N986DL

Part: STRUCTURE — DAMAGED (R1 DOOR) · airframe 69,803 hrs · 50,721 cycles

FOUND BOTTOM OF R1 DOOR DAMAGED AND SEAL TORN. RMVD R1 DOOR AND COMP. STEPS B 1-2 OF INST. PER MD88 M/M 52-41. COMP. INST OF R1 DOOR PER MD 88 M/M 52-41 CKS GOOD. RMVD AND RE-INST R1 DOOR SLIDE PER AMDS 2561-4964. RII C/W. (LP4755951)

Part: WIRE — LOOSE (APU GENERATOR) · airframe 69,548 hrs · 50,501 cycles

AT GATE SRQ APU GEN FELL OFF LINE, RESETS NO HELP, NO VOLTS OR FREQ. FOUND GEN FEED WIRE 3X4D2N LOOSE AND BURNED ALSO GEN. TERMINAL BURNED OFF. RMVD APU & GEN. INST. APU GEN. PER M/M 24-20. RE-INST APU PER M/M 49-10 APU LK CKS & OPS CKS. (LP0761874)

Part: CAM LOCK — MISSING (APU DOOR) · airframe 69,278 hrs · 50,261 cycles

LEFT APU DOOR MISSING ONE CAMLOCK. INSTALLED THE CAMLOCK IAW CMM 52-44-2. OK FOR SERVICE. REPORTED DUE TO POSSIBILITY THAT CAM LOCK COULD HAVE DEPARTED THE AIRCRAFT IN FLIGHT.

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 69,030 hrs · 50,057 cycles

THE CREW RETURNED THE AIRCRAFT TO ATL AFTER EXPERIENCING A COMPRESSOR STALL IN THE NR 1 ENGINE DURING CLIMB. THE ENGINE WAS KEPT RUNNING AT IDLE AND THE QRH WAS COMPLIED WITH. STATION CFR SAW FLAMES (IN THE ENGINE ONLY) SO THE FLIGHT CREW PULLED THE FIRE HANDLE FOR THE NR 1 ENGINE. MAINTENANCE FOUND TURBINE DAMAGE AND METAL IN TAIL PIPE SO THE ENGINE WAS REPLACED.

Part: DOOR FRAME — CRACKED (MLG DOOR) · airframe 67,327 hrs · 48,816 cycles

LEFT WHEEL WELL BS 937 MLG DOOR FRAME CRACKED. COMPLIED WITH HFEC IAW ERA 497265-14MA, TWO CRACKS COMING FROM PREVIOUS STOP DRILLS. REMOVED THE MLG DOOR FRAME, AND INSTALLED A NEW MLG DOOR FRAME IAW ERA 497265-14 MA, SECTION III.

Part: VANE — DEBONDED (TE FLAP) · airframe 67,327 hrs · 48,816 cycles

FLAP VANE HAS AN AREA OF DEBONDING, AFT OF GROUND SPOILER PANEL. REPLACED THE FLAP VANE IAW AMM 27-51-03

Part: VANE — DEBONDED (TE FLAP) · airframe 67,327 hrs · 48,816 cycles

FLAP VANE HAS AREA OF DEBONDING AT JUNCTION OF INBD AND OTBD FLIGHT SPOILERS. REPLACED THE FLAP VANE ASSY IAW AMM 27-51-03.

Part: VANE — DEBONDED (RT WING TE FLAP) · airframe 67,327 hrs · 48,816 cycles

RT FLAP VANE JUST AFT OF GROUND SPOILER HAS AREA OF DISBOND. REMOVE AND REPLACED FLAP FIXED VANE IAW AMM 27-51-03 AND ERA 563105-14, REV ORG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,604 hrs · 47,496 cycles

EMERGENCY LIGHTS AFT TAIL UPPER DO NOT TURN ON. CHANGED BATTERIES PACK AFT RIGHT LAV. OPERATIONAL CHECK OK.

Part: SUPPORT — DAMAGED (NLG) · airframe 65,278 hrs · 47,286 cycles

RIGHT NLG STEERING ACTUATOR DAMAGED RIGHT SIDE NLG SUPPORT WEB. INSTALLED REPAIR IAW SRM 53-05 REPAIR 47A STEP (B) (3) (B).

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,187 hrs · 47,232 cycles

CABIN CEILING EMERGENCY STANDBY LIGHT INOP FROM ROW 22 TO 26. REPLACED BATTERY PACK IN THE OVERHEAD BIN 24 RT. LIGHT CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,132 hrs · 47,184 cycles

EMERGENCY POWER CEILING LIGHTS INOP AT ROW 22-26, 33 AND 36. REMOVED & REPLACED 4 EA BATTERY PACK BATTERIES. CEILING LIGHTS AT 22-26 & 33-36. OPS CCK GOOD.

Part: ACTUATOR — INOPERATIVE (CABIN PRESSURE) · airframe 63,514 hrs · 46,022 cycles

PRESSURIZATION AUTO INOPERATIVE. MANUAL SYS WAS MARGINAL. MOVE INDICATOR 2" WITH NO CHANGE IN RATE. THEN .2500" WOULD GIVE 100 FPM. PERFORMED BITE OF BOTH AUTO PRESSURE CONTROLLERS. AC MOTOR FAULTS ON BOTH 1 AND 2. C/W AMDS W/C 2132-01033-01 AND T/S IAW TSM 21-32. R & R ACTUATOR ASSY IAW AMM 21-32. R & R OUTFLOW VALVE IAW AMM 21-32-05. COMPLETED W/C 2132-01033-01. ALL MAINTENANCE COMPLETE.

Part: B-NUT — LEAKING (ENGINE OIL) · airframe 63,142 hrs · 45,772 cycles

LEFT OIL PRESSURE LOW AT 24,000. FOLLOWED BY ZERO OIL QTY. SHUTDOWN LT ENGINE IN FLIGHT. FOUND LOOSE B-NUT AT 8 O`CLOCK POSITION, RT ABOVE STARTER. OIL LINE IS DISCONNECTED. REPLACED IAW AMDS W/C 7100-4682-LT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,098 hrs · 45,746 cycles

MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHTS AT BOTH FORWARD OVERWING EXIT DOORS INOPERATIVE. THE BATTERIES WERE REPLACED AND THE LIGHTS TESTED OK.

Part: WARNING HORN — FALSE ACTIVATION (ANTI ICE SYS) · airframe 63,074 hrs · 45,730 cycles

DURING TAKEOFF AND LANDING WITH ENGINE ANTI-ICE ON, NO WING ANTI-ICE SMOKE ALARMS IN BOTH AFT LAVS CAME ON, THEN SILENCED AFTER SEVERAL MINUTES. AT FL 360 WITH ONLY ENGINE ANTI-ICE ON, GOT RT AIR CONDITIONING SUPPLY TEMP HIGH ANNUNCIATION WITH SOME CABIN SMOKE AND FUMES AND ALARMS IN LAVS AGAIN. TURNED OFF ENGINE ANTI-ICE AND LIGHT WENT OUT AND SMOKE DISSAPATED, AND ALARMS STOPPED. REMOVED DUCT ASSY FOR LT AND RT COALESCER BAGS AND CEILING PANEL SRO 9250138-11 IN TAIL COMPARTMENT, FASTENER IN LT BIN. REPLACED SMOKE DETECTOR IN RT AFT LAV DUE TO BEEPING. DUCT AMM 21-20-02. R & R LT, RT COALESCER BAGS. AMM 21-20-02. USED BOROSCOPE TO VIEW INSIDE OF SADDLE DUCTS AND NOSE BULLET IAW MC DIRECTION. NO EVIDENCE OF LEAKING FOUND. CHECKED LT AND RT CROSSFEED VALVES, ACM AND DUCTING. PERFORMED PACK BURNOUT. REF AMM 36-00-00. NO FAULTS. LT, RT AUG VALVES OPS CHECK GOOD. CHECKED ICE PROTECTION PRESSURE REGULATING VALVE/ LT AND RT CROSSFEED VALVES/APU CHECK VALVE AND APU LOAD CONTROL VALVE FOR OIL CONTAMINATION. NONE FOUND. REF AMM 21-20-02. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (BS 238) · airframe 62,489 hrs · 45,344 cycles

DENT ON PREVIOUS DOUBLER REPAIR, BS 238 BETWEEN LONG 17 - 18L ON OUTER FUSELAGE SKIN. REPAIRED IAW ER/A 273447-14, REV E.

Part: DOOR FRAME — CORRODED (BS 370-427) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON PAN AT C1 CARGO DOOR JAMB FROM, BS 370 TO 427. BOTH SURFACES. C1 CARGO DOOR JAMB WAS REPAIRED IAM ER/A 539907-14, REV ORIGINAL.

Part: FRAME — UNKNOWN (BS 1338) · airframe 62,489 hrs · 45,344 cycles

LOWER CHORD SPLICE ROUND ON BS 1338 BETWEEN LONGERONS 26-27L AND 26-27R. AREA WAS REPAIRED IAW ETI-88-15-372 REV 1 AND ER/A 539897-14, REV.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

CRACK ON SKIN SURFACE AT LT INBD FLAP OTBD GUIDE VANE APPROXIMATELY ON BS XRS=121-TO XRS =124. DAMAGE AREA WAS REPAIRED IAW ERA NR 539946-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 1210) · airframe 62,489 hrs · 45,344 cycles

ELONGATED HOLE ON INTERNAL FUSELAGE SKIN, BELLY DRAIN HOLE, BS 1210 BETWEEN LONGERONS 29 - 30L. REPAIRED IAW ETI-88-15-373, REV 1 AND ER/A 539904-14, REV ORIG.

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 62,489 hrs · 45,344 cycles

CRACKED CHANNEL ON FLOOR PANEL NR 256A, 465E AND 541F AT CABIN PASSENGER FLOOR PANELS WERE REPAIRED IAW SRM 53-05, FIG 131B.

Part: FRAME — CRACKED (BS 1174) · airframe 62,489 hrs · 45,344 cycles

CRACK ON FRAME BS 1174, LONGERON 5L. THE FRAME WAS REPAIRED IAW SRM 51-30-2 AND 51-30-5 AND ETI 88-15-393 AND ER/A 539932-14, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON 12R, BS 1437. THE LONGERON WAS ATTENDED WITH ER/A 539936-14, REV ORIG.

Part: SKIN — CRACKED (BS 1418) · airframe 62,489 hrs · 45,344 cycles

CRACK OF 0.150" LENGTH ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERON 2-3 LT, SM, CARD 2, ZONE 65. DAMAGE WAS REPAIRED IAW ER/A 539886-14, AD REV: ORIGINAL. REPAIR APPROVAL IS LIMITED TO 75,000 TOTAL CYCLES ONLY. ADDITIONAL E/A, ER/A REVISION, IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. THIS WILL BE MONITORED WITH LOG 2198806.

Part: SPAR CAP — CRACKED (ELEVATOR) · airframe 62,489 hrs · 45,344 cycles

CRACK WAS FOUND OF 4.000" ON ELEVATOR SPAR CAP OF THE LT ELEVATOR BETWEEN BS XE=136 AND XE=140. SM, CARD 35, ZONE 60. CRACK WAS REPAIRED IAW ER/A 539903-14, REV ORIGINAL. PERFORM DECAL INSPECTION CONDITION IAW TOPP 30-10-70, PAGE 13, PARAGRAPH I. RII COMPLETED.

Part: SKIN — CRACKED (BS 1309-1322) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON FUSELAGE SKIN INTERNAL DOUBLER BETWEEN BS 1309-1322 AND LONGERONS 20-23L. REPAIRED IAW ER/A 508134-14, REV B.

Part: BLANKET — CRACKED (RT WING) · airframe 62,489 hrs · 45,344 cycles

CRACK ON T/E OF RT WING HEATER BLANKET STATION APPROXIMATELY XW=91.155. RT WING HEATER BLANKET WAS REPAIRED IAW ER/A 494597-14AD MA, REV A.

Part: WEB — CRACKED (STAIRWAY) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CRACK AND CORROSION ON VENTRAL STAIRWAY MOVABLE CEILING SKIN AT AFT SECTION. REPAIR WAS ACCOMPLISHED IAW ETI 88-15-389, REV 1 AND ER/A 539926-14, REV ORIGINAL.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 62,489 hrs · 45,344 cycles

QRO MAINTENACE FOUND THAT THE L1 DOOR SLIDE PACK LACING WAS MISSING. A NEW LACING WAS INSTALLED IAW AES PACKING INSTRUCTIONS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,050 hrs · 47,127 cycles

AFT LAVATORY SERVICE DOOR CUTOUT SKIN & DOUBLER CORRODED REPAIR. REPAIRED IAW ER/A.

Part: CARGO TRACK — CORRODED (BS 1212-1309) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON RT TIE TRACK BETWEEN BS 1212 -- 1309 AT AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND SRM 51-10-4, CORROSION WAS FOUND EXCESSIVE DUE TO TIE TRACK WAS REPLACED.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION OUT LIMITS ON INTERCOSTAL BETWEEN LONGERON 27 LT AND LONGERON 28LT, FROM BS Y=1309 TO Y=1322 AT AFT CARGO COMPARTMENT. NEW INTERCOSTAL WAS REPLACED DUE TO EXCESSIVE DAMAGE IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 21 AND 14, 51-30-5 AND DWG 9936718.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON TIE TRACK BETWEEN Y=1155 TO Y=1003 RT SIDE AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE DAMAGE, TIE TRACK WILL BE REPLACED. NEW TRACK WAS DRILLED IAW SRM 51-10-4 NEW TRACK WAS INSTALLED IAW SRM 51-30-1.

Part: DUCT — CRACKED · airframe 62,489 hrs · 45,344 cycles

CRACK ON Y DUCT INLET FLANGE. CRACK ON WYE DUCT WAS WELDED IAW ER/A 503276-14MA REV C AND REA WORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21.

Part: CARGO TRACK — CORRODED (BS 1212-1309) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON LT TIE TRACK BETWEEN BS Y=1212 TO Y=1309 AT AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED DUE TO EXCESSIVE DAMAGE IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21 AND DWG 5936660.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,489 hrs · 45,344 cycles

CRACK ON INNER PAN BETWEEN BEAM 1-2 AT MID CARGO COMPARTMENT DOOR FWD EDGE. CRACK ON INNER PAN BETWEEN BEAM 1-2 WAS REPAIRED IAW ETI-88-15-387, REV ORIGINAL AND ERA 539925-14, REV ORIGINAL.

Part: FRAME — DAMAGED (BS 1287) · airframe 62,489 hrs · 45,344 cycles

DAMAGE AT FRAME BS 1287 BETWEEN LONGERONS 11-12R. DAMAGE WAS BLENDED OUT, FOUND AREA OUT LIMITS, AND REPAIRED IAW SRM 53-01 AND 53-01 AND 51-30-2.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,489 hrs · 45,344 cycles

CRACK ON VERTICAL STABILIZER SKIN LT SIDE BETWEEN BS XFS=12 TO XFS=17, JUST UP TO RAM AIR DUCT. VERTICAL STABILIZER SKIN LT SIDE BETWEEN XFS=12-17 WAS REPAIRED IAW 55-01, FIG 2, 51-10-3, PARA 14, 21, 51-30-8.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 62,489 hrs · 45,344 cycles

ELONGATED BORES ON HINGE FITTING OF CONTROL TAB AT LT ELEVATOR BS XET=80. FITTING BRACKET ASSY ELEVATOR TAB LT WAS REPLACED IAW SRM 51-10-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,489 hrs · 45,344 cycles

CRACK INNER PAN BETWEEN FWD UPPER CORNER AND BEAM5 OF MID CARGO COMPARTMENT DOOR. CRACK ON INNER PAN BETWEEN FWD UPPER CORNER AND BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8 HFEC WAS PERFORMED AND NO CRACK WERE FOUND.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON PREVIOUS REPAIR PARTS OF FRAME BETWEEN LONGERON 28LT TO LONG 28RT BS 1309 AT AFT CARGO COMPARTMENT. REPAIR INSTALLED AND CIC WAS APPLIED IAW SRM 51-30-5, 51-10-4, 53-03, FIG 2A, 51-10-3, PAR 14, 21, 38 F.

Part: FRAME — CRACKED (BS 1418) · airframe 62,489 hrs · 45,344 cycles

CRACKED FRAME CAP BS Y=1418, LONGERON 2RT AND 2LT AT AFT ACC COMPARTMENT. A/A, SM STIFFENER, CAP WAS REPLACED IAW DWG SR09530003, REV. S AND SRM 51-30-2 AND SRM 51-30-5. LENGTH OF CRACK: .565".

Part: LONGERON — CRACKED (BS 1380) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON 13 LT ON BS 1380 AFT ACCESSORIES COMPARTMENT. CRACKED LONGERON 13 LT ON BS 1380 WAS REPLACED IAW SRM 53-14-4, 51-30-2, 51-10-3, PAR 21 AND 14 AND 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1003-1222) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON TIE TRACK BETWEEN Y=1222 TO Y=1003 LT SIDE AT AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED IAW SRM 51-30-1, 51-10-4, 51-10-3 PAR 14 AND 21 AND 51-30-5.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,489 hrs · 45,344 cycles

CRACK ON VERTICAL STABILIZER SKIN LT SIDE BETWEEN BS XFS=12 TO XFS=17, JUST UP TO RAM AIR DUCT, SM. VERTICAL STABILIZER SKIN LT SIDE BETWEEN XFS=12-17 WAS REPAIRED IAW SRM 55-01, FIG 2, 51-10-5, PARG 14, 21, AND 51-30-8. CRACK 0.156" AND 0.281".

Part: LONGERON — CRACKED (BS 1380) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON 11L AT BS 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3, PAR 21 AND 14.

Part: SHEAR TIE — CRACKED (BS 1418) · airframe 62,489 hrs · 45,344 cycles

CRACKED FRAME CLIP BS 1418 BETWEEN LONG 1 - 2R. FRAME CLIP WAS REPLACED IAW SRM 53-14-4, 53-03, FIG 3, 51-10-2 AND 51-10-3 PAR 14 AND 21. DIMENTION OF CRACKS IS 0.750".

Part: WEB — WORN (BS 1344) · airframe 62,489 hrs · 45,344 cycles

WEAR ON TITANIUM WEB BS 1344 BETWEEN LONGERONS 27L & 27R. REPAIRED, AND INSTALLED IAW SRM 51-30-2 AND ER/A 094719-14MA, REV A.

Part: FLOOR PANEL — DELAMINATED (BS 826-1003) · airframe 62,489 hrs · 45,344 cycles

DELAMINATED FLOOR PANEL BETWEEN BS 826 - 1003 IN PAX CABIN. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201, REPLACED IAW AMM 53-20-01-201, AND DWG 9936639, REV- P.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

WEAR AT L/E DOUBLER REPAIR OF INBD VANE OTBD FLAP RT WING. INBD VANE OTBD FLAP RT WING WAS REPAIRED IAW SRM 57-03D, PAR 11 AND CARD 2000-8149-08, JOB 000-0034.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,489 hrs · 45,344 cycles

CRACKS ON RIB IN L/E VERTICAL STABILIZER. RIB REPLACED IAW DWG 9911882, ID:2, REV. B AND C AND DWG 9911884.

Part: SHEAR TIE — CRACKED (BS 1451) · airframe 62,489 hrs · 45,344 cycles

CRACKED FRAME CLIP, BS 1451 BETWEEN LONGERON 1 - 3L, A/A, CARD 23, ZONE 61. FRAME CLIP WAS REPLACED IAW SRM 51-30-5, 51-10-2, 51-10-3, PAR 14 AND 21, AND DWG 9911860 RE, LT LENGTH CRACK: .190".

Part: TAB — DENTED (RT ELEVATOR TAB) · airframe 62,489 hrs · 45,344 cycles

DENTS ON RT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE, SM, CARD 22, ZONE 60. RT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE WAS REPAIRED IAW SRM 55-04, PAR 2 AND A/C 0986, CARD 2000-8149-07, JOB 000-0030.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,489 hrs · 45,344 cycles

DAMAGED METALLIZED ON RUDDER TAB, APP, VHS, ZONE 00, CARD 115. RUDDER TAB WAS REPAIRED IAW SRM 51-70-1A, P.23 AND OP. N. RII COMPLETED.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

WEAR AT UPPER/LOWER T/E SKIN INBD EDGE OF OTBD VANE OTBD FLAP LT WING. OTBD VANE OTBD FLAP LT WING WAS REPAIRED IAW SRM 57-03D, PAR II AND CARD 2000-8149-03, JOB 000-0027.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,489 hrs · 45,344 cycles

CRACKS ON RT RIBS BS ZFS=30 AND ZFS=23 AT L/E VERTICAL STABILIZER, SM. RIBS BS ZFS=30 AND ZFS=23 L/E VERTICAL STABILIZER WERE R & R IAW SRM 55-02D, FIG 27 AND DWG 9911885, REV. G. PERFORM INSPECTION EVERY "C" CHECK FOR NEW CRACKS IAW SRM 55-02, FIG 27, SHEET 11, RIB ZFS=30.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON INTERNAL FACE OF AFT LAVATORY SERVICE PANEL AT AFT CARGO COMPARTMENT C3, SM. AFT LAVATORY SERVICE PANEL WAS REPLACED IAW DWG 5914792, REV. AG AND SRM 51-30-2 AND 51-30-5.

Part: VANE — WORN (LT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

WEAR AT INBD VANE OTBD FLAP UPPER INBD EDGE LT WING. INBD VANE OTBD FLAP UPPER INBD EDGE LT WING WAS REPAIRED IAW ER/A 492663-14MA, REV ORIGINAL.

Part: FINGER DOUBLER — CORRODED (BS 1204-1218) · airframe 62,489 hrs · 45,344 cycles

CORROSION ON FINGER DOUBLER BETWEEN LONGERON 26 LT TO 25 LT AND BS Y=1204 TO Y=1218 AT AFT CARGO COMPARTMENT, SM. NEW SECTION OF FINGER DOUBLER Y=1204 TO Y=1218 WAS REPLACED IAW SRM 53-04, FIG 12E, ER/A 511165-14MA, REV. C. HFEC INSPECTION WAS ACCOMPLISHED NO CRACKS WERE FOUND AFTER DAMAGE REMOVED IAW NDT SPM 06-10-01-001.

Part: DOUBLER — WRONG PART (BS 1309) · airframe 62,489 hrs · 45,344 cycles

INCORRECT FUSELAGE SKIN INTERNAL TITANIUM DOUBLER BETWEEN BS 1309 AND LONGERONS 18L-23L. TITANIUM DOUBLER WAS REPLACED IAW D-DWG 5911423, REV. CD. RII COMPLETED.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,489 hrs · 45,344 cycles

CRACKED DOOR PAN BETWEEN DOOR STOP FITING NR 9 AND 8 AT RT AFT EMERGENCY EXIT OVERWING. DOOR PAN BETWEEN DOOR STOP FITTING NR 9 AND NR 8 AT RT EMERGENCY EXIT OVERWING WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,489 hrs · 45,344 cycles

MISSING METALIZED COATING AT BOTH SKIN FACES OF RUDDER AND PAINT. SH-CP-SM, CARD 7 ZONE 65. METALIZED COATING AT BOTH SKIN FACES OF RUDDER AND PAINT WAS REPAIRED IAW SRM 51-70-1A, PAR 23 AND 51-10-3B. BALANCE CHECK WILL BE PERFORMED WITH CARD 39, ZONE 65. RII COMPLETED.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON 4R AT BS 1437 CRACKED LONGERON 4R BS 1437 WAS REPLACED AND INSTALLED NEW IAW SRM 53-02, FIG 18 AND SRM 51-10-3, PAR 21 AND 14.

Part: SHEAR TIE — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

CRACKED LOWER TEE CAP BS 1437, LONGERON 2R AND 2L AT AFT ACCESSORY COMPARTMENT. A/A, SM, CARD 63, ZONE 61. CAP WAS REPAIRED IAW 53-01, FIG. 2, LENGTH CRACKS: 3.625", 1.625", 4", 3.062".

Part: LONGERON — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONG 3L AT BS 1437, A/A, SM, CARD 20, ZONE 61. CRACKED LONG 3L AT BS 1437 WAS REPLACED AND REPAIRED IAW SRM 53-02, FIG 18 AND 51-10-3, PAR 21, 14. LENGTH CRACK: 0.180. RII COMPLETED.

Part: FRAME — DAMAGED (BS 1485) · airframe 62,489 hrs · 45,344 cycles

ELONGATED HOLES ON FRAME BS 1485. HOLES WERE DRILLED TO NEXT SIZE IAW 51-10-4, DUE TO EXCESSIVE DAMAGE WAS ATTENDED IAW SRM 53-01, FIG 2, SRM 51-10-3 PAR 21, 14 AND 51-30-2.

Part: DOOR FRAME — CRACKED · airframe 62,489 hrs · 45,344 cycles

CRACK AND ELONGATED HOLE AT LOWER LT CORNER OF FS 1338 VENTRAL DOOR LOWER JAMB. AREA WAS REPAIRED IAW SRM 53-05, FIG 34. MAINTENANCE REQUIREMENTS: PERFORM REPETITIVE VISUAL INSPECTION OF BLIND FASTENERS EVERY 8000 CYCLES.

Part: SHEAR TIE — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

CRACKED FRAME CLIP BS 1437 BETWEEN LONGERON 1 TO 2 RT AT AFT ACC COMPARTMENT. FRAME CLIPS BS 1437 BETWEEN LONGERON 1 TO 2 LT AND RT AFT ACCESSORY WERE REPLACED IAW SRM 51-30-5, 51-10-3 PAR 14-21, AND DWG 9911840, REV. DC.

Part: TAB — DENTED (ELEVATOR) · airframe 62,489 hrs · 45,344 cycles

DENT ON ELEVATOR CONTROL TAB SKIN, PN 5910413-508, S/N 49626. ELEVATOR CONTROL TAB PN 5910413, SN 49626 WAS REPAIRED IAW SRM 55-04 P2 AND AC 0986, CARD 2000-8149-07.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,489 hrs · 45,344 cycles

DELAMINATED FLOOR PANEL BETWEEN BS 1003 TO 1338. FLOOR PANEL REPLACED IAW AMM 53-20-01-201.

Part: DOUBLER — UNSECURE (BS 180-200) · airframe 62,489 hrs · 45,344 cycles

GAPPING BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER EXISTING REPAIR, BS Y=180-200 BETWEEN LONGERONS 26-27RT. REMOVE FINGER DOUBLERS, NEW FINGER DOUBLER WERE FABRICATED WERE TREATED AND PAINTED IAW SRM 51-30-2, 51-10-3, PAR 14 AND 21 AND 53-04, FIG 128.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,489 hrs · 45,344 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL REPLACED IAW AMM 53-20-01-201.

Part: SHEAR TIE — CORRODED (BS 1380) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

INITIAL WEAR AND CORROSION ON FRAME TEE BS 1380 BETWEEN LONGERONS 28L - 28R. FRAME TEE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9912246115, REV DE.

Part: INTERCOSTAL — CRACKED (BS 1357) · airframe 62,489 hrs · 45,344 cycles

CRACK FOUND ON INTERCOSTAL BELOW 6 PULLEY BRACKET BS 1357, X= -18, Z=0, AT RT LAVATORY FLOOR STRUCTURE. INTERCOSTAL WAS REMOVED IAW SRM 51-30-2 , 51-30-5. CRACKS WERE STOPPED IAW SRM 53-01, FIG 2. HFEC INSPECTION WAS ACCOMPLISHED AROUND STOP DRILLS, 4 EAS. NO MORE CRACKS WERE FOUND IAW NDT SPM 06-10-01-001. REPAIR DOUBLER WAS FABRICATED IAW SRM 53-01, FIG 2 AND DWG 9115540, REV AJ. DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21. DOUBLER WAS INSTALLED IAW SRM 53-01, PG 2. INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 1309) · airframe 62,489 hrs · 45,344 cycles

CRACK ON LONGERON 6L BS 1309 AT PASSENGER CABIN. DAMAGE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. LENGTH CRACK .125 , AND SRM 51-10-3, PAR 14.21.38, AMM 20-30-01. (LP2204125)

Part: DOOR FRAME — CRACKED (ACCESSORY BAY) · airframe 62,489 hrs · 45,344 cycles

CRACK ON FWD ACCESSORY DOOR JAMB BS Y=63 AT 7 O`CLOCK POSITION. DAMAGE ON FWD DOOR JAMB WAS REPAIRED IAW SRM 53-01, FIGURE 2, SHEET 3.

Part: DOOR — CRACKED (RT MLG) · airframe 62,489 hrs · 45,344 cycles

DURING RUB STRIPS REMOVAL, A CRACKED PAN ON RT MLG FWD UPPER EDGE, BS 940. RT MLG DOOR WAS REPLACED FOR A REPAIRED DOOR.

Part: SUPPORT FITTING — CORRODED (RT MLG ACTUATOR) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AND WEAR AT RT BEARING OF MLG RETRACT ACTUATOR SUPPORT FITTING. RT BEARING OF MLG RETRACT ACTUATOR SUPPORT FITTING WAS REPLACED IAW CMM 20-10-7, PAR D1-A.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 62,489 hrs · 45,344 cycles

CRACKED CHANNEL ON FLOOR PANEL 1079A AT CABIN PAX. CHANNEL WAS REPAIRED IAW SRM 51-70-1D P. 10.

Part: CUSP WEB — CRACKED (BS 987-998) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION OF OUT LIMITS ON LT CUSP WEB X 54 TO X 60, BS 987 - 998. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131 A7 A REPAIR WAS FABRICATED IAW SRM 53-05, FIG 131A-7. THE REPAIR WAS TREATED, AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. THE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON END 2R, BS 1418. LONGERON END REPLACED IAW SRM 51-30-5 AND 53-14-4, 53-02, FIG.18.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,489 hrs · 45,344 cycles

CRACK FOUND ON BEAM 4 OF R1 DOOR. THE BEAM WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-10-3 PAR 14/21, 51-10-4.

Part: CUSP WEB — CORRODED (BS 503-589) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON RT CUSP WEB MEMBRANE FROM BS 503 - 589 UPPER AND LOWER SURFACE BETWEEN X -54 TO X -60. THE CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 53-05, FIG 131A-24, 51-10-3 PARA 14/21.

Part: PAN — CRACKED (R1 DOORWAY) · airframe 62,489 hrs · 45,344 cycles

CRACKED PAN FWD EDGE JUST BELOW OF LOWER HINGE ON R1 DOOR. REPAIR WAS ACCOMPLISHED IAW SRM 52-03D, FIG 3.

Part: CUSP WEB — DAMAGED (BS 1025-1093) · airframe 62,489 hrs · 45,344 cycles

DURING CUSP WEB INSPECTION WAS FOUND OUT OF LIMITS AREAS BS 1025 - 1093 ON LT CUSP WEB BETWEEN X 54 AND X 60. DAMAGE REMOVED, A REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 53-05 FIG 131A-17, 51-10-3 PAR 21,14, 38, 51-30-5, 53-05 FIG 131A-14.

Part: CUSP WEB — CORRODED (BS 598-646) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON RT CUSP WEB FROM BS 598 - 646 BETWEEN X -54 TO X -60 AT PAX CABIN. AREAS WAS REPAIRED IAW SRM 53-05, FIG 131A-6, SHEET 1, AND TREAT AND PAINT FABRICATED REPAIR PARTS APPLY CIC IAW SRM 51-10-3, PAR 14 AND 21, 38. INSTALL REPAIR PARTS.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

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

Part: LONGERON — CRACKED (BS 1309) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON 5R AT BS 1309. A NEW SECTION OF THE LONGERON AND SPLICES WAS INSTALLED IAW SRM 51-30-2, 51-30-5 AND 53-02, FIG. 18.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

CRACK AT INBD FWD ATTACH FITTING CUTOUT HOLE SKIN, UPPER SKIN, ON OTBD VANE INBD FLAP LT WING. OTBD VANE INBD FLAP LT WAS REMOVED IAW AMM 27-51-01. VANE, NR 2 LT. LT INBD FLAP, OTBD VANE WAS REPLACED AND WAS INSTALLED UNDER CARD 148, ZONE 10.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,489 hrs · 45,344 cycles

CRACKED R1 DOOR BEAM 1 FWD EDGE. CRACKED R1 DOOR BEAM 1 WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5 AND DWG 9911579, REV EP.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION BARRIEL NUT NR 24 ON LT HORIZONTAL STABILIZER. AREA WAS REPAIRED IAW ERA 539899-14, REV. ORIGINAL AND BOLT AND BARREL NUT NR 24 LT WERE REMOVED AND INSTALLED IAW SRM 51-30.

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON RT CUSP WEB X -54 TO X -60 BS 1060 - 1079. REPAIR FABRICATED, TREATED PAINTED AND INSTALLED IAW SRM 51-30-1, 53-05 FIG 131A-7, 51-30-2 PAR 14 AND 21, 51-10-3 PAR 38.

Part: CUSP WEB — CORRODED (BS 660-676) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON RT CUSP WEB MEMBRANE DOUBLER REPAIR FROM BS 660 TO 676 BTW X-54 TO X-60. THE CUSP WEB DOUBLER REPAIR WAS REPLACED IAW SRM 53-05, FIG 131A-10.

Part: CUSP WEB — NOT REPORTED (BS 712-720) · airframe 62,489 hrs · 45,344 cycles

FASTENER ON EDGE OF LIGHTING HOLE ON RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 712 TO 720. PREVIOUS REPAIR DOUBLER WAS REMOVED IAW SRM 51-30-5 FITTING WAS REMOVED, DAMAGE WAS REMOVED, HFEC INSPECTION WAS PERFORMED AND NO CRACKS WERE FOUND, REPAIR DOUBLER WAS FABRICATED, TREATED AND PAINTED IAW SRM 53-05, FIG 131, 51-10-3 PAR 21, 14. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2. FITTING WAS INSTALLED IAW SRM 51-30-1. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON DOUBLER PREVIOUSLY REPAIRED AT C3 CARGO DOOR JAMB BS=115 TO 1211. SPACER AND STRAPS WERE REPLACED IAW SRM 53-05, FIG 123, 51-30-5, 51-10-3.

Part: SKIN — DAMAGED (BS 184) · airframe 62,489 hrs · 45,344 cycles

CRACK ON OUTER FUSELAGE SKIN NEXT TO LIGHTNING STRIKE WAS FOUND DURING NDT INSPECTION, BS 184 BETWEEN LONGERON 28 LT TO 29 LT, REF NRC 59, ZONE 100, CARD 275, ZONE 100. AREA WAS REPAIR IAW SRM 53-04-2, PAR 3C 2, A, 1A WITH DIMENSION HOLE .187" 51-10-3 PAR 14 AND 21 AND 51-30-2. INSPECTION WAS PERFORMED, NO CRACKS WERE FOUND; IAW SRM 53-04-2, PAR 3C, 2, A1, A2 MAINTENANCE REQUIREMENTS, PERMANENT REPAIR, VISUAL INSPECTION PERFORMED, REPETITIVE EVERY 8,000 CYCLES REF 53-04-2. THE LOG 2197743 WAS CREATED BY MISTAKE. THE MONITOR WILL BE INSPECTED WITH THIS LOG CREATED.

Part: WEB — CRACKED (BS 1437) · airframe 62,489 hrs · 45,344 cycles

FOUR CRACKS ON WEB BS 1437 BETWEEN LONGERONS 5R-5L. THE WEB WAS REPLACED IAW SRM 53-14-4, 51-30-5.

Part: CUSP WEB — WORN (BS 617) · airframe 62,489 hrs · 45,344 cycles

WEAR OUT OF LIMITS ON CUSP WEB, BS 617 BETWEEN X=44, 54, LT SIDE AT CABIN PAX AREA. DAMAGE WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 131A AND SRM 51-10-3, PAR 14 AND 21.

Part: SKIN — CRACKED (BS 184) · airframe 62,489 hrs · 45,344 cycles

CRACK ON OUTER FUSELAGE SKIN NEXT TO LIGHTNING STRIKE WAS FOUND DURING NDT INSPECTION, BS 184 BETWEEN LONGERON 28 LT TO 29 LT. AREA WAS REPAIR IAW SRM 53-04-2 PAR 3C 2, A, 1A WITH DIMENTIONS HOLE .187", 51-10-3, PAR 14 AND 21 AND 51-30-2.

Part: SKIN — DAMAGED (BS 126-136) · airframe 62,489 hrs · 45,344 cycles

LIGHTNING STRIKE ONE FUSELAGE SKIN BETWEEN BS 126 - 136 LONGERONS 27 - 28L. AREAS REPAIRED IAW SRM 51-10-3, PAR 15.

Part: CUSP WEB — CORRODED (BS 890-892) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB X 54 - X 60, BS 890 - 892. REPAIR FABRICATED IAW SRM 53-05, FIG 131A-13. REPAIR TREATED/PAINTED IAW SRM 51-10-3, PAR 21,14 AND INSTALLED IAW SRM 51-30-2.

Part: BOLT — CRACKED (LT YOKE MOUNT) · airframe 62,489 hrs · 45,344 cycles

CRACKING ON CHROME PLATING ON LT LOWER YOKE MOUNT BOLT. YOKE MOUNT BOLT WAS REPLACED AND INSTALLED.

Part: CUSP WEB — CORRODED (BS 733-740) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON RT CUSP WEB BETWEEN BS X -54 TO -60 AND BS 733 - 740 IN PAX CABIN. CORROSION WAS ATTENDED IAW SRM 53-05, FIG 131A-6, 51-30-2, 51-10-3 PAR 21, 14, AND 38.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON LOWER AND UPPER SURFACE LT CUSP WEB BS 446 - 465, X 54 -X 60. CORROSION WAS FOUND EXCESSIVE THEREFORE AREA WAS REPAIRED IAW SRM 53-05, FIG 131A -13 SH 1.

Part: WEB — CRACKED (BS 210) · airframe 62,489 hrs · 45,344 cycles

CRACKED WEB BS 210, LONGERON 11L . DAMAGE WAS REMOVED AND AREA WAS REPAIRED IAW SRM 53-05, PAR 153.

Part: CUSP WEB — CORRODED (BS 1164-1174) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON REPAIR ON LT CUSP WEB X=44 TO X=54, STA 1164 - 1174. PREVIOUS REPAIR WAS REMOVED AND NEW DOUBLER REPAIR WAS INSTALLED IAW SRM. 51-30-2, 53-05, FIG 131A, 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 770-776) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON RT CUSP WEB BTW X=-54 TO -60 AND BS 770 -- 776. NEW REPAIR DOUBLER WAS FABRICATED REPAIR WERE TREATED AND PAINTED, REPAIR INSTALLED CIC WAS APPLIED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 38, 53-05 FIG. 131A-11.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON COUNTERSINK OF FUEL ACCES PANEL 2302C. BUSHING WAS INSTALLED IAW SRM 51-22-2A.

Part: SEAT TRACK — CORRODED (BS 231) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON SEAT TRACK BS 231, X=44. SEAT TRACK WAS REPLACED IAW SRM 51-30-1; 51-30-5 AND 51-10-4.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

WEAR AT T/E LOWER SKIN OF INBD VANE OTBD RT WING TE FLAP . REPAIRED IAW ER/A 492663-14MA, REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 1225-1237) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION, OUT LIMITS, ON RT CUSP WEB BETWEEN BS X -54 TO -60 AND BS 1225 - 1237 IN PAX CABIN. THE CUSP WEB WAS REPAIRED IAW SRM 51-30-1, 51-30-2, 51-30-5, 53-05, FIG 131A AND 51-10-3, PAR 21, 14, AND 38.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1373C. A BUSHING WAS INSTALLED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON COUNTERSINK OF ACCESS PANEL 1476C. REPAIRED AND FOUND WITHIN LIMITS. BUSHING WAS FABRICATED AND COUNTERSINK IAW SRM 51-22-2A. AREA AND BUSHING WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR NR 14 AND NR 21. NEW BUSHING WAS INSTALLED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON COUNTERSINK, OF ACCESS PANEL 1357C. BUSHING WAS INSTALLED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AT SETTLEMENT AND COUNTERSKIN AREAOF FUEL ACCESS PANEL 1307C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A CON II AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0396.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AT SETTLEMENT AREA AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1462C. ACCESS PLATE 1462C WAS REPLACED AND WILL BE INSTALLED UNDERCARD 2800-0390, JOB NR 001-0402.

Part: SUPPORT FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

AD/AA CORROSION AT BORE DIAMETER, INNER, OF RT MLG RETRACT ACTUATOR SUPPORT FITTING. CORROSION ON BORE WAS REMOVED WITH A INITIAL MEASURE OF DIAMETER 2.250" AND FINAL MEASURE AFTER REWORK OF 2.260" WITHIN LIMITS IAW DWG SR09570087, REV B FPI WAS PERFORMED AND AREA WAS TREATED IAW SRM 51-10-3, PAR 21.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AT BORE OF LT MLG RETRACT ACTUATOR SUPPORT FITTING. BORE WAS REPAIRED, CORROSION WAS REMOVED, WITH FINAL MEASURE: WITHIN LIMITS IAW DWG SR09570087, REV B.

Part: CUSP WEB — CORRODED (BS 826-845) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB X=54 TO 60 BETWEEN BS 826 - 845 AT PAX CABIN FLOOR STRUCTURE. FASTENERS WERE REMOVED IAW SRM 51-30-2. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131-A-13. REPAIR PARTS WERE TREATED/PAINTED IAW SRM 51-10-3 PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 131-A-13. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: ACCESS PANEL — PUNCTURED (LT WING) · airframe 62,489 hrs · 45,344 cycles

PUNCTURES SECOND DUAL ACCESS PANEL, LT WING. ACCESS PANEL WAS REPAIRED IAW ERA 530866-14.

Part: CUSP WEB — CORRODED (BS 484-503) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION, OUT LIMITS, ON RT CUSP WEB BETWEEN BS X=-54 TO -60 BS 484 - 503 AT PAX CABIN FLOOR STRUCTURE. DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED, REPAIR PARTS WERE TREATED AND PAINTED, REPAIRED PARTS WERE INSTALLED, CIC WAS APPLIED IAW SRM 53-05, FIG 131A-7, 51-10-3, PAR 14, 21 AND 38, 51-30-2.

Part: CUSP WEB — CORRODED (BS 218) · airframe 62,489 hrs · 45,344 cycles

CRACKS ON LT CUSP WEB FROM BS 218 X=44 - X=54. CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 4 AND 51-30-5.

Part: SUPPORT FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

A CORROSION AROUND BORE INBD FACE OF RT MLG RETRACT ACTUATOR SUPPORT FITTING. CORROSION ON BOTH FACE OF BORE WAS REMOVED WITH A INITIAL MEASURE OF 1.237" AND A FINAL MEASURE AFTER REWORK OF 1.230". WITHIN LIMITS IAW DWG 5935812, REV BB FPI WAS PERFORMED AND REWORKED AREA WAS TREATED IAW SRM 51-10-3, PAR 21.

Part: WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

SEVERAL CORROSION POINTS ON MEMBRANE FROM BS 160 TO 200 AND FROM X=44 TO X=54. CORROSION WERE REMOVED DAMAGE WERE EVALUATED DUE TO EXCESIVE CORROSION WILL BE REPLACED MEMBRANE WAS FABRICATED, MEMBRANE AND PARTS TREATED, PAINTED AND INSTALLED IAW SRM 51-30-10, 51-10-4 AND 51-10-3, PAR 14, 21.

Part: ACCESS PANEL — PUNCTURED (RT WING) · airframe 62,489 hrs · 45,344 cycles

PUNCTURED FUEL ACCESS PANEL, RT WING. ACCESS PANEL WAS REPAIRED IAW ER/A ADMA.

Part: CUSP WEB — CORRODED (BS 440-503) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON RT CUSP WEB MEMBRANE FROM BS 440 TO 503 UPPER AND LOWER SURFACES INCLUDING REPAIR DOUBLERS AT PAX CABIN BETWEEN X=-54 TO X=-60. AREA OUT OF LIMITS WAS ATTENDED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-30-3 PARR. 14, 21, 26, 53-05, FIG 131A-11.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1470C. ACCESS WAS REPLACED IAW SRM 51-22-2A CONDITIONER II AND WILL BE INSTALLED UNDER CARD 28-0390, JOB 001-0402.

Part: LONGERON — CRACKED (BS 160) · airframe 62,489 hrs · 45,344 cycles

CRACK ON BS 160 AND LONGERON 4LT SIDE AT C PAX. DAMAGE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1454C RT WING. ACCESS PLATE 1454C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0402.

Part: LONGERON — CRACKED (BS 160) · airframe 62,489 hrs · 45,344 cycles

CRACK ON BS 160 AND LONG 3L SIDE AT C. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 389-408) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON 17R BETWEEN BS 389 TO 408 AT PASSENGER CABIN INTERNAL STRUCTURE. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: DOOR FRAME — CORRODED (BS 640-685) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON SPACER FWD FACE AT MID CARGO LOWER DOOR FRAME FROM BS 640 TO 685. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123.

Part: CUSP WEB — CORRODED (BS 1045) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION OUT LIMITS ON RT CUSP WEB BETWEEN RBL 54 TO 60 BS 1045 AT PAX CABIN FLOOR STRUCTURE. AREA OUT LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: LONGERON — CRACKED (BS 524) · airframe 62,489 hrs · 45,344 cycles

CRACK ON LONGERON 4R AT BS 524 APPROXIMATELY AT PAX CABIN. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 845-864) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION OUT LIMITS ON LT CUSP WEB X=54 TO 60 BETWEEN BS 845 TO 864 AT PAX CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 53-05, FIG 131A-14, 51-10-3 PAR 14, 21 AND 38, SRM 51-30-2.

Part: LONGERON — CRACKED (BS 541) · airframe 62,489 hrs · 45,344 cycles

CRACK ON LONGERON 4L, BS 541 AT PAX CABIN. LONGERON 4LT WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON COUNTERSINK, 4 E/AS OF FUEL ACCESS PLATE NR 1456C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON COUNTERSINK, 4 E/AS OF FUEL ACCESS PLATE NR 1355C. THE ACCESS PANEL WAS REPLACED

Part: HOUSING — CORRODED (RUDDER BEARING) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AND TOOL MARKS ON HOUSING OF RUDDER BEARING. RUDDER BEARING HOUSING REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-10-4.

Part: WEB — CORRODED (BS 160-200) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

SEVERAL CORROSION POINTS ON MEMBRANE FROM BS 160 TO 200 X=7 TO X=14. FASTENERS WERE REMOVED. FOR EXCESIVE CORROSION AREAS WILL BE REPAIRED. DAMAGE WAS REMOVED, REPAIR DOUBLERS WERE FABRICATED, TRIMMED AND DRILLER, TREATED AND PAINTED. DOUBLERS WERE INSTALLED IAW SRM 51-30-2, 33-01, FIG 4, SH 4, 51-10-3 PAR 14 AND 21.

Part: SLAT TRACK — WORN (LT WING) · airframe 62,489 hrs · 45,344 cycles

WEAR ON SLAT TRACK NR 13 AT LT WING. LT SLAT TRACK NR 13 WAS REPLACED IAW AMM MD-88 27-80-01. RII COMPLETED.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

DELAMINATED UPPER AND LOWER SKIN APPROXIMATELY, BETWEEN BS XV2=313-320 ON OTBD VANE OF OTBD FLAP AT RT WING. SH-CP-SM, CARD 143, ZONE 10. UPPER AND LOWER SKIN APPROXIMATELY, BETWEEN XV2=313-320 ON OTBD, VANE OF OTBD FLAP AT RT WING WAS REPAIRED IAW SRM 57-03D, PAR II AND CARD 2000-8149-05, CREW O2 "1121163" JOB 000-0018.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION AT SETTLEMENT AND COUTER SKIN AREAS OF THE ACCESS PANEL 2301C, FOUND TO BE OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED.

Part: LONGERON — CRACKED (BS 1338) · airframe 62,489 hrs · 45,344 cycles

CRACK ON LONGERON END 7R BS 1338 AT PASSENGER CABIN. LONGERON END WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-5; 51-10-2; 51-10-3 PAR 14, 21 AND DWG 4913329, REV "A".

Part: LONGERON — CRACKED (BS 1338) · airframe 62,489 hrs · 45,344 cycles

CRACKED LONGERON END 14R BS 1338. THE LONGERON END WAS REMOVED, FABRICAED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-5, 51-10-2, 51-10-3 PAR 14, 21 AND DWG 4913329, REV. A.

Part: TAB — DENTED (LT ELEVATOR) · airframe 62,489 hrs · 45,344 cycles

DENTS ON LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE, SM. DUE TO SEVERAL DENTS, THE ANTI-FLOAT TAB WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2730-4334, JOB-0208.

Part: PAN — CRACKED (BS 1003-1022) · airframe 62,489 hrs · 45,344 cycles

CRACKED RT WINDOW RING PAN ON UPPER AFT BETWEEN BS 1003 TO 1022 AT PASSENGER CABIN INTERNAL STRUCTURE. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 1231-1250) · airframe 62,489 hrs · 45,344 cycles

CRACKED LT WINDOW RING PAN UPPER AFT CORNER BETWEEN BS 1231 AND 1250. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN BEAMS NR 2 AND 3 AT AFT CARGO DOOR. AFT CARGO DOOR WAS REMOVED IAW AMM 52-52. AFT CARGO DOOR WAS REPLACED & WILL BE INSTALLED UNDER CARD 5200-4538.

Part: PAN — CRACKED (BS 927-946) · airframe 62,489 hrs · 45,344 cycles

CRACKED LT WINDOW RING PAN UPPER FWD CORNER BETWEEN BS 927 AND 946. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: BEARING — DAMAGED (RUDDER YOKE) · airframe 62,489 hrs · 45,344 cycles

DAMAGE RUDDER YOKE BEARING. RUDDER YOKE BEARING WAS REPLACED, ITS WAITING FOR INSTALLATION ON PART RACK UNDER 2720-2126, JOB 001-0344.

Part: PAN — CRACKED (BS 1212-1231) · airframe 62,489 hrs · 45,344 cycles

CRACKED RING PAN FWD UPPER CORNER BETWEEN BS 1212 AND 1231 RT SIDE AT C PAX. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIG. , 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 788-807) · airframe 62,489 hrs · 45,344 cycles

CRACKED LT WINDOW RING PAN UPPR FWD CORNER BETWEEN BS 807 TO 788 AT PASSENGER CABIN. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 1136-1155) · airframe 62,489 hrs · 45,344 cycles

CRACKED RT WINDOW RING PAN ON LWR FWD BETWEEN BS 1136 TO 1155 AT PASSENGER CABIN INTERNAL STRUCTURE. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 218) · corrosion level 2 · airframe 62,489 hrs · 45,344 cycles

CORROSION ON SEAT TRACK PLUG BS 218 X=22LT. THE PLUG WAS REPLACED IAW SRM 53-05, FIG 4A, SH 3.

Part: PAN — CRACKED (BS 579-598) · airframe 62,489 hrs · 45,344 cycles

CRACKED RT WINDOW RING PAN ON LOWER AFT CORNER BETWEEN BS 579 - 598 AT PASSENGER CABIN INTERNAL STRUCTURE. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIG , 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 522-541) · airframe 62,489 hrs · 45,344 cycles

CRACKED RT WINDOW RING PAN ON UPPER FWD CORNER BETWEEN BS 522 TO 541 AT PASSENGER CABIN INTERNAL STRUCTURE. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 1079-1098) · airframe 62,489 hrs · 45,344 cycles

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

Part: PAN — CRACKED (BS 1155-1174) · airframe 62,489 hrs · 45,344 cycles

CRACKED RT WINDOW RING PAN ON LWR FWD BETWEEN BS 1155 TO 1174 AT PASSENGER CABIN INTERNAL STRUCTURE. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 804-816) · airframe 62,489 hrs · 45,344 cycles

CRACKED LT WINDOW RING PAN LOWER FWD CORNER BETWEEN BS 804 TO 816 AT PASSENGER CABIN. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 1041) · airframe 62,489 hrs · 45,344 cycles

CRACKED LT WINDOW RING PAN UPPER AFT AND LOWER FWD CORNERS BETWEEN BS 1041. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL, 487747-14 MA REV ORIGINAL.

Part: PAN — CRACKED (BS 845-864) · airframe 62,489 hrs · 45,344 cycles

CRACKED LT WINDOW RING PAN UPPER FWD CORNER BETWEEN BS 845 TO 864 AT PASSENGER CABIN. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122. HFEC NO CRACKS FOUND. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV ORIGINAL ER/A 487747-14 MAREV. ORIGINAL.

Part: VANE — PUNCTURED (RT WING TE FLAP) · airframe 62,489 hrs · 45,344 cycles

PUNCTURE AT LOWER SKIN OF CENTER VANE OF OTBD FLAP RT WING. FLAP GUIDE VANE WAS REPLACED ITS ON PART RECKS WAITING FOR ITS INSTALLATION UNDER CARD 5730-0483, JOB 001-0163.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 62,489 hrs · 45,344 cycles

SEVERAL DENTS ON RT ELEVATOR CONTROL TAB UPPER SURFACE. RT ELEVATOR TAB WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2730-4182, JOB 001-0207.

Part: TAB — DENTED (LT ELEVATOR) · airframe 62,489 hrs · 45,344 cycles

DENTS ON LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE. DUE TO SEVERAL DENTS THE ANTI-FLOAT TAB WAS REPLACED AMD WILL BE INSTALLED UNDER CARD 2730-4334, JOB 001-0208.

Part: TAB — DENTED (LT ELEVATOR) · airframe 62,489 hrs · 45,344 cycles

SEVERAL DENTS ON LT ELEVATOR CONTROL TAB LOWER & UPPER SURFACE. THE TAB WAS REMOVED IAW AMM 27-30. LT ELEVATOR CONTROL TAB WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2730-4334, JOB 001-0208.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,166 hrs · 45,104 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 27-31 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: SKIN — CRACKED (BS 1380) · airframe 59,359 hrs · 43,192 cycles

AFT FUSELAGE SKIN CRACKED AT BS 1380, 10 INCHES ABOVE RT PYLON. COMPLIED WITH PRI 527352-14, REV O AND REPAIRED IAW ERA 527352-14, REV ORIGINAL.

Part: BULKHEAD WEB — CRACKED (BS 1437) · airframe 59,348 hrs · 43,183 cycles

TAIL INTERIOR VERTICAL BULKHEAD, BS 1437 FWD WEB CRACKED EMINATING FROM UNDER INBD ANGLE NEXT TO 2" PNEU. REMOVED SHEAR TIE. REPAIRED WEB IAW SRM 51-70-04. FABRICATED NEW SHEAR TIE AND INSTALLED IAW DWG 9911840.

Part: BULKHEAD — CRACKED (BS 1463) · airframe 59,348 hrs · 43,183 cycles

TAIL INTERIOR LT VENT BOX, CANTED BULKHEAD BS 1463 AFT WEB HAS MULTIPLE CRACKS. REPAIRED IAW SRM 51-70-4 FIG 2.

Part: RELEASE CABLE — FRAYED (TAIL CONE) · airframe 59,348 hrs · 43,183 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CABLE TO BE FRAYED. MAINTENANCE REMOVED AND REPLACED THE TAILCONE RELEASE CABLE.

Part: FRAME — CRACKED (BS 1510) · airframe 59,348 hrs · 43,183 cycles

TAILCONE UPPER FRAME AT BS 1510 HAS CRACKS AT APPROXIMATELY 1:00 AND 10:00 O`CLOCK POSITIONS. REMOVED AND REPLACED FRAME IAW DWG 9911843.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,735 hrs · 42,176 cycles

DURING PREFLIGHT CHECK, FLIGHT CREW NOTED THE COCKPIT EMERGENCY LIGHTS INOPERATIVE. BATTEIES REPLACED IAW AMM 33-53 AND OPS CHECKED NORMAL.

Part: DOOR — NOT REPORTED · airframe 57,714 hrs · 42,164 cycles

CARGO DOOR REPAIRED IAW AA 5230-01159.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,454 hrs · 41,973 cycles

DURING LINE CHECK, THE SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE IN FIRST CLASS. REPLACED B5-211 POWER SUPPLY AND BATTERY PACK IAW AMM 33-53. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,208 hrs · 41,110 cycles

DURING LINE MX CHECK IN FLL, THE EMERGENCY EXIT SIGN AT ROW 24 WAS FOUND TO BE INOPERATIVE. THE BATTERY PACK WAS FOUND TO BE DISCHARGED AND WAS REPLACED IAW AMM 33-53-00. OPERATION CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 55,721 hrs · 40,804 cycles

DURING LINE CHECK, MX FOUND TWO EMERGENCY PATHWAY LIGHT IN THE CABIN WERE INOPERATIVE. MX REPLACED WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: CARGO TRACK — CORRODED (BS 1153) · airframe 55,677 hrs · 40,781 cycles

CORROSION AFT CARGO BAY TIE DOWN TRACK CORRODED BS 1153, STR 28R. CORROSION ON AFT CARGO BAY TIE DOWN TRACK BS 1153 STR 28R FOUND TO BE OUT OF LIMITS. SPLICED IN NEW SECTION OF TIE DOWN TRACK FROM BS 1107.5-1155 AND REPAIRED IAW SRM 53-05, FIG 4C.

Part: THRESHOLD — CORRODED (BS 640-688) · airframe 55,677 hrs · 40,781 cycles

CORROSION ON CENTER CARGO DOORWAY, LOWER THRESHOLD, NUMEROUS AREAS, BS 640-688. FOUND CORROSION ON CENTER CARGO DOORWAY, LOWER THRESHOLD TO BE OUT OF LIMITS IN NUMEROUS AREAS BS 640-685. CORRECTED BY INSTALLING REPAIR IAW SRM 53-05, FIG 123.

Part: LUG — NOT REPORTED (HORIZONTAL STAB) · airframe 55,674 hrs · 40,779 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG, REPAIRED IAW AA 5500-01011.

Part: SKIN — BUCKLED (RT ELEVATOR) · airframe 55,674 hrs · 40,779 cycles

ELEVATOR UPPER AND LOWER SKIN FOUND BUCKLED. REAR SPAR DAMAGED. RT ELEVATOR WAS REPAIRED ON WO 460465 FORM TRACKING NR N-57019. ER/A 508136-14 HAS BEEN COMPLIED WITH. MONITOR SET UP ON LOG PAGE 0722122. 955563C 01FEB13. REQUIRED INSPECTION COMPLIED WITH 702950 01 FEB 13.

Part: FRAME — CORRODED (BS 1271) · airframe 55,674 hrs · 40,779 cycles

AFT CARGO BAY FRAME IS CORRODED BS 1271, STR 29L-29R. CORROSION WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED LOWER SECTION OF CORRODED FRAME AND INSTALLED REPAIR IAW SRM 53-03, FIG 2A. RII COMPLIED WITH.

Part: INTERCOSTAL — CORRODED (BS 1322-1337) · airframe 55,674 hrs · 40,779 cycles

FOUND INTERCOSTAL BETWEEN BS 1322 AND 1337 2.5" ABOVE L22 TO BE CORRODED. REMOVED INTERCOSTAL BS 1322 AND BS 1337 2.5" ABOVE L22. CORROSION FOUND TO BE OUT OF LIMITS. DAMAGED AREA L=3"X W=2" X 100 PERCENT MATERIAL LOSS, REPLACED WITH NEW INTERCOSTAL IAW SRM 51-30-2.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 55,674 hrs · 40,779 cycles

CORROSION ON AFT CARGO DOORWAY, LWR THRESHOLD JAMB PREVIOUS REPAIR FWD AND AFT ENDS AROUND FASTENERS MRB 53-100-15. NO ALLOWABLE DAMAGE FOR PREVIOUS REPAIR ON AFT CARGO DOORWAY LWR THRESHOLD JAMB. REMOVED FASTENERS. THE CORRODED -9 REPAIR PART WAS FABRICATED AND INSTALLED IAW SRM 53-05, SEC 140, FIG 123.

Part: OXYGEN SYSTEM — MALFUNCTIONED (CABIN) · airframe 55,674 hrs · 40,779 cycles

THE PASSENGER OXYGEN SYS IN THE CABIN FAILED TO DEPLOY, IN MANUAL OR IN AUTOMATIC MODE, WHEN TESTED. ONLY THE LT ROW, FROM SEAT 1 TO THE OVER-WING EXITS, FUNCTIONED. MX FOUND A WIRE (W636E220) HAD SHORTED TO GROUND AT TERMINAL NR 8 ON STRIP 53-154. THE CORRECTIVE ACTION WAS TO RE-SEAT THE PSU CONNECTOR AT ROW 2. OPS CHECK OF THE PASSENGER OXYGEN SYS WAS SATISFACTORY PERFORMED IN BOTH MANUAL AND AUTOMATIC DEPLOY MODES. THE ACFT HAS RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (BS 1271) · airframe 55,674 hrs · 40,779 cycles

NOTED CORROSION ON SHEAR TIE, BS 1271, BETWEEN LONGERON 29R TO 30R. REMOVED CORROSION ON SHEAR TIE, BS 1271, LONGERON 29R-30R AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1, SHT 3. REPLACED SECTION OF SHEAR TIE AT BS 1271 LONGERON 28R-28L IAW SRM 53-03 FIG 3 & FIG 35.

Part: FLOOR SUPPORT — CORRODED (BS 1155) · airframe 55,674 hrs · 40,779 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BS 1155 STR 28R. CORROSION ON FLOOR SUPPORT IN AFT CARGO BAY BS 1155 STR 28R WAS FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT AND INSTALLED (NEW) FABRICATED FLOOR SUPPORT IAW SRM 53-01, 53-10-3, 51-10-2A, 51-10-3, 51-10-4, & 51-30-2.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 55,674 hrs · 40,779 cycles

LONGERON 23L FILLER STRIP FROM STA 1309-1287 HAS CORROSION MRB NR 53-100-15. REPLACED LONGERON 23L FILLER STRIP FROM STA 1309-1287 IAW SRM 51-30-2.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 55,698 hrs · 40,793 cycles

RT HORIZ STAB ELEVATOR DAMAGED ON T/E AT XE119. DAMAGE EXTENDS TO UPPER SKIN, INTERNAL FINGER DOUBLER, T/E, CHANNEL, AND LOWER SKIN. DAMAGE FOUND TO BE OUTSIDE SRM CH 55 ALLOWABLE LIMITS.

Part: SKIN — DENTED (PAX DOOR) · airframe 55,674 hrs · 40,779 cycles

FORWARD ENTRY BOTTOM OF DOOR OUTER SKIN IS BENT AND DENTED. FOUND DENT AND BEND ON FWD ENTRY BOTTOM OF DOOR TO BE OUT OF LIMITS. INSTALLED SKIN REPAIR IAW SRM 52-05 FIG 64.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 55,674 hrs · 40,779 cycles

CORROSION ON FWD CARGO DOORWAY, LWR THRESHOLD JAMB, NUMEROUS ARE AS BS 380-420. COMPLIED WITH PRI ER/A 508135-14, REV 0 AND ER/A508135-14, REV ORIGINAL ASSOCIATED ER/A 14-508135, ADDED FOR AC 0986.

Part: BRACKET — BENT (L1 DOOR) · airframe 55,225 hrs · 40,490 cycles

L1 DOOR BENT. REMOVED L1 DOOR TO FACILITATE REPAIR. REPLACED BENT BRACKET IAW DWG 5910081. REINSTALLED L1 DOOR IAW AMM 52-11-984486. CHECKED DOOR WARNING SYSTEM. OPS CHECKED GOOD IAW AMM 52-11.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,069 hrs · 40,376 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,344 hrs · 39,898 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHTS IN THE TAIL SECTION TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,327 hrs · 39,888 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE FIRST TWO EMERGENCY PATH LIGHTS IN THE TAIL SECTION TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LANYARD — BROKEN (R1 DOOR SLIDE) · airframe 54,087 hrs · 39,734 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE 1R DOOR SLIDE LANYARD CABLE TO BE BROKEN. MAINTENANCE REPLACED THE SLIDE LANYARD AND RETURNED THE AIRCRAFT TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,202 hrs · 38,476 cycles

STA 1418 S-2R SKIN CRACK. REPAIRED PER ERA 495160-14 REV 0.

Part: SKIN — NOT REPORTED (HORIZONTAL STAB) · airframe 52,188 hrs · 38,464 cycles

HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01086.

Part: SPAR — CRACKED (WING) · airframe 51,206 hrs · 37,808 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,934 hrs · 37,644 cycles

DURING LINE CHECK MX FOUND LT AND RT FWD OVERWING OVERHEAD LIGHT INOPERATIVE. MX REPLACED BATTERIES. OPS OF LIGHTS NOW CHECKS OK.

Part: HOUSING — NOT REPORTED (NLG) · airframe 50,866 hrs · 37,601 cycles

NLG HOUSING ASSY REPAIR, OVERHAUL IAW ERA 489342-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,789 hrs · 369,236 cycles

MX FOUND THE ESCAPE PATH LIGHT AT SEAT 2C TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,653 hrs · 36,178 cycles

OVERWING EMERGENCY LIGHTS INOP. REPLACED CONNECTOR OVERWING EMERGENCY LIGHT OPS NORMAL.

Part: BOOT — DAMAGED (RT PACK) · airframe 48,616 hrs · 36,153 cycles

AT 2000 MSL HOT ODOR NOTICED IN C/P SIMILAR TO HOT DUCTS F/A CALLED TO REPORT LAV SMOKE DETECTOR ON F/O SIDE NO SMOKE PRESENT MEX VALVE WERE AT MID RANGE DUCT TEMPT 80 DEG. INSPECTED ACFT FOR LEAKS NTF. INSPECTED APU INLET NTF. REPLACED 2 DUCT BOOTS RT PACK STATED OPN 5089 DUCT BURN ACCOMPLISHED TO ITEM 5. COMPLETED OP 5089 DUCT BURN

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,605 hrs · 36,146 cycles

FUSELAGE EXTERIOR LT NOSE GEAR DOOR CUTOUT AT AFT HINGE IN RADIUS. REPAIRED SKIN IAW SRM 53-05 FIG 67.

Part: ATTACH ANGLE — CRACKED (BS 1463 L4L) · airframe 48,605 hrs · 36,146 cycles

AFT ACCESORY COMPARTMENT LONGERON 4L ATTACH ANGLE IS CRACKE DAT STA 1463. REPLACED ATTACH ANGLE IAW DRAWING NR 9911839 IAW SRM 51-30-2, 51-30-5, 51-10-3, 51-10-4, 51-20-0. THIS OCCURRED DURING HMV IN DHN.

Part: FRAME — CORRODED (BULKHEAD) · airframe 48,605 hrs · 36,146 cycles

AFT CARGO COMPARTMENT FWD SIDE OF APB, TEE CHORD AND FRAME AFT SIDE HAS CORROSION AT L-30 TO L29L. MRB 53-100-17 REPLACE BOTH TEE CHORD AND T-CAP/FRAME/ANGLE.

Part: LONGERON — CORRODED (BS 1287-1308) · airframe 48,605 hrs · 36,146 cycles

AFT CARGO COMPT. STA 1287 TO 1308 L22L IS CORRODED. REMOVED CORROSION ON L22L FOUND TO BE 100 PERCENT MATL LOSS CUTOUT DAMAGED LONGERON 22L FROM STA 1250 TO 1305 REPAIRED LONGERON IAW SRM 53-02 FIG 18.

Part: ATTACH ANGLE — CRACKED (BS 1463) · airframe 48,605 hrs · 36,146 cycles

AFT ACCESSORY COMPARTMENT LONGERON 6L ATTACH ANGLE IS CRACKED AT STA 1463. REPLACED ANGLE IAW SRM 51-30-2,51-30-5,51-10-3,51-10-4,51-20-0 AND DWG NR 9911839 DURING HMV AT DHN.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 48,605 hrs · 36,146 cycles

FUSELAGE EXTERIOR LT FWD SIDE OF WHEEL WELL OPENING OTBD BELOW HYD HAND PUMP SUPPORT ANGLE INSIDE CRACKED. REPLACED ANGLE AND INSTALLED IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 48,605 hrs · 36,146 cycles

DURING HMV THE MAIN PAX FLOOR SUPPORT AT LT STA 160 TO 200 LBL 55 HAD CORROSION. REPLACED SUPPORT IAW SRM 53-14-1 FIG 11 SH 2,53-01 FIG 1 SH 3, 51-10-3, 51-30-02,51-30-05.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 48,605 hrs · 36,146 cycles

AFT ACCESSORY AIRSTAIRS STEP NR 6 FWD FACE PANEL AND ATTACHMENT ANGLE HAS SEVERAL AREAS OF CORROSION. REPLACED ANGLE IAW SRM 51-10-4, 51-10-2, 52-60-0.

Part: ATTACH ANGLE — CRACKED (BS 1463 L5L) · airframe 48,605 hrs · 36,146 cycles

AFT ACC COMPT LONG. 5L, ATTACH ANGLE IS CRACKED AT STA 1463. REMOVED, FABBED AND INSTALLED NEW ANGLE IAW SRM 51-30-02, 51-30-5, 51-10-03, 51-10-04, 51-20-00 AND DWG 9911839.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · airframe 48,605 hrs · 36,146 cycles

DURING HMV3, FOUND AFT CARGO COMPARTMENT NR 3 RT TIE DOWN TRACK HAS SEVERAL SPOTS OF CORROSION BS 1212 TO 1322. REMOVED CORROSION IAW SRM 51-10-03 100 PERCENT MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-01 FIG 1. REMOVE TIE DOWN TRACK STA 1212-1322 RT SIDE IAW SRM 51-30-01. DRILLED NEW TIE DOWN TRACK IAW SRM 51-10-2 AND 51-10-4 PN 59366634505, INSTALLED IAW SRM 51-30-01 AND 51-30-5.

Part: SKIN — DENTED (BS 530 S26-27R) · airframe 41,050 hrs · 31,399 cycles

FOUND AIRCRAFT FUSELAGE DAMAGED AT APPROX STA 530 BETWEEN LONGERON 26R AND 27R. REMOVED DAMAGE. FABRICATED REPAIR PER SRM 53-04 FIG 12B CLASS I REPAIR. OK TO TREAT AND PAINT AREA AND REPAIR PIECE QC1509. TREATED AND PAINTED AREA AND REPAIR PER SRM 53-04 FIG 12B. TREAT AND PAINT OK. OK TO INSTALL REPAIR QC1509, INSTALLED REPAIR PER SRM 53-04 FIG 12B. REPAIR INSTALLATION OKQC1418.

Part: TRIM SWITCH — DEFECTIVE (COCKPIT) · airframe 40,282 hrs · 30,859 cycles

RETURNED TO ATL PRIMARY STABILIZER TRIM FAILED ALTERNATE, TRIM OK. FOUND CO PILOTS LONG TRIM CONTROL SWITCH OTBD SW NOT RETURNING TO SPRING LOADED CENTER POSITION ALLOWING SWITCH FLOAT AND MAKE CONTINUITY THROUGH SWITCH. REPLACED COPILOTS PRIMARY TRIM SWITCH ASSY NOW PRIMARY TRIM, OPS CKS GOOD PER 27-40-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,911 hrs · 30,576 cycles

COCKPIT EMERGENCY EXIT LIGHT, L1 DOOR AND RIGHT SVC DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES, CHECK OK.

Part: ENGINE — FAILED (NR 2) · airframe 34,615 hrs · 26,775 cycles

INFLT SHUT DOWN DUE TO LOSS OF OIL QTY AND HIGH OIL TEMP. REPLACED ENGINE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 32,318 hrs · 25,169 cycles

F/C CABIN EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,291 hrs · 21,510 cycles

03C EMERGENCY TRACK LIGHT INOP. REPLACED LIGHT ASSY 333201532, NOW TESTS OK.

Part: INLET — CONTAMINATED (APU) · airframe 24,542 hrs · 19,480 cycles

ATB DUE F/A REPORTED AN ELEC ODOR AND ANOTHER REPORTED OILY. MTC FOUND LIGHT CONTAMINATION IN APU INLET. CLEANED INLET AND PERFORMED DUCT BURNOUT.

Part: PSEU — MALFUNCTIONED (E/E BAY) · airframe 24,234 hrs · 19,248 cycles

GEAR UNSAFE LIGHTS REMAINED ON AFTER GEAR RETRACTION. AFTER CHECK LIST ACCOMPLISHED UNSAFE LIGHTS REMAINED ON, ALL OTHER SYSTEMS NORMAL. PSEU NO FAULTS, GEAR POSITION SENSORS CHECK GOOD. CHECKED GEAR HANDLE SWITCH, ALT GEAR HANDLE SWITCH, ALL CHECKED GOOD. REPLACED PSEU PRECAUTIONARY, JACKED AIRCRAFT, ALL LANDING GEAR INDICATIONS CHECKED NORMAL ON GEAR SWING.

Part: LINE — RUPTURED (HYDRAULIC SYS)

APPROXIMATELY 30 MINUTES BEFORE ARRIVING ATL, THE RIGHT HYD SYSTEM DECREASED TO 3 QUARTS AND ZERO HYD PRESS FOLLOWED BY APU SHUTDOWN. RAN THE EMERG PROCEDURES IAW POM. UPON GEAR EXTEND THE GEAR WENT DOWN BUT THE GEAR DOORS DID NOT COME BACK UP. REPLACED RUPTURED FLEX LINE AT CASE DRAIN FILTER.

Part: GENERATOR — FAILED (LEFT)

APPROX 4 MIN AFTER T/O, CAPT PFD AND ND BEGAN TO FAIL AND BLANK. ABOUT 2 MIN LATER LT GEN FAILED, RT GEN DID NOT PICK UP LOAD. PWR WOULD SHIFT BETWEEN FAILING AND X-TIE. STARTED APU AS BACKUP AND LT GEN WAS OK FOR REMAINDER OF FLT.

Part: TRANSDUCER — SHEARED (NR 1 MLG)

A/C OVERRAN RUNWAY. FOUND NR 1 MAIN ANTI-SKID TRANSDUCER PIN SHEARED. REPLACED TRANSDUCER.

Part: ELECT OUTLET — SHORTED (CABIN)

ON PREFLT, FOUND UTILITY C/B OPEN WHEN RESET SPARKS FROM UTILITY OUTLET. FWD UTILITY OUTLETS TO MCO COLLARED, C/B SUSPECT PLUG DAMAGED.

Part: FLIGHT MODE ANN — SHORTED (LT COCKPIT)

PUNGENT SMOKE IN COCKPIT ON TAXI-OUT, RETURNED TO GATE. FOUND CAPTS FMA CAUSING SMOKE IN COCKPIT. REPLACED CAPTS FMA, ALL INSTRUMENTS CK NORMAL. NO WIRING TROUBLE NOTED. FLIGHT MODE ANNUNCIATOR (DPN 229001002) (P/N 4032434-902) (S/N 91112590).

Part: SWITCH — FAILED (MLG)

ON TAKEOFF, THE LANDING GEAR WARNING HORN CAME ON (UNTIL IT WAS RAISED). WHEN GEAR HANDLE WAS RAISED, THE RED LIGHT STAYED ON AND THE GEAR DOOR LIGHT WENT OUT. CYCLED THE LANDING GEAR AND GOT 3 DOWN AND LOCKED (NORMAL INDICATIONS). WHEN GEAR WAS RAISED AGAIN, THE RED WARNING LIGHT REMAINED LIT. REPLACED SWITCH S-320, SYSTEM CKS NORMAL PER M/M.

Part: ANGLE — CRACKED (NR 2 ENG PYLON)

NR 2 ENG PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED 1 INCH. FOUND DURING D-1 LTR CK TPAMM. REPAIRED PER SRM 54-04A FIG 4.