# Service difficulty reports: N8076U, cancelled May 17, 2006 A list on [N8076U, cancelled May 17, 2006](https://openairdocs.org/deregistered/N8076U-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 2 · 96 reports - [SDR RRXA010061](https://openairdocs.org/sdr/RRXA010061.md): Engine · flamed out · Jul 25, 2001 · N8076U · Doug DC871F · Engine (Turbine/Turboprop) > NR 4 ENGINE IN FLIGHT FLAME OUT 35000. IAW UAL M/M 71-00-40 PGS 201-206 POWER LOSS/FLAME- OUT INVESTIGATED & CHECKED THE FOLLOWING: ENGINE INLET/ EXHAUST, CHIP DETECTORS, MAIN FUEL PUMP, FUEL CTRL.,NR 3 ENGINE FUEL BOOST PUMP, IGNITOR, FUEL QTY CHECKED LINE L - [SDR RRXA010046](https://openairdocs.org/sdr/RRXA010046.md): Doubler · corroded · May 10, 2001 · N8076U · Doug DC871F · Fuselage Main, Plate/Skin > DURING FCD A53-4R2 INSPECTION OF LWR FUSELAGE CORROSION. MX DISCOVERED CORROSION BEYOND LIMITS. REMOVED CORROSION, FABRICATED NEW FINGER DOUBLER AND INSTALLED PER EO 01-143 WITH APPROVED 8110-3 DATED 5/12/01. - [SDR RRXA011040](https://openairdocs.org/sdr/RRXA011040.md): Restrictor Valve · failed · Apr 26, 2001 · N8076U · Doug DC871F · Landing Gear Retraction/Extension System > ON/BEFORE LANDING, WITH LANDING GEAR HANDLE PLACED DOWN, DOORS WARNING LIGHT ON, LANDING GEAR UNSAFE LT MLG GREEN LIGHT NOT ILLUM. ALT DOOR LT LIGHT ON LT GEAR WOULD NOT EXTEND. RAN EMERGENCY CHECKLIST AND PERFORMED EMERGENCY LEFT GEAR UP LANDING. REMOVED A - [SDR RRXA010013](https://openairdocs.org/sdr/RRXA010013.md): Pressure Switch · inoperative · Feb 27, 2001 · N8076U · Doug DC871F · Engine Oil Pressure > NR 4 ENGINE LOW OIL PSI LIGHT INOP. TRANSFERRED TO DMI LIST AS CONTROL B-9616122-0962 CAT: B MEL 7906 ATA 7910 DUE DATE 02MAR01 PLACARD INSTALLED. REMOVED AND REPLACED NR 4 ENG LOW OIL PRESS SW, OPS AND LEAK CHECK GOOD IAW DC-8 M/M 79-32-2. (LOW OIL PRESS S - [SDR RRXA010004](https://openairdocs.org/sdr/RRXA010004.md): Ballast · odor · Jan 10, 2001 · N8076U · Doug DC871F · Flight Compartment Lighting > STRONG SMOKE ODOR COMING FROM FIRST OFFICERS SIDE, SUSPECT LIGHT BALLAST. TRANSFERRED TO DMI LIST AS CONTROL C-9755071-227 CAT: C MEL 3301 ATA 3310 DUE DATE 20JAN01 PLACARD INSTALLED. REMOVED AND REPLACED LIGHTING BALLAST SIX PACK IAW DC-8 M/M 33-10-0. - [SDR RRXA003683](https://openairdocs.org/sdr/RRXA003683.md): Tire · failed · Nov 4, 2000 · N8076U · Doug DC871F · Tire > ON LANDING TIRES NR 3 & 4 BLEW. REMOVED AND INSPTED AXEL THREADS. REPLACED NR 3 & 4 WHEEL ASSEMBLIES IAW DC-8 MM 32-41-05. FOUND MLG ANTI-SKID INOP, TROUBLESHOT SYSTEM, FOUND BAD ANTI-SKID CONTROL VALVE. REMOVED AND REPLACED CONTROL VALVE IAW DC-8 MM 32-43-3 - [SDR RRXA003138](https://openairdocs.org/sdr/RRXA003138.md): Splice · cracked · Sep 24, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK ALONG RADIUS OF THE STRESS PANEL ATTACH POINT END SPLICE AT STA Y=780 AND X=-12, 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- - [SDR RRXA003312](https://openairdocs.org/sdr/RRXA003312.md): Angle · corroded · Sep 19, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A DENT TO THE DOOR JAMB FRAME IN C-CARGO COMPT AT STA 1169 AND LBL 14 WATERLINE -58, 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- - [SDR RRXA003131](https://openairdocs.org/sdr/RRXA003131.md): Web · cracked · Sep 18, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SIDE CUSP WEB AT STA 880 RT, 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 RRXA003132](https://openairdocs.org/sdr/RRXA003132.md): Web · cracked · Sep 16, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP WEB AT STA 880 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-2-0. - [SDR RRXA003133](https://openairdocs.org/sdr/RRXA003133.md): Intercostal · cracked · Sep 15, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AND DOUBLER BETWEEN FLOORBEAMS AT STA 320 - 324 AND X+40 Z-2, 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 - [SDR RRXA003135](https://openairdocs.org/sdr/RRXA003135.md): Angle · cracked · Sep 14, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FAIRING ATTACH ANGLE AT STA 640, 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 51-1-24 AND 51-1-21. - [SDR RRXA003321](https://openairdocs.org/sdr/RRXA003321.md): Seat Track · corroded · Sep 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TRACK AT FASTENER HOLE AT FS 1482 AND X=50R, 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 53-2-3 FIG 1F. (CORROS - [SDR RRXA003134](https://openairdocs.org/sdr/RRXA003134.md): Intercostal · cracked · Sep 8, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL BETWEEN STA 1380 - 1400 AND LBL -18 WATERLINE -35, 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 51-1-24, 5 - [SDR RRXA003136](https://openairdocs.org/sdr/RRXA003136.md): Angle · cracked · Sep 6, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BLEED AIR CONNECTOR DOOR LANDING AT THE RT RAM AIR INLET, 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. - [SDR RRXA003329](https://openairdocs.org/sdr/RRXA003329.md): Fitting · corroded · Aug 28, 2000 · N8076U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT WHEEL WELL FITTING AT STA 899 AND L23R, 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 51-3-0 FIG 1F. (CORRO - [SDR RRXA000427A](https://openairdocs.org/sdr/RRXA000427A.md): Longeron · corroded · Aug 20, 2000 · N8076U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP SIDE FRAME AT STA 1080 RBL-48 THROUGH LBL 448 AND ABOVE LONGERON L33.35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FA - [SDR RRXA003160](https://openairdocs.org/sdr/RRXA003160.md): Skin · cracked · Aug 15, 2000 · N8076U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE HEAT VENT ON THE RT WING CENTER L/E INTERIOR AT STA 352, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 - [SDR RRXA003148](https://openairdocs.org/sdr/RRXA003148.md): Seat Track · corroded · Aug 12, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT STA Y398-428 AND X23-X27, 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 53-2-3 FIG F. CORROSION DAM - [SDR RRXA003146](https://openairdocs.org/sdr/RRXA003146.md): Seat Track · corroded · Aug 12, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE AFT SIDE OF THE NR 3 LEFT SEAT TRACK AT STA 230 - 240 AND LBL 25 - 29, 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 S - [SDR RRXA003145](https://openairdocs.org/sdr/RRXA003145.md): Seat Track · corroded · Aug 12, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT STA 190 - 205, 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 53-2-3. CORROSION DAMAGE RECORDED IN E - [SDR RRXA003314](https://openairdocs.org/sdr/RRXA003314.md): Doubler · cracked · Aug 11, 2000 · N8076U · Doug DC871F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FWD CARGO COMPT DOOR LEFT EDGE EXTERIOR, 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, 51-1-20D AND PD-05-52-0 - [SDR RRXA003147](https://openairdocs.org/sdr/RRXA003147.md): Fitting · corroded · Aug 11, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE FITTING INSIDE BOTTOM LIGHTENING HOLE ON THE FWD CARGO NR 2 DOOR CUTOUT AFT JAMB AT STA 565 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA - [SDR RRXA003328](https://openairdocs.org/sdr/RRXA003328.md): Seat Track · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE SEAT TRACK FLANGE AT STA 1362 AND X+=45 Z+0, 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 53-2-3 FIG 1F. (CORROS - [SDR RRXA003327](https://openairdocs.org/sdr/RRXA003327.md): Seat Track · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT STA 1600 AND X+45 X+44, 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 53-2-3 FIG 1F. (CORROSION DAM - [SDR RRXA003326](https://openairdocs.org/sdr/RRXA003326.md): Seat Track · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE SEAT TRACK AT STA 1620 - 1640 AND LT X+44, 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 53-2-0 AND 53-2-3 FIG 1. - [SDR RRXA003324](https://openairdocs.org/sdr/RRXA003324.md): Frame · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FRAME SPLICE FWD SIDE OF FRAME AT STA 520 AND L36, 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, 51-1-20D - [SDR RRXA003319](https://openairdocs.org/sdr/RRXA003319.md): Frame · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WHEEL WELL FRAME AT STA 879 ABOVE L24R, 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 53-2-6, 51-1-24 AND 5 - [SDR RRXA003155](https://openairdocs.org/sdr/RRXA003155.md): Skin · cracked · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE HOT AIR VENTS ON THE LT WING L/E AT STA 282, 341 AND 285, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EA PD08-57-041. - [SDR RRXA003152](https://openairdocs.org/sdr/RRXA003152.md): Seat Track · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT STA 1660-1675 AND X-43 TO X-45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-0 AND 51-1-8 PA - [SDR RRXA003143](https://openairdocs.org/sdr/RRXA003143.md): Frame · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AT STA 540 AND L29L TO 36, 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 FIG 1B. COR - [SDR RRXA003141](https://openairdocs.org/sdr/RRXA003141.md): Seat Track · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT STA 1660-1680 AND X+44, 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 53-2-3 PG 35. CORROSION DAMAG - [SDR RRXA003130](https://openairdocs.org/sdr/RRXA003130.md): Angle · cracked · Aug 10, 2000 · N8076U · Doug DC871F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND A CRACK ON FWD SIDE OF SUPPORT FRAME ON THE LT WING TRAILING EDGE FLAP WELL AT STA XW 27, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 - [SDR RRXA003129](https://openairdocs.org/sdr/RRXA003129.md): Fitting · cracked · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK IN THE RADIUS OF THE RIGHT SIDE KEEL BEAM SUPPORT FITTING AT STA Y+791 X-1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DC-8 SRM 51- - [SDR RRXA003128](https://openairdocs.org/sdr/RRXA003128.md): Floorbeam · corroded · Aug 10, 2000 · N8076U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM TOP STRAP AT STA 1580 AND X+30 THROUGH X+43, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUPPORT IAW DC-8 SRM 51-1-4 A - [SDR RRXA003325](https://openairdocs.org/sdr/RRXA003325.md): Frame · corroded · Aug 9, 2000 · N8076U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME IN THE FWD CARGO COMPT AT STA 600 AND L31L TO L27R, 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 51-1-2 - [SDR RRXA003320](https://openairdocs.org/sdr/RRXA003320.md): Longeron · corroded · Aug 9, 2000 · N8076U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON UPPER SIDE OF LONGERON AT STA 500 AND L31R, 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 53-2-1 FIG 7 AND 53-2-0. - [SDR RRXA003159](https://openairdocs.org/sdr/RRXA003159.md): Skin · cracked · Aug 9, 2000 · N8076U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE HOT AIR VENT ON THE LT WING CENTER L/E AT STA 347 - 354, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EA PD08-57-041. - [SDR RRXA003158](https://openairdocs.org/sdr/RRXA003158.md): Skin · cracked · Aug 9, 2000 · N8076U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE HOT AIR VENT ON THE LT WING CENTER L/E AT STA 366 - 360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EA PD08-57-041. - [SDR RRXA003151](https://openairdocs.org/sdr/RRXA003151.md): Bracket · cracked · Aug 9, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER MOUNTING BRACKET ON THE FWD ACCESSORY COMPT AFT BULKHEAD AT STA 70 X-3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 S - [SDR RRXA003323](https://openairdocs.org/sdr/RRXA003323.md): Longeron · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND FASTENERS ON THE LONGERON AT STA 1060 TO 1070 AND L33L, 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, - [SDR RRXA003322](https://openairdocs.org/sdr/RRXA003322.md): Strap · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INTERCOSTAL STRAP OVER FRAME AT STA 1080 ABOVE L35R, 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, 51- - [SDR RRXA003318](https://openairdocs.org/sdr/RRXA003318.md): Longeron · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON AROUND FASTENERS AT STA 1070 TO 1080 AND L36, 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 A - [SDR RRXA003317](https://openairdocs.org/sdr/RRXA003317.md): Fitting · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND IG CORROSION DAMAGE TO THE T-ANGLE BELOW FLOOR LEVEL ATTACHED TO SKIN AT STA 920 AND L21R TO L22R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC - [SDR RRXA003316](https://openairdocs.org/sdr/RRXA003316.md): Floorbeam · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM AROUND HUCKBOLTS AT STA 920 AND -21-X61 THROUGH -X67, 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 53-2 - [SDR RRXA003154](https://openairdocs.org/sdr/RRXA003154.md): Skin · cracked · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING CENTER L/E INTERIOR HEAT VENT AT STA 302 AND 408, 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 57-2-0 AND EA P - [SDR RRXA003153](https://openairdocs.org/sdr/RRXA003153.md): Skin · cracked · Aug 8, 2000 · N8076U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING CENTER L/E HOT AIR VENT AT STA 419, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-8 AND EAPD08-57-036. - [SDR RRXA003149](https://openairdocs.org/sdr/RRXA003149.md): Web · cracked · Aug 8, 2000 · N8076U · Doug DC871F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE DOOR WEB AT FWD END OF C-BAGGAGE DOOR AT STA 1172 AND -X10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW D - [SDR RRXA003142](https://openairdocs.org/sdr/RRXA003142.md): Seat Track · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT FS 1680-1700 AND X=25, 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 53-2-3 PG 35. CORROSION DAMAGE - [SDR RRXA003137](https://openairdocs.org/sdr/RRXA003137.md): Fitting · corroded · Aug 8, 2000 · N8076U · Doug DC871F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING FOR FRAME TO FUSELAGE FWD SIDE OF FITTING AT STA Y=880 AND L21R-L22R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW Next page: https://openairdocs.org/deregistered/N8076U-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 = 'N8076U' AND deregistration_id = 'N8076U-2006-05-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8076U-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.