-00-00-5. OK FOR SERVICE.

Part: TRANSMITTER — OUT OF ADJUST (TE FLAP SYS) · airframe 101,204 hrs · 30,058 cycles

AT 121 KNOTS DURING TAKEOFF, RECEIVED AN AUDIBLE WARNING FOR THE FLAPS, FOLLOWED BY A WARNING FOR THE SLATS. . REJECTED TAKEOFF AT 130 KNOTS. PERFORMED A FLAP INDICATION TEST, FOUND TRANSMITTER IN LIMITS . LIB, RIB, & LOB ARE BELOW OR AT LOW END OF TOLERANCE. ADJUSTED THE FLAP POSITION TRANSMITTERS LIB, RIB, AND LOB IAW 27-50-00-5. ALL FLAP TRANSMITTERS NOW CHECKED GOOD IAW AMM 27-50-00-5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 100,954 hrs · 29,942 cycles

NR 3 AC PACK COMPARTMENT STA 475 BULKHEAD WEB, A/C CHECK VALVE FASTENER HOLE AT 4:30 POSITION HAS A .5 INCH CRACK PROPAGATING THROUGH HOLE. REPAIRED PER EA 8-5310-T0336280.

Part: PANEL — DELAMINATED (LT WING) · airframe 100,954 hrs · 29,942 cycles

LT WING, PANEL 541 LB IS DELAMINATED/SPLIT. REPAIRED LT WING, PANEL 541 LB AT THE DELAMINATED/SPLIT AREA REF SRM 51-71-00 VOL 2 PG 1-47 AND DRAWING NUMBER ARC0357.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 100,954 hrs · 29,942 cycles

MAIN DECK APPROX STA 1265, CENTER LINE X.8.5 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (BS 565) · airframe 100,954 hrs · 29,942 cycles

MAIN DECK SEAT TRACK BS 565, LBL 8.5 SHOWS DAMAGE. REPAIRED IAW SRM 53-70-00, FIG 1.

Part: SEAT TRACK — DAMAGED (BS 1581) · airframe 100,954 hrs · 29,942 cycles

SEAT TRACK BS 1581, LBL 75 DAMAGED. REPAIRED IAW SRM 53-70-00, FIG 1.

Part: SEAT TRACK — WORN (BS 625) · airframe 100,954 hrs · 29,942 cycles

SEAT TRACK AT BS 625, RBL 27.5 IS DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 100,954 hrs · 29,942 cycles

MAIN DECK, APPROX STA 1039 LBL 75 GROOVE/ GOUGE WORN INTO TRACK. SEAT TRACK IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1.

Part: CHANNEL — CRACKED (BS 555) · airframe 100,954 hrs · 29,942 cycles

NR 3 A/C COMPARTMENT BS 555, LONGERON 34R FRAME J-CHANNEL HAS A 1.5 INCH CRACK. INSTALLED A TYPICAL FORMED CHANNEL REPAIR IAW SRM 53-00-01, FIG.8, SHEET 2, PAGE 30 & 31, VOL I.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 100,954 hrs · 29,942 cycles

MAIN CARGO COMPT APPROX STA 1601 RBL 75 SEAT TRACK IS DAMAGED. REPAIRED SEAT TRACK PER SRM 53-70-00 FIG 1.

Part: FRAME — CRACKED (BS 1841) · airframe 100,954 hrs · 29,942 cycles

CENTER CARGO BAY, APPROXIMATELY BS 1841, LBL 6 AND RBL 6, FRAME WEB IS CRACKED. REPAIRED THE FRAME IAW SRM 51-00-01, FIG 10, SHT 5, VOL I.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 100,954 hrs · 29,942 cycles

LEFT OTBD FLAP UPPER SKIN HAS A .75 INCH CRACK AT XOF 572. 5 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 100,954 hrs · 29,942 cycles

LEFT OTBD FLAP UPPER SKIN HAS A 2.0 IN. CRACK AT XOF 563. 12 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 100,954 hrs · 29,942 cycles

LEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A .4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 100,954 hrs · 29,942 cycles

LOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT UPPER AFT CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-T0336191.

Part: SKIN — CRACKED (FUSELAGE) · airframe 100,954 hrs · 29,942 cycles

LOWER FUSELAGE NR 1 ACM EXHAUST DOOR CUT OUT, AFT LOWER CORNER IS CRACKED FROM SKIN EDGE TO FASTENER HOLE. ACCOMPLISHED EA WORK CARD 8-5340-0336191. MAJOR REPAIR.

Part: DOOR — CRACKED (ACM DOOR) · airframe 100,954 hrs · 29,942 cycles

LOWER FUSELAGE NR 3 ACM ACCESS DOOR UPPER FLANGE PREVIOUS REPAIR HAS CONTINUED TO CRACK. REPAIRED THE NR 3 ACM DOOR UPPER FLANGE CRACK IAW EA 8-5240-T0336127.

Part: BULKHEAD WEB — CRACKED (NLG WW) · airframe 100,954 hrs · 29,942 cycles

NOSE WHEEL WELL RIGHT VERTICAL PANEL AT APPROX STA 480 HAS A CRACK APPROX 6 INCH LONG. INSTALLED WEB SECTION AND DOUBLERS REF. SRM 53-00-01 FIG.10 (SHEET 5) VOLI.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 100,954 hrs · 29,942 cycles

BS 595, BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2 INCH. CRACK EXTENDED THROUGH THE RADIUS. REPAIED THE BULKHEAD TEE CAP IAW EA T 8-5310-T0335740, PART 1 & 2.

Part: WEB — CRACKED (BS 471-501) · airframe 100,954 hrs · 29,942 cycles

NOSE WHEEL WELL LEFT VERTICAL WEB PANEL BS 315, HAS A CRACK BEHIND THE HYDRAULIC LINES. REMOVED AND REPLACED DAMAGED SECTION OF THE WEB IAW SRM 53-00-01, FIG 10, SHT 4, 5, 7, PGS 50, 51, 53, AND DWG NCA6046, AND ACA3837.

Part: WARNING MESSAGE — FALSE INDICATION (ZONE 600) · airframe 100,311 hrs · 29,583 cycles

AT FL 350, HAD A LEVEL 3 AIR MANIFOLD 3 FAILURE. RAN QRH, ALERT WENT AWAY. DECLARED AN EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRPORT. CHECKED MANIFOLD FAILURE INDICATORS IN CAC AND FOUND RT MANIFOLD PRESSURE SWITCH FAULTING IAW AMM 36-23-03-4-0, 36-00-01-5-0, 36-00-02-5-0. REMOVED AND REPLACED THE RT MANIFOLD PRESSURE SWITCH IAW AMM 36-23-03-4. CARRIED OUT PRESSURE DECAY TEST WITH APU IAW AMM 36-00-01-5. DECAY TEST PASSED. LEAK CHECKED DUCTING FROM CAC TO INBD SIDE OF NR 3 ENGINE. NO LEAKS FOUND. CARRIED OUT ENGINE RUN UP IAW JRA 5 & 6, FUEL BURN INDICATED DURING RUN UP WAS 240, FUEL ON BOARD WENT FROM 50,400 TO 50,200 LBS. CARRIED OUT A DECAY TEST WITH ENGINES IAW AMM 36-00-02-5. ALL TESTS PASSED. CHECKED MANIFOLD FAILURE INDICATORS IN CAC. AFTER ENGINE RUNS, NO FAULTS INDICATED. ACFT OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (R1 DOOR) · airframe 99,822 hrs · 29,378 cycles

R1 DOOR SLIDE LIGHT ILLUMITATED. PERFORMED OPERATIONAL CHECK OF THE R1 DOOR SLIDE BOTTLE PRESSURE LIGHT IAW AMM 25-61-03-5-0. TESTED GOOD SEVERAL TIMES. OK FOR SERVICE.

Part: TEST SWITCH — FAULTY (R1 DOOR) · airframe 98,136 hrs · 28,656 cycles

R1 DOOR EVAC SLIDE, REMOTE PRESSURE PRESS TO TEST INDICATING SYS INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01, CATEGORY C, EXPIRATION 24 FEB 16. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. SYS PRESS VERIFIED, OK FOR SERVICE. R & R R1 DOOR SLIDE PRESS TO TEST SWITCH ASSEMBLY IAW AMM 25-61-03-2. OPERATIONS CHECKED GOOD.

Part: SKIN PANEL — CRACKED (LT HORIZ STAB) · airframe 976 hrs · 28,421 cycles

LEFT HORIZONTAL STABILIZER SKIN PANEL 7281-1, HAS A .700" CRACK JUST FWD OF REAR SPAR CAP, FWD BARREL NUT HOLE. R & R SECTION OF SKIN PANEL, PLANK, IAW EA 8-5510-T0320816.

Part: SPAR CAP — CRACKED (LT HORIZ STAB) · airframe 976 hrs · 28,421 cycles

LEFT HORIZONTAL STABILIZER, UPPER OUTER REAR SPAR CAP, FWD BARREL NUT HOLE HAS A .400" VERTICAL CRACK EXTENDING FROM BELOW THE BARREL NUT AT THE 5:00 POSITION. R & R SECTION OF REAR SPAR CAP IAW EA 8-5510-T0320816.

Part: PANEL — DELAMINATED (LT WING) · airframe 976 hrs · 28,421 cycles

LEFT WING HINGE PANEL 551DB HAS DELAMINATION. REPAIRED THE HINGE PANEL IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (ZONE 400) · airframe 976 hrs · 28,421 cycles

AFT ENG INLET DUCT, RT SIDE PANEL 364JR DELAMINATED, LOWER FWD. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL. II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (ZONE 400) · airframe 976 hrs · 28,421 cycles

AFT ENG INLET DUCT, RT SIDE PANEL 364JR, LOWER SFT DELAMINATED. REPAIRED PANEL 364JR IAW SRM 51-71-00 VOL II. PREPPED & PAINTED IAW SRM 51-21-02 VOL II.

Part: WIRE — DAMAGED (ELECTRICAL) · airframe 976 hrs · 28,421 cycles

FOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00- 16, WDM 52-33-01 AND E8-7-2810-5002 PT1.

Part: WIRE — DAMAGED (ELECTRICAL) · airframe 976 hrs · 28,421 cycles

FOUND WIRE DAMAGED, LOCATED AT BS 1240, RT SIDE OF CENTERLINE OF ACFT. REPLACED WIRE IAW SWPM 20-10-03, 20-00-16, WDM 28-21-03, AND E8-2810-7-5002 PT1.

Part: WIRE — DAMAGED (ELECTRICAL) · airframe 976 hrs · 28,421 cycles

FOUND WIRE DAMAGED, LOCATED AT BS 1346, RT OF CENTERLINE OF ACFT. SPLICED IN A NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 29-12-01, AND E8-2810-7-5002 PT 1.

Part: WIRE — DAMAGED (ELECTRICAL) · airframe 976 hrs · 28,421 cycles

FOUND DAMAGED WIRE LOCATED AT BS 1346, RT SIDE OF CENTERLINE. SPLICED IN NEW WIRE IAW SWPM 20-10-03, 20-00-16, WDM 33-32-02, AND E8-2810-7-5002 PT1.

Part: FUEL DOOR — DAMAGED (RT WING) · airframe 976 hrs · 28,421 cycles

RIGHT WING REFUEL & DEFUEL DOOR, PUNCTURED ON UPPER MID SURFACE. REPAIR IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (NR 5 SPOILER) · airframe 976 hrs · 28,421 cycles

LEFT WING NR 5 SPOILER PANEL HAS DELAMINATION, UPPER SURFACE. REPAIR SPOILER IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: BATTERY — FAILED (ZONE 100) · airframe 976 hrs · 28,421 cycles

WHILE UNDERGOING A C CHECK HEAVY MX VISIT, IN THE HANGAR A FIRE STARTED IN THE CTR ACCESSORY COMPARTMENT OF THE ACFT. TROUBLESHOOTING WAS UNDERWAY FOR THE FOLLOWING FINDING, CAC, BATTERY CHARGER BATTERY FAULT T SENSE B. A PUSHED BACK PIN HAD BEEN FOUND & CORRECTED IN A PLUG IN THE OVERHEAT DETECTION SYS & IT WAS TIME TO VERIFY IF IT WAS A GOOD FIX. THE MAIN BATTERIES WERE REINSTALLED & RECONNECTED. THE INSTANT THE BATTERY SWITCH IN THE COCKPIT WAS PLACED IN, THE ON POSITION THE GROUNDING CABLE ADJACENT THE B BATTERY OVERHEATED & THE WIRE INSULATION CAUGHT FIRE. THE BATTERY POWER SWITCH WAS IMMEDIATELY SWITCHED TO THE OFF POSITION & EXTERNAL POWER WAS REMOVED FROM THE ACFT. A TYPE B C PORTABLE FIRE EXTINGUISHER WAS USED TO EXTINGUISH THE FIRE. THE EXTINGUISHING AGENT WAS VACUUMED UP SO THAT ANY STRUCTURE THAT MAY HAVE BEEN EXPOSED TO A HEAT SOURCE CAN BE INSPECTED IAW THE SRM. NON-ROUTINES TO REPLACE THE WIRES HAVE BEEN GENERATED. THE MAIN BATTERY IS SUSPECT & HAS BEEN REMOVED FOR REPLACEMENT.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK SEAT TRACK STATION 899 LT, X=47.50 DAMAGED WORN SPLICED SEAT TRACK AS REQUIRED IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK, SEAT TRACK STATION 1401 RT, X 47.50 IS DAMAGED & WORN. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK SEAT TRACK STATION 939 RT, X=27.50 DAMAGED & WORN. REMOVED DAMAGED SECTION OF SEAT TRACK. REPLACED SEAT TRACK IAW SRM 53:70:00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK SEAT TRACK STATION 879 RT, X=47.50 DAMAGED & WORN. SPLICED SEAT TRACK AS REQUIRED IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK SEAT TRACK, STATION 1019 RT, X 47.50 IS WORN & DAMAGED. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK, SEAT TRACK AT STATION 1521 RT, X 47.5 IS DAMAGED & WORN. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK, SEAT TRACK STATION 1381 LT, X 47.50 DAMAGED & WORN. R & R SECTION OF SEAT TRACKS IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 976 hrs · 28,421 cycles

MAIN DECK, SEAT TRACK AT STATION 1401 RT, X 27.50 IS DAMAGED. SPLICE SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: ACCELEROMETER — FAILED (AUTOPILOT SYS) · airframe 974 hrs · 28,357 cycles

ON LANDING TOUCHDOWN, AUTO BRAKES & AUTO SPOILERS KICKED OFF. SPOILERS WOULD NOT MOVE TO GND SPOILER POSITION. R & R LINEAR ACCELEROMETER UNIT IAW AMM 22-11-01-2. CHECKED GOOD, NO FAULT BALL & OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 965 hrs · 27,944 cycles

L1 PRESS CHECK LIGHT WONT ILLUMINATE WHEN PRESSED. R & R LIGHT BULB. OPERATIONS CHECKED GOOD ALL IAW AMM 25-61-03-2.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 965 hrs · 27,942 cycles

L1 DOOR SLIDE LOW PRESS LIGHT INOPERATIVE. REPLACED BATTERIES ON L1 DOOR SLIDE LOW PRESS LIGHT. ADJUSTMENT & TEST GOOD.

Part: BOTTLE — HANDLER ERROR (DOOR) · airframe 964 hrs · 27,908 cycles

RAMP BLEW SLIDE BOTTLE MEL 05 FEB 15. RELEASED FOR SERVICE IAW MEL 52-10-03 CATEGORY C. MAIN ENTRY, IDENTIFY DOOR OR SLIDE & RAFT INOPERATIVE. SERVICED DOOR AIR RESERVOIR PER AMM 52-11-07-2, SYSTEM OK FOR SERVICE

Part: BOTTLE — HANDLER ERROR · airframe 964 hrs · 27,909 cycles

RAMP BLEW SLIDE BOTTLE.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 96,311 hrs · 27,837 cycles

AFTER TAKEOFF, PACKS 2 & 3 AIR OUTPUT WAS OF OBNOXIOUSLY BAD QUALITY WITH A VERY STRONG ODOR OF DIRTY SOCKS & FUEL. BOTH PACKS WERE CHECKED INDIVIDUALLY WITH THE SAME BAD AIR OUTPUT FROM EACH. OXYGEN MASK USED. OPERATED NR 2 PACK ON NR 1 BLEED SEEMED TO HELP. R & R COALESCE BAGS ON ALL 3 PACKS.

Part: ENGINE — OVERSPEED (NR 3) · airframe 95,520 hrs · 27,509 cycles

REJECTED TAKEOFF AT 85 KIAS DUE TO NR 3 ENGINE EXCEEDANCE N1 120.6 FOR FIVE SECONDS. ACCOMPLISHED NR 3 ENGINE N1 OVERSPEED INSPECTION. CHECKED FAN ROTOR FOR FREEDOM ROTATION, CHECKED FIRST STAGE FAN FOR EXCESSIVE RUB, CHECKED INLET & EXHAUST AREA FREE OF PARTICLES. INSPECTION ACCOMPLISHED IAW AMM 72-00-00-6-1 2B. ACFT GOOD FOR SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,422 hrs · 27,473 cycles

EMPENNAGE AFT ACCESSORY FWD COMPARTMENT FWD BULKHEAD DOUBLER BELOW APU SUPPLY DUCT FOUND CORRODED. CORRODED DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW DOUBLER FABRICATED BY MACHINING AS PER DRAWING AJC7267 REVISION A. PNEUMATIC SYSTEM ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 36-00-03-5 REVISION 16.2. HORIZONTAL STABILIZER ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-40-00-5 REVISION 16.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (RT WING) · airframe 95,422 hrs · 27,473 cycles

RIGHT WING, TELESCOPIC DUCT ASSEMBLY UPPER DOOR SKIN CUT OUT FOUND CRACKED. REPAIRED IAW EA 8-5730-T0309163 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING LE BEADED DOUBLER AT XOS 635 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (RT WING) · airframe 95,422 hrs · 27,473 cycles

RIGHT WING LE BEADED DOUBLER AT XOS 753 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: RIB — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING FIXED LE SUPPORT RIB AT XOS 584 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II REVISION 101. NEW RIB FABRICATED IAW DRAWING ARB22931 REVISION H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING LE BEADED DOUBLER AT XOS 669 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING LE BEADED DOUBLER AT XOS 642 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING LE BEADED DOUBLER AT XOS 607 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (RT WING) · airframe 95,422 hrs · 27,473 cycles

RIGHT HAND WING LE BEADED DOUBLER AT XOS 670 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: RIB — CRACKED (RT WING) · airframe 95,422 hrs · 27,473 cycles

RIGHT WING LE FIXED LE SUPPORT RIB AT XOS 738 FOUND CRACKED. RIB REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II REVISION 101. NEW RIB FABRICATED IAW DRAWING ARB22923 REVISION D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING, TELESCOPIC DUCT UPPER DOOR SKIN CUT OUT FOUND CRACKED. REPAIRED IAW EA 8-5730-T0309190 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: DOUBLER — CRACKED (LT WING) · airframe 95,422 hrs · 27,473 cycles

LEFT WING LE BEADED DOUBLER AT XOS 648 FOUND CRACKED. REPAIRED OUT IAW SRM 57-10-00 FIGURE 71 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.

Part: SKIN — CRACKED (LT WING) · airframe 95,566 hrs · 27,526 cycles

LEFT WING PRESS REFUEL PANEL DOOR OPENING, SUSPECT CRACK AT FWD INBD CORNER. REQUEST HFEC TO CONFIRM. REPAIRED CRACK INBD OF PRESS REFUEL PANEL IAW EA 8-5710-T08739 PART 1.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 93,976 hrs · 26,836 cycles

REJECTED TAKEOFF AT 100 KTS FOR LEVEL 2 ENGINE RPM HIGH. N1 RPM NR 3 = 121.1. PERFORMED NR 3 ENGINE INSPECTION IAW MM 72-00-00-6-1, PAR B 1 & 2. CHECKED OK. NO DAMAGE NOTED. PERFORMED NR 3 ENGINE INSPECTION IAW MM 72-00-00-6-1 PAR B, 1 AND 2. CHECKED OK. NO DAMAGE NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (FUEL SYSTEM) · airframe 93,389 hrs · 26,594 cycles

AFTER TAKEOFF, RECEIVED A LVL 1 FUEL CONTAMINATED ALERT. DURING RETURN TO LANDING ALERT WENT AWAY. INTERROGATED ALL THREE AIU'S. NO FAULTS FOUND. R & R NR 1, 2, AND 3 ENG FUEL FILTERS IAW MM 73-11-02. NO CONTAMINANTS FOUND. RAN NR 1, 2, AND 3 ENGINES IAW JRH. ALL PERAMETERS NORMAL. LEAK CHECKED NORMAL. IAW FIM 73-31-01, B, SYS IS OK. ACFT OK FOR SERVICE.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 91,960 hrs · 26,018 cycles

EMERGENCY LIGHTING FAILED TEST. EMERGENCY LIGHT BATTERY 2 LOW ALERT DURING TEST. TROUBLESHOT, FOUND WIRE B962-1410-24 PULLED FROM BLOCK S30-4. REINSTALLED IAW W/D 33-50-01 AND MM 20-30-02-2. EMERGENCY LIGHTING BATTERY, OPS CHECKED NORMAL.

Part: FEEDER CABLE — BURNED (NR 1 PYLON) · airframe 91,960 hrs · 26,018 cycles

NR 1 ENGINE PYLON VIEW THROUGH DOOR 438BL, FEEDER CABLES FOUND CHAFING AGAINST STRUCTURE, ARCING, AND BURNED. FEEDER CABLE REPLACED EO 8-2450-7-5009 01, PART 1.

Part: BULKHEAD WEB — CRACKED (NLG WW) · airframe 91,939 hrs · 26,011 cycles

NLG WHEEL WELL LT BULKHEAD FWD CORNER HAS A CRACK IN THE WEB. COMPLIED WITH EA 8-5310-161338 AND SRM 53-30-00, FIG 6.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 91,403 hrs · 25,800 cycles

DURING CLIMB OUT, LOST ENG NR 2 AFTER SHUTTING OFF ENG ANTI ICE AT ABOUT 18,000; RAN QRH AND RETURNED TO AIRPORT. ALL ENG INDICATIONS SEEMED NORMAL. ROLL BACK OF EGT AND N1 ONLY. CREW REPORTED THEY DID NOT TRY A RESTART. PERFORMED RIG CHECK OF FUEL LEVER AND THROTTLE IAW MM 73-20-01-2. ALSO PERFORMED LEAK CHECK AND OPS CHECK OF FUEL FLOW TRANSMITTER AND FUEL PUMP, AND MEC. NO LEAKS NOTED. ALSO PERFORMED ENGINE RUN UP FORM M-3488. NR 2 ENG OPS CHECKED NORMAL IAW JRH , OK FOR SVC.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 90,914 hrs · 25,612 cycles

ON TAXI OUT VERY STRONG FUMES NOTED BY CAPTAIN AND F/O. APU WAS OFF ALL 3 ENGINES RUNNING WITH PACKS 2, 3 ON (1 DEFERED) RETURNED TO GATE CLEANED AIR DUCTS OF ODOR IAW MM 21-53-00-7. OK FOR SERVICE. REMOVED ALL 3 WATER SEPARATOR COALESCERS FOUND. LUBE IN EACH SPRING MECHANISM, CLEANED ALL RESIDUE AND CHANGED ALL BAGS. REINSTALLED MM 21-53-03-2-0. PACK BURN IN PROGRESS, CLEANED AIR DUCTS OF ODOR IAW MM 21-53-00-7. OK FOR SERVICE. FINAL CLOSED.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 90,017 hrs · 25,275 cycles

NR 2 OIL FILTER ALERT - SHUTDOWN NR 2 ENGINE. ALL OTHER ENGINE INDICATIONS NORMAL. R & R NR 2 ENGINE PER WORKCARD 71T1701. OPS AND LEAK CHECKED OK.

Part: CONTROL PANEL — DAMAGED (EMERGENCY POWER) · airframe 89,966 hrs · 25,257 cycles

EMERGENCY POWER OFF LIGHT INOP. EMERGENCY POWER OFF LIGHT INOP. RELEASED FOR SERVICE PER MEL: 24-08-03-01. REPLACED ELECTRICAL SYSTEM CONTROL PANEL PER MM 24-08-02-4. OPERATION TESTED NORMAL PER MM 24-08-02-5.

Part: CONTROL UNIT — FAILED (OIL FILTER) · airframe 89,839 hrs · 25,204 cycles

NR 2 ENGINE OIL FILTER ALERT. DID NOT EXTINGUISH. SHUTDOWN ENG 2 IAW QRH. DTW R IN WORK AT THIS TIME. REMOVED, REPLACED AND INSPECTED SCAVENGER FILTER ELEMENT IAW MM 79-20-02-2 AND FOUND NO CONTAMINATION. ALSO REMOVED MASTER CHIP DETECTOR AND FOUND NO CONTAMINATION. ACFT REQUIRES ENGINE RUN FOR LEAK CHECK AND THE NR 2 ENGINE PLATFORM TO BE CLOSED. CFDS FAULT REVIEW AND FAULT HISTORY OF AIU 2 SHOWED INTERNAL FAULT. REMOVED AND REPLACED NR 2 AIU IAW M/M CH 31-43-02-4-0. OPS TEST GOOD IAW MM CH 31-43-02-5-0. R-T-S PASS ON ALL 3 AIU. NR 2 ENGINE GROUND RUN UP OPS CHECK AND LEAK CHECK GOOD. CLOSED NR 2 ENGINE COWLINGS AND WORK PLATFORM. OK FOR SERVICE.

Part: SWITCH — FAILED (NR 2 OIL SYSTEM) · airframe 89,612 hrs · 25,122 cycles

ON INITIAL CLIMBOUT, RECEIVED ENG 2 OIL FILTER ALERT. USED MIN IDLE POWER AS ALERT WENT ON AND OFF SEVERAL TIMES FOR SEVEAL MINUTES EVENTUALLY REMAINED ON STEADY AT MIN IDLE. RED TABS FOR ALERT SHUTDOWN NR 2 ENGINE, RETURN TO DEPARTURE. NO OTHER ABNORMAL ENGINE PARAMETERS NOTED. FUEL DUMP REQ OF 8000 LBS TO MAX LANDING WEIGHT. R & R OIL STRAINER CLOGGING SWITCH REF 79-35-01-2 REN NR 2 ENG REF JRH OIL STRAINER SHOWED NORMAL THROUGH MCDU NO FAULTS OR WARNINGS DURING RUN ACFT RETURNED TO NORMAL NO FURTHER ACTION REQUIRED AT THIS TIME. PLACARD REMOVED.

Part: SKIN — CRACKED (ZONE 500) · airframe 88,381 hrs · 24,643 cycles

LH WING DEEP WEAR ON UPPER EXTERNAL SKIN L/E AT STA XOS405 PERFORMED REPAIR IAW SRM 57-10-00 PAG.96 FIG.28 VOL.1

Part: SKIN — CHAFED (ZONE 500) · airframe 88,381 hrs · 24,643 cycles

LEFT WING DEEP WEAR ON EXTERNAL SKIN L/E FROM STA XOS 430 TO STA XOS 465 PERFORMED REPAIR IAW SRM 57-10-00 FIG.40 SH.1 VOL.1

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

MAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB AT STA 1251 REPAIRED IAW SRM 53-50-00 FIG 19, SH 1, VOL 1.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

MODERATE CORROSION ON INTERIOR STRUCTURE OF LOWER AFT CARGO COMPT DOOR SILL. REPAIRED IAW EA 8-5310-123168 AND SRM 53-50-00 FIG.22, FIG.1, FIG.9, FIG.15A VOL.1.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

LT WING UPPER SIDE WING TO FUSELAGE FILLETS. AFTER REMOVING THE FILLETS 151 FT AND 151 ET WITH NRC NR N00866 THE FOLLOWING DEFECT HAVE BEEN FOUND EXFOLIATION CORROSION ON LONGERON. PERFORMED REPAIR IAW E.A. 8-5310-137606

Part: PANEL — DELAMINATED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

RT WING UPPER SURFACE T/E. REMOVING WING PANEL ARC0340-504 WITH N00458. FOUND DELAMINATION ON AFT EDGE. (REMOVED PART). REPAIRED DELAMINATION IAW SRM 51-71-00 PAR.16 VOL.2

Part: SKIN — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

CTR CARGO COMPT BILGE, 2 EA U/S ANCHOR PLATE ON SKIN. DURING ANCHOR PLATE REPLACEMENT FOUND CORROSION ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG.13 SH.6 VOL.1.

Part: WEB — CRACKED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

COCKPIT AREA FOUND CRACKS ON WEB. REPAIRED CRACK IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.

Part: SKIN — DENTED (ZONE 300) · airframe 88,381 hrs · 24,643 cycles

RT HORIZONTAL STAB EXTERIOR SURFACE FOUND DEEP NICK ON SKIN. (REMOVED PART). REPAIRED EDGE FWD SKIN IAW SRM 55-10-00 FIG.13 VOL.1, REPAIRED LEADING REAR SKIN IAW SRM 55-00-01 FIG.3 SH.2 VOL.1

Part: SKIN — DENTED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

EXT FUSELAGE LOWER SURFACE FOUND 1 EA DENT ON SKIN 3" X 1" DEEP .060". (UNDER CUTOUT UPPER CARGO DOOR). REPAIRED SKIN IAW SRM 53-50-00, FIG 6, VOL I.

Part: SKIN — WORN (RT WING SLAT) · airframe 88,381 hrs · 24,643 cycles

RT WING L/E SLAT DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 VOL.1

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

AFT CARGO COMPT BILGE FOUND NR 4 HOLES ON NUTPLATE CORROSION ON ANGLE SUPPORT FLOOR PANEL. REPAIRED AREAS IAW SRM 53-00-01 FIG.9 SH.7 VOL.1

Part: SKIN — DENTED (LT ELEVATOR) · airframe 88,381 hrs · 24,643 cycles

DURING INSP LT HOR STAB INBD ELEVATOR FOUND DEEP DENT 1.50" X 1.50" DEEP.068" ON UPPER SKIN. REPAIRED SKIN IAW SRM 55-10-00 FIG.8 VOL.1

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 88,381 hrs · 24,643 cycles

RT HORIZ STAB FOUND CRACK ON UPPER SKIN OF DETACHABLE ELEVATORS. REPAIRED SKIN IAW SRM 55-00-01 FIG.3 VOL1

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

AFT CARGO COMPT BILGE FOUND CORROSION ON CAP FRAME AND FRAME LONGERON. TRMIMED AND REPLACED FRAME SECTION, SPLICE IAW SRM 53-30-00 FIG.5 VOL.1 & 53-00-01 FIG.10 VOL.1 & DWG AGA7125.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 88,381 hrs · 24,643 cycles

DURING INSP RT HOR STAB L/E EXT SURFACE FOUND 1 EA DEEP DENT 1" X 1" DEEP .118" ON SKIN ( REMOVED PART ). REPAIRED L/E SKIN IAW SRM 55-10-00 FIG.13 SH.1-2-3 VOL.1

Part: FRAME — CRACKED (BS 1501) · airframe 88,381 hrs · 24,643 cycles

RT MLG WHEEL WELL, FOUND CRACK ON FRAME. TRIMMED OUT DAMAGED SECTION OF FRAME IAW SRM 53-30-00 FIG.5 VOL.1. INSTALLED NEW SECTION OF FRAME & SPLICE IAW SRM 53-00-01 FIG.10 SH.5 VOL.1

Part: WEB — CRACKED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

MAIN CABIN R3 DOOR UPPER JAMB CRACK ON WEB. REPAIRED WEB IAW SRM 53-50-00 FIG.19 VOL1

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

MAIN CABIN COCKPIT FOUND CRACK ON HORIZONTAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 53-00-01 FIG.2 SH.2 VOL.1

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

MAIN CABIN, COCKPIT FOUND CRACK ON HORIZONTAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 53-00-01 FIG.2 SH.2 VOL.1.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 88,381 hrs · 24,643 cycles

RT MLG WHEEL WELL FOUND CRACK ON HORIZONTAL WEB. REPAIRED IAW SRM 53-00-01 FIG.10 SH.1 VOL.1

Part: CARGO TRACK — CRACKED (BS 755) · airframe 88,381 hrs · 24,643 cycles

FWD CARGO COMPT FOUND CRACK ON TRACK. REMOVED AND REPLACED SECTION OF TRACK IAW SRM 53-70-00 FIG.1 SH.1 VOL.1.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 88,381 hrs · 24,643 cycles

FWD CARGO COMPT FOUND CRACK ON TRACK. REPLACED TRACK SECTION, USED EXISTING SPLICES IAW SRM 53-70-00 FIG.1 SH.1 VOL.1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 88,381 hrs · 24,643 cycles

DURING INSP OF HORIZONTAL STAB CONSTANT SECTION, FOUND 2 PANELS CRACKED PN 7229-1 POS NR3 & 7226-1 POS NR18, PLEASE VERIFY APPLICABILITY & REVISION OF EO 8-5510-7-4308 IAW SECTION C. ACCOMPLISHED E.A.8-5510-133497 IAW SB DC10-55-016. REMOVED AND REPLACED PANEL P/N ALC7225-1 IAW S.B. DC10-55-016 GROUP 2 AT LOWER COSTANT SECTION FOLLOWING.

Part: WEB — CRACKED (ZONE 200) · airframe 88,381 hrs · 24,643 cycles

MAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB. REPAIRED CRACK IAW SRM 53-50-00 FIG.19 SH.2 VOL.1

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

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

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

AFT FUSE WASTE TANK, SEVERE CORROSION ON STRUT. REPAIRED STRUT IAW SRM53-00-01 FIG.9 VOL.1

Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 88,381 hrs · 24,643 cycles

LT WING L/E FOUND CRACK ON OLD REPAIR OF INTERNAL INTERCOSTAL. REPAIRED INTERNAL INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

RT WING L/E FOUND CRACKS ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED BEADED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1.

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

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

Part: RIB — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

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

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

RT WING LWR SURFACE FOUND CRACK ON SKIN OF WING TIP. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 SH.2 VOL.1

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

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

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

RT WING L/E FOUND CRACK ON LWR EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 88,381 hrs · 24,643 cycles

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

Part: FRAME — CRACKED (ZONE 100) · airframe 88,381 hrs · 24,643 cycles

DURING INSPECTION CAC INT. FOUND CRACK ON FRAME. REPAIRED FRAMES IAW SRM 53-30-00 FIG.7 VOL.1.

Part: BEAM — CRACKED (ZONE 100) · airframe 88,381 hrs · 24,643 cycles

FWD CARGO COMPT, FOUND CRACK ON BEAM. PERFORMED REPAIR ON BEAM IAW SRM 53-60-01 FIG.3 VOL.1

Part: DOUBLER — CRACKED (LT WING) · airframe 88,381 hrs · 24,643 cycles

LT WING L/E FOUND CRACK ON INTERNAL DOUBLER. REPAIRED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,381 hrs · 24,643 cycles

LWR CTR CARGO COMPT, SEVERE CORROSION ON CHANNEL.

Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 88,381 hrs · 24,643 cycles

LT WING L/E FOUND CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1

Part: PANEL — CRACKED (ZONE 500) · airframe 88,381 hrs · 24,643 cycles

LT WING L/E FOUND CRACK ON CHORD FIXED PANEL. REPAIRED L/E LOWER STRINGER IAW SRM 57-10-00 FIG.49 VOL.1.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 88,381 hrs · 24,643 cycles

LT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 88,381 hrs · 24,643 cycles

LT WING OTBD FLAP LWR SKIN FOUND MANY DEEP NICKS. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, VOL I.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 88,381 hrs · 24,643 cycles

LT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 88,381 hrs · 24,643 cycles

EXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN 1"X 1" DEEP 0.060". PERFORMED HFEC INSPECTION IAW NDTSPM 06, NO CRACK FOUND. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG.13 SH.2 & SH.5 VOL.1.

Part: SEAT TRACK — GOUGED (BS 735-755) · airframe 86,205 hrs · 23,589 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 735-755 LBL 8. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 SHEET 4.

Part: SEAT TRACK — GOUGED (BS 615-635) · airframe 86,205 hrs · 23,589 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 615-635 RBL 8. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 5.

Part: SEAT TRACK — GOUGED (BS 615-635) · airframe 86,205 hrs · 23,589 cycles

MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 615-635 RBL 48. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1.

Part: MOTOR — BURNED (COCKPIT SEAT) · airframe 86,058 hrs · 23,507 cycles

UPON TAKING RUNWAY, FUMES NOTICED IN THE COCKPIT. TAXIED CLEAR BACK TO THE RAMP. FUMES INCREASED, DECLARED EMERGENCY, EVACUATED THE AIRCRAFT. UPON FURTHER INSPECTION, FOUND S/O'S SEAT CONTROL C/B POPPED, AND STRONG ODOR FROM SEAT MOTOR. UPON FURTHER INSPECTION, FOUND S/O'S SEAT CONTROL C/B POPPED, AND STRONG ODOR FROM SEAT MOTOR. REMOVED AND REPLACED SEAT IAW MM 25-11-03-4, OPS CHECKS GOOD. RAN PACKS FOR ONE HOUR THREE DIFFERENT TIMES, NO EVIDENCE OF FUMES. WHILE SERVICING O2, DID NOT NOTICE ANY EVIDENCE OF FUMES IN E/E COMPARTMENT.

Part: ENGINE — DAMAGED (NR 2) · airframe 83,410 hrs · 22,361 cycles

NR 2 ENG S/N 530393, RT LPT CASE 3 O'CLOCK POSITION BURN THRU HOLE APPROX .500" DIAMETER, AND HEAT DISTRESS AROUND LPT TURBINE CASE. REMOVED AND REPLACED NR 2 ENG PER FEDEX W/C 71T1101, W/C 71T1701 AND N/R 563.

Part: SENSOR — FAULTY (L/E SLAT) · airframe 81,383 hrs · 21,596 cycles

SLAT DISAGREE LIGHT ILLUMINATED WITH FLAP EXTENSION FROM 22 TO 35 AND REMAINED ON. PERFORMED RED TABS. LANDED WITH 22/EXT CONFIGURATION. ACCOMPLISHED DETAILED VISUAL INSPECTION OF THE SLAT CABLES BOTH LEFT AND RIGHT WING, PERFORMED PCU BITE TEST ALL CHANNELS PASS, PERFORMED SLAT TIMING TEST REF: 27-80-00-5-1 PASSED TEST. PERFORMED SLAT POSITION TEST PANEL CHECK REF: 27-80-00-6 PANEL PASSED TEST. CLEANED INBOARD SLAT SENSOR AND TARGET (MASSIVE AMOUNT OF GREASE ON TARGET & SENSOR). REMOVED AND REPLACED LEFT AND RIGHT NR 4 SLAT SENSOR BOTH A & B CHANNELS, PERFORMED ANOTHER PCU BITE TEST ALL CHANNELS PASSED.

Part: SKIN — CANNING (RT INBD FLAP) · airframe 80,779 hrs · 21,336 cycles

RIGHT INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE HAS A LARGE SKIN SECTION OIL CANNING. REPLACED SKIN PNL ASSY IAW DC-10 SRM 51-31-01 AT MAE ON N/R N01147.

Part: DOOR FRAME — GOUGED (FUSELAGE) · corrosion level 2 · airframe 80,779 hrs · 21,336 cycles

FUSELAGE CORROSION/GOUGES ON MAIN CARGO DOOR FRAME. COMPLIED WITH EA 8-5310-82067. FUSELAGE CORROSION GOUGES ON MAIN CARGO DOOR FRAME.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 80,779 hrs · 21,336 cycles

MAIN CARGO DECK SHORT SEAT TRACK FITTING IS CORRODED AT RBL 89 STA 1821 TO 1853. REMOVED CORROSION IAW SRM 53-70-00 VOL 1, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED FLOOR PANELS IAW M/M 53-21-04-2. REMOVED DAMAGED TRACK IAW SRM 51-31-01. NEW SEAT TRACK FAB ON TRAVLER T4/467895 IAW SRM 51-10-01. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01. INSTALLED FLOOR PANELS IAW M/M 53-21-04-2.

Part: HINGE — CORRODED (WINGS) · airframe 76,971 hrs · 20,188 cycles

NR S 32 C/W E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 04/18/03. COMPLIED WITH E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK.

Part: HINGE — CORRODED (WINGS) · airframe 76,971 hrs · 20,188 cycles

NR S 31 C/W E.A.8-5740-68783-L/H I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION .COMPLIED WITH E.A.8-5740-68783. ON 04/18/03.

Part: BRACKET — WORN (WING TO BODY) · airframe 76,971 hrs · 20,188 cycles

NR S-27 COMPLY WITH EA8-5331-68781 FUSELAGE-WING TO BODY FILLET- ATTACH BRACKET WEAR REPAIR P/N ANB7245. COMPLIED WITH EA8-5331-68781 FUSELAGE-WING TO BODY FILLET- ATTACH BRACKET WEAR REPAIR P/N ANB7245.

Part: SUPPORT — CRACKED (RT O/B FLAP) · airframe 76,971 hrs · 20,188 cycles

RIGHT O/B FLAP I/B HINGE FAIRING SUPPORT STRUCTURE CRACKED LWR AFT END OF HINGE. CLOSING ACTION ON 04/15/03. REMOVED SUPPORT STRUCTURE IAW SRM 51-31-01, FOUND -T- ANGLE CRACKED. REMOVED -T- ANGLE IAW SRM 51-31-01. SENT TO FAB, FAB SUPPORT AND -T- ANGLE ON TRAVELER T2/326984. INSTALLED REPAIR PARTS IAW SRM 51-31-01. PAINTED PARTS IAW FED-EX ENG REPORT 99-15 REV B.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 76,971 hrs · 20,188 cycles

MAIN DECK UNDER F/R STRUCTURE STA 515 TO 535 LBL 8.5 TO RBL 8.5 FINGER DOUBLER CORRODED AND FASTENER HEADS CORRODED AND BROKEN OFF. CLOSING ACTION ON 04/20/03. REMOVED AND REPLACED FINGER DOUBLER IAW SRM 53-12-01 AND SRM 51-31-01. FAB NEW DOUBLER IAW SRM 53-12-01, TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED DOUBLER IAW SRM 51-31-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 76,971 hrs · 20,188 cycles

NR 995 AFT CARGO AFT WALL LWR SUPPORT ANGLE IS CORRODED LBL 25 TO LBL 60 STA 1967. CLOSING ACTION ON 04/16/03 ON N/R 00995. REMOVED CORROSION, FOUND ANGLE TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED ANGLE IAW SRM 51-35-01. FAB ANGLE ON TRAVELER T2/326614, INSTALLED IAW SRM 51-31-01.

Part: SEAT TRACK — CORRODED (MAIN CARGO DECK) · airframe 76,971 hrs · 20,188 cycles

MAIN CARGO DECK SEAT TRACK STA 675 TO 735 RBL 75 AT TRACK FLANGE CLIP NUT HOLES TOP AND BOTTOM CORRODED. CLOSING ACTION ON 04/14/03. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REINSTALLED NEW SEAT TRACK IAW SRM 51-31-01, FAB NEW SEAT TRACK ON MAE TRAVELER T2/326222.

Part: PULLEY — BROKEN (RIGHT WING) · airframe 76,971 hrs · 20,188 cycles

RT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN.

Part: PULLEY — BROKEN (RT WING) · airframe 76,971 hrs · 20,188 cycles

RT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. R/R PULLEY BRACKET & PULLEY.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 76,971 hrs · 20,188 cycles

FWD CARGO PIT CEILING PANEL HAT TRACK CRACKED AT FS 970 RBL 48. CLOSING ACTION ON 04/14/03. HAT TRACK REMOVED IAW SRM 53-31-01. NEW HAT TRACK FAB ON TRAVELER T2/325808. NEW HAT INSTALLED IAW SRM 51-31-01.

Part: PULLEY — BROKEN (RT WING) · airframe 76,971 hrs · 20,188 cycles

RT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. CLOSING ACTION ON 04/18/03. REPLACED RT INBOARD FLAP FOLLOW-UP CABLE O/B PULLEY BRACKET, PULLEY AND SHAFT IAW M/M 20-20-07-2 AT M/M 20-50-02-2.

Part: MANIFOLD — DENTED (ENGINE AIR SYS) · airframe 76,971 hrs · 20,188 cycles

NR 1 ENGINE SIDE LONGITUDINAL CDP AIR 14TH STAGE MANIFOLD FWD END 90 DEG ELBOW PART HAS 2 EA ADJACENT DENTS. CLOSING ACTION ON 04/14/03. ON N/R 00425. REMOVED AND REPLACED CDP AIR TUBE MANIFOLD AT 14TH STAGE IAW M/M 75-00-04-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,971 hrs · 20,188 cycles

MAIN DECK SEAT TRACK STA 595 TO 675 AND STR FOR FLOORBOARDS BAD. CLIP NUTS HOLES CORRODED TOP AND BOTTOM. BLENDED DAMAGE TRACK IAW SRM 53-10-00 STA 595 TO 620 FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR SECTIONS AND SPLICES IAW SRM 53-70-00.

Part: STRUCTURE — CRACKED (T/R SUPPORT) · airframe 76,971 hrs · 20,188 cycles

COMPLY WITH EA 8-7832-68786 NR 1 ENGINE RM T/R-DISPOSITION OF CRACK IN T/R FWD SUPPORT EXTRUSION. CLOSING ACTION ON 04/15/03. COMPLIED WITH EA 8-7830-68786. NR 1 ENGINE RT T/R-DISPOSITION OF CRACK IN T/R FWD SUPPORT EXTRUSION.

Part: SLAT TRACK — WORN (LT WING) · airframe 76,971 hrs · 20,188 cycles

COMPLY WITH EA 8-2780-68790 FLIGHT CONTROLS-SLATS-REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9. CLOSING ACTION ON 04/14/03. COMPLIED WITH EA 8-2780-68790 FLIGHT CONTROLS-SLAT- REWORK OF WORN AREA ON LT WING SLAT TRACK NR 9.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 76,971 hrs · 20,188 cycles

LEFT MLG W/W AFT O/B STRUCTURE HAS CRACKED L-ANGLE. CLOSING ACTION ON 04/11/03. REMOVED ANGLE IAW SRM 51-31-01, FAB ANGLE ON TRAVLER T2/325914. INSTALLED ANGLE IAW SRM 51-31-01.

Part: BRACKET — CRACKED (NR 2 ENGINE) · airframe 76,971 hrs · 20,188 cycles

NR 2 ENGINE FAN CASE ANTI-ICE HOT DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT HAS CRACK. CLOSING ACTION ON 04/10/03. REMOVED AND REPLACED NR 2 ENGINE FAN CASE ANTI-ICE HOT AIR DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT IAW M/M 70-00-00-2.

Part: SEAL — TORN (CARGO DOOR) · airframe 76,971 hrs · 20,188 cycles

AFT PIT LOWER CTR DOOR SEAL TORN. CLOSING ACTION ON 04/11/03. NEW SEAL FAB ON TRAVELER T2/324829, LOCATED AND DRILLED IAW SRM 51-31-01, TREATED AND PRIMED IAW SRM 51-21-01, TO BE INSTALLED ON W/C 53SI1516-01.

Part: FLANGE — GOUGED (NR 3 PYLON) · airframe 76,971 hrs · 20,188 cycles

NR 3 PYLON FAIRING 487AR MOUNTING FLANG BOTH SIDES GOUGED. REMOVED AT MOUNTING FLANGES IAW SRM 51-31-01, FOUND BOTH FLANGES TO BE OUT OF LIMITS IAW SRM 51-00-00. FAB 2 NEW FLANGES USING MAT 301-1/4 HARD .05056 IAW SRM 54-31-02, INSTALLED FLANGES IAW SRM 51-35-01.

Part: BRACKET — BROKEN (NR 1 PYLON) · airframe 76,971 hrs · 20,188 cycles

NR 1 PYLON NUT PLATE BRACKET BROKEN FOR 473FL LT SIDE. CLOSING ACTION ON 04/09/03 REMOVED BRACKET IAW SRM 51-35-01. RECEIVED NEW BRACKET FROM FAB SHOP ON TRAVLER T2/324972, DRILLED AND LOCATED PER SRM 51-31-01. TREATED AND PRIMED PER SRM 51-21-01, INSTALLED PER SRM 51-35-01.

Part: LIGHT — FAILED (STROBE) · airframe 76,971 hrs · 20,188 cycles

UPPER AND LOWER BEACON FAILS FLASH RATE CHECK. CLOSING ACTION 04/09/03. REMOVED AND REPLACED UPPER AND LOWER BEACON ASSEMBLIES. OP'S CHECK GOOD IAW M/M 33-45-00-4.

Part: HINGE — GOUGED (TAIL CONE) · airframe 76,971 hrs · 20,188 cycles

TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC 7011-1. CLOSING ACTION ON 04/09/03. COMPLIED WITH EA 8-5240-68763, TAIL CONE - PATIO DOOR HINGE REPAIR P/N AKC 7011-1.

Part: SEAL — GOUGED (NR 3 ENGINE) · airframe 76,971 hrs · 20,188 cycles

NR 3 ENGINE O/B CORE COWL UPPER SEAL AFT OF AFT HINGE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED DAMAGED SEAL IAW SRM 51-35-01. FAB NEW SEAL ON TRAVELER T2/304970. INSTALLED SEAL IAW SRM 51-35-01.

Part: STRIP — WORN (TAILCONE) · airframe 76,971 hrs · 20,188 cycles

TAIL CONE AFT END OF RT PATIO DOOR, METAL CLOSEOUT STRIP IS WORN THRU (MARKED) 6 INCH LENGTH. CLOSING ACTION ON 04/07/03. REPLACED CLOSEOUT STRIP IAW SRM 51-31-01. NEW CLOSEOUT, FAB PER MAE TRAVLER T2/324996.

Part: SILL — GOUGED (CARGO DOORWAY) · airframe 76,971 hrs · 20,188 cycles

CENTER CARGO DOOR JAMBS AFT STRUCTURE 2 EA UPPER CHAFE PLATES ARE GOUGED. CLOSING ACTION ON 04/07/03. REMOVED 2 EA SCUFF PLATES IAW SRM 51-31-01. REMOVED GOUGES FROM AFT SCUFF PLATE. NEG MATERIAL LOSS IAW SRM 53-00-01. ROUTED LWR SCUFF PLATE FAB SHOP. RECEIVED NEW SCUFF PLATE FROM FAB SHOP. TREATED AND PRIMED 2 EA SCUFF PLATES IAW SRM 51-21-01. INSTALLED 2 EA SCUFF PLATES IAW SRM 51-31-01.

Part: INTERCOSTAL — CRACKED (TAILCONE) · airframe 76,971 hrs · 20,188 cycles

N 132 TAILCONE LT MAINT PLATFORM WEB IS CRACKED BETWEEN 2EA ACTUATOR ROD/STIFFNERS/ SUPPORT ANGLES PARALLER TO MAINT PLATFORM AT NON-SKID AREA. CLOSING ACTION ON 04/07/03. REMOVED CRACKED DOUBLER AND INTERCOSTAL IAW SRM 51-35-01. FABRICATED REPAIR DOUBLER IAW DC-10 SRM 53-52-01,53-00-01. FABRICATED NEW INTERCOSTAL ON M.A.E. TRAVELER T2/325492. INSTALLED NEW REPAIR DOUBLER AND INTERCOSTAL IAW DC-10 SRM 51-35-01.

Part: ANGLE — CHAFED (NR 3 PYLON) · airframe 76,971 hrs · 20,188 cycles

NR 3 PYLON ANGLE CHAFED THROUGH AT AFT RIB SUPPORT FOR PANEL 487FL. CLOSING ACTION ON 04/07/03. REMOVED RIB SUPPORT IAW SRM 51-31-01. FAB NEW RIB SUPPORT ON TRAVELER T2/325651. LOCATED AND DRILLED NEW PART IAW SRM 51-31-01. TREATED AND PRIMED RIB SUPPORT IAW SRM 51-21-01. INSTALLED NEW RIB SUPPORT IAW SRM 51-31-01.

Part: BRACKET — CRACKED (NR 3 PYLON) · airframe 76,971 hrs · 20,188 cycles

NR 3 PYLON FLUID LINE SUPPORT BRACKET CRACKED JUST OUTBOARD OF THROTTLE CABLE QUARDANT. CLOSING ACTION ON 04/08/03. REMOVED SUPPORT BRACKET IAW SRM 51-31-01. FAB NEW SUPPORT BRACKET ON TRAVELER T2/325535. LOCATED AND DRILLED NEW PART IAW SRM 51-31-01. INSTALLED SUPPORT BRACKET IAW SRM 51-31-01.

Part: SEAL — WORN (TAILCONE) · airframe 76,971 hrs · 20,188 cycles

TAIL CONE AFT END OF LT PATIO DOOR, 13 INCH METAL CLOSEOUT SEAL IS WORN, UPPER TO LOWER SURFACE. CLOSING ACTION ON 04/07/03. REMOVED CLOSEOUT STRIP SEAL LWR AFT END OF LT PATIO DOOR IAW SRM 51-31-01. FAB NEW CLOSEOUT STRIP SEAL PER TRAVELER T2/325001. INSTALLED CLOSEOUT STRIP SEAL PER SRM 51-31-01.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 73,540 hrs · 19,016 cycles

AFTER T/O, LANDING GEAR WOULD NOT RETRACT.

Part: STRUCTURE — DAMAGED (SPOILER)

ON POSTFLIGHT FOUND NR 2 SPOILER DAMAGED. REMOVED AND REPLACED NR 2 SPOILER.

Part: FUSE — CRACKED (HYS SYS)

99-182 - AFT GEAR RETRACTION, HYD QUAN AND PRESSURE ON NR 3 SYS DROPPED TO 0. REPLACED THE CRACKED LOCK OUT FUSE PER MM 32-31-06-2 ALSO NR 3 HYD SYS CASE DRAIN FILTER CK IS OK PER MM 29-12-02-2 AND MM 29-12-17-2. LEAK CK IS OK CLOSED SECURED AND NR 3 ENG COWLING C/W RII.

Part: SPAR — CORRODED (WS 118-112)

LEFT AFT UPPER CORNER OF THE CENTER WING BOX AT BS 118 TO 112 TO INCLUDE THE CLOS RIB AND ATTACH UPPER SKIN PLATES AT BS 1370 TO 1358 WERE FOUND WITH EXFOLIATION CORROSION DURING C-CHECK INSP IN THE LT MLG WHEEL WELL. ALL CORROSION HAS BEEN REMOVED, WAITING FOR THE ENG AUTH FOR REPAIR OR DISPOSITION.

Part: SKIN — DAMAGED (NR 1 LE SLAT)

ON WALKAROUND FOUND LT NR 1 L/E SLAT INBD FAIRING MISSING. ALSO, DAMAGE TO L/E SLAT ASSY. *S/D* REPLACED NR 1 L/E SLAT (LT) ASSY WITH FAIRING PER MM 27-80-01-4.

Part: FIRE LOOP — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENG FIRE DETECT SYS LOOP-B LT ON IN FLT, RED TABS ACCOMPLISHED, CHECKED OK. APPROX 2 HRS LATER NR 1 ENG FIRE LIGHTS ON. ACCOMPLISHED RED TABS, EMERGENCY LANDING ABQ. LANDED OVERWEIGHT.

Part: CADC — MALFUNCTIONED (NR 2)

DURING T/O ROLL, F/O AIRSPEED INDICATOR REMAINED AT ZERO. ON CLIMBOUT, IT BEHAVED AS AN ALTIMETER. RETURNED AND LANDED AT LAX. REMOVED AND REPLACED NR 2 CADC. FOUND FLEX LINE LOOSE ON FRONT OF NR 2 DIGITAL AIR DATA COMPUTER NR 2 CADC, OPS CK OK IAW MM 34-16-01-2-2. F/O PITOT/STATIC SYSTEM LEAK CK IAW MM 34-16-01-2-2.

Part: SKIN — CRACKED (RT HORIZ STAB)

RT HORIZ STAB UPPER AFT SKIN PANEL HAS .5625 INCH CRACK AT K/B AFT CORNER APPROX 1 INCH FROM PANEL AFT EDGE, ADJACENT TO WORKING BULKHEAD.

Part: SKIN — CRACK (LT TE FLAP)

LT WING O/B FLAP, I/B UPPER SURFACE T/E SKIN HAS 5 INCH CRACK. REPAIRED PER SRM 57-10-00 PG 10 FIG 7.

Part: BRACKET — CRACKED (LT LE FLAP)

LEFT O/B SLAT DRIVE OUTER BRACKET CRACKED .187 LONG IN FILLET RADIUS OF FWD FLANGE.