N906DL

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 81,750 hrs · 62,596 cycles

FA REPORTS WEAKNESS IN AISLE FLOOR AT ROW 14. REMOVED FLOOR PANEL AT ROW 14. INSTALLED SERV PANEL AT ROW 14. ALL CKS GOOD. OK FOR SEV PER AMM 25-30.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,636 hrs · 62,492 cycles

COCKPIT AND FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. R & R THE FWD BATTERY PACKS IAW AMM 33-53. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,333 hrs · 61,437 cycles

ROWS 1 - 4, OVERHEAD EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-53.

Part: EXTINGUISHER — LOW PRESSURE (COCKPIT) · airframe 79,748 hrs · 60,977 cycles

COCKPIT FIRE EXTINGUISHER OUT OF GREEN RANGE. SWAPPED THE FLIGHT DECK BOTTLE WITH AFT CABIN HALON BOTTLE. REMOVED AND REPLACED THE AFT HALON FIRE EXTINGUISHER.

Part: LONGERON — NICKED (BS 1315) · airframe 79,145 hrs · 60,484 cycles

NICKS ON OTBD LEG OF LONGERON 22L AT AFT LAV SERVICE PAN AREA . REPAIRED IAW ERA 560964-14.

Part: DOOR — CORRODED (BS 1315) · corrosion level 2 · airframe 79,145 hrs · 60,484 cycles

BS 1315, STRINGER 20L, AFT LAV SERVICE DOOR CORRODED. REPAIRED IAW ERA 560718-14.

Part: PAN — CORRODED (LAVATORY) · airframe 79,145 hrs · 60,484 cycles

CORROSION. AFT LAVATORY PAN AND ANGLE. REPAIRED IAW ER/A 560718-14.

Part: ANGLE — CRACKED (BS 1463) · airframe 79,145 hrs · 60,484 cycles

ANGLE IS CRACKED ON THE AFT SIDE OF BS 1463 CANTED FRAME RT SIDE OTBD OF MOISTURE CONTAINER FOR RUDDER LIMITER. REPLACED THE ANGLES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,947 hrs · 60,337 cycles

FOUND SEVERAL EMERGENCY LIGHTS INOP. R&R BATTERYS IN POWER SUPPLY B5106 OPS OK PER AMM 33-50.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 78,731 hrs · 60,178 cycles

FOUND PIN PULLED ON THE L1 PAX DOOR SLIDE. R & R THE L1 PAX DOOR SLIDE IAW AMDS 2561-4964.

Part: FRAME — CRACKED (BS 1510) · airframe 78,583 hrs · 60,060 cycles

CANTED TAILCONE SUPPORT FRAME BS 1510 CRACKED AT RT LOWER GUIDE PIN. REMOVED AND REPLACED THE FRAME IAW DWG 9911843-501.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 78,320 hrs · 59,875 cycles

CENTER FLOOR PANEL BETWEEN SEAT ROWS 2B - 2C HAS A SOFT SPOT. REPLACED THE FLOOR PANEL IAW AMM 53-20.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 78,092 hrs · 59,694 cycles

EMERGENCY SEAT MOUNTED LIGHT DAMAGED. SECURED EMERGENCY LIGHT LENS IAW AMM 33-50. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,202 hrs · 59,029 cycles

CEILING MOUNTED EMERGENCY LIGHTS INOP AT ROW 3+4. REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 4 PER AMM 33-53-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,812 hrs · 58,724 cycles

EXTERIOR EMERGENCY ILLUMINATION SYSTEM INOPERATIVE. REPLACED L2-662 AND L2-663 LT AND RT EMERGENCY LIGHT OVERWING SOCKETS OVERWING LIGHTS LAMPS AND CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,805 hrs · 58,716 cycles

LEFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. RESET AND CLEANED THE LIGHT. OPS NORMAL.

Part: PIN — DISENGAGED (R1 DOOR SLIDE) · airframe 75,912 hrs · 58,076 cycles

MAINTENANCE FOUND R1 DOOR EMERGENCY ESCAPE SLIDE PARACHUTE PINS DISENGAGED. THE R1 DOOR EMERGENCY ESCAPE SLIDE WAS REPLACED.

Part: SKIN — DAMAGED (RT WING) · airframe 75,886 hrs · 58,056 cycles

LIGHTNING STIKE RT WING TIP JUST INBD OF AFT POSITION LIGHT. REPAIRED, BLENDED AREA IAW SRM 57-03D, FIG 1, PG 5.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,772 hrs · 57,969 cycles

AFT LEFT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. SECURED LOOSE LIGHT ASSY AT AFT LT EMERGENCY EXIT DOOR.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 75,748 hrs · 57,954 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. MAINTENANCE REPLACED THE SEAT HARNESS AND THE LIGHT CHECKED OK.

Part: PAN — CRACKED (BS 1041-1250) · airframe 74,248 hrs · 56,913 cycles

CRACK ON LT WINDOW RING PAN UPPER /AFT CORNER BETWEEN BS 1041-1060, 1231-1250. DAMAGE WAS REMOVED NDT INSPECTION CHECK, NO CRACKS. ANGLES AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5, SRM 53-05, FIG 122 AND ER/AS 487747-14MA, REV A, 493648-14MA, REV A.

Part: STRINGER — CRACKED · airframe 74,248 hrs · 56,913 cycles

CRACK ON STRINGER 17 AT BS XCW=10 RT SIDE, CENTER TANK. DAMAGE WAS REPAIRED ER/A 537731-14AD, REV. ORIGINAL AND ER/A 537741-14, REV ORIGINAL.

Part: DOUBLER — CORRODED (RT MLG WW) · corrosion level 2 · airframe 74,248 hrs · 56,913 cycles

CORROSION ON PRODUCTION DOUBLER OF CENTER WING REAR SPAR BS XCW= 53 AT RT MLG WHEEL WELL. DAMAGE WAS REPAIRED IAW: ER/A 536507-14, REV ORIG.

Part: SKIN — CRACKED (BS 1418) · airframe 74,248 hrs · 56,913 cycles

CRACKED FUSELAGE SKIN BETWEEN LONGERONS 1-2R, BS 1418. REPAIRED IAW ER/A 537730-14AD REV ORIGINAL, M.

Part: SKIN — DAMAGED (BS 731-750) · airframe 74,240 hrs · 56,908 cycles

LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 731 AND 750 RT SIDE. WINDOW BELT WAS REPAIRED IAW ETI-88-15-270, REV 1 AND ER/A 537735-14AD, REV ORIGINAL "ON CRITICAL ZONE". AREA NOT A CRITICAL ZONE WAS ATTENDED WITH SRM 53-05, FIG. 111, SRM 51-10-3 PAR 21. MAJOR REPAIR. MEASURE NDT SPM 04-00-07, PAR 5, FIG 3, SH 1-2. ORIGINAL THICKNESS 0.130", REMAINING 0.118" WITHIN LIMITS IAW SRM 53-05, FIG III. OLYMPUS NDT 38DL PLUS SONOPEN, V260SM 28AUG15. RII COMPLETED.

Part: SKIN — CRACKED (BS 375) · airframe 74,248 hrs · 56,913 cycles

CRACK WAS FOUND AT FUSELAGE SKIN UPPER FWD CORNER, DOOR JAMB BS 375 BETWEEN LONGERONS 19-20R, REPAIRED IAW ETI-88-15-261, REV ORIG AND ER/A 536516-14AD, REV ORIG.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REMOVED AND FOUND WITHIN LIMITS IAW DWG SR09570087, REV B AND CORROSION ON BOTTOM BORE WAS REMOVED WITH FINAL LENGTH 1.208" OUT OF LIMITS IAW DWG 5935812, REV BB, THEREFORE THIS ACTIVITY WAS ACCOMPLISHED IAW ETI-88-15-268, REV 2 AND ER/A 537732-14AD, REV ORIG MAJOR REPAIR. RII COMPLETED.

Part: STRUCTURE — DAMAGED · airframe 74,240 hrs · 56,908 cycles

ELONGATED HOLE DUE TO INADEQUATE DRILL HOLE ON LT LOWER ACCESS DOOR CUTOUT XRS=189.0 TO 214.0. ELONGATED HOLE WAS REPAIR IAW ETI 88-15-278, REV ORIGINAL. AREA WAS REPAIRED IAW ER/A NR 536495-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1510) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME, BS 1510 AND 3 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT (SM) (ZONE 61) (CARD 48). CRACK, FABRICATED DOUBLER AND FILLER, INSTALL DOUBLER AND FILLER IAW SRM 51-10-3 PAR 14 AND 21 AND ER/A 497316-14MA REV ORIGINAL HFEC INSPECTION EQUIPMENT MENTOR, EXP 10-MAR-16. DIMENTION CRACK IS 0.968".

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT AND RT ANGLE FWD, MID, AND AFT SECTION AT STAIRWAY WALKING BRIDGE. ANGLES WERE BLENDED AND TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21, AND 26. AREA WAS OUT OF LIMITS AND WAS REPAIRED IAW SRM 53-01, FIG 4, TRANS: V260-RM. EQ GAGE THICKNESS 35DL. ORIGINAL THICKNESS IS .032" MIN, REMAINING THICKNESS IS 0.022", ASSOCIATED ER/A 00-511165, ADDED FOR AC 0906.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 74,240 hrs · 56,908 cycles

CRACKED VERTICAL STABILIZER SPAR FWD. SPAR WAS REPAIRED IAW SRM 55-02D, FIG. 26. LENGTH CRACK .750".

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 74,240 hrs · 56,908 cycles

ELONGATED HOLE ON FWD/AFT HINGE AT MID CARGO COMPARTMENT DOOR. AFT HINGE AT MID CARGO DOOR WAS REPAIRED IAW ER/A 497387-14MA, REV B AND INSTALLED IAW AMM 52-31-02. FWD HINGE AT MID CARGO DOOR WAS REPLACED BY NEW PART AND INSTALLED IAW AMM 52-31-02, FINAL I.D: 0.810" ON FWD HINGE AND 0.784" ON AFT HINGE.

Part: SKIN — CRACKED (BS 168-180) · airframe 74,240 hrs · 56,908 cycles

SIX CRACKS WERE FOUND ON FUSELAGE SKIN, FWD SERVICE DOOR JAMB, UPPER FWD CORNER BETWEEN BS 168 - 180. FUSELAGE SKIN FWD SERVICE DOOR JAMB WAS REPAIRED IAW ER/A 536494-14AD, REV ORIGINAL AND ETI-88-15-242, REV 3. MAJOR REPAIR.

Part: FLOOR PANEL — BROKEN (NOT REPORTED) · airframe 74,240 hrs · 56,908 cycles

BROKEN CHANNEL AND FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 51-20-0, 51-70-1, PARA 10.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,269 hrs · 56,929 cycles

CORROSION ON FORWARD BULKHEAD AT CATWALK BRIDGE. TASK 53-062-03. CRACK WAS FOUND. CRACK WAS STOPPED. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-03, 53-01, FIG 2, 53-14-3, 51-30-02 AND ERA 511165-14MA, REV C.

Part: SKIN — DAMAGED (BS 712-750) · airframe 74,240 hrs · 56,908 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 712 - 750 AND LONGERONS 28 - 29R. LIGHTNING STRIKE WAS BLENDED OUT IAW SRM 53-04-1, PAR 5B 1. REWORKED AREA WAS MEASURED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2. FOUND OUT OF LIMITS IAW SRM 53-4-1, PAR 5.E, CONDITION 3. REPAIRED WITH ER/A 536447-14, REV ORIG AND ETI 88-15-279.

Part: FRAME — CRACKED (BS 1463) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME BS 1463. REPAIRED IAW SRM 51-30-2, DWG 9953015, REV CB-38 AND -40 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1401) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 2L BS 1401. DAMAGE LONGERON SECTION WAS REMOVED. NEW SECTION LONGERON AND REPAIR SPLICE WERE ADJUSTED AND DRILLED, NEW LONGERON SECTION AND REPAIR SPLICE WERE TREATED AND PAINTED, NEW LONGERON SECTION AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-30-2, 53-02, FIG 18, 51-10-3, PAR 14 AND 21.

Part: SKIN — DAMAGED (BS 712-731) · airframe 74,240 hrs · 56,908 cycles

LIGHTNING STRIKE ON WINDOW BELT BETWEEN BS 712 - 731, FWD LOWER CORNER AND AFT MID SECTION. WINDOW BELT WAS REPAIRED IAW MD-88, ER/A 537734-14AD REV ORIGINAL.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 74,240 hrs · 56,908 cycles

CRACK ON FWD CLIP OF INTERCOSTAL ZEE IN LT FWD OVERWING EMERGENCY EXIT DOOR. NEW CLIP AND INNER SKIN WERE INSTALLED IAW DWG 9957735, REV-G, SRM 51-10-2, 51-10-4, 51-30-1, 51-30-2, 51-30-5.

Part: FRAME — CRACKED (BS 1485) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME BS 1485. FRAME WAS REPAIRED IAW SRM 53-01, FIG 2. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER STOP DRILL,

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON RT TIE TRACK BETWEEN BS 1212 - 1322. THE TIE TRACK WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, 26, 51-10-4, 51-30-1, AND 53-05 FIG 4C AND NDT SPM 0400-07, FIG 3, PAR 3, SHEET 1-2.

Part: CARGO TRACK — CORRODED (BS 1003-1220) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

SEVERAL CORROSION POINTS ON LT TIE TRACK FROM BS 1003 TO 1220. DAMAGED TIE TRACK WAS REMOVED IAW SRM 51-30-1. NEW TIE TRACK WAS DRILLED IAW SRM 51-10-4, AND TREATED AND PAINTED IAW SRM 51-10-3, PARA 21 AND 14, AND WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: HINGE — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON RT ELEVATOR NR 6 HINGE UPPER AND LOWER BORES. HOLES TO ATTACH EYEBOLT. IN REF OR NRC 16 ACFT ZONE 60. DAMAGE RT ELEVATOR NR 6 HINGE HOLES UPPER AND LOWER WERE REAMED WITH ID 0.626 AND 0.629. THEREFORE OUT LIMITS IAW CMM 27-30-2, TABLE FIG 601 AND HINGE WAS REPLACED AND WILL BE INSTALLED UNDER CARD N 20, ZONE 30. RII COMPLETED. PRIMARY STRUCTURE RETAIN FOR RECORDS.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 74,240 hrs · 56,908 cycles

CRACK ON ANGLE BEHIND STOP 1 IN RT AFT OVERWING EXIT DOOR. CARD 86, ZONE 201. NEW CLIP WAS INSTALLED IAW DOWN 9957735, REV G, SRM 51-30-1, 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3, PARAGRAPH 14 AND 21.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 74,240 hrs · 56,908 cycles

CRACKED PAN BEHIND STOP NR 1 AT RT FWD OVERWING EMERGENCY EXIT DOOR, CARD 321, ZONE 201. NEW DOUBLER WAS INSTALLED IAW SRM 52-05D, FIG 51, 51-30-1, 51-30-2, 51-10-2, 51-10-4, 51-30-5, 51-10-3, PARAGRAPH 14 AND 21. HFEC INSPECTION WAS ACCOMPLISHED ON PAN BEHIND STOP NR 1 AFTER STOP DRILL.

Part: LONGERON — CRACKED (BS 1380) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 13L BS 1380. DAMAGE LONGERON SECTION WAS REPLACED IAW SPM 53.14.4, FIG 2, ITEM 4, SRM 51.30.2, SRM 51.30.5, AND SRM 51.10.4, SRM 51.10.3 PAR 14. 21.

Part: PAN — CRACKED (L1 DOOR) · airframe 74,240 hrs · 56,908 cycles

CRACKED PAN BETWEEN BEAMS 7 AND 8 AT L1 DOOR FWD EDGE. CRACKED PAN REPAIRED IAW SRM 52-05-D, FIG 41.

Part: CARGO TRACK — CORRODED (BS 1110-1155) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION OUT LIMITS ON RT TIE TRACK BETWEEN BS 1110 - 1155 IN AFT CARGO COMPARTMENT. NEW SECTION TIE TRACK WAS REPLACED, TREATED, AND PAINTED IAW SRM 51-10-4, 53-05, FIG 4G, 51-10-3, PAR 21 AND 14, 51-30-5, AND 51-30-1.

Part: SHEAR TIE — CORRODED (BS 732) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FRAME SHEAR TIE BS 732 BETWEEN LONGERONS 28 - 29L. AREA WAS REWORKED. REPAIR FABRICATED, REPAIR TREATED/PAINTED, AND INSTALLED IAW SRM 51-10-3, PAR 26, 21, 14, 53-01 AND 51-30-2.

Part: FRAME — CRACKED (BS 1474) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME BS 1474 LONGERON 18L. CRACKED FRAME WAS REPAIRED IAW SRM 51-30-2, 53-01, FIG 2, SHEET 4 AND 51-01 PAR 21(A), 53-01, FIG 2, SHEET 4, 51-10-3 PAR 14 AND 21 AND 51-30-5.

Part: UNKNOWN — CRACKED (L1 DOOR AREA) · airframe 74,240 hrs · 56,908 cycles

CRACK ON AFT FRAME AND BEAM NR 8 L1 DOOR. INTERCOSTAL AND PRODUCTION DOUBLER WERE REPLACED IAW SRM 51-30-2 CRACK LENGTH 0.250.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 74,240 hrs · 56,908 cycles

CRACKS ON UPPER FWD AND AFT CORNERS OF RT AFT OVERWING EMERGENCY EXIT DOOR. DOUBLERS WERE INSTALLED IAW SRM 52-05D, FIG 51, 51-10-2, 51-10-4, 51-30-1, 51-30-2, 51-30-5, 51-10-3 PARA 14 AND 21.

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 74,240 hrs · 56,908 cycles

BROKEN INTERCOSTAL BETWEEN BEAMS NR 4 AND 5, AFT OF OPERATING MECHANISM AT L1 DOOR. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: FRAME — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME LOWER CAP BS 1437 LONGERON 2L. FRAME WAS REPAIRED IAW SRM 53-01, FIG 2, SHEET 4. HFEC INSPECTION WAS PERFORMED AFTER STOP DRILL, NO MORE CRACKS WERE FOUND IAW NDT SPM 06-10-01-001.

Part: LONGERON — CRACKED (BS 1418) · airframe 74,240 hrs · 56,908 cycles

CRACKED REPAIR ON LONGERON 2R BS 1418. DAMAGE SECTION WAS REMOVED, NEW SECTION LONGERON AND REPAIR SPLICE, NEW SECTION LONGERON AND SPLICE WERE TREATED AND PAINTED, NEW LONGERON AND SPLICE WERE INSTALLED IAW SRM 51-20-2, 53-02, FIG 18, 51-10-3, PAR 14 AND 21.

Part: TEE FITTING — CORRODED (BS 1383) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON TEE , LONGERON 23L IN BS 1383. TEE REMOVED, DOUBLER REPAIR FABRICATED, DOUBLER REPAIR TREATED, PAINTED, REPAIR INSTALLED, AND TEE INSTALLED IAW SRM 51-10-3, PAR 21.14 AND SRM 51-30-5.

Part: DOUBLER — DAMAGED (SKIN) · airframe 74,240 hrs · 56,908 cycles

BENT LOWER EDGE ON EXTERNAL SKIN DOUBLER. THE DOUBLER WAS REMOVED IAW SRM 51-30-2 AND A NEW DOUBLER WAS FABRICATED IAW SRM 52-05D, FIG 37. THE NEW DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21 AND INSTALLED IAW SRM 51-30-2.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 74,240 hrs · 56,908 cycles

CRACKED FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-01, FIG 4, 51-10-3, PAR 21 AND 14.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 74,240 hrs · 56,908 cycles

DELAMINATION ON LWR & UPPER SURFACE OF LT ELEVATOR CONTROL TAB, VHS, SH-CP-SM, ZONE 2 CARD 65. LT ELEVATOR CONTROL TAB WAS REPAIRED IAW ER/A 537738-14, REV ORIGINAL AND CARD 2000-8149-06, CREW 02, JOB NR 000-0011. PERMANENT REPAIR WAS PERFORMED IAW ER/A 537738-14, REV ORIGINAL SECTION I, PERFORM SECTION II WITHIN EVERY FULL, C-CHECK INTERVAL AFTER SECTION I, GVI, TAP TEST IAW NDT SPM CHAPTER 05-10-02-.00, CONTACT LIAISON ENGINEERING IF DISCREPANCIES ARE FOUND FOR FURTHER INSTRUCTIONS.

Part: FRAME — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME ANGLE BS 1437 LONGERON 2L. THE FRAME ANGLE WAS REMOVED, AND A NEW FRAME ANGLE WAS FABRICATED, TREATED AND PAINTED. THE NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-30-5, 53-14-4, 51-10-3 PAR 14 AND 21 AND 51-30-2.

Part: DOUBLER — CRACKED (BS 425) · airframe 74,240 hrs · 56,908 cycles

TWO CRACKS ON INTERNAL PRODUCTION DOUBLER WERE FOUND AT LWR AFT CORNER DOOR JAMB BS 425 BETWEEN LONGERON 26-27R. DAMAGE INTERNAL PRODUCTION DOUBLER WAS REMOVED IAW SRM 53-05, FIG 105. HFEC WAS PERFORMED IAW NDT SPM 06-10-01-001, AND NO CRACKS WERE FOUND AROUND OF AREA AFTER CUT OUT DAMAGE. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 105. REPAIR AREA AND REPAIR PARTS WERE TREATED AND PAINTED IAW 51-10-3, PAR 21,14. CONICAL WASHER WERE INSTALLED IAW MD-88 53-05, FIG 105. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5.

Part: SPAR — DAMAGED (RT) · airframe 74,240 hrs · 56,908 cycles

ELONGATED HOLE WAS FOUND ON REAR SPAR. RT REAR SPAR CAP WAS REPLACED IAW DWG SR09550030, REV C AND SRM 51-10-3, AND 21, 51-30-2 / 51-30-5 AND 51-30-1.

Part: LONGERON — CRACKED (BS 1380) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 17L BS 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: FRAME — CRACKED (BS 1452) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME BS 1452 LONGERON 1. THE FRAME WAS REPLACED IAW DWG 9911860, REV L, SRM 51-30-2 AND 51-30-5.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON RT ELEVATOR NR 6 HINGE FITTING. THE RT ELEVATOR HINGE FITTING WAS REPAIRED IAW ER/A NR 537742-14, REV ORIGINAL.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION FOUND ON FRAME BS 1380 BETWEEN LONGERONS 24L & 24R. THE FRAME WAS REPLACED IAW SRM 57-10-3, 51-30-2, 51-30-5 AND DWG 9912246.

Part: ANGLE — CRACKED (EXIT DOOR) · airframe 74,240 hrs · 56,908 cycles

CRACK ON FWD ANGLE OF UPPER CHANNEL IN LT FWD OVERWING EMERGENCY EXIT DOOR. A NEW ANGLE WAS INSTALLED IAW DWG 9957735, REV G, SRM 51-10-2, 51-30-5, AND 51-10-2 PARA 14 AND 21.

Part: SKIN — CRACKED (BS 1463) · airframe 74,240 hrs · 56,908 cycles

CRACKED FUSELAGE SKIN JUST FWD OF CANTED FRAME BS 1463 AND LONG 2L. REPAIR FABRICATED IAW ETI 88-15-272 AND ER/A 537728-14, REV ORIG. REPAIR WERE TREATED AND PAINTED IAW SRM 51-10-3. MAJOR REPAIR.

Part: PAN — CRACKED (CARGO DOOR FRAME) · airframe 74,240 hrs · 56,908 cycles

CRACKED OUTER PAN ON STOP FITTING NR 1 AFT EDGE AT MID CARGO DOOR. THE PAN WAS REPAIRED IAW ER/A: 455904-14MA, REV A HFEC WAS PERFORMED.

Part: FLOORBEAM — CRACKED (BS 927) · airframe 74,240 hrs · 56,908 cycles

CRACKED FLOORBEAM AT BS 927 AND X-44, Z-2. FLOORBEAM WAS REPLACED IAW SRM 51-10-04, 51-30-01, 51-30-02, 51-30-05, AND DWG 5930561, REV AC.

Part: FLOORBEAM — CORRODED (BS 1322) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FLOORBEAM BS 1322, X -20, X-42. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-05, FIG 20A AND ER/A 397783-14MA.

Part: FRAME — CRACKED (BS 1452) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME ANGLE BS 1452 BETWEEN LONGERONS 2 & 3L. A NEW FRAME ANGLE WAS FABRICATED AND INSTALLED IAW DWG 9911860, REV C, SRM 51-30-2, AND 51-10-2.

Part: FRAME — CRACKED (BS 1322) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME BS 1322 LONGERON 17L. REPAIRED THE FRAME IAW ER/A 493647-14MA, REV B.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 5R BS 1437. REMOVED THE LONGERON SECTION IAW SRM 53-02, PAR 12, REPAIRED IAW SRM 53-02, FIG 18. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 1452) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME ANGLE DOUBLER BS 1452 BETWEEN LONGERONS 2 & 3L. A NEW FRAME ANGLE WAS FABRICATED AND INSTALLED IAW DWG 9911860, REV LT, SRM 51-30-2 AND 51-10-2.

Part: LONGERON — CRACKED (BS 1174) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 9R BS 1174. DAMAGE SECTION LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 74,240 hrs · 56,908 cycles

CRACKED COCKPIT FLOOR PANEL 120D. A NEW FLOOR PANEL WAS ADJUSTED AND DRILLED IAW SRM 51-10-4.

Part: FITTING — CRACKED (BS 905) · airframe 74,240 hrs · 56,908 cycles

CRACK ON FITTING AT BS 905 X -51 AND Z -2. ADJUSTED AND DRILLED NEW FITTING IAW DWG 3922286, REV D, SRM 51-10-4, NEW FITTING WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, NEW FITTING WAS INSTALLED IAW SRM 51-30-5.

Part: HINGE — CORRODED (HORIZONTAL STAB) · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT HORIZONTAL STABILIZER HINGE BOLT AND SLEEVE. BOLTS & SLEEVES WERE REPLACED.

Part: LONGERON — CRACKED (BS 464) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 4R BS 464. THE LONGERON WAS REPAIRED IAW SRM 53-05, FIG 18, 51-10-3, PARR 21, 14, 51-10-4, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 74,240 hrs · 56,908 cycles

CRACKS WERE FOUND ON THE UPPER FWD AND AFT CORNERS OF LT AFT OVERWING EMERGENCY EXIT DOOR PAN. REPAIR INSTALLED IAW SRM 52-05D, FIG 51 51-30-1, 51-30-2, 51-30-5, 51-10-2 AND 51-10-3 PARA 14, 21.

Part: CUSP WEB — CRACKED (BS 1295-1298) · airframe 74,240 hrs · 56,908 cycles

A CRACK WAS FOUND ON THE RT CUSP WEB BETWEEN X -54 TO X -60, BS 1295 - 1298. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A. HFCE INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER DAMAGE REMOVED.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 12L, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 408) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 16L BS 408. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, AND 51-10-3, PAR 21, 14

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FUEL ACCESS PANEL 1361C. THE CORROSION WAS REMOVED. REMOVED AND REPLACED THE ACCESS PANEL IAW AMM 28-40-2.

Part: SKIN — WORN (CARGO DOOR) · airframe 74,240 hrs · 56,908 cycles

WEAR ON DOUBLER ON AFT/FWD LWR CORNER AT FWD CARGO COMPARTMENT DOOR OUTER SKIN. DOUBLERS WERE REPLACED IAW ER/A 486624-14MA, REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 1077-1086) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION OUT OF LIMITS FOUND ON LT CUSP WEB BETWEEN X 54 AND X 60, BS 1077 - 1086 . THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: FRAME — CRACKED (BS 1322) · airframe 74,240 hrs · 56,908 cycles

CRACKED FRAME, BS 1322 LONGERON 17R. FRAME WAS REPAIRED IAW 493697-14MA, REV "B".

Part: GUIDE VANE — DAMAGED (RT WING TE FLAP) · airframe 74,240 hrs · 56,908 cycles

NICKS AND GOUGES FOUND ON INBD GUIDE VANE L/E OF INBD RT WING TE FLAP. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03D.

Part: FLOORBEAM — CORRODED (BS 1322) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FLOORBEAM BS 1322 X 21, X 43. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIG 20A.

Part: LONGERON — CORRODED (BS 1380-1385) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LONGERON 24L BS 1380 - 1385. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-10-4, SRM 51-10-3, PAR 14 AND 21, AND INSTALLED IAW SRM 51-30-2,51-30-5 SRM 51-30-5, AND SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 490-522) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON RT CUSP WEB BS 490 - 522, X -54 TO -60. THE CUSP WEB WAS REPLACED.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 5L BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-2, FIG 18. MAJOR REPAIR.

Part: LONGERON — CRACKED (BS 1431) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 11R BS 1431. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. HFEC WAS PERFORMED IAW NDT SPM 06-10-01-001.

Part: CUSP WEB — CORRODED (BS 1220-1231) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB BETWEEN X 54 - X 60 AND BS 1220 - 1231. REMOVED CORROSION, AND REPAIRED IAW SRM 53-05, FIG 131A, 51-10-3 PAR 21, 14 , AND 53-14-3.

Part: INTERCOSTAL — CRACKED (BS 1271-1287) · airframe 74,240 hrs · 56,908 cycles

CRACKED INTERCOSTAL BS 1271 - 1287 BL 0. HREC INSPECTION ACCOMPLISHED FOUR CRACKS WERE FOUND IAW NDT SPM 06-10-01 .001, DAMAGE WAS CUTOUT AND STOP DRILLED IAW SRM 51-01, PAR 20 AND 53-01, FIG 4. A REPAIR WAS FABRICATED IAW SRM 53-01, FIG 4 AND INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 560-579) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB BETWEEN X 54 - 60 AND BS 560 - 579. THE CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-24, SHEET 1 AND SRM 51-30-1 AND 51-30-2.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 74,240 hrs · 56,908 cycles

WEAR AT UPPER SKIN OF OTBD GUIDE VANE OF OTBD FLAP LT WING. REPAIRED IAW SRM 57-03D, PAR. II .

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 74,240 hrs · 56,908 cycles

WEAR AT L/E DOUBLER ON INBD GUIDE VANE OF OTBD FLAP, LT WING. INBD GUIDE VANE OF OTBD FLAP LT WING WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: FRAME — CORRODED (BS 1418) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FRAME ANGLE, BS 1418, BETWEEN LONGERONS 24-25L. THE FRAME ANGLE WAS REPLACED, TREATED AND PAINTED AND INSTALLED IAW SRM 53-14-4, 51-10-3, P. 14 AND 21, 51-30-2.

Part: LONGERON — CRACKED (BS 540) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 4L BS 540. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18. MAJOR REPAIR.

Part: CUSP WEB — CORRODED (BS 1168-1174) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON RT CUSP WEB, X -54 TO -60 BETWEEN BS 1168 - 1174. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: INTERCOSTAL — CRACKED (BS 938) · airframe 74,240 hrs · 56,908 cycles

CRACKED INTERCOSTAL X 7, BS 938 AT KEELBEAM. THE INTERCOSTAL WAS REPLACED IAW DWG 9936368, REV AW AND SRM 51-30-1 AND 51-30-5.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 74,240 hrs · 56,908 cycles

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

Part: LONGERON — CRACKED (BS 1307) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 8R BS 1307. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: BARREL NUT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON NR 1 BARREL NUT, XH 6-22, RT SIDE AT HORIZONTAL STABILIZER. REPAIRED IAW ETI- 88-15-256, REV 1, AND ER/A 536512-14, REV ORIGINAL.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 74,240 hrs · 56,908 cycles

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

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORRSION ON FUEL ACCESS PANEL 1409C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FUEL ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 74,240 hrs · 56,908 cycles

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

Part: INTERCOSTAL — CRACKED (BS 1401) · airframe 74,240 hrs · 56,908 cycles

CRACKED REPAIR ON INTERCOSTAL BS 1041, X -0. INTERCOSTAL AND REPAIR WERE REMOVED, REPAIR WAS FABRICATED, TREATED, PAINTED AND INSTALLED, INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-3.

Part: ACCESS PANEL — CORRODED (UNREPORTED WING) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION FOUND ON THE ACCESS PANEL 1357C COUNTERSINK. THE CORROSIONWAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 51-22-2A, PAR 6, FIG 8. BUSHINGS WERE FABRICATED IAW SRM 51-22-2A, PARA 6, FIG 8. THE BUSHINGS AND AREA WERE TREATED AND THE BUSHINGS WERE INSTALLED IAW SRM 51-22-2A AND 51-10-3, PARA 21.

Part: CUSP WEB — CORRODED (BS 738-810) · airframe 74,240 hrs · 56,908 cycles

CRACK ON LT CUSP WEB X 54 - 60 BETWEEN BS 738 - 740, AND 808 - 810. DAMAGE WAS REMOVED AND DOUBLER WAS FABRICATED IAW SRM 53-05, FIG 131A -1, DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21, 14, AND INSTALLED IAW SRM 51-30-2, 51-30-5,

Part: INTERCOSTAL — CRACKED (BS 1287-1309) · airframe 74,240 hrs · 56,908 cycles

CRACK ON INTERCOSTAL BS 1287 - 1309 BL 0. INTERCOSTAL REMOVED, AND A NEW INTERCOSTAL WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3 AND 51-10-4.

Part: LONGERON — CRACKED (BS 927) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 7L BS 927. FABRICATED A NEW LONGERON IAW SRM 53-02, FIG 18. THE LONGERON WAS REMOVED IAW SRM 53-02, FIG 18. REPAIR INSTALLED IAW SRM 53-02, FIG 18.

Part: INTERCOSTAL — CRACKED (BS 965-984) · airframe 74,240 hrs · 56,908 cycles

CRACKED INTERCOSTAL BETWEEN BS 965 - 984 AND X 53. REPAIRED THE INTERCOSTAL AND INSTALLED IAW SRM 53-01, FIG 2.

Part: FLOOR SUPPORT — CRACKED (BS 769-788) · airframe 74,240 hrs · 56,908 cycles

CRACK ON FLOOR SUPPORT AT BS 769 - 788 BL 0. THE FLOOR SUPPORT WAS REMOVED, AND A NEW FLOOR SUPPORT WAS DRILLED, TREATED, PAINTED, INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 PG 14, 21 AND 51-10-4.

Part: CUSP WEB — CORRODED (BS 1231-1245) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION OUT OF LIMITS WAS FOUND ON RT CUSP WEB BETWEEN X=-54 AND X= -60 BETWEEN BS 1231 - 1245. THE DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-13. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131-A13. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 131A-13 CIC WAS APPLIED IAW SRM 51-10-3.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 16L BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-04, FIG 14, SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1307) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 8L, BS 1307. REPAIRED IAW SRM 53-02, FIG 18, PAR 12.

Part: CUSP WEB — CORRODED (BS 579-655) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION FOUND ON THE LT CUSP WEB X 54 - 60, BS 579 - 655. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131 A.

Part: FINGER DOUBLER — CORRODED (BS 1155-1183) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FINGER DOUBLER BS 1155 - 1183 BETWEEN LONGERONS 25-26L. THE FINGER DOUBLER WAS REMOVED & REPLACED IAW DWG 5936022, REV BR, 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON 16R BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4, FIG 14, SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 304-313) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 304 -313 AND X 54 TO 60. REPAIRED IAW SRM 53-05, FIG 131A-14, 51-10-3, PAR 14, 21 AND 38, 51-30-1, 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (RUDDER) · airframe 74,240 hrs · 56,908 cycles

DAMAGED METALLIZED ON RUDDER SKIN BOTH SIDE. METALLIZED ON RUDDER SKIN BOTH SIDE WERE REPAIRED IAW SRM 51-70-1A.

Part: SEAT TRACK — CORRODED (BS 1231-1236) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON REPAIR PLUG OF SEAT TRACK X 22 BS 1231 - 1236. REPLACED THE REPAIR PLUG IAW SRM 53-05, FIG 4A, AMD 51-30-1.

Part: CUSP WEB — PUNCTURED (BS 888) · airframe 74,240 hrs · 56,908 cycles

PUNCTURE ON THE RT CUSP WEB BS 888, X -52. THE CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 1.

Part: ANGLE — CRACKED (AFT PRSR BLKHD) · airframe 74,240 hrs · 56,908 cycles

CRACKED ANGLE ON THE AFT PRESSURE BULKHEAD AT BS 1338, LONGERON 7R. THE ANGLE WAS REPLACED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 674-680) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON THE LT CUSP WEB BS 674 - 680 BETWEEN X 54-60. REPAIRED IAW SRM 51-30-5,53-05, FIG 131A-6, AND 51-10-3, PAR 14, 21, 38.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON AFT CARGO DOOR FRAME LOWER BEAM. REPAIRED IAW SRM 51-30-5, 53-05, FIG 123, 51-10-3 PAR 14-21, AND 51-10-3, PAR 38.

Part: FLOOR SUPPORT — CORRODED (BS 172-197) · airframe 74,269 hrs · 56,929 cycles

CORROSION ON FLOOR SUPPORT BS 172 AND 197, X=-54. R & R THE FLOOR SUPPORT IAW SRM 51-30-02AND 51-30-05.

Part: FLOORBEAM — WORN (BS 617) · airframe 74,269 hrs · 56,929 cycles

WEAR ON FLOORBEAM BS 617 BETWEEN X=22 TO X=-22 AT CABIN FLOOR STRUCTURE. R & R FLOOR SUPPORT IAW SRM 51-30-05 AND 53-14-02.

Part: CUSP WEB — CORRODED (BS 484-503) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON CUSP WEB REPAIR DOUBLER BS 484 - 503 X -54 TO -60. REPAIRED IAW SRM 53-05.

Part: CUSP WEB — CORRODED (BS 1005) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON THE LT CUSP WEB, BS 1005 X 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 1236-1250) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER X 54 TO X 60 BETWEEN BS 1236-1250. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (BS 905-925) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB ON DOUBLER REPAIR BS 905 - 925 X 54 - 60. DOUBLER WAS REMOVED IAW SRM 51-30-2. DOUBLER AND RING DOUBLER WERE FABRICATED IAW SRM 53-05 FIG 131A-13. REPAIR TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3 PAR 21-14 AND 51-30-2.

Part: PAN — CRACKED (BS 965) · airframe 74,240 hrs · 56,908 cycles

CRACKED RT RING PAN BS 965 FWD UPPER CORNER AT CABIN FUSELAGE STRUCTURE. DAMAGE WAS REPAIRED IAW SRM 53-05.

Part: LONGERON — CRACKED (BS 1338) · airframe 74,240 hrs · 56,908 cycles

CRACKED END ON LONGERON 1, BS 1338. LONG END WAS REPLACED IAW SRM 53-14-3 AND 51-10-3, PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FUEL ACCESS PLATE COUNTERSINK HOLES NR 1355C, CORROSION ON ACCESS PLATE WAS REMOVED, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS .532" AND FOUND 3 COUNTERSINK ADJACENT, OUT OF LIMITS, MEASURE .548, .538" ON ACCESS PLATE NR 1355C, THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: CUSP WEB — CORRODED (BS 291-294) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 291-294, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: NONE — NONE (BS 313-503) · airframe 74,240 hrs · 56,908 cycles

CRACK ON RING PAN LOWER AFT POSITION BETWEEN BS 313 - 503, RT SIDE. INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW MD NDT SPM PART 6 06-10-01.001.

Part: PAN — CRACKED (BS 1022-1041) · airframe 74,240 hrs · 56,908 cycles

CRACK ON LT RING PAN BS 1022 - 1041 UPPER AND LOWER AFT AT CABIN FUSELAGE STRUCTURE. DAMAGE WAS REPAIRED IAW SRM 53-05, PAR 139, FIG 122,.

Part: CUSP WEB — CORRODED (BS 460-465) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION FOUND ON THE RT CUSP WEB BS 460 - 465 X -54 TO X -60. THE DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-13. A REPAIR WAS FABRICATED IAW SRM 53-05, FIG 131A-13. THE REPAIR WAS TREATED, AND PAINTED IAW SRM 51-10-3, PAR 21, 14 AND INSTALLED IAW SRM 51-30-2 .

Part: CUSP WEB — CORRODED (BS 712-720) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LEFT CUSP WEB X 54 - 60 BETWEEN BS 712 - 750. REPAIRED IAW SRM 53-05, FIG 131A-2.

Part: LONGERON — CRACKED (BS 1336) · airframe 74,240 hrs · 56,908 cycles

CRACKED LONGERON END 17R BS 1336 IN PAX CABIN. LONGERON REPLACED IAW SRM 53-14-3, 51-30-5 AND 51-10-3 PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON FUEL ACCESS PANEL 1303C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: PAN — CRACKED (BS 313-332) · airframe 74,240 hrs · 56,908 cycles

CRACK ON RING PAN UPPER AFT POSITION BETWEEN BS 313 - 332 RT SIDE. DAMAGE WAS REPAIRED IAW SRM 53-05, PAR 139, FIG 122, AND ER/A 487747-14 MA, REV A.

Part: CUSP WEB — CORRODED (BS 846-905) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON LT CUSP WEB ON DOUBLER PREVIOUS REPAIR, STA Y=846 TO 905 X 52 TO 60, CFS, MRB 53-037-01, CARD 137, ZONE 201. DOUBLER WAS REMOVED IAW SRM 51-30-2 NEW DOUBLER AND NEW RING DOUBLER WERE FABRICATED IAW SRM 53-05, FIG 131A-10. NEW PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 21, 14 AND INSTALLED IAW SRM 51-30-2. PRIMARY STRUCTURE.

Part: SEAT TRACK — CORRODED (BS 370-747) · corrosion level 2 · airframe 74,240 hrs · 56,908 cycles

CORROSION ON PLUG BS 370, 642, AND 747 AT LT SEAT TRACK X=54. PLUG`S WERE REPLACED IAW 53-05, FIG 4A.

Part: FRAME — CRACKED (BS 905) · airframe 72,077 hrs · 55,395 cycles

BS 905 OVERWING FRAME CRACKED, LONGER THAN 0.125. REMOVED AND REPLACED THE FRAME IAW DWG SR09530282-7013 AND WORK CARD 5310-01415-0301.

Part: LATCH — BROKEN (TAILCONE) · airframe 72,118 hrs · 55,429 cycles

DURING AN A-CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE UPPER LT SIDE SLIDING BLOCK FOR THE TAILCONE LATCH WAS WORN BEYOND ALLOWABLE LIMITS. MAINTENANCE REPLACED THE UPPER SLIDING BLOCK FOR THE LT SIDE, RIGGED THE TAILCONE AFTER INSTALLATION, AND FOUND THE SYS OPS.

Part: FRAME — CRACKED (BS 845) · airframe 72,077 hrs · 55,395 cycles

LT BS 845 OVERWING FRAME CRACKED. REPAIRED IAW WORK CARD 5310-01415-0301.

Part: CAM — DAMAGED (TAILCONE RELEASE) · airframe 72,118 hrs · 55,429 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE CAM RELEASE MECHANISM SPLINES WERE DAMAGED. MAINTENANCE REPLACED THE CAM MECHANISM AND THE OPS CHECK WAS GOOD.

Part: STRUCTURE — DAMAGED (BS 1437) · airframe 72,077 hrs · 55,395 cycles

EMPENNAGE RT SIDE FASTENER EMITTING RUST, POSSIBLY SHEARED AT RT SKATE ANGLE AND SKIN CRACKED AT RIVET AND RIVETS LOOSE 3EA. BETWEEN L-1 & L -2 BS 1437, COMPLIED WITH PRI 528364-14, REV O. REPAIRED IAW FINAL ER/A 528364-14 REV ORIGINAL.

Part: FRAME — CRACKED (BS 845) · airframe 72,077 hrs · 55,395 cycles

LEFT BS 845 OVERWING FRAME CRACKED. REPAIRED IAW WORK CARD 5310-01415-0301.

Part: LANYARD — MISINSTALLED (TAILCONE SLIDE) · airframe 72,077 hrs · 55,395 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE HAD AN IMPROPERLY INSTALLED LANYARD. THE LANYARD WAS NOT ATTACHED TO THE FLOOR ANCHOR AS DESIGNED. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE TAILCONE SLIDE LANYARD WAS INSTALLED CORRECTLY.

Part: RETAINER — CORRODED (TAILCONE RELEASE) · airframe 72,077 hrs · 55,395 cycles

MAINTENANCE DISCOVERED THAT THE INTERIOR TAILCONE RELEASE HANDLE RETAINMENT CLIPS WERE CORRODED OUT OF ALLOWABLE LIMITS. THE CLIPS WERE REPLACED AND THE FUNCTIONAL CHECK, PULL FROM CLIPS, WAS COMPLETED SATISFACTORILY.

Part: STRUCTURE — CORRODED (DOOR FRAME) · airframe 72,118 hrs · 55,429 cycles

MID CARGO DOOR FRAME AFT LOWER CORNER CORRODED. REPLACED STRUCTURE IAW DWG 5930483.

Part: LATCH — WORN (TAILCONE) · airframe 72,072 hrs · 55,390 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE UPPER LT HAND LATCH ARM WAS WORN BEYOND ALLOWABLE LIMITS. THE TAILCONE RELEASE ARM WAS REPLACED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: LATCH — WORN (TAILCONE) · airframe 72,072 hrs · 55,390 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE UPPER RT LATCH ARM WAS WORN BEYOND ALLOWABLE LIMITS. THE TAILCONE RELEASE ARM WAS REPLACED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,614 hrs · 55,059 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING NEAR DOOR L2 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: PIN — UNSECURE (R1 DOOR SLIDE) · airframe 71,505 hrs · 54,988 cycles

DURING LINE CHECK, MAINTENANCE DISCOVERED THAT THE PARACHUTE PINS WERE NOT INSTALLED ON THE R1 DOOR SLIDE. MAINTENANCE R & R THE SLIDE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,432 hrs · 54,935 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 15ED INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN IN THE HARNESS. THE WIRE HARNESS WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 68,660 hrs · 53,085 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24DE IN THE CABIN WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.

Part: SKIN — DENTED (RT WING LE SLAT) · airframe 68,452 hrs · 52,944 cycles

DURING SCHEDULED MX, THE RT WING INBD L/E SLAT WAS FOUND DENTED. REPAIR WAS ACCOMPLISHED IAW ERA 508145-14, REV O.

Part: THRESHOLD — CORRODED (BS 662-682) · airframe 68,452 hrs · 52,944 cycles

DURING A SCHEDULED MX VISIT, CORROSION WAS FOUND ON THE MID CARGO BAY THRESHOLD BS 662-682, RBL 22. REPAIRS WERE ACCOMPLISHED IAW SRM 53-05, FIG 123, OPTION 2 AND SRM 51-30-5. REQUIRED INSPECTION COMPLETED.

Part: LONGERON — DAMAGED (BS 1388) · airframe 68,452 hrs · 52,944 cycles

LONGERON 11, RT LOWER FLANGE DAMAGED DUE TO CHAFE FROM AIR CONDITIONING LINE AT BS 1388. FOND BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-01, STEP 3, FIG 1, SHT 3. REPAIRED IAW SRM 53-2, REPAIR 12.

Part: THRESHOLD — CORRODED (BS 1174-1192) · airframe 68,452 hrs · 52,944 cycles

CORROSION FOUND ON AFT CARGO BAY THRESHOLD BS 1174-1192 RBL 22 AROUND DOOR STOP PADS FITTINGS. REPAIRED IAW SRM 53-05, FIG 123, OPTION 1 AND SRM 51-30-5.

Part: DOOR FRAME — UNKNOWN (MLG) · airframe 65,555 hrs · 50,900 cycles

R & R LT FWD MLG DOOR JAMB FRAME AS REQUIRED IAW ER/A 50527-14, ORIGINAL DWG 5930584 AND SRM 51-10-3, ALODINE AND PRIME OF BARE METAL, SRM 51-10-4, FASTENER HOLE DRILLING, SRM 51-30-1, 51-30 AND 51-30-5 FASTENER INSTALLATION.

Part: WIRE — BROKEN (CATWALK) · airframe 65,548 hrs · 50,895 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE MIDDLE EMERGENCY PATHWAY LIGHT FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR AND RE-PINNED IT. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SPAR CAP — CRACKED (RT WING) · airframe 65,435 hrs · 50,800 cycles

FOUND 1.2 INCH CRACK IN RT WING LOWER SPAR CAP WHILE PERFORMING INSPECTION PER EA 09-471576-12 AD REV A OPN NR 0502. INSTALLED REPAIR PER EA 09-471576-12 AD REV A ME06 OPN NR 0601 AND DRAWING J060271 (TEMPORARY REPAIR).

Part: SPAR — CRACKED (WING) · airframe 65,435 hrs · 50,800 cycles

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

Part: SOCKET — DEFECTIVE (CABIN) · airframe 64,569 hrs · 50,190 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. MAINTENANCE REPLACED LIGHT SOCKET ASSEMBLY AT SEAT PER AMM 33-53. OPERATION OF LIGHT CHECKS OK.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 63,363 hrs · 49,410 cycles

DURING LINE CHECK, MX FOUND FWD LOWER LT EMERGENCY EXIT PATH LIGHT ABOVE CATWALK IN TAIL COMPARTMENT TO BE INOPERATIVE. MX RETERMINATED WIRES IAW SWPM 20.

Part: SLIDE — MISRIGGED (L1 DOOR) · airframe 63,363 hrs · 49,410 cycles

DURING LINE CHECK MX FOUND THE L1 DOOR SLIDE LANYARD INSTALLED IMPROPERLY AND THE R1 DOOR LANYARD FRAYED. MX REPOSITIONED THE L1 DOOR SLIDE LANYARD AND REPLACED THE R1 DOOR SLIDE LANYARD. ALL WORK COMPLETED UNDER AMM 25-62-00.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 61,809 hrs · 48,344 cycles

VERT STAB LT SPAR CHORD CRACK. REPAIRED IAW ERA 482730-14 ON NR 73. (DLM88101466)

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 61,809 hrs · 48,344 cycles

VERT STAB RT SPAR CHORD 2 HOLES CRACKED BELOW ZFS 52. REPAIRED ON NR 72 IAW ERA 482731-14. (DLM88101465)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,728 hrs · 48,283 cycles

THE EMERGENCY FLOOR LIGHT AT SEAT 19D WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 61,257 hrs · 47,994 cycles

MAINTENANCE FOUND THE EMERGENCY PATH LIGHT AT SEAT 31DE TO BE INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR AND THE SYSTEM THEN OPERATED NORMALLY. AN OPERATIONAL CHECK WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (L1 DOOR) · airframe 54,460 hrs · 43,572 cycles

FOUND ON ARRIVAL DAMAGE 2 FT AFT 1L DOOR AT FLOOR LEVEL A 5 INCH BY 1 INCH GOUGE. REPAIRED PER SRM 53-04D PAGE 33 ITEM B CLASS 1 REPAIR. WHILE DOWN FOR REPAIR ALSO WORKED MSU C/N C05037125 ACTL 3102 FOR PREVIOUS DAMAGE INCORP, ORATING A FOUR CORNER DOUBLER REPAIR PER SRM 53-04D PAGE 33 ITEM B CLASS 1 REPAIR. REF ITEM 011 OF LOGSHEET G774302.

Part: PUMP — INOPERATIVE (CENTER TANK) · airframe 51,393 hrs · 41,505 cycles

C/B J21 AFT CENTER FUEL BOOST PUMP POPPED SHORTLY AFTER T/O, PERFORMED QRH. WITH CENTER FORWARD FUEL BOOST PUMP SUPPLYING BOTH LEFT AND RIGHT ENGINES INLET FUEL LO PRESSURE MESSAGES ILLUMINATED INTERMITTENTLY. FOUND HIGH RESISTANCE AT TERM 2 AT S3-10 TO PUMP. REPLACED CTR AFT BOOST PUMP PER M/M. OPS CHECK GOOD.

Part: WIRE HARNESS — BURNED (CABIN) · airframe 49,743 hrs · 40,217 cycles

PRIMARY STAB TRIM C/B POPPED. SIMULTANEOUS TAIL CONE UNSAFE LIGHT ON OAP. FOUND WIRE BUNDLE BURNED IN MID CABIN CEILING AREA. REPAIRED WIRING.

Part: ACM — ODOR (RT ACM BAY) · airframe 48,221 hrs · 39,149 cycles

AT FL310 RT PACK TRIPPED AFTER RUNNING FULL HOT. STARTED DESCENT AND LEFT PACK ALSO TRIPPED. CABIN APPROACHED 10,000. F/A'S NOTICED SMELL FROM PACKS IN CABIN. PACKS RECOVERED AFTER LEVEL AT 8000 FT. INSPECTED LT AND RT PACKS FOR BLOWN DUCTS AND ACM'S FOR ROTATION, ALL OK. CLEANED CABIN AND COCKPIT TEMP SENSORS. RAN PACKS IN AUTO AND MANUAL FULL COLD AND FULL HOT WITH APU AND ENGINES. ALL OPN IS NORMAL. PACKS CHECK OK.

Part: VALVE — STICKING (OXYGEN MASK) · airframe 48,221 hrs · 39,149 cycles

CAPT'S O2 MASK HAS STICKING VALVE. FOUND KINK IN O2 MASK SUPPLY LINE. REPLACED MASK ENCLOSURE BOX PER M/M. LEAK AND OPERATIONAL CKECK GOOD.

Part: FUSE — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 47,514 hrs · 38,650 cycles

EMERGENCY AISLE LIGHTS INOP ROW 31 THRU 48 SECTION. REPLACED FUSE IN POWER SUPPLY.

Part: TAPE — LOOSE (F/O 3R WINDOW) · airframe 45,931 hrs · 37,563 cycles

PRESSURE SENSITIVE TAPE COVERING CURING WINDOW SEALANT ON FIRST OFFICER'S AFT WINDOW 3R CAME OFF INFLIGHT. ALL ENGINE INDICATIONS NORMAL/NO ENGINES SHUTDOWN IN FLIGHT. A/C ATB. PERFORMED GEN VISUAL INSP OF RT ENGINE, NO DEFECTS FOUND. REMOVED REMAINING TAPE DUE SEALANT CURED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,838 hrs · 36,804 cycles

EMERGENCY PATH POWER SUPPLY INOP ROWS 31-38. REPLACED POWER SUPPLY

Part: SWITCH — INOPERATIVE (MLG) · airframe 44,537 hrs · 36,568 cycles

NOSE WHEEL UNSAFE INDICATION AFTER TAKEOFF. FOLLOWED APPROPRIATE CHECKLIST STILL HAD UNSAFE INDICATION. NLG IND VISUAL INSPECTION CONFIRMED GEAR DOWN. RETURNED FOR LANDING. FOUND PROX SENSOR D1-32 INOP. REPLACED AND SWUNG GEAR. CHECKS OK PER M/M.

Part: RELAY — FAILED (E/E BAY) · airframe 40,769 hrs · 33,809 cycles

ELECTRICAL ODOR COMING FROM E/E. FOUND VAPOR COMING FROM BATTERIES. REPLACED BATTERIES, CHARGER, TEMP SENSOR AND R2-56 RELAY.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 40,640 hrs · 33,710 cycles

FWD ENTRY DOORS AND COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 39,021 hrs · 32,491 cycles

ON T/O SMOKE/ODOR IN AIRCRAFT. SMOKE ALARM GOING OFF IN AFT LAV. SMOKE STOPPED AT ALT. SMOKE AND ALARM STARTED AGAIN ON FINAL APPROACH FOUND REVERSER STOW LINE IN AFT FUSELAGE LEAKING AT SWAGE RE-SWAGED RT SIDE REVERSER STOW LINE LK AND OPS WITH NO DEFECTS NOTED. PERFORMED OPN 5088 DUCT BURNOUT. NO SMOKENOTED

Part: LINE — LEAKING (HYD SYSTEM) · airframe 38,992 hrs · 32,472 cycles

IRREG: DURING APPROACH TO LANDING WITH WING A/I (TAIL SELECTED) AND APU ON STRONG FUMES IN AFT LAV (CAPTS SIDE) AND SMOKE DET CAME ON - FOUND HYDRAULIC LINE LEAKING IN TAIL COMPARTMENT - TIGHTENED SAME - PERFORMED DUCT BURNOUT

Part: APU — CONTAMINATED (APU BAY) · airframe 38,628 hrs · 32,204 cycles

ENGINE ANTI-ICE ON SMELLED FUMES AFTER PLACING WING ANTI-ICE ON. SMOKE ALARMS IN REAR SOUNDED ON APPROACH WITH POWER AT IDLE. FUMES SMELLED DURING CLIMB, CRUISE, DESCENT WITH ALL AND CROSSED FEEDS OPEN. APU OFF TEMP CONTROL AT 12 O''''CLOCK, LT LAV SMOKE DECT SOUNDED SHORTLY AFTER WING ANTI-ICE PLACED TO TAIL OPERATION. FOUND APU WET WITH OIL. REPLACED APU, ALSO PERFORMED DUCT BURNOUT OPN 5088.

Part: WATER SEPARATOR — FAILED (ACM BAY)

ON CLIMBOUT, TAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER LT ENG BROUGHT BACK TO IDLE/LT PACK OFF. F/A COMPLAINED OF SMOKE SMELL IN CABIN, THEN UNABLE TO MAINTAIN CABIN PRESSON RT PACK. REPLACED RT WATER SEPARATOR ANTI ICE VALVE.

Part: WINDOW — OUT OF ADJUST (COCKPIT)

CAPT'S ESCAPE WINDOW WILL NOT OPEN. ADJUSTED CAPT'S SLIDING WINDOW, OPS CK OK.

Part: SKIN — DENTED (BS 322)

SKIN WAS FOUND DENTED AT APPROX BS 332 BETWEEN S19 AND S20R. A CUTOUT OF 8.2 BY 3.2 WAS MADE TO REMOVE THE DAMAGE. REPAIRED PER ERA 332600-14.

Part: SKIN — DENTED (BS 425)

A DENT WAS FOUND IN THE FUSELAGE SKIN AND UNDERLYING DOOR SURROUND DOUBLER AFT OF THE C1 DOOR AT APPROX L21R. REPAIRED PER ERA 332617-14.

Part: SKIN — GOUGED (BS 167-188)

A GOUGE WAS FOUND ON THE FUSE SKIN BETWEEN STA 167 TO 188 AT L21R. CUTOUT IS 6.2 BY 21.2. REPAIRED PER ERA 332597-14.

Part: SKIN — GOUGED (BS 588)

FUSE SKIN WAS FOUND TO HAVE A GOUGE FWD OF STA 588 BELOW L17R. DAMAGE REMOVAL RESULTED IN A CUTOUT OF APPROX 2.9 BY 30. REPAIRED PER ERA 332627-14.

Part: LIGHT — INOPERATIVE (CABIN)

EMER FLASHLIGHT AT FWD F/A JUMPSEAT INOP. REPLACED FLASHLIGHT.

Part: ADC — MALFUNCTIONED (E/E COMPT)

ON APP GPWS WARNING OF MODE 4A TOO LOW GEAR TOO LOW TERRAIN GEAR WAS DOWN FLAPS AT 40 DEG. GO-AROUND WAS ACCOMPLISHED AND GPWS CMPTR C/B PULLED. REPLACED R2-1 RELAY, REPLACED GPWS CMPTR, TESTS OK. REPLACED ADC CMPTR DUE TO HISTORY. PERFORMED CK OUT PER M/M 34-45-00 PARA F MODE 4, TESTS OK.

Part: LINE — LEAKING (RT PYLON)

ACFT LOST ALL RT SYST HYD FLUID DURING CLIMBOUT. FOUND HYD PRESSURE LINE IN RT PYLON LEAKING. REPLACED LINE SYST, LEAK CHECKED OK.

Part: AIR DISTRIBUTION — ODOR (CABIN)

ON T/O PASSENGER REPORTED RUMBLING NOISE AND BURNT RUBBER SMELL. INSPECTED LANDING GEAR, RAN PACKS AND NO TROUBLE FOUND.

Part: LIGHT — BROKEN (CABIN)

TRACK LIGHTING LIGHTS LOOSE AT ROWS 25-21-18-15-3. REPLACED LENS AND INSTALLED LIGHTS AT SEATS 25-21-18-15-3. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: HYD LINE — LEAKING (RT WW)

AFTER T/O, STRONG FUME/SMELL THROUGHOUT CABIN AND COCKPIT. DECLARED EMERGENCY LANDING AND DURING TAXI COCKPIT'S SMOKE ALARM SOUNDED. FOUND TRANS PUMP SUPPLY LINE LEAKING IN RT W/W, REPLACED LINE.

Part: JAMB — CORRODED (FWD CARGO DOOR)

DURING LETTER CHECK, THE FORWARDD CARGO DOOR OPENING WAS FOUND WITH EXTENSIVE CORROSION ON THE LOWER JAMB PAN. A SPLICE REPAIR WAS ACCOMPLISHED PER MD-88, SRM 53-05, FIG 44.

Part: FRAME — CORRODED (C-1 DOOR CUTOUT)

FOUND DURING D-1 LETTER CHECK - CORROSION AT C-1 DOOR CUT-OUT LOWER THRESHOLD/FRAME. REPAIRED PER SRM 53-05 FIG 44 AND ERA 359982-14.

Part: SKIN — CRACKED (BS 1271-1322)

FUSELAGE SKIN DAMAGED BETWEEN FS 1271 AND 1322 BETWEEN S24L AND 30L, DUE TO CONTACT WITH GROUND SUPPORT EQUIPMENT. STRINGERS 25L, 26L AND 27L ARE DAMAGED AND NEW SECTIONS ARE SPLICED IN PER SRM REFERENCE DL ERA 273500-14 REV A.

Part: AIR COND — ODOR (FLIGHT DECK)

ON FINAL APPROACH TO ATL, HAD AFT LAV SMOKE DETECTORS ACTIVATE. NOTICED SOME SMOKE ODOR IN FLT DECK. MTC CHECKED PACK OPERATION AND APU INTAKE FOR CONTAMINATION, COULD NOT DUPLICATE, RETURNED TO SERVICE.

Part: ANGLE — CRACKED (MLG WW)

FOUND DURING C-1 LETTER CHECK, MLG WHEEL WELL AFT JAMB AFT ANGLE CRACKED .75 INCH. REPAIRED PER SRM 53-05 FIG 101.