N997DL

Part: STATIC PORT — LEAKING (RIGHT) · airframe 71,900 hrs · 52,250 cycles

SDR REPORTED DUE TO DECLARED EMERGENCY PER MCC REPORT. AFTER TAKEOFF, AIRSPEED ERRATIC. DISCONNECTED AUTOPILOT + AUTOTHROTTLES. RECEIVED VECTORS FROM ATL. CONFIRMED ALTITUDE AND HEADING ACCURACY FROM ATL. CONFIRMED GROUND SPEED READOUT C/W PITOT/STATIC SYS LK CK OF CAPT AND F/O SYS LK CK GD ACCURACY OF A/S AND ALT WITHIN TOLERANCE ALL PER MD88 AMM 34-11. FOUND STBY IND SLOW TO RESPOND FOUND QUICK DISCONNECT FOR STATIC LINE AT STBY IND LOOSE. REMOVED + REPLACED FLEX STATIC LINE TO INDICATOR AND CONNECTOR TO INDICATOR REF MD88 AMM 34-13. REMOVED + REPLACED STANDBY ALTIMETER/AIRSPEED IND. REF MD88 AMM 34-13. FOUND RIGHT SIDE ALTERNATE STATIC PORT TUBE LEAKING. REMOVED AND REPLACED RIGHT SIDE ALTERNATE STATIC PORT PER MD88 AMM 34-11. NEEDS LEAK CHECKED. LK CK OF R/H ALT STATIC PORT GD PER MD88 AMM 34-11 FOUND 1ST + 2ND LINE FROM R/H STATIC PORT LEAKING AT B-NUTS OF UNION RPLD BOTH LINES AND UNION STBY IND LK CK GD AND ACCURATE PER MD88 AMM 34- 11 REQS CLAMPING OF LWR LINE AND B/B CLOSE UP. CLAMP UP + B/B CLOSE UP C/W. INDICATOR, STAN OFF 88-3411-9-0001 00344 ON 88-3411-9-0001 00774. (LP6640896)

Part: FITTING — CRACKED (TAILCONE) · airframe 71,670 hrs · 52,027 cycles

UPPER LT FITTING ON TAILCONE CRACKED. REMOVED UPPER LT TAILCONE FITTING. REPLACED UPPER LT FITTING ANGLE PER SRM 53-54-0 PAGE 3. OK FOR SERVICE. (LP1272698)

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,670 hrs · 52,027 cycles

TAILCONE ATTACH FRAME CRACKED @2:00 POSITION AT PIN. REMOVED FRAME P/N 9911843-6. DRILLED UP REPLACEMENT FRAME P/N 5966769U501 PER DWG 9911843. (458779) INSTALLED NEW FRAME IAW DWG 9911843. (LP1272701)

Part: BEARING — EXCESS PLAY (TAILCONE) · airframe 71,670 hrs · 52,027 cycles

TAIL CONE RELEASE HAS PLAY AND IS CONTACTING THE FRAME. REMOVED TAIL CONE MECHANISM PER AMM 53-53-02. 542402. REPLACED RELEASE CAM BEARING IAW CMM 53-50-07. REINSTALLED MECHANISM IAW AMM53-53. NO PLAY NOTED PASSED TORQUE CHECK. (LP1272607)

Part: FRAME — CRACKED (RT MLG WW) · airframe 71,649 hrs · 52,009 cycles

RT FWD MAIN LANDING GEAR WHEEL FRAME CRACK. INSTALLED NEW RT FWD MLG W/W FRAME SECTION REF ERA 581127-14 REV 0 PERMANENT REPAIR. (LP6026692)

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 70,872 hrs · 51,329 cycles

CRUISING AT FL 320 FLOW LIGHT CAME ON. OUTFLOW VALVE FULLY CLOSED. DESCENDED NORMALLY. FLOW LIGHT EXTINGUISHED AT APPROXIMATELY FL240. TIGHTEN FITTING FOR RT PILOT PRESSURE REGULAR SENSE LINE. REPLACED SEALS FOR UNION LT PRESSURE REGULATOR VALVE TO HEAT EXCHANGER PREFOMED DUAL PACK CONFIDENCE CHECK PER AMDS 2132-1002. BOTH PACKS FAILED. REPLACED RT PACK COLENSSE SOCK. FOUND LT LEAK EXCHANGER SPRAY NUZZLE DAMAGE REQUIRES REPLACEMENT. INSPECTED SPRAY NOZZLE ON LT HEAT EXCHANGER FOUND NO DAMAGE OPS CHECK PASSED REPLACEMENT NOT REQUIRED. INSPECTED PACKS FOR STUCK TURBINES BOTH PACK CHECK GOOD. ALL DUCTS NO LEAKS FOUND PERFORMED PACK CONFIDENCE CHECK FOUND MID CARGO MASSIVE LEAK AT BEAM OF DOOR AND DOOR IS CRACKED, REMOVED DOOR. INSTALLED MID CARGO DOOR PER AMM 52-31 PERFORMED PHEU. HELTH CHECK PER 2120-2277, 2120-2258 AND DUEL PACK T/S HOC PER 2132-1002 ALL LEAK AND OPS CHECKS ARE WITH IN LIMITS. PERFORMED ALL NO GO ODI PREVENTION NOTIFIED MCC. SDR REPORTED DUE TO MID CARGO DOOR BEING CRACKED CAUSING PRESSURIZATION LOSS. (LP5423322)

Part: SKIN — CORRODED (LAV SERVICE DOOR) · corrosion level 2 · airframe 70,804 hrs · 51,268 cycles

ON WALK AROUND FOUND CORROSION LWR FWD CORNER OF AFT LAV SERVICE DOOR AREA. C/W REPAIR PER ERA 577463-14 REV ORIG - ALL RII ITEMS C/W. (LP5673084)

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,527 hrs · 51,025 cycles

ROW 25 EMERGENCY EXIT SIGN INOP BOTH SIDES. R+R BATTERIES FOR BATTERY PACK IAW MM 33-53. LIGHT CKS OK. (LP5832910)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,527 hrs · 51,025 cycles

3C SEAT EMERGENCY LIGHT INOP. RELAMPED BULBS. LIGHTS CKS OK AT 3C. REF MM 33-53. (LP5832911)

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 69,488 hrs · 50,137 cycles

SHIP 997 ON FLIGHT 296 FROM ATL TO RDU DECLARED AN EMERGENCY DUE TO AN EOAP LOW RIGHT HYDRAULIC SYSTEM QUANTITY MESSAGE. CORRECTIVE ACTION: RDU MAINTENANCE FOUND THE RUDDER SHUTOFF VALVE SUPPLY LINE LEAKING. A TEMPORARY LINE WAS INSTALLED AND DEFERRED PER LOG SHEET 4412988. NO GO ODI PREVENTION WORK CARDS WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP0747893)

Part: FASTENER — MISSING (LT WING) · airframe 69,316 hrs · 49,981 cycles

FASTENERS MISSING FROM LT AILERON CLOSEOUT PANEL. INSTALLED FASTENERS. OK FOR SVC. SDR REPORTED DUE TO THE FACT THAT THE FASTENERS COULD HAVE DEPARTED THE AIRCRAFT DURING FLIGHT.

Part: LENS — MISSING (POSITION LIGHT) · airframe 69,110 hrs · 49,821 cycles

RIGHT POSITION LIGHT LENS WAS MISSING. REMOVED AND REPLACED THE RT POSITION LIGHT ASSY IAW AMM 33-43, OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,671 hrs · 49,454 cycles

FAILED EMERGENCY LIGHT BATTERY PACK AT BS 1338. THE BATTERY PACK WAS REPLACED IAW AMM 33-53-00. OPS TESTED GOOD IAW AMM 33-53-00.

Part: SCREW — OUT OF TOLERANCE (HORIZONTAL STAB) · airframe 68,665 hrs · 49,448 cycles

DURING A HORIZONTAL STABILIZER ACTUATOR ASSEMBLY END PLAY CHECK, THE FINAL END PLAY READ MORE THAN 0.040 INCH. SCREW AND NUT WERE REMOVED AND REPLACED IAW AMM 27-40-01-401, AND AMDS 2742-4520.

Part: CHANNEL — CRACKED (MLG DOOR FRAME) · airframe 68,661 hrs · 49,446 cycles

A CRACKED AFT CHANNEL, ON THE FWD RT MLG WW DOOR FRAME BS 937, RBL 55. THE CHANNEL WAS REPLACED IAW SRM 51-30-02, AND SRM 51-30-05.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 68,661 hrs · 49,446 cycles

FLOOR PANEL 693C DELAMINATED AT AFT END. THE FLOOR PANEL WAS REPLACED IAW AMM. 53-20-01-201.

Part: DUCT — DAMAGED (APU) · airframe 68,605 hrs · 49,402 cycles

APU FAILED INFLIGHT LEFT GEN DEFERRED. EMERGENCY WAS DECLARED. FOUND APU SURGE VALVE DUCT DAMAGE. R&R SURGE VALVE DUCT PER AMM 49-50. R&R NR 1 ENG GENERATOR DRIVE AND CONSTANT SPEED DRIVE PER AMM 24-10. OPS AND LEAK CHK OF ALL OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,277 hrs · 49,160 cycles

SEAT ROW 23 RT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. SYSTEM CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,742 hrs · 48,783 cycles

OVERWING EMERGENCY LIGHT INOP. T/S, R&R OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK PER MM 33-53. OPS CHK - GOOD. OK FOR SVC.

Part: WIRE HARNESS — FAILED (EMERGENCY LIGHTS) · airframe 67,622 hrs · 48,706 cycles

EMERGENCY LIGHTS AT SEATS 18 AND 22 DE INOPERATIVE. REPLACED THE EMERGENCY LIGHT HARNESSES AT SEATS 18 AND 22 DE. OPS CHECKED GOOD IAW SPWM 20 AND EWIS.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 67,622 hrs · 48,706 cycles

OVERHEAD EMERGENCY LIGHTS AT ROWS 10 AND 13 INOPERATIVE. FOUND THE BATTERIES BAD AT SEAT ROWS 10 THRU 13 AND REPLACED IAW SPWM 20 AND EWIS. OPS CK GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 67,426 hrs · 48,577 cycles

SEAT 13ED EMERGENCY LIGHT INOPERATIVE. FOUND THE WIRES PULLED FROM THE CONNECTOR. REPLACED THE WIRE HARNESS. OPS CHECKED GOOD IAW AMM33-52.

Part: SKIN — CRACKED (BS 1407) · airframe 67,189 hrs · 48,394 cycles

FUSELAGE SKIN CRACKED AT BS 1407, LONGERON 2L. COMPLIED WITH PRI 540097-14AD REV C REV 0.

Part: DOUBLER — DAMAGED (NR 2 PYLON BLKHD) · airframe 66,617 hrs · 47,948 cycles

NR 2 PYLON HYD SUPPLY HOSE FITTING LOOSE IN FIREWALL. REMOVED ORIGINAL REPAIR. FABRICATED REPAIR DOUBLER PER RI 560468-14. CLEANED UP HYD PRESSURE LINE HOLE IAW STEP 3 RI 560468-14, COMPLIED WITH HFEC SURFACE SCAN INSP PER MD88 NDT MANUAL MDC-93K0393 PARA 6. CH 06.01.001 NO DISCREPENCIES. COMPLETED DOUBLER FABRICATION, APPLIED PRIMER. INSTALLED A REPAIR DOUBLER AND IDENTIFIED REPAIR IAW RI560468-14 23.

Part: ENGINE — FAILED (NR 2) · airframe 64,954 hrs · 46,752 cycles

AFTER TAKEOFF, APPROACHING 5000 MSL, LOST OIL PRESSURE AND RIGHT ENGINE HAD SEVERE VIBRATIONS, LOSS OF RIGHT HYDRAULIC SYSTEM. VIBRATIONS STILL PRESENT ON WINDMILLING ENGINE. RETURNED FOR SINGLE ENGINE LANDING. NR 2 ENGINE WAS REPLACED.

Part: ENGINE — FAILED (NR 2) · airframe 64,954 hrs · 46,752 cycles

RETURNED TO DEPARTURE DUE TO RIGHT ENGINE ISSUES. THE CREW REPORTED THAT ON TAKEOFF AT FL50 THE NR 2 ENGINE LOST OIL PRESSURE, HYDRAULICS AND STARTED VIBRATING. THE QRH WAS FOLLOWED AND THE ENGINE WAS SHUT DOWN. THE NR 2 ENGINE WAS REPLACED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,857 hrs · 45,928 cycles

DURING SERVICE CHECK, FOUND COCKPIT, R1, L1 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER PACK BATTERIES IAW AMM 33-50. OPS CHECK GOOD.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION AND WEAR ON SEATING AREA OF SECONDARY ACCESS PANELS, 1409C, 1410C AT RT WING. HEATER BLANKET WAS REPLACED IAW AMM 30-80-02, PAGE BLOOCK 401.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON SEATING AREA OF SECONDARY ACCESS PANELS, 1303C, 1307C AT LT WING. HEATER BLANKET WAS REPLACED IAW AMM 30-80-02, PAGEBLOCK 401.

Part: LANYARD — TORN (TAILCONE SLIDE) · airframe 63,601 hrs · 45,748 cycles

MAINTENANCE FOUND THE TAILCONE LANYARD TORN. THE LANYARD WAS REPLACED.

Part: BEAM — CRACKED (BS 1485) · airframe 63,601 hrs · 45,748 cycles

CRACKED VENTRAL STAIR BEAM 1485 X=10 AT AAC. CRACKED BEAM WAS ATTENDED WITH SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2 AND 51-30-5.

Part: BUSHING — CORRODED (RT WING) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION FOUND ON BUSHINGS AT RT OVERWING HEATER BLANKET REAR SPAR. BUSHINGS 1, 2, 6, 7, 8, 9 AND 10 WERE REPLACED IAW SRM 51-30-10 AND BUSHINGS 3, 4 AND 5 WERE REPLACED IAW ER/A 545121-14AD, REV A, ETI-88-16-165, R8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,601 hrs · 45,748 cycles

CRACKED LONGERON 15 RT AT CENTER WING FUEL TANK BS XEW 12. REPAIR WAS ACOMPLISHED IAW ETI-88-16-143, REV 3 AND ETI-88-16-145, REV ORIGINAL AND ER/A 545092-14, REV ORIGINAL AND ER/A 545095-14, REV ORIGINAL.

Part: DOOR FRAME — CRACKED (LT NLG DOOR) · airframe 63,601 hrs · 45,748 cycles

CRACKED NLG DOOR JAMB, LT SIDE. LT JAMB AND LT STEP WERE REMOVED IAW SRM 51-30-2 AND SRM 51-30-5. REPAIR WAS ACCOMPLISHED IAW ER/A NR 545103-14 AND ETI-88-16-149, REV ORIGINAL LT JAMB AND LT STEP WERE. INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CORRODED (BS 196) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION UNDER LOWER R1 DOOR JAMB FLOOR LEVEL CUSP ANGLE RBL 60, BS 196. CUSP ANGLE WAS REPAIRED IAW SRM 53-05, FIG 55 AND ETI-88-16-153, REV 5, ER/A 545109-14, REV ORIG.

Part: FRAME — CRACKED (BS 1437) · airframe 63,601 hrs · 45,748 cycles

CRACKED FRAME CLIPS 1437 BETWEEN LONGERON 1RT AND 3RT. FRAME CLIPS WERE REPLACED IAW DOUGLAS DWG NR 9953016, REV AT, ETI-88-16-191 REV 1 AND ER/A 545160-14, REV.

Part: CARGO TRACK — CORRODED (BS 1155-1222) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON LT CARGO TRACK FROM BS 1155 TO 1222 IN THE AFT CARGO BAY. CARGO TRACK WAS REPAIRED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4 AND 51-10-3, PAR 14, 21.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 63,601 hrs · 45,748 cycles

PUNCTURED LOWER SURFACE COVER ON INBD VANE OTBD FLAP XV1=211 AT LT WING. REPAIR FABRICATED IAW SRM 57-01, FIG 3. REPAIR TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. REPAIR INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (BS 1419) · airframe 63,601 hrs · 45,748 cycles

CRACKED FUSELAGE SKIN 1419 BETWEEN LONG 1 AND 2 RT AT AAC. AREA WAS REPAIRED I IAW ETI-88-16-152, REV. 1 AND ER/A 545106-14AD REV ORIGINAL.

Part: FLOOR SUPPORT — DAMAGED (BS 769-786) · airframe 63,601 hrs · 45,748 cycles

ELONGATED HOLES ON FLOOR SUPPORT MID CARGO COMPARTMENT BETWEEN BS 769 TO 786.5 AND LONGERON 27R-28R. ETI-88-16-146 WAS ACCOMPLISHED ON PN 5936594-529 LT AND PN 5936594RH IAW ERA 545098-14, REV A.

Part: SKIN — WORN (BS 133) · airframe 63,601 hrs · 45,748 cycles

WORN PREVIOUS DOUBLER REPAIR ON FWD FUSELAGE SKIN BS 133 LONG 15L AT FWD FUSELAGE. REPAIRED IAW ETI-88-16-187, REV 1 AND ER/A 545154-14, REV ORIGINAL.

Part: DOUBLER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AT MID CARGO DOOR JAMB. NEW SPACER WAS FABRICATED AND TREATED, PAINTED, WAS INSTALLED IAW SRM 53-05, FIG 123, 51-10-3 PAR 21,14-51-30-5.

Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON FRAME BS 1271 BETWEEN LONGERON 30 AND 29 LT AT AFT CARGO COMPARTMENT. FRAME WAS REPAIR IAW SRM 53-03, FIG 2A AND 51-10-3 P14, 16, 51-30-5, 51-30-2.

Part: FRAME — CRACKED (BS 1485) · airframe 63,601 hrs · 45,748 cycles

CRACK ON FRAME WEB BS 1485 BELOW VENTRAL ACTUATOR FITTING. FRAME WEB WAS REPAIRED IAW SRM 51-01, PAR 21, 53-03 FIG 43, 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON BARRIEL NUTS NR 13, 20 AND 25 XH -27. CORROSION ON BARRIEL NUTS NR 13, 20 AND 25 XH =-27 WAS REPAIRED IAW ERA NR 545115-14, REV: ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1460C. ACCESS PLATE NR 1460C WAS REPLACED IAW SRM 51-22-2A COND II.

Part: TEE FITTING — SCRATCHED (BS 1338) · airframe 63,601 hrs · 45,748 cycles

SCRATCH ON 1338 TEE LOWER SECTION BETWEEN LONGER ON 29LT AND 30 AFT SURFACE AT AAC. TEE "CAP" BETWEEN LONGERON 23RT TO 23LT FROM BS 1338 WAS REPLACED IAW SRM 51-30-2 , 51-30-5 AND 53-03D PARA 32, FIG 37A.

Part: TRIPLER — CRACKED (BS 1438) · airframe 63,601 hrs · 45,748 cycles

CRACKED PRODUCTION TRIPLER BS 1438 BETWEEN 1 TO 2 RT AT AFT ACCESSORY COMPARTMENT. PRODUCTION DOUBLER ABOVE REPORTED WAS REPLACED IAW DWG 5912141, REV BR AND SRM 51-30-2 /51-30-5/51-10-3.

Part: ACCESS PANEL — UNKNOWN (RT WING) · airframe 63,601 hrs · 45,748 cycles

PERFORM SERVICE TO FUEL TANK ACCESS PLATES ON RT WING. SERVICE ON ACCESS NR 1476C, 2302C, 1478C, 1464C AND 1466C WERE PERFORMED AND ACCESS NRS 1410C, 1436C,1472C, 1414C, 1456C, 1470C, 1462C, 1454C, 1460C AND 1409C WERE REPLACED IAW AMM 57-30-03.

Part: FRAME — CRACKED (BS 1437) · airframe 63,601 hrs · 45,748 cycles

CRACKED FRAME FITTING BS 1437 BETWEEN LONG 1 AND 2R. FITTING WAS REPLACED IAW DWG 9953016, REV AT AND 51-30-5.

Part: SKIN — CRACKED (BS 1418-1437) · airframe 63,601 hrs · 45,748 cycles

CRACKED SKIN SPLICE BETWEEN 1418 AND 1437 BETWEEN LONGERON 2RT AND 3RT AT, AAC. REPAIR WAS ACCOMPLISHED IAW ETI 88-16-147 AND ERA 545100-14, REV ORIGINAL.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION OUT OF LIMITS ON FRAME DOUBLERS BS 1309 BETWEEN LONGERON 29R AND 29L . REPAIR DOUBLERS WERE REPLACED IAW SRM 51-30-5, 53-03, FIG 2A.

Part: SKIN — DAMAGED (BS 492) · airframe 63,601 hrs · 45,748 cycles

DAMAGE ON EXTERNAL FUSELAGE SKIN BS 492 BETWEEN LONGERON 25 - 26R. FOUND WITHIN LIMITS IAW SRM 53-04-1, PAGE 7.D CONDITION 1A. HFEC INSPECTION WAS ACCOMPLISHED ON EXTERNAL FUSELAGE SKIN. NO CRACKS WERE FOUND IAW 53-04-01, PAR 7D, 1, B .

Part: SKIN — DENTED (LT ELEVATOR) · airframe 63,601 hrs · 45,748 cycles

SEVERAL DENTS ON UPPER LOWER SURFACE AT CONTROLTAB AT LT ELEVATOR. LT ELEVATOR CONTROL TAB WAS REPLACED AND INSTALLED IAW AMM 27-30-03-201.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

CRACKED W-CHANNEL ON FLOOR PANEL 886 C. NEW CHANNEL WAS INSTALLED ON THE RT SIDE OF THE FLOOR PANEL 886C IAW DWG 9936639, REV P DRILLED SRM 51-10-4, REMOVED SRM 51-30-1.

Part: CHANNEL — BENT (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

BENT W-CHANNEL ON FLOOR PANEL 826D. NEW CHANNEL WAS INSTALLED ON THE LEFT SIDE OF THE FLOOR PANEL NR 826D IAW DWG 9936639, REV P. DRILLED SRM 51-10-4, REMOVED SRM 51-30-1.

Part: WEB — CORRODED (BS 1338) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT, LT WEBS BS 1338. WEBS RT, LT WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5 AND 53-14-3, FIG 7.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON FRAME TEE BS 1380 BETWEEN LONGERON 25 LT AND 25 RT AT ACCESSORY FRAME TEE FROM BS 1380 BETWEEN LONGERON 25 LT AND 25 RT WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DELAMINATED (NOT REPORTED) · airframe 63,601 hrs · 45,748 cycles

DELAMINATED SKIN BELOW PREVIOUS REPAIR. SKIN BELOW PREVIOUS REPAIR WAS REPAIRED IAW SRM 57-03D, PAR. 11.

Part: DOOR FRAME — WORN (APU DOORWAY) · airframe 63,601 hrs · 45,748 cycles

WEAR ON FWD APU DOOR JAMB BETWEEN X=0 AND X=14 AT ACC. ALL WEAR WAS WELDED, REPAIRED IAW ER/A 094719-14MA.

Part: CARGO TRACK — CORRODED (BS 1041) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON TIE TRACK BETWEEN BS 1041 AND X=18 RT AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE DAMAGE, TIE TRACK WAS REPLACED IAW SRM 51-10-3, 14-21, 51-10-4, 51-30-2, 51-30-1, FROM BS 1007 TO 1155.

Part: FERRULE — BROKEN (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

BROKEN FERRULE ON FLOOR PANEL. REPLACED FERRULE IAW AMM 53-20-01-201.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,601 hrs · 45,748 cycles

DENTS ON OUTER SKIN OF C3 CARGO COMPARTMENT DOOR BETWEEN BEAMS 5, 2, 3 AND 4. SKIN WAS REPLACED IAW SRM 51-30-2.

Part: LONGERON — CRACKED (BS 1418) · airframe 63,601 hrs · 45,748 cycles

CRACKED LONGERON 2 LT BS 1418. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3, PAR 14, 21 AND 51-30-5.

Part: DOOR FRAME — CORRODED (BS 1148-1155) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROISON ON WEB OF DOOR FRAME BETWEEN BS 1148 - 1155 AND BETWEEN LONGERON 25 TO 26R AT AFT CARGO COMPARTMENT. THE WEB WAS REPAIRED IAW SRM 53-01, FIG 4 51-10-3 PAR, 14, 21, 38, AND 51-30-2.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,601 hrs · 45,748 cycles

CRACKED LONGERON 16L, BS 1437 AT ACC. CRACKED LONGERON SECTION WAS REPLACED IAW DC-9/MD-80 SRM 53-14-4, FIG 2, 51-30-2, 51-30-5 PAR 8 AND 7.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 63,601 hrs · 45,748 cycles

DELAMINATED ON UPPER AND LOWER SKIN ON INBD VANE OTBD FLAP BETWEEN BS XV1=117 TO 121 AND BS XV1=124.5 APPROXIMATELY AT RT WING ING. UPPER AND LOWER SKIN ON INBD VANE OTBD FLAP BETWEEN BS=XV1=117 TO 121 AND BS -XV1=124.5 APPROXIMATELY AT RT WING REPAIRED IAW SRM 57-03D, PAR II.

Part: CARGO TRACK — CORRODED (BS 1250-1271) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1250 TO 1271 AT AFT CARGO COMPARTMENT. CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 21 AND 14.

Part: FRAME — CRACKED (BS 1437) · airframe 63,601 hrs · 45,748 cycles

CRACKED FRAME BS 1437 LONGERON 8 L. DAMAGE AREA WAS REPAIRED IAW SRM 51-70-4 AND DWG 9911840, REV DC.

Part: FERRULE — DELAMINATED (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

DELAMINATED AND MISSING FERRULES ON FLOOR PANEL. DAMAGE FERRULE REPLACED IAW AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,601 hrs · 45,748 cycles

CRACK ON LONGERON 4 LT AND BS 1437 AT AFT ACCESORIES COMPARTMEMT. CRACK ON LONGERON 4LT WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-5, 51-10-3.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON BARREL NUTS HORIZONTAL STABILIZER XH=7, NR 11, 12 AND 14. ALSO XH=-7, 10, 11 AND 13. REPAIR WAS PERFORMED IAW ER/A 545116-14 REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 1470C. FUEL ACCESS PLATE WAS REPLACED.

Part: STRUCTURE — CRACKED (BS 1309) · airframe 63,601 hrs · 45,748 cycles

CRACKED CLIP ON BS 1309 AND LONG BETWEEN LONG 15 AND 16RT SUDE AT C PAX. CLIP WAS REPLACED IAW SRM 51-30-5 AND DWG 9912243.

Part: STRUCTURE — CORRODED (SPOILER) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON HOLE INBD, OTBD LUG OF LEVER SUPPORT AT RT INBD FLIGHT SPOILER. THIS REPAIR WAS PERFORMED IAW ER/A 545123-14, REV ORIGINAL.

Part: FLOOR PANEL — DELAMINATED · airframe 63,601 hrs · 45,748 cycles

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

Part: STRUCTURE — CORRODED (SPOILER) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON HOLE OTBD LUG OF LEVER SUPPORT AT RT OTBD FLIGHT SPOILER. REPAIR WAS PERFORMED IAW ER/A 545124-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AREA OF FUEL ACCESS PLATE NR 1371C. FUEL ACCESS PLATE WAS REPLACED.

Part: STRUCTURE — CORRODED (SPOILER) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON HOLE OTBD LUG OF LEVER SUPPORT AT LT FLIGHT SPOILER. THIS REPAIR WAS PERFORMED IAW ER/A 545124-14, REV ORIGINAL.

Part: STRUCTURE — CORRODED (SPOILER) · airframe 63,601 hrs · 45,748 cycles

ELONGATED HOLE INBD LUG OF LEVER SUPPORT AT LT INBD FLIGHT SPOILER. THIS REPAIR WAS PERFORMED IAW ER/A 545123-14, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (NLT WW) · airframe 63,601 hrs · 45,748 cycles

CRACKED INTERCOSTAL X= 10 AND X=-10 STA Y=39 AT WHEEL/WELL AREA OF NLG. INTERCOSTAL WAS REPAIRED IAW SRM 51-30-2, 53-01 FIG 2 AND DWG 9911500, REV DH.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON HORIZONTAL STABILIZER RT BARREL NUT XH= -7 HOLE 14 . REPAIR WAS PERFORMED IAW ER/A 545116-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1361C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1355C. FUEL ACCESS PLATE WAS REPLACED.

Part: INTERCOSTAL — CRACKED (BS 1287-1309) · airframe 63,601 hrs · 45,748 cycles

CRACKED INTERCOSTAL BETWEEN BS 1287 - 1309. INTERCOSTAL WAS REMOVED TO FACILITATE THE REPAIR AND POSTERIORILY REINSTALLED IAW SRM 51-30-2 AND 51-30-5. REPAIR ACCOMPLISHED IAW ER/A 380521-14MA, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1418) · airframe 63,601 hrs · 45,748 cycles

CRACKED FRAME BS 1418 BETWEEN LONGERONS 3 LT AND 3 RT. STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-10-3 PAR 21 AND 14 AND DWG 5913595, REV AP.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1462C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1367C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1414C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1456C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1454C. FUEL ACCESS PLATE WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 1041-1060) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB UPPER AND LOWER SURFACE FROM 1041-1060 BETWEEN X=54 -X=60 LT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 131, A-6, 51-10-3 PAR 14, 21, 38 , 51-30-2, 51-30-5, 51-30-1.

Part: FLOOR PANEL — PUNCTURED · airframe 63,601 hrs · 45,748 cycles

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

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1472C. ACCESS WAS REPLACED IAW SRM 51-22-2A, COND. II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 2302C. FOUND NR 1 HOLE OUT OF LIMITS WITH .671" BUSHING WAS FABRICATED AND INSTALLED WITH OD .439" AND COUNTERSINK .635" IAW SRM 51-22-2A PAR 6, COND. II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1466C. FOUND NR 1 HOLE OUT OF LIMITS WITH .571" BUSHING WAS FABRICATED AND INSTALLED WITH OD .329" AND COUNTERSINK .508" IAW SRM 51-22-2A, PAR 6, COND II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NR 1410C. ACCESS WAS REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: PAN — CRACKED (BS 1193-1212) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN STRUCTURE AT FWD LOWER CORNER AND AFT UPPER CORNER BETWEEN BS 1193-1212 RT SIDE. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND ER/A 487747-14MA, REV ORIGINAL AND 493648-14MA REV: A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1464C. FOUND NR NR 1 HOLE OUT OF LIMITS WITH .540" BUSHING WAS FABRICATED AND INSTALLED WITH OD .329" AND COUNTERSINK .517" IAW SRM 51-22-2A, PAR 6 COND II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA AT FUEL ACCESS PLATE 1335 C. CORROSION WAS REMOVED, ACCESS WAS MEASURED AND WAS FOUND NR 1 HOLE OUT OF LIMITS WITH .675", BUSHING WAS FABRICATED AND INSTALLED WITH OD .439", COUNTERSINK .635" IAW SRM 51-22-2A, PAR 6, CONDITION II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1307C. ACCESS WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: CUSP WEB — CORRODED (BS 541-560) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB UPPER AND LOWER SURFACE BS 541-560 BETWEEN X=54-X=60 LT SIDE. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-14 , 51-10-3 PAR 14/21, 51-30-1, 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 2301C. ACCESS WAS REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: CUSP WEB — CORRODED (BS 1231-1250) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 1231-1250 AND X=-54 TO X=-60. CORROSION WAS REPAIRED IAW SRM 53-05, 51-30-5, 51-10-3, PAR 14, 21, 38. REPAIR DOUBLER WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1436C. ACCESS WAS REPLACED IAW SRM 51-22-2A CONDITION II.

Part: CHANNEL — CRACKED · airframe 63,601 hrs · 45,748 cycles

CRACK ON CHANNEL AT FLOOR PANEL NR 693A. CRACK ON CHANNEL WAS ATTENDED IAW SRM 53-05 FIG 131B, SH 3, 51-10-3 PAR 14, 21 AND 38, 51-30-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1478C. FOUND 5 HOLE OUT OF LIMITS, MAXIMUM HOLE MEASURED WITH .543" BUSHING WAS FABRICATED AND INSTALLED WITH OD .329" COUNTERSINK .509" IAW SRM 51-22-2A, PAR 6, CONDITION II.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,601 hrs · 45,748 cycles

CRACKED FLOOR PANEL 693A. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05,51-30-2.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

SURFACE CORROSION ON RT CUSP WEB BETWEEN BS 579-598 AND X=-54 TO X=-60, CARD 83, ZONE 201. CUSP WEB RT 503 TO 598 WAS REPLACED IAW SRM 51-30-1, AMM 20-30-1, 51-30-2, 51-30-5, DWG 9930538, REV BF.

Part: FLOOR PANEL — PUNCTURED (NOT REPORTE) · airframe 63,601 hrs · 45,748 cycles

PUNCTURE ON FLOOR PANEL 769G. THE FLOOR PANEL WAS REPAIRED SRM 53-01, FIG 4 , 51-30-2.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACED IAW SRM 51-10-2, DWG 9957828, REV: Y.

Part: CUSP WEB — CORRODED (BS 1028-1030) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB, UPPER AND LOWER, BS 1028 TO 1030 BETWEEN X=54-X=60 LT SIDE. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 131-A -13 , 51-30-2, 51-30-5 , 51-10-3 PAR 14, 21, 38.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,601 hrs · 45,748 cycles

CRACK ON FLOOR PANEL NR 389A AND DISBONDED RUBSTRIP AT CAB PAX. CRACK WAS REPAIRED AND STRIP WAS BONDED IAW SRM 53-01, FIG 4 , 51-30-2 , 51-20-0.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,601 hrs · 45,748 cycles

DAMAGE METALIZED ON RUDDER. DAMAGE METALIZED WAS REPAIRED IAW ERA NR 092613-14MA.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,601 hrs · 45,748 cycles

CRACK ON LONGERON 7R, BS 1338. LONGERON REMOVED AND REPLACED IAW SRM 51-30-5, FABRICATED IAW SRM 53-14-3, FIG 4.

Part: CUSP WEB — CORRODED (BS 948-961) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB PREVIOUS REPAIR FROM BS 948 - 961, X 54 - X 60, LT SIDE. DOUBLER PREVIOUS REPAIR WAS REMOVED IAW SRM 51-30-5, PAR 8. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131, A-13. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5, PAR 7. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: BOLT — DAMAGED (ENGINE MOUNT) · airframe 63,601 hrs · 45,748 cycles

DAMAGED UPPER YOKE BOLT TREADS TO ATTACH FWD VIBRATION ABSORBER. UPPER YOKE BOLT WAS REPLACED IAW AMM 71-20-03-201.

Part: BEARING — CORRODED (RUDDER YOKE) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RUDDER YOKE BEARING. BEARING WAS REPLACED IAW AMM 27-20-03.

Part: CUSP WEB — CRACKED (BS 864-868) · airframe 63,601 hrs · 45,748 cycles

CRACK ON CUSP WEB BS 864-868 BETWEEN X=+54 TO X=+60. REMOVED DAMAGE AND FABRICATE A REPAIR IAW SRM 53-05, FIG 131, A-1, SH 1.

Part: PAN — CRACKED (BS 1174-1193) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN STRUCTURE AT FWD LOWER CORNERS BETWEEN BS 1174-1193 RT SIDE. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-05 FIG 122 AND ERA 487747-14MA REV ORIGINAL AND REV A.

Part: PAN — CRACKED (BS 1022-1060) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN STRUCTURE AT AFT LOWER CORNERS BETWEEN BS 1022-1041 AND BS 1041-1060 LT SIDE. REPAIR PARTS WERE FABRICATED, AND INSTALLED IAW SRM 53-05, FIG 122 AND ER/A 487747-14MA, REV ORIGINAL AND REV A.

Part: PAN — CRACKED (BS 886-905) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 886-905, RT AT CABIN PAX. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 122 AND ERA 487747-14MA, REV: ORIGINAL.

Part: VANE — WORN (RT WING TE FLAP) · airframe 63,601 hrs · 45,748 cycles

WEAR ON PREVIOUS REPAIR UPPER SURFACE ON OTBD VANE, OTBD FLAP, BS XV2-371 AT RT WING. UPPER SURFACE ON OUTBD VANE, OUTBD FLAP, BS XV2-371 RT WING WAS REPAIRED IAW SRM 57-03 PAR II.

Part: WEB — CORRODED (BS 139-140) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON WEB, BS 139-140, X=15 LT. WEB WAS REPAIRED IAW SRM 53-01, FIG 4, 51-30-2 , 51-10-3, PARA 21, 14, 36.

Part: LONGERON — CRACKED (BS 541) · airframe 63,601 hrs · 45,748 cycles

CRACKED LONGERON 4R, BS 541 AT PAX CABIN. REPAIR THE LONGERON IAW SRM 53-02, FIG 18 AND 51-30-2 , 51-30-5.

Part: CUSP WEB — CORRODED (BS 722-731) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 722-731 AND X=-54 TO X=-60, CARD 86 ZONE 201. TRACK WAS REMOVED, DOUBLER WAS REMOVED, DOUBLER AND RING DOUBLER WERE FABRICATED, REPAIR PARTS WERE TREATED AND PAINTED, DOUBLERS AND RING DOUBLERS WERE INSTALLED TRACK WAS INSTALLED, CIC WAS APPLIED IAW SRM 51-30-1, 55-05, FIG 131A-13, 51-30-5, 51-10-3, 14, 21, 38, 51-30-2.

Part: CUSP WEB — CORRODED (BS 826-845) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB UPPER AND LOWER SURFACE FROM BS 826-845 BETWEEN X=44-X=60 LT SIDE. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 131A-6 , 51-10-3, PAR 14, 21, 51-30-5, 51-30-2.

Part: SKIN — DAMAGED (BS 346-750) · airframe 63,601 hrs · 45,748 cycles

LIGHTNING STRIKE ON WINDOW BELT FWD AREA FROM STA 370-389, 346-365 AND 731-750. LIGHTNING STRIKES WERE REPAIRED BY BLENDED OUT AND DIMENTIONS AS FOLLOW: (UT) WAS ACCOMPLISHED IAW NDT-SPM 04-00-07, PAR 5, FIG 3 ON 370-389 RT AT FWD SECTION, ORIGINAL THICKNESS 0.110" AND REMAINIG 0.108" ON BS 346-365 RT AT FWD SECTION, ORIGINAL THICKNESS 0.140" AND REMAINING 0.138" BOTHS ARE IN ZONE 3, ON STAY=731-750 RT AT FWD SECTION, ORIGINAL THICKNESS 0.145" AND REMAINING 0.143" IT IS IN ZONE 1, ALL ARE IN NO CRITICAL ZONE, THEREFORE ALL ARE WITHIN LIMITS IAW SRM 53-05, FIG 111. PANAMETRICS OLYMPUS 38DL SONOPEN V260.EXP.DATE 27-OCT-16. PERFORM DECAL VISUAL INSPECTION EVERY C-CHECK IAW TOPP 30-10-70, PAR I, PAGE 13.

Part: SEAT TRACK — CORRODED (BS 200-256) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON SEAT TRACK -22 BETWEEN BS 200 -256. SEAT TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21.

Part: BEAM — CRACKED (PAX DOOR) · airframe 63,601 hrs · 45,748 cycles

CRACKED BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR L1. BEAM WAS REPAIRED IAW SRM 52-05-D, FIG 97, SHEET 3, 51-30-2, 51-30-5, 51-10-3 PAR 14/21 AND 51-10-2.

Part: CUSP WEB — CORRODED (BS 522-541) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB PREVIOUS REPAIR FROM BS 522-541 BETWEEN X=54-X=60 LT SIDE. REPLACED IAW SRM 51-30-1, 51-30-5, 51-30-2, 53-05, FIG 131A-7, 51-10-3 PAR 21, 14 AND 38.

Part: CUSP WEB — CORRODED (BS 788-807) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT CUSP WEB, PREVIOUS REPAIR BETWEEN BS 788-807 AND X=-54 TO X=-60. PREVIOUS DOUBLER WAS REMOVED, REPAIR PARTS WERE FABRICATED, REPAIR PARTS WERE INSTALLED, CIC WAS APPLIED, IAW SRM 51-30-2, 53-05, FIG 131A-2, 51-10-3, PAR 14, 21, 38.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 598-617 AND X=-54 TO X=-60. CUSP WEB WAS ATTENDED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 131A-7, 51-10-3 PAR 14, 21 AND 38.

Part: CUSP WEB — CORRODED (BS 996) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 996 AND X=-54 TO X=-60. REMOVE AND INSTALLED REPAIR PARTS ON RT CUSP WEB BETWEEN BS 996 AND X=-54 TO X=-60 IAW SRM 51-30-3 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 370-389) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT SEAT TRACK PLUG X=-54 BETWEEN BS 370 TO BS 389. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED, CIC WAS APPLIED IAW SRM 51-10-3 PAR 38, 51-30-1, 53-05 FIG 4A, SH 1.

Part: SEAT TRACK — CORRODED (BS 316-982) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON SEAT TRACK PLUGS BS 316-982 AT X=22. SEAT TRACK PLUGS REPLACED IAW SRM 51-30-1, 53-05, FIG 4A, SH 1 AND 51-10-3, PAR 38.

Part: SKIN — CRACKED (PAX DOOR) · airframe 63,601 hrs · 45,748 cycles

CRACKED EXTERNAL REPAIR DOUBLER FWD LOWER CORNER AT PASSENGER ENTRANCE DOOR. REPAIR DOUBLER WAS REPLACED IAW SRM 51-30-2, 52-05D FIG 37, 51-10-3, PAR 14/21.

Part: BUSHING — CORRODED (RT MLG) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON INNER SURFACE OF FITTING BUSHING RT MLG. CORROSION ON BUSHING BORE RT WAS REMOVED IAW DWG SR 09570087, REV B, NOTE II, MEASURE AFTER REWORK ID 2.337", THEREFORE IS WITHIN LIMITS FOR REPAIR IAW DWG SR09570087, REV: B, NOTE II.

Part: CUSP WEB — PUNCTURED (BS 484-492) · airframe 63,601 hrs · 45,748 cycles

PUNCTURED RT CUSP WEB BETWEEN BS 484-492 AND X=-44 TO X=-54. PUNCTURED ON RT CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 51-10-3 PAR 19 AND 21 AND 38, 53-05, FIG 131A-17.

Part: SEAT TRACK — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON RT SEAT TRACK PLUG X=-22 BETWEEN BS 1231 TO 1212. PLUG WAS REMOVED. NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-05, FIG 4A, SH1.

Part: PAN — CRACKED (BS 237-258) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN AFT LOWER CORNER BETWEEN BS 237-258 LT AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED, WAS PERFORMED IAW SRM 06-10-01-001. NO CRACKS. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122.

Part: PAN — CRACKED (BS 769-788) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN STRUCTURE UPPER FWD AND LOWER AFT CORNERS BETWEEN BS 788 AND BS 769 LT SIDE. DAMAGE AND FASTENERS WERE REMOVED, WAS PERFORMED IAW NDT SPM 06-10-01-001, WO CRACKS. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-5, 51-30-2, 53-05, FIG 122.

Part: PAN — CRACKED (BS 769-788) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 769-788 RT AT CABIN PAX. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5, 51-30-2.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,601 hrs · 45,748 cycles

WORN PREVIOUS REPAIR DOUBLERS ON AFT AND FWD LOWER CORNER AT FWD CARGO COMPARTMENT DOOR. REPAIR DOUBLERS WERE REPLACED IAW SRM 51-30-2 AND ER/A 486624-14 REV ORIGINAL.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 63,601 hrs · 45,748 cycles

CRACK ON MID CARGO COMPARTMENT DOOR SKIN NEXT TO OPEN, CLOSE HANDLE HSG MID CARGO COMPARTMENT DOOR SKIN WAS REPAIRED IAW ER/A 486446, MA REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 389-408) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

SEVERE CORROSION ON RT CUSP WEB BETWEEN BS 389-408 AND X=-54 TO X=-60. CUSPS WEB WERE REPAIRED IAW SRM 53-05, FIG 131A AND 51-10-3, PAR 14, 21, 38.

Part: PAN — CRACKED (BS 655-674) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 655-674, RT AT CABIN PASSENGER DAMAGE AND FASTENER WERE REMOVED IAW SRM 53-05, FIG 122 AND 51-30-2.

Part: PAN — CRACKED (BS 788-807) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 788-807RT CABIN PASSENGER. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED, REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 984-1003) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON CUSP WEB PREVIOUS REPAIR FROM BS 984-1003 BETWEEN X=54-X=60 LT SIDE. CUSP WEB PREVIOUS REPAIR WAS REPLACED IAW SRM 51-30-5 AND 53-05, FIG 131A-14.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 63,601 hrs · 45,748 cycles

DELAMINATED ON INBD AT ANTI-FLOAT TAB UPPER, LOWER SURFACE LT ELEVATOR. DUE TO EXCESSIVE DAMAGE REPLACED IAW SRM 55-04, PAR 2C.

Part: PAN — CRACKED (BS 617-636) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 617-636 RT AT CABIN PAX. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.

Part: PAN — CRACKED (BS 275-294) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN AFT LOWER CORNER BETWEEN BS 294-275 LT AT CABIN PAX. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED ANS INSTALLED IAW SRM 51-30-5, 51-30-2.

Part: CUSP WEB — CORRODED (BS 370-389) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

SEVERE CORROSION ON RT CUSP WEB BETWEEN BS 370-389 AND X=-54 TO X=-60. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 131A AND 51-30-2, 51-10-3 PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 419-703) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON SEAT TRACK PLUG BS 419 TO 422, 455 TO 458, 671 TO 674, 701 TO 703 AT X=54 ON CABIN PASSENGER PLUGS WERE REMOVED, NEW PLUGS WERE INSTALLED IAW SRM 51-30-1, 53-05 FIG 4A, SH 1.

Part: PAN — CRACKED (BS 351-370) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN FWD UPPER CORNER BETWEEN BS 351-370 RT AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED REPAIR PARTS WERE FABRICATED. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5.

Part: PAN — CRACKED (R1 DOOR FRAME) · airframe 63,601 hrs · 45,748 cycles

CRACKED PAN ABOVE FRAME NR 4 FROM AREA AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03 D FIG. 3.

Part: PAN — CRACKED (BS 788-807) · airframe 63,601 hrs · 45,748 cycles

CRACK ON RING PAN STRUCTURE AT UPPER FWD CORNER BETWEEN BS 788 AND 807 ALSO UPPER FWD CORNER BETWEEN BS 807 AND 826 LT SIDE. RING PAN WERE REPAIRED IAW SRM 53-05, FIG 122, 51-30-2 AND 51-30-5 CRACK LONG WAS 0.125" HFEC WAS PERFORMED NO CRACKS WERE FOUND AFTER TRIM OUT.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 63,601 hrs · 45,748 cycles

WEAR ON UPPER SKIN T/E OF OTBD VANE OTBD FLAP BS XV2-297 CANT AT LT WING. WEAR ON UPPER SKIN T/E OF OTBD VANE OTBD FLAP BS XV2=297 LT WING WAS REPAIRED IAW ERA 521199-14MA REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENTAREAOF FUEL ACCESS PLATE NR 1303C AND 1409C. FUEL ACCESS PLATE NR 1303C AND 1409C WERE REPLACED IAW SRM 51-22-2A CONDTION III.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1303C AND 1409C. FUEL ACCESS PLATE NR 1303C AND 1409C WERE REPLACED IAW SRM 51-22-2A, CONDTION III.

Part: CUSP WEB — CRACKED (BS 674-693) · corrosion level 2 · airframe 63,601 hrs · 45,748 cycles

CORROSION ON LT CUSP WEB, OUT LIMITS, BETWEEN BS 674 TO 693. CORROSION OUT LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A-14 51-30-5, 51-30-2, 51-10-3 PAR 14, 21, 26, 38.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

CRACK ON CHANNEL AT FLOOR PANEL 1003F. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, AR 145.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

CRACKED CHANNEL ON FLOOR PANEL 927E. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, PAR 145.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,601 hrs · 45,748 cycles

CRACK ON CHANNEL, AFT SIDE AT FLOOR PANEL 1003A. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, PAR 145.

Part: FAIRING — CRACKED · airframe 62,492 hrs · 45,039 cycles

TAIL TOP, RT LWR BANANA FAIRING LWR EDGE HAS TWO 1 INCH LONG CRACKS AT 36 & 40 INCHES AFT OF FWD END. REPAIRED IAW ER/A 464895-14MA, REV F.

Part: FAIRING — CRACKED · airframe 62,492 hrs · 45,039 cycles

TAIL TOP, RT UPPER BANANA FAIRING UPPER EDGE HAS A 15 INCH LONG CRACK ABOVE AFT ATTACH POINT. REPAIRED IAW ER/A 464895-14MA REV F.

Part: LONGERON — DAMAGED (BS 1341) · airframe 62,492 hrs · 45,039 cycles

TAIL INTERIOR A .2500" ALUMINUM LINE IS CONTACTING LONGERON 13R AT BS 1341. REPAIRED IAW SRM 53-02, FIG 18 AS A REF.

Part: SKIN — GOUGED (VERTICAL STAB) · airframe 62,492 hrs · 45,039 cycles

VERTICAL STABILIZER TIP MID SECTION RT AFT SKIN HAS 2 DEEP 3" LONG GOUGES, ABOVE HORIZONTAL STABILIZER HINGE. REPAIRED IAW PRI 540664-14, REV 0 AND C/W ERA 540664-14, REV A.

Part: SKIN — WORN (VERTICAL STAB) · airframe 62,492 hrs · 45,039 cycles

VERTICAL STABILIZER LT SIDE SKIN IS WORN AT HORIZONTAL STABILIZER SIDE LOAD ROLLER. REPAIRED IAW PRI 540677-14, REV 0 AND WAITING FOR FINAL ER/A.

Part: SKIN — CRACKED (BS 1410) · airframe 62,492 hrs · 45,039 cycles

SKIN BENEATH DIAMOND DOUBLER CRACKED BS 1410 AT LONGERON 2L. REPAIRED IAW PRI 540097-14, REV 0 AND WAITING FOR FINAL ER/A.

Part: DOUBLER — CRACKED (BS 1410) · airframe 62,492 hrs · 45,039 cycles

TAIL INTERIOR - DIAMOND SHAPED ACFT SKIN DOUBLER AT BS 1410 IB OF L2L IS CRACKED 2 PLACES. SEE NR FOR ADDITIONAL INFORMATION 001-0279:5300-2551/018 00077, WORK TO BE ACCOMPLISHED ON NR 137 AND PRI/ERA 540097-14AD, REV ORIG.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 61,632 hrs · 44,427 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE UNDERSEAT HARNESS. THE WIRE HARNESS WAS REPAIRED AND THE SYSTEM RETURNED TO NORMAL OPERATION. LP 7126129.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 61,031 hrs · 44,017 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROWS 1-12 FLOOR LIGHTS INOPERATIVE AFTER ERA 531288-14MA WAS COMPLETED. MAINTENANCE R & R CONNECTOR PLUG P1-791 ON B5-211 IAW WDM 33-51-14 AND REPLACED B5-211 POWER SUPPLY AND BATTERY. OPS CKS NML IAW AMM 33-53.

Part: SLIDE — NO TEST (TAILCONE) · airframe 61,006 hrs · 44,003 cycles

MAINTENANCE DEPLOYED THE TAILCONE IAW TAILCONE DEPLOYMENT WC 2562-7267. THE SLIDE INITIALLY FAILED TO INFLATE. APPROXIMATELY 45 SECONDS AFTER TAILCONE DEPLOYMENT, THE SLIDE DID INFLATE COMPLETELY AND REMAINED INFLATED FOR OVER 10 MINS. MAINTENANCE INSTALLED A NEW TAILCONE SLIDE ASSY.

Part: PBE — DAMAGED (COCKPIT) · airframe 60,500 hrs · 43,656 cycles

MAINTENANCE DISCOVERED THAT THE COCKPIT PROTECTIVE BREATHING EQUIPMENT BEHIND THE CREW SEATS WAS DAMAGED. THE PBE WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,903 hrs · 43,244 cycles

OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 27-30. REPLACED BATTERIES IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 59,801 hrs · 43,185 cycles

MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTS ON SEAT 25ED WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,407 hrs · 42,908 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 22-30 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 58,843 hrs · 42,516 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 13D WAS INOPERATIVE. FOUND A BROKEN WIRE, REPAIRED AND SYSTEM RETURNED TO NORMAL OPERATION.

Part: CABLE — WORN (TAILCONE) · airframe 57,375 hrs · 41,616 cycles

DURING SCHEDULED CHECK, TAILCONE TELEFLEX CABLE WAS NOTED TO BE WORN. SPIRAL WRAP WAS SHOWING WEAR & COMING OFF OF THE CABLE. REPLACED TELEFLEX CABLE IAW AMM 53-53-02-201-1.

Part: FRAME — CRACKED (BS 1485) · airframe 57,375 hrs · 41,616 cycles

WEB ON LEFT SIDE OF CANTED FRAME BS 1485 CRACKED AT 10:00 POSITION. REPAIRED IAW ER/A 519100-14, REV O.

Part: SKIN — CRACKED (BS 1380) · airframe 57,375 hrs · 41,616 cycles

MULTIPLE CRACKS NOTED ON SKIN BS 1380, 14R JUST ABOVE PYLON. REPAIRED IAW ER/A 519023-14 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: PIN — CORRODED (TAILCONE RELEASE) · airframe 57,372 hrs · 41,614 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE TEE PIN AND BUSHINGS WERE FOUND TO BE RUSTED. THE TEE PIN BUSHINGS AND ASSOCIATED HARDWARE WERE REPLACED IAW AMM 53-53 AND THE REQUIRED FUNCTIONAL CHECKED AND INSPECTION WAS ACCOMPLISHED.

Part: SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 57,372 hrs · 41,614 cycles

CORROSION FOUND AT THE AFT CARGO DOOR SILL. CORROSION WAS BLENDED AND EXCEEDED SRM MINIMUMS. REPLACED C3 CARGO BEAM IAW DWG 5930483.

Part: GAUGE — OBSTRUCTED (TAILCONE SLIDE) · airframe 57,372 hrs · 41,614 cycles

DURING SCHEDULED CHECK, THE TAILCONE SLIDE PRESSURE GAUGE WAS FOUND TO BE OBSTRUCTED FROM VIEW BY TAPE. TAILCONE SLIDE COVER WAS REPLACED IAW AMM 25-62-01 AND WC 2500-4484. REQUIRED INSPECTION COMPLETED.

Part: HOOK AND LOOP — MISSING (TAILCONE SLIDE) · airframe 57,372 hrs · 41,614 cycles

DURING SCHEDULED CHECK, HOOK AND LOOP FOR THE RELEASE LANYARD NORMALLY LOCATED ON THE TOP OF THE TAILCONE SLIDE COVER WAS MISSING. TAILCONE SLIDE COVER WAS REPLACED IAW AMM 25-62-01 & WC 2500-4484. THE REQUIRED INSPECTION WAS ALSO COMPLETED.

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 57,372 hrs · 41,614 cycles

DURING SCHEDULED CHECK, PLASTIC COATED TAILCONE RELEASE CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH THE CONDUIT CONNECTION TO THE TEE PIN. CABLE REPLACED IAW AMM 53-53 AND THE FUNCTIONAL CHECKED AND INSPECTION WAS COMPLETED.

Part: SKIN — CORRODED (ZONE 100) · airframe 57,372 hrs · 41,614 cycles

CORROSION FOUND ON THE AFT CARGO SKIN UNDER THE SEAL DEPRESSOR FROM STA 1155-1212. REPAIRED IAW ER/A 519203-14.

Part: SKIN — CRACKED (BS 1437) · airframe 57,372 hrs · 41,614 cycles

DURING SCHEDULED CHECK, A SKIN CRACK WAS NOTED AT BS 1437 BETWEEN LONGERON 2 & 3L. REPAIRED IAW ER/A 519049-14.

Part: GUSSET — CORRODED (BS 1212) · corrosion level 2 · airframe 57,372 hrs · 41,614 cycles

DURING SCHEDULED CHECK, AFT CARGO DOOR FRAME CORNER GUSSET AT BS 1212 FOUND CORRODED AND OUT OF LIMITS. REPAIRED IAW SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 57,372 hrs · 41,614 cycles

AFT CARGO DOOR FRAME FLOOR SUPPORT TEE BS 1136-1218-CORROSION. REPLACED T-SECTION DUE TO CORROSION OUT OF LIMITS. REPLACED IAW DWG 5936660.

Part: RELEASE MECH — FAILED (TAILCONE) · airframe 57,372 hrs · 41,614 cycles

ACFT FAILED INITIAL DROP CHECK OF THE TAILCONE RELEASE SYS. RELEASE MECHANISM CAM EXCEEDED 45 POUNDS ALLOWABLE PULL LIMIT. TEE PIN ADJUSTED IAW MANUAL AND THE SYSTEM RECHECKED. TAILCONE DROPPED AT 10 POUNDS OF MEASURED PULL FORCE. THE RII STEPS WERE COMPLETED AND SIGNED OFF.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT) · airframe 56,768 hrs · 41,177 cycles

DURING LINE INSPECTION, THE FLOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 20. MX ADJUSTED AND SECURED A LOOSE WIRING HARNESS IAW AMM 33-53 AND THE SYS CHECKED GOOD.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT) · airframe 56,768 hrs · 41,177 cycles

DURING LINE INSPECTION IN MEM, THE FLOOR ESCAPE PATH LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 12. MX ADJUSTED AND SECURED A LOOSE WIRING HARNESS IAW AMM 33-53 AND THE SYS CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 56,320 hrs · 40,863 cycles

SEAT MOUNTED EMERGENCY PATH LIGHT INOPERATIVE AT ROW 13D. SECURED LOOSE CONNECTOR AT SIDEWALL OPERATION CHECKS OK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,996 hrs · 39,346 cycles

CORROSION ON SEAT TRACK LBL 44 BS 218 MAIN CABIN. REMOVED EXISTING SEAT TRACK SPLICE FROM BS 198-228-LBL 44 PER DC9/MD80 SRM 51-30-5 STEP 8 A,B. INSTALLED SEAT TRACK P/N 5936566-75 LBL 44 BS 198 BS 228 IAW MD88 SRM 53-05 PAR 32 VIEW A. REPAIR ACCOMPLISHED AT ATS/PAE NRC 00029 WORK ORDER 717808.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,996 hrs · 39,346 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND CABIN CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROW 23-26. REPLACED BATTERY PACK B5-104 PER WDM/AMM. OPS CHECKED GOOD.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 53,654 hrs · 39,151 cycles

VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION IN FASTENER HOLE, LOWER LEFT AFT CORNER HOLE.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 53,654 hrs · 39,151 cycles

VERTICAL STAB REMOVABLE LEADING EDGE HAS CRACK INDICATION AT LOWER LEFT AFT CORNER HOLE. REPAIRED PER ERA501898-14AD REV ORIGINAL.

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 53,112 hrs · 38,810 cycles

FLIGHT CREW DIVERTED FOLLOWING THE "FIRE WARNING" ILLUMINATING FOR THE NR 1 ENGINE. MAINTENANCE FOUND DAMAGE TO UPPER ENGINE COWL AND NOSE COWL FROM A BLOWN ANTI-ICE DUCT. NOSE COWL ANTI-ICE DUCT AND ANTI-ICE VALVE WERE BOTH REPLACED ALONG WITH THE UPPER ENGINE COWL AND NOSE COWL.

Part: WIRE — BROKEN (CABIN) · airframe 53,091 hrs · 38,794 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE RED EMERGENCY PATHWAY LIGHTING IN THE GALLEY WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE UNDER THE CARPET AND REPLACED THE LIGHT ASSEMBLY. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 52,633 hrs · 38,496 cycles

EMERGENCY LIGHTS AT 18 ED ARE INOPERATIVE. MAINTENANCE FOUND BROKEN HARNESS AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,531 hrs · 37,739 cycles

DURING LINE CHECK MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED OVERWING EMERGENCY EXIT POWER SUPPLY AND BATTERY PER AMM 33-53. OPERATION OF LIGHTS NOW CHECKS OK.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 50,190 hrs · 36,890 cycles

DURING LINE CHECK MX FOUND FWD RED EMERGENCY PATH LIGHTING, FLOOD LIGHT INOPERATIVE. MX FOUND CUT WIRE AND SPLICED IT IAW STANDARD WIRING PRACTICE, MM CHAP 20. OPERATION OF LIGHT NOW CHECKS OK.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 48,758 hrs · 35,913 cycles

EXFOLIATION CORROSION ON MID CARGO COMPT LOWER DOOR JAMB BEAM BTWN ST Y=636 AND 693. REPAIRED IAW SRM 53-05, FIG 123.

Part: SUPPORT — CORRODED (RT MLG) · airframe 48,758 hrs · 35,913 cycles

PITTING CORROSION ON GEAR FITTING BORE OF BUSHING AT RT MLG REPAIRED IAW EA 09-093855-03AD, REV B 0204.

Part: GUIDE VANE — NICKED (RT WING TE FLAP) · airframe 48,758 hrs · 35,913 cycles

NICKS ON INNER SURFACE AT RT WING INBD FLAP OTBD GUIDE VANE. REPAIRED IAW SRM 57-04.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,758 hrs · 35,913 cycles

EXFOLIATION CORROSION ON AFT PASSENGER ENTRANCE DOOR LOWER JAMB BETWEEN STA Y=1350 X=4 TO X=10 AND X=-5 TO X=-9.5. REPAIRED PER ERA 481731-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,758 hrs · 35,913 cycles

HIDDEN DAMAGED ON FUSELAGE SKIN BELOW REPAIR DOUBLER AT STA Y = 582 BETWEEN LONGERON 19RT AND 21RT. REPAIRED PER ERA 481740-14 REV ORIG.

Part: FITTING — CORRODED (LT MLG) · airframe 48,758 hrs · 35,913 cycles

SCRATCHES AND PITTING CORROSION ON LT GEAR FITTING BORE OF BEARING. REPAIRED PER EA 09-093855-03AD REV B 0104.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 48,758 hrs · 35,913 cycles

CRACK ON INNER PAN BELOW FWD STOP NR 4 AT FWD CARGO. REPAIRED IAW SRM 52-05, FIG 50.

Part: PAN — DAMAGED (WINDOW) · airframe 48,758 hrs · 35,913 cycles

TOOL MARK ON WINDOW OUTER RING PAN UPPER FWD CORNER BETWEEN STA Y=446-465 AT FUSELAGE SKIN LT SIDE. REPAIRED IAW ERA 481298-14, REV ORG.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 48,758 hrs · 35,913 cycles

LIGHTNING STRIKE ON FWD LOWER SECTION OF RT WINDOW FRAME NR 16 STA Y=351-370. REPAIRED IAW ERA 481298-14, REV ORIG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,758 hrs · 35,913 cycles

EXFOLIATION CORROSION ON DOOR JAMB STA Y=370 TO Y=427 OF FWD CARGO COMPT. REPAIRED IAW SRM 53-05D, FIG 804D.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 48,758 hrs · 35,913 cycles

LIGHTNING STRIKE AND SCRIBE LINE ON UPPER AND LOWER SECTION OF RT WINDOW FRAME NR 26 BTW STA Y=446-465. REPAIRED IAW ERA 481298-14, REV ORG.

Part: SKIN — CRACKED (BS 192 L22L) · airframe 48,758 hrs · 35,913 cycles

FUSELAGE SKIN CRACKED AT STA Y=192 AND LONGERON 22 LT. REPAIRED IAW EA 09-069085-12AD REV E ME 02.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 48,758 hrs · 35,913 cycles

LIGHTNING STRIKE ON LOWER SECTION OF RT WINDOW FRAME NR 14 BETWEEN STA Y=332-351. REPAIRED IAW ERA 481298-14, REV ORG.

Part: APU — FAULTY (APU BAY) · airframe 47,512 hrs · 35,173 cycles

ON CLIMBOUT SMOKE IN MID AND AFT CABIN SMOKE ALARMS WENT OFF, RETURNED TO LGA. FOUND APU INLET CONTAMINATED WITH OIL. RAN APU SEVERAL TIMES TO INSPECT FOR LEAKS. NO LEAKS FROM APU COMPONENTS FND OIL LEAKING AT FWD POSITION OF APU DOOR. SUSPECT INTERNAL APU LEAK. APU WILL BE PLACED ON MCO. PERFORMED OP 5088 AND OP 5089.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,044 hrs · 32,418 cycles

ELECTRIC ODOR IN OVERHEAD LIGHTS AROUND ROW 38. RAN APU TURNED. ON CABIN LIGHTS. MADE SEVERAL PASSES THRU CABIN. CHECKED LOWER BB. NO SMOKE OR ODOR SOURCE NOTED.

Part: PSEU — INTERMITTENT (MLG) · airframe 33,786 hrs · 26,112 cycles

INTERMITTENT UNSAFE GEAR INDICATION (LEFT MAIN). REPLACED PSEU.

Part: PSEU — FAILED (MLG) · airframe 33,786 hrs · 26,112 cycles

ON APPROACH HAD LT MLG UNSAFE INDICATION. A/C LANDED WITH GEAR DOORS DOWN DUE TO ALT GEAR EXTENSION. A/C WAS FERRIED TO BOS FOR GEAR MTC. IN BOS CHECKED OUT ALL 3 LT GEAR PROX SWITCHES WITH ELEC TEST KIT. ALL CHECKS OK. SHOOK DOWN WIRING HARNESS FOR ALL 3 PROX SWITCH CHECKS. JACKED AND CYCLED GEAR. ALL CHECKS OK. REPLACED PSEU PER MM.

Part: WIRE — BROKEN (RELAY) · airframe 32,804 hrs · 25,459 cycles

WHILE T/S FOR RT GEN INOP, APU GOT TRIPPED OFF WITH CROSS-TIE LOCKOUT, FOUND BROKEN TERMINAL ON RELAY R2-40. TERMINAL HAD ARCED AND WORN ON A WIRE BUNDLE CAUSING DAMAGED WIRING. ARCING WAS FOUND WHILE AC ON GROUND DURING MTC. REPLACED RELAY AND REPAIRED DAMAGED WIRING.

Part: STARTER — SEIZED (NR 2 ENGINE) · airframe 32,129 hrs · 25,006 cycles

ON ENG START WOULD NOT ACCELERATE ENGINE PAST 16 PERCENT AND A TAILPIPE FIRE ENSUED. REPLACED SEIZED STARTER.

Part: PISTON — CORRODED (NLG) · airframe 31,780 hrs · 24,757 cycles

NLG PISTON HAS HAD DIA 9 MACHINED TO 2.8045 INCH. DAMAGE REWORKED PER 339514-14.

Part: FCU — MALFUNCTIONED (NR 2 ENGINE) · airframe 30,729 hrs · 24,021 cycles

NR 2 ENGINE ROLLED BACK DURING LEVEL OFF AT 8000 FT. ENGINE SHUTDOWN PER CHECKLIST. MTC IN PROGRESS. REPLACED NR 2 ENGINE FCU, PWR AND FUEL CUTOFF TELE-FLEX PUSH/PULL CABLES.

Part: SKIN — DENTED (FS 200, L-17L) · airframe 27,632 hrs · 21,747 cycles

FUSELAGE / SKIN / FS 200 / LONG. 17L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND WITH A DEEP DENT JUST AFT OF THE L1 DOOR AT FS 200 AND LONGERON 17L. THE DENT WAS REMOVED WITH A CUTOUT THROUGH ALL SKIN LAYERS. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 382116-14, REV B.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 26,717 hrs · 21,064 cycles

SHORTLY AFTER T/O STRONG ELECT SMELL IN COCKPIT AND FWD GALLEY AREA RETURNED TO FIELD. FOUND BURNING SMELL COMING FROM F/C GALLEY OVEN. REPLACED OVEN AND FOOD CARRIER. OPERATED NEW OVEN, CKS GOOD AND SMELL GONE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 26,690 hrs · 21,043 cycles

AFT GALLEY COFFEEMAKER SMOKING. REMOVED AND REPLACED AFT COFFEEMAKER. A/C RIGHT SIDE COFFEEMAKER OPS CHECKS NORMAL.

Part: OVEN — DIRTY (AFT GALLEY) · airframe 25,048 hrs · 19,823 cycles

AFT GALLEY, FWD MOST OUTBOARD OVEN STARTED SMOKING (CLOSEST TO 2 LEFT DOOR). STOPPED WHEN TURNED OFF. REMOVED DIRTY FOOD TRAYS FROM OVEN. RAN OVEN, OPS CHECK NORMAL. NO MORE SMOKE NOTED.

Part: SWITCH — BURNED (COCKPIT)

SMOKE FROM LEFT SIDE OF O/H PANEL WHEN IGNITION TURNED ON FOR TAKEOFF. DISSIPATED WHEN IGNITION WAS TURNED OFF. ABORTED TAKEOFF AT 15 KTS. FOUND IGNITION SELECTOR COVERED WITH BLACK SOOT. REPLACED IGNITION SELECTOR SWITCH.

Part: O-RING — FAILED (RT HYD SYST)

RIGHT HYDRAULIC QUANTITY DECREASED TO 4 QTS IN FLIGHT WITH AMBER WARNING LIGHT ON INDICATOR. PROCEDURES FOLLOWED AND SYSTEM TURNED OFF UNTIL PRIOR TO LANDING. AFTER LANDING RIGHT QUANTITY INDICATED 2 QTS WITH NORMAL PRESSURE. FOUND PRESSURE LINE TO RUDDER POWER PACK LEAKING AT UNION. REPLACED O-RING, SERVICED RT SYSTEM AND LEAK OPS CHECK OK.

Part: SKIN — DENTED (BS 39)

TWO DENTS WERE FOUND IN THE UNPRESSURIZED AREA OF THE NOSE SKIN JUST AFT OF THE RADOME. THE DAMAGE WAS REMOVED WITH A 6 BY 17 CUTOUT. REPAIRED PER ERA 363630-14.

Part: SKIN — DENTED (BS 218)

FUSELAGE SKIN WAS FOUND DENTED AT APPROX FS 218 BETWEEN L18L AND L19L. REPAIRED PER ERA 332080-14.

Part: FRAME — CRACKED (BS 1418)

CRACK FOUND AT L2R ON THE FUSELAGE STA 1418 FRAME. CRACK WAS 1 INCH IN LENGTH. REPAIRED PER ERA 332078-14.

Part: HYD LINE — FAILED (RT ENGINE)

NR 2 HYD QTY FELL TO 3 QTS IN FLT. TURNED SYS OFF. TURNED SYS BACK ON FOR FLAP AND GEAR EXT AND QTY DROPPED TO 1 QT. REPLACED NR 2 ENGINE PRESSURE LINE.

Part: HYD LINE — LOOSE (RT MLG WW)

RIGHT HYDRAULIC QUANTITY DROPPED TO 1 WITH LOW QTY LIGHT INFLIGHT. C/W POM AND TURNED OFF RIGHT HYD PUMP, QTY INCREASED TO 5. TIGHTENED B-NUT ON ABS MANIFOLD IN RIGHT WHEEL WELL, LEAK CHKS GOOD.

Part: OIL SYST — LEAKING (APU)

CABIN AND COCKPIT FILLED WITH SMOKE AFTER T/O. PERFORMED HIGH PRESS PNEU DUCT BURN OUT PER MM 21-00-02 PGS 209 TO 216.

Part: STRIKER — CRACKED (RT MLG DOOR JAMB)

DURING D-1 LETTER CHECK, FOUND RT WW AFT DOOR JAMB STRIKER CRACKED 1 INCH. REPAIRED PER SRM 53-05 FIG 81A.

Part: SKIN — PUNCTURE (RT SERVICE DOOR)

SHOP INSPECTION FOUND INNER SKIN PUNCTURE ON FWD SERVICE DOOR. REPAIRED PER SRM 52-05, FIG 7.

Part: RIB — CRACK (RT WHEEL WELL)

FOUND DURING C-2 LETTER CHECK, CRACK IN CROSSOVER RIB AT AFT I/B CORNER OF RT WHEEL WELL CUTOUT. REPAIRED PER SRM 53-05 FIG 101.