N984DL

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 69,459 hrs · 49,870 cycles

RIGHT ENGINE LOOP B LIGHT ILLUMINATED DURING FLIGHT PER QRH LOOP A SELECTED. NORMAL FIRE TEST LOOP DETECTOR LEFT IN A POSITION FOR REMAINDER OF THE FLIGHT. SELECTED RT ENG FIRE LOOP TO BOTH AND RAN TEST OPS NORMAL NO FAULT NO HISTORY OK FOR SVC.

Part: BATTERY PACK — NOT REPORTED (CABIN) · airframe 68,012 hrs · 48,764 cycles

OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK OPS CHECK. REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-53-00 PERFORMED SATISFACTORY OPS CHECK.

Part: BEARING — NICKED (LT ELEVATOR) · airframe 68,012 hrs · 48,764 cycles

LEFT ELEVATOR NR 1 HINGE BEARING NICKED. REMOVED THE HINGE BEARING HOUSING IAW OVERHAUL MANUAL 27-30-1. REMOVED AND REPLACED THE BEARING AND REINSTALLED HINGE HOUSING IAW CMM 27-30-1 AND SOPM 20-10-7.

Part: SEAL — DAMAGED (HORIZONTAL STAB) · airframe 68,012 hrs · 48,764 cycles

ON INSTALLATION OF LEFT ELEVATOR TO HORIZONTAL STAB, DAMAGE WAS FOUND ON THE AFT SPAR REAR CAP, XE225. REPAIRED LT HORIZONTAL STAB T/E SPAR SEAL IAW ER/A 398032-14MA.

Part: CUSP WEB — CRACKED (BS 807) · airframe 68,012 hrs · 48,764 cycles

ON REMOVAL OF THE RT SIDE FLOOR WEB, A CRACK WAS NOTICED AT FWD CORNER CUT OUT. REPAIRED THE CUSP WEB AT BS 807 IAW SRM 53-05, PAR 144, FIG 131A-21, DWG 9910151, REV BU, REV CH, AND DWG 9930538 REV CE.

Part: WIRE — DAMAGED · airframe 67,676 hrs · 48,509 cycles

ACFT DIVERTED, DURING CLIMB OUT, PASSING THROUGH 26K, A STRONG ACRID ODOR BECAME APPARENT IN THE COCKPIT. FLIGHT ATTENDANTS REPORTED SAME ODOR IN CABIN. BEGAN DESCENT DIVERSION. AFTER APPROXIMATELY 1-1.5 MINUTES BOTH OIL TEMP HIGH LIGHTS ILLUMINATED. THROTTLES WERE AT IDLE. PERFORMED QRH PROCEDURES AND LIGHTS EXTINGUISHED AND ODOR DISSIPATED. UNEVENTFUL LANDING. MAINTENANCE PERFORMED WC2120-2367 AND 2120-2368, FOUND CHAFED & BARE WIRE P70A10 FOR BUSS OUT, EMERGENCY LIGHT DC & AC TO CIRCUIT BREAKER C19 AND C21 WITH BROKEN STRANDS AND BURN MARKS. THE WIRE WAS REPLACED IAW WSPM 20-20-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — PUNCTURED (NR 1 SLAT) · airframe 67,554 hrs · 48,421 cycles

DURING A SERVICE CHECK, FOUND A DENT WITH A PUNCTURE ON BACKSIDE OF RT NR 1 SLAT, 45 INCHES FROM INBOARD, 2.25 X 1.87 L X .195 DEEP. REMOVED AND REPLACED THE SLAT IAW AMDS CARD 2700-4224-RH-01.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 66,551 hrs · 47,710 cycles

HORIZONTAL STABILIZER UPPER RT AFT SKIN PANEL CRACKED. DRILLED END CRACK 0.250 DRILLED IAW SR09550028. ENLARGE STOP DRILL IAW SR09550028 STEP 42. HFEC INSP AREA IAW NDTM 06-1001.001 NO DEFECTS NOTED. ALODINED & PRIMED. SEALED AREA REINSTALLED FILLER AND APPLIED 2 LAYERS SPEED TAPE AND SEALED.

Part: CAM — NO TEST (TAILCONE RELEASE) · airframe 66,551 hrs · 47,710 cycles

TAILCONE RELEASE MECHANISM CAM FAILS TORQUE CHECK IAW STEP 12 OF AMDS 5350-01077-0101. ADJUSTED IAW AMM 53-53-02-201, OPS CHECKED GOOD, OK FOR SERVICE IAW AMDS 5350-01077-0101.

Part: APU — CONTAMINATED · airframe 66,449 hrs · 47,632 cycles

DURING THE BOARDING PROCESS, THE CREW NOTIFIED MAINTENANCE OF A BURNING SMELL IN THE CABIN. THE APU WAS RUNNING AND THE PACKS WERE BEING OPERATED TO WARM THE CABIN. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH DE-ICE FLUID. THE APU INLET AND DOOR ASSEMBLY WERE CLEANED. THE PNEUMATIC SMOKE/ODOR IN THE CABIN TROUBLESHOOTING WORK CARD WAS ACCOMPLISHED. A DUCT BURNOUT WAS PERFORMED AND THE COALESCER BAGS WERE REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FASTENER — DAMAGED (R1 DOOR) · airframe 66,214 hrs · 47,469 cycles

1R DOOR GIRT BAR HOLDER DETACHED FROM DOOR. ACARS INBD WRITE UP. REPLACED FASTENERS ON GIRT BAR HOLDER. CKS GOOD.

Part: CUSP WEB — CORRODED (BS 715-718) · corrosion level 2 · airframe 63,048 hrs · 45,246 cycles

CORROSION ON CUSP WEB BS 715-718 BETWEEN X -54 TO -60 AT CABIN PAX IN REF CARD 149, ZONE 201. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131A -13.

Part: VANE — DAMAGED (FLAPS) · airframe 62,926 hrs · 45,160 cycles

AFTER LANDING , WHEN FLAPS WERE RAISED TO 0 THE RT FLAP INDICATOR READS 5 AND LT FLAP INDICATOR READS 0, FELT SLIGHT BINDING WHEN ATTEMPTING TO RETRACT SLATS SO LT FLAPS OUT. INBD AND OTBD FLAP VANE GUIDE OF INBD FLAP WERE REPLACED FOR A SERVICIABLE FLAP VANE GUIDE IAW AMM 27-51-03-201, REF VENDOR 20000072035.

Part: HEATER BLANKET — CORRODED (RT WING) · corrosion level 2 · airframe 62,926 hrs · 45,160 cycles

CORROSION ON RT WING HEATER BLANKET AROUND FUEL ACCESS PANEL CUTOUT. THE HEATER BLANKET WAS REPLACED IAW AMM 30-80-02-401. TESTED THE HEATER BLANKET, FOUND OK IAW AMM 30-80-02-501.

Part: SKIN — CRACKED (BS 1418) · airframe 62,920 hrs · 45,156 cycles

A 0.187 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERONS 2 - 3L AND A CRACK OF 0.531" BETWEEN LONGERON 1 AND 2R. FUSELAGE SKIN WAS REPAIRED IAW ER/A 536455-14AD, REV ORIGINAL AND ETI 88-15-204, REV 2.

Part: BUSHING — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON REPAIR BUSHINGS AND ELONGATED BUSHINGS ON RT HEATER BLANKET T/E. DAMAGE BUSHINGS WERE REPLACED IAW ER/A 537709-14AD, REV "A" AND EA: 09-070683-03, AD REV L. MAJOR REPAIR.

Part: SKIN — CORRODED · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION FOUND BETWEEN FUSELAGE SKIN AND INBD DOUBLER AT AFT WASTE LAVATORY SERVICE PANEL. CORROSION WAS REMOVED IAW ETI-88-15-224, REV 1 AND ER/A 536427-14, REV ORIGINAL.

Part: TRUNNION — CORRODED (MLG) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION IN RT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REWORKED WITH FINAL DIMENTION ID 2.377" WITHIN LIMITS IAW DWG SR09570087, REV B, FPI WAS ACCOMPLISHED RT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE NO CRACKS WERE FOUND AFTER REWORKED IAW CARD 5740-01139-04B, STEP 8.

Part: TRUNNION — CORRODED (MLG) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION AND BLEND OUTS IN LT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REWORKED WITH FINAL DIMENTION: ID 2.2735" WITHIN LIMITS IAW DWG SR09570087, REV B FPI WAS ACCOMPLISHED LT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE NO CRACKS WERE FOUND AFTER REWORKED IAW CARD 5740-01139-04B, STEP 8.

Part: ANGLE — CRACKED (BS 1463 FRAME) · airframe 62,920 hrs · 45,156 cycles

CRACKED SPLICE ANGLE ON CANTED FRAME STA Y=1463 AND RBL 18. REPAIRED IAW ERA 536514-14, REV.

Part: FRAME — CRACKED (BS 1497) · airframe 62,920 hrs · 45,156 cycles

CRACKED FRAME BS 1497 . FRAME WAS REPAIRED IAW ER/A 536485-14, REV ORIGINAL AND ETI-88-15-234, REV 2.

Part: PAN — CRACKED (PAX DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED PAN ON PAX DOOR BETWEEN BEAM 8 AND FWD EDGE. THE DOOR WAS REPAIRED IAW SRM 52-05D, FIGURE 18A.

Part: INTERCOSTAL — CRACKED (BS 1271-1288) · airframe 62,920 hrs · 45,156 cycles

CRACKED INTERCOSTAL BETWEEN BS 1271 - 1288. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2, FABRICATED IAW DWG 9936580, REV BT, AND INSTALLED IAW SRM 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1193-1250) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION FOUND ON THE LT CARGO TRACK BS 1193 - 1250. THE CARGO TRACK WAS REPLACED.

Part: BEAM — CORRODED (BS 685-690) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION FOUND ON THE BEAM BETWEEN BS 685 - 690 OF THE MID CARGO LOWER DOOR FRAME. THE BEAM WAS REPAIRED IAW SRM 53-05, FIG 123. MAJOR REPAIR.

Part: LONGERON SPLICE — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON THE LONGERON SPLICE, BS 1287 - 1309, LONGERON 30. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-2 AND 51-30-5.

Part: FINGER DOUBLER — CORRODED (BS 579-598) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON FUSELAGE SKIN FINGER DOUBLER BELOW LONGERON 26L, BS 579 - 598. THE FINGER DOUBLER WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, AND SRM 51-10-3 PAR 14, 21 & 33.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,920 hrs · 45,156 cycles

CRACKED INTERCOSTAL BELOW HYD MANUAL PUMP AT LT MLG WHEEL WELL. THE INTERCOSTAL WAS REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR.21 AND 14, 51-10-2 AND 53-01.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON THE COUNTERSINK AND SETTLEMENT AREA OF THE FUEL ACCESS PANEL 1335C. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANLE WAS REPLACED IAW SRM 51-22-2A.

Part: ANGLE — CRACKED (BS 1007) · airframe 62,920 hrs · 45,156 cycles

CRACKED ANGLE BEHIND LT SIDE WALL SUPPORT AT BS 1007, Z -6. THE ANGLE WAS REPAIRED IAW SRM 53-01, 51-30-2, 53-01, FIG 2, 51-10-3 PAR 14 AND 21.

Part: INTERCOSTAL — CORRODED (BS 1380-1390) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INTERCOSTAL FROM BS 1380 - 1390 LONGERON 26L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-14-4, FIG 1, NDT SPM 04-00-07, FIG 3, PAR 5, SH 1 AND 2.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 62,920 hrs · 45,156 cycles

CRACKED ANGLE BETWEEN VSS 2 - 26 TO -15 AT VERTICAL STABILIZER INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-05, 51-30-2, 51-10-3 PAR 21 AND 14 SRM 51-10-2 AND DWG 5912188, REV BD.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LOWER DOOR FRAME IN THE FWD CARGO BAY. REPAIRED IAW SRM 53-05, FIG 44A.

Part: DOUBLER — CRACKED (BS 693) · airframe 62,920 hrs · 45,156 cycles

CRACKED INNER PRODUCTION DOUBLER, BS 693 BETWEEN LONGERONS 23-24R. THE DOUBLER WAS REWORKED IAW SRM 53-05, FIG 109. TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON THE UPPER DOOR FRAME BEAM BETWEEN BS 1174 - 1193 IN THE AFT CARGO BAY. THE BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4 AND 51-10-3 PARA 21, 14 AND 36.

Part: FRAME — CRACKED (BS 1343) · airframe 62,920 hrs · 45,156 cycles

WEAR AND A CRACK WAS FOUND ON FRAME BS 1343 LONGERONS 26L - 26R. THE FRAME WAS REPAIRED IAW ERA 094719-14MA, REV A.

Part: LONGERON — CORRODED (BS 1338-1380) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION FOUND ON LONGERON 24L BETWEEN BS 1338 - 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: TAB — DENTED (RT ELEVATOR) · airframe 62,920 hrs · 45,156 cycles

RT ELEVATOR GEARED TAB, DENTED ON UPPER SURFACE. THE TAB WAS REPAIRED IAW SRM 55-04.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 62,920 hrs · 45,156 cycles

CRACK ON UPPER DOOR FRAME FOR THE RT AFT OVERWING EMERGENCY DOOR. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05, FIG 32 AND 51-01, PAR 4, 21.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,920 hrs · 45,156 cycles

CRACKED RIB STA ZFS 49.62 AT VERTICAL STABILIZER. L/E INNER STRUCTURE, RIBS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 51-10-4.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON FRAME AND FRAME CLIP AT BS 1287 BETWEEN LONGERONS 28LT AND 28RT IN AFT CARGO COMPARTMENT. SUMMARY CORROSION WAS REMOVED IAW SRM 51-10-3 THEN NDT SPM 04-00-01 WITH AN ORIGINAL THICK OF 0.063" ON FRAME 1287 AND REM. THICK 0.004 AND IT IS OUT OF LIMITS THE MEASURE ON FRAME CLIP AT THE SAME BS, HAS AN ORIGINAL THICKNESS OF 0.063 AND REMAINING IS 0.043, SO IT IS OUT OF LIMITS AND IS NECCESSARY TO REPAIR THEN DAMAGE WAS REMOVED IAW SRM 53-03 D, FIG 2A AND REPAIR PARTS WERE FABRICATED IAW THE SAME REF TO THE FRAME AND FRAME CLIP. THE REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 AFTER THAT REPAIR PART AND SLANT SUPPORT & FRAME CLIP WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5 FINALLY CIC WAS APPLIED IAW SRM 51-10-3, PAR 38, PANAMETRICS OLYMPUS 38 DL PLUS TRANSDUCER SONOPEN V260-RM, EXP 28-AGO-15, RCF AMC-PND-151.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,920 hrs · 45,156 cycles

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

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,920 hrs · 45,156 cycles

CRACKED LT RIB BS ZFS 36.50 AT VERTICAL STABILIZER L/E INNER STRUCTURE. RIB WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PAR 14, 21.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,920 hrs · 45,156 cycles

CRACKED RIB XFS 30.00 IN VERTICAL STABILIZER L/E INNER STRUCTURE. RIB REMOVED IAW SRM 51-30-2 AND 51-30-5 AND A NEW RIB WAS DRILLED IAW SRM 51-10-4, AND REPAIRED IAW SRM 55-02, FIG 27. NEW RIB INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SEAT TRACK — WORN (BS 1188-1196) · airframe 62,920 hrs · 45,156 cycles

WEAR ON THE LEFT SEAT TRACK X 44 BETWEEN BS 1188 - 1196. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1, SRM 53-05, FIG 4B-1, NDT SPM 04-00-07, PAR 5, FIG 3 SH-1AND 2, SRM 53-05, FIG 4F, SRM 51-10-4, SRM 51-10-3, PAR 14 AND 21, AND SRM 51-30-5.

Part: CUSP WEB — DAMAGED (BS 1174-1250) · airframe 62,920 hrs · 45,156 cycles

WAVINESS IN LEFT CUSP WEB BETWEEN X 44 - 54, BS 1174 - 1250. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, SRM 51-30-2, SRM 53-05, FIG 131A-6, SRM 51-10-3, PAR 14 & 21 AND SRM 51-30-5.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON REPAIR OF LWR DOOR JAMB AT AFT CARGO COMPARTMENT. DOUBLER WAS REPLACE IAW SRM 53-05, FIG 123. PRIMARY STRUCTURE.

Part: INTERCOSTAL — CRACKED (BS 886-905) · airframe 62,920 hrs · 45,156 cycles

CRACKED INTERCOSTAL AT BS 886 - 905 LONGERON 17L. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 62,920 hrs · 45,156 cycles

CRACKED FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05, FIG 131C.

Part: TEE FITTING — CORRODED (BS 1380) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON TEE ANGLE AT BS 1380 BETWEEN LONGERONS 28L - 28R. DAMAGED TEE ANGLE WAS REMOVED, AND A NEW TEE ANGLE WAS DRILLED, TREATED AND PAINTED, THE TEE ANGLE WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5 AND DWG 9912246, REV D E. MAJOR REPAIR

Part: DOOR FRAME — CRACKED (PAX ENTRY) · airframe 62,920 hrs · 45,156 cycles

TWO CRACKS FOUND ON UPPER LT CORNER OF AFT ENTRY DOOR FRAME. REPAIRED IAW SRM 53-05, FIG 29, SHEET 1.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 62,920 hrs · 45,156 cycles

CRACKED RT RIB ZFS 43.00 IN VERTICAL STABILIZER L/E INNER STRUCTURE. THE RIB R WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9911882, REV "B".

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 62,920 hrs · 45,156 cycles

DELAMINATED FLOOR PANEL IN PASSENGER CABIN . A NEW FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201 AND .

Part: SKIN — DAMAGED (RUDDER) · airframe 62,920 hrs · 45,156 cycles

DURING MAINTENANCE ACTIVITIES, BROKEN SKIN OVER PREVIOUS REPAIR RT UPPER SURFACE OF RUDDER. THE SKIN WAS REPAIRED IAW SRM 51-70-1AD, PAR 23.

Part: FLOORBEAM — CORRODED (BS 1338) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON THE FLOORBEAM AT BS 1338 X -30, X -34, X -37, AND X -44 . THE FLOORBEAM WAS REPAIRED IAW SRM 51-30-5, 51-30-2 AND ERA 397783-14MA.

Part: INTERCOSTAL — CRACKED (BS 769-788) · airframe 62,920 hrs · 45,156 cycles

CRACKED INTERCOSTAL X 0 BETWEEN BS 769 - 788. THE CRACK WAS STOPPED DRILLED AND REPAIRED IAW SRM 53-01, FIG 2, SHEET 4.

Part: CUSP WEB — CORRODED (BS 1183-1187) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON RT CUSP WEB BS 1183 - 1187, X -54 TO -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (BS 731-763) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LT CUSP WEB FROM BS 731 - 763 BETWEEN X 54 AND X 60. THE CORROSION WAS REMOVED ON DAMAGE, REPAIRED IAW SRM 53-05, FIG 131A-14, SRM 51-30-2, 51-30-1, AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1460C ON THE RT WING. CORROSION REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM: 51-22-2A.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION WAS FOUND IN AN INTERNAL FASTENER HOLE OF THE ACCESS DOOR CUTOUT BETWEEN STRINGERS 12 AND 15, XRS=189 - XRS=214 ON THE LT WING. THE CORROSION WAS REMOVED AND REPAIRED IAW SRM 51-22-2A, PAR 7.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION WAS FOUND INTERNAL FASTERNER HOLE AT ACCESS DOOR CUTOUT BETWEEN STR 12 AND 15 AND BETWEEN BS XRS 189 TO XRS=214 ON RT WING, CARD 118, ZONE 10. RII: N ENTR 181463 W SUMMARY: CORROSION ON FASTENER HOLE AT ACCESS DOOR WAS REPAIRED IAW SRM 51-22-2A, PAR.6.

Part: CUSP WEB — CORRODED (BS 892-896) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LT CUSP WEB BS 892 - 896 BETWEEN X 54 TO X 60. REPAIRED IAW SRM 53-05, FIG 131A-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED EXTERNAL PAN ON AFT EDGE AND BEAM NR 5 AT MID CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-03D.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 62,920 hrs · 45,156 cycles

DAMAGED FERRULE ON FLOOR PANEL. FLOOR PANEL FERRULE REPLACED AND CLEANED IAW SRM 53-20-01-201.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED STOP FITTING ON FWD EDGE AND BEAM NR 2 AT MID CARGO DOOR. THE STOP FITTING WAS REPLACED IAW SRM 51-30-1, 51-30-5.

Part: CUSP WEB — CORRODED (BS 1098-1112) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON RT CUSP WEB UPPER/LOWER SURFACE BETWEEN X -54 TO X -60 BS 1098 - 1101, AND BS 1112. REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

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

Part: FITTING — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED FITTING ON LOWER EDGE BS 1193 ON AFT CARGO DOOR INNER STRUCTURE. THE FITTING WAS REMOVED IAW SRM 51-30-2 AND 51-30-5 AND A NEW FITTING WAS DRILLED IAW SRM 51-10-4, TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21 AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACK ON ANGLE AT BS 1193 BETWEEN LOWER EDGE AND BEAM NR 1 IN AFT CARGO DOOR. THE ANGLE WAS REMOVED IAW SRM 51-30-2 AND 51-30-5 AND A NEW ANGLE WAS FABRICATED IAW DWG 9957664 ,TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21 AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED FWD EDGE ON BEAM NR 1 AT FWD SERVICE DOOR. A NEW BEAM WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 62,920 hrs · 45,156 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED AND CLEANED IAW AMM 53-20-01-201 AND DS 900-1-2-2 N 2.

Part: SKIN — DAMAGED (BS 729) · airframe 62,920 hrs · 45,156 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 729 BETWEEN LONGERON 3 - 4R. DRILLED OUT IAW SRM 53-04-2, PAR 3C, 2, A, 1, A AND FIGURE 1. HFEC WAS ACCOMPLISHED AFTER STOP DRILL AND NO CRACKS WERE FOUND IAW SRM 53-04-2, PAR 3, C, 2, A, 1, A, 2.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1373C. THE ACCESS PLATE WAS FOUND OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 584) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORRSION ON LT CUSP WEB OF BS 584 BETWEEN X 54 - 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 503-588) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON UPPER AND LOWER SURFACE OF THE CUSP WEB BETWEEN X -54 TO X -60 BS 503 - 511, BS 544 - 553 AND BS 560 - 588.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 62,920 hrs · 45,156 cycles

CRACK ON FLOOR PANEL 541F IN THE PAX CABIN. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05, FIG 131C.

Part: CUSP WEB — DAMAGED (BS 964-986) · airframe 62,920 hrs · 45,156 cycles

ELONGATED HOLES AND BENT LT CUSP WEB BETWEEN BS 964-986. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-19 AND SRM 51-10-3, PAR 14 AND 21.

Part: RIB — CRACKED (LT WING) · airframe 62,920 hrs · 45,156 cycles

CRACKED RIBS AND ANGLES XRS 418 - 424 ON LT WING L/E. REPAIRED IAW SRM 57-06A, FIG 5, SRM 51-30-2 AND DWG 5937523, REV AD.

Part: FLOORBEAM — CORRODED (BS 1322) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON FLOORBEAM AT BS 1322 X -26 - 33. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIG 20 A.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACK ON FWD PAN SECTION AREA OF STOP FITTING NR 1 ON FWD CARGO DOOR. PAN REPAIRED IAW SRM 51-30-2 AND 52-05 D FIG 50. MAJOR REPAIR.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

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

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 62,920 hrs · 45,156 cycles

DELAMINATED FLOOR PANEL IN THE PAX CABIN. FLOOR PANEL FABRICATED IAW IAW AMM 53-20-01-201.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED EXTERNAL PAN ON FWD EDGE AND BEAM NR 1 AT MID CARGO DOOR. REPAIRED IAW SRM 52-03 D, FIG 8, PAR 5.

Part: SEAT TRACK — CORRODED (BS 637) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LT SEAT TRACK X 54 BETWEEN BS 637. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 380-435) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

DURING MAINTENANCE ACTIVITIES WAS FOUND CORROSION OUT OF LIMITS ON SEAT TRACK X -54, BS 380 - 435. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A AND SRM 51-10-3, PAR 14 AND 21.

Part: CHANNEL — BROKEN (NOT REPORTED) · airframe 62,920 hrs · 45,156 cycles

BROKEN CHANNEL . THE CHANNEL WAS REPLACED IAW DWG 9936639, REV P.

Part: PANEL — CORRODED (LT SLAT) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD, MID, OTBD RIB ON THE LT SLAT PANEL. REPAIRED IAW SRM 57-02, PAR 9 AND ER/A 536457-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 313) · airframe 62,920 hrs · 45,156 cycles

LIGHTNING STRIKE ON PREVIOUS REWORK AT FUSELAGE SKIN AT BS 313 BETWEEN LONGERONS 3 - 4R. REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 17.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF LT WING FUEL ACCESS PANEL 1367C. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1311C. CORROSION WAS REMOVED AND MEASURED. THE MAX DIAMETER ALLOWED IS .660" AND 3 HOLES ADJACENT WERE FOUND WITH: .673, .682 AND .687. FUEL ACCESS NR 1311C WAS REPLACED LIMITS IAW SRM: 51-22-2A.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 62,920 hrs · 45,156 cycles

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

Part: WEB — CORRODED (BS 160-180) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON DIAPHGRAM IN BS 160, X=-40, BS 180, X=-44 TO -52 AND AROUND PREVIOUS DOUBLER BS 190-200, X=-50 AT FLOOR CABIN STRUCTURE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-70-04, 51-30-02, AND 51-30-05.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,920 hrs · 45,156 cycles

DAMAGED METALIZED ON RUDDER LOWER ACCESS COVER 6508A. REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: CUSP WEB — CORRODED (BS 503-588) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON UPPER/LOWER SURFACE RT CUSP WEB BETWEEN X=-54 TO X=-60 BS 503-588, DAMAGE FOUND BS 578 X -60 WILL BE ATTENDED WITH CARD 316, ZONE 201. DUE TO EXCESSIVE CORROSION ON BS 503 - 511 AND BS 544 - 553 WAS REPAIRED IAW SRM 53-05, 131A-11, AND SRM 53-05, FIG 131A-6.

Part: LONGERON — CRACKED (BS 522-541) · airframe 62,920 hrs · 45,156 cycles

CRACKED LONGERON 4L BETWEEN BS 522 - 541. LONGERON WAS REMOVED AND REPLACED IAW 53-02, FIG 18, 51-10-4, SRM 51-10-3, PAR 14 AND 21, 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 927) · airframe 62,920 hrs · 45,156 cycles

CRACKED LONGERON 10L BS 927. LONGERON END WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PAR 21 AND 14. AND DWG 4925315-REV A.

Part: LONGERON — CRACKED (BS 522-541) · airframe 62,920 hrs · 45,156 cycles

CRACKED LONGERON 4R BETWEEN BS 522-541. THE LONGERON WAS REPAIRED IAW SRM 53-02 PARAGRAPH 12, FIGURE 18. CLASSIFIED AS MAJOR REPAIR.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS NR 2302C. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1409C. BLEND OUT REPAIR NOT PERMITTED AND FOUND OUT LIMITS. FUEL ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1307) · airframe 62,920 hrs · 45,156 cycles

LONGERON 8L CRACKED AT BS 1307 . LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: PAN — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CPCP EXFOLIATION CORROSION ON OTBD PAN OF AFT LAVATORY WASTE SERVICE PANEL. DUE TO EXCESSIVE CORROSION ON OTBD PAN OF AFT LAVATORY WASTE SERVICE PANEL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 988-992) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACES BETWEEN BS X -54 AND X -60 FROM BS 988 - 992. REPAIRED IAW SRM 53-05, FIG 131A-2, 51-30-2, 51-10-3, PAR 14, 21 AND 38.

Part: SKIN — DELAMINATED (RT ELEVATOR TAB) · airframe 62,920 hrs · 45,156 cycles

DELAMINATED UPPER AND LOWER SKIN ON RT ELEVATOR CONTROL TAB. RT ELEVATOR CONTROL TAB WAS REPLACED.

Part: SKIN — DAMAGED (BS 598-636) · airframe 62,920 hrs · 45,156 cycles

LIGHTNING STRIKES ON PREVIOUS REWORK AT FUSELAGE SKIN AT STA Y=598 AND Y=636 BETWEEN LONGERONS 3 - 4R. REPAIRED IAW SRM 53-04-2, 3C, 1, AND. FIG 2, SHEET 13.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1303C. REPAIR NOT PERMITTED AND FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM: 51-22-2A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1371C. CORROSION WAS REMOVED AND FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — DAMAGED (BS 468-565) · airframe 62,920 hrs · 45,156 cycles

LIGHTNING ON PREVIOUS REWORK AT FUSELAGE SKIN BS 465, 503 AND 565 BETWEEN LONGERON 3 - 4R. BLENDED OUT IAW SRM 53-04-1, PAR.5.

Part: CUSP WEB — CORRODED (BS 855-858) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 855-858, X -52 TO -60. AREA WAS REPARIED IAW SRM 53-05.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1410C. CORROSION WAS REMOVED AND FOUND OUT LIMITS. FUEL ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: BEAM — CRACKED · airframe 62,920 hrs · 45,156 cycles

CRACK ON ANGLE AND BEAM NR 1 AT L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-05D, FIG 97, SHEET 8.

Part: CUSP WEB — CORRODED (BS 693-748) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON RT CUSP WEB LOWER/UPPER SURFACE BETWEEN BS 693-700, 712-731 AND 739-748, X=-50 TO -60. TASK 53-037-02. BS 722-725 ARE OUT OF LIMITS.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,920 hrs · 45,156 cycles

DAMAGED METALIZED COATING ON RUDDER SKIN. RUDDER REPAIRED IAW SRM 57-70-1A, PAR 23.

Part: CUSP WEB — CORRODED (BS 722-725) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON CUSP WEB BETWEEN BS 722-725, X=-54 TO -60. TASK 53-037-02. REPAIRED IAW SRM 53-005, FIG 13 AND 51-30-02, 51-10-03.

Part: CUSP WEB — CORRODED (BS 807-905) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON RT CUSP WEB BETWEEN BS -52 TO -60, BS 807-826, 845-864, 886-905 CABIN FLOOR STRUCTURE. TASK 53-37-02. BS 855-858 OUT OF LIMITS WILL BE ATTENDED ON NRC 292.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD MID RIB AT LT SLAT PANEL NR 4. REPAIRED IAW SRM 57-02, PAR 9 AND ER/A 536464-14, REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 230-233) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON RT SEAT TRACK X -22 BETWEEN, BS 230-233. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: ACCESS PANEL — DAMAGED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION AND TOOL MARKS ON COUNTERSINK AND OTBD SKIN AT FUEL ACCESS NR 1361C, LW, AYP, CARD 154, ZONE 00, RII: N ENTR 146629 W SUMMARY, FUEL ACCESS PLATE 1361C IS OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 1081-1084) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 1081 - 1084 X=-54 TO -60. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-05 AND 51-10-03.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1476C, RT WING. ACCESS PLATE OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1307C, LW, CARD 149, ZONE 00, RII: N ENTR 181463 W, FUEL ACCESS PLATE 1307C IS OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 62,920 hrs · 45,156 cycles

CRACK ON FWD PAN SECTION AREA OF STOP FITTING NR 4 AT FWD CARGO DOOR. RII: N ENTR 983062 W SUMMARY: REPAIR WAS ACCOMPLISHED ON CRACK PAN OF STOP NR 4 IAW SRM 52-05 D, FIG 50 AND CRACK WAS FOUND 0.187 OF LENGTH.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1436C RT WING. ACCESS PLATE OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 693-700) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LT CUSP WEB FROM BS 693 - 700 AND X 54 - 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND 51-30-2 AND 51-10-3, PAR 21 AND 14 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 693-700) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LT CUSP WEB FROM BS 693 - 700 AND X 54 - 60 . CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-2, 51-10-3, PAR 21 AND 14 AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 779-781) · airframe 62,920 hrs · 45,156 cycles

CRACK ON RT CUSP WEB FROM BS 779 TO 781 AND X -54 TO -60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: ACCESS PANEL — DAMAGED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION AND TOOL MARKS ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1377C, LW, CARD 145, ZONE 00, RII: N ENTR 181463 W SUMMARY: FUEL ACCESS PLATE 1377C IS OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS NR 1470C, RT WING. ACCESS PLATE OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1464C RT WING. ACCESS PLATE IS OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 62,920 hrs · 45,156 cycles

TOOL DAMAGE ON OTBD SKIN OF FUEL ACCESS 1355C. FUEL ACCESS PLATE IS OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED STOP FITTING NR 1 AND 2 STA Y=427 AT FWD CARGO DOOR. STOP FITTING REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1456C, RT WING. ACCESS PLATE OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD MID, OTBD RIB HOLES AT RT SLAT PANEL NR 1, CARD 1 ZONE 12. RII: N ENTR 983062 WSUMMARY: CORROSION ON INBD, MID OTBD RIB HOLES AT RT SLAT PANEL NR 1 WAS REPAIRED IAW SRM 57-02, PAR 9.

Part: SKIN — WORN (BS 1300-1309) · airframe 62,920 hrs · 45,156 cycles

WEAR ON FUSELAGE SKIN REPAIR DOUBLER BETWEEN BS 1300-1309 AND LONGERONS 18 TO 20 RIGHT. PREVIOUS REPAIR DOUBLER WAS REMOVED AND NEW EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04-2, FIG 2, SHEET 9 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 1174-1193) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON RT CUSP WEB, BS X=-54 TO -60 AND Y= 1174 TO 1193. TASK 53-037-02. BS Y=1183 TO 1187 WAS FOUND TO BE OUT OF LIMITS.

Part: SKIN PANEL — CORRODED (RT WING) · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD, MID, OTBD RIB HOLES AT SLAT PANEL NR 2 RT SIDE. CORROSION ON INBD, MID, OTBD RIB HOLES AT SLAT PANEL NR 2 WAS REPAIRED IAW 57-02, PAR.9.

Part: CUSP WEB — CORRODED (BS 750-788) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON RIGHT CUSP WEB UPPER/LOWER SURFACE BETWEEN BS X=-54 TO -60 AND Y=750 TO 769, 769 TO 788, TASK 53-037-02. AREA IS WITHIN LIMITS BUT BS Y=779-781 WILL BE ATTENDED ON CARD 294.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD, MID RIB HOLES AT RT SLAT PANEL NR 4. CORROSION ON INBD, MID RIB HOLES AT RT SLAT PANEL NR 4 WAS REPAIRED IAW SRM 57-02, PA 9.

Part: BULKHEAD WEB — CORRODED (BS 1338) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON WEB OF AFT PRESSURE BULKHEAD OF BS 1338 BETWEEN LONGERONS 27L - 27R. BULKHEAD WEB WAS REPLACED IAW SRM 53-14-3, 51-30-2, 51-30-5 AND 51-10-3 PAR 21 AND 14.

Part: CUSP WEB — CRACKED (BS 905-910) · airframe 62,920 hrs · 45,156 cycles

CRACKED RT CUSP WEB BETWEEN BS X= -52 TO -55 AND Y= 905 TO 910. CUSP WEB WAS STOP DRILLED AND INSPECTION HFEC IAW SRM 51-01, PAR 21. FABRICATED DOUBLER OF REPAIR AND INSTALLED IAW SRM 53-05, FIGURE 131A-1.

Part: CUSP WEB — CORRODED (BS 200) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON CUSP WEB, BS 200 AND LBL 44 AT CABIN FLOOR STRUCTURE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 511165-14 MA, REV C AND SRM 51-70-04, FIG 2.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD/OTBD RIB HOLES AT RT SLAT PANEL. CORROSION REMOVED IAW PS 900-1-2-1 N 1 AND INSTALLED NEW BUSHINGS IAW SRM 57-02, PAR 9.

Part: CUSP WEB — CORRODED (BS 927-1003) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON RT CUSP WEB, UPPER/LOWER SURFACE BETWEEN BS X=-54 TO -60, Y=927-946, 946-965, 965-984, AND 984-1003, TASK 53-037-02. AREAS OUT OF LIMITS WILL BE ATTENDED WITH NRC 297 AND 298.

Part: ANGLE — CRACKED (BS 237) · airframe 62,920 hrs · 45,156 cycles

CRACKED FRAME ANGLE AT BS 237 BETWEEN LONGERONS 17 - 18L AT FUSELAGE CABIN STRUCTURE. FRAME ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3, PAR 14 AND 21.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED STOP FITTING PROJECTION BEAMS AFT EDGE AT AFT CARGO COMPARTMENT DOOR. RII: N ENTR 983062 W SUMMARY: STOP FITTING WAS REMOVED IAW SRM 51-30-1 AND 51-30-5 AND STOP FITTING WAS DRILLED IAW SRM 51-10-4 AND NEW STOP FITTING WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21 AND NEW STOP FITTING WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 66,137 hrs · 47,417 cycles

CORROSION ON FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED IAW DWG 9957828 REV Y AND SRM 51-10-3 PAR 14, 21.

Part: LONGERON — CRACKED (BS 237) · airframe 62,920 hrs · 45,156 cycles

CRACK ON LONGERON 17 LT AND BS 237 AT FUSELAGE CABIN STRUCTURE. SECTION OF LONGERON WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21, AND 51-30-2, 53-02, FIG 18.

Part: RIB — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON RIBS HOLES AT LT SLAT PANEL 1, CORROSION WAS REMOVED IAW REPAIR SRM 57-02, PAR 9.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL. THE FUEL ACCESS PANEL WAS FOUND OUT LIMITS AND REPLACED IAW SRM 51-22-2A.

Part: RIB — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD, MID, OTBD RIB HOLES AT RT SLAT PANEL NR 3. CORROSION WAS REMOVED AND FABRICATED BUSHINGS. INSTALLED NEW BUSHINGS IAW SRM 57-02, PAR 9.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON INBD, MID,OTBD RIBS HOLES AT LT SLAT PANEL NR 2, SM, CARD 19, ZONE 11. RII: N ENTR 537749 W SUMMARY: CORROSION ON INBD (MD) OUTBD RIBS HOLES AT LT SLAT 2 WAS REMOVED IAW SRM 57-02, PAR 9 HOLES WERE MEASURED AFTER REWORK OTBD RIB AFT HOLES ID: 0.938", INBD HOLE WITH ID: 0.941 AND FWD OTBD HOLE WITH ID: 0.9375, MID RIB AFT INBD HOLE WITH ID: 0.9375", AFT OTBD HOLE WITH ID: 0.938" FWD OUTBD HOLE WITH ID: 0.939" AND FWD INBD HOLE WITH 0.942", INBD RIB FWD HOLE WITH ID 1.1225" AND AFT HOLE WITH ID: 1.1235" THEREFORE WITHIN LIMITS OF MAX OF REPAR IAW SRM 57-02, PAR 9 BUSHINGS WERE FABRICATED IAW SRM 57-09, PAR 9.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL. FUEL ACCESS PANEL WAS FOUND OUT LIMITS AND REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1414C. FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER RT CUSP WEB BETWEEN X -54 TO -60 AND BS 446 - 465 AT PAX CABIN FLOOR STRUCTURE. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCES PANEL. FUEL ACCESS PANEL WAS FOUND TO BE OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 655-700) · airframe 63,075 hrs · 45,260 cycles

CORROSION ON LT CUSP WEB BETWEEN X=54 TO 60 AND BS 655 - 700 . AREAS WITH CORROSION WERE REWORKED IAW SRM 51-10-3 PAR 26, 21, 14 AND FASTENERS WERE INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 788-807) · airframe 62,920 hrs · 45,156 cycles

INITIAL CRACKED RT CUSP WEB BETWEEN X -44 TO -60 AND BS 788 - 807. THE CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131, A-24.

Part: SKIN — DAMAGED (BS 1300-1309) · airframe 62,920 hrs · 45,156 cycles

WEAR ON FUSELAGE SKIN REPAIR DOUBLER BETWEEN STA Y=1300-1309 AND LONGERON 18 RT TO 20 RT. PREVIOUS REPAIR DOUBLER WAS REMOVED AND NEW EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04-2, FIG 2, SHEET 9 AND 51-30-2 SET UP A DECAL CONDITION MONITOR A1 C-CHECK INTERVALS IAW TOPP 30-10-10, PAR "I".

Part: CUSP WEB — CORRODED (BS 680-693) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

INITIAL CORROSION ON RT CUSP WEB BETWEEN X -54 TO -60 AND BS 680 - 693. REPAIRED IAW SRM 51-10-3, PAR 14, 21, 38, 51-30-2, 51-30-8, 51-30-1 AND SRM 53-05, FIG 131A-1.

Part: CUSP WEB — CORRODED (BS 647-655) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

CORROSION ON LT CUSP WEB BETWEEN STA X=54 TO 60 AND Y=647 TO 655 AT PAX CABIN FLOOR STRUCTURE. RII:N ENTR 537749 W SUMMARY, CORROSION ON CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131-A.

Part: CUSP WEB — CORRODED (BS 733-739) · corrosion level 2 · airframe 62,920 hrs · 45,156 cycles

INITIAL CORROSION ON PREVIOUS REPAIR DOUBLER. RT CUSP WEB BETWEEN BS X=-54 TO -60 AND Y= 733 TO 739 AT PAX CABIN FLOOR STRUCTURE. PREVIOUS REPAIR WAS REPLACED, IAW SRM 53-05, FIG 131A-9.

Part: PAN — CRACKED (L4 DOOR) · airframe 62,920 hrs · 45,156 cycles

CRACKED DOOR PAN ON DOOR STOP NR 4 AT LT FWD OVERWING EMERGENCY EXIT DOOR. PAN WAS REPAIRED IAW SRM 52-050, FIG 51, 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3 PARA 14 AND 21. PRIMARY STRUCTURE, RII COMPLETED.

Part: WINDOW FRAME — CRACKED · airframe 62,920 hrs · 45,156 cycles

CRACK ON WINDOW RING PAN AFT UPPER CORNER, STA Y=408, Y=1022, Y=1041, Y=1060 AND Y=1098 AT PAX CABIN. WINDOW RING PAN AFT UPPER STA Y=408, Y=1022, Y=1041, Y=1060 AND Y=1098 WERE REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV A, ER/A 487747-14MA, REV.

Part: WINDOW FRAME — CRACKED · airframe 62,920 hrs · 45,156 cycles

CRACK ON WINDOW RING PAN FWD LOWER CORNER STA Y=946, Y=788, Y=984 AND Y=1022 AT PAX CABIN, CARD 73, ZONE 100. WINDOW RING PAN FWD LOWER CORNER STA Y=946, Y=788, Y=984 AND Y=1022 WERE REPAIRED IAW SRM 53-05, FIG.122 AND ER/A 493648-14MA, REV A ER/A 487747-14MA REV ORIGINAL ASSOCIATED ER/A 00-493648, ADDED FOR AC 0984.

Part: CUSP WEB — WORN (BS 465) · airframe 62,920 hrs · 45,156 cycles

WEAR ON LT CUSP WEB BS Y=465 BETWEEN X=44 TO 54 AT PAX CABIN FLOOR STRUCTURE. WEAR WAS BLENDED OUT IAW SRM 53-01, FIG. 1 AND REPAIRED AREA SRM 53-05, FIG 131A-1 AND SRM 51-10-3, PAR 21 AND 14 NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2 WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.020" AND REMAINING THICKNESS IS 0.010",THEREFORE, IS OUT OF LIMITS IAW ER/A 508307-14MA, REV. A.

Part: WINDOW FRAME — CRACKED · airframe 62,920 hrs · 45,156 cycles

CRACK ON WINDOW RING PAN AFT LOWER CORNER BS 905 AT PAX CABIN, CARD 72, ZONE 100. CRACK ON WINDOW RING PAN AFT LOWER CORNER ON BS Y=905 WAS REPAIRED IAW SRM 53-05 FIG.122 AND ER/A 493648-14MA, REV A, ER/A 487747-14MA, REV ORIGINAL.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 62,920 hrs · 45,156 cycles

CRACKED FLOOR PANEL PAX CABIN . FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: WINDOW FRAME — CRACKED · airframe 62,920 hrs · 45,156 cycles

CRACK ON WINDOW RING PAN AFT UPPER CORNER STA Y=1136, Y=1174, Y=1193, Y=1212 AND Y=1250 AT PAX CABIN, CARD 71, ZONE 100. WINDOW RING PAN AFT UPPER CORNER WERE REPAIRED IAW SRM 53-05, FIG. 122 AND ER/A 487747-14MA, REV. ORIGINAL ER/A 493648-14MA, REV. A ASSOCIATED ER/A 00-487747.

Part: CUSP WEB — PUNCTURED (BS 906) · airframe 62,920 hrs · 45,156 cycles

CRACKED LT CUSP WEB STA X=48 AND X=906 AT PAX CABIN FLOOR STRUCTURE. CRACKED ON CUSP WEB SIDE LT, THIS DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131-A-1, REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131-A-1, THIS PARTS WERE TREATED AND PAINTED IAW SRM 51-10-03, P.14 AND 21 AND REPAIR PARTS WERE INSTALLED IAW 51-30-02.

Part: CUSP WEB — PUNCTURED (BS 896) · airframe 62,920 hrs · 45,156 cycles

PUNCTURE ON LT CUSP WEB STA X=53 AND Y=896 AT PAX CABIN FLOOR STRUCTURE. DAMAGE WAS REMOVED-NEW PART REPAIR WAS FABRICATED -PART WAS TREATED AND PAINTED-NEW PART WAS INSTALLED IAW SRM 53-05, FIG 131 A-1, SRM 53-05, FIG 131 A-1 SRM 51-10-3, PAR 21, PAR 14 -SRM 53-05, FIG 131 A-1.

Part: TERMINAL — LOOSE (WINDOW HEAT) · airframe 61,989 hrs · 44,517 cycles

CREW RETURNED THE ACFT FOLLOWING A STRONG ODOR OF ELECTRICAL FUMES AS THEY CLIMBED THROUGH 1500 FT. SMOKE APPEARED NEAR RT UPPER CORNER OF THE COPILOTS WINDSCREEN. WINDOW HEAT WAS SECURED AND THE SMOKE DISSIPATED. MAINTENANCE FOUND THE TERMINAL BLOCK R5-38 MOUNT SCREW LOOSE AT TERMINAL P, WINDOW HEAT GROUND. CONTACT SURFACE BETWEEN BLOCK AND WINDSHIELD IS BURNED/ARCED. SECURED TERMINAL BLOCK SCREW AND RESET CB Z-24.

Part: FILTER — CLOGGED (NR 1 ENGINE OIL) · airframe 60,416 hrs · 43,415 cycles

DIVERTED DUE TO LT ENG OIL STRAINER CLOG MESSAGE. ENGINE AT IDLE. R & R NR 1 ENGINE OIL FILTER, R & R 1 ENGINE.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 59,852 hrs · 43,062 cycles

TAIL INTERIOR SHEAR TIE CRACKED ON FWD. SIDE OF FRAME BS 1380, BETWEEN L11-12R. REPAIRED IAW ERA 524366-14, REV ORIG.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 59,852 hrs · 43,062 cycles

CRACK FOUND DURING HFEC 06-10-01-001 ON NR 2 PYLON. REPAIRED IAW ERA 524353-14, REV ORIG.

Part: UNKNOWN — UNKNOWN (PITCH CONTROL) · airframe 58,846 hrs · 42,448 cycles

DIVERTED FLIGHT, UNCOMMANDED PITCH CONTROL ISSUES IN CRUISE. MAINTENANCE CHECKED LT AND RT TABS FOR FAIR, ELEVATOR BODY CABLE TENSIONS, AND USED THE RIG PIN R-2 FOR LT AND RT ELEVATOR SECTORS -ALL CHECKED GOOD. PERFORMED HORIZONTAL STABILIZER JACKSCREW AND NUT INSPECTION FOR WEAR AND THE ACTUATOR CHECKED GOOD. NO TROUBLE FOUND. LUBED STABILIZER JACKSCREW AND CHECKED FLIGHT RECORDER AND COCKPIT VOICE RECORDER READOUTS WITH NO ANOMALIES FOUND WITH EITHER. FUNCTIONAL CHECK FLIGHT PERFORMED WITH NO TROUBLE FOUND IAW LP NR 9978894.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,624 hrs · 42,277 cycles

PILOT DISCOVERED EXTERIOR OVERWING EMERGENCY LIGHTS WOULD REMAIN ILLUMINATED WHEN THE SWITCH IS PLACED IN THE ARM POSITION. REPLACED POWER SUPPLY AND BATTERY. OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,592 hrs · 42,251 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE FWD OVERWING ESCAPE HATCH IN THE CABIN WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,555 hrs · 42,218 cycles

DURING ROUTINE LINE CHECK, MX NOTED THE CEILING MOUNTED EMERGENCY EXIT LIGHTS WERE INOPERATIVE FROM ROW 2 THROUGH 24. THE EMERGENCY LIGHT BATTERIES WERE REPLACED AND OPS CHECKED NORMAL IAW AMM 33-50.

Part: CABLE — DISCONNECTED (CATWALK) · airframe 57,431 hrs · 41,446 cycles

FOUND VENTRAL STAIR TO CATWALK CABLE DISCONNECTED. THE VENTRAL STAIRS WERE PLACED ON MEL IAW 52-00-03. THE CABLE WAS LATER RECONNECTED DURING OVERNIGHT MX, THE MEL PLACARD WAS REMOVED AND OPERATION CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 56,950 hrs · 41,156 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE ENTRY WAY HAD FAILED. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: STOP — CORRODED (BULKHEAD DOOR) · airframe 56,332 hrs · 40,746 cycles

DOOR STOP CORROSION, AFT CABIN BULKHEAD DOOR, 2 EA ON BOTTOM OF DOOR. REMOVED DOOR STOPS AND REPLACED WITH NEW MPN 9915565-297 IAW CMM 52-63-1 AND DWG 9915565 DUE TO CORROSION OUT OF LIMITS.

Part: FRAME — CORRODED (BS 1309) · airframe 56,321 hrs · 40,739 cycles

AFT CARGO FRAME WEB LWR CORD CORROSION. STA 1309 LBL 12 TO RBL 12 AFT SIDE OF FRAME. BLENDED AREAS OF CORROSION. UT OF BLENDED AREAS IAW 04-00-07, FIG 3. FOUND .042 REMAINING MATERIAL AT BL-0, OUT OF LIMITS IAW SRM 53-01. CORROSION CONTAINED. PERFORMED REPAIR IAW SRM 53-03D, FIG 2A SHEETS 2 AND 5.

Part: SKIN — CRACKED (LT WING) · airframe 56,321 hrs · 40,739 cycles

LT UPPER WING SKIN STATION XFS = 533.220 CRACKED. REPAIRED IAW ERA 508040-14, LOG 0623358.

Part: CABLE — OUT OF LIMITS (TAIL CONE) · airframe 56,321 hrs · 40,739 cycles

PERFORMED TAILCONE RELEASE SYS OPS CHECK AND FOUND THE TAILCONE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS. THE LOCKING CABLE CLAMPS DID NOT CLEAR THE LOWER END OF THE CONDUITS BY AT LEAST .5" WITH LATCHES IN THE FULL OPEN POSITION. THE CABLE CONDUITS WERE ADJUSTED AND RIGGED BACK INTO SPECIFICATIONS IAW AMM 53-53-00.

Part: RELEASE CABLE — OUT OF LIMITS (TAIL CONE) · airframe 56,321 hrs · 40,739 cycles

PERFORMED TAILCONE RELEASE SYS FUNCTIONAL CHECK AND FOUND THAT THE AFT DOOR EMERGENCY HANDLE RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS. THIS DISCREPANCY IS THAT THE DOOR COULD BE OPENED WITH LESS THAN THE REQUIRED 8 POUNDS OF PULL FORCE. THE TAILCONE RELEASE SYSTEM CABLE WAS ADJUSTED AND RIGGED BACK INTO SPECIFICATIONS.

Part: SHEAR TIE — CORRODED (BS 1211) · airframe 56,321 hrs · 40,739 cycles

AFT CARGO FRAME SHEAR TIE HAS CORROSION, BS 1211, RBL 5. REMOVED SHEAR TIE, FOUND CORROSION IS OUT OF LIMITS IAW SRM 53-03-FIG 3. INSTALLED NEW SHEAR TIE IAW SRM 51-30, 868414.

Part: SHEAR TIE — CORRODED (BS 1211 RBL 5) · airframe 1 hrs · 1 cycles

AFT CARGO FRAME SHEAR TIE CORRODED STA.1211 RBL5. REPAIRED BY REPLACEMENT OF SHEAR TIE IAW SRM 53-03.

Part: STIFFENER — CRACKED (NLG WW) · airframe 56,321 hrs · 40,739 cycles

NLG W/W CUTOUT BOX WEB ON RT OTBD SIDE AT FWD FASTENER HOLE COMMON TO WHEEL ALIGNMENT VERT STIFFENER STA 47 IS CRACKED. STOP DRILLED CRACK, HFEC CHECKED, DAMAGE CONTAINED, INSTALLED DOUBLER REPAIR IAW SRM 53-05D, FIG 815D.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 56,101 hrs · 40,592 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 20 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A WIRE DISCONNECTED IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,981 hrs · 40,521 cycles

DURING LINE CHECK, MAINTENANCE THE FORWARD OVERWING EMERGENCY EXIT SIGNS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,575 hrs · 40,244 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE AFT SECTION OF THE CABIN TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,567 hrs · 40,238 cycles

DURING LINE CHECK, MAINTENANCE FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,565 hrs · 40,237 cycles

DURING CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT SIGN LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,411 hrs · 40,142 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY ESCAPE LIGHTING TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION AFTER A SUCCESSFUL FUNCTIONAL CHECK OF THE SYSTEM.

Part: PLATE — WORN (TAIL CONE) · airframe 55,308 hrs · 40,082 cycles

WHILE DOING TAILCONE FUNCTIONAL CHECK, OPN 6908 AD, INSPECTION WROTE UP TAILCONE ALIGNMENT PIN RECEPTACLES 20 EA AS WORN/ELONGATED. REPLACED 20 RECEPTACLES.

Part: POWERPACK — LEAKING (RUDDER) · airframe 55,308 hrs · 40,082 cycles

RUDDER POWER PACK LEAKING HYD FLUID AND CONTAMINATED TAILCONE SLIDE, STRAPS, AND DEPLOYMENT CABLE. RUDDER PCU WAS REPLACED PER MM. ALSO, REPLACED SLIDE, SLIDE COVER, WASHED CATWALK, AND REPLACED ANTI SKID TAPE.

Part: BRACKET — CRACKED (TAILCONE) · airframe 55,308 hrs · 40,082 cycles

DURING INSPECTION, BOTH OF THE UPPER LATCH SUPPORT BRACKETS WERE FOUND TO BE CRACKED. MAINTENANCE INSTALLED NEW BRACKETS FOR BOTH POSITIONS PER DRAWING 9911957.

Part: FRAME — CRACKED (BS 1510) · airframe 55,308 hrs · 40,082 cycles

FRAME 1510 CRACKED AT 2 O`CLOCK POSITION AT TAILCONE ALIGNMENT PIN. INSTALLED DOUBLER PER ER/A 503339-14.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 54,644 hrs · 39,684 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 12DE IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE SEAT WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,885 hrs · 39,186 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE FORWARD HALF OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,885 hrs · 39,186 cycles

FLOOR PANEL 107B HAS SEVERAL DENTS AND PUNCTURE. FABRICATED FLOOR PANEL 1079BIN REF TO TRAVELER 89024020001 DWG 9936654 REV S AND MS88 MM 53-20-01-201. AT SAA/SAT DURING HMV ON W/O 89028960001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,885 hrs · 39,186 cycles

CORROSION ON FLOOR STRUCTURE FROM STA 140-200 LBL 7. REMOVED CORROSION AT STA 140-200 LBL 7, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT AT STA 140-200, LBL 7 IAW DC9/MD80 SRM 51-30-01.

Part: LIFE RAFT — DAMAGED (CABIN) · airframe 53,885 hrs · 39,186 cycles

LIFE RAFT HAS A HOLE IN IT. REPLACED LIFE RAFT P/N 4600-117. DURING AT SAA SAN ANTONIO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,885 hrs · 39,186 cycles

CORROSION ON FLOOR STRUCTURE FROM STA 140-200 RBL 7. REMOVED CORROSION ON FLOOR SUPPORT, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW FLOOR SUPPORT AT STA 140-200 RBL 7 I AW DC9/MD80 SRM 51-30-01 PG 11-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,885 hrs · 39,186 cycles

FOUND SEAT TRACK AT LBL 22 CORRODED BETWEEN STA 1212-1231 WHILE WORKING SEAT TRACK MOD. REMOVED SEAT TRACK SECTION BETWEEN STA 1193-1212 LBL 22, FABRICATED SPLICE PLATE AND SEAT TRACK AND INSTALLED PER DC9/MD80 SRM 53-05 FIG 4F AT SAA SAT.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 53,499 hrs · 38,929 cycles

DURING LINE CHECK, MAINTENANCE FOUND ROW 19DE EMERGENCY PATHWAY LIGHTS INOPERATIVE. MAINTENANCE REPLACED SEAT HARNESS. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,212 hrs · 38,717 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHT AT SEAT 3 CD MISSING. MAINTENANCE INSTALLED NEW LIGHT ASSEMBLY PER MD88 AMM 33-50. OPERATION OF LIGHT NOW CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,684 hrs · 38,363 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT 14D INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AT 14D. OPERATION OF LIGHT NOW CHECKS OK.

Part: PAN — CRACKED (LAVATORY) · airframe 51,502 hrs · 37,636 cycles

FWD LAV PANEL PAN CUTOUT CRACKED AT UPPER AFT EDGE. REPAIRED IAW ER/A 485789-14 REV ORIG.

Part: SENSE LINE — LOOSE (AC BAY) · airframe 50,948 hrs · 37,295 cycles

CREW REPORTED HAZE/SMOKE IN THE CABIN ON CLIMBOUT AND APPROACH WITH AN ASSOCIATED "AIR COND RT TEMP HIGH" LIGHT ON. THE CREW TURNED OFF THE RIGHT HP BLEED WHICH RESULTED IN THE TEMPERATURE AND AC PRESSURE RETURNING TO NORMAL. THE HAZE QUICKLY CLEARED SOON AFTER. MAINTENANCE FOUND THE DOWNSTREAM SENSE LINE TO THE RIGHT AUGMENTATION VALVE LOOSE AND SECURED IT. COMPLIED WITH THE OPN 5089 PNEUMATIC SYSTEM DUCT BURN OUT PROCEDURES, AS WELL AS OPNS 5009, 5088 AND 5010 (2010-D0803)(DLM88101778).

Part: UNKNOWN — ODOR (CABIN) · airframe 50,944 hrs · 37,293 cycles

AFTER TAKEOFF STRONG ODOR IN CABIN SMOKE/HAZE DETECTORS ACTIVATED SMOKE STOPPED WITH PACKS OFF A/C ATB TO LGA (DLM88101763).

Part: TRANSFORMER — OVERHEATED (AFT GALLEY LIGHT) · airframe 49,660 hrs · 36,506 cycles

F/A`S REPORT BURNING ODOR FWD OF AFT GALLEY. OPENED SEVERAL CABIN CEILING PANELS CLOSED CABIN CEILING AND ACCESS PANELS FOUND READING LIGHT TRANSFORMER T1-106 VERY WARM REPLACED TRANSFORMER PERF OP 5088 NOP TROUBLE FOUND PERF OP 5089 PNEU SYS DUCT BURNOUT INSP ENTIRE CABIN AND GALLEYS NO ODOR PRESENT ACFT OK FOR SERVICE.

Part: TRANSFORMER — ODOR (MID CABIN LIGHTS) · airframe 49,660 hrs · 36,506 cycles

F/A`S REPORT BURNING ODOR AFT GALLEY. OPENED SEVERAL CLOSED CABIN CEILING AND ACCESS PANELS FOUND READING LIGHTS TRANSFORMER T1-106 VERY WARM REPLACED TRANSFORMER. PERFORMED OPN 5088 NO TROUBLE FOUND PERF OPN 5089 PNEU DUCT BURNOUT INSPECTED ENTIRE CABIN AND GALLEYS NO ODOR PRESENT. ACFT OK FOR SERVICE.

Part: BLANKET — CORRODED (RT WING) · airframe 48,736 hrs · 35,906 cycles

RT WING HEATER BLANKET AFT ACCESS CUTOUT HAS CORROSION AROUND TOP SIDE. HEATER BLANKET REPLACED ON 1792N01178.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

AFT CARGO LEFT LONGERON 29 BETWEEN STA 1136-1155 INTERCOSTAL HAS CORROSION. REPLACED INTERCOSTAL.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

FWD CARGO FS 370-408 DOOR CUT OUT LOWER JAMB HAS CORROSION SEVERAL PLACES MRB 53-139-05.

Part: FORMER — CRACKED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

MAIN CABIN STA 617 BETWEEN L15L - L16L FORMER IS CRACKED. REPLACED FORMER.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 48,736 hrs · 35,906 cycles

FWD WET AREA FLOOR PANEL 160G HAS CORROSION. REPLACED PANEL IAW SRM 51-10-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

CABIN STA 1174 LBL 56 UNDER O/B SEAT TRACK AFT OF L2 DOOR CUSP WEB HAS CORROSION AT SKIN LAP. REPLACED CUSP WEB.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

AFT ACCESSORY STA 1510 L7R ATTACHMENT FRAME HAS APPROX 1 INCH CRACK IN RADIUS AT AFT END. INTERCOSTAL REPLACED ON NR 1792N00983.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

MAIN CABIN INTERIOR FUSELAGE ATTACH FITTING FS 1156 AT LONGERON 18R, ATTACH FITTING HAS CORROSION. REPLACED FITTING.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

MAIN CABIN STA 427-446 LT CUSP WEB HAS CORROSION. REPLACED CUSP WEB.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

AFT CARGO COMPARTMENT CORROSION ON STRINGER BS 1278-1294 STRINGER 26L.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

FS 986 LBL 7 FWD KEEL ANGLE CRACKED. REPLACED ANGLE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

AFT ACCY DURING NDT INSP OF RT DORSAL FIN ATTACH FITTING FOUND SHEAR TIE I/B OF FITTING CRACKED APPROX 2 INCHES, END OF CRACKED MARKED. REPLACED SHEAR TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

CRACKED SHEAR TIE I/B DORSAL FITTING. REPLACED SHEAR TIE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

AFT CARGO FS 1147 AND 1155 RIGHT LONGERON 29 AND 30 INTERCOSTAL CORRODED. REPLACED INTERCOSTAL IAW SRM 51-30-5/51-30-2.

Part: WEB — CORRODED (FUSELAGE) · airframe 48,736 hrs · 35,906 cycles

AFT CARGO FS 1212 AND 1220 RT LONGERON 26 AND 29 WEB CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 48,606 hrs · 35,821 cycles

RIGHT HORIZ STAB UPPER AFT SKIN PANEL / INBOARD END CRACKED. SKIN REPLACED IAW ER/A 460410-14AD REV B ON PEMCO PD 1000-3 ROUTINE 1792R840.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,623 hrs · 33,997 cycles

LIGHTNING STRIKE FOUND ON UPPER AFT CORNER OF WINDOW 21L CUTOUT. AREA BLENDED AND INSPECTED.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 42,426 hrs · 31,969 cycles

HORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL CRACK REPAIR. THE UPPER AFT SKIN OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .625" CRACK NEAR INBD AFT EDGE OF THE PANEL. THE CRACK WAS ROUTED OUT WITH A SMALL CUTOUT ON A TIME LIMITED BASIS PER ER/A 460410-14. PERMANENT REPAIR REQUIRES REPLACEMENT OF THE SKIN PANEL.

Part: SKIN — DAMAGED (FS 294-332) · airframe 39,489 hrs · 29,950 cycles

LIGHTNING STRUCK THE FUSELAGE AT SEVERAL PLACES ON THE WINDOW BELT SKIN BETWEEN FS 294-332, RT SIDE. THE DAMAGE WAS BLENDED AND THE AREAS TREATED AND INSPECTED TO ENSURE ALL DAMAGE WAS REMOVED.

Part: CONDUIT — DAMAGED (LT MLG WW) · airframe 34,673 hrs · 26,475 cycles

AFTER T/O FROM RSW HAD A LT GEAR UNSAFE LIGHT. CYCLED GEAR HANDLE, NO HELP. DIVERTED TO MCO. FOUND LT GEAR CONDUIT DAMAGED AND INTERFERRING WITH GEAR. PINNED AND SAFTIED LANDING GEAR. MTC FERRY A/C TO ATL FOR GEAR MTC.

Part: DUCT — BROKEN (NR 1 ENGINE) · airframe 34,057 hrs · 26,052 cycles

NR 1 ENGINE, INBOARD SIDE 8TH STAGE ENGINE ANTI ICE DUCT IS BROKEN. REPLACED DUCT.

Part: RELIEF VALVE — FAULTY (NR 1 ENGINE) · airframe 28,989 hrs · 22,486 cycles

INFLIGHT NR 1 ENG OIL PRESSURE 65 PSI AND FLASHING. REPLACED PRESSURE RELIEF VALVE. RAN ENG, OPN CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,415 hrs · 22,065 cycles

EMERGENCY LIGHT ON SEAT ROW 21DE INOP. RELAMPED, OPS NORMAL.

Part: BPCU — FAULTY (E/E BAY) · airframe 27,665 hrs · 21,534 cycles

LT BUS POWER INTERUPTIONS AT 33000 FT. RAN AC POWER INTER- CHECKLIST. APU WAS STARTED AND EMERGENCY DECLARED AND A DESCENT INTO PHL. PHL MTC FOUND LEFT ENGINE FREQS AT 383 ON ENGINE RUN. WOULD NOT HOLD BUS WHEN LOADED DOWN. REPLACED BUSS POWER CONTROL UNIT.

Part: PAN — CORRODED (C-1) · airframe 26,982 hrs · 21,033 cycles

C-1 DOORWAY THRESHOLD JAMB PAN CORRODED BEYOND LIMITS. REPAIRED PER MD-80 DRD 53-05-D FIG 804D.

Part: BRACKET — CORRODED (LT HORIZ STAB)

XE225.834 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORIZ STAB WAS FOUND TO CONTAIN CORROSION. REPAIRED AND REWORKED PER ERA 331301-14.

Part: FRAME — CRACKED (BS 1418)

FS 1418 WAS CRACKED AT L2L ON, WHICH IS ONE OF THE TYP LOCATIONS. REPAIRED PER ERA 331297-14.

Part: BRACKET — CORRODED (LT HORIZ STAB)

THE XE204.114 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORIZ STAB WAS FOUND TO HAVE CORROSION. REPAIRED AND REWORKED PER ERA 331309-14.

Part: CLEVIS — SHEARED (AIRSTAIR DOOR)

DURING FLIGHT, AC WAS PASSING THROUGH 34,000 FT WHEN THEY EXPERIENCED DEPRESSURIZATION AND GOT A FWD STAIRWAY DOOR WARNING LIGHT. THE CREW DIVERTED TO DCA AND FERRIED THE AC TO TPA. TPA MTC FOUND THE AFT 2 CLEVIS BOLTS OF THE FWD AIRSTAIR DOOR SHEARED. REPLACED AFT 2 CLEVIS BOLTS PER MTC MNL,M/M 52-62-00.

Part: PROX SENSOR — MALFUNCTIONED (RT MLG)

AMBER GEAR DOOR OPEN LIGHT STAYED ON AFTER GEAR RETRACTION. MAINTENANCE IN PROGRESS, REPLACED RIGHT GEAR DOOR PROX SENSOR. SWUNG GEAR CHECKS OK.

Part: ENGINE — FOD (NR 1)

AT 35,000 FEET, HEARD/FELT LOUD THUMP FROM LT SIDE. LT ENGINE INSTRUMENTS ROLLED BACK ON ITS OWN; REDUCED LT THROTTLE TO IDLE THEN SHUT DOWN BY CHECK LIST. INSP INLET AND EXHAUST-ALL OK-REPLACED LT INLET COWL AND NOSE BULLET. EPR LEAK CKS GOOD. BORESCOPED 6TH/7TH STAGE OF COMPRESSOR. ALL OK. RAN ENG TO TAKEOFF POWER. ALL IND NORMAL. ALSO REPLACED F/C LAV TANK ASSY DUE TO PREVIOUS WRITE-UPS ON LAV LEAKAGE. PRESS A/C, LEAK CKS OK. CLEANED BLUE STREAK FROM FUSELAGE AREAS. ENGINE TOTAL CYCLES, 13,376.

Part: BULB — MISSING (CABIN)

EMERGENCY LIGHT AT ROW 21CD MISSING. REPLACED PIGTAIL BULB AND LENS.

Part: CSD — FAILED (NR 2 ENGINE)

AT 33,000 FT RT GEN VOLTS AND FREQS UNSTABLE AND DROPPED OFF LINE. RT CSD OIL TEMP WENT OFF SCALE ABOVE RED LINE. TRIED TO DISCONNECT CSD, WOULD NOT DISCONNECT. REPLACED NR 2 ENG CSD AND GEN, CSD GARLOCK SEAL. FLUSHED OIL, COOLER LINES, RAN ENG, OPN NORMAL.

Part: DNLOCK SWITCH — FAILED (NLG)

NLG GREEN LIGHT DID NOT ILLUMINATE WITH GEAR HANDLE EXTENDED. NLG WAS UP AND RED LIGHT WAS NOT ON. AFTER 2 ANNUN/OIG LIGHT TESTS, GREEN LIGHT ILLUMINATED NORMALLY. REMOVED AND REPLACED S1-412 NLG DOWN AND LOCKED SWITCH. JACKED AND SWUNG NLG SEVERAL TIMES, ALL INDICATIONS NORMAL.

Part: STRIKER ANGLE — CRACKED (LT MLG W.W.)

ITEM DEFERRED FROM C-2 CHECK 07/25/94, TIME LIMITED REPAIR INSTALLED AT LEFT MLG WHEEL WELL AFT O/B STRIKER ANGLE PER SRM 53-05 FIG 81A. INSTALLED PERMANENT REPAIR PER SRM 53-05 FIG 81A.

Part: NOSE COWL — DELAMINATED (NR 1 ENG)

FOUND DURING D-1 LETTER CHECK, SOUND SUPPRESSION SCREEN DELAMINATED AT 0300 POSITION INSIDE NOSE COWL. REPAIRED PER SRM 54-04A.