N952DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,794 hrs · 53,896 cycles

LT AND RT NACELLE OVER WING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK AND RACK IAW AMM 3353.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,562 hrs · 53,707 cycles

EMERGENCY LIGHT AT FWD GALLEY WAS INOPERATIVE. REPLACED THE LIGHT ASSY AND TESTED IAW AMM 33-50. TESTED OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 70,455 hrs · 52,113 cycles

OVERWING EMERGENCY LIGHT FAILED DURING CHECK. EMERGENCY LIGHTS BATTERY PACK WAS REPLACED IAW AMM 33-53-00.

Part: STRINGER — CRACKED (RT WING) · corrosion level 2 · airframe 70,444 hrs · 52,103 cycles

A FOUR INCH CRACK WAS FOUND ON THE RT WING MAIN FRAME STRINGER 11 XRS 160. REPAIRED THE STRINGER IAW ER/A 552847-14 AD REV. ORIGINAL AND DRAWING SR09570100 REV. B.

Part: AXLE — DAMAGED (NLG) · corrosion level 2 · airframe 70,455 hrs · 52,113 cycles

CORROSION ON CYLINDER AND HOUSING WORN ON AXLE OF NOSE LANDING GEAR. NLG CYLINDER AND HOUSING WAS REPLACED.

Part: PAN — CRACKED (L1 DOOR) · airframe 70,444 hrs · 52,103 cycles

CRACKED FWD UPPER CORNER PAN OF THE L1 DOOR. THE PAN WAS REPAIRED IAW SRM 52-05 PAR 14 FIG 18A.

Part: FRAME — CRACKED (BS 1380) · airframe 70,444 hrs · 52,103 cycles

CRACKED FRAME ANGLE BS 1380 BETWEEN LONGERONS 13 - 14R. THE FRAME ANGLE WAS REPAIRED IAW SRM 53-01 FIG 2 SHEET 4.

Part: DOOR FRAME — CORRODED (BS 636-693) · corrosion level 2 · airframe 70,444 hrs · 52,103 cycles

MID CARGO BAY CORROSION WAS FOUND ON THE LOWER DOOR FRAME PREVIOUS REPAIR BS 636 - 693. THE SPACER WAS REPLACED IAW SRM 53-05 FIG 123.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,385 hrs · 50,592 cycles

FLIGHT CREW FOUND THAT THE COCKPIT EMERGENCY LIGHTS WOULD NOT FULLY EXTINQUISH. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK BATTERIES AND THE LIGHTS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,174 hrs · 50,441 cycles

BOTH LT & RT EMERGENCY OVERWING DOOR EXIT IDENTIFIERS INOPERATIVE AT ROW 24. REPLACED EMERGENCY BATTERIES AT ROW 24 OVERHEAD AND OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,516 hrs · 49,262 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE FORWARD OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: FRAME — CRACKED (TAIL) · airframe 65,226 hrs · 48,380 cycles

TAIL INTERIOR FRAME WEB HAS A ONE INCH CRACK AT INTERIOR RELEASE HANDLE SUPPORT STRUCTURE. REPAIRED IAW ER/A 530319-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1463) · airframe 65,226 hrs · 48,380 cycles

TAIL INTERIOR SKIN DOUBLER HAS A ONE INCH CRACK LONGERON 2R BS 1463. REPAIRED IAW FINAL ER/A 530325-14, SEC I AND II REV ORIGINAL.

Part: PIN — WORN (TAILCONE RELEASE) · airframe 65,226 hrs · 48,380 cycles

MAINTENANCE DISCOVERED THAT THE RELEASE LATCH TEE PIN FOR THE TAILCONE WAS FRAYED AND WORN OUT OF ALLOWABLE LIMITS. THE TEE PIN WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: SKIN — CRACKED (BS 1463) · airframe 65,226 hrs · 48,380 cycles

TAIL INTERIOR SKIN DOUBLER HAS A ONE INCH CRACK LONGERON 2 RT, BS 1463. REPAIRED IAW PRI 530325-14, REV. 1.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 65,107 hrs · 48,302 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 23D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A WIRE PULLED OUT OF THE CONNECTOR. THE WIRE WAS REINSTALLED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,107 hrs · 48,302 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 23, 24, & 25 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,977 hrs · 48,202 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 23D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 64,546 hrs · 47,880 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 27D WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND THE SYS RETURNED TO NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,877 hrs · 47,390 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THAT THE LEFT EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,521 hrs · 47,150 cycles

OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE BETWEEN ROWS 14-20 & 25-30. REPLACED ASSOCIATED EMERGENCY LIGHT BATTERIES IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: CABLE — FRAYED (TAILCONE JET) · airframe 61,738 hrs · 45,847 cycles

DURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON CABLES WERE DAMAGED BY FRAYING. THE SYSTEM WAS REPAIRED BY CABLE REPLACEMENT, ADJUSTMENT, AND RIGGING IAW AMM 20-10-17, 201.

Part: SKIN — CORRODED (BS 763) · corrosion level 2 · airframe 61,738 hrs · 45,847 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING BS 763 BETWEEN LONG 27R-28R IN REF 663, ZONE 50. REF 334 ZONE 50. CORROSION ON FUSELAGE SKIN WAS REMOVED IAW SRM 51-10-3, PAR 26, WITH ORIGINAL THICKNESS IS 0.091" AND MINIMUM REMAINING THICKNESS 0.029" WAS FOUND OUT LIMITS, IT WAS REPAIRED IAW SRM 53-04, FIG 57 AND 51-30-5.

Part: CAM — WORN (TAILCONE JET) · airframe 61,738 hrs · 45,847 cycles

DURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON RELEASE MECHANISM CAM BASE WAS WORN BEYOND ALLOWABLE LIMITS. THE SYS WAS REPAIRED BY CAM BASE REPLACEMENT IAW AMM 53-53-02.

Part: SKIN — DAMAGED (BS 237) · airframe 61,738 hrs · 45,847 cycles

DAMAGE ON FUSELAGE SKIN BS 237 UNDER PREVIOUS REPAIR DOUBLER LWR EDGE. IN REF, NRC 303 A/C ZONE 50. PREVIOUS REPAIR WAS REMOVED IAW SRM 51-30-2 AND 51-30-30 REPAIR PARTS WERE FABRICATED AND INSTALLED IAW AMR 09531227, REV 2 AND ER/A 514796-14, REV, ORIG RII COMPLETED.

Part: SKIN — CORRODED (BS 1105-1119) · corrosion level 2 · airframe 61,738 hrs · 45,847 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING RUB STRIPS STA Y=1105 AND 1119 IN REF NRC 664 ACFT ZONE 50. (REF 673, ZONE 50) STA. Y= 1105 DUE TO EXCESSIVE CORROSION AREA WAS REPAIRED AND DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIG 57, 51-10-3 PAR 21 AND 14 STA Y=1119 CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26 AND WAS ATTENDED WITH ER/A 514786-14 REV ORIG RII COMPLETED BY INSPECTOR AIG 200800734 ID DELTA 298092 ASSOCIATED ER/A 51-478614 ADDED FOR AC 0952.

Part: SKIN — DENTED (BS 222) · airframe 61,738 hrs · 45,847 cycles

DENT ON FUSELAGE SKIN BS 222 BETWEEN LONGERON 17-18L. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-04-5 FIG 3 AND AMR 09531227, REV 2 AND ER/A 514796-14 REV ORIG.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 61,738 hrs · 45,847 cycles

CORROSION ON LOWER DOOR FRAME BEAM STA Y=1155-1212 AT AFT CARGO COMPARTMENT. (C3) (MRB 53-019-02). CORROSION WAS BLENDED OUT IAW SRM 51-10-3. PAR 21 AND 14 (UT) AND REMAINING THICKNESSES WERE FOUND OUT OF LIMITS IAW DWG 5936038, REV "A" AND SRM 53-05 FIG 123.; AREA WAS REPAIRED IAW SRM 53-05, FIG 123A AND ER/A 512899-14 REV ORIG PANAMETRICS NDT33-TRANSDUCER SON OPEN V260SM EXP. DATE 13-JUL-13 REF AMX PND-159 AND 162. RII COMPLETED BY INSPECTION STAMP HAG DELTA ID 870444. CORROSION LEVEL 2. ASSOCIATED ER/A 51-289914 ADDED FOR AC 0952.

Part: BULKHEAD — DAMAGED · airframe 61,744 hrs · 45,851 cycles

SCRATCHES ON AFT PRESSURE BULKHEAD LWR TEE BETWEEN LONG 29 - 30L. DAMAGE WAS REMOVED IAW AMR 09531223, REV 1, NEW SECTION TEE WAS INSTALLED IAW AMR 09531223, REV 1 AND ER/A 514780-14, REV ORG.

Part: PAN — CRACKED (PAX DOOR) · airframe 61,738 hrs · 45,847 cycles

CRACKED OUTER PAN ON INBD EDGE BETWEEN BEAM N.4 AND UPPER FACE OF LOWER HINGE IN FWD EDGE AT FWD SERVICE DOOR. (R1)(REF 311, ZONE 50). PAN WAS REPAIRED IAW ER/A 512895-14 REV ORG REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-05 ASSOCIATED ER/A 51-289514, ADDED FOR AC 0952.

Part: LONGERON — CORRODED (BS 1345-1380) · airframe 61,738 hrs · 45,847 cycles

DURING SCHEDULED INSPECTION, LEVEL 2 CORROSION WAS FOUND ON LONGERON 24 LT FROM STA Y= 1345 TO Y=1380. LONGERON 24 LT WAS REPLACED BETWEEN, Y=1338-1429, IAW SRM 51-30-2 AND 51-30-5 DUE TO EXFOLIATION CORROSION.

Part: CARGO TRACK — CORRODED (BS 1220-1322) · airframe 61,738 hrs · 45,847 cycles

DURING SCHEDULED INSPECTION, CORROSION FOUND ON CARGO TRACK BS 1220-1322 IN AFT CARGO BAY. CARGO TRACK REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 61,738 hrs · 45,847 cycles

DURING SCHEDULED INSPECTION, CORROSION FOUND ON CARGO TRACK BS 1007 TO 1155 IN AFT CARGO BAY. CARGO TRACK REPLACED IAW SRM 51-30-2 AND 51-30-1, 51-30-5.

Part: HEATER BLANKET — CRACKED (LT WING) · airframe 61,738 hrs · 45,847 cycles

CRACK ON AFT SECTION OF LT WING HEATER BLANKET. LT WING HEATER BLANKET WAS REPLACED DUE TO 1 CRACK OF 0.531 WAS FOUND IAW AMM 30-80-02, PAGEBLOCK 401 AND 601 AND ER/A 494597-14 AD MA REVISION A. RII COMPLETED BY INSPECTION STAMP DELTA ID NR 298092, LIC 200800734 AIG ASSOCIATED ER/A 49-459714, ADDED FOR AC 0952.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,738 hrs · 45,847 cycles

CRACKED INNER PAN INNER SIDE OF FWD EDGE AT MID CARGO COMPARTMENT DOOR BETWEEN BEAM 1 AND LOWER EDGE, ALSO BETWEEN BEAM NR 4 AND 5. (C2). MID CARGO COMPARTMENT DOOR INNER PAN CRACKS REPAIR WAS ACCOMPLISHED IAW ER/A 514781-14 REV. ORIG.

Part: LONGERON — CRACKED (BS 1307) · airframe 61,738 hrs · 45,847 cycles

CRACKED LONGERON 5R BS 1307 AT RT AFT LAVATORY AREA. CRACKED LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,738 hrs · 45,847 cycles

CRACKED PAN BELOW STOP FITTING NR 4 ON FWD EDGE OF MID CARGO COMPARTMENT DOOR. REF CARD 111, ZONE 51 AND (T0 280178) (REF NRC NR 622, ZONE 50). REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIG 50, HFEC INSP WAS PERFORMED IAW NDT SPM 06-10-01. 001 RII COMPLETED BY INSPECTOR.

Part: LONGERON — CRACKED (BS 807) · airframe 61,738 hrs · 45,847 cycles

CRACKED LONGERON 3R, BS 807 AT PASSENGER CABIN. SECTION DAMAGE WAS REPLACED IAW SRM 52-03, FIG 18. NEW SPLICE WERE ADJUSTED AND INSTALLED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 160 L2L) · airframe 61,738 hrs · 45,847 cycles

CRACKED LONGERON NR 2 LT BS 160. FASTENERS AND LONGERON WERE REMOVED IAW 51-30-3 AND 51-30-2. NEW LONGERON AND SPLICE IAW SRM 53-14-2 AND 53-02. NEW LONGERON AND SPLICE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — WORN (LT WING) · airframe 61,738 hrs · 45,847 cycles

WEAR ON L/E AROUND OF LT WING SLAT TRACK CUT OUT. AREAS WERE BLENDED OUT IAW SRM 57-01 AND AREA OUT OF LIMITS WAS ACOMPLISHED WITH AMR 09570520 AND ER/A 512889-14, REV ORIG AND AREAS WERE TREATED AND IDENTIFIED IAW ER/A 512889-14, REV ORIG AND SRM 51-10-3.

Part: STOP FITTING — DAMAGED (CARGO DOOR) · airframe 61,738 hrs · 45,847 cycles

HIDDEN DAMAGED CRACKED INNER PAN OUTER SURFACE ON STOP FITTING NR 2 POSITION AFT EDGE OF FWD CARGO DOOR. REPAIRED IAW SRM 52-050, FIG 50.

Part: SKIN — DAMAGED (BS 389-408) · airframe 61,738 hrs · 45,847 cycles

CRACKS ON PREVIOUS REPAIR DOUBLERS OF FWD CARGO COMPARTMENT DOOR BARRIER INBD CHANNEL UPPER SUPPORT BS A 389 AND 408. (PREVIOUS REPAIR DOUBLERS WERE REMOVED AND NEW REPAIR DOUBLERS WERE INSTALLED IAW ER/A 38-309914 REV.

Part: LONGERON — CRACKED (4 LEFT) · airframe 61,738 hrs · 45,847 cycles

CRACKED LONGERON NR 4 LT BS 160AT PAX CABIN. DAMAGE SECTION OF LONGERON WAS REPLACED IAW SRM 53-02, FIS .18

Part: CHANNEL — CRACKED (BS 939) · airframe 61,738 hrs · 45,847 cycles

CRACKED FWD Z CHANNEL, BS 939 AT RT MLG DOOR INBD AND OTBD EDGE. CRACK FWD CHANNEL AND OUTER EDGE WERE REMOVED. NEW CHANNEL DRILLED, ADJUSTED, AND INSTALLED IAW SRM 51-30-2 51-10-4 AND 51-10-3, PAR 14/21 AND OTBD EDGE FILLER SECTION TAPERED SHIM AND REPAIR ANGLE WERE FABRICATED AND INSTALLED AND IDENTIFIED REAPAIR IAW ER/A NR 48334-14MA, REV ORIGINAL.

Part: LONGERON — DAMAGED (BS 541 L4L) · airframe 61,738 hrs · 45,847 cycles

CRACKED LONGERON 4L BS 541 AT PASSENGER CABIN. DAMAGED LONGERON WAS REMOVED, NEW LONGERON AND SPLICES WERE DRILLED AND ADJUSTED AND INSTALLED IAW SRM 53-02, FIG 18.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 61,738 hrs · 45,847 cycles

CRACKED OTBD Z CHANNEL AT RT MLG DOOR FWD EDGE. OTBD CHANNEL REPAIRED AND FABRICATED DOUBLER REPAIR INSTALLED IAW ER/A 487626-14 MA REV. ORIG.

Part: DOOR FRAME — DAMAGED (CARGO BAY) · corrosion level 2 · airframe 61,738 hrs · 45,847 cycles

CORROSION ON MID CARGO COMPARTMENT LWR DOOR JAMB BEAM. REPLACED IAW SRM 53-05, FIG 123 AND ER/A 46312914, REV "A".

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,738 hrs · 45,847 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN. FOUND WITH LIMITS IAW SRM 53-04-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,738 hrs · 45,847 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN AT RT ALTERNATE STATIC PORT CRITICAL AREA. FOUND WITHIN LIMITS IAW SRM 53-04-1,

Part: PAN — DAMAGED (BS 807) · airframe 61,738 hrs · 45,847 cycles

CRACKED LT WINDOW RING PAN AT AFT LWR CORNER BETWEEN BS 807. DAMAGE REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 984) · airframe 61,738 hrs · 45,847 cycles

CRACKED LT WINDOW RING PAN AT FWD LWR CORNER BS 984. DAMAGE REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-05 FIG 122.

Part: SKIN — CRACKED (BS 389) · airframe 61,738 hrs · 45,847 cycles

WHILE PERFORMING REPETITIVE INSPECTION OF LIGHTNING STRIKE DAMAGE AT BS 389, ABOVE STR 9L, FOUND CRACK IN SKIN. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-04-2, FIG 2.

Part: SKIN — CRACKED (BS 465) · airframe 61,738 hrs · 45,847 cycles

WHILE PERFORMING REPETATIVE INSPECTION OF LIGHTNING STRIKE DAMAGE AT BS 465 ABOVE STR 9L, FOUND CRACK IN SKIN. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIG. 2.

Part: BOTTLE — LOW PRESSURE (ESCAPE SLIDE) · airframe 61,485 hrs · 45,692 cycles

DURING LINE INSPECTION, THE AFT SERVICE DOOR ESCAPE SLIDE PRESSURE WAS FOUND TO BE LOW. THE AFT SERVICE DOOR ESCAPE SLIDE WAS R & R IAW AMDS CARD 2500-4484. PRESSURE AND CLEARANCE CHECKS ARE CORRECT. REQUIRED INSPECTION COMPLETED.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 60,752 hrs · 45,165 cycles

VERTICAL STABILIZER FRONT SPAR HAS AN OVERSIZED HOLE. PERFORMED LFEC HFEC AND BHEC INSPECTIONS OF LT AND RT VERTICAL STABILIZER. NO CRACKS INDICATED. PERFORMED DETAILED INSPECTION TO VERTICAL STAB L/E STRUCTURE. C/W SECTION 2 OF ERA 489672-14AD REV B .

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,558 hrs · 45,021 cycles

DURING LINE CHECK, MX FOUND NUMEROUS OVERHEAD EMERGENCY PATHWAY LIGHTS IN THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 59,907 hrs · 44,540 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 11D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR AND REPAIRED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,466 hrs · 44,231 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH THE LEFT AND RIGHT OVERWING EMERGENCY EXIT SIGNS AT ROW 24 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND THE BATTERIES; OPS CHECKED SYSTEM.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 59,466 hrs · 44,231 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 12DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS DISCONNECTED, SECURED CONNECTOR , FUNCTIONALLY CHECKED SYSTEM.

Part: LANYARD — MISROUTED (R2 DOOR SLIDE) · airframe 58,904 hrs · 43,879 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND R2 DOOR SLIDE LANYARD MISROUTED. MAINTENANCE CORRECTLY ROUTED SLIDE LANYARD PER AMM. AIRCRAFT OKAY FOR SERVICE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 58,368 hrs · 43,565 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3C IN THE CABIN, WAS INOPERATIVE. MAINTENANCE RE-SEATED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE SYSTEM.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 58,296 hrs · 43,512 cycles

DURING PSV CHECK ON 07NOV11, FOUND RT HORIZ STAB REAR SPAR CRACKED AFT OF BARREL NUT HOLE THAT ATTACHES TO HORIZ CONSTANT SECTION. VERIFIED WITH HFEC LENGTH IS APPROX 0.300 ON AN INCH, MARKED END. HORIZ STAB PRESENTLY BEING REMOVED FOR REPAIR, MORE INFO WILL BE PROVIDED AS KNOWN.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 58,296 hrs · 43,512 cycles

EXTERIOR SKIN AT STA 1437 LT OF VERTICAL STAB 12" 2EA CRACK SEMINATING FROM FASTENER HOLE. ACCOMPLISHED SKIN REPAIR PER ERA 497569-14 REV O.

Part: WIRE — PULLED (CABIN) · airframe 57,938 hrs · 43,257 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT SEAT 1C, 17D, AND 28D. MAINTENANCE REPAIRED PULLED WIRES FROM LIGHT CONNECTORS AT SEAT 1C, 28D. LIGHT HARNESS WAS REPLACED AT SEAT 17D PER AMM 33-53. OPERATION OF LIGHT CHECKS OK.

Part: DEFOG SYSTEM — SHORTED (SLIDING WINDOW) · airframe 57,779 hrs · 43,136 cycles

DURING TAXI TO GATE IN LGA F/O OPENED WINDOW AND WIRES CAUGHT FIRE. MAINTENANCE CAPPED AND STOWED WIRES PER SWPM 20-10-04 AND C/B Z24 WAS PULLED AND COLLARED. MAINTENANCE REPAIRED THE FIRST OFFICER'S WINDOW ANTI-FOG WIRING PER SWPM, CHAPTER 20. RIGHT ANTI-FOG SYSTEM NOW CHECKS GOOD.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 57,581 hrs · 42,984 cycles

C/W OPN 8959 AD FOUND RT UPPER AFT SKIN PANEL CRACK APPROX 1 INCH LONG. C/W EA 09-460214-12 AD REV E ME 24 OPN 2401 CATEGORY A REPAIR TRIM-OUT. REPETITIVE AT 1,000 FC AND PERM REPAIR AT 4,000 FC EA.

Part: ANGLE — CORRODED (FLOOR PANEL) · airframe 56,342 hrs · 42,173 cycles

NRC 73 FLOOR PANEL CORRODED AFT END OF FLOOR PANEL AT C-3 DOOR. REMOVED AND REPLACED Z-ANGLE.

Part: LIGHT — INOPERATIVE (SEAT 28C) · airframe 55,575 hrs · 41,671 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT SEAT 28C INOPERATIVE. MX REPLACED LIGHT ASSY AT SEAT28C. OPS CHECK OF LIGHT IS NOW OK.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 54,649 hrs · 41,054 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHTS AT ROW 23DE INOP. MX FOUND LOOSE WIRE AND SECURED WIRE IN PROPER PLACE. OPS CHECK OF LIGHTS IS GOOD. (DLM88101464)

Part: CONTROL CABLE — FOD (FLAP/SLATS) · airframe 50,766 hrs · 38,574 cycles

WHEN SLATS/FLAPS WERE EXTENDED FROM CLEAN POSITION, THE AIRCRAFT ROLLED APPROXIMATELY 20-30 DEGREES UNCOMMANDED. INSPECTED AIRCRAFT, FOUND SCREWDRIVER STUCK IN CONTROL CABLES ABOVE E/E DOOR AT STA 116. REMOVED TOOL. RAN FLIGHT CONTROLS, FLAPS/SLATS, AILERON AND RUDDER TRIM. ALL CHECKS NORMAL. NO DAMAGE FOUND. OK FOR SERVICE.

Part: CUSP WEB — CORRODED (BS 892-897) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON RT CUSP WEB AT STA 892 AND 897, REPAIR PER ERA 398191-14MA.

Part: SKIN — NONE (BS 218) · airframe 47,537 hrs · 36,383 cycles

TEMPORARY REPAIR ON STA 218 AND LONG 23-25 RT, REPAIRED PER SRM 53-04D FIG 12B ON N/R T0064057 ON HMV IN GDL.

Part: FITTING — CRACKED (BS 1348) · airframe 47,537 hrs · 36,383 cycles

CRACK ON STRUCTURE OF RIGHT OF AFT PASSENGER DOOR JAMB FITTING WAS REPLACED IAW DWG 5917579.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON FITTING IN FWD LWR CORNER OF C-3 AT JOINT WITH FUSELUGE SKIN AND DOOR JAMB BEAM. (TASK 57-53300). REPLACED PER DRWG, 5930483 ON N/R T0064934 IN HMV AT GDL.

Part: ANGLE — CRACKED (STA.787 27/28LH) · airframe 47,537 hrs · 36,383 cycles

CRACKED FITTING BETWEEN FRAME AND INTERCOSTAL AT STA 787 BETWEEN LONGERON 27 LH AND 28LH. REPLACED FITTING PER DRWG 5956034 ON N/R T0065338 IN HMV AT GDL.

Part: FLOORBEAM — CRACKED (BS 905) · airframe 47,537 hrs · 36,383 cycles

CRACKED FLOOR SUPPORT FITTING AT STA. 905 AND X=44. REPLACED FITTING PER DRWG 9923417 REV.B ON N/R T0064339 ON HMV IN GDL.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 47,537 hrs · 36,383 cycles

PITTING CORROSION ALONG BEAM OF LOWER C-3 DOOR JAMB, TASK 57-53300. REPAIRED PER SRM 53-05 FIG 63 ON N/R T0064677 ON HMV IN GDL.

Part: STIFFENER — CRACKED (BS 1338) · airframe 47,537 hrs · 36,383 cycles

FOUND CRACK ON STIFFENER ON STA 1338 AT 12 HRS POSITION. REPLACED IAW DWG 9915562.

Part: PAN — CORRODED (FWD CARGO DOOR) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON FWD CARGO COMPARTMENT DOOR JAMB LWR BEAM. REPLACED IAW SRM 53-05D FIG 804.

Part: SKIN — NONE (BS 180) · airframe 47,537 hrs · 36,383 cycles

TEMPORARY REPAIR ON STA 180 AND BETWEEN LONG 23 AND 25 RT. REPAIRED PER SRM 53-04D FIG 12B ON N/R T0064056 ON HMV IN GDL.

Part: FLOORBEAM — CRACKED (BS 886) · airframe 47,537 hrs · 36,383 cycles

FOUND BROKEN FLOOR SUPPORT FITTING AT STA.886 AND X=22. REPLACED PER DRWG 3925817 REV C ON N/R T0064394 AT HMV IN GDL.

Part: CUSP WEB — CORRODED (BS 612) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON RT CUSP WEB STA Y=612, REPAIR PER ERA 398191-14MA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,537 hrs · 36,383 cycles

CRACK ON FUSELAGE SKIN FROM FS Y=1439 AND BETWEEN LONGERON 3 RT AND 5 RT, TASK 50-53300. REPAIRED PER SRM 53-04D FIG.27 ON N/R T0064049 ON HMV IN GDL.

Part: ANGLE — CRACKED (BS 693) · airframe 47,537 hrs · 36,383 cycles

CRACK ON ANGLE (RACK SUPPORT) AT FS 693, LONG 21 LT (TASK 51-53300). REPLACED PER DRWG 5939741 ON N/R T0064838 ON HMV IN GDL.

Part: STIFFENER — CRACKED (L1 DOOR) · airframe 47,537 hrs · 36,383 cycles

FOUND CRACKED STIFFENER AT L1 DOOR BEAM NR 8. REPLACED IAW DWG 4916056.

Part: SKIN — CRACKED (LT WING) · airframe 47,537 hrs · 36,383 cycles

CRACK ON LEFT WING FIXED LEADING EDGE AT STA. XFS=238. REPAIRED PER ERA 380953-14MA ON N/R T0064417 AT HMV IN GDL.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 47,537 hrs · 36,383 cycles

FOUND CRACKED AFT BRACKET AT R-1 SERVICE DOOR BEAM NR 4. REPLACED BRACKET PER DRWG 9911582 ON N/R T0065303 IN HMV AT GDL.

Part: CUSP WEB — CORRODED (BS 727) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON LT CUSP WEB AT STA 727, REPAIR PER ERA 398191-14MA.

Part: CUSP WEB — CORRODED (BS 1098 -1117) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON RT CUSP WEB FRON STA 1098 TO 1117 REPAIR PER ERA 398191-14MA REV A.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 47,537 hrs · 36,383 cycles

FOUND CORROSION ON C-2 LOWER DOOR JAMB FROM FS=636 TO FS 693 (TASK 51-53300). REPAIRED PER SRM 53-05D FIG 63 ON N/R T0064848 AT HMV IN GDL.

Part: CUSP WEB — CORRODED (BS 1136-1174) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON RT CUSP WEB FRONT STA 1136 TO 1174 DAMAGE, REMOVED PER SRM 53-01 AND ERA 398191-14MA.

Part: CUSP WEB — CORRODED (BS 467-473) · airframe 47,537 hrs · 36,383 cycles

EXFOLIATION CORROSION ON RT CUSP WEB BETWEEN STA Y=467 TO 473. REPAIR PER ERA 398191-14MA.

Part: STRUCTURE — CRACKED (PAX DOOR FRAME) · airframe 47,537 hrs · 36,383 cycles

FOUND CRACK ON STRUCTURE OF RIGHT SIDE OF AFT PASSENGER DOOR JAMB STA 1348 Z 20. REPLACED IAW DWG 5917579.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,537 hrs · 36,383 cycles

THE NR 2 CARGO DOOR OPENING LOWER THRESHOLD HAD CORROSION REVOAL IN SEVERAL LOCATIONS. LOCAL BLENDING RESULTED IN THE AFT C/L DOOR STOP HOLE BREAKING OUT. REPAIR PER SRM 53-05 FIG 63 INSTALLED.

Part: SKIN — CORRODED (BS 661) · airframe 47,537 hrs · 36,383 cycles

A OF FUSELAGE SKIN AND DOOR SURROUND DOUBLER CORRODED BELOW THE C2 DOOR THRESHOLD. THE LOWER AFT DOUBLER CORNER AND THE SKIN AFT OF FS 661 WERE REPLACED AND ATTACHED WITH A SPLICE REPAIR. THIS SPLICE REPAIR ELIMINATED ER/A 385988-14.

Part: FITTING — DAMAGED (MLG) · airframe 47,537 hrs · 36,383 cycles

DURING HMV, MLG FITTING WAS FOUND WITH BORE OVERSIZED BEYOND AD AND SERVICE REWORK DRAWING LIMITS. BOEING WAS CONTACTED FOR APRPOVAL TO INSTALL OVERSIZED BUSHING, AND PROVIDED APPROPRIATE APPROVALS AS DETAILED IN 273922-14AD REVISION A.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,612 hrs · 35,776 cycles

FS 260, LONG 17-18, GROUND DAMAGE CUTOUT REPAIR. THE FUSELAGE SKIN WAS DAMAGED BY THE JET WAY. THE DAMAGE WAS REMOVED WITH A 8" BY 11" SKIN CUTOUT AND A SECTION OF LONGERON 17 REMOVED. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER AND THE LONGERON REPAIRED WITH AN FORMED ALUMINUM REPAIR SECTION PER THE MD-88 SRM. THE REPAIRS WERE DOCUMENTED PER ER/A 460339-14.

Part: DUCT — LEAKING (A/C BAY) · airframe 43,782 hrs · 33,933 cycles

AFTER TAKEOFF GOT FLOW LIGHT ON PRESS PANEL, ENG AND WING ANTI ICE WERE ON. RIGHT PACK TEMP ERRATIC. DIFF PRESSURE STOPPED AT 1.5 PSID. CABIN WOULD NOT PRESSURIZE. REPLACED LEAKING AC DUCT.

Part: ODOR — DETECTED (COCKPIT) · airframe 40,281 hrs · 31,421 cycles

DURING NORMAL T/O POWER APPLICATION AT APPROX 130 KNOTS BOTH PILOTS NOTICED A STRONG ELEC ODOR. FLT ATTENDANT CALLED AT 3000 FT WITH SAME IN CABIN. RETURNED TO ATL. PERFORMED OPN 5088 - UNABLE TO DUPLICATE CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGNECY LIGHT) · airframe 38,375 hrs · 30,097 cycles

AFT CABIN EMERGENCY PATH LIGHTS ALL INOP FROM SEAT ROW 31 AFT. TROUBLESHOT EMERGENCY LIGHT SYSTEM IN AFT CABIN, FOUND BAD BATTERY CHARGER ASSEMBLY IN OVERHEAD AT ROW 36-37. REMOVED AND REPLACED BATTERY CHARGER. ALL EMERGENCY LIGHTS OPERATE NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,214 hrs · 29,987 cycles

THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED. THE CORROSION WAS REMOVED WITH A 4 X 7 INCH CUTOUT THROUGH BOTH LAYERS. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385988-14, REV A.

Part: OVEN — SMOKE (GALLEY) · airframe 35,168 hrs · 27,817 cycles

CLIMBING OUT OF SAT AT APPROXIMATELY 8000 FT, FA REPORTED SMOKE COMIING FROM FWD GALLEY AC WAS LEVELED AT 14000 FT FLT CREW SHUT OFF GALLEY POWER. SMOKE DISSAPATED DIVERTED TO AUS WITHOUT INCIDENT. REMOVED F/C OVEN AND INSPECTED FOR HEAT AND OVEN WIRE HARNESS, NONE FOUND. REPLACED OVEN.

Part: PIN — CORRODED (LT MLG) · airframe 33,903 hrs · 26,877 cycles

DURING INSPECTION OF THE MLG AT HMV THE LT MLG FWD TRUNNION ATTACH PIN WAS FOUND TO HAVE CORROSION CAUSING LOOSENESS IN THE ATTACH POINT.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,903 hrs · 26,877 cycles

FUSELAGE CABIN FLOOR PANEL WAS FOUND DELAMINATED AND CRACKED. REPAIR PER ER/A 411006-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,704 hrs · 26,723 cycles

SEAT 21D EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, CHECKS GOOD.

Part: TARGET — OUT OF ADJUST (CARGO DOOR) · airframe 33,658 hrs · 26,693 cycles

AFTER T/O ROLL STARTED AFT CARGO LIGHT CAME ON. REJECTED T/O AT 30 KTS. ADJUSTED PROX TARGET.

Part: WIRE — BROKEN (CABIN) · airframe 33,240 hrs · 26,365 cycles

ON LAYOVER, FOUND SEAT 19CDE EMERGENCY LIGHT OUT. FOUND HARNESS WIRE BROKEN. RESECURED WIRE, OPS NORMAL.

Part: CONNECTOR — FAILED (CABIN LIGHTS) · airframe 30,388 hrs · 24,281 cycles

CABIN LIGHTING CONNECTOR ABOVE SEAT 2CD SHORTED AND BURNT P1-2101 AND R5-2101. REMOVED AND REPLACED CONNECTORS, OPERATES NORMAL NOW.

Part: TRANSMITTER — FAILED (RT HYD SYSTEM) · airframe 30,308 hrs · 24,217 cycles

WHEN SPOILERS DEPLOYED LOST LT HYD SYS PRESSURE. REPLACED LEFT HYDRAULIC PRESSURE TRANSMITTER.

Part: INDICATOR — DAMAGED (COCKPIT) · airframe 29,128 hrs · 23,337 cycles

IN TAKEOFF AND LANDING CONFIGURATION 2.5 UNITS OF AILERON TRIM REQUIRED TO FLY PRESSURE OFF. FOUND COCKPIT TRIM INDICATION MECHANISM DAMAGED. REPLACED TRIM INDICATION PLATE.

Part: SWITCH — LOOSE (COCKPIT)

EN ROUTE, THE FLT CREW REPORTED THEY PUSHED THE P A BUTTON ON THE OVERHEAD AND SPARKS CAME FROM THE SWITCH ASSY. CAPT RECEIVED A SHOCK. MAINTENANCE FOUND THE SWITCH ASSY LOOSE IN THE PANEL. SYSTEM CHECKED NORMAL AFTER TIGHTENING THE SWITCH ASSY.

Part: LIGHTS — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTS INOP FROM ROW 29 TO AFT OF ACFT.

Part: HYD LINE — CHAFED (NR 2 PRESS MOD)

DURING DESCENT, HYD PRESS LOW LIGHT ON FLAT PLATE DISPLAY ILLUMINATED. IMMEDIATELY LOST ALL HYDRAULIC QTY, ACCOMPLISHED PROCEDURE FOR LOSS OF RIGHT HYD SYSTEM. MANUALLY LOWERED GEAR AND LANDING WAS UNEVENTFUL.