N917DE

Part: LATCH — WORN (TAILCONE) · airframe 59,968 hrs · 43,145 cycles

UPPER LEFT TAIL CONE ATTACH LATCH LOCK IS WORN. R & R AND ADJUSTED LATCH IAW AMM 53-53-00.

Part: SKIN — WORN (VERTICAL STAB) · airframe 58,108 hrs · 41,843 cycles

VERTICAL STABILIZER RT SIDE EXTERIOR HAS 7 X .3750" AREA OF DEEP WEAR APPROXIMATELY .10" ABOVE & FWD OF HORIZONTAL STABILIZER CTR AFT SPAR. NR FOR ADDITIONAL INFORMATION 001-0341:5300-2551/010 00141. REPAIRED IAW PRI 539282-14, REV "0" AND ER/A 539282-14, REV ORIGINAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,108 hrs · 41,843 cycles

ACFT ON RT FUSELAGE, SIGNIFICANT DENT 8.5" FORWARD AND 11.8" ABOVE THE ALTERNATE STATIC PORT CENTER. ALSO, THERE ARE 8 OTHER SMALL DENTS WITHIN THE CONTROLLED AREA 18", WHICH EXCEEDS THE MAXIMUM OF 2 DENTS, 1 SIDE IN THIS AREA. NR FOR ADDITIONAL INFORMATION 044-0001: 3411-2108/001 00197 COMPLIED WITH PRI 538316-14, REV "0" AND ER/A 538316-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1436) · airframe 58,108 hrs · 41,843 cycles

SKIN HAS A .5" LONG CRACK, LATERAL AXIS, AT BS 1436.5. OTBD END OF CRACK IS 1.25" INBD OF L4R RIVET ROW. INSTALLED REPAIR IAW SRM 53-01, FIG 4, SHT 4.

Part: FRAME — CRACKED (BS 1510) · airframe 58,108 hrs · 41,843 cycles

TAIL INTERIOR, AFT CANTED FRAME AT BS 1510 HAS .5 INCH LONG CRACK AT CONE ALIGN PIN, 11:30 O`CLOCK POSITION. REPAIRED IAW PRI 538315-14, REV "0" AND ER/A 538315-14, REV ORIGINAL.

Part: SHEAR TIE — CORRODED (BS 1149) · corrosion level 2 · airframe 58,108 hrs · 41,843 cycles

AFT CARGO HAD SIGNS OF CORROSION ON SHEAR TIE BS 1149 BETWEEN LONGERONS 29 AND 30R. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9936074.

Part: ANGLE — CRACKED (L1 DOOR FRAME) · airframe 58,108 hrs · 41,843 cycles

L1 MAIN CABIN DOOR, NR 1 BEAM AFT END ANGLE CRACKED. REPAIRED IAW SRM 52-05D, FIG 97.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 58,108 hrs · 41,843 cycles

AFT CARGO BARRIER DOOR REPAIR DOUBLER ON INBD SKIN LOOSE. REPAIRED IAW ERA 094625-14MA, REV 0.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,955 hrs · 41,734 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT DOOR 2L AND SEAT 33 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,482 hrs · 41,423 cycles

DURING LINE CHECK FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK. OPS CHECKED NORNMAL IAW AMM 33-53-00.

Part: SKIN — CRACKED (BS 1380) · airframe 57,220 hrs · 41,247 cycles

CRACKS WERE FOUND EMANATING FROM A FASTENER HOLE AT BS 1380. THE CRACK IS LOCATED AT FIRST FASTENER COMMON TO FS 1380 SHEAR TIE JUST ABOVE THE SKIN SPLICE AT L-14L. STARTING AT OR PRIOR TO 5JUN15, AND REPETITIVELY EVERY 30 DAYS THEREAFTER, ACCOMPLISH VISUAL INSPECTION OF THE REPAIRED AREA. ASSOCIATED ER/A 00-525667, ADDED FOR AC 9017. LP 1927009.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 57,110 hrs · 41,180 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT 10D WERE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND THE OPS TEST WAS GOOD. LP 6963534.

Part: SKIN — CRACKED (BS 1458) · airframe 54,687 hrs · 39,404 cycles

FUSELAGE SKIN CRACKED ABOVE PYLON AT FASTENER BS 1458.02. REPAIRED IAW SRM 53-01, FIG 4, SHEET 4 AND ERA 525667-14, REV ORIGINAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,648 hrs · 39,373 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT LIGHTS IN THE FIRST CLASS SECTION WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,866 hrs · 38,148 cycles

DURING LINE INSPECTION, THE INTERIOR CEILING MOUNTED EMERGENCY ESCAPE SYSTEM (EES) LIGHTS AT THE 1L & 1R DOORS AS WELL AS THE COCKPIT OVERHEAD EES LIGHT WERE NOTED TO BE INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW AMM 33-53 AND OPERATION CHECKED NORMALLY.

Part: PIN — WORN (TAIL CONE) · airframe 51,229 hrs · 36,978 cycles

DURING TAIL CONE DROP, MX FOUND INTERNAL TEE PIN WORN. REPLACED T-PIN IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,078 hrs · 36,864 cycles

DURING SERVICE CHECK, MX FOUND CEILING EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. MX TROUBLESHOT AND R & R BATTERIES IN BATTERY PACK B5-28. OPS CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,960 hrs · 36,770 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHTS AT SEAT 31, 34-38, PATHWAY LIGHT FIXTURES, AFT LT SERVICE DOOR EXIT AND AFT CABIN EXIT SIGN INOPERATIVE. FOUND POWER SUPPLY BAD AT STA 1233R. R & R POWER SUPPLY AND BATTERIES. OPS CHECK GOOD.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 50,806 hrs · 36,650 cycles

L/E OF LEFT HORIZONTAL STABILIZER HAS DAMAGE 6FT OTBD OF VERTICAL STABILIZER. DENT IS 9'6" FROM VERTICAL STABILIZER. DENT MEASURES 2" WIDE AND 3" LONG. MAXIMUM DEPTH .150. PERFORMED HFED INSPECTION IAW NDT SPM. NO FAULTS FOUND. REPAIRED DAMAGE IAW SRM 53-03.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 50,696 hrs · 36,560 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 12DE INOPERATIVE. MAINTENANCE REPAIRED WIRES AT SEAT 12DE FOR THE EMERGENCY LIGHTS PER SWPM. OPERATION CHECKS GOOD.

Part: CABLE — LOOSE (L2 DOOR SLIDE) · airframe 49,802 hrs · 35,944 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND L2 DOOR SLIDE CABLE LOOSE. SECURED CABLE. AIRCRAFT OKAY FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,672 hrs · 35,859 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD ZONE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IN B5-23 OPERATION CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,505 hrs · 35,761 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND OVERWING AFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATION CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,376 hrs · 35,682 cycles

DURING CHECK, MAINTENANCE FOUND OVERWING EMERGENCY EXIT SIGN, 2ND ROW, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES AT 2ND ROW OVERWING EMERGENCY EXIT. OPERATION CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

HIDDEN DAMAGE: CORROSION IN OUTER FUSELAGE SKIN BETWEEN STA Y=1112-1114 AND LONG 27L-28L (RUB STRIP AREA)(IN REF TO229014)(FS). CORROSION WAS OUT OF LIMITS PER 51-10-3 PAR G 26. REPAIR DOUBLER WAS INSTALLED PER DC9/MD88 SRM 53-04D FIG 53 AND IS PERMANENT REPAIR PER IAW PS 900-S-1 N04.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

CORROSION ON SKIN FUSELAGE UNDER FILLET FAIRING RUBSTRIPS FROM STA Y=1095-Y1104 LONG 30-28 RT IN REF NRC T0229337 T0229335. CORROSION WAS OUT OF LIMITS SO REPAIR DC9/MD80 SRM 53-04D FIG 53 WAS APPLIED AND IS IDENTIFED AS PERMANENT IAW PS900-5-1-N04.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

CORROSION ON CUSP ANGLE STA Y=200 X=-54 AT W1. REPLACED CUSP ANGLE STA Y=167-200 X=-54 IAW MD88 SRM 53-05 FIG 55.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 48,787 hrs · 35,280 cycles

DENT ON LT ELEVATOR GEARED TAB UPPER SKIN. LT ELEVATOR GEAR TAB WAS REPAIRED IAW MD88 SRM 55-04 PARA 3A.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

DURING HMV CORROSION WAS FOUND ON MID CARGO COMPARTMENT LWR DOORJAMB BEAM BETWEEN STA Y=636-693 C2. REF MD88 SRM 53-05 FIG 123 FOR REPAIR.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 48,787 hrs · 35,280 cycles

DENTS ON RT ELEVATOR ANTI-FLOAT TAB UPPER/LOWER SKIN. ELEVATOR ANTI-FLOAT TAB WAS REPAIRED IAW MD88 SRM 55-04 PARA3A AND 2A.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

PUNCTURE ON RT CUSP WEB IN STA Y=416 AND Y=422 BTW X=-53 AT FLOOR STRUCTURE PAX CABIN. CUSP WEB WAS REPLACED IAW MD88 SRM 53-20-02D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,746 hrs · 10,372 cycles

CORROSION ON FUSELAGE SKIN UNDER FILLET PANELS FAIRING RUBSTRIPS FROM STA Y=1095-1079 BTW LONG 28RT-30 AND FROM STA Y=1136-1112 BTW LONG 25RT-28RT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,746 hrs · 10,372 cycles

CORROSION ON FUSELAGE SKIN UNDER FILLET PANELS FAIRING RUBSTRIPS FROM STA Y=1095-1110 BTW LONG 27RT-29RT.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

CORROSION ON INNER PRODUCTION DOUBLER BTW STA Y=1022 AND 1041 BTW LONGERONS 28L AND 29L, ALSON FRAME IN STA Y=1041 BTW 28L AND 28R AT AFT CARGO COMPARTMENT. CORROSION ON FUSELAGE SKIN WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

HIDDEN DAMAGE; CORROSION ON FUSELAGE SKIN PREVIOUS REPAIR BTW STA Y=767-772,775-778 LONG 27R-29R. RUB STRIP AREA. DOUBLER REPAIR WAS ACCOMPLISHED IAW ERA 498170-14 REV ORIG.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

DURING HMV CORROSION WAS FOUND ON RT CUSP WEB X=-54 TO X=-60 STA Y=617 TO 636, 636 TO 655, 655 TO 674, 674 TO 693 AND 693 TO 712 AT FLOOR STRUCTURE PAX CABIN. REF MD-88 SRM 53-20-02D FOR REPAIR.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

DURING HMV CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LWR DOOR JAMB BEAM AFTER REPAIR PARTS REMOVED BTW STA Y=1155 TO 1212. REF MD88 SRM 53-05 FIG 123 FOR REPAIR.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

CORROSION ON FINGER DOUBLER OF PREVIOUS REPAIR BETWEEN LONG 30 AND 29 LT AND STA Y=446-465 AT FWD CARGO COMPARTMENT. REPAIR WAS ACCOMPLISHED IAW ERA 090454-14 REV B.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

AT HMV TRANSFERRED FROM SMS ERA 456396-14 REV D SEC III PERMANENT REPAIR TO FUSELAGE SKIN AT STA Y=110-140 LONGERON 28R-29L.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

CORROSION ON RT CUSP WEB X=54 TO X=60 STA 617 T0 636 636 TO 655 655 TO 674 674 TO 693 693 TO 712 AT FLOOR STRUCTURE PAX CABIN. CUSP WEB WAS REMOVED AND REPLACED PER IAW DC9/MD80 SRM 51-30-02, 51-30-05, 51-30-1 FROM STA 598 TO 712.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

CORROSION AT AFT LAV SERVICE DOOR CUTOUT SURROUND DOUBLER. REPAIRED PER ERA 494539-14 REV ORIG.

Part: BLANKET — PUNCTURED (LT WING) · airframe 48,787 hrs · 35,280 cycles

PUNCTURE ON LT WING UPPER SKIN HEATER BLANKET. REPAIRED PER ERA 497028-14AD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,787 hrs · 35,280 cycles

TRANSFERRED FROM SMS ERA456396-14 CODE 9-53-31-10 REV D SEC PERMANENT REPAIR. REPAIR WAS DONE PER AMR 0953959 REV ORIG.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 48,594 hrs · 35,124 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,124 hrs · 34,776 cycles

DURING PSV VISIT IN MSP FOUND AFT LAV SERVICE PANEL CUTOUT CORRODED INTO SKIN. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER. WORKED ON NRC 66 PER ERA 494539-14.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 48,124 hrs · 34,776 cycles

DURING PSV VISIT IN MSP FOUND CRACK ON VERTICAL LEADING EDGE ZFS26.8 LEFT SIDE FWD OF CUTOUT. REMOVED DAMAGE INSTALLED FILLER AND DOUBLER PER MD-88 SRM 53-01 FIG 4. WORKED ON N/R 101.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 48,124 hrs · 34,776 cycles

A 5 INCH CRACK ON VERTICAL STAB STA 1418 FWD OF AIR SCOOP ON LEADING EDGE. FOUND DURING PSV VISIT MSP NON ROUTINE NR 68. REPLACED CLIP PER SRM 51-01. PART NUMBER 5912188U49.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,936 hrs · 34,642 cycles

FUSELAGE SKIN STA 1437, S3R CRACK REPAIRED IAW ERA 493755-14.

Part: CONNECTOR — LOOSE (CABIN) · airframe 47,608 hrs · 34,398 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY ESCAPE LIGHT AT SEAT 31D INOPERATIVE. MAINTENANCE RE-SECURED LOOSE CONNECTOR AT LIGHT. OPERATION OF LIGHT NOW CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,499 hrs · 34,322 cycles

DURING LINE CHECK, MX FOUND ROWS 31-38 EMERGENCY PATHWAY LIGHTS INOPERATIVE. MX REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,474 hrs · 34,302 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT AT ROW 2CD INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,733 hrs · 33,806 cycles

FLIGHT CREW FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN INOPERATIVE. MX REPLACED THE FIRST CLASS EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYS.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,276 hrs · 33,511 cycles

C-3 THRESHOLD CORRODED 25-50 PERCENT THICKNESS. REMOVED REPAIRED BY SRM 53-05 FIG 123 ON NR 44. (DLM88102966)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,898 hrs · 33,249 cycles

MX FOUND THE EMERGENCY PATH LIGHT AT SEAT 26D TO BE INOPERATIVE. MX REPLACED THE EMERGENCY PATH LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 45,295 hrs · 32,835 cycles

ON FLIGHT CHECK MX FOUND EMERGENCY LIGHTS AT ROW 1-12 WERE INOPERATIVE. MX FOUND LOOSE WIRE UNDER CARPET NEAR FORWARD GALLEY. MX REPAIRED WIRE AND OPS CHECK OF LIGHTS NOW CHECK GOOD. (DLM88101511)

Part: SOCKET — SHORTED (CABIN LIGHTS) · airframe 42,523 hrs · 31,016 cycles

OVERHEAD LIGHT ABOVE 14ABC STARTED SMOKING. FOUND SOCKET AT UPPER SIDE WALL LIGHT 14C SHORTED. SIDE WALL LAMP SOCKET MFG P/N BV03112N36 NIS. DEACTIVATED LIGHTS (PULLED C/B) DEFERED PER MEL 33-00-02.

Part: LATCH — DEFECTIVE (COWLING) · airframe 41,100 hrs · 30,120 cycles

ENGINE UPPER COWL DOOR LATCH REPLACED IAW EA 09-056907-12, ME06.

Part: PAN — CORRODED (FUSELAGE) · airframe 40,747 hrs · 29,862 cycles

CORROSION WAS FOUND AT C1 LOWER THRESHOLD JAMB PAN AND REPAIRED PER SRM 53-05D FIG 804D.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 38,946 hrs · 28,708 cycles

A MAJOR REPAIR TO PRIMARY STRUCTURE WAS ACCOMPLISHED TO THE FWD CARGO DOOR JAMB PER SRM 53-05D FIG 804D DUE TO CORROSION.

Part: SKIN — DENTED (BS 110-140) · airframe 34,941 hrs · 26,117 cycles

FOUND SKIN DENTED AT FS 110 - FS 140 L28R-L29L. DAMAGED SKIN CUTOUT AND REPAIR DOUBLER INSTALLED.

Part: TIRE — FAILED (NLG) · airframe 34,941 hrs · 26,117 cycles

A LOUD THUMP PRIOR TO ROTATION AND UNSAFE NOSE UP INDICATION ON FLT 1046/0629/06 FROM DEN TO ATL. FOUND NOSE TIRE SEPARATION AND CAUSE TWO DENTS AND ONE GOUGE IN THE LWR SKIN BEHIND THE E/E DOOR CUT OUT. REPAIR PER ERA 456396-14 REV A ON NONROUTINE 001.

Part: ENGINE — MAKING METAL (NR 1) · airframe 34,787 hrs · 26,017 cycles

CLIMBING THROUGH 8000K HEARD A LOUD BANG ACCOMPANIED BY VIBRATIONS. LEFT ENGINE RPM ROLLED BACK AND EGT RISING. ACCOMPLISHED CHECKLIST AND SHUT DOWN ENGINE. NO FIRE WARNING RIGHT INSP INLET AND EXHAUST, NO DAMAGE NOTED. REPLACED MAIN OIL FILTER 1386688. INSP LEFT ENG INLET AND EXHAUST FOUND METAL IN TAIL PIPE 1386688. REPLACED LEFT ENGINE PER TRANS 9T102. CHECK GOOD.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 24,554 hrs · 18,819 cycles

AFT RT SMOKE DETECTOR SOUNDED ON TAXI OUT. FUMES/HAZE REPORTED NEAR WING AREA. APU, LEFT ENGINE, AND BOTH PACKS WERE OPERATING. RETURNED TO GATE. ODOR PRESENT WITH LEFT PACK ONLY. INPS APU INLET, CKS OK. INSPECTED LT PACK, OIL CLEAN AND ROTATES FREELY. INSPECTED DUCTS, NO CONTAMINATION FOUND. REPLACED SOILED WATER SEPARATOR BAG LEFT SIDE, RAN A/ PACK PER OPN 5088 WITH APU AND E.

Part: HARNESS — CHAFED (AFT CARGO BAY) · airframe 21,523 hrs · 16,598 cycles

AFT CARGO LOADING SYSTEM WILL NOT WORK. FOUND WIRE BUNDLE BURNED 6 INCHES AFT FROM DISCONNECT PLUG P1-9035 OF THE AFT CARGO LOADING SYSTEM DUE TO CHAFING ON SCREW SHANK ON THE FORWARD SIDE OF THE MOVING WALL. RE-TERMINATED CONNECTOR P1-9035.

Part: SENSOR — OUT OF ADJUST (LE FLAP)

DURING SLAT RETRACTION DISAGREE LIGHT REMAINED ILLUMINATED. POM PROCEDURE FOLLOWED AND LIGHT REMAINED ON. FOUND D SENSOR RT WING STICKING IN THE CLOSE POSITION WITH SLAT UP. ADJUSTED MECH TARGET GUIDES AND LUBRICATED, OPN NOW CKS NORMAL PER MM.

Part: SKIN — DENTED (BS 229 - 249)

THERE WERE SEVERAL DENTS FOUND BELOW THE CUSP LINE BETWEEN FS 229 AND 249. THE DENTS WERE CUT OUT AND REPAIRED PER ERA 334035-14 AT HMV.

Part: SKIN — DENTED (BS 229 - 237)

SEVERAL DENTS WERE FOUND ABOVE THE CUSP LINE BETWEEN FS 229 AND FS 237. THE DAMAGE WAS CUT OUT AND REPAIRED PER ERA 334043-14 AT HMV.

Part: SKIN — DENTED (BS 310)

THIS AIRCRAFT RECEIVED GROUND DAMAGE TO THE FUSELAGE SKIN AT FS 310 AND LONGERON 26L. THE DAMAGE RESULTED IN A 5.5 X 33 CUTOUT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334042-14.

Part: COMPUTER — FAILED (FLIGHT MANAGE)

CLIMBOUT OF EWR TOTAL IRU FAIL LIGHTS. LOSS OF NAVIGATION PLATFORM, NO HEADING. REPLACED NR 1 IRU, ALIGNED BOTH IRUS. SYS CK GOOD PER MM.

Part: COALESCER BAG — CONTAMINATED (TAIL COMPT)

SHORTLY AFTER T/O, BURNING SMELL IN CABIN DISSIPATED AT 10,000 FEET. REPLACED COALESCER BAGS, PERFORMED BURNOUT AND NO SMELL NOTED.

Part: APU — CONTAMINATED (CABIN)

ATB OIL SMOKE SMELL IN CABIN. FOUND RESIDUAL OIL IN APU INLET. FWD APU TO MCO. RAN ENGINES, NO OIL SMELL NOTED.

Part: LIGHT — BROKEN (CABIN)

ON L/O, FOUND ROW 18 D, E, EMERGENCY LIGHT ON FLOOR LIGHT ASSY BROKEN. REPLACED LIGHT ASSY.

Part: EEL POWER SUPPLY — INOP (CABIN)

DURING PREFLIGHT, FOUND FORWARD CABIN EMERGENCY FLOOR TRACK LIGHTS FAIL TO TEST. REPLACED POWER SUPPLY, OPERATION NORMAL.