N805UP
Registered owner: WHEELS UP PARTNERS LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CIRCADIAN AVIATION LLC (O2GA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
INSPECTION TYPE:N/A ON CLIMB WITH CABIN PRESSURE DIFFERENTIAL BETWEEN 1.5 - 3.5 PSI THERE WAS A LOUD AIR LEAK FROM CABIN DOOR AREA. NOISE LEVEL WAS SUCH THAT COCKPIT COMMUNICATIONS WERE LIMITED. ACCOMPLISHED AIR TURNBACK. REMOVED LOOSE SEALANT AT MAIN CARGO DOOR UPPER FORWARD SEAL AREA. RESEALED AND PRESSURIZED PER MM 21-31-00-2. NO LEAKS NOTED.
CRACK IN SKIN STA 25 STRINGER 33. CORROSION FOUND. REMOVED FASTENERS & MADE 3" C/O IN SKIN AT STA 25 L34-33R PER SRM 51-01-08-0. REMOVED CORROSION PER SRM 51-01-08. REPAIR COMPLETED REF NRC 225282 & 225283. PERMANENT REPAIR AT OR BEFORE NEXT C-CHECK PER DC8-5330-30787.
INSPECTION TYPE:N/A CLIMBING THROUGH FL360 THE NR 4 ENGINE FLAMED OUT. DESCENDED TO FL220 AFTER ACCOMPLISHING THE IN FLIGHT ENGINE FLAMEOUT CHECKLIST TO ATTEMPT A RESTART. FOLLOWED THE IN FLIGHT ENGINE START CHECKLIST AND ATTEMPTED 1 RESTART. AFTER DRY MOTORING ENG FOR SEVERAL MINS OPS CHECK OF IGNITION SYS COMPLETED WITH NO FAULTS NOTED. ENG WAS RUN SEVERAL TIMES USING A AND B IGNITION SEPARATELY WITH NO FAULTS NOTED. AFTER FURTHER REVIEW OF EVENT REPORT 18355, IT WAS NOTED THE NR 4 BOOST PUMP WAS OFF. UNABLE TO DUPLICATE.
LT OVERWING EMERGENCY EXIT DOOR BINDING. LUBRICATED SEAL AND ALL MOVING PARTS IAW MM 12-80-00. OPS CHECK GOOD.
IFSD - LOSS OF OIL QTY OIL QTY JUST ABOVE ZERO, OIL PRESSURE FLUCTUATING AT 40 PSI DURING ENGINE SHUTDOWN NR 2 ENG WINDMILLING SHUTDOWN AT 15 PSI PRESS FOR ONE HOUR. REMOVED AND REPLACED STARTER REDUCER PLUG PACKING IAW DC8 IPC 80-10-00/30 ITEM 150. SERVICE NR 2 ENG STARTER IAW DC8 MM 80-10-01-2. T/S IAW CFM MM 71-00-00. PERFORMED ENG RUN AND LEAK CHECK. NO LEAKS FOUND. OK TO RETURN TO SERVICE IAW CFM MM 72-00-00.
ESCAPE SLIDE PRESSURE OUT OF GREEN BAND. DEFERRED PER MEL 52-7-4. REMOVED AND REPLACED EVACUATION SLIDE ASSY PER AMM 25-60-01-2.
SKIN CRACK AT UPPER EDGE NEAR AFT CURVE OF L1 DOOR APPROX 1/2 INCH LINEAR, PARALLEL TO T/E OF DOOR. PERFORMED INTERIM REPAIR IAW UPS EO NR DC8-5210-28486-A PARAGRAPH 6A. PERM REPAIR OR PART REPLACEMENT WITHIN 25 FLIGHT CYLES. D367801 ASSIGNED BY AMC.
INSPECTION TYPE:N/A SLIDE CAME OUT OF COVER WHEN RT GIRT BAR WAS TAKEN OUT OF LOCK DETENT. RESECURED FWD ENTRY DOOR SLIDE/CONTAINER - SLIDE CHECKS OK IAW DC8 AMM 25-60-01-2. A/C OK FOR SERVICE.
INSPECTION TYPE:N/A RESTOW ESCAPE SLIDE. RESTOWED ESCAPE SLIDE IAW MM 25-60-01-2.
INSPECTION TYPE:C2 INSPECTION FOUND PREVIOUS LWR CORNER REPAIR AT STA 1220 THE CUTOUT WAS TO CLOSE TO EDGE AND EXTENDS DOUBLER BEYOND NORMAL LENGTH. REMOVED AND REPLACED RIVETS WITH HI-LOKS AT C-3 DOOR LWR AFT CORNER IAW SAA EA 008-5330-01-A0809 REV-A, UPS EO DC8-5330-26611-B, SRO 8530019, AND FAA FORM 8100-9.
INSPECTION TYPE:C2, 6 INCH CRACK ON CUSP AT FS 1220 RIGHT SIDE FLOORBEAM FITTING L21R. REPAIRED CUSP AT STA 1133 - 1248 L21R IAW SAA EA008-5330-01-A0815, UPS RAA DC8-53-20622, SRM TR 53-180, AND FAA FORM 8100-9.
INSPECTION TYPE:C2 MAIN CARGO FLOORBEAM AT STA 280 RBL 24 CRACKED FROM EXFOLIATION CORROSION. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 280 RBL 24 IAW SRM 51-2-1 PG 8 FIG 1. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR 51-130 FIG 1 SHEET 1.
INSPECTION TYPE:C2 18TH RIB FROM BOTTOM OF RUDDER ON L/E CRACKED. STOP DRILLED CRACK ON 18TH RIB FROM BOTTOM OF L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 18TH RIB IAW SRM 55-06-00 FIG 028.
INSPECTION TYPE:C2 ATTACH ANGLE FOR VERT FIN L/E TO FUSELAGE BENT AND CRACKED RIGHT SIDE FS 1690. REMOVED ATTACH ANGLE FOR VERT FIN TO FUSELAGE AT STA 1690 IAW SRM 51-3-0. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER AT FS 1690 VERT FIN L/E TO FUSELAGE IAW SRM 53-02-05 FIG 16A.
INSPECTION TYPE:C2 12TH RIB FROM BOTTOM OF RUDDER ON L/E IS CRACKED. STOP DRILLED CRACK ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0 FIG 2 SHEET 2.
INSPECTION TYPE:C2 HFEC INSP DETECTED A CRACK ON THE C-4 (D-PIT) LWR AFT DOOR JAMB CORNER STARTING AT FASTENER GOING FWD TO EDGE OF DOOR CUTOUT. CUT OUT DAMAGED AREA AT D-PIT LWR AFT DOOR JAMB CORNER (STA 1440) IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED REPAIR TRIPLER, DOUBLER, AND FILLER AT D-PIT LWR AFT DOOR JAMB CORNER (STA 1440) IAW SRM 53-2-0 FIG 22 TR 53-188.
INSPECTION TYPE:C2 AFTER REMOVAL OF C-2 (B-PIT) SCUFF PLATE FOUND CORROSION ON FUSELAGE SKIN. REMOVED CORROSION AND FOUND SKIN TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. PROCURED AND INSTALLED REPLACEMENT SKIN FROM STA 450-610 L31L-L31R IAW SRM 51-1-20D, AND SRM 51-1-21.
INSPECTION TYPE:C2 C-PIT, AT UPPER CORNER OF CROSS SLIDE DOOR CUTOUT, FITTING HAS 4.5" CRACK STA 1200 RBL 65. REMOVED CRACK FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAW SRM 51-1-20D. INSTALLED REPLACEMENT FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAW SRM 51-1-21.
INSPECTION TYPE:C2 A/C COMPT FWD BULKHEAD CORRODED AT STA 8 BL 0. REMOVED CORRODED WEB AND CHANNEL AT STA 8 BL 0 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR WEB, AND CHANNEL AT STA 8 BL 0 IAW SRM 51-09-00 FIG 068A, AND EO DC8-5350-7876.
INSPECTION TYPE:C2 AIR CONDITIONING COMPT LONGERON CORRODED AT STA 45 L30R AND 5 INCH LONG CRACK STA 65. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS 44 CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00-0, 51-1-20D AND DWG 5644310.
INSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS32 CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5 5-02-00-0, 51-1-20D AND DWG 5644310.
INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-2 (B-PIT) DOOR JAMB UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 20. REMOVED STEEL DOUBLER FROM B-PIT DOOR JAMB UPPER FWD CORNER IAW SRM 51-01-21A. FABRICATED AND INSTALLED CORRECT TRIPLER, DOUBLER, AND FILLER AT B-PIT UPPER FWD DOOR JAMB CORNER IAW SRM 53-2-0 FIG 20 AND SRM TR 53-186.
INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-3(C-PIT) DOOR JAMB LWR FWD CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG 22 AND/OR DWG SRO8530019. REPAIRED DOOR CORNER IAW SAA EA 008-5310-01-A0755.
INSPECTION TYPE:SV TRANSFERRED FROM LOG PAGE 683072/1; REF DMI D-340854: SKIN GOUGES AT BS 120 BETWEEN L16L - L17L. REPAIRED FUSELAGE SKIN AT STA 120, L16L - 17L IAW SAA SK 008-5302- 01-A0556, UPS RAA DC8-53-20603, BAC SRID 1-264826789, AND FAA FORM 8100-9.
INSPECTION TYPE:N/A ON SHUTDOWN EMERGENCY EXIT LIGHTS DISARM CHECK FAIL TO GIVE PROPER INDICATION. LIGHT SHOULD ILLUMINATE. RELAMPED, OPS CHECKS GOOD.
F/O'S SMOKE GOGGLES SCRATCHED AND FOGGY. REPLACED CAPTAIN'S SMOKE GOGGLES PER 25-60-05-2.
INSPECTION TYPE:N/A ON PREFLIGHT FOUND EMERGENCY EXIT LIGHTS OVER ENTRY DOOR & IN COMPANION WAY OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKS OK.
NO EMERGENCY LIGHTS ON TEST. EMERGENCY BATTERY PACK REPLACED, BUT EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN DISARMED. FOUND WIRE PULLED OUT OF SOCKET NR 8 ON P1-1345. REPLACED SOCKET PER MM 20-50-01-8 AND WDM 33-50-01 PG 5. TEST GOOD PER MM 33-50-01-2.
INSPECTION TYPE:C1 LONGERON 10L END FITTING CRACKED AT STA 1770. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D.
INSPECTION TYPE:C1 INTERNAL DOUBLER CRACKED AT STA 1880 BETWEEN SKIN AND LONG 34R. CORRODED FROM 1861-1890. REMOVED DOUBLER FROM STA 1770-1890. FAB REPLACEMENT DOUBLER FROM SHT7075T6 -.025. INSTALLED DOUBLER REF DWG 5649328, SRM 51-1-21, 51-1-8, 51-1-20D.
INSPECTION TYPE: C1, AFT CARGO BS 1420 LT CUSP, APROX LBL 60 ON FWD SIDE OF FRAME, SEVERE CORROSION UNDER & AROUND NUTCLIPS APPROX .5 INCH DIA SEAT TRACK. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3. REMOVED AND REPLACED SEAT TRACK SECTION AND INSTALLED SPLICES STA 1410 TO 1430 LBL 60 IAW 53-2-3 FIG 8A, 51-1-20D AND 51-3-0.
INSPECTION TYPE: C1, FITTING CRACKED UNDER FLOORBEAM, STA 700 RBL 24 MAIN CABIN. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D.
INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK SCALLOPS WORN BEYOND LIMITS STA 1360-1380, LBL 24. REMOVED FLOORBOARDS TO FOM. REMOVED SEAT TRACK FROM 1300-1460. FAB RPLACEMENT SEAT TRACK FROM S2772660 EXTRUSION. INSTALLED SEAT TRACK, NEW SPLICE FITTING, AND FLOORBOARDS REF SRM 53-2-3 FIG 12, 51-3-0, 51-1-8.
INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT RT PRIMARY HEAT EXCHANGER CUTOUT AT LOWER AFT CORNER. CRACK APPROX 1 INCH LONG. CUT OUT DAMAGED SKIN, NDT VERIFIED. FAB DOUBLER AT FILLER FROM SHT2024 T3-.100. INSTALLED CONICAL WASHERS AND ALL REPAIR PARTS REF SRM ADDM EO DC8-5330-4732-D.
INSPECTION TYPE: C1, FINGER DOUBLER CRACKED & HAS SHEARED RIVET HEADS IN MAIN CABIN SUBFLOOR, STA 875 LBL 5. REMOVED FINGER DOUBLER & FOUND IT HEAVILY CORRODED ON UNDERSIDE. NO CORROSION NOTED ON PRESSURE WEB. FAB REPLACEMENT FINGER DOUBLER FROM 2024T3-.050. INSTALLED & SEALED DOUBLER REF DWG5645332, SRM 51-1-21, 51-1-8, 51-1-20D, 51-1-11.
INSPECTION TYPE: C1, SPAR-TO-WING ATTACH ANGLE CRACKED IN MAIN CABIN SUBFLOOR, STA 798 RBL 55. FAB REPLACEMENT ANGLE REF DWG3643112 ON SAA SERVICE ORDER 7034920. REMOVED & REPLACED ANGLE REF SRM 51-1-20D, 51-3-2, 51-1-24, 51-1-20D. FUEL LEAK CHECK C/W ON TC8000.
INSPECTION TYPE: C1, LONGERON FITTING CRACKED IN MAIN CABIN STA 902-910 LONG 4L. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20B, 51-1-21, 51-1-20D.
INSPECTION TYPE: C1, BATH-TUB FITTING CRACKED ON LONG 4R, STA 902. REMOVED AND REPLACED FITTING REF SRM 51-1-20D.
INSPECTION TYPE: C1, MAIN CABIN FLOORBEAM FITTING CRACKED AT STA 702 LBL 25 (SUBFLOOR). REMOVED & REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-11.
INSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD VERTICAL STIFFENER TO FLOORBEAM ATTACH FITTING CRACKED, SUBFLOOR LBL 25. FABRICATED REPLACEMENT FITTING REF DWG 5773275 ON SAA TRAVELER 0001. REMOVED & REPLACED FITTING REF SRM 51-1-8, 51-1-20D.
INSPECTION TYPE: C1, TIE ANGLE CRACKED ON FWD SIDE OF AFT PRESSURE BULKHEAD TO LONG 6R. REMOVED CRACKED ANGLE. FAB REPLACEMENT ANGLE FROM SHT7075/0-.080 AND HEAT TREATED TO T6 ON SAA SERVICE ORDER 7034928. INSTALLED ANGLE REF DWG 5773844, SRM 51-1-21, DPS7.00-1.
INSPECTION TYPE:C1, COMPT 60 L17R HAS 3 INCH CRACK AND LONGERON END FITTING HAS .5 INCH CRACK 1770. REMOVED AND REPLACED L17R AND END FITTING AT STATION 1770 IAW 51-1-8, 51-1-20D, 53-2-2 AND 51-1-21.
INSPECTION TYPE:C1 LONGERON 11L SPLICE FITTING CRACKED STA 660-680. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-3-2, NDTSPM06-10-01.
INSPECTION TYPE: C1, LONGERON 3R END FITTING CRACKED IN MAIN CABIN, STA 902-920. REMOVED & REPLACED FITTING REF SRM 51-1-20D.
INSPECTION TYPE: C1, ATTACH FITTING CRACKED ON LONG 11R STA 680. FAB REPLACEMENT FITTING FROM 7075 T6 PLATE ON SAA SERVICE ORDER 7034927. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-21.
INSPECTION TYPE:C1 ANGLE CRACKED INSIDE L1 DOOR JAMB AT STA 35. NDT VERIFIED CRACK TERMINATED AT FASTENER HOLE. FAB REPAIR DOUBLER FROM SHT2027T3-.063. TREAT, PRIME, INSTALL REPAIR REF SRM 51-1-21, 51-1-8, 51-3-0, 53-2-0 FIG 1B, 51-1-21A, DWG 5597646.
INSPECTION TYPE: C1, AFT PRESSURE BULKHEAD CRACKED AT LBL 35 NEAR LONG 11L. REMOVED EXISTING REPAIR AT SITE. CUT OUT DAMAGE. NDT VERIFIED. FAB-27 DOUBLER (SHT7075T6-.063), -25 DOUBLER (7075T6-.032), -9 FILLERS (7075T6-.050). TREAT, PRIME & INSTALL REPAIR REF SRO8530007.
INSPECTION TYPE:C1 LONGERON 15R CRACKED UNDER CANTED FRAME AT STA 1734 REMOVED LONG FROM 1725-1766, END FITTING, CLIP AT STA 1752. FAB REPLACEMENT LONG SECTIONS (S1616757 EXTRUSION), 2 SPLICE FITTINGS ON SERVICE ORDER 7034948 (S2645716 EXTRUSION), 4 REPAIR STRAPS (SHT7075T6-.080) INSTALLED ALL PARTS REF SRM 53-2-2 FIG 10, 53-5-3 FIG 5, 51-1-21, 51-1-20D, 51-1-8, DWG DC8-53B-009, NDTSPM06-10-01.001, DPS4.707.
INSPECTION TYPE:C1 LONGERON 14R CRACKED UNDER CANTED FRAME AT STA 1756. REMOVED LONG SECTION, END FITTING, CLIP. FAB REPLACEMENT LONG SECTION (S1616757 EXTRUSION), 2 STRAPS (SHT7075T6-.080), SPLICE FITTING ON SVC ORDER 7034949 (S2645716 EXTRUSION). INSTALLED ALL PARTS REF SRM 53-2-2 FIG 10, 51-1-20D, 51-1-21, 51-1-8, DWG DC8-53B-009, NDTSPM06-10-01.001, DPS4.707.
INSPECTION TYPE: C1, LONGERON ATTACH FITTING CRACKED AT STA 702 LONG 15R. FAB REPLACEMENT FITTING REF DWG3779978 ON SAA SERVICE ORDER 7034926. REMOVED & REPLACED FITTING REF SRM 51-1-20D.
INSPECTION TYPE:C1 LONGERON 15L CRACKED NEAR STA 1760. REMOVED LONG FROM STA 1739-1766, SHEAR TIE AT STA 1746, END FITTING AT STA 1766. FABRICATED REPLACEMENT LONG SECTION (S1616756 EXTRUSION), REPAIR SPLICE ON SERVICE ORDER 7034944 (S2645716 EXTRUSION), 2 SPLICE STRAPS (SHT7075T6-.080) INSTALLED ALL PARTS REF SRM53-2-2 FIG 10, DWG DC8-53B -009, 51-1-21, 51-1-20D, 51-1-8, NDTSPM06-10-01.001, DPS4.707.
INSPECTION TYPE: C1, VERTICAL WEB CRACKED IN LT FLAP COVE FWD OF, AND BELOW XW3 FLAP HINGE FITTING. STOP DRILLED CRACK. NDT VERIFIED. FAB REPAIR DOUBLER FROM SHT7075T6-.071. TREAT, PRIME, INSTALL REPAIR REF DWG5643117, NDT/SPM06-10-01.001, SRM 53-2-0 FIG 1D, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C1 AC COMPT FS 55.00 MAIN CABIN SUBFLOOR AREA RBL 48.00 FWD O/B SIDE OF FLOORBEAM INTERSECTION VERTICAL ATTACH FITTING HAS A CRACK BETWEEN FASTENERS. REMOVED AND REPLACED VERTICAL ATTACH FITTING AT FS 55.00 RBL 48.00 IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE:C1 FRAME CRACKED AT STA 55 BETWEEN L24R & L25R AT DUCT SUPPORT ROD MOUNT. CUT OUT CRACKED FRAME SECTION. FAB FILLER AND 2 REPAIR ANGLES FROM SHT 7075/0-.071, HEAT TREAT TO T6 ON SAA SVC ORDER 7034931. INSTALLED ALL PARTS REF SRM 53-2-0 FIG 2, 51-1-21, 53-2-0, 51-1-8, 51-1-20D, DPS7.00.
INSPECTION TYPE:C1 LONG 14L CRACKED NEAR STA 1760. REMOVED LONG SECTION FROM 1746-1766. REMOVED SHEAR TIE AT 1757. FABRICATED REPLACEMENT LONG SECT FROM EXTRUSION S1616757, 2 SPLICE STRAPS (SHT7075-T6 .080), REPAIR SPLICE (S2645716 EXTRUSION) ON SERVICE ORDER 7034945 & INSTALLED ALL PARTS REF DWG DC8-53B-009, SRM 53-2-2 FIG 10, 51-1-21, 51-1-20D, 51-1-8, NDTSPM06-10-01.001, DPS4.707.
DROP CORROSION ABOVE WING BOTTLE BOLT, LOCATED IN RIGHT W/W FWD BULKHEAD, UPPER O/B CORNER. REMOVED RIGHT OVERWING EMERGENCY HATCH AND PANEL 292F TO FOM. REMOVED CORRODED PAD FROM RIGHT WHEEL WELL IAW DC8 SRM 51-1-20D. INSTALLED PAD AND PANEL 292F IAW DC8 SRM 51-1-20D, 51-3-1, AND 51-3-0. INSTALLED RIGHT OVERWING EMERGENCY HATCH IAW DC8 SMM 52-20-02.
RIGHT WING ROOT HAS CORROSION (EXFOLIATION). A/C FERRIED TO TCO DEFERRED (276424) AND TRANSFERRED TO NRC 469644 RMVD RH OVERWING EMERGENCY HATCH TO FOM. RMVD R/H OVERWING TO FUSELAGE FILLET PNL 292F TO FOM. RMVD CORRODED PAD FR R/H W/W IAW DC8-SRM 51-1 -20. RCVD NEW 2751738-2 FTG LOCATED & DRILLED IAW DC8 SRM 51-1-24. OK TO INSTALL. INSTALLED FTG, OK TO INSTALL PNL 292F IAW DC8-SRM-51-3- 0. OK TO INSTALL DOORWING EMERG HATCH. RMVD RH OVERWING EMERG HATCH P NL 292F. RMVD CORODED PAD FR RT WW & REINSTALLED PAD & PNL.
INSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT TEST. R&R EMERGENCY LIGHT BATTERY PACK. P/N ON AND OFF 5708403, S/N ON FLS/ST/7021, S/N OFF CAW250.
INSPECTION TYPE:N/A NR 3 ENGINE SLOW TO RESPOND TO THROTTLE INPUT DURING BOOST TO START NR 2 ENGINE. APPROX 10 MIN INTO FLT OIL QTY DECREASED TO 4 QTS. ENGINE SHUTDOWN ACCOM AT 2 QTS, IAW CHECKLIST. WINDMILL TIME OF APPROX 40 MIN WITH 2-5 PSI. FOUND NR 3 STARTER SERVICING CAP OFF CAUSING STARTER TO FAIL AND OIL TO VENT OVERBOARD. STARTER REMOVED AND REPLACED IAW MM 80-10-01. SERVICED ENG OIL, OPS CHECKS GOOD IAW MM 71-00-00.
FASTENERS MISSING AND LOOSE BOTTOM EDGE OF LEFT FWD EMERGENCY DOOR. CW EO DC8-5220-18984-A INTERIM REPAIR DEFERRED PER EO FOR REPETITIVE INSP AND PERM REPAIR.
INSPECTION TYPE: C3, PERFORM LT WING AND RT WING FWD SPAR INSPECTION OF LWR SPAR CAP PER EO DC8-5 710-14184-C AS REQUIRED. REAMED 1 DISCREPANT HOLE ON L/W TO .3230, PERFORMED HFEC AND NO CRACKS NOTED PER DAC SPM 06-10-01.003. CHECKED SPAR THICKNESS AT .689 & L/E SKIN AT .143. FAB'D BUSHINGS FOR REPAIR IAW DAC DWG 4709980 & SRM 51-1-25. REAMED HOLE TO PRE COIN SIZE AND STRESS COINED PER DPS 3.67-56. INSTALLED BUSHINGS PER SRM 51-1-23.
INSPECTION TYPE: C3, O/B AFT STRINGER 51 END FT CRACKED AT XRS 74.000 NR 2 MAIN. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. DRILLED LOCATED DEBURRED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. LEAK CHECK TO BE ACCOMPLISHED ON UPS T/C 8000 ITEM 26.
INSPECTION TYPE:C3 LT WING FRONT SPAR LOWER CAP XFS 7 HAS A CRACK INDICATION FOUND BY HFEC. STOP DRILLED CRACK, FABBED REPAIR ALODINED AND PRIMED INSTALLED REPAIR.
INSPECTION TYPE: C3, LAP SPLICE BLENDED OUT OF LIMITS L21L/FS 1600. REMOVED DAMAGED SECTION OF CUSP DOUBLER 9750448-29. FAB REPLACEMENT PART, ALODINED, PRIMED & INSTALLED IAW TIMCO REO G09045. FAB FINGER DOUBLER IAW DAC DWG 9750448, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.
INSPECTION TYPE: C3, ALC STA 1490 L34R SPLICE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1000 ABOVE L33R FRAME IS CORRODED. REMOVED FRAME CAP IAW DC8 SRM 51-1-21 & 51-1-20D. LOCATED DRILLED AND DEBURRED NEW FRAME CAP 9755885-7 IAW DC8 SRM 51-1-21 & 51-1-20D. INSTALLED NEW FRAME CAP IAW DC8 SRM 51-1-21 & 51-1-20D.
INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1160 BETWEEN L33R-34R Z-FITTING IS CRACKED. REMOVED CRACKED FITTING. FABRICATED REPAIR DOUBLER & SHIM IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING REPAIR DOUBLER AND SHIM IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C3, AFT PIT LONG 35 RT DENTED STA 1377. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21.
INSPECTION TYPE:C3 AFT PIT LONG 34R STA 1420-1440 CORRODED. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D AND 51-1-21.
INSPECTION TYPE: C3, LT WING UPPER FRONT SPAR SHOWS EVIDENCE OF STRESS CORROSION AT APPROX ST A XRS 540. REMOVED CORROSION IAW DC8 SRM 51-1-8, FAB REPAIR STRAP AND FILLER IAW R EO G09022. ALODINED AND PRIMED REPAIR IAW DC8 SRM 51-1-8. INSTALLED REPAIR STRAP AND FILLER IAW REO G09022. FAB AND INSTALLED 1 BUSHING .3775 IAW DAC DWG 4709981 & REO G09022 AND DC8 SRM 51-1-25.
INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1040-1060 AT L28R SPLICE FITTING IS CRACKED. REMOVED CRACK FITTING. LOCATE NEW FITTING, DRILL EXISTING FASTENER HOLES AND DEBURRED IAW DC8 SRM 51-3-2. REMOVED LOWER FILLET PANEL FOR ACCESS IAW DC8 SRM 51-3-0. INSTALLED NEW FITTING AND LOWER FILLET PANEL IAW DC8 SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE: C3, NR 4 ALT TANK STR 59 END FITTING CRACKED STA XW 428 INSIDE PNL 505B. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C3, NR 1 ALT FUEL TANK STR 59 STA 408 END FITTING CRACKED INSIDE PNL 505B. REMOVED CRACKED FITTING PER DC8 SRM 51-1-20D. DRILLED, LOCATED AND DEBURRED NEW END FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW END FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE: C3, AFT CARGO PIT AT FS 1210 BETWEEN L33R-34R T-BOLT LATCH BACKUP FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2 -0. LOCATED, TRIMMED AND DRILLED UP FITTING 3754930-1 AND REPAIR FITTINGS 5894282-501, 5894282-502, IAW DC8 SRM 53-2-0. INSTALLED FITTING AND REPAIR FITTING IAW DC8 SRM 53-2-0, 51-1-20D.
INSPECTION TYPE:C3, L2 LOWER FWD DOOR JAMB CORNER CRACKED TWO PLACES. FAB NEW SEAL RETAINER IAW DAC DWG 5751115. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FAB PAN REPAIR DOUBLER IAW DAC DWG 5751040, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAL RETAINER AND DOUBLER AND DOOR PAN IAW DC8 SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE: C3, CORROSION IN RT FWD UPPER CORNER OF RT MLG WHEEL WELL. REMOVED FITTING PN 3646772, REMOVED CORROSION FROM WEB IAW DC8 SRM 51-1-8, LESS THAN . 002 INCH, W/IN LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING P/N 3646772, LOCATED DRILL AND INSTALLED FITTING IAW DC8 SRM 51-1-21. REMOVED FLOORBOARD FROM STA 850-890 RBL 40 & FILLET PANEL 292F TO GAIN ACCESS TO REPAIR, INSTALLED FLOORBOARD AND FILLET PANEL IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C3, LEFT WING FLAP HINGE SUPPORT FITTING AT STA XF 339 7332 CRACKED AT OUTBOARD SIDE JUST FWD OF FLAP FWD SPAR. REMOVED BASE FITTING, CENTER FITTING, SLIDER PANEL, OUTBOARD TRACK, CLOSURE PANELS AND SPRING PANEL IAW DC8 SRM 51-3-0. LOC AND DRILLED BASE FITTING AND CENTER FITTING IAW DAC DWG 5751174. ALODINED AND PRIMED FITTINGS IAW DC8 SRM 51-1-8. INSTALLED BASE FITTINGS AND CENTER FITTINGS IAW DAC DWG 5751174. RE-INSTALLED PANELS AND OUTBOARD SLIDER TRACK IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C3, L1 DOOR UPPER FWD CORNER CRACKED BY CUTOUT, MARKED. FOUND WITH NDT ON SKIN MAT ID -17 DOUBLER 7075-T6 .063 PO 3874552 -15 DOUBLER 7075-T6 .080 PO 3958421 FILLER 7075-T6 .050 PO 3924131 IAW DC8 SRM 53-2-0. FAB DOUBLER TRIPER IAW DC8 SRM 53-2-0 FIG 15. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER TRIPLER IAW DC8 SRM 53-2-0.
INSPECTION TYPE: A, CORROSION IN RT FWD UPPER CORNER OF RIGHT MLG WHEEL WELL. FERRY TO TCO. REMOVED LITE SURFACE CORROSION, LESS THAN .002 INCH MATERIAL, W/IN LIMITS IAW DC8 SRM 53-2-0. ALODINED IAW DC8 SRM 51-1-8, OK TO PRIME. AFTER FURTHER INSPECTION, FITTING FOUND TO BE CRACKED. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.
INSPECTION TYPE:N/A RIVETS POPPED DUE TO CORROSION BETWEEN STA 120 & 130 LONGERON 31R 2 LAP SEAM. REMOVED CORRODED SECTION OF FINGER DOUBLER & SKIN. VERIFIED CORROSION REMOVED ACCOMPLISHED REPAIR PER SRM 53-2-1
INSPECTION TYPE:N/A, 1 BULB INOP CREW ENTRY EMERGENCY LIGHT. RELAMPED AS REQUIRED.
INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK, CKS GOOD IAW MM CHP 33.
INSPECTION TYPE:C2 LT WING LE SECTION BETWEEN NR 1 & 2 ENGINE SLOT DOOR ACTUATOR ATTACH BRACKET IS CRACKED APPROX 50 INCHES FROM OTBD LWR SIDE RMVD OB SECTION OF LT OB SLOT, SETAINER & SEAL FABBED NEW ATTACH BRA CKET FITTING IAW DAC DWG 4770278 INSTALLED NEW ATTACH FITTING REINST ALLED OB SECTION OF OB SLOT, SEAL & RETAINER IAW UPS DC8 MM 2702 270 0 & 51-3-0 OPS CHECK GOOD
INSPECTION TYPE:C2, NR 2 MAIN FUEL TANK STRINGER SPLICE FITTING PN 3704841 IS CRACKED. LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 INSTALLED NEW FITT ING IAW DC8 SRM 51-1-20D
INSPECTION TYPE:C2 AFT PIT AT FS 1160 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT REMOVE OLD FITTING INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D & 51-3-2
INSPECTION TYPE:C2 AFT PIT AT FS 1220 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION IAW DC8 SRM 51-1-8 ORIGINAL THICKNESS 0.125 MINIMUM REMAINING THICKNESS IS 0.063 & FOUND TO BE OUT OF LIMITS RMVD CORROSION LOCATED & DRILL NEW FITTING IAW DC8 SRM 51-1-21 AND INSTALLED FIT TING IAW DC8 SRM 51-1-20D
INSPECTION TYPE: C2, AFT CARGO PIT AT FS 1420 AT BL0 IN CEILING AT D PIT DOOR COVER ATTACH BRACKET IS CRACKED REMOVED CRACKED ATTACH ANGLE IAW DC8 SRM 51-1-21 AND 51-1-20D CVD NEW P ART 5616673-64 ANGLE LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24 INSTALLED ANGLE IAW DC8 SRM 51-1-20D
INSPECTION TYPE:C2 MAIN CABIN STA 1306 AT X=0 (TRACK D) TRACK SCALLOP IS WORN AS MARKED. TRIMMED OUT DAMAGED AREA AND INSTALLED PLUG IAW DC8 SRM 53-2-3
INSPECTION TYPE:C2 MAIN CABIN TRACK B ST 1450 TO 1470 CORRODED. CUT SEAT 1430 TO 1470 IAW DC8 EO 5320-8309 AND REPAIR IAW WITH SAME
INSPECTION TYPE:C2 STANTION SUPPORT CRACKED ATTACHED TO FRAME STA 1060 RH SIDE AFT PIT. REMOVED CRACKED STANTION SUPPORT STRUT IAW DC8 SRM 51-1-20D RCVD NEW SU PPORT PN 3773077-509N W/ PO 355450 LOCATED & DRILLED HOLES IAW DC8 S RM 51-1-24 INSTALLED STANTION IAW DC8 SRM 51-1-20D
INSPECTION TYPE:C2 AFT CARGO PIT FS 1220 AT LONG 31R INSIDE X SLIDE DOOR AFT TORQUE BOX FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8 FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 RMVD FITTING IAW DC8 SRM 51-1-21 RCVD LOCATED DRILLED IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D
INSPECTION TYPE:C2 CORROSION ON UPPER SURFACE OF CUSP FITTING AT & BETWEEN FS 110 - 1120. REMOVED FITTING INSTALLED NEW FITTING PN 4643162 PO 355728
INSPECTION TYPE: C2, STATION Y=8, X=0 FLOOR WEB CRACKED & GOUGED AT SEVERAL AREAS D128. REMOVED FLOOR ATTACH ANGEL, CUT OUT DAMAGE IN WEB FABBED & INSTALLED FILLER & DOUBLER IAW DC8 SRM 53-2-0 FIG 23 AND 51-1-21 ALODINED & PRIME D IAW DC8 SRM 51-1-8
INSPECTION TYPE: C2, MAIN CABIN STA 920 LT FLOORBEAM CORRODED AT FRAME JOINT FWD AND AFT. REMOVED AND REPLACED FLOORBEAM STRAP IAW DAC DWG 5646864 ALODINED A ND PRIMED IAW DC8 SRM 51-1-8
INSPECTION TYPE:C2 MAIN CABIN STA 920 LT FLOORBEAM CORRODED AT FRAME JOINT FWD AND AFT. REMOVED AND REPLACED FLOOR BEAM STRAP IAW DAC DWG 5646864 ALODINED & PRIMED IAW DC8 SRM 51-1-8
INSPECTION TYPE: C2, MAIN CABIN STA 780 RT SIDE, BY SEAT TRACK H BEAM FITTING. SUPPORT CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20 51-1-24 AND 51-3-0
INSPECTION TYPE:C2 AFT PIT FWD ENTRY CARGO DOOR STA 1220 LONG 34R FITTING CRACKED RMVD CRACKED FITTING IAW DC8 SRM 51-1-20D RECD LOCATED & DRILLED NEW FITTING & REPAIR ANGLES IAW DC8 SRM 53-2-0 AND INSTALLED IAW DC8 SR M 51-1-20D
INSPECTION TYPE:C2 AFT PIT AFT ENTRY DOOR CRACKED TOP OF SCUFF PLATE STA 1410 L34R. REMOVED DOOR SCUFF PLATE SEAL COMPRESSOR LWR HOLAF FABBED REPAIR IN STALLED NEW SEAL COMPRESSOR INSTALLED REPAIR & SCUFF PLATE IAW DC8 S RM 51-1-21 &51-1-20D
INSPECTION TYPE:C2 FWD PIT FWD DOOR STA 280 LONG 31R FITTING CRACKED AND CORRODED INSIDE TORQUE BOX. REMOVED FITTING IAW DC8 SRM 51-1-21 DRILLED NEW FITTING IAW DC8 SRM 51- 1-24 AND DC8 SRM 51-1-20D INSTALLED NEW FITTING IAW DC8S RM 51-1-20D
INSPECTION TYPE: C2, MLG WW PRESSURE DECK STIFFENER STA 960 LBL 48 HAS POPPED RIVETS AND CORROSION COMING FROM UNDERNEATH. REMOVED & REPLACED FITTING IAW DAC DWG 3640087 AND DC8 SRM 51-1-21 AND 5 1-1-20D
INSPECTION TYPE:C2 FS 1800 TAIL SECTION UPPER TORQUE BOX FWD STIFFENER CRACKED. FABBED NEW STIFFENER PER TIMCO REO G07973
INSPECTION TYPE:C2 FLC C1 DOOR TORQUE BOX AREA STA 280 L33R UPPER FLANGE HAS CORROSION. REMOVED CORROSION, REMOVED WEB ZEE FITTING FABED DOUBLER & MODIFIED ZEE FITTI NG IAW REO G07967 INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D
INSPECTION TYPE:C2 SEAT TRACK B EXFOLIATED STA 1140. REPAIRED IAW EO DC8-5320-8309
INSPECTION TYPE:C2 FLC AT STA 70 INTERCOSTAL AT APPROX RBL 27 TO RBL 35 CRACKED & CORRODED ***CPCP*** REMOVED INTERCOSTAL. FABBED INTERCOSTAL IAW DAC DWG 5613064 ALODINED & PR IMED IAW DC8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D & 51-1-21
EMERG LIGHTS INOP. REPLACED EMERG BATTERY PACK 60-1223-5 S/N 338N) 341(OFF)
INSPECTION TYPE:N/A, EMERGENCY LIGHTS STAY ON WITH SWITCH IN ARMED POSITION. FOUND EMERGENCY EXIT LIGHTING C/B POPPED. RESET C/B. PERFORMED GROUND OPS CHECK. SYS CHECKS GOOD. OK FOR SERVICE.
ON PREFLIGHT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. R & R EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK OK P/N ON 5708458-503 SN ON NC 2624 P/N OFF 60-1223-5 SN OFF 348
INSPECTION TYPE:N/A, EMERGENCY LIGHTS FAILED TO TEST ON GROUND. REMOVED AND REPLACED EMERGENCY LT BATTERY PER PER MM 33-50-01, GROUND OPS TEST NORMAL.
EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK P/N ON/OFF 5708458-503 S/N ON 2024 S/N OFF 783.
CREW ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR INOP. REPOSITIONED GIRT BAR LOCKING CLIPS ON FLOOR, GIRT BAR LOCK CKS GOOD.
INSPECTION TYPE:N/A, F/O SLIDE WINDOW WILL ONY OPEN INTERMITTENTLY. ADJUSTED F/O CLEARVIEW WINDOW PER MM 56-10-03, OPS CHECK GOOD.
INSPECTION TYPE-C1, LT LONGERON NR 11, STA 660 CRACKED. REMOVED DAMAGE, FAB DOUBLER ANGLES AND FILTER REPAIR IAW REO-06405. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED REPAIR IAW DC-8 SRM 51-1-21.
INSPECTION TYPE-C/CK, INTERCOSTAL END FITTING AT STA 857 LONGERON 19L IS CRACKED. REMOVED CRACKED END FITTING IAW DC8 SRM 51-1-20D. MATERIAL ID FOR NEW END FITTING 7075-T651 PLATE PO 265699 IAW DAC DWG 4750422. FABRICATED NEW END FITTING IAW DAC DWG 4750422, PERFORMED DYE-PENETRANT INSPECTION IAW MIL-S-271F, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW END FITTING DC8 SRM 51-1-20D.
INSPECTION TYPE-C/CK, FS 70 L33R CORRODED FRAME. CORRODED BEYOND LIMITS MATERIAL ID IAW DC8 SRM 53-2-5. FABRICATED IAW DC8 SRM 53-2-5, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C/CK, REMOVED AND REPLACED MAIN FRAME STA 920 LEFT HAND LOWER DUE TO CORR BLENDOUT. REMOVED CUSP MEMBRANE WEB, MAINFRAME AND LONG 21 AND INTERCOSTAL AT FS 920 LEFT HAND IAW DC8 SRM 51-1-20D AND 51-1-21. MAIN FRAME FOUND TO BE WITHIN LIMITS AFTER BLENDOUT IAW REO 06417, MATERIAL ID FOR SPLCIES ON CUSP WEB 301 1/2 HARD STAINLESS STEEL .025 PO 211819 IAW UPS EO DC8 5330-2159B, ALODINED AND PRIMED ALL PARTS IAW DC8 51-1-8.
INSPECTION TYPE-C/CK, MAIN CABIN SEAT TRACK NR 7 R EXFOLIATED BELOW STA 280-300. REMOVED FLOOR PANELS CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8 ON SEAT TRACK. REMOVED CORROSION IAW DC8 SRM 51-1-8, UNDER SEAT. REMOVED SEAT TRACK FS 290 TO 610, DRILLED NEW SEAT TRACK AND SPLCIES IAW DC8 S RM 51-1-24, ALODINED AND PRIMED SEAT TRACK SPLICES IAW DC8 SRM 51-1-8, INSTALLED SPLICES IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C1, AFT PIT FS 1040 CORROSION UNDER LOWER SURFACE OF FRAME FLANGE AT L36 WHERE NUT PLATE IS MISSING. FABRICATED REPAIR PARTS IAW DC-8 DWG 53-0229, ALODINED AND PRIMED IAW DC-8 51-1-8, INSTALLED PARTS IAW DC-8 SRM 51-1-21 (51-1-16 AND 51- 3-0).
INSPECTION TYPE-C1, AFT PIT FS 1100 CORROSION UNDER LOWER SURFACE OF FRAME FLANGE AT L36. FABRICATED ANGLE DOUBLER, FILLER AND SHIMS IAW DWG DC-8-53-0229, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED ANGLER DOUBLER, FILLER SHIMS FRAME CAP AND GUSSETS IAW DWG DC-8 53-0229 AND DC-8 SRM 51-1-21.
INSPECTION TYPE-C/CK, FWD A/C BAY STA 50 L33R CORRODED BEYOND LIMITS. MAT'L ID IAW DC8 SRM 53-2-3. LOCATED AND DRILLED AND DEBURRED NEW LONGERON AND END FITTING AND SPLICE IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON FITTING LONGERON AND LONGERON SPLICE IAW DC8 SRM 51-1-21D.
INSPECTION TYPE-C/CK, SEAT TRACK F HAS AREAS OF CORROSION ENTIRE LENGTH FROM FS 857-1020. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACKS RBL 60 FROM STA 1020, FABRICATED NEW SEAT TRACK AND SEAT TRACK SPLICES IAW DC8 SRM 53-2-3 AND DC8 532 0-8309. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK AND REPAIR SPLICES IAW DC8 SRM 51-3-0 AND 53-2-3.
INSPECTION TYPE-C/CK, MAIN CABIN SEAT TRACK NR 6R GOUGED STA 280-300. REMOVED CORRODED GOUGED SEAT TRACK STA 230-3501. INSTALLED NEW SEAT TRACK FROM STA 230-350. INSTALLED SPLCIES STA 230, 270, AND 350 IAW DC8 SRM 53-2-3 AND DC8 SRM 51-3-0. INSTALLED FLOORBEAMS EACH SIDE OF THE SEAT TRACK STA 270-350 IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C/CK, MAIN CARGO DOOR FITTING IS CRACKED VERIFY B-1 NDT. REMOVED AND REPLACED FITTING IAW UPS DC8 SRM 51-1-21 AND SRM 51-1-24.
INSPECTION TYPE-C1, FITTING AT STA 1180, LONG 34R CRACKED. REMOVED CRACKED FITTING, SPLICE ANGLE FABRICATED PER SRM 53-2-0 FIG 26. DRILLED FITTING AND SPLICE ANGLE IAW DC-8 SRM 53-2-0, FABRICATED FILLERS IAW DC-8 SRM 53-2-0, ALODINED AND PRIMED IAW DC-8 SRM 51-1- 8, INSTALLED IAW DC-8 SRM 51-1-20D.
INSPECTION TYPE-C1 Z FITTING AT STA 1180, LONG 28R-27R CORRODED. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51-1-20D.
INSPECTION TYPE-C, MAIN CABIN AT STA 176 AND L9R CORNER OF PRESS BULK ANGLE CRACKED. REMOVED EXISTING ANGLE -24 AND DYEPENED, INSPECTED AERA TO FIND END CRACK. STOP DRILLED CRACK, FOUND PREVIOUSLY REPAIRED, REINSTALLED ANGLE.
INSPECTION TYPE-C/CK, FWD CARGO BAY, RIGHT HAND BAY TUNNEL AREA STA 200 FLOORBEAM AND WEB AT CUSP AREA IS CORRODED. CORROSION EXFOLIATED OUT OF LIMITS IAW SRM 53-2-0. REMOVED FLOORBEAM, ALODINED AND PRIMED IAW DC8S RM 51-1-8, INSTALLED DOUBLER ON CUSP IAW DC8-5330-2159-B AND SRM 51-1-21, INSTALLED PREVIOUSLY REMOVED SEAT TRACK IAW DC8 SRM 51-3-0, INSTALLED FLOORBEAM IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C1, AFT CABIN STA 1680 TO 1700 RBL 28 INTERCOSTAL HAS A CRACK AND CORROSION ON BOTTOM SIDE. INSTALLED REPAIRED ANGLE, STOP DRILLED CRACK, ALODINED AND PRIMED.
INSPECTION TYPE-C, FWD PIT STA 347 INTERIOR OF C1 DOOR FWD TORQUE BOX FORMED ANGLE CORRODED AT L35L. REMOVED ANGLE IAW DC-8 SRM 51-1-24, OUT OF LIMITS IAW DCF-8 SRM 53-20, FABBED NEW ANGLE IAW DAC DWG 9754020, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW DC-8 51-1-20D.
INSPECTION TYPE-C1, AFT PIT LONG TIE FITTING AT STA 1510 LONG 29L HAS BLEND OUT OF LIMITS. REMOVED SPLICE FITTING, FABRICATED REPAIR STRAP IAW REO 06413, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED STRAP AND SPLICE IAW DC-8 SRM 51-1-20D.
INSPECTION TYPE-C1, FLOOR ATTACH SUPPORT ANGLE IS CRACKED AT FS 1230 AFT OF TORQUE BOX AT LONG 36. CUT OUT DAMAGE, FABRICATED REPAIR ANGLE, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8 AND REPAIR ANGLE IAW DC-8 SRM 53-2-0.
INSPECTION TYPE-C1, AFT PIT FS 1120 FRAME SECTION AT L31L AND L33L CORRODED. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE IAW DAC DWG 9758049, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51-1-2 0D.
INSPECTION TYPE-C, FWD PIT STA 340 AT L27R INTERNAL TORQUE BOX CRACKED FITTING. REMOVED ANGLE SWITCH AND STRIKER IAW DC-8 SRM 51-3-0, DRILLED FITTING IAW DC-8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC08 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51-1-20D.
INSPECTION TYPE-C/CK, LONGERON 33 RIGHT CORRODED AT STA 1650-1660. REMOVED EXISTING LONG SECTION, REPLACED WITH NEW SECTION (P/N 575777 8-1).
INSPECTION TYPE-C/CK, LONGERON 25 RIGHT HAS REPAIR AT FS 1560-1590 CORRODED BULGED. REMOVED PREVIOUS REPAIR ANGLE IAW DC8 SRM 51-1-21, CORROSION WAS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMGED SECTION OF LONGERON AND SPLCIED IN NEW SECTION IAW DC8 SRM 53-4-1, 53-2-2 AND 51-1-20D. APPLIED ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE-C/CK, INTERCOSTAL END FITTING STA 857, LONGERON 18L IS CRACKED. REMOVED CRACKED END FITTING IAW DC8 SRM 51-1-20D. MATERIAL ID FOR NEW FITTING 7075-T651 IAW DAC DWG 4750423 PO 265699, FABRICATED NEW END FITTING IAW DAC DWG 4750423. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW FITTING IAW DC8 51-1-20D.
INSPECTION TYPE-C, CORROSION ON FRAME UNDERSIDE AT STA 1705 BETWEEN L20 AND L21 RT SIDE. REMOVED CORRODED IAW DC-8 SRM 51-1-8 OUT OF LIMITS, REO REC, FABBED DOUBLER ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW REO 06 410.
INSPECTION TYPE-C1, RT AFT SERVICE DOOR INTERNAL AFT BOTTOM CORNER NR 6 HORIZ BEAM CRACKED. STOP DRILLED CRACKS, FABBED DOUBLER IAW3 DC-8 SRM 52-2-0 FIG 2, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED WITH HI-LOKS AND RIVETS IAW DC-8 SRM 51-1-20D AND 51-1-21.
INSPECTION TYPE-C1, LT WING LEADING EDGE O/B SLOT, O/B END HAS FASTENERS PULLING THRU SKIN. REPAIRED PER TIMCO REO NR 06403.
INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS, OPS CKS OK.
FLAP SPLIT AFTER REACHING 35 DEG POSITION. AT 35 DE. FLAPS WERE WITHIN 4 DEG. FOUND LEFT CENTER FLAP ACTUATOR DISCONNECTED AT ROD END, BOLT MISSING. LEFT CENTER FLAP FITTING GOUGED. REPLACING ACTUATOR AND FITTING.
INSPECTION TYPE-N/A, EEL BATTERY VOLTAGE IS 19 VOLTS. REMOVED AND REPLACED EEL BATT PACK IAW MM 33-50-33 (P/N F5708458-503) (S/N ED2) ON, (S/N FTL004) OFF.
INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK LIGHTS.
DURING D CHECK INSPECTION, FOUND T BOLT BACKUP FITTING CRACKED AT F/S 332. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND INTERCOSTAL TIE CLIP ON FWD SIDE OF FS 1140 FRAME AT LONGERON 33RT CRACKED. REMOVED CRACKED CLIP, DRILLED NEW CLIP, TREATED, PRIMED AND INSTALLED NEW CLIP IAW DC8 SRM 51-1-8, 53-1-0, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON FINGER DOUBLER AT LONGERON 31RT FS 200 TO 220. REMOVED CORRODED SECTION OF FINGER DOUBLER, FABRICATED, NEW FINGER DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 53-2-2, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 35 RT END FITTING FS 1790. REMOVED END FITTING, DRILLED NEW END FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND LONGERON 35 RT END FITTING CORRODED FS 1680 TO 1690. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND FITTING CRACKED FS 270 BETWEEN LONGERON 34RT AND 35RT. REMOVED CRACKED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON T-BOLT BACK UP FITTING FS 1169. REMOVED CORRODED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE-D, FOUND CRACKED FITTING FS 320 BETWEEN LONGERON 35 AND 34 RT. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
DURING D CHECK INSPECTION, FOUND LONGERON 2 LT CORRODED AND CRACKED AT F/S -1. REMOVED DAMAGED SECTION OF LONGERON, DRILLED NEW SECTION OF LONGERON AND SPLICES, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-2, 53-1-0, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON T-BOLT FITTING AT FS 330. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-3-0, 53-1-0, 51-1-20D.
DURING D CHECK INSPECTION, FOUND FOOT CRACKED AT FRAME F/S 380 BETWEEN LONGERON 35 AND 34 RT. REMOVED CRACKED SECTION OF CLIP, FABRICATED NEW SECTION OF CLIP AND SPLICES, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 51-3-0, 51-1-21.
DURING D CHECK INSPECTION, FOUND CORROSION ON T BOLT BACK UP FITTING F/S 308. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW T BOLT BACKUP FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON FINGER DOUBLER UNDER LONGERON 31 RT AT FS 260. REMOVED CORRODED SECTION OF FINGER DOUBLER, FABRICATED NEW FINGER DOUBLER SECTION, DRILLED, TREATED, PRIMED AND INSTALLED IAW DACO DWG 5753892 AND DC8 SRM 51-1-8, 51-1-21, 53-1-0.
INSPECTION TYPE-D, FOUND C-PIT DOOR JAMB, LOWER AFT CORNER INNER AND OUTER SKIN CRACKED APPROX FS 1219. REMOVED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON T-BOLT FITTING AT FS 314. REMOVED CORRODED T-BOLT FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-3-0, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON FUSE SKIN AND SPLICE FITTING FS 1690 TO 1680 AT LONGERON 34RT. REMOVED CORROSION FROM FUSELAGE SKIN WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON T-BOLT FITTING AT STA 305. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-3-0, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON T-BOLT FITTING FS 290. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON T-FITTING FS 322. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-3-0, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND T-BOLT FITTING CORRODED FS 1211. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON A PIT DOOR T-BOLT BACK UP FITTING FS 312. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-2-0, 53-1-0, 51-1-20D, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON FINGER DOUBLER AT FS 400, LONGERON 31 LT. REMOVED CORRODED SECTION OF FINGER DOUBLER, FABRICATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF FINGER DOUBLER FS 355, 450 IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D, 53-1-0.
INSPECTION TYPE-D, FOUND CORROSION ON FITTING 340 BETWEEN LONGERON 32 AND 33 RT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON FINGER DOUBLER AT FS 418 TO 440 AT LONGERON 31 RT. REMOVED CORRODED SECTION OF FINGER DOUBLER FROM FS 355 TO 450 FABRICATED FINGER DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-1-0, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON C-PIT DOOR T-BOLT FITTING FS 1185. REMOVED CORRODED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON INNER SKIN FS 1690 TO 1680 AT PRODUCTION SPLICE FITTING LONGERON 36. REMOVED FITTING, REMOVED CORROSION FROM SKIN, WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG 1F. TREATED AND PRIMED SKIN IAW DC8 SRM 51-1-8, FOUND CORROSION ON FITTING TO BE OUT OF LIMITS DRILLED NEW FITTING, TREATED PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 53-1-0.
INSPECTION TYPE-D, FOUND FITTING CRACKED FS 270 BETWEEN LONGERON 36 AND 35 LT. REMOVED CRACKED FITTING, DRILLED UP NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 34 LT FS 270 TO 280. REMOVED SECTION OF LONGERON, DRILLED, TREATED, PRIMED, AND INSTALLED NEW LONGERON SECTION IAW DC8 SRM 53-1-0, 53-2-0, 51-1-21, 51-1-20D, 51-1-8.
INSPECTION TYPE-D, FOUND FITTING CORRODED AT FS 272 BETWEEN LONGERONS 33 AND 34 LT. REMOVED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21.
INSPECTION TYPE-D, FOUND LONGERON 36 CRACKED FROM FS 200 TO 260. REMOVED SECTION OF LONGERON FS 200 TO 363, DRILLED UP NEW SECTION OF LONGERON, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-N/A, DURING D-CHECK INSPECTION FOUND CORROSION ON A PIT DOOR T-BOLT BACK UP FITTING FS 295. REMOVED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW T-BOLT BACK UP FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-N/A, DURING D-CHECK INSPECTION FOUND ATTACH ANGLE CRACKED APPROX 1 INCH AT AFT PRESSURE BETWEEN LONGERON 8 AND 9 RT FS 1766 STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-5 FIG 9, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION IN BARREL NUT HOLE ON LONGERON 32RT END FITTING AFT OF FS 1690. REMOVED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 53-1-0, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON FRAME TO FUSELAGE SKIN CLIP AT FS 1746 BETWEEN LONGERON 36 AND 34 RT. REMOVED CORRODED SECTION OF CLIP, FABRICATED NEW CLIP, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-5-1, 51-1-8, 51-1-21.
INSPECTION TYPE-N/A, DURING D-CHECK INSPECTION FOUND FITTING CRACKED AT LONGERON 26RT AFT OF F/S 1690. REMOVED CRACKED FITTING, DRILLED NEW FITTING, TEATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 32RT FS 1739 TO 1746. REMOVED SECTION OF LONGERON FS 1690 TO 1766, DRILLED NEW LONGERON SECTION, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON PRODUCTION SPLICE (FRAME) AFT LOWER LEG AFT FS 70 UNDERNEATH LONGERON 33 LT END FITTING. REMOVED CORRODED SECTION OF FRAME, DRILLED NEW SECTION OF FRAME, DOUBLERS AND SPLICE ANGLES, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-5, 51-1-21, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 34LT AT FS 1723, 1739 AND 1746. REMOVED LONGERON SECTION FROM FS 1690 TO 1766, DRILLED UP NEW SECTION OF LONGERON AND SPLICE AT FS 1743, TREATED, PRIMED AND INSTALLED LONGERON SECTION AND SPLICE IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 36 AT FS 1723, 1739, 1746, 1750. REMOVED LONGERON SECTION FROM FS 1690, DRILLED UP NEW SECTION OF LONGERON, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-1-0, 51-1-21.
DURING D CHECK INSPECTION, FOUND PRODUCTION SPLICE FITTING CRACKED AT F/S 1690 LONGERON 34 LT. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-21.
INSPECTION TYPE:D DURING D CHECK, INSPECTION FOUND BULGE IN EXTERNAL FUSELAGE SKIN F/S 200 TO 210 AT LONGERON 31RT. FOUND FINGER DOUBLER CORRODED, REMOVED SECTION OF FINGER DOUBLER FROM F/S 190 TO 220, FABRICATED NEW SECTION OF FINGER DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D
INSPECTION TYPE-D, FOUND FRAME TO LONGERON/INTERCOSTAL FITTING CRACKED FS 837 AT LONGERON 13RT. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED FITTING IAW DC8 SRM 53-1-0, 51-1-21, 51-1-8.
INSPECTION TYPE-D, FOUND FORWARD LOWER FRAME FITTING CRACKED AT AFT OVERWING EXIT FS 798, LONGERON 19 RT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-1-21, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND ATTACH BRACKET (FITTING) CRACKED AT LONGERON 10RT AT FS 1343. REMOVED CRACKED ATTACH BRACKET, DRILLED, TREATED, PRIMED AND INSTALLED NEW ATTACH BRACKET IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LT HORIZ STAB L/E AT XFS 178 UPPER SURFACE. REMOVED CORROSION, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 55-2-1, 51-1-21, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION IN NUMEROUS AREA OF BELLY SKIN FS 1690 TO 1890 LONGERON 28 LT TO 28 RT (P/N 5649329-49) DOUBLER, (P/N 5649329-75N) SKIN. REMOVED CORRODED SKIN, FITTING, TRIMMED AND DRILLED NEW SKIN AND DOUBLER IAW DACO DWG 5649329 AND DC8 SRM 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:D DURING D CHECK, INSPECTION FOUND CORROSION ON FRAME TO SKIN ATTACH CLIP STA 140 LONG 35LT TO 36. REMOVED SECTION OF ATTACH CLIP, FABRICATED NEW SECTION OF CLIP, AND SPLICES, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 53-1-0, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON RT WING OTBD LEADING EDGE AROUND INBD WEIGHT STA XA 620 TO 646. REMOVED CORRODED (DOOR) SKIN, FABRICATED NEW SKIN, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-1-0, 57-2-0, 51-1-8, 51-3-0.
DURING D CHECK INSPECTION, FOUND CORROSION ON BELLY SKIN IN NUMEROUS AREAS F/S 190-450 LONGERON 31 LT TO 31 RT. REMOVED CORRODED SKIN, DRILLED, TREATED, PRIMED AND INSTALLED NEW SKIN IAW DACO DWG 5755271, AND DC8 SRM 51-1-8, 51-1-21, 51-1-20D.
DURING D CHECK INSPECTION, FOUND CORROSION ON FRAME AT F/S 200 LONGERON 36. REMOVED CORROSION, FABICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20D, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON FRAME AT LONGERON 36 ATTACH BOLTS FS 200. REMOVED CORROSION, FABICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON TIE PLATE AT FS 1020 LONGERON 16 LT. REMOVED CORRODED TIE PLATE, FABRICATED NEW TIE PLATE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-3-0, 51-1-21.
DURING D CHECK INSPECTION, FOUND INTERCOSTAL TO FRAME TIE FITTING CRACKED ON LONGERON 35 LT AFT SIDE OF FS 1240 FRAME. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON FRAME FS 260 BETWEEN LONGERONS 35 RT AND 36. REMOVED CORROSION, FABRICATED REPAIR ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND FITTING ON AFT SIDE OF FRAME FS 1228 CRACKED BETWEEN LONGERON 32 RT AND 33 RT. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON FITTING FS 323 BETWEEN LONGERON 32 AND 33 RT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON FITTING FS 272 BETWEEN LONGERON 32 AND 33 LT. REMOVED CORRODED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON FWD SIDE OF FRAME FS 1460. REMOVED CORRODED FRAME SPLICE, FABRICATED NEW SPLICE, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
DURING D CHECK INSPECTION, FOUND CORROSION ON LONGERON 31 LT AND FINGER DOUBLERS F/S 75 TO 105. REMOVED CORROSION FROM FINGER DOUBLERS WITH IN LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED CORROSION FROM LONGERON 31 LT. FABRICATED REPAIR DOUBLERS, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D AND DACO ROD SKETCH 97-11-07-005, ACIM REA 97801 UPS EO DC8-53-2067A.
INSPECTION TYPE-D, FOUND CORROSION ON FRAME TO FUSE SKIN ATTACH CLIP AT FS 120. REMOVED 2 EA CLIPS, FABRICATED NEW CLIP, DRILLED, TREATED, PRIME AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON FITTING FS 1614 TO 1620 AT LONGERON 21RT. REMOVED CORRODED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8.
INSPECTION TYPE-D, FOUND SKIN BULGED AND FASTENER HEADS POPPED AT FS 1788 EXTERIOR, RT SIDE OF FWD TAIL SKID. REMOVED AND REPLACED SKIN ON N/R 59X 647132.
INSPECTION TYPE-D, FOUND CORROSION ON VERTICAL SUPPORT FROM FRAME TO FLOORBEAM FS 100 RT TUNNEL AREA. REMOVED CORRODED VERTICAL SUPPORT, DRILLED NEW SUPPORT, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND INTERCOSTAL TIE CLIP (FITTING) ON FWD SIDE OF FRAME FS 1140 AT LONGERON 35 LT CRACKED. REMOVED CRACKED CLIP, DRILL NEW TIE CLIP, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 35RT FS 270 TO 280. REMOVED LONGERON SECTION FROM FS 190 TO 388, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF LONGERON IAW DC8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-20D.
DURING D CHECK INSPECTION, FOUND CORROSION ON FITTING F/S 1220 BETWEEN LONGERON 32A AND 33 RT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-2-0,53-1-0, 51-1-21, 51-1-20D.
DURING D CHECK INSPECTION, FOUND LONGERON SPLICE CRACKED F/S 1270 LONGERON 36. REMOVED CRACKED FITTING (SPLICE), DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 51-1-8, 53-1-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 34RT FS 1766. REMOVED SECTION OF LONGERON FS 1690 TO 1766, DRILLED NEW SECTION OF LONGERON, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 53-2-0, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 34RT AT FS 324. REMOVED SECTION OF LONGERON, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF LONGERON IAW DC8 SRM 51-1-20D, 51-1-8, 53-2-0 AND DACO DWG 9754913.
DURING D CHECK INSPECTION, FOUND LONGERON SPLICE AT F/S 1270, LONGERON 35 LT CRACKED ON FWD END. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D, 51-1-21.
DURING D CHECK INSPECTION, FOUND CORROSION ON FUSE INTERIOR SKIN F/S 1240 UNDER LONGERON 36. REMOVED CORRODED AREA OF SKIN, FABRICATED REPAIR FILLER AND DOUBLERS, DRILLED, TREATED, PRIMED AND INSTALLED IAW DACO ROD SKETCH 97-10-23-009 AND DC8 SRM 51-1-8, 51-1-20D, 51-1-21 DC8-53-2073A.
DURING D CHECK INSPECTION, FOUND INTERCOSTAL TO FRAME TIE FITTING CRACKED ON LONGERON 35 LT FWD SIDE OF FRAME F/S 1240. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING, IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.
DURING D CHECK INSPECTION, FOUND CORROSION ON TORQUE BOX UPPER SKIN BETWEEN LONGERONS 35RT TO 30 RT F/S 270-280. REMOVED CORROSION FROM WEB, FABRICATED FILLER, DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 53-1-0, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON FRAME AROUND LONGERON 36 ATTACH BOLTS FS 460. REMOVED CORRODED SECTION OF FRAME, FABRICATED REPAIR DOUBLERS, FILLER DRILLED, TREATED PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 53-1-0, 51-1-21.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 33LT FS 320 TO 340. REMOVED LONGERON SECTION FROM FS 190 TO 388, DRILLED NEW SECTION OF LONGERON, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
DURING D CHECK INSPECTION, FOUND CORROSION ON FUSE SKIN FROM LONGERON 32 TO 35 LT, F/S 1152 TO 1160. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND FILLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D, AND DACO ROD SKETCH 97-10-21-012.
INSPECTION TYPE-D, FOUND LONGERON 35 RT SPLICE FITTING CRACKED AT FS 1270. REMOVED CRACKED FITTING, DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D AND DACO DWG 5750322.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON 34 RT FS 70 TO 80. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-3-0, 53-1-0, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON LONGERON END FITTING, LONGERON 33 LT AT FS 70. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-21, 51-1-21DI.
INSPECTION TYPE-D, FOUND CORROSION ON FLOOR FRAME IN COCKPIT FS 1000 BL 7 LT TO 7 RT. REMOVED CORROSION FROM FRAME, FABRICATED REPAIR DOUBLERS, DRILLED, TREATED, PRIMED, AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 53-1-0, 51-1-21.
INSPECTION TYPE-D, FOUND FRAME TO LONGERON 31 LT ATTACH CLIPS CORRODED FS 40. REMOVED CORROSION FROM CLIP, INBD CLIP BEYOUD LIMITS, FABRICATED NEW CLIP, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-1, 51-1-8, 51-1-20D.
INSPECTION TYPE-D, FOUND AFT PRESSURE BULKHEAD CRACKED FS 1766, BL 24 TO 28 LT, WL +66. REMOVED DAMAGED AREA, FABRICATED DOUBLER, FILLER, FINGER DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-5 FIG 14A, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND CORROSION ON T FWD SIDE OF VERTICAL BEAM ON AFT PRESSURE BULKHEAD AT BOTTOM. REMOVED CORROSION FROM T-CAP, FABRICATED REPAIR ANGLE, TREATED, PRIMED AND INSTALLED IAW DACO FAX FILE 97-10-20-001, SK97725 AND DC8 SRM 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-D, FOUND LONGERON 24LT CRACKED APPROX 4INCHES FS 857 TO 861. REMOVED AND REPLACED LONGERON 24LT ISW DACO LONGERON REPLACEMENT GUIDE AND DC8 SRM 51-1-8, 51-1-20D, 51-3-0.
INSPECTION TYPE-D, FOUND CORROSION ON BELT FRAME (CAP) AT FS 1100 BL 0 TO 16LT. REMOVED CAP, DRILLED NEW CAP, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND FWD SERVICE DOOR INNER SKIN CRACKED AT LOWER EDGE FS 163. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND RT AFT SERVICE DOOR JAMB WEB CRACKED FS 1619, 25 ABOVE FLOOR LEVEL. REMOVED CRACKED WEB, FABRICATED NEW WEB, DRILLED, TREATED, PRIMED AND INSTALLED WEB IAW DC8 SRM 53-1-0, 53-2-0, 51-1-21, 51-1-8.
DURING D CHECK INSPECTION, FOUND CORROSION ON FRAME CAP F/S 1020 ABOVE LONGERON 31 RT AND 31 LT. REMOVED CORRODED CAP FROM FRAME, DRILLED NEW CAP AND SPLICES, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 53-2-0, 53-1-0, 51-1-20D, 51-1-21.
INSPECTION TYPE-, FOUND CORROSION ON FUSELAGE FRAME BOTTOM SIDE AT FS 1100 BL 9LT. REMOVED CORROSION FROM FRAME IAW DC8 SRM 51-1-8, FABRICATED REPAIR DOUBLERS, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND LT WING OUBD LEADING EDGE INBD LOWER SECTION SKIN CRACKED .5 AT STA XFS 648. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW UPS EO DC8-5720-4087.
INSPECTION TYPE-D, FOUND SKIN BULGED AROUND ATTACH SCREWS ON LT WING L/E STA XFS 710. REMOVED CORROSION AND DAMAGED AREA, FABRICATED DOUBLER, FILLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-1, 57-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-D, FOUND SKIN BULGED AND RIVET PULLING ON UPPER AFT EDGE OF LEADING EDGE STA XFS 342 TO 428 LT. REMOVED CORRODED AREA FROM XFS 304 TO 429, FABRICATED REPAIR DOUBLER AND FILLER DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-1 FIG 38, 51-1-8, 51-1-21 AND DACO FAX FILE ACTION NR 347304.
INSPECTION TYPE:N/A, AT STA 70 RT LONGERON 21 APPROX 30 IN I/B AT STAINLESS DRAIN BOX FLOORBEAM HAS SURFACE CORROSION. *S/D* COMPLETED REPAIRS TO FLOORBEAM - REF SPECIAL VISIT NON-ROUTINE CARD S 253640 TO 253763 THIS CLEARS D130991 MAJOR REPAIR.
INSPECTION TYPE: DLY. EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHK, PART NR ON 60-1223-5, S/N 286, OFF 5708458-503, OFF A056.
INSPECTION TYPE 'C', 32 PYLON STUB WING SLOT SECTION O/B END HAS SEVERAL CRACKS INSIDE OF AREA. STOP DRILLED CRACKS AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-57 -0667.
INSPECTION TYPE 'C', RT WING LEADING EDGE O/B EDGE ATTACH POINTS HEAVY CHAFED. FAB DOUBLER, ALODINED AND INSTALLED IAW UPS EO DC8-57-0665.
INSPECTION TYPE 'C', LWR AUX SPAR CAP HAS A CRACK IN THE BOLT HOLE. DRILLED NEW FITTING AND INSTALLED FITTING IAW SRM 51-1-20D, 51-3-2, 5 1-1-24 AND UPS EO DC8-5720-0956F.
INSPECTION TYPE 'C', STATION 240 RT FLOOR BEAM SUPPORT LWR END IS CORRODED AT FUSELAGE FRAME. REMOVED GUSSET AND ATTACH ANGLE, FAB REPAIR DOUBLERS, REINSTALLED GUSSET AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-20D, 51-1-21 AND 53-2-0.
INSPECTION TYPE 'C', NR 3 PYLON STUB WING SLOT SECTION OUTER I/B END HAS CRACKS. FAB REPAIR FILLER AND DOUBLERS, ALODINED, PRIMED AND INSTALLED IAW TIMCO REO 01915 AND UPS EO DC8-57-0668.
INSPECTION TYPE 'C', UPPER AUX SPAR CAP HAS CRACK IN ATTACHMENT HOLE WHICH EXTENDS TO EDGE. DRILLED FITTING AND INSTALLED IAW 51-3-2, 51-1-20D AND 51-1-24 TO BE INSTALLED ON UPS TASK CARD NR 1056.
CREW REPORTED, F/O'S OTB BACKGROUND LIGHT INOP IN NORMAL AND EMERGENCY. MAINTENANCE REPAIRED WIRE AT RECEPTACLE.
CREW REPORTED, ON CLIMBOUT NR 1 OIL QUANTITY DROPPED TO 2 QTS, THEN PROGRESSIVELY DROPPED TO 0. OIL PRESSURE STARTED TO FLUCTUATE NR 1 ENGINE SHUTDOWN, OCCURRED AT FL 310. WINDMILLING DATA N1 28.9, N2 14.9, 0 PSI OIL PRESSURE, 0 OIL QUANTITY. ENG OIL LOSS GAUGED BY STARTER INTERNAL FAILURE. REMOVED AND REPLACED STARTER ASSY AS PER MM 80-10-01, SERVICED STARTER OIL AND ENG OIL QTY TO PROPER LEVEL. RAN OPS, CK'D STARTER AND ENG FOR LEAKS, NO LEAKS FOUND.
WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.