N318FE

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL QTY) · airframe 99,512 hrs · 29,827 cycles

PDIS 318 28-40 7406 18FEB20 MEM FACT U LOGPAGES:3248935 LVL 2 FUEL QTY/USED CHK" ALERT- QRH PROCEDURES FOLLOWED. ALERT WENT OUT. REOCCURED AFTER ABOUT 5 MINS. UPDT 18FEB20 08:14 MEM U PERFORMED FSC TEST REF MD10-30 AMM 28-08-01-5. ALL TEST PASS. PERFORMED FQGS TEST REF MD10-30 AMM 28-41-00-5. ALL TEST PASS. REOP 18FEB20 11:34 U DSCRP IS REOPEN FOR WORK. AMT MECHANIC: 144602 FACT 18FEB20 11:36 MEM U PER MOCC PERFORMED STICKING OF ALL THREE FUEL TANKS NO.1 TANK READINGS ARE STICK READING AFT INNER WAS 18 FUEL CAL READS 6,O20 COCKPIT DISPLAY READING IS 6,000. TANK NO.2 STICK READING 13.5 FUEL CAL READS 6,830 COCKPIT DISPLAY READING IS 6,200. TANK NO.3 STICK READING 17 FUEL CAL READS 5,470 COCKPIT DISPLAY READS 5,800. REF MD10-30 AMM 12-11-07-3. BEFORE STICKING TANKS SUMPED TANKS FOUND WATER IN TANKS 1 AND 3.

Part: COMPARATOR — MALFUNCTIONED · airframe 98,454 hrs · 29,304 cycles

IAS COMPARATOR AND "SEL ELEV FEEL MAN" AND "SEL FLAP LIM OVRD". CAPTAIN AIRSPEED 9 KNOTS SLOWER THAN F/O AND SBY. CAPTAIN SHOWED 35 KNOT TAILWIND WITH A 3 KNOT HEADWIND ON F/O SIDE. APPRX FL160 HAD MODERATE PRECIP WHEN FIRST FAULT "IAS COMPARATOR" SHOWED. SHORTLY AFTER HAD A/P TRIP. CAPT SWITCHED TO CADC 2 FOR REMAINDER OF FLT. . FCC 1&2 HAVE 12 FAULTS CORRELATING TO DEBRIEF, RESULTING FROM "ADIRU-1 AD/ADIRU-2 AD" "TAS INV" AND "CAS INV" INCLUDING "A/T SNGL", "P F/D BOV", "A/P DISC", "F/L SNGL" AND "ELF SNGL". FACT 02JUN19 05:10 SLC U FOUND CAPT PITOT DRAIN OBSTRUCTED (NOT TOTALLY PLUGGED), WATER WAS SLOWLY SEEPING OUT, CLEARED DRAIN HOLES AND DRAINED APPRX 5CC'S OF REMAINING WATER. CHECKED F/O AND SBY PITOT DRAINS - NO OBSTRUCTIONS. BACK PURGED PITOT LINE FROM ADM Q/D FITTING UNTIL WATER WAS GONE. BLEW OUT SOME MINOR DEBRIS, BUT NO BUGS PUMPED UP CAPT PITOT SYSTEM, VERIFIED NO LEAKS AND IAS MATCHED TESTER AT VARIOUS SPEEDS. CHKD PITOT HEAT, OPS NML. REF AMM 34-11-00-2, 34-16-01-4 AND 34-16-00-5-1. PERF AUTO LAND SYSTEM RETURN-TO-SERVICE TEST ON EACH FCC (1 AND 2), ALL TESTS PASSED, 30-DAY PERIODIC AUTOLAND TIMER RESET - REF AMM: 22-00-00-2.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 98,133 hrs · 29,137 cycles

AFT FUSELAGE CUT OUT FOR ACCESS PANEL 311AB- LATCH LAND AREAS WORN / DAMAGED (KNIFE & CHAFED EDGES). CHECKED LIMITS, DAMAGED AREA FOUND TO BE OUT OF LIMITS, ORIG MAT .050", SEVERAL AREAS EXCEED 20% (.035") IAW SRM 53-00-01. REMOVED EXISTING REPAIR PARTS IAW SRM 51-31-01. FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND FILLER IAW EA. T8-5310-29098 BP2, (FUSELAGE- AFT LOWER SKIN REPAIR AT 311AB ACCESS DOOR- LATCH LAND AREAS WORN / DAMAGED). MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 98,133 hrs · 29,137 cycles

SEAT TRACK RBL 8. F/H 1273, 1266, 1199, 1193 AND 1133 HAS WORN AND BROKEN SCALLOPS. BLENDED AREA ON SEAT TRACK RBL 8 STA 1199-1133 IAW SRM 53-70-00 CHECKED LIMITS, MAX MATERIAL REMOVE AT SEAT TRACK UPPER CROWN IS .025 AFTER REWORK MATERIAL LOSS IS 0.040 FROM STA 1199 FOUND OUT OF LIMITS, FOR STA 1193 SCALLOPS BROKEN IS OUT LIMITS IAW SRM 53-70-00 FIG 5 TR 83340, RECEIVED NEW SEAT TRACK SECTION P/N 60-4508 BATCH NUMBER 000341727. REMOVED AND INSTALLED NEW SEAT TRACK SECTION RBL 8 STA 1133 TO 1209 IAW SRM 53-70-00. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 1059) · airframe 98,133 hrs · 29,137 cycles

MAIN CABIN SEAT TRACK CORRODED ON RT FLOOR FLANGE F/S 1059 RBL 7 (APPROX). REMOVED CORROSION IAW SRM 53-00-01, FOUND TO BE OUT OF LIMITS ORIG MAT .090 AFTER REWORK .045 IAW SRM 53-70-00 FIG 5 TR 88614. REMOVED & REPLACED DAMAGED SEAT TRACK SECT RBL 7 FROM STA 1049-1129 IAW SRM 53-70-00 SEAT TRACK P/N 60-4508 BATCH 0003002295, SPLICE PLATE FROM 7075-T6. 050C BATCH 0003002295, SPLICE HAT 60-7158 BATCH 0003416710. MAJOR REPAIR

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 98,133 hrs · 29,137 cycles

MCD AT STA 939 SEAT TRACK 47.50 SCALLOP DAMAGED. EVALUATED DAMAGE SCALLOP RT IS .110", LT SCALLOP IS .120" BOTH SCALLOPS STA 939 AT 47.5 SEAT TRACK ARE FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 TR 86354, RECEIVED NEW SEAT TRACK P/N 60-71-58, BATCH 003416710, LOCATED AND DRILLED IAW SRM 53-70-00, REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. MAJOR REPAIR.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 97,134 hrs · 28,610 cycles

DURING CRUISE AT FL330, NOTICED A METALLIC BURNING ODOR. DONNED MASKS AND FOLLOWED QRH FOR FIRE SMOKE OR FUMES CHECKLIST. COCKPIT FILLED WITH A GREY HAZY SMOKE. SMOKE AND FUMES LASTED FOR LESS THAN TWO MINUTES. DIVERTED, AND COMPLIED WITH ALL STEPS OF TSI 21-54/5470. RAN ENGINES AND A/C PACKS FOR 20 MINUTES. NO ODOR PRESENT AT ANY TIME. THE COALESCER BAGS WERE DIRTY WITH NO ODOR AND WERE REPLACED. RAN ENGINES IAW JRH.

Part: SHAFT — BROKEN (L1 DOOR) · airframe 96,561 hrs · 28,320 cycles

MDIS 318 52-10 5068 25DEC17 MEM FACT U RAMP REPORTED THAT L1 DOOR STOPPED IN THE MIDWAY WHEN OPENING OR CLOSING. FOUND SHAFT IN L-1 DOOR PDM AFT DRUM BROKEN. ITEM 410 IN IPC 52-11-50-01. REPLACED SAME REF. ASSEMBLY PROCEDURE IN CMM 52-11-09 STEP 2. B. (5) TO (7). COMLETED OPS CHECK (BLOWING DOOR) STILL REQUIRES RESET AND SERVICING. STILL REQUIRES GIRT BAR INSTALL. FACT 25DEC17 22:02 MEM U AMM: 52-10-01-6-0 INSTALLED GIRT BAR. RESET AND SERVICED BOTTLE. VERIFIED DOOR WOULD ARM. REF. AMM 52-11-07-2 INSTALLED PANELS AND OPS CHECKED NORMAL.

Part: SEAT TRACK — DAMAGED (BS 635-674) · airframe 95,111 hrs · 27,628 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT APPROX. BS 635, LONGERON 48L. REMOVED AND REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-70-00, FIG.1, PAPE 6.1-6B, VOL.1 AND DWG SR10-53-002.

Part: SKIN — CRACKED (RT WING) · airframe 95,111 hrs · 27,628 cycles

RT WING FIXED L/E NOSE, ABOVE NR 3 PYLON, O/B BOTTOM SIDE, GAP FAIRING IS CRACKED AT THE FWD ATTACH FASTENERS. REPLACED SKIN PANEL AS REQUIRED PER DWG ARB2326 AND SRM 51-31-01,VOL 2.

Part: NUT PLATE — DAMAGED (E/E BAY) · airframe 95,111 hrs · 27,628 cycles

AFT ACCESSORY BAY, NUTPLATE BROKEN ON LT SIDE JUST FWD OF BS 2164. REPAIRED IAW SRM 53-00-01, FIG 4, SHT 2, VOL 1.

Part: SPAR WEB — CRACKED (NR 3 PYLON) · airframe 95,111 hrs · 27,628 cycles

NR 3 PYLON INSIDE ACCESS PANEL 487CL LT SIDE UPPER SPAR WEB PAN IS CRACKED APPROX 3 INCHES AT STA YN248, JUST UNDER FUEL LINE AT SUPPORT FITTING LOCATION. REPAIR PER DWG.

Part: TEE FITTING — CRACKED (BS 1156) · airframe 95,111 hrs · 27,628 cycles

BS 1156 TEE CAP FWD HORIZONTAL LEG HAS A CRACK AT THE AFT FASTENER HOLE UNDER THE SPLICE PLATE ONE ROW ABOVE LONGERON 37L. REPAIRED LT TEE CHORD IAW EA 8-5310-T0330606

Part: STRUCTURE — CRACKED (RT WING SLAT) · airframe 95,111 hrs · 27,628 cycles

RIGHT WING, NR 2 SLAT, INTERIOR SIDE HAS A CRACK AND MISSING FASTNER. OTBD CORNER OF SLAT INBD SIDE. REPAIRED IAW SRM 57-10-00 FIG 31, PAGE 109 AND DWG 6225

Part: BULKHEAD — CRACKED (RT WING) · airframe 95,111 hrs · 27,628 cycles

RIGHT WING LEADING EDGE SPAR BULKHEAD XORS562. SCALLOPED WING SKIN CRACKED ABOVE OTBD SLAT TRACK NR 10 PULLEY. INSTALLED REPAIR DOUBLER ON IAW SRM 57-10-00 FIG 71 VOL 1.

Part: RIB — CRACKED (LT WING) · airframe 95,111 hrs · 27,628 cycles

LT WING FIXED LE RIB HAS SMALL CRACK AT UPPER AFT END 10 IN I/B OF NR 15 SLAT TRACK. INSTALLED REPAIR ANGLE REF SRM 57-20-00 FIG 1 SHEET 1 VOL. 1.

Part: WEB — CRACKED (TAILCONE) · airframe 95,111 hrs · 27,628 cycles

RT TAILCONE PATIO DOOR FWD OPERATING CRANK ATTACH BRACKET SEPARATING FROM FLOOR. REMOVED AND REPLACED WEB.

Part: CHANNEL — CORRODED (BS 840) · airframe 95,111 hrs · 27,628 cycles

FWD CARGO BAY FRAME J CHANNEL AND FASTENERS ARE SHOWING SURFACE CORROSION AT BS 840, LONGERONS 51L AND 51R. REPAIRED THE CHANNEL IAW SRM 53-30-00. FIG 8, SHEET 1, VOL 1.

Part: SKIN — CRACKED (RT WING) · airframe 95,111 hrs · 27,628 cycles

RIGHT WING WING TIP, LOWER SKIN LE AT APPROX XW 918 AND OUTBD OF STRINGER 5, CRACKED. REPAIRED THE SKIN IAW SRM 57-10-00 FIG 85 SHTS 3-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 95,111 hrs · 27,628 cycles

FWD AVIONICS COMPARTMENT, STA 465 AT LONGERON 37L FUSELAGE FRAME IS CRACKED, 2017-01-03. REPAIRED FRAME REF SRM 53-30-00 FIG 11 SHEETS 1 THRU 4.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 95,111 hrs · 27,628 cycles

NR 1 PYLON REQUIRES REMOVAL FOR ACCESS TO REPAIR PYLON BULKHEAD FLANGE CRACK REF N676 THIS WORK ORDER. REMOVED AND REPLACED PYLON BULKHEAD PER DAC DWG AUB7025.

Part: SEAT TRACK — WORN (BS 1691-1731) · airframe 95,111 hrs · 27,628 cycles

MAIN DECK SEAT TRACK BS 1720 RBL 103 FOUND WORN. REPAIRED THE SEAT TRACK IAW SRM 53-70-00 FIG. 1 SHEET 1 PAGE 3 VOL. 1.

Part: SKIN — DAMAGED (SPOILER) · airframe 95,111 hrs · 27,628 cycles

RIGHT WING NR 3 SPOILER HAS A DEEP CHAFE/GOUGED AREA ON LOWER T/E SECTION . REPAIRED IAW SRM 51-71-00 VOL.II.

Part: SEAT TRACK — WORN (BS 1090-1096) · airframe 95,111 hrs · 27,628 cycles

MAIN DECK SEAT TRACK BS 1090, RBL 103 WORN. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 2, VOL 1 AND JPF ITEMS 3-5.

Part: SEAT TRACK — DAMAGED (BS 1383-1389) · airframe 95,111 hrs · 27,628 cycles

MAIN DECK SEAT TRACK BS 1383 - 1389, RBL 75 WORN. CLEANED AND LIMITS VERIFIED., INSTALLED REPAIR IAW SRM 53-70-01 FIG. 1 VOL 2 AND SRM 51-41-01 VOL 2 ALONG WITH JPF ITEMS2-5.

Part: SEAT TRACK — WORN (BS 1019) · airframe 95,111 hrs · 27,628 cycles

MAIN DECK SEAT TRACK DAMAGED AT BS 1019, LBL 8 MAIN DECK SEAT TRACK SECTION REMOVED AND REPAIRED IAW JPF NR 3 AND 4 AND IN IAW SRM 53-70-00 VOL. I FIG. 2A PG.11.

Part: SEAT TRACK — DAMAGED (BS 635-674) · airframe 95,111 hrs · 27,628 cycles

MAIN DECK SEAT TRACK IS DAMAGED AT BS 635, LONGERON 48L. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG. 1 VOL. 1.

Part: SKIN — DELAMINATED (TE FLAP VANE) · airframe 95,111 hrs · 27,628 cycles

RIGHT HAND OUTBOARD FLAP VANE TOP SURFACE UNDER NR 5 RUBSTRIP IS DELAM. REPAIRED RT O/B FLAP TOP SURFACE PER SRM 57-00-01 VOL I FIG 4 SHT 1.

Part: TEE FITTING — CRACKED (BS 595 BULKHEAD) · airframe 95,111 hrs · 27,628 cycles

BS 595 BULKHEAD TEE CAP FWD HORIZONTAL LEG HAS A .5 INCH CRACK AT LONGERON 39L. REPAIRED IAW EA 8-5310-T0330367.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 94,861 hrs · 27,522 cycles

MAIN CARGO DOOR ACTUATOR SUPPORT CORRODED AND PITTED. REMOVED AND REPLACED FITTING PER DWG 6084.

Part: THERMOCOUPLE — MALFUNCTIONED (NR 3 ENGINE) · airframe 94,447 hrs · 27,342 cycles

DURING CRUISE AT FL350, LEVEL 2 ENGINE 3 EGT HIGH. ENGINE NR 3 EXCEEDANCE LEVEL 1. THE EGT EXCEEDANCE 1000 DEGREE EGT FOR SERIES 30 QRH ENG EGT HI CHECKLIST WAS ACCOMPLISHED. ENGINE INDICATIONS WERE NORMAL AT MINIMUM THRUST. THE ENGIN EXCEEDANCE REMAINED DURING ENTIRE FLIGHT AND WAS ANNUNCIATED AGAIN ON LANDING. THE NR 3 ENGINE REMAINED AT IDLE DURING THE REST OF THE FLIGHT AND SHUTDOWN AFTER LANDING. R & R NR 3 ENGINE FWD EGT LEAD, AFT EGT LEAD, BOT RT THERMOCOUPLE AND UPPER RT THERMOCOUPLE IAW MM 77-21-02-2. ACCOMPLISHED ENGINE RUN AND EGT VERIFIED NORMAL IAW JRH CH'S 6 AND 7, EGT STEADY AND WITHIN PRESCRIBED PARAMETERS.

Part: BRAKE — OVERHEATED (MLG) · airframe 94,201 hrs · 27,243 cycles

BRAKE TEMPERATURE NR 7 LEVEL 2 HOT BRAKE. BRAKE TEMP WAS 750 DEG & INCREASING RIGHT AFTER GEAR RETRACTION, AT 11,000 & 230KNTS THE GEAR WAS EXTENDED. THE TEMP CONTINUE INCREASING & REACHED 880 AFTER GEAR EXTENDED. COMPLIED WITH QRH PROCEDURES. AN EMER WAS DECLARED & A SAFE LANDING COMPLETED.

Part: WIRE HARNESS — DEFECTIVE (NR 2 ENGINE) · airframe 94,057 hrs · 27,186 cycles

ON DESCENT RECEIVED 3 DIFFERENT INTERMITTENT NR 2 ENG FIRE WARNINGS. NO SIGN OF FIRE, NO RED LIGHT IN FIRE HANDLE. FOUND BAD HARNESS FOR PYLON B LOOP SEGMENT. R & R HARNESS FROM P1-8224 - P1-8694.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 93,276 hrs · 26,872 cycles

ELECTRICAL ODOR DETECTED. DONNED O2 MASKS & DIVERTED BACK. PERFORMED AIR CONDITIONING PACK & DISTRIBUTION DUCT ODOR TASK IAW AMM 21-53-00-7. OPERATIONS CHECKED NORMAL. R & R REMAINING COALESCE BAGS 1 & 2 IAW AMM 21-54-03-2. NO SMELL PRESENT OF ELEC ODORS WITH POWER OFF & POWER ON. ALL 3 ENGS RUNNING. ALL 3 PACKS RUNNING & INDIVIDUALLY.

Part: PRESSURE SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 927 hrs · 26,625 cycles

AT FL 350 WITH ENG & WING ANTI-ICE ON, RECEIVED A LEVEL 3 AIR MANIFOLD 1 FAIL. ALERT GONE AT APPROX 15,000'. USED THROTTLE 1 FOR APPROACH & LANDING & ALERT DID NOT RETURN. REPLACED LT NR 1 MANIFOLD PRESS SWITCH IAW AMM 36-23-03-4. NO LEAKS NOTED.

Part: BATTERY — FAILED (LIFE RAFT) · airframe 922 hrs · 26,403 cycles

L1 DOOR LIFE RAFT WILL NOT TEST. R & R BATTERIES. OPERATIONS CHECKED GOOD.

Part: TUBE — OUT OF ALIGNMENT (NR 2 ENGINE) · airframe 918 hrs · 26,251 cycles

LEVELING AT FL 340 HAD A LEVEL 2 NR 2 ENGINE FAULT. COMPLIED WITH QRH, UNABLE TO GET SATISFACTORY ENGINE FIRE TEST. RECEIVED FIRE WARNING & COMPLIED WITH QRH FOR ENGINE FIRE SEVERE DAMAGE. WHEN INSPECTING NR 2 ENGINE FIRE LOOPS, FOUND LEFT 7TH STAGE LOW PRESSURE TURBINE COOLING TUBES MISALIGNED. ADJUSTED THE TUBES IAW AMM 75-22-07-02.

Part: LINE — FAILED (BLEED SYS) · airframe 917 hrs · 26,197 cycles

RECEIVED AIR MANIFOLD ONE FAIL ALERT. BLEED ONE TURNED OFF & ALERT WENT AWAY. RETURN TO FIELD. TEMP COMING OUT OF BLEED ONE AT THE TIME WAS 210 C. FOUND SENSE LINE TO NR 1 FAN AIR VALVE BAD. R & R SENSE LINE.

Part: CHIME — INOPERATIVE (COCKPIT DOOR) · airframe 916 hrs · 26,167 cycles

COCKPIT DOOR CHIME WILL NOT CHIME. REMOVED AND REPLACED PER AMM 52-54-01. OPS CHECKED GOOD IAW AMM 52-54-01-5

Part: ANGLE — CORRODED (BS 1368) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

FOUND FOUR DOME NUTS BROKEN AT AFT FUSELAGE LOWER AUX FUEL CELL BLADDER PANEL. REPAIRED IAW EA 8-5730-T0313783 REV . MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

FOUND CORROSION AT BS 1368 ON TOP SIDE OF LOWER AUX FUEL CELL BLADDER PANEL LANDING. REPAIRED IAW EA 8-5730-T0313685 REV.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

CENTER CARGO DOOR AFT LOWER CUT OUT CORNER, REPAIR HAS DAMAGE. REPLACED DAMAGED AREA IAW SRM 53-00-01. REMOVED DOUBLERS TWO EACH IAW SRM 51-31-01. FABRICATED NEW ANGLE & REPAIR ANGLE. FABRICATED NEW DOUBLERS THREE EACH. INSTALLED ANGLE, REPAIR ANGLE & NEW DOUBLERS IAW SRM 51-31-01 & SRM 53-50-00 FIG 26 SHEETS 3, 4 & 5. TREATED & PRIMED IAW SRM SRM 51-21-01. APPLIED TOPCOAT IAW SRM 51-21-02. MAJOR REPAIR.

Part: ANGLE — CORRODED (BS 1368) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

FOUND CORROSION AT BS 1368 ON LT VERTICAL SECTION OF LOWER AUX FUEL CELL BLADDER PANEL LANDING. REMOVED DAMAGE & FABRICATED A NEW ANGLE. INSTALLED IAW SRM 51-31-01.

Part: FLOORBEAM — CORRODED (BS 1701) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

CENTER CARGO BAY BS 1701 LBL 5, FLOORBEAM HAS CORROSION ON UNDERSIDE OF CAP. REPAIRED IAW SRM 53-00-01 FIG 9, AND SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR PANEL BETWEEN STATION 1853 - 1887 LBL 8 - RBL 8 IS DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1102745 MATERIAL A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1884 - 1853 LBL 24, END OF PANEL FASTENER PULLED THROUGH. FABRICATED NEW FLOOR PANEL ON T14 1103645 MATERIAL A402H 48X144 BATCH 2704087. REMOVED & INSTALLED PANEL IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR SUPPORT LOCATED AT STATION 1887 - 2007 FWD EDGE EXFOLIATED & BROKEN AT LBL 24. R & R MAIN DECK FLOOR SUPPORT IAW SRM 51-31-01. FLOOR SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. MAJOR REPAIR.

Part: FRAME — GOUGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

LEFT CABIN, BS 535 STRINGER -23L, FRAME INBD FLANGE, PREVIOUS REPAIR, GOUGED. GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A, ORIGINAL MATERIAL 0.125 INCHES, D=0.100 INCHES. REMOVED PREVIOUS REPAIR IAW SRM 51-31-01, FABRICATED, LOCATED & DRILLED TWO EACH ANGLES FROM T14 1105527 & T14 1105524, FILLER & SHIM IAW SRM 53-30-00, 7075-T6 .090 & 7075-T6 .125. TREATED & PRIMED PARTS IAW SRM 51-21-01. INSTALLED TWO EACH ANGLES, SHIM & FILLER IAW SRM 53-30-00 TR14450. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1561 - 1661 RBL 8 - 24, DAMAGED AROUND EDGE & INSERTS. REMOVED FLOOR PANEL IAW AMM 53-21-04-2. FABRICATED NEW FLOOR PANEL ON T14 1102741 USING A402H 48X144 IAW SRZ-25-005 REV K. INSTALLED NEW FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 675 - 735 LBL 47 - 74 PUNCTURED, DENTED & WORN. R & R FLOOR PANEL IAW AMM 53-21-04-2. FABRICATED NEW PANEL ACA7373-8 ON T14 1102696 MAT A402H 44X144 BATCH 2704169. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 879 - 979 RBL 47 - 74 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103085 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 795 - 835 RBL 74 - 107, PUNCTURED & DENTED. REMOVED DAMAGED FLOOR PANEL & FABRICATED NEW FLOOR PANEL ON T14 1105513, PN FX-ADA8344-3, SRM 51-62-01 & DWG SRZ-25-005. INSTALLED NEW FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1099 - 1159 LBL 8 - 27, PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103524, MATERIAL A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 755 - 795 RBL 94 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1102919 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 755 - 775 RBL 24 - 47 PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103011 MAT A402H 48X144 BATCH 2677229. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1099 RBL 74 - 107 MULTIPLE DENTS & PUNCTURES. FABRICATED NEW FLOOR PANEL ON T14 1103526 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1099 - 1159 LBL 74 - 107 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1103731 MAT A402H 48X144 BATCH 2708047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1821 - 1853 LBL 74 - 107 MULTIPLE DENTS. FABRICATED NEW FLOOR PANEL ON T14 1102699, MATERIAL A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1561 - 1661 RBL 74 - 107 MULTIPLE PUNCTURES. FABRICATED NEW FLOOR PANEL ON T14 1102742 MATERIAL A402H 48X144. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1099 RBL 27 - 47 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103528 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1009 LBL 47 - 74 EDGES CHIPPED & DISBONDED. FABRICATED NEW FLOOR PANEL ON T14 1103529 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1099 LBL 74 - 107 PUNCTURES & DENTS. FABRICATED NEW FLOOR PANEL ON T14 1103733 MAT A402H 48X144 BATCH 2208047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1361 - 1481 LBL 27 - 47 MULTIPLE DENTS. FABRICATED NEW FLOOR PANEL ON T14 1103647 MATERIAL A402H 48X144 BATCH 2708047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 755 - 795 RBL 74 - 86 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1102920 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1821 - 1884 LBL 47 - 74 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1102698, MATERIAL A402 48X144 BATCH 2704619. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1099 - 1157 RBL 47 - 74 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1104149 MAT A402H 48X144 BATCH 2708047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1099 RBL 47 - 74 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103527 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 735 - 795 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103071 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1361 - 1481 LBL 74 - 107 MULTIPLE DENTS. FABRICATED NEW FLOOR PANEL ON T14 1103521 MATERIAL A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1099 - 1159 LBL 8 - RBL 8 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1103525 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1099 - 1159 LBL 27 - 47 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1103523 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1661 - 1741 LBL 24 - 47 PUNCTURES. FABRICATED NEW FLOOR PANEL ON T14 1103440 MATERIAL A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 795 - 879 RBL 8 TO LBL 8 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103534 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1561 - 1661 LBL 74 - 107 PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1102700 MATERIAL A402H 48X144. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1099 LBL 27 - 47 MULTIPLE DENTS. FABRICATED NEW FLOOR PANEL ON T14 1103732 MAT A402H 48X144 BATCH 2708047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1159 - 1219 RBL 75 - 107 DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1102506 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1321 - 1361 LBL 27 - 47 DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1103075 MATERIAL A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 979 - 1099 RBL 8 - LBL 8, AFT EDGE CHIPPED & DISBONDED. FABRICATED NEW FLOOR PANEL ON T14 1103084 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 795 - 835 LBL 74 - 107 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103735 MAT A402H 48X144 BATCH 2708047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1821 - 1863 LBL 8 TO RBL 8 PUNCTURED & AFT EDGE FASTENERS PULLED THROUGH. FABRICATED NEW FLOOR PANEL ON T14 1102697, MATERIAL A402H 48X144 BATCH 2704169. REMOVED & INSTALLED NEW FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 795 - 824 RBL 24 - 48 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103734 MAT A402H 48X144 BATCH 2708047. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1219 - 1261 RBL 74 - 86 DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1103077 MATERIAL A402H 48X144 BATCH 2704169. PANEL INSTALLED ON ROUTINE CARD 53C2505-01. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 879 - 979 LBL 74 - 107 MULTIPLE DENTS & PUNCTURES. FABRICATED NEW FLOOR PANEL ON T14 1103530 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 735 - 840 LBL 47 - 74 PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103014 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 824 - 879 RBL 47 DENTED & PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1103532 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED NEW PANEL IAW AMM 53-21-04-2 & SRZ-25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 735 - 755 LBL 8 - 24 PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103013 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 795 - 879 RBL 8 - 27 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103533 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 735 - 824 RBL47 - 74 PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103004 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 735 - 755 RBL 74 - 107 PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103008 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 824 - 879 LBL 47 - 74 , PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103536 BATCH 2704163 MAT A402H 48X144. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 735 - 755 RBL 8 - LBL 8 PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103012 MAT A402H 48X144 BATCH 2677229. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 795 - 879 LBL 27 - 47, PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1103535 MAT A402H 48X144 BATCH 2704163. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ-25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 735 - 795 LBL 27 - 47 PUNCTURED, DENTED & DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1102505 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED FLOOR PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 735 - 755 RBL 27 - 47, PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1103010 MAT A402H 48X144 BATCH 2704169. REMOVED & INSTALLED PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

LEFT SIDE WALL BS 1159 - 1179 STRINGER 17L CORRODED. REMOVED CORROSION IAW SRM 53-00-01. ORIG MATERIAL .100 MATERIAL LOSS .075 REMAINING MATERIAL .025 FOUND TO BE OUT OF LIMITS USING TR 83340 IAW SRM 53-00-01. FABRICATED NEW LONGERON ON T14 1102066 7075 T73511 BATCH 0002498047. R & R LONGERON IAW SRM 51-31-01. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL 879 - 979 LBL 47 - 74 FWD & OTBD PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1103531 BATCH 2704163 MAT A402H 48X144. REMOVED & INSTALLED NEW PANEL IAW AMM 53-21-04-2 & SRZ 25-005 REV K. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

UPON REMOVAL OF FLOOR PANEL STATION 1561 - 1661 RBL 8 - 249, NR N00591, FOUND SEAT TRACK FLANGE IS EXFOLIATED AT RBL 27.50 AT STATION 1563. BLENDED AREA IAW SRM 53-70-00. ORG MAT=.080", MAT LOSS=.080" REMAINING=.000". FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00,FIG 5,SHEET 2. SEAT TRACK AT STA 1563,RBL 27.50. FABRICATED NEW SEAT TRACK USING P/N 60-10964 BATCH# 0002064395 IAW SRM 53-70-00,FIG1 SHEET 3, FABRICATED SPLICE HAT USING 60-7158/7075-T6511,BATCH#0001366488 AND SPLICE PLATE USING 7075-T6 .050" BATCH # 0002646460 IAWSRM53-70-00 FIG1 SHEET 4. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1, SHEETS 3&4. MAJOR REPAIR

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1301 - 1361 RBL 74 - 107 MULTIPLE PUNCTURES. NEW FLOOR PANEL FABRICATED IAW SRZ-25-005 & SRM 51-62-01 ON T14 1104588. PANEL TO BE INSTALLED ON ROUTINE CARD 000604. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1381 - 1501 LBL 8 - 24 PUNCTURED & DENTED. NEW FLOOR PANEL FABRICATED IAW SRZ-25-005 & SRM 51-62-01 ON T14 1104587. PANEL TO BE INSTALLED ON ROUTINE CARD 000604. MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR PANEL STATION 1887 - 2007 LBL 24 IS DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1103736 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON NR 1057. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR PANEL STATION 1887 - 1920 LBL 8 - 27 IS DELAMINATED & MISSING INSERTS. FABRICATED NEW FLOOR PANEL ON T14 1103538 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON NR 1020 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,519 hrs · 26,088 cycles

AFT CARGO FLOOR INNER SKIN THE DRAIN FITTING ATTACH DOUBLER HAS CORROSION STATION 1871- 1887 BETWEEN STRINGER -52R TO -51R. REMOVED CORRODED DOUBLERS, FABRICATED NEW DOUBLERS & INSTALLED IAW SRM 53-20-00 FIG 6. CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR PANEL STATION 1887 - 1920 RBL 8 - 27 IS DELAMINATED & IS MISSING INSERTS. FABRICATED NEW FLOOR PANEL ON T14 1103537 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON NR N1020. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1219 - 1261 LBL 74 - 82 MULTIPLE DENTS. CLEANED PANEL IAW AMM 12-22-07-01. UPON FURTHER INSPECTION DAMAGE EXCEEDS SRM IAW SRM 53-60-00 FIG 7. FABRICATED NEW FLOOR PANEL ON T14 1103650 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1159 - 1261 LBL 8 - 27 PUNCTURED & DENTED. AFTER FURTHER INVESTIGATION THE PUNCTURED & DENT DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-60-00 FIG 7 DIM =6.2. FABRICATED NEW FLOOR PANEL ON T14 1103522 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1301 - 1361 LBL 72 - 107 DENTED & INSERTS MISSING. FABRICATED NEW FLOOR PANEL ON T14 1103648 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2501-01. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1261 - 1301 RBL 74 - 107 MULTIPLE PUNCTURES. CLEANED FLOOR PANEL IAW AMM 12-22-02-7. UPON FURTHER INSPECTION FOUND FLOOR PANEL TO BE BEYOND REPAIR LIMITS IAW SRM 53-60-00 FIG 6. FABRICATED NEW FLOOR PANEL ON T14 1103649 USING A402H 48X144 IAW SRZ25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL STATION 1281 - 1321 RBL 8 - 27 MISSING INSERTS. FABRICATED NEW FLOOR PANEL ON T14 1103076 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1361 - 1481 RBL 74 - 107 PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL T14 1103073 USING A402H 48X144 IAW SRZ -25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 91,519 hrs · 26,088 cycles

MCD FLOOR PANEL WITH LT MLG INSPECTION ACCESS PLATE HOLE IS DAMAGED. FABRICATED NEW FLOOR PANEL FOR STATION 1361 - 1481 LBL 47 - 74 ON T14 1100705 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1219 - 1261 RBL 86 - 107 PUNCTURED & DELAMINATE. FABRICATED NEW FLOOR PANEL ON T14 1103078 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR PANEL BS 1820 - 2007 RBL 8 - RBL 27 IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL BS 1157 - 1239 RBL 27 - 47, DENTED & DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

MAIN DECK FLOOR PANEL BS 1920 - 2001 LBL 8 - LBL 27 IS DELAMINATED & HAS TORN INSERT. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL BS 1159 - 1239 LBL 47-74, PUNCTURED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — WORN (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL BS 595 - 675 LBL 74 - 107 PUNCTURED & WORN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL BS 1401 - 1501 LBL 8 - RBL 8 DELAMINATED & INSERTS MISSING. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL STATION 1501 - 1561 RBL 8 - 27 DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1102504 USING A402 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 595 - 675 RBL 47 - 74, PUNCTURED, DENTED & WORN. FABRICATED NEW FLOOR PANEL ON T14 1101719 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 230 FL FIT CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 1481 - 1561 LBL 27 - 47, DELAMINATED AT LARGE DENT. FABRICATED NEW FLOOR PANEL ON T14 1103646 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (BS 1501-1561) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL BS 1501 - 1561 LBL 8 - RBL 8, AFT RT CORNER DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K. FLOOR PANEL INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL, BS 615 - 715 LBL 8 - 27, PUNCTURED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL, BS 595 - 675 RBL 27 - 47, PUNCTURED, DENTED & WORN. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DENTED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 595 - 675 LBL 47 - 75, PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL ON T14 1101873 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 230 FL FIT CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 1159 - 1239 LBL 27 - 47 PUNCTURED & DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1103081 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 1157 - 1261 RBL 8 - 27, DENTED & DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1103080 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BS 500) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL BS 500 RBL 57, FWD END INSERT MISSING. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K. FLOOR PANEL INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BS 500-795) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL, BS 500 - 795 RBL 100, PUNCTURED, DENTED & CORNER CHIPPED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 1119 - 1139 RBL 47 - 59 ACCESS PANEL DELAMINATED. FABRICATED NEW FLOOR PANEL ON T14 1103083 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BS 755-795) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL, BS 755 - 795 LBL 87-102, PUNCTURED, EDGE DAMAGED & INSERT MISSING. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BS 500-595) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL, BS 500 - 595 LBL 80, PUNCTURED & DENTED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 1361 - 1481 RBL 27 - 47, PUNCTURED. FABRICATED NEW FLOOR PANEL ON T14 1103074 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 53C2505-01 CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 91,519 hrs · 26,088 cycles

CABIN FLOOR PANEL, STATION 595 - 675 LBL 27 - 47, PUNCTURED & INSERT DAMAGED & MISSING. FABRICATED NEW FLOOR PANEL ON T14 1101872 USING A402H 48X144 IAW SRZ-25-005 REV K. PANEL INSTALLED ON WORK CARD 230 FL FIT CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (BS 735-755) · airframe 91,519 hrs · 26,088 cycles

FLOOR PANEL, BS 735 - 755 LBL 74 - 107, PUNCTURED & WORN. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 REV K AND INSTALLED. CLASSIFIED AS A CAT A MAJOR REPAIR.

Part: SKIN — CRACKED (ZONE 600) · airframe 90,673 hrs · 25,718 cycles

DURING WALK AROUND, RT WING FWD INBD CORNER OF SLAT DRIVE MECHANISM ACCESS DOOR APPEARS TO HAVE AN 1.5 INCH CRACK IN FIXED PANEL SKIN. INSTALLED DOUBLER REPAIR IAW SRM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 90,548 hrs · 25,668 cycles

FOUND L1 DOOR EVACUATION SLIDE REMOTE INDICATOR PRESS TO TEST LIGHT INOPERATIVE. REPLACED BATTERIES IN L1 DOOR SLIDE REMOTE INDICATOR PRESS TO TEST SWITCH IAW MM.

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 88,962 hrs · 24,989 cycles

DURING CLIMBOUT WITH AIRFRAME & ENGINE ANTI ICE ON, RECEIVED LEVEL 3 BLEED AIR 1 TEMP HIGH ALERT. PROCEEDED WITH QRH PROCEDURE. SHUTOFF BLEED AIR 1 AND TEMP DECREASED. ALERT WENT OUT. PEAK TEMP NOTED 295 DEG C. CLAMP ON LOW PRESSURE CHECK VALVE FAILED ALLOWING ENGINE BLEED TO DAMAGE FAN AIR VALVE WIRE HARNESS. LP DUCTING FROM RT SIDE WAS DAMAGED. DAMAGED DUCTING WAS REPLACED WITH NEW IAW WRI 72-00/0285, DAMAGED WIRE HARNESS WAS REPLACED IAW WRI 24-97/0301. PERFORMED PNEUMATIC SYSTEM TEST IAW MM 36-00-03-5 AND ENGINE RUN IAW JRH, ALL NORMAL WITH NO FAULTS.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 88,186 hrs · 24,645 cycles

FRAME MISREPAIRED AT BS 383. REPAIRED FRAME IAW SRM 53-00-01, FIG 8. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 500) · airframe 88,186 hrs · 24,645 cycles

LT OTBD FLAP BOTTOM SKIN HAS A CLUSTER OF SHARP DENTS JUST INBD OF VANE ROLLER ACCESS PANEL 557DB. INSPECTED DAMAGE AREA FOUND TO BE SERIES OF GOUGE SHARP CREASE DENTS TO INCLUDE ONE LOSE FASTENER - OUT OF LIMITS IAW SRM 57-10-00 PG 162A TO 48, HFEC DENT IAW NTSPM 06-10-01 NO CRACK FOUND. FABRICATED REPAIR DOUBLER IAW SRM 57-10-00, FIG 85, INSTALLED REPAIR DOUBLER IAW SRM 51-31-01, RSC TRACKING EA 8-5750-163986. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (BS 1708) · airframe 88,186 hrs · 24,645 cycles

CENTER CARGO DOOR FWD FRAME CORRODED AT LOWER CORNER BS 1708 BETWEEN L42 - 43R. REPAIRED DOOR FRAME IAW SRM 53-50-00 FIG 22, VOL 1. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (BS 1708) · corrosion level 2 · airframe 88,186 hrs · 24,645 cycles

LWR CTR CARGO COMPARTMENT DOOR FWD FRAME HAS CORROSION IN TWO LOCATIONS, AT ROLLER FITTINGS. REPAIRED DOOR FRAME BS 1708 L38 -43R IAW SRM 53-50-00, FIG 22 VOL 1. MAJOR REPAIR.

Part: FITTING — CORRODED (BS 1727) · airframe 88,186 hrs · 24,645 cycles

CENTER CARGO DOOR SILL FITTING CORRODED AT NR 2 LATCH SPOOL ASSY AREA, BS 1727, L43R. REPAIRED IAW SRM 53-50-00 FIG 15A, VOL I. R & R NR 2 LATCH SPOOL IAW MM 52-32-00-5. OP'S CHECK GOOD IAW MM 52-32-00-5. MAJOR REPAIR.

Part: FITTING — CORRODED (BS 1718) · airframe 88,186 hrs · 24,645 cycles

CENTER CARGO DOOR SILL FITTING CORRODED AT NR 1 LATCH SPOOL ASSY AREA, BS 1718, L43R. REPAIRED IAW SRM 53-50-00, FIG 15A, VOL I. REMOVED AND REINSTALLED NR 1 LATCH SPOOL ASSY IAW MM 52-32-00-5. OPS CHECKED GOOD IAW MM 52-32-00-5. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1721) · airframe 88,186 hrs · 24,645 cycles

SHEAR TIE AT FRAME BS 1721, L43 - 45R CORRODED. REMOVED AND INSTALLED SHEAR TIE IAW SRM 51-31-01 VOL 2. MAJOR REPAIR.

Part: FITTING — CORRODED (BS 1765) · airframe 88,186 hrs · 24,645 cycles

CENTER CARGO DOOR SILL FITTING CORRODED AT NR 4 LATCH SPOOL ASSY AREA BS 1765, L43R. REPAIRED IAW SRM 53-50-00 FIG 15A, VOL I. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1725) · airframe 88,186 hrs · 24,645 cycles

SHEAR TIE AT FRAME BS 1725 L43 - 45R CORRODED. REMOVED AND INSTALLED SHEAR TIE IAW SRM 51-31-01 VOL 2.

Part: FITTING — CORRODED (BS 1746) · airframe 88,186 hrs · 24,645 cycles

CENTER CARGO DOOR SILL FITTING CORRODED AT NR 3 LATCH SPOOL ASSY AREA BS 1746, L43R. REPAIRED IAW SRM 53-50-00, FIG 15, VOL I. FOUND WITHIN LIMITS. REMOVED AND REINSTALLED NR 3 LATCH SPOOL IAW MM 52-32-00-5. OP'S CHECKED GOOD IAW MM 52-32-00-5. MAJOR REPAIR.

Part: RHEOSTAT — INOPERATIVE (PANEL LIGHTS) · airframe 85,565 hrs · 23,630 cycles

BURNING ODOR ORIGINATING FROM THE VICINITY OF THE FIRE HANDLE. UPON ENTERING COCKPIT, FOUND OVERHEAD PANEL LIGHTS CIRCUIT BREAKER POPPED. RESET AND HAD ODOR OF SOLDER EMINATING FROM OVERHEAD PANEL. TRIED ADJUSTING OVERHEAD PANEL LIGHTS FOUND RHEOSTAT NOT FUNCTIONING WITH LIGHTS ON STUCK FULL BRIGHT. RHEOSTAT HAD NO EFFECT. NEEDS RHEOSTAT REPLACEMENT.

Part: LEAD — FAILED (THERMOCOUPLE) · airframe 85,448 hrs · 23,587 cycles

NR 3 ENGINE EGT EXCEEDED, 35 MINS AFTER T/O AT FL 320, ATS SELECTED, CLIMB PWR, TO CLIMB TO FL 340. LVL 1 ALERT ENG 3 EXCEDENCE EGT 1056 AMBER, EGT CLIMB POWER NORMAL AT 840C EGT FLUCTUATED. N1 N2 FF STEADY. NR 3 ENG IDLE, EGT STARTED FLUCTUATING & CLIMBED TO 1076 RED LEVEL 3 EGT HIGH ALERT. THEN EGT AMBER X, THEN BACK TO 300C. PRECAUTIONARY ENG 3 SHUTDOWN IN FLT. WINDMILL N1 & N2. OIL PRESS GOOD, WINDMILL ABOUT 35 MINS. R & R THERMOCOUPLE LEAD IAW MM77-21-05-01, RAN NR 3 ENG IAW JRH CHP 5, OPS CK NORMAL. ERASED ENG EXEEDENCE IAW FIM 45-31. R & R THERMOCOUPLE PN 8TK34AC2 IAW MM 77-21-05-01, RAN NR 3 ENG IAW CHP 5. OPS CK NORMAL. ERACED ENG EXCEDENCE IAW FIM 45-31. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R THERMOCOUPLE LEAD PN 8TK34ACA2 IAW MM 77-21-05-01, RAN NR 3 ENG IAW JRH CHP 5, OPS CK NORMAL. ERASED ENG EXEEDENCE IAW FIM 45-31.

Part: SWITCH — LOOSE (LANDING LIGHT) · airframe 84,728 hrs · 23,314 cycles

DURING TAXI OUT, TURNED OFF NOSE LIGHT AND FLASH OF LIGHT AND LOUD POP WAS HEARD COMING FROM NOSE LIGHT SWITCH. OBSERVED RT NOSE LIGHT CB POPPED. RETURNED TO GATE. FOUND NOSE LIGHT SWITCH LOOSE. TIGHTEN NOSE GEAR TAXI LIGHT SW AND OPS NORMAL REF SWP, CHAP 20. OK FOR SERVICE. FINAL CLOSED.

Part: SKIN — CRACKED (RT WING) · airframe 84,482 hrs · 23,206 cycles

RT WING-CRACK FOUND AT THE TRAILING END OF LOWER WING SKIN,APPROX.WING STATION XORS 419. CRACKED SILL IS ACCEPTABLE FOR STRENGTH AND WILL REMAIN IN SERVICE REF.E.A.8-5710-142474.

Part: SENSOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 81,926 hrs · 22,360 cycles

DURING T-OFF, WHILE SETTING POWER TARGET 114.4 WHEN N1 REACHED APPROX 98-99 PERCENT (70KTS) N2 EXCEEDENCE ON NR 01 ENGINE, RESET T-OFF AT 70KTS AMBER ENG 1 EXCEDENCE DISPLAYING, AMBER 109,9 N2 DISPLAYED VCP R NO RESTRICTION REF: 72-00-00-6 1, NR 1 ENGINE, N2 EXCEEDENCE 109.9 REQUIRES BOROSCOPE WITHIN 10 FLIGHT CYCLES REF AMM 72-00-00-6 IAW AMM 72-00-00-6-1 INSPECTED NR 01 ENG INTAKE/EXHAUST. NO DAMAGED FOUND A/C OK FOR 10 CYCLES. VCP R OIL REFERENCE: 72-00-00-6 1 TERMINATING ACTION REQUIRED AT OR BEFORE: SPEC: 10 CYCLES, EXPIRATION: 22,370 CYCLES. C/W BORESCOPE INSP IAW MM 72-00-00-6 FOUND ONE BLADE NICKED AND TORN THAT NEEDS BLENDED ON THE NR 1 STAGE OF THE HPC. BLADE IS MARKED WITH A (NR 27) ON IT FOR REF. NO OTHER DAMAGED NOTED MM 72-36-00-2. REMOVED AND REPLACED CIT SENSOR IAW AMM 73-20-02-2 AND CORE SPEED SENSOR IAW AMM 77-12-01-2, CKD OK.

Part: GENERATOR — MALFUNCTIONED (NR 2) · airframe 81,382 hrs · 22,168 cycles

REJECTED TAKE-OFF X 2 FOR LEVEL 2 "GEN DRIVE 2 FAULT ". FIRST TIME CAME ON FOR 2 SECONDS. SECOND ATTEMPT CAME ON STEADY WITH POWER AT T/O THRUST. GEN DRIVE 2 FAULT CLEARED WITH POWER REDUCED. OPENED RT SIDE NR 2 ENGINE FAN COWL TO INSPECT NR 2 ENGINE GENERATOR, FOUND GENERATOR OIL LOW, SERVICED GENERATOR, ALSO INSPECTED GENERATOR, DPI INDICATOR IS OK, NO MAJOR LEAKS FOUND ON GENERATOR WHEN COWL FIRST OPENED. CLOSED NR 2 ENGINE FAN COWLS PER MM 71-14-00, MANUAL 24-10, AND 12-12-05 IN MM, NOW DOWN TO OPS CHECK OF CSD. PERFORMED HIGH POWER RUN GEN. CHECKED GOOD.FREQS AND VOLTS NORMAL CSD OIL TEMP AND RISE TEMP GOOD AND PRESSURE NORMAL.

Part: ACTUATOR — LEAKING (MLG) · airframe 80,490 hrs · 21,907 cycles

LEFT BOGEY ACTUATOR LEAKING.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

UPPER CARGO DOOR FOUND CORROSION ON UPPER EXT FACE OF LWR JAMB. REPAIRED AREA IAW EA NR 8-5310-125423.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 80,224 hrs · 21,813 cycles

RT WING LEADING EDGE FOUND INTERCOSTAL CRACK.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 80,224 hrs · 21,813 cycles

RT WING LEADING EDGE FOUND INTERCOSTAL CRACK. REPAIR AREA IAW SRM 57-00-01 FIG 10 SHEET 1 VOL 1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 80,224 hrs · 21,813 cycles

RT WING INBD FLAP FOUND DEEP DENT ON UPPER SKIN 0.50 INCH BY 0.50 INCH DEEP .062 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1 VOL I.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND SEVERE CORROSION ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: WEB — CRACKED (ZONE 400) · airframe 80,224 hrs · 21,813 cycles

ENGINE PYLON NR 1 FOUND 3 CRACKS ON UPPER FWD SECTION STRUCTURE, RT SIDE, FIRST CRACK 2 INCHES LONG ON INT ANGLE AT STA YN 213, SECOND CRACK 2 INCHES LONG ON WEB AT STA YN 213 RT, THIRD CRACK 2 INCHES LONG ON WEB AT STA YN 213 LT.

Part: WEB — CRACKED (ZONE 400) · airframe 80,224 hrs · 21,813 cycles

ENGINE PYLON NR 1 FOUND 3 CRACKS ON UPPER FWD SECTION STRUCTURE, RT SIDE, FIRST CRACK 2 INCHES LONG ON INT ANGLE AT STA YN 213, SECOND CRACK 2 INCHES LONG ON WEB AT STA YN 213 RT, THIRD CRACK 2 INCHES LONG ON WEB AT STA YN 213 LT. REPAIR AREA IAW SRM 54-20-00 FIG 5 AND FIG 17 SHEET 1 VOL.1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 80,224 hrs · 21,813 cycles

RT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .074 INCH (SUSPECT CRACK ). REPAIRED DENT IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.

Part: SKIN — DENTED (ZONE 600) · airframe 80,224 hrs · 21,813 cycles

RT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .066 INCH (SUSPECT CRACK ). REPAIRED DENT IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

MAIN DECK, FROM STA 808 TO STA 879 AT X=-75, CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIR PER SRM 53-70-00 VOL 1 FIG 1 SHEET 1.

Part: SKIN — WORN (ZONE 600) · airframe 80,224 hrs · 21,813 cycles

RT WING L/E, FOUND DEEP WEAR ON SKIN AND PANEL LOWER SIDE L/E AT STA XORS 264. REPAIR IAW SRM 57-10-00 VOL 1 FIG 15 .

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 80,224 hrs · 21,813 cycles

MAIN DECK, FROM STA 808 TO STA 879 AT X=-75, CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIR PER SRM 53-70-00 VOL.1 FIG.1 SHEET 1.

Part: SKIN — WORN (ZONE 600) · airframe 80,224 hrs · 21,813 cycles

RT WING L/E, FOUND DEEP WEAR ON SKIN AND PANEL LOWER SIDE L/E AT STA XORS 264. REPAIR AREA IAW SRM 57-00-01 VOL 1 SHT 3 FIG 1A.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 80,224 hrs · 21,813 cycles

RT STAB INBD ELEV, XE 136, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH AND 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 FIG 3 SHEET 2 VOL 1.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 80,224 hrs · 21,813 cycles

RT STAB INBD ELEV, XE 118, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.

Part: SKIN — DENTED (ZONE 300) · airframe 80,224 hrs · 21,813 cycles

RT STAB INBD ELEV, XE 136, DENTED ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 FIG 3 SHEET 2 VOL.1.

Part: SKIN — DENTED (ZONE 300) · airframe 80,224 hrs · 21,813 cycles

RT STAB INBD ELEV, XE 118, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.

Part: FRAME — CRACKED (BS 555) · airframe 80,224 hrs · 21,813 cycles

RT AIR COND COMPT FOUND CRACK ON CAP OF FRAME.

Part: FRAME — CRACKED (BS 555) · airframe 80,224 hrs · 21,813 cycles

RT AIR COND COMPT FOUND CRACK ON CAP OF FRAME, SEE NRC N00755 AND N00756. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.

Part: FRAME — WORN (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

LT AIR COND COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-00-00 FIG 4A VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

AVIONIC COMPT FOUND CRACK ON FRAME.

Part: FORMER — CRACKED (ZONE 500) · airframe 80,224 hrs · 21,813 cycles

LT WING L/E INT FOUND CRACK ON FORMER.

Part: FORMER — CRACKED (ZONE 500) · airframe 80,224 hrs · 21,813 cycles

LT WING L/E INT FOUND CRACK ON FORMER. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

RT AIR COND COMPT FOUND CRACK ON VERTICAL WEB.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 80,224 hrs · 21,813 cycles

AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: WEB — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

RT AIR COND COMPT FOUND CRACK ON VERTICAL WEB. REPAIRED AREA IAW SRM 53-40-00 FIG 34 VOL I.

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

AFT FUSELAGE WASTE TANK COMPT, FOUND EXFOLIATION CORROSION ON STRUT BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 7 VOL I.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON BEAM LOWER SIDE.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 80,224 hrs · 21,813 cycles

AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 80,224 hrs · 21,813 cycles

AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON BEAM LOWER SIDE. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.

Part: STRUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

AFT FUSE WASTE TANK COMPT, FOUND EXFOLIATION CORROSION ON STRUT BULKHEAD.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 80,224 hrs · 21,813 cycles

AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE.

Part: BEAM — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPT, CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 80,224 hrs · 21,813 cycles

LT WING OUTBD FLAP FOUND CRACKS ON LWR SKIN.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPT, CRACK ON BEAM.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL UPPER SIDE. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 7.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 80,224 hrs · 21,813 cycles

LT WING OTBD FLAP FOUND CRACKS ON LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 65 VOL I.

Part: SKIN — CRACKED (RT NR 2 SLAT) · airframe 80,224 hrs · 21,813 cycles

DURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN.

Part: SKIN — CRACKED (RT NR 2 SLAT) · airframe 80,224 hrs · 21,813 cycles

DURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 31 VOL I.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 80,224 hrs · 21,813 cycles

DURING INSPECTION OF COSTANT AND OUTER SECTION MACHINED SKIN PANELS ON HORIZONTAL STAB, FOUND NR 5 PANELS WITH CRACK, ARE WITHIN LIMITS IAW TABLE MM PANELS P/N: 7228-1, 7227-1, 7281-2, 7226-1 AND 7225-1SEE ATTACHED SHEET FOR DETAIL.

Part: NONE — NONE (NOT AN SDR) · airframe 80,224 hrs · 21,813 cycles

MAIN CABIN EXISTING ANGLE REPAIR ON TEE FLOOR SUPPORT.

Part: SKIN — WORN (NR 6 SLAT) · airframe 80,224 hrs · 21,813 cycles

RT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE.

Part: SKIN — WORN (RT NR 6 SLAT) · airframe 80,224 hrs · 21,813 cycles

RT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 30 SHT 1 VOL I.

Part: NONE — NONE (NOT AN SDR) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.

Part: NONE — NONE (NOT AN SDR) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION.

Part: SKIN — CRACKED (ZONE 600) · airframe 80,224 hrs · 21,813 cycles

RT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.

Part: NONE — NONE (NOT AN SDR) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.

Part: NONE — NONE (NOT AN SDR) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.

Part: NONE — NONE (NOT AN SDR) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.

Part: SKIN — CRACKED (RT WING) · airframe 80,224 hrs · 21,813 cycles

RT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE.

Part: SUPPORT BEAM — UNKNOWN (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION. REPLACED SUPPORT IAW DWG AFA0039.

Part: CHANNEL — CORRODED (BS 879) · corrosion level 2 · airframe 80,224 hrs · 21,813 cycles

FWD CARGO COMPT CHANNEL WITH SEVERE EXFOLIATION CORROSION. WORK COVERED BY NRC N00418.

Part: SKIN — DENTED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

DURING INSPECTION EXT FUSELAGE LWR SURFACE FOUND DEEP DENT AND NICK 3 INCH BY .75 INCH DEEP .047 INCH ON SKIN.

Part: SKIN — DENTED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

EXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074 INCH ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I.

Part: SKIN — DENTED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

EXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN.

Part: SKIN — DENTED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

EXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074" ON SKIN.

Part: SKIN — DENTED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

EXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 7 VOL I.

Part: SKIN — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

EXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER).

Part: SKIN — CRACKED (ZONE 100) · airframe 80,224 hrs · 21,813 cycles

EXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER). REPAIRED SKIN IAW SRM 53-20-00 VOL I FIG 2.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 78,762 hrs · 21,165 cycles

NR 3 MAIN CARGO DOOR JAMB SUPPORT FITTING P/N AFA7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED SUPPORT BRACE, STRAP, VERTICAL STRAP, 2 EACH INTERCOSTALS, CLIP, WEB AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPPORT BRACE, STRAP, VERTICAL STRAP, 2 EACH INTERCOSTALS, CLIP AND WEB IAW SRM 51-31-01. DOOR RIG ACCOMPLISHED ON ORIGINAL EO T 5230-110698.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 78,762 hrs · 21,165 cycles

NR 7 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING P/N AFA7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED BACKUP FITTING, SUPPORT BRACE, STRAP, VERTICAL STRAP, SEAT TRACK SPLICE, INTERCOSTAL IAW SRM 51-31-01. CUT WEB IAW SRM 53-50-00. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPPORT BRACE, STRAP, VERTICAL STRAP, SEAT TRACK SPLICE, AND INTERCOSTAL IAW SRM 51-31-01. MANUFACTURED REPAIR DOUBLER FOR WEB AND INSTALLED REPAIR IAW SRM 51-31-01 AND SRM 53-00-01.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 78,762 hrs · 21,165 cycles

NR 6 MAIN CARGO DOOR JAMB SUPPORT FITTING P/N AFA 7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAIN AFTER REAMING TO .520. REMOVED BACKUP FITTING, ANGLE, INTERCOSTAL AND WEB IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED ANGLE, INTERCOSTAL, AND WEB IAW SRM 51-31-01. DOOR RIGGED ON ORIGINAL EO T 8-5230-110698.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 78,762 hrs · 21,165 cycles

NR 5 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING P/N AFA 7132-1 REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED 2 EACH SUPPORT BRACES, STRAP, WEB, INTERCOSTAL, AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED 2 EACH SUPPORT BRACES, STRAP, WEB, AND INTERCOSTAL IAW SRM 51-31-0. DOOR RIG ON ORIGINAL EO T 8-5230-110698.

Part: FITTING — CRACKED (CARGO DOORWAY) · airframe 78,762 hrs · 21,165 cycles

NR 4 MAIN CARGO DOOR JAM SUPPORT FITTING P/N AFA 7132-1, REQUIRES REPLACEMENT DUE TO CRACKS REMAINING AFTER REAMING TO .520. REMOVED SUPPORT BRACE, STRAP, CLIP, INTERCOSTAL AND BACKUP FITTING IAW SRM 51-31-01. INSTALLED NEW BACKUP FITTING AND REINSTALLED SUPPORT BRACE, STRAP, CLIP, AND INTERCOSTAL IAW SRM 51-31-01. DOOR RIG ACCOMPLISHED ON ORIGINAL EO T 8-5230-110698.

Part: SUPPORT FITTING — CRACKED (T/E FLAP) · airframe 77,398 hrs · 20,583 cycles

LT O/B FLAP I/B HINGE FWD SUPPORT FITTING CRACKED AT FWD NOSE SECTION REMOVED FASTENERS FOR NDT ACCESS. PERFORMED HFEC INSPECTION ON FWD HINGE SUPPORT FITTING I/B AND O/B HALVES FROM FWD END TO PERIPHERY AND IMMEDIATE AREAS OF THE FIRST THREE FASTENERS (3EA). NO DISCONTINUITY FOUND. PERFORMED HFEC INSPECTION ON THE O/B HALVE OF THE HINGE FITTING FIRST HOLE FROM THE FWD END, CRACK FROM FWD END TO THE HOLE DOES NOT PROPAGATE BEYOND THE FIRST HOLD. NO DISCONTINUITY WAS FOUND BEYOND THE FIRST HOLE.

Part: TRANSMITTER — MALFUNCTIONED (FUEL PRESSURE) · airframe 77,336 hrs · 20,555 cycles

LEVELED AT FL290 ATC SLOWED US TO 250 KNOTS. S/O REPORTED NR 3 ENGINE FUEL PRESSURE GAUGE STARTED TO FLUCTUATE. NOTICED NR 3 N1 RPM DROPPING AND ASSOCIATED REDUCTION IN EGT AND N2. PERFORMED IN FLIGHT ENG SHUT DOWN. RETURNED AND LANDED MEM WITHOUT INCIDENT. REMOVED NR 3 ENGINE MEC AND FUEL PUMP ASSY IAW DC10-30 AMM 73-20-01-2, MATED MEC AND FUEL PUMP ON BENCH IAW DC10-30 AMM 73-20-01-2. REINSTALLED MEC AND FUEL PUMP IN REFERENCE TO DC-10-30 M/M 73-12-01-2 AND 73-20-01-2. PERFORMED IDLE LEAK CHECK, NO LEAKS NOTED AND IDLE SPEEDS WERE WITHIN LIMITS OF JRH. FUEL FLOW TRANSMITTER REPLACED PER DC 10 AMM 73-31-02-2 . PERFORMED MAX POWER ASSURANCE RUN ALL PARAMETERS WITHIN LIMITS.

Part: BULKHEAD — CRACKED (NR 3 PYLON) · airframe 76,929 hrs · 20,379 cycles

NR 3 PYLON AFT BULKHEAD IB HORIZONTAL FLANGE AT RADIUS IS CRACKED FROM FWD EDGE TO AFT RADIUS, APPROX 2 INCHES IN LENGTH H.F.E.C. INDICATION AND VARIFED WITH BOROSCOPE. (PICTURE TAKEN) ENGINEERING NOTIFIED. REPLACED BULKHEAD PER WO 00033604 AND EA 8-5410-90834.

Part: DRIVE ASSY — MALFUNCTIONED (LT WING SLAT) · airframe 75,959 hrs · 19,956 cycles

SEPERATING GREASE ON RETAINER RING ON LT WING OUTBOARD SLAT DRIVE MECHANISM CENTER-FWD BEARING . REMOVED AND REPLACED LT O/B SLAT DRIVE MECHANISM IAW DC10-30 MM 27-83-02-2 RIG CHECKED AND LEAK CHECKS GOOD IAW DC10-30 MM 27-83-02-2 .

Part: FRAME — DAMAGED (BS 959) · airframe 75,959 hrs · 19,956 cycles

FWD CARGO PIT AFT FRAME STA 959 IS DAMAGED FROM PREVIOUS REPAIR. REPAIRED FRAME IAW EA 8-5310-91333, FUSELAGE - FWD LOWER CARGO DOOR JAMB STA 959 CHORD AND SKIN - REPAIR AND DC10 SRM 51-39-01 PG 5 STEP 10 VOL II AND DC10 SRM 53-50-00 FIG 22 SHEET 9 VOL I.

Part: UNKNOWN — UNKNOWN · airframe 75,959 hrs · 19,956 cycles

REPAIR LOCATED AT STA. 859 , LONG. 41L-42R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA . VISUALLY INSPECTED REPAIR AT STA. 859 , LONG 41R-42R , FOUND TO BE WITHIN LIMITS IAW SRM 53-20-00 FIG. 13 SHEET 9 VOL I. WITH RESPECT TO SIZE, SHAPE, SPACING AND EDGE DISTANCE . THIS REPAIR WAS NOT REMOVED FOR THIS INSPECTION .

Part: SEALANT — MISSING (DOOR HINGE) · airframe 75,959 hrs · 19,956 cycles

SEALANT MISSING AND RUSTY UPPER FLANGE AT AFT END OF UPPER CARGO DOOR HINGE. REMOVED AND REPLACED HINGE SECTION IAW DC10-30 SRM 51-33-01 VOL II, AND FED EX AMM 20-50-02-2. REMOVED AND REINSTALLED DOOR LINER IAW DC10-30 AMM 20-50-02-2 FIG 203. TORQUE WRENCH T8481I.

Part: REPAIR — UNKNOWN (TE FLAP) · airframe 75,959 hrs · 19,956 cycles

REPAIR LOCATED AT STA LT INBD FLAP LOWER SURFACE XIFH 189-195 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION USING FAA APPROVED DATA. INSPECTED REPAIR FOUND TO BE OUT OF LIMITS WITH REGARDS TO FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER IAW DC10-30 SRM 51-35-02 VOL II AND SRM 57-00-01 FIG 4 VOL I. ALODINED AND PRIMED IAW DC10-30 SRM 51-21-01 VOL I, N/R N00955, WORK ORDER NR 00031289.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 75,959 hrs · 19,956 cycles

SEALANT MISSING AND RUSTY AT UPPER FLANGE FORWARD AND AFT END OF CENTER CARGO DOOR. REMOVED AND REPLACED HINGE SECTION IAW DC10-30 SRM 51-33-01 VOL II AND DC10-30 MM 20-50-02-2 FIG 203. TORQUE WRENCH T8481I, N/R N00712, WORK ORDER 00031289.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,959 hrs · 19,956 cycles

LOWER SKIN AT STA 1069 AT ADF ANTENNA CORRODED. REMOVED CORROSION IAW DC10-30 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .068, AFTER BLENDING .047 , .021 MATERIAL LOST OUT OF LIMITS IAW DC10-30 SRM 53-00-01 VOL II. FABED REPAIR DOUBLER IAW DC10-30 SRM 53-20-00 PG 85 VOL I . ALODINED AND PRIMED IAW DC10-30 RSM 51-21-01 VOL II. INSTALLED REPAIR IAW DC10-30 SRM 53-20-00 PG 87 VOL I. N/R # N00921 WORK ORDER NR 00031289.

Part: RAIL — CRACKED (BS 1682) · airframe 75,959 hrs · 19,956 cycles

LOWER CARGO DOOR CUTOUT RAIL STA 1682 L-43R HAS CRACK ON END IN RADIUS. REPAIRED RAIL WITH REPAIR ANGLE IAW DC10-30 SRM 53-00-01 FIG 9 VOL I SHEET 7. ALODINED AND PRIMED IAW DC10-30 SRM 51-21-01 PAR 31 VOL I.

Part: REPAIR — MISINSTALLED (AILERON) · airframe 75,959 hrs · 19,956 cycles

REPAIR LOCATED AT LEFT OUTBOARD AILERON OUTBOARD END T/E WEDGE REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED OLD REPAIR NOT WITHIN FAA APPROVED DATA. FABRICATED NEW WEDGE SECTION AND ZEE IAW DC10-30 SRM 57-26-00 FIG 10 VOL I. ALODINED AND PRIMED IAW DC10-30 SRM 51-21-01 VOL II. INSTALLED REPAIR IAW DC10-30 SRM 57-20-00 FIG 10 VOL I AND DC10-30, 51-35-02 VOL II.

Part: TRIPLER — CORRODED (FUSELAGE) · airframe 75,959 hrs · 19,956 cycles

REPAIR LOCATED AT STA 999-1026 LONG 51L-50R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION USING FAA APPROVED DATA. FOUND REPAIR TO BE MAJOR, REMOVED TRIPLER TO GAIN ACCESS AND FOUND CORROSION IAW DC10-30 SRM 51-33-01 VOL I AND SRM 51-35-01 VOL I. REMOVED CORROSION ON TRIPLER IAW DC10-30 SRM 51-21-01 VOL II. FOUND TO BE OUT OF LIMITS IAW DC10-30 SRM 53-00-01 FIG 1A VOL II. FABBED TRIPLER IAW DC10-30 SRM 53-20-01 FIG 7 VOL I. ALODINED AND PRIMED IAW DC10-30 SRM 51-21-01 VOL I. INSTALLED TRIPLER IAW DC10-30 SRM 51-35-01 VOL II AND SRM 51-33-01 VOL II .

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 75,959 hrs · 19,956 cycles

MAIN CABIN SEAT TRACK GOUGED BS 744 LBL 47.0. REMOVED FLOORBOARDS TO FOM IAW DC10-30 SRM 51-31-01 VOL II. FOUND SEAT TRACK TO BE OUT OF LIMITS AND FABBED IAW DC10 SRM 53-42-01 VOL II. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED SEAT TRACK, FLOORBOARDS, AND SEALED IAW DC10 SRM 51-31-01VOL II AND SRM 51-40-01AND DC10 SRM 53-21-01-2 PG 1.

Part: FRAME — CORRODED (ZONE 100) · airframe 75,959 hrs · 19,956 cycles

CORROSION AT STA BS 1997 FRAME, FORWARD SIDE/LOWER LEG/BOTTOM SIDE AT LONGERON L43-R AND EXTENDING 2 FASTENERS EITHER SIDE OF LONGERON. REMOVED FRAME AND SPLICES IAW DC 10 SRM 51-35-01 VOL II. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. FOUND OUT OF LIMITS IAW DC 10 SRM 53-00-01 VOL II FIG 1B. FORMED FRAME SECTION AND SPLICES IAW DAC DRAWING AJC1363 AND DC 10 SRM 53-30-00 VOL I FIG 5. ALODINED AND PRIMED IAW DC 10 SRM 51-21-01 VOL II. LOCATED, DRILLED, AND INSTALLED IAW DC 10 SRM 51-35-01 VOL II SIGNED BY TIMCO MECH 1985 AND QC352, THIS IS A MAYOR REPAIR.

Part: WEDGE — DAMAGED (ZONE 500) · airframe 75,959 hrs · 19,956 cycles

LEFT OUTBOARD FLAP WEDGE STA XOFH 681 TO STA 747 HAS SEVERAL SKIN REPAIRS WITH LEAKING FASTENERS, AND LARGE AREA OF LEAKING FASTENERS ON TOP SKIN. REMOVED DAMAGED SKIN IAW DC 10 SRM 51-31-01 VOL II. FABRICATED NEW SKIN ASSEMBLY IAW DAC DRAWING ARC1953. INSTALLED NEW SKIN IAW DAC DRAWING ARC1953 AND DC 10 SRM 51-31-01 VOL II. BONDED SKIN IAW FEDEX EA NR 8-5750-91326. TITLE, LEFT WING OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE UPPER SKIN DAMAGE REPAIR. THIS IS A MINOR REPAIR SIGNED BY TIMCO MECH 7749 AND QC280 REFERENCE FEDEX SNRM N00567.

Part: ENGINE — OVERTEMP (NR 3) · airframe 73,135 hrs · 18,938 cycles

NR 3 ENGINE OVERTEMP ON TAKEOFF AT 700 FT AGL. TEMP ROSE TO 984 DEG FOR 30 SECONDS. SHUT DOWN ENGINE. TRIED RETARDING THROTTLE TO COOL ENGINE BUT WHEN THROTTLE WAS INCREASED N1 AND N2 CONTINUED TO DETERIORATE. NR 3 ENG IS APPROVED FOR REMOVAL. DURING INSPECTION OF EXHAUST FOUND METAL IN TAILPIPE.

Part: GENERATOR — CONTAMINATED (NR 2 & NR 3) · airframe 72,423 hrs · 18,682 cycles

AT ROTATION (MAIN WHEEL LIFTOFF), CAPTAIN LOST ALL INSTRUMENTS. THE FOLLOWING LIGHTS ILLUMINATED ON S/O PANEL: GEN 1 OFF, L EMER AC BUS OFF, AC BUS 1 OFF, AC BUS TIE 1 ISOL, L EMER DC BUS OFF, DC BUS 1 OFF. SEVERAL WARNING HORNS GOING OFF THAT COULD NOT BE SILENCED. ON T/O ROLL, ALL ENGINES WERE PRODUCING THRUST, BUT IT TOOK ENGINE NR 1 N2 GAUGE UNTIL 100 KNOTS TO SHOW A PROPER INDICATION, IT WAS CYCLING PRYOR TO THAT. WHILE FLYING BACK TO KIND, GEN NR 1 KEPT COMING ON LINE DROPING OFF. EVENTUALLY IT FIXED ITSELF JUST PRIOR TO LANDING, EVEN PARALLELED THE GENS. HEAVY RAIN CAME THROUGH WHILE A/C SAT ON RAMP. DRIED VISIBLE WATER, FACT 1, NR 2, NR 3 ENG AC GENERATOR ADJ/TEST GOOD PER MM.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 69,291 hrs · 17,687 cycles

RIGHT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108 RT WING SKIN PANEL AT STA XIS 168.66 TO XORS 130.40, STRINGER 1R AND 22R, AREAS 1 THRU 33 PER SRM CHAPT 51 AND SRM 57-10-00 IN COMPLIANCE WITH EA 8-5710-67582. REF SNRM N111, N177, AND N776.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,291 hrs · 17,687 cycles

LEFT WING UPPER SKINS HAVE PATCHES OF LOCAL INTERGRANULAR CORROSION FROM THE WING LEADING EDGE, AFT TO THE AFT SPAR AREAS. *S/D* REMOVED CORROSION IN SUBJECT AREA OF ARB3121 AND ARB3108, LT WING PANEL, AT STATION XIS 168.66 TO XORS 130.40, STRINGER 7L AND 19L, AREAS A-THRU -I IN ACCORDANCE WITH SRM CHAPT 51 AND SRM 57-10-00 IN COMPLIANCE WITH EA 8-5710-67584. REF SNRM N238, N332, AND 775.

Part: COMPRESSOR — DAMAGED (NR 3 ENGINE) · airframe 68,795 hrs · 17,504 cycles

ON TAKEOFF AND JUST 5 AFTER ROTATION HEARD LOUD NOISE AND ENGINE NR 3 ROLLED BACK TO APPROXIMATELY 35 PERCENT N1. ENGINE OVER TEMP LIGHT CAME ON MOMENTARILY. ENGINE CONTINUED TO WINDMILL. DUE TO NOISE AND VIBRATION PULLED ENGINE FIRE HANDLE AND BLEW NR 1 BOTTLE. FOUND SOME SMALL METAL PIECES IN THE TAILPIPE JUST AFT OF BLADES IN THE SHROUD AREA. EGT INDICATOR RECORDED MAX EGT AT 999 FOR 1 SECOND. REMOVED BORESCOPE PLUGS B1-3, B1-11, B3-1 AND B3-2. ENGINE HAS MASSIVE BLADE DAMAGE, WELL BEYOND MM LIMITS FROM ABOUT 12TH STAGE ON BACK, ENGINE REQUIRES REMOVAL.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 68,722 hrs · 17,475 cycles

LOST ALL FLUID ON HYDRAULIC NR 2 SYS, RUDDER STANDBY POWER OFF LIGHT ILLUMINATED. DUMPED FUEL AND LANDED AT AIRPORT. PERFORMED HYDRAULIC SYSTEM NR 2 LEAKAGE FAULT ISOLATION AND TRACED PROBLEM AT NON-REV SHUTOFF VALVE. REMOVED AND REPLACED DEFECTIVE O-RING, FILL UP HYDRAULIC SYSTEM TO PROPER LEVEL AND RETURN TO NORMAL. NR 2 SYSTEM EDP HYDRAULIC DID NOT WORK LONGER W/O FLUID, REMOVED AND REPLACED SYSTEM NR 2 HYDRAULIC MANIFOLD FILTERS IAW MM. VISUALLY CHECKED EDP CDASE FILTER, FOUND OK TO SERVICE. PERFORMED DEEP LEAK CHECKS. RUN HYDRAULIC ELECT PUMP AND MOTORIZED NR 2 ENG MOVE FLT SURFACES AND NO LEAKS NOTED. ACFT OK TO SERVICE.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 68,691 hrs · 17,468 cycles

LOST HYDRAULIC NR 2 FLUID, RUDDER STANDBY POWER OFF, LIGHT ILLUMINATED, LANDED WITHOUT INCIDENT. PERFORMED HYDRAULIC SYSTEM NR 2 FAULT ISOLATION AND TRACED PROBLEM TO NONREVERSIBLE S/O VALVE. REPLACED DEFECTIVE O-RING, SERVICED HYDRAULICS TO PROPER LEVEL. CREW NR 2 SYSTEM EDP DID NOT WORK LONG WITHOUT FLUID, AS PRECAUTIONARY ACTION REMOVED AND REPLACED NR 2 HYD MANIFOLD FILTERS IAW MM. CHECKED EDP CASE DRAIN FILTERS ALL OK. PERFORMED LEAK CHECK, MOTORIZED NR 2 ENG CHECKED FLT SURFACES AND NO LEAKS NOTED. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

AFT T/O RED NOSE GEAR IND LIGHT STAY ILLUM.

Part: A/C PACK — SMOKE (NR 2)

00-338 NR 2 AC PACK INTRODUCED SMOKE INTO COCKPIT WHEN UTILIZED IN FLT. AS PER PREVIOUS WRITE UP COMPLIED WITH RED TAB PROC FOR AIR COND SMOKE. RELEASE FOR SERVICE PER MEL/CDL:12-1. CK AND CLEANED COALESCER RAN NR 2 PACK FOR 1 HOUR. NO SMOKE OR ODOR NOTICED.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 63,450 hrs · 15,749 cycles

CORROSION FOUND ON LONGERON 31R BETWEEN FS 1421 & FS 1441. *S/D* REMOVED AND REPLACED PER SRM 53-10-00 FIG 2 VOL 1.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 63,450 hrs · 15,749 cycles

CORROSION FOUND ON LONGERON 30R BETWEEN FS 1421 & 1441. *S/D* REMOVED AND REPLACED PER SRM 53-10-00 FIG 2, VOL 1.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 63,450 hrs · 15,749 cycles

CORROSION FOUND ON LONGERON 32R, FS 1481. *S/D* REMOVED AND REPLACED PER SRM 53-10-00 FIG A, VOL 1.

Part: SKIN — CRACKED (COWL) · airframe 63,450 hrs · 15,749 cycles

NR 1 ENGINE LT CORE COWL FWD SKIN FOUND CRACKED. *S/D* REMOVED AND REPLACED PER EA 1-7110-52071.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 63,450 hrs · 15,749 cycles

LT WING TRAILING EDGE O/B FLAP UPPER SKIN FOUND WITH CRACK LOCATED AT APPROX 16 INCHES FROM O/B EDGE. *S/D* REMOVED AND REPLACED PER SRM 57-10-00 VOL.

Part: SKIN — CRACKED (RT WING) · airframe 63,450 hrs · 15,749 cycles

RT WING LEAD EDGE LWR SKIN CRACK AT CUTOUT OF SLAT TRACK NR 14. *S/D* REMOVED AND REPLACED PER SRM 57-10-00 FIG 68 VOL 1.

Part: RELAY — STUCK (MLG)

00-47 - AUTO THROTTLES RETARDED TO HOLD SPD. ALL FOUR RED WARNING GEAR LIGHTS ILLUMINATED WHEN CLIMB BEGAN, WITH THROTTLE RED WARNING LIGHT FOR GEAR WOULD NOT GO OUT. REMOVED AND REPLACED RELAY AND OPS CK LANDING GEAR HANDLE TEST, OPS CK OK.

Part: WARNING LIGHT — ILLUMINATED (A/C DOOR)

AIR COND DOORS LT ILLUM AT ALT 310 APPROX 10 MIN THEN WENT OUT. COMPLIED WITH RED TABS. DEFERED PER MEL 52-4D, COMPLIED WITH MX PROC 52-4C. VERIFIED A/C DOORS ARE LATCHED AND CLOSED. REMOVED AND REPLACED A/C DOOR WARNING RELAY R2-5431 PER SMP. REMOVED AND REPLACED NR 1 A/C COMPARTMENT DOOR WARNING SWITCH PER MM 52-70-07-2, OPS CK NORM.

Part: TUBE — FAILED (ANTI-ICE SYSTEM)

00-22 AT CR FL 310 SEL, WING ANTI-ICE ON, HAD NR 1 MANIFOLD FAILURE LIGHT ILLUM. PNEU SUPPLY OFF FOR NR 1 ON FOR 2/3, ISOL VLV 1-2 OPEN AT TIME OF FAILURE. REMOVED AND REPLACED NR 4 L/E SLAT PER DC10-30 MM 27-80-01-4-2, LEAK AND OPS CK GOOD. INSTALL NR 4 SLAT PER EA 8-3011-49033.

Part: SWITCH — FAILED (NR 1 MANIFOLD)

AT LEVEL 290 GOT A NR 1 MANIFOLD FAIL LIGHT. REPLACED MANIFOLD FAILURE DETECTION PRESSURE SWITCH AS PER AMM 36-23-03-4. PERFORMED OPS CHECK PER MM 30-11-00-2, MM 36-23-03. OPS CHECK GOOD.

Part: O RING — FAILED (NR 2 ENGINE)

99-183 - LOST ALL OIL QTY FOR NR 2 ENG WITH ACCOMP. REPLACED O-RING. REINSTALLED CHIP DETECTOR SERVICED ENG, OIL TO FULL RAN ENG PER JRH CHP 5A. NO LEAKS NOTED. OK FOR SERVICE MM 71-00-00.

Part: TARGET — FAILED (NLG)

NOSE GEAR INDICATED UNSAFE UPON GEAR RETRACTION AFTER ALT GEAR EXTENSION CHECK. AFTER CYCLING NOSE GEAR INDICATED UNSAFE BOTH UP AND DOWN AML NR 865177. *S/D* REMOVED AND REPLACED INSULATION BLANKET, WIRING BUNDLE AND NOSE LAND GEAR LOCK SENSOR TARGET.

Part: SEAT TRACK — CORRODED (BS 765)

SURFACE CORROSION ON FLOOR TRACK ALONG BS 765, 27 INCH RBL. *S/D* FLOOR TRACK SURFACE CORROSION FOUND EXCEED LIMITS. CARRIED OUT REPAIR BY INSTALLING FABRICATED FLOOR TRACK AND HAT SECTION SPLICE AS PER SRM 53-70-00 FIG 1 VOL 1 REV 76.

Part: TRACK — CORRODED (BS 1871)

SNRM 0030 - CORRODED TIE DOWN (TWO EACH) ON FLOOR TRACK LOCATED APPROX ALONG BS 1871, 8 INCH LBL.

Part: FRAME — CRACKED (CARGO DOORWAY)

CENTER CARGO COMPARTMENT, DOOR CUTOUT AFT EDGE LOWER CORNER FOUND WITH CUT/CRACK (ADJACENT TO COMPARTMENT FLOOR LEVEL). OPENED UP AREA, FOUND ADDITIONAL DAMAGE. REQUEST ENGINEERING EVALUATION. *S/D* CARRIED OUT REPAIR AS PER EA 8-5310-40362 AND SRM 53-50-00 FIG 9 VOL 1.

Part: BRACKET — BROKEN (RT MLG)

UPON GEAR RETRACTION, RIGHT HAND MAIN INDICATED UNSAFE. RECYCLED GEAR, INDICATIONS REMAINED SAME. FOUND UPLOCK TARGET SENSOR BRACKET BROKEN. PLACED ON OPEN ITEM LIST FOR INSTALLATION AT COMPLETION OF FERRY FLIGHT TO JFK. GEAR TO BE SWUNG BEFORE INSTALLATION TO BE SURE THAT NOTHING IS OUT OF RIG WHICH MAY HAVE CAUSED THIS TO BREAK. REMAINDER OF BRACKET ALONG WITH CONDUIT IS SECURED ADJACENT LINKAGE PER FERRY PERMIT 97-01 (2300Z). REPLACED LATCH CYLINDER LEVER AND TARGET SENSOR. ADJUSTED PER M.M. 32-34-03. AFTER RETRACTION TEST ALL COCKPIT INDICATIONS FOR LANDING GEAR NORMAL. NO UNSAFE CONDITION EXIST PER M.M. 32-30-00.

Part: RIB — CRACKED (NR 1 LE SLAT)

NR5032, LT WING NR 1 SLAT O/B RIB FRAME HAS A2 INCH CRACK INDICATION AS VIEWED THROUGH LWR BORESCOPE ACCESS HOLE. * REMOVED AND REPLACED RIB PER SRM 53-00-01.

Part: SKIN — CORROSION (WS 118)

SNRM 6022, RT WING AT STA XCW118 TOP SURFACE OF WING HAS HEAVY CORROSION JUST FWD OF R3 DOOR. *S/D* BURNISHED CORROSION CK BY NDT AND FOUND TO BE WITHIN LIMITS PER SRM 57-10-00 FIG 61. TREATED, PRIMED.