N941DL

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 73,740 hrs · 55,154 cycles

EMERGENCY LIGHT, ROW 10 INOPERATIVE. REPLACED THE WIRE HARNESS IAW AMM 33-53. OPS CHECKED GOOD.

Part: CABLE — OBSTRUCTED (MLG HANDLE) · airframe 72,863 hrs · 54,427 cycles

ON APPROACH, THE GEAR HANDLE WOULD NOT MOVE MORE THAN ONE INCH OUT OF THE UP POSITION. PERFORMED QRH ALTERNATE GEAR EXTEND. GEAR PINS INSTALLED AFTER LANDING. FOUND INSULATION BLANKET TAPE JAMMED IN GEAR HANDLE CABLE & PULLEY BELOW COCKPIT FLOOR. REMOVED TAPE AND PERFORMED GEAR HANDLE OPERATION IAW AMM 32-31-01. REMOVED GEAR PINS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,420 hrs · 54,089 cycles

DURING A SERVICE CHECK, FOUND CEILING EMERGENCY LIGHTS AT SEATS 32 AND 34 EXTREMELY DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK B5-107 AND BATTERY IAW AMM 33-53. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 72,189 hrs · 53,907 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 24 - 27. TROUBLESHOT IAW WDM 33-51. FOUND CONNECTOR DISCONNECTED AFT OF SEAT ROW 27. LIGHTS OPS CHECKED GOOD. OK FOR SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,853 hrs · 52,989 cycles

CPCP INSPECTION- AFT CARGO BILGE, FLOOR SUPPORT LOWER-J ANGLE CORRODED FROM L29L TO L30, STA 1287. REPLACED J CHANNEL IAW SRM 53-03, FIG 2A.

Part: UNKNOWN — MALFUNCTIONED (TAILCONE) · airframe 70,775 hrs · 52,926 cycles

TAILCONE WOULD NOT RELEASE WITH INTERIOR HANDLE OPERATION IAW AMDS 5350-01077-0101, STEP 11A. CORRECTED ON NON-ROUTINE. CHECKS PASSED IAW AMDS 5350-01077-0101. PULL CHECK WITH-IN LIMITS AT 33LBS.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · corrosion level 2 · airframe 70,775 hrs · 52,926 cycles

ON FOLLOW UP OF NR 221 FOUND SUPPORT BRACKET CRACKED, CORRODED STA 1287 ON FRAME LONGERON 28 LT. AFT CARGO COMPARTMENT. R & R FITTING REF DWG 9957739. FOUND TO BE LEVEL 2 CORROSION.

Part: ATTACH FITTING — CRACKED (LT SPOILER) · airframe 70,775 hrs · 52,926 cycles

LT WING, GROUND SPOILER ACTUATOR SUPPORT FITTING CRACKED AT INBD FORWARD END. REPLACED SPOILER ATTACH FITTING IAW DWG 5936832 AND SRM 51-30-00.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,775 hrs · 52,926 cycles

FOUND ON F/U TO NR 219, AFT CARGO T-ANGLE CORRODED AT STA 1192. 8" INBD SILL CUTOUT. REPLACED SUPPORT IAW DWG 5936660.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,775 hrs · 52,926 cycles

FUSELAGE, FORWARD PASSENGER AIR STAIR DOOR CORRODED ON INTERIOR AT FORWARD AND AFT LOWER CORNERS. R & R DOOR FRAME IAW SRM 51-30-00.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,201 hrs · 53,256 cycles

CPCP INSPECTION, AFT CARGO BILGE THRESHOLD SILL SPACER CORRODED FROM STA 1155 TO 1212. REMOVED AND REPLACED SPACER REF ERA 499523-14MA REV ORIG. REMOVED CORROSION REF SRM 53-05 FIG 1.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 70,594 hrs · 52,791 cycles

R1 SLIDE PRESSURE LOW. REPLACED THE R1 SLIDE IAW AMDS W/C 2561-4964.

Part: GIRT BAR — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 68,728 hrs · 51,485 cycles

THE CREW DISCOVERED THAT THE GIRT BAR FOR THE EMERGENCY ESCAPE SLIDE AT DOOR 1L WOULD NOT REMAIN IN THE ARMED POSITION. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE GIRT BAR WAS REINSTALLED BY MAINTENANCE AND THE FOLLOW-UP FUNCTIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (SEAT 3D) · airframe 68,591 hrs · 51,389 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 3D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK.

Part: FAIRING — DAMAGED · airframe 67,014 hrs · 50,272 cycles

FWD TOP END OF UPPER RT BANANA FAIRING DAMAGED. REMOVED PREVIOUSLY INSTALLED DOUBLER, REMOVED DAMAGE MATERIAL FROM FAIRING REF ERA 464895-14MA. ACCOMPLISHED HFEC NDT SPM 06-10-01-001. DAMAGED CONTAINED. TRIMED AND PILOT DRILLED DOUBLER FROM PN 55-0018-003. FABRICATED FILLER FROM .032, 2024T3. FILLER AND REPAIR DOUBLER IN PLACE IAW ERA 464894-14MA. INSTALLED FASTENERS IN REPAIR IAW ERA 464895-14MA. ALODINED REPAIR DOUBLER. INSTALLED FAIRING ON ACFT. THIS IS A PERMANENT REPAIR INSTALLED DECAL. LP1854028.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,625 hrs · 49,267 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 65,503 hrs · 49,190 cycles

MAINTENANCE DISCOVERED THAT SEVERAL OF THE TAILCONE RELEASE SYSTEM GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 65,113 hrs · 48,900 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT 1C. MAINTENANCE FOUND A CONNECTOR LOOSE AND SECURED, LIGHTS RETURNED TO AN OPERATIVE STATE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,846 hrs · 48,686 cycles

FUSELAGE SKIN DAMAGED AT THE FWD SIDE OF THE DOOR CUT OUT. REPAIRED IAW ER/A 524694-14, REV ORIG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,595 hrs · 48,523 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS AT SEATS 18D-21D IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,330 hrs · 48,353 cycles

CREW REPORTED THE EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND OPS GOOD.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 63,796 hrs · 47,981 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT SOCKET ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,625 hrs · 47,864 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS CABIN AND ROWS 11 & 12 HAD FAILED. MX REPLACED THE BATTERIES AND CHARGER. OPS CHECKED GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 62,574 hrs · 47,104 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 38 AND AFT IN THE CABIN WERE INOPERATIVE. MX FOUND A LOOSE WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN AND THE SYS RETURNED TO NORMAL OPERATION.

Part: HEATER BLANKET — PUNCTURED (RT WING) · airframe 62,006 hrs · 46,708 cycles

PUNCTURE ON SECONDARY ACCESS COVER CUT OUTS NR 1409C AND 1410C AT RT WING HEATER BLANKET. HEATER BLANKET (RT) WAS REPLACED IAW AMM 30-80-02, PAGE BLOCK 401, PARA 401.

Part: HEATER BLANKET — PUNCTURED (LT WING) · airframe 62,006 hrs · 46,708 cycles

PUNCTURE ON SECONDARY ACCESS COVER CUT OUTS NR 1303C AND 1307C AT LT WING HEATER BLANKET. (RT WING/LT WING) REF NRC (T0 270123). HEATER BLANKET (LT) WAS REPLACED IAW AMM 30-80-02 PAGE BLOCK 401. RII COMPLETED BY INSPECTOR JAC 200802799 AM DELTA ID 852050.

Part: SKIN — CORRODED (BS 769) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER IN FUSELAGE SKIN STA Y=769 BETWEEN LONG S27 RH AND 28 RH. DOUBLER WAS REPLACED IAW SRM 53-04, FIG 57 AND 51-10-3 PAR 14, 21, 26, 51-30-5. RII COMPLETED.

Part: BULKHEAD — DAMAGED (BS 1338) · airframe 62,006 hrs · 46,708 cycles

TOOL MARKS ON AFT PRESSURE BULKHEAD TEE CAP STA2 Y=1338 BTW PROJECTION LONGS 24RH AND 25RH AT AFT ACCESSORY COMPARTMENT. 3 (A/A) 4 (REF. NRC 532, ZONE 532) TEE CAP STA= 1338 BETWEEN PROJECTION LONGS 22RT AND 22LT WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 5910130, REV EJ.

Part: SKIN — CORRODED (BS 775-826) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FAIRING STA Y= 775 - Y= 826 BETWEEN LONGS 27 RH TO 30. CORROSION OUT OF LIMITS WILL BE REPAIRED IAW SRM 53-04D, PAR 57 WITH NRC 822, ZONE 50. RII COMPLETED.

Part: FLOOR SUPPORT — CORRODED (BS 1117-1155) · airframe 62,006 hrs · 46,708 cycles

CORROSION AND ELONGATED HOLES ON FLOOR SUPPORT OVERLONG 28RT BETWEEN BS 1117-1155 AT AFT CARGO COMPARTMENT. (C3)(MRB 53-139-05) REF. NRC (T0 270632). FLOOR SUPPORT WAS REPLACED IAW DWN 5936660, REV B2 AND SRM 51-30-1 AND 51-30-2.

Part: SKIN — CORRODED (BS 807) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=807 BETWEEN LONGS 30 AND 29 RT. FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=807 WAS REPAIRED IAW SRM 53-04, FIG 57. RII COMPLETED.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,007 hrs · 46,709 cycles

LIGHTNING STRIKE ON RT WINDOW BELT UPPER AFT CORNER BETWEEN BS 712 AND 731. RT WINDOW BELT WAS REPAIRED IAW AMR 09531174, REV 2 AND ER/A 509663-14, REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 1003-1222) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON LT CARGO TRACK BETWEEN STA Y=1003 AND Y= 1222 AT AFT CARGO COMPARTMENT. CARGO TRACK WAS REPLACED IAW SRM 51-30-2 AND 51-30-1 AND 51-10-3, PARA 14 AND 21 (UT) WAS ACCOMPLISHED ORIGINAL THICKNESS IS .060 THEREFORE AREAS OUT LIMITS IAW SRM 53-01, FIG 1.

Part: LONGERON — CORRODED (BS 1280-1309) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON LONGERON 25L BS 1280-1309. LONGERON SECTION REPLACED IAW SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1271-1300) · airframe 62,006 hrs · 46,708 cycles

CORROISON FOUND ON LONGERON 24L BETWEEN BS 1271-1300, AFT CARGO BAY. LONGERON SECTION BETWEEN BS 1265-1331 WAS REPLACED IAW SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1287-1338) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON LONG 29R BETWEEN BS 1287-1338. LONGERON WAS REPLACED IAW DWG 596667 AND SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CORRODED (BS 1287-1307) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON LONGERON 22L BS 1287 AND 1307 AT AFT CARGO BAY. LONGERON REPAIRED IAW SRM 53-02, FIG. 18.

Part: ANGLE — CORRODED (PRESSURE BLKHD) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON ANGLE BS 1338 BETWEEN LONGERON 28L/R AT AFT CARGO BAY PRESSURE BULKHEAD. ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 9915561, REV CG 51-30-5 (UT) WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.100" REMAINING THICKNESS IS 0-048" AND FOUND OUT LIMITS IAW SRM 53-01, FIG 1.

Part: SKIN — WORN (LT WING) · airframe 62,006 hrs · 46,708 cycles

WEAR ON LT WING LOWER SKIN LOWER SKIN DUE TO INTERFERENCE WITH FLAP FWD HINGE FAIRING STA XW=99 AND XW=111 APROX (LW)(REF.NRC: T0 270112). DAMAGE WAS ATTENDED IAW ER/A 509661-14, REV ORIG AND SRM 51-30-5 AND 51-10-3, FAIRINGS WAS INSTALLED CORRECTLY AND INTERFERENCE WAS CORRECTED. RII COMPLETED.

Part: CUSP WEB — CORRODED (BS 864-885) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER RT CUSP WEB, STAY=864 TO 885, BETWEEN X=-54 TO -60 AT CABIN FLOOR STRUCTURE. REPLACED DOUBLERS IAW SRM 53-05D, 51-30-2.

Part: LONGERON — CRACKED (BS 886-905 L5R) · airframe 62,006 hrs · 46,708 cycles

CRACK ON LONGERON 5R BS 886 - 905. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1429 L12L) · airframe 62,006 hrs · 46,708 cycles

CRACKED LONGERON 12 LT AT BS 1429 AT AFT ACCESSORY COMPARTMENT. LONGERON REPAIRED IAW SRM 53-02, FIG-18.

Part: LONGERON — CRACKED (BS 965 L2R) · airframe 62,006 hrs · 46,708 cycles

CRACKED LONGERON 2R BS 965. LONGERON REPAIR IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 927 L3R) · airframe 62,006 hrs · 46,708 cycles

CRACKED LONGERON 3R BS 927 LONGERON REPAIR IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 503-511) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 503 TO 511 AND BETWEEN X=-54 TO X=-60 (FCS). REPAIR DOUBLER WAS REPLACED IAW ER/A 398191-14NA.

Part: LONGERON — CRACKED (BS 465) · airframe 62,006 hrs · 46,708 cycles

CRACK ON LONGERON NR 4LT STA Y=465 AT PAX CABIN. LONGERON WAS REPAIR IAW SRM 53-02 FIG 18.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 62,006 hrs · 46,708 cycles

WEAR AND CORROSION AROUND INNER DOUBLER OF AFT LAVATORY SERVICE PANEL FROM BS 1307-1322, BETWEEN LONG 19-22L. WEAR WAS BLENDED OUT AND CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. MEASURED AND FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED REPAIR DOUBLER AND FILLERS IAW ER/A 397822-14 MA, REV ORIG.

Part: PAINT — PEELING (RUDDER) · airframe 62,006 hrs · 46,708 cycles

FLAKES ON RUDDER SKIN PAINT COAT ON RT SIDE BETWEEN STA ZRS 50 TO ZRS 72 AND LT SIDE BETWEEN STA ZRS 91 AND LT SIDE BETWEEN, STA ZRS 105 (VHS) REF NRC (T0 271294). RUDDER REPAIRED AREAS WERE PAINTED IAW EA 09-461041-03, REV C AND DLA DWN 11-08941 REV E. ASSOCIATED ER/A 09-461041 ADDED FOR AC 0941.

Part: LONGERON — CRACKED (BS 1309-1322) · airframe 62,006 hrs · 46,708 cycles

CRACKED LONGERON 8R BS 1309 AND 1322 AT PAX CABIN.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 62,006 hrs · 46,708 cycles

CORROSION ON AFT CARGO BAY LOWER DOOR FRAME BEAM. SPACER REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 123.

Part: LONGERON — CRACKED (BS 845 L4R) · airframe 62,006 hrs · 46,708 cycles

CRACK ON LONGERON 4R BS 845 AT PAX CABIN. LONGERON 4 RT REPAIR IAW SRM 53-02, FIG 18.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,003 hrs · 46,707 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING ABOVE ROWS 22-26 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,019 hrs · 45,981 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE FORWARD OVERWING EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 60,937 hrs · 45,916 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 30D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AND REPLACED THE LIGHT ASSEMBLY. THE SYSTEM HAS RETURNED TO NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 29DE) · airframe 60,175 hrs · 45,347 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 29DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SEAT 29DE AND RE-TERMINATED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,692 hrs · 45,016 cycles

WHILE IN MSP FOR C CHECK VISIT A DENT WAS FOUND JUST AFT OF STA 427 BETWEEN L28R AND L29R. A HFEC OF THE DENTED AREA REVEALED A CRACK. THE CRACK WAS TRIMMED OUT AND A REPAIR WILL BE INSTALLED FOLLOWING MD80 SRM 53-04 FIG 38A. THE SKIN IS MADE FROM 0.05" THICK 2024-T3 CLAD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,451 hrs · 44,864 cycles

MAIN CABIN FLOOR TRACK CORRODED BETWEEN STA 168-200 AND RBL 7. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED FLOOR TRACK FABRICATED REPLACEMENT AND INSTALLED STA 168-200 RBL 7 IAW DC9/MD80 SRM 51-30-1 DURING PAX MOD AT ST AEROSPACE SAN ANTONIO.

Part: CONNECTOR — LOOSE (CABIN) · airframe 59,304 hrs · 44,769 cycles

DURING A LAYOVER CHECK MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT 4DC AND 15ED INOPERATIVE. MAINTENANCE RESECURED THE CONNECTORS AT EACH LOCATION. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,534 hrs · 44,204 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. MAINTENANCE REPLACED LIGHT AND HARNESS AT SEAT. OPERATION OF LIGHT NOW CHECKS OK.

Part: BRAKE — FIRE (RT MLG) · airframe 58,478 hrs · 44,160 cycles

UPON LANDING, THE TOWER REPORTED SEEING A FIRE ON THE RIGHT SIDE OF THE AIRCRAFT. THE AIRCRAFT STOPPED ON RUNWAY 26 R AT TAXIWAY BRAVO WHERE AN EMERGENCY EVACUATION TOOK PLACE. IT IS BELIEVED TO HAVE BEEN A BRAKE FIRE.

Part: SLIDE — MISINSTALLED (TAILCONE) · airframe 58,478 hrs · 44,160 cycles

AIRCRAFT EXPERIENCED A FIRE EVENT IN ATL, AND PASSENGER EVACUATED VIA THE AIRCRAFT DOORS AND TAIL CONE SLIDES. THE L1 AND L2 DOOR SLIDES OPERATED AS DESIGNED, AND THE TAIL CONE DEPLOYED AS DESIGNED; HOWEVER, THE TAIL CONE SLIDE DID NOT DEPLOY. MANUAL TAIL CONE SLIDE DEPLOYMENT WAS ATTEMPTED, BUT WAS ALSO UNSUCCESSFUL. THE EVENT INVESTIGATION DETERMINED THE SLIDE WAS NOT INSTALLED IN COMPLIANCE WITH MAINTENANCE INSTRUCTIONS, AND THE MIS-CONFIGURATION PREVENTED SLIDE OPERATION.

Part: PIN — MISSING (TAIL CONE) · airframe 57,083 hrs · 43,226 cycles

MEDICAL PERSONNEL ATTEMPTED TO ENTER THROUGH THE AFT AIRSTRAIRS. FLIGHT ATTENDANT DID NOT PROPERLY DISARM THE DOOR AND WHEN EMT TRIED TO OPEN DOOR, THE TAIL CONE SEPARATED BUT THE EMERGENCY EVACUATION SLIDE DID NOT DEPLOY. MAINTENANCE FOUND TAIL CONE RELEASE MECHANISM PIN MISSING. RELEASE MECHANISM WAS REPLACED PER AMM 53-53-02-201. TAIL CONE RELEASE CAM WAS REMOVED, INSPECTED, AND RE-INSTALLED PER AMM 53-53-02. ORIGINAL SLIDE WAS RE-INSTALLED PER OPN 7915 AMM 25-62-01-201 RII COMPLETED BY QC1984. (2010-D1318)

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 55,422 hrs · 42,146 cycles

FOUND EMERGENCY LIGHT INOP AT SEAT 2C AND 27D. REPLACED LENS AND BULBS AT SEAT 2C AND REPAIRED WIRE AT SEAT 27D. ALL CKS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,413 hrs · 42,142 cycles

FOUND EMERG LIGHT INOP AT SEAT 2C AND 27D. REPLACED LENS AND BULBS AT 2C AND REPAIRED WIRES AT 27D. ALL CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,272 hrs · 42,058 cycles

APROX 5 FT FWD OF MID CARGO DOOR DIRECTLY ON BOTTOM OF A/C FOUND CORROSION BULGE AND SKIN CRACKED AREAS MARKED. TRANSFERED TO NR 001. ACCOMPLISHED PERM REPAIR PROCEDURE IAW FINAL ERA 479960-14, REV A.

Part: LIGHT — INOPERATIVE (SEAT 13D) · airframe 55,254 hrs · 42,046 cycles

ESCAPE PATH LIGHT AT 13D INOPERATIVE. REPLACED LIGHT ASSY CHECKS GOOD MCO AND PLAC REMOVED.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 52,000 hrs · 39,871 cycles

VERTICAL STABILIZER FRONT SPAR RT CHORD CRACKED THROUGH THREE FASTENER HOLES AT ZFS=52. DAMAGE CUT OUT OF FLANGE AND REINFORCED WITH A REPAIR ANGLE.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,652 hrs · 36,994 cycles

FUSELAGE SKIN REPAIR AT STA 250, LONGERON 30 - DENT WITH CREASE. PERMANENT REPAIR INSTALLED PER AMX DRAWING AMR0953571 AND ERA 383116-14.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,652 hrs · 36,994 cycles

SUPERFICIAL CORROSION O AFT PASS DOOR JAMB - CORROSION ON LOWER HORIZ SECTION OF AFT PAX DOOR JAMB FWD SURFACE NEAR STA 1338. CORROSION REMOVED, PERMANENT REPAIR INSTALLED PER SRM 53-05D FIG 34.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,652 hrs · 36,994 cycles

EXFOLIATION CORROSION ON DOOR JAMB AFT CARGO COMPARTMENT - LOWER SECTION. CORROSION REMOVED AND PERMANENT REPAIR INSTALLED PER SRM 53-05D FIG 63.

Part: TAB — CORRODED (ELEVATOR) · airframe 47,652 hrs · 36,994 cycles

DELAMINATION ON LT HORIZ STAB ELEVATOR CONTROL TAB AT STA XET=80.750TO XET=66.625. PERMANENT REPAIR INSTALLED PER AMX REPAIR DRAWING AMR0955070 AND ERA 458461-14.

Part: SKIN — DENTED (FS 260 L29-30L) · airframe 47,652 hrs · 36,994 cycles

DURING THE CURRENT HMV, ADDITIONAL DAMAGE WAS FOUND IN THE AREA OF REPAIR DOUBLER INSTALLED PER ERA 383116-14. THE EXISTING REPAIR WAS REMOVED, AND A BOEING APPROVED REPAIR, WHICH INCREASED THE SIZE OF THE EXISTING REPAIR, INSTALLED. LOCATED AT FS 237 TO 256, L-29L TO L-30.

Part: CONTROL PANEL — FAILED (CABIN PRESSURE) · airframe 40,170 hrs · 31,805 cycles

ON TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. LOUD NOISE COMING FROM F/O'S SLIDING WINDOW. EVEN IN MANUAL PRESSURE MODE A/C WOULD NOT PRESSURIZE WELL. PERFORMED PAPER TEST ON WINDOW. NO RESISTANCE ON THE UPPER AFT PART OF WINDOW. BIT BOTH PRESSURE CONTROLLERS. BOTH FAULT AC MOTOR WITH NO ASSOCIATED ALERTS IN FLIGHT DECK RIGGED F/O'S WINDOW. REPLACED OVERHEAD PRESS CONTROL PANEL. PRESSURIZED A/C F/O'S WINDOW LEAK CHECKS GOOD. PRESS CONTROLLER RESET. PRESSURIZATION NOW CHECKS GOOD. A/C OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,686 hrs · 30,040 cycles

THE FUSELAGE SKIN WAS FOUND WITH A .75 INCH CRACK AT FS 1418, JUST OUTBOARD OF THE VERTICAL STAB TO FUSELAGE ATTACH ANGLE AND STRINGER 1L. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH A TITANIUM REPAIR DOUBLER PER ER/A 384509-14, REV A.

Part: SKIN — CORRODED (FS 237, S-30) · airframe 35,931 hrs · 28,741 cycles

FUSELAGE / SKIN / FS 237 / STRG. 29L-30 / TCAS ANTENNA : CORROSION AND CRACK REPAIR THE FUSELAGE SKIN WAS FOUND WITH CORROSION AND SMALL CRACKS AT THE LOWER TCAS ANTENNA INSTALLATION AT FS 237 BETWEEN STRINGERS 29L & 30. THE ENTIRE ANTENNA AREA OF THE SKIN WAS CUTOUT TO REMOVE ALL DAMAGE. THE CUTOUT MEASURED 20" X 18". THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 383116-14.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,307 hrs · 28,272 cycles

EMERGENCY TRACK LIGHTING DAMAGED AT 34D. REPAIRED SAME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,697 hrs · 27,113 cycles

FOUND ON LAYOVER OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.

Part: RUDDER PEDAL — OBSTRUCTED (COCKPIT) · airframe 33,239 hrs · 26,802 cycles

AFTER PUSHBACK FLIGHT CREW INITIALLY COULD NOT DEPRESS THE LEFT RUDDER PEDAL DURING FLIGHT CONTROL CHECK. RETRACTED FLAPS/SLATS, DISAGREEMENT LIGHT ILLUMINATED AND LEFT RUDDER PEDAL WAS OPERATIONAL, RTB. VISUALLY INSPECTED RUDDER SYSTEM CONTROLS ON AIRCRAFT FORFREEDOM OF MOVEMENT OR BINDING RUDDER TRAVEL NORMAL. FOUND CAPPED WIRE BUNDLE AT F/O LT RUDDER PEDAL TUNNEL HANGING DOWN WITH BROKEN TY-WRAP.RESECURED BUNDLE. RUDDER CHECK NORMAL.

Part: FIRE LOOP — FALSE INDICATION (NR 2 ENGINE) · airframe 31,540 hrs · 25,518 cycles

RT ENGINE FIRE INDICATION INFLT. CREW FOLLOWED POM PROCEDURES, LIGHT STILL ON. CREW BLEW BOTH BOTTLES, LIGHT STILL ON. CREW SHUT ENGINE DOWN. FOUND BAD CONNECTION ON UPPER BURN THRU BARRIER FOR LOOP B. REPLACED UPPER BURN THROUGH BARRIER LOOPS AND LOWER ENGINE FIRE LOOPS. REPLACED FIRE BOTTLES.

Part: STRIKER PLATE — OUT OF ADJUST (CARGO DOOR)

AFT CARGO DOOR ILLUMINATED IN FLIGHT. ADJ AFT CARGO DOOR STRIKER PLATE, OPS CK NORMAL.

Part: PROX SENSOR — MALFUNCTIONED (NLG)

ON APPROACH WITH LANDING GEAR SELECTED DOWN, CREW DID NOT GET A GREEN DOWN AND LOCKED LIGHT ON THE NOSE GEAR. ALSO, THE RED LIGHT WAS OUT. WHILE EXECUTING A GO-AROUND, THE GREEN NOSEGEAR DOWN AND LOCKED LIGHT ILLUMINATED. REPLACED NOSE GEAR LOCKED PROX SENSOR AND NOSE GEAR DOWN SWITCH. JACKED AIRCRAFT AND PERFORMED GEAR SWING, NO FAULTS NOTED DURING CK.

Part: COALESCER BAG — CONTAMINATED (CABIN)

DURING INITIAL CLIMB, DIRTY SOCK SMELL IN CABIN. SMELL CLEARED AFTER APPROX 10 MINS. REPLACED WATER SOCKS.

Part: SKIN — DENTED (BS 313-332)

GROUND DAMAGE HAS BEEN TRIMMED OUT FROM JUST FORWARD OF FS 313 TO JUST AFT OF FS 332 AND FROM JUST ABOVE S-23 TO JUST BELOW S-25. CUT OUT SIZE IS APPROX 15.5 INCHES HIGH AND 20 INCHES LONG. ACCOMPLISHED REPAIRS PER DL ERA 273564-14.