N988DL

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,567 hrs · 49,664 cycles

SEAT 19 E/D EMER LIGHT INOP. RELAMPED SEAT 19 E/D. CHECKS GOOD. (LP4807188)

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 68,167 hrs · 49,322 cycles

SKIN CRACKED FROM EOP THRU FASTENER AND OUT THE OTHER SIDE. LOWER AFT SKIN PANEL P/N 5930503-105 AT STA 883 STRINGER 17. CENTER LT FUEL TANK. APPROX 2 INCHES. REPAIRED IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,167 hrs · 49,322 cycles

STRINGER 17 LT IS CRACKED AT APPROX LBL15 AT THE O/B END OF THE 5935874-501 FITTING. REPAIRED IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.

Part: SKIN — CRACKED (FUEL TANK) · airframe 68,167 hrs · 49,322 cycles

FUEL LEAKING FROM LT CENTER TANK. POSSIBLE SKIN CRACK LEFT OF CENTER KEEL BEAM. CRACK INDICATION IN LWR SKIN AT APPROX STA 883 STR 17 BY HFEC IAW MDC 93KO393 NDT SPM PART 6-10-01.001. REPAIR IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 68,167 hrs · 49,322 cycles

SKIN CRACKED AT FASTENER LOWER FWD SKIN PANEL P/N 5930503-103 AT STA 883 STRINGER 17. CENTER LT FUEL TANK. DIRECTLY FWD OF AFT SKIN CRACK REF NRC. REPAIRED IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.

Part: SKIN — GOUGED (LT WING SLAT) · airframe 65,701 hrs · 47,364 cycles

LEFT WING L/E SLAT NR 3 EXTERNAL SKIN HAS A GOUGE NEXT TO THE END. REMOVED DAMAGE AND EVALUATED, ORIGINAL .100 LOSS .024, REMAINING .076, AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-01. REPAIRED AREA IAW ERA 556444-14, REV O.

Part: STRUT — DAMAGED (NLG) · airframe 65,701 hrs · 47,364 cycles

DURING NLG SHOCK STRUT SEAL REPLACEMENT, FOUND METERING PIN AND INNER TUBE DAMAGED. REMOVED AND REPLACED NLG METERING PIN, SUPPORT TUBE, RESTRICTOR SUPPORT ASSY HEAD AND LOWER STRUT PISTON ASSY IAW CMM 32-21-04 AND AMDS.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 65,701 hrs · 47,364 cycles

AFT ACCESSORY BAY LT AFT SIDE OF CANTED FRAME 1463 ATTACH CLIP IS CRACKED AROUND INBD FASTENER L7L INSIDE OF LOUVER PANEL REF AA 5310-01456-01.

Part: STAND OFF — CRACKED (RT MLG WW) · airframe 65,701 hrs · 47,364 cycles

AUX HYD PUMP POWER CABLE RT WW WIRING STANDOFF SUPPORT BRACKET CRACKED. LOCATED JUST I/B OF THE HYD SERVICE ACCESS PANEL. REMOVED AND INSTALLED THE STAND OFF IAW SRM 51-30-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,466 hrs · 46,472 cycles

EMERGENCY LIGHT AT SEAT 17EF IS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED GOOD IAW AMM 33-53.

Part: TERMINAL — LOOSE (LAVATORY) · airframe 64,176 hrs · 46,250 cycles

DURING CRUISE, THE FLIGHT ATTENDANTS DETECTED AN ELECTRICAL ODOR MOST NOTICEABLE AT THE AFT FLIGHT ATTENDANT JUMP SEAT POSITION. THE CREW PERFORMED QRH SMOKE/ODOR PROCEDURE AND DIVERTED TO TPA. MAINTENANCE TROUBLESHOT PER WORK CARD 2120-2367 AND FOUND AFT LEFT LAVATORY OCCUPIED DOOR SWITCH S1-228 TERMINAL LUG LOOSE AND INTERMITTENTLY CONTACTING THE DOOR FRAME. THE TERMINAL LUG WAS REPLACED PER AMM 20-50. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 64,055 hrs · 46,168 cycles

DURING PREFLIGHT, FOUND EMERGENCY LIGHTS ON AND BATTERIES DEAD LIGHTS WILL COME ON FOR 5 SECONDS THEN DIE. REPLACED THE BATTERY PACKS IAW WORK CARD 3350-7353. EMERGENCY LIGHTS CHECKED GOOD IAW AMM 33-53-00.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 64,028 hrs · 46,152 cycles

ENROUTE, DIVERTED DUE TO FLIGHT ATTENDANTS REPORTING AN ELECTRICAL ODOR IN THE FIRST CLASS CABIN. MAINTENANCE FOUND A FORWARD GALLEY COFFEEMAKER HOT PLATE WAS BURNING COFFEE AND CAUSING ELECTRICAL ODOR. THE COFFEE MAKER WAS DEFERRED PER NEF (LP# 9480325) AND A FULL DUCT BURNOUT WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — CRACKED (RAM AIR) · airframe 63,973 hrs · 46,119 cycles

VERTICAL RAM AIR INLET DUCT SKIN CRACKED. REPAIRED IAW SRM 55-05 FIG 3 AND RI 553770-14 REV ORIG.

Part: DUCT — CRACKED (RAM AIR) · airframe 63,973 hrs · 46,119 cycles

VERTICAL RAM AIR INLET DUCT SKIN LEFT SIDE CRACKED DORSAL FIN AREA. CRACK 7" LONG. IAW ENGINEERING PERFORMED DETAILED VISUAL INSP OF CRACK AND SURROUNDING AREA. STOP DRILLED CRACK IAW INSTRUCTIONS.

Part: A/C PACK — FAILED (RIGHT) · airframe 63,930 hrs · 46,095 cycles

THE RIGHT PACK CYCLED TWICE AND SHUTDOWN AND THEN SMOKE WAS REPORTED IN THE AFT CABIN. THE COCKPIT AND CABIN TEMPERATURE SELECTORS WHERE BOTH FOUND IN THE MANUAL FULL HOT POSITION. OVERHEATING OF THE RIGHT PACK WAS SUSPECTED. VERIFICATION OF THE RIGHT ACM'S ABILITY TO SPIN FREELY WAS ACCOMPLISHED AND THE ACM OIL LEVEL CHECKED FULL. AN OPERATIONAL CHECK OF THE RIGHT PACK WAS PERFORMED WITH NO TROUBLE WAS FOUND. NO LEAKS WERE NOTICE. A SINGLE PACK CONFIDENCE CHECK WAS PERFORMED AND CHECKED OKAY IAW AMM21-00-00-501. THE LEFT PACK TEMP CONTROL VALVE WAS FOUND INOPERATIVE IN AUTO. THE LEFT PACK TEMP CONTROL VALVE WAS REPLACED PER AMM 21-61. THE LEFT FLOW CONTROL VALVE WAS FOUND TO BE NOT OPENING FULLY. THE LEFT FLOW CONTROL VALVE WAS REPLACED AND CHECKED OKAY PER AMM 21-31. APU AND PACKS WERE OPERATED FOR 2 HOURS. NO SMOKE OR ODOR WAS NOTED. THE SMOKE/ODOR CHECK LIST WAS PERFORMED PER AMDS 2120-2367. THE PNEUMATIC SYSTEM BURNOUT WAS ACCOMPLISHED PER AMDS 7100-2619. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 63,089 hrs · 45,465 cycles

AFT CATWALK LOWER CENTER EMERGENCY LIGHT INOPERATIVE. CRIMPED BROKEN WIRE AT CONNECTOR IAW SWPM 20 AND WDM 3351. OPS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 1338) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON FLOORBEAM, BS 1338 BETWEEN X -13 TO -17. FLOORBEAM WAS REPAIRED IAW ER/A 397783-14MA, REV ORIGINAL.

Part: ANGLE — CORRODED (BS 685-690) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON CUSP WEB ANGLE BS 685 - 690 BETWEEN RBL 54 TO 60. AREA WAS REPAIRED IAW ER/A.

Part: TAB — NOT REPORTED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

BUSHING GEARED TAB ATTACH POINTS WERE REPLACED. FITTING ON GEARED TAB ATTACH POINTS WAS REMOVED AND NEW FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW CMM 27-30-1, AMM 20-30-01-201, SRM 51-10-4, 51-10-3, PAR 21 AND 14 AND 51-30-2. FREE PLAY WAS CORRECTED.

Part: BUSHING — CORRODED (RT ELEVATOR TAB) · airframe 60,554 hrs · 43,634 cycles

FREEPLAY AND CORROSION ON BUSHING OF CONTROL TAB ATTACH POINTS AT RT ELEVATOR. CONTROL TAB ATTACH POINTS WERE REPLACED IAW CMM 27-30-1. FITTING ON BS XET=48.293 WAS REMOVED IAW AMM 20-30-01-201 NEW FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14 AND 51-30-2.

Part: FINGER DOUBLER — CORRODED (BS 1291-1295) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON INNER FINGER DOUBLER BETWEEN BS 1291 - 1295, LONGERONS 25 - 26L. THE FINGER DOUBLER WAS REPAIRED IAW SRM 51-30-2, 53-04, FIG 12E, 51-10-1, FIG 36 AND 51-10-3, PAR 14, 21.

Part: TRAY — CORRODED (LAVATORY) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL TRAY. EXCESSIVE CORROSION ON PANEL TRAY WAS REPLACED IAW DWG 5914792, ITEM 3, REV: AG AND SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LOWER DOOR FRAME. REPAIRED IAW SRM 53-05, FIG 123, SRM 51-10-3, PAR 14, 21, AND SRM 51-30-5.

Part: SKIN — CORRODED (BS 1322-1338) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON LOWER INTERCOSTAL AT AFT LAVATORY SERVICE PANEL, BETWEEN BS 1322 TO 1338, LONGERONS 21 - 22L. THE INTERCOSTAL WAS REPLACED IAW SRM.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 60,554 hrs · 43,634 cycles

CRACKED RIBS ON FIXED L/E OF VERTICAL STABILIZER. RIBS WERE R & R IAW SRM 55-02 D, FIG 27 AND 51-30-5 TO 51-30-2 AND DWGS 9911881, ID, 2 REV C. AND 9911882: ID 2, REV B.

Part: DOUBLER — WORN (LAV SRVICE PANEL) · airframe 60,554 hrs · 43,634 cycles

WORN INNER DOUBLER OF AFT LAVATORY SERVICE PANEL.

Part: DOUBLER — WORN (LAV SRVICE PANEL) · airframe 60,554 hrs · 43,634 cycles

WORN INNER DOUBLER OF AFT LAVATORY SERVICE PANEL. DOUBLER WAS BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. THE DOUBLER WAS REPLACED IAW DWG 5911423, ITEM 43, REV: CD, SRM 51-30-2 AND 51-30-5.

Part: FINGER DOUBLER — CRACKED (BS 1174-1193) · airframe 60,554 hrs · 43,634 cycles

CRACKED FINGER DOUBLER BETWEEN LONGERON 25-26L BS 1174 - 1193. THE FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12E, 51-30-2, 51-30-5 AND 51-10-3, PAR 38.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON THE LEFT CARGO TRACK BETWEEN BS 1007 TO 1322 IN THE AFT CARGO COMPARTMENT. A NEW CARGO TRACK WAS INSTALLED IAW SRM.

Part: FINGER DOUBLER — CORRODED (BS 1209-1231) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON THE FINGER DOUBLER BETWEEN LONGERONS 25-26L BS 1209 - 1212, 1228 - 1231. THE FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12E , 51-30-2 , 51-30-5 AND 51-10-3, PAR 38.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 60,554 hrs · 43,634 cycles

CRACKED INNER PAN BELOW STOP FITTING NR 3 IN FWD CARGO BAY AFT EDGE. REPAIR WAS ACCOMPLISHED IAW SRM 52-05D, FIG 50. CRACK LONG 0.150".

Part: LONGERON — CORRODED (BS 1231-1250) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON PREVIOUS REPAIR OF LONGERON 29L BETWEEN BS 1231 - 1250. THE REPAIR WAS REPLACED IAW SRM 51-30-5, PAR 13, SRM 53-02, FIG 19, AND SRM 51-10-3, PAR 21, 14 AND 38.

Part: FRAME — CRACKED (BS 1451) · airframe 60,554 hrs · 43,634 cycles

CRACKED FRAME BS 1451, BETWEEN LONGERONS 1-3L. THE FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3 PAR 14,21.

Part: SKIN — CORRODED (BS 1307-1322) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION BETWEEN DOUBLER AND SKIN AT AFT LAVATORY SERVICE PANEL, BETWEEN BS 1307 - 1322, LONGERONS 21-22L. REPAIRED IAW ETI 88-15-248, REV 2 AND ER/A 536500-14, REV:ORIG.

Part: INTERCOSTAL — CRACKED (BS 1309-1322) · airframe 60,554 hrs · 43,634 cycles

A CRACK WAS FOUND ON THE INTERCOSTAL BETWEEN LONGERONS 27-28L. BS 1309 - 1322. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3, PAR 14 AND 21.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON THE RT CARGO TRACK BETWEEN BS 1212 - 1322, UPPER AND LOWER SURFACES. THE CARGO TRACK WAS REMOVED AND REPLACED IAW IAW SRM 51-10-3, PAR 21, 14, AND 51-30-1.

Part: FRAME — CRACKED (BS 1510) · airframe 60,554 hrs · 43,634 cycles

CRACKS FOUND ON FRAME, BS 1510 . THE FRAME WAS REPLACED IAW DWG 9911843, REV SRM 51-30-2 , 51-10-4 , AND 51-10-3.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

DENTS FOUND ON PREVIOUS REPAIR OF MID GUIDE VANE ON THE LT WING OTBD FLAP. A NEW DOUBLER WAS INSTALLED IAW SRM 57-03, PARR II.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

DENTS FOUND ON REPAIR OF INBD GUIDE VANE LOWER SURFACE ON LT WING INBD FLAP. THE REPAIR WAS REPLACED IAW SRM 57-03D.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1007 - 1155, UPPER AND LOWER SURFACES. DAMAGE CARGO TRACK WAS REMOVED, AND A NEW CARGO TRACK WAS DRILLED, TREATED AND PAINTED. THE CARGO TRACK WAS INSTALLED IAW SRM 51-30-1,51-10-4, AND 51-10-3 PAR 21,14.

Part: HINGE — CRACKED (VENTRAL DOOR) · airframe 60,554 hrs · 43,634 cycles

A CRACK WAS FOUND ON AFT VENTRAL DOOR UNDER UPPER HINGE FITTING. REPAIRED IAW SRM 51-30-2 AND 51-30-1, 51-10-3, PAR 14/21, 51-01, PAR 4 CAP 21 AND 52-05D, FIG 34.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 60,554 hrs · 43,634 cycles

CRACKED RIBS ON FIXED L/E OF VERTICAL STABILIZER, THE RIBS WERE REPAIRED AND REPLACED IAW SRM 55-02D, FIG 27 AND 51-30-5 TO 51-30-2 AND DWG 9911881, ID, 2 REV. C AND 9911882. ID, 2, REV B.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 60,554 hrs · 43,634 cycles

DAMAGED METALLIZED SKIN ON RUDDER CONTROL TAB. METALLIZED SKIN WAS REPAIRED IAW SRM 51-70-1A, PAR 23 AND JIC 2000-8149-16.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LONGERON 22L BETWEEN BS 1287 - 1309 IN CARGO BAY. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 14 AND 21.

Part: SKIN — CORRODED (BS 1307-1322) · airframe 63,749 hrs · 45,960 cycles

THE FUSELAGE SKIN & INTERNAL DOUBLER AT THE AFT LAV WASTE PANEL BS 1307-1322, L21 - 22L, WERE CORRODED AND REQUIRED REPAIR DOUBLERS.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PLATE NR 1361C. FUEL ACCESS PLATE NR 1361C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PLATE NR 1466C. FUEL ACCESS PLATE NR 1466C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PLATE NR 1460C. FUEL ACCESS PLATE NR 1460C WAS REPLACED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 693) · airframe 60,554 hrs · 43,634 cycles

CRACK FOUND ON LONGERON 6L BS 693. THE LONGERON WAS REPAIRED IAW ER/A 536506-14 REV. ORIGINAL.

Part: GUIDE VANE — WORN (RT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

WEAR ON REPAIR OF INBD GUIDE VANE L/E AT RT WING OTBD FLAP. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03, PARR II .

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 60,554 hrs · 43,634 cycles

CRACKED LT AND RT INTERNAL DORSAL FIN ANGLES BETWEEN STA Y=1401-1418 AT VERTICAL STABILIZER ROOT. INTERNAL DORSAL FIN ANGLES BETWEEN BS Y=1401 TO Y=1418 AT VERTICAL STABILIZER ROOT WERE REPLACED IAW SRM 51-30-5. CRACK LENGTH: 1.125".

Part: SKIN — CRACKED (BS 375) · airframe 60,554 hrs · 43,634 cycles

TWO CRACKS FOUND ON THE FUSELAGE SKIN FWD UPPER DOOR FRAME CORNER BS 375 BETWEEN LONGERONS 20 - 21R. THE AREA WAS REPAIRED IAW SRM 53-05, FIG 105, 51-30-5 AND 51-10-3 PAR 14,21. MAJOR REPAIR.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON LONGERON 20L BETWEEN BS 1287 - 1309. THE LONGERON WAS REPLACED IAW SRM 53-14-3 ITEM 21, 51-10-3, 51-30-2, 51-30-5, 51-10, 3B, AND 51-10-01.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF THE FUEL ACCESS PANEL 1367C. THE ACCESS PANEL WAS REPLACED.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

WORN LT WING OTBD FLAP, OTBD GUIDE VANE INBD T/E SKIN. THE SKIN WAS REPAIRED IAW SRM 57-03, PAR 11.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION IN A BARREL NUT HOLE ON THE LT HORIZONTAL STABILIZER OUTER SKIN. REPAIRED IAW SRM 55-03D, PAR 30 AND ER/A 536502-14, REV ORIGINAL.

Part: STIFFENER — CRACKED (AFT PRSUE BLKHD) · airframe 60,554 hrs · 43,634 cycles

CRACKED END STIFFENER AT LONGERON 14R OF THE AFT PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW SRM 51-30-5 , 51-10-4 , 51-10-3 PAR. 14 AND 21.

Part: ANGLE — CORRODED (BS 1338) · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON THE ANGLE AT BS 1338 BETWEEN LONGERONS 28R TO 28L. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR FOUND ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1409C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A .

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND IN BARREL NUT HOLE ON THE RT HORIZONTAL STABILIZER OUTER SKIN. REPAIRED IAW SRM 55-03, PAR 30 AND ER/A 536502-14, REV, ORIGINAL.

Part: FLOOR SUPPORT — CRACKED (BS 769-788) · airframe 60,554 hrs · 43,634 cycles

CRACKED FLOOR SUPPORT BS 769 - 788. THE FLOOR SUPPORT WAS REPAIRED IAW ER/A 380524-14MA, REV ORIG AND SRM 51-30-5.

Part: STOP FITTING — CRACKED (BS 370) · airframe 60,554 hrs · 43,634 cycles

CRACKED STOP FITTING NR 3 BS 370 AT THE FWD CARGO DOOR. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-01, SRM 51-30-05, SRM 51-10-04, AND SRM 51-10-03

Part: INTERCOSTAL — CRACKED (BS 189) · airframe 60,554 hrs · 43,634 cycles

CRACKED INTERCOSTAL BS 189. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: PLATE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT UPPER PLATE BARREL NUT HOLE, XH=7.2. THE PLATE WAS REPAIRED IAW ETI-88-15-238, REV 2 AND ER/A 536489-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1470C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF FUEL ACCESS PANEL 1454C. THE ACCESS PANEL WAS REPLACED AND INSTALLED.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1462C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1478C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1335C. THE ACCESS PANEL WAS REPLACED.

Part: FRAME — CRACKED (BS 1485) · airframe 60,554 hrs · 43,634 cycles

CRACKED FRAME BS 1485, LONGERON 25R. THE FRAME WAS REPAIRED IAW SRM 53-03D, FIG 43, SHEET 3.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1371C. THE ACCESS PANEL WAS REPLACED.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 60,554 hrs · 43,634 cycles

CRACKED NR 1 BEAM ON FWD EDGE OF FWD SERVICE DOOR. THE BEAM WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3, 51-10-4 AND 52-41-0.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 60,554 hrs · 43,634 cycles

SEVERAL DENTS AT RT SLAT PANEL NR 2 OTBD SKIN. FOUND WITHIN LIMITS IAW SRM 57-30, PAR 18, FIG 18

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1355C. THE ACCESS PANEL WAS REPLACED.

Part: VANE — NICKED (RT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

NICK ON OTBD UPPER SURFACE OF THE OTBD GUIDE VANE ON THE RT WING OTBD FLAP. REPAIRED IAW SRM 57-03D PARR 11.

Part: VANE — WORN (RT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

WEAR ON THE INBD TRAILING EDGE OF THE OTBD GUIDE VANE ON THE RT WING OTBD FLAP. REPAIRED IAW ERA 521199-14MA, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1464C. THE ACCESS PANEL WAS REPLACED.

Part: SKIN — DENTED (NR 2 SLAT) · airframe 60,554 hrs · 43,634 cycles

SEVERAL DENTS AT RT SLAT PANEL NR 2 OTBD SKIN. DENTS WERE MEASSURE WITH FOLLOW BS 237 CONDITIONS DEPTH OF DENT 0.015", DIAMETER 0.800" DENT ON REGION "A" AND WITHIN LIMITS IAW SRM 57-03, PAR 18, FIG 18, ALSO ON BS 227, X=0.005, D=0.900, REG A. WITHIN LIMITS IAW SRM 57-03, PAR 18, FIG 18. PERFORM DECAL CONDITION INSPECTION EACH C-CHECK. HFEC INSPECTION WAS PERFORMED AND NO CRACKS WERE FOUND.

Part: RUB STRIP — DELAMINATED (RT WING TE FLAP) · airframe 60,554 hrs · 43,634 cycles

DELAMINATED RUB STRIP OF OTBD GUIDE VANE UPPER SURFACE ON RT WING OTBD FLAP. THE RUB STRIP WAS BONDED IAW SRM 51-20-0.

Part: FLOOR PANEL — PUNCTURED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

PUNCTURE ON FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

DAMAGED FERRULE ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201 AND REPLACED THE FERRULE IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

DELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-70-1D, PAR 10.

Part: SKIN — CORRODED (NR 3 SLAT) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RIB HOLES AT RT SLAT PANEL NR 3 STA, XOS=287, XOS=332 AND XOS=379. CORROSION ON RIB HOLES AT RT SLAT PANEL NR 3 STA, XOS=287, 332 AND 379 WERE REMOVED IAW SRM 57-02, PAR 9, FINAL ID: D=1.123", 2 HOLES, STA 379, D=1.124", STA 287, AND D=0.934, 2 HOLES AND D=0.937", 2 HOLES, STA 332 THEREFORE WITHIN LIMITS OF REPAIR IAW SRM 57-02, PAR 9.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

DELAMINATED FLOOR PANEL 769C. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1338) · airframe 60,554 hrs · 43,634 cycles

CRACK ON LONGERON 7R BS 1338. LONGERON WAS REPLACE IAW SRM 51-30-5 , 53-14-3, FIG 4-A AND 51-10-3 PAR 14 AND 21.

Part: MOUNT — DAMAGED (RT ENGINE) · airframe 60,554 hrs · 43,634 cycles

SCRATCHES ON LOWER BUSHING OF AFT ENGINE MOUNT AT RT PYLON. SCRATCHES ON LOWER HOLE BUSHING OF FWD ENGINE MOUNT AT RT PYLON WERE REPAIRED IAW SRM 54-04D, FIG 12A.

Part: SEAT TRACK — CORRODED (BS 827-951) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON RT SEAT TRACK X=-54 BTW BS 827 - 829 , 933 - 936 AND 951 - 950. THE SEAT TRACK WAS REPAIRED IAW SRM.

Part: SKIN — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT WING SLAT PANEL XOS 198 AND XOS 24. THE SLAT PANEL WAS REPAIRED IAW SRM 57-02, PAR 9.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON REPAIR DOUBLER AND DOOR JAMB BEAM AT MID CARGO BAY. DOOR FRAME BEAM WAS REPAIRED IAW SRM 53-05, FIG 123.

Part: PANEL — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT WING SLAT PANEL NR 3 XOS=286. THE SLAT PANEL WAS REPAIRED IAW SRM 57-02, PAR 9.

Part: SKIN — CORRODED (NR 4 SLAT) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT WING NR 4 SLAT PANEL XOS=380. SLAT WAS REPAIRED IAW SRM 57-02, PAR 9.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201 PAR 7.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PLATE NR 1410C. FUEL ACCESS PLATE NR 1410C WAS REPLACED.

Part: SKIN — CORRODED (RT SLAT) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RIB HOLES AT RT SLAT PANEL, NR 0, XFS 40. CORROSION ON RIB HOLES AT RT SLAT PANEL WAS REPAIRED IAW SRM 57-02, PAR 9.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 60,554 hrs · 43,634 cycles

CRACKED SHEAR TIE BS 1380 BETWEEN LONGERONS 13-16RT. SHEAR TIE REPLACED IAW SRM 53-14-4, FIG 1 AND 51-30-2 , 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 60,554 hrs · 43,634 cycles

LONGERON 16L, CRACKED AT BS 1437. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3 PAR 21 AND 14.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

DAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PANEL 1365C. THE ACCESS PANEL WAS REPLACED.

Part: NOT REPORTED — DAMAGED (RT WING) · airframe 60,554 hrs · 43,634 cycles

DENT AND TOOL DAMAGE ON RT WING L/E, XOS 248. THE WING L/E WAS REPAIR IAW SRM 57-06A, PARA 9. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1363C. THE ACCESS PANEL WAS REPLACED.

Part: STRAP — WORN (BS 630-700) · airframe 60,554 hrs · 43,634 cycles

WORN STRAPS, BS 630 - 700 LONGERON 28R. STRAPS WERE REMOVED IAW SRM 51-30-5, NEW STRAPS INSTALLED IAW DWG 5936039, REV C.

Part: LONGERON — CRACKED (BS 522) · airframe 60,554 hrs · 43,634 cycles

CRACK LONGERON 4L AT BS 522. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21, 51-10-4.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF THE FUEL ACCESS PANEL 1311C. THE ACCESS PANEL WAS REPLACED.

Part: LONGERON — CRACKED (BS 1437) · airframe 60,554 hrs · 43,634 cycles

CRACKED LONGERON 16R AT BS 1437. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (BS 1380) · airframe 60,554 hrs · 43,634 cycles

CRACKED WEB AT BS 1380 LONGERON 21L. THE WEB WAS REPAIRED IAW SRM 53-01, FIG 4, 51-10-3, PAR 21 AND 14 AND 51-30-2.

Part: CUSP WEB — CRACKED (BS 905) · airframe 60,554 hrs · 43,634 cycles

A CRACK WAS FOUND ON THE CUSP WEB AT BS 905, RBL 48. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: SKIN — DAMAGED (BS 750-769) · airframe 60,554 hrs · 43,634 cycles

LIGHTNING STRIKE ON RT WINDOW BELT, FWD UPPER CORNER, BETWEEN BS 750 - 769. REPAIRED IAW NDT/SPM 04-00-07, PAR 5 FIG 3 FOUND WITHIN LIMITS IAW ER/A 536492-14, REV A SECTION I.

Part: SKIN — DAMAGED (RUDDER) · airframe 60,554 hrs · 43,634 cycles

DAMAGED METALLIZED ON RUDDER SKIN RT SIDE LOWER AREA. THE SKIN WAS REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: SEAT TRACK — CORRODED (BS 453-517) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON LT SEAT TRACK X 22 BETWEEN BS 453 - 517. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, PAR 8, FIG 4A

Part: CUSP WEB — CORRODED (BS 1042-4049) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON RT CUSP WEB BS 1042 TO 1049 BTW X=54-X=60AT PAX CABIN. THE AREA WAS REPAIRED IAW SRM.

Part: CHANNEL — CRACKED (NOT REPORTED) · airframe 60,554 hrs · 43,634 cycles

CRACKS WERE FOUND ON THE HAT CHANNEL. THE HAT CHANNEL WAS REPAIRED IAW SRM 53-05, FIG 131C AND 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 1095) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON LT CUSP WEB BS 1095 BTW LBL 54 TO 60 AT PAX CABIN. THE CUSP WEB WAS REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 1231-1250) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON THE RT CUSP WEB, BS 1231 - 1250 BETWEEN X -54, X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-7, 51-10-3, PAR 21, 14.

Part: CUSP WEB — CORRODED (BS 503-598) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RT CUSP WEB FROM BS 503 - 598. A NEW CUSP WEB WAS DRILLED AND INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 796-799) · airframe 60,554 hrs · 43,634 cycles

CRACK ON CUSP WEB, BS 796 - 799, X=44 TO 41. REPAIRED IAW SRM 51-30-2, 53-05, FIG 13, A-13, 51-30-5, 51-30-1, 51-10-3 PAR 14 AND 21, CRACK IS 0.750".

Part: CUSP WEB — CORRODED (BS 490) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON RH PREVIOUS REPAIR CUSP WEB BS 490 BTW X=-54 TO X=-60. THE CUSP WEB WAS REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 1064-1076) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON RT CUSP WEB, BS 1064 - 1076 BETWEEN X 54 - 60 . THE DAMAGE WAS REMOVED, A REPAIR FABRICATED IAW SRM 53-05, FIG-131A-7, TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. REPAIR INSTALLED IAW SRM 53-05, FIG-131A-7.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 598 - 617 AND X -54 TO -60. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-30-2, 51-10-3, PARR 14, 21.

Part: CUSP WEB — CORRODED (BS 657-663) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT CUSP WEB, BS 657 - 663, X 54 TO X 60. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-2, 51-10-3, PARR 14,21.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 2301C. THE ACCESS PANEL WAS REPLACED.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RIB HOLES XIS=136.42 ON LT WING SLAT PANEL. RIB REPAIRED IAW SRM 57-02, PAR 9.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RIB HOLES XIS= 83.534 ON LT WING SLAT PANEL. RIB WAS REPAIRED IAW SRM 57-02, PAR 9.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PLATE 1303. THE ACCESS PANEL WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A 6B AND REPLACED.

Part: CUSP WEB — CORRODED (BS 611-615) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT CUSP WEB, BS 611 - 615 X 54 - 60. REPAIRED IAW SRM 53-05, FIG 131A-14, SRM 51-10-3, PAR 14-21, SRM 51-30-2, 51-30-5.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON FLOOR PANEL 160G AT PAX CABIN. THE FLOOR PANEL WAS REPLACED.

Part: FITTING — DAMAGED (RT WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND A SCRATCH ON RT MAIN GEAR SUPPORT FITTING BORE, RT WING. THE DAMAGE WAS REPAIRED AND FOUND WITHIN LIMITS IAW DWG 5R09570087, REV B. FPI INSPECTION WAS PERFORMED AND DID NOT FIND A CRACK IAW PS 900-6-3. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 60,554 hrs · 43,634 cycles

CRACK ON CABIN FLOOR PANEL 256A. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-10-3, PAR 14 AND 21 AND SRM 53-01, FIG 4, SHEET 4.

Part: CUSP WEB — CORRODED (BS 469-471) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 469 - 471 X -54 TO -60. : CORROSION REMOVED IAW SRM 53-05, FIG 131A -13 SRM 51-10-3 , PAR 14, 21 AND 51-30-2, 51-30-5.

Part: FITTING — DAMAGED (LT WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND SCRATCH ON LT MAIN GEAR SUPPORT FITTING BORE ON THE LT WING. DAMAGE ON FITTING WAS REPAIRED AND FOUND WITHIN LIMITS IAW DWG SR09570087.

Part: CUSP WEB — CORRODED (BS 1239-1250) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BETWEEN BS 1239-1250 X 56 - 60. CORROSION WAS REMOVED IAW SRM 51-30-5 , SRM 51-30-1, SRM 53-05, FIG 131A-6 AND SRM 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 1418) · airframe 60,554 hrs · 43,634 cycles

CRACKED LONGERON 2L BS 1418 . THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18 AND SRM 51-30-5, SRM 51-10-3 PAR 14 , 21. MAJOR REPAIR.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 63,749 hrs · 45,960 cycles

CORROSION ON CABIN FLOOR PANEL 256E. THE FLOOR PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION AND WEAR ON COUNTERSINK OF FUEL ACCESS PLATE 1436 ON RT WING. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2.

Part: SEAT TRACK — CORRODED (BS 216-219) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT SEAT TRACK PLUG REPAIR IN X 22 BETWEEN BS 216 - 219. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 60,554 hrs · 43,634 cycles

CRACKED SHEAR TIE ON BS 1380 BTW LONGERON 12-15L. SHEAR TIE REPLACED IAW SRM 53-14-4, FIG 1 AND TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21 AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: DOUBLER — MISINSTALLED (LT ELEVATOR) · airframe 60,554 hrs · 43,634 cycles

LOOSE AND IMPROPERLY INSTALLED FASTENERS ON DOUBLER OF LT ELEVATOR XHR=217. DOUBLER WAS REPLACED IAW SRM 51-30-2, 55-22-0, 51-10-3, PAR 14.

Part: SKIN — DAMAGED (BS 157-198) · airframe 60,554 hrs · 43,634 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 157 BETWEEN LONGERONS 5 - 6 RIGHT , BS 165- 198 LONGERONS 4 - 6 RIGHT. LIGHTNING STRIKES WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-04-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,554 hrs · 43,634 cycles

LIGHTING STRIKE ON SKIN BS 349 AND LONGERON 3R, BS 377 AND LONGERON 23R, BS 410 BETWEEN LONGERONS 2 - 3R, AND BS 453 BETWEEN LONGERONS 2 - 3R. LIGHTNING STRIKES WERE BLENDED OUT AND FOUND WITHIN LIMITS IAW SRM 53-04-1, PAR 5C, REPAIRED IAW SRM 53-04-2, PAR 3C, 2, A, 1, A.

Part: SKIN — DAMAGED (BS 693-750) · airframe 60,554 hrs · 43,634 cycles

LIGHTINING STRIKE ON FUSELAGE SKIN BETWEEN BS 693-712 AND BS 731-750 LONGERONS 28 - 29 LEFT. LIGHTNING STRIKES WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-04-1, PAR 5C. BS 694 - 701 LONGERONS 28-29LEFT WERE REPAIRED IAW SRM 53-04-2 PAR 3C, 2, A, 1, A.

Part: SKIN — DAMAGED (BS 233-297) · airframe 60,554 hrs · 43,634 cycles

LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 233, 255, 275 AND 297 BETWEEN LONGERON 1 AND LONGERON 2 RIGHT. LIGHTNING STRIKES WERE BLENDED AND FOUND WITHIN LIMITS IAW SRM 53-04-1 PAR. 5D. BS 255 WAS REPAIRED IAW SRM 53-04-2, PAR 3C, 2, A,1, A.

Part: DOUBLER — DAMAGED (RT ELEVATOR) · airframe 60,554 hrs · 43,634 cycles

LIGHTNING STRIKE ON T/E DOUBLER OF RT ELEVATOR XHR 217. DOUBLER WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR 14, 55-22-0.

Part: CUSP WEB — CORRODED (BS 514-522) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON LT CUSP WEB BTW BS 514 TO 522, X=54 TO X=60 ON PREVIOUS REPAIR DOUBLER. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-9.

Part: SEAT TRACK — CORRODED (BS 607-626) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION ON PREVIOUS REPAIR PLUGS ON SEAT TRACK, Y54 BETWEEN BS 607 - 626. PLUGS WERE REPLACED IAW SRM 53-05, FIG 4A, SHEET 1, 51- 30-1, 51-10-3 PAR 14 AND 21.

Part: PAN — CRACKED (BS 946) · airframe 60,554 hrs · 43,634 cycles

CRACKED LT FWD LOWER RING PAN, BS Y=946 AT PAX CABIN, FCS, SM, CARD 64, ZONE 201. RII: N ENTR 416812 W SUMMARY: AREA WAS REPAIRED IAW SRM 53-05, FIG 122, SHEET 5, SRM 51-10-2 , 51-10-4 , 51-10-3 , 51-30-2 , 51-30-5 AND ERAS 487747-14, REV ORIGINAL AND 493648-14MA REV A. CRACK IS .115".

Part: PAN — CRACKED (BS 807) · airframe 60,554 hrs · 43,634 cycles

CRACKED LEFT UPPER FWD RING PAN, BS 807 AT PAX CABIN. REPAIRED IAW SRM 53-05, FIG 122, SHEET 5, 51-10-2 , 51-10 -4 , 51-10-3 , 51-30-2 , 51-30-5 AND ERA'S 487747-14MA, REV ORIGINAL AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 886) · airframe 60,554 hrs · 43,634 cycles

CRACKED LT UPPER FWD RING PAN BS Y=886 AT PAX CABIN, FCS, SM, CARD 62, ZONE 201, RII: N ENTR 416812 W, SUMMARY: AREA WAS REPAIRED IAW SRM 53-05, FIG 122, SHEET 5, SRM 51-10-2 , 51-10-4 , 51-10-3 , 51-30-2 , 51- 30-5 AND ERA'S 487747-14MA REV ORIGINAL, 493648-14MA REV A. ASSOCIATED ER/A 00-487747, ADDED FOR AC 0988.

Part: PAN — CRACKED (BS 465) · airframe 60,554 hrs · 43,634 cycles

CRACKED LT UPPER FWD WING PAN, BS Y=465 AT PAX CABIN, FCS, SM, CARD 60, ZONE 201. RII: N ENTR 416812 W SUMMARY: AREA WAS ATTENDED IAW SRM 53-05, FIG 122, SHEET 5, SRM 51-10-2 , 51-10-4 , 51-10-3 , 51-30-2 , 51-30-5 AND ERA'S 487747-14MA, REV. ORIGINAL , 493648-14MA, REV A. CRACK IS .095" ASSOCIATED ER/A 00-487747.

Part: PAN — CRACKED (BS 655-750) · airframe 60,554 hrs · 43,634 cycles

CRACKED RT WINDOW RING PAN UPPER AFT CORNER BETWEEN BS Y=655 TO Y=674 AND Y=731 TO Y=750, CFS, SM, CARD 46, ZONE 201, RII: N ENTR 416812 W SUMMARY: RING PAN UPPER, AFT CORNER BETWEEN BS Y=655 TO Y=674 AND Y=731 TO Y=750 WERE REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3, PAR 21 AND 14 ER/A 493648-14MA, REV A AND 487747 REV ORIGINAL. CRACK IS .270" AND .120" ASSOCIATED ER/A 00-487747 ADDED FOR AC 0988.

Part: PAN — CRACKED (BS 115-1212) · airframe 60,554 hrs · 43,634 cycles

CRACKED RT WINDOW RING PAN UPPER, AFT CORNER BETWEEN STAY=1155 TO Y=1174 AND Y=1193 TO Y=1212. RING PAN REPAIRED IAW SRM 53-05. FIG 122 AND 51-30-2 , 51-30-5 AND 51-10-3, P. 21/14 ER/A 493648-14MA, REV A , ER/A 487747-14MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 807-905) · airframe 60,554 hrs · 43,634 cycles

CRACKED RT WINDOW RING PAN LOWER, FWD CORNER BETWEEN BS Y=807 TO Y=826 AND UPPER, AFT CORNER BETWEEN BSY=886 TO Y=905, CFS, SM, CARD 47, ZONE 201. RII: N ENTR 416812 W SUMMARY: RING PAN LOWER, FWD CORNER BETWEEN BS Y=807 TO Y=826 AND UPPER,AFT CORNER BETWEEN STA Y=886 TO Y=905 WERE REPAIRED IAW SRM 53-05, FIG 122 AND 51-30-2 , 51-30-5 , AND 51-10-3, PAR 21 AND 14. ER/A 493648-14MA, REV A, ER/A 487747-14MA, REV ORIGINAL.CRACK IS .260" AND .135" ASSOCIATED ER/A 00-487747 ADDED FOR AC 0988.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 60,554 hrs · 43,634 cycles

CORROSION FOUND ON A REPAIR DOUBLER ON FRAME BS 1309 BETWEEN LONGERONS 28L - 28R IN THE AFT CARGO BAY. THE DOUBLER WAS REPLACED IAW SRM 53-03, FIG 2A SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, AND SRM 51-10-3, PAR 14-21-38.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,455 hrs · 42,846 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT 27DE. MAINTENANCE R & R THE LIGHTS AND THE OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 59,258 hrs · 42,727 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT WIRE HARNESS AT SEAT 32DE WAS DAMAGED. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: TERMINAL — BROKEN (EMERGENCY LIGHTS) · airframe 58,659 hrs · 42,304 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FOR THE MIDDLE OF THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN TERMINAL END, RETERMINATED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: LIGHT — BROKEN (SEAT 18DE) · airframe 58,598 hrs · 42,256 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 18DE WAS BROKEN. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,806 hrs · 41,107 cycles

DURING LINE CHECK, NOTED FIRST CLASS OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY B5-100 IAW AMM AND OPS NORMAL.

Part: SKIN — CRACKED (BS 1361) · airframe 55,961 hrs · 40,524 cycles

FUSELAGE SKIN BS 1361 L-14R CRACK REPAIRED IAW ERA 518047-14.

Part: WEB — CRACKED (BS 1485) · airframe 55,961 hrs · 40,524 cycles

DURING SCHEDULED CHECK, A CRACK WAS FOUND IN THE AFT ACCESSORY COMPARTMENT RT VENT BOX AT BS 1485 WEB BELOW UPPER HORIZONTAL. REPAIRED IAW SRM 53-03, FIG 49 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,947 hrs · 40,518 cycles

DURING SCHEDULED INSPECTION, CEILING MOUNTED EMERGENCY LIGHTS POWERED BY BATTERY PACK B5-104 WERE INOPERATIVE. BATTERIES WERE REPLACED IAW AMM 33-50-00 AND OPERATION CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,947 hrs · 40,518 cycles

DURING SCHEDULED INSPECTION, CEILING MOUNTED EMERGENCY ESCAPE LIGHTS FROM THE GALLEY TO ROW 26 AND ROW 31 AND AFT WERE NOTED TO BE INOPERATIVE. THE EMERGENCY LIGHT BATTERIES WERE REPLACED AND OPERATION CHECKED NORMALLY IAW AMM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,947 hrs · 40,518 cycles

DURING SCHEDULED IN INSPECTION, THE TAIL COMPARTMENT OVERHEAD EMERGENCY EXIT LIGHTS WERE NOTED TO BE INOPERATIVE. EMERGENCY LIGHT BATTERIES IN B5-28 WERE REPLACED IAW AMM 33-53 AND OPS CHECKED NORMALLY.

Part: FASTENER — LOOSE (APU) · airframe 52,489 hrs · 38,205 cycles

AFTER TAKEOFF FLIGHT CREW NOTED SMOKE IN THE CABIN & COCKPIT. CREW DECLARED AN EMERGENCY AND RETURNED TO GCM. MAINTENANCE FOUND APU INLET CONTAMINATED WITH OIL DUE TO A LEAK AT THE SIGHT GLASS & THE FILL HOUSING TO GEARBOX SPLIT LINE. MAINTENANCE RETORQUED SIGHT GLASS AND FILLER MOUNT HARDWARE, NO FURTHER LEAK NOTED. MAINTENANCE CLEANED APU INLET DOOR ASSY & SURROUNDING AREA. PACK BURNOUT PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE.

Part: PANEL — CORRODED (FUSELAGE) · airframe 52,320 hrs · 38,106 cycles

DURING CURRENT PSV VISIT AT MSP, CORROSION DAMAGE WAS REPORTED ON THE LEFT WINDOW BELT PANEL BETWEEN BS 1174-1193, LOCATED ON THE INNER SURFACE, UPPER AFT SIDE. THE DAMAGE WAS CLEANED UP PER MD88 SRM 53-05 FIG 111 AND THE COMPLETED WINDOW BELT PANEL BLEND OUT MAPPING WAS DOCUMENTED IN ERA 501454-14 REV O. WORK WAS ACCOMPLISHED ON NRC 228. HIGH FREQ EDDY CURRENT INSPECTED AND NO CRACKS EXIST. THIS REPAIR IS AN ENGINEERING APPROVED TIME LIMITED REPAIR. IDENTIFIED PER PS 900-5-1. NO. 04. ENTERED INTO LOGBOOK AND NOTIFIED MCC.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 52,320 hrs · 38,106 cycles

DURING PSV IN MSP AND DURING AD INSPECTION PER 09-470871-12AD REF "F DISCREPANT HOLES WERE FOUND COMMON TO THE LOWER FIXED L/E SKIN. THREE HOLES EXCEEDED THE LIMITS OF SG09550004 REV "A". SUBJECT HOLES WERE REPAIRED PER ER/A 501324-14AD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,320 hrs · 38,106 cycles

NRC 88 RT FUSELAGE CRACKED 4EA PLACES AT STA 1418 BETWEEN LONGERON 2R-3R, NRC 215 CROWN SKIN CRACKED AT STA 1418 RBL -2 1/2 TO RBL 4, DAMAGE CONTAINED, INSTALLING REPAIRS PER PRI -501207-14.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 52,320 hrs · 38,106 cycles

NRC 76 LT FUSELAGE SKATE ANGLE AT STA 1474 HAS 2EA LOOSE FASTENERS. REPAIRED PER ERA 501215-14 REV ORIGINAL.

Part: WIRE — BROKEN (CABIN) · airframe 50,875 hrs · 37,136 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS AT ROW 28 - 30 INOP. MAINTENANCE RE-TERMINATED BROKEN WIRES AT ROW 20, 28, 29, AND 30. OPERATION OF LIGHTS CHECKS OK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 50,258 hrs · 36,715 cycles

ON SHORT FINAL CREW GOT A MID CARGO SMOKE WARNING ALONG WITH FIRE BELL WARNING. ALL THREE LAV SMOKE DETECTORS WERE ALSO GOING OFF. CREW FOLLOWED QRH FOR CARGO FIRE BLEW FIRE BOTTLES IN CARGO AND DECLARED EMERGENCY INTO ATL. AIRCRAFT LANDED AND FIRE TRUCKS MET THE FLIGHT. ATL MAINTENANCE FOUND BOTH FIRE BOTTLE IN CARGO USED. BOTTLES WERE REPLACED PER AMM. SQUIB TEST WAS GOOD PER AMM. CARGO BIN WAS INSPECTED AND THERE WAS NO SIGNS OF SMOKE OR FIRE. THERE WAS NO SMELL IN CARGO EXCEPT OF FIRE SUPPRESSION BOTTLES. ALL THREE LAV SMOKE DETECTORS WERE REPLACED AND TESTED.

Part: CONTROL PANEL — SMOKE (COCKPIT) · airframe 49,391 hrs · 36,177 cycles

WHEN CREW INITIAL POWER UP OF COCKPIT AN ACRID AND WHITE SMOKE EMITTED FROM CAPTAINS SIDE FMA. C/B WAS PULLED AND SMOKE DISAPPEARED. MX CONFIRMED SOURCE OF SMOKE & ODOR WAS FROM CAPTAIN FMA PANEL. NO OTHER DAMAGE WAS NOTED. THE CAPTAINS FMA WAS REPLACED IAW AMM 22-17-00-201. FMA OPERATES NOW NORMAL AND ACFT IS OK FOR SERVICE.

Part: SPAR — CRACKED (WING) · airframe 49,048 hrs · 35,970 cycles

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

Part: FUSE — INOPERATIVE (BATTERY CHARGER) · airframe 47,883 hrs · 35,222 cycles

MX FOUND THE AFT CABIN EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPLACED THE FUSE IN THE EMERGENCY BATTERY CHARGER.

Part: WIRE — BROKEN (CABIN) · airframe 47,726 hrs · 35,107 cycles

EMERGENCY ESCAPE PATH LIGHT INOP AT 14D. FOUND WIRE BROKEN AT LIGHT. REPLACED LIGHT ASSY.

Part: DUCT — DAMAGED (NR 2 NACELLE) · airframe 44,187 hrs · 33,006 cycles

ON CLIMB-OUT AT LEVEL OFF THE RT ENGINE THROTTLE WAS BOUND. UNUSUAL RESISTANCE TO MOVING TO IDLE. AFTER BRINGING THE ENGINE BACK TO IDLE THE THROTTLES OPERATED NORMALLY. FOUND THE NUMBER 2 ENG COWL ANTI-ICE DUCT BLOWN WHICH CAUSED DAMAGE TO THE UPPER ENGINE COWL.

Part: BEARING — MISSING (RT MLG DOOR) · airframe 41,788 hrs · 31,535 cycles

GEAR DOOR UNSAFE LIGHT ON AFTER EXTENSION. AFTER GO AROUND GEAR WAS RETRACTED AND EXTENDED MANUALLY. A/C LANDED WITH GEAR DOORS OPEN. DOOR BUMPERS WERE GROUND DOWN WITH NO DAMAGE TO THE DOORS. FOUND RT MLG DOOR ROLLER MISSING.

Part: CHARGER — UNKNOWN (E/E BAY) · airframe 36,700 hrs · 28,133 cycles

WHILE REPOSITION AIRCRAFT FOUND SMOKE COMING FROM UNDER FUSELAGE FWD OF E/E DOOR. FOUND AIRCRAFT BATTERIES OVERCHARGING. REPLACED CHARGER, BATTERIES AND TEMP SENSORSD PER M/M, SYSTEM CHECK NORMAL.

Part: TIRE — FAILED (NR 3) · airframe 36,031 hrs · 27,660 cycles

F/A REPORTED BURNING RUBBER SMELL IN CABIN AFTER T/O, RT ENGINE STALLED DURING CLIMB. FOUND NR 3 TIRE TREAD SEPARATED AND MISSING. REPLACED TIRE AND REPAIRED FLAP DAMAGE.

Part: ENGINE — FAILED (NR 1) · airframe 35,209 hrs · 27,048 cycles

LT ENGINE FAILED AT 15K FT AND 300 KNOTS - REPLACED ENGINE FOR INTERNAL FAILURE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,689 hrs · 25,969 cycles

FIVE OVERHEAD EMERGENCY LIGHTS INOP NEAR OVERWING EXIT. REPLACED BATTERIES ON B5-104 BATTERY PWR SUPPLY PACK.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 32,785 hrs · 25,313 cycles

FL230 LOST RIGHT HYD QTY QTY DOWN TO 4 QTS. SHUT OFF RT HYD ENG PUMP PER CKLIST. QTY REMAINED CONSTANT AT 4 QTS UNTIL PUMP WAS TURNED ON IN PREP FOR LANDING. QTY THEN DECREASED TO 1 QT. MAINTENANCE NOTED HYD FLUID UNDER AIRCRAFT. APU NOT STARTED PER CREW CKLIST. ALSO NO LOW PRESSURE INDICATION FOR HYD. INSTALLED TEMP LINE ON RT SYS PRESS TRANS. LEAK CK'D GOOD. OK FOR 350 HRS PER M/M 20/12/09. INSP AFTER 175 FLT HOURS.

Part: SCHRADER VALVE — LEAKING (NLG) · airframe 30,367 hrs · 23,650 cycles

ON TAKEOFF NLG DID NOT APPEAR TO RETRACT, HAD RED UNSAFE LIGHT ILLUMINATED. RAN POM PROCEDURE NLG REMAINED UNSAFE IN RETRACT POSITION-REPLACED NLG SCRADER VALVE FOR LEAKING.

Part: VALVE — LEAKING (NLG) · airframe 29,737 hrs · 23,224 cycles

UPON GEAR RETRACTION NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUM. HAD NOISE INDICATING GEAR NOT FULLY RETRACTED. AIR RETURN TO IAD. MAINTENANCE FOUND NLG STRUT FLAT. UPPER SHRAEDER VALVE LEAKING. REPALCING SAME AND SERVICING STRUT.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,748 hrs · 20,998 cycles

ON T/O ROLL AFT F/A SMELLED ELECTRICAL OR RUBBER BURNING. NO SMOKE BUT HAZE IN CABIN - THOROUGHLY INSPECTED AIRCRAFT - NTF - PERFORMED OPN 5088 DUCT BURNOUT.

Part: BULB — FAILED (CABIN) · airframe 24,386 hrs · 19,253 cycles

RED FLOOR EMERGENCY LIGHTS ACROSS FROM AFT GALLEY INOP. RELAMPED SAME, CHECKS GOOD.

Part: FLASHLIGHT — FAILED (CABIN)

JUMPSEAT 2L FWD FLASHLIGHT SEAL MISSING/BROKEN. FOUND FLASHLIGHT NOT FLASHING. REPLACED FLASHLIGHT, CKS OK.

Part: POWER SUPPLY — INOP (CABIN)

AFT CABIN E-PATH LIGHT SECTION INOP. REPLACED POWER SUPPLY AND BATTERIES, SYSTEM CHECKS NORMAL.

Part: OVEN — DIRTY (GALLEY)

FIRST CLASS OVEN SMOKING IN CABIN. FOUND PAPER AND SHIPPING DOCUMENTS ON F/C OVEN INSERT. CLEANED OVEN AND REMOVED INSERT.

Part: BATTERY — DISCHARGED (CABIN)

FWD CABIN EMERGENCY FLASHLIGHT INDICATOR LIGHT INOP. REPLACED BATTERY AND BULB, NOW CKS GOOD.

Part: GCU — FAILED (E/E COMPT)

ON T/O ROLL (115 KTS), LT AC BUS FAIL WITH AC CROSSTIE LOCK-OUT. ABORTED T/O. CHECKED LT AND RT CSD OIL SERV AND FILTER BUTTON FOUND LT ENG GEN CONT UNIT DIST FAULT ILLUM. CHECKED LT GEN SYS DPCTS. CKS OK INSP GEN LEADS ON LT ENG. NO DEFECTS NOTED. REPLACED LT GCU, RAN ENGS X-TIES AND GEN OPN NORMAL.

Part: FRAME — CRACKED (BS 1418)

FS 1418 FRAME WAS FOUND CRACKED AT L2L AND L2R. CRACKS WERE BOTH 1 INCH IN LENGTH. REPAIRED PER ERA 331500-14.

Part: SKIN — DENTED (BS 1325)

FUSELAGE SKIN WAS FOUND DENTED AND GOUGED FROM FS 1309 TO FS 1338 AT L23R. REPAIRED PER ERA 331520-14.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

THE WINDOW BELT PANEL ON BOTH THE RT AND LT SIDE OF THE FUSELAGE INCURRED LIGHTNING STRIKE DAMAGE. DAMAGE WAS SUSTAINED TO THE UPPER AFT CORNERS OF BOTH THE NR 6 RT WINDOW SURROUND AND THE NR 19 LT WINDOW SURROUND. A BOTH LOCATIONS, THE DAMAGE WAS BURNISHED SMOOTH TO A MAX DEPTH OF 0.025 OVER AN APPROX AREA OF .5 BY .25. REPAIRED PER ERA 362551-14.

Part: BULB — FAILED (RT MLG)

RT MAIN GEAR INDICATION LIGHT INOP IN FLIGHT. RELAMPED, CHKS OK.

Part: BULB — FAILED (CABIN)

3 WHITE EMERGENCY EXIT TRACK LIGHTS INOP AT ROWS 15, 23 AND 30. RELAMPED SAME, OPN NORMAL.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN)

DURING DEPARTURE, BOTH AUTO PRESSURIZATION CONTROLLERS FAILED AND BOTH CONTROLLERS FAULT AC MOTOR. VERIFY CHECK, NO FAULTS. REPLACED OUTFLOW VALVE ACTUATOR GEARBOX AND AC MOTORS, CHECKS GOOD PER MM CHECK.