N946DL

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,243 hrs · 54,130 cycles

ON SVC CK FOUND OVERHEAD EMERGENCY LIGHTS INOP ROW 17-21. REPLACED EMER LIGHT BATTERIES AT ROW 17 OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,199 hrs · 53,365 cycles

LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50, OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,444 hrs · 52,807 cycles

CEILING EMERGENCY LIGHTS OUT AT ROWS 23, 24, AND 25. REPLACED BATTERIES IN POWER SUPPLY AT ROW 25, SN-22718. OPS CHECK OK. REF AMM 33-53-00-401.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,528 hrs · 52,108 cycles

CEILING EMERGENCY LIGHTS OUT AT SEATS 22C, 24C, 24D, AND 25C. REPLACED BOTH BATTERIES IN POWER PACK. REF AMM 33-53-00. OPS CHECK OK. PN ON 2 AD-4002P BATTERIES.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,513 hrs · 52,096 cycles

OVERHEAD EMERGENCY LIGHTS ROW 16-19 INOPERATIVE. R & R BATTERIES IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 69,013 hrs · 51,719 cycles

VERTICAL STABILIZER HAS A CRACK ON TOP L/E. REMOVED DAMAGED SKIN BETWEEN STOP DRILLS. TRIMMED OUT DAMAGED AREA. HFEC IAW SPM 6-10-01.001. FABRICATED AND INSTALLED INTERNAL DOUBLER AND FILLER IAW PRI 544417-14, REV O. IDENTIFIED REPAIR IAW 900-5-1, NR 4. RECEIVED FINAL ER/A 544417-14, REV ORIGINAL SECT 1 C/W.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 67,829 hrs · 50,898 cycles

MAINTENANCE FOUND CATWALK MARKER FOR EMERGENCY LIGHTS INOPERATIVE. BROKEN WIRES WERE FOUND AT QUICK DISCONNECT AND RETERMINATED.

Part: FRAME — CRACKED (MLG WW) · airframe 67,798 hrs · 50,872 cycles

DURING SERVICE CHECK, FOUND T-SHAPED CRACK ON FORWARD EDGE OF GEAR OPENING RT SIDE. REPLACED FRAME FWD RT SIDE MAIN WHEEL WELL IAW DWG 5930584, OPS CHECKED, DOOR CHECKED GOOD.

Part: LANYARD — FRAYED (L1 DOOR SLIDE) · airframe 66,687 hrs · 50,045 cycles

MAINTENANCE FOUND L-1 DOOR SLIDE LANYARD FRAYED AND IN POOR CONDITION. THE L1 DOOR SLIDE WAS REPLACED.

Part: SKIN — CRACKED (BS 1338) · airframe 65,411 hrs · 49,174 cycles

CRACK DISCOVERED AT BS 1338, LONGERON 3L ON SKIN ONE INCH FWD. 0.125 INCH IN LENGTH. ACCOMPLISHED REPAIR IAW ERA 529397-14AD, REV ORIGINAL SEC I.

Part: SKIN — CRACKED (BS 1338) · airframe 65,411 hrs · 49,174 cycles

CRACK IN SKIN TWO INCHES FWD OF BS 1338, LONGERON 3L. ACCOMPLISHED REPAIR IAW ERA 529397-14AD, REV ORIGINAL SEC I.

Part: LATCH — FAILED (TAILCONE RELEASE) · airframe 65,419 hrs · 49,178 cycles

DURING THE TAILCONE RELEASE SYSTEM OPS CHECK, MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION IN THE RELEASE CABLE SYSTEM. THE TAILCONE UPPER RT LATCH PIN HUNG ON THE DROP. MAINTENANCE REPLACED THE LATCH AND CLEANED AND LUBED THE CABLE CONDUITS AND TAILCONE.

Part: STRINGER FITTING — CRACKED (BS 1338) · airframe 65,411 hrs · 49,174 cycles

FOUND STRINGER 3L END FITTING CRACKED AT BS 1338, VERIFIED WITH EDDY CURRENT. REPAIRED IAW PRI 529458-14, REV 0, BY REPLACEMENT OF END FITTING .

Part: FRAME — CRACKED (TAILCONE) · airframe 65,231 hrs · 49,022 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM ALIGNMENT PIN FRAME WAS CRACKED OUT OF ALLOWABLE LIMITS. THE CANTED FRAME WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: ANGLE — CRACKED (TAILCONE) · airframe 65,137 hrs · 48,957 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE LOCK PAD ANGLES WERE CRACKED BEYOND ALLOWABLE LIMITS. THE TAILCONE ASSEMBLY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.

Part: BAYONET — LOOSE (TAILCONE RELEASE) · airframe 65,185 hrs · 48,989 cycles

MAINTENANCE DISCOVERED THAT FOUR OF THE BAYONETS FOR THE TAILCONE RELEASE SYSTEM WERE LOOSE BEYOND ALLOWABLE LIMITS. THE BAYONETS ATTACHMENT HARDWARE WAS REMOVED, REINSTALLED, AND PROPERLY SECURED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,221 hrs · 48,283 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT ALL OF THE OVERHEAD EMERGENCY LIGHT IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN 2 OF THE POWER SUPPLIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,162 hrs · 47,572 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 22, 24, & 25 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — CORRODED (BS 647) · airframe 61,818 hrs · 46,603 cycles

CORROSION ON FUSELAGE SKIN, BS 647 BETWEEN L29-30L. REPAIRED IAW ER/A 512876-14 REV ORIG

Part: SKIN — DAMAGED (BS 1003-1022) · airframe 61,818 hrs · 46,603 cycles

LIGHTNING STRIKES ON LT WINDOW BELT FWD LOWER CORNER AND ALSO MID LOWER SECTION BETWEEN BS 1003-1022. REPAIRED IAW ER/A 512849. REV ORIGINAL.

Part: TEE FITTING — DAMAGED (BS 1338) · airframe 61,818 hrs · 46,603 cycles

DAMAGED TEE FITTING BS 1338 L29-30R AT AFT PRESSURE BULKHEAD. TEE FITTING REPLACED IAW SR09530001, REV J AND SRM 53-03, FIG 37 AND ER/A 512881-14, REV ORIG.

Part: SKIN — DAMAGED (BS 731-750) · airframe 61,818 hrs · 46,603 cycles

LIGHTNING STRIKE ON LT WINDOW BELT FWD LOWER CORNER BETWEEN BS 731-750. REPAIR ON LT WINDOW BELT FWD LOWER CORNER BETWEEN BS 731-750 WAS ACOMPLISHED WHITH 1 EXTERNAL REPAIR DOUBLER IAW ER/A 512848-14 REV ORIGINAL;

Part: SKIN — DAMAGED (BS 579-598) · airframe 61,817 hrs · 46,602 cycles

LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER BETWEEN BS 579 - 598. REPAIRED IAW ER/A 512847-14, REV ORIGINAL.

Part: FRAME — CORRODED (BS 1332) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON FRAME BS 1332 BETWEEN LONGERONS 22-24R AT AFT CARGO COMPARTMENT (C3). CORROSION WAS REMOVED AND NEW FRAME WAS INSTALLED DWG 9958238 REV CF AND SRM 51-30-2 AND SRM 51-30-5.

Part: DOUBLER — CRACKED (BS 424.625) · airframe 61,817 hrs · 46,602 cycles

CRACK ON INTERNAL DOUBLER AT BS 424.625 BETWEEN LONGERON 26-27R ON LOWER AFTER DOOR JAMB CORNER AT FWD CARGO COMPARTMENT. AREA DAMAGE WAS REMOVED AND PARTS OF REPAIR WERE TREATED AND PAINTED IAW ER/A 512878-14, REV ORIGINAL REPAIR WAS PERFORMED IAW ER/A 512878-14 AD REV ORIG. SRM 53-05, FIG 105 CONFIGURATION -7011.

Part: SKIN — CRACKED (LT WING) · airframe 61,817 hrs · 46,602 cycles

CRACK OF 0.0109" APPROX ON INTERNAL SURFACE OPEN HOLE CLOSE TO STRINGER 15, XCW=202.716 AT LT LOWER ACCESS DOOR CUT OUT. REPAIR WAS ACCOMPLISHED WITH ER/A NR 512852-14 AD REV ORIG WITH PLUG REPAIR.

Part: SEAT TRACK — CORRODED (BS 857-859) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT SEAT TRACK X=54 FROM BS 857-859 AT PAX CABIN. SEAT TRACK REPAIRED IAW SRM 53-05, FIG 4A.

Part: CUSP WEB — CORRODED (BS 595) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON MEMBRANE CUSP WEB X=50-60 BS 595. REMOVED CORROSION, REMOVED AREA OF OUT LIMITS, FABRICATE DOUBLER AND RING DOUBLERS, AND PERFORM REPAIR. CORROSION LEVEL 2.

Part: CUSP WEB — CORRODED (BS 655-666) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BS 655-666 BTW X=54 TO X=60 AT PAX CABIN. AREA DAMAGE WAS REPAIRED IAW SRM 53-05 FIG 131A-14 DUE TO AREA OUT LIMITS.

Part: SEAT TRACK — CORRODED (BS 1214-1295) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT SEAT TRACK X=54 FROM BS 1214-1295 AT PAX CABIN.

Part: SKIN — CORRODED (BS 610-628) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON INNER FUSELAGE SKIN PREVIOUS REPAIR DOUBLER BETWEEN STA Y=610 TO Y=628 LONG, 28RY AND 29 LT REF (T0 277241). REPAIR FILLER WAS REMOVED IAW SRM MD-88 51-30-5. FABRICATED AND INSTALLED, AND PROTECTED AGAINST CORROSION IAW SRM 51-10-3 PAR 14-21 AND 41. CORROSION LEVEL 2. ASSOCIATED ER/A 45-768714 ADDED FOR AC 0946.

Part: CUSP WEB — CORRODED (BS 1072-1087) · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS ON CUSP WEB UPPER/ LOWER SURFACE BETWEEN 895-900 AND 1072-1087 X=-54 TO X=-60. IN REF NRC 153 ZONE 58 AND CUSP WEB WERE REPAIRED IAW SRM 53-05, FIG 231A. CORROSION LEVEL 2.

Part: SEAT TRACK — CORRODED (BS 1174-1212) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT SEAT TRACK X=54 BETWEEN BS 1174 - 1212 AT PAX CABIN. REMOVED SEAT TRACK AND CORROSION, MEASURE DRILLED NEW SEAT TRACK IAW SRM 51-10-3 PAR 26, 21, 14, 38, 53-05, FIG 4B1 AND 51-30-2, 51-30-1.

Part: CARGO TRACK — CORRODED (BS 1117-1222) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON (LT) TIE TRACK BTW STA Y=1117-1222 AT AFT CARGO COMPARTMENT (C3) REF. NEW TIE TRACK BTW STA Y 1117-1222 WAS REPLACED IAW SRM 53-24-00 AND 51-30-1 AND 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 1322-1338) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON INTERCOSTAL FROM BS 1322 TO 1338 BETWEEN LONGERON 21 - 22L AT AFT CARGO COMPARTMENT. INTERCOSTAL REPLACED IAW DWG 5911423, REV CC AND THESE WERE DRILLED, TREATED, AND INSTALLED IAW SRM 51-30-2, 51-10-3.

Part: SKIN — CORRODED (BS 617-623) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON PREVIOUS REPAIR FILLER BS 617-623 BETWEEN L29 AND 30R CARGO COMPARTMENT INNER SKIN. DAMAGED FILLER REPLACED IAW ER/A 457687-14, REV "B" .

Part: FRAME — CORRODED (BS 1380) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON FRAME 1380 STA X=13 AND X=-13. REF. (T0 276519). FRAME TEE WAS REPLACE IAW DWG 9912246, REV DE (FRAME TEE WAS REMOVED AND NEW FRAME TEE WAS INSTALLED ) IAW SRM 51-30-2 , 51-30-5. CORROSION LEVEL 2.

Part: SUPPORT — CRACKED (BS 1117) · airframe 61,817 hrs · 46,602 cycles

CRACKED LT SLANT PANEL SUPPORT IN STA Y=1117 BETWEEN LONGS 26L AND 27L AT AFT CARGO COMPARTMENT. (C3) REF (T0 276564). SUPPORT WAS REMOVED, FABRICATED AND REPLACED IAW ER/A 413029-14 MA REV C, ASSOCIATED ER/A 41-302914 ADDED FOR AC 0946.

Part: CARGO TRACK — CORRODED (BS 1212-1287) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON THE TRACK LT SIDE FROM STA Y=1212 TO Y=1287. ALSO CRACK ON SAME LT TIE TRACK STA Y=1260 OF AFT CARGO COMPARTMENT. (C3) (MRB 53-139-05) (REF 335,ZONE 57) (T0 276485). TIE TRACK WAS REMOVED NEW TIE TRACK WAS INSTALLED IAW SRM 51-30-1.

Part: CARGO TRACK — CORRODED (BS 1212-1287) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON RT TIE TRACK FROM STA Y=1212 TO 1287 OF AFT CARGO COMPARTMENT. (C3) (MRB 53-139-05) (REF 336,ZONE 57) (T0 276486). TIE TRACK WAS REMOVED, CORROSION WAS REMOVED, MEASURED (OUT OF LIMITS) NEW TIE TRACK WAS DRILLER, TREATED AND PAINTED AND INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 693-712) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT FLOOR CUSP WEB UPPER AND LOWER SURFACE X=54 TO X=60 AT STA Y=693-712 PAX CABIN (CFS) REF. (T0 276219). REMOVE AREA DAMAGED, FABRICATED REPAIR PARTS, AND REPAIR WEB IAW SRM 53-05 FIG 31A-8. CORROSION LEVEL 2. (LP #0818374)

Part: STRAP — CORRODED (BS 1239-1309) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON STRAPS ABOVE LONGERON 23L BETWEEN BS 1239-1309, AFT CARGO COMPARTMENT. STRAPS WERE REMOVED AND INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 660-663) · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB FROM BS 660-663. DAMAGED REMOVED AND DOUBLER AND FILLER FABRICATED AND AREA WAS REPAIRED IAW SRM 51-70-4, FIG 1.

Part: CUSP WEB — CORRODED (BS 1098-1174) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON RT FLOOR CUSP WEB UPPER AND LOWER SURFACE X=-54 TO X=-60 AT STA Y=1098-1117, 1117-1120, 1136-1147, 1147-1155, 1155-1174 PAX CABIN. (CFS) (MRB 53-037-01)(REF 154, ZONE 58) (T0 276209). REMOVE CORROSION, MEASURE, REMOVE SEAT TRACK, CUSP WEB FITTINGS, CUSP WEB CLIPS, ELECTRICAL WIRE CLIPS, AND WEB, DRILL NEW WEW WEB, TREAT/PAINT, INSTALL NEW WEB, ELECTRICAL WIR CLIPS, CUSP WEB CLIPS, CUSP WEB FITTING, SEAT TRACK IAW SRM 51-30-2, 51-30-5, 51-30-1, 51-10-3 PAR 14,21,26.

Part: CUSP WEB — CORRODED (BS 1161-1174) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT CUSP WEB BETWEEN STA Y=1161-1174 AND X=44 TO X=60 AT PAX CABIN IN REF NRC (T0 276378) AND CARD 251. REF NRC NR 618, ZONE 58 (T0 277205). AREA OUT LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A-21 DUE TO AREA OUT LIMITS REF NRC 251.

Part: SHEAR TIE — CORRODED (BS 1380) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON FRAME 1380 STA X=13 AND X=-13. FRAME TEE WAS REPLACE IAW DWG 9912246, REV DE (FRAME TEE WAS REMOVED, NEW FRAME TEE WAS INSTALLED.) IAW SRM 51-30-2, 51-30-5.

Part: LONGERON — CORRODED (BS 1343-1380) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LONGERON 24L BS 1343-1380 IN AFT ACCESSORY COMPARTMENT. CORROSION WAS REMOVED, DAMAGE SECTION LONGERON WAS REMOVED AND NEW SECTION AND SPLICE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5, 53-02, FIG 18. ORIGINAL TICKNESS IS 0.080" AND MINIMUM REMAINING THICKNESS IS 0.053".

Part: CUSP WEB — CORRODED (BS 544-548) · airframe 61,817 hrs · 46,602 cycles

AD CORROSION ON LT FLOOR CUSP WEB, PREVIOUS REPAIR DOUBLER X=54 TO X=60 AT STA Y=544 TO Y=548 PAX CABIN. (CFS) (MRB 53-037-01) (REF 167 ZONE 58) (T0 276222). AREA WAS REPAIRED IAW SRM 53-05, FIG 131 (DOUBLER OF EXISTING REPAIR WAS REMOVED, PREVIOUS REPAIR DOUBLER WAS EXTENDED BECAUSE A NEW DAMAGED, DAMAGED WAS REMOVED, FABRICATED A NEW DOUBLER, NEW DOUBLER WAS INTALLED).

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,817 hrs · 46,602 cycles

CRACK ON INNER PAN OUTER SURFACE AT C-1 DOOR. PAN WAS STOP DRILLED, DOUBLER FABRICATED, AND INSTALLED IAW SRM 52-05 D, FIG 50, SRM 51-10-3 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 670-735) · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS ON LT SEAT TRACK X=22 FROM BS 670-735 PAX CABIN. IN REF NRC 130 ZONE 58 AND PLUGS WERE REPLACED IAW SRM 53-05, FIG 4A AND INSTALLED WITH 51-30-1.

Part: CUSP WEB — CORRODED (BS 218) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LOWER AND UPPER SURFACE OF RT CUSP WEB BETWEEN X=-54 TO X=-60 STA Y=218. CUSP WEB FROM STA Y=218 TO STA Y=237 WAS REPLACED IAW DWG 9930538 AND SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS IN TWO COUNTERSINKS ON FUEL ACCESS PANEL. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-A, CONDITION II. COUNTERSINKS WERE REWORKED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION OUR OF LIMITS ON THREE COUNTERSINKS ON FUEL ACCESS PANEL. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-2A CONDITION II. COUNTERSINKS WERE REWORKED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS IN FOUR COUNTERSINKS ON FUEL ACCESS PLATE. NEW BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-A CONDITION II. COUNTERSINKS WERE REWORKED.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE INNER PAN AFT SECTION AT BEAM NR 1 AND BEAM NR 5 C-3 DOOR. INNER PAN AFT SECTION AT BEAM NR 1 WAS REPAIRED IAW ER/A 461218-14. INNER PAN AFT SECTION AT BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: ACCESS PANEL — CORRODED (WING) · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS ON THREE COUNTERSINKS ON FUEL ACCESS PANEL. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-2A CONDITION II. COUNTERSINKS WERE REWORKED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS IN FOUR COUNTERSINKS ON FUEL ACCESS PLATE. NEW BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-A, CONDITION II. COUNTERSINKS WERE REWORKED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS IN TWO COUNTERSINKS ON FUEL ACCESS PANEL. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-A, CONDITION II. COUNTERSINKS WERE REWORKED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION OUT OF LIMITS ON FIVE COUNTERSINKS ON FUEL ACCESS PANEL. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 51-22-2A CONDITION II. COUNTERSINKS WERE REWORKED.

Part: LONGERON — CRACKED (BS 1418 L5L) · airframe 61,817 hrs · 46,602 cycles

CRACK ON LONGERON 5LT AT BS 1418 IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-02, FIG 18 -DAMAGE SECTION REMOVED, FABRICATED SPLICE, SPLICE AND NEW SECTION LONGERON INSTALLED.

Part: FRAME — CRACKED (BS 1322) · airframe 61,817 hrs · 46,602 cycles

CRACKED FRAME BS 1322 LONGERON 17R AT FUSELAGE INTERNAL STRUCTURE. FRAME REPAIRED IAW ER/A 493697-14MA, REV B. DAMAGED CUT OUT, FABRICATE FILLER AND DOUBLER AND INSTALLED.

Part: CUSP WEB — CORRODED (BS 541-617) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON RT FLOOR CUSP WEB UPPER AND LOWER SURFACE X=-54 TO X=-60 AT STA Y=541-552, 557-560, 563-573, 577-579, 594-598, 598-617 PAX CABIN. (CFS) (MRB 53-037-01) REF 149, ZONE 58 (T0 276204). DUE EXCESSIVE CORROSION ON CUSP WEB TO STA Y=541-552, 557-566, 563-573, 577-579, 594-598 WAS REPLACED ALL CUSP WEB (STA Y=503-598) IAW SRM 51-30-2, 51-30-1 AND 51-10-4 AND STA 598-617 WILL BE ATTENDED WITH NRC (T0 277258) AND CARD 650, ZONE 58.

Part: SEAT TRACK — CORRODED (BS 514-515) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON SEAT TRACK X=-54 STA Y=514 TO 515 IN PASSENGER CABIN. REPAIR SEAT TRACK WAS REPLACED IAW SRM 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 1053-1057) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT SEAT TRACK X=54 FROM BS 1053 AND 1057 AT PAX CABIN. REPAIRED IAW SRM 53-05, FIG 4A.

Part: FRAME — CRACKED (BS 1322) · airframe 61,817 hrs · 46,602 cycles

CRACKED FRAME STA Y=1322 LONGERON 17L AT FUSELAGE INTERNAL STRUCTURE. FRAME WAS REPAIRED IAW ERA 493697-14MA REV B. DAMAGED CUT OUT FABRICATED FILLER/DOUBLER REPAIR DOUBLER / FILLER INSTALLED.

Part: LONGERON — CORRODED (BS 1293-1326) · corrosion level 2 · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LONGERON 25L BETWEEN BS 1293-1326 AT AFT CARGO COMPARTMENT. LONGERON SECTION REPLACED IAW SRM 53-14-3, FIG 4 AND SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — DAMAGED (BS 1003-1022) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED INSPECTION, FOUND DAMAGE ON CUSP WEB BETWEEN BS 1003 AND 1022 BELOW SEAT X=-54. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 131A-4.

Part: LONGERON SPLICE — CRACKED (BS 1292-1296) · airframe 61,817 hrs · 46,602 cycles

CRACKED LONGERON SPLICE 25L BS 1292-1296, SPLICES WERE REPLACED IAW DWG 5936021, REV EH AND DWG 5936667 REV CD AND SRM 51-30-5.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED MX, EVIDENCE OF LIGHTNING STRIKE DAMAGE WAS NOTED ON LT ELEVATOR GEARED TAB T/E FROM XET=88-90. LT ELEVATOR GEARED TAB REPAIRED IAW SRM 55-04, PAR 3.

Part: FLOORBEAM — CORRODED (BS 1168) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULE MX, CORROSION WAS FOUND ON THE GIRT BAR FLOOR SUPPORT AT BS 1168 BETWEEN RBL44 TO 54. REPAIRED IAW SRM 51-10-4.

Part: TEE FITTING — CORRODED (BS 1161) · airframe 61,817 hrs · 46,602 cycles

CORROSION WAS FOUND ON TEE FITTING, BS 1161 BELOW OF LT CUSP WEB BETWEEN X=44 TO 60 AT PAX CABIN. FITTING WAS REPLACED IAW SRM 51-30-5, 51-10-3 PARA 21 & 14 AND 51-10-4.

Part: SKIN — CRACKED (BS 173) · airframe 61,817 hrs · 46,602 cycles

CRACK OF 0.046" OF LENGTH AT STA Y=173 AND BETWEEN LONG 11RT AND 12RT ON FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER AT FWD SERVICE DOOR JAMB. REPAIR ON UPPER FWD DOOR JAMB CORNER RT SIDE BETWEEN STA Y=173 AND LONG 11RT AND 12RT BY CRACK WAS ACCOMPLISHED IAW SRM 53-05; DAMAGE CUT OUT DOUBLERS FABRICATED AND REP DOUBLERS INSTALLED.

Part: CUSP WEB — CORRODED (BS 826-845) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED MX, CORRISION WAS FOUND OUT OF LIMITS ON THE LT CUSP WEB UPPER AND LOWER SURFACE AT STA Y=826-845 IN THE PASSENGER CABIN. CORROSION DAMAGE ON LT CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: LONGERON — CRACKED (BS 200 L4L) · airframe 61,817 hrs · 46,602 cycles

CRACKED LONGERON 4LT ON STA Y=200 AT PAX CABIN. REPLACED SECTION LONGERON 4LT IAW SRM 53-02, FIG 18 AND 51-30-2 & 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED MX, FUEL TANK ACCESS COVER ON THE LT WING FOUND TO BE CORRODED BEYOND ACCEPTABLE LIMITS IN THE FASTENER COUNTERSINK AREAS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED MX, FUEL TANK ACCESS COVER ON THE RT WING WERE FOUND TO BE CORRODED BEYOND ACCEPTABLE LIMITS IN THE FASTENER COUNTERSINK AREAS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: FRAME — CORRODED (BS 1271) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON FRAME BS 1271 BETWEEN LONG 29 AND 30R, IN THE AFT ACCESSORY COMPARTMENT. THE CORROSION WAS DETERMINED TO BE OUT OF LIMITS AND THE DAMAGED SECTION OF FRAME WAS REPLACED IAW SRM 53-03, FIG 2A.

Part: SKIN — CRACKED (BS 1437 L3-4R) · airframe 61,817 hrs · 46,602 cycles

CRACK ON FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3 TO 4R. SKIN REPAIRED IAW SRM 53-04, FIG 27. DAMAGE CUT OUT AND REPAIR DOUBLERS INSTALLED.

Part: LONGERON — BENT (BS 256-275) · airframe 61,817 hrs · 46,602 cycles

BENT LONGERON HAT LT BETWEEN BS 256 TO 275 AT CABIN FUSELAGE STRUCTURE. SECTION OF LONGERON WAS REPAIR AND REPLACED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,817 hrs · 46,602 cycles

CORROSION ON LT FLOOR CUSP WEB, PREVIOUS REPAIR DOUBLER X=54 TO X=60 AT STA Y=874 TO Y=881 AT PAX CABIN. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-05, FIG 131A-14.

Part: LONGERON — CRACKED (BS 541) · airframe 61,817 hrs · 46,602 cycles

DURING SCHEDULED INSPECTION, LONGERON 4 LT WAS FOUND CRACKED AT BS 541. REPAIR WAS ACCOMPLISHED IAW SRM 53-02, PARA 12 FIG 18.

Part: LONGERON — CRACKED (BS 1296) · airframe 61,817 hrs · 46,602 cycles

CRACK ON LONGERON 8LT BS 1296 AT INNER FUSELAGE STRUCTURE. LONGERON SECTION DAMAGE WAS REMOVED AND NEW LONGERON SECTION WAS INSTALLED IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 59,819 hrs · 45,181 cycles

DURING INSPECTION PER EA 09-470871-12AD, A DAMAGED HOLE WAS FOUND ON THE RT LOWER AFT PORTION OF THE REMOVABLE LEADING EDGE SKIN. THE DAMAGED HOLE IS THE 11TH HOLE UP FROM ZFS=52. A TRIM OUT REPAIR FOR THIS HOLE LOCATION IS NOT ALLOWED PER SG09550004 REV. B.

Part: SILL — CORRODED (BS 1155) · airframe 1 hrs · 1 cycles

AFT CARGO DOOR SILL HAS CORROSION AT BS 1155 FORWARD CORNER. REPLACED CORNER FITTING AND REMOVED ADDITIONAL CORROSION IN AREA PER SRM 51-30-05 WITHIN LIMITS.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

TOP GUSSET AT STATION 1218 BETWEEN L29 TO L30 IS CORRODED. ON NON-ROUTINE 180 ON 25APR2012.

Part: FITTING — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

ON APRIL 25TH THE SHEAR CLIP AT STATION 1212 BETWEEN L29 AND L39 WERE CORRODED. AFT CARGO COMPARTMENT. PART WAS REPLACED.

Part: CONNECTOR — CORRODED (TAILCONE) · airframe 59,819 hrs · 45,181 cycles

TAIL CONE LOCK ANNUNCIATION SWITCH BACKSHELL CORRODED. DEPOSITS AFT OF T-PIN LOCATION. FOUND ON INITIAL INSPECTION ON PSVT CHECK IN MSP WHILE PERFORMING TAIL CONE DROP TEST. REF NON-ROUTINE #195.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

CUSP MEMBRANE AT L1 DOORWAY CORRODED AT STA 180 TO STA 190 APPROX LBL 56, REPAIRED PER ERA 502645-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

FWD LEFT DOOR FLOOR SUPPORT AT STATION-200 IS CORRODED. ON 22APR2012 PART WAS REPLACED PER SRM 53-01.

Part: FLOOR SUPPORT — CORRODED (BS 200 LBL 54) · airframe 59,819 hrs · 45,181 cycles

FLOOR SUPPORT AT STA 200 LBL 54 CORRODED. REPAIRED BY REPLACEMENT OF NEW PART SRM 53-01.

Part: BEAM — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

CORROSION AFT CARGO BEAM L28R MULTIPLE AREAS, C3 BEAM, REPAIRED PER MD88 SRM 53-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

CORROSION SPOTS ON LBL 44.5 AFT CABIN AREA, FRAME 1098, REPLACED SECTION OF SEAT TRACK FROM STA 1068 TO STA 1127 SPLICE TO SPLICE PER MD88 SRM 53-05 FIG 4.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

CORROSION ON FWD AND AFT DOOR THRESHOLD CORNER SUPPORTS C3.21APR12. REMOVED AND REPLACED SUPPORTS PER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

FWD CABIN FLOOR STRUCTURE CORROSION ON SEAT TRACK, STA 145.5 TO STA 255, LBL 44. REPLACED SEAT TRACK SECTION TO FACTORY SPLICE STA 196 TO STA 304 PER MD88 SRM 53-05 AND MD88 DWG 5930547.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,819 hrs · 45,181 cycles

WEB CRACKED AT BS 37 RADOME ALIGNMENT PIN 7:30 POSITION, CRACKED 6 INCHES OTBD OF LT HOLD OPEN ROD LWR FITTING. REPAIRED PER ERA 502910-14 BY INSTALLATION OF FORMER REPAIR.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 59,819 hrs · 45,181 cycles

WHILE IN MSP FOR PSV AND DURING INSPECTION PER EA 09-470871-12AD A DAMAGED HOLE WAS FOUND ON THE RT LOWER AFT PORTION OF THE REMOVABLE LEADING EDGE SKIN. THE DAMAGED HOLE IS THE 11TH HOLE UP FROM ZFS=52. A TRIMOUT REPAIR FOR THIS HOLE LOCATION IS NOT ALLOWED PER SG90550004 REV "B". REPAIR ACCOMPLISHED PER ER/A 502550-14AD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,661 hrs · 45,068 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.

Part: SLIDE — MALFUNCTIONED (TAILCONE) · airframe 59,605 hrs · 45,031 cycles

THE EMERGENCY EVACUATION SLIDE LOCATED IN THE TAIL CONE DID NOT DEPLOY WHEN TESTED. THE SLIDE PACK WAS REPLACED AND THE AIRCRAFT RETURNED TO REVENUE SERVICE. P/N 259001305 S/N 0369.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 59,347 hrs · 44,880 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 22 IN THE CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: FRAME — CRACKED (LT MLG WW) · airframe 58,446 hrs · 44,284 cycles

FOUND CRACK IN LEFT MAIN WHEEL WELL FORWARD FRAME OUTBOARD EDGE. REPLACED FRAME PER BAC DWG 5930584 457226 PERFORMED OPERATIONAL CHECK OF GEAR DOOR OPEN SWITCH IAW MD-88 AMM 32-60.

Part: WIRE — BROKEN (CABIN) · airframe 57,380 hrs · 43,495 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT INOPERATIVE AT ROW 13D. FOUND WIRE BROKEN ON LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATION CHECKS GOOD.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 56,594 hrs · 42,958 cycles

DURING LINE CHECK, MX FOUND L-1 DOOR SLIDE AND BUSTLE LOOSE FROM DOOR. MX VISUALLY INSPECTED SLIDE. FOUND IT OK FOR CONTINUED SERVICE. REINSTALLED SLIDE AND GIRT BAR D-RING.

Part: PIN — BROKEN (WIRE HARNESS) · airframe 54,599 hrs · 40,747 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY FLOOR LIGHT AT36DE INOPERATIVE. MAINTENANCE REPLACED BROKEN PIN IN HARNESS. OPERATION OF LIGHT NOW CHECKS OK. (2010-D1254) (DLM88102863).

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 55,240 hrs · 42,054 cycles

MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT WIRE ON THE OVERWING EMERGENCY DOOR SEAT TO BE SHORTED. MAINTENANCE REWIRED THE LIGHT. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INDICATOR — STUCK (ENGINE EPR) · airframe 54,945 hrs · 41,843 cycles

FLIGHT CREW ABORTED TAKE-OFF AT 60 KNOTS DUE TO NR 1. ENGINE EPR INDICATION STUCK. CREW TAXIED CLEAR OF RUNWAY, PLACED NR 1 EPR SYS ON MCO AND FLIGHT DEPARTED. MX LATER R & R THE EPR TRANSMITTER AND SNUBBER. THE MCO WAS REMOVED.

Part: LIGHT — BROKEN (SEAT 13E) · airframe 54,654 hrs · 41,651 cycles

MX FOUND THE EMERGENCY LIGHT AT SEAT 13E TO BE BROKEN. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS GOOD AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 53,842 hrs · 41,123 cycles

EMERGENCY FLOOR LIGHTING INOP. RE-TERMINATED WIRING AT SEAT 18CD AND 23CD UNDER SEAT. CONNECTOR FOR SEAT LIGHTS - OPS CHECKS GOOD.

Part: SKIN — BULGED (FUSELAGE) · airframe 53,174 hrs · 40,675 cycles

TEMP REPAIR PER ERA 476571-14 REV A, SKIN CORRODED BULGED STATION 564.

Part: ENGINE — POWER LOSS (NR 1) · airframe 50,247 hrs · 38,726 cycles

AT CRUISE HAD LT ENG EPR 1.40 AND RT ENG EPR 1.88 WITH BOTH N1'S AT 75. COULD ONLY CLIMB AT 500 FPM AT 300 KIAS. PRESSURE CHECKED PT2 AND PT7 LINES NR 1 AND NR 2 ENGS. FOUND P FLEX LINE THRU PYLON LEAKING ON NR 2 ENG. REPLACED LINE. PUM EPR SYSTEM UP WITH TEST BOX PER M/M. ALL TEST CHECK GOOD. RAN ENG PER M/M. ALL CKS GOOD.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 47,666 hrs · 36,999 cycles

RUSTED HI-LOCK AT STA Y=351, LONGERON 4 RT. FASTENER REPLACED IAW SRM 51-30-5 NR T0056459.

Part: STRUCTURE — CORRODED (BS 275) · airframe 47,661 hrs · 36,995 cycles

CORROSION AT STA Y=275 BETWEEN LONGERONS 3 RT AND 6 LT. REPAIRED IAW SRM 51-30-5 NR T0056455.

Part: STRUCTURE — CORRODED (BS 1271) · airframe 47,655 hrs · 36,989 cycles

CORROSION AT STA Y=1271 LONGERONS 9 RT, 5 RT, 3 RT, 2 RT, 4 LT, AND 5 LT. REPAIRED IAW SRM 51-30-5 NR T0056452.

Part: STRUCTURE — CORRODED (BS 1287) · airframe 47,648 hrs · 36,982 cycles

CORROSION AT STA Y=1287, LONGERONS 5-4 RT. REPAIRED IAW SRM 51-30-5 NR T0056451.

Part: STRUCTURE — CORRODED (BS 1193) · airframe 47,642 hrs · 36,977 cycles

CORROSION AT STA 1193 AND LONGERON 26 LT. REPAIRED IAW SRM 51-30-5 NR T0056323.

Part: ATTACH FITTING — BROKEN (BS 237) · airframe 47,642 hrs · 36,977 cycles

BROKEN INTERCOSTAL ATTACH FITTING AT BS 237 BETWEEN LONGERONS 27 LT AND 28 LT. REPLACED INTERCOSTAL CLIP IAW DWG 9915554 NR T0056349.

Part: SEAT TRACK — CORRODED (BS 220-226.) · airframe 47,642 hrs · 36,977 cycles

CORROSION ON SEAT TRACK X=44 BETWEEN STA Y=220 TO 226. SEAT TRACK SECTION BETWEEN STA 200 TO 303 REPLACED WITH REPAIR SPLICE AT STA 303 IAW SRM 53-05 FIG 4F VIEW A.

Part: INTERCOSTAL — CRACKED (BS 788) · airframe 47,642 hrs · 36,977 cycles

CRACK ON INTERCOSTAL OF FLOOR SUPPORT AT STA Y=788 X=0. INTERCOSTAL FABRICATED AND REPLACED IAW SRM 51-70-5 NR T0056354.

Part: WEB — CRACKED (BS 1485) · airframe 47,634 hrs · 36,971 cycles

CRACK ON WEB AT STA Y=1485 CANT AT 10:00 POSITION NRT0057036 WEB REPAIRED IAW SRM 53-01.

Part: SKIN — CORRODED (BS 293-299 L21R) · airframe 47,634 hrs · 36,971 cycles

CORRODED LOCK FASTENERS ON FUSELAGE SKIN STA 293-299 LONGERON 21 RT. REPLACED HI-LOCKS IAW SRM 51-30-5 NR T0056012.

Part: FLOOR SUPPORT — CRACKED (BS 864) · airframe 47,634 hrs · 36,971 cycles

CRACK ON FLOOR SUPPORT AT STA Y=864 X=-1. SUPPORT REPLACED IAW SRM 51-30-2 NRT0056134.

Part: SUPPORT — CRACKED (RT MLG WW) · airframe 47,627 hrs · 36,966 cycles

CRACK ON RT HYD REFILL FILTER BRACKET IN RT MLG WW. SUPPORT REPLACED IAW EA 09-076074-03 ME02 OPN 0203 NR T0056109.

Part: COVER — CRACKED (CREW CABIN) · airframe 47,627 hrs · 36,966 cycles

CRACK ON RT COVER NEXT TO CONNECTION JACK HEAD SET BOOM AND MICROPHONE IN CREW CABIN. REPAIRED DAMAGE IAW MM25-00-00-801 NR T0056117.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 47,627 hrs · 36,966 cycles

PNS-ATL FLT 467 SHORTLY AFTER T/O, A HOT OVEN/BURNING SMELL FLT 1238 BY CP AND CABIN CREW. IT DISSIPATED W/IN FEW MINUTES. FLT 1238 ATL-SRQ HAPPEN 2ND TIME ODOR WAS STRONGER AND LASTED LONGER. SUSPECTED POSSIBLE BIRD INGESTION. FLT 930 SRQ-ATL, STRONG ELECTRICAL SMELL ON DESCENT. F/A'S SAID SMELLED LIKE SULFUR OR MATCH ODOR VERY STRONG IN COCKPIT. MTC IS IN PROGRESS DNTC. INSPECTED APU INLET AND BOTH ENGINE INTAKES NO TROUBLE FOUND RAN PACKS USING APU AND ENGINES NO SMELL OBSERVED REPLACED AND RT COALESCER BAGS REMOVED BURNT DEBRIS FROM F/C OVEN.

Part: WEB — CRACKED (BS 1474-1485) · airframe 47,627 hrs · 36,966 cycles

CRACKED LT UPPER WEB BETWEEN STA 1474-1485 AT AFT ACCESSORY COMPARTMENT. WEB FABRICATED AND INSTALLED IAW DOUGLAS DRAWING 9923630 NR T0057063.

Part: WEB — CRACKED (BS 1474-1485) · airframe 47,627 hrs · 36,966 cycles

CRACKED UPPER WEB BETWEEN STA 1474 TO 1485 AT AFT ACCESSORY COMPARTMENT. REFABRICATED NEW WEB IAW SRM 53-34-0 FIG 7. WEB INSTALLED IAW SRM 51-30-2 AND SRM 53-34-0 FIG 7 NR T0057062.

Part: CUSP WEB — CORRODED (BS 984-1003) · airframe 47,627 hrs · 36,966 cycles

PITTING CORROSION ON LEFT CUSP WEB BETWEEN STA 984 TO 1003. LEFT CUSP WEB BETWEEN STA 984 T0 1003 REPLACED IAW DWG 9930612 NR T0057018.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 47,627 hrs · 36,966 cycles

CRACK IN FWD SECTION OF MID CARGO COMPARTMENT DOOR AREA OF LOCK PINS. CRACK STOP DRILLED. NO CRASKS FOUND PAST STOP DRILL IAW NDT SPM 06-10-01-001. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 52-05 FIG 26A NR T0057058.

Part: ANGLE — CRACKED (RT MLG DOOR) · airframe 47,627 hrs · 36,966 cycles

CRACK ON ANGLE AT RT MLG DOOR FWD OUTBD. SECTION CHANNEL TRIMMED IAW SRM 52-05D FIG 811D. EDDY CURRENT INSP FOUND NO CRACKS IAW NDT SPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR IAW SRM 52-05D FIG 811D NR T0057071.

Part: SUPPORT — CRACKED (BS 826) · airframe 47,627 hrs · 36,966 cycles

CRACK ON STANDARD ELECTRONIC LOWER SUPPORT AT STA Y=826 LT SIDE. HFEC PERFORMED IAW NDT SPM 06-10-01-001. NO CRACKS FOUND. SUPPORT REINSTALLED IAW SRM 51-30-2 NR T0056355.

Part: STEP — CRACKED (BS 1497-1510) · airframe 47,627 hrs · 36,966 cycles

CRACKS ON RT UTILITY STEP BETWEEN STA 1497 CANTED AND 1510 CANTED. CRACKS STOPPED PER SRM 53-01 FIG 2 SHEET 4. DOUBLER FABRICATED REF SRM 53-01 FIG 2. DOUBLER AND SUPPORT INSTALLED REF SRM 51-30-2 NR T0056531.

Part: SKIN — CORRODED (BS 457-476) · airframe 47,627 hrs · 36,966 cycles

CORRODED LOCK FASTENERS ON FUSELAGE SKIN DOUBLER STA 457-476, LONGERONS 23-25 RT. FASTENERS REPLACED IAW SRM 51-30-5 NR T0056026.

Part: LONGERON — CRACKED (BS 208 L11L) · airframe 47,624 hrs · 36,963 cycles

CRACK ON SPLICE AT STA Y=208, LONGERON 11 LT. REPLACED DOUBLER IAW SRM 53-01 FIG 2 NR T0056782.

Part: SKIN — CRACKED (BS 1437 L4-5R) · airframe 47,624 hrs · 36,963 cycles

CRACK ON FUSELAGE SKIN AT STA 1437 BETWEEN LONGERONS 4 RT AND 5 RT. EDDY CURRENT INSPECTION PERFORMED ON SKIN. NO CRACKS WERE FOUND ACCORDING TO NDT SRM 06-10-01-001 NR T0056624.

Part: SKIN — CORRODED (BS 1400-1426) · airframe 47,624 hrs · 36,963 cycles

CORROSION ON FUSELAGE SKIN STA 1400-1426 LONGERON 2 RT. SKIN REPAIRED IAW SRM 51-30-5 NR T0056167.

Part: SKIN — CRACKED (BS 1309 L6-7R) · airframe 47,624 hrs · 36,963 cycles

CRACK ON FUSELAGE SKIN AT STA 1309 BETWEEN LONGERONS 6 RT AND 7 RT. DOUBLER REPLACED IAW SRM 53-04D FIG 31 NR T0056620.

Part: LONGERON — CRACKED (STA 160 L25L) · airframe 47,624 hrs · 36,963 cycles

CRACK ON LONGERON 25 LT AT STA 160. INSTALLED NEW SECTION OF LONGERON IAW SRM 53-02 FIG 18.

Part: ACCESS PANEL — CORRODED (VERTICAL STAB) · airframe 47,624 hrs · 36,963 cycles

CORROSION ON ACCESS 6301A VERTICAL STAB L/E. REPAIRED IAW SRM 51-30-1, NR T0056168.

Part: STRUCTURE — CORRODED (BS 1174) · airframe 47,618 hrs · 36,958 cycles

CORROSION AT STA 1174 AND LONGERONS 26 LT T0 24 LT. REPAIRED IAW SRM 51-30-3 NR T0056322.

Part: SKIN — CORRODED (BS 870-879) · airframe 47,618 hrs · 36,958 cycles

CORROSION ON DOUBLER REPAIR STA 870-879 LONGERONS 3-5 RT. REPAIRED IAW SRM 51-30-5 NR T0056174.

Part: SKIN — CRACKED (BS 1319) · airframe 47,618 hrs · 36,958 cycles

TEMPORARY REPAIR INSTALLED ON FUSELUGE SKIN AT STA 1319 BETWEEN LONGERONS 22 AND 23 RIGHT. INSTALLED PERM REPAIR PER SRM 53-04D ON N/R T0056053,HMV/GDL.

Part: SKIN — CRACKED (LT WING) · airframe 47,618 hrs · 36,958 cycles

CRACK ON LT WING FIXED TRAILING EDGE UPPER SKIN. PERM REPAIR INSTALLED PER SRM 57-03D FIG 802D ON N/R T0056674, HMV/GDL.

Part: LONGERON — CRACKED (BS 160 L4L) · airframe 47,618 hrs · 36,958 cycles

CRACK ON LONGERON 4 LT STA Y=160. FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-02 FIG 18.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 47,618 hrs · 36,958 cycles

CORROSION ON FED UPPER CORNER OF C2 DOOR JAMB. REPAIRED IAW SRM 51-30-2 NR T0056177.

Part: STRUCTURE — CORRODED (BS 997) · airframe 47,618 hrs · 36,958 cycles

CORROSION ON RT WW AFT EDGE STA Y=997, X=-25. REPAIRED IAW DWG 5962021 NR T0056306.

Part: SPLICE — CRACKED (BS 990) · airframe 47,618 hrs · 36,958 cycles

FOUND CRACK ON UNION SPLICE AT STA Y=990 X=-6. ANGLE REMOVED, FABRICATED AND INSTALLED IAW DWG 5936395 NR T0056307.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,618 hrs · 36,958 cycles

GENERAL SURFACE CORROSION ON C1 LOWER DOOR JAMB. CORROSION REMOVED, SURFACE THICKNESS WITHIN LIMITS. TREATED AND PAINTED IAW SRM 51-10-3D NR T0056370.

Part: SUPPORT — CRACKED (BS 788) · airframe 47,618 hrs · 36,958 cycles

CRACK ON RT SIDE WALL PANEL SUPPORT AT STA Y=788. STIFFENER REMOVED, FABRICATED AND INSTALLED IAW SRM 53-24-0DNR T0056353.

Part: SUPPORT — CRACKED (BS 525 L24L) · airframe 47,616 hrs · 36,957 cycles

CRACK ON LT SIDE WALL PANEL STRUCTURE AT STA Y=525 AND LONG 24LT. SUPPORT REMOVED, FABRICATED AND INSTALLED IAW SRM 53-24-0D NR T0056350.

Part: STRUCTURE — CORRODED (BS 256) · airframe 47,616 hrs · 36,957 cycles

CORROSION AT STA Y=256 LONGERON 2 RT. REPAIRED IAW SRM 51-30-5 NR T0056453.

Part: CUSP WEB — CORRODED (BS 1136-1174) · airframe 47,616 hrs · 36,957 cycles

EXFOLATION CORROSION ON CUSP WEB BETWEEN STA Y=1136 AND STA Y=1174 TASK CARD 58-53313. REPAIRED DOUBLER IAW SRM 53-05D FIG 835D.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 47,616 hrs · 36,957 cycles

CORROSION ON LEFT TRAPEZOIDAL ANGLE AT FWD UPPER L MLG WW CORNER. NEW ANGLE FABRICATED AND INSTALLED IAW DOUGLAS DRAWING 5935852 N/R T0056098.

Part: FRAME — CRACKED (BS 1446) · airframe 47,616 hrs · 36,957 cycles

REPAIR 3 CRACKS ON CANTED FRAME OUTER CAP. LEFT SIDE 2 CRACKS OF 1/2" LONG AND 1.125" LONG AT L-4L AND ONE 1/2" CRACK AT L-3L. INSTALLED NEW FRAME IAW SRM 53-03D FIG 30.

Part: ANGLE — CRACKED (RT MLG DOOR) · airframe 47,616 hrs · 36,957 cycles

FOUND CRACK ON ANGLE AT R MLG DOOR FWD JAMB. NEW ANGLE FABRICATED AND INSTALLED IAW SRM52-05D FIG 811D.

Part: SKIN — CRACKED (BS 1437) · airframe 47,616 hrs · 36,957 cycles

CRACK ON FUSELAGE SKIN AT STA Y=1437 BETWEEN LONGERONS 4 AND 5 LT. INSTALLED PERM REPAIR IAW 53-04D FIG 27 ON N/R TOO57038, HMV/GDL.

Part: SKIN — CRACKED (BS 1309) · airframe 47,616 hrs · 36,957 cycles

CRACK ON FUSELAGE SKIN AT STA 1309 BETWEEN LONGERONS 6 AND 7 LT. PERMANENT REPAIR INSTALLED PER SRM 53-04D FIG 32, ON N/R TOO56614-HMV-3/GDL.

Part: VANE — DENTED (RT WING) · airframe 47,616 hrs · 36,957 cycles

DENT ON MID GUIDE VANE OF RIGHT OUTBD FLAP. MID GUIDE VANE WAS REPAIRED IAW SRM 57-03D PARA 8 FIG 9A ON N/R T0056900.

Part: SKIN — CRACKED (BS 1437) · airframe 47,616 hrs · 36,957 cycles

FOUND CRACK ON FUSELAGE SKIN AT Y-1427 BETWEEN LONGERON 4 LT AND 5 LT. DAMAGE WAS REPAIRED AS PERMANENT FOLLOWING ALL INSTRUCTIONS AND RECOMMENDATIONS ON SRM 53-04D FIG 27 ON NR CARD T005703B.

Part: SKIN — CRACKED (BS 1474) · airframe 47,616 hrs · 36,957 cycles

TRANS FROM OMI/CMI C/N C02247494 DUE AT HMV SRM 53-04D FIG 12B PERM REPAIR TO 2EA CRACKS IN EMPENNAGE AT STA 1474 12 INCHES LT OF AIRSTAIR CUTOUT. PERM REPAIR ACCOMPLISHED PER SRM 53-04D FIG 12B.

Part: RIB — BROKEN (LT WING) · airframe 47,616 hrs · 36,957 cycles

BROKEN RIB IN LT FIXED L/E AT STA XFS=218. RIB REMOVED IAW SRM 51-30-2. RIB AND DOUBLER INSTALLED IAW SRM 51-06B FIG 17 N/R T0056247.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,616 hrs · 36,957 cycles

FOUND CORROSION ON SEAT TRACK X = -54 AT STATIONS Y=271, 307, 326, 344, 364, 381, 416, 430, 448, 465, 470, 481, 498, 515, 531, 547, AND 564. DAMAGE AT STATIONS ABOVE WAS REMOVED IAW SRM 53-05D FIG 4A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,616 hrs · 36,957 cycles

EXFOLIATION CORROSION ON FUSELAGE SKIN AT FWD JACK POINT. REMOVED CORROSION IAW SRM 51-10-3D. SKIN THICKNESS WITHIN LIMITS REF SRM 53-01 FIG 1 N/R CARD T0056045.

Part: CUSP WEB — CORRODED (BS 737) · airframe 47,616 hrs · 36,957 cycles

EXFOLIATION CORROSION ON RT CUSP WEB AT STA Y=737 ON UPPER AND LOWER SURFACE. DOUBLER REPAIRED AND INSTALLED PER ERA 398191-14MA REV A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,616 hrs · 36,957 cycles

CRACK ON DOOR JAMB IN AFT EXTERNAL A/C SERVICE PANEL AT AFT OUTBD CORNER. FABRICATED AND INSTALLED DOUBLER REF SRM.

Part: DOOR FRAME — CRACKED (L MLG DOOR) · airframe 47,616 hrs · 36,957 cycles

CRACK ON LEFT MLG DOOR JAMB AT FWD OUTER SIDE. DOOR JAMB REPLACED IAW DRAWING 5930584 N/R T0056090.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 47,616 hrs · 36,957 cycles

LT MAIN LANDING GEAR DOOR INNER AND OUTER SKINS CRACKED. CRACKS STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED.

Part: CUSP WEB — CORRODED (BS 1221-1231) · airframe 47,613 hrs · 36,956 cycles

EXFOLIATION CORROSION ON RIGHT CUSP WEB BETWEEN STA Y=1221 AND Y=1231 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A.

Part: DOOR — DAMAGED (MLG) · airframe 47,613 hrs · 36,956 cycles

THE LT MLG DOOR HAD A DAMAGED REPAIR. THE OLD REPAIR WAS REPAIRED WITH A STOP DRILLED AND DOUBLERS ON THE INNER AND OUTER SKIN.

Part: CUSP WEB — CORRODED (BS 589) · airframe 47,613 hrs · 36,956 cycles

EXFOLIATION CORROSION ON RIGHT CUSP WEB AT SAT Y=589 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A.

Part: SKIN — DAMAGED (RT TE FLAP) · airframe 47,613 hrs · 36,956 cycles

THE RHS INBOARD FLAP REMOVALBE PANEL LOWER SKIN REQUIRED A SKIN SPLICE PER 461910-14.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 47,613 hrs · 36,956 cycles

DURING CURRENT HMV, TWO DELAMINATED AREAS WERE FOUND ON LHS ELEVATOR ANTI FLOAT TAB BETWEEN 202 AND 216.5. AREA WAS REPAIRED PER BOEING INSTRUCTIONS AS CONTAINED IN 461319-14.

Part: CUSP WEB — CORRODED (BS 542) · airframe 47,613 hrs · 36,956 cycles

CORROSION ON LEFT CUSP WEB AT STA Y=542 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A.

Part: CUSP WEB — CORRODED (BS 864-886) · airframe 47,613 hrs · 36,956 cycles

CORROSION ON LEFT CUSP WEB BETWEEN STA Y=864 AND Y=886 (TASK CARD 58-53313). REPAIRED PER ERA 398191-14MA REV A. NRC T0056688

Part: VANE — DELAMINATED (TE FLAPS) · airframe 47,613 hrs · 36,956 cycles

INAPPROPRIATE REPAIR AND DELAMINATION WERE REPAIRED TO A LT WING OUTBD FLAP CENTER FIXED GUIDE VANE, NEAR THE INBD END. REPAIR INCLUDED A 16" WIDE SKIN SPLICE, AND A SECOND 11" WIDE DOUBLER. THE REPAIR IS PERMANENT.

Part: ATTACH FITTING — CORRODED (MLG) · airframe 47,613 hrs · 36,956 cycles

WING MLG ATTACH FTGS, SIDE SUPPORT FITTINGS. CORROSION FOUND IN THE HOLE BORE AND COUNTER BORE. CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED.

Part: ANGLE — CORRODED (PRESSURE BLKHEAD) · airframe 47,613 hrs · 36,956 cycles

AFT BULKHEAD INTERNAL ANGLE BETWEEN L28L AND L28R CORRODED. PART REPLACED.

Part: SKIN PANEL — CRACKED (HORIZONTAL STAB) · airframe 47,534 hrs · 36,900 cycles

FOUND CRACK, HORIZONTAL STAB UPPER SKIN SPLICE, RT.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,233 hrs · 36,671 cycles

HORIZONTAL STAB RT UPPER AFT SKIN, INBD AFT EDGE HAS CRACK REPAIR. THE UPPER AFT SKIN OF THE RT HORIZONTAL STAB WAS FOUND WITH A 1.25" CRACK AT THE INBD, AFT EDGE OF THE PANEL. THE CRACK WAS HFEC INSPECTED AND STOP DRILLED ON A TIME-LIMITED BASIS. THE PERMANENT REPAIR IS A REPLACEMENT OF THE SKIN PANEL. THE REPAIR WAS ACCOMPLISHED PER ER/A 460229-14.

Part: SKIN — CORRODED (FS 617 L29-30R) · airframe 46,205 hrs · 35,939 cycles

THE FUSELAGE SKIN IS CORRODED BETWEEN L29R AND L30R AT FS 617. THE FUSELAGE SKIN CORROSION WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: CYLINDER — FAILED (NLG) · airframe 39,812 hrs · 31,371 cycles

NOSE GEAR DID NOT EXTEND DURING NORMAL EXTENSION. REPLACED NOSE GEAR BUNGEE CYLINDER.

Part: WIRE — SHORTED (YAW DAMPER) · airframe 39,415 hrs · 31,102 cycles

CLIMBING THRU 11,500 ACCELERATING THRU 280 KTS THE DFG SW A C/B POPPED. A/P AND A/T DISSENGAGED. A/T ALERT WINDOW BLANK, YAW DAMP OFF MSG, MACH TRIM INOP MSG AND NOTICEABLE YAW. FOUND WIRE 1C610X20RD SHORTED TO GROUND AT TOP OF VERTICAL STAB. REPAIRED WIRING RAN NR 1 AND NR 2 A/P RTS ALL CHECKS GOOD. CB DFGS SWITCH A DOES NOT POP.

Part: BRAKE — SEIZED (NR 2 MAIN) · airframe 38,818 hrs · 30,708 cycles

GROUND ABORT NR 2 BRAKE LOCKED UP DURING TAXI. REPLACED NR 2 ASSY PER M/M. ALSO REPLACED NR 2 WHEEL ASSY PER M/M.

Part: DISPLAY — FAILED (WX RADAR SYS) · airframe 36,352 hrs · 28,995 cycles

AFTER TAKEOFF FROM ATLANTA WEATHER RADAR DISPLAY BECAME DISTORTED AND FAILED SHORTLY AFTER. SMOKE APPEARED FROM RADAR UNIT. CIRCUIT BREAKERS FOR RECEIVER AND INDICATOR PULLED. SMOKE DISSIPATED.AFTER TROUBLESHOOTING, FOUND INDICATOR AT FAULT. REPLACED INDICATOR SYSTEM OPS CHECK NORMAL.

Part: HOSE — TORN (RT PACK) · airframe 36,271 hrs · 28,937 cycles

TAIL COMPARTMENT TEMP HIGH LITE ILLUMINATED WHILE PASSING FL250 ON CLIMBOUT. POM PROCEDURES C/W. LEFT THROTTLE AT IDLE IN LITE EXTINGUISHING FOR APPROX. 5 MINUTES, THEN REILLUMINTED. LITE WENT OUT AT 12000 MSL FOR DURATION. RIGHT PACK UNABLE TO MAINTAIN PRESSURIZATION. ENGINE AND AIRFOIL ANTIICE NOT USED ANY TIME. FOUND BOT BLOWN ON RT TEMP CONROL SYSTEM. REPLACED BOOT AND SECURED DUCT. PRESSURIZED A/C. NO LEAKS. RAN ENG AT IDLE AND T/O.NO LEAKS. OK FOR SERVICE.

Part: TARGET — BROKEN (LT GEAR DOOR) · airframe 33,755 hrs · 27,095 cycles

ON APPROACH TO ATL GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS DOWN AND LOCKED. REPLACED LEFT GEAR DOOR PROX TARGET

Part: FAN — SEIZED (CARGO BAY) · airframe 30,365 hrs · 24,608 cycles

ON DEPARTURE FROM KLIT, FLT ATTENDANT INFORMED CREW OF A MOLDY/SULFUR TYPE SMELL IN THE AFT CABIN. THE SMELL QUICKLY WENT AWAY. PASSED THRU A RAIN SHOWER AT THE TIME. ALL COCKPIT INDICATIONS WERE NORMAL. FOUND RECIRC FAN FROZEN. REPLACED SAME, CKS GOOD.

Part: SERVO — FAILED (AILERON)

DESCENDING FROM FL 350 TO FL 280 THE A/P TRIPPED OFF THE A/C WOULD NOT TURN TO THE RIGHT.(YOKE WOULD NOT GO PAST NUETRAL, LEFT TURN OK, A/C WOULD TURN RIGHT WITH RUDDER AND AILERON TRIM. AT APPROXIMATELY 18,000 FT THE CONTROLS BECAME EFFECTIVE. PRESSING THE A/P DISCONNECT BUTTON DID NOT ELIMINATE THE PROBLEM. FOUND THE AILERON SERVO MODEL FAILURE ON THE DFGC FLIGHT FAULT REVEIW. REPLACED SAME RTS PASSES ON BOTH DFGC. INSPECTED AILERON CABLES AND PULLEYS AND ADJUSTED CABLE TENSION.

Part: SWITCH — FAILED (NLG)

NOSE GEAR LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. NO RE-INDICATION, AND COCKPIT NOSE GEAR PIN EXTENDED. LIGHTS TESTED NORMALLY. NOSE GEAR LIGHT ILLUMINATED ON TAXI IN. REPLACED NOSE GEAR DOWN SWITCH S1-412.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, FOUND F/C EMERGENCY SEAT TRACK LIGHTING INOP. REPLACED BATTERY PACK DELTA (P/N 337101963) (S/N 72125) OFF, (S/N 65889) ON. TRACK LIGHTING OPS CHECK GOOD.

Part: B-NUT — LOOSE (LT TR CTL VALVE)

LEFT HYD PRESS LOW LIGHT ANNUC 10 MINUTES FROM LANDING. LT ENGINE HYD PUMP OFF. AUX AND XFER PUMP ON PER POM. PRESS NORMAL BUT QTY STILL DECREASING. FOUND LEAK AT B-NUT AT LT T/R CONT VLV TIGHTENED.

Part: BALLAST — FAILED (CABIN)

STRONG ODOR ASSOCIATED W/ PACKS TURNED ON. REPLACED LIGHT BALLAST AT SEAT 14DE.

Part: PROXIMITY BOX — MALFUNCTIONED (RT MLG)

AFTER T/O, PIT GEAR DOOR LIGHT STAYED ON AND RIGHT MLG IND UNSAFE LIGHT ON WITH VIBRATION. INSP ALL GEAR, PROX SWS, LATCH MECHANISMS, JACKED A/C, CYCLED GEAR AND ALL INDS NORM. REPLACED PROX BOX DUE TO HISTORY.

Part: DFGC — FAILED (E/E COMP)

DURING T/O ROLL, LOST ALL FLT GUID DISPLAY, NR 1 PFD F/D WITH FAIL LIGHTS .A/T KICKED OFF MACH TRIM, YAW DAMP AND WINDSHEAR INOP LIGHTS ILLUM ON AOP. NO C/BS POPPED, REJECTED T/O AT 120 KTS 35 DEG F, AT CVG 890MSL. MAX BRK TEMP OF 285, NO OVHT BRK LIGHT. REPLACED NR 1 DFGC, RAN RTS CKTS GOOD.

Part: DE-ICE FLUID — OVER FILLED (AIR FOIL DE-ICE)

LIGHT SMOKE IN CABIN WHEN AIRFOIL DE-ICE SELECTED. FOUND RES OVER FILLED BOTTLES FULL, HYD FLUID LEAKING INTO KEEL BEAM AREA THEN ON SKIN INTO APU INTAKE. CLEANED BOTTLES, RAN AC SYSTEM AND NO SMOKE NOTED.

Part: SKIN — DENTED (BS 256)

THE FUSELAGE SKIN AT STA 256 BETWEEN STR 19L AND 20L WAS FOUND DENTED. THE DENT IS 6 INCH BY 6 INCH BY .25 DEEP AND DOES NOT AFFECT THE UNDERLYING STRUCTURE. THE DENT WILL BE TRIMMED OUT AND REPAIRED IN ACCORDANCE WITH ERA 266789-14.

Part: SKIN — CRACKED (C-1 DOOR CUTOUT)

DURING C-2 CHECK, THE FUSELAGE SKIN AT THE AFT EDGE OF THE C-1 DOOR WAS FOUND WITH AN EXISTING STOP DRILL HOLE. HOLE WAS TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED.

Part: AHARS — FAILED (LT/RT COCKPIT)

IN FLIGHT BOTH CAPTS AND F/O COMPASSES TUMBLE. AIRCRAFT RETURNED TO DFW. REPLACED BOTH AHARS UNITS AND SYS OPNS NORMAL.