N915DL

Part: SCHRADER VALVE — FAILED (NLG STRUT) · airframe 79,752 hrs · 61,320 cycles

SHIP 0915 - ATB, GEAR - AFTER TAKEOFF THE NOSE GEAR INDICATED RED AND WITH THE ASSOCIATED AIR NOISE. CREW SUSPECTED NOSE GEAR WAS STILL DOWN. CORRECTIVE ACTION: MAINTENANCE FOUND NOSE LANDING GEAR STRUT FLAT. THE UPPER SCHRADER VALVE REPLACED. THE NOSE GEAR WAS SERVICED AND A GEAR SWING WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. SDR REPORTED DUE TO EMERGENCY BEING DECLARED.( (LP5089532)

Part: BATTERY — DISCHARGED (CABIN) · airframe 79,385 hrs · 61,012 cycles

ROW 10-15 OVERHEAD EMER LIGHT OUT. R&R ROW 10-15 EMER LIGHT BATTERIES PER AMM 33-53. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 79,385 hrs · 61,012 cycles

AFT WINDOW EXIT SIGN LIGHT INOP BOTH SIDES. R&R AFT WINDOW EXIT SIGN BATTERY PER AMM 33-53. OPS CHECK GOOD.

Part: WIRE HARNESS — BURNED · airframe 79,244 hrs · 60,895 cycles

ON ROLLOUT MULTIPLE OAP LT ON, MULTIPLE CB'S POPPED, ON TAXI IN LT GEN WOULD NOT PICK UP RT BUS, AT GATE APU WOULD NOT PICK UP RT BUS UNTIL RT ENGINE SHUT DOWN. FOUND F1-7 FUSE BURNED ON R2-45 CROSS TIE RELAY. R/R FUSE AND R2-45. INSPECTED T3 FEEDER ON ALL PWR RELAYS. NTF. R/R AC BUS CTL PANEL. RAN ENGINES AND APU AND EXT PWR. ALL CROSSTIE FUNCTIONS NML. WHEN PACK FANS SWITCHED ON FOUND PROBLEMS. FOUND SEVERAL WIRE BUNDLES BURNED IN TAIL CEILING AREA. MD88 AMM 2420. WIRES REPAIRED ON N/R'S 1-19. (LP4699160)

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 79,244 hrs · 60,895 cycles

REPAIR STRINGER S2777922-5 4RT BETWEEN STATIONS 1380 AND 1418 PER SRM 53-02 PARA 12 FIG 18. REMOVED DAMAGED STRINGER, FABRICATED REPAIR PARTS PER SRM 53-02 PARA 12 FIG 18, TREATED, AND PAINTED REPAIR PARTS INSTALLED REPAIR PARTS COMPLIED WITH SRM 53-02 PARA 12 FIG 18 STRINGER REPAIR. INSPECTED STRINGER REPAIR PER SRM 53-02. WIRE SUPPORT INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,244 hrs · 60,895 cycles

REPAIR DAMAGED SKIN FOUND ON AFT FUSELAGE UPPER BETWEEN STATIONS 1380 AND 1401, STRINGER 3R TO 5R PER SRM 53-04-03 PG 40 VIEW C. REMOVED DAMAGE SKIN FABRICATED REPAIR PER MD-88 SRM 53-04-03 FIG 5. INSTALLED REPAIR PARTS AND COMPLIED WITH MD-88 SRM 53-04-3 FIG 5 SHEET 3 CLASS 2 REPAIR. (LP #0752975)

Part: BEARING — WORN (TAILCONE) · airframe 79,211 hrs · 60,866 cycles

TAILCONE RELEASE MECHANISM CAM BEARING WORN. REMOVED AND REPLACED SPACER BEARING ON TAILCONE RELEASE MECHANISM PER AMM 53-50.

Part: SWITCH — DAMAGED (TAILCONE) · airframe 79,211 hrs · 60,866 cycles

TAILCONE UNSAFE MSG FAILED TO ILLUMINATE WITH EXT HANDLE REF CARD 5350-01077-0101. FOUND C/P P1-779 CORRODED AND SW S1-537 DAMAGED - RPLD P1-779 AND S1-537 PER WSPM CHAP 20.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 79,046 hrs · 60,719 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 3CD. FOUND THE CONNECTOR WAS PARTIALLY LOOSE, CONNECTED , AND OPS CHECKED GOOD IAW AMM 33-53-01.

Part: COWLING — DELAMINATED (NR 1 ENGINE) · airframe 79,005 hrs · 60,685 cycles

NOSE COWL FOR NR 1 ENG DELAM AT 12:00 POSITION-OPENING FOR T&I DUCT ACCESS. REPLACED NR 1 ENGINE NOSE COWL P/N 5930645-509, S/N 2480001.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,002 hrs · 59,830 cycles

WALK AROUND FOUND CORROSION ON BELLY SKIN APPROX 7 FT AFT OF C2 CARGO DOOR RT OF CNT LINE AT SKIN SPLICE. VERIFIED CORROSION AT FS 758 BETWEEN LONGERONS 29R AND 28R. REMOVED FASTENERS COMMON TO BUTT SPLICE FOR VERIFICATION. REMOVED FASTENERS COMMON TO INTERNAL SPLICE OF EXISTING REPAIR & LONGERONS 29R AND 28R TRANSFERRED TO NR 1. REPAIR COMPLETED IAW ERA 467521-14 REV C.

Part: BATTERY — FAILED (SMOKE DETECTOR) · airframe 77,550 hrs · 59,509 cycles

F/C LAVATORY SMOKE DETECTOR SOUNDING, BATTERY REMOVED. NO SMOKE OR ODORS PRESENT. REPLACED THE SMOKE DETECTOR BATTERY.

Part: INDICATOR — MALFUNCTIONED (FUEL PANEL) · airframe 76,509 hrs · 58,646 cycles

FUELING PANEL QTY INDICATION INOPERATIVE. THE FUEL SPILL WAS DETERMINED TO BE A PROCEDURAL ERROR. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE COCKPIT DISPLAY UNIT AND IT MATCHED THE LSDU, TESTED OK IAW AMM 28-40.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED PREVIOUS REPAIR ON FRAME STA Y=1485 CANT NEAR TO ACTUATOR. DOUBLER WAS FABRICATED AND REPLACED PER SRM 53-03 PAR 38 FIG 43 SHEET 3.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED LOWER DOOR JAMB WEB STA Y=370 PROJECTION LONG 27R AT FWD CARGO COMPARTMENT. LOWER DOOR JAMB WEB STA Y=370 PROJECTION LONG 27R AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 558172-14AD REV ORIGINAL, SECTION I AND ETI-88-17-191 REV 3.

Part: DOUBLER — CRACKED (BS 198) · airframe 76,411 hrs · 58,575 cycles

A CRACK WAS FOUND ON INTERNAL DOUBLER BS 198 BETWEEN LONGERONS 17R TO 18R AT LOWER AFTER DOOR FRAME CORNER OF FWD SERVICE DOOR. REPAIRED IAW AMM 53-05, PAR 168, FIG, 178.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED REPAIR DOUBLER ON FWD ACCESSORY COMPARTMENT DOOR JAMB. AREA WAS REPAIRED PER ETI-88-17-194 REV 5 AND ER/A 559494-14 REV ORIGINAL.

Part: DOUBLER — CRACKED (SERVICE DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACK WAS FOUND ON INTERNAL DOUBLER STA Y=198 BTW LONGS 17R TO 18R AT LOWER AFTER DOOR JAMB CORNER OF FWD SERVICE DOOR (R1). DOUBLER AND TRIPLER WERE FABRICATED PER SRM 53-05 PAR 168 FIG 178.

Part: CAP — CRACKED (BS 1437) · airframe 76,411 hrs · 58,575 cycles

CRACK ON OUTER CAP BS 1437, LONGERON 2R. THE CAP WAS REPAIRED IAW ER/A 558132-14, REV ORIG, AND ETI-88-17-170, REV 3.

Part: CAP — CRACKED (BS 1437) · airframe 76,411 hrs · 58,575 cycles

CRACKED INNER CAP BS 1437 LONGERON 2L AND 2R. THE INNER CAP WAS REPAIRED IAW ER/A 558132-14, REV.

Part: FRAME — CRACKED (BS 1485) · airframe 76,411 hrs · 58,575 cycles

CRACKED FRAME BS 1485. THE FRAME WAS REPAIRED IAW ER/A 558162-14, REV ORIG. AND ETI-88-17-188, REV 2.

Part: FRAME — CRACKED (BS 1485) · airframe 76,411 hrs · 58,575 cycles

CRACKED FRAME BS 1485. THE FRAME WAS REPAIRED IAW ER/A 558162-14, REV ORIG, AND ETI-88-17-188, REV 2.

Part: FRAME — CRACKED (BS 1437) · airframe 76,453 hrs · 58,604 cycles

FRAME BS 1437 AT THE BULKHEAD UPPER & LOWER CAPS FOUND CRACKED. REPAIRED IAW ER/A 88-558132-14, SECTION II.

Part: DOUBLER — CRACKED (BS 1463 SKIN) · airframe 76,411 hrs · 58,575 cycles

CRACKED FUSELAGE INTERNAL DOUBLER BS 1463. REPAIRED THE DOUBLER IAW ER/A 558149-14.

Part: FRAME — CRACKED (BS 1463) · airframe 76,411 hrs · 58,575 cycles

CRACKED FRAME BS 1463. REPAIRED IAW SRM 53-03D, FIG 38A, 51-30-5, AND 51-30-2.

Part: STEP — CORRODED (VENTRAL STAIRS) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON WEB OF STEP 5 AT VENTRAL STAIRWAY. WEB WAS FABRICATED AND REPLACED PER DWG 9915570 REV BW & SRM 51-30-5 & 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CORROSION ON FUSELAGE SKIN INNER PRODUCTION DOUBLER OUTBD OF LONG 26L BTW STA Y=589-598 AT MID CARGO. DOUBLER WAS REPLACED PER SRM 53-34-0 FIG 2, 51-10-1 FIG 36 SHEET 6, 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED INTERCOSTAL BTW FLOORBEAMS STA Y 1287 AND Y 1307, X 0 AT PAX CABIN.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON LT WING ACCESS PANEL 1307C. FUEL ACCESS PLATE WAS REPLACED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON TEE BTW STA Y=1401 TO Y=1425 AT LONG 25L. REPAIRED PER ETI-88-17-183 REV 1 AND ER/A 558154-14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON ACCESS AT PLATE NR 1307C. REPLACED PANEL.

Part: SKIN — NOT REPORTED (RT WING) · airframe 76,411 hrs · 58,575 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE ) ON LOWER SKIN AT XRS =163 TO 168 REAR SPAR AT RT WING. INSPECTED PER ERA 558123-14AD.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON AREA COUNTERSINK ON FUEL TANKS ACCESS PLATES NR 1303C AND 1311C. FUEL ACCESS PLATES 1303C AND 1311C WERE REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORRODED COUNTERSINK ON ACCESS PANEL 1335C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

DISCREPANT AREA WAS FOUND ON UPPER FWD DOOR FRAME CORNER SKIN WITH DOUBLER AND TRIPLER REPAIRS PRESENT. REPAIRED IAW ER/A 558115-14AD, REV ORIGINAL, AND ETI-88-17-169, REV ORIGINAL.

Part: DOUBLER — CRACKED (BS 427) · airframe 76,411 hrs · 58,575 cycles

CRACK WAS FOUND ON INTERNAL DOUBLER BS 427 BETWEEN LONGERONS 26R TO 27R AT LOWER AFTER DOOR FRAME OF THE FWD CARGO DOOR. THE DOUBLES WAS REPAIRED IAW ETI-88-17-173, REV 1, AND ER/A 558125-14AD, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 1414C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON RUB STRIP, UPPER SURFACE LEFT WING ACCESS PANEL. THE RUB STRIP WAS CLEANED IAW PS 900-1-2-1 N 0.01 AND REINSPECTED AND NO DAMAGE WERE FOUND; RUB STRIP ON UPPER SURFACE LEFT WING ACCESS NUMBER 1303C, WERE REPLACED PER DC9/MD80 SRM 51-22-2A.PAR 4. (LP0070378)

Part: SKIN — DAMAGED (RUDDER) · airframe 76,411 hrs · 58,575 cycles

DAMAGE METALIZED SKIN AT LT AND RT SIDE OF RUDDER. METALIZED SKIN WAS REPAIRED IAW ER/A 092613, REV C AND SRM 51-70-1A, PAR 23.

Part: CARGO TRACK — CORRODED (BS 503-522) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON CARGO TRACK BETWEEN BS 503 AND 522 IN THE FWD CARGO BAY. DAMAGE SECTION OF THE CARGO TRACK WAS REPLACED IAW SRM 51-10-1, FIG 26, SHEET 2, SRM 51-10-4, SRM 51-30-2, AND 51-30-1.

Part: RUB STRIP — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON RUB STRIPS UPPER SURFACE RIGHT WING ACCESS PANELS 1409C, 1410C, 1414C. THE RUBSTRIPS WERE REPLACED IAW SRM 51-22-2A, PAR 4.

Part: INTERCOSTAL — CRACKED (BS 937-944) · airframe 76,411 hrs · 58,575 cycles

CRACKED RT INTERCOSTAL BS 937 - 944 INNER KEEL BEAM AREA. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-2, SRM 53-14-3, AND DWG 9936368, REV AW.

Part: FRAME — CRACKED (BS 1463) · airframe 76,411 hrs · 58,575 cycles

CRACKED FRAME WEB BS 1463. THE FRAME WAS FABRICATED AND REPLACED IAW DWG 9953015, REV AH, SRM 51-30-2, AND 51-30-5.

Part: SKIN — CRACKED (RT WING) · airframe 76,411 hrs · 58,575 cycles

CRACK INDICATIONS WERE FOUND ON THE LOWER ACCESS DOOR CUTOUT BETWEEN XRS 189 TO 214 ON THE RT WING. REPAIRED IAW ETI-88-17-168, REV 1, AND ER/A 558107-14AD, REV ORIG.

Part: CARGO TRACK — CORRODED (BS 236) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON THE CARGO TRACK, RT BS 236 FWD CARGO BAY. THE DAMAGE SECTION OF THE CARGO TRACK WAS REPLACED IAW SRM 51-10-1, FIG 26, SHEET 2, SRM 51-10-4, SRM 51-30-2, AND 51-30-1.

Part: SKIN — CRACKED (LT WING) · airframe 76,411 hrs · 58,575 cycles

CRACK ON THE LT WING ON LOWER ACCESS CUTOUT BETWEEN XRS 189 TO 214. REPAIRED IAW ETI-88-17-168, REV 1, AND ER/A 558107-14AD, REV ORIG.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 3R, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-01, 51-30-5, 51-30-2, AND 51-10-3, PAR 14, 21.

Part: SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION IN A SLIDE LATCH SUPPORT BETWEEN BS 160 TO 200, RBL 54 TO 60. THE LATCH SUPPORTS WERE REPLACED IAW DWG 9936534, REV BW, AND SRM 51-10-4.

Part: ANGLE — CORRODED (BS 160-200) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON ANGLE BETWEEN BS 160 TO 200, RBL 54 TO 60. THE ANGLE WAS REPLACED IAW DWG 9957828-19, REV AB AND SRM 51-10-2.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 4L, BS 1437. THE LONGERON WAS REPAIRED IAW 53-02, FIG 18, 51-30-5, 51-30-2, 51-10-3 PAR 14 & 21, AND 51-30-1.

Part: CARGO TRACK — CORRODED (BS 427-446) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON THE CARGO TRACK BETWEEN BS 427 AND 446 IN THE FWD CARGO BAY. THE DAMAGE SECTION OF THE CARGO TRACK WAS REPLACED IAW SRM 51-10-1, FIG 26, SHEET 2.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACKED INNER PAN ON FWD EDGE OF BEAM NR 5 AT AFT CARGO DOOR. CRACKED INNER PAN ON FWD EDGE OF BEAM NR 5 AT AFT CARGO DOOR WAS REPAIRED PER SRM 52-05 FIG 50.

Part: CRANK ASSY — CORRODED (BS 1485) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSIN ON RUDDER THROUGH LIMITER CRANK BS 1485 11 HRS POSITION IN THE AFT ACCESSORY COMPARTMENT. RUDDER THROUGH LIMITER CRANK WAS REPLACED.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

WORN EXTERNAL LOWER REPAIR DOUBLERS AT AFT CARGO DOOR. DOUBLERS WERE REPLACE PER DWG NR 5910141 REV FE, DPS 4.710-3 AND SRM 51-30-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

GOUGE ON FUSELAGE SKIN STA 987 AND LONGERON 2L. GOUGE ON FUSELAGE SKIN WAS REPAIRED PER ETI-88-17-171 REV ORIGINAL AND ER/A 558135-14 REV ORIGINAL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACKED OUTER PAN ON LOWER EDGE BTW STA Y=653 AND Y=677 IN MID CARGO COMPARTMENT DOOR. CRACKED OUTER PAN WAS REPAIRED PER SRM 52-03D FIG 8.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

WORN EXTERNAL LOWER REPAIR DOUBLERS AT FWD CARGO DOOR. EXTERNAL LOWER REPAIR DOUBLERS AT FWD CARGO DOOR WERE REPLACED PER ER/A 486624-14MA REV ORIGINAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION IN LT CUSP WEB BTW STA Y= 1079 TO Y= 1098. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131A-7, 51-30-02, 51-30-05, 51-30-01 AND 51-10-3 PAR 14, 21, 38.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACKED FITTING AND T ANGLE AT STA Y=674 BTW BEAM 1 AND LOWER EDGE IN MID CARGO COMPARTMENT DOOR. CRACKED FITTING AND T ANGLE WERE REPLACED PER SRM 51-30-2 AND 51-30-5 & DWG 9957664 REV N.

Part: DOUBLER — CORRODED (B 1060-1079) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON RT PREVIOUS REPAIR DOUBLER BETWEEN BS 1060 - 1079. THE DOUBLER ON CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-7, AND 51-30-5.

Part: TAB — DENTED (RT ELEVATOR) · airframe 76,411 hrs · 58,575 cycles

DENT ON GEARED TAB UPPER SURFACE AT RT ELEVATOR. THE TAB WAS REPAIRED IAW SRM 55-04 P 2.

Part: SKIN — CRACKED (BS 161-162) · airframe 76,411 hrs · 58,575 cycles

TWO CRACKS WERE FOUND ON FUSELAGE SKIN AND INTERNAL DOUBLER, BS 161 AND 162, LONGERONS 11R TO 12R AT UPPER FORWARD DOOR FRAME OF FWD SERVICE DOOR. SKIN WAS REPAIRED IAW SRM 53-05, FIG 176.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACK AT ANGLE BETWEEN BEAM NR 6 AND BS 171 L1 DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-2, AND DWG 9955750, REV U.

Part: TAB — DENTED (RT ELEVATOR) · airframe 76,411 hrs · 58,575 cycles

DENTS ON ANTI-FLOAT TAB UPPER SURFACE ON THE RT ELEVATOR. ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-04, P3.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 76,411 hrs · 58,575 cycles

PUNCTURES AND DAMAGE FERRULES ON FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01-201

Part: BEAM — CORRODED (CAROG DOOR FRAME) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON THE AFT CARGO DOOR FRAME LOWER BEAM, LONG 28R. CORROSION WAS REMOVED, REWORKED AREAS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 26, 14, 21, & 38.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

WEAR ON PRODUCTION DOUBLER AT LOWER AFT CORNER OF MID CARGO COMPARTMENT DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CRACKED (BS 769-788) · airframe 76,411 hrs · 58,575 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 769 & 788 , BL 0. THE FLOOR SUPPORT WAS REPAIR IAW SRM 51-70-5 FIG 1.

Part: FLOOR PANEL — CRACKED · airframe 76,411 hrs · 58,575 cycles

CRACK ON FLOOR PANEL. THE FLOOR PANEL WAS REPARED IAW SRM 51-10-2, 51-30-2, AND 53-05, FIG 131B.

Part: CUSP WEB — CORRODED (BS 1244) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON LEFT CUSP WEB BS 1244 BETWEEN LBL 54 TO 60. REPAIR FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A-13, AND SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 434-451) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON RT CUSP WEB, BS 434 - 451, RBL 54 - 60. DAMAGE AREA WAS REPAIRED IAW SRM 53-05 FIG 131A-10. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER DAMAGE REMOVED IAW NDT SPM 06-10-01.001.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACKED CARGO DOOR TEE ANGLE BETWEEN BEAMS 5 AND BS 427. REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1401) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 2L, BS 1401. REPAIRED THE LONGERON IAW SRM 53-02, PAR 12, FIG 18, 51-30-2, 51-30-5, AND 51-10-3, PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 918) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON RIGHT CUSP WEB BS 918, RBL 54 - 60. THE CUSP WEB WEB REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: SKIN — CRACKED (BS 161-162) · airframe 76,411 hrs · 58,575 cycles

TWO CRACKS WERE FOUND ON FUSELAGE SKIN AND INTERNAL DOUBLER BS 161 AND 162 BETWEEN LONGERONS 11R TO 12R AT UPPER FORWARD DOOR FRAME OF FWD SERVICE DOOR. THE SKIN WAS REPAIRED IAW SRM 53-05, FIG 176.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,411 hrs · 58,575 cycles

CRACK ON INNER PAN AT OUTBD EDGE, BS 693 BETWEEN BEAMS 1 AND 2 IN MID CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, FIG 26A.

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON THE LT CUSP WEB BETWEEN BS 1060 - 1079. CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-14 AND 51-30-2.

Part: FLOOR PANEL — DELAMINATED · airframe 76,411 hrs · 58,575 cycles

DELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1401) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 2L, BS 1401. REPAIRED THE LONGERON IAW SRM 53-20, PAR 12, FIG 18, 51-30-2, 51-30-5, AND 51-10-3, PAR 14, 21.

Part: FRAME — WORN (BS 1344) · airframe 76,411 hrs · 58,575 cycles

WORN TITANIUM FRAME ON BS BS 1344, BTW LBL 20 TO RBL 20. THE FRAME WAS REPAIRED IAW ER/A 094719-14MA REV A.

Part: CUSP WEB — CRACKED (BS 351-370) · airframe 76,411 hrs · 58,575 cycles

CRACKED RT CUSP WEB BETWEEN BS 351 TO 370, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A, 51-30-5, AND 51-30-2.

Part: CUSP WEB — CRACKED (BS 845) · airframe 76,411 hrs · 58,575 cycles

CRACKED RT CUSP WEB BS 845, RBL 58. THE CUSP WEB WAS REPAIR IAW SRM 53-05, FIG 131 A-2, SHEET 1.

Part: CHANNEL — CRACKED (CABIN) · airframe 76,411 hrs · 58,575 cycles

CRACKS ON CHANNEL OF FLOOR PANEL 1174F. THE CHANNEL WAS REPAIR IAW SRM 53-05, FIG 131B.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION IN LT CUSP WEB AT STA Y=1009 AND X=54 TO X= 60. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131A-13.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORRODED PREVIOUS REPAIR DOUBLER ON RT CUSP WEB STA Y 716 AND X- 57 AT PAX CABIN. DOUBLER AND RING DOUBLER ON RT CUSP WEB STA Y=716 AND X- 57, WAS REPLACE PER SRM 51-30-2; 51-30-5; 53-05 FIG 131A-14; AND 51-10-3 PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON AREA COUNTERSINK ON FUEL TANKS ACCESS PLATES NR 1409C AND 1464C. PANELS WERE REPLACED.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACK ON CHANNEL AT FLOOR PANELS NR 389G AND 465A. FLOOR PANEL 389G AND 465A WAS STOP DRILLED THE END OF CRACK WITH 0.250" PER SRM 53-05 FIG 131B. DOUBLER (2) WAS FABRICATED AND INSTALLED PER SRM 51-10-2 AND 53-05 FIG 131B AND 51-30-2.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON DIAPHRAGM BTW STA Y=200-210 BTW X=-44 TO X=-54. AT PAX CABIN FLOOR STRUCTURE. CORROSION REMOVED AND DOUBLER REPAIR WAS FABRICATED PER SRM 53-05 FIG 131A-1 AND WAS INSTALLED PER SRM 51-30-8.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON LT WING ACCESS PANEL 1307C. REPLACED PANEL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 3L AT STA 160. REPAIRED PER SRM 53-02 FIG 18.

Part: WINDOW — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED LOWER/AFT CORNER ON RT WINDOW PAN STA Y= 905. REPAIRED PER SRM 53-05 FIG 122 AND ER/A 493648-14MA.

Part: PAN — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED UPPER/FWD CORNER ON RT WINDOW PAN STA Y= 886. REPAIRED PER SRM 53-05 FIG 122 AND ERA 493648-14MA.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 2R, ON STA Y=1418. SECTION REPLACED PER SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION ON ANGLE OF FLOOR SUPPORT STA Y=160 BTW X=12 TO X=54. ANGLE OF FLOOR SUPPORT STA Y=160 BTW X=12 TO X=54 WAS REPLACED PER DWG 9955780 REV LA, AND WAS INSTALLED PER SRM 51-30-1 AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION FLOOR SUPPORTS ON STA Y=1155 BTW LT SEAT TRACKS X 22 AND X 44 AT PAX CABIN. FLOOR SUPPORT ON STA Y 1155 WAS REPLACED PER PER SRM 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED WEB Y=148 ABOVE LONGERON 27L AT E&E COMPARTMENT. REPAIRED PER SRM 53-01 FIG 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION AND ELONGATED HOLE ON FLOOR SUPPORT STA Y= 180, Y=197, Y=200 BTW X=-22 TO X=-54. REPAIRED PER SRM 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CORROSION ON FLOOR SUPPORTS STA X=-44 AND X=54 FROM STA Y=160 TO Y=200 AT PAX CABIN. REPAIRED PER SRM 51-30-2 & 51-30-5.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 76,411 hrs · 58,575 cycles

CRACKED UPPER AFT CLIP OF RT FWD EMERGENCY EXIT. CLIP WAS REPLACED PER SRM 51-30-1, 51-30-5 AND DWG 9957735 REV G.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 4L AT STA 160. CRACKED LONGERON 4L AT STA 160 WAS REPAIRED PER SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (BS 160) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 2L AT BS 160. THE LONGERON WAS REPAIRED IAW SRM. 53-02, FIG 18.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,411 hrs · 58,575 cycles

CORROSION IN L1 SCUFF PLATE SUPPORT BTW STA Y=195 TO Y=200 AND X=56. REPAIRED PER 51-30-2 & 51-30-8.

Part: STOP FITTING — CRACKED (EMERGENCY EXIT) · airframe 76,411 hrs · 58,575 cycles

CRACKED UPPER FWD STOP OF RT FWD EMERGENCY OVERWING EXIT DOOR. UPPER FWD SECTION PAN WAS REPAIRED PER SRM 52-05 PAR 53 FIG 51.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 76,411 hrs · 58,575 cycles

CRACK IN LT CUSP WEB STA 812. LT CUSP WEB STA 812 WAS REPAIRED PER SRM 53-05 FIG 131A.

Part: LONGERON — CRACKED (BS 427) · airframe 76,411 hrs · 58,575 cycles

CRACKED LONGERON 10R, BS 427. THE LONGERON WAS REPAIRED IAW SRM 53-02, PAR 12, FIG 18.

Part: CUSP WEB — CRACKED (BS 810) · airframe 76,411 hrs · 58,575 cycles

CRACKED RT CUSP WEB BS 810, RBL 58, THE CRACK WAS 1.125 INCHES LONG. REPAIRED IAW SRM 53-05, PAR 144, FIG 131A-14, AND SRM 51-30-05.

Part: HOOK AND LOOP — MISSING (TAILCONE SLIDE) · airframe 76,411 hrs · 58,575 cycles

MISSING AND DISBONDED HOOK AND LOOP ON TAILCONE EVACUATION SLIDE HOUSING. THE HOOK AND LOOP WAS REPLACED IAW AMM 25-61-02-020-801.

Part: SLEEVE — TORN (CONNECTOR) · airframe 76,411 hrs · 58,575 cycles

TORN SLEEVE ON CONNECTOR AT RT AUXILIARY HYDRAULIC PUMP. SLEEVE ON CONNECTOR AT RT AUXILIARY HYDRAULIC PUMP WAS REPAIRED IAW SWPM 20-10-01, AND ERA 467688-14M AAD, SHEET 4, STEP 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,406 hrs · 58,572 cycles

LT AND RT EXIT SIGNS AT ABOVE WING, AFT DOORS, ABOVE WINDOWS, LIGHTS INOPERATIVE. REPLACED THE BATTERIES FOR EXIT LIGHTS IAW AMM 33-53. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,246 hrs · 58,453 cycles

OVERHEAD EMERGENCY LIGHTS ROW 11-15 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AT ROW 12 CDE OVERHEAD BIN IAW AMM 33-53. THE EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,269 hrs · 57,746 cycles

ON GEAR EXTENSION RIGHT OUTBOARD ANTISKID LIGHT ILLUMINATED. PERFORMED GO AROUND AND AFTER EXTENSION ON NEXT APPROACH NO LIGHTS ILLUMINATED ALL NORMAL. ACCOMPLISHED ANTISKID SYS TEST IAW AMM 32-43. TEST NORMAL. PER MC REMOVED NR 4 MLG TIRE HUB CAP AND INSP XDCR FOR SECURITY & CONDITION. XDCR IS SECURE, PINS GOOD.

Part: TIRE — FAILED (MLG) · airframe 74,532 hrs · 57,150 cycles

RETURNED TO DEPARTURE DUE TO A SUSPECTED TIRE FAILURE AND MULTIPLE NR 2 ENGINE COMPRESSOR STALLS. ENGINE POWER REDUCED TO IDLE DURING CLIMB OUT AND WAS NOT SHUTDOWN. MAINTENANCE FOUND NUMBER 4 MLG TIRE TREAD DISBONDED AND WAS INGESTED INTO THE NUMBER 2 ENGINE. REPLACED NR 3 AND 4 MLG WHEEL/TIRE ASSEMBLIES. REPLACED NR 2 ENGINE. MADE REPAIRS TO RIGHT INBOARD FLAP.

Part: SKIN — CRACKED (BS 1418) · airframe 73,912 hrs · 56,705 cycles

FUSELAGE EXTERIOR SKIN HAS 1" CRACK FROM FASTENER AT BS 1418 JUST BELOW STR 2 LT. REPAIRED IAW PRI 546964-14AD, REV 0 AND COMPLY WITH ER/A 546964-14AD, REV ORIGINAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 71,859 hrs · 55,193 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 19D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,644 hrs · 55,025 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.

Part: RELEASE CABLE — MISROUTED (TAILCONE) · airframe 70,089 hrs · 54,057 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EXTERIOR RELEASE CABLE WAS MISROUTED. THIS IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE CABLE ROUTING WAS CORRECTED IAW THE MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,492 hrs · 53,595 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 12 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BULB RECEPTACLE, LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: RELEASE CABLE — DAMAGED (TAILCONE) · airframe 68,572 hrs · 52,945 cycles

MAINTENANCE DISCOVERED THAT THE INSULATION ON THE LT RELEASE LATCH CABLE FOR THE TAILCONE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPAIRED IAW ER/A 523964-14 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: FRAME — CORRODED (BS 1250) · corrosion level 2 · airframe 68,573 hrs · 52,946 cycles

AFT CARGO BAY, BS 1250 FRAME HAS CORRODED. CORROSION WAS OUT OF LIMITS IAW SRM 53-01. REPAIRED IAW SRM 53-03.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 68,564 hrs · 52,940 cycles

CRACK ON HORIZONTAL STABILIZER UPPER LT AFT SKIN PANEL. STOPPED DRILLED CRACK IAW DWG SR09550028, REV D, COMPLIED WITH HFEC.

Part: ATTACH ANGLE — CRACKED (L1 DOOR) · airframe 68,564 hrs · 52,940 cycles

TWO CRACKS FOUND ON ATTACH ANGLE INSIDE L1 DOOR AT UPPER FWD CORNER. REMOVED DOUBLER ON ATTACH ANGLE INSIDE L/L DOOR UPPER FWD CORNER IAW SRM 51-30-01, 51-30-05, LOCATED AND DRILLED HOLES NEW DOUBLERS IAW DWG N 9955752, ALODINED AND PRIMED HOLES AND AREA IAW SRM 51-10-3, PARA 21,14. INSTALLED NEW DOUBLER IAW DWG N 9955752.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 68,564 hrs · 52,940 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,564 hrs · 52,940 cycles

FWD CARGO DOOR SKIN HAS KNIFE EDGE ON AFT DOUBLER LOWER SIDE. REMOVED DAMAGED DOUBLER ON C1, FWD CARGO DOOR IAW SRM 51-30-2. LOCATED AND DRILLED NEW DOUBLER, IAW SRM 51-10-3. INSTALLED NEW DOUBLER IAW SRM 52-05. ID-TAGGED REPAIR IAW DPS 900-5-1 NO.04.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 68,564 hrs · 52,940 cycles

CARGO DOOR SKIN HAS KNIFE EDGE ON FWD DOUBLER, LOWER SIDE 75-05. REMOVED DAMAGED DOUBLER AT FWD CARGO DOOR SKIN FWD LOWER SIDE IAW SRM 51-30-02. LOCATED AND DRILLED NEW DOUBLER IAW SRM 52-05, FIG 65. CHAMFERED EDGES OF DOUBLER IAW SRM 52-05, FIR 65. TREATED AND PRIMED HOLES AND BARE METAL ON THE PLANE AND DOUBLER IAW SRM 51-10-03. INSTALLED SPACERS IAW SRM 51-30-011. INSTALLED FASTENERS IAW SRM 52-05, FIG 65.

Part: SPRING — BROKEN (EMERGENCY EXIT) · airframe 67,794 hrs · 52,425 cycles

DURING LINE CHECK, FOUND AFT DOOR EMERGENCY EXIT MECHANISM ARM SPRING BROKEN. REPLACED SPRING IAW MM 53-53.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 67,383 hrs · 52,141 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19D IN THE CABIN WAS INOPERATIVE. MX FOUND A BROKEN WIRE, REPAIRED THE WIRING, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CONDUIT — DAMAGED (TAILCONE) · airframe 64,904 hrs · 50,366 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE SYS LATCH CABLE FORK END WAS BENT OUT OF ALLOWABLE LIMITS AND FOUND THAT THE CABLE CONDUIT WAS WORN AS WELL. THE CONDUIT WAS REPAIRED AND INSTALLED. T

Part: SKIN — CRACKED (BS 1486) · airframe 1 hrs · 1 cycles

AFT FUSELAGE CRACKED BS 1486 , REPAIRED IAW ER/A 507131-14, REV 0 WITH INSTALLATION OF FILLER AND DOUBLER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,337 hrs · 49,973 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FORWARD OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,157 hrs · 49,855 cycles

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

Part: WIRE — DEFECTIVE (CABIN) · airframe 62,701 hrs · 48,891 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE PIGTAIL AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 62,701 hrs · 48,891 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 34D IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,292 hrs · 48,580 cycles

MAIN CABIN LT CUSP WEB STA 1022-1041 COROSION. INSTALLED DOUBLER TRIPLER REPAIR PER SRM 51-30-2 / 51-30-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,284 hrs · 48,574 cycles

SDR. AFT ACCESSORY COMPARTMENT STA 1451 FORMER SHEAR TIE CLIP CRACKED BETWEEN LONGERON 1 AND 3R. FABRICATED SHEAR TIE CLIP IAW DRAWING NR 9911860 ITEM 17. INSTALLED SHEAR TIE CLIP STA 1451 BETWEEN LONGERON 1 AND 3R IAW MD 80 SRM 51-30-5 PG 12. AT SAA/SAT DURING HMV ON N/R 230278 W/O 88404420001.

Part: UNKNOWN — SMOKE (CABIN) · airframe 62,073 hrs · 48,429 cycles

DIVERTED TO JAX DUE TO SMOKE IN THE CABIN, LAVATORY SMOKE DETECTORS DID NOT SOUND, SMOKE DISSIPATED AFTER LANDING. BORESCOPE BOTH ENGINES - NO FAULTS FOUND. RAN ENGINES AT POWER, NO ODORS OR SMOKE. PERFORMED OPN 5089. RAN ENGINES AGAIN - STILL NO ODORS OR SMOKE. WILL POSITION FERRY TO ATL.

Part: ACM — LEAKING (RIGHT) · airframe 62,069 hrs · 48,426 cycles

CREW REPORTED THAT WHEN USING THE RIGHT AIR COND PACK IN THE FULL HOT POSITION THE CABIN HAD A SLIGHT HAZE PRESENT. HAZE DISSIPATED WHEN TEMP SELECTION WAS REDUCED. MAINTENANCE IN DTW PERFORMED FOUND THE RIGHT ACM AND APU BOTH PUTTING OIL INTO THE PNEUMATIC SYSTEM. THE AIRCRAFT WAS REPOSITIONEDTO MSP FOR FURTHER MAINTENANCE.

Part: PNEUMATIC SYSTEM — ODOR (CABIN) · airframe 62,057 hrs · 48,420 cycles

CREW REPORTED FUMES AND HAZE IN THE CABIN WHICH DISSIPATED ONCE THE ANTI-ICE SYSTEM WAS TURNED OFF. MAINTENANCE OPERATED THE ENGINES AT TAKEOFF POWER AND HAD EVIDENCE OF AN OIL SMELL BUT DID NOT FIND ANY EVIDENCE OF OIL IN THE 8TH& 13TH STAGE DUCTS (PER BORESCOPE INSPECTIONS OF DUCTS). MAINTENANCE THEN PERFORMED PNEUMATIC SYSTEM BURNOUT AND CHANGED THE COALESCER BAGS. SECOND FULL-POWER ENGINE OPERATION WITH ANTI-ICE ON, DID NOT PRODUCE ANY SMOKE OR SMELL IN CABIN.

Part: WIRE — PULLED (CABIN) · airframe 61,975 hrs · 48,359 cycles

DURING LINE CHECK MAINTENANCE FOUND RED EMERGENCY PATH LIGHTAT SEAT 24DE INOPERATIVE. MAINTENANCE INSTALLED NEW LIGHT CONNECTOR DUE TO WIRES BEING PULLED OUT. OPERATION OF LIGHTS NOW CHECKS OK.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACK UPPER FOWARD CARGO DOOR JAMB CORNER. REMOVED AND REPLACED TRIPLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACK ON FRAME STA 937 AND X=-6 BELOW KEEL BEAM. STOPPED DRILLED CRACKS AND INSTALLED FABRICATED REPAIR PART.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CORROSION ON INTERNAL DOUBLER OF AFT LAVATORIES SERVICE PANEL. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PARTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACK ON FUSELAGE SKIN AT STA 1437. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PART.

Part: SPAR — CRACKED (LT WING) · airframe 61,887 hrs · 48,300 cycles

CRACKED NEW REAR SPAR BEAM LT WING. REMOVED DAMAGED AREA.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,887 hrs · 48,300 cycles

CRACK ON AFT PAN OF THE FWD CARGO DOOR. CRACK WAS STOPPED DRILLED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

LIGHTNING STRIKES ON UPPER FWD AND MID SECTION OF LT STA 769-788 FRAME 59. REMOVED FASTENERS, FABRICATED DOUBLER AND INSTALLED.

Part: SUPPORT — CRACKED (NLG WW) · airframe 61,887 hrs · 48,300 cycles

CRACKED NLG TORQUE LINK SUPPORT. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PARTS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACKED ANGLE ON STA Y=827, X=-42 AND Z=-8 AT WING BOX. REMOVED DAMAGED AREA AND INSTALLED DOUBLER.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACKED LONG 16RT AT STA 1437. REMOVED AND REPLACED LONG AT 16RT STA 1437.

Part: PULLEY — CORRODED (TAILCONE) · airframe 61,887 hrs · 48,300 cycles

DURING MAINTENANCE VISIT, MECHANIC FOUND RUSTED AND DAMAGED HARDWARE AND PULLEYS ON TAIL CONE RELEASE SYSTEM. MAINTENANCE REMOVED AND REPLACED DAMAGED AND RUSTY PULLEYS AND HARDWARE.

Part: SPAR — CRACKED (LT WING) · airframe 61,887 hrs · 48,300 cycles

THREE CRACKS ON LEFT WING REAR SPAR. REMOVED AND REPLACED SECTION OF WEB FROM XRS 103-204.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACK ON FRAME AT STA 1322 AND LONG 17 RT. REMOVED AND INSTALLED FRABRICATED REPAIR DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CRACK ON FRAME STA 1322. REMOVED DAMAGE FROM FRAME STA 1322 AND INSTALLED FABRICATED REPAIR DOUBLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

LIGHTNING STRIKE AFT LWR FUSELAGE STA 769-788 RT FRAME 60. REMOVED FASTENERS, FABRICATED DOUBLER AND INSTALLED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CORROSION ON RT CUSP WEB STA 1079-1165. REMOVED AND REPLACED CUSP WEB FROM STA 1079-1165.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,887 hrs · 48,300 cycles

CORROSION ON RT CUSP WEB STA 1147-1250. REMOVED AND REPLACED CUSP WEB FROM STA 1174-1250.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,688 hrs · 48,173 cycles

CORROSION ON CUSP WEB STA 498 TO 503 CABIN FLOOR. REMOVED AND REPLACED CUSP WEB FROM STA 389 TO 503.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 60,308 hrs · 47,242 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS IN SEATS 27 THRU 35 INOPERATIVE. MX REPLACED BATTERY CHARGER AT SEAT 36 NO HELP. REPLACED BLOWN FUSE. OPS CHECK OF LIGHTS NOW CHECKS OK.

Part: FUSE — BLOWN (CABIN) · airframe 59,770 hrs · 46,887 cycles

THE PILOTS FOUND THE EMERGENCY LIGHTS FROM SEAT 23 THROUGH SEAT 36 TO BE INOPERATIVE. MAINTENANCE REPLACED TWO EXIT LIGHT BATTERY FUSES. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 59,170 hrs · 46,483 cycles

DURING A LAYOVER CHECK, MX FOUND THE SEAT EMERGENCY LIGHTS FROM ROW 27-36 TO BE INOPERATIVE. MX FOUND THE WIRING AT 36D TO BE SHORTED AND DAMAGED. SEVERAL FUSES ON THE BATTERY PACKS WERE BLOWN. THE WIRING WAS STOWED. THE SYS CHECKED NORMALLY AND THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 36D) · airframe 59,170 hrs · 46,483 cycles

SEAT EMERGENCY LIGHTS INOP FROM ROW 27-36.

Part: SKIN PANEL — DAMAGED (VERTICAL STAB) · airframe 59,115 hrs · 46,459 cycles

VERTICAL STAB UPPER FIXED L/E REMOVABLE PANEL OVERSIZED HOLES REPAIRED IAW ERA 481049-14.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 59,115 hrs · 46,459 cycles

VERTICAL STABILIZER FRONT SPAR CHORD ZFS52 FATIGUE CRACKS.

Part: SOCKET — FAILED (EMERGENCY LIGHT) · airframe 59,100 hrs · 46,445 cycles

FOUND OVERWING EMERGENCY LIGHTS INTERIOR AND ESCAPE PATH LIGHTS INOP FROM 27-38. FOUND BLOWN FUSES IN EMERGENCY LIGHT CHARGER ASSY B5-211 AND B5-212- REPLACED FUSES- FOUND BAD WIRE UNDER SEAT 28 AND BAD LIGHT SOCKET AT 37399262 R & R LIGHT ASSYS AT SEATS 28 AND 37. REPAIRED WIRE AND REPLACED UNDER SEAT HARNESS AT 37- OPS CKS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,100 hrs · 46,445 cycles

FOUND FWD ENTRY DOORS AND FIRST CLASS SEATS EMERGENCY LIGHTS INOP. R & R FWD SEAT BATTERY CHARGER- NOW TESTS ARE NORMAL.

Part: POWER SUPPLY — INOPERATIVE (COCKPIT) · airframe 59,067 hrs · 46,425 cycles

COCKPIT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERIES PER M/M.

Part: POWER SUPPLY — INOPERATIVE (COCKPIT) · airframe 59,067 hrs · 46,425 cycles

COCKPIT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERIES PER M/M

Part: SKIN — CORRODED (BS 750 L30) · airframe 54,182 hrs · 43,298 cycles

FUSELAGE SKIN FOUND WITH CORROSION AT STA 750, L-30. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR.

Part: SKIN — CORRODED (BS 719) · airframe 54,182 hrs · 43,298 cycles

FUSELAGE SKIN FOUND WITH CORROSION AT STA 719, L30. CUTOUT DAMAGED SKIN/DOUBLER AND INSTALLED REPAIR DOUBLER/TRIPLER.

Part: SKIN — CORRODED (BS 643 L30) · airframe 54,182 hrs · 43,298 cycles

FUSELAGE SKIN FOUND WITH CORROSION AT STA 643, L30. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER/TRIPLER.

Part: LENS — MISINSTALLED (COCKPIT) · airframe 53,413 hrs · 42,842 cycles

ON GEAR EXTENSION FOR LANDING, RT MAIN GEAR IND LIGHT WOULD NOT ILLUM. FOUND RT MLG LIGHT LENS INSTALLED INCORRECTLY. CREW VERBAL RELAMP ATTEMPTED. REPLACED LIGHT LENS, RT GEAR IND CKS GOOD. PROX BOX CKS GOOD. NO SENSOR FAULTS, P/N 658-1881-03.

Part: SUPPORT FITTING — UNKNOWN (CARGO DOORWAY) · airframe 52,778 hrs · 42,432 cycles

FWD, MID, AFT CARGO DOOR STOP PAD SUPPORT FITTINGS REPLACED IAW EA 09-451701-12, ME11.

Part: WIRE — DAMAGED (DOWNLOCK SENSOR) · airframe 52,222 hrs · 42,077 cycles

ON DEPARTURE AFTER GEAR HANDLE UP RED LIGHT ILLUMINATED IN NOSE GEAR LANDING GEAR LIGHT. ALL OTHERS INCLUDING GEAR DOOR LIGHTS WERE EXTINGUISHED. RAN QRH PROCEDURE GEAR DOWN THREE GREEN ILLUMINATED. NOSE GEAR DOWN LIGHT ILLUMINATED WITHIN ONE SEC OF GEAR HANDLE DOWN. MTC IN PROGRESS ON LANDING GEAR SYSTEM. FOUND WIRING BAD ON DOWN LOCK SENSOR. REPAIRED WIRE WITH RAY SPLICE CYCLED NOSE GEAR SEVERAL TIMES ALL INDICATION GOOD.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 51,659 hrs · 41,690 cycles

HORIZ STAB REAR SPAR UPPER CAP, UPPER AND LOWER AFT SKIN REPAIRED IAW EA 09-460214-12, ME02.

Part: FITTING — OVERSIZED (MLG ACTUATOR) · airframe 49,951 hrs · 40,600 cycles

THE LT AND RT MLG RETRACT ACTUATOR SUPPORT FITTINGS WERE OVERSIZED. CONFIRMED THAT PREVIOUS BORE OVERSIZING WAS IN COMPLIANCE WITH AD 2004-25-14. REF. 9-093855-3AD, AD 2004-25-14

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,567 hrs · 39,655 cycles

EMERGENCY PATH LIGHTS INOP SEAT ROW 37 AND 38. REPLACED BATTERY CHARGER AND RELAMPED EMERGENCY PATH LIGHTS IN SEATS 37 AND 38.

Part: COVER — MISINSTALLED (SLIDE) · airframe 48,184 hrs · 39,398 cycles

DURING K-1 LETTER CHECK, FOUND TAILCONE SLIDE COVER AFT MOUNTS NOT INSTALLED. WROTE NR CARD 102 TO REINSTALL COVER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,189 hrs · 38,528 cycles

DAMAGE FOUND WHILE ACOMPLISHING EO 9-62073-12 AT HMV, CRACK IN STA 1446 LONGERON 5R. REPAIRED PER SRM 53-03 FIG 30 AS PER EO 9-62073-12. OPERATION 103 INSTRUCTIONS.

Part: BRACKET — BROKEN (NR 1 ENGINE) · airframe 42,705 hrs · 35,290 cycles

LOUD NOISE FROM AFT LAV / LEFT ENGINE AREA. DIVERTED. FOUND FUEL HEAT SUPPORT BRACKET BROKEN ON LEFT ENGINE. REPLACED BRACKET RAN ENGINE. ALL ENGINE INDICATIONS NORMAL

Part: WIRE — BROKEN (AIRSTAIRS) · airframe 39,626 hrs · 33,122 cycles

FOUND BROKEN WIRE ON EMERGENCY LIGHT IN AIRSTAIR AREA. REPAIRED SAME.

Part: ODOR — DETECTED (CABIN) · airframe 39,225 hrs · 32,826 cycles

ON CLIMBOUT OF PWM CREW NOTICED ODOR THAT RESEMBLED CAR EXHAUST IN CABIN. ENG AT 1.77 EPR BOTH PACKS ON. CREW REPORT THAT SMELL WAS NOT ACRID LIKE ELECTRICAL. A/C WAS BEING FERRIED TO ATL. T/S PER OPN 5088 PNEUMATIC DISTRIBUTION CABIN SMOKE/ODOR FIG 5 AND FIG 7, NO TROUBLE FOUND AND NO SMOKE OR ODOR NOTED. PER OPN 5088 PERFORMED DUCT BURNOUT OPN 5089 A/C OK FOR SERVICE.

Part: BOOT — SPLIT (A/C BAY) · airframe 37,394 hrs · 31,479 cycles

TAIL COMP TEMP HIGH LIGHT CAME ON AT CLIMB PWR AT 22,000 FEET, ALSO MASTER WARNING. REPLACED BLOWN BOOT FROM CABIN TEMP CONTROL VALVE.

Part: GENERATOR — FAILED (APU)

DURING CLIMB THROUGH 300 FL, THE APU GEN TRIPPED OFF. TRIED TO RESET AND WORKED FOR A WHILE AND TRIPPED AGAIN. TRIED RESET AND GOT AC X-TIE LOCKOUT. NOW RT GEN ONLY POWERING THE RT BUS. REPLACED APU GCU. RAN HEAVY LOAD, OP CKS GOOD.

Part: SKIN — GOUGED (BS 541-588)

FUSELAGE SKIN, FS 541-588 STRINGER 26L, GOUGE REPAIR. THE UPPER SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND GOUGED BETWEEN FS 541 AND 588. THE DAMAGED SECTION OF SKIN WAS CUT AWAY FROM THE UPPER SKIN. AN ALUMINUM FILLER WAS INSTALLED WITH AN INTERNAL TITANIUM DOULBER TO REPAIR THE DAMAGE PER ER/A 367832-14, REV A.

Part: SKIN — GOUGED (BS 588-636)

FUSELAGE SKIN FS 588-636, STRINGER 26L, SKIN GOUGE REPAIR. THE UPPER SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND BADLY GOUGED FROM FS 588 TO FS 636. THE SKIN PANEL WAS CUT AT FS 645 FROM STRINGER 26L TO STRINGER 18L AND THE DAMAGED SECTION REMOVED. A NEW SECTION WAS SPLICED IN WITH AN EXTERNAL ALUMINUM SPLICE DOUBLER PER ER/A 367833-14, REV A.

Part: VALVE — INOPERATIVE (NR 1 ENGINE)

AIRBORNE RETURN, RIGHT PACK WOULD NOT PRESSURIZE AIRCRAFT. REPLACED RIGHT PNEUMATIC PILOT PRESS REG. PERFORMED HIGH POWER ENGINE RUN AND CKD OPERATION OF RIGHT PACK, CKS OK.

Part: WIRE — DAMAGED (LT MLG)

AT GEAR EXTENTION LT MAIN INDICATED UNSAFE. FOLLOWED CHECK LIST PROCEDURES. LDG GEAR CYCLED ONCE, NO HELP. FOUND CONDUIT AND WIRING FOR MLG DOWN SENSE TORN DUE TO NR 2 TIRE FAILURE. REPLACED SAME. ALSO, REPLACED NR 1 AND NR 2 WHEEL/TIRE ASSEMBLIES. ALSO, FOUND DOWNLOCK BUNGEE SPRING AND RT SPRAY DEFLECTOR DAMAGED. REPLACED BOTH UNITS. NO DAMAGE TO OTHER AREAS. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

AFT CABIN FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT ASSY.

Part: BATTERY PACK — LOOSE IN RACK (CABIN)

EMERGENCY PATH LIGHTS IN FIRST CLASS INOP. RESEATED BATTERY PACK.

Part: CONNECTOR — LOOSE (AFT AIRSTAIR)

EMERGENCY LIGHT SIGN IN AFT AIRSTAIR INOP. RESEATED PUSHED PINS IN QUICK DISCONNECT IN AFT COMPARTMENT.

Part: CIRCUIT BREAKER — FAILED (RT AC BUS)

AFT CENTER FUEL BOOST PUMP C/B POPPED ON ROTATION. RETURNED TO DFW. A PHASE MISSING AT PUMP C/B. REPLACED RT A/C BUS C/B B1-738.