# Service difficulty reports: N8084U, cancelled May 17, 2006 A list on [N8084U, cancelled May 17, 2006](https://openairdocs.org/deregistered/N8084U-2006-05-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 168 reports - [SDR RRXA010064](https://openairdocs.org/sdr/RRXA010064.md): Indicator · failed · Aug 7, 2001 · N8084U · Doug DC871F · Engine EGT/TIT Indicating System > NR 1 EGT REACHED 907 DEGREES C FOR APPROX 8 SEC ON MAX POWER T/O. 92 PERCENT N2 & 28 DEGREES C OAT AT DAY. FOUND NR 1 ENGINE EGT INDICATOR READS 24-34 DEGREES HIGH. NO DEFECTS ON HARNESS R&R NR 1 EGT INICATOR 077-20-1, CK GOOD WITH TEST SET, ENGINE RUN REQ - [SDR RRXA010062](https://openairdocs.org/sdr/RRXA010062.md): Floor Panel · damaged · Aug 4, 2001 · N8084U · Doug DC871F · Fuselage Floor Panel > UPPER DECK CARGO FLOOR AT STA 781, 30 AND TO THE RT HAS A HOLE. REPAIRED GOUGE IN FLOOR PANEL IAW DC-8 SRM 53-2-3 FIG 6. - [SDR RRXA002749](https://openairdocs.org/sdr/RRXA002749.md): Frame · corroded · Jun 30, 2000 · N8084U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FWD SIDE OF FRAME AT STA 20 AT CUSP LINE RT SIDE OF CABIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SR - [SDR RRXA002719](https://openairdocs.org/sdr/RRXA002719.md): Nut Plate · missing · Jun 29, 2000 · N8084U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A BROKEN NUT PLATE ON THE RIGHT O/B SLOT UPPER SIDE SCREW AT STA XS 515, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8 - [SDR RRXA002720](https://openairdocs.org/sdr/RRXA002720.md): Link · damaged · Jun 23, 2000 · N8084U · Doug DC871F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND THAT THE FLAP LINK SUPPORT (CANOE FITTING) NEEDS TO BE REPLACED AT STA XW 219.498, 339.723 & 97.906 IAW DC-8 MM 27-51-12 RIGHT SIDE PER S/B 27-260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC- - [SDR RRXA002718](https://openairdocs.org/sdr/RRXA002718.md): Retainer · misinstalled · Jun 23, 2000 · N8084U · Doug DC871F · Wing, Attach Fittings > DURING A MAINTENANCE VISIT FOUND CANOE FITTING BOLT RETAINER INSTALLED ON WRONG SIDE OF FITTING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPR - [SDR RRXA002750](https://openairdocs.org/sdr/RRXA002750.md): Bulkhead · damaged · Jun 21, 2000 · N8084U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND NUMEROUS PATCHES TO THE FWD LWR CARGO COMPT MID BULKHEAD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED 8110-3 DATED - [SDR RRXA002738](https://openairdocs.org/sdr/RRXA002738.md): Pressure Panel · corroded · Jun 20, 2000 · N8084U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING AFT LT TOP PANEL AT STA 848.00 AND LBL 60 TO 58 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAI - [SDR RRXA002699](https://openairdocs.org/sdr/RRXA002699.md): Skin · dented · Jun 19, 2000 · N8084U · Doug DC871F · Elevator Structure > DURING A MAINTENANCE VISIT FOUND A DENT TO THE RT. ELEVATOR L/E AT STA XE 120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. ACCEPTABLE TO RETURN TO SERVICE IAW E.O. 00-107 WITH APPROVED 8110-3 DATED 6-19-00. - [SDR RRXA002740](https://openairdocs.org/sdr/RRXA002740.md): Drag Link · broken · Jun 19, 2000 · N8084U · Doug DC871F · Landing Gear Retraction/Extension System > DURING A MAINTENANCE VISIT FOUND THE ATTACHMENT LUG BROKEN OFF TOP OF RT MAIN LANDING GEAR DRAG LINK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH A - [SDR RRXA002739](https://openairdocs.org/sdr/RRXA002739.md): Bracket · cracked · Jun 19, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SUPPORT BRACKET AT STA FS 857 AND LBL 47 LT MAIN W/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH - [SDR RRXA002745](https://openairdocs.org/sdr/RRXA002745.md): Angle · corroded · Jun 16, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER CARGO COMPT AT CUSP LINE AT STA 1240 LT XCW 64 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW D - [SDR RRXA002717](https://openairdocs.org/sdr/RRXA002717.md): Skin · cracked · Jun 16, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES AND SMALL CRACK TO THE RT WING CENTER LEADING EDGE O/B SLOT EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO N - [SDR RRXA002755](https://openairdocs.org/sdr/RRXA002755.md): Angle · corroded · Jun 15, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BULKHEAD AFT SIDE ANGLE AT STA 70 AND L22R TO L25R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 - [SDR RRXA002695](https://openairdocs.org/sdr/RRXA002695.md): Pressure Panel · corroded · Jun 15, 2000 · N8084U · Doug DC871F · Wing, Rib/Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR CENTER WING AREA/BOTTOM RT PLATE AND BOTTOM LT PLATE SCREWS AND BOLTS AT STA 700 - 781 AND L35L - L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM - [SDR RRXA002659](https://openairdocs.org/sdr/RRXA002659.md): Skin · lightning strike · Jun 14, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND LIGHTENING STRIKE DAMAGE TO THE RT WING TIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1. - [SDR RRXA002762](https://openairdocs.org/sdr/RRXA002762.md): Frame · corroded · Jun 13, 2000 · N8084U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CIRCUMFERENTIAL FRAME AFT SIDE AT STA 1140 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-1 - [SDR RRXA002692](https://openairdocs.org/sdr/RRXA002692.md): Skin · cracked · Jun 13, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK 3 INCHES LONG ON THE LT WING CENTER LEADING EDGE T/E DOUBLER AT STA 339.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO - [SDR RRXA002716](https://openairdocs.org/sdr/RRXA002716.md): Skin · damaged · Jun 12, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE SURFACE 8 INCHES AFT OF L/E LWR ON THE RT WING L/E AT STA XW 336.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO N - [SDR RRXA002698](https://openairdocs.org/sdr/RRXA002698.md): Skin · damaged · Jun 12, 2000 · N8084U · Doug DC871F · Horizontal Stabilizer, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A DIMPLED WASHER ON THE RT HORZ STAB I/B LEADING EDGE SCREW AT STA XFS 178.7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW EO NR 00-107 WITH APPRO - [SDR RRXA002694](https://openairdocs.org/sdr/RRXA002694.md): Skin · corroded · Jun 12, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER PANEL SPACERS ON THE LOWER CENTER WING AREA EXTERNAL AT STA 680 - 700 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST - [SDR RRXA002774](https://openairdocs.org/sdr/RRXA002774.md): Skin · loose · Jun 9, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND ABOUT 75 RIVETS LOOSE AND PULLING ON O/B REVERSER OUTSIDE SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPR - [SDR RRXA002760](https://openairdocs.org/sdr/RRXA002760.md): Frame · damaged · Jun 9, 2000 · N8084U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A HOLE IN THE UPPER FLANGE AT STA 1440 ABOVE L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED 8110-3 D - [SDR RRXA002743](https://openairdocs.org/sdr/RRXA002743.md): Plate · gouged · Jun 9, 2000 · N8084U · Doug DC871F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A DENTED/GOUGED B PIT KICK PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21, 53-2-0 AND 51-1-20D. - [SDR RRXA002742](https://openairdocs.org/sdr/RRXA002742.md): Skin · damaged · Jun 9, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND SHEARED EXTERIOR FASTENERS AT STA 305 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 5-3-00. - [SDR RRXA002741](https://openairdocs.org/sdr/RRXA002741.md): Fitting · cracked · Jun 9, 2000 · N8084U · Doug DC871F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT UPPER T/E FLAP WELL FITTING AT STA XW-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED - [SDR RRXA002713](https://openairdocs.org/sdr/RRXA002713.md): Panel · cracked · Jun 9, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK AND ELONGATED HOLES TO THE CAN''T PRESS WEB PANEL AT STA 508 AND XCW 463, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 - [SDR RRXA002704](https://openairdocs.org/sdr/RRXA002704.md): Finger Doubler · corroded · Jun 9, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AND REINFORCEMENT BRACKET AT STA 8 TO -12-X59-Z-10 RT SIDE OF CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND - [SDR RRXA002689](https://openairdocs.org/sdr/RRXA002689.md): Fitting · damaged · Jun 9, 2000 · N8084U · Doug DC871F · Wing, Attach Fittings > DURING A MAINTENANCE VISIT FOUND A BROKEN TAB AND GOUGED FITTING ON THE 508 CAN''T WEB SUPPORT ATTACHMENT FITTING TO FRONT SPAR LOWER ATTACHMENT AT STA XCW 463, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51- - [SDR RRXA002688](https://openairdocs.org/sdr/RRXA002688.md): Panel · cracked · Jun 9, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK AND HOLES ELONGATED ON THE 508 CAN''T PRESSURE WEB PANEL AT STA XCW 463, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR - [SDR RRXA002665](https://openairdocs.org/sdr/RRXA002665.md): Skin · damaged · Jun 9, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND I/B EDGE SKIN BROKEN OFF WHERE FLIGHT SPOILER RETRACTS DOWN ON THE LT UPPER TRAILING SURFACE O/B AT STA 340 AT XRS 367, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FA - [SDR RRXA002655](https://openairdocs.org/sdr/RRXA002655.md): Doubler · damaged · Jun 9, 2000 · N8084U · Doug DC871F · Landing Gear Doors > DURING A MAINTENANCE VISIT FOUND A PATCH REPAIR THAT IS TORN NEAR SEAL ON THE LT MLG DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21, 51-1-21A, - [SDR RRXA002775](https://openairdocs.org/sdr/RRXA002775.md): Fairing · cracked · Jun 8, 2000 · N8084U · Doug DC871F · Aerodynamic Fairings > DURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 2 INCHES LONG ON THE O/B REV TOP FAIRING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7 - [SDR RRXA002767](https://openairdocs.org/sdr/RRXA002767.md): Plate · gouged · Jun 8, 2000 · N8084U · Doug DC871F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND SEVERAL DENTS/GOUGES AROUND D PIT DOOR EXTERNAL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND 51-1-21. - [SDR RRXA002715](https://openairdocs.org/sdr/RRXA002715.md): Fitting · corroded · Jun 8, 2000 · N8084U · Doug DC871F · Wing, Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING ON THE RT WING AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORRO - [SDR RRXA002710](https://openairdocs.org/sdr/RRXA002710.md): Vane · damaged · Jun 8, 2000 · N8084U · Doug DC871F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND ENLARGED SCREW HOLES ON THE NR 2 RT FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-2 AND EO NR 00-107 WITH APPROVED 8110- - [SDR RRXA002690](https://openairdocs.org/sdr/RRXA002690.md): Fitting · corroded · Jun 8, 2000 · N8084U · Doug DC871F · Wing, Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING AT STA 410 LT WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROSION DA - [SDR RRXA002776](https://openairdocs.org/sdr/RRXA002776.md): Skin · cut · Jun 7, 2000 · N8084U · Doug DC871F · Nacelle/Pylon, Plate/Skin > DURING A MAINTENANCE VISIT FOUND SEVERAL CUTS IN NR 4 ENG O/B T/R INTER RING COWL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATE - [SDR RRXA002714](https://openairdocs.org/sdr/RRXA002714.md): Skin · damaged · Jun 7, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND OVERSIZED ATTACH HOLES TO THE STUB WING OVER NR 3 ENG O/B UPPER SURFACE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED - [SDR RRXA002707](https://openairdocs.org/sdr/RRXA002707.md): Angle · cracked · Jun 7, 2000 · N8084U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACKED NR 11 RIB ON THE RT WING NR 3 STUB LWR LT RIB ANGLE AT STA XS 246, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00- - [SDR RRXA002691](https://openairdocs.org/sdr/RRXA002691.md): Skin · cracked · Jun 7, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SCREW HOLE 33 INCHES FROM LEADING FROM SPAR LWR, ON LT CENTER SECTION L/E AT STA 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL - [SDR RRXA002662](https://openairdocs.org/sdr/RRXA002662.md): Skin · damaged · Jun 7, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND LOOSE SCREWS ON THE LEFT O/B SLOT L/E AT STA 520 33 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-1 - [SDR RRXA002656](https://openairdocs.org/sdr/RRXA002656.md): Panel · bulged · Jun 7, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E UPPER SURFACE AT STA XE 245, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 00-107 WITH APPRO - [SDR RRXA002759](https://openairdocs.org/sdr/RRXA002759.md): Frame · corroded · Jun 6, 2000 · N8084U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP OF CIRCUMFERENTIAL FRAME AT STA 1400 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53- - [SDR RRXA002752](https://openairdocs.org/sdr/RRXA002752.md): Longeron · corroded · Jun 5, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LWR CARGO BILGE AT STA 350 AND L35R LT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2 - [SDR RRXA002726](https://openairdocs.org/sdr/RRXA002726.md): Rib · cracked · Jun 5, 2000 · N8084U · Doug DC871F · Wing, Rib/Bulkhead > DURING A MAINTENANCE VISIT FOUND A CRACK THROUGH UNDER GUSSET ON THE NR 11 LOWER RIB ON THE RT WING L/E MIDDLE SECTION AT STA XFS 350, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA - [SDR RRXA002701](https://openairdocs.org/sdr/RRXA002701.md): Longeron · corroded · Jun 2, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND CRACK TO LONGERON 31R AT STA 8 TO -67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PART IAW DC-8 SRM 51-1-0 AND 51-1-2 - [SDR RRXA002790](https://openairdocs.org/sdr/RRXA002790.md): Longeron · corroded · Jun 1, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE INSIDE LONGERON UNDER CIRCUMFERENTIAL FRAME AT STA 600 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. - [SDR RRXA002770](https://openairdocs.org/sdr/RRXA002770.md): Frame · broken · Jun 1, 2000 · N8084U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND A BROKEN FRAME AND SEAT TRACK AT STA 240 3RD SEAT TRACK FROM LT SIDE OF CABIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 0 - [SDR RRXA002766](https://openairdocs.org/sdr/RRXA002766.md): Rib · damaged · Jun 1, 2000 · N8084U · Doug DC871F · Passenger/Crew Doors > DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LT SIDE L2 DOOR LWR RIB FWD NUT PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED 8110-3 Next page: https://openairdocs.org/deregistered/N8084U-2006-05-17/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N8084U' AND deregistration_id = 'N8084U-2006-05-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8084U-2006-05-17/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.