N981DL

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,708 hrs · 52,905 cycles

EMERGENCY LIGHT NOT COMING ON IN THE COCKPIT. REMOVED AND REPLACED BATTERY FOR THE FORWARD CEILING PANEL AND THE COCKPIT CEILING EMERGENCY LIGHT REF MD88 AMM 33-55. OPS CHECK GOOD. P/N AD-4002P. (LP5298878)

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,256 hrs · 52,510 cycles

ON SVC FOUND LT W/W DOOR JAMB CRACKED. STOP DRILLED ONE UNTERMINATED CRACK BRANCH AS PER ENGINEERING EVALUATION, EMAIL DATED 06 SEP 18. REPLACED LT FWD DOOR JAMB FRAME PER BAC DWG 5930584.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 70,759 hrs · 52,099 cycles

AISLE FLOOR PANEL SPONGY APPROX STA 285. RMVD DAMAGE FLOOR PANEL PER AMM 53-20. INSTALLED NEW DMFG PART ON WO 10981 PER AMM 53-20. CKS GOOD. A/C OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,625 hrs · 51,993 cycles

FWD EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FWD EMERGENCY LIGHT BATTERIES. OP CHECKED GOOD IAW AMM 33-53.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 69,636 hrs · 51,181 cycles

LOST PRESSURIZATION AT FL 310 BOTH AC PACKS IN AUTO. BOTH 1 AND 2 AUTO PRESSURE CONTROLLERS SHOWED "INOP" ANNUNCIATION. PERFORMED AUTO PRESS CONTROLLER BITE. FOUND BOTH CONTROLLERS FAULTED. RESET CONTROLLERS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PIN — LOOSE (EVAC SLIDE) · airframe 69,636 hrs · 51,181 cycles

FOUND L1 DOOR SLIDE ENGAGEMENT PIN LOOSE/OUT. R&R L1 DOOR SLIDE PER W/C 2561-4964.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 68,668 hrs · 50,424 cycles

SEAT 11D EMERGENCY LIGHT INOP. REPLACED AISLE EMERGENCY LIGHT SEAT HARNESS.

Part: SLIDE — DEFECTIVE (TAILCONE) · airframe 68,289 hrs · 50,133 cycles

TAIL SLIDE PACK UNRAVELING, WON'T FIT INTO PACK COVER. TAILCONE SLIDE ASSY REPLACED PER OPN 2561-4001 JOB 000- 0004. SLIDE OFF 88-2561-9-0003 00821.

Part: STRUT — CORRODED (NLG) · corrosion level 2 · airframe 68,289 hrs · 50,133 cycles

CORROSION AT LOWER END OF NLG PISTON. REPLACED CYLINDER IAW WORKCARD 3221-6192.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 67,846 hrs · 49,792 cycles

ENGINE ANTI-ICE USED TWICE. BOTH TIMES DURING USE, AN ODOR WAS NOTICED THROUGHOUT THE CABIN AND COCKPIT. OZONE TYPE ODOR. IT CEASED WHEN ENGINE ANTI-ICE WAS SELECTED OFF. INSPECTED RHT NR 1 & 2 ENGINE ANTI-ICE DUCTS. CHECKED OK. RAN ENGINES NO ODOR NOTED. CREW STATED NO SMOKE, JUST ODOR. VERIFIED NO APU CONTAMINATION. CLEANED THE MLG WW, BELLY, 48 SEC, & APU INLET. BORESCOPED LT AUG VALVE, LT PRV, LT CROSSFEED VALVE, LT FLOW CONTROL VALVE, & CENTER MANIFOLD FOR OIL, NO OIL CONTAMINATION FOUND FROM NR 1 ENG PREVIOUS HOC. PERFORMED BOTH ALT DUCT BURN & FULL DUCT BURN, NO SMOKE ODOR NOTED. REPLACED COALESCER BAGS. A/C OK FOR SERVICE. C/W ALL NO GO ODI PROCEDURES.

Part: FUSE — BLOWN (CABIN LIGHT) · airframe 67,355 hrs · 49,429 cycles

F/A ON AFT JUMPSEAT REPORTED HEARING 3 POPS AND SEEING ONE BRIGHT FLASH ON FINAL APPROACH, AFTER GEAR EXTENSION BUT BEFORE LANDING ALSO REPORTED AN ELECTRICAL ODOR THAT DISSIPATED AFTER LANDING. PERFORMED PNEUMATIC SYSTEM DUCT BURNOUT, NO DEFECTS NOTED. ENGINE PARAMETERS NORMAL. PERFORMED PNEUMATIC DIST. CABIN SMOKE/ODOR TROUBLESHOOTING AND FOUND BLOWN FUSE AT AFT LEFT LAVATORY MIRROR LIGHT AND REPLACED, OPS CHECKED GOOD. NO OTHER FAULTS FOUND.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,786 hrs · 49,017 cycles

AT LEFT AND RIGHT AFT OVERWING EXITS, UPPER EXIT SIGN LIGHTS INOP. REPLACED POWER SUPPLY B5-105 PER AMM 33-53.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,640 hrs · 48,903 cycles

CEILING EMERGENCY LIGHTS INOP BETWEEN ROW 21 AND 34. REPLACED BATTERIES IN EMERGENCY POWER PACK FOR LIGHTS AT ROW 21-34 CHECKS GOOD IAW AMM 33-53.

Part: ENGINE — FAILED (NR 1) · airframe 66,347 hrs · 48,667 cycles

RETURNED TO DEPARTURE WITH A REPORTED NR 1 ENGINE FAILURE. THE COMPRESSOR STALLED DURING CLIMB. THE CREW REPORTED THAT AFTER THE COMPRESSOR STALL, THE ENGINE PARAMETERS WERE NORMAL AT IDLE. THE AIRCRAFT RETURNED WITH THE NUMBER 1 ENGINE AT IDLE POWER. MAINTENANCE FOUND METAL IN THE TAIL PIPE WITH 4TH STAGE TURBINE DAMAGE. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP8454996)

Part: ENGINE — FAILED (NR 1) · airframe 66,232 hrs · 48,585 cycles

AT TAKEOFF ROTATION, THE LEFT ENGINE FAILED. REPLACED THE NR 1 ENGINE IAW SPC 88-7110-9-0010.

Part: SLEEVE — DISCONNECTED (THROTTLE CABLE) · airframe 65,645 hrs · 48,142 cycles

DURING TAXI OUT, ABOUT 2 MIN AFTER RT ENGINE START AND DURING T/O WARNING, CHECK RT ENGINE AUTO CANCELED TO MAX POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. EGT C664 HAD TO SHUTDOWN WITH FUEL LEVER. FOUND PUSH/PULL THROTTLE CABLE OUTER SLEEVE DISCONNECTED ON ENGINE SUPPORT BRACKET FIRING. THE ENGINE WAS REPLACED.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 65,399 hrs · 47,963 cycles

ON B-CHECK FOUND 12" CRACK IN PANEL 3703A. C/W SECTION I TIME LIMITED REPAIR IAW ERA 545854-14.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 64,814 hrs · 47,564 cycles

MAINTENANCE FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE PINS PULLED OUT. THE EMERGENCY ESCAPE SLIDE PACK WAS REPLACED AT DOOR L1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,402 hrs · 47,254 cycles

MAINTENANCE FOUND BOTH COCKPIT EMERGENCY LIGHTS INOPERATIVE. BATTERY PACKS WERE REPLACED.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 64,256 hrs · 47,160 cycles

RT WHEEL WELL FWD GEAR DOOR JAMB CRACKED. INSTALLED PERM REPAIR ERA 541708-14, REV ORIGINAL, OK FOR SERVICE.

Part: ACM — SMOKE (LEFT) · airframe 63,826 hrs · 46,826 cycles

ACFT IN MEM RUNNING A/C PACKS OFF OF START CART EXPERIENCED SMOKE HAZE IN CABIN WITH ODOR. TURNED OFF LEFT PACK. SMOKE CLEARED A BIT BUT WAS STILL PRESENT. DISCOVERED RT ACM OVERSERVICED. DRAINED AND SERVICED RT ACM TO PROPER LEVEL IAW AMM 12-12. R & R RT ACM IAW AMM 21-58. OPS, LEAK CHECK GOOD.

Part: SKIN — CRACKED (BS 372-374) · airframe 63,300 hrs · 46,457 cycles

FOUR CRACKS ON FUSELAGE SKIN OF 0.125", 0.062", 0.156", AND 0.281" OF LENGTH LOCATED BETWEEN BS Y=372 TO Y=374 AND LONG 20RT-21RT AT FWD CARGO DOOR JAMB UPPER CORNER. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 105 OM FUSELAGE SKIN, AND ER/A 536461-14AD, REV ORIGINAL, MAJOR REPAIR.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON 14R BS 1380. LONGERON REPAIRED IAW ER/A 536440-14, REV ORIGINAL.

Part: LONGERON — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

DURING MAINTENANCE ACTIVITIES, FOUND CORROSION OUT OF LIMITS ON LONGERON 22 LT FROM STA Y=1155 TO STA Y =1174 IN REF CARD 156, ZONE 100, CARD 269, ZONE 100.02. RII: Y ENTR 008590 W SUMMARY: SECTION LONG 22 LT FROM STA Y=1155 TO STA Y=1174 WAS R & R IAW SRM 51-30-2 AND 51-30-5. SPLICE TO LONGERON 22 LT WAS FABRICATED IAW SRM 53-02, PAR 12, FIG 18 AND WAS INSTALLED IAW SRM 51-30-5.

Part: ANGLE — CRACKED (BS 1380 FRAME) · airframe 63,300 hrs · 46,457 cycles

CRACKED FRAME ANGLE BS 1380 BETWEEN LONGERON 15-16R . FRAME ANGLE WAS REMOVED AND FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-14-4 AND 51-10-3, PAR 14 AND 21.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 63,300 hrs · 46,457 cycles

BROKEN STRANDS ON TAIL CONE RELEASE CABLE. RELEASE CABLE WAS REPLACED.

Part: BEAM — CORRODED (BS 1200-1212) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON AFT CARGO COMPARTMENT UPPER BEAM FROM BS 1200 - 1212. BEAM WAS REPLACED IAW SRM 51-30-5. . .

Part: SKIN — CRACKED (BS 1406) · airframe 63,300 hrs · 46,457 cycles

CRACKED FUSELAGE SKIN UNDER REMOVED DOUBLER AT AFT ACCESSORY COMPARTMENT, BS 1406 BETWEEN LONGERONS 1-2R. DAMAGE WAS REPAIRED WITH ER/A 534412-14AD, REV ORIG.

Part: DOUBLER — CORRODED (BS 579) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON PRODUCTION DOUBLER BS 579 BETWEEN LONGERON 28 - 29L. AREA WAS REPAIRED IAW ER/A 536442-14, REV ORIGINAL.

Part: TAB — DENTED (LT ELEVATOR) · airframe 63,300 hrs · 46,457 cycles

DENT ON LT ELEVATOR ANTI-FLOAT TAB. LT ELEVATOR ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-04, PAR 2.

Part: SKIN — CRACKED (BS 1463) · airframe 63,300 hrs · 46,457 cycles

CRACKED INNER FUSELAGE SKIN JUST FWD OF CANTED FRAME, STA 1463 AND PROYECTION LONG 2R AT AFT ACCESSORY COMPARTMENT, RII: N ENTR 797732 W, SKIN DAMAGE WAS REPAIRED IAW ER/A 536423-14, REV ORIGINAL PERFORM A GENERAL VISUAL INSPECTION OF THE REPAIR WITHIN EVERY 3,000 CYCLES IAW ER/A 536423-14, REV ORIGINAL SEC II AND LOG PAGE 2008291. THIS INSPECTION WILL BE MONITORED WITH LOG PAGE 2008291.

Part: SKIN — DAMAGED (BS 636-655) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKES ON RT WINDOW BELT BETWEEN BS 636-655 FWD EDGE AND AFT UPPER CORNER. THE WINDOW BELT WAS REPAIRED IAW ER/A 536435-14, REV ORIGINAL.

Part: SKIN — SCRATCHED (BS 750-769) · airframe 63,300 hrs · 46,457 cycles

SCRATCHES ON RT WINDOW BELT, BS 750-769, LWR EDGE. REPAIRED.

Part: HOUSING — WORN (DOOR HANDLE) · airframe 63,300 hrs · 46,457 cycles

MID-CARGO DOOR HANDLE HOUSING WORN. DAMAGED HOUSING WAS REPLACED IAW SRM 51-30-2.

Part: SUPPORT FITTING — DAMAGED (RT MLG) · airframe 63,300 hrs · 46,457 cycles

SCRATCH ON RT MLG SUPPORT FITTING BORE IN REF CARD 12, ZONE 18, CARD 14, ZONE 018. DAMAGE ON BEARING BORE WAS REPAIRED IAW ETI-88-15-182, REV ORIGINAL AND ER/A 474111-14AD REV A.

Part: SUPPORT FITTING — CORRODED (MLG) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON MLG SUPPORT FITTING BUSHING BORE. DAMAGE WAS REPAIRED IAW DWG SR 09570087, REV BB AND ETI-88-15-182, REV ORIGINAL AND ER/A 474111-14AD, REV A.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LONGERON 19R BETWEEN FRAME Y=1287 AND Y=1309 AT AFT CARGO COMPARTMENT. FASTENER WAS REMOVED, CORROSION SECTION LONGERON DAMAGE WERE REMOVED. NEW SECTION LONGERON WAS DRILLED, TREATED, PAINTED, INSTALLED SPLICES. REPAIRS WERE DRILLED, ADJUSTED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3. PAG 14, 21, 51-30-2, 51-30-5, 53-02, FIG 18.

Part: KEELBEAM — CRACKED (RT MLG WW) · airframe 63,300 hrs · 46,457 cycles

CRACKED ANGLE BELOW KEEL BEAM AT RT MLG W/W AFT INBD CORNER. ANGLE BELOW KEEL BEAM AT RT MLG W/W AFT INBD CORNER WAS REPAIRED IAW ER/A 413026-14 MA, REV ORIGINAL CRACK .125.

Part: SKIN — DAMAGED (BS 731-750) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKES ON RT WINDOW BELT STA Y=731-750, AFT UPPER CORNER. RT WINDOW BELT STA Y= 731-750 WAS REPAIRED IAW ETI-88-15-192, REV 1 AND ER/A 536436-14AD, REV ORIGINAL PERFORM HFEC INSPECTION EVERY 24 MONTHS IAW ERA 536436-14AD. RII COMPLETED.

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

DURING MAINTENANCE ACTIVITIES WAS FOUND, CORROSION OUT OF LIMITS BS 1307 BETWEEN LONGERON 26LT AND 30 AT AFT CARGO COMPARTMENT IN REF CARD 248, ZONE 100, CARD 273, ZONE 100. FRAME WAS REPAIRED IAW SRM 53-03D, FIGURE 2A.

Part: INTERCOSTAL — CRACKED (BS 1287-1307) · airframe 63,300 hrs · 46,457 cycles

CRACKED INTERCOSTAL X=0 BETWEEN STA Y=1307 TO Y=1287 ALSO X=3 BETWEEN STA Y=1287 TO Y=1279 AT FLOOR STRUCTURE CABIN. SM, W2, CARD 301, ZONE 201. INTERCOSTAL WERE REMOVED IAW SRM 51-30-2, 51-30-5, NEW INTERCOSTAL STA: Y=1287-1307 WAS DRILLED IAW SRM 51-10-4. INTERCOSTAL STA= Y= 1287-1387 WAS DRILLED IAW SRM 51-10-4. INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21, 14. NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2. OUTFLOW VALVE CONTROL CABLE BRACKET WAS REMOVED IAW AMM 20-30-01-201. INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5. DIMENSION CRACK STA Y= 1271-1307 IS 0.750 DIMENSION CRACK STA Y= 1271-1237 IS 1.500.

Part: LONGERON — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

DURING MAINTENANCE ACTIVITIES, FOUND CORROSION OUT OF LIMITS ON LONGERON 22 LT FROM STA Y=1155 TO STA Y =1174 IN REF. CARD156, ZONE 100. CARD 269, ZONE 100. SECTION LONG 22 LT FROM STA Y=1155 TO STA Y=1174 WAS R & R IAW SRM 51-30-2 AND 51-30-5. SPLICE TO LONGERON 22LT WAS FABRICATED IAW SRM 53-02, PAR 12, FIG 18 AND WAS INSTALLED IAW SRM 51-30-5. PERFORM DECAL VISUAL INSPECTION EVERY C-CHECK IAW TOPP 30-10-70, PAGE 13, PAR. I. RII COMPLETED BY INSPECTION.

Part: SKIN — DAMAGED (BS 655-674) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKES ON RT WINDOW BELT BETWEEN STA Y= 655-674 FWD WAS REPAIRED ON UPPER CORNER: WITH DIMENTIONS AS FOLLOWS (UT) WAS ACCOMPLISHED IAW NDT-SPM PART 4, 04-00-078 PAR 5 FIG 3, STA Y=655-674 RT, PLACE FWD UPPER CORNER, ORIGINAL THICKNESS 0.120, REMAINING THICKNESS 0.118. THESE ARE IN ZONE 1 AND CRITICAL. STA Y=655-674 RT, PLACE UPPER EDGE, ORIGINAL THICKNESS 0.110, REMAINING THICKNESS 0.104, ZONE THEREFORE THESE ARE WITHIN LIMITS IAW SRM 53-05, FIG 111 AND ER/A 536452-14, REV.

Part: CARGO TRACK — DAMAGED (BS 218-332) · airframe 63,300 hrs · 46,457 cycles

ELONGATED HOLE ON CARGO TRACK BETWEEN LONGERON 28 AND 27 BS 218-332. THE CARGO TRACKS WERE REPAIRED IAW SRM 51-1014/21/38, 51-30-1, 51-30-2 AND 51-30-5 AND ER/A NR 529371-14MA, REV. ORIGINAL.

Part: CHANNEL — CRACKED (CABIN) · airframe 63,300 hrs · 46,457 cycles

CRACKED CHANNEL ON FLOOR PANEL NR 886C AND 886D. CHANNELS WERE REPLACED ON FLOOR PANELS 886C AND 826D IAW DWG 9936639, REV P.

Part: STIFFENER — CRACKED (AFT PRESS BLKHD) · airframe 63,300 hrs · 46,457 cycles

CRACK ON STIFFENER OF AFT PRESSURE BULKHEAD AT 12HRS POSITION. STIFFENER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 21 AND 14 AND DWG 9915562, REV "P". DIMENTION CRACK IS 0.750".

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON MID CARGO DOOR TEES AT STA Y=655 AND 674 BTW LWR EDGE AND BEAM 1 ALSO CORROSION ON ANGLE BESIDE TEE STA Y=674. TEES WERE REPLACED IAW SRM 51-30-2 AND 51-30-1.

Part: SKIN — DAMAGED (BS 408-427) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKE ON LT FUSELAGE WINDOW BELT AFT EDGE BETWEEN BS Y=408 TO Y=427. LIGHTNING STRIKE ON LT FUSELAGE WINDOW BELT AFT EDGE BETWEEN BS Y=408 TO Y=427 WERE REPAIRED IAW ERA 536438-14, REV. ORIGINAL. ORIGINAL THICKNESS 0.086". REMAINING THICKNESS 0.094" ON AFT LWR CORNER AND ORIGINAL THICKNESS 0.094" AND REMAINING THICKNESS 0.087" ON FWD UPPER CORNER ON CRITICAL ZONE, SRM 53-05, FIG 111 ON NO CRITICAL ZONE. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK. RII COMPLETED.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON 4L BS 1437. THE LONGERON WAS REMOVED, LONGERON FABRICATED AND DRILLED, SPLICE LONGERON WAS TREATED AND PAINTED AND INSTALLED IAW SRM 53-02, FIG 18, 51-10-3 PAR 14 AND 21 AND 51-30-5. CLASSIFIED AS MAJOR REPAIR.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 63,300 hrs · 46,457 cycles

PUNCTURE ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: TEE FITTING — CRACKED (BS 1174-1193) · airframe 63,300 hrs · 46,457 cycles

CRACKED AFT CARGO DOOR INBD TEE BS 1174 ALSO INBD AND OTBD TEE BS 1193 BETWEEN BEAM 5 AND UPPER EDGE. REMOVED AND REPLACED IAW SRM 51-30-2, AND SRM 51-30-2.

Part: FRAME — CRACKED (BS 1510) · airframe 63,300 hrs · 46,457 cycles

CRACKED CANTED FRAME BS 1510 BETWEEN 10-2 O'CLOCK POSITION. FRAME WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PARR 21, 14, AND DWG 9911843 REV AC.

Part: SKIN — DAMAGED (BS 560-598) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKE ON FUSELAGE WINDOW BELT AFT UPPER CORNER BETWEEN BS Y=560 TO Y=579 AND STA Y=579 TO Y=598. LIGHTNING STIKE ON FUSELAGE WINDOW BELT AFT UPPER CORNER BS Y= 579 TO Y=598 IN REF. CARD 19, ZONE 100 WERE REPAIRED IAW ER/A 536451-14, REV ORIGINAL, WITH DIMENSIONS: ORIGINAL THICKNESS 0.11"/0.86" REMAINING THICKNESS 0.110"/0.080" UPPER CORNER, AND ON FWD UPPER CORNER ER/A 536450-14, REV ORIGINAL THICKNESS 0.105" REMAINING 0.098" TIME LIMITED. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK. RII COMPLETED.

Part: SKIN — CRACKED (LT WING) · airframe 63,300 hrs · 46,457 cycles

CRACKED SKIN AND BRACKET OF LT SLAT TRACK DOOR NR 7 AT LT WING. SLAT TRACK DOOR WERE BONDED IAW DWG 512356-14.

Part: FRAME — CRACKED (BS 1307) · airframe 63,300 hrs · 46,457 cycles

CRACKED FRAME BS 1307 AT INTERSECTION WITH LONGERON 1 AT PAX CABIN. FRAME WAS REPAIRED IAW ER/A 536426-14 REV ORIG CRACK LENGTH: .675".

Part: SUPPORT ANGLE — CRACKED (BS 1380) · airframe 63,300 hrs · 46,457 cycles

CRACKED FRAME ANGLE BS 1380 BETWEEN LONGERONS 15-16L . SUPPORT FRAME ANGLE WERE REMOVED, TREATED, PAINTED AND INSTALLED NEW SECTION WAS FABRICATED FRAME IAW SRM 51-30-5, 51-30-2, 51-30-3, 51,10-3 PAR 21,14.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON BARREL NUT HOLE NR 14 BS XH=7 AT HORIZONTAL STABILIZER. DAMAGE ON BARREL NUT HOLE NR 14 WAS REPAIRED IAW ETI 88-15-177, REV 1 AND ER/A 536424-14 REV ORIG FINAL DIAMETER OF REWORK 0.778.

Part: STOP FITTING — WORN (TAILCONE) · airframe 63,300 hrs · 46,457 cycles

WEAR AND ELONGATE STOP PADS AROUND TAILCONE FRAME. PADS WERE REMOVED AND REPLACED IAW SRM 51-30- 2.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,300 hrs · 46,457 cycles

DELAMINATED FLOOR PANEL. A NEW FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: INTERCOSTAL — WORN (BS 1322-1338) · airframe 63,300 hrs · 46,457 cycles

WORN INTERCOSTAL BS 1322-1338 BETWEEN LONGERONS 21- 22L . INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CORRODED (BS 1338) · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LONGERON 22L BS 1338. REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON NR 16R AT AFT ACCY COMPARTMENT BS 1437. SM, ZONE 61. LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND 53-14-4, FIG 4, LONG CRACK .800".

Part: LONGERON — CRACKED (BS 1437) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON 3R BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LONGERON 22L BS 1287 - 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. MAJOR REPAIR.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 63,300 hrs · 46,457 cycles

WORN REPAIR DOUBLER ON RT WING INBD FLAP INBD VANE. INBD FLAP INBRD VANE WAS REPAIRED.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,300 hrs · 46,457 cycles

MISSING AND DAMAGED FERRULE IN FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-0-201.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON 16L BS 1437. THE LONGERON WAS REPLACED IAW SRM 51-30-2 & SRM 51-30-5 & SRM 53-14-4 FIG 4.

Part: SPAR — DAMAGED (HORIZONTAL STAB) · airframe 63,300 hrs · 46,457 cycles

ELONGATED HOLE ON UPPER REAR SPAR AT RT HORIZONTAL STABILIZER BS XHR=209, HINGE 6, VHS, SM, CARD 6, ZONE 034. DAMAGE ON HOLE, UPPER REAR SPAR WAS REPAIRED IAW ETI-88-15-190 REV ORIG AND ER/A 536434-14.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,300 hrs · 46,457 cycles

CRACK ON LONGERON END 17R, BS 1338 AT FUSELAGE CABIN STRUCTURE. LONGERON END REPLACED IAW SRM 53-14-3, 51-30-5.

Part: FRAME — CRACKED (BS 1451) · airframe 63,300 hrs · 46,457 cycles

CRACKED FRAME BS 1451 LONGERON 1. REMOVED AND REPLACED THE FRAME IAW SRM 51-30-2, 51-30-5, SRM 51-10-4 , SRM 51-10-3 PAR. 21-14, AND SRM 51-30-2, 51-30-5.

Part: LONGERON — CORRODED (BS 1338) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON TEE CAP BS 1338, PROJECTION LONGERON 28LT AT AFT CARGO COMPARTMENT, C3, SM, IN REF CARD 2, ZONE 57, MRB 53-139-05, CARD 11 ZONE 57. TEE CAP WAS FOUND WITH EXCESSIVE CORROSION THEREFORE TEE CAP STA Y=1338 WAS PREPARED IAW SRM 53-03, FIG 37 AND EXTERNAL SKIN, PN 5911429-151 WAS CUT OUT AND REPAIRED IAW ER/A 512884-14MA REV. ORIGINAL MAJOR REPAIR.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON 13L AT AFT ACCESSORY COMPARTMENT BS 1380. THE LONGERON WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND 53-14-4, ITEM 4.

Part: DOUBLER — CORRODED (BULKHEAD) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON AFT PRESSURE BULKHEAD PRODUCTION DOUBLER BETWEEN LONGERON 29 RT TO 29 LT AT AFT CARGO COMPARTMENT, C3, SM, MRB 53-139-05, CARD 3, ZONE 57. PRODUCTION DOUBLER WAS FOUND WITH EXTENSIVE CORROSION THEREFORE AFT PRESSURE BULKHEAD PRODUCTION DOUBLER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 AND D, DWG 5910130, REV EG PRIMARY STRUCTURE.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RIB HOLES STA XOS=332 AT RT WING SLAT PANEL NR 3, RW,SH-CP-SM, CARD 5, ZONE 12. DAMAGE ON RIB HOLES STA XOS= 332 WAS REPAIRED. IT WAS IN AFT HOLES WITH FINAL DIMENTIONS: 1D= 0.938", THEREFORE WITHIN LIMITS IAW SRM 57-02, PAR 9 AND REPAIR BUSHINGS WERE FABRICATED AND INSTALLED AND DAMAGE ON FWD HOLES WAS REPAIRED WITH FINAL DIMENTIONS: 1D= 0.944", OUT OF LIMITS.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE . DAMAGE ON BUSHING BORE WAS REPAIRED WITH FINAL DIAMETER: 2.2885" THEREFORE WITHIN LIMITS IAW DWG SR09570087, REV BB.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,300 hrs · 46,457 cycles

CRACKED INNER PAN AT AFT CARGO DOOR AFT END AND BEAM NR 5. CRACK ON INNER PAN WAS STOPPED IAW SRM 51-01. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AROUND STOP DRILL 51-01 (21) NEW DOUBLER WAS FABRICATED AND PAINTED IAW SRM 51-03D, FIG. 8 AND 51-10-3 PAR 14. NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-03D, FIG 8 LONG CRACK 1.5".

Part: LONGERON — BENT (BS 256) · airframe 63,300 hrs · 46,457 cycles

BENT LONGERON 17L BS 256. REMOVED AND REPLACED THE LONGERON SECTION IAW SRM 53-02, FIG 18.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 63,300 hrs · 46,457 cycles

CRACK ON UPPER OF AFT PRESSURE BULKHEAD STIFFENER 4 AND STA X=60. ANGLE WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4.

Part: SEAT TRACK — CORRODED (BS 1116-1121) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LT SEAT TRACK X=44 BETWEEN BS 1116-1121. DUE TO EXCESSIVE DAMAGE ORIG 0.100", MIN IS 0.040", SECTION SEAT TRACK WAS REPLACED IAW 51-30-1, 51-30-2, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21, SRM 53-05, FIG 4F.

Part: ANGLE — CRACKED (BS 237) · airframe 63,300 hrs · 46,457 cycles

CRACKED ANGLES ON BS 237 BETWEEN LONGERON 27-28L AND 27-28R AT FWD CARGO COMPARTMENT. ANGLES WERE REPLACED IAW SRM 51-30-2, DWG 9915554, REV U, SRM 51-10-3 AND 51-30-5.

Part: DOUBLER — WORN (LAV SERVICE PANE) · airframe 63,300 hrs · 46,457 cycles

WEAR ON AFT ACCESSORY TITANIUM DOUBLER AT AFT LAVATORY SERVICE PANEL AREA. DOUBLER WAS REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-30-5 AND DWG 5911423, REV CD.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON BARREL NUT HOLES NR 10, 15 BS XH=27.34 AT LT HORIZONTAL STABILIZER. BARREL NUT HOLES NR 10, IS WERE ACCOMPLISHED IAW ERA 536433-14, REV ORIG. RII COMPLETED.

Part: LONGERON SPLICE — CORRODED (BS 1196-1209) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LONGERON SPLICE NR 29L BETWEEN BS 1196-1209 . LONGERON SPLICE R & R IAW SRM 51-30-5.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 63,300 hrs · 46,457 cycles

CRACKED FWD CARGO DOOR SKIN AT AFT UPPER EDGE OF HANDLE CUT OUT. CRACKS WERE REMOVED IAW ER/A 486446-14MA, REV ORIGINAL, HFEC WAS PERFORMED IAW ER/A 486446-14, MA REV ORIGINAL.

Part: DOOR FRAME — CRACKED (FWD CARGO DOOR) · airframe 63,300 hrs · 46,457 cycles

CRACKED INNER PANEL AT FWD CARGO DOOR AFT END AND BEAM NR 4. DAMAGES MEASURED WITHIN LIMITS IAW SRM 52-03D, FIG 10. TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, STOP FITTING NR 4 SEAL AND RETAINER WERE INSTALLED IAW SRM 51-10-3.

Part: CUSP WEB — CORRODED (BS 1198-1212) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION FOUND ON THE LEFT CUSP WEB X 56 - 60 BETWEEN BS 1198 - 1212. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A -G.

Part: CUSP WEB — CORRODED (BS 631-693) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION FOUND ON THE RIGHT CUSP WEB BETWEEN X 54 TO X 60 AND BS 631, 636, 638, 648, 655, 657, 674 AND 693. THE CUSP WEB WAS REPLACED IAW DWG 9930538, REV 13F, SRM 51-30-2,51-30-5,51-30-1 AND 51-30-8.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON BARREL NUT HOLES NR 8, 10, 14, 16, 20, 21, 24 AND 25 AT RT HORIZONTAL STABILIZER. BARREL NUT HOLES NR 8, 10, 21, 24 AND 25 RT WERE ACCOMPLISHED IAW ERA 536425-14, REV, ORIGINAL BARREL NUT HOLES NR 16, 20 RT WERE ACCOMPLISHED IAW ERA 536433-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1485) · airframe 63,300 hrs · 46,457 cycles

A CRACKED FRAME WAS FOUND AT BS 1485 JUST BELOW VENTRAL STAIR HYD ACTUATOR AT AFT ACCESSORY BAY. THE FRAME WAS REPAIRED IAW SRM 53-03, FIG 43.

Part: CUSP WEB — CORRODED (BS 846-906) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION FOUND ON LEFT CUSP WEB X=47 TO X=51 BS 846, 885, AND 906. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1

Part: CUSP WEB — CORRODED (BS 1003-1079) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RT CUSP WEB BETWEEN BS X=-54 TO -60 AND Y=1003 TO 1022, 1022 TO 1041, 1041 TO 1060, 1060 TO 1079. CUSP WEB WERE REMOVED AND FABRICATED IAW SRM 51-30-2, 51-10-4, 53-14-3, 51-10-3, PAR 26. REPAIR PARTS AND CUSP WEB WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. REPAIR INSTALLED ON CUSP WEB IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 684-750) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION FOUND ON LEFT CUSP WEB BETWEEN X=54 - 60 AND BS 684 - 693, 693, 712, 731 AND 750. THE CUSP WEB WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-30-1, SRM 51-10-3, SRM PAR 14-21 AND DWG 9930538, REV BF.

Part: SKIN — DAMAGED (BS 546.25) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKE ON SKIN BS 546.25 AND LONGERON 10L. REPAIRED IAW SRM 53-04-2, FIG 2.

Part: CUSP WEB — CRACKED (BS 500) · airframe 63,300 hrs · 46,457 cycles

CRACKED RT CUSP WEB BS 500 BETWEEN X-54 TO X-60. HFEC INSPECTION ACCOMPLISHED, TWO CRACKS OF 0.250" AND 0.370" WERE FOUND IAW NDT SRM 06-10-01.001. A REPAIR WAS FABRICATED IAW SRM 53-05 FIG. 131A-10. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-10. AREA AND REPAIR WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21 DOUBLERS REPAIR INSTALLED IAW 51-30-5, & 51-30-1.

Part: SKIN — CRACKED (PAX DOOR) · airframe 63,300 hrs · 46,457 cycles

A CRACK WAS FOUND ON FWD ENTRY DOOR SKIN NEXT TO HANDLE HOUSING RUBSTRIP. THE FWD ENTRY DOOR SKIN WAS REPAIRED IAW ER/A 501106-14, REV B.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 63,300 hrs · 46,457 cycles

CRACK ON LOWER ANGLE OF AFT PRESSURE BULKHEAD STIFFENER X-54 AND Z 62. THE ANGLE WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 21 - 14, AND DWG 9915558, REV BA.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION FOUND ON LT WING SLAT PANEL RIB HOLES XOS=580. THE RIB WAS REMOVED IAW SRM 51-30-2 AND 51-30-8. A NEW RIB WAS DRILLED IAW SRM 51-10-4, TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21 AND INSTALLED IAW SRM 51-30-2 AND 51-30-8.

Part: DOUBLER — CORRODED (BS 760-778) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON OTBD FUSELAGE SKIN BETWEEN BS 760 - 778 AND LONGERON 27 - 28 RT. DOUBLER WAS REPLACED IAW ER/A 331081-14, REV A AND SRM 51-30-2 AND 51-30-5.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,300 hrs · 46,457 cycles

CRACKED INNER SKIN ON RT WING SLAT XOS=240.081. CRACK WAS FOUND .312 IN LENGTH IAW NDT SPM 06-10-01.001. DOUBLER REPAIR AND FILLER WERE FABRICATED IAW SRM 57-01,FIG 5, SHEET 2. REPAIR TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. REPAIR INSTALLED IAW SRM 51-30-8.

Part: SKIN — DAMAGED (BS 607) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 607.437 LONGERON 9L. AREA OUT LIMITS AND WAS REPAIRED IAW SRM 53-04-2, FIG 2, SH 3.

Part: SKIN — DAMAGED (BS 562) · airframe 63,300 hrs · 46,457 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 562.375 AND LONGERON 10 LT. THE SKIN WAS REPAIRED IAW SRM 53-04-2, FIG 2. DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3. DOUBLER WAS INSTALLED IAW SRM 53-04-2, FIG 2.

Part: FRAME — CRACKED (BS 1437) · airframe 63,300 hrs · 46,457 cycles

CRACKED FRAME ANGLE BS 1437 BETWEEN LONGERON 12-13R IN AFT ACCESSORY COMPTARTMENT. FRAME CLIP WAS FABRICATED IAW SRM 53-14-4 FIG 3, SHEET 4 AND INSTALLED IAW SRM 51-30-2.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,300 hrs · 46,457 cycles

DAMAGE METALIZED COAT ON SKIN PANEL LT/RT SIDE AT RUDDER VERTICAL STABILIZER. METALIZED COAT ON SKIN PANEL LT/RT SIDE AT RUDDER VERTICAL STABILIZER WERE REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: CUSP WEB — CORRODED (BS 1117-1212) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 TO -60 AND BS 1098 - 1117, 1136 - 1155, 1155 - 1174, 1174 - 1193, 1193 - 1212 AT PAX CABIN FLOOR STRUCTURE. CUSP WEB REMOVED IAW SRM 51-30-2, 51-30-5. A NEW CUSP WEB WAS DRILLED IAW SRM 51-10-4 & DWG 9930612, REV, THE NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2, 5130-5.

Part: DOUBLER — CORRODED (BS 803-814) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON PREVIOUS REPAIR ON OTBD FUSELAGE SKIN BETWEEN BS 803 - 814 BETWEEN LONGERON 28 - 30 RT. PREVIOUS REPAIR WAS REPLACED IAW ER/A 331097-14, REV A.

Part: SKIN — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RIB HOLES AT RT WING SLAT PANEL NR 5 STA XOS=580, RW, SH-CP-SM, CARD 2 ZONE 012. SKIN AND STRUCTURE, NEW RIB WAS DRILLED, TREATED AND PAINTED, INSTALLED AND SKIN AND STRUCTURE WERE INSTALLED AND REMOVED IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 14/21 AND 51-30-8.

Part: DOUBLER — CORRODED (BS 781-797) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON OTBD FUSELAGE SKIN BETWEEN BS 781 - 797 AND LONGERONS 28 - 29R. DOUBLER WAS REPLACED IAW ER/A 331081-14, REV A.

Part: DOOR FRAME — CRACKED (FWD CARGO) · airframe 63,300 hrs · 46,457 cycles

CRACKED FWD CARGO DOOR OUTER PANE UNDER ANGLE GUIDE. BETWEEN BEAMS NR 1 AND 2. IN REF ORNRC 113, ZONE 100, CARD 259, ZONE 100. CRACK ON OUTER PAN WAS STOP DRILLED AND REPAIRED IAW SRM 52-05D, FIG 26A.

Part: VANE — DAMAGED (NR 1 TE FLAP) · airframe 63,300 hrs · 46,457 cycles

SEVERAL NICKS ON PREVIOUS REPAIR DOUBLER AT NR 1 FLAP VANE. THE PREVIOUS DOUBLER WAS REPLACED IAW SRM 57-03D, PAR 11.

Part: LONGERON — CORRODED (BS 1287-1297) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LONGERON 20L BETWEEN BS 1287 TO 1297. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND 53-14-3.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON FRAME CAP BS 1380 BETWEEN LONGERONS 24L-24R. THE FRAME TEE WAS REPLACED IAW SRM 51-30-2, 51-30-5, 53-14-4.

Part: PANEL — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RIB HOLES XOS= 610 AT LT WING SLAT PANEL NR 5. CORROSION ON RIB HOLES STA XOS= 610 AT LT WING SLAT PANEL NR 5 WAS REMOVED, REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR 9.

Part: CUSP WEB — CRACKED (BS 1244-1250) · airframe 63,300 hrs · 46,457 cycles

CRACK ON RT CUSP WEB BETWEEN BS 1244 TO 1250, X=-56 TO X=-60. CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON NR 13R IN AFT ACCESSORY COMPARTMENT BS 1380. THE LONGERON WAS REPLACED IAW SRM 53-14-14, FIG 2, ITEM 4 AND 51-30-2, 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1365C COUNTERSINK HOLES AND SETTLEMENT AREA. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED, MAX DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND SEVEN COUNTERSINKS OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A COND II.

Part: LONGERON — CORRODED (BS 1332) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LONGERON 30, BS 1332. REPLACED THE LONGERON IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, AND SRM 51-10-3 PARA 14 & 21.

Part: LONGERON — CRACKED (BS 1309) · airframe 63,300 hrs · 46,457 cycles

CRACK ON LONGERON 8R AT BS 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, REPAIR PARTS WERE FABRICATED IAW SRM 53-02, FIG 18, REPAIR TREATED AND PAINTED IAW SRM 51-10-3, PARAGRAPHS 14, 21, REPAIR INSTALLED IAW SRM 53-02, FIG 18.

Part: RIB — CORRODED (LT WING LE SLAT) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RIB HOLE, STA XIS=136 AT LT WING SLAT PANEL 1. CORROSION ON RIB HOLE STA 136 WAS REMOVED, WAS FABRICATED BUSING AND INSTALLED IAW SRM 57-02, PAR. 9C, 1, 2.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1357C COUNTERSINK HOLES AND SETTLEMENT AREA. CORROSION WAS REMOVED, COUTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS .532" AND WERE FOUND 3 COUTERSINKS ADJACENTS OUT OF LIMITS, THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PLATE 1307C COUNTERSINK HOLES. REPLACED THE ACCESS PANEL.

Part: FLOORBEAM — CORRODED (BS 1338) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON FLOORBEAM BS 1338 X -20. THE FLOORBEAM WAS REPAIRED IAW SRM 53- 05 FIG. 20A, 51-30-1, 51-30-5, AND 51-10-3 PAR. 21, 14, AND 38.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,300 hrs · 46,457 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PLATE 1335C COUNTERSINK HOLES. REPLACED THE ACCESS PANEL 1335C.

Part: SEAT TRACK — CORRODED (BS 307) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON SEAT TRACK PLUG REPAIR X-54 AND BS 307 . PLUG WAS REPLACED IAW SRM 53-05, FIG 4, 51-30-1, 51-10-3, PAR, 38.

Part: ANGLE — CORRODED (BS 693) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON ANGLES OF FRAME BS 693 BETWEEN LONGERON 28 - 30L. THE ANGLES WERE REPAIRED IAW SRM 51-30-02, 51-30-05, 51-10-03 PAR 14, 21, 38 AND 51-10-02, 53-03 D FIG 3.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 63,300 hrs · 46,457 cycles

INITIAL CRACK ON SEAL PAN IN CUT OUT THE LOWER HINGE AT FWD SERVICE DOOR. REPAIR WAS ACCOMPLISHED IAW SRM 52-03D, FIG 3, 51-10-3 PAR 14/21, 51-30-4.

Part: CUSP WEB — CORRODED (BS 1079-1089) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RT CUSP WEB BS 1079-1089 BETWEEN X=56 - X=60. FASTENERS WERE REMOVED, FITTING BS 1097 LT WAS REMOVED, DAMAGE WAS REMOVED, NEW REPAIRS PARTS WERE FABRICATED, REPAIR PARTS WERE TREATED AND PAINTED, REPAIRS PARTS ANGLE AND FITTING WERE INSTALLED, AND CIC WAS APPLIED IAW SRM 51-30-5, 51-30-1, 53-05, FIG 131A, 51-10-3, PAR 14 AND 21, 51-30-2 AND 51-10-3, PAR 38.

Part: BEAM — CRACKED (BS 187) · airframe 63,300 hrs · 46,457 cycles

CRACK ON INTERNAL BETWEEN BEAMS 4 AND 5 AND BS 187 IN FWD ENTRY L1 DOOR. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — CRACKED (BS 200-206) · airframe 63,300 hrs · 46,457 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON FUSELAGE SKIN BETWEEN BS 200 TO 206.5 AND BETWEEN LONGERONS 18 TO 26 RT.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 63,300 hrs · 46,457 cycles

LIGNTNING STRIKE ON LT ELEVATOR PLATE NEXT TO TIP. TIP END WAS REPLACED IAW SRM 51-10-2, 51-10-3, PAR 21, 14, 51-30-2, 51-30-8, AND 51-30-1.

Part: CUSP WEB — CORRODED (BS 835-841) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON PREVIOUS DOUBLER REPAIR X=55 TO X=60 BS 835-841. DUE TO EXCESSIVE CORROSION, PREVIOUS REPAIR WAS REMOVED IAW SRM 51-30-2 AND 51-30-5 AND NEW CUSP WEB WAS FABRICATED IAW SRM 53-05, FIG 131A AND NEW DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: RIB — DAMAGED (TE FLAP) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION AND SCRATCHS ON RIB HOLES NR 2 BS XOS= 240 WERE REMOVED IAW SRM 57-02 PAR 9. REWORKED HOLES WERE MEASURED INBD LUG FWD HOLE 0.939" AND AFT HOLE 0.941". BUSHINGS WERE FABRICATED IAW SRM 57-02, PAR 9, C, TABLE 1, 1, 2. BUSHINGS WITH OD 0.942" BUSHINGS WITH OD 0.940", 1 EA, BUSHINGS WITH OD 0.939", 2 EAS. BUSHINGS AND REWORKED AREAS WERE TREATED IAW SRM 51-10-3, PAR 21. NEW BUSHINGS WERE INSTALLED IAW SRM 57-02 PAR 9. USED TOOL: CALIPER DIGITAL GD-573 AJM DUE DATE 26-SEP-15. PRIMARY STRUCTURE.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,300 hrs · 46,457 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL 1464C COUNTERSINKS INLET AND SETTLEMENT AREA. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: CUSP WEB — CORRODED (BS 561-572) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORRODED PREVIOUS REPAIR DOUBLER ON RT CUSP WEB X 54 TO X 60, BS 561-572. THE CUSP WEB WAS FABRICATED, AND REPLACED IAW SRM 53-05 FIG. 131A.

Part: LONGERON — CRACKED (BS 1380) · airframe 63,300 hrs · 46,457 cycles

CRACKED LONGERON 11R AT AFT ACC COMP BS 1380. REPLACED THE LONGERON IAW SRM 53-02, FIG 18.

Part: INTERCOSTAL — CRACKED (BS 1352) · airframe 63,300 hrs · 46,457 cycles

CRACK ON INTERCOSTAL BEHIND SIX PULLEY BRACKET BS 1352 AND X=-22. INTERCOSTAL WAS REPLACED, INTERCOSTAL WAS REPAIR IAW SRM 51-30-2, 51-30-1, 53-01, FIG 2.

Part: CUSP WEB — CORRODED (BS 987-1000) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON LT CUSP WEB X 55 TO X 60, BS 987-1000. A NEW CUSP WEB REPLACED IAW SRM 53-05 FIG. 131A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON LT WING FUEL TANK ACCESS PANEL 1379C COUNTERSINKS. CORROSION REMOVED AND WERE FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW DC-SRM 51-22-2A CONDITION II.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,300 hrs · 46,457 cycles

CRACKED PAN ON BEAM FWD EDGE AT LT AFT EMERGENCY EXIT DOOR, SM, ZONE 201, CARD 73. AREA WAS REPAIRED IAW SRM 52-05D FIG 51, 51-30-1, 51-30-2, 51-30-5, AND 51-10-3 PARA 14 AND 21. CRACK 1. PRIMARY STRUCTURE.

Part: CUSP WEB — CORRODED (BS 421-424) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON LT CUSP WEB, BS 421 - 424, X 55 TO X 60. DAMAGE REMOVED, AND A REPAIR FABRICATED IAW SRM 53-05 FIG 131A-13. THE REPAIR WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 21, 14, AND INSTALLED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 455-461) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

REPAIR DOUBLER CORRODED ON THE RT CUSP WEB, X 54 TO X 60, BS 455 - 461. REPAIRED IAW SRM 51-30-5, 51-30-1, 51-30-2, 53-05 FIG 131A-14, 51-10-3 PAR 21, 14, AND SRM 51-30-2, 51-30-5, 51-30-1.

Part: CUSP WEB — CORRODED (BS 581-596) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON THE LT CUSP WEB X 55 TO X 60, BS 581 - 596. REPAIRED IAW SRM 53-05 FIG 131-A-7, 51-10-3 PAR 14, 21, AND 38, 51-30-2, AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 764-766) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON LT CUSP WEB X 54 TO X 60, BS 766 - 764. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-13, 51-10-3 PAR 21, 38, 14, AND 51-30-05.

Part: CUSP WEB — CORRODED (BS 1062-1066) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION OUT LIMITS ON CUSP WEB BS 1062 TO 1066 AND X 56 TO X 60. DAMAGE WAS REMOVED AND A REPAIR WAS FABRICATED IAW SRM 53-05 FIG. 131A-13, 51-30-2, 51-10-3 PAR. 21 AND 14.

Part: CUSP WEB — CORRODED (BS 562-578) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON THE LT CUSP WEB X 55 TO X 60 FROM BS 562 - 578. INSTALLED A REPAIR IAW SRM 51-30-1, SRM 51-30-2, SRM 53-05 FIG 131A-14 SHEET 1, SRM 51-10-3 PAR 21-14-38

Part: CUSP WEB — CORRODED (BS 984-1003) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON RT CUSP WEB BETWEEN X -54 - 60 AND BS 984 - 1003. REPAIRED THE CUSP WEB IAW SRM 53-05 FIG 131A-3, 51-10-3 PAR 14, 21.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON FUEL ACCESS PANEL 1409C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SEAT TRACK — CORRODED (BS 270-271) · corrosion level 2 · airframe 66,757 hrs · 48,997 cycles

CORROSION ON THE RT SEAT TRACK BS 270 - 271 X -54. PLUG WAS REMOVED IAW SRM 51-30-1 AND 51-20-0. A NEW PLUG WAS INSTALLED IAW SRM 53-05 FIG 4A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,118 hrs · 46,348 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM ROWS 16-25 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS TESTED SATISFACTORILY. LP 7267468.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 62,909 hrs · 46,214 cycles

MAINTENANCE FOUND 1L DOOR SLIDE LOOSE. L1 SIDE RAFT WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,219 hrs · 45,746 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN THE COCKPIT AND AT DOORS L1 & R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: SPAR CAP — CRACKED (RT WING) · airframe 61,952 hrs · 45,564 cycles

MAINTENANCE FOUND A 1.25 INCH LONG CRACK ON THE RT WING REAR SPAR LOWER CAP. THIS CRACK FALLS UNDER SB 57A242, CONDITION 2A. C/W PRI 504296-14AD, REV A, REV 0, 1, 2, 3, 4, 5 AND ERA 504296-14AD, REV A PERMANENT REPAIR INSTALLED.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 61,102 hrs · 44,956 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT 35DE WERE INOPERATIVE. MAINTENANCE FOUND WIRE HARNESS IN POOR CONDITION AND REPLACED. OPS CHECKED NORMAL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 60,383 hrs · 44,457 cycles

WIRE BROKEN TO EMERGENCY LIGHT IN TAIL COMPARTMENT. LIGHT IS INOPERATIVE. CONNECTED QUICK DISCONNECT, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,976 hrs · 44,204 cycles

WHITE SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT 22D AND 33D. REPLACED LAMP 22D IAW AMM33-50, OPS OK.

Part: UNKNOWN — UNKNOWN · airframe 59,513 hrs · 43,894 cycles

C-3 CARGO LOWER BEAM REPAIRED IAW ERA 520305-14, LOG 1179098.

Part: SKIN — DAMAGED (BS 1315) · airframe 59,521 hrs · 43,898 cycles

FUSELAGE AFT LAV SERVICE DOOR CUTOUT FS 1315 & L-22L SKIN & SURROUND DOUBLER REPAIRED IAW ERA 501813-14, T484790, LOG 0582213, LOG 1176332.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, THE TAIL CONE RELEASE KEVLAR CABLE WAS NOTED TO BE FRAYED. CABLE REPLACED IAW AMM 53-53.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, TAIL CONE GUIDE PIN RECEPTICLES WERE FOUND TO BE WORN FOWARD FRAME FACE. REPLACED ALL GUIDE PIN RECEPTICALS IAW AMM 51-30.

Part: CLAMP — LOOSE (TAILCONE) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, TAIL CONE RELEASE CABLE CONDUITS WERE FOUND TO BE LOOSE AT THE 7 O-CLOCK POSITION AT BS 1510. CABLE CONDUIT CLAMPS REPLACED AND ADJUSTED IAW AMM 53-53.

Part: ARM — BENT (TAILCONE RELEASE) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, RT TAILCONE RELEASE LATCH ARM ALIGNMENT PIN WAS FOUND BENT. REPLACED TAILCONE LATCH ASSY IAW AMM 53-53.

Part: BUSHING — WORN (TAILCONE) · airframe 59,513 hrs · 43,894 cycles

DURING CHECK, THE TAIL CONE TEE PIN BUSHINGS WERE FOUND WORN BS 1490. BUSHINGS REPLACED IAW AMM 53-53.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 59,513 hrs · 43,894 cycles

DURING CHECK, THE KEVLAR CABLE RELEASE CAM BASE WAS FOUND TO BE WORN IN THE AFT ACCESSORY BAY AT BS 1510. CAM BASE REPLACED IAW AMM 53-53.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 59,513 hrs · 43,894 cycles

DURING CHECK, THE TAIL CONE RELEASE TEE PIN WAS FOUND TO BE WORN ON THE LT SIDE AT BS 1490. REPLACED THE TEE PIN IAW AMM 5353.

Part: SPRING — WORN (TAILCONE RELEASE) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, FOUR TAIL CONE LATCH SPRINGS WERE FOUND TO BE WORN. LATCH SPRINGS REPLACED IAW AMM 53-53.

Part: SKIN — CRACKED (BS 1418) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, A CRACK WAS FOUND ON THE FUSELAGE CROWN SKIN OUTBOARD OF THE BS 1418 SKATE ANGLE BETWEEN L2-3R. REPAIRED PER ER/A 520298-14AD.

Part: SKATE ANGLE — CRACKED (BS 1418) · airframe 59,513 hrs · 43,894 cycles

DURING SCHEDULED CHECK, TWO CRACKS WERE FOUND AT THE LEFT SKATE ANGLE AT BS 1418. ONE OF THE CRACKS RUNS UNDER THE SKATE ANGLE. REPAIRED IAW ER/A 520299-14AD.

Part: UNKNOWN — UNKNOWN (DOOR) · airframe 59,347 hrs · 43,768 cycles

FWD, MID, AFT CARGO DOORS REPAIRED IAW AA 5230-01159.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,319 hrs · 43,748 cycles

DURING ROUTINE SERVICE CHECK IN MSP, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED POWER SUPPLY AND LIGHT ASSEMBLIES L2-717 & L2-718 IAW APPROVED WIRING DIAGRAM MANUAL 33-51. OPS THEN CHECKED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,296 hrs · 43,730 cycles

DURING LINE CHECK, OVERHEAD EMERGENCY LIGHT LENS AT ROW 22 WAS FOUND TO BE MISSING. THE LENS WAS REPLACED IAW AMM 33-53.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,857 hrs · 43,400 cycles

DURING SCHEDULED INSPECTION, MX NOTED THE EMERGENCY ESCAPE PATH LIGHT AT ROW 22D WAS INOPERATIVE. THE EMERGENCY LIGHT SEAT LEG CONNECTION WAS RESECURED AND OPERATION THEN CHECKED NORMALLY.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 58,857 hrs · 43,400 cycles

DURING SCHEDULED INSPECTION, MX NOTED THE EMERGENCY ESCAPE PATH LIGHT AT ROW 16D WAS INOPERATIVE. THE EMERGENCY LIGHT WALL CONNECTION WAS RESECURED AND OPERATION THEN CHECKED NORMALLY.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,351 hrs · 43,075 cycles

DURING SCHEDULED LINE MX CHECK, THE SEAT MOUNTED EMERGENCY PATH LIGHTS AT ROW 31DE TO 36DE WERE FOUND TO BE INOPERATIVE. NEW FUSES WERE INSTALLED IN THE BATTERY CHARGER AND OPERATION CHECKED NORMALLY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 58,279 hrs · 43,025 cycles

DURING LINE MX SERVICE CHECK, THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 16D WAS FOUND TO BE INOPERATIVE. THE SEAT CONNECTOR WAS FOUND TO BE LOOSE AND WAS SECURED. SYS CHECKED NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,069 hrs · 42,874 cycles

DURING OVERNIGHT MX, THE SEAT MOUNTED EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 27 AFT. REPLACED FUSES IN BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 57,553 hrs · 42,520 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-36 OF THE CABIN WERE INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CABLE — OUT OF RIG (TAILCONE RELEASE) · airframe 56,851 hrs · 41,979 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE LATCH CABLES WERE OUT OF ALLOWABLE RIG LIMITS. THE CABLES WERE ADJUSTED AND THE SYS WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 56,480 hrs · 41,693 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE UPPER EMERGENCY ESCAPE EXIT SIGNS AT 25A AND 25E WERE INOPERATIVE. MAINTENANCE FOUND A WIRE LOOSE AT THE GROUNDING STUD. THE WIRE WAS SECURED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SPAR — CRACKED (RT WING) · airframe 56,078 hrs · 41,396 cycles

RIGHT WING SPAR CRACKED. REPAIRED IAW ER/A 09-471576-12.

Part: THRESHOLD — CORRODED (BS 160-200) · airframe 55,998 hrs · 41,353 cycles

R1 DOOR FILLER PLATE AT THRESHOLD TO FLOOR PANEL UPPER SURFACE, BS 160-200 RBL 53-56, MRB 53-013-02-01. CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS. FABRICATED, DRILLED AND COUNTERSUNK A SERVICEABLE R1 DOOR FILLER PLATE IAW DRAWING NR 9957828 REV AB SRM 51-10-4 FIG 3 SH 1 AND SRM 51-10-4 FIG 7.

Part: UNKNOWN — UNKNOWN · airframe 55,985 hrs · 41,348 cycles

HS HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.

Part: UNKNOWN — UNKNOWN · airframe 55,985 hrs · 41,348 cycles

HS UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01086.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,998 hrs · 40,663 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31 AND AFT IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,960 hrs · 39,930 cycles

CREW WROTE UP PEANUT BULB EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERIES FROM THE POWER SUPPLY IN THE FORWARD GALLEY. OPERATION OF LIGHTS NOW CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,802 hrs · 39,807 cycles

CREW WROTE UP EMERGENCY FLOOR LIGHTING AT SEAT 1CD INOPERATIVE. MAINTENANCE RE-LAMPED AND NO HELP, FORWARDED LIGHT TO MCO. MAINTENANCE REPLACED LIGHT ASSEMBLY AT SEAT 1CD. OPERATION OF LIGHT NOW CHECKS OK. MCO/PLAC REMOVED.

Part: RELAY — FAULTY (COCKPIT) · airframe 53,529 hrs · 39,613 cycles

FLIGHT CREW REPORTS ELECTRICAL ODOR INTERMITTENTLY COMES FROM UNDER GLARESHIELD ON CAPTAIN'S SIDE, NOT SURE OF SOURCE. NO SMOKE NOTED. MAINTENANCE REPLACED R2-51 RELAY AND ASSOCIATED WIRING, BUT ALSO REPLACED THE R7-48 AND R7-49 DIODES AS PRECAUTIONARY. THE TERMINAL LUGS WERE RE-TORQUED AND SECURED AND A FUNCTIONAL CHECK OF ALL THE APPLICABLE RELAYS WAS ACCOMPLISHED. AIRCRAFT IS OKAY FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 53,428 hrs · 39,544 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS AT ROWS 23, 24 AND 29 INOPERATIVE. MX RELAMPED ROW 23, R & R SEAT HARNESS ROW 24, AND R & R LAMP HOLDER ROW 29. ALL WORK IAW MM. OPS CK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 53,428 hrs · 39,544 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE AT ROWS 4, 13 AND 30. MX FOUND CONNECTORS LOOSE. SECURED CONNECTORS IAW MM. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN · airframe 52,299 hrs · 38,842 cycles

INSTALLED TEMP REPAIR IAW SRM 57-06B-D, FIG 14, UPPER WING L/E SURFACE CRACK.

Part: SPAR — CRACKED (WING) · airframe 52,299 hrs · 38,842 cycles

WING REAR SPAR CRACKING AT XRS 164, REPAIRED IAW AA 5710-01110.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 51,202 hrs · 38,083 cycles

THE EMERGENCY LIGHTS JUST AFT OF THE CABIN DOOR WERE FOUND TO BE INOPERATIVE. MX FOUND THE CONNECTOR BAD ON THE LIGHT AND REPLACED IT. SYS OPS WAS NORMAL THEREAFTER. (DLM88101443)

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 50,438 hrs · 37,543 cycles

SEAT MOUNTED EMER LIGHTS AT 24DE INOP RED DUAL UNIT. RELAMPED NO HELP REPLACED SOCKETS NO HELP FOUND BROKEN CONNECTOR AT SIDEWALL REPLACED SAME, CKS GOOD.

Part: GROUND STUD — CORRODED (EMERGENCY LIGHTS) · airframe 50,438 hrs · 37,543 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 24 INOPERATIVE. RELAMPED NO HELP OPENED CEILING PANELS REPLACED SOCKETS, NO HELP. FOUND GROUND LUG CORRODED CLEANED LUG, CKS GOOD. REINSTALLED CEILING PNLS.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 50,210 hrs · 37,395 cycles

SEAT MOUNTED EMER LIGHT AT 30DE INOP. RELAMPED NO HELP R & R SOCKET ASSY NO HELP. FOUND BROKEN CONNECTOR AT SIDEWALL RELAMPED SAME, CKS GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 49,638 hrs · 37,023 cycles

AT APPRX 1700 FT, HEARD LOUD BANG FOLLOWED BY RT ENG ROLLING BACK AND EGT ROCKETING THRU 600 DEG. CREW SHUT THE FUEL OFF. C/W ENGINE CHANGE NR 2 IAW TRANSMITTAL NR 9T102 AD.

Part: FLOORBEAM — CRACKED (FS 200 LBL5) · airframe 48,798 hrs · 36,446 cycles

MAIN CABIN FS 200 RBL 5-LBL 5 FLOORBEAM CRACKED. REPLACED SAME.

Part: FLOOR PANEL — TORN (CARGO BAY) · airframe 48,798 hrs · 36,446 cycles

FWD CARGO FLOOR PANEL KF TORN. REPLACED SAME.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 48,798 hrs · 36,446 cycles

MAIN CABIN FS 180 LBL 16-LBL 36 FLOORBEAM CORRODED. REPLACED FLOOR SUPPORT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,798 hrs · 36,446 cycles

FUSELAGE SKIN BLEND OUT FOUND OUT OF LIMITS FS 346 L18R-19R. REPAIRED PER SRM 53-04D FIG 12B.

Part: SKIN — GOUGED (FS 200 L23R-24R) · airframe 48,798 hrs · 36,446 cycles

FUSELAGE SKIN GOUGED FS 517 LONGERON 23R-24R. REPAIRED PER SRM 53-04D FIG 12B.

Part: INTERCOSTAL — CRACKED (FS 771) · airframe 48,798 hrs · 36,446 cycles

INTERCOSTAL CRACKED AT FS 771 BL 0. REPLACED INTERCOSTAL.

Part: CAP — LEAKING (APU OIL) · airframe 39,092 hrs · 29,965 cycles

SMOKE IN THE CABIN REPORTED BY FLIGHT ATTEND. ATB TO CVG. FOUND PACKING ON APU OIL CAP LEAKING. REPLACED AND PERFORMED DUCT BURNOUT WITH APU INLET WASH.

Part: HYDRAULIC LINE — LOOSE (HYD SYSTEM) · airframe 35,872 hrs · 27,680 cycles

RT HYD SYS QUANTITY DROPPED TO ONE WITH GOOD PRESSURE INDICATED. SHUTOFF RT ENGINE DRIVEN PUMP AND EXECUTED MANUAL GEAR EXTENSION AND EMERGENCY LANDING. FOUND RIGID LINE LEAKING ON RT ENGINE HYDRAULIC PUMP. TIGHTENED SAME LEAK, CKS GOOD.

Part: SENSOR — OUT OF ADJUST (LT WING SLAT) · airframe 34,312 hrs · 26,582 cycles

AFTER T/O ON SLAT RETRACTION, GOT THE SLAT DISAGREE LIGHT. FLAPS WERE UP. RECYCLED FLAPS TO NO AVAIL. FOLLOWED POM PROCEDURE AND RETURNED TO DFW. REQUIRED 2 UNITS OF RUDDER TRIM TO THE LEFT FOR LEVEL FLIGHT. OPERATED NORMALLY DURING EXTENSION FOR LANDING. FOUND LEFT WING SENSOR OUT OF ADJUSTMENT. ADJUSTED SAME.

Part: SENSOR — STICKING (LEFT WING) · airframe 33,536 hrs · 26,071 cycles

AFTER TAKEOFF WHEN SLATS WERE RETRACTED, THE DISAGREEMENT LIGHT REMAINED ON. ALL OTHER INDICATIONS AND POSITIONS NORMAL. T/S AND FOUND SENSOR D32 ON LEFT WING STICKING. LUBRICATED SAME, OPS CHECK NORMAL PER M/M.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 33,500 hrs · 26,044 cycles

LIGHTNING STRIKES OCCURRED TO MULTIPLE FASTENER LOCATIONS THROUGH THE FUSELAGE SKIN AND POTABLE WATER SERVICE DOOR SURROUND DOUBLER. A CUTOUT MEASURING 3.7 INCH (FWD-AFT) X 3.8 INCH (UP-DOWN) WAS MADE WITH THE LOWER EDGE BEING 3 INCH FROM THE UPPER EDGE OF THE POTABLE WATER SERVICE PANEL CUTOUT. THE SKIN IS 0.050 INCH 2024-T3 CLAD SHEET. THE SURROUND DOUBLER IS 0.063 INCH 7075-T6 CLAD SHEET. DAL ER/A 379042-14 INSTALLS A 0.063 INCH 2024-T3 CLAD DOUBLER AND 0.071 INCH 7075-T6 CLAD TRIPLER SIMILAR TO MD80 SRM 53-04, F12B, EXCEPT FINGER DOUBLERS WERE OMITTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,028 hrs · 25,002 cycles

1 C TRACK LIGHT INOPERATIVE. RELAMPED OPS CHECK OK

Part: VALVE — MALFUNCTIONED (A/C BAY) · airframe 30,157 hrs · 23,604 cycles

DURING CLIMBOUT, FLIGHT ATTENDANT REPORTED HAZE AND SMOKE IN CABIN. AFT RT SMOKE DETECTOR SOUNDED. CREW S/O LEFT PACK. THE A/C DEPRESSURIZED. PASSENGER MASKS DEPLOYED. CREW PERFORMED EMERGENCY DESCENT AND SMOKE REMOVAL CHECK LIST. ODOR SMELLED LIKE PLASTIC MELTING. FOUND DUCT DISCONNECTED AT ACM DIS. REMOVED COALESCER ASSY FOUND BAGS MELTED. REPLACED ASSY'S AND BAGS. FOUND CAPS INSTALLED ON BOTH LT AND RT AUG VALVES. REPLACED LT AND RT AUG VALVES. REPLACED O2 MASKS AND GEN. CONNECTED DUCT ON ACM DISCHARGE AND PERFORMED TEST 5, 6, 7 PER PFHB A/C SYS CKS OUT, BOTH PACKS OPS NORMAL.

Part: DUCT — DISCONNECTED (A/C BAY) · airframe 30,156 hrs · 23,602 cycles

SMOKE IN CABIN. FOUND RT ACM DISCHARGE CABIN SUPPLY DUCT DISCONNECTED JUST FWD OF ACM. RECONNECTED SUPPLY DUCT AND REMOVED WATER SEPARATORS DUE TO INSULATION INGESTION. FOUND RT WATER SEPARATOR BAG MELTED. REPLACED BAGS AND REINSTALLED WATER SEPS.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 29,254 hrs · 22,939 cycles

SMOKE IN CABIN, PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.

Part: HYDRAULIC SYSTEM — LEAKING (NR 1 ENGINE) · airframe 27,561 hrs · 21,679 cycles

ON FINAL APPROACH AND CONFIG WITH ENG HEAT ON, SMOKE DETECTOR ACTIVATED (AFT LAV CAPT SIDE) FOR 30 SEC - FOUND HYDRAULIC LEAK ON NR 1 ENGINE TIGHTENED LINE - PERFORMED DUCT BURNOUT.

Part: LINE — RUPTURED (RT MLG WW) · airframe 26,546 hrs · 20,914 cycles

AFTER LANDING RT HYDRAULIC SYSTEM PRESS AND QTY DROPPED TO ZERO. A/C STOPPED AND TOWED TO GATE. FOUND RUPTURED AUX PRESS LINE. REPLACED LINE, PUMP AND FILTER.

Part: TRANSFORMER — INOPERATIVE (E/E BAY) · airframe 25,864 hrs · 20,383 cycles

GROUND SERVICE BUS T/R INOP. NO LIGHTS OR FLUSH MOTORS IN ANY LAV. NO LOAD, NO NR 2 T/R. REMOVED AND REPLACED NR 2 T/R, OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,666 hrs · 20,242 cycles

ON LAYOVER CHECK, FOUND CABIN EMERGENCY LIGHTS IN AFT CABIN INOP ON EMERGENCY LIGHT CHECK. REPLACED BATTERY PACK AND PERFORMED EMERGENCY LIGHT CHECK AGAIN. ALL EMERGENCY LIGHTS OPERATED NORMALLY.

Part: MOTOR — ODOR (CABIN) · airframe 25,453 hrs · 20,081 cycles

SHORTLY AFTER TAKEOFF, FLT ATTENDANT REPORTED A STRONG BURNING RUBBER ODOR IN AFT CABIN AREA AIR TURNBACK. RAN BOTH ACM W/APU AND ENG BLEED AIR. NO ODORS PRESENT. INSP A/C FOR FLUID LEAKS AND APU INLET CONTAMINATION, NONE PRESENT. PERFORMED RECIRC FAN CHECK OUT PER MM, OPS NORMAL. FOUND AFT LEFT LAV MOTOR BURNED OUT, POSSIBLE CAUSE OF ODOR. REPLACED SAME, OPS NORMAL. A/C OK FOR SERVICE.

Part: SKIN — CORRODED (BS 826)

CORROSION FOUND UNDER RUB STRIP AT FS 826 AND L30. REPAIRED PER ERA 331105-14.

Part: SKIN — CORRODED (BS 807)

CORROSION FOUND UNDER RUB STRIP AT FS 807 AT L29L AND L29R. REPAIRED PER ERA 331097-14.

Part: SKIN — DENTED (BS 218)

SKIN WAS DENTED AT STA 218 AND L18L TO L19L. REPAIRED PER ERA 331096-14.

Part: FRAME — CORRODED (BS 1307)

FS 1307 FRAME WAS FOUND CORRODED NEAR L29L. REPAIRED PER ERA 331068-14.

Part: SKIN — CORRODED (BS 765-773)

SKIN WAS CORRODED UNDER RT RUB STRIP FROM FS 759 TO FS 773 BETWEEN L27R AND L29R. REPAIRED PER ERA 331081-14.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN WAS DENTED AT APPROX STA 237, BETWEEN S17L AND S18L. SKIN CUT OUT IS 12 BY 8. REPAIRED PER 331082-14.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN DENTED AT FS 237 BETWEEN S18L AND S19L. CUT OUT DIMENSIONS ARE 9 BY 8. REPAIRED PER ERA 331095-14.

Part: FRAME — CRACKED (BS 1418)

FS 1418 CRACKED L2L TO L2R AT TYP LOCATIONS. REPAIRED PER ERA 331065-14.

Part: COALESCER BAG — CONTAMINATED (CABIN)

SMOKE AND BURNT RUBBER SMELL IN CABIN ON CLIMBOUT. REPLACED COALESCER BAGS, INSPECTED AIRCRAFT AND NO DISCREPANCIES NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK, CHECKS NORMAL.

Part: LINE — LEAKING (RT HYD SYS)

RIGHT HYD SYSTEM FAILED DURING SLAT EXTENTION ON DESCENT. MANUALLY EXTENDED LANDING GEAR, LANDED ATL. FOUND PRESSURE LINE FROM RT FILTER MODULE LEAKING. REPLACED LINE, OPERATION NORMAL.

Part: FRAME — CRACKED (RT MLG DOOR)

FOUND DURING D-2 LETTER CHECK, .25 INCH CRACK AT O/B CORNER OF MLG DOOR FRAME ON EXISTING DOUBLER. REPAIRED PER SRM 53-05 NR 81A.

Part: SKIN — CRACKED (NLG W/W CUTOUT)

R/T NOSE W/W DOOR HINGE AFT HINGE CUTOUT, .75 INCH CRACK FUSE SKIN. FOUND AT D-2 LTR CK. REPAIRED PER SRM 53-05 FIG 62A.

Part: SKIN — CRACKED (NLG DOOR CUTOUT)

LT NOSE W/W DOOR AFT HINGE CUTOUT, .25 INCH CRACK IN FUSE SKIN. FOUND AT D-2 LTR CK. REPAIRED PER SRM 53-05 FIG 62A.