N980DL

Part: O-RING — LEAKING (APU OIL BOWL) · airframe 72,428 hrs · 53,404 cycles

FUMES SMELLED BY FA AND PAX IN AFT CABIN AFTER T/O DURING INITIAL CLIMB.AFT CA-SIDE LAV SMOKE DETECTOR ACTIVATED.NO SMOKE NO FLAME NO HEAT OBSERVED.QRH COMPLETED .TAKEOFF FLAP 2 ,D43,NO UNUSUAL ENGINE INDICATIONS NOTED. C/W NO GO ODI 2172 STEPS 1 AND 2[904531] C/W AMDS 2120-2367 PNEUMATIC T/S FOUND APU OIL FILTER BOWL SMALL LEAK.REPLD, O-RING CKS GOOD. C/W AMDS 2120-2368 C/W 2900-2002,2003 H/C INSP,C/W 4900-1184 APU INLET CLEANING.AMDS CARD 7100-2619.FULL BURN.A/C READY FOR SERVICE. (LP5001816)

Part: BATTERY — FAILED (SMOKE DETECTOR) · airframe 72,376 hrs · 53,362 cycles

2L LAV SMOKE DETECTOR SOUNDED INTERMITTENTLY IN FLIGHT. NO SMOKE OR FIRE. REPLACED BATTERY IN 2L SMOKE DETECTOR, OPS NORM. 2R LAV SMOKE DETECTOR BASE BROKEN. REPLACED SMOKE DETECTOR. OPS NORM. (LP4753570)

Part: SWITCH — DEFECTIVE (TAILCONE) · airframe 71,853 hrs · 52,908 cycles

TAIL CONE UNSAFE DURING CLIMBOUT. QRH COMPLETED. REPLACED INTERNAL RELEASE HANDLE STOWAGE DUE TO POOR CONDITION REMOVED AND REPLACED AFT INDICATION SWITCH PER AMM 53 -50 INSTALLED TAIL CONE PER AMM 53-53. C/W RII INSTALLED OPS CK SWITCH AND INSTALL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,728 hrs · 52,795 cycles

CEILING EMERGENCY LIGHTS FROM ROW 22-25 WERE INOPERATIVE. R & R THE BATTERIES IAW AMM 33-53. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,728 hrs · 52,795 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 1 - 4 INOPERATIVE. REPLACED THE BATTERY PACK B5-100. OPS CHECKED GOOD. OK FOR SERVICE IAW AMM 33-53.

Part: PIN — DISLODGED (EVAC SLIDE) · airframe 71,376 hrs · 52,499 cycles

L1 DOOR SLIDE TOP PARACHUTE PIN DISLODGED. INSPECTED L1 DOOR SLIDE ALL LACING OK, BOTTLE PRESSURE OK, SLIDE STILL PACKED. REENGAGED TOP PARACHUTE PIN REF AMM 25-62 OK FOR SVC SLIDE PIN NEVER INSTALLED.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 71,213 hrs · 52,364 cycles

CAPT'S SIDE AFT LAV ALARM SOUNDING W/NO SMOKE INDICATIONS. COULD NOT DUPLICATE. A/C OK FOR SVC.

Part: SMOKE DETECTOR — BROKEN (LAVATORY) · airframe 71,193 hrs · 52,352 cycles

LAVATORY SMOKE DETECTOR WILL NOT TURN OFF, LOCATIONS:203. R&R SMOKE DETECTOR DUE TO BROKEN BASE. REF AMM 26-17. OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,891 hrs · 52,110 cycles

FOUND CEILING EMERGENCY LIGHTS OUT AT ROWS 16-24. REPLACED BATTERY PACKS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 70,852 hrs · 52,079 cycles

EMERGENCY LIGHTS AT SEAT 25B WAS FOUND INOPERATIVE. REINSTALLED PULLED PIN, OPS CHECK OK IAW AMM 33-50.

Part: UNKNOWN — ODOR (CABIN) · airframe 70,794 hrs · 52,037 cycles

FLIGHT ATTENDANTS REPORTED THE AFT LEFT LAVATORY SMOKE DETECTOR SOUNDED. FAINT BURNING ODOR IN CABIN AND COCKPIT. ENGINE ANTI-ICE WAS SELECTED ON. SHUT OFF GALLEY POWER AND UPPER SIDEWALL LIGHTS IAW QRH. PLACED PACKS TO FULL COLD. SMOKE ALARM STOPPED THEN CAME BACK FOR APPROXIMATELY 3 MINUTES. ODOR DISSIPATED. DIVERTED. FLIGHT ATTENDANT DESCRIBED SWEET POLLEN ODOR, NO SMOKE, THAT DISSIPATED. PERFORMED NOGO ODI. PERFORMED T/O ENGINE POWER RUN WITH NO SMOKE OR ODOR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,636 hrs · 51,908 cycles

B5-105 BATTERY PACK WON`T TURN ON AFT OVERWING EMERGENCY LIGHTS. REPLACED THE BATTERY PACK. CHECKED GOOD IAW WDM 33-51 AND SPWM 20.

Part: MECHANISM — CORRODED (EVAC SLIDE) · airframe 70,589 hrs · 51,870 cycles

DURING TAIL CONE ESCAPE SLIDE DEPLOYMENT TEST SLIDE HOLD DOWN STRAP CONNECTORS FAILED TO RELEASE WITH INSTALLATION CORRECT PER AMM. MECHANISM IS RUSTY. REPLACED STRAP AND INSTALLED IAW W/K 2562-7267 CKS OK.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 70,425 hrs · 51,741 cycles

AFT LEFT LAV SMOKE DETECTOR, INTERMITTENT FALSE AURAL ALARMS. R&R LAV DETECTOR BATT PER AMM 26-13. OK FOR SVC.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 70,395 hrs · 51,717 cycles

AFT LAV SMOKE DETECTOR INTERMITTENT ALARM ON CLIMBOUT. NO SMOKE-ODORS OR FUMES PRESENT. REMOVED SMOKE DETECTOR BATTERY IN LT AFT LAV AND REINSTALLED SMOKE DETECTOR. C /W M PROCEDURES - VERIFIED TRASH CONTAINER EMPTY AND LOCKED AND PLACARDED DOOR CLOSED. FWD TO MCO AND PLACARDED PER MEL 26-00-07. R&R AFT LT LAV SMOKE DET ASSY OPS CK OK REF AMM 26-10 MCO/PLCD RMVD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 70,349 hrs · 51,685 cycles

L1 & R1 DOORS AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. AFTER TROUBLESHOOTING, FOUND THE BATTERY PACK FAILED. REPLACED THE BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-50.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 70,147 hrs · 51,528 cycles

MOMENTARY ALARM AFT LEFT LAV NO SMOKE SMELLED QUIT AFTER A BIT. R&R SMOKE DET AND BATTERY. OPS CKS GOOD.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 70,140 hrs · 51,523 cycles

ATB/IFSD - RETURNED TO ATL DUE TO RIGHT ENGINE COMPRESSOR STALLS WITH VIBRATIONS AT TOP OF CLIMB. PULLED THE ENGINE BACK TO IDLE. CREW FOLLOWED QRH AND SHUT DOWN ENGINE DUE TO VIBRATIONS. EMERGENCY DECLARED. MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. THE RIGHT ENGINE WAS REPLACED.

Part: ENGINE — FAILED (RIGHT) · airframe 70,126 hrs · 51,514 cycles

RETURNED TO DEPARTURE DUE TO RIGHT ENGINE COMPRESSOR STALLS WITH VIBRATIONS AT TOP OF CLIMB. PULLED THE ENGINE BACK TO IDLE. CREW FOLLOWED QRH AND SHUT DOWN ENGINE DUE TO VIBRATIONS. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. ENGINE CHANGE REQUIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,248 hrs · 50,021 cycles

CRACK ON FUSELAGE SKIN STA 1022 BETWEEN LONGERONS 13/14L. REPAIRED PER ETI-17-17-038 REV 1 AND ER/A 556345-14.

Part: STIFFENER — CRACKED (LT NACELLE) · airframe 68,248 hrs · 50,021 cycles

CRACK ON STIFFENER IN FWD LT NOSE COWL BULKHEAD NS 19.430 NEAR 6 O`CLOCK. THE STIFFENER WAS REPLACED IAW SRM 54-40-0, FIG 6, ITEM 12, SRM 51-30-8, AND ER/A 556386-14, REV ORIGINAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,248 hrs · 50,021 cycles

CRACKED FUSELAGE SKIN BTW LONG 27R TO 28R BTW STA Y= 83.55 TO 110. CRACKED FUSELAGE SKIN BTW LONG 27R TO 28R BTW STA Y=83.55 TO 110. (FUS) WAS REPAIRED PER SG09530030 REV-, AND SRM 53-05 PAR 162, FIG 158.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,248 hrs · 50,021 cycles

PAX CABIN, CRACKED DOOR JAMB OF AFT LT OVERWING EMERGENCY EXIT (UPPER SURFACE). DOOR JAMB WAS REPAIRED PER SRM 53-05 PAR 42 FIG 32.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 68,248 hrs · 50,021 cycles

WORN FWD & AFT LOWER EXTERNAL PRODUCTION DOUBLERS AT AFT CARGO DOOR. AFT DOUBLER WAS REPLACED IAW SRM 51-30-2. THE FWD DOUBLER WAS BLENDED OUT IAW SRM 52-01, FIG 1, SHEET 3.

Part: SPAR — DAMAGED (RT WING) · airframe 68,136 hrs · 49,942 cycles

RIGHT WING REAR SPAR WS 164 LEAKING. COMPLIED WITH PRI 548718-14AD, REV 0-6.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 67,697 hrs · 49,625 cycles

WHILE PERFORMING SERVICE CHECK, FOUND SEAT 25ED FORWARD EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE SOCKET IN CONNECTOR. CHANGED CONNECTOR, OPS CHECKED GOOD.

Part: BRACKET — CRACKED (TAILCONE) · airframe 67,667 hrs · 49,604 cycles

TAILCONE UPPER RT LATCH BRACKET LOWER L BRACKET IS CRACKED. REMOVED, FABRICATED, DRILLED, TREATED, PRIMED, AND INSTALLED A NEW BRACKET IAW SRM 51-10-02.

Part: FRAME — CRACKED (BS 1437) · airframe 67,666 hrs · 49,602 cycles

FRAME BS 1437 CRACKED ON LT SIDE IN AREA OF ACM FAN BRACKET. INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 51-70-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,666 hrs · 49,602 cycles

CRACKED 1510 FRAME RT UPPER ALIGNMENT PIN. REPAIRED PER ERA 497316-14MA REV ORIGINAL.

Part: FRAME — WORN (FUSELAGE) · airframe 67,666 hrs · 49,602 cycles

WEB ON 1388 CANT FRAME WORN FROM LOOSE DUCT. INSTALLED REPAIR IAW SRM 51-70-4 FIG 2.

Part: FRAME — CRACKED (BS 1380) · airframe 67,666 hrs · 49,602 cycles

DURING ODI INSPECTION FOR SMOKE. FOUND DAMAGE TO WEBBING ON FRAME BS 1380 AND CRACKS IN SUPPORT BRACKET PIN. INSTALLED A TIME LIMITED REPAIR IAW ERA 553587-14 REV ORG.

Part: UNKNOWN — ODOR (CABIN) · airframe 67,666 hrs · 49,602 cycles

SMOKE AND FUMES IN CABIN PRIOR TO BOARDING FOR FIRST FLIGHT. THE CABIN SUPPLY TEMP WAS FULL HOT. THE CREW INFORMED MAINTENANCE THAT BOTH PACK TEMP SELECTORS WERE SELECTED TO FULL HOT IN MANUAL MODE. THE NO GO ODI CHECKLIST AND THE SMOKE ODOR WORK CARD 2120-2367 WERE COMPLIED WITH. A PNEUMATIC SYSTEM DUCT BURNOUT WAS COMPLIED WITH. NO PROBLEMS WERE NOTE AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,795 hrs · 48,884 cycles

AISLE EMERGENCY LIGHTS INOPERATIVE FROM ROW 31 AFT. FOUND CONNECTIONS AT LIGHT ASSY L2-846 IN TAIL COMPARTMENT. RECONNECTED L2-846 LIGHT ASSY CORRECTLY AND REPLACED F1 FUSE AT B5-212 POWER SUPPLY. ALL LIGHTS OPS CK GOOD.

Part: SPAR CAP — CRACKED (RT WING) · airframe 66,683 hrs · 48,801 cycles

FOUND CRACK ON AFT SIDE OF RT WING SPAR LOWER CAP AT STA XRS=164.000. NR FOR ADDITIONAL INFORMATION 035-0001: 5710-01110-05/001, 00012. REPAIR PRI 548718-14, REV 2, ER/A 548718-14AD REV A, VA 83880AD AND AMDS 5710-01110-06. COMPLIED WITH ALL SFAR 88 AND CDCCL REQUIREMENTS RECEIVED FINAL ER/A.

Part: SPAR — DAMAGED (RT WING) · airframe 66,683 hrs · 48,801 cycles

FOLLOW UP TO NR 33, RT WING REAR SPAR WEB HAS A CIRCUMFERENTIAL DAMAGE AROUND FASTENER BORE LOCATED 4" INBD FROM INBD LOWER STUD, ON THE SECOND LOWER ROW OF PULLED FASTENERS. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY, NR FOR ADDITIONAL INFORMATION 035-0001:5710-01110-05/013 00035. REPAIR IAW PRI 548718-14, REV 2, ER/A 548718-14AD, REV A.

Part: SPAR — DAMAGED (RT WING) · airframe 66,683 hrs · 48,801 cycles

FOLLOW UP TO NR 33: RT WING REAR SPAR WEB HAS 2 CIRCULAR DAMAGE MARKS APPROXIMATELY 0.125" IN DIAMETER LOCATED 3" INBD FROM INBD LOWER STUD, ON THE SECOND LOWER ROW OF PULLED FASTENERS. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 035-0001:5710-01110-05/012 00034. REPAIRED IAW PRI 548718-14, REV NR 2, ER/A 548718-14AD, REV A.

Part: SPAR — CRACKED (WING) · airframe 66,683 hrs · 48,801 cycles

WING REAR SPAR CRACKED XRS 164.

Part: SPAR — CRACKED (WING) · airframe 66,674 hrs · 48,793 cycles

WING REAR SPAR CRACKING AT XRS 164.

Part: VANE — WORN (RT WING TE FLAP) · airframe 63,107 hrs · 46,353 cycles

WEAR ON INBD EDGE AT RT OTBD FIXED GUIDE VANE OF OTBD FLAP. REPAIR WAS PERFORMED IAW SRM 57-03D, PAR II.

Part: SUPPORT — CRACKED (RUDDER SENSOR) · airframe 63,107 hrs · 46,353 cycles

DURING MAINTENACE ACTIVITIES, RUDDER POSITION SENSOR SUPPORT WAS FOUND CRACKED. RUDDER POSITION SENSOR SUPPORT WAS REPLACED IAW AMM 20-30-01.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,107 hrs · 46,353 cycles

CRACKS ON INNER/OUTER PAN BETWEEN BEAM 1 AND 2 AT MID CARGO COMPARTMENT DOOR, AFT EDGE. THIS NRC WAS ACCOMPLISHED IAW ER/A 532538-14, REV ORIGINAL AND ETI-88-15-083, REV 3.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK SETTLEMENT AREA ALSO WEAR ON STICK FUEL ACCESS PLATE NR 1460C AT RT WING. FUEL ACCESS AND STICK WERE REPLACED IAW AMM 28-40-02 AND FUEL ACCESS WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0393. LP1851016

Part: CABLE — DAMAGED (TAILCONE) · airframe 63,107 hrs · 46,353 cycles

SRQ MAINTENANCE FOUND THE KEVLAR CABLE ON THE TAILCONE ASSY DAMAGED AND REPLACED IT. LP1853504.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK SETTLEMENT AREA ALSO WEAR ON STICK FUEL ACCESS PLATE NR 1466C AT RT WING. ACCESS PLATE NR 1466C WAS REPLACED. LP1851023

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK SETTLEMENT AREA ALSO WEAR ON STICK FUEL ACCESS PLATE NR 1472C AT RT WING. ACCESS PLATE NR 1472C WAS REPLACED. LP1851028.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 63,107 hrs · 46,353 cycles

NICKS ON PREVIOUS REPAIR DOUBLER OF INBD FIXED AT LT WING INBD FLAP. DOUBLER WAS REPLACED IAW SRM 57-03D, PAR II, FIG 11 AND ATTENDED WITH OPN 1031. LP1851626.

Part: BAR — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LOWER FLEX JOINT BAR AT LT WING FLAP. FLEX JOINT BAR WAS REMOVED IAW AMM 20-30-01 AND BLEND OUT IN HOLES AT FLEX JOIN BAR WAS PERFORMED IAW SRM 51-10-3 AND WAS FOUND OUT OF LIMITS IAW ER/A 532537-14, REV ORIGINAL. THEREFORE NEW FLEX JOINT BAR WAS INSTALLED IAW AMM 27-51-07.

Part: NONE — NONE (NONE) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

DURING H-CK2, ER/A 532540-14, SECTION I INSTALLED AN SRM 53-04, PAR 57 EXCEPT FOR A MINOR DEVIATION. THE PURPOSE OF THIS LOGPAGE IS TO MONITOR THE SECTION II REPETITIVE INSPECTION. THIS CARD WAS ATTENDED WITH ER/A 532540-14, REV ORIG AND SRM 53-04, FIG 57.

Part: HEATER BLANKET — CRACKED (LT WING TE) · airframe 63,107 hrs · 46,353 cycles

CRACKED LT HEATER BLANKET AFT T/E. CRACKED LT HEATER BLANKET AFT T/E WAS REPAIRED IAW ER/A 532501-14AD, REVISION ORIGINAL.

Part: BRACKET — CRACKED (NR2 SLAT TRACK) · airframe 63,107 hrs · 46,353 cycles

DURING MAINTENANCE ACTIVITIES WAS CRACKED THE SLAT BRACKET NEAR TO RT SLAT TRACK NR 2, STA XCW=104 AT RT WING. BRACKET NEAR TO RT SLAT TRACK NR 2 STA XCW=104 AT RT WAS REPLACED IAW AMM 20-30-01 AND 27-80-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK ALSO SETTLEMENT AREA FUEL ACCESS PLATE NR 1414C AT RT WING. FUEL ACCESS PLATE 1414C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: TAB — DAMAGED (RUDDER) · airframe 63,107 hrs · 46,353 cycles

EXPOSED COMPOSITE MATERIAL ON BOTH FACE OF RUDDER CONTROL TAB. BOTH FACES OF RUDDER CONTROL TAB WERE REPAIRED IAW SRM 51-70-1, AD PAR 23.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 63,107 hrs · 46,353 cycles

LIGHTNING STRIKE ON LT ELEVATOR GEARED TAB T/E. DOUBLER WAS FABRICATED AND TREATED, AREA WAS TREATED, DOUBLER WAS INSTALLED IAW SRM 55-04, PAR 3, 51-70-2D, PAR 10 AND 13. LP1850123

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 63,107 hrs · 46,353 cycles

DISBONDED REPAIR DOUBLER ON LT ELEVATOR GEARED TAB T/E. NEW DOUBLER WAS FABRICATED AND INSTALLED AT LT ELEVATOR GEARED TAB T/E IAW SRM 55-04, PAR 3 AND 51-70-2D PAR 18. LP1850106

Part: BEAM — CRACKED (FUSELAGE) · airframe 63,107 hrs · 46,353 cycles

CRACKED OUTER PANE PROJECTION BEAM 1 FWD SECTION ON FWD SERVICE DOOR. DOUBLER REPAIR WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 52-03D FIG 3, 51-30-2, 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT TIE TRACK FROM STA Y=1212 TO Y=1322 AT C3. DUE TO EXCESSIVE DAMAGE TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FRAME TEE STA Y=1380 BTW X=-17 TO X=17 AT A/A. FRAME TEE WAS REPLACED AND REPAIRED IAW ER/A 532534-14, REV. ORIG, AND DWG 9912246, REV CE AND SRM 51-10-3, PAR 14, 21 SRM 51-30-2, SRM 51-30-5.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT RT WING L/E FILLET PANEL ON STA Y=803, LONG 29-28, RT ORIGINAL'S 0.157" AND REMAINING'S 0.088". ON STA Y=800, LONG 29-28, RT IS 0.150" AND REMAINING'S IS 0.087". ON STA Y=797, LONG 29-28, RT ORIGINAL'S 0.144" AND REMAINING'S 0.107". ON STA Y=793, LONG 29-28, RT IS 0.138" AND REMAINING'S 0.106". ON STA Y=790, LONG 29-28 RT IS 0.130" AND REMAINING'S 0.088", AND STA Y=786, LONG 29-28, RT IS 0.122" AND REMAINING'S 0.089". THEREFORE THESE ARE OUT OF LIMITS. REWORKED AREAS WIHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21 AND 14 AND 53-04, PAR 57. AREAS OUT OF LIMITS WILL BE ATTENDED WITH NRC 239.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 63,107 hrs · 46,353 cycles

MAINTENANCE FOUND BROKEN WIRES ON TAILCONE EXTERNAL RELEASE HANDLE CABLE NR 583 AT AFT ACCESSORY COMPARTMENT MAINTENANCE REPLACED TAILCONE EXTERNAL RELEASE HANDLE CABLE NR 583 AT AFT ACCESSORY COMPARTMENT.

Part: CARGO TRACK — CORRODED (BS 1220-1322) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT TIE TRACK FROM STA Y=1220 TO Y=1322 AT C3. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-5 AND 51-10-3, PAR 14 AND 21.

Part: CARGO TRACK — CORRODED (BS 1220) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT TIE TRACK SPLICE STA Y=1220 AT AFT CARGO COMPARTMENT. SPLICES WERE REPLACED IAW SRM 53-24-0 , 51-30-1 AND 51-30-5 , 51-10-3, PAR 14 AND 21.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FLOOR PANELS 769A AND 769G. FLOOR PANELS 769A AND 769G WERE REPLACED IAW SRM 51-10-3, 51-10-4.

Part: BUSHING — CORRODED (MLG MOUNT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON SUPPORT FITTING BUSHING AT RT MLG. RT MLG SUPPORT FITTING BUSHING WAS REPLACED IAW CMM 20-10-7 AND DWG SR09570087, REV B.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 63,107 hrs · 46,353 cycles

CRACKED RIBS ON L/E INTERNAL STRUCTURE, STA 43.000, LT, 30.000 LT. 17.656 RT AND -1.562 RT. RIBS WERE REPLACED IAW SRM 51-30-2, SRM 51-30-5 AND SRM 51-10-3, PAR 14, 21.

Part: BUSHING — CORRODED (MLG MOUNT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON SUPPORT FITTING BUSHING AT LT MLG. LT MLG SUPPORT FITTING BUSHING WAS REPLACED IAW CMM 20-10-7 AND DWG SR09570087, REV B.

Part: FRAME — CRACKED (BS 1510) · airframe 63,107 hrs · 46,353 cycles

CRACKS ON FRAME STA Y=1510 CANT BETWEEN 3 AND 6 HRS POSITION AT A/A. FRAME WAS REPLACED IAW DWG 9911843 SRM 51-30-2, 51-10-4, 51-10-3.

Part: TAB — PUNCTURED (RT ELEVATOR) · airframe 63,107 hrs · 46,353 cycles

PUNCTURE ON RT ELEVATOR CONTROL TAB LOWER SKIN. NUMBER OF DAMAGES EXCEED 4 FOR REPAIR SO BE REPLACED IAW SRM 55-04 P.2.

Part: BRACKET — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED INTERNAL BRACKET ON NR 8 SLAT TRACK HOUSING AT LT WING FIXED L/E STA XRS 260 APPROXIMATELY SLAT TRACK NR 8 AT LT WING WAS REMOVED IAW AMM 27-80-07. INTERNAL BRACKET ON HOUSING OF SLAT TRACK NR 8 AT LW WAS REMOVED, IAW AMM 20-30-01. NEW BRACKET WAS TREATED AND PAINTED IAW SRM 51-10-30. BRACKET ON HOUSING OF SLAT TRACK NR 8 WAS INSTALLED IAW AMM 20-30-01 AND SLAT TRACK NR 8 WAS INSTALLED AND ADJUSTED IAW AMM 27-80-01.

Part: TRACK — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT TIE TRACK FROM STA Y=1003 TO Y=1220 AT C3. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: TRACK — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT TIE TRACK FROM STA Y=1003 TO Y=1155 AT C3. DUE TO EXCESSIVE DAMAGE TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — CONTAMINATED · airframe 63,107 hrs · 46,353 cycles

PRESENCE OF WATER ON RT ELEVATOR ANTI-FLOAT TAB HONEYCOMB STRUCTURE. RT ELEVATOR ANTI-FLOAT TAB WAS REPLACED DUE TO EXCESSIVE DAMAGE AND PN WAS VERIFIED IAW IPC 55-20-04 AND WILL BE INSTALLED UNDER CARD 2730-4182, JOB 001-0200.

Part: CUSP WEB — CRACKED (BS 829-951) · airframe 63,107 hrs · 46,353 cycles

CRACKED AND CORROSION RT CUSP WEB FROM X -54 TO X -60 BETWEEN BS 829-951. CORROSION REMOVED IAW SRM 51-10-3, PAR 14, 21 26-38. CRACKED AREA WAS REPAIRED WITH NRC 20000043945, CARD 244, ZONE 201.

Part: PAN — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED PAN BELOW AFT STOP NR 3 AT AFT CARGO COMPARTMENT DOOR. CRACK ON PAN BELOW AFT STOP NR 3 WAS REPAIRED IAW SRM 52-05D, FIG 50.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK, SETTLEMENT AREA AND ALSO TOOL MARKS OF FUEL ACCESS PLATE NR 1361C AT LT WING. ACCESS DOOR 1361C WAS REPLACED AND PN WAS VERIFIED IAW IPC 57-30-00-058 AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0387. (LP1835010)

Part: ANGLE — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED 2 ANGLES BETWEEN UPPER FUSELAGE SKIN AND DORSAL FIN BASE AT L/E RAM AIR SCOOP AREA STA Y= 1407 TO Y= 1427.

Part: BEAM — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACK ON BEAM NR 4, STA Y=171 AT FORWARD SERVICE DOOR. 1 PLATE, 2 INTERCOSTAL, 3 DOUBLER HAT, INNER SKIN 4 SUPPORTS AND FRAME WERE REMOVED IAW SRM 51-20-2 AND 51-30-5. NEW BEAM WAS DRILLED IAW SRM 51-10-4. HOLE DRILLED TREATED AND PAINTED IAW SRM 51-10-3 PARA. 14 AND 21. NEW BEAM AND REMOVED PARTS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB BETWEEN STA Y=1246 TO Y= 1250, X=54 TO X=60 AT PAX CABIN. DAMAGE WAS REMOVED, REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 131A-6, SHT -1.

Part: INTERCOSTAL — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED INTERCOSTAL ON LT INBD MLG DOOR BETWEEN STA Y=948-953. CRACKED INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. NEW INTERCOSTAL WAS FABRICATED IAW SRM AND DWG 51-10-2, 5930583-257, DWG 5930583, REV CK. NEW INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. NEW INTERCOSTAL INSTALL IAW SRM 51-30-2.

Part: CUSP WEB — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACK ON LT CUSP WEB STA Y=845, X=54 AND ALSO ON STA Y= 907, X=54 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131-3 AND SRM 51-10-3 PAR. 14, 21 AND SRM 51-30-5.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1303C AT LT WING. FUEL ACCESS PLATE 1303C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: SKIN — CRACKED (DOOR) · airframe 63,107 hrs · 46,353 cycles

CRACK ON EXTERNAL SKIN AROUND EXTERNAL HANDLE CUTOUT AT FWD ENTRY DOOR. CRACK WAS FOUND OF 0.500" OF LENGTH. CRACK ON EXTERNAL SKIN WAS STOPPED DRILL IAW ERA 501106-14 MA REV-"B". HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001 AND ERA 501106-14MA REV A. NO CRACKS WERE FOUND. DOUBLER REPAIR WAS FABRICATED IAW ERA 501106-14MA, REV "B". AREA WAS TREATED AND PAINTED. DOUBLER WAS PAINTED IAW SRM 51-10-3, PAR 14 AND 21. CONICAL WASHER'S WERE INSTALLED IAW ERA NR 501106-14MA, REV "B". DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND ERA NR 501106-14 MA REV "B".

Part: CUSP WEB — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT CUSP WEB PREVIOUS REPAIR DOUBLER STA Y= 446-465, Y=526-528, Y=579-595, NAD Y=830-840, X=54 TO X=60 AT CABIN FLOOR STRUCTURE. AREAS WERE REPAIRED IAW SRM 53-05 FIG 131A-1, 51-10-3 PARA .14-21.

Part: RUDDER — NONE · airframe 63,107 hrs · 46,353 cycles

THE RUDDER WAS PAINTED. PERFORM WEIGHT AND BALANCE PROCEDURE. WEIGHT AND BALANCE ON RUDDER WAS PERFORMED AND RUDDER TAIL MOMENT IS +630.5 THEREFORE WAS FOUND WITHIN OF LIMITS IAW SRM 55-40-1.

Part: TAB — DAMAGED · airframe 63,107 hrs · 46,353 cycles

NICK ON LOWER SURFACE AT LT ELEVATOR CONTROL TAB STA XHS=32. DAMAGE LT CONTROL TAB WAS REPLACED DUE TO EXCEEDING 4 REPAIRS IAW SRM 55-04 PARA 2.

Part: PAN — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACK ON INNER PAN ABOVE BEAM NR 4, STA Y=168 AT FORWARD SERVICE DOOR. DOUBLER WAS FABRICATED IAW SRM 52-03, FIG. 3. NEW DOUBLER AND AREA WERE TREATED AND PAINTED IAW SRM 51-10-3 PARA 14 AND 21, NEW REPAIR DOUBLER WERE INSTALLED IAW SRM 52-03, FIG 3.

Part: LONGERON — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED LONGERON 12LT FROM STA Y=1437 AT A/A. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CRACKED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CRACK ON LT CUSP WEB STA Y=747 FROM X=56 TO X=60 CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK ALSO SETTLEMENT AREA FUEL ACCESS PLATE NR 1456C AT RT WING. ACCESS PLATE WAS FOUND OUT OF LIMITS THEN WAS REPLACED IAW SRM 51-22-2A, IPC 57-30-00 AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: BEAM — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACK ON BEAM NR 1 BETWEEN FWD EDGE AND FRAME STA Y=175 AT FORWARD SERVICE DOOR. 1 STIFFENER, 4 FITTINGS, 2 CLIPS, 1 PLATE, 2 INTERCOSTALS, 6 RETAINER, 1 BEAM AND INNER SKIN WERE REMOVED IAW SRM 51-30-2, 51-30-5. NEW BEAM WAS DRILLED IAW SRM 51-10-4. NEW BEAM HOLES WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21. 1 STTIFENER, 4 FITTING, 2 CLIPS, 1 PLATE, 2 INTERCOSTALS, 6 RETAINERS, 1 BEAM AND INNER SKIN WERE INSTALLED IAW SRM 51-30-2, AND 51-30-5.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1371C AT LT WING. REPLACED FUEL ACCESS PLATE UNDER CARD NR 231.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1377C COUNTERSINK HOLES, 5EA. REPLACED FUEL ACCESS PLATE IAW IPC 57-30-00.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK, SETTLEMENT AREA AND ALSO FUEL ACCESS PLATE NR 1462C AT RT WING. PLATE WAS FOUND OUT OF LIMITS THEN WAS REPLACED IAW SRM 51-22-2A, IPC 57-30-00.

Part: DOOR FRAME — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED RT AFT OVERWING EMERGENCY EXIT UPPER DOOR JAMB. UPPER DOOR JAMB WAS REPAIRED IAW SRM 53-05, FIG 32 AND SRM 51-30-2.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1371C COUNTERSINK HOLES 4 EA . REPLACED FUEL ACCESS PLATE IAW IPC 57-30-00.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND TOOL MARKS OF FUEL ACCESS PLATE NR 1377C AT LT WING. REPLACED FUEL ACCESS PLATE UNDER CARD NR 230.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1355C COUNTERSINK HOLES, 1EA. FUEL ACCESS PLATE 1355C COUNTERSINK HOLES. 1 EA WAS REPAIRED IAW SRM 51-22-2A, PAR 6.

Part: SKIN — DAMAGED · airframe 63,107 hrs · 46,353 cycles

DAMAGE METALIZED AND PAINT COAT ON RUDDER SKIN BOTH SIDES. RUDDER WAS REPAIRED IAW SRM 51-70-1A, PARR 23.

Part: CUSP WEB — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACK ON RT CUSP WEB FROM STA Y=913 TO Y=915 BETWEEN X=-54 TO X=-60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, SRM 51-10-3, PAR 14, 21 SRM 51-30-2.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON CUSP ANGLE PREVIOUS REPAIR DOUBLER BETWEEN Y=679 AND Y=693 X=-60. REPAIR DOUBLER WAS REPLACED IAW ER/A 474509-14, REV A AND SRM 51-10-3, PAR 14, 21, 51-30-5. (LP1831409)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1357C COUNTERSINK HOLES, 5 EA. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: CUSP WEB — CORRODED · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT CUSP WEB STA Y=665 BETWEEN X=54 TO X=60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6 AND SRM 51-10-3 IAW 14,21, SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK, SETTLEMENT AREA AND ALSO TOOL DAMAGE OF FUEL ACCESS PLATE NR 1373C AT L WING. FUEL ACCESS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1436C COUNTERSINK HOLES, 4EA. ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: CUSP WEB — CORRODED (BS 503-598) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

SEVERAL AREAS OF CORROSION ON RT CUSP WEB BETWEEN BS 503 - 598 X -60. CUSP WEB REPLACED IAW DWG 9930538, REV BF AND SRM 53-14-2, FIG 4, SRM 51-10-3, PAR 14, 21, AND SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1335C COUNTERSINK HOLES, 1EA. BUSHING WAS FABRICATED IAW SRM 51-22-2A BUSHING AND REWORKED AREA WERE TREATED IAW SRM 51-10-3 P.21. NEW BUSHING ON ACCESS PLATE NR 335C WAS INSTALLED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 615) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT CUSP WEB BS 615 BETWEEN X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14 AND SRM 51-30-2 AND SRM 51-10-3, PAR 14,21.

Part: STRUCTURE — DAMAGED · airframe 63,107 hrs · 46,353 cycles

LOOSE FASTENERS ON LOWER EDGE RT SIDE ABOVE LOWER SPLICE OF VERTICAL STABILIZER REMOVABLE L/E. HOLES, 17E/AS WERE REWORKED AND BUSHINGS WERE FABRICATED, PROTECTED ALSO INSTALLED IAW SRM 55-03D.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUEL ACCESS PLATE 1478C COUNTERSINK HOLES, 4EA. BUSHINGS WERE FABRICATED IAW SRM 51-22-2A. BUSHINGS AND REWORKED AREA WERE TREATED IAW SRM 51-10-3 P .21. NEW BUSHINGS ON ACCESS DOOR NR 1428C WERE INSTALLED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK ALSO SETTLEMENT AREA , FUEL ACCESS PLATE NR 1409C AT RT WING. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390 JOB 001-0393.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1470C AT RT WING. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0393.

Part: CUSP WEB — CRACKED (BS 807-815) · airframe 63,107 hrs · 46,353 cycles

CRACKED CUSP WEB BETWEEN BS 807 - 815 X -56. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 131A-4.

Part: CUSP WEB — CORRODED (BS 521) · airframe 63,107 hrs · 46,353 cycles

CRACK ON LT CUSP WEB BS 521, X 60. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-9, 51-30-5, AND 51-10-3 PAR 14, 21.

Part: CUSP WEB — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED RT CUSP WEB BETWEEN Y=788 AND Y=807 X=-45. CUSP WEB WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A , 51-30-1, 51-30-2 AND DWG 9930538, REV: CF.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK SETTLEMENT AREA FUEL ACCESS PLATE NR 1410C AT RT WING. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1363C AT LT WING. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1307C AT LT WING. FUEL ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1379C AT LT. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED.

Part: SEAT TRACK — CORRODED (BS 1228-1232) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT SEAT TRACK PLUG X 54 BTW BS 1228 - 1232. REPAIR PLUG WAS REPLACED IAW SRM 53-05 FIG 4A AND SRM 51-10-3, PAR 14, 21,38 SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT CUSP WEB REPAIR DOUBLER BETWEEN BS 465 AND 484 X -60. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05.

Part: BEAM — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKS ON FWD AND AFT EDGE BEAM NR 1 AT FWD ENTRY DOOR. CRACKS ON FWD AND AFT EDGE BEAM 1 WERE REPAIRED IAW SRM 52-05, FIG 97 AND 98 SHEET 3.

Part: ANGLE — CRACKED · airframe 63,107 hrs · 46,353 cycles

CRACKED ANGLE CLIP BELOW BEAM NR 1, STA Y=172 AT FORWARD SERVICE DOOR. FABRICATED IAW DWG 9911579. CLIP WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. NEW CLIP WAS INSTALLED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1365C AT LT WING. FUEL ACCESS WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: CUSP WEB — CORRODED (BS 1184-1187) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB BETWEEN BS 1184 - 1187, X -54 TO X -60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: FLOOR PANEL — BROKEN · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR PANELS NR 1307C AND 1307A. FLOOR PANEL NR 1307C AND 1307A WERE REPAIRED IAW SRM 51-70-1D, PARR 10.

Part: PANEL SUPPORT — BROKEN (BS 674) · airframe 63,107 hrs · 46,353 cycles

BROKEN SLANT PANEL SUPPORT BS 674 BETWEEN LONGERONS 24 -28L. BROKEN SUPPORT WAS REPLACED IAW ER/A 413029-14MA.

Part: SKIN — CORRODED (BS 1033-1131) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT AFT FILLET PANEL AREA BETWEEN BS 1033 - 1131 AND LONGERONS 18 - 30L. CORROSION AND FASTENERS WERE REMOVED. REWORKED AREAS WERE TREATED AND PAINTED AND FASTENERS REMOVED WERE INSTALLED IAW SRM 51-10-3, PAR 26, 21 AND 14, 53-04, PAR.57 AND 51-30-5.

Part: SKIN — CORRODED (BS 1033-1131) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT RT AFT FILLET PANEL AREA BETWEEN BS 1033 - 1131 LONGERONS 3-18R . CORROSION REMOVED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 26-21 AND 14, 53-04, PAR 57 AND 51-30-5.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,107 hrs · 46,353 cycles

CRACKED PAN NEAR TO DOOR STOP 11 ON RT FWD EMERGENCY EXIT DOOR. AREA WAS REPAIRED IAW SRM 52-05D, FIG 51, 51-10-3 PARA 14 AND 21, 51-30-1, 51-30-2, 51-30-5 AND 51-10-2.

Part: SKIN — WORN (CARGO DOOR) · airframe 63,107 hrs · 46,353 cycles

WEAR ON FWD PRODUCTION DOUBLER OUTER SKIN AT FWD CARGO DOOR. DAMAGED DOUBLER WAS REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3 PAR 14/21, ER/A 486624-14 MA.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 63,107 hrs · 46,353 cycles

CRACKED ANGLE ON FWD EDGE, STOP FITTING 12, AT RT AFT OVERWING EMERGENCY EXIT DOOR . THE ANGLE WAS FABRICATED IAW SRM 51-30-2, 51-30-5 DWG 9957735 REV G AND 51-10-3 PARA 14 AND 21.

Part: FRAME — WORN (BS 1401) · airframe 63,107 hrs · 46,353 cycles

WORN FRAME BS 1401 BETWEEN LONGERON 20 - 22R. FRAME REPLACED IAW SRM 53-14-4, FIG 1 AND 51-10-3 PAR 21 AND 14.

Part: SUPPORT — CRACKED (BS 1174) · airframe 63,107 hrs · 46,353 cycles

CRACKED TEE SUPPORT ON INTERCOSTAL STA Y=1174 BETWEEN BEAM 1 AND LOWER EDGE AT AFT CARGO DOOR. CRACKED TEE SUPPORT WAS REMOVED IAW SRM 51-30-2, SRM 51-30-2. NEW TEE SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 63,107 hrs · 46,353 cycles

CRACKED ANGLE ON BEAM 1 AND DOOR STOP 1 OF RT/FWD EMERGENCY EXIT DOOR. THE ANGLE WAS FABRICATED IAW SRM 51-30-5,51-30-2, 51-10-3 PARA 14 AND 21 AND DWG 9957735, REV G.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON PAX CABIN FLOOR PANEL 160G. FLOOR PANEL REPLACED IAW DWG 9957828, SRM 51-10-3, PAR 14, 21, 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 749-788) · airframe 63,107 hrs · 46,353 cycles

CRACK ON INTERCOSTAL BETWEEN BS 749-788 AND X 1. THE INTERCOSTAL WAS REPLACED IAW DWG 9936580, REV B AND SRM 51-10-3, PAR 14,21, SRM 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 440) · airframe 63,107 hrs · 46,353 cycles

CRACKED CUSP WEB BS 440 BETWEEN X -60. REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-2 AND 51-10-3 PAR 14, 21.

Part: FLOOR PANEL — DELAMINATED · airframe 63,107 hrs · 46,353 cycles

DELAMINATED FLOOR PANELS 120C, 160F, 389C, 541C, 769D, 826D. FLOOR PANELS NRS. 160F, 389C, 541C, 769D, 826D AND 886C. WERE FABRICATED IAW AMM 53-20-01-201. FLOOR 120C WAS INSPECTED AND NO DAMAGE WAS FOUND.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 63,107 hrs · 46,353 cycles

CRACKED ANGLE ON BEAM 1 AND DOOR STOP 12 OF LT FWD EMERGENCY EXIT DOOR. THE ANGLE WAS FABRICATED, TREATED, PAINTED, INSTALLED IAW SRM 51-30-1, 51-30-5, DWG 9957735, REV G.

Part: FRAME — CRACKED (BS 1437) · airframe 63,107 hrs · 46,353 cycles

CRACKED FRAME ANGLE BS 1437 LONGERONS 16 - 17R. FRAME ANGLE WAS REPLACED IAW DWG 9911840, REV DC AND SRM 51-30-2 , 51-30-5 , 51-10-3, PAR 21 AND 14.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,107 hrs · 46,353 cycles

CRACKED PAN NEAR TO DOOR STOP 4 ON LT FWD EMERGENCY EXIT DOOR. AREA WAS REPAIRED IAW SRM 52-05D, FIG 51, 51-30-2, 51-30-5, 51-30-1, 51-10-3 PARA 14 AND 21.

Part: CUSP WEB — CRACKED (BS 1009) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CRACK ON LT CUSP WEB BS 1009, X 54 TO X 60. DAMAGE REMOVED, DOUBLER FABRICATED AND INSTALLED IAW SRM 53-05, FIG 151A-3.

Part: STIFFENER — CRACKED (BS 1338) · airframe 63,107 hrs · 46,353 cycles

CRACK ON STIFFENER AT BS 1338 X 0 PRESSURE BULKHEAD LONGERON 1. STIFFENER WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 458) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON CUSP WEB, BS 458 X -60. REPAIRED IAW SRM 53-05, FIG 131A-13 AND 51-30-2,51-10-3, PAR 14,21.

Part: FLOOR PANEL — PUNCTURED · airframe 63,107 hrs · 46,353 cycles

PUNTURED PAX CABIN FLOOR PANELS NR 256D AND 886D. FLOOR PANEL NR 886D WAS FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL 256D WAS WORKED IN NRC 135.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL. SERVICE PANEL WAS REPLACED IAW DWG 5914792 AND SRM 51-30-2/51-30-5/51-10-3 AND 51-10-4.

Part: FLOOR PANEL — DEBONDED · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR PANEL AND DISBONDED CHANNEL. FLOOR PANEL WAS REPAIRED AND BONDED IAW SRM 51-70-1 D AND DPS 1.07-39.

Part: SKIN — CORRODED (BS 807-1033) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT RT OVERWING FILLET PANEL AREA BETWEEN BS 807 - 1033 AND LONGERONS 17 - 18R. REMOVE CORROSION AND REWORKED AREAS WERE MEASURED. ORIGINAL THICKNESS ON STA Y=927-950, LONG 18-17 RT IS 0.160" AND REMAINING'S 0.157" ON STA Y=960-1003 LONGERONS 18-17 RT 0.125" AND REMAINING'S 0.119"AND STA Y=1003-1020 ORIGINAL'S 0.063" AND REMAINING'S 0.060", THEREFORE THESE ARE WITHIN LIMITS IAW SRM 53-04, PAR.57. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR. 26, 21 AND 14.

Part: SKIN — CORRODED (BS 807-864) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT RT FWD UNDERWING FILLET PANEL AREA BETWEEN BS 807 - 864 AND LONGERONS 28 - 30R. CORROSION WAS REMOVED AND REWORKED AREA WAS MEASURE STAY=824, LONGERON 30-29 RT IS 0.160" AND REMAINING'S 0.147". ON STA Y= 820-817 LONGERON 30-29, RT ORIGINAL'S 0.080" AND REMAINING'S 0.075" AND STA Y=813-807, LONG 29-28 RT ORIGINAL'S 0.170" AND REMAINING'S 0.160", THEREFORE IT'S WITHIN LIMITS, RESPECTIVELY. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR.26,21 AND 14 AND 53-04, PAR 57.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,107 hrs · 46,353 cycles

CRACKED LONGERON 13L BS 1437. LONGERON REPAIRED IAW SRM 53-02, FIG. 18, 51-30-5, 51-30-2 AND 51-10-3.

Part: SKIN — CORRODED (BS 807-1033) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN LT OVERWING FILLET PANEL AREA BETWEEN BS 807 - 1033 AND LONGERONSS 17 - 18LT. CORROSION WAS REMOVED AND REWORKED AREA WAS MEASURE. ORIGINAL THICKNESS ON STA Y=819-824, LONG 18-17 LT IS 0.063" AND REMAINING IS 0.061". ON STA Y=859-863, LONGERON 18 LT ORIGINAL IS 0.100" AND REMAINING IS 0.92". ON STA Y=899-900 LONG 18-17 LT ORIGINAL IS 0.125" AND REMAINING IS 0.120". ON STA Y=920-929, LONG 18-17 LT ORIGINAL IS 0.160" AND REMAINING IS 0.154". ON STA Y=946-965, LONG 18-17 LT ORIGINAL IS 0.160" AND REMAININGS IS 0.153". ON STA Y=966-1003, LONG 18-17 LT, ORIGINAL IS 0.125" AND REMAINING IS 0.119", THEREFORE THESE ARE WITHIN LIMITS, RESPECTIVELY. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21 AND 14 AND 53-04, PAR.57.

Part: SKIN — CORRODED (BS 726-807) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT LT WING L/E FILLET PANEL AREA BETWEEN BS 726 - 807 AND LONGERONS 17-30L. CORROSION WAS REMOVED AND REWORKED AREAS WERE MEASURED ORIGINAL THICKNESS ON STA Y=805, LONGERON 29-28 LT IS 0.157" AND REMAINS 0.142" ON STA Y=803, LONG 29-28 LT IS 0.153" AND REMAINING'S 0.149" ON STA Y=850 LONG 29-28 LT IS 0.160" AND REMAINING'S 0.140" ON STA Y=770, LONGERON 27-26 LT ORIGINAL'S 0.090" AND REMAINING 0.074" ON STA Y=768, LONGERON 27-26 LT ORIGINAL'S 0.087" AND REMAINING'S 0.080" ON STA Y=759-741, LONG 28-26 LT ORIGINAL'S 0.063" AND REMAINING'S 0.058" ON STA Y=740-726, LONGERON 26-18 LT ORIGINAL'S 0.063" AND REMAINING'S 0.054" AND STA Y=743-807, LONG 18-16 LT ORIGINAL'S 0.063" AND REMAINING'S 0.055". THEREFORE THESE ARE WITHIN LIMITS. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR. 26, 21 AND 14 AND 53-04, PAR.57.

Part: LONGERON — CORRODED (BS 1338) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LONGERON 29L BS 1338. THE LONGERON WAS REPLACED IAW SRM 51-10-3 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1418) · airframe 63,107 hrs · 46,353 cycles

CRACKED LONGERON 2L BS 1418. LONGERON REPAIRED IAW SRM 53-02 FIG 18, 51-10-3 AND 51-30-5.

Part: STOP FITTING — CRACKED (CARGO DOORWAY) · airframe 63,107 hrs · 46,353 cycles

CRACKED STOP FITTINGS, ON FWD EDGE AND AFT EDGE BETWEEN BEAMS 1-2 AT FWD CARGO DOOR. DAMAGE STOPS FITTINGS WERE REMOVED. NEW STOP FITTINGS WERE DRILLED. HOLES OF STOP FITTINGS WERE TREATED AND PAINTED. NEW FITTINGS WERE INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4, 51-10-3 PAR 21/14.

Part: LONGERON — CRACKED (BS 1418) · airframe 63,107 hrs · 46,353 cycles

CRACKED LONGERON 2R FROM BS 1418. LONGERON REPAIRED IAW SRM 53-02, FIG 18, 51-10-3 AND 51-30-5.

Part: SKIN — CORRODED (BS 807-864) · airframe 63,107 hrs · 46,353 cycles

CORROSION ON FUSELAGE SKIN AT LT FWD UNDERWING FILLET PANEL AREA BETWEEN BS 807 - 864 AND LONGERONS 28 - 30L. CORROSION WAS REMOVED AND REWORKED AREA WAS MEASURE. ORIGINAL THICKNESS ON STA Y=815-820, LONG 30-29 LT IS 0.080" AND REMAINING'S 0.076" AND STA Y=820-826, LONG 29-30LT ORIGINAL'S 0.160" AND REMAINING'S 0.136", THEREFORE THESE ARE WITHIN LIMITS, RESPECTIVELY. REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3,PAR. 26,21 AND 14 AND 53-04, PAR.57.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON REPAIR SPACER AT CENTER LOWER CARGO BAY DOOR FRAME BS 636-693. REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123A SRM 51-10-3 PAR 14, 21.

Part: SKIN — CORRODED (BS 1774-1184) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON REPAIR DOUBLER BS 1774 - 1184 BETWEEN LONGERONS 22 - 23L. DOUBLER REPLACED IAW SRM 53-04, FIG 12D AND SRM 51-30-2, SRM 51-30-5 AND 51-10-3 PAR 14, 21, 38.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,107 hrs · 46,353 cycles

DELAMINATED FLOOR PANEL. FABRICATED A NEW FLOOR PANEL IAW AMM 53-20-01-201 AND PS900-5-2 NR 2.

Part: INTERCOSTAL — CRACKED (BS 1346) · airframe 63,107 hrs · 46,353 cycles

CRACK ON INTERCOSTAL BS 1346 AND X -19. INTERCOSTAL REPAIRED IAW SRM 53-01, FIG 4.

Part: BUSHING — WORN (LT AILERON) · airframe 63,107 hrs · 46,353 cycles

WORN HINGE BUSHING AT LT AILERON TRIM TAB L/E. BUSHING AT LT AILERON TRIM TAB L/E WERE R & R IAW CMM 27-101.

Part: CUSP WEB — CRACKED (BS 224-226) · airframe 63,107 hrs · 46,353 cycles

CRACK ON LT CUSP WEB, BS 224-226 BETWEEN X 54 TO X 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6 SRM 51-10-3 PAR 14, 21 AND SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (BS 1380-1387) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON INTERCOSTAL X -14 BETWEEN BS 1380 TO 1387. INTERCOSTAL REPAIRED IAW SRM 53-01, FIG 4.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT HORIZONTAL STABILIZER UPPER BARREL NUT HOLES NR 12, STA XH=6.625. DAMAGE ON BARREL NUT HOLE NR 12 WAS REWORKED IAW ER/A 532521-14, REV ORIG AND ETI-88-15-067 R1.

Part: CUSP WEB — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON REPAIR DOUBLER ON RT CUSP WEB BETWEEN BS 1155 TO 1174, X -50 TO X -60. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-5, SRM 51-10-3, PAR 14, 21, AND SRM 51-30-5.

Part: FLOOR SUPPORT — BROKEN (CABIN) · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR SUPPORT. FLOOR SUPPORT REPAIRED IAW SRM 53-05, FIG 131C.

Part: FLOOR SUPPORT — BROKEN (CABIN) · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR SUPPORT. THE FLOOR SUPPORT REPAIRED IAW SRM 53-05, FIG. 131C.

Part: WEB — CRACKED (BS 1463) · airframe 63,107 hrs · 46,353 cycles

CRACKED WEB ON BS 1463. WEB REPLACED IAW SRM 53-14-4, FIG 3, ITEM 8 AND 35, SRM 51-31-2, 51-30-5 AND SRM 51-10-3, PAR 14, 21.

Part: MECHANISM — WORN (TAILCONE RELEASE) · airframe 63,107 hrs · 46,353 cycles

MAINTENANCE FOUND A WORN TAILCONE RELEASE MECHANISM CAM ON STA Y=1510 CANTED BULKHEAD AT THE 11 O'CLCOCK POSITION. MAINTENANCE REPLACED THE RELEASE MECHANISM CAM.

Part: FLOORBEAM — CRACKED (BS 927) · airframe 63,107 hrs · 46,353 cycles

CRACKED FLOORBEAM AT BS 927 X 54. FLOORBEAM WAS REPLACED IAW SRM 51-30-5.

Part: FLOOR SUPPORT — BROKEN (CABIN) · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-05, FIG 131C.

Part: FLOOR SUPPORT — BROKEN (FUSELAGER) · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-05, FIG 131C.

Part: DOOR FRAME — MISREPAIRED (CARGO BAY) · airframe 63,107 hrs · 46,353 cycles

SPACER REPAIR ON AFT CARGO DOOR FRAME MISREPAIRED. REPLACED IAW SRM 53-05, FIG 123.

Part: FRAME — CRACKED (BS 1451) · airframe 63,107 hrs · 46,353 cycles

CRACKED FRAME BS 1451, BETWEEN LONGERONS 3R - 9L. FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9911860, REV L.

Part: RIB — CORRODED (SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL NR 3 RIB FWD BORE, STA XOS=380. DAMAGE WAS REPAIRED IAW ETI-88-15-046 AND ER/A NR 532495-14, REV ORIGINAL.

Part: STRUCTURE — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RIB HOLES AT LT WING SLAT PANEL NR 4, STA XOS= 380. DAMAGE WAS REPAIRED IAW ETI-88-15-051 AND ER/A NR 532502-14, REV ORIGINAL.

Part: RIB — CORRODED (NR 2) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION AND WEAR ON RT SLAT PANEL, NR 2 RIB FWD BORE STA XOS=285. DAMAGE WAS REPAIRED IAW ETI-88-15-044 AND ER/A NR 532498-14, REV ORIGINAL.

Part: RIB — CORRODED (RT SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL NR 4 RIB FWD BORE AT STA XOS=380. DAMAGE WAS REPAIRED IAW ETI-88-15-048 R1 AND ER/A NR 532500-14, REV ORIGINAL.

Part: RIB — CORRODED (NR 2 SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL NR 2 RIB INBD FWD BORE STA XOS=198. CORROSION ON RT SLAT PANEL NR 2 RIB INBD FWD BORE XOS= 198 WAS REMOVED. FABRICATED BUSHINGS. INSTALLED BUSHINGS IAW SRM 57-02, PAR 9.

Part: RIB — CORRODED (NR 4 SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL NR 4 INBD RIB FWD BORE AT STA XOS= 429. DAMAGE WAS REPAIRED IAW ETI-88-15-048 AND ER/A NR 532500-14, REV ORIGINAL.

Part: SPACER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON REPAIR SPACER AT AFT LOWER CARGO DOOR FRAME BS 1154-1121. SPACER REPLACED IAW SRM 53-05, FIG 123.

Part: FLOOR SUPPORT — BROKEN (CABIN) · airframe 63,107 hrs · 46,353 cycles

BROKEN FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-05, FIG 131C.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 63,107 hrs · 46,353 cycles

CRACK ON FLOOR SUPPORT. REPAIRED IAW SRM 53-05, FIG 131C.

Part: FLOOR SUPPORT — BROKEN (CABIN) · airframe 63,107 hrs · 46,353 cycles

FLOOR SUPPORT BROKEN. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-05, FIG 131 C.

Part: RIB — CORRODED (RT SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL NR 1 RIB OTBD FWD BORE STA XIS=136. DAMAGES WERE REWORKED AND MEASURED WITH ID 0.938". FABRICATED AND INSTALLED NEW BUSHINGS IAW SRM 57-02, PAR 9.

Part: SEAT TRACK — CORRODED (BS 1256-1260) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON REPAIR PLUG OF SEAT TRACK X -22, BS 1256-1260. REPAIR PLUG WAS REPLACED SRM 53-05, FIG 4A AND 51-10-3 PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 1281-1285) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON REPAIR PLUG ON SEAT TRACK X=-22, BS 1281-1285. THE REPAIR PLUG WAS REPLACED IAW SRM 53-05, FIG 4A AND 51-10-3, PAR 14 AND 21.

Part: RIB — CORRODED (SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL RIB OTBD FWD BORE AND INBD AFT BORE, XIS=40. DAMAGES WERE REWORKED AND MESURED WITH I.D. 0.940". FABRICATED AND INSTALLED BUSHINGS IAW SRM 57-02, PAR 9.

Part: PANEL — CORRODED (SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT SLAT PANEL NR 0, RIB INBD/OUTBD AFT BORES AT STA XIS= 12. DAMAGES WERE REWORKED AND MEASURED WITH ID 1.064. INSTALLED NEW BUSHINGS IAW SRM 57-02, PAR 9.

Part: RIB — CORRODED (RT SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SLAT PANEL NR 1 RIB INBD AFT BORE STA XIS= 83. REPAIRED THE DAMAGE. BUSHINGS FABRICATED AND INSTALLED IAW SRM 57-02, PAR.

Part: RIB — CORRODED (LT SLAT) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON LT SLAT PANEL NR RIB INBD, OTBD AFT BORES AT STA XIS= 40. DAMAGES WERE REWORKED AND MESURED WITH ID 0.9385". BUSHINGS WERE FABRICATED AND INSTALLED NEW BUSHINGS IAW SRM 57-02, PAR 9.

Part: PAN — CRACKED (BS 807-1041) · airframe 63,107 hrs · 46,353 cycles

CRACKED LT WINDOW RING PAN BETWEEN BS 807-826 AT FWD/ UPPER CORNER AND BETWEEN BS 1022-1041 AT FWD LWR CORNER. AREA DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 122, ER/A 493648-14 MA REV ORIGINAL, AND 487747-14 MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 1041-1174) · airframe 63,107 hrs · 46,353 cycles

CRACKED RT WINDOW RING PAN AT AFT UPPER CORNER BETWEEN BS 1041-1060 AND BS 1155-1174. AREA DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 122, ER/A'S 487747-14 MA REV ORIGINAL AND 493648-14 MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 1079-1098) · airframe 63,107 hrs · 46,353 cycles

CRACKED LT WINDOW RING PAN BETWEEN BS 1079-1098 AT FWD UPPER/ LWR CORNERS. AREA DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 122, ER/A'S 493648-14MA, REV ORIGINAL AND 487747-14 MA, REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 657-662) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION FOUND ON THE RT SEAT TRACK X=-54 REPAIR PLUG STA Y=657-662. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A 51-10-3, PAR 14, 21,38.

Part: SEAT TRACK — CORRODED (BS 857-861) · corrosion level 2 · airframe 63,107 hrs · 46,353 cycles

CORROSION ON RT SEAT TRACK X=-54 REPAIR PLUG BS 857-861. PLUG WAS REPLACE IAW SRM 53-05, 51-10-3, 51-30-1.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 61,003 hrs · 44,853 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT THE OVERWING HATCHES AND SEAT ROWS 24-30 WERE INOPERATIVE. REPLACED A FUSE AT THE POWER SUPPLY AND SPLICED A WIRE AT ROW 28 AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,665 hrs · 44,638 cycles

DURING LINE CHECK, NOTED EMERGENCY LIGHTS INOPERATIVE SEATS 24-30. FOUND OPEN FUSE AT BATTERY PACK B5-211 AND B5-212. REPLACED FUSES. CHECKED OK IAW WDM 33-51-14.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 60,190 hrs · 44,331 cycles

DURING LINE CHECK, NOTED EMERGENCY LIGHT AT SEAT 14DE WAS INOPERATIVE. REPLACED WIRE HARNESS IAW AMM 33-53 AND OPS CHECKED NORMAL.

Part: DOOR — DAMAGED (CARGO DOOR) · airframe 59,911 hrs · 44,139 cycles

CARGO DOOR DAMAGED. REPAIRED IAW AA 5230-01159.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

DURING LINE CHECK, RT TAILCONE RELEASE CABLE WAS FOUND TO BE FRAYED. REPLACED CABLE IAW WC 5350-01077-0101.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

DURING LINE CHECK, LT TAILCONE RELEASE CABLE WAS FOUND TO BE FRAYED. REPLACED CABLE IAW WC 5350-01077-0101.

Part: LATCH — WORN (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

UPPER LT TAILCONE LATCH ARM AND CLAMP NR 20 WORN. REPLACED LATCH ARM AND SLIDER BLOCK ASSY NR 20 CLAMP IAW AMM 53-53-00.

Part: LATCH — LOOSE (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

THIS UPPER RT TAILCONE LATCH ASSY IS LOOSE IN ITS FRAME. TIGHTENED LATCH ASSY BASE IN FRAME IAW AMM 53-53-00.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 59,911 hrs · 44,139 cycles

THE TAILCONE RELEASE TEE PIN IS WORN AT THE TAIL CONE RELEASE MECHANISM LT SIDE. REPLACED "T" PIN AND BUSHINGS IAW AMM 53-53.

Part: LATCH — LOOSE (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

THE LOWER LT TAILCONE LATCH ASSY IS LOOSE IN ITS FRAME AND IS MISSING A FASTENER. REPLACED MISSING FASTENER. RETIGHTENED LATCH ASSY BASE IN FRAME IAW AMM 53-53-00.

Part: LATCH — LOOSE (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

UPPER LT TAILCONE LATCH ASSY IS LOOSE IN ITS FRAME. TIGHTENED LATCH BASE ASSY IN FRAME IAW AMM 53-53-00.

Part: LATCH — WORN (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

THE UPPPER RT TAILCONE LATCH SPADE IS WORN. REPLACED SPADE IAW AMM 53-53-11-00.

Part: LATCH — LOOSE (TAILCONE) · airframe 59,911 hrs · 44,139 cycles

THE LOWER RT TAILCONE LATCH ASSY IS LOOSE IN ITS FRAME. TIGHTENED LATCH ASSY BASE IAW AMM 53-53-00.

Part: FRAME — CRACKED (BS 866) · airframe 59,911 hrs · 44,139 cycles

DURING SCHEDULED CHECK, UPPER RADIUS OF THE LT OVERWING FRAME TAB AT BS 866 WAS FOUND TO BE CRACKED. REPLACED FRAME IAW AMDS WC 5310-01415-031.

Part: STRUCTURE — DAMAGED (NLG WW) · airframe 59,911 hrs · 44,139 cycles

THE NLG RT SIDEWALL HAD DAMAGE FROM CONTACTING THE STEERING ACTUATOR. THE GOUGED AREA WAS BLENDED AND THE REMOVED MATERIAL EXCEEDED ALLOWABLE LIMITS. REPAIR ACCOMPLISHED IAW SRM 53-05, FIGURE 36 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKATE ANGLE — CRACKED (BS 1465) · airframe 59,911 hrs · 44,139 cycles

DURING SCHEDULED CHECK, RT VERTICAL STABILIZER SKATE ANGLE WAS FOUND TO BE CRACKED BETWEEN FASTERS AT BS 1465. REPAIRED IAW ER/A 519524-14.

Part: SKATE ANGLE — CRACKED (BS 1465) · airframe 59,911 hrs · 44,139 cycles

DURING SCHEDULED CHECK, LT VERTICAL STABILIZER SKATE ANGLE FOUND TO BE CRACKED BETWEEN FASTENERS AT BS 1465. REPAIRED IAW ER/A 519523-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,425 hrs · 43,776 cycles

DURING ROUTINE SERVICE CHECK, FWD CABIN EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE. MX REPLACED THE FORWARD POWER SUPPLY IAW AMM 33-53 AND OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,293 hrs · 42,977 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT THE OVERWING EXITS WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BLANKET — MISSING · airframe 57,051 hrs · 42,045 cycles

NO FOD HEATER BLANKET. REPAIRED IAW ERA 506734-14.

Part: ACM — SEIZED · airframe 56,891 hrs · 41,941 cycles

FLIGHT LEVEL 330, FLIGHT CREW NOTED AN ACRID ODOR IN COCKPIT THAT THEN TRAVELED BACK TOWARDS THE MID CABIN. ODOR DISSIPATED AND NEVER RETURNED. FLIGHT UNEVENTFULLY LANDED AT DESTINATION. ON INSPECTION, MAINTENANCE FOUND THE ACM HAD SEIZED. MAINTENANCE REPLACED THE ACM AND CLAMP, PERFORMED A SUCCESSFUL LEAK CHECK AND RETURNED THE AIRCRAFT TO SERVICE.

Part: MOUNT — CORRODED (LAVATORY) · airframe 56,420 hrs · 41,594 cycles

DURING LINE CHECK, MAINTENANCE FOUND CORROSION ON THE AFT LEFT LAV MOUNT PLATE DOUBLER. MAINTENANCE REMOVED AND REREPLACED THE MOUNT PLATE AND REINSTALLED THE LAV AND SEATS.

Part: SKIN — CRACKED (LT WING) · airframe 56,415 hrs · 41,590 cycles

LEFT WING L/E SKIN LOWER SURFACE XOS 245 CRACKED. REPAIRED IAW ERA 502458-14.

Part: FRAME — CORRODED (BS 1271 L22-29R) · airframe 56,415 hrs · 41,590 cycles

CORROSION IN THE FRAME STA 1271 ATTACH HOLES L30 BILGE AREA OF AFT CARGO COMPARTMENT. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND INSTALLED NEW UPPER AND LOWER SPLICES, FILLER ON BS 1271 BETWEEN L29R AND R22R IAW SRM 53-03D PG 16 FIG 2A.

Part: SILL — CORRODED (DOOR FRAME) · airframe 56,415 hrs · 41,590 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME LOWER SILL. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED SPACER ON AFT CARGO DOOR FRAME LOWER SILL IAW SRM 51-30-5 PG1.

Part: SKIN — DENTED (BS 239 L17L) · airframe 56,415 hrs · 41,590 cycles

ACCOMPLISH ERA 489526-14 REV D, CODE 53-31-20, PERMANENT REPAIR SEC V PERMANENT REPAIR AT NEXT PSV. FUSELAGE SKIN AT FS239 L-17L DENT ON EXISTING REPAIR DOUBLER. COMPLIED WITH ERA 489526-14 REV D SEC V AT SAA SAT PSV18 NR 4.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 56,409 hrs · 41,586 cycles

HORIZONTAL STAB UPPER CENTER SKIN PANEL IS DAMAGED. REPAIRED IAW AA 5510-01086.

Part: LUG — DAMAGED (HORIZONTAL STAB) · airframe 56,409 hrs · 41,586 cycles

HORIZONTAL STAB HINGE RIB PIVOT BEARING LUG DAMAGED. REPAIRED IAW AA 5500-01011.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 56,409 hrs · 41,586 cycles

VERTICAL STAB FRONT SPAR AND SKIN DAMAGED. REPAIRED IAW AA 5530-01045.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 56,100 hrs · 41,364 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 26E IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 55,938 hrs · 41,262 cycles

FLIGHT CREW FOUND EMERGENCY LIGHTS FROM ROW 24-30 INOPERATIVE. MAINTENANCE FOUND MULTIPLE FUSES BLOWN IN POWER SUPPLY. REPLACED FUSE, OPS CHECKED GOOD PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 55,474 hrs · 40,966 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 2C/D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,075 hrs · 40,688 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 24-30 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 54,562 hrs · 40,309 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT 26DE INOPERATIVE. MAINTENANCE RE-SECURED LOOSE CONNECTOR FROM SEAT. OPERATION OF LIGHT NOW CHECKS OK.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 54,114 hrs · 39,996 cycles

DIVERTED TO CVG DUE TO ELECTRICAL/SMOLDERING ODOR IN CABIN FROM ROW 16 AFT, NO VISUAL SMOKE REPORTED. MAINTENANCE INSPECTED CABIN AND GALLEYS. FOUND LIGHT BALLAST ABOVE 16 ABC, TO BE BAD AND REPLACED IT. ACCOMPLISHED DUCT BURNOUT PER OPN 5089. NO CONTAMINATION OF APU INLET AREA NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 53,807 hrs · 39,759 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHT INOPERATIVE AT ROW 12 DE. MX FOUND WIRES BROKEN AND INSTALLED NEW TRACK LIGHT QUICK DISCONNECT. OPS CHECKS GOOD. ACFT IS OK FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 53,619 hrs · 39,628 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 26EF INOPERATIVE. MAINTENANCE TIGHTENED A LOOSE CONNECTION AT LIGHT ASSEMBLY. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 52,628 hrs · 38,995 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS AT SEATS 1 THRU 13 AND FORWARD GALLEY RED LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING AT SEAT 13D. (2010-D1363) (DLM88103193)

Part: SPAR — DAMAGED (WING) · airframe 52,585 hrs · 38,968 cycles

WING REAR SPAR DAMAGED. REPAIRED IAW AA 5710-01110.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 51,109 hrs · 37,991 cycles

MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT SEAT 12DE TO BE INOPERATIVE. MAINTENANCE FOUND A PUSHED BACK PIN AT THE CONNECTOR. MAINTENANCE SECURED THE PIN. AN OPERATIONAL CHECK WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BUSHING — DAMAGED (RT MLG SUPPORT) · airframe 49,039 hrs · 36,615 cycles

BUSHING BORE ON RT MLG SUPPORT WITH OVERSIZED MEASUREMENT. A NEW OVERSIZED REPAIR BUSHING WAS NOT INSTALLED AS REQUESTED PER INSTRUCTIONS GIVEN ON RELATED ERA 475233-14AD REV ORIG DATED 01 JUNE 09. BUSHING WAS REPLACED IAW EA 09-093855-03AD REV B, DRAWING 4935859, AND ERA 475233-14AD REV ORIG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,039 hrs · 36,615 cycles

EXFOLIATION CORROSION ON ANGLE STA X=15 Y=1350 AT W2. ANGLE WAS REPLACED IAW ERA 474504-14.

Part: ANGLE — CORRODED (BS 673-693) · airframe 49,039 hrs · 36,615 cycles

EXFOLIATION CORROSION ON RIGHT CUSP ANGLE BETWEEN STA Y=673-693. FABRICATED REPAIR PARTS AND INSTALLED IAW ERA 474509-14 AND SRM 51-10-3.

Part: SUPPORT — CORRODED (RT MLG) · airframe 49,039 hrs · 36,615 cycles

BUSHING BORE ON RT MLG SUPPORT WITH OVERSIZED MEASUREMENT. BUSHING BORE FOUND WITHOUT DAMAGE. ID BORE SIZE 2.503. BUSHING BORE TREATED IAW SRM 51-10-3.

Part: BULKHEAD — CORRODED (HORIZONTAL STAB) · airframe 49,039 hrs · 36,615 cycles

EXFOLIATION CORROSION ON BARREL NUT HOLES OF HOR STAB UPPER BULKHEAD AT JOINT WITH CONSTANT SECTION. BARREL NUT HOLES WERE REPAIRED IAW ERA 475238-14.

Part: DOOR FRAME — CORRODED (C3 CARGO BIN) · airframe 49,039 hrs · 36,615 cycles

EXFOLIATION CORROSION ON C3 CARGO BIN LOWER DOOR JAMB AND BEAM FROM STA Y=1155 TO 1212. REPLACED CORRODED PIECES IAW SRM'S 51-30-2, 51-30-5, AND 53-05 FIG 123.

Part: SKIN — DAMAGED (RUDDER) · airframe 49,039 hrs · 36,615 cycles

DAMAGED METALLIZED SURFACE OF RUDDER. RUDDER REPAIRED IAW OPN 1031, CARD 1247, AND SRM 51-70-1AD PARA 23.

Part: PIN — CORRODED (TAILCONE) · airframe 49,039 hrs · 36,615 cycles

RUSTED GUARD PINS AND HARDWARE ON TAILCONE RELEASE CONTROL CABLES. GUARD PINS WERE REPLACED IAW AMM 20-30-01-201.

Part: TUBE — WORN (TAILCONE) · airframe 49,039 hrs · 36,615 cycles

WORN OUT GUIDE TUBE OF TAILCONE RELEASE CABLE SYSTEM RH LOWER SECTION. REPLACED GUIDE TUBE IAW AMM 20-30-01-201.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,039 hrs · 36,615 cycles

DENTS ON FUSELAGE SKIN BTW STA Y=238 AND Y=252 LONG 16L AND 18L. REPLACED DAMAGED AREAS IAW SRM 53-04D FIG 12B.

Part: FITTING — CRACKED (TAILCONE) · airframe 49,039 hrs · 36,615 cycles

CRACKED FITTING TO ATTACH TAILCONE RT UPPER POSITION. REPAIR PIECES WERE FABRICATED IAW DRAWING 9911959 ITEM 43 REV AV AND INSTALLED IAW DRAWING 9911957 REV AV.

Part: BLOCK — WORN (TAILCONE) · airframe 49,039 hrs · 36,615 cycles

WORN OUT BLOCK ON TAILCONE RELEASE CABLE SYSTEM AT 2HS POSITION. WORN BLOCKS WERE REPLACED IAW AMM 53-53-00-201.

Part: DOOR FRAME — CORRODED (STA 370 - 427) · airframe 49,039 hrs · 36,615 cycles

EXFOLIATION CORROSION ON LWR DOORJAMB BTW STA Y=370-427. REPAIRED DOORJAMB IAW SRM 53-05D FIG 804D.

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 48,884 hrs · 36,529 cycles

LIGHTNING STRIKE AT WINDOW 17L DAMAGE CLEANED UP PER SRM 53 -05 FIGURE 111 AND ERA 474350-14.

Part: DUCT — DAMAGED (NR 2 ENGINE) · airframe 47,886 hrs · 35,863 cycles

RT ENGINE FIRE LIGHT CAME ON DURING FLIGHT. FOUND BLOWN DUCT AT AFT SIDE OF COWL ANTI-ICE VALVE. REPLACED DUCT FROM 13TH STAGE SADDLE DUCT TO COWL ANTI-ICE VALVE.

Part: DOUBLER — CORRODED (FS 1307 L21) · airframe 47,865 hrs · 35,847 cycles

INTERNAL SURROUND DOUBLER FOR THE AFT LAV PAN WAS CORRODED ALONG THE LOWER EDGE. THE CORROSION WAS CUT OUT, AND AND EXTERNAL REPAIR DOUBLER WAS INSTALLED.

Part: PRESSURE PANEL — LEAKING (MLG WHEEL WELL) · airframe 39,580 hrs · 30,392 cycles

MLG WHEEL WELL SLANT PRESSURE PANEL REPAIRED IAW 09-085387-12.

Part: WIRE — CHAFED (HYD PUMP) · airframe 39,373 hrs · 30,231 cycles

SPARKS REPORTED COMING FROM RIGHT MLG WHEEL WELL DURING TAXI IN TO GATE. FOUND AUX HYDRAULIC PUMP POWER C/B POPPED AND WIRE BUNDLE GOING TO PUMP CHAFED AND BURNT IN WHEEL WELL AT HANDLE OF HYD SERVICE HAND PUMP. REPAIRING DAMAGED WIRING.

Part: B-NUT — CRACKED (NR 2 ENGINE) · airframe 37,828 hrs · 29,154 cycles

RT START VALVE WOULD NOT OPEN. REPLACED START DUCT AND SECURED LOOSE B-NUT.

Part: SWITCH — UNSERVICEABLE (TAIL CONE) · airframe 36,121 hrs · 27,914 cycles

ON LAYOVER CHECK FOUND TAIL CONE EMERGENCY HANDLE CABLE UNDONE WITH NO MSG IN COCKPIT SHOWING TAIL CONE UNSAFE. REPLACED SWITCH S1-538, NOW OPS NORMAL. RECONNECTED CABLE PER M/M 53-53-00-501 STEP 7 H-K.

Part: ENGINE — STALLED (NR 1) · airframe 31,999 hrs · 25,123 cycles

LT ENGINE COMPRESSOR STALL WHEN THROTTLES WERE ADVANCED FOR TAKEOFF ON RUNWAY AT EWR. INSPECTED INLET AND EXHAUST OF LT ENGINE WITH NO OBVIOUS DEFECTS. REPLACED LT ENGINE PRBC AND RAN ENGINE PER PFHB TEST E WITH NORMAL RESULTS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,485 hrs · 24,754 cycles

THREE CENTER AISLE EMERGENCY LIGHTS INOP IN F/C CABIN. REPLACED BATTERIES IN POWER SUPPLY B5-100. LIGHTS NOW OP NORMAL.

Part: WIRE — BROKEN (SEAT 31) · airframe 28,069 hrs · 22,176 cycles

SEAT 31DE E-PATH LIGHT INOP FOUND WIRES BROKEN TO LIGHT ASSY. REPAIRED WIRES BY SPLICING WIRES OPS CHK NML

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 26,938 hrs · 21,372 cycles

DURING CLIMB RIGHT HYD QTY DECREASED FROM 9 TO 4 QTS. PER POM RTB. GEAR FLAPS EXT NORMALLY W/RT SYS AT 3100 PSI AND 2 QTS. FOUND ENG HYD LINE BAD. REPLACED SAME, SERVICED AND BLEED HYD SYS, ALL CKS GOOD.

Part: VALVE — FAULTY (NR 2 ENGINE) · airframe 26,832 hrs · 21,301 cycles

AIR TURNBACK DUE TO HIGH ENG OIL PRESSURE ON NUMBER 2 ENGINE. OIL PRESSURE WAS BETWEEN 64 PSI AND 78 PSI WHILE PASSING THROUGH 23,000 FT. MASTER CAUTION LIGHTS AND ENG CUE LIGHT WERE ALSO FLICKERING BUT NO ENGINE MESSAGE. REPLACED OIL PRESSURE RELIEF VALVE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PRIOR TO DEPARTURE CREW FOUND F/C EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS POWER SUPPLY.

Part: BATTERY — DISCHARGED (CABIN)

FLASHLIGHT AT AFT F/A JUMP SEAT DID NOT FLASH. REPLACED BATTERY.

Part: HYD LINE — CHAFED (NR 2 ENGINE)

ON DEPARTURE, FELT VIBRATION FOLLOWED BY RT SYS HYD FAILURE. FOUND HYD PRESS LINE CHAFED NR 2 ENG PYLON. REPLACED LINE, INSPECTED AND REPLACED NR 2 ENG HYD PUMP FILTERS. RAN ENG PER PFHB, NO LEAKS FOUND. NR 2 ENG HYD PUMP CKS OK.

Part: THROTTLE CABLES — JAMMED (NR 2 ENGINE)

ON LEVEL OFF AT 5,000 FEET, THE NR 2 THROTTLE JAMMED. PUSHED BACK AND CONSIDERABLE FORCE WAS REQUIRED TO PUSH THE THROTTLE FORWARD AGAIN. FOUND RT ENGINE ANTI-ICE DUCT BLOWN AND ENGINE CONTROL CABLES DAMAGED. REPLACED DUCT AND CABLES AND REPAIRED DAMAGED COWL.

Part: SKIN — DENTED (BS 498-543)

DENT RUNNING FROM FS 498 TO 543 AT L20R WAS CUT OUT AND REPAIRED. REPAIRED PER ERA 265770-14, REV B.

Part: CROSSTIE RELAY — FAILED (E/E COMPT)

ON CLIMBOUT 18K, LOST BOTH SETS OF FLT INSTR/AUTO PILOT AND AUTO THROTTLES. PROCEDURE OPEN AC XTIE AND LAND C/W. REGAINED ELECT POWER. ISOLATED PROBLEM TO AC XTIE RELAY. ITEM WAS PLACED ON MCO PER MEL AC XTIE SWITCH OPEN.

Part: STRUT — REQD SERVICE (NLG)

AFTER T/O, NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR DOWN, ALL THREE GREEN, RAISED GEAR, MAINS UP AND LOCKED, NOSE GEAR UNSAFE RED. REPLACED RT NOSE GEAR SPRAY DEFLECTOR AND SERVICED NOSE GEAR STRUT. SWUNG NOSE GEAR, OPS CKS OK.

Part: STRUCTURE — DAMAGED (FUSELAGE)

A/C DAMAGED BY RAMP PERSONNEL RT SIDE 2 FT FWD OF WATER SERVICE PANEL 8 INCHES BELOW FLOOR LINE. REPAIRED PER SRM 53-04 PG 218A.

Part: SKIN — CRACKED (FWD FUS)

FOUND DURING D-2 LETTER CHECK, .125 INCH CRACK AT LT NLG DOOR HING CUTOUT IN FUSELAGE SKIN. REPAIRED PER SRM 53-05 FIG 2A.

Part: DOOR FRAME — CORROSION (C-1 CARGO COMP)

FOUND DURING D-2 LETTER CHEC, CORROSION AT C-1 DOOR FRAME LOWER RADIUS. REPAIRED PER SRM 53-05 FIG 63.