N985DL

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 70,984 hrs · 51,396 cycles

AFT LAV SMOKE DETECTER RT GOING OFF. AFT RT LAV SMOKE DETECTOR NOT TESTING REPLACED SAME OPS NORMAL. (LP4822100)

Part: FAIRING — MISSING (TE FLAP) · airframe 70,904 hrs · 51,323 cycles

LEFT WING NR 2 FLAP SECONDARY INB FAIRING MISSING. LT WING NR 2 FLAP SECONDARY INB FAIRING FWD TO CDL 57-50-03. REPORTED DUE TO POSSIBILITY THAT PART MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP5352438)

Part: INSTRUMENT PANEL — UNSECURE (COCKPIT) · airframe 70,728 hrs · 51,169 cycles

REJECTED TAKEOFF AT 100KNTS DUE TO COPILOTS INSTRUMENT PANEL COMING OUT. MAINTENANCE SECURED PANEL AND PERFORMED A HIGH ENERGY STOP INSPECTION. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 70,550 hrs · 51,014 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 31 AFT. AFTER TESTING FROM AFT BATTERY PACK, ALL LIGHTS OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,497 hrs · 50,965 cycles

DURING SVC CK, FOUND CEILING EMERGENCY LIGHTS OUT AT ROWS 16-20. REMOVED AND REPLACED BATTERY PACK AT ROW 17DC PER AMM 33-53. LIGHTS CK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 70,497 hrs · 50,965 cycles

DURING SVC CK, FOUND SEAT 14 AISLE EMERGENCY LIGHT OUT. FOUND LOOSE CONNECTOR UNDER SEAT. RESECURED CONNECTOR. CKS GOOD.

Part: LUG — CRACKED (HORIZ STAB) · airframe 69,553 hrs · 50,224 cycles

HORIZONTAL STABILIZER JACKSCREW ACTUATOR GEAR BOX, LEFT ATTACH POINT TO HORIZONTAL STAB, AFT LUG IS CRACKED. COMPLETED JACKSCREW ASSY INSTALLATION AND OP'S CHECK PER 2742-4540 AND AMM 27-40-01.

Part: NUT PLATE — BROKEN (VERTICAL STAB) · airframe 69,553 hrs · 50,224 cycles

VERTICAL STABILIZER TIP, HORSESHOE ANGLE (AROUND TOP OF THS JACKSCREW MOTOR) FOR TOP CAP ATTACHMENT, MISSING/BROKEN NUTPLATES AT BOTH AFT ENDS. INSTALLED NUT PLATES REF SRM 51-30-02.

Part: LAMP — INOPERATIVE (EMERENCY LIGHTS) · airframe 69,099 hrs · 49,902 cycles

SEAT 31ED EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-00, OPS CHECKED GOOD.

Part: SKIN PANEL — CRACKED (RT HORIZ STAB) · airframe 67,764 hrs · 48,854 cycles

LFEC INSPECTION OF HORIZONTAL STABILIZER RT UPPER CENTER SKIN PANEL PER STEP 5. OF WORKCARD SHOWS A CRACK INDICATION FROM AFT EDGE OF SKIN FORWARD APPROXIMATELY 1" IN LENGTH. REPAIRED PER ERA 559453-14AD.

Part: CABLE — WORN (TAILCONE RELEASE) · airframe 67,764 hrs · 48,854 cycles

UPPER LEFT TAILCONE LATCH RELEASE CABLE IS WORN. REPLACED CABLE ASSY IAW AMM 20-10-17.

Part: CONNECTOR — DAMAGED (ANTI SKID SYSTEM) · airframe 67,357 hrs · 48,555 cycles

LEFT INBOARD AND LEFT OUTBOARD ANTI-SKID AMBER MESSAGES INFLIGHT. CREW DECLARED EMERGENCY. FOUND CONNECTOR TO P1-1148 WITH PUSHED PINS. REPLACED THE CONNECTOR AND SYSTEM CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,205 hrs · 48,443 cycles

FOUND LEFT AND RIGHTT BS 875 OVERWING FWD EMERGENCY EXIT LIGHTS OUT. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53. OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 66,837 hrs · 48,169 cycles

AT ALTITUDE 310, FLIGHT ATTENDANTS REPORTED A STRONG ELECTRICAL ODOR FROM FORWARD PART OF FIRST CLASS. TURNED OFF SIDE PANEL LIGHTS AND ODOR DISSAPATED AFTER 5-10 MINS. COMPLIED WITH JIC 2120-2367 THROUGH STEP 6. COMPLETED DUCT BURNOUT . NO ODOR PRESENT. APU AND ENGINES CLEAN. RAN ENGINES TO TAKE OFF POWER AND NO ODOR PRESENT.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 66,424 hrs · 47,905 cycles

DURING TAILCONE CHECK, FOUND FOUR TAILCONE RECEPTICALS WORN AND LOOSE. REMOVED AND REPLACED THE RECEPITCALS IAW SRM 51-30-02.

Part: RECEPTACLE — LACK OF LUBE (TAILCONE) · airframe 66,424 hrs · 47,905 cycles

DURING TAILCONE FUNCTIONAL CHECK, THE TAILCONE DID NOT DROP PROPERLY WITH AFT CABIN DOOR OPENED IN THE ARMED POSITION. FOUND RECEPTICALS DRY WITH LITTLE LUBE. CLEANED AND LUBED RECEPTICALS. PERFORMED SUCCESSFUL TEST OF AFT CABIN DOOR PER AMDS 5350-010077-0101. (LP2774959)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,287 hrs · 47,812 cycles

EMERGENCY LIGHT AISLE (13D) INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50. OPS CK OK.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 65,824 hrs · 47,481 cycles

L2 SLIDE BOTTLE PRESSURE LOW. R & R L2 SLIDE AMDS CARD 2561-4002, MPN D29985-103, SN OFF 0980. ALL RII STEPS HAVE BEEN ACCOMPLISH IAW AMDS 2561-4002.

Part: WIRE — DAMAGED (CABIN) · airframe 65,486 hrs · 47,240 cycles

SEAT 12E EMERGENCY LIGHT INOPERATIVE. REPAIRED SEAT FRAME WIRING. OPS CKS GOOD. REF SWPM 20-10.

Part: TRIM TAB — DAMAGED (RT ELEVATOR) · airframe 64,723 hrs · 46,712 cycles

LIGHTNING STRIKE DAMAGE TO RT OTBD ELEVATOR TRIM TAB. ANTI-FLOAT TAB REPLACED ON AMDS WC 2730-4382.

Part: FLOOR PANEL — PUNCTURED (AFT CARGO BAY) · airframe 63,548 hrs · 45,894 cycles

A PUNCTURE IN AFT CARGO BAY FLOOR JUST FWD OF DOOR. INSTALLED A REPAIR IAW SRM 53-05.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 62,718 hrs · 45,314 cycles

MISSING REPAIR BUSHING ON CUTOUT FUEL ACCESS RT WING. BUSHING AND CUTOUT ACCESS PANEL WAS REPAIR IAW ETI-88-15-186, REV 1, ER/A 534394-14 REV ORIGINAL.

Part: ACCESS PANEL — DAMAGED (LT WING) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON PREVIOUS REPAIR BUSHINGS AT LT WING SETTLEMENT AREA OF ACCESS PANEL 1357C. ACCESS PANEL WAS REPAIRED.

Part: BEARING — DAMAGED (RT MLG ACTUATOR) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION AND SCRATCHES ON RT MLG ACTUATOR SUPPORT FITTING BUSHING AND BEARINGS. ACTUATOR SUPPORT FITTING BUSHING AND BEARING ON RT MLG WERE R & R UNDER CARD 10, ZONE 18 AND CARD 5740-01139-04B. RII COMPLETED.

Part: BUSHING — DAMAGED (LT MLG ACTUATOR) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION AND SCRATCHES ON LT MLG ACTUATOR SUPPORT FITTING BUSHING AND BEARING. ACTUATOR SUPPORT FITTING BUSHING AND BEARING ON LT MLG INSTALLED UNDER CARD 5740-01139-04A, JOB 089-0001 AND CMM 20-10-7. BEARING AND BUSHING WERE REPLACED ON CARD 11, A/C ZONE 17 AND CARD 5740-01139-04A. RII WAS COMPLETED.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION WAS FOUND ON THE LT MLG ACTUATOR SUPPORT FITTING BEARING BORE. THE AREA WAS REPAIRED IAW ER/A 534421-14AD REV ORIGINAL AND A NEW BEARING WAS REPLACED.

Part: LONGERON — CORRODED (BS 1338) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON LONGERON 22L BS 1338 IN AFT CARGO BAY. REPLACED THE LONGERON IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON COUNTERSINK SETTLEMENT AREA AND UPPER SURFACE ON FUEL ACCESS PANEL 1409C ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: INTERCOSTAL — CORRODED (BS 769-788) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON INTERCOSTAL STA Y=769-788 BETWEEN LONGERONS 27-28RT. THE INTERCOSTAL WAS REPLACED IAW DWG 9915554, REV J, SRM 51-10-4, 51-30-1, 51-30-2, 51-30-5, AND 51-10-3 PAR 14-21.

Part: BEAM — CORRODED (BS 644-671) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON LOWER FWD FLANGE BS 652-671 AND VERTICAL FACE BS 644 AT MID CARGO COMPARTMENT DOOR FRAME BEAM REF ORNRC 154 ZONE 100 MRB 53-018-02, CARD 219, ZONE 100. MID CARGO DOOR JAMB BEAM WAS REPAIRED IAW SRM 53-05, FIG 123A, OPTION 2 AND ER/A 534411-14 REV. ORIGINAL. RII COMPLETED BY INSPECTION STAMP: HAG, LIC: 200802796 TECHOPS. ID 870444, ASSOCIATED ER/A 00-534411, ADDED FOR AC 0985. LP 1986715.

Part: LONGERON — CORRODED (BS 1136-1250) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON LONGERON 23L BETWEEN BS 1136 - 1250. THE LONGERON WAS REPLACED IAW SRM 53-01 FIG 18 51-30-2, 51-30-5, AND 51-10-3, PAR 38.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON BARREL NUT HOLE NR 13 AT LT HORIZONTAL STABILIZER STA XH=6.625. DAMAGE ON BARREL NUT HOLE WAS REPAIRED IAW ETI-88-15-173, REV 1 AND ER/A 534422-14, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1003) · airframe 62,718 hrs · 45,314 cycles

CRACK ON LONGERON 20L BS 1003. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 22, 51-30-3, 51-10-3 PAR 14, 21, 38.

Part: TAB — DENTED (RT ELEVATOR) · airframe 62,718 hrs · 45,314 cycles

DENT ON ANTI-FLOAT TAB UPPER SURFACE AT RT ELEVATOR. ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-04 PAR 2.

Part: SHEAR TIE — CRACKED (BS 1437) · airframe 62,718 hrs · 45,314 cycles

SHEAR TIE BS 1437 BETWEEN LONGERONS 16 - 17R IS CRACKED. THE SHEAR TIE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1466C AT RT WING. CORROSION WAS REMOVED IAW SRM 51-22-2A AND COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.660" AND MAX DIAMETER MEASURED IS 0.670" IN 3 ADJACENT HOLES THEREFORE OUT OF LIMITS IAW SRM 51-22-2A AND WAS REPLACED.

Part: INTERCOSTAL — CRACKED (NLG WW) · airframe 62,718 hrs · 45,314 cycles

CRACKED INTERCOSTAL Y=37 AND X=11, X=-11 AT NLG WHEEL WELL. LT INTERCOSTAL WAS REPAIRED IAW 51-01, PAR 4, STEP 21 AND DOUBLER WAS FABRICATED IAW SRM 53-14-1, 51-10-2, DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21/14.

Part: LONGERON — CRACKED (BS 1003) · airframe 62,718 hrs · 45,314 cycles

CRACK ON LONGERON 20R BS 1003. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 22, 51-30-5, 51-10-3 PAR 14,21,38.

Part: SHEAR TIE — CRACKED (BS 1446) · airframe 62,718 hrs · 45,314 cycles

SHEAR TIE ON BS 1446 LONGERONS 17 - 18L IS CRACKED. THE SHEAR TIE WAS REPLACED IAW SRM 53-14-4, FIG. 3.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,718 hrs · 45,314 cycles

CRACKED LONGERON 16L, BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4, FIG 4 AND DWG 5910228, REV KF AND SRM 51-30-5.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,720 hrs · 45,315 cycles

DAMAGE ON FERRUL AND PUNCTURE ON PAX CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201 AND INSTALLED IAW AMM 53-20-01-201.

Part: SKIN — DAMAGED (BS 237) · airframe 62,718 hrs · 45,314 cycles

PERFORM REPAIR ON FUSELAGE SKIN Y=237 BETWEEN. LONGERONS 18-20L, REF MON 88, CARD 220 ZONE 00. PERMANENT REPAIR WAS PERFORMED IAW SRM 53-04-5, FIG 3, CLASS I AND UNDER MONITOR NR 88. PERFORM DECAL INSPECTION ON PREVIOUS REPAIR AT EVERY "C" CHECK IAW TOPP 30-10-70, PAGE 13. RII COMPLETED. MONITORED ASSY A/C: Y ENG POS: APU: LRU: 88-2000-9-0001, SER: 00985, LP 1984967.

Part: FRAME — CRACKED (BS 1485) · airframe 62,718 hrs · 45,314 cycles

CRACKED FRAME BS 1485. REPAIRED IAW SRM 53-03, PAR 38, FIG 43.

Part: INTERCOSTAL — CRACKED (BS 1338) · airframe 62,718 hrs · 45,314 cycles

CRACKED INTERCOSTAL ON BS 1338 LONGERON 3R, AFT FACE. REPAIRED THE INTERCOSTAL IAW SRM 53-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 1460C AT RT WING, CARD 205, ZONE 00. CORROSION ON ACCESS DOOR 1460C WAS REMOVED IAW SRM 51-10-03 AND COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER MEASURED IS 0.578", 6 HOLES THERFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A AND WAS REPLACED AND WILL BE INSTALLED.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 TO X=-60, BS 579- 598. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-5, AND 51-10-3 PARR 14 , 21. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PARR 5, FIG 3, SHT 1, 2. AND FOUND OUT OF LIMITS IAW ER/A 511165-14 REV C.

Part: LONGERON — CRACKED (BS 1309) · airframe 62,718 hrs · 45,314 cycles

CRACK ON LONGERON 8 BS 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18 AND SRM 51-10-3 PAR 14, 21 SRM 51-30-2, SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,718 hrs · 45,314 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 1311C AT LT WING. REPLACED THE ACCESS PANEL.

Part: CUSP WEB — CORRODED (BS 984-1003) · corrosion level 2 · airframe 62,720 hrs · 45,315 cycles

CORROSION ON DOUBLER OF REPARATION ON CUSP WEB BETWEEN STA Y=984 TO Y=1003 AND X=-54 TO X=-60, RT SIDE. CUSP WEB WAS REPLACED IAW SRM 53-05 , 51-30-2, 51-30-5 AND 51-10-3 PAR 14 , 21.

Part: CUSP WEB — CRACKED (BS 800-807) · airframe 62,718 hrs · 45,314 cycles

CRACKED LT CUSP WEB BETWEEN X= 54-60, BS 800-807. CUSP WEB REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 62,718 hrs · 45,314 cycles

DAMAGED METALLIZED FABRIC SKIN ON LT & RT SIDE OF RUDDER CONTROL TAB. RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1A PAR 23. CLASSIFIED AS A MAJOR REPAIR.

Part: TAB — DAMAGED (RUDDER) · airframe 62,718 hrs · 45,314 cycles

DAMAGED RUDDER CONTROL TAB UPPER SECTION. RUDDER TAB WAS REPAIRED IAW SRM 51-70-1A, PAR 23 AMD 51-90-0 PAR 8K.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,718 hrs · 45,314 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1335C AT LT WING. REPLACED THE ACCESS PANEL.

Part: FLOOR SUPPORT — CRACKED (BS 1271-1307) · airframe 62,718 hrs · 45,314 cycles

CRACKED INTERCOSTAL ON X=0 BETWEEN BS 1307 AND 1287 AND CRACKED X=3 BETWEEN BS 1287 AND 1271. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PAR 14,21 AND AMM 20-30-01, AND SECOND CRACK REPAIRED IAW SRM 51-30-2, 51-01 PAR 4, STEP 21, 9, 51-01 PAR 4B, 53-01, FIG 2.

Part: SKIN — DAMAGED (BS 229-262) · airframe 62,718 hrs · 45,314 cycles

WAVENING ON OTBD FUSELAGE SKIN BETWEEN BS 229 TO 262, LONGERONS 16 - 18L. FUSELAGE SKIN WAS REPLACED IAW SRM 53-04, FIG 12C AND SRM 51-10-3, PAR 14, 21 AND SRM 51-30-2 AND 51-30-5.

Part: DOOR FRAME — CORRODED (BS 1350) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON VENTRAL DOOR FRAME BS 1350 BETWEEN X=18 TO X=-18. THE VENTRAL DOOR JAMB WAS REPAIRED IAW SRM 53-05, FIG 34.

Part: CUSP WEB — CORRODED (BS 1202-1207) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT CUSP WEB, X 54 TO X 60 AND BS 1202 -1207. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG.131A-7, 51-10-3 PAR 14, 21, AND 51-30-1, 51-30-5.

Part: DOUBLER — CORRODED (SERVICE PANEL) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON PRODUCTION DOUBLER AT AFT LAVATORY SERVICE PANEL. THE DOUBLER WAS REPAIRED IAW ER/A 534417-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1410C, ON RT WING. ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,718 hrs · 45,314 cycles

CRACKED LONGERON 1 ON BS 1437. LONGERON SECTION REPLACED IAW SRM 53-14-4 AND 53-02, FIG 18 AND 51-10-3, PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,718 hrs · 45,314 cycles

CORROSION FOUND ON FOUR COUNTERSINK HOLES OF FUEL ACCESS PANEL 1456C ON RT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A.

Part: INTERCOSTAL — CRACKED (FUELAGE) · airframe 62,718 hrs · 45,314 cycles

CRACKED AFT INTERCOSTAL BETWEEN PAN AND BEAM 1 AT L1 DOOR. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON THE LT CUSP WEB X 44 TO X 54, BS 1155 - 1174 . REPAIRED IAW SRM 53-05-FIG. 131A-1, 51-30-2, 51-30-5, AND 51-10-3 PARS 14, 21, AND 38.

Part: CUSP WEB — CORRODED (BS 995-999) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

LEFT CUSP WEB X 54-60 , 995-999, THE CORROSION WAS REMOVED IAW SRM 53-05 FIG 131A-2, SRM 51-10-3 PAR 21 AND 14, AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 1022-1041) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT CUSP WEB BS 1022 - 1041, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 51-10-3 PAR 14, 21, 51-30-2, 53-05 FIG 131A-7, 51-30-1, 51-30-3 PAR 38.

Part: CUSP WEB — CORRODED (BS 1090-1098) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT CUSP WEB BS 1090 - 1098, X 54 TO X 60. REPAIRED IAW SRM 51-30-5 AND 51-30-2

Part: INTERCOSTAL — CORRODED (BS 1136-1155) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

SURFACE CORROSION ON INTERCOSTAL, LONGERON 29L, BS 1136 - 1155. THE INTERCOSTAL WAS REPLACED IAW SRM 53-14-3 TYPE E2 FIG 3A AND 51-10-2.

Part: SEAT TRACK — CORRODED (BS 1231-1235) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT SEAT TRACK X 22, BS 1231 - 1235. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, 51- 10-4, 51-30-1, 51-30-5, AND 51-10-3 PAR 14 AND 21.

Part: DOUBLER — CORRODED (BS 826-845) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON DOUBLER BS 826 - 845, X -54 TO X -60. REMOVED CORROSION IAW 51-10-3 PAR 26, AND A NEW DOUBLER FABRICATED IAW 51-10-2, DRAWING PL9910151.

Part: CUSP WEB — CORRODED (BS 890-1008) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT CUSP WEB, BS 890 - 1008, X 54 TO X 60. THE AREA WAS REPAIRED IAW SRM 53-05 FIG. 131A-21 FIG. 131A-10 AND SRM 51-10-3 PAR 14, 21, 38, AND SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORRODED COUNTERSINKS ON THE FUEL ACCESS PANEL 1478C FOR RT WING. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1454C ON RT WING. THE CORROSION WAS REMOVED IAW SRM 51-103 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 1142) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON PREVIOUS REPAIR OF THE CUSP WEB, BS 1142, X 54 AND X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-1, SRM 51-10-3 PAR 21, 14, AND SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 769-788) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORRODED REPAIR ON CUSP WEB BS 769 - 788, X -54 TO X -60. THE REPAIR WAS REPLACED IAW SRM 51-30-2 AND 53-05 FIGURE 131A.

Part: CUSP WEB — CORRODED (BS 912-940) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BS 912 - 940, X -54 AND X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131 A.

Part: SEAT TRACK — CORRODED (BS 934-937) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT SEAT TRACK X 22 BS 934 - 937. REPAIRED IAW SRM 53-05 FIG 4A SHEET 1, SRM 51-10-3 PAR 14-21, AND SRM 51-10-4.

Part: CUSP WEB — CORRODED (BS 850) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BS 850, X -54 AND X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 1261-1264) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION OUT OF LIMITS ON THE RT CUSP WEB BS 1261-1264, X -54 AND X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-13.

Part: CUSP WEB — CORRODED (BS 655-674) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB, X -54 TO X -60, BS 655 - 674. THE AREA WAS REPAIRED IAW SRM 53-05 FIG 131A-1 SHEET, 51-10-3 PAR 14, 21, 51-30-2, AND 51-30-8.

Part: CUSP WEB — CORRODED (BS 545) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT CUSP WEB BS 545 BETWEEN X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-13, 53-30-5, AND 51-10-3 PAR. 21 AND 14.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,718 hrs · 45,314 cycles

DAMAGED METALLYZED ON RT SIDE BETWEEN LOWER EDGE TO ZR 32, ZR 42- ZR 93 AND ZR 108- ZR 159 ALSO LT SIDE BETWEEN ZR 45-ZR 52 AND ZR 104-ZR 108 AT RUDDER, CARD 47, ZONE 65, METALLIZED ON RT SIDE AND LT WERE REPAIRED IAW SRM 51-70-1A, PARR 23 AND OPN 1031, A/C 0985 CARD 2000-8149-07, CREW 02 JOB 000-0059. RII COMPLETED. LP 1973694.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1357C ON LT WING. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A AND THE ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 1223-1228) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION OUT OF LIMITS ON CUSP WEB BS 1223 TO 1228, X -54 AND X -60. THE DAMAGE WAS REMOVED AND A REPAIR FABRICATED IAW SRM 53-05 FIG-131A -3. THE REPAIR WAS INSTALLED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1355C ON THE LT WING. THE CORROSION WAS REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1363C ON LT WING. CORROSION WAS REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A AND THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINKS OF FUEL ACCESS PANEL 1464C ON THE RT WING. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF ACCESS PANEL1436C ON THE RT WING. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 564) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BS 564 BETWEEN X -54 TO X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-13.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACED IAW SRM 51-30-2; 51-30-5, 51-10-3 PAR 14, 21, AND DWG 9957828 REV AB.

Part: CUSP WEB — DAMAGED (BS 1199-1206) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CUSP WEB BETWEEN BS 1199 AND 1206 X -54 TO X -60 DAMAGED. THE DAMAGE WAS REMOVED IAW SRM 53-05 FIG 131A-1 AND A REPAIR WAS FABRICATED, TREATED, AND PAINTED IAW SRM 51-10-3 PAR-21 AND 14, AND INSTALLED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 598-655) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BETWEEN X -54 TO X -60 AT BS 598 - 617, 617 - 636, AND 636 - 655. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-13.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON FRAME BS 1380 BETWEEN LONGERONS 24R TO 24L. THE FRAME WAS REPLACED IAW DWG 9912246 REV. DE, SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BETWEEN X -54 TO X -60 AND BS 465 - 484. THE AREA WAS REPAIRED IAW SRM 53-05 FIG 131A-14, 51-30-01, AND 51-10-3 PARR 14-21.

Part: CUSP WEB — CORRODED (BS 1024) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BS 1024 BETWEEN X -54 AND X -60. THE DAMAGE WAS REMOVE IAW SRM 53-05 FIG. 131A-8, A NEW DOUBLER WAS FABRICATED IAW SRM 53-05 FIG-131A-8. REPAIR WAS INSTALLED IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1060-1064) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON LT SEAT TRACK X 54 BETWEEN BS 1060 TO 1064. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4A.

Part: CUSP WEB — CORRODED (BS 1144-1163) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB BS 1144, 1163 BETWEEN X -54 AND X -60. THE DAMAGE WAS REMOVED, A REPAIR WAS FABRICATED IAW SRM 53-05 FIG-131A-3. THE REPAIR WAS INSTALLED IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 522) · airframe 62,718 hrs · 45,314 cycles

CRACKED LONGERON 4R AT BS 522. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: WEB — CORRODED (BS 693-712) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON THE LT WEB UPPER AND LOWER SURFACE BETWEEN X 59 ADN X 60 BS 693 - 712. THE WEB WAS REPAIRED IAW SRM 53-05 FIG. 13A, 51-10-3, 51-30-2.

Part: DOUBLER — CORRODED (BS 655-845) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON DOUBLER REPAIR ON LT CUSP WEB BETWEEN X 54 AND X 60 BS 655 - 660, 834 - 845. REPAIR DOUBLERS WERE REMOVED IAW SRM 51-30-2 AND 51-30-5. THE DOUBLERS WERE FABRICATED IAW SRM 53-05 FIG. 131. THE DOUBLERS WERE TREATED, PAINTED, AND INSTALLED IAW SRM 51-10-3 PAR. 14 AND 21, 51-30-2, 51-20-5.

Part: LONGERON — CRACKED (BS 541) · airframe 62,718 hrs · 45,314 cycles

CRACKED LONGERON 4L AT BS 541. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1361C AT LT WING. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A AND ACCESS DOOR WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 484-503) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON PREVIOUS REPAIR OF CUSP WEB AT BS 484 - 503 BETWEEN X -54 TO X -60. THE REPAIR WAS REPLACED IAW SRM 53-05 , 51-10-3, 51-30-2, AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 313-332) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON CUSP WEB BETWEEN BS 313 TO 332 AND X 54 TO X 60. REPAIRED IAW SRM 53-05 FIG 131-A-13.

Part: STRUCTURE — CORRODED (DOOR) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RUB STRIP SETTLEMENT AREA AT LT MLG OUTBOARD DOOR. FIXED DOOR WAS REMOVED IAW AMM 32-12-21-201. AREA WAS BLENDED, UT WAS ACCOMPLISHED,FOUND OUT OF LIMITS. REPLACED IAW SRM 51-10-03, 52-10, AND NDT SPM 04-00-07.

Part: STRUCTURE — CORRODED (RT MLG DOOR) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RUB STRIP SETTLEMENT AREA AT RT MLG OUTBOARD DOOR. THE DOOR WAS REMOVED IAW AMM 32-12-21 201. AREAS WAS BLENDED (UT) WAS ACCOMPLISHED, FOUND OUT OF LIMITS. THE DOOR WAS REPLACED IAW SRM 51-10-03, 52-01, AND NDT SPM 04-00-07.

Part: DOUBLER — CORRODED (BS 807-845) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR DOUBLER BS 807 - 845 BETWEEN X -54 AND X -60. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05 FIG 131A-14 SRM 51-10-4 SRM 51-10-3 PAR. 14, 21, 38, SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 275-294) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON CUSP WEB BETWEEN BS 275 TO 294 AND X 54 TO X 60 BOTH SURFACE LT SIDE. AREA WAS REPAIRED IAW SRM 53-05 FIG. 131A-13 AND SRM 51-10-3 PAR. 14, 21 SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 332-351) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON DOUBLER OF REPARATION ON CUSP WEB AND ANGLE BETWEEN BS 332 - 351 AND X 54 TO X 60 LT SIDE. DOUBLER WAS REPLACED IAW SRM 53-05 FIG. 131A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 66,344 hrs · 47,850 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1470C ON RT WING. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 62,085 hrs · 44,882 cycles

MAINTENANCE FOUND EMERGENCY LIGHT INOPERATIVE AT 22D. MAINTENANCE REPLACED THE SEAT WIRE HARNESS IAW AMM 33-53. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,264 hrs · 44,335 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,904 hrs · 42,786 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT THE DOOR IN THE FIRST CLASS CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,904 hrs · 42,786 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT THE DOOR IN THE AFT CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,178 hrs · 42,246 cycles

DURING ROUTINE LINE INSPECTION, THE COCKPIT AND GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE FORWARD EMERGENCY LIGHT BATTERY PACK WAS REPLACED IAW AMM 33-53 AND OPS THEN CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,807 hrs · 41,984 cycles

DURING LINE CHECK, MX FOUND THAT SEVERAL OF THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE CABIN, INOPERATIVE. MX REPLACED BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: SLIDE — INOPERATIVE (SERVICE DOOR) · airframe 56,933 hrs · 41,423 cycles

MX FOUND THE FORWARD SERVICE DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE DEFLATED (PRESSURE INDICATION WAS IN THE RED BAND). THE COMPLETE FORWARD DOOR SLIDE ASSY WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 56,199 hrs · 40,918 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-33 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE SEAT WIRE HARNESS.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 55,414 hrs · 40,389 cycles

DURING PSV, FOUND CORROSION ON AFT CARGO DOOR SILL BEAM. REMOVED AND REPLACED BEAM PER SRM 51-01.

Part: SUPPORT — CORRODED (BS 1212 RBL 27) · airframe 55,414 hrs · 40,389 cycles

AFT CORNER SUPPORT IS CORRODED AT BS 1212 RBL 27. REPLACED IAW SRM 53-01.

Part: BRACKET — CORRODED (BS 1212 RBL 27) · airframe 55,414 hrs · 40,389 cycles

C-3 CORNER BRACKET AT STA 1212 RT L-27 CORRODED. REPAIRED BY REPLACEMENT OF PART P/N NR 5936469-1.

Part: SUPPORT — CORRODED (BS 1155 RBL 27) · airframe 55,414 hrs · 40,389 cycles

FORWARD CORNER SUPPORT CORRODED BS 1155 C-3 CARGO DOORWAY AREA. REPLACED83.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 54,882 hrs · 40,047 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SPAR — CRACKED (WING) · airframe 52,171 hrs · 38,328 cycles

WING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 51,233 hrs · 37,740 cycles

FLIGHT CREW RETURNED THE ACFT TO DEPARTURE JUST AFTER TAKEOFF DUE TO SMOKE IN THE COCKPIT AND A HAZE IN THE AFT CABIN. MX FOUND BIRD REMAINS IN THE NR 1 ENG INLET. BOROSCOPE OF NR 1 ENGINE REVEALED BIRD REMAINS BACK TO THE 7TH STAGE BUT NO DAMAGE. DUCT BURN OUT PROCEDURES, OPS 5089, WERE ACCOMPLISHED. THE ACFT HAS RETURNED TO SERVICE.

Part: MODULE — MALFUNCTIONED (ANTI SKID SYS) · airframe 50,214 hrs · 37,051 cycles

LT AND RT OTBD ANTISKID MSG ILLUMINATED ON APPROACH. UNABLE TO FIX INFLT, DIVERTED. T/S IAW AMM - R & R ANTISKID MODULE IAW AMM - TEST OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,706 hrs · 36,734 cycles

EMERGENCY SEAT LIGHT OUT AT SEATS 10 - 12, 14 AND 31. RELAMPED 10-12 CK NORMAL. REPLACED LIGHT ASSY AT 14 AND 31. ALL CK NORMAL IAW AMM.

Part: TIRE — WORN (NOSE WHEEL) · airframe 48,823 hrs · 36,200 cycles

ACFT PULLED TO RT DURING TO ROLL. ENGINES SPOOLED EVENLY- LOW SPEED ABORT AT APPROX 15KTS - RETURNED TO GATE. INSPECTED NOSE GEAR AND SPRAY DEFLECTOR AND TESTED STEERING AT GATE. NO TROUBLE FOUND, REMOVED AND REPLACED LT AND RT NOSE TIRES IAW AMM 32-40-02-201. FLT CREW PERFORMED TAXI CK AND STEERING WAS REPORTED NORMAL- NO PULLING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 48,777 hrs · 36,164 cycles

DENT IN FUSELAGE SKIN AFT OF L1 DOOR ABOVE CUSP LINE. REPAIRED SKIN PER SRM 53-04D FIG 12B.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,777 hrs · 36,164 cycles

FUSELAGE SKIN AT STA 237 2 INCHES ABOVE LONGERON 18L EXISTING REPAIR IS DENTED. REPAIRED SKIN PER SRM 53-04D FIG 12C WITH NEW SKIN SECTION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,777 hrs · 36,164 cycles

FWD CARGO STA 364-370 INTERCOSTAL CORRODED. REPAIRED BY REPLACING INTERCOSTAL PER SRM 51-30-02 & 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

MAIN CABIN MAIN FRAME STA 886 CRACKED ON LT SIDE. REMOVED AND REPLACED MAIN FRAME AT STA 886 PER EA09-460094-12AD REV A.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

FRAME CORRODED AT STA 1308 ABOVE LONGERON 30 FRAME. REPAIRED PER SRM 53-05D FIG 5 AT LONGERON 30.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

FUSELAGE SKIN DENTED AT STA 237 ABOVE LONGERON 18L. REPAIRED PER SRM 53-04D FIG 12C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

AFT ACCESSORY STA 1463 CANTED FRAME L-3-L Z ANGLE HAS CRACK. REMOVED DAMAGED ANGLE, REPAIRED ANGLE IAW MD80 SRM 51-70-5 FIG 1. RE-INSTALLED ANGLE.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

MAIN CABIN STA 1174 TO 1193 LT CUSP WEB HAS CORROSION AND CRACKED APPROX 1 INCH. REMOVED CORROSION FROM CUSP WEB (WITHIN LIMITS IAW MD 80 SRM 53-01). REPAIRED CRACKED AREA AT STA 1174 LT SIDE BL-53 IAW MD80 SRM 53-05D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

FWD CARGO STA 364 TO 370 RBL 3 INTERCOSTAL HAS CORROSION AT MATING SURFACE.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

MAIN PAX CABIN LT SIDE CUSP WEB HAS CORROSION AT AFT OF BS 665, LBL 54 (CPCP 46-53304). REMOVED CORROSION THAT WAS OUT OF LIMITS, .010 MATERIAL LOSS. REMOVED DAMAGED SECTION OF CUSP WEB. REPAIRED IAW MD80 SRM 53-05D FIG 827D.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

AFT ACCESSORY STA 1463 SRT 3R TO 7R AFT SIDE OF CANTED FRAME 3 EA ATTACHED ANGLES CRACKED. REPLACED ANGLES PER SRM 51-30-5.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 48,772 hrs · 36,161 cycles

COCKPIT FLOOR PANEL CRACKED NR 4415B. INSTALLED REPAIR PER SRM 53-01 FIG 2 AND DWG PL9957802.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

CABIN CUSP WEB LT SIDE BS 451 LBL 54 CORRODED. REPAIRED PER 53-05D FIG 827D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

MAIN PASSENGER CABIN BETWEEN STA 200-218 RBL 22 SEAT TRACK LEVEL 2 CORROSION.

Part: SUPPORT BRACKET — CRACKED (LE SLAT) · airframe 48,772 hrs · 36,161 cycles

LEFT WING L/E NR 3 SLAT TRACK CABLE SUPPORT BRACKET (DOUBLER) CRACKED X1569. REPAIRED IAW SRM 57-06B FIG 21 SHEET 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,772 hrs · 36,161 cycles

FUSELAGE EXTERNAL STATION 413 L 28R SKIN HAS DENT APPROX L 1 INCH, W .25 INCH X D .25 INCH.

Part: STRUT — DAMAGED (NLG) · airframe 43,913 hrs · 33,124 cycles

AFTER TAKEOFF GEAR HANDLE UP GOT RED NOSE GEAR INDICATION SOUNDED LIKE NOSE GEAR DID NOT RETRACT, RETURNED TO ATL. MTC IN PROGRESS ON NOSE STRUT. REPACKED NOSE LANDING GEAR C/W OPN 4702 ACJIC CARD 5 RETRACT AND EXTENSION CHECKS NORMAL.

Part: PRESSURE PANEL — DAMAGED (MLG WW) · airframe 39,990 hrs · 30,528 cycles

MLG WHEEL WELL - SLANT PRESSURE PANEL REPAIRED IAW 09-085387-12 ME01. C/W 09-085387-12 ME01.

Part: GENERATOR — BURNED (NR 1 ENGINE) · airframe 39,112 hrs · 29,921 cycles

LEFT GENERATOR OFF LIGHT WITH CROSSTIE LOCKOUT, LEFT ENGINE FIRE INDICATION, REPLACED GENERATOR AND CSD.

Part: BALLAST — FAILED (EMERGENCY LIGHT) · airframe 37,093 hrs · 28,490 cycles

SMOKE IN CABIN COMING FROM OVERHEAD ROW 15. FOUND BALLAST BAD AT ROW 14 D, E (P1-2100). REPLACED BOTH BALLAST. ALSO REPLACED HARNESS THAT IS IN POOR CONDITION (DDL 339201635). PERFORMED OPERATIONAL CHECK, CHECKS NORMAL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 35,620 hrs · 27,437 cycles

LEFT SYSTEM HYD QTY WENT TO 3 QTS. TURNED OFF LEFT ENG DRIVEN PUMP PER POM. RE-ENGAGED LEFT ENG HYD PUMP DURING FINAL APPROACH. LEFT HYD QTY EVENTUALLY WENT TO ZERO. FOUND BLUE FLEXIBLE PRESSURE LINE LEAKING IN TAIL CONE AREA. REPLACED FLEX LINE, LT ENG DRIVEN PUMP, TRANSFER PUMP AND FILTERS. FLUSHED LEFT HYD SYSTEM AND CLEANED AFT TAIL CONE AREA.

Part: TIRE — DAMAGED (LT MLG) · airframe 35,433 hrs · 27,305 cycles

NR 2 MAIN TIRE LOST RECAP ON TAKEOFF. DAMAGE TO LT IB FLAP AND BUTE DOOR. ALSO DAMAGE TO LOWER LT ENGINE INLET COWL AT 6 O'CLOCK POSITION LOWER SIDE. NO DAMAGE TO ENGINE FAN BLADES. REPAIRED/REPLACED DAMAGED PARTS.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 32,679 hrs · 25,418 cycles

L2 SLIDE FEEL OUT OF DOOR WHEN DOOR WAS OPENED. FOUND SLIDE STILL ARMED INFLATED WHILE HANGING BUT DID NOT OPEN. REPLACED SLIDE PER MM.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 32,351 hrs · 25,186 cycles

DURING CLIMB OUT SLAT DISAGREE LIGHT ILLUMINATED WITH SLAT HANDLE IN UP POSITION AND GOOD INDICATION . REPLACED FLAP HANDLE POSITION SWITCH SLAT OPERATION AND INDICATION NORMAL RAN BITE ON PSEU NO FAULTS

Part: COFFEEMAKER — OVERHEATED (R-1 GALLEY) · airframe 31,653 hrs · 24,723 cycles

ON ENTRY INTO AIRCRAFT FIRST OFFICER AND FLIGHT ATTENDENT SMELLED ELECTRICAL TYPE ODOR IN AIRCRAFT. FOUND R1 GALLEY COFFEEMAKER OVERHEATING. REPLACED.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 27,690 hrs · 21,807 cycles

FLT ATT REPORTED SMELL FROM AFT OF A/C ON TAKEOFF OUT OF CHS SMELL SMOKE, BUT NO SMOKE. TRANSFER FEEDS CLOSED. AIRFOIL A/I OFF ENG A/I OFF. APU OFF, SMOKE DISSIPATED AFTER 5 MINS. REPLACED COALESCER BAGS.

Part: COALESCER BAG — CONTAMINATED (A/C PACK) · airframe 25,630 hrs · 20,287 cycles

FLT 635 AIR TURNBACK AFTER F/A''S REPORTED STRONG SMELL OF SMOKE IN CABIN. ON DESCENT F/A''S REPORTED SMELL RETURNED. PRIOR TO LIFTOFF CAPT NOTICED A MYLAR BALLOON DRIFT BY HIS WINDOW. C/C INSPECTED INLET AND EXHAUST ON RT AND LT ENGS AND FOUND MYLAR BALLOON IN RT INLET. REMOVED SAME, CHECKED AND SVC LT AND RT ACM, CHECKED 8 AND 13 STAGE DOMES. NO OIL FOUND. CLEANED APU INLET DOOR, REPLACED LT AND RT WATER SEPARATOR BAGS. RAN ENGS PER PFHB WITH PACKS ON, ALL NORMAL AND NO SMELL NOTED.

Part: SPRING — BROKEN (STAB TRIM) · airframe 24,689 hrs · 19,579 cycles

STAB TRIM INOP. FOUND BOTH STAB TRIM SUITCASE HANDLE SPRINGS BROKEN. REPLACED BOTH SUITCASE HANDLE DETENT SPRINGS, OPS NORMAL.

Part: OVEN — DIRTY (GALLEY)

ELECTRICAL / PLASTIC FUMES. SUSPECTED SOURCE FORWARD GALLEY OVEN WAS NOT ON AT THE TIME. FOUND PLASTIC SHIPPING TAG STILL ON FWD GALLEY OVEN LINER. REMOVED LINER, RAN OVENS. CHECKS OK.

Part: OVEN — ODOR (GALLEY)

SMOKE IN CABIN. FOUND GALLEY OVEN CAUSING SMELL, CORRECTED.

Part: LANYARD — BROKEN (L1 DOOR SLIDE)

FWD ENTRY L1 DOOR LANYARD BROKEN. REPLACED L-1 DOOR SLIDE LANYARD AND LOCK ASSY.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER, NOW OPS NORMAL.

Part: FRAME — CRACKED (BS 1418)

AT FS 1418, MTC FOUND A CRACK AT L2L AND L2R ON THE FS 1418 FRAME. REPAIRED PER ERA 331389-14.

Part: SKIN — DENTED (BS 219)

FUSELAGE SKIN WAS FOUND DENTED AT STA 219 BETWEEN S18L AND 19L. REPAIRED PER ERA 331377-14.

Part: SKIN — DENTED (BS 237)

THE LT SIDE OF THE FUSELAGE SKIN WAS FOUND WITH TWO DENTS, ONE AT STA 237 ABOVE LONGERON 19L AND ONE AT FS 237 BELOW LONGERON 19L. THE FORMER AT STA 237 WAS FOUND CRACKED AND IT WAS REPLACED. THE DENTS WERE CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER. THIS REPAIR IS APPROVED UNDER MD-88 SRM 53-04, FIG 12B.

Part: AIR DISTRIBUTION — SMOKE (CABIN)

AT 2500-3000 FEET ON APPROACH, F/A REPORTED SMOKE SMELL IN CABIN. CAPTAIN DECLARED AN EMERGENCY. THE TOWER REPORTED THAT THE A/C WAS DESCENDING THROUGH A LAYER OF SMOKE. F/A CONTINUED TO SMELL SMOKE WITH NO VISUAL SMOKE IN CABIN. A/C WAS INSPECTED AT END OF RUNWAY AND CLEARED TO GATE WITH NO FURTHER INCIDENT.

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHTS NOT WORKING TOWARDS REAR OF A/C, LAST SECTION OF LIGHTS. INBOUND ITEM FOUND BROKEN WIRE. RETERMINATED.

Part: HYD LINE — WORN (RIGHT)

RT HYD FLUID WENT TO 1 QUART AND PRESSURE ZERO CLIMBING THROUGH 14,000 FEET. FOLLOWED CHECKLIST, RETURNED TO ATL. FOUND FORWARD LINE TO RT HYD HOUSING WORN THROUGH. REPLACED LINE, CHECKED PUMP FILTER FOR METAL, NONE FOUND. REPLACED FILTER, LEAK AND OP CHECKS NORMAL. GEAR EXTENDED PER EMERGENCY PROCEDURE. DOORS STRUCK GROUND. INSPECTED DOORS, NO DAMAGE FOUND EXCEPT SKIDS WORN. REPLACED BOTH SKIDS.

Part: PROX BOX — MALFUNCTIONED (NLG)

ON GEAR RETRACTION, NOSE UNSAFE LIGHT REMAINS ILLUMINATED. RAN POM, LIGHT EXTINGUISHED ON APPROACH. TROUBLESHOT SYSTEM, REPLACED PROXIMITY BOX, ALL CHECKS NORMAL. NOSE GEAR SWING CHECKS OK.

Part: TRANSDUCER — FAILED (LT MLG)

ON LANDING ROLLOUT, BRAKING EFFECTIVENESS ON THE LEFT SIDE WAS ALMOST NON-EXISTENT, SOMEWHAT MORE EFFECTIVE AT TAXI SPEEDS. RESET LEFT GEAR IN LINE FUSE, VERIFIED BRAKES ARE OPERATING AT GATE, PERFORMED HIGH SPEED TAXI, FOUND ANTI-SKID INOP. OPERATES NORMAL WITH ANTI-SKID OFF. REPLACED BOTH WHEEL TRANSDUCERS, OPERATION NORMAL.

Part: PISTON — CRACKED (LT MLG)

WHILE PERFORMING ERA 335832-14, FOUND LEFT MAIN GEAR PISTON CRACKED O/B AND I/B LUG AT TORQUE LINK (S/N MALSS019).

Part: HYD LINE — FAILED (TAIL COMP)

DURING CRUISE, LOST RIGHT SYSTEM HYD QTY AND PRESS. LANDED MSY. FOUND HYDRAULIC LINE CHAFED THROUGH IN TAIL COMP. INSTALLED TEMPORARY LINE FOR RETURN TO SERVICE. SUBSEQUENTLY, A PERMANENT LINE WAS INSTALLED.

Part: ANGLE — CRACKED (LT PYLON)

FOUND DURING D-1 LETTER CHECK, .75 INCH CRACK UPPER AFT LT PYLON TO FUSELAGE SKIN ATTACH ANGLE. REPAIRED PER SRM 54-04A.

Part: DUCT — CRACKED (NR 1 ENGINE)

ON CLIMB-OUT, AT AVL WITH ENGINE ANTI-ICE ON, GOT LEFT ENGINE FIRE WARNING. FOLLOWED APPROPIRATE PROCEDURES, WARNING CEASED WHEN POWER WAS REDUCE. FOUND ENGINE NOSE COWL AFT ANTI-ICE AIR DUCT BROKEN. REPLACED DUCT, OPERATION NORMAL.