N730UP

Part: STRUCTURE — DAMAGED (COCKPIT)

INSPECTION TYPE:N/A HOLE IN FLOOR PIT 31 STA 320. C/W INTERIM REPAIR REF EO DC8-5320-8724 APPX C, PERMANENT REPAIR.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE)

ESCAPE SLIDE PRESSURE GAUGE CAN NOT BE SEEN. REPACKED CHUTE. CK'S OK.

Part: SLIDE — DISLODGED (EMERGENCY EXIT)

ESCAPE SLIDE FELL OUT OF CABIN EXIT DOOR. REINSTALLED ESCAPE SLIDE PER DC8 AMM REF 25-60-01-2.

Part: STRINGER CLIP — CRACKED (S65) · airframe 72,792 hrs · 49,170 cycles

INSPECTION TYPE:C3 NR 2 MAIN TANK INSIDE FUEL PANEL 506C HAS CRACKED CLIP ON STRINGER 65. REMOVED CRACKED CLIP IN NR 2 MAIN TANK STRINGER 65 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPLACEMENT CLIP IN NR 2 MAIN TANK STRINGER 65 IAW DWG 4613090, AND SRM 51-3-2, AND SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,792 hrs · 49,170 cycles

REPLACE LWR BELLY SKIN FROM STA 190 TO 450 DUE TO CORROSION AND EXISTING NON STANDARD REPAIRS. REMOVED AND REPLACED FUSE LWR BELLY SKIN STA 190 TO 450 AND FABRICATED AND INSTALLED INTERNAL DOUBLER AT STA 360-450.

Part: DOOR FRAME — CRACKED (FS1400 L22R) · airframe 72,792 hrs · 49,170 cycles

HFEC AND VISUAL INSP DETECTED A .250" CRACK ON THE C-4 (D PIT) UPPER FWD JAMB CORNER.CUT OUT DAMAGED AREA AT UPPER FWD JAMB CORNER STA 1400 IAW SRM 53-02-00 FIG 21. FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIR TRIPLER, AND FILLER IAW SRM 53-02-00 FIG 21, 51-1-8, AND SRM 51-01-26

Part: SKIN — CRACKED (FS 418 L21R) · airframe 72,792 hrs · 49,170 cycles

HFEC AND VISUAL INSP DETECTED A .250" CRACK ON THE RT FWD T-1 DOOR AFT JAMB CORNER. CUT OUT DAMAGED AREA ON RT FWD T-1 DOOR AFT DOOR JAMB IAW SAA EA 008-5320-01-A0156. FABRICATED AND INSTALLED REPAIR, 1 FILLER, -2 DOUBLER, AND -3 TRIPLER IAW UPS EO DC8-5330-24205-A, SAA EA NR 008-5320-01-A0156, BAC MESSAGE NR 1-182681850-2, SRM 53-02-OO FIG 18 TR NR 53-199, AND FAA FORM 8100-9.

Part: SKIN — CORRODED (FS 400 L36) · airframe 72,792 hrs · 49,170 cycles

CORROSION FOUND ON SKIN AND FASTENERS UNDER FWD ADF LOOP ANTENNA. CUTOUT CORROSION FROM SKIN UNDER ADF LOOP ANTENNA IAW SRM 51-06-08. FABRICATED AND INSTALLED FOUR FINGER DOUBLERS, AND REPAIR DOUBLER IAW SRM 53-02-01 FIG 7, 51-1-26, AND SRM 51-1-8.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,792 hrs · 49,170 cycles

FOUND TWO CRACKS ON WEB AFT SIDE OF STA 1766 RT SIDE AT L16R. STOP DRILLED TWO CRACKS AT AFT PRESS BULKHD STA 1766 L16R IAW 53-2-0. FABRICATED AND INSTALLED -1 FILLER, -2 FINGER DOUBLER -3 DOUBLER IAW UPS EO FILE NR DC8-53-20547, SAA EA NR 008-5320-01-A0158 BAC SERV REQUEST NR 1-182442136, AND FAA FORM 8100-9 ALL DATED 21 APRIL 06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,792 hrs · 49,170 cycles

FOUND MAIN CABIN APPROX STA 880 L22R RBL 57 FLOORBEAM CRACKED APPROX 4" FROM LIGHTNING HOLE TO FASTENER. CUT FLOORBEAM AT STA 879 RBL 49.03, FABRICATED AND INSTALLED -1,-2 -3,-4 REPAIR ANGLES, AND FLOORBEAM EXTRUSION IAW UPS RAA DC8-53- 20546, SAA EA# 008-5320-01-A0157, DATED 20 APR 06, FAA FORM 8100-9 DATED 19 APR 06, BAC SRV REQUEST 1-181038586.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,792 hrs · 49,170 cycles

AFTER REMOVAL B-PIT SCUFF PLATE TO FOM NDT INSPECTION IAW EO DC8- 5330-20206-D FOUND CORROSION ON FUSELAGE SKIN. INCREASED RADIUS TO MIN 1.0" IAW SAA EA NR 008-5320-01-A0154. FABRICATED AND INSTALLED -1, -2 SLEEVE, -3 DOUBLER, -4 TRIPLER, AND -5 FILLER IAW UPS EO DC8-5330-24211-A, SAA EA NR 008-5320-01-A0154, BAC TELEFAX DHS-SAT-00-00230H DATED 30/MAY/06, BAC MESSAGE NR 1-181038119-3 BAC MESSAGE NR 1-181038119-5, AND FAA FORM 8100-9 ALL DATED 4/25/06

Part: BATTERY BEACON — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS FAIL TEST. DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW AMM 35-50-01-2. OPERATIONAL TEST GOOD. PN OFF 60-1223-5 SN OFF 248 PN ON 5708458-503 SN ON FTL31.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 1320 SHEAR TIE IS CRACKED BELOW LONG 21L. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 9755510 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (LT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 LT WING FLAP LINK SUPPORT ASSY IS CRACKED AT FLAP HINGE 3. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM. 51-1-20D, 51-3-0.

Part: STRAP — BROKEN (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 360 LBL 12 STRAP IS BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633833 AND SRM 51-1-21.

Part: STRAP — BROKEN (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 440 AT LBL 12 HAS STRAP BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633853 AND SRM. 51-1-21.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 210 FINGER DOUBLER AND SPLICE PLATE ARE CORRODED BEYOND LIMITS BETWEEN LONG 21L TO 31L AND STATION 210 LONG 25R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER, SPLICE PLATE AND SPLICE FITTING IAW DWG 5779916,4653726 AND SRM 51-1-20D, 51-1-21

Part: DOUBLER — CRACKED (LT CENTER DOOR) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, LT CENTER SERVICE DOOR TORQUE TUBE CUTOUT DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 52-2-0 FIG 2.

Part: LONGERON — CRACKED (MAIN CABIN) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 680 LONG. 9L IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 650-680,FABRICATED AND INSTALLED LONGERON SECTION IAW SRM. 53-2-2 FIG. 10.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 300 BETWEEN LONG 34L-35L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG. 2D.

Part: FITTING — CRACKED (WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 NR 1 ALT. TANK AT XRS 440 APPROX. STRINGER 59 FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW DWG.5644972, 3645612 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (LEFT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, INSIDE NR 1 ALT FUEL TANK STATION XRS 440 STRINGER 58 BOOST PUMP FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 STATION 1730 LONGERON 14R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 1720 TO 1740 AND INSTALLED SPLICES AND STRAPS IAW SRM. 53-2-2 FIG. 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 1730 LONGERON 15L IS CRACKED. REMOVED LONGERON SECTION, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED REPAIR STRAPS AND SPLICES IAW SRM 53-2-2 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 1741 LONG 17L IS CRACKED. REMOVED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION AND INSTALLED SPLICE FITTINGS AND STRAPS IAW SRM 53-2-2 FIG 10.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 300 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 33R-34R. REMOVED AND REPLACED FITTING IAW DWG. 3755824 AND SRM. 53-2-0 FIG. 2D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 34L TO 35L. REMOVED AND REPLACED FITTING IAW DWG. 3755845 AND SRM. 53-2-0 FIG. 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 AFT TORQUE BOX UPPER FRAME IS CRACKED AT STATION 1220 LONGERON 34L TO 35L. REMOVED AND REPLACED FRAME GUIDE FITTING IAW DWG 9754055 AND SRM 51-3-0

Part: FITTING — CRACKED (LOWER CARGO) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 280 BANANA FITTING IS CRACKED BETWEEN LONG 31R-32R. REMOVED AND REPLACED FITTING IAW DWG 3755827 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 781 LOWER HORIZONTAL ANGLE AT LBL 60 APPROX IS CRACKED OVER WING BOX. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG.3643111 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (RT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, NR 3 MAIN FUEL TANK HAS STRINGER 51 END FITTINGS CRACKED AT XRS 74. REMOVED AND REPLACED FITTINGS IAW DWG. 3704841 AND SRM. 51-1-20D, 51-3-0

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 STATION 1120 FRAME CAP IS CORRODED BEYOND LIMITS AT LONG 36. REMOVED AND REPLACED FRAME CAP IAW DWG 5764343 AND REPAIRED FRAME IAW DWG DC8-53A-010, EO DC8-5310-11728-A, SRM 51-1-20D, 51-1-21

Part: FITTING — CRACKED (LEFT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, NR 2 MAIN TANK STRINGER 51 AT XRS 50 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4614391 AND SRM 51-1-20D.

Part: FITTING — CRACKED (RT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 NR 4 ALT TANK HAS STRINGER 59 FITTING CRACKED AT XRS 428 AND XRS 440 REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 5644973 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 1160 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 1140 LONGERON TO FRAME ATTACH FITTING IS CRACKED AT LONG 35R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 STATION 1152 OB OF LONG 35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 AFT SIDE STATION 1766 J-FRAME TO LONGERON LONG 19R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5773844 AND SRM 51-3-0.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 STATION 1766 AFT SIDE LONG 17R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5773844 AND SRM. 51-3-0.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 RINGER DOUBLER IS CORRODED BEYOND LIMITS ON LEFT MLG, WHEEL WELL UPPER PRESSURE WEB AT STATION 960-980 LBL 65. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-7-1 FIG 10 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (MLG WW) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 920 LONGERON 24L IS CRACKED ABOVE GEAR UPLATCH. NDT VERIFIED CRACKS TERMINATED AT FASTENER HOLES. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, AFT OF STATION 1766 J-FRAME TO LONG. 13L SHEAR TIE IS CRACKED REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG.5773844 AND SRM. 51-1-20D.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 KEEL BEAM WEB ATTACH ANGLE IS CRACKED AT STATION 857 RBL 6. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5613920 AND SRM 51-1-20D, 51-3-0.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, NR 1 PYLON UPPER AFT END HAS PN 57567901 CRACKED AT YN 384.942. REMOVED CRACK FROM FITTING BY REMOVING INTEGRAL STIFFNER IAW UPS. ENGINEERING FILE NR DC8-54-20038 AND SAA SK 730-344.

Part: FRAME — CORRODED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 1580 FRAME IS CORRODED BEYOND LIMITS RIGHT SIDE AT CUSP LEVEL. REMOVED FRAME SECTION, FABRICATED FRAME SECTION AND REPAIR ANGLES AND INSTALLED IAW SRM 53-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 160-1180 INTERCOSTAL ABOVE C-PIT DOOR IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753770 AND SRM 51-1-21, 51-1-21A.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 L-1 DOOR LOWER AFT CORNER HAS CRACKED L-ANGLE. REMOVED, FABRICATED AND REPLACED L-ANGLE IAW SRM 52-3-1 FIG 1, AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 850 LONGERON 2L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, M/M 20-14-00.

Part: RIB — CRACKED (LT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 LT WING LE UPPER RIB IS CRACKED AT XFS 641. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2

Part: FITTING — CRACKED (FUSLEAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 685 LONGERON 2 RT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D, 51-1-21.

Part: CUSP WEB — CRACKED (MAIN CABIN) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 1265 LONGERON 21L (CUSP) IS CRACKED. REMOVED CUSP SECTION BETWEEN STATION 1280 TO 1380, FABRICATED AND INSTALLED CUSP SECTION AND SPLICES IAW SRM 53-2-5 FIG 15A.

Part: RIB — CRACKED (LT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 358. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 603. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (R-1 DOOR) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, R-1 DOOR INTERIOR SIDE LOWER PAN AFT INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5615762 AND SRM 52-2-0 FIG 6.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, LT STATION 781 FITTING IS CRACKED AT LONG 17L. REMOVED, FABRICATED AND REPLACED FITTING IAW UPS ENGINEERING FILE NUMBER DC8-53-20416A, AND SAA SK 730-108-A AND DWG 5641007.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 850 LONGERON 5R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, AND M/M 20-14-00.

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14R. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5895045 AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 STATION 680 AFT SIDE LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D & 51-3-0.

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14L. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5895045 AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, AFT SIDE OF STATION 680 FRAME LONG. 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3779762 AND SRM. 51-1-20D

Part: FITTING — CRACKED (MAIN CABIN) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1 STATION 680 END FITTING FWD. SIDE OF FRAME IS CRACKED AT LONG. 9L. REMOVED AND REPLACED FITTING IAW DWG. 3775762 AND SRM. 51-1-20D

Part: FITTING — CRACKED (FRAME TO LONG) · airframe 71,966 hrs · 48,533 cycles

INSPECTION TYPE: C1, STATION 781 LONGERON TO FRAME ATTACH FITTING IS CRACKED AT LONG 18L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS ON. PACK REPLACED PART.

Part: SLIDE — DEPLOYED (PAX DOOR)

INSPECTION TYPE: B, WHILE ADJUSTING SIGHT GAUGE ON L1, EVAC-SLIDE INADVERTENTLY DEPLOYED SLIDE. ALL PROCEDURES WHILE ADJUSTING WERE DONE IAW MM 25-60-04. SLIDE WAS PUNCTURED ON CREW ENTRY STAIRS WHILE INFLATING. REMOVED EVAC-SLIDE FROM ACFT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 EMERGENCY EXIT LIGHTS FAILED OPS CHECK. RANG OUT WIRING PER WDM 33-50-01, WIRING CHECKED OUT GOOD. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, AND OPS CHECKED GOOD IAW DC8 M/M 33-50-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 FITTING IN TORQUE BOX AT STA 1150 IS CORRODED BEYOND LIMITS AT LONG 31R. REMOVED AND REPLACED FITTING IAW DWG 3754914, AND SRM 51-3-0.

Part: SKIN — CRACKED (RT WING) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2, RIGHT WING CENTER LEADING EDGE LOWER SKIN IS CRACKED INBOARD OF XW408. STOP-DRILLED CRACKED, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087 FIG 1 APPX C.

Part: SPAR CAP — DAMAGED (RT WING) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 RIGHT WING REAR SPAR UPPER CAP HAS ELONGATED HOLES BETWEEN XRS 456 AND XA 500. OVERSIZED HOLES, NDT VERIFIED NO CRACKS AT HOLES, FABRICATED AND INSTALLED BUSHINGS IAW 8110-3 APPROVED SAA SK 730-143, AND UPS ENGINEERING FILE NUMBER DC8-57-20051.

Part: WEB — CORRODED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 CORROSION BETWEEN LONGERON AND FRAME ATTACH PLATE AFT OF TORQUE BOX STA 1160 AT LONG 35R TO 33R WEB IS CORRODED BEYOND LIMITS. REMOVED EXISTING DOUBLER, CUT OUT CORRODED SECTION OF WEB, FABRICATED AND INSTALLED WEB SECTION, SPLICE PLATES, FRAME REPAIR ANGLES, CLIPS, INTERCOSTAL, AND UPPER TORQUE BOX WEB IAW DWG 9754949, 3753772, 9754947, 5753893, AND SRM 53-2-0 FIG 1B, DC8-5310-11728-A APPX A.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STA 540 SHEAR TIE IS CRACKED BETWEEN LONG 31L AND 32L. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-2-0 FIG 2B.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STA 540 SHEAR TIE IS CRACKED BETWEEN LONG 35R AND 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-2-0 FIG 2B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STATION 940 LONGERON 24L IS CRACKED. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-2 FIG 5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STA 90 INTERCOSTAL IS CRACKED AT LONG 33L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5750726 AND SRM 51-1-21, 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STA 1400 FRAME IS CRACKED BELOW LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, AND FILLER IAW DC8-5310-11728-A, AND DWG DC8-53A-011.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STA 90 INTERCOSTAL IS CRACKED AT LONG 33R. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 REMOVE EXISTING REPAIR DOUBLER ON L-1 DOOR LOWER FWD TO AFT CORNER TO EVALUATE DAMAGE, INTERNAL DOUBLER CRACKED AT LONG 21L, AND SKIN DAMAGED STA 31-70 BETWEEN LONG 21L TO 14L. REMOVED EXISTING REPAIR, CUTOUT DAMAGE AREAS AND SKIN SEGMENT BETWEEN STA 31 TO 70 BETWEEN LONG 21L TO 14L, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLERS, TRIPLERS, FILLERS, AND SKIN SEGMENT IAW 8110-3 APPROVED SAA SK730-509, EO DC8-5330-17087-A, SRM 53-2-0 FIG 15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 STA 1660 LONG 11R IS CRACKED. STOP DRILLED CRACK NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED REPAIR STRAP ALONG WITH SKIN DOUBLER AND TRIPLER AND FILLER.

Part: SKIN — CRACKED (LT WING) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 360.25. STOP-DRILLED CRACK, NDT VERIFIED STOPDRILLS TERMINATES CRACK. INSTALLED CONICAL WASHERS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-7767-A AND SRM 51-1-26.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON R-1 DOOR UPPER FWD CORNER AND REP AIR PER DC8 SRM 53-2-0 FIG 14, SKIN IS CRACKED STA 160 LONG 10R. REMOVED STEEL DOUBLER, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED DOUBLER,TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 14 REF TEMP REVISION 53-109.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2, NR 1 PYLON OUTBOARD SIDE SKIN IS CRACKED AT YN 343. NDT VERIFIED CRACK TERMINATES AT END OF PART. FABRICATED AND INSTALLED DOUBLER IAW DC8 70 SERIES SRM 54-2-0 FIG 6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS DOUBLER ON THE R2 DOOR UPPER AFT CORNER AND REPAIR FUSELAGE SKIN CRACKED AT STA 1660 LONG 10R AT UPPER CORNER. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2, REMOVE STEEL DOUBLER ON L-1 DOOR UPPER AFT CORNER AND REPAIR IAW SRM 53-2-0 FIG 15. REMOVED EXISTING DOUBLER, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLERS ON L2 DOOR LOWER FWD CORNER AND REPAIR IAW SRM 53-2-0 FIG 18, STA 1620 LONG 21L SKIN IS CRACKED. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, FILLER, AND REPAIR BUSHINGS IAW SRM 53-2-0 FIG 18 AND EO DC8-5330-17068-A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,117 hrs · 47,866 cycles

INSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON L1 DOOR UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 15 AT STA 25 LONG 10L AREA. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS BATTERY PACK INOP. EMERGENCY LIGHTS BATTERY PACK REMOVED AND REPLACED AS PER MM 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER M/M 33-50-01.

Part: CONTAINER — DAMAGED (CABIN)

INSPECTION TYPE:PFLT REF M231085 SLIDE ASSY OUT OF DOOR, BAR HOLDER BROKEN OFF OF CONTAINER. REMOVED AND REPLACED SLIDE EVAC CONTAINER. REINSTALLED SAME SLIDE ASSY INTO CONTAINER PER MM 25-60-01 3B, P/N ON & OFF-5750113-505, S/N ON-TAG645594A. OK FOR SERVICE.

Part: GENERATOR — SMOKE (NR 2)

DURING TAXI OUT NR 2 BUS POWER FAIL LIGHT ILLUMINATED NR 2 GEN UNPAR'LD LIGHT ILLUMINATED AND LEFT EMERG AC BUS POWER FAIL LIGHT ILLUMINATED ATTEMPTED TO PERFORM BUS POWER FAIL LIGHT ILL CHECKLIST COCKPIT SMOKE CONTINUED, SECURED 1-4 GENS MOVED A/C TO ISOLATED AREA ACCOMP EMERGENCY EVAC PROCEDURES DUE TO SMOKE IN COCKPIT. INSPECTED RELAYS AND WIRES ON NR 2 GENERATOR SYSTEM IN FLIGHT DECK AND GALLEY AREA. RAN BOTH PACKS AND RECIRC FAN WITH NO EVIDENCE OF SMOKE NOTED. NR 2 BUS PWR FAIL LIGHT, REPLACED NR 2 GENERATOR RELAY BUT NO HELP, DEFERRED NR 2 GENERATOR SYSTEM PER MEL 24-1-1.

Part: RELAY — FAILED (CABIN)

INSPECTION TYPE:ASE DURING MX INSPECTION FOUND EMERGENCY LIGHTS FAILING OPERATIONAL TEST. CAUSE FOUND TO BE A STICKING EMERGENCY LIGHT CONTROL RELAY. REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY AND RELAY UNIT

Part: RELAY — FAILED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS FAILED OPS CHECK, FOUND EMERGENCY LIGHT CONT RELAY STICKING. R&R EMERGENCY LIGHTING BATTERY AND RELAY UNIT AND PERFORMED OPS CK PER MM 33-50-01 PARA 2 & 4 OPS CKS NORMAL.

Part: A/C PACK — SMOKE (LEFT)

LT PACK TRIP LIGHT CAME ON IN FLIGHT FOLLOWED BY A STRONG SMELL OF ELECTRICAL SMOKE. SMOKE SMELL WENT AWAY AFTER PERFORMING SMOKE OF UNKNOWN ORIGIN CHECKLIST. PERFORMED OPERATIONAL CHECK PER MM 21-60-00 ON TEMP CONTROL ON LEFT PACK SYSTEM CHECK NORMAL NO LEAKS OR SMOKE IN COCKPIT

Part: SEPARATOR — MALFUNCTIONED (AC BAY)

INSPECTION TYPE:IN FUMES IN C/P DURING ENTIRE FLIGHT, SEEM TO BE COMING FROM EITHER PACK. ON GROUND FOUND R PACK EMITTING ODOR. DER R PACK PER MEL 21-38-1. PERF MAINTENANCE PROCEDURES. M 210419 ASSIGNED PLACARDS INSTALLED. REMOVED AND REPLACED RT WATER SEPARATOR IAW 21-55-03. PERFORMED ADJUSTMENT AND TEST IAW 21-55-00. ALL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT SAFETY CK. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK GOOD.

Part: BELLCRANK — DAMAGED (NOSE GEAR DOOR)

INSPECTION TYPE:N/A DURING DESCENT AT 340 KIAS, LOUD NOISE FROM NOSE WHEEL AREA. ALSO A CCOMPANIED BY MODERATE AIRFRAME VIBRATION. BOTH WENT AWAY WHEN GEAR CAME DOWN. ON BASE LEG, ANOTHER LOUD NOISE (THUD). REPLACED FWD NOSE GEAR DOOR TORQUE TUBE BELLCRANK.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT ELEVATOR UPPER SKIN IS CRACKED AT XE 190. REPAIRED SKIN IAW SRM 55-2-0 FIG 2.

Part: FRAME — CORRODED (AFT CABIN) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1746 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG 29L AND 30L. REPAIRED FRAME IAW EO DC8-5310-11728-A AND DC8-53A-010.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 390 LONG 35R SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3754026 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER SPLICE PAN IS CRACKED AT XS 250. REMOVED, FABRICATED AND REPLACED SPLICE PAN IAW DWG 5769859 AND SRM 51-1-21.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT STA 380 LONG 36. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 730-429.

Part: SKIN — GOUGED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 520 AT LONG 31R EXTERIOR IS GOUGED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 730-037.

Part: ANGLE — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 702.85 SHEAR TIE FITTING IS CRACKED BETWEEN LONG 35L AND 36. REMOVED AND REPLACED FITTING IAW DWG 3753757 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 660 SHEAR TIE BETWEEN LONG 34L-34R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED IAW DWG 5616509 AND SRM 51-1-21.

Part: RIB — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 366.5 AND 372.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: ANGLE — CRACKED (LT WING) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769589 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (LT WING) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 250.089. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-1-20D, 51-1-21.

Part: PAN — CORRODED (ACCESS BAY DOOR) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, FWD ACCY COMP DOOR PAN HAS AREA CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 FIG 23.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 70 LONG 35L IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 FIG 10.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 341. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (A/C BAY) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 70 LONG 35L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4610355 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XS497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — GOUGED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E RIB XS 510 IS GOUGED BEYOND LIMITS. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, KEEL BEAM IS CORRODED BEYOND LIMITS AT STA 660 - 680 AT LONG 36. REPAIRED IAW 8110-3 APPROVED DH SK 730-934.

Part: RIB — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 647.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 280 LONG 34R TORQUE BOX SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754055 AND SRM 51-3-0.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 556.250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 304. REMOVED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING LOWER INTERNAL DOUBLER IS CRACKED AT XFS 250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW 5769699 AND SRM 51-1- 21.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 341.5. REPAIRED IAW 8110-3 APPROVED DH SK 730-808.

Part: RIB — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED BEYOND LIMITS AT XS 503.789. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769859 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 335.250. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769530 AND SRM 51-1-20D.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E RIB IS CRACKED AT XFS141.25. REPAIRED RIB IAW SRM 55-2-0 FIG 2.

Part: RIB — CRACKED (HORIZONAL STAB) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT HORIZONTAL STAB L/E LOWER RIB IS CRACKED AT XFS 116.25. REPAIRED IAW SRM 55-2-0 FIG 2.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123 STA -23 BL 0 FLOORBEAM UPPER FLANGE IS CRACKED. REPAIRED FLOORBEAM IAW SRM 53-2-0 FIG 1B.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT XFS 172.5. REPAIRED IAW SRM 55-2-0 FIG 2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 620 - 640 LONG 35L-36 INTERNAL SKIN IS CORRODED BEYOND LIMITS. REPAIRED IAW 8110-3 APPROVED DH SK 730-651.

Part: INTERCOSTAL — CRACKED (COCKPIT) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA -80 LBL 59 VERTICAL INTERCOSTAL IS CRACKED. REPAIRED INTERCOSTAL IAW SRM 53-2-0 FIG 1B.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 640 SHEAR TIE IS CORRODED BEYOND LIMITS BETWEEN LONG 34L AND 34R. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5616509 AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1746 AT RBL 16 FLOORBEAM INTERCOSTAL IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 FIG 1B AND 1D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1340 LONG 11L UPPER AFT CORNER OF CENTER LEFT SERVICE DOOR OPENING SKIN IS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 18.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1231 - 1237 LONG 35L INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 798 LBL 50 FLOORBEAM TO WING BOX LOWER ANGLE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1537 INTERCOSTAL IS CRACKED AT LONG 33L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753792 AND SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1690 LONG 26R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 723.75. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1690 LONG 28L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1520 AT LONG 27L VERTICAL FLOORBEAM SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 3610417 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 716.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 980 - 1000 LONG 23L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1560 LONG 34R IS CORRODED BEYOND LIMITS. REPAIRED LONGERON IAW SRM 53-2-0 FIG 10.

Part: FITTING — CRACKED (CABIN) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1690 LONG 26L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1160 AT LONG 27R FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D, 51-1-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 822 FLOORBEAM ATTACH FITTING IS CRACKED AT LBL 24. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4646547 AND SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 869 BL 0 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5645332 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1690 LONG 32R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324N AND SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1480 BETWEEN LONG 35L AND 36 SHEAR TIE IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-0 FIG 2A.

Part: FITTING — CRACKED (CABIN) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1690 LONG 34R END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1219 LONG 17R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1287 LONG 23R FRAME TO CUSP FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755584 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 680 A-FRAME FITTING IS CRACKED BETWEEN LONG 22L AND 23L. REMOVED AND REPLACED FITTING IAW DWG 3642983 AND SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 1690 LONG 30L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 798 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751639 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 660 -680 LONG 11L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 850 LONG 7L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 280 AT LONG 27R FITTING IN TORQUE BOX BELOW VERTICAL SUPPORT IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 850 LONG 9L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D.

Part: SKIN — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING CENTER L/E SKIN IS CRACKED AT XW 257. REPAIRED IAW SRM 57-2-1 FIG 2H.

Part: SKIN — CRACKED (LT WING LE) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, LEFT WING AUX TANK LOWER SKIN IS CRACKED AT XFS 138.75. REPAIRED IAW SRM 57-2-0 FIG 2A.

Part: FRAME — CRACKED (A/C BAY) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24R. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FRAME — CRACKED (A/C BAY) · airframe 69,919 hrs · 46,983 cycles

INSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24L. REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FIRE WARNING — ACTIVATED (NR 4 ENGINE)

INSPECTION TYPE:N/A, NR 4 FIRE WARNING CAME ON AFTER SHUTTING DOWN ENGINES. RAN PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. LIGHT WENT OUT AFTER 30 SECONDS AND TESTED NORMAL. REMOVED AND REPLACED FIRE BOTTLE ON RIGHT WING OUTBOARD POSITION PER 26-20-01. INSPECTED MEC FOR RIGGING OF FUEL SHUT OFF, POWER LEVER, VSV, VBV, NO DEFECTS NOTED. CHECK OF FIRE SENSING ELEMENTS REF LP 06 9874/2.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE-C, RT L/E BETWEEN ENG NR 3 AND NR 4 HAS CRACKED RIB AFT OF O/B SLOT ACTUATOR BOTTOM SIDE. REPAIRED IAW SRM 57-2-0.

Part: LONGERON — CORRODED (BS 85-90)

INSPECTION TYPE-C, LONGERON 29R BETWEEN FS 85 AND 90 CORROSION REMOVAL IS BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 FIG 10.

Part: RIB — CRACKED (WS 225)

INSPECTION TYPE-C, RIB CRACKED ON RT WING L/E AT APPROX STA XS 225 NR 3 ENG STUB WING. REPAIRED IAW SRM 57-3-1.

Part: LONGERON — CRACKED (BS 180)

INSPECTION TYPE-C, LONG 28R O/B FLANGE CRACKED AT FRAME 180 ATTACH BOLT. REPAIRED IAW SRM 53-4-1.

Part: INTERCOSTAL — CRACKED (BS 360-380)

INSPECTION TYPE-C, INTERCOSTAL CRACKED BTWN FS 360 TO 380 AT LONG-33R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 51-1-20D AND DWG 5750726.

Part: SHEAR TIE — CRACKED (BS 1200)

INSPECTION TYPE-C, SHEAR TIE FITTING CRACKED AT FS 1200 BTWN LONG 33R AND 34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 250.089)

INSPECTION TYPE-C, VERT ANGLE CRACKED BTWN RIBS ON RT WING L/E AT STA XS 250.089. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 9752397.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-C, FS 1040 TO 1060 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: FITTING — CRACKED (BS 1225 S)

INSPECTION TYPE-C, FS 1225 BTWN STR 30R TO 33R SHEAR TIE FITTING IS CRACKED IN 2 PLCS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3755847.

Part: FITTING — CRACKED (BS 1200)

INSPECTION TYPE-C, FS 1200 AT STR 27L DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3753776.

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE-C, FS 1180 AT STR 27L DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 9753776.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING T/E RIB CRACKED AT NR 5 SPOILER NR 2 HINGE, (INBD RIB). REPAIRED IAW SRM 57-2-0.

Part: SHEAR TIE — CRACKED (BS 1160)

INSPECTION TYPE-C, FS 1160 AT STR 33R SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 1340-1360)

INSPECTION TYPE-C, FS 1340 TO 1360 STR 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED JUST ABOVE PNEUMATIC DUCT AT STA XOLDI 6.225. REPAIRED IAW SRM 57-2-0.

Part: CARGO TRACK — CRACKED (BS 1320)

INSPECTION TYPE-C, FS 1320 ABOVE STR 33L CARGO TRACK HAS HEAVY CORROSION AND IS CRACKED AT FS 1260. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5759223.

Part: RIB — CRACKED (WS 710)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 710 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CORRODED (BS 20)

INSPECTION TYPE-C, HEAVY CORROSION ON RT CUSP TO FRAME FITTING FS 20. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1600)

INSPECTION TYPE-C, FRAME CRACKED FS 1600 L-21L FWD OF FITTING. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CRACKED (WS I6.225)

INSPECTION TYPE-C, RT WING L/E SKIN ON TOP AT STA XOLDI 6.225 HAS 2 CRACKS AROUND RIVETS 8 FWD OF FRONT SPAR. REPAIRED IAW SRM ADDN DC8-5720-4087.

Part: RIB — CRACKED (WS 766.250)

INSPECTION TYPE-C, RT WING L/E AT XFS 766.250 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 747.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 747.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 697.5)

INSPECTION TYPE-C, RT WING L/E AT STA XFS 697.5 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: LONGERON — CRACKED (BS 978)

INSPECTION TYPE-C, LONGERON 24R CRACKED IN HORIZONTAL FLANGE AT AFT END FS 978. REPAIRED IAW SRM 53-2-2.

Part: SKIN — CRACKED (WS 304-310)

INSPECTION TYPE-C, RT WING L/E SKIN ON TOP AT FRONT SPAR, BTWN STA XFS 304.00 TO 310.25 HAS 3 CRACKS AROUND FASTENERS. REPAIRED IAW SRM 57-2-1 AND 57-3-1.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING T/E AT FLAP STA 3.00 THE I/B RIB IS CRACKED AT MID SPAN. REPAIRED IAW SRM ADDN DC8-5720-6998.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE-C, LT WING UPPER SKIN CRACKED JUST I/B OF STA XRS 74 STR 11. REPAIRED IAW SRM 57-2-1.

Part: GUSSET — CRACKED (RT WING)

INSPECTION TYPE-C, RT FLAP AT SPLIT UNDER SURFBOARD LWR RIB SUPPORT GUSSET IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT GUSSET IAW SRM 51-1-21 AND DWG 5642970.

Part: SKIN — CRACKED (WS 193-250)

INSPECTION TYPE-C, RT WING L/E STUB WING OVER NR 3 PYLON ON TOP HAS MANY CRACKS DUE TO CORROSION FROM STA XFS 193.00 TO 250.089. REPAIRED IAW SRM ADDN DC8-5720-4087-B.

Part: SKIN — CRACKED (WS 74.5)

INSPECTION TYPE-C, RT WING UPPER SURFACE AT STA XRS 74.5 AND STR 12 THE EXTERIOR SKIN IS CRACKED. REPAIRED IAW SRM 57-2-1.

Part: DOUBLER — CORRODED (FUSELAGE)

CORROSION ON INNER DOUBLER BELOW EXT AIR CONDITIONING RECEPTACLE ON RT SIDE ABOVE FWD E/E COMP. REMOVED CORROSION ON INNER DOUBLER. ACCOMPLISHED EO DC8-5330-8942-D INTERM REPAIR.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-C, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMER EXIT LIGHT BATTERY PACK, CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS VERY DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKS GOOD.

Part: STRINGER — CRACKED (WS 508)

INSPECTION TYPE: C. RT WING STRINGER 53 JUST INBOARD OF CANT STA 508 IS CRACKED. REPAIRED STRINGER PER SRM 57-2-2, SRM 57-2-0 AND UPS EO.

Part: FITTING — CRACKED (WS S98)

INSPECTION TYPE: C. LT WING STA XRS98 FLAP CARRIAGE FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D.

Part: FRAME — CORROSION (BS 1020)

INSPECTION TYPE: C. HEAVY CORROSION ON BELT FRAME FS 1020 LONGERONS 35R-36. REPLACED BELT FRAME SECTION PER SRM 51-1-21.

Part: DOUBLER — CRACKED (NR 1 PYLON)

INSPECTION TYPE: C. MOLD LINE DOUBLER HAS APPROX A 1.50 INCH LONG CRACK AT FWD EDGE INSIDE NR 1 PYLON FOOTSTOOL WS XFS539. REPAIRED PER DOUGLAS DRAWING 5803955 AND UPS EO.

Part: SKIN — CRACKED (LT WING LE)

INSPECTION TYPE-C, ADJACENT SKIN OUTBOARD OF LT WING INBOARD SLOT IS CRACKED. REPLACED SKIN PANEL SECTION PER SRM 51-1-4 AND SRM 51-3-0.

Part: KEEL BEAM — CRACKED (BS 890)

INSPECTION TYPE-C, CRACK AND HEAVY CORROSION INSIDE KEEL BEAM PANEL APPROX FS 890 RT SIDE WHEEL WELL. REPAIRED PANEL SECTION PER SRM 53-2-0.

Part: FITTING — CRACKED (WS 98)

INSPECTION TYPE: C. LT WING FLAP STA XRS98 INBOARD CARRIAGE FITTING HAS 12 INCH LONG CRACK. REPLACED FITTING PER SRM 51-3-0 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 879)

INSPECTION TYPE: C. RT TRAPEZOID FITTING CRACKED AT HOLD-ON FWD SIDE JUST BELOW LONGERON 24R. REPAIRED FITTING PER DAC DRAWING NR 5750776.

Part: TAB — DELAMINATED (RT AILERON)

INSPECTION TYPE: C. RT AILERON CONTROL TAB DELAMINATED. REPLACED TAB ASSY PER MM 27-11-04.

Part: SPOILER — DELAMINATED (NR 1 SPOILER)

INSPECTION TYPE-C, LT NR 1 SPOILER DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: SKIN — CRACKED (RT WING)

WING SKIN CRACKED ON LOWER SURFACE INBOARD OF NR 4 PYLON JUST OUTBOARD OF NR 4 ALT AFT SUMP. CRACKED VERIFIED BY EDDY CURRENT INSPECTION. TRANSFERRED TO DMI D 115401. TRANSFERRED TO N/R 449303.

Part: FITTING — CRACKED (PAX DOOR)

DURING B-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR DRAGGING. DURING TROUBLESHOOTING, FOUND LOWER FUSELAGE MOUNTED FITTING ASSEMBLY FOR TORQUE TUBE CRACKED FITTING. REPLACEMENT C/W.

Part: ENGINE — FLAME-OUT (NR 1)

INSPECTION, NR 1 ENGINE FLAMED OUT IN FLIGHT. NR 1 ENGINE OVER PRESSURE LIGHT REMAIN'S ILLUMINATED. PERFORMED TROUBLESHOOTING PROCEDURES PER MM 71-00-00 PAGE 153-169, NO ABNORMALITIES NOTED.

Part: AILERON LIGHT — ILLUMINATED (COCKPIT)

CREW REPORTED, AILERON CONTROL MANUAL LIGHT ILLUMINATED IN FLIGHT, NO LOSS OF HYD CHECKLIST COMPLETED AND LANDING UNEVENTFUL. INSPECTED AIL CABLES, PWR PACKS AND ALL ASSOCIATED SYSTEMS AND NO VISUAL DEFECTS NOTED. AIL HYD PWR SYSTEMS CHECKS NORMAL PER MM 27-10-00.

Part: SKIN — CRACKED (NR 3 CARGO DOOR)

WHILE ON GROUND, MAINTENANCE FOUND NR 3 PIT DOOR SKIN CRACKED UPPER AFT CORNER. REMOVED AND REPLACED BROKEN DOUBLER PER SRM 52-2-0.

Part: FITTING — CORROSION (FS 290)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING, FS 290, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D.

Part: SPLICE FITTING — CRACKED (FS 920)

WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 24L SPLICE FITTING AT FS 920. INSTALLED REPAIR PER UPS EO DC8-5310-6968A.

Part: FITTING — CORRODED (FS 305)

WHILE IN S2-CHECK, MAINTENANCE FOUND CORROSION ON STA 305 FITTING, BETWEEN LONG 33A AND 33B RT. REPLACED PER SRM 51-1-20D.

Part: CASTING — CORROSION (FS 290)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON T-HOOK CASTING FS 290, LONGERON 33A. INSTALLED REPAIR PER SRM 51-1-20D.

Part: CASTING — CORROSION (FS 320)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON T-HOOK CASTING FS 320, LONGERON 33A. INSTALLED REPAIR PER SRM 51-1-20D.

Part: SKIN — CORROSION (FS 1490-1690)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BELLY SKIN FS 1490 TO 1690, LONGERON 31L TO 31R. REPLACED BELLY SKIN PER DOUGLAS DRAWING 5615374.

Part: FITTING — CORRODED (FS 1560)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON UPPER CUSP FITTING, LONGERON 21L, FS 1560. REPLACED FITTING PER SRM 51-1-20D.

Part: SHEAR TIE — CORROSION (FS 1060)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE FWD AND AFT SIDES, LONGERONS 36 TO 35L, FS 1060. INSTALLED REPAIR PER SRM 53-2-2.

Part: FRAME — CORROSION (FS 100)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME, FS 100, BETWEEN LONGERONS 36R AND 34R. INSTALLED REPAIR PER SRM 53-2-0.

Part: SPLICE — CORRODED (FS 1270)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON SPLICE, FS 1270, LONG 34L, ON BOTTOM SIDE. REPLACED SPLICE PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 100)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON END FITTING, LONGERON 36, FS 100. REPLACED FITTING PER SRM 51-1-20D.

Part: VANE ASSY — DELAMINATED (NR 6 TE FLAP)

WHILE IN S2-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING NR 6 FLAP VANE ON AFT TRAILING EDGE. REPLACED VANE ASSY PER MM 27-51-14.

Part: FITTING — CORRODED (FS 322)

WHILE IN S2-CHECK, MAINTENANCE FOUND CORROSION ON STA 322 FITTING, BETWEEN LONG 33A AND 33B RT. REPLACED PER SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 445-455)

WHILE IN S2-CHECK, MAINTENANCE FOUND CORROSION ON SPLICE AND FINGER DOUBLERS AT FS 445 TO 455, LONGERON 34L TO 35R. REPLACED DOUBLERS PER DOUGLAS DRAWING 5755271-7.

Part: FITTING — CRACKED (FS 850-857)

WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 4R END FITTING AT FS 850 TO 857. REPLACED PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1179)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON AT FITTING, FS 1179, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0.

Part: LONGERON — CORRODED (FS 70-100)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 31R, FS 70 TO 100. INSTALLED REPAIRED PER UPS EO DC8-5310-6898A.

Part: SKIN — CRACKED (WS 426.76)

WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E LWR SKIN AND DOUBLER, XFS 426.76. INSTALLED REPAIR PER UPS EO FILE NR DC8-57-0547.

Part: FRAME — CRACKED (FS 52)

WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK ON FUSE FRAME AT FS 52 RT SIDE, 6 INCHES ABOVE FLIGHT DECK SUB FLOOR, APPROX 1 INCH LONG. INSTALLED REPAIR PER UPS EO FILE DC8-5310-6967A.

Part: DOUBLER — CORROSION (FS 53-32)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON FLIGHT DECK PRESSURE DOUBLER, LT SIDE, JOINING WITH FUSELAGE, FS -53 TO FS -32. REPLACED DOUBLER PER SRM 51-1-21.

Part: SKIN — CORROSION (FS 1740-1766)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN, FS 1766, LONGERON 34L AND FS 1740 TO 1766, LONGERON 28L TO 30L. REPLACED BELLY SKIN PER DOUGLAS DRAWING 5649329.

Part: FITTING — CORROSION (FS 1535-1542)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON FITTING LONGERON 33, AT FS 1535 TO 1542. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORROSION (FS 1650)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 31R, FS 1650. INSTALLED REPAIR PER UPS EO DC8-5310-6977A.

Part: SPLICE — CRACKED (FS 420-440)

WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK AND CORROSION ON LONGERON 36 SPLICE FITTING, FS 420 TO 440. REPLACED FITTNG PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 299)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING, FS 299, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D.

Part: LONGERON — CORROSION (FS 280-360)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 33L-A, FS 280 TO 360, AND END FITTING, FS 360.

Part: SPLICE — CORROSION (FS 1350)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON SPLICE, FS 1350, LONGERON 31L. REPLACED SPLICE PER SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 1540)

WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK ON ATTACH ANGLE FS 1540, LONGERON 33R. REPLACED ANGLE PER SRM 51-1-21D.

Part: CARGO TRACK — CORROSION (FS 1310-1410)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON CARGO TRACK AROUND FASTENER HOLES, FS 1310 TO 1410, LT. INSTALLED REPAIR PER SRM 53-1-0.

Part: RIB — CRACKED (RT WING)

WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E UPPER RIBS, 5 EA AT STATIONS XFS 884, 778, 766, 754, 748. INSTALLED REPAIR PER SRM 57-2-2.

Part: CARGO TRACK — CORROSION (FS 980-1070)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON CARGO TRACK AROUND FASTENER HOLES, FS 980 TO 1070, LT. INSTALLED REPAIR PER SRM 53-2-0.

Part: LONGERON — CRACKED (FS 1742)

WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 16L AT FS 1742. INSTALLED REPAIR PER SRM 53-2-2.

Part: FITTING — CRACKED (FS 1870)

WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 36R END FITTING, FS 1870. REPLACED PER SRM 51-1-20D.

Part: SKIN — CORRODED (FS 80-100)

WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON INNER SKIN BETWEEN LONGERONS 30L AND 32L, AT FS 1746. REPLACED SKIN PER DOUGLAS DRAWING NR 5649329.

Part: DOUBLER — CORRODED (FS 12-8)

DURING 'S2' CHECK, MAINTENANCE FOUND FLIGHT DECK FASTENERS SHEARED DUE TO CORROSION ON DOUBLER AT FS 12 TO 8, L/T O/B SIDE. REPLACED DOUBLER PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1760)

DURING 'S2' CHECK, MAINTENANCE FOUND LONGERON END FITTING 32R CORRODED AT FS 1760. REPLACED FITTING PER SRM 51-1-21, 51-1-20D.

Part: DOUBLER — CORRODED (FS 70-90)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON FINGER DOUBLER AT FS 70 TO 90, LONGERON 21R. REPLACED DOUBLER PER SRM 51-1-21.

Part: DOUBLER — CORRODED (FS 1360)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER AT FS 1360, LONGERON 25L TO 26L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-2-1.

Part: DOUBLER — CORRODED (FS 1720-1760)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON SKIN DOUBLER AT FS 1720 TO 1760, LONGERON 28L. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1, 51-1-21.

Part: FITTING — CORRODED (AFT SERVICE DOOR)

DURING 'S2' CHECK, MAINTENANCE FOUND AFT SERVICE DOOR CORRODED FITTING AT TOP FWD HINGE. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 1746)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32L AT FS 1746. REPLACED LONGERON PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1350)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF LONGERON 25L SPLICE FITTING AT FS 1350. REPLACED FITTING PER SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 70-80)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON JACK PAD INNER DOUBLER AT FS 70 TO 80, LONGERON 34L TO 34R. REPLACED DOUBLER PER SRM 51-1-20D.

Part: DOUBLER — CORRODED (WS 373)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER AT STA XFS 373, RT WING LEADING EDGE LOWER SIDE. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-57-0546.

Part: SKIN — CORRODED (VERTICAL STAB)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON 4 MOUNTING HOLES OF VERTICAL STABILIZER ANTENNA ON STABILIZER SKIN. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0.

Part: SKIN — CORRODED (FS 1350)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE INNER DOUBLER AND SKIN AT FS 1350, LONGERONS 26 TO 27L. REPAIRED PER SRM 51-1-8, 53-2-1.

Part: SKIN — CORRODED (FS 1148)

DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN AT FS 1148, LONGERON 33R AND FS 1280 TO 1300, LONGERONS 34 TO 35L. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5330-2827D.