N956DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,873 hrs · 56,056 cycles

EMERGENCY ROW LIGHTS ABOVE SEATS 24, 25 INOP. REMOVED AND REPLACED BATTERIES PER MD88 AMM 33-53. ALL LIGHTS OPS CHECK GOOD. (LP5001016)

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 74,714 hrs · 55,910 cycles

SHIP 0956 - WHILE ON APPROACH INTO ATL, THE COCKPIT NOTICED AN ELECTRICAL SMELL AND THIN SMOKE FROM THE LEFT WINDSHIELD HEAT TERMINAL. THE WINDSHIELD ANTI-ICE WAS TURNED OFF AND THE ODOR AND LIGHT SMOKE IMMEDIATELY DISSIPATED. CORRECTIVE ACTION: MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD, HEAT CONTROLLER, AND TERMINAL HARDWARE PER THE MAINTENANCE MANUAL. (LP 5352102)

Part: BUTTON — MISSING (WING) · airframe 74,656 hrs · 55,853 cycles

THIS IS A FOLLOW ON LOG FOR LP4763518 CLOSED IN ERROR PANEL INBOARD OF FUELING ACCESS PANEL MISSING BUTTON THAT FAIRS TO PANEL SKIN. LATCH WORKS AND SECURES ITS LOCATION. REPL LATCH. SDR REPORTED DUE TO FACT THAT LATCH MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP0770002)

Part: BUTTON — MISSING (WING) · airframe 74,632 hrs · 55,829 cycles

RAMP, ON THEIR WALK-AROUND INSPECTION OF AIRCRAFT NOTED LATCH (CENTER) OF THE PANEL INBOARD OF FUELING ACCESS PANEL MISSING BUTTON THAT FAIRS TO PANEL SKIN. LATCH WORKS AND SECURES ITS LOCATION. REPORTED DUE TO THE POSSIBILITY THAT PART MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP4763518)

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 74,444 hrs · 55,649 cycles

F/A REPORTS A/C RIGHT AFT LAV SMOKE ALARM CHIRPING, LOW BATTERY. INSTALLED NEW SMOKE DETECTOR PER AMM 2613 - OPS CKS NML. SECURITY SEALS INSTALLED.

Part: UNKNOWN — UNKNOWN (EMERGENCY POWER) · airframe 74,392 hrs · 55,601 cycles

EMERGENCY POWER INOPERATIVE. PERFORMED EMERGENCY LIGHTS TEST IAW AMM 33-53 OPS, TESTED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,868 hrs · 55,147 cycles

BOTH AFT OVERWING UPPER EXIT LIGHTS INOP. REPLACED BATTERIES AT B5105 REF AMM 33-53. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 73,787 hrs · 55,085 cycles

FLT ATTENDANTS REPORT A CHIRPING SOUND, INTERMITTENTLY FROM AFT RIGHT LAVATORY. REPLACED THE AFT RIGHT LAVATORY SMOKE DETECTOR BATTERY IAW AMM 26-13. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (OIL TEMP BULB) · airframe 73,546 hrs · 54,894 cycles

IN FLIGHT SHUTDOWN AND AN AIR TURNBACK WITH A LEFT ENGINE OIL ISSUE. CREW REPORTED LEFT OIL TEMP CLIMBED TO 180 DEGREES AND IAW QRH SHUTDOWN THE ENGINE. MAINTENANCE FOUND THE LEFT ENGINE OIL TEMP BULB CONNECTOR LOOSE. THE OIL TEMP RISE WAS ABLE TO BE DUPLICATED BY SHAKING THE CONNECTOR WIRES. THE CONNECTOR WAS REPLACED AND PINS REPLACED. AN ENGINE RUN WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,530 hrs · 54,882 cycles

SEAT 24DE - ROW 30DE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY AT BS 1233 IAW AMM 33-53.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,418 hrs · 54,793 cycles

EMERGENCY LIGHTS INOPERATIVE, ROW 24 - 36. REPLACED THE BATTERY BASE B5-212, CHECKED OK IAW WDM 33-51.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,395 hrs · 54,778 cycles

DURING LINE CHECK, THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 13 INOPERATIVE. INSTALLED A NEW BULB IAW MM 33-51. OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 73,395 hrs · 54,778 cycles

ALL EMERGENCY LIGHTS AFT OF OVERWING EXIT INOPERATIVE. FOUND THE FUSE BLOWN IN FWD BATTERY PACK B5-211. REPLACED THE FUSE AND OPS CHECKED GOOD IAW MM 35-50.

Part: UNKNOWN — ODOR (CABIN) · airframe 73,381 hrs · 54,765 cycles

DUE TO PILOT REPORT OF FUMES IN CABIN AFTER TAKE OFF. AFT LAVATORY SMOKE ALARMS ACTIVATED. COMPLIED WITH NO GO ODI PREVENTION 2172. NO TROUBLE FOUND.

Part: PIN — MISSING (L1 DOOR SLIDE) · airframe 72,990 hrs · 54,456 cycles

DURING INSPECTION OF THE L1 DOOR SLIDE, FOUND THE PARACHUTE PINS NOT INSTALLED. R & R THE L1 DOOR SLIDE IAW W/C 2561-4964.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,514 hrs · 54,095 cycles

SEATS 24DE-30DE EMERG LIGHTS INOP. R/R EMERG LIGHTS POWER SUPPLY PER AMM 33-51. OPS CHK GOOD. (LP3546186)

Part: FUSE — BLOWN (CABIN) · airframe 72,075 hrs · 53,750 cycles

EMERGENCY LIGHTS SEAT MOUNTED NOT WORKING FROM ROW 24 TO 31. T/S PER WDM 33-51-14, FOUND FUSES BLOWN ON POWER SUPPLY B5-212. REPLACED FUSES. OPS CHECK PER AMM 33-53. CHECKS OK.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 71,933 hrs · 53,622 cycles

LEFT VERTICAL STAB FRONT SPAR CAP HAS 4 CRACK INDICATIONS INSIDE FASTENER HOLES ABOVE AND BELOW LEADING EDGE SKIN SPLICE STA. ZFS=52.267. REPAIR PER ERA 561317-14AD REV ORIG. (LP0195348)

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 71,932 hrs · 53,621 cycles

L1 DOOR SLIDE1. THE LACE CABLE PIN REMOVED AND SAFETY PIN NOT INSTALLED P/N D29982-225S/N 27452. THE GIRT BAR CABLE IS FRAYED. REPLACED SLIDE ASSY PER OPN 2561-4964.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 71,932 hrs · 53,621 cycles

AFT CARGO BAY, LOWER SILL CORRODED, ALONG ENTIRE LENGTH, AT NUMEROUS NUTPLATE HOLES.

Part: GCU — FAILED (LT & RT) · airframe 71,908 hrs · 53,601 cycles

DURING SHORT FINAL, TOTAL ACFT ELECTRICAL FAILURE OCCURRED. LANDED ON EMERGENCY POWER. RAN QRH AND LEFT GENERATOR RESET. RIGHT GENERATOR VOLTS AND FREQUENCY READ ZERO. LEFT GCU HAS GCU FAULT. REPLACED LEFT AND RIGHT GCUS IAW AMM 24-20. RAN BOTH ENGINES AND RIGHT GEN STILL INOP. FOUND RIGHT GENERATOR SHAFT SHEARED. REPLACED RIGHT GENERATOR IAW AMM 24-20. ENGINE GENERATOR RUN GOOD. PERFORMED BATTERY AND CHARGER CHECK AMM 24-23-01.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 71,667 hrs · 53,422 cycles

DURING SERVICE CHECK, EMERGENCY LIGHTS AT SEAT ROWS 24 TO 30 INOPERATIVE. TROUBLESHOT IAW WDM 33-51-14. FOUND A BAD FUSE F-2 AT THE B5-212 BATTERY PACK. REPLACED THE FUSE, OPS NORMAL.

Part: STIFFENER — CRACKED (BS 1463) · airframe 70,727 hrs · 52,677 cycles

SEVERAL CRACKS ON AFT FUSELAGE WATER PROTECTION LOUVER SHIELD STIFFENER BETWEEN LONGERON 5 & 7L, BS 1463. REPLACED THE STIFFNER IAW DRAWINGS 9911839 AND 995305.

Part: ATTACH ANGLE — CRACKED (BS 1463) · airframe 70,727 hrs · 52,677 cycles

LOWER FWD VENT LOUVER ATTACH ANGLE CRACKED AT BS 1463. REPLACED THE ANGLE IAW DRAWINGS 9911839 AND 9953015.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 70,582 hrs · 52,559 cycles

EMERGENCY LIGHT CHECK FOUND HATCH FLOOR LIGHTS L2-834, L2-835, L2-836, L2-837 INOPERATIVE. TROUBLESHOT IAW WDM 33-51-14 SHEET 1 AND SHEET 2. FOUND BLOWN FUSE AT B5-211, P1791 11. REPLACED THE FUSE, BLEW AGAIN, R & R THE BATTERY CHARGER ASSY B5-211 IAW AMM 33-53-00. OPS CHECKED OK.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 69,748 hrs · 51,952 cycles

DAMAGE TO TRAILING EDGE FLAP SECTION RT SIDE AT FLAP STA. 263. REMOVED SKIN ON FLAP SECTION (LWR SKIN) REMOVED DAMAGED RIB. FABRICATED NEW SKIN PANEL FOR 7075-T6 .063". ROUTED TO COMPOSITE SHOP FOR BONDING. WEIGHED REPLACEMENT SKIN 7.5LBS WEIGHED ORIGINAL SKIN PANEL 6.5 LBS. INSTALLED RIB AND SKIN IAW PRI 551315-14. INSTALLED 2 OUTBOARD SECTIONS OF T/E FLAP IAW MD 88 AMM 27-51-01. OK FOR SERVICE. INSTALLED LINKS BETWEEN 2 TRAILING EDGE FLAP WEDGE AND SAFTIED. (LP2708829)

Part: FUSE — DEFECTIVE (CABIN) · airframe 69,659 hrs · 51,885 cycles

CABIN EMERGENCY LIGHT AT SEAT 24 TO 30 INOPERATIVE. TROUBLESHOT IAW WDM 33-51 AND FOUND BAD FUSES. R & R FUSES IAW AMM 33-50. OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,623 hrs · 51,853 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OUT FROM ROWS 24EF THRU 30 E AND F RT SIDE. REMOVED & REPLACED THE POWER SUPPLY, OPS CHECKED GOOD.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 66,855 hrs · 49,891 cycles

RIGHT ELEVATOR GEARED TAB UPPER SURFACE HAS APPROXIMATELY .5 SQUARE FOOT OF DELAMINATED. R & R GEAR TAB. OP'S CHECKS COMPLETED ON AMDS 2730-4130.

Part: BLOCK — OUT OF RIG (TAILCONE) · airframe 66,855 hrs · 49,891 cycles

THE TAIL CONE UPPER RT BAYONET LOCK CABLE SLIDING BLOCK WAS FOUND OUT OF RIG, IT HAD A .7500" GAP ABOVE THE BAYONET LEVER PIN, WHERE ZERO GAP IS PERMITTED. MSP MAINTENANCE CHECKED AND ADJUSTED THE SLIDING BLOCK. IT IS WITHIN LIMITS NOW.

Part: FAIRING — CRACKED (LT WING SLT TRK) · airframe 66,855 hrs · 49,891 cycles

LT WING L/E SLAT TRACK NR 7 LOWER FAIRING PANEL CRACKED. NEW PN 9954169-537, FABRICATED IAW ERA 512356-14MA. FABRICATED NEW PANEL IAW ER/A 512356-14MA. FIT CHECKED AND FINAL ADJUSTMENT OK.

Part: SKIN — DELAMINATED (RT WING TE) · airframe 66,855 hrs · 49,891 cycles

RT WING T/E, UPPER SURFACE PANEL DELAMINATED JUST OTBD OF FUSELAGE. R & R THE PANEL IAW DWG 9936821.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,462 hrs · 51,739 cycles

CRACKS WERE FOUND EMANATING FROM 3 FASTENER HOLES AT BS 1380 AND L-14R. ERA 538627-14, SECTION I ISSUED FOR REPAIR ALONG LONGERON 14R SKIN LAP JOINT, AT STA 1380.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 66,855 hrs · 49,891 cycles

LT WING, CENTER FLAP VANE UPPER SURFACE CHAFED THRU JUST AFT OF INBD FLT SPOILER OTBD END. REPLACE DOUBLER REF SRM 51-70-02 DRD.

Part: SKIN — CORRODED (BS 252) · airframe 69,972 hrs · 52,114 cycles

THE FUSELAGE SKIN IS CORRODED UNDER THE LOWER TCAS ANTENNA DOUBLER, BS 252 BETWEEN LONGERONS 29 AND 30.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 63,445 hrs · 47,508 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE TAIL WERE INOPERATIVE. MAINTENANCE REPLACED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: PANEL — DISLODGED (TAILCONE) · airframe 62,964 hrs · 47,205 cycles

CAPTAIN DISCOVERED A CEILING PANEL IN TAILCONE WAS HANGING DOWN AND BLOCKING EGRESS PATH. CEILING PANEL SECURED.

Part: HEATER BLANKET — DAMAGED (RT WING) · airframe 62,307 hrs · 46,746 cycles

A VOID AREA WAS FOUND OF 240 SQUARE INCHES AT RT WING HEATER BLANKET AND FOUND OUT OF LIMITS IAW 5700-2232. RT HEATER BLANKET PANEL WAS REPLACED IAW AMM 30-80-02. OPS TEST OK IAW AMM 30-80-02-501.

Part: HEATER — DAMAGED (LT WING) · airframe 62,307 hrs · 46,746 cycles

DURING INPECTION FOR VOIDS, A SINGULAR VOID AREA WAS FOUND, 193 SQUARE INCHES AT LT WING HEATER BLANKET, OUT LIMITS IAW CARD 5700-2232. FIG 1, STEP 1(B). LT WING HEATER BLANKET PANEL WAS REPLACED IAW AMM 30-80-02. OPS TEST OK IAW AMM 30-80-02-501.

Part: LEVER — WORN (TAILCONE RELEASE) · airframe 62,308 hrs · 46,747 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE LOCK-PIN LEVERS AT THE UPPER RT POSITIONS WERE WORN BEYOND ALLOWABLE LIMITS. LOCK-PIN LEVERS WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 62,308 hrs · 46,747 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN. THE CAM BASE WAS REPLACED IAW AMM 53-53-02.

Part: LONGERON — CORRODED (BS 490) · airframe 62,307 hrs · 46,746 cycles

CORROSION ON LONGERON 30 BS 490, IN FWD CARGO BAY. CORROSION REMOVED, AND FOUND OUT OF LIMITS, LONGERON REMOVED BS 455 - 494, NEW LONGERON AND SPLICE INSTALLED IAW SRM 53-02, FIG 18, 51-10-3, PAR 21-14, 51-30-5, 51-30-2, 51-10-2, 51-10-2A AND DWG 3936478, REV D.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,307 hrs · 46,746 cycles

LIGHTNING STRIKES ON RT WINDOW BELT FRAME BETWEEN BS 446 TO 465 AT AFT LOWER CORNER AND FWD LOWER CORNER. DAMAGE BLENDED AND WITHIN LIMITS IAW ER/A 517520-14, REV ORIGINAL.

Part: SUPPORT — BROKEN (BS 1117-1079) · airframe 62,307 hrs · 46,746 cycles

BROKEN COMPOSITE MATERIAL LATERAL SLANT SUPPORTS AT BS 1117 AND 1079 BETWEEN LONGERONS 26-28L, AFT CARGO BAY. SLANT SUPPORTS WERE REPLACED IAW ER/A 413029-14 MA REV D.

Part: FRAME — CRACKED (BS 1510) · airframe 62,307 hrs · 46,746 cycles

CRACK ON PREVIOUS REPAIR ON FRAME AT BS 1510. DOUBLER WAS REMOVED IAW 51-30-5. NEW DOUBLER WAS INSTALLED IAW ER/A 497316-14MA, REV ORG.

Part: SUPPORT — BROKEN (BS 1098) · airframe 62,307 hrs · 46,746 cycles

BROKEN COMPOSITE MATERIAL LATERAL SUPPORT AT BS 1098 BETWEEN LONGERONS 26 - 28R, AFT CARGO COMPARTMENT. SUPPORT WAS REPLACED IAW ER/A 413029-14MA REV D.

Part: DOOR — DAMAGED (SLAT) · airframe 62,307 hrs · 46,746 cycles

WEAR ON SLAT DOORS. BLENDED AND FOUND WITHIN LIMITS BUT NR 12 IS OUT OF LIMITS. FABRICATED IAW ER/A 512356-14 MA, REV ORIG.

Part: DOOR — WORN (SLAT) · airframe 62,307 hrs · 46,746 cycles

WEAR ON SLAT DOORS LT WING. NR 12 IS OUT OF LIMITS. FABRICATED IAW ER/A 512356-14MA, REV ORIG.

Part: TEE FITTING — DAMAGED (BS 1338) · airframe 62,307 hrs · 46,746 cycles

NICKS ON TEE BETWEEN LONGERONS 26 AND 27 LEFT BS 1338 AT AFT CARGO. TEE REMOVED, NEW TEE INSTALLED IAW DWG SR09530056, REV J AND SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION IN THE COUNTERSINK HOLES OF WING FUEL ACCESS PLATE 1410C. BLEND OUT WAS NOT PERMITTED TO THE EXTENT REQUIRED AND THE PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION IN THE COUNTERSINK HOLES OF WING FUEL ACCESS PLATE 1414C. BLEND OUT WAS NOT PERMITTED TO THE EXTENT REQUIRED AND THE PANEL WAS REPLACED.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 62,307 hrs · 46,746 cycles

TOOL DAMAGE ON OTBD WALL OF DOME NUT AT LT WING CUTOUT LOWER FUEL TANK ACCESS PLATE NR 1355C. REPAIRED IAW ER/A 519123-14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION IN THE COUNTERSINK HOLES OF WING FUEL ACCESS PLATE 1363C. BLEND OUT WAS NOT PERMITTED TO THE EXTENT REQUIRED AND THE PANEL WAS REPLACED.

Part: SKIN — DAMAGED (BS 750-769) · airframe 62,307 hrs · 46,746 cycles

LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 750-769 FWD AND AFT LWR CORNER. REPAIRED IAW ER/A 519111-14.

Part: ACCESS PANEL — CORRODED (WING) · airframe 62,307 hrs · 46,746 cycles

CORROSION IN THE COUNTERSINK HOLES OF WING FUEL ACCESS PLATE 1357C. BLEND OUT WAS NOT PERMITTED TO THE EXTENT REQUIRED AND THE PANEL WAS REPLACED.

Part: ACCESS PANEL — DAMAGED (WING) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION, IN THE COUNTERSINK HOLES OF WING FUEL ACCESS PLATE 1409C. BLEND OUT WAS NOT PERMITTED TO THE EXTENT REQUIRED AND THE PANEL WAS REPLACED.

Part: ACCESS PANEL — DAMAGED (WING) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION IN THE COUNTERSINK HOLES OF WING FUEL ACCESS PLATE 1303C. BLEND OUT WAS NOT PERMITTED TO THE EXTENT REQUIRED AND THE PANEL WAS REPLACED.

Part: FORMER — CORRODED (BS 1380) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION ON FORMERS BS 1380 BETWEEN X=12. CORROSION REMOVED WAS BEYOND ACCEPTABLE LIMITS AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-70-5, FIG 1.

Part: LONGERON — CRACKED (BS 693) · airframe 62,307 hrs · 46,746 cycles

CRACKED LONGERON 6L INTERSECTING FRAME BS 693. REPAIRED IAW 519118-14.

Part: LONGERON — CRACKED (BS 1431) · airframe 62,307 hrs · 46,746 cycles

CRACKED LONGERON 9L AT BS 1431. SECTION OF LONGERON WAS REMOVED. REPAIR SPLICE FABRICATED, NEW LONGERON AND SPLICES WERE DRILLED AND PRIMER, INSTALLED IAW SRM 53-02, FIG 18 , 51-30-2, 51-30-5, 51-10-3 PAR 21/14.

Part: CUSP WEB — CORRODED (BS 907-1019) · airframe 62,307 hrs · 46,746 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 TO -60 BS 907-1019. REWORKED PER LIMITS IDENTIFIED IN ER/A 511165-14. STA 995-999 IS BEYOND ACCEPTABLE LIMITS AND WAS REPAIRED ON NON ROUTINE 636 IN ZONE 58.

Part: LONGERON — CRACKED (BS 1431) · airframe 62,307 hrs · 46,746 cycles

CRACKED LONGERONS 9 & 10R AT INTERSECTION WITH AFT ACC COMP CANTED FRAME BS 1431. SECTION DAMAGE REMOVED, SPLICE WERE FABRICATED, NEW LONGERONS SECTION WERE DRILLED AND ADJUSTED, WERE TREATED AND PAINTED REPAIR PARTS AND LONGERONS SECTION WERE INSTALLED IAW SRM 53-02, FIG 18 51-10-3, PAR 21/14.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,307 hrs · 46,746 cycles

CRACKED LONGERON NR 1 ON INTERSECTION WITH FRAME 1437, ALSO DRILLED HOLES ON SAME LONG STA 1418 AT AFT ACC COMP. DAMAGE LONGERONS WERE REMOVED NEW LONGERON WERE DRILLED AND ADJUSTED, SPLICE AT STA Y=1418 WAS DRILLED AND ADJUSTED, LONGERONS AND SPLICE WERE TREATED AND PAINTED, WERE INSTALLED IAW SRM 53-02, FIG 18 AND ER/A 517518-14 REV ORIGINAL.

Part: LONGERON — CORRODED (BS 1287-1322) · airframe 62,307 hrs · 46,746 cycles

CORROSION ON LONGERON 27LT BETWEEN STA Y=1287-1322 ATAFT CARGO COMPARTMENT REF CARD 310, ZONE 57, AND (T0 292485) MRB 53-139-05. LONGERON 27 LT WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: FRAME — DAMAGED (BS 1485) · airframe 62,307 hrs · 46,746 cycles

CRACKED PREVIOUS REPAIR FRAME ON BS 1485 AND X=-16 AT AFT ACCESSORY COMPARTMENT. CRACKED REPAIR REMOVED, DAMAGE FRAME WAS CUT OUT, WAS FABRICATED NEW REPLACEMENT SECTION OF FRAME AND SPLICE, WERE TREATED AND PAINTED AND REPAIR PARTS WERE INSTALLED IAW ER/A 385948-14 MA REV. ORIGINAL.

Part: STRUCTURE — DAMAGED (RUDDER TAB) · airframe 62,307 hrs · 46,746 cycles

DAMAGED FLAME SPRAY ON RUDDER CONTROL TAB. DAMAGED FLAME SPRAY ON RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1, AD PAR 23 AND CARD 2000-8149-08, 6467033, JOB 000-0046. RII COMPLETED.

Part: DUCT — CRACKED · airframe 62,307 hrs · 46,746 cycles

CRACK ON LT RADIO RACK EXHAUST DUCT STA Y=256 275 BETWEEN, LONG 20LH-21LH AT FUSELAGE SKIN (FS). LT RADIO RACK EXAHUST DUCT WAS REPAIR IAW ER/A 464964-14MA, REV A.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 62,307 hrs · 46,746 cycles

DAMAGED FLAME SPRAY ON BOTH RUDDER SURFACES. DAMAGE FLAME SPRAY ON BOTH RUDDER SURFACES WERE REPAIRED IAW SRM 51-70-1 AD PAR 23 AND AC 0956.

Part: FRAME — CRACKED (BS 1418) · airframe 62,307 hrs · 46,746 cycles

CRACKED FRAME ANGLE BS 1418 AND LONG 2L AT AFT ACCESSORY BAY. DAMAGE LONGERON SECTION AND CRACKED FRAME ANGLE WERE REMOVED, NEW LONGERON SPLICE AND NEW FRAME ANGLE WERE DRILLED AND ADJUSTED, TREATED, AND PAINTED. INSTALLED IAW SRM 53-02, FIG 18 51-10-3, PAR 21/14, 51-30-5 AND 51-30-2.

Part: FRAME — CRACKED (BS 1174) · airframe 62,307 hrs · 46,746 cycles

CRACK ON FRAME AT BS 1174 AND LONGERON 6L. REPAIRED IAW ER/A 495237-14MA AND AMR 0953914 REV.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,307 hrs · 46,746 cycles

CRACKED LONGERON 2R AT INTERSECTION WITH AFT ACCESSORY COMP FRAME 1418. DAMAGE LONGERON SECTION WAS REMOVED, NEW LONGERON SECTION WAS DRILLED, ADJUSTED, TREATED, PAINTED, AND WAS INSTALLED IAW SRM 53-02, FIG 18, 51-10-3, PAR 21/14. RII COMPLETED.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,307 hrs · 46,746 cycles

CRACKED LONGERON 3L AT INTERSECTION WITH AFT ACC COMPARTMENT FRAME 1437. DAMAGED SECTION WAS REMOVED, NEW LONGERON SECTION WAS DRILLED AND ADJUTED, SPLICE WAS FABRICATED, TREATED, PAINTED AND WAS INSTALLED IAW SRM 53-02, FIG 18, 51-10-3, PAR 21/14. RII COMPLETED.

Part: CABLE — FRAYED (R1 DOOR SLIDE) · airframe 62,307 hrs · 46,746 cycles

MX DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1R HAD A FRAYED CABLE. A FAILURE OF THIS CABLE WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE DOOR SLIDE CABLE WAS REPLACED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,307 hrs · 46,746 cycles

CRACKED FUSELAGE SKIN ON FWD UPPER CORNER AT R1 DOOR CUT OUT. DAMAGE AREA WAS REMOVED. REPAIR PARTS, FILLER, DOUBLER AND TRIPLER WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, FIG 112, 51-30-2, 51-30-5, 51-10-3, PAR 14/21 AND REPAIR WAS IDENTIFIED IAW PS 900-5-1, NO 04 INSPECT THE SUBJECT REPAIR AS DESCRIBED IN SRM 53-05, FIG 112, GN 22, SRM 51-10-5C AT THE FOLLOWING INTERVALS INITIAL 28,000 REPETITVE 20,000. RII COMPLETED.

Part: CUSP WEB — CORRODED (BS 900) · corrosion level 2 · airframe 62,307 hrs · 46,746 cycles

CORROSION ON LT CUSP WEB BS 990 BETWEEN X=54 AND X=60. DAMAGED WAS REMOVED, DOUBLER, FILLER WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, FIG 131A-1, SRM 51-10-3 AND PS 900-5-1.

Part: RELEASE CABLE — CORRODED (TAILCONE) · airframe 62,307 hrs · 46,746 cycles

MX DISCOVERED THE TAILCONE EMERGENCY RELEASE CABLE WAS CORRODED BEYOND ALLOWABLE LIMITS. CABLE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS.

Part: LONGERON — DEFORMED (BS 237) · airframe 62,307 hrs · 46,746 cycles

DEFORMED LONGERON 17L AT INTERSECTION WITH FRAME BS 237 PAX CABIN. REPLACED SECTION LONGERON, DAMAGE IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (BS 1418) · airframe 61,548 hrs · 46,187 cycles

SKIN DAMAGED AT BS 1418 L2L. REPAIRED IAW ER/A 489706-14AD, REV C.

Part: SKIN — DAMAGED (BS 1418) · airframe 61,548 hrs · 46,187 cycles

SKIN DAMAGED AT BS 1418 L2R. REPAIRED IAW ER/A 489706-14AD, REV C.

Part: WEB — CRACKED (BS 1485) · airframe 61,548 hrs · 46,187 cycles

BELT FRAME WEB CRACKED AT CANTED BS 1485 NEAR 8:00 POSITION, AT INTERIOR TAIL CONE JETTISON HANDLE SUPPORT STRUCTURE. REMOVED ATTACH CLIPS AND MADE NEW ONES IAW DWG 9911867. REINSTALLED SWITCH CONNETOR, 2 CLAMPS, AND CONE JETTISON HANDLE ASSY. C/W PRI 515158-14, REV 0. RECEIVED FINAL ER/A 515158-14, REV ORIG ASSOCIATED ER/A 14-515158 ADDED FOR AC 0956.

Part: SKIN — CORRODED (BS 636 L28-29R) · airframe 61,548 hrs · 46,187 cycles

DURING SCHEDULED INSPECTION, CORROSION FOUND AT C2 WEDGE BS 636 ON TOP OF WEB L28-29R. CORROSION REMOVED IAW SRM 53.01, FIG 1.

Part: SHEAR TIE — CORRODED (BS 636) · airframe 61,548 hrs · 46,187 cycles

DURING SCHEDULED INSPECTION, CORROSION FOUND AT C2 BS 636 L29L TO L29R. CORROSION WAS BLENDED AND DETERMINED TO BE OUT OF LIMITS. NEW SHEAR TIE FABRICATED IAW DWG S25061915S AND INSTALLED IAW DAC 9936073.

Part: SKIN — CORRODED (BS 719 L29L) · airframe 1 hrs · 1 cycles

FUSELAGE FS 719 L29L AFT ALTIMETER CUTOUT CORRODED. REPAIRED IAW ERA 513976-14.

Part: ANTENNA — DAMAGED (TCAS) · airframe 61,409 hrs · 46,075 cycles

LOWER TCAS ANTENNA DAMAGED. LOWER TCAS ANTENNA REMOVED REF 34-46. FOUND CORROSION UNDER ANTENNA DOUBLER, REMOVED SAME. INSTALLED IAW REPAIR IAW ER/A 513946-14, REV ORIG.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,499 hrs · 45,391 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT SEATS IN THE CENTER WING SECTION WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: DUCT — BLOWN (NR 2 ENGINE) · airframe 59,634 hrs · 44,786 cycles

DURING CLIMB, FLIGHT CREW NOTED AN INTERMITTENT FIRE LIGHT AND AURAL WARNING ON THE NR 2 ENGINE. FLIGHT CREW THEN PERFORMED AN UNEVENTFUL AIR TURN BACK. ON INSPECTION, MAINTENANCE FOUND THE PNEUMATIC DUCT ON THE TOP OF THE NR 2 ENGINE TO BE BLOWN. MAINTENANCE REPLACED THE DUCT, RAN THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE.

Part: LANYARD — DISCONNECTED (L2 DOOR SLIDE) · airframe 59,288 hrs · 44,532 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 2L HAD THE GIRT BAR CABLE DISCONNECTED. THE DOOR SLIDE LANYARD WAS CONNECTED.

Part: LIGHT — INOPERATIVE (ROW 27) · airframe 59,202 hrs · 44,489 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 27D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,996 hrs · 44,368 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT TWO OF THE EMERGENCY PATHWAY LIGHTS HAD FAILED. MAINTENANCE DETERMINED THAT THE BATTERIES WERE DEFECTIVE AND REPLACED THEM. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,980 hrs · 44,357 cycles

FLOOR SUPPORT CORROSION STA 254 LBL 3 AFT END. REPAIRED BY REPLACEMENT OF PART 5930544-143 REF MD88 SRM 51-01.

Part: SEAT TRACK — CORRODED (BS 205 - 222) · airframe 58,980 hrs · 44,357 cycles

SEAT TRACK LBL 22 AT STA 205 AND STA 222 HAS CORROSION. REPAIRED BY REPLACEMENT SECTION AND SEAT TRACK SPLICE. REF SRM 53-05 FIG 4F.

Part: FLOOR SUPPORT — CORRODED (BS 160 LBL7) · airframe 58,980 hrs · 44,357 cycles

FLOOR SUPPORT AT STA 160 LBL 7 CORRODED. REPAIRED BY REPLACEMENT OF PART REF SRM 51-01.

Part: FLOOR SUPPORT — CORRODED (BS 160 RBL 7) · airframe 58,980 hrs · 44,357 cycles

FLOOR SUPPORT CORRODED AT BS 160 RBL 7. CORRECTED BY REPLACEMENT.

Part: OIL TANK — OVERSERVICED (APU) · airframe 58,542 hrs · 44,048 cycles

THE INBOUND CREW REPORTED AN "ACRID SMELL" AND "HAZE" IN THE CABIN. UPON ARRIVAL, MAINTENANCE FOUND THE APU WAS OVER-SERVICED AND THE OIL CAP WAS LEAKING. APU SERVICED TO CORRECT LEVEL AND OIL CAP REPLACED. A DUCT BURNOUT WAS SATISFACTORILY PERFORMED AND NO FURTHER SMELL WAS NOTED. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 1418) · airframe 56,079 hrs · 42,322 cycles

SKIN CRACKED A STA 1418, BELOW RAM AIR SCOOP ON LT SIDE, NR 63 AND RT SIDE NR 62. RIVETS LOOSE IN SAME AREAS. REPAIRS COMPLETED IAW ERA 489706-14.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,685 hrs · 42,089 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHT AT ROW 17 AND 22 INOPERATIVE. MX REPAIRED THE HARNESS CONNECTOR AT ROW 22. OPS OF LIGHTS NOW CHECKS GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 53,600 hrs · 40,659 cycles

SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT 25 DE INOP. FOUND CONNECTOR BROKEN ON PIGTAIL. RETERMINATED WIRE CKS GOOD.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 52,550 hrs · 39,966 cycles

C/W LT HORIZ STAB UPPER CAP SPLICE.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 52,467 hrs · 39,915 cycles

DURING INSPECTION PER EO 09-470871-12 FOUND RT VERTICAL SPAR CHORD CRACKED AT ONE FASTENER HOLE ABOVE ZFS=52. HOLE WAS OVER SIZED AND BUSHED PER ER/A 476785-14 ORIG.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 52,467 hrs · 39,915 cycles

DURING L/C INSP PER EA 09-470871-12 FOUND RT SPAR CHORD OF VERTICAL STABILIZER ABOVE ZFS=52 WAS CRACKED IN ONE FASTENER HOLE. A/C WAS GROUNDED AND PART REPAIRED PER ER/A 476845-14 ORIG. ALSO VERTICAL LEADING EDGE WAS FOUND WITH SKIN FASTENER HOLES ELONGATED JUST ABOVE FZS=52. ERA 476845-14 ORIG REPAIRS THIS DAMAGE.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 45,300 hrs · 35,138 cycles

ATL TOWER REPORTS SMOKE COMING FROM LEFT ENGINE ON LANDING. FOUND LEFT ENG THRUST REV ACT LEAKING. FOUND LEFT ENG I/B THRUST REVERSER ACTUATOR LEAKING. REPLACED SAME PER M/M.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 41,576 hrs · 32,510 cycles

ADVANCED POWER FOR TAKEOFF, INITIATED T/O ROLL. NO RESPONSE FROM NR 2 ENGINE, DISCONTINUED T/O. RAN BOTH ENGINES PER PFHB.

Part: HYDRAULIC LINE — WORN (A/C BAY) · airframe 41,194 hrs · 32,226 cycles

LEFT HYD QTY DROPPED PRESSURE FAILED TO ZERO. REPLACED ENG HYD PRESSURE LINE IN TAIL COMPARTMENT.

Part: CARTRIDGE — WILL NOT TEST (CARGO) · airframe 39,491 hrs · 31,003 cycles

GREEN LIGHT ON SQUIB 2 AFT CARGO FIRE WILL NOT TEST, LIGHT CHECKS GOOD. T/S PER M/M AND FOUND NR 2 BOTTLE AFT SQUIB BAD. REPLACED SQUIB PER M/M.

Part: LENS — DISLODGED (AFT LIFE RAFT) · airframe 38,105 hrs · 30,018 cycles

DURING LETTER CHECK M-2, FOUND EMERGENCY LIGHT AT AFT RAFT AREA INOP, REF NRC 76. FOUND EMERGENCY LIGHT AND STANDBY LIGHT ON AFT RAFT INSTALLED IN OPPOSITE POSITION. INSTALLED PER MM. OPS CHECK GOOD PER MM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 37,749 hrs · 29,760 cycles

ABORT TAKEOFF 80 KIAS. NR 1 ENGINE POSSIBLE COMP STALL. TAILPIPE FIRE MAX EGT NOTED 770. BOTH BOTTLES FIRED. FIRE DEPT APPLIED HALON TO TAILPIPE. REPLACED ENGINE AND BOTTLES.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 33,707 hrs · 26,921 cycles

FLOOR PANELS WERE FOUND DELAMINATED AND CRACKED. REPAIR PER ER/A 411194-14.

Part: OIL CAP — DAMAGED (APU) · airframe 32,292 hrs · 25,883 cycles

AFTER T/O SMOKE ALARM WENT OFF AT 6500 FT SMOKE WASN'T EVIDENT IN COCKPIT FUMES WERE EVIDENT IN CABIN - FOUND APU OIL CAP O-RING CUT - REPLACED SAME - CLEANED AREA - PERFORMED DUCT BURNOUT

Part: GENERATOR — SHORTED (APU) · airframe 31,629 hrs · 25,399 cycles

INFLIGHT ATL-EWR APU GENERATOR DROPPED OFFLINE AND WOULD NOT RESET. FLIGHT DIVERTED TO KCVG. FOUND APU GENERATOR FIELD SHORTED. REPLACED APU ASSY PER MM. LEAK CHECKS OK. OPS NORMAL.

Part: CONTROLLER — FAILED (NR 1) · airframe 29,990 hrs · 24,204 cycles

AFTER TAKEOFF HAD A FLOW LIGHT ON AUTO PRESS CONTROLLER RT PACK OUTPUT WAS LOW. REPLACED AUTO PRESSURE CONTROLLER NR 1 FOR BEING FAILED.

Part: ACM — FAILED (LEFT)

UNABLE TO MAINTAIN CABIN PRESSURE AT FL350 WITH ENG ANTI-ICE ON. OUTFLOW VALVE INDICATED FULL CLOSED AND FLOW LIGHT ILLUMINATED. INCREASED POWER ON BOTH ENGS AND LOWERED AIRCRAFT ALTITUDE BUT CABIN ALTITUDE CONTINUED TO CLIMB. WHEN CABIN ALT REACHED 10600 FT CREW DIVERTED TO AMA. FERRIED A/C TO DFW. FOUND LEFT ACM SEIZED. REPLACED ACM. PRESSURIZED AIRCRAFT, ALL OPERATION CHECKS GOOD. CHECKED RIGHT PACK, OPERATION GOOD.

Part: SOCKET — FAILED (CABIN)

AN ELECTRICAL BURNING ODOR REPORTED BY PASSENGER AND F/A S BETWEEN ROWS 20-27. FOUND SIDEWALL LIGHT BALLAST SOCKETS AT ROW 23DE BURNED. DEACTIVATED LIGHT FOR RETURN TO SERVICE, SOCKETS WERE REPLACED.

Part: BOLT — SHEARED (SERVICE DOOR)

AFT LEFT SERVICE DOOR INSIDE HANDLE INOP. FOUND INTERIOR HANDLE RETAINING BOLT SHEARED. INSTALLED NEW BOLT DOOR OPN NML REF IPC 52-40-11-03 ITEM 720.

Part: SKIN — CRACKED (FUSELAGE)

FOUND DURING F-1 LETTER CHECK, .25 INCH CRACK AT AFT HINGE CUTOUT OF LEFT AFT NOSE GEAR DOOR IN FUSELAGE SKIN. REPAIRED PER SRM 53-05 FIG 62A.

Part: DOOR SKIN — CRACKED (CARGO COMP)

FOUND DURING F-1 LETTER CHECK, C-3 DOOR HANDLE CUTOUT SKIN CRACKED .75 INCH FWD SIDE. REPAIRED PER SRM 52-05 FIG 30.

Part: RIB — CRACKED (FUSELAGE)

FOUND ON F1 LTR CK, AFT CROSS OVER RIB AT KEEL BEAM CRACKED. REPAIRED PER SRM 53-05 FIG 101.

Part: ANGLE — CRACKED (LT PYLON)

FOUND DURING F-1 LETTER CHECK, NBR 1 ENG UPPER PYLON ATTACH ANGLE CRACKED 1.5 INCHES APPROX 10 INCHES FROM AFT END REPAIRED PER SRM 54-04A FIG 4.