N868UP
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
THE CREW EXPERIENCED A LEFT MAIN LANDING GEAR BRAKE ISSUE DURING TAXI. POST INSPECTION LEFT MAIN TIRES WERE FLAT SPOTTED. MAINTENANCE REPLACED THE #1 AND #2 WHEEL/ TIRE AND BRAKE ASSEMBLIES. PILOT SIDE LEFT BRAKE MASTER CYLINDER WAS ALSO REPLACED. SYSTEM AND TAXI CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
LOST HYD QTY AFTER T/O ON GEAR RETRACT. REPLACED RT MLG ACT AS PER MM 32-32-02-2 STEP C ALTERNATE METHOD. OPS CHECK GOOD, LEAK CHECK GOOD, OK TO CONTINUE SERVICE.
INSPECTION TYPE:N/A THE SIGHT GAUGE FOR THE EMERGENCY SLIDE IS NOT IN VIEW TO READ PRESS AND EQUIPMENT DUE DATE. REPOSITIONED THE EMERGENCY SLIDE PACK AS NEEDED. OK FOR SERVICE.
INSPECTION TYPE:N/A UNABLE TO MAINTAIN PRESSURIZATION. FOUND LEFT CLAMP PACK DISCONNECTED PERFORMED DECAY CHECK PER AMM 21-31-00-2. ALSO PERFORMED COOLING PACK ADJUSTMENT TEST 21-55-00-5.
DENT IN MAIN ENTRY DOOR AROUND AFT FRAME.
INSPECTION TYPE:N/A ESCAPE SLIDE PARTIALLY DEPLOYED. ESCAPE SLIDE PACK REMOVED FOR REPACKING. REPACKED AND REINSTALLED ESCAPE SLIDE. OK FOR SERVICE. REF MM 25-60-01-2.
CREW ESCAPE SLIDE SHOWS LOW PRESSURE. DEFERRED CREW EMERGENCY ESCAPE SLIDE PER MEL 52-7-4. PLACARD INSTALLED. R&R EMERGENCY EVAC SLIDE PER MM 25-60-01-2. THIS CLEARS M371295 PLACARD REMOVED.
INSPECTION TYPE:N/A AFT PRESS BULKHEAD J BEAM CRACKED. REMOVED FASTENERS 6" L & R OF BL 0 FOR ACCESS FOR FOM. REPAIRED PER EO DC8-5310-6598-C. MATCH DRILLED 3 REPAIR ANGLES AND CLIPS. ACCOMPLISHED APPENDIX B STEPS 7 - 12.
INSPECTION TYPE:N/A ESCAPE ROPE ABOVE CAPTAIN'S WINDOW FELL OUT. REPLACED CAPTAIN'S ESCAPE ROPE PER MM 25-60-02-2.
INSPECTION TYPE:N/A ON PREFLIGHT, EMERGENCY LIGHT INVERTOR INOP. FOUND FUSE P21AB BLOWN. R&R RUSE. OPS CHECK GOOD.
INSPECTION TYPE:N/A ESCAPE ROPE CAPTAINS SIDE FELL OUT ON SHORT FINAL. REPACKED CAPTAINS ESCAPE TAPE PER MM 25-60-02-2.
INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01-2. OPS CHECK NORMAL.
INSPECTION TYPE:SP EMERGENCY LIGHTING FAILED OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW DC8 AMM 33-50-01-2. OPS CHECK GOOD.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW MM 33-50-02-2. OPS CHECK GOOD.
INSPECTION TYPE:C1 EXFOLIATED CORROSION ON WEB AT STA -99 - -80 RBL 30-50. REMOVED CORROSION ON WEB AT STA -99 TO -80 RBL 30-50 IAW SRM 51-1-8 FABRICATED AND INSTALLED SPLICE DOUBLER AND REPAIR DOUBLER AT STA -80 TO -90 RBL 30-50 IAW SRM 51-1-20D, AND DWG 5612298.
INSPECTION TYPE:C1 CRACK AT NR 4 ALT LWR FRONT SPLICE PLATE BETWEEN XRS 428 AND XRS 463. REMOVED CRACKED SPLICE FITTING AT NR 4 ALT TANK LWR FRONT SPAR CAP BETWEEN XRS 428-XRS 463 IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPAIR SPLICE FITTING IAW DWG 3644046, AND SRM 51-03-02, 51-01-20D.
INSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT STA 1050 L31R. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-3-0, 51-1-20D.
INSPECTION TYPE:C1 MAIN CABIN ATTACH FITTING CRACKED AT STA 857.125 L19R. REMOVED FITTING AT STA 857.125 L19R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR FITTING AT STA 857.125 L19R IAW SRM 51-03-02 SRM 51-1-20D.
INSPECTION TYPE:C1 HEAVY CORROSION UNDER SPLICE FITTING, L24R STA 45. REMOVED CORRODED LONGERON SPLICE FITTING AT STA 45-55 L24R IAW SRM 51-1-21. FABRICATED AND INSTALLED L24R SPLICE FITTING AND STIFFENER AT STA 45-55 IAW SRM 53-3-3 FIG 2, 51-3-2, AND SRM 51-1-20D.
INSPECTION TYPE:C1 EXTERIOR FUSELAGE, L-1 DOOR HOLD OPEN RECEPTICAL CUTOUT HAS .375 INCH CRACKED IN AFT LWR CORNER. TRIMMED OUT DAMAGED AREA L-1 DOOR HOLD OPEN CUTOUT AFT LWR CORNER IAW SRM ADDENDUM DC8-5330-19684-A. FABRICATED AND INSTALLED REPAIR DOUBLER AT THE L-1 DOOR HOLD OPEN CUTOUT AFT LWR CORNER IAW SRM ADDENDUM DC8-5330-19684-A.
INSPECTION TYPE:C1 HFEC INSPECTED DETECTED A CRACK ON THE D-PIT UPPER FWD CORNER APPROX .156" ON LWR SIDE OF FASTENER AND .156" UPPER SIDE OF FASTENERS. CUT OUT DAMAGED AREA AT STA 1400 L23R IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND TRIPLER AT STA 1400 L23R D-PIT UPPER FWD DOOR CORNER IAW SRM 53-2-0 FIG 21 AND SRM TR 53-188.
INSPECTION TYPE:C3 CRACKED UPPER RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE. STOP DRILLED CRACK ON UPPER RIB INSIDE PANEL 518A LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED ANGLE DOUBLER ON RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002, AND SRM 51-1-20D.
INSPECTION TYPE:C1 MAIN CABIN LONGERON FRAME AND SHEAR TIE HAS DRILLED STOP MARK AND FRAME HAS SEVERAL OPEN HOLES AT STA 80 L20R. REMOVED DAMAGED SECTION OF FRAME. FABRICATED 2 EACH REPAIR SPLICES, 1 FRAME SECTION AND 1 SHEAR TIE. INSTALLED IAW SRM 53-02-00-0 FIG 002, 51-3-2.
INSPECTION TYPE:C1 SEAT TRACK HEAVILY CORRODED STA 1510 RBL 45. REMOVED SEAT TRACK FROM STA 1490-1550 RBL 45. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-3-0, 53-07-03 FIG 7-3 FIG 003.
INSPECTION TYPE:C1 CANTED FRAME CAP DENTED/GOUGED BEYOND LIMITS, MAIN CABIN STA 1707 L21R. REMOVED DAMAGED FRAME CAP AT STA 1707 L21R IAW SRM 51-1-21. FABRICATE AND INSTALLED FRAME CAP AT STA 1707 L21R IAW SRM 53-2-0, 51-1-20D AND DWG 5612146.
INSPECTION TYPE:C1 L10R END FITTING CRACKED AT STA 1763, MAIN CABIN. REMOVED CRACKED END FITTING AT STA 1763 L10R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 1763 L10R IAW SRM 51-3-2, AND SRM 51-1-20D.
INSPECTION TYPE:C1 R2 DOOR JAMB WEB CRACKED, 2 PLACES, AT DOOR SNUBBER, STA 1618 L15R TO L16R. REMOVED WEB FROM R2 DOOR JAMB AT FS 1618 L15R-L16R IAW SRM 51-1-21. FABRICATED AND INSTALLED WEB AT STA 1618 L15R-L16R IAW DWG 5772656 AND SRM 51-3-2 AND SRM 51-1-20D.
INSPECTION TYPE:C1 CRACK IN END FITTING, L17R, STA 1763, MAIN CABIN. REMOVED L17R END FITTING AT STA 1763 IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED L17R END FITTING AT STA 1763 IAW SRM 51-3-2, AND SRM 51-1-20D.
INSPECTION TYPE:C1 APB BRACKET CRACKED STA 1766 L6L MAIN CABIN. REMOVED, FABRICATED AND INSTALLED APB BRACKET IAW SRM 51-1-21, 51-1-2 0D AND DWG 5773844.
INSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING CRACKED STA 900 L10L. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-2-15.
INSPECTION TYPE:C1 MAIN CABIN FWD OF THE 857.123 L6L END FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE:C1 HOLE DRILLED THRU EDGE OF FRAME, INTO RADIUS, MAIN CABIN STA 1600 L9R. REMOVED SPLICE ANGLE AND CUT OUT DAMAGE, FABRICATED AND INSTALLED -J- DOUBLER AND FILLER IAW EO DC8-5310-11728B AND DWG DC-853A-011A.
INSPECTION TYPE:N/A EMERGENCY LIGHTS BATTERY CHARGING (K5) CB POPPED, TRIED TO RESET & WILL NOT STAY IN. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY & RELAY MODULE IAW MM 33-50-01-2. OPS CHECKS GOOD.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT TEST. SET -EMERGENCY EXIT LIGHTING CONTROL- CIRCUIT BREAKER. EXIT LIGHTS OPERATION NORMAL. REF AMM 33-50-00-0.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. OPS CHECKS NORMAL REF MM 33-50.
ESCAPE SLIDE GAUGE UNREADABLE. DEFERRED M336910. REMOVED & REPLACED CONTAINER COVER ASSY. REINSTALLED LIFE RAFT W/REF TO MM 25-60-01-2. OPS CK NORMAL. THIS CLEARS M336910.
EMERGENCY LIGHTS BATTERIES DISCHARGED. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-50-01-2.
INSPECTION TYPE:N/A LEFT MLG CLOSEOUT PANEL AFT OF MAIN GEAR DOOR TANG CUTOUT IS CRACKED. REPAIRED CLOSEOUT PANEL IAW DC8 SRM CAPT 51-00. INSTALLED NEW Z-CHANNEL IAW DC8 SRM 51-1-21.
INSPECTION TYPE:SP 3 MAIN-CRACK ONE HALF INCH CENTER SPAR AFT SURFACE AT XRS26. REPAIRED CENTER SPAR CAP IAW SAA EA 008-5710-01-A0218, UPS RAA DC8-57-20169.
TAIL COMPT 60 L17R HAS 2.5 IN CRACK AT END FITTING STA 1771 (LWR SURFACE OF UPPER LEG). REMOVED FABRICATED AND INSTALLED L17R STA 1771 IAW SRM'S 53-2-2 FIG10, 51-1-21, 51-1-20D, 51-3-0 AND DWG 5649327.
C3 TAIL 60 COMPT L17LHAS 1.5 CRACK AT END FITTING STA 1771 (LWR SURFACE OF UPPER LEG). REMOVED FABRICATED AND REPLACED LONGERON 17L STA 1771 IAW SRM'S 51-1-21, 51-1-20D, 51-3-0 AND DWG 5649327.
INSPECTION TYPE: C3, RIGHT STA 98 FLAP UPSTOP FITTING CRACKED. GAINED ACCESS TO REPAIR SITE. REMOVED & REPLACED FITTING REF SRM 51-3-0, 51-1-8, 51-1-21, 51-1-15. RESTORED REPAIR AREA.
INSPECTION TYPE:C3, LONGERON SPLICE FITTING CORRODED BEYOND LIMITS, STA 1260 - 1280 L34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8.
INSPECTION TYPE:C3 FUSELAGE SKIN CRACKED AT STA 1350 L35R. CUT OUT DAMAGED SKIN, NDT VERIFIED, ALL DAMAGE REMOVED. FAB FILLER FROM SHT2024T3-.071 & DOUBLER FROM SHT2024T3-.080 REF SRM 51-9-0, 53-2-1 FIG 8, 53-4-0 FIG 21A, 53-4-1 FIG 16. INSTALLED REPAIR PER SRM 51-1-21, 51-1-20D, 51-1-8, 53-2-1 FIG 8.
INSPECTION TYPE:C3, L1 DOOR LOWER HINGE CUTOUT CRACKED ON FRAME. REMOVED LOCAL INTERCOSTAL & SEAL RETAINER TO FOM. STOP DRILLED CRACK & VERIFIED PER NDT/SPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT 2024T3-0 -.071. INSTALLED ALL PARTS REF SRM 52-3-1 FIG 1, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE:C3, RT WING CENTER L/E RIB CRACKED AT XFS 335.25. NDT VERIFIED CRACK TERMINATES AT RIVET HOLE REF SPM06-10-01.001. FAB 2 STACKED REPAIR ANGLES FROM SHT 7075T6-.040. INSTALLED REPAIR PER SRM 57-3-3 FIG 5, 57-2-0 FIG 2, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C3 LOWER NR 5 T-BOLT BACKUP FITTING CORRODED BEYOND LIMITS AT C-PIT TORQUE BOX. REMOVED AND REPLACED FITTING REF SRM 53-2-0 FIG 1F, 51-1-20D.
INSPECTION TYPE: C, CRACK SPLICE FITTING AFT CARGO STA 1040 - 1060, L31R. REMOVED AND REPLACED SPLICE FITTING STA 1040 - 1060, L31R IAW DC8 SRM 51-1-21D, SRM 51-1-8, SRM 51-1-20 AND 51-1-11.
INSPECTION TYPE: C3, LONGERON 35L CRACKED STA 1260-1280. REMOVED 2 CLIPS & 1 INTERCOSTAL AT STA 1270. REMOVED SPLICE FITTING AT STA 1350. REMOVED SPLICE FITTING AT STA 1270. REMOVED AND REPLACED LONGERON SECTION FROM 1270-1350. REINSTALLED ALL FOM PARTS. ALL REF SRM 51-1-20D, 51-1-21, 51-20-00.
INSPECTION TYPE:C3 CRACK INSIDE THE NR 4 -T- BOLT BACKUP FITTING STA 320 REMOVED FITTING TO FOM. FOUND BOTH ATTACH CLIPS CRACKED (-1 & -2). REMOVED & REPLACED BOTH ATTACH CLIPS AND RE-INSTALLED BACKUP FITTING REF SRM 51-1-20D, 51-3-0, 53-2-0 FIG 2D, 51-1-8, 51-1-15.
INSPECTION TYPE:C3 LONGERON 34L CRACKED AT STA 1260-1280. REMOVED SPLICE AT STA 1270 L34L. REMOVED L34L FROM SPLICE AT STA 1350 TO STA 1270. FAB & INSTALL REPLACEMENT LONGERON SECTION FROM 3758593-1 BETWEEN STA 1270-1350 AND SPLICE FITTING AT STA 1270 REF SRM 51-1-21, 51-1-20D, 51-1-8, 51-1-15.
INSPECTION TYPE: C3, BANANA FITTING CRACKED AT STA 1200 LONGERON 26L. CUT WEB ABOVE L27L TO FOM FITTING REMOVAL. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8. REPAIRED WEB REF DWG9751879 USING SHT2024-T3 /.020 PER SRM 53-2-0 FIG 1D, 51-1-21, 51-1-20D.
INSPECTION TYPE:C3, LONGERON 34R CRACKED STA 1260-1280. REMOVED SPLICE FITTINGS AT STA 270 & 1350. OPENED BELLY SKIN FROM L31 LT TO L31 RT TO FOM FROM STA 1300-1350. CLEANED, TREATED, PRIMED AREA. REMOVED AND REPLACED LONGERON 34R FROM STA 1270-1350. REINSTALLED BELLY SKIN & SPLICE FITTINGS REF SRM 51-1-20D, 51-1-21, 51-1-8.
INSPECTION TYPE:C3, CRACKED BANANA FITTING AT STA 1160 LONGERON 33R. GAINED ACCESS TO FITTING. REMOVED AND REPLACED FITTING PER SRM 51-1-20D, 51-1-8, 51-3-0. RESTORED AREA TO ORIGINAL CONFIG.
INSPECTION TYPE:C3, LT WING ATTACHMENT RIB CRACKED AT XW454. CUT OUT DAMAGE, VERIFIED PER NDT SPM06-10-01.001. FABRICATED REPAIR DOUBLER FROM SHT7075-0-.100 & FILLER FROM SHT7075T6-.090 REF DWG 9753297. HEAT TREAT TO T6 PER DPS7.00-1. INSTALLED REPAIR PER SRM 57-2-0 FIG 2 & 2A, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C3 LONGERON 15L CRACKED AT SHEAR TIE STA 1754. REMOVED END FITTING, CLIP, LONGERON SECTION FROM 1744 - 1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 STRAPS FROM SHT 7075T6-.080, SPLICE FITTING FROM S2645716. TREATED, PRIMED, INSTALLED ALL REPAIR & REMOVED PARTS REF SRM 51-1-8, 53-2-2 FIG 10 & 11, 51-1-20D.
INSPECTION TYPE:C3 LONGERON 14L CRACKED UNDER SHEAR TIE AT STA 1756. REMOVED END FITTING, INTERNAL DOUBLER & CLIP. CUT & REMOVED LONGERON SECTION FROM 1747 - 1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 STRAPS FROM SHT7075T6-.080, SPLICE FITTING FROM S2645716. TREATED, PRIMED & INSTALLED ALL REMOVED AND REPAIR PARTS REF SRM 53-2-2 FIG 10 & 11, 51-1-8, 51-1-20D.
INSPECTION TYPE:C3 LONGERON 14R CRACKED UNDER CLIP AT STA 1756. REMOVED DAMAGE SECTION OF L14R FROM APPROX STA 1745-1766. REMOVED SHEAR TIE, END FITTING TO FOM. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 SPLICE STRAPS FROM SHT7075T6-.080, AND 1 SPLICE FITTING FROM S2645716. TREAT, PRIMED, AND INSTALLED ALL PARTS REF SRM 53-2-2, 51-1-8, 51-1-20D, 51-1-21.
INSPECTION TYPE:C3 LONGERON 15R CRACKED UNDER SHEAR TIE AT STA 1754. REMOVED END FITTING AND CLIP TO FOM. REMOVED DAMAGED SECTION OF L15R FROM APPROX STA 1745-1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, SPLICE STRAPS FROM SHT7075T6-.080, SPLICE FITTING FROM S2645716. TREAT, PRIME & INSTALL ALL PARTS REF SRM 53-2-2, 51-1-8, 51-1-21, 51-1-20D.
FLOORBEAM LOWER FWD FLANGE HAS A 4.00 INCH CRACK F/S 920 RBL 65.0. FLOORBEAM SPLICE SEGMENT REPAIRED FROM RBL 31.40 TO RBL 70.0 IAW SAA SK 868-105.
INSPECTION TYPE: C, FINGER DOUBLER AT RBL 70 BETWEEN FS 879 - 902 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FINGER DOUBLER IAW DC8 SRM 51-1-21, DWG 5645332, AND DC8 SRM 51-1-8.
INSPECTION TYPE: C, NR 4 STUB WING INBOARD L/E RIB CRACKED AT L/E. REMOVED, FABBED, AND INSTALLED NR 4 INBOARD STUB WING TAPERED FLANGE IAW DC8 SRM 51-1-21, DWG 9753297, SRM 51-1-8 AND DC8 SRM 51-1-21A.
INSPECTION TYPE: C, CRACKS AFT CARGO PIT STA 1240 L35L. REMOVE EXISTING PRODUCTION SPLICE AND FITTING AND STOP DRILL CRACKS. FAB AND INSTALL SPLICE ANGLE. FAB AND INSTALL FRAME FITTING IAW DC8-SRM 51-1-21, 51-1-20, SR ADD DC8 5320-6176-B, SAA TRAVELER 0073 SRM 51-1-8, AND 51-3-2.
INSPECTION TYPE:C3 LONGERON 15L CRACKED UNDER SHEAR TIE AT STA 1734. REMOVED SHEAR TIE AT STA 1734. REMOVED LONGERON SECTION FROM STA 1766 - APPROX STA 1725. FAB REPLACEMENT LONGERON SECTION FROM EXTRUSION S1616757, 2 SPLICE STRAPS FROM SHT7075T6-.080, -39 SPLICE FITTING FROM EXTRUSION S2645716 & INSTALLED REPAIR REF SRM 53-2-2 FIG 10, 11 51-1-8, EO DC8-5340-8038, 51-1-20D, RE-INSTALLED SHEAR TIE REF SRM 51-1-20D.
INSPECTION TYPE:C3 TORQUE BOX FITTING CORRODED BEYOND LIMITS AT STA 1220 L30L. REMOVED AND REPLACED FITTING REF SRM 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C3, SPLICE FITTING CRACKED ON LONGERON 34R AT STA 600 - 620. REMOVED AND REPLACED FITTING PER SRM 51-1-20D, 51-1-8.
INSPECTION TYPE:C3 RIB CRACKED AT UPPER END, LT WING STA XFS 828.75. STOP DRILLED CRACK AND NDT VERIFIED PER NDT/SPM06-10-01.001. FAB DOUBLER AND FILLER FOM SHT7075T6-.050, TREATED, PRIMED & INSTALLED SAME REF SRM 57-3-0 FIG 20, 57-2-0 FIG 2, 51-1-8, 51-1-21, 51-1-20D, 57-3-3 FIG 7.
INSPECTION TYPE:C3, FOUND CRACKED CLIP IN MAIN CABIN, LONGERON 3L. FABRICATED REPLACEMENT CLIP FROM SHT2024T3-.040 REF DWG 5772678. REMOVED & REPLACED CLIP REF SRM 51-1-8, 51-1-20D.
INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD HORIZONTAL -J- BEAM CRACKED, AFT SIDE, NEAR L13R. STOP DRILLED CRACK, VERIFIED REF SPM06-10-01.001. FABRICATED REPAIR PARTS FROM SHT 7075-0-.100. HEAT TREATED TO T6. INSTALLED REPAIR REF EO DC8-5310-6598-C.
INSPECTION TYPE:C3, LEFT WING CENTER L/E INTERNAL DOUBLER CRACKED BETWEEN XFS 422.75 & XOLDI 6.225. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6-.080 PER DWG 5769891. REMOVED & REPLACED DOUBLER PER SRM 51-1-8, 51-1-20D, 51-1-21, 51-1-15.
INSPECTION TYPE: C, RT WING O/B LEADING EDGE HAS CRACKED UPPER RIB AT STA 776. REMOVED FASTENERS, STOP DRILLED, FABBED AND INSTALLED FILLER IAW DC8 SRM 51-1-21, 57-2-0, 57-3-3 FIG 7, 57-2-0 FIG 2, 51-1-8, AND 51-1-20D.
INSPECTION TYPE:C3, LEFT WING O/B LEADING EDGE LOWER INTERNAL DOUBLER CRACKED NEAR XFS 623. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6-.080 REF DWG 5769545. REMOVED & REPLACED DOUBLER REF SRM 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C3 INNER DOUBLER CRACKED AT DRAIN HOLE NEAR XFS 591, RIGHT WING O/B LEADING EDGE. REMOVED OLD REPAIR DOUBLER, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL FAB REPLACEMENT INTERNAL DOUBLER FROM SHT7075T6-.080. REMOVED AND REPLACED INNER DOUBLER AND REINSTALLED REPAIR DOUBLER, REF SRM 57-2-1 FIG 3A, 51-1-21, 51-1-8, 51-1-20D, DWG 5769545, NDT SPM 06-10-01.001.
INSPECTION TYPE: C3, INBOARD END FITTING CRACKED AT RIGHT OUTBOARD SLOT UPPER DOOR. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-3-0, DWG 3770144. OPS CHECK SLOT PER AMM27-80-05-4, 27-80-00. CHECK GOOD.
INSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 847. STOP DRILLED CRACK, VERIFIED STOP DRILL REF NDTSPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT7075T6-.050. INSTALLED REPAIR REF SRM 51-1-21, 51-1-20D, 51-1-8, 57-2-0 FIG 6, 57-3-3, 57-2-0 FIG 2.
INSPECTION TYPE:N/A CIRCUMFERENTIAL TIE STRAP BELOW AFT DOOR FRAME AT LOWER DOOR CUTOUT HAS EXFOLIATION CORROSION. ACCOMPLISHED EO DC8-5310-20796 BLENDED OUT CORROSION. REPEAT INSP'S AT EVERY C-CHECK PERFORMED VLT THICKNESS CK & HFEC PER UPS EO DC8-5310-20796. NO CRACKS DETECTED. XFRD TO D284984.
INSPECTION TYPE:N/A, NR 3 PIT DOOR CUTOUT AT LWR AFT CORNER HAS CRACK AT DOUBLER. REMOVED CRACKED FITTING & ATTACHING FITTINGS. DRILLED UP NEW FITTINGS, OK TO INSTALL. INSTALLED 80 PERCENT OF FASTENERS IN NEW FITTING. COMPLETED NEW INSTALLATION OF NEW FITTING & ATTACHING FITTINGS PER SRM 51-1-20D.
INSPECTION TYPE:N/A WILL NOT MAINTAIN PRESSURIZATION. EMERGENCY DELARED AND REQUESTED IMMEDIATE DESCENT PER EVENT REPORT. FOUND LEFT ACM TEMP UNCONTROLLABLE. R/R'D LEFT ACM PER 21-55-01-4 OPS CHECKS GOOD.
LOST PRESSURIZATION IN FLIGHT - CABIN ALTITUDE CLIMBED AT A RAPID RATE
INSPECTION TYPE: C-2, FORWARD PIT STA 140, BL45R AT CUSP, SUPPORT FITTING CORRODED. FABRICATED NEW PART IAW DAC DWG 5613430. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED AND DRILLED IAW DAC DWG 5613430 AND DC8 SRM 51-1- 20. INSTALLED FITTING IAW DC8 SRM 51-1-20D. REINSTALLED MAIN CABIN SIDEWALL PANEL AT STA 100-150 R AND FWD PIT PANEL AB40 IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C-2, AFT PIT DOOR SLIDE AREA STA 1210 BETWEEN LONG 31R-32R END FITTING CORRODED. REMOVED EXISTING FITTINGS, LOCATED, DRILLED AND DEBURRED NEW FITTINGS P/N 3754930-1N, 5894282-501, & 5894282-502 IAW DC8 SRM 51-3-2 AND INSTALLED FITTINGS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C-2, FWD CARGO PIT FUSELAGE FRAME LOWER FLANGE CORRODED STA 500 L34L-L35R. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. FABRICATED -5 & -7 REPAIR PARTS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABRICATED SHIMS .080 7075-T6 (PO 395941.1) IAW DC8 SRM 53-2-0. ALODINED AND PRIMED SHIMS IAW DC8 SRM 51-1-8. INSTALLED SHIMS, -5 &-7 REPAIR PARTS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C-2 SEAT TRACK -D- FROM STA 1020 TO 1060 CORRODED ON UNDERSIDE AT CLIP NUTS. REMOVED DAMAGED TRACK, REPLACED WITH NEW TRACK AND UPS SPLICES.
INSPECTION TYPE: C-2, SEAT TRACK FOUND CORRODED AT STA 1580 TRACK -H- UNDER SIDE. REMOVED DAMAGED SEAT TRACK, REPLACED PER DC8 SRM 53-2-3 AND 51-3-0.
INSPECTION TYPE: C2, AT STA 1540 STR 24L CRACK INSIDE OF HAT SECTION OF STRINGER AFT PIT. REMOVED DAMAGED SECTION OF LONG IAW DC8 SRM 53-2-2,TR 53-153. FAB NEW SECTION OF LONG FROM EXT S141597 IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, DRILLED 2 SPLICES TO FIT IAW DC8 SRM 53-2-2 FIG 10 TR 53-153. INSTALLED LONGERON SECTION AND 2 SPLICES IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C-2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK -D- STA 1219 SCOLLOPS WORN. REMOVED AND REPLACED TRACK SECTION AND SPLICED PER UPS EO DC8-5320-5 167-C.
INSPECTION TYPE: C-2, AFT FUSELAGE SECTION STA 1690 PRODUCTION RING IS CORRODED BETWEEN L2 6L-L28L. REMOVED AND REPLACED SPLICES AND RING ANGLE SECTION AT L26R, L26L, L34L, & L28R DUE TO CRACKED AND CORRODED IAW DC8 SRM 53-2-5 FIG 8C-1 SHT 1, 51-1-20D, & DAC DWG 5612141.
INSPECTION TYPE: C2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK F STA 774 HAS WORN SCALLOPS. BLENDED SCALLOP AND FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGE AREA IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C-2, MAIN CABIN SEAT TRACK -E- GOUGED AT FS 220. REMOVED DAMAGE SEAT TRACK, REPLACED WITH NEW TRACK AND UPS SPLICES IAW UPS EO DC8-5320-5167-C & DC8 SRM 53-2-3.
INSPECTION TYPE: C-2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK -E- STA 596 WORN. REMOVED AND REPLACED TRACK SECTION IAW DC8 EO-5320-5167-C.
INSPECTION TYPE: C2, MAIN CABIN SEAT TRACK G GOUGED AT FS 280. DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGE SCOLLOPS IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED PART IAW DC8 SRM 53-2-3. INSTALLED PART IAW DC8 SRM 53-2-3.
INSPECTION TYPE: C-2, R2 AFT SERVICE DOOR HAS CRACK INDICATION AT LOWER AFT CORNER FOUND BY RADIOGRAPHIC INSPECTION. REMOVED AND ROUTED OUT CRACK IN DOOR PAN. FABBED REPAIR IAW DC8 SRM 53-2-0 AND DAC DWG 5772789. REINSTALLED DOOR PAN STOPS, AND GUIDES IAW DC8 SRM 51-1-21 AND 51-3-0.
INSPECTION TYPE: C2, SEAT TRACK WORN FS 710 LBL 50 DOT EO314. BLENDED AREA AND FOUND OUT OF LIMITS AT FS 685 AND 690. ROUTED OUT DAMAGE IAW DC8 SRM 53-2-3. ALODINED, PRIMED AND INSTALLED PLUG IAW DC8 SRM 53-2-3.
INSPECTION TYPE: C2, ALL STA 1400 L30R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVEED CORRODED FITTING IAW DC8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C-2, ALC STA 1400 L33R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C-2, INT CABIN CANTED FRAME AFT OF 1710 FRAME DEEP CHAFE ON TRIPLER LONG 29L. INSTALLED DOUBLER ON FRAME IAW UPS DWG DC8-53A-011 AND EO DC8-5310-1 1728-A.
INSPECTION TYPE: C-2, LOWER EXTERIOR FUSELAGE AT STA 1690 BOTTOM AREA SKIN SIGN OF BULGING. CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED SKIN, FABBED NEW SKIN SECTION IAW DGIS DWG 5649329. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW SKIN SECTION IAW DGIS DWG 5649329 AND DC8 SRM 51-1-21.
INSPECTION TYPE: C-2, AFT PIT SEAT TRACK CORRODED AROUND CLIPNUTS. NUT PLATES IN SEVERAL ARE AS STA 980 TO 1260. REMOVED DAMAGE SEAT TRACK. INSTALLED NEW TRACK AND UPS SPLICE PARTS IAW DC8 SRM 51-3-0.
INSPECTION TYPE:C-2 CRACK INDICATION THROUGH PAINT AT RT AFT TYPE 2 EMERGENCY EXIT DOOR CUTOUT UPPER AFT CORNER STA 1340 L12R. REMOVED FASTENERS IN REPAIR AREA, CUTOUT CRACKED AREA OF OUTER SKIN AND FABRICATED -15 DOUBLER -17 DOUBLER AND -19 FILLER IAW TINCO REO-G 08971. ALODINED AND PRIMED -15, -17, -19 IAW DC8 SRM 51-1-8. INSTALLED -15, -17, AND -19 IAW REO G08971.
INSPECTION TYPE: C-2, R1 UPPER FWD DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT FASTENER HOLE OF FIRST FASTENER ROW AT APPROX 45 DEGREES POINT OF CORNER RADIUS. REMOVED DAMAGE AREA, FABBED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 53- 2-0 AND REVISION 53-154. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE: C-2, FUSELAGE EXTERIOR SKIN CRACKED STA 1750 L15L-16L. CONFIRMED CRACK WITH HFEC IAW NDT SPM 06-10-01. FABRICATED FILLER AND DOUBLERS IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, INSTALLED FILLER AND DOUBLERS IAW DC8 SRM 51-1-20D AND 51-1-21, CONFIRMED CRACK REMOVED IAW HFEC IAW 06-10-01, CLOSED UPPER AND LOWER SIDEWALL PANELS IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C-2, L2 LWR FWD DOOR JAMB CORNER EXTERNAL FUSELAGE SKIN CRACKED AT SECOND FASTENER HOLE BELOW TRIMOUT. ROUTED OUT CRACKED AREA IAW DC8 SRM 53-2-0. VERIFIED CRACK REMOVED IAW NDT SPM 06-10-01.001. FABBED -7 & -9 DOUBLERS AND -19 FILLER IAW DC 8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -7 & -9 DOUBLERS & -19 FILLER IAW DC8 SRM 53-2-0. EDGE SEALED IAW DC8 SRM 51-1-11. INSTALLED DUCTS IAW DC8 MM 20-11-00.
INSPECTION TYPE: C-2, R1 LOWER AFT DOOR JAMB CORNER HAS A CRACK FOUND WITH NDT. REMOVED DAMAGE IAW DC8 SRM 53-2-0. FABBED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 53-2-0.
INSPECTION TYPE: C-2, L2 UPPER AFT DOOR JAMB CORNER HAS A CRACK FOUND WITH NDT. CUT OUT CRACKED AREA IAW DC8 SRM 53-2-0 FIG 18. VERIFIED CRACK REMOVAL IAW MD NDT SPM 06-10-01.001. FABIRCATED AND INSTALLED DOUBLER, TRIPLER AND SKIN FILLER IAW DC8 SRM 53-2-0 FIG 18. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY UNIT IAW MM 33-50-01, OPS OK.
INSPECTION TYPE:IN 2 ADJACENT CRACKS AND DISTORTION IN PIT 31 DOOR LOWER EDGE NR 1 PIT DOOR HAS 2 CRACKS IN LOWER SKIN APPROX 14 INCHES FROM TRAILING EDGE. TRIMMED OUT DAMAGED SKIN ENCOMPASSING BOTH CRACKS AND INSTALLED NEW FASTENER, PER EO DC8-5230-14302.
IN CLIMB OUT, KEPT INCREASING FLOW TO MAINTAIN DESIRED CAB PRESS FOR F L330. APPROX 5 MIN AFTER REACHING FL330 WE LOSSED CONTROL OF BOTH AUTO AND MANUAL CAB CONTROL. CABIN REACHED FL230 RAN CHECKLIST AND DESEN DED TO FL230. FOUND AIR LEAK AT THE NR 3 PIT DOOR. CHECKED DOOR SEAL & EXTERNAL LATCHING MECH. FOUND LOWER DOOR HOOK RIDE UP ON TEE BOLT IF DOOR NOT SHUT RIGHT (REF LP023577) DEFERRED M263884. REF LP 23583 - RERIGGED DO OR PER MM 52-31-00 OPS CHECK GOOD, THIS CLEARS M263884.
INSPECTION TYPE:IN ON PDC FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01. OPS CHECKS GOOD.
INSPECTION TYPE: IN, AILERON POWER S/O LEVER FROZEN. CLEANED AND LUBED AILERON HYD S/O CABLES GOING THRU BULKHEAD IN LT W/W CABLES HAD BUILD UP OF ANTI CORROSION COMPOUND. SYS OPS CKS GOOD PER MM 27-10-00.
INSPECTION TYPE:C1 FWD PIT STA 385 LONG 31L HAS CORROSION FWD OF SPLICE. REMOVED PRODUCTION SPLICE IAW DC8 SRM 51-1-24, CLEANED AREA IAW DC8 SRM 51-1-8, LOCATED DRILLED PRODUCTION SPLICE IAW DC8 SRM 51-3-2, INSTALLED PRODUCTION SPLICE IAW DC8 SRM 21-1-20D.
INSPECTION TYPE:C1 FWD CARGO PIT STA 320 L 34R - 35R FITTING IS CORRODED. REMOVED Z-FITTING, FAB SPLICE AND DRILLED NEW FITTING IAW SRM 53-2-0, ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21D.
INSPECTION TYPE:C1 STA 1265 LONGERON 35R LONGERON SPLICE CRACKED. REMOVED LONGERON SPLICE IAW DC8 SRM 51-1-20D, RECEIVED NEW SPLICE P/N 3759258 -2N S/N TAG 0049957, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1 -24, INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C1 BEAM FITTING ABOVE RT AFT O/W EXIT L14R HAS EXFOLIATION RUNNING ALONG FASTENER HOLES. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D 51-1-21 AND 51-3-0.
INSPECTION TYPE:C1 AFT PIT STA 1040 SHEAR CLIP FWD SIDE BETWEEN L36 & L35L IS EXFOLIATED. REMOVED CORRODED SECTION OF SHEAR TIE, FABED NEW SECTION OF SHEAR TIE ALODINED AND PRIMED INSTALLED NEW SECTION OF SHEAR TIE IAW DC8 SRM 53-2-0 & 51-1-8.
INSPECTION TYPE:C1 AFT PIT STA 1060 FRAME CAP CORRODED ABOVE LONG 36. REMOVED CORROSION IAW DC8 SRM 51-1-8, AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. DRILLED, REAMED NEW HOLES IAW DC8 SRM 51-3-2, INSTALLED NEW FRAME CAP IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C1 MAIN CABIN STA 1750 BEAM SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C1, FITTING CRACKED AT FS 834 APPROX 70 INCHES BELOW LT CUSP. REMOVED AND REPLACED FITTING AT FS 834 10 INCHES BELOW CUSP LINE IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C1, MAIN CABIN FITTING CRACKED L19RT AT FS 857. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C1, FS 1160 L34L-L35L Z-FITTING IS CORRODED. REMOVED CORRODED FITTING, RECD NEW ONE ACQUIRED MAT ID FOR REPAIR ANGLES AND FABED ALODINED AND PRIMED ALL BARE AREAS AND INSTALLED FITTING AND REPAIR (REF) DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
INSPECTION TYPE:C1 MAIN CABIN LT STA 1250 LONG 10L IS CORRODED. REMOVED AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2.
INSPECTION TYPE:C1 MAIN CABIN LT STA 1250 LONG 10L IS CORRODED. REMOVED AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2.
INSPECTION TYPE:C1 MAIN CABIN STA 1100 LONG 9L IS CORRODED. REMOVED AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2.
INSPECTION TYPE:C1, MAIN CABIN RT CUSP WEB HAS 2 PUNCTURES AND A CRACK BETWEEN FS 520 & FS 540. REMOVED DAMAGED AREA IAW DC8 SRM 53-2-0, FABBED REPAIR PARTS AND INSTALLED IAW DC8-5330-2159.
INSPECTION TYPE:C1, FWD PIT STA 363 BETWEEN LONG 35L AND 35R SKIN HAS CORROSION AND BARE METAL. REMOVED CORROSION AT FWD PIT STA 363 BETWEEN L35L AND 35R IAW DC8 SRM 51-1-8, ALODINED 7 PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE:C1, T-FITTING BENEATH KEEL BEAM IN LT WHEEL WELL IS CRACKED FS 920. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, INSTALLED CENTER SKIN IAW DC8 SRM 51-3-0.
INSPECTION TYPE:C1, FWD CARGO COMPT LONGERON 34R CRACKED AT FS 550. REMOVED LONG SECTION 34R FROM STA 345 TO 630 IAW DC8 SRM 51-1-21, REMOVED SHEAR TIE SECTION FROM STA 460 - 480 TO FOM IAW DC8 SRM 51-1-20, 51-2-0, FABED SHEAR TIE, REPAIRS INSTALLED, LONGERON AND REPAIR PARTS IAW DC8 SRM 51-1-21.
INSPECTION TYPE:C1 FWD CARGO COMPT STA 550 LONG 34R CRACKED. REPAIRED LONGERON PER DC8 SRM 53-2-2 AND SHEAR TIES PER DC8 SRM 53-2-0.
INSPECTION TYPE:C1 FWD CARGO PIT AT FS 510 - 520 LONG 33R IS CRACKED AT UPPER I/B FLANGE. REMOVED LONGERON 33R FS 395 TO FS 650 IAW DC8 SRM 51-1-20, LOCATED AND DRILLED NEW LONGERON IAW DC8 SRM 51-1-24, INSTALLED NEW LONGERON 33R AND TORQUE BOX CLOSEOUT IAW DC8 SRM 51-1-20D, INSTALLED KICKPLATE IAW DC8 SRM 51-1-20.
INSPECTION TYPE:C1, FWD CARGO PIT AT FS 120 AT LONG 39R 30R FRAME HAS BROKEN OUT PIECE OF METAL AND IS CRACKED. REPAIRED FRAME IAW EO DC8-5310-11728A.
INSPECTION TYPE:C1 FWD CARGO PIT AT FS 220 - 240 LONGERON 35R IS CORRODED. REPAIRED LONGERON PER DC8 SRM 53-2-2 FIG 10.
INSPECTION TYPE:C1, FWD PIT TORQUE BOX STA 320 L27L HAS CRACKED Z-FITTING. REMOVED FITTING, FABBED DOUBLER IAW 53-2-0, ALODINED AND PRIMED IAW SRM 51- 1-8, INSTALLED IAW 51-1-21.
INSPECTION TYPE:C1, FWD PIT STA 350 FITTING BETWEEN LONG 35L & 36L IS CRACKED. REMOVED Z-FITTING, FABBED SPLICES IAW SRM 53-2-0, ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED IAW 51-1-21.
INSPECTION TYPE:C1, FWD PIT STA 390 BETWEEN LONG 32R & 33R SKIN IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8 MAT ID FOR EXTERNAL DOUBLER 7075-T6 .03 2 IAW DC8 SRM 53-4-1. FABD DOUBLER IAW DC8 SRM 53-2-1, ALODINED AND PRIMED DOUBLER AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-21 AND 51-1-20D. INSTALLED SPLICERS AND LONGERON AND SHEAR TIE IAW DC8 SRM 51-1-20D & 51-1-21.
INSPECTION TYPE:C1 C2 DOOR JAMB WEB HAS CRACK EMINATING FROM NUT PLATE HOLE STA 545. REMOVED DAMAGED AREA IAW DC8 SRM 53, FABD REPAIR ANGLE IAW DC8 SRM 53-2-0, HEAT TREAT 2024-0 TO 2024-T4, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0.
INSPECTION TYPE:C1, MAIN CABIN FITTING CRACKED INSIDE OF INTERCOSTAL L19 RT AT FS 834. REMOVED CRACKED FITTING, DRILLED NEW FITTING (P/N 37799782) TO FIT IAW DC8 SRM 51-1-24, INSTALLED FITTING WITH HI-LOKS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:N/A WHILE BEING VECTORED FOR AN APPROACH INTO SDF, SMOKE & FUMES WERE EX PERIENCED IN THE COCKPIT. BOTH EFIS SCREENS ON THE CAPT'S SIDE WENT BLANK & SOME KIND OF POWER SURGE WAS HEARD. SHORTLY THEREAFTER THE CAPTS EFIS SCREENS RETURNED TO OPERATION. R/R NR 1 DPU.
INSPECTION TYPE:N/A, AFTER LANDING GEAR HANDLE SELECTED UP, A LARGE BANG WAS HEARD WITH A FOUL SMELL THROUGHOUT THE COCKPIT, NO OTHER ABNORMAL INDICATIONS. EMERGENCY DECLARED WITH CENTER CONTROLLER. INSPECTED AIRCRAFT FOR DAMAGE CHECKED INLETS FOR FOD AND BIRDS. RAN PACKS AND CHECKED FOR LEAKS AND ODOR, NO SMELL NOTED. AIRCRAFT STILL NEED GEAR SWING. FOUND RIGHT DUCT BLOWN OFF AFT OF COALESCER ASSY. RE-ATTACHED DUCT, GEAR OPS CHECK NORMAL.
INSPECTION TYPE:N/A, INFLIGHT EMERGENCY COCKPIT LIGHTS ARE ILLUMINATED WHEN EMERGENCY LIGHT SWITCH WAS IN THE ARMED POSITION. INSPECTED SYSTEM AND DISCOVERED POPPED C/B. RESET BREAKER AND OPS CHECK EMERGENCY LIGHTING SYSTEM. SYSTEM OPERATES NORMAL.
EMERGENCY EXIT LIGHTS INOP. ON PRE-FLIGHT CK, REMOVED AND REPLACED EMERGENCY BATTERY PACK. SYSTEM OPS CK GOOD.
INSPECTION TYPE:N/A, DURING MECHANICS PRE-DEPARTURE EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK, SYS OPS NORMAL PER 33-50-01.
UPON TAXI, CREW DETECTED SMOKE IN COCKPIT AFTER PREF CHECK WAS ACCOMPLISHED, SUSPECT ELECTRICAL. PERFORMED A/C GENERATOR MAINT PRACTICES IAW MM 24-20-00. ALL CHECKS GOOD, NO EVIDENCE OF SMOKE IN COCKPIT. AIRCRAFT OK FOR SERVICE.
INSPECTION TYPE-N/A, ON DESCENT NR 2 ENG SLIGHT VIBRATION AND COMP STALL PLUS OR MINUS 10 TO 15 PERCENT, N1 FLUCT, NO TEMP CHANGE. PUSHED THROTTLE UP TO TROUBLESHOOT AND ENG FLAMED OUT. SHUTDOWN ENG IN ACCORDANCE WITH QRH.
INSPECTION TYPE-C123, STA 1580 TO 1620 LT CUSP WEB BARE METAL AND CORROSION. REMOVED CORROSION, NOT WITHIN LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED DAMAGED SECTION OF CUSP IAW DC8 SRM 51-1-20D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE:D, STA 70, L20L REPAIR ON FRAME TOP CORNER CRACKED, GOUGED ON LWR AFT EDGE REPAIRED IAW REO-06184.
INSPECTION TYPE-C123, TRAP FITTING AND O/B VERTICAL STIFFENER HAVE ELONGATED HOLES ON LT SIDE. BUSHINGS MATERIAL ID AND FABRICATION ON UPS NR 244479. INSTALLED BUSHINGS PER REO 06222. INSTALLED O/B VERTICAL STIFFENER IAW DC8 SRM 51-1-20D, 2 BOTTOM BOLTS TO BE INSTALLED ON UPS N/R 244479.
INSPECTION TYPE:D, MAIN CABIN FRAME CRACKED AT STA 200 L20R. FAB REPAIR ANGLE AND FILLER IAW REO 06149 AL AND PRI IAW DC8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:D, FS 857-869 INTERCOSTAL CORROSION AT RADIUS 1ST INTERCOSTAL INBD OF SKIN FITTING. REPLACED INTERCOSTAL WITH NEW INTERCOSTAL.
INSPECTION TYPE-C123, AFT PIT FS 1020 BETWEEN L33R AND L32R CIRC FRAME CORRODED. CORROSION OUT OF LIMITS. REPLACED FRAME SECTION IAW DC8 SRM 53-2-0 AND 53-4-1 AND 51-1-20D.
INSPECTION TYPE:C123, AFT PIT FS 1000 CIRC FRAME AT LONGERON 36 CRACKED AND HAS SHEARED FASTENERS. REMOVED DAMGED FRAME IAW SRM 53-2-0. FAB NEW ONE IAW DAC DWG 9755885 AND REO-06189. INSTALLED IAW REO-06189 AND DC8 SRM 53-2-0.
INSPECTION TYPE:D, FILLET PNL 191AA HAS CORROSION AND BARE METAL A-708 RACK NR 25. FAB -3 PANEL, -5 AND -7 FILLERS IAW DAC DWG 5701940. ALODINED AND PRIMED PANEL L AND FILLER IAW DC8 SRM 51-1-8. INSTALLED FILLERS IAW DC8 SRM 51-1- 21 AND DC8 SRM 71-2-2.
INSPECTION TYPE-C123, STA 1540, L334R HAS SHEARED FASTENERS THROUGH SKIN. FABBED REPAIR CHANNEL AND FILLER IAW REO 06201, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21D.
INSPECTION TYPE:D, AFT PIT FS 1040 T-CAP AT L33L CORRODED UNDER NUT PLATE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. FAB REPAIR ANGLE DOUBLER AND FILLER IAW DAC 08-53-0229. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DAC 08-53-0229.
INSPECTION TYPE-C123, RT WING L/E LOWER T-CAP FLANGE, STA XRS505 ANGLE CRACKED. REMOVED DAMAGE FROM FLANGE FAB DOUBLER FOR REPAIR IAW DAC DRAWING NR R08570014. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-3-0.
INSPECTION TYPE-123D, LT WING O/B LEADING EDGE STA 495 FRAME CRACKED AT PNEU DUCT SUPPORT. FABRICATED DOUBLER IAW DC8 SRM 57-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C123, STA 1180 RT AT C3 DOOR CUTOUT FLOORBEAM FITTING CRACKED. REMOVED CRACKED FITTING AND REPLACED WITH NEW FITTING IAW DC8 SRM 51-1- 24, 51-1-20D AND 51-3-0.
INSPECTION TYPE:D MAIN CABIN, CORROSION ON INSIDE OF UPPER LIP ON LONG 12R STA 781-798. REMOVED CORROSION INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL.
INSPECTION TYPE:D, LWR BULKHEAD TEE FITTING CRACKED INSIDE NR 1 MAIN TANK AT XW408 FROM STR 63 TO CORNER FITTING AT FRONT SPAR, VERIFIED WITH HFEC. RECEIVED NEW FITTINGS AND INSTALLED IAW DC8 SRM 51-1-28.
INSPECTION TYPE:D, AFT PIT LT TUNNEL FS 1220 AT L27L INSIDE TQ BOX HAS CRACKED FITTING. REMOVED DAMAGED FRAME SECTION FAB REPLACEMENT FRAME PER DAC DWG 9754 921. INSTALLED PER DC8 SRM 51-1-20D.
INSPECTION TYPE:D, STA 50, LBL 29 INTERCOSTAL CORROSION INBD LWR SIDE. REMOVED CORROSION, INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL. REMOVED CORROSION FOUND OUT OF LIMITS, FABBED REPAIR DOUBLER, ALODINED AND PRIMED INSTALLED REPAIR DOUBLER.
INSPECTION TYPE-C123, MAIN CABIN HAS CORROSION ON INSIDE UPPER AND LOWER LIP ON LO9NG 11R STA 781 TO 798. REMOVED CORRODED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL.
INSPECTION TYPE:D, AFT ACC STA 1690 L22R END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C123, LT WING LOWER LEADING EDGE I/B STA XWO ANGLE CRACKED AT O/B END OF ANGLE. FAB DOUBLER IAW 57-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-21. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:D, MAIN CABIN CORROSION ON LONGERON 19R INTERCOSTAL STA 680-702. REPLACED CORROSION INTERCOSTAL WITH NEW INTERCOSTAL.
INSPECTION TYPE:D, RT CENTER TAIL CONE SKIN STA 1916-1951 IS CORRODED. FAB NEW SKIN IAW DC8 DAC DWG 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.
INSPECTION TYPE:D, LT CENTER TAIL CONE SKIN STA 1916-1951 IS CORRODED. FAB NEW SKIN IAW DC8 DWG 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.
INSPECTION TYPE:D, LT MOST FWD TAIL CONE SKIN STA 1890-1916 IS CORRODED. FAB NEW SKIN IAW DAC DW3G 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.
INSPECTION TYPE-C123, FRAME AT STA 1889 IS CORRODED AND HAS DOUBLE DRILLED HOLES. REMOVED PREVIOUS CAP FRAME AND SPLICE ANGLES. GEN REO FOR REPAIR INFO. FABRICATED NEW FRAME SECTION AND 4 SPLICE ANGLES. ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS PER REO 06060.
INSPECTION TYPE-123D, LT ELEVATOR T/E STA XE117 FAIRING ATTACH HOLE CRACKED. REPAIRED AREA IAW DC8 SRM 55-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE-123D, MAIN CABIN LONG 6L END FITTING CRACKED FWD SIDE OF STA 857 FRAME. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-123D, MAIN CABIN LONG 10R END FITTING CRACKED FWD SIDE OF STA 680 FRAME. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-123D, MAIN CABIN LONG 6R END FITTING CRACKED FWD SIDE OF STA 857 FRAME. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-123D, MAIN CABIN LONG END FITTING FWD SIDE OF STA 680 FRAME. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-123D, MAIN CABIN, LONG 3L END FITTING CRACKED FWD SIDE OF STA 680. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:D, RT MOST FWD TAIL CONE SKIN STA 1890-1916 IS CORRODED. FAB NEW SKIN IAW DAC DWG 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.
INSPECTION TYPE-C123, AFT PIT STA 1135 L23R Z-FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:D, CORROSION BEHIND EMERGENCY STRAP BRACKET LT OVERWING ENTRY. REMOVED CORROSION BRACKET AND INSTALLED NEW BRACKET. REMOVED CORROSION OUT OF LIMITS AFT BLEND. GEN RFTS, MAT ID 7075T6.063. OK TO FAB. FABBED, OK TO ALODINE AND PRIME. ALODINED AND PRIMED AND INSTALLED.
INSPECTION TYPE:D, CORROSION BEHIND EMERGENCY STRAP BRACKET, LT OVERWING ENTRY. REMOVED BRACKET, FABBED NEW ONE IAW DAC DWG 5779947 AND REO 06168. INSTALLED IAW DAC DWG 5779947.
INSPECTION TYPE-C123, STA 160R SIDE FRAME BOTTOM IS CRACKED. REPLACED DAMAGED SECTION OF FRAME.
INSPECTION TYPE-C123, LT HAND SKI FITTING IN CTR TANK LEAKING FUEL. REMOVED AND REPLACED SKI FITTING IAW REO-06186.
INSPECTION TYPE-123D, FUSELAGE SKIN REPLACEMENT NEEDS REPAIR SPLICES BOTH SIDE (LT& RT). CUT SKIN PANEL 5750365 (AT APPROX 690), FABRICATED REPAIR SPLICE LONG ERON STRAPS INTERNAL AND EXTERNAL DOUBLER WITH FINGER DOUBLER IAW DC8 SRM 53-2-1 AND REO 06044.
INSPECTION TYPE:D, SKIN FWD OF TAIL CONE AT STA 1885 IS BULGED AND DENTED. FAB NEW SKIN SECTION IAW DAC 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALL IAW DC8 SRM 51-1-21.
INSPECTION TYPE-C123, LONG 24L CRACKED AT STA 870. REMOVED AND REPLACED LONG 24L.
DURING ENGINE START OF NR 2 ENG F/O NOTICED SMOKE COMING FROM AROUND F/O'S INST PANEL AND BELOW. CREW SHUT DOWN ENG'S AND EVAC A/C TURNED ON COCKPIT LIGHTING. POWERED UP ALL COCKPIT INSTRUMENTS. COULD NOT LOCATE ANY SHORTED WIRING OR BURNED LIGHTING BALLAST. ALL SYSTEM APPEAR TO OPERATE NORMALLY. A/C OK FOR CONTINUED SERVICE.
INSPECTION TYPE-C, FS 55 LBL 25 TO 33 FLOORBEAM HAS NUMEROUS HOLES BROKEN OUT ON EDGE OF FLOORBEAM. REPAIRED IAW DHC-SK-868-115.
INSPECTION TYPE-C, INTERCOSTAL ATTACH ANGLE AT FS 882 RBL 61 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20D 53-2-0.
INSPECTION TYPE-C, FS 1700 LONGERON 29L HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONG IAW SRM 53-2-0 FROM FS 1690 TO 1705.
INSPECTION TYPE-C, FS 1690 AT LONGRON 29L END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, AFT ACCESSORY COMPT FS 1660 FLOORBEAM RBL 44 IS CORRODDED BEYOND LIMITS. REPAIRED IAW DHC SK-868-794.
INSPECTION TYPE-C, LONGERON 31R I/B END FITTING AT FS 70 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-3-0.
INSPECTION TYPE-C, FS 1690 LONGERON END FITTING CRACKED JUST ABOVE L-21L. REMOVED AND REPLACED FITTING IAW SRM 5-1-20.
INSPECTION TYPE-C, FS 640 BETWEEN LONGERON 35L AND 36 FITTING CRACKED ON LOWER FLANGE. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C, FS 1655 TO 1690 LONGERON 33L CRACKED AT END. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D AND 5757778-1.
INSPECTION TYPE-C, FS 280 FRAME AT L-34 AND 35R HAS CORROSION REMOVAL BEYOND LIMITS. REPAIRED IAW SRM 51-1-21, 51-1-20D, AND DHC SK-868-939.
INSPECTION TYPE-C, FRAME FS 55 FORMER BETWEEN LONGERONS 34L TO 34R HAS PREVIOUS REPAIR, CUT IN HALF AND CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FORMER IAW SRM 51-1-21 AND DWG 5613836.
INSPECTION TYPE-C, FRAME LOWER FLANGE FS 1060 FROM LONG 36 TO 34R HAS CORROSION REMOVAL BEYOND LIMITS. REPAIRED IAW SRM 53-2-0, 51-1-20, AND 51-1-21.
INSPECTION TYPE-C, AFTER GAINING ACCESS TO MCD FRAME ON NR 674396, FOUND ADDITIONAL DOUBLE DRILLED HOLES AND 2 HOLES THAT WERE FLUSH PLUGGED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FRAME IAW SRM 51-1-21, 51-1-20D, 51-3-0, AND DWG 5772787.
INSPECTION TYPE-C, FS 34 BTWN LONG 34L AND 34R SHEAR TIE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 51-1-21 AND DWG 5613836.
INSPECTION TYPE-C, AFT ACCY COMPT FS 1645 BTWN LONG 27R AND 28R INTERNAL DOUBLER CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-20 AND DWG 5773311.
INSPECTION TYPE-C, FUSELAGE SKIN CORROSION REMOVAL IS BEYOND ALLOWABLE LIMITS AT FS 1100 LONGERON 22R. REPAIRED IAW SRM 53-2-0 AND 51-1-20.
INSPECTION TYPE-C, CORRODED LONGERON END FITTING AT FS 1690 L-26L AFT FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.
INSPECTION TYPE-C, CRACKED AND CORRODED LONGERON AND END FITTING AT FS 1655 S-29L. REMOVED, FABRICATED LONGERON AND INSTALLED LONGERON. REPLACED FITTING IAW SRM 51-1-21 AND DWG 5757779.
INSPECTION TYPE-C, FS 900 STRAP BETWEEN FRAME AND FUSELAGE SKIN CORRODED JUST ABOVE LONGERON 24R. ALSO, CORROSION PROGRESSES TO INTERNAL SURFACE OF FUSELAGE SKIN. REPAIRED IAW DHC SK-868-902.
INSPECTION TYPE-C, FS 1640 AT LBL 38 THE FLOORBEAM TOP FLANGE IS CRACKED AND CORRODED LBL 30. REPAIRED IAW DHC-868-894.
INSPECTION TYPE-C, LONGERON 34L CORRODED BEYOND LIMITS FS 8 TO 70. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-3-3, AND 51-1-21.
INSPECTION TYPE-C, LONGERON 34R CORRODED BEYOND LIMITS FS 8 TO 70. FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-3-3 AND 51-1-21.
INSPECTION TYPE:C LONG 33R LWR INTERCOSTAL BETWEEN F/S 1240-1260 HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-20, 51-1-21, AND 53-4-0.
INSPECTION TYPE-C, LONG 31L FINGER DOUBLER AT FS 1500 HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1- 21, 51-1-12, 51-1-20D, 53-4-1.
INSPECTION TYPE-C, WING BOX FINGER DOUBLER FS 920 TO 940 BL 0 HAS NUMEROUS RIVET HEADS POPPED. REMOVED FINGER DOUBLER, REMOVED CORROSION OUT OF LIMITS, REPAIRED IAW DHC SK-868-626.
INSPECTION TYPE-C, FS 279 AT STR 32L TIE FITTING HAS HEAVY CORROSION INSIDE TORQE BOX. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND 51-1-20D.
INSPECTION TYPE-C, AFT ACCY COMPT F/S 1540 TO 1580, THE LBL 50 SEAT TRACK HAS HEAVY EXFOLIATION CORROSION AROUND THE CLIP NUTS IN THE INBD AND OUTBD UPPER FLANGES. REMOVED, FABRICATED AND INSTALLED SECTION OF TRACK IAW SRM 53-2-3 AND 51-3-0.
INSPECTION TYPE-C, FS 440 TO 460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C, MODERATE CORROSION UNDER WING BOX FINGER DOUBLER FS 960 TO 980 RBL 60. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-2-0, 53-7-1.
INSPECTION TYPE-C, C-3 CARGO PIT FLOOR SUPPORT ANGLE AT FS 1220 BTWN LONG 30L TO 36 HAS HEAVY CORROSION THROUGHOUT, AROUND NUT PLATES. REPAIRED IAW SRM 53-2-0 AND 51-1-20.
INSPECTION TYPE-C, FS 8 TO 35 STR 36 IS CORRODED. FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND DWG 3615532.
INSPECTION TYPE-C, FS 380 TO 400 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.
INSPECTION TYPE-C, LONG 34R SPLICE FITTING BTWN FS 1260 TO 1280 CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, STR 33R FROM FS 25 TO 70 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND DWG 3642838.
INSPECTION TYPE-C, LONG 36 SPLICE FITTING BTWN FS 1260 AND 1280 CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, STR 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C, RT TRAPIZOID FITTING HAS 4 CRACKS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 51-1-21 AND DWG 5611440.
INSPECTION TYPE-C, LONG 31R SPLICE FITTING CRACKED BTWN FS 1040 TO 1060. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.
INSPECTION TYPE-C, AFT ACCY COMPT FS 1690, THE FWD SIDE LONG 26R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, FS 660 BTWN STR 35L TO 36 FRAME TO KEEL TIE FITTING IS CRACKED ON UPPER FLANGE. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-1-0.
INSPECTION TYPE-C, FS 340 TO 380 RBL 44 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-3-0, 53-2-3.
INSPECTION TYPE-C, LONGERON 30R FS 8 TO 70 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-3-1, 51-3-0, 51-1-21 AND DWG 2641455.
INSPECTION TYPE-C, FS 980 AT LONGERON 30R ON AFT WALL OF WHEEL WELL HAS HEAVY CORROSION PRESURE WEB. REPAIRED IAW DHC SK-868-727.
INSPECTION TYPE-C, FS 660 TO 680 BTWN STR 35L TO 36 SKIN AT ANTENNA COAX HAS HEAVY CORROSION. ACCOMPLISHED TEMPORARY REPAIR IAW DHC SK-868-599. SKIN TO BE REPLACED AT NEXT D-CHECK OR 18 MONTHS WHICH EVER COMES FIRST.
INSPECTION TYPE-C, FS 980 TO 990 LBL 48 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-1-20 AND 53-2-3.
INSPECTION TYPE-C, FS 860 TO 870 RBL 44 THE SEAT TRACK HAS HEAVY INTERNAL CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-1-20, 53-2-3.
INSPECTION TYPE-C, FS 1516 LBL 59 SEAT TRACK IS WORN BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3, 51-3-0.
INSPECTION TYPE-C, FS 120 TO 130 LBL 24 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3.
INSPECTION TYPE-C, BELLY SKIN CORROSION FS 55 TO 70 BTWN LONGERONS 33R AND 35R BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED SKIN IAW SRM 51-1-20, SRM ADDN DC8-5330-8942.
INSPECTION TYPE-C, FINGER DOUBLER AT LONGERON 31R FROM FS 8 TO 70 CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21.
INSPECTION TYPE-C, LONGERON 31L I/B END FITTING AT FS 70 CORROSION REMOVAL IS BEYOND ALLOWABLE LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0, 51-1-20D, 53-1-0, AND DWG 4614397.
INSPECTION TYPE-C, FS 1380 TO 1385 LBL 48 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 51-3-0, 51-1-21, 51-1-20D AND 53-2-3.
INSPECTION TYPE-C, FS 582 TO 592 LBL 24 THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 53-2-3.
INSPECTION TYPE-C, FS 941, LBL 24 SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED TRACK IAW SRM 53-2-3, 53-2-0.
INSPECTION TYPE-C, REMOVED 5 RIVETS AND FOUND HEAVY CORROSION, CRACKED AND BROKEN INTERNAL DOUBLER AT 33L TO 32L FS 1612. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20, 53-4-1, 51-1-8.
INSPECTION TYPE-C, FS 180 TO 260 RBL 59 SEAT TRACK IS WORN BEYOND LIMITS AT EACH PLUG. REMOVED AND REPLACED SECTION OF TRACK IAW SRM 51-3-0, 53-2-3, AND 51-1-20D.
INSPECTION TYPE-C, UPPER LT CUSP TO FRAME FITTING AT FS 440 HAS MODERATE CORROSION I/B ANGLE O/B SURFACE. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, NR 1 CARGO PIT AT FS 280 RT SIDE FLOORBEAM SUPPORT FITTING IS CRACKED AT BOTTOM. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C, LT UPPER CUSP TO FRAME FITTING HAS HEAVY CORROSION AT 1620. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-5-0 AND DWG 9750448.
INSPECTION TYPE-C, MODERATE CORROSION UNDER WING BOX FINGER DOUBLER FS 920 TO 922 LBL 60. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW SRM 53-1-0 AND 51-1-20D.
INSPECTION TYPE-C, FS 182 RBL 44 SEAT TRACK IS WORN BEYOND LIMITS AND CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-1-20D.
INSPECTION TYPE-C, FS 1590 TO 1630 LBL 44 SEAT TRACK IS WORN BEYOND LIMITS SEVERAL PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 53-1-0, 51-3-0.
INSPECTION TYPE-C, FS 1440 TO 1450 LBL 24, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3 AND 51-3-0.
INSPECTION TYPE-C, FS 680 LBL 24, SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-4-1 AND 51-1-20D.
INSPECTION TYPE-C, FS 680 RBL 24 SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND 53-4-1.
INSPECTION TYPE-C, FS 660 BELOW RT CUSP LWR SURFACE, FRAME HAS 2 LARGE CRACKS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 53-1-0 AND DWG 3646688.
INSPECTION TYPE:C F/S 680 LBL 44, SEAT TRACK SUPPORT FITTING IS CRACKED. FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM51-1-20 AND DWG 5773275.
INSPECTION TYPE-C, RT WING L/E O/B SECTION I/B END SKIN IS CRACKED ON L/E JUST O/B OF NR 4 PYLON. REPAIRED IAW SRM 57-2-1.
INSPECTION TYPE-C, RIVET BROKEN AND FUSELAGE SKIN CRACKED FS 1723 LONG 13 AND 14 RT. REMOVED RIVET, REPAIRED SKIN AND INSTALLED RIVET IAW SRM 51-1-21, 53-2-1, 51-1-20D.
INSPECTION TYPE-C, FS 680 BL 0 SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 53-4-1, 51-1-29D AND DWG 5773275.
INSPECTION TYPE-C, FS 350 TO 356 RBL 24 SEAT TRACK HAS HEAVY CORROSION. REPLACED SECTION OF TRACK IAW SRM 53-2-3.
INSPECTION TYPE-C, FS 680 RBL 44 SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-4-1 AND 51-1-20D.
INSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 THE UPPER ATTACH CLIP IS CRACKED IN HALF. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 57-5-2, 51-1-21, 51-1-20D.
INSPECTION TYPE-C, FS 610 STR 35R HEAVY CORROSION BTWN TEAR STRAP AND FINGER DOUBLER. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER AND SPLICE STRAP IAW SRM 53-2-0, DWG 5779913 AND DHC SK-868-489.
INSPECTION TYPE-C, LT OTBD SLOT VANE, OUTER SKIN AT THE INBD END HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW SRM ADDN DC8-5720-7767-A.
INSPECTION TYPE-C, LT WING STA 410 CANOE FITTING INBD SIDE BRACE ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, THE LT WING OTBD L/E, UPPER SKIN AT STA XFS592.25 HAS HEAVY CORROSION AND IS CRACKED AT 1 INCH FASTENER. REPAIRED IAW SRM 57-2-1 FIG 38.
INSPECTION TYPE-C, WEB AT AFT FRAME OF MAIN CARGO DOOR FS 270 HAS 50 HOLES DRILLED IN WITH SEVERAL DOUBLE DRILLED HOLES FROM STR 7L TO 17L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-1-21, DWG 5772787, AND SRM 53-4-1. FRAME REPLACED ON N/R 674926.
INSPECTION TYPE-C, THE LT ALRN TRIM TAB, UPPER AND LWR SKINS ARE DELAMINATED AT THE INBD T/E. REPAIRED IAW SRM 57-8-0 AND 57-2-3.
INSPECTION TYPE-C, LT WING OTBD L/E LWR SKIN AT STA XFS 303 TO 305 HAS HEAVY CORROSION AND IS CRACKED AT 2 FASTENERS. REPAIRED IAW DC8-5720-4081-B.
INSPECTION TYPE-C, LT WING LWR L/E SKIN JUST INBD OF THE NR 1 PYLON HAS HEAVY EXFOLIATION CORROSION, AREA WAS PREVIOUSLY REWORKED. REPAIRED IAW SRM ADDN DC8-5720-4087.
INSPECTION TYPE-C, FS 9 STR 33R END FITTING HAS HEAVY CORROSION ON UPPER MOUNT LEG. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 51-1-21, AND DWG 4612650N.
INSPECTION TYPE-C, FS 70 FWD SIDE STR 29L END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-3-1, 51-1-21, 51-1-29D.
INSPECTION TYPE-C, FS 70 FWD SIDE STR 27L END FITTING HAS MODERATE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-3-1 AND 51-1-29D.
INSPECTION TYPE N/A, ATB DUE TO LANDING GEAR DR/LANDING GEAR UP NOT LATCHED LT ON. DISCOVERED DWN LCK CYL ACT ROD END EYELET FAILURE. THIS ALSO LED TO GOUGES IN THE ATTACHMENT FITTING OF THE UPPER DWN LCK LINKS FWD AND AFT. FOUND LT OVERCENTER BUNGEE ACTUATOR ROD END FAILED. REMOVED AND REPLACED ACTUATOR AND BOTH UPPER OVERCENTER LINKS ON LT GEAR PER MM 32-32-03 PG 201 TO 207 AND PERFORMED GEAR RETRACT OPERATION, ALL FUNCT NORMAL. (P/N 5714918-2) (S/N 71 RH) OFF, (P/N 5714918-1) ON.
PILOT REPORTED, HYD FLUID LOSS. FOUND STANDBY RUDDER PUMP PRESSURE LINE CHAFED AND REPLACED IAW MM 29-00-00.