N933DL

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 75,167 hrs · 56,490 cycles

WHILE C/W PACK CONFIDENCE CHECK, FOUND A LARGE LEAK AT THE TOP OF AFT BAG BIN DOOR. 6 IN CRACK IN TOP OF BAG BIN DOOR. DOOR WAS REPLACED IAW AMM 52-31.

Part: BALLAST — MISWIRED (CABIN LIGHTS) · airframe 73,907 hrs · 55,436 cycles

AFT STAIRWAY FLUORESCENT LIGHT FOUND INOPERATIVE. FOUND THE BALLAST MISWIRED. CONNECTED LEFT BALLAST IAW WDM 33-23-01. OPS CHECKED OK.

Part: LIGHT — SPARKS (COCKPIT) · airframe 72,586 hrs · 54,484 cycles

FIRST OFFICER`S FLIGHT KIT LIGHT SPARKED IN FLIGHT. R & R THE LIGHT IAW AMM 33-10-00 OPS CHECKED OK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 71,751 hrs · 53,851 cycles

ROW 20ED EMERGENCY SEAT LIGHT INOPERATIVE. REMOVED & REPLACED UNDERSEAT HARNESS. OPS CHECK GOOD.

Part: ACM — CONTAMINATED (RIGHT) · airframe 71,716 hrs · 53,826 cycles

ACFT DIVERTED DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND LIGHT OIL FILM ON EXIT OF RIGHT ACM. REPLACED RIGHT ACM PER AMM. COMPLIED WITH DUCT BURNOUT, NO SMOKE OR ODOR NOTED. THE AIRCRAFT RETURNED TO SERVICE.

Part: OIL CAP — DETACHED (APU) · airframe 71,716 hrs · 53,826 cycles

RETURNED DUE TO SMOKE IN THE AFT CABIN. MAINTENANCE FOUND APU INLET CONTAMINATED WITH OIL. MAINTENANCE FOUND OIL CAP OFF. CLEANED APU INLET AND DUCTS AND COMPLIED WITH DUCT BURNOUT. AIRCRAFT WAS RETURNED TO SERVICE.

Part: HYDRAULIC SYSTEM — CONTAMINATED · airframe 71,241 hrs · 53,474 cycles

ENROUTE RT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MAN. RT HYD PRESSURE "0" , HYD QTY INITIALLY WENT TO 3 QTS THEN TO 19 QTS. FOLLOWED QRH PROCEDURE NORMAL LANDING AND CONFIGURATION. FOUND BOTH HYD SYS REQUIRED BLEED DUE TO AIR IN SYS. REPLACED RT HYD FILTERS AND FOUND NO DEBRIS. SERVICED SYS AND RAN ENGINE AND CYCLES ALL SYSTEMS. ALL PRESSURES CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,153 hrs · 53,406 cycles

MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROWS 11 AND 15. THE BATTERY PACK BATTERIES WERE REPLACED. THE LIGHTS CHECKED OK.

Part: RUDDER PEDAL — BINDING (COCKPIT) · airframe 70,535 hrs · 52,976 cycles

CAPT RUDDER PEDALS BIND AT HALF TRAVEL. FOUND CABLE ATTACH BOLT COTTER PIN EATCHING ON PLASTIC SESRIS COVER REMOVED BOLT. OK TO INSTALL. CAPT RUDDER PEDAL CABLE 2A BOLT INSTALLED BOLT IAW AMM 27-20. OPS CHECK GOOD.

Part: ACCESS DOOR — CRACKED (POTABLE WATER) · airframe 72,516 hrs · 54,434 cycles

CRACK AND CORROSION ON POTABLE WATER SERVICE ACCESS DOOR. CRACK AND CORROSION WERE ATTENDED WITH ER/A.

Part: SKIN — CRACKED (BS 1463) · airframe 70,508 hrs · 52,954 cycles

CRACKED PREVIOUS REPAIR DOUBLER ON INNER FUSELAGE SKIN BETWEEN LONGERONS 2L-2R NEXT TO BS 1463. DAMAGE AREA WAS REPAIRED IAW ER/A 541633-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 295-296) · airframe 70,508 hrs · 52,954 cycles

ELONGATED FASTENERS HOLE ON FUSELAGE SKIN AT BELLY DRAIN ATTACHMENT POINT BS 295-296 BETWEEN LONGERON 30 AND 29 LT C1 CARGO. DAMAGE WAS CUT OUT REPAIR PARTS WERE FABRICATED, TREATED AND PAINTED REPAIR PARTS WERE INSTALLED IAW SRM 53-04-2, FIG 2, 51-10-3 PAR 21, 14, 51-30-5, 51-30-2.

Part: SKIN — CRACKED (BS 1309) · airframe 70,506 hrs · 52,953 cycles

CRACK ON FUSELAGE SKIN BS 1309 BETWEEN LONGERONS 6 - 7L. REPAIRED IAW ETI-88-16-035 R2 AND ER/A 541634-14, REV. ORIGINAL.

Part: VANE — WORN (RT WING TE FLAP) · airframe 70,506 hrs · 52,953 cycles

WEAR ON PREVIOUS REPAIR DOUBLER ON MID FLAP VANE GUIDE AT RT WING OTBD FLAP. MID FLAP VANE GUIDE AT RT WING OTBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: WEB — CRACKED (BS 1485) · airframe 70,506 hrs · 52,953 cycles

CRACKED MEMBRANE OF BS 1485 AFT FACE AND 2HRS POSITION. CRACK WAS STOPPED AND REPAIRED ON MEMBRANE IAW SRM 51-01, PAR 21 AND SRM 53-01, FIG 2.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 70,506 hrs · 52,953 cycles

CRACKED INNER ANGLE ON DORSAL FIN, REF BS 1427 BETWEEN LONGERONS 1 AND 2 RT. ANGLES WERE REPLACED IAW DWG 5912188 AND SRM 51-30-5.

Part: FRAME — CRACKED (PAX DOOR) · airframe 70,506 hrs · 52,953 cycles

CRACKED FRAME NR 8 ON AFTER EDGE AREA OF FWD ENTRY DOOR. FRAME NR 8 OF FWD ENTRY DOOR WAS REPAIRED IAW SRM 52-05D, FIG 111.

Part: SKIN — DAMAGED (BS 1155-1174) · airframe 70,506 hrs · 52,953 cycles

SCRATCH ON RT WINDOW BELT BETWEEN BS 1155 - 1174 UPPER SURFACE. SCRATCHES WERE BLEND OUT FOUND WITHIN LIMITS IAW SRM 53-05, FIG 111 AND ER/A 543131.14, REV ORIGINAL. AREAS WERE TREATED IAW SRM 51-10-03, PAR 21.

Part: LONGERON — CRACKED (BS 160) · airframe 70,506 hrs · 52,953 cycles

CRACK ON LONGERON 4LT BS 160 AT CPAX. CEILING PANEL AT LONGERON 4 LT 160 WAS REMOVED IAW AMM 20-30-01-201, FASTENERS WERE REMOVED IAW SRM 51-30-5, HFEC INSPECTION ACCOMPLISHED IAW DC/MD NDTSPM 06-10-01- 001. NO CRACKS WERE FOUND CEILING PANEL, WAS RE-INSTALLED IAW AMM 20-30-01.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 70,506 hrs · 52,953 cycles

CRACKED AFTER PAN REPAIR DOUBLER BETWEEN FRI 5/6 AT ROLLER TRACK AREA OF FWD ENTRY DOOR. DOUBLER WAS REPLACED IAW SRM 51-30-2, 51-30-1, 51-30-4, 51-10-2, 51-10-3 PAR 14 AND 21 AND DWG 5914121, REV AV.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 70,506 hrs · 52,953 cycles

CRACKED INTERCOSTAL BETWEEN FRAME 4/5 ON COVER HANDLE ATTACHMENT AREA OF FWD ENTRY DOOR. INSTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR 14/21 AND 51-10-4.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 70,506 hrs · 52,953 cycles

DAMAGE FUEL SECOND ACCESS PLATE 1307C. FUEL SECOND ACCESS PLATE WAS REPLACED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,216 hrs · 54,907 cycles

ER/A 538941-14 SECTION 1 ACCOMPLISHED AND CLASSIFIED AS A MAJOR REPAIR. CRACK IN THE FUSELAGE SKIN NEAR THE AFT LAV SERVICE DOOR CUTOUT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,513 hrs · 52,224 cycles

PRIOR TO PUSH BACK, GROUND CREW FOUND A CRACK AROUND THE AFT LAV SERVICE RECEPTICLE SKIN. COMPLIED WITH ERA 538941-14, REV "ORIGINAL.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 68,926 hrs · 51,821 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 26D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND WIRES PULLED OUT OF THE LIGHT SOCKET. THE LIGHT ASSEMBLY WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: LANYARD — DAMAGED (PAX DOOR SLIDE) · airframe 67,906 hrs · 51,113 cycles

DURING EMERGENCY EQUIPMENT CHECK FOUND PAX DOOR SLIDE LANYARD FRAYED AND DAMAGED. REPLACED LANYARD IAW AMM 25-62-00.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 67,608 hrs · 50,904 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24DE WAS INOPERATIVE. FOUND WIRES BROKEN IN THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,895 hrs · 50,383 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN ROWS 14-22 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SHEAR TIE — CORRODED (BS 1830) · airframe 65,496 hrs · 49,421 cycles

SHEAR TIE CRACKED BS 1830 & L14L. REPAIRED IAW ER/A 522746-14 REV ORIG.

Part: SKIN — CRACKED (BS 1380) · airframe 65,496 hrs · 49,421 cycles

FUSELAGE SKIN CRACKED IN TWO PLACES BETWEEN L13-14L BS 1380. HFEC CHECKED IAW NDTSPM 06-10-01.001. REPAIRED IAW PRI 522688-14, REV 0.

Part: CAM — DAMAGED (TAILCONE RELEASE) · airframe 65,496 hrs · 49,421 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS MISSING HARDWARE; WHICH CAUSED IT TO BE OUT OF ALLOWABLE RIG LIMITS, EXCESSIVE FORE & AFT PLAY. THE CAM BASE WAS REPLACED AND MISSING SPACERS/SHIMS WERE THEN INSTALLED. THE SYSTEM WAS RIGGED TO SPECIFICATIONS AND THE RII WAS SATISFACTORY.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 65,496 hrs · 49,421 cycles

MAINTENANCE DISCOVERED THAT BOTH THE LT UPPER AND THE RT UPPER RELEASE SPADE RECEPTACLE FOR THE TAILCONE WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 63,940 hrs · 48,316 cycles

DURING LINE CHECK, MX FOUND THAT NUMEROUS OVERHEAD EMERGENCY LIGHTS FAILED. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,579 hrs · 48,037 cycles

CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE SEAT 01C WAS INOPERATIVE DURING THE FLIGHT. MX INSTALLED THE EXIT SIGN ON THE RT SIDE OF THE FRONT CABIN ABOVE 01C.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,381 hrs · 47,897 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN OVER THE FWD OVERWING EXIT HATCH WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 62,466 hrs · 47,261 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 34, 35, & 36 OF THE CABIN WERE INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: SEAT TRACK — CORRODED (BS 541-799) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN SEAT TRACK AT LBL 22 HAS CORROSION GOUGES AND BARE METAL FROM BS 541 TO 799. REPAIRED IAW SRM 53-01, FIG 4F.

Part: SEAT TRACK — CRACKED (BS 218-627) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN RT RBL 55 OTBD SEAT TRACK HAS SEVERAL AREAS WITH CORROSION GOUGES AND BARE METAL BS 218 TO 627. REPAIRED IAW SRM 53-05, FIG 4F.

Part: FRAME — CRACKED (BS 1401) · airframe 62,350 hrs · 47,172 cycles

AFT VENTRAL AREA FRAME CRACKED IN RADIUS STA 1401 LONGERON. REPAIRED IAW ER/A 507873-14, REV ORIGINAL.

Part: DOOR FRAME — CRACKED (FWD CARGO) · airframe 62,350 hrs · 47,172 cycles

WHILE ACCOMPLISHING NDT INSPECTION, OPEN NR 87052 AD DETECTED1 EA CRACK AT FWD CARGO DOOR JAMB AFT LOWER CORNER .5 INCH CRACK EMANATES FROM EDGE OF DOOR JAMB OPENING TO FASTENER HOLE ON EXTERNAL SKIN. REPAIRED IAW ER/A 507054-14MA REV ORIG.

Part: CUSP WEB — CORRODED (BS 1136-1174) · airframe 62,350 hrs · 47,172 cycles

LEFT CUSP MEMBRANE BS 1136 TO 1174 X=44 TO 58 HAS COROSION AT NUMEROUS LOCATIONS INCLUDING DOUBLER. REPLACED DOUBLER IAW SRM 53-14, RIG 12 AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 1309-1338) · airframe 62,350 hrs · 47,172 cycles

LT AFT LAV AFTER REMOVAL OF LONGITUDINAL FLOOR SUPPORT. CHANNELS AT STA 1309 TO 1338 X 17 FOUND CORROSION AT MOUNT HOLES AT STA 1309 AND 1322 FLOORBEAM, 4 EA HOLES. REPAIRED IAW SRM 53-05, FIG 79A.

Part: SEAT TRACK — CORRODED (BS 945-1031) · airframe 62,350 hrs · 47,172 cycles

LEFT SEAT TRACK X=22 BS 945 TO 1031 SEGMENT HAS CORROSION AND COUGES. INSTALLED AFT SPLICE FITTING AND SEAT TRACK IAW SRM 51-3-10 AND 51-10-4.

Part: CUSP WEB — CORRODED (BS 522-541) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN RT STA 522 TO 541 CUSP WEB HAS SEVERAL AREAS WITH CORROSION. REPAIRED IAW SRM 51-30-2.

Part: LONGERON SPLICE — CORRODED (BS 1240 L30) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO LONGERON 30 SPLICE FITTING T/E FLANGE IN CHANNEL HAS CORROSION AT BS 1240. INSTALLED NEW SPLICE FITTING ON L30 AT BS 1196 TO 1244 IAW SRM 53-02, FIG 16 PG43.

Part: SEAT TRACK — CORRODED (BS 722-799) · airframe 62,350 hrs · 47,172 cycles

SEAT TRACK AT RBL 55 HAS CORROSION, GOUGES AND BARE METAL FROM BS 722 TO 799. INSTALLED NEW SEAT TRACK FS 550-799 RBL 54 IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 1031-1309) · airframe 62,350 hrs · 47,172 cycles

CABIN SEAT TRACK RT SEGMENT BS 1031-1309, X=-22 HAS CHAFE DAMAGE, CORROSION, AND SCRIBE MARKS. INSTALLED SEAT TRACK FROM TS 1260-1309 RBL22 IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN SEAT TRACK AT LBL 22 HAS CORROSION, GOUGES, AND BARE METAL FROM STA 799 TO STA 937. INSTALLED NEW SEAT TRACK LB L22 STA 799-937 IAW SRM 51-30-1.

Part: FLOORBEAM — CORRODED (BS 1079) · airframe 62,350 hrs · 47,172 cycles

CABIN FLOOR SUPPORT STA 1079 X=22 TO -22 HAS CORROSION AT PANEL MOUNT HOLES ON LOWER SIDE. REPLACED FLOOR SUPPORT IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 799-937) · airframe 62,350 hrs · 47,172 cycles

AFTER REMOVAL OF SEAT TRACK AT X 54 STA 799-937 ON CUSP WEB MEMBRANE FOUND 1EA SHEARED RIVET ON DOUBLER AT STA 905 1EA LOC OF CORROSION AND 1EA CRACK AT STA 866 AND CORROSION AT STA 864 AND 845. REPLACED WEB IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 945-1031) · airframe 62,350 hrs · 47,172 cycles

RIGHT SEAT TRACK AT X=-22 STA 945 TO 1031 SEGMENT HAS CORROSION. INSTALLED NEW SEAT TRACK RBL 22 STA 937 TO 1031 SEGMENT IAW SRM 51-30-5.

Part: LONGERON — CRACKED (BS 200 L4L) · airframe 62,350 hrs · 47,172 cycles

LONGERON 4L CRACKED BS 200. REPAIRED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 1162-1174) · airframe 62,350 hrs · 47,172 cycles

RT CUSP WEB MEMBRANE STA 1136 TO 1174 HAS CORROSION ON TOP SIDE AT 8 EA LOCATIONS INCLUDING DOUBLER OTBD OF SEAT TRACK AT X 54 AND 1 EA DING AT STA 1162. REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 693-731) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN CUSP WEB HAS CORROSION FROM BS 693 TO 731. REPLACED IAW SRM 51-10-4.

Part: CUSP WEB — CORRODED (BS 1060-1098) · airframe 62,350 hrs · 47,172 cycles

LT CUSP MEMBRANE BS 1060-1098 HAS CORROSION AT STA 1061, 1079, AND 1085. INSTALLED CUSP WEB, FRAME FEET FITTINGS AND CUSP SPLICE ANGLE IAW SRM 51-30-2, 51-30-5, 51-30-1 STA 1022 -1098.

Part: SEAT TRACK — CORRODED (BS 541-799) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN SEAT TRACK AT RBL 22 HAS COROSION GOUGES AND BARE METAL FROM BS 541 TO 799. REPLACED SEAT TRACK IAW SRM 53-05.

Part: SKIN — DENTED (BS 248 S17-18L) · airframe 62,350 hrs · 47,172 cycles

ACCOMPLISH ER/A 476169-14 REV B CODE 9-53-31-20 PERMANENT REPAIR DENT FS 248, STR18L AND 17L. REPAIRED IAW ER/A 476169-14, REV B PERMANENT REPAIR.

Part: CUSP WEB — CORRODED (BS 1003-1022) · airframe 62,350 hrs · 47,172 cycles

LEFT CUSP MEMBRANE X=56 TO X=44, STA 1003 TO 1022, HAS 2EA CRACKS AT STA 1022 WITH AREA BULGED. INSTALLED CUSP WEB STA 1003 TO 1022 AND 3EA CLIPS IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 799-937) · airframe 62,350 hrs · 47,172 cycles

SEAT TRACK LBL 55 HAS CORROSION, GOUGES AND BARE METAL STA 937 TO STA 799. INSTALLED REPLACEMENT SEAT TRACK STA 799-937LBL 54 IAW SRM 51-30-1.

Part: LONGERON — CRACKED (BS 200 L2L) · airframe 62,350 hrs · 47,172 cycles

LONGERON 2L, CRACKED BS 200. REPAIRED PER SRM 53-02, FIG 18.

Part: CREASE BEAM — DAMAGED (BS 1221 LBL 58) · airframe 62,350 hrs · 47,172 cycles

AFTER REMOVAL OF CREASE BEAM UPPER SPLICE FOUND ONE HOLE ENLONGATED TO 0.242" IN CREASE BEAM ONLY BS 1221 LBL 58. REPAIRED IAW ER/A 507659-14, REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 560-598) · airframe 62,350 hrs · 47,172 cycles

LEFT CUSP WEB HAS CORROSION FROM STA 560 TO 598. INSTALLED NEW CUSP WEB FS 530-598 IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 712-788) · airframe 62,350 hrs · 47,172 cycles

CABIN RT CUSP WEB MEMBRANE STA 712-788 HAS NUMEROUS LOCATIONS WITH CORROSION AROUND AREA EXPOSED BY SEAT TRACK REMOVAL. REPAIRED IAW SRM 51-30-5.

Part: SKIN — CORRODED (AFT CARGO DOOR) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO DOOR INTERNAL SKIN WEB HAS CORROSION THROUGH OUT. REPAIRED IAW SRM 52-01, PG 10.

Part: CUSP WEB — CORRODED (BS 1174-1212) · airframe 62,350 hrs · 47,172 cycles

LEFT CUSP MEMBRANE STA 1212 TO 1174, X=94 TO CUSP ANGLE HAS 9EA LOCATIONS WITH CORROSION ON TOP SURFACE AND 5EA LOCATIONS WITH CORROSION ON BOTTOM SIDE. REPLACED CUSP WEB LT STA 1174-1250 IAW SRM 5130-2.

Part: CUSP WEB — CORRODED (BS 1022) · airframe 62,350 hrs · 47,172 cycles

RT CUSP WEB MEMBRANE STA 1022 TO 1060 HAS SEVERAL LOCATIONS WITH CORROSION OTBD OF SEAT TRACK AT X 54. REPAIRED IAW SRM 51-30-2.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO DOOR EXTERNAL SKIN HAS A CREASE ELEVEN INCHES FROM AFT SIDE AND TWENTY EIGHT INCHES FROM BOTTOM SIDE AND AREA HAS MULTIPLE DENTS. REPAIRED IAW ER/A 507034-14, REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 1309) · airframe 62,350 hrs · 47,172 cycles

TWO NUT PLATE HOLES AT FLOORBEAM BS 1309 F17 F19 HAVE CORROSION. REPAIRED IAW ER/A 507361-14, REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1338) · airframe 62,350 hrs · 47,172 cycles

AFT LAV FLOORBEAM AT STA 1338 HAS CORROSION AT X=5, 26, 32,36, 46" L/H. X=-18, -19, -24, -31, -34, -37, -39, -47 RIGHT. INSTALLED NEW CAP ANGLE AT STA 1338 LBL 10 TO LBL 56.5 IAW SRM 51-30-5 PG1 AND 51-30-2 PG1.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION BETWEEN STA 655 TO 674. REPLACED WEB IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 826-843) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN CUSP WEB HAS CORROSION BETWEEN BS 826 TO 843. REPAIRED IAW SRM 53-05 FIG 131A-2.

Part: DOUBLER — CORRODED (BS 579-587) · airframe 62,350 hrs · 47,172 cycles

MID CARGO PIT STA 579-587 BETWEEN L28L-L29L RING DOUBLER CORRODED. INSTALLED SHROUD/DOOR ASSY, LONGERON SPLICE AND NEW RING DOUBLER IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1032-1136) · airframe 62,350 hrs · 47,172 cycles

LEFT SEAT TRACK AT X44, STA 1032 TO 1136 SEGMENT HAS CORROSION AND GOUGES AT LOCATIONS MARKED. REPAIRED IAW SRM 53- 05, FIG 4F, PG 32.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,350 hrs · 47,172 cycles

LOWER FUSELAGE BILGE DRAIN ASSY HAS FOUR SECURING RIVETS MISSING, HOLE DAMAGE AND ONE HOLE CRACKED. BELLY SKIN DENTED INSTALL OF BUSHINGS AND FASTENERS INSTALLED IMPROPERLY. REPAIRED IAW ER/A 507375-14, REV ORIG.

Part: SUPPORT — CORRODED (BS 1167) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO BILGE AREA ANTANNA SUPPORT STRUCTURE CLIP BS 1167 ABOVE LONGERON 30 IS CORRODED. INSTALLED NEW SUPPORT CLIP STA 1162 L-30 AFT CARGO IAW SRM 51-30-5.

Part: SUPPORT ANGLE — CORRODED (BS 788) · airframe 62,350 hrs · 47,172 cycles

MID CARGO BAY FWD SIDE BS 788 BETWEEN L27-28R CARGO TRACK INBD SUPPORT ANGLE IS CORRODED. REPLACED SUPPORT ANGLES IAW SRM 51-30-2.

Part: SKIN — CORRODED (BS 763-776) · airframe 62,350 hrs · 47,172 cycles

MID CARGO BAY BS 763-776 BETWEEN L27R-L29R PREVIOUS REPAIR HAS CORROSION. INSTALLED REPAIR DOUBLER AND TRIPLER & FILLERAT FUSELAGE SKIN BETWEEN STA762 TO 777 LONG 27R TO LONG 29R IAW SRM 53-04 FIG 57.

Part: INTERCOSTAL — CORRODED (BS 769-788 L27L) · airframe 62,350 hrs · 47,172 cycles

MID CARGO PIT BS 788 TO 769 BTW L27L AND L28L INTERCOSTAL HAS CORROSION UNDER CARGO TRACK. REPLACED IAW SRM 51-30-1.

Part: FRAME — CORRODED (BS 1309 L22L/R) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO TRANSVERSE FRAME FROM LONGERONS 22L TO 22R AT STA 1309 HAS NUMEROUS LOCATIONS WITH COROSION OF AFT SIDE LOWER FLANGE (CHANNEL) AND ON AFT FACE. REPAIRED IAW SRM 53-03D FIG 5 PG 32.

Part: CUSP WEB — CORRODED (BS 389-446) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN BS 389-446 LT CUSP WEB HAS SEVERAL AREAS WITH CORROSION. REPAIRED IAW SRM 53-05, FIG 131A-10.

Part: FLOORBEAM — CORRODED (BS 1322) · airframe 62,350 hrs · 47,172 cycles

AFT LAV FLOORBEAM AT STA 1322 HAS CORROSION AT X 21, 34, 42(LT) X -18, -19, -41 (RT) LOCATION BLENDED AT X21 AND X42 STA 1322 BEAM ARE REPAIR DOUBLERS/FILLERS FROM PRIVIOUS REPAIR. REPAIRED IAW ER/A 507360-14, REV ORIG.

Part: SKIN — DENTED (BS 1271 L27R) · airframe 62,350 hrs · 47,172 cycles

RT EXTERIOR FUSELAGE SKIN BS 1271, L27R AREA CREASED AND DENTED. REPAIRED IAW ER/A 507037-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 408-428) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN BETWEEN BS 408 & 428, RT CUSP WEB HAS CORROSION. INSTALLED WEB IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 1031-1164) · airframe 62,350 hrs · 47,172 cycles

LEFT SEAT TRACK STA 1031-1164, SEGMENT X=22 HAS CHAFE DAMAGE AND CORROSION. INSTALLED NEW SEAT TRACK AND SPLICE LBL 22 STA 1031-1164 IAW SRM 51-36-4.

Part: CREASE BEAM — CRACKED (BS 1232) · airframe 62,350 hrs · 47,172 cycles

FOUND CREASE BEAM CRACKED AT STA 1232 LT SIDE WHILE REMOVING SHEAR TIES. REPAIRED IAW ER/A 507659-14, REV ORIG.

Part: FLOORBEAM — CORRODED (BS 256) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN FLOORBEAM STA 256 LT SIDE UNDER FLOOR PANEL 200B AND 200A SUPPORT BRACKET HAS CORROSION AT NUT PLATE HOLE. REPAIRED IAW SRM 51-10-3B.

Part: SKIN — CORRODED (BS 1229) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO BILDGE AREA SKIN HAS CORROSION AT STA 1229 AT DRAIN MOUNT HOLES RT OF LONGERON 30. REPAIRED IAW ER/A 507364-14, REV ORIG.

Part: LONGERON — CORRODED (BS 809-1322 L29L) · airframe 62,350 hrs · 47,172 cycles

AFT CARGO LONGERON 29L HAS CORROSION FROM STA 1322 TO 809, 1291, 1264 AND 1266. REPAIRED IAW SRM 53-02, FIG 19.

Part: SEAT TRACK — CORRODED (BS 1164-1309) · airframe 62,350 hrs · 47,172 cycles

LEFT SEAT TRACK AT X=22 SEGMENT STA 1164 TO 1309 HAS CHAFE DAMAGE AND CORROSION. INSTALLED NEW SEAT TRACK STA 1164-1309 IAW SRM 51-30-4.

Part: CUSP WEB — CORRODED (BS 215-722) · airframe 62,350 hrs · 47,172 cycles

IN MAIN CABIN AFTER REMOVAL OF SEAT TRACK AT X=54 STA 215 - 722 FOUND CORROSION ON CUSP WEB MEMBRANE AT STA 285, 314, 333, 336A CHAFE AT STA 256 AND A DENT AT STA 315. REPAIRED IAW ER/A 398191-14MA, REV B.

Part: CUSP WEB — CORRODED (BS 905-927) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN RT CUSP WEB HAS CORROSION BETWEEN BS 905 TO 927. REPAIRED IAW SRM 53-05, FIG 131A-2.

Part: FRAME — GOUGED (BS 712-788) · airframe 62,350 hrs · 47,172 cycles

DURING REMOVAL OF LT CUSP WEB STA 712 TO 788 FOUND A GOUGE ON FRAME LT LOWER END STA 769 JUST ABOVE L18 POSITION. REPAIRED IAW ER/A 507675-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 598-712) · airframe 62,350 hrs · 47,172 cycles

MAIN CABIN CUSP WEB LT SIDE HAS CORROSION ON UPPER AND LOWER SURFACES AT PREVIOUS REPAIRS FROM BS 598 TO 712. REPLACED IAW SRM 57-30-1.

Part: SEAT TRACK — CORRODED (BS 1164-1309) · airframe 62,350 hrs · 47,172 cycles

SEAT TRACK AT X=44 BS 1164-1309 SEGMENT HAS CORROSION. REPAIRED IAW SRM 53-05, FIG 4F.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,897 hrs · 46,883 cycles

AFT CARGO FLOOR PANEL TORN IN TWO PLACES. DAMAGED AREA EXCEEDED REPAIRABLE LIMITS PER AMM 25-52-01 PB 801.

Part: SEAT TRACK — CORRODED (BS 222 LBL 4) · airframe 61,640 hrs · 46,712 cycles

PASSENGER CABIN SEAT TRACK HAS CORROSION AT BS 222, LBL4, ON INVESTIGATION FOUND DAMAGE TO SEAT TRACK TO BE OUT OF LIMITS PER SRM 53-05 PG 28 FIG 4B-1. REPLACED SEAT TRACK IAW SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 61,637 hrs · 46,711 cycles

FOUND FWD AND AFT GIRT BAR FLOOR BRACKETS CORRODED AT R-1 DOOR MRB 53-037-01. DAMAGE WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW IAW AMM 20-30-01.

Part: SEAT TRACK — CORRODED (BS 214) · airframe 61,637 hrs · 46,711 cycles

PASSENGER CABIN SEAT TRACK HAS CORROSION AT BS 214, RBL 22. REPAIRED SEAT TRACK IAW SRM 53-05 FIG 4 MRB 53-037-01.

Part: CONTROL WHEEL — OBSTRUCTED (COCKPIT) · airframe 61,315 hrs · 46,490 cycles

SHIP 933 DIVERTED TO SAV DUE TO AUTO PRESSURIZATION FAULT AND A JAMMED MANUAL CONTROL WHEEL. MAINTENANCE REMOVED SCREW (FOD) THAT HAD FALLEN FROM THE MODE CONTROL PANEL AND JAMMED INTO THE MANUAL CONTROL WHEEL.

Part: DOUBLER — CRACKED (BS 1437 FWD) · airframe 60,206 hrs · 45,754 cycles

FOUND CRACKED ANGLE DOUBLER AT STA 1437, FWD SIDE (ATTACH BULKHEAD FOR VERT) BETWEEN LONGERON ON 0-1 LEFT. REPLACED SEVERED CORDS & INSTALLED DOUBLER REPAIR IAW ER/A 496317-14 REV 0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,206 hrs · 45,754 cycles

DURING PSV IN MSP, A CRACK TO THE FUSELAGE SKIN WAS FOUND AT STA 1418 S2L. REPAIR ACCOMPLISHED PER ER/A 496283-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,206 hrs · 45,754 cycles

DURING PSV IN MSP, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT APPROXIMATELY STA 1437 BETWEEN L3R-L4R. REPAIR ACCOMPLISHED PER ER/A 496284-14.

Part: SKIN — DAMAGED (BS 180 S28R) · airframe 59,323 hrs · 45,119 cycles

ON WALK AROUND FOUND A SMALL HOLE AT STA 180 STR 28R. INSTALLED A PERMANENT REPAIR PER DRAWING SG09530001.

Part: WIRE — BROKEN (CABIN) · airframe 59,214 hrs · 45,028 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATHWAY LIGHTS AT ROW 20D INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN ON LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATION CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 58,354 hrs · 44,454 cycles

C-3 BAG FIN LOWER SILL HAS LIGHT CORROSION AROUND STOP PADS. REMOVED CORROSION, FOUND BEAM OUT OF LIMITS IAW SRM 53-05D, FIG 123. REPLACED BEAM.

Part: SILL — CORRODED (C-3 THRESHOLD) · airframe 58,354 hrs · 44,454 cycles

C-3, BAG BIN LOWER SILL HAS LIGHT CORROSION AROUND STOP PADS. REPLACED BEAM DUE TO 2 SPOTS GROUND BEYOND THE 50 PERCENT ALLOWED IAW SRM 53-05, FIG 123.

Part: LANYARD — FRAYED (EVA SLIDE) · airframe 58,201 hrs · 44,364 cycles

DURING LINE CHECK MAINTENANCE FOUND DOOR SLIDE LANYARD FRAYED AT L1 DOOR AND L2 DOOR SLIDE LANYARD INSTALLED IMPROPERLY. MAINTENANCE REPLACED L1 DOOR SLIDE LANYARD AND REPOSITIONED L2 DOOR SLIDE LANYARD. ACCOMPLISHED IAW 25-62-00. (2010-D1383) (DLM88103218)

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 57,471 hrs · 43,904 cycles

MX FOUND THE EMERGENCY LIGHT AT SEAT 24D TO BE INOPERATIVE. MX RE-TERMINATED A BROKEN WIRE. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 57,413 hrs · 43,868 cycles

MX FOUND THE EMERGENCY LIGHTS FROM SEAT ROW 24 TO BE INOPERATIVE. MX CHECKED THE WIRING AND BATTERY PACKS AND ALL CHECKS GOOD. REPLACED POWER SUPPLY FUSES. A SYSTEM CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: FITTING — LEAKING (ACTUATOR) · airframe 56,740 hrs · 43,431 cycles

F/A REPORTED BOTH AFT SMOKE DET GOING AND HAZE IN CABIN. FOUND FITTING ON LT AUTOBRAKE MANIFOLD LEAKING. REPLACED O-RING ON FITTING. LK CKS GOOD. ALSO SEE ITEM 5 THIS LOG PAGE. ACFT OK FOR SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 56,303 hrs · 43,113 cycles

FOUND ON CHECK SEAT 4C EMERGENCY PATH LIGHT OUT. REPLACED BOTH BULBS NO HELP. RESEATED WIRE CONNECTION NOW OPS OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 56,052 hrs · 42,960 cycles

EMERGENCY LIGHT AT SEAT 18DE INOP. RELAMPED NO HELP. FOUND NO VOLTS AT OTBD CONNECTOR. FOUND WIRE RIPPED OUT OF INBD SEAT CONNECTOR. WILL NEED REPIN AND CONNECTOR. REPAIRED WIRE HARNESS EMERG LIGHTS AT 18E OPS NML. REMOVED MCO/PLAC.

Part: CSD — UNSERVICEABLE (NR 1 ENGINE) · airframe 51,612 hrs · 40,115 cycles

LEFT GEN FAILED DURING INITIAL CLIMB-OUT WITH AN OPEN BUS TIE THE APU GEN WAS RUNNING AT THE TIME AND CARRIED THE LEFT GEN LOAD FWD LT GEN TO MCO AND PLAC PER MEL24-00-01A LT CSD DISC VERIFIED APU OIL FULL AND PERFORMED A CROSSTIE CK. CKD GCU. NO FAULTS. CHKD CSD CHIP DETECTOR. NO METAL FOUND. REPLACED LT GEN CSD PER M/M. ALSO REPLACED LT ENG GCU. RAN ENGINE CKD GEN/CSD OUTPUT OPERATION PER M/M. ALL CKS GOOD MCO PLAC REMOVED. GCU OFF S/N UM 3656C ON XJ2125B DPN.

Part: WINDOW — MISINSTALLED (CABIN) · airframe 51,130 hrs · 39,825 cycles

CABIN WINDOWS IMPROPERLY INSTALLED RESULTED IN FATIGUE CHIPPING OF 2 OUTER PANES. REPLACED DAMAGED PANES.

Part: HYDRAULIC LINE — LOOSE (NR 1 ENGINE) · airframe 50,626 hrs · 39,498 cycles

LEFT HYD PRESSURE SYSTEM FAIL IN FLT PRESSURE DROPPED TO ZERO AND QTY DROPPED TO 2 QTS. FOUND PRESSURE LINE AT NR 1 ENG DISCONNECT LEAKING. TIGHTENED LINE AND RAN ENG, THRUST REVERSER AND ELEC PUMPS. NO LKS FOUND.

Part: STRUT — BINDING (NLG) · airframe 48,922 hrs · 38,397 cycles

AIR TURN BACK AFTER TO WHEN GEAR HANDLE RAISED NOSE GEAR RED UNSAFE LIGHT REMAINED ON WITH NOISE AND VIBRATION FOLLOWED QHR PRODECURE RETURNED TO LGA. MAINTENENCE IN PROGRESS JACKED A/C VISUAL CK NOSE GEAR FOUND RT AFT DOOR ROD BINDING REMOVED DOOR ROD AND NOSE PISTON/CYL ASSY. REPLACED NOS STRUT SEALS PER MM. REPLACED RT AFT DOOR ROD INSTALLED PISTON/CYL ASSY SER NOSE STRUT PER MM SWUNG GEAR. OPS CK GOOD DOWN JACKED A/C.

Part: SKIN — CRACKED (BS 163-197)

EXT FS L-22L CRACK INDICATIONS NOTED FROM FASTENER COUNTERSINK EDGE AT FS-190 0.02" AT 4 O'CLOCK, FS-193 0.03" AT 4 O'CLOCK, FS-194 0.015" AT 4 O'CLOCK, FS-195 0.06" AT 1 O'CLOCK AND 0.04" AT 4 O'CLOCK, FS-197 0.03" AT 4 O'CLOCK. REPAIRED FS-163 TO FS-197.5 BY TRIMMING OUT CRACKED AREAS, FABRICATED AND INSTALLED DOUBLER 50" BY 22-5/8" FROM 7075-T6 .071" AND FILLER 34-7/8" BY 3" FROM 2024-T3 .050" IAW DELTA EA 09-069085-12 AD REV D DATED 07-15-05 ME02.

Part: FRAME — CRACKED (BS 1322) · corrosion level 2

CORROSION ON FRAME AT FS 1322 AT L-26L TO L-26R. CUT OUT CORRODED AND CRACKED AREA OF FRAME AT L-30. FABRICATED AND INSTALLED 2 FRAME REPAIRS APPROX 12.50" LONG FROM 7075-O .71" HEAT TREATED PER DELTA P.S. 900-4-1 NO. 1, REPAIR FILLER 3.90" BY .40" BY .90" BY .90" FROM 7075-O .063" HEAT TREATED PER DELTA P.S. 900-4-1 NR 1, AND PLATE 12.75" BY 2" BY 12.25" FROM 7075-T6 .071" IAW DC-9/MD-88 SRM 53-03D FIG 2A.

Part: FRAME — CORRODED (BS 1418) · corrosion level 2

CORROSION BETWEEN 5 AND 7 O'CLOCK POSITION FRAME STA 1418, VENTRAL STAIRWAY. CUT OUT CORRODED SECTION OF WEB FRAME. FABRICATED AND INSTALLED WEB REPAIRS 28" BY 6.25 FROM 7075-T6 .063" AND 6.25" BY 5.5" FROM 7075-T6 .071" IAW DC-9/MD-80 SRM 53-14-4 FIG 1, 51-70-4 FIG 1 AND 51-30-2.

Part: SKIN — DAMAGED (BS 754)

LIGHTNING STRIKE BLEND OUT, OUT OF LIMITS FS 754 2 INCHES BELOW L-27R. FABRICATED AND INSTALLED REPAIR DOUBLER 5.0" BY 4.25" FROM 2024-T3 .032" IAW DC-9/MD-80 SRM 53-04D, 51-10-3D.

Part: SKIN — LIGHTNING STRIKE (BS 730 S27R)

S/O 291023 N/R NR21879 LIGHTNING STRIKE BLEND OUT AT FS 730 1.25 INCHES ABOVE L-27R OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR 6 INCHES X 5 INCHES FROM 2024-T3 .032 INCHES IAW SRM 53-04 FIG. 38, 51-10-3D.

Part: SKIN — LIGHTNING STRIKE (BS 736)

S/O 291023 N/R NR 21880 LIGHTNING STRIKE BLEND OUT AT FS 736 ABOVE L-27R OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR 6.25 INCHES X 6.0 INCHES FROM 2024-T3 .032 INCH IAW SRM 53-04 FIG. 38, 51-10-3D.

Part: SKIN — DAMAGED (BS 739)

LIGHTNING STRIKE BLEND OUT OUT OF LIMITS FS 739 BETWEEN L-28R AND L-29R. FABRICATED AND INSTALLED REPAIR DOUBLER 6.5" BY 4.0" FROM 2024-T3 .032" IAW DC-9/MD-80 SRM 53-04D , 51-10-3D.

Part: SKIN — DAMAGED (BS 607)

LIGHTNING STRIKE BLENDED OUT OF LIMITS IN FUSELAGE SKIN AT FS 607 ABOVE L-24R. FABRICATED AND INSTALLED 2 SKIN REPAIRS 5.75" BY 8.0" FROM 6AL-4V .032" AND 15.75" BY 13.75" FROM 6AL-4V .025" IAW DC-9/MD-88 SRM 53-04 FIG 45D.

Part: SKIN — GOUGED (FUSELAGE) · airframe 47,586 hrs · 37,491 cycles

FUSELAGE SKIN SPLICE AT FS 474-538, STR 19-21R, ACCOMPLISH PERMANENT REPAIR PER MD88 SRM 53-04 FIGURE 12C.

Part: ANGLE — CORRODED (BS 1350) · corrosion level 2

CORROSION ON FLOOR STRUCTURE FS 1350 AT FWD EDGE OF AFT VAULT DOOR CUTOUT. FABRICATED AND INSTALLED -2 REPAIR ANGLE APPROX. 8" BY 6" BY 3" BY 2" BY 1" FROM 7057-O .040 HEAT TREATED PER DELTA PS 900-4-1 NR 1, IAW DC-9/MD-88 SRM 53-05 FIG 34.

Part: WINDOW FRAME — DENTED (BS 503-598)

DENT FS 543 RT L-14R. REMOVED AND REPLACED WINDOW PANEL P/N 9958156-1 IAW BOEING DWG 5932737 REV P.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 44,513 hrs · 35,272 cycles

RIGHT ENGINE FLAME OUT DURING CLIMBOUT FROM ATL. REPLACED FUEL PUMP FOR SHEARED SHAFT AND GEARBOX.

Part: APU — FAILED (APU BAY) · airframe 42,486 hrs · 33,787 cycles

APU GEN KICKED OFF INFLIGHT WITH A/C XTIE LOCKOUT RESULTING IN RT A/C BUS UNPOWERED. REPLACED GCU.

Part: FAN — FAULTY (CARGO BAY) · airframe 42,077 hrs · 33,487 cycles

ODOR REPORTED MID CABIN BY SEVERAL PAX. FOUND NR 1 LOW RANGE ALT FAN AS CAUSE OF ODOR. DEACTIVATED FAN, NR 1 LRRA INOP. REPLACED SAME.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,963 hrs · 32,030 cycles

ON INSPECTION, FOUND EMERGENCY PATH LIGHTING INOPERATIVE FROM ROWS 31-38 FOUND BROKEN WIRES AT ROW 36. REPAIRED WIRING AND LIGHTS NOW OPERATE NORMALLY.

Part: ATTACH FITTING — CRACKED (L/E SLAT) · airframe 39,371 hrs · 31,634 cycles

NR 3 SLAT MIDDLE ATTACH FITTING CRACKED BETWEEN ATTACH POINT AND EDGE OF FITTING 100 PERCENT. REPLACED SAME.

Part: RADOME — DAMAGED (NOSE) · airframe 39,352 hrs · 31,625 cycles

ON ARRIVAL DFW FOUND RADOME DAMAGED. LOWER LEFT CENTER. APPROX 6 INCHES IN DIAMETER, SPONGY FEELING. REPLACED RADOME

Part: PIN — PULLED (EVAC SLIDE) · airframe 35,841 hrs · 29,038 cycles

L1 DOOR SLIDE CABLE PINS PULLED. REPLACED SLIDE.

Part: WIRE — EXPOSED (WINDOW SENSOR) · airframe 35,017 hrs · 28,404 cycles

WINDOW R1 SENSOR SMOKED WHEN ANTI-FOG TURNED ON AND CAPTS ADI WENT BLANK THEN RETURNED. CA FOUND TERMINAL ON THERMAL SWITCH FOR ANTI FOG SYS. INSULATION CRACKED AND RUBBING ON CONTACT SPRING. RE ROUTED WIRES ON HEATING ELEMENT SENSOR

Part: LINE — LEAKING (HYD SYSTEM) · airframe 34,140 hrs · 27,776 cycles

LEFT HYDRAULIC QUANTITY DECREASED INFLIGHT FROM 11 QUARTS TO 4 QUARTS. FOLLOWED POM PROCEDURE AND QUANTITY INCREASED TO 19 QUARTS. TURNED LEFT ENGINE AND AUXILLARY AND TRANSFER PUMPS BACK ON AND QUANTITY WENT SLOWLY BACK TO ZERO AND PRESSURE ZERO. REPLACED LINE FROM THRUST REVERSER BYPASS VALVE TO CASE DRAIN FILTERS. REPLACED CASE DRAIN FILTERS AND TRANSFER PUMPFILTER. LEAK CHECKS GOOD.

Part: SWITCH — ARCED (COCKPIT) · airframe 33,781 hrs · 27,526 cycles

ON FINAL APP NOTICED SMOKE COMING FROM CAPT EXT LIGHT CONTROL PANEL. FLOOD AND WING LIGHTS ON, NOSE LIGHTS OFF. TURNED OFF ALL LIGHTS AND SMOKE CEASED. LANDED UNEVENTFUL AND TAXIED IN. REMOVED LT WING/NOSE LIGHT SW FOR ACCESS. FOUND LT WING LANDING LIGHT SW ARCED AT CASE. REPLACED SAME.

Part: WIRE — CHAFED (NR 2 GENERATOR) · airframe 32,595 hrs · 26,661 cycles

NR 2 ENGINE GENERATOR FEEDER CABLE WAS FOUND CHAFING ON A HYDRAULIC FILTER BOWL ASSY AT STA 1360 IN THE AFT ACCESSORY COMPARTMENT. CABLE WAS REPAIRED PER MM AND CABLE RELOCATED TO AVOID CONTACT.

Part: SKIN — DENTED (FUSELAGE) · airframe 32,595 hrs · 26,661 cycles

FUSELAGE SKIN DENTED APPROX FS 1287 STR 22. REPAIRED PER ERA334724-14.

Part: FILTER — CLOGGED (NR 2 ENGINE) · airframe 32,005 hrs · 26,229 cycles

FLT 1892/02 ATL-CLE NR 2 ENG OIL STRAINER CLOG MSG ILLUM. CREW FOLLOWED POM PROC AND MSG REMAINED. SHUT DOWN ENG AND DIVERTED TO TYS. MTC FOUND CARBON IN FILTER. REPLACED ENGINE.

Part: RIVET — SHEARED (RUDDER TRIM) · airframe 31,973 hrs · 26,201 cycles

A/C YAWED LT AND RT FOR SEVERAL CYCLES AT APPROX FL250 AND MACH .75 TO MACH .76. INSPECTED RUDDER TAB HINGES AND SHEAR RIVETS ON RUDDER SHIMMY DAMPENER, CKS OK. CHECKED FLT FAULTS NONE AND RAN RTS TEST, ALL GOOD. NO TROUBLE FOUND.

Part: FILTER — CLOGGED (NR 2 ENGINE) · airframe 31,875 hrs · 26,131 cycles

NR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. ENGINE SHUT DOWN AFTER POM PROCEDURES FOLLOWED. REPLACED STRAINER, RAN ENGINE.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 31,695 hrs · 25,994 cycles

DURING SLAT EXTENTION ON APPROACH, LEFT HYDRAULIC SYSTEM PRESSURE WENT TO 0. LEFT HYDRAULIC QUANTITY REMAINED STEADY AT 19 QTS. REMOVED AIR FROM SYS, REPLACED ENG DRIVEN PUMP PER M/M, CKS OK. NO LEAKS, OPERATED ALL FLIGHT CONTROLS, PRESS REMAINED STEADY, OK FOR SERVICE.

Part: HYD LINE — CHAFED (RT PYLON)

LOSS OF THE RIGHT HYD SYSTEM. INITIALLY LOST THE RIGHT PRESSURE THEN THE RIGHT HYD QTY WENT TO ZERO WITH THE TRANSFER AND AUX PUMPS. FOUND FLEXIBLE HYD PRESSURE LINE FROM PYLON TO ENG DISCONNECT WORN THRU AT CLAMP. REPLACED HOSE AND CLAMP.

Part: HYD LINE — RUPTURED (LT TR UNIT)

APU AIR CONDITIONING PUTS SMOKE IN CABIN. FOUND RUPTURED LEFT THRUST REVERSER HYD PRESS LINE.

Part: CHARGER — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTS FWD OF ROW 13 AND FWD SVC AND MAIN DOOR IDENTIFIERS INOP. REPLACED CHARGER AND BATTERY.

Part: LIGHT — MISSING (CABIN)

EVENT OCCURANCE 09/06/97 1 EMERGENCY FLOOR TRACK LIGHT IN AFT CABIN MISSING. REPLACED EMERGENCY FLOOR TRACK LIGHT BULB AND RED MODULE.

Part: FRAME — CRACKED (RT MLG WW)

TWO INCH CRACK FOUND AT WHEELWELL FWD FRAME O/B END. FOUND AT A-1 LETTER CHECK. REPAIRED PER SRM 53-05 FIG 78A.