N968DL

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 73,020 hrs · 53,686 cycles

FOUND L1 DOOR SLIDE ENGAGEMENT PINS PULLED OUT OF SLIDE PACK. REMOVED AND REPLACED L1 DOOR SLIDE ASSY PER W/C 2561-4964. OK FOR SVC. (LP5300902)

Part: SKIN — CRACKED (CARGO DOOR) · airframe 72,621 hrs · 53,340 cycles

AFT CARGO DOOR SKIN, CREASED AND VISUAL INDICATION OF CRACK AT LOWER SURFACE, JUST AFT OF CENTER. REPLACED AFT CARGO DOOR REF AMM 52-31-00. (LP0779958)

Part: RUDDER — DAMAGED (TAIL) · airframe 72,621 hrs · 53,340 cycles

COMPOSITES SHOWING ON MULTIPLE AREAS ON RUDDER. REMOVED RUDDER ON WORKCARD 2720-4187. INSTALLED NEW RUDDER ON WORKCARD 2720-4421. RIGGED RUDDER ON WORKCARD 2720-7454.

Part: SUPPORT ANGLE — CORRODED (BS 1117) · corrosion level 2 · airframe 72,621 hrs · 53,340 cycles

CORROSION ON FRAME SUPPORT ANGLE. AFT CARGO, STA 1117, ABOVE STR 30. REPAIRED IN REF TO MD88 SRM 51-70-5 PARA 3 FIG 2. (LP0770016)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,528 hrs · 53,267 cycles

FOUND EMERGENCY LIGHTS EXIT SIGNS INOP AT SEATS 25 A, B, C, E, D. REMOVE AND REPLACE POWER SUPPLY AT SEAT 25 STA 908R PER AMM 33-53. OPS CKS GOOD.

Part: CABLE — BROKEN (TAILCONE) · airframe 71,760 hrs · 52,612 cycles

TAIL CONE INADVERTENTLY DROPPED AND THE SLIDE RAFT DID NOT INFLATE. FOUND CABLE ASSY TAIL CONE JETTISON BROKE, REMOVED BROKEN CABLE 1/2 FROM A/C TAIL CONE RELEASE SYS FUNCTION CHK ACCOMPLISHED ON TASK CARD 5350-01077-0101 CARD 7037790.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 71,523 hrs · 52,428 cycles

AFT RIGHT LAVATORY SMOKE ALARM SOUNDED. NO SMOKE OR ODORS. NO TROUBLE FOUND.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 71,283 hrs · 52,232 cycles

SEAT 27D SEAT MOUNTED EMERGENCY LIGHT INOP. REPLACED SEAT MOUNTED WIRE HARNESS PER SWPM 20-90-03. CKS GOOD.

Part: CONNECTOR — BROKEN (CABIN) · airframe 71,283 hrs · 52,232 cycles

SEAT 23D SEAT MOUNTED EMERGENCY LIGHT INOP. FOUND CONNECTOR BROKEN AT SEAT FRAME REPLACED SAME. REF SWPM 20-90-03. CKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,141 hrs · 52,123 cycles

EMERGENCY LIGHTS ABOVE EXIT ROW SEATS INOP. REPLACED BATTERIES IAW AMM 33-53.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 70,961 hrs · 51,975 cycles

HIDDEN DAMAGE: CRACK ON LONGERON SPLICE 29L BTW STA Y=1193 TO Y=1212 AT AFT CARGO COMPARTMENT BILGE AREA. DAMAGE SPLICE WAS REPLACED PER SRM 51-30-5 AND DWG 3914677-507 REV CD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,683 hrs · 51,771 cycles

NUMERIOUS EMERGENCY LIGHTS IN THE OVERHEAD CABIN INOPERATIVE. REPLACED THE BULBS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 69,839 hrs · 51,058 cycles

DURING CLIMB OUT, CENTER WINDSCREEN CRACKED. QRH PROCEDURE COMPLIED WITH. REPLACED CENTER WINDSHIELD IAW AMM 56-10.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 69,437 hrs · 50,749 cycles

EMERGENCY LIGHT AT SEAT 33D WILL NOT ILLUMINATE. SECURED THE WIRE, OPS CKS GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 68,964 hrs · 50,407 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT SEATS 13D AND 21D. REPLACED THE WIRE HARNESS, OPS CHECKED GOOD IAW AMM 33-53.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,321 hrs · 49,937 cycles

EMERGENCY EXIT SIGNS AT ROW 25 ABC AND 25 DE INOPERATIVE. REPLACED THE BATTERIES IAW AMM 33-53. CHECKED GOOD.

Part: CONDUIT — OUT OF POSITION (TAILCONE) · airframe 67,757 hrs · 49,500 cycles

TAIL CONE FUNCTION CHECK FAILED STEP 7D (5). LOCKING CABLE CLAMP DOES NOT CLEAR LOWER END OF CONDUITS AT LEAST 1/2". REPOSITIONED CONDUITS PER STEP 5 RECHECKED. IAW AMDS 5350-01077-0101.

Part: CABLE — DAMAGED (TAILCONE) · airframe 67,757 hrs · 49,500 cycles

TAILCONE FUNCTION- BALL END OF CABLE TO LOCK IN CLIP. FIGURE 2. ITEM 13. REPLACED THE CABLE IAW AMDS 5350-010177-0101.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,204 hrs · 48,411 cycles

MAINTENANCE FOUND BOTH AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY SUPPLY POWER PACK WAS REPLACED.

Part: SLIDE — NO TEST (TAILCONE) · airframe 66,205 hrs · 48,412 cycles

THE TAILCONE AND TAILCONE SLIDE FAILED THE DEPLOYMENT CHECK IAW FORECAST NR 88-0525-8-0408. MAINTENANCE CHECKED RIGGING AND EXERCISED THE EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARMING HANDLE SEVERAL TIMES AND THE SLIDED DEPLYED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,061 hrs · 48,315 cycles

MAINTENANCE FOUND AFT OVERWING EXITS EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK FOR THE AFT OVERWING EMERGENCY EXIT LIGHTS WAS REPLACED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,249 hrs · 47,729 cycles

MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN CABIN BETWEEN SEATS 27 AND 29. MAINTENANCE REPLACED THE BATTERIES AND POWER SUPPLY AT ROW 29 OVERHEAD BIN. OPS CHECKED OK.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 64,961 hrs · 47,509 cycles

THE L1 DOOR SLIDE FELL OUT OF COVER AND BOTH LACING PINS PULLED OUT OF SLIDE. MAINTENANCE INSTALLED A NEW SLIDE ASSY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,654 hrs · 47,310 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT. RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 63,696 hrs · 46,726 cycles

MAINTENENCE FOUND SEAT 25DE RED EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENACE REPAIRED THE CONNECTOR AND ALSO REPAIRED A WIRE AT A SECOND LOCATION UNDER THE SEAT. OPS CHECKED OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 63,223 hrs · 46,413 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEATS 13-23. MAINTENANCE FOUND A BROKEN WIRE AND INSTALLED A SPLICE. OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 62,963 hrs · 46,228 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 21D WAS INOPERATIVE. MAINTENANCE REPLACED THE PIG TAIL AT SEAT 21D AND THE OPS CHECK WAS GOOD.

Part: FLOOR SUPPORT — DEBONDED · airframe 62,486 hrs · 45,869 cycles

DISBONDED FLOOR SUPPORTS. FLOOR SUPPORTS REPLACED IAW SRM 51-10-4 AND 51-30-1.

Part: STRAP — MISINSTALLED (TAILCONE SLIDE) · airframe 62,488 hrs · 45,871 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE SLIDE PACK FLOOR ATTACH STRAP NOT ATTACHED CORRECTLY. MAINTENANCE INSTALLED THE STRAP CORRECTLY AND THE RII STEPS WERE COMPLETED.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 62,486 hrs · 45,869 cycles

CORROSION ON RT CARGO TRACK BS 1212 - 1322. CORROSION REMOVED AND FOUND OUT OF LIMITS. CARGO TRACK REMOVED AND REPLACED IAW SRM 51-10-3, PAR 26, 14, 21, 51-30-1.

Part: TEE FITTING — NICKED (BS 1338 BULKHEAD) · airframe 62,486 hrs · 45,869 cycles

NICKS ON AFT PRESSURE BULKHEAD TEE BS 1338 LONGERONS 24 - 25R IN AFT ACCESSORY BAY. AFT PRESSURE BULKHEAD TEE WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-3, PAR 14, 21 AND DWG 5910130, REV ET.

Part: SUPPORT — CRACKED · airframe 62,486 hrs · 45,869 cycles

CRACKED SUPPORT Y=37 AND X=10. SUPPORT WAS REMOVED IAW SRM 51-30-2, REPAIRED IAW SRM 53-01, FIG 2 AND INSTALLED IAW SRM 51-30-2 CRACK LENGTH.

Part: SKIN — DAMAGED (RT WING) · airframe 62,486 hrs · 45,869 cycles

ENLOGATED HOLE ON RT WING SKIN BELOW HEATER BLANKET AFT SECTION XCW=174. RT WING REPAIRED IAW ER/A 526972-14 AD REV "A".

Part: WEB — CORRODED (BS 429-433) · corrosion level 2 · airframe 62,486 hrs · 45,869 cycles

CORROSION ON AFT WEB BETWEEN LONGERONS 25 AND 26R BS 429 - 433. AFT WEB REPAIRED IAW ER/A 528224-14 REV ORIG.

Part: RUB STRIP — DEBONDED (BS 731-826) · airframe 62,480 hrs · 45,866 cycles

DISBONDING RUB STRIPS BS 731 - 826 LONGERONS 24 - 30R. DEBONDED RUB STRIPS WERE REMOVED AND NEW RUBSTRIPS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW ER/A 479444-14, MA REV E.

Part: TAB — DAMAGED (RUDDER) · airframe 62,486 hrs · 45,869 cycles

PEEL OF PAINT COAT AND DEBONDED T/E ALUMINIUM COMPENSATOR TAB OR RUDDER CONTROL TAB. RUDDER CONTROL TAB REPAIRED IAW SRM 51-70-1AD PARAGRAPH 23.

Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION FOUND ON FRAME BETWEEN LONGERONS 29R - 28L BS 1271 IN AFT CARGO BAY. FOUND OUT LIMITS IAW SRM 53-01, FIG 1. FRAME REPAIRED IAW SRM 53-03D, FIG 2A.

Part: SKIN — CORRODED (BS 769) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR DOUBLER BS 769 LONGERON 28R ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET AREA. AREA WAS REPAIRED IAW 53-04, FIG 57.

Part: DOOR FRAME — CORRODED (BS 1154-1211) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON AFT CARGO DOOR FRAME BS 1154-1211. CARGO DOOR FRAME REPAIRED IAW SRM 53-05, FIG 123A.

Part: INTERCOSTAL — CRACKED (BS 1306) · airframe 62,480 hrs · 45,866 cycles

CRACKED INTERCOSTAL BS 1360 LONGERON 3R IN AFT ACCESSORY BAY. INTERCOSTAL REPAIRED IAW SRM 53-01, FIG 2 AND 51-30-2, 51-30-5 TO 51-10-3, PAR 21 AND 14 RT.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 62,480 hrs · 45,866 cycles

DURING MAINTENANCE, FOUND OTBD BUTTE DOOR ON LT INBD FLAP CRACKED. DAMAGE WAS REMOVED IAW SRM 57-01, FIG 5 DOUBLERS AND FILLER WERE FABRICATED IAW SRM 57-01, FIG 5 AND DWG 5936802, REV D. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21. REPAIR PARTS WERE INTALLED IAW SRM 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1222-1322) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1222 - 1322 IN AFT CARGO BAY . CARGO TRACK WAS REPLACED IAW SRM 51-30-1; 51-30-2; 51-10-4, 51-10-3 21, 14 & 38.

Part: ACCESS PANEL — DAMAGED (FUSELAGE) · airframe 62,480 hrs · 45,866 cycles

ELONGATED HOLE ON ACCESS PANEL 3325C. ACCESS NR WAS FABRICATED AND REPLACED IAW DWG 5936123, REV AM.

Part: ACCESS PANEL — WORN (RT WING) · airframe 62,480 hrs · 45,866 cycles

WEAR ON ACCESS PANEL INNER SKIN BELOW HINGE AREA AND ELOGATED HOLES OUTER SECTION OF RT WING L/E LOWER SURFACE. ACCESS PANEL REPAIRED IAW SRM 51-30-2, SRM 57-01, FIG 3, SHEET 2, SRM 51-10-3, PAR 14 AND 21, AND 51-20-0.

Part: SKIN — DAMAGED (BS 678) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

SKIN COUNTERSINK BS 678 LONGERON 30 WAS DAMAGED. DAMAGE ON SKIN REPAIRED WITH ETI-88-14-167 AND ER/A 528221-14 REV ORIGINAL.

Part: COVER — DAMAGED · corrosion level 2 · airframe 62,488 hrs · 45,871 cycles

CORROSION AROUND OF SECONDARY ACCESS COVER 1409 AT RT HEATER BLANKET. HEATER BLANKET WAS REPLACED IAW AMM 30-80-02-401.

Part: FLOORBEAM — CRACKED (BS 1155) · airframe 62,480 hrs · 45,866 cycles

DURING MAINTENANCE ACTIVITIES WAS CRACKED FLOORBEAM BS 1155 IN AFT CARGO COMPARTMENT. FLOORBEAM REPLACED IAW SRM 51-30-2, 51-0-3.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CARGO TRACK BS 1007 - 1155 IN AFT CARGO BAY. CARGO TRACK REPLACED IAW SRM 51-30-2 AND SRM 51-30-1, SRM 51-04-4 AND SRM 51-103, PAR 14, 21.

Part: TEE FITTING — NICKED (BS 1338 BULKHEAD) · airframe 62,486 hrs · 45,869 cycles

NICKS ON AFT PRESSURE BULKHEAD TEE BS 1338 BETWEEN LONGERONS 24 - 25L IN AFT ACCESSORY BAY . AFT PRESSURE BULKHEAD TEE WAS REPLACED IAW SRM 51-30-2 51-30-5, SRM 51-10-3, PAR 14, 21 AND DWG 5910130, REV ET.

Part: FLOOR SUPPORT — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 1212 - 1155 IN AFT CARGO BAY . FLOOR SUPPORT REPLACED IAW 51-10-3 PAR 26, 14 AND 21, 51-30-5, 53-01 FIG 1, 51-30- 2, 51-10-4, & 51-30-1.

Part: FRAME — CRACKED (BS 1510) · airframe 62,486 hrs · 45,869 cycles

CRACKED FRAME BS 1510 BETWEEN 4 O'CLOCK POSITION TO 7 O'CLOCK POSITION IN AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (BS 788 BULKHEAD) · airframe 62,480 hrs · 45,866 cycles

CRACKED ANGLE ON VERTICAL SUPPORT OF BULKHEAD BS 788 X=38 Z=-28 IN MID CARGO BAY. ANGLE REPLACED IAW DWG 5936628-213 AND SRM 51-30-2.

Part: SKIN — DAMAGED (RWS 289) · airframe 62,480 hrs · 45,866 cycles

LOWER SKIN STA XOS=289 AT RT WING DAMAGED. AREA REPAIRED IAW ER/A NR 526971-14, REV ORG, AND ETI-88-14-126, REV 4.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON INNER SKIN LOWER SIDE OF FWD LAVATORY SERVICE PANEL. SKIN REPAIRED IAW ETI-88-14-131 REV 5 AND ER/A 526976-14 REV. ORIG.

Part: FRAME — CRACKED (BS 1510) · airframe 62,480 hrs · 45,866 cycles

CRACK ON FRAME, BS 1510 AT 11 O'CLOCK POSITION, IN AFT ACCESSORY BAY. FRAME REPLACED IAW SEM 51-30-2 AND 51-30-5.

Part: CARGO TRACK — CORRODED (BS 427-455) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 427 - 455 AT FWD CARGO BAY. CARGO TRACK REPAIRED IAW SRM 53-05, FIG 4G.

Part: SUPPORT — CRACKED (BS 1338-1345) · airframe 62,480 hrs · 45,866 cycles

CRACKED SUPPORT ON BS 1338-1345 LONGERON 25R IN LOWER AFT ACCESSORY BAY. SUPPORT WAS REPAIRED IAW SRM 53-01.

Part: LONGERON — CRACKED (BS 995) · airframe 62,480 hrs · 45,866 cycles

CRACKED LONGERON 20L BS 995. DAMAGE WAS REMOVED AND REPAIR FABRCATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, 51-10-3, PAR 21 AND 14 AND 53-02, FIG 22.

Part: SKIN — CORRODED (BS 1315) · corrosion level 2 · airframe 62,488 hrs · 45,871 cycles

AT HMV 4, CORROSION WAS FOUND ON EXISTING BS 1315 L22 DOUBLER AND TRIPLER. REPAIRS WERE REPLACED. ACCOMPLISH ER/A 502881-14, REV B OR LATER REVISION SECTION III INSPECTION WITHIN EVERY 8000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION II PERMANENT REPAIR. ASSOCIATED ER/A 88-502881 ADDED FOR AC 0968. AREA WAS REPAIRED IAW ER/A 502881-14, REV B AND ETI-88-14-148, REV 2.

Part: SKIN — WORN (BS 1497-1510) · airframe 62,480 hrs · 45,866 cycles

WEAR ON FUSELAGE SKIN BETWEEN BS 1497-1510. WEAR REMOVED AND FABRICATED FOR REPAIR DOUBLER ND FILLER IAW SRM 53-01, FIG 4.

Part: ANGLE — CRACKED (BS 788) · airframe 62,480 hrs · 45,866 cycles

CRACKS ON ANGLE AT BS 788 BETWEEN LONGERON 27 - 28L AND 27 - 28R AT MID CARGO BAY. ANGLE REPLACED IAW SRM 51-30-5 AND 51-10-3, PAR 14 AND 21.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,480 hrs · 45,866 cycles

EXPOSED COMPOSITE MATERIAL ON RT & LT SURFACES OF RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1A, PH 23 AND JIC 000-0033.

Part: SUPPORT — CORRODED (BS 370-427) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION AND ELONGATED HOLES ON SCUFF PLATE SUPPORT BS 370-427 LONGERON 29R AT FWD CARGO BAY. SCUFF PLATE SUPPORT REPLACED IAW SRM 51-10-3, PAR 14, 21 AND 26, 51-10-4, 53-001, FIG 1., 51-30-2 AND 51-30-1.

Part: DOUBLER — CRACKED (FAIRING) · airframe 62,480 hrs · 45,866 cycles

CRACKED REPAIR DOUBLER ON LOWER FAIRING ASSY 3703A. REPAIR DOUBLER WAS REMOVED IAW SRM 51-30-2, NEW DOUBLER AND FILLER WERE FABRICATED IAW SRM 55-01, FIG 4. NEW DOUBLER AND FILLER WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, REPAIR PARTS WERE INSTALLED IAW SRM 55-01, FIG 4.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 62,480 hrs · 45,866 cycles

CRACKED REPAIR DOUBLER ON VERTICAL STABILIZER AROUND ACCESS PLATE 6301A CUTOUT. REPAIR DOUBLER REMOVED AND REPLACED IAW SRM 55-05, FIG 3 AND 51-30-2, 51-10-3, PAR 14 AND 21 AND PS900-5-1, NR 04.

Part: WEB — CRACKED (ACCESSORY BAY) · airframe 62,480 hrs · 45,866 cycles

CRACKED WEB ON RT SIDE OF VENTRAL STAIRWAY SHROUD TO TORQUE TUBE AT ACCESSORY COMPARTMENT, BS 1485. WEB WAS REMOVED IAW SRM 51-30-2 AND 51-30-5 NEW WEB WAS DRILLED IAW SRM 51-10-4. NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — CRACKED · airframe 62,480 hrs · 45,866 cycles

DURING MAINTENANCE, FLOOR PANEL WAS FOUND CRACKED. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05, FIG 131B, SRM 51-10-3 & 51-30-2.

Part: STRUCTURE — WORN (BUTTE DOOR) · airframe 62,480 hrs · 45,866 cycles

WORN REPAIR ON INBD EDGE OF LT INBD BUTTE DOOR AT OTBD FLAP. DOUBLER REPLACED IAW SRM 57-01, FIG 3, SRM 51-30-2, 51-30-1, SRM 51-10-3 PAR 14 AND 21.

Part: SUPPORT — CRACKED (RT WING) · airframe 62,480 hrs · 45,866 cycles

CRACK ON SUPPORT OF REFUEL OVERPRESSURE IN FUEL SERVICE PANEL AT RT WING. SUPPORT WAS REPLACED IAW SRM 51-10-3, PAR 14-21 AND DWG 3920769, REV E.

Part: SKIN — WORN (BUTTE DOOR) · airframe 62,480 hrs · 45,866 cycles

WORN SKIN ON INBD BUTTE DOOR OF LT INBD FLAP. SKIN REPLACED IAW SRM 57-01, FIG 3 51-10-3, PAR 14 AND 21 51-30-1, 51-30-2.

Part: CHANNEL — DAMAGED (BS 941) · airframe 62,480 hrs · 45,866 cycles

HOLES ELONGATE AFT DOOR FRAME CHANNEL BS 941 X -24 TO X 24. CHANNEL WAS REPLACED IAW SRM 51-30-2, 51-10-3, PAR 14, 21 SRM 51-10-4, STA 941.

Part: CUSP WEB — CORRODED (BS 1055-1070) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON CUSP WEB X-54 TO -60, BS 1070-1055, RT SIDE. CUSP WEB REPAIRED IAW SRM 51-30-5, FIG 131.

Part: CUSP WEB — CANNING (BS 1022-1060) · airframe 62,480 hrs · 45,866 cycles

DEFFECT OIL CANNING ON CUSP WEB RBL 44 - 60 BS 1022-1060. CUSP WEB REPAIRED IAW SRM 51-30-5, FIG 131 SRM 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1212 - 1231 LONGERON 29L IN AFT CARGO BAY. INTERCOSTAL REPLACED IAW SRM 51-30-2; 51- 30-3, 51-30-5, 51-10-3 PARA 21 AND 14.

Part: CARGO TRACK — CORRODED (BS 1146-1219) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1146 - 1219. CORROSION REMOVED IAW SRM 51-10-3, PAR-26 AND FOUND OUT OF LIMITS SRM 53-01, FIG-1, CARGO TRACK REMOVED AND REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, SRM 51-30-2 AND 51-30-1.

Part: TEE FITTING — CORRODED (BS 1380) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON TEE FITTING ON FRAME, BS 1380, BETWEEN X 15 TO X-15. TEE FITTING REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, & 51-10-3, PAR 26 21-14.

Part: FITTING — CRACKED (BS 1338) · airframe 62,480 hrs · 45,866 cycles

CRACKED FITTING ON BS 1338 AND BL 0 AT UPPER VENTRAL DOOR. FITTING REPLACED IAW SRM 51-30-2 & 51-30-5 AND DWG 9915562, REV V.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 62,480 hrs · 45,866 cycles

ACCESS PANEL 1410C DAMAGED. ACCESS PANEL REPLACED.

Part: ANGLE — CORRODED (BS 180-200) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON CUSP ANGLE BETWEEN BS 180 - 200 Y-60. ANGLE REPAIRED IAW SRM 53-05, FIG 55 AND ER/A 521188-14 MA REV ORIG AND ER/A 526990-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 788-807) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB, X-54 TO X-60, BS 788-807. CUSP WEB REPAIRED IAW SRM 53-14-2 AND 53-05, FIG 131A AND TREATED/PAINTED SRM 51-103.

Part: DOOR FRAME — CRACKED (BS 918) · airframe 62,480 hrs · 45,866 cycles

CRACK AT LT AFT EMERGENCY EXIT UPPER DOOR FRAME BS 918. DOOR FRAME REPAIRED IAW DWG J060238, SRM 53-05, FIG 32, 53-30-2 AND 53-30-8.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1367C. ACCESS PANEL WAS REWORKED AND WAS FOUND OUT OF LIMITS. ACCESS PANEL REPLACED.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 62,480 hrs · 45,866 cycles

FLOOR PANEL 769A CRACKED. REPAIRED IAW SRM 51-20-0, 53-01, FIG 4, SHEET 4.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL1466C. ACCESS PANEL REPLACED.

Part: PAN — CRACKED (R1 DOORWAY) · airframe 62,480 hrs · 45,866 cycles

CRACKED PAN ON R1 DOOR FRAME LOWER SECTION AT THRESHOLD R1 SERVICE DOOR. PAN REPAIRED IAW ETI 88-14-141, REV 2 AND ER/A 526990-14, REV, ORIGINAL.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION FOUND ON COUNTERSINKS OF ACCESS PANEL ON RT WING UPPER SURFACE. CORROSION REMOVED IAW SRM 51-10-3 AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON COUNTERSINK AREA OF ACCESS PANEL 1335, LT WING UPPER SURFACE. ACCESS PANEL REPLACED.

Part: CUSP WEB — CORRODED (BS 660-683) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB X-54 TO X-58 BS 660-683. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-12, SRM 51-10-3, PAR 14, 21.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON ACCESS PANEL LT WING UPPER SURFACE. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND WITHIN LIMITS IAW SRM 51-22- 2A. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1311C. ACCESS PANEL WAS REWORKED AND FOUND OUT OF LIMITS. ACCESS PANEL REPLACED.

Part: RIB — WORN (BS 1401) · airframe 62,480 hrs · 45,866 cycles

WORN RIBS BS 1401 BETWEEN X=18 AND X=-18 AT VENTRAL STAIRWAY SHROUD. RIBS REPAIRED IAW SRM 53-01, FIG 2 AND DWG 9911998, REV D.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL 1472C. ACCESS PANEL REMOVED IAW SRM 51-10-30 AND FOUND OUT OF LIMITS. ACCESS PANEL REPLACED IAW AMM 28-40-02.

Part: CUSP WEB — CANNING (BS 727-731) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

OIL CANNING AND CORROSION ON REPAIR DOUBLER OF RT CUSP WEB X=-54, BS 727-731. CUSP WEB REPAIRED IAW SRM 51-30-2, 53-05, FIG 131A-10 , 51-10-3, PAR 14 & 21 AND 51-30-5.

Part: CUSP WEB — CANNING (BS 1174-1250) · airframe 62,480 hrs · 45,866 cycles

OIL CANNING ON CUSP WEB X=-44 TO -54 BS 1174-1250. CUSP WEB REPLACED IAW SRM 51-30-23, & 51-30-5, 51-30-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,480 hrs · 45,866 cycles

CRACKS IN ANGLES OF MID CABIN FLOOR PANEL. FLOOR PANEL REPLACED ANGLES REMOVED SRM 51-30-1 DRILLED SRM 51-10-4 INSTALLED DWG 9936639, REV P .

Part: FLOOR PANEL — DEBONDED (FWD CABIN) · airframe 62,480 hrs · 45,866 cycles

DISBONDED HONEYCOMB IN FWD CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-20.

Part: CUSP WEB — CORRODED (BS 543) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 AND X=-60 BS 543. REPAIRED IAW SRM 53-05, FIG 131A-9 AND SRM 53-10-3, PAR 14,21.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 62,480 hrs · 45,866 cycles

CRACKED RT FLOOR PANEL 4416A IN COCKPIT. FLOOR PANEL REPAIRED IAW AMM 25-00-00-801.

Part: CUSP WEB — DAMAGED (BS 826-845) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB AND REPAIR DOUBLER BS 826-845 BETWEEN X=54-60. CRACK WAS FOUND ON CUSP WEB, SPLICE IS BENT, MISSING SEALANT ON REPAIR AND MISINSTALLED FASTENERS. REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: SKIN — MISREPAIRED (BS 314) · airframe 62,480 hrs · 45,866 cycles

IMPROPER REPAIR ON FUESELAGE SKIN BS 314 BETWEEN LONGERON 27-28L. REPAIRED IAW SRM 53-04-2, PAR 36, 2, 1A.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT HORIZONTAL STABILIZER. PREVIOUS REPAIR BUSHING WAS FOUND WITH SCRATCHES. CORROSION REPAIRED IAW ER/A 526991-14 REV ORIGINAL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 62,480 hrs · 45,866 cycles

DAMAGED FERRULE IN FWD CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FRAME — CRACKED (BS 1485) · airframe 62,480 hrs · 45,866 cycles

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

Part: SKIN — CORRODED (BS 466-478) · corrosion level 2 · airframe 62,488 hrs · 45,871 cycles

CORROSION ON PREVIOUS REPAIR DOUBLERS X=-52 TO X=- 60 FROM STA Y=466 TO 478, RT CUSP WEB AT FLOOR STRUCTURE, MRB 53-037-01, SM. MISSING SEALANT LIGHTNING HOLES, IMPROPER INSTALL FASTENERS, BURRS BELOW REPAIR AREA. REF CARD 98 Z.201, CARD 312, ZONE 201. RE-WRITE FROM CARD 98, ZONE 201. PREVIUS REPAIR WAS ATTENDED IAW SRM 51-20-0, 51-30-2 AND PS 900-142-1 N1.

Part: INTERCOSTAL — CRACKED (BS 937) · airframe 62,480 hrs · 45,866 cycles

CRACKED INTERCOSTAL BS 937 X=60 IN LT WHEEL WELL. INTERCOSTAL REMOVED, NEW FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 506-514) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR DOUBLERS X=-55 TO X=-60 ON RT CUSP WEB BS 506 - 514. REPAIR DOUBLERS REPLACED IAW SRM 53-05, FIG 131A-24, SRM 51-10-3, PAR 14,21 SRM 51-30-5.

Part: SUPPORT — BROKEN (BS 1231-1250) · airframe 62,480 hrs · 45,866 cycles

BROKEN SLANT SUPPORT BS 1231 - 1250 BETWEEN LONGERONS 26 - 27L IN AFT CARGO BAY. BROKEN SLANT SUPPORT WAS REPLACED IAW SRM 51-30-2; 51-10-4, 51-10-3 PAR 21,14 AND ER/A 413029-MA, REV D.

Part: BRACKET — CRACKED (TAILCONE) · airframe 62,480 hrs · 45,866 cycles

CRACKED RT UPPER ATTACH TAILCONE BRACKET. BRACKET REMOVED AND REPLACED IAW SRM 51-30-2, DWG 991195, REV: AV, SRM 51-10-3P 14/21 AND SRM 51-30-2.

Part: ANGLE — CRACKED (BS 1463) · airframe 62,480 hrs · 45,866 cycles

CRACKED ANGLE BS 1463 BETWEEN LONGERONS 3 - 5R IN AFT ACCESORY BAY. R & R ANGLE IAW SRM 51-30-5, SRM 51-10-2 SRM 53-14-4 & SRM 51-10-3 PAR 14 AND 21.

Part: SUPPORT — CRACKED (BS 1231) · airframe 62,480 hrs · 45,866 cycles

CRACKED SLANT SUPPORT BS 1231 BETWEEN LONG 29R - 28L IN THE AFT CARGO BAY. CRACKED SLANT SUPPORT REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 21,14 AND ER/A 413029-14MA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,480 hrs · 45,866 cycles

DELAMINATED FLOOR PANEL. REPAIRED IAW HMM 52-20-01-201.

Part: CUSP WEB — CORRODED (BS 550-558) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR DOUBLER X=-52 TO X=-60, BS 550 - 558 ON RT CUSP WEB. REPAIR DOUBLER REPLACED IAW SRM 53-05, FIG 131A-14.

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 62,480 hrs · 45,866 cycles

CRACKED STIFFENER BELOW OF MIXING TUBE SETTLEMENT AREA INNER SURFACE OF NOSE COWL AT RT ENGINE. STIFFERNER REPLACED IAW DWG 5938038, REV "AL".

Part: ANGLE — CRACKED (BS 522 BULKHEAD) · airframe 62,480 hrs · 45,866 cycles

CRACKED ANGLE ON SIDEWALL SUPPORT UPPER SECTION BS 522 IN FWD CARGO BAY ON AFT BULKHEAD. ANGLE REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CRACKED (BS 218-237) · airframe 62,480 hrs · 45,866 cycles

SEVERAL CRACKS ON CUSP WEB X=-54, BS 218-237. CUSP WEB REPLACED IAW SRM 51-30-2 AND 51-10-3, PAR 21 AND 14.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,480 hrs · 45,866 cycles

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

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL 1460C COUNTERSINKS. ACCESS PANEL FOUND OUT OF LIMITS AND WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 997-999) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB FROM BS 997 - 999 BETWEEN X=54 TO 60. REPAIRED IAW SRM 53-05, FIG 131A -13 AND RMS 41-10-3, PAR 14.21.

Part: ACCESS PANEL — CRACKED (COCKPIT) · airframe 62,480 hrs · 45,866 cycles

CRACKED COCKPIT ACCESS PANEL 4415A. ACCESS PANEL REPAIRED AND INSTALLED IAW SRM 53-01 FIG 2, SRM 51-10-3, PAR 14, 21 AND SRM 51-30-2.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 62,480 hrs · 45,866 cycles

DELAMINATION ON UPPER AND LOWER SKIN AT LT ELEVATOR ANTI-FLOAT TAB. LT ANTI-FLOAT TAB WAS REPLACED.

Part: WEB — CRACKED (BS 1485) · airframe 62,480 hrs · 45,866 cycles

CRACKED WEB AT BS 1485 LONGERON 15R IN THE AFT ACCESSORY COMPARTMENT. THE WEB WAS REPAIRED IAW SRM 53-01 AND 51-10-3 PAR 21,14.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON HORIZONTAL STABILIZER LT INBD HINGE PLATE LUG HOLE. AT VERTICAL STABILIZER, SM, CORROSION WAS ATTENDED IAW SRM 55-02, FIG 28 HOLE HINGE LT INB ID 1.3755 THEREFORE ITS WITHIN LIMITS IAW SRM 55-02, FIG 28.

Part: SKIN — DAMAGED (BS 275-294) · airframe 62,480 hrs · 45,866 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN LONGERON 7L BETWEEN BS 275- 294. REPAIRED IAW SRM 53-04-1 PAR 6C, 2 COND, 2 AND 53-04-1, PAR 6D, 1 COND 1 AND SRM 51-30-2 AND 51-10-3, PAR 14-21.

Part: CUSP WEB — CORRODED (BS 566-578) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION FOUND ON REPAIR DOUBLERS X=-54 TO X=-60 BS 566 - 578 ON RT CUSP WEB. REPAIR DOUBLERS ON CUSP WEB WERE REPLACED IAW 53-05, FIG 131 A-6.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON HORIZONTAL STABILIZER RT OTBD HINGE PLATE LUG HOLE. AT VERTICAL STABILIZER, SM, CARD 131, ZONE 060. CORROSION WAS ATTENDED IAW SRM 55-02, FIG 28, HOLE HINGE RT OTBD ID 1.376 THEREFORE IT`S WITHIN LIMITS IAW SRM 55-02, FIG 28.

Part: INTERCOSTAL — CORRODED (BS 1149-1155) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON INTERCOSTAL BS 1149-1155 LONGERON 29 -30R. INTERCOSTAL REPLACED IAW DWG 5936071 AND SRM 51-30-5 AND 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 466-478) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR DOUBLERS X=-52 TO X=-60 FROM BS 466 - 478 ON RT CUSP WEB. DOUBLER REPLACED IAW SRM 53-05, FIG 131, A-6 AND 51-10-3, PAR 21 AND 14.

Part: SKIN — CORRODED (BS 726-807) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING BS 726 - 807 BETWEEN LONGERONS 18 - 19RT. CORROSION WAS REMOVED AND FOUND WITHIN LIMITS, TREATED AND PAINTED IAW SRM 51-10-3, PAR 26,21 AND 14 AND 53-04, PAR.57B, 2, A.

Part: SKIN — CORRODED (BS 726-826) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING AREA BS 726 - 826 BETWEEN LONGERONS 22 - 30R. CORROSION REMOVED, REWORKED AREA TREATED AND PAINTED AND FOUND WITHIN LIMITS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,480 hrs · 45,866 cycles

CRACKED ANGLE BETWEEN AFT PAN AND NR 4 BEAM AT FWD R1 SERVICE DOOR. ANGLE WAS REMOVED, NEW FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, DGW 9911582, REV T, SRM 51-1-3, PAR 14 AND 21 AND SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 706-712) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER, BS 706-712 X =54-60. REPAIR DOUBLER REPLACED IAW SRM 53-05, FIG 131A-1.

Part: SKIN — CORRODED (BS 1079-1131) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUESELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING AREA BS 1079 - 1131 BETWEEN LONGERONS 24 TO 30L. CORROSION REMOVED AND FOUND WITHIN LIMITS.

Part: INTERCOSTAL — CORRODED (BS 1380) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION FOUND ON INTERCOSTAL BS 1380 + 15 AT LOWER AFT ACCESSORY COMPARMENT. REPAIRED IAW SRM 51-70-5, FIG 1 & 51-10-3, PAR. 21, 14 AND 38.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,480 hrs · 45,866 cycles

CRACK ON PAN AT UPPER CORNER OF RT AFT EMERGENCY EXIT DOOR. PAN REPAIRED IAW SRM 52-05D, FIG 51.

Part: SEAT TRACK — CORRODED (BS 894-1026) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT SEAT TRACK X=54, BS 894-1026. CORROSION REMOVED IAW SRM 51-10-3 PAR 26-(VT) AND FOUND OUT OF LIMITS IAW SRM 53-05, FIG 4B. SEAT TRACK REPLACED IAW SRM 53-05 FIG 4F, SRM 53-05 FIG. 4F AND DWG -3925837, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 148-200 X=-5 TO -5. FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-30-1, 51-10-3 PAR 14 - 21 AND 51-10-4.

Part: CUSP WEB — CRACKED (BS 545) · airframe 62,480 hrs · 45,866 cycles

CRACKED LT CUSP WEB AT BS 545 BETWEEN X=54 TO 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 582) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB X= -54 TO X=-58 BS 582. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A - 13.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 62,480 hrs · 45,866 cycles

CRACK ON NR 1 BEAM AT FWD SERVICE DOOR. NR 1 BEAM WAS REMOVED AND A NEW BEAM WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-4, SRM 51-10-3, PAR 14 AND 21.

Part: SKIN — CORRODED (BS 1060-1131) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET AREA FAIRING BS 1060-1131 BETWEEN LONGERON 18-24LT. CORROSION REMOVED AND REWORKED AREA FOUND TO BE WITHIN LIMITS AND WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21, 21 AND 14 AND 53-04, AR 57B (2)(A).

Part: SKIN — CORRODED (BS 947-1068) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING AREA BS 947 - 1068 LONGERON 18L. CORROSION WAS REMOVED AND REWORKED AND FOUND WITHIN LIMITS AND WAS TREATED AND PAINTED IAW 51-10-3, PAR 26,21 AND 14 AND 53-04, PAR 57B (2)(A).

Part: SKIN — CORRODED (BS 927-1098) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING AREA BS 927-1098 LONGERON 18RT. CORROSION REMOVED AND REWORKED AREA FOUND TO BE WITHIN LIMITS AND WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 26,21 AND 14 AND 53-04, PAR 57B (2)(A).

Part: SKIN — CORRODED (BS 726-826) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING AREA BS 726-826 BETWEEN LONGERONS 24 - 30L. CORROSION REMOVED AND REWORKED AREA FOUND TO BE WITHIN LIMITS AND WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21 AND 14 AND 53-04 PAR 57B (2)(A).

Part: SKIN — CORRODED (BS 1079-1131) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING AREA STA Y=1079 TO Y=1131 BETWEEN LONGERONS 24LT-30 MRB 57-600-01, CARD 171, ZONE 10, CORROSION AND SOME FASTENERS WERE REMOVED REWORKED AREA IT`S WITHIN LIMITS AND WAS TREATED AND PAINTED FASTENERS REMOVED WERE INSTALLED IAW SRM 53-04, PAR 57B (2)(A) AND 51-10-3, PAR 26, 21 AND 14 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 640) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB X=-54 TO X=-58 BS 640. CUSP WEB REPLACED IAW SRM 53-05, FIG 131A-5 SRM 51-10-3, PAR 14, 21, 38 SRM 51-30-5.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 62,480 hrs · 45,866 cycles

CRACKED ANGLE AT FORWARD SERVICE DOOR. ANGLE REMOVED AND NEW FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-5, DWG 9911579 REV L SRM 51-10-3 PAR 14 AND 21.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR SPACER ON MID CARGO BAY DOOR FRAME BS 655-674. SPACER REPLACED IAW SRM 53-05, FIG 123, SRM 51-10-3 14, 21-38, SRM 51-30-5.

Part: CUSP WEB — DAMAGED (BS 946-984) · airframe 62,480 hrs · 45,866 cycles

ELONGATED HOLES ON LT CUSP WEB BS 946-984 BETWEEN X=44-X=60. CUSP WEB REPAIRED IAW SRM 53-05 FIG 131A-11, SRM 51-10-3, PAR 21 AND 14 AND SRM 51-30-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,480 hrs · 45,866 cycles

CRACKED ANGLE BETWEEN AFT PAN AND NR 1 BEAM AT FWD R1 SERVICE DOOR. ANGLE WAS REMOVED, NEW FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-5, SRM 51-10-3, PAR 14 AND 21 DWG 9911579, REV L.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LEFT MAIN FUEL TANK ACCESS PLATE 1371C COUNTERSINK HOLES. ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 1414C, 1409C, 1436C, 1410 ON RT WING UPPER SURFACE. CORROSION REMOVED IAW SRM 51-22-2A. ACCESS PANELS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1373C COUNTERSINK HOLES. ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 1184-1233) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON CUSP WEB X=-54 TO -60 BS 1184-1233 RT SIDE. FASTENERS AND CORROSION WERE REMOVED IAW SRM 51-30-2 AND 51-30-3, PAR-26.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,480 hrs · 45,866 cycles

CRACK ON LONGERON 16L, BS 1437 IN AFT ACCESSORY BAY. LONGERON REPLACED IAW SRM 53-14-4 AND 51-30-2, 51-10-3 PAR 21, 24.

Part: CUSP WEB — CORRODED (BS 826-845) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB AND REPAIR DOUBLER BS 826-845 X=54-60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 62,480 hrs · 45,866 cycles

FWD REPAIR DOUBLER ON FWD CARGO DOOR WORN. DAMAGE DOUBLERS REMOVED AND REPLACED IAW SRM 51-30-2, SRM 52-05D FIG 806D, SRM 51-10-3 PAR 14 AND 21, AND INSTALLED IAW 51-30-2.

Part: CUSP WEB — CORRODED (BS 561-712) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB, X=-54 TO X=-58 FROM BS 561 - 712. CORROSION REMOVED IAW SRM 51-10-3 PAR 21, 14 AND 26 IAW ER/A 508307-14, A REV A.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,480 hrs · 45,866 cycles

CRACK ON PAN AT FWD UPPER CORNER OF RT FWD EMERGENCY EXIT DOOR. FWD UPPER CORNER PAN WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1365C, COUNTERSINK HOLES. ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 237-256) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON CUSP WEB BS 237-256 BETWEEN X=54 AND X=60. CUSP WEB REPAIRED AND INSTALLED, IAW SRM 53-05 FIG 161, A-14, AND SRM 51-10-3 PAR 14 AND 21 AND SRM 51-30-2 AND 51-30-5.

Part: BUSHING — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON BUSHING ON AFT EDGE OF RT WING HEATER BLANKET. BUSHING REPLACED IAW SRM 51-30-10.

Part: LONGERON — CRACKED (BS 160) · airframe 62,480 hrs · 45,866 cycles

CRACK ON LONGERON 3L BS 160. LONGERON REPAIRED IAW SRM 53-02, FIG 18, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,480 hrs · 45,866 cycles

CRACK ON PAN AT FWD UPPER CORNER OF LT FWD EMERGENCY EXIT DOOR. PAN WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: CUSP WEB — CORRODED (BS 523-530) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR DOUBLER X=-55 TO X=-60, BS 523 - 530 ON RT CUSP WEB. REPAIR DOUBLER REPLACED IAW SRM 53-05, FIG 131A.

Part: SKIN — DAMAGED (BS 617-693) · airframe 62,480 hrs · 45,866 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN LONGERONS 4-5R, BS 617-693. REPAIRED IAW SRM 53-04-1, PAR 6C, 2, COND 2 AND 53-04-1 PAR 6D, 1 COND 1 ALSO SRM 51-30-2.

Part: SEAT TRACK — WORN (BS 797-1006) · airframe 62,480 hrs · 45,866 cycles

LT SEAT TRACK X=54 BETWEEN BS 797-1006 WORN. WEAR REMOVED IAW SRM 51-10-3, PAR 26. FOUND OUT OF LIMITS IAW SRM 53-05, FIG 4B. SEAT TRACK REPLACED IAW SRM 53-05, FIG 4F.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1355C. ACCESS PANEL REPLACED.

Part: FRAME — CRACKED (BS 1451) · airframe 62,480 hrs · 45,866 cycles

CRACK ON FRAME, BS 1451 LONGERON 1, AFT ACCESSORY BAY, FRAME REPLACED IAW SRM 51-30-2 AND 51-30-5, 51-10-3, PAR 21 AND 14 DWG 99118060-3, REV= L.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PLATE 1478C. ACCESS PANEL REPLACED.

Part: CUSP WEB — CORRODED (BS 644-655) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER BS 644-655 X=54-60. REPAIR REPLACED IAW SRM 53-05, FIG 131A-14 AND 51-30-2, 51-10-3 PAR 14-21.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL 1454C. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1357C. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PANEL 1307C. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL 1456C. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT MAIN FUEL TANK ACCESS PANEL 1464C. FUEL TANK ACCESS PANEL REPLACED.

Part: FLOOR SUPPORT — CRACKED (BS 984-965) · airframe 62,480 hrs · 45,866 cycles

CRACKED FLOOR SUPPORT BS 984 - 965 X=-34 . FLOOR SUPPORT REMOVED, NEW FLOOR SUPPORT DRILLED, ADJUSTED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5 51-10-4, 51-10-3, PAR 21 AND 14.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 62,480 hrs · 45,866 cycles

DISBONDED HONEYCOMB IN AFT CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (BS 465-557) · corrosion level 2 · airframe 62,488 hrs · 45,871 cycles

CORROSION ON LT CUSP WEB UPPER/LOWER SURFACE, STA Y=465-484 AND Y=541-557 X=54-60 AT CABIN FLOOR STRUCTURE, MRB 53- 037-01, SM, CARD 53, ZONE 201. CORROSION WAS ATTENDED IAW SRM 51-10-3, PAR 26, 21, 14 AND 38 CORROSION ON STA Y=545 WAS FOUND AOUT LIMITS THEREFORE WILL BE ATTENDED WITH NRC 20000019100, CARD 291, ZONE 201.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,480 hrs · 45,866 cycles

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

Part: CUSP WEB — CRACKED (BS 256-275) · airframe 62,480 hrs · 45,866 cycles

CRACKED CUSP WEB BETWEEN BS 256-275, X=54-60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131 A -6.

Part: CUSP WEB — CORRODED (BS 826-845) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB X=-48 TO X=-60, BS 826 - 845. CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-2, 51-60-0, 51-10-3 PARA 14, 21, PSG00-5-1-04.

Part: RIB — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON SLAT TRACK SUPPORT RIB ON XOS=286, XOS=240, XOS=198 OF SLAT TRACK 2 RT. CORROSION ON SLAT TRACK SUPPORT RIB HOLES ON STA XOS= 286, XOS=240, XOS=198 OF SLAT TRACK 2 RT WERE REMOVED. BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR. 9.

Part: LONGERON — CRACKED (BS 160) · airframe 62,480 hrs · 45,866 cycles

CRACKED LONGERON 4 LT BS 160 AT CABIN FUSELAGE STRUCTURE. LONGERON REPLACED IAW SRM 53-02, 51-30-5 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 731-750) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR OF RT CUSP WEB X= -54 TO X=60 BETWEEN BS 731 - 750. REPAIR WAS REPLACED IAW SRM 53-05, FIG 131A-14, 51-30-2, 51-10-3, PAR 14, 21 51-10-3, PAR 38.

Part: CUSP WEB — CORRODED (BS 682-688) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER BS 682-688, X =54-60. CORROSION REMOVED IAW SRM 51-30-2, 55- 05, FIG 131A-13, 51-10-3, PAR 14 AND 21 AND 51-10-3, PAR 38.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,480 hrs · 45,866 cycles

CRACK ON LONGERON 2L BS 1418. LONGERON REPLACED IAW SRM 53-14-4.

Part: RIB — CORRODED (NR 2 SLAT) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT SLAT PANEL NR 2 RIB FITTING FWD LUG HOLE STA XOS=285, CARD 14, ZONE 11 CORROSION ON LT SLAT PANEL NR 2 RIB FITTING FWD LUG HOLE STA XOS 285 WAS REMOVED WITH A ID 01.1225" AND WAS INSTALLED A BUSHING WITH AN OD 0 1.123" IAW SRM 57-02.

Part: STRUCTURE — CORRODED (TAIL) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON HORIZONTAL STABILIZER LT/RT HINGES PLATES INNER SURFACES AT VERTICAL STABILIZER. CORROSION WAS REMOVED IAW SRM 51-10-3, SRM 55-02, FIG 28, SRM 51-10-3, PAR. 14.

Part: STRUCTURE — WORN (CARGO DOOR) · airframe 62,480 hrs · 45,866 cycles

REPAIR DOUBLER OF AFT HINGE AT AFT CARGO DOOR WORN. AFT CARGO DOOR HINGE WAS REMOVED IAW AMM 52-31-02, DOUBLER REMOVED IAW SRM 51-30-2, DOUBLER FABRICATED IAW SRM 52-05, FIG 35A. NEW DOUBLER TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21 AND INSTALLED IAW SRM 51-30- 2.

Part: CUSP WEB — CORRODED (BS 452-568) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER BS 452-568 X=60 - 54. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-2.

Part: RIB — CORRODED (NR 3 SLAT) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT SLAT PANEL NR 3, RIB FITTING FWD LUG HOLE STA XOS=285. CORROSION ON LT SLAT PANEL NR3 RIB FITTING FWD LUG HOLE STA XOS =285 WAS REPAIRED IAW SRM 57-02, PAR 9 WITH A BUSHING ON THE HOLE.

Part: WEB — PUNCTURED (BS 200) · airframe 62,480 hrs · 45,866 cycles

PUNCTURE ON LT WEB BS 200, BETWEEN X=22 TO X=26 AT PAX CABIN FLOOR STRUCTURE. DAMAGE WERE REMOVED IAW SRM 51-10-4 AND 53-01 HOLES WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21 PLUGS WERE INSTALLED IAW SRM 51-10-3 AND 51-10-4.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,480 hrs · 45,866 cycles

DAMAGED FERRULE IN AFT CABIN FLOOR PANEL. FLOOR PANEL FABRICATED AND REPLACED FERRULE IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,480 hrs · 45,866 cycles

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

Part: CUSP WEB — CORRODED (BS 750-769) · airframe 62,480 hrs · 45,866 cycles

CORROSION ON REPAIR OF RT CUSP WEB X=-54 TO X=60 BETWEEN BS 750 - 769. REPAIR REPLACED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 958-973) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-44, BS 958 - 973. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-15, 51-10-3 PAR 14 AND 21.

Part: SKIN — CRACKED (BS 1380) · airframe 62,480 hrs · 45,866 cycles

CRACK ON FUSELAGE SKIN BS 1380 BETWEEN LONGERONS 13 - 14R. REPAIRED IAW SRM 53-04, FIG 18, SRM 51-10-3, PAR 21-14, SRM 51-30-2, SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 661-681) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT SEAT TRACK PLUGS X=-54, BS 661 - 681. DAMAGED PLUGS WERE REMOVED AND NEW PLUGS WERE REWORKED TREATED, PAINTED AND INSTALLED IAW SRM 51-30-1, 53-05 AND 51-10-3, PAR 21 AND 14.

Part: SEAT TRACK — CORRODED (BS 610-613) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON LT SEAT TRACK BETWEEN BS 610-613. , DAMAGE REMOVED AND REWORKED AND INSTALLED IAW SRM 51-30-1,53-05 AND 51-10-3,

Part: SEAT TRACK — CORRODED (BS 412-432) · corrosion level 2 · airframe 62,480 hrs · 45,866 cycles

CORROSION ON RT SEAT TRACK PLUGS, BS 412-432 X=-54. DAMAGE PLUGS WERE REMOVED AND NEW PLUGS WERE REWORKED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-1, 53-05 AND 51-10-3, PAR 21 AND 14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,398 hrs · 45,815 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE IN THE TAILCONE AREA. MAINTENANCE REPLACED THE BATTERY PACKS AND THE LIGHTS OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,405 hrs · 45,819 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT 24DE. MAINTENANCE R & R THE BATTERY PACK AT 24DE AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: PIN — OUT OF POSITION (L1 DOOR SLIDE) · airframe 62,212 hrs · 45,680 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THE L1 DOOR SLIDE PARACHUTE PINS OUT OF POSITION. MAINTENANCE R & R THE SLIDE PACK.

Part: SKIN — DAMAGED (BS 427) · airframe 61,638 hrs · 45,274 cycles

NON ROUTINE CHECK, FUSELAGE DAMAGE AT BS 427 AFT OF ACFT GROUND HOOKUP DOOR. REPAIRED IAW PRI 523787-14, REV O-5.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,155 hrs · 44,956 cycles

DURING LINE CHECK, NOTED THE SEAT EMERGENCY PATH LIGHT AT SEAT 14 WAS INOPERATIVE. REPLACED LIGHT HARNESS AT SEAT 14DE IAW AMM 33-53 AND OPS CHECKS GOOD.

Part: COVER — DAMAGED (TAILCONE SLIDE) · airframe 59,265 hrs · 43,611 cycles

TAILCONE SLIDE COVER IN POOR CONDITON, PLACARDS AND RELEASE LANYARD HOOK AND LOOP AND WORDING ON HOOK AND LOOP PATCH IS IN POOR CONDITON. REPLACED SLIDE COVER PLACARD AND INSTALLED NEW RELEASE LANYARD WITH HOOK AND LOOP IAW AMM 53-53.

Part: BRACKET — LOOSE (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

TAILCONE TOP LT LOCK RECEIVER BRACKET TO CONE RIVETS LOOSE. REPLACED LOOSE RIVETS IAW SRM 51-30. REQUIRED INSPECTION COMPLETED.

Part: BRACKET — LOOSE (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

TOP RT TAILCONE RECEIVER BRACKET, LOOSE RIVETS TO CONE SKIN. REPLACED LOOSE RIVETS IAW SRM 51-30.

Part: BRACKET — LOOSE (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

BOTTOM LT TAILCONE RECEIVER, LOOSE RIVETS ON BRACKET. REPLACED LOOSE RIVETS IAW AMM 51-30.

Part: SUPPORT BRACKET — BROKEN (TAIL CONE) · airframe 59,265 hrs · 43,611 cycles

TAILCONE SPRING SUPPORT BRACKETS BROKEN OR MISSING. REPLACED BRACKETS AND SPRING & ROUTED CABLE THROUGH PULLEY. TAIL CONE INSTALLATION AND FUNCTIONAL CHECKS ON AMDS WC 5350-01077-0101.

Part: SEAT TRACK — CORRODED (BS 886-905) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED INSPECTION, THE LT SIDE OTBD SEAT TRACK WEB UPPER SURFACE WAS FOUND TO BE CORRODED BETWEEN STA 886 & 905. REPAIRED IAW SRM 51-70-4.

Part: LATCH — LOOSE (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAIL CONE LATCH RECEPTICAL WAS FOUND TO BE LOOSE AT THE TOP RT TAIL CONE LATCH. THE RECEPTICAL WAS VERY LOOSE AND WORKING. REPLACED HARDWARE & RETIGHTENED IAW AMM 53-53-00.

Part: LATCH — WORN (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAIL CONE RELEASE LATCH LT TOP WAS FOUND TO BE WORN AND LOOSE ON FRAME. INSTALLED NEW SPADE, CLEANED AND LUBED LATCH ASSEMBLY. REPLACED SPADE IAW AMM 53-53-00. REQUIRED INSPECTION COMPLETE.

Part: LATCH — WORN (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULE MX, THE TAIL CONE RELEASE LATCH LT BOTTOM WAS FOUND TO BE WORN AND LOOSE ON FRAME. INSTALLED NEW SPADE, CLEANED AND LUBED LATCH ASSY. REPLACED SPADE IAW AMM 53-53-00. REQUIRED INSPECTION COMPLETE.

Part: WARNING LIGHT — ILLUMINATED (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAILCONE WARNING LIGHT ILLUMINATED ON THE OVERHEAD ANNUNCIATOR PANEL. FOUND CIRCUIT BREAKER OUT, R-24 RELAY FOR TAILCONE UNSAFE. CHECKED SWITCH AND LIGHT FUNCTION IAW AMM 53-53-00 FUNCTIONS NORMALLY.

Part: CONDUIT — OUT OF RIG · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, BOTH TAIL CONE LOCK CABLE CONDUITS WERE FOUND TO BE OUT OF RIG LIMITS. ADJUSTED CONDUITS FOR CLEARANCE IAW AMM 53-53-00 AND AMDS 5350-01077-0101. REQUIRED INSPECTION COMPLETED.

Part: HANDLE — UNSECURE (TAILCONE RELEASE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAILCONE RT LOWER LATCH HANDLE WAS FOUND NOT POSITIVELY SEATED IN DOWN POSITION. REPLACED SPRING AND ADJUSTED IAW AMM 53-53-00. REPLACED ARM ON LATCH ASSY FUNCTIONAL CHECK COMPLIED WITH ON AMDS WC 5350-01077-0101.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAILCONE ALIGNMENT RECEPTACLES WERE FOUND WORN. ALSO NOTED SEVERAL ARE LOOSE. REPLACED RECEPTACLES IAW SRM 51-01.

Part: CAM — MISINSTALLED (TAILCONE RELEASE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAILCONE RELEASE CAM ASSY WAS FOUND TO BE IMPROPERLY INSTALLED. THE TAILCONE RELEASE CAM FAILED THE TORQUE REQUIREMENT CHECK. REMOVED CAM ASSY & REPLACED SPACER, PERFORMED CAM TORQUE CHECK IAW AMM 53-53-00 AND AMDS 5350-01077-0101, STEP 7. TORQUE WITHIN LIMITS. COMPLIED WITH REQUIRED INSPECTION.

Part: SLIDER — WORN (TAILCONE RELEASE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAILCONE RELEASE RT UPPER SLIDER BLOCK WAS FOUND WORN. R & R TAILCONE RT UPPER SLIDER BLOCK IAW AMM 53-53-00. REQUIRED INSPECTION COMPLETED.

Part: RELEASE CABLE — MISINSTALLED (TAILCONE) · airframe 59,265 hrs · 43,611 cycles

DURING SCHEDULED MX, THE TAILCONE RELEASE CABLE WAS FOUND IMPROPERLY INSTALLED IN THE SLIDER BLOCK AT THE LT SIDE OF THE TAILCONE SLIDER BLOCK FOR OUTSIDE RELEASE. REPOSITIONED TAILCONE OUTSIDE RELEASE SLIDER BLOCK CABLE IAW AMM 53-53-00. REQUIRED INSPECTION COMPLETED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,020 hrs · 42,071 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31 AND AFT IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — CRACKED (BS 1315 L22L) · airframe 56,948 hrs · 42,027 cycles

FUSELAGE CRACKED AT STA FS 1315.

Part: MODULE — INOPERATIVE (CABIN) · airframe 56,940 hrs · 42,020 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROW 25 OF THE AIRCRAFT TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT MODULE AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,897 hrs · 41,987 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE AFT SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS. RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 56,460 hrs · 41,688 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROW 31 AFT INOPERATIVE. MAINTENANCE FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR. LIGHTS OPERATE NORMAL.

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 56,341 hrs · 41,606 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 13-23 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER PACK B5-101 AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 56,196 hrs · 41,501 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-36DE OF THE CABIN AND IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: HANDLE — FAILED (TAILCONE) · airframe 55,654 hrs · 41,111 cycles

THE TAIL CONE AFT EXTERIOR CHECK HANDLE FAILED PULL TEST.

Part: CABLE — FAILED (AILCONE) · airframe 55,654 hrs · 41,111 cycles

THE AFT INTERIOR TAIL CONE HANDLE FAILED PULL TEST.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

CRACKED FUSELAGE SKIN STATION 1418, S-2R. C/W ERA 496865-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

CRACKED FUSELAGE SKIN AT STATION 1418 L-2L. C/W ERA 496864-14.

Part: RELEASE SYSTEM — FAILED (TAILCONE) · airframe 55,654 hrs · 41,111 cycles

EXTERIOR CLIP PULL TEST WITH THE OUTSIDE HANDLE FAILED DURING AMDS WORK CARD 6908.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

ON 09OCT CORROSION WAS FOUND AT STA 200-256 ON RBL 22 SEAT TRACK. REPAIRED PER MD88 SRM 53-05 LEVEL II CORROSION FINDING.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

DURING PSV CHECK AT MSP, THE RT CROWN FUSELAGE SKIN PANEL STA 1437 BETWEEN LONGERON 2R-3R JUST BELOW THE VERTICAL STABILIZER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE CRACK ORIGINATED FROM THE TOP FASTENER ADJACENT TO SKATE ANGLE. REFERENCEA/C NR 190.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

ON 09OCT11 LEVEL II CORROSION FOUND AT STA 200-256 ON LBL 45 SEAT TRACK. REPAIRED PER MD88 SRM 53-05.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

DURING PSV AT MSP, LT CROWN FUSELAGE SKIN PANEL STA 1437 BETWEEN LONGERON 2L-3L JUST BELOW THE VERTICAL STABILIZER ATTACH ANGLE WAS FOUND TO BE CRACKED. THE CRACK ORIGINATED FROM THE TOP FASTENER ADJACENT TO SKATE ANGLE. REF NR 105.

Part: TAIL CONE — NO TEST (FUSELAGE) · airframe 55,654 hrs · 41,111 cycles

WHILE PERFORMING THE TAIL CONE RELEASE FUNCTIONAL CHECK OPN 6908AD THE TAIL CONE WOULD NOT DEPLOY. NON-ROUTINE CARDS WERE WRITTEN FOR THE REQUIRED REPAIRS.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 55,543 hrs · 41,026 cycles

DURING SERVICE CHECK MAINTENANCE FOUND OVERHEAD COCKPIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED FORWARD BATTERY PACK PER AMM 33-53-00. OPERATION OF LIGHTS NOW CHECKS OK.

Part: SENSOR — SHORTED (MLG DOOR) · airframe 53,073 hrs · 39,294 cycles

DURING FLIGHT AT 26K FT AND SPEED OF 310KTS, THE AMBER "GEAR DOOR OPEN" LIGHT CAME ON. CREW SLOWED TO 280 KTS AND CONTINUED TO DESTINATION. DURING DESCENT, AT 12K FT, THE LIGHT WENT OUT. ACFT LANDED UNEVENTFULLY AND UPON ARRIVAL MX FOUND THE RT MLG DOOR OPEN, SENSOR D1-29 INTERNALLY SHORTED TO GROUND, AND THE DOOR TARGET BRACKET CRACKED. MX REPLACED D1-29 AND TARGET BRACKET IAW AMM. PSEU TESTS ARE SATISFACTORY AND THE ACFT HAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (BS 370-408 L28R) · airframe 48,245 hrs · 36,203 cycles

DURING HMV CORROSION WAS FOUND ON LWR BEAM AFT FWD CARGO COMPARTMENT BTW STA Y=370 TO 408 AND LONGERON 28 RT. AREA WAS REPAIRED IAW RM 53-05D FIG 804.

Part: BEAM — CORRODED (BS 636-693 L28R) · airframe 48,245 hrs · 36,203 cycles

DURING HMV CORROSION WAS FOUND ON LWR BEAM AFT MID CARGO COMPARTMENT BTW STA Y=636 TO 693 AND LONGERON 28 RT. AREA WAS REPAIRED IAW SRM 53-05 FIG 123.

Part: BEAM — CORRODED (BS 1155-1212) · airframe 48,245 hrs · 36,203 cycles

DURING HMV3 CORROSION WAS FOUND ON LWR BEAM AT AFT CARGO COMPARTMENT BTW STA Y=1155 TO1212 AND LONGERON 28 RT. AREA WAS REPAIRED IAW SRM 53-05 FIG 123.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,245 hrs · 36,203 cycles

DURING HMV A MISSING ID TAG WAS FOUND ON FUSELAGE REPAIR AT STA Y=113 LONGERON 23 LT. SKIN WAS REPAIRED IAW SRM 53-04 FIG 12C.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 48,245 hrs · 36,203 cycles

DURING HMV A CRACK WAS FOUND ON AFT OTBD FRAME BTW BEAMS 3 TO 4 AT FWD CARGO DOOR C1. FRAME WAS REPAIRED IAW SRM 52-05D FIG 50.

Part: SKIN — CRACKED (BS 332-351) · airframe 48,245 hrs · 36,203 cycles

DURING HMW LIGHTNING STRIKE WAS FOUND ON FUSELAGE SKIN BTW LONGERON 26-27 RT AND STA Y=332-351. AREA WAS REPAIRED IAW SRM 53-04D FIG 12C.

Part: LIGHT — DAMAGED (CABIN) · airframe 38,350 hrs · 29,508 cycles

AS PAX DEPLANED AN ELECTRICAL ODOR WAS NOTICED IN CABIN. FOUND BURNED FLUORESCENT TUBE HOLDER AT 11DE. REPLACED SAME.

Part: RELAY — FAILED (APU STARTER) · airframe 35,487 hrs · 27,537 cycles

JUST PRIOR TO DEPARTURE, SMOKE COMING FROM APU COMPARTMENT. FOUND APU STARTER ON FIRE. DISCHARGED BOTH ENG/APU FIRE BOTTLES. REPLACED APU.

Part: CONTROL CABLE — RESTRICTED (NR 1 ENGINE) · airframe 34,248 hrs · 26,690 cycles

DURING TAXI, RT ENGINE THROTTLE WOULD INITIALLY NOT GO PAST APPROX 1-2 INCHES OF TRAVEL. FOUND INSULATION WRAPPED AROUND RT ENGINE THRUST REVERSER CONTROL CABLE PULLEY. REF FOR PULLEY 78-30-00-1B SHEET 1 ITEM 185. AFTER REMOVAL OF INSULATION THROTTLE MOVEMENT NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,114 hrs · 26,605 cycles

SEAT 22ED EMERGENCY LIGHT INOP. REPLACED BATTERY PACK ASSY.

Part: BEAM — CORRODED (PAX DOORWAY) · airframe 32,891 hrs · 25,734 cycles

DURING HMV-2, CORROSION DAMAGE WAS FOUND ON THE C2 & C3 JAMB BEAMS. THE JAMB BEAM DOOR STOP HOLES WERE OUT OF TOLERANCE AFTER CLEAN UP. CORROSION WAS REPAIRED PER MD80 SRM 53-05 FIGURE 63 BY BLENDING AND USE OF A REPAIR DOUBLER.

Part: GCU — FAILED (NR 1 ENGINE) · airframe 32,431 hrs · 25,435 cycles

LEFT GENERATOR OFF MESSAGE ILLUMINATED AT 7000 FT ON CLIMBOUT NO VOLTS OR FREQS. FOUND NR 1 GCU FAULT LIGHT ILLUMINATED. REPLACED NR 1 GCU. REPLACED NR 1 CSD AND GEN PER AMM. NR 1 GEN, OPS CHECK GOOD.

Part: HYDRAULIC LINE — CHAFED (HYD SYSTEM) · airframe 31,962 hrs · 25,084 cycles

DURING DESCENT THROUGH 15,000 FT RECEIVED LOW RT HYD PRESS AND QUANTITY MESSAGES, HAD NOT USED FLAPS OR SPOILERS AT THAT POINT. HYD PRESSURE WAS ALREADY 0 AND HYD QTY WAS 1 QUART. RT PUMP WAS UNFEATHERED FOR 2 MINUTES BEFORE COMING TO THAT POINT IN CKLIST. FOUND BRAIDED PRESSURE LINE AT 2 ENG EDP PRESS FILTER MODULE CHAFED. REMOVED LINE. REPLACED LINE. LEAK CHECK OK. REPLACED RT ENG EDP RT EDP PRESS FILTER AND CASE DRAIN FILTER PER AMM. OPS AND LEAK CHECK OK.

Part: ACM — FAILED (A/C BAY) · airframe 31,611 hrs · 24,805 cycles

RUBBER SMELL REPORTED BY PAX AND FLT ATTENDANTS SHORTLY AFTER T/O. CLEARED QUICKLY, TOWER REPORTED NO RUBBER ON RUNWAY. REMOVED AND REPLACED LEFT ACM PER MM, LEAK AND OPS CHECKS GOOD.

Part: ENGINE — ERRATIC (#2 ENGINE) · airframe 30,480 hrs · 23,958 cycles

SIGNIFIGANT THROTTLE REDUCTION AFTER T/O LT ENG EPR READ 2.08. RT ENG READ 1.54 ALL OTHER INDICATIONS NORMAL. REPLACED NBR 2 ENG. EPR TRANSMITTER.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 30,223 hrs · 23,766 cycles

ON APPROACH INTO BDL RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER LOWERING GEAR. PERFORMED PUSH-TO-TEST LIGHT DID NOT ILLUMINATE. PERFORMED FLY-BY OF TOWER TO VERIFY GEAR DOWN AND VISUALLY CONFIRMED GEAR WAS DOWN. CONFIRMED BULBS WERE BURNT OUT ON RIGHT GEAR LIGHT ASSY. RELAMPED SAME.

Part: POWER SUPPLY — UNSERVICEABLE (B5-211) · airframe 30,098 hrs · 23,683 cycles

ALL INTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK FOR OUTPUT LOGIC BEING INCORRECT. ALL OPS NOW NORMAL

Part: ENGINE — FAILED (NR 1) · airframe 29,381 hrs · 23,150 cycles

NR 1 ENG FAILED ON LANDING. SPEED WAS 135 KIAS THROTTLES WERE AT REV IDLE. NO OVERTEMP NOTED. REMOVED AND REPLACED NR 1 ENG.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 29,181 hrs · 23,009 cycles

LOSS OF HYD FLUID ON RT SIDE. STOPPED AT 1 QT. MTC FOUND LINE TO RT HYD FILTER MODULE LEAKING. LINE WAS REPLACED.

Part: CHARGER — OVERHEATED (FWD E/E BAY) · airframe 28,778 hrs · 22,720 cycles

PRIOR TO DEPARTURE RAMP REPORTED SMOKE COMING FROM FUSELAGE AFT OF NOSE GEAR. FOUND BATTERIES OVERHEATED AND VERY HOT. A/C HAD A SUNDSTRAND CHARGER INSTALLED (P/N 249001276) (S/N 5030008). REPLACED BATTERIES AND CHARGER.

Part: SHUTOFF VALVE — STUCK (OXYGEN MASK) · airframe 27,854 hrs · 22,069 cycles

CAPTS O2 MASK SHUTOFF VALVE KNOB STUCK OPEN. REPLACED CAPTS O2 MASK. OPS CHECK NORMAL.

Part: REGULATOR — FAILED (CABIN PRESSURE) · airframe 27,623 hrs · 21,910 cycles

FUMES IN THE AFT CABIN. SMOKE DETECTOR 2L ALARMED. REPLACED RT PACK PRESSURE REGULATOR AND A/C PILOT PRESSURE REGULATOR, CHECKS GOOD.

Part: DUCT — BLOWN (NR 2 ENGINE) · airframe 26,949 hrs · 21,417 cycles

AT APPROX 2500 FT AFTER T/O, MASTER CAUTION WITH ASSOCIATED NR 2 ENG B LOOP LIGHT ILLUM. SHORTLY THERE AFTER NR 2 ENG FIRE HANDLE ILLUM WITH ASSOCIATED FIRE LIGHTS. PULLED THROTTLE BACK AND LIGHTS WENT OUT. RAN POM PROCEDURES AND LANDED. TWO PAX REPORTED A BURNING MECHANICAL SMELL AND A POP AFTER TAKEOFF. FOUND NR 1 ENG ANTI-ICE VALVE DUCT BLOWN. REPLACED SAME.

Part: OVEN — DIRTY (GALLEY)

IN FLIGHT FWD AND AFT OVENS GENERATED SMOKE WHEN USED. REMOVED FOOD CARRIER FROM FWD OVEN WITH INTRACOMPANY SHIPPING ORDER NR N 132323 TAPED TO SIDE OF CARRIER AND CLEANED FOOD DEBRIS FROM AFT OVEN. SHIPPING TICKET SHOWED EVIDENCE OF BURNING.

Part: GENERATOR — FAILED (NR 2 ENGINE)

IN CRUISE FL330, RIGHT GEN TRIPPED OFF AND AC X-TIE LOCKOUT MSG ON EOAP. TRIED ONE RESET NO HELP. DIVERTED TO JFK. REPLACED GCU.

Part: COALESCER — CONTAMINATED (CABIN)

IMMEDIATELY AFTER TAKEOFF, F/A NOTICED STRONG ODOR IN AFT CABIN, DESCRIBES AS BURNING RUBBER. PERFORMED DUCT BURN OUT. REPLACED COALESCER BAGS.

Part: HYD PUMP — INOPERATIVE (NR 1 ENGINE)

AFTER TAKEOFF, RT HYD PRESS WENT TO ZERO WITH - RIGHT HYD LOW, MSG ON OAP. FOLLOWED POM PROCEDURES AUX/TRANS PUMPS TURNED ON. PRESS RETURNED TO NORMAL DECLARED EMERGENCY. REPLACED RT ENG HYD PUMP AND FILTERS.

Part: HYD LINE — CHAFED (RT HYD SYST)

LOST RT HYS SYSTEM IN FLT. FOUND PRESSURE FLEX LINE CHAFED THRU GOING TO HYD PRESSURE FILTER MODULE. REPLACED LINE, LEAK CHECK GOOD.

Part: BOLT — BROKEN (LT MLG)

ON WALKAROUND, FOUND LT MLG ACTUATOR ROD END ATTACH BOLT BROKEN. REPLACED BOLT.

Part: COALESCER BAG — DIRTY (CABIN)

SLIGHT SMOKE IN CABIN AFTER T/O, SET OFF BOTH SMOKE ALARMS. SMOKE CLEARED AFTER A FEW MIN. PERFORMED DUCT BURNOUT PER M/M, RAN PACKS WITH ENGS TO T/O PWR. REPLACED WATER SEPARATOR BAGS, ALL CK OK.

Part: DFGS SWITCH — FAILED (FTL DECK)

DURING CRUISE AT FL 330, AIRCRAFT ROLLED HARD TO THE RIGHT, YAW DAMP AND MACH TRIM AUTOMATICALLY DISCONNECTED AND THE DFGS SWITCH C/B POPPED. A/C RETURNED TO ATL. REPLACED DFGS SWITCH A C/B RTS ON BOTH DFGS, CHECKS OK.

Part: HYD LINE — FAILED (TAIL COMP)

DURING CRUISE, LOST ALL RIGHT HYDRAULIC QTY AND PRESSURE, LANDED ATL. REPLACED HYD LINE ON PRESSURE SIDE OF ENGINE FILTER MODULE.