# Service difficulty reports: N8085U, cancelled May 17, 2006 A list on [N8085U, cancelled May 17, 2006](https://openairdocs.org/deregistered/N8085U-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 · 99 reports - [SDR RRXA010054](https://openairdocs.org/sdr/RRXA010054.md): Accumulator · failed · Jun 23, 2001 · N8085U · Doug DC871F · Drag Control System > SPOILER PUMP INOP. FOUND SPOILER ACCUMULATOR BLADDER BLOWN AND SPOILER RESERVIOR EMPTY. REMOVED AND REPLACED SPOILER ACCUMULATOR AND SERVICED SPOILER RESERVOIR IAW MM 29-12-02. SPOILER PUMP OP CK GOOD IAW M/M 27-63-25. - [SDR RRXA011044](https://openairdocs.org/sdr/RRXA011044.md): Wheel · vibration · May 8, 2001 · N8085U · Doug DC871F · Wheel/Ski/Float > AT ROTATION NOSE GEAR VIBRATION FELT AND METALLIC SOUND HEARD. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL ASSY IAW DC8 MM 32-41-10. OPS CHECKS GOOD. - [SDR RRXA010027](https://openairdocs.org/sdr/RRXA010027.md): Door · malfunctioned · Mar 24, 2001 · N8085U · Doug DC871F · Landing Gear Door Retract Section > LOUD NOISE AND BUFFET FROM NOSE SECTION. RIGHT NOSE LANDING GEAR DOOR IN OPEN POSITION WHEN AIRCRAFT TAXIED IN. INSPECTED NOSE GEAR DOORS FOR CONDITION AND OPERATION NO DEFECTS NOTED. RE-SET POSITION, AIRCRAFT OK FOR FURTHER FLIGHT DC-8 M/M 32-20-00. - [SDR RRXA010003](https://openairdocs.org/sdr/RRXA010003.md): Adi · malfunctioned · Jan 8, 2001 · N8085U · Doug DC871F · Attitude Gyro and Indicating System > CAPTAINS GYRO AND FLIGHT DIRECTOR FLAGS IN VIEW WHEN A/C PITCHES UP OR DOWN 3 DEG AND HORIZON FREEZES IN POSITION. REMOVED AND REPLACED CAPT''S ADI, OPS CKS GOOD IAW UAL MM 41-20 -22. - [SDR RRXA001096](https://openairdocs.org/sdr/RRXA001096.md): Cover · damaged · Dec 20, 2000 · N8085U · Doug DC871F · Turbine Engine Oil System > PRECAUTIONARY SHUTDOWN NR 4 ENGINE, NO OIL QUANTITY OR PRESSURE. FOUND HAND CRANKING PAD COVER DAMAGED AND REPLACED COVER. SERVICED ENG, OIL AND LEAK CHECK NORMAL. INSPECTED CHIP DETECTORS AND OIL FILTERS, NO CONTAMINATION FOUND. - [SDR RRXA001095](https://openairdocs.org/sdr/RRXA001095.md): Duct · failed · Dec 17, 2000 · N8085U · Doug DC871F · Pneumatic Distribution System > CLIMBING THRU 12,000 FEET NR 2 ENGINE FIRE WARNING SOUNDED. SECURED ENGINE PER EWW QRH. UPON INSPECTION OF ENGINE FOUND HIGH STAGE BLEED DUCT CRACKED AT FLEX COUPLING. REMOVED AND REPLACED HIGH STAGE BLEED DUCT IAW DC-8 M/M CH 36-11-61 AND FIRE WARNING CHEC - [SDR RRXA002173](https://openairdocs.org/sdr/RRXA002173.md): Frame · corroded · Mar 18, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT AFT SIDE OF FRAME AT FS 1340 AND LONGERON 30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC- - [SDR RRXA002189](https://openairdocs.org/sdr/RRXA002189.md): Spar Cap · corroded · Mar 16, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SPAR CAP IN THE CABIN INT BELOW FLOOR LEVEL AT STA 857 AND RBL 48 THROUGH LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED SPAR - [SDR RRXA002187](https://openairdocs.org/sdr/RRXA002187.md): Attach Angle · corroded · Mar 16, 2000 · N8085U · Doug DC871F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE INT ON ATTACH ANGLE AT STA 857 TO 859 AND L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-8 - [SDR RRXA002188](https://openairdocs.org/sdr/RRXA002188.md): Angle · corroded · Mar 3, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE INT AT STA 857 TO 879 AND L12R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE ASSY IAW DC-8 SRM 51-1-21D FIG 34 S - [SDR RRXA002186](https://openairdocs.org/sdr/RRXA002186.md): Skin · corroded · Mar 2, 2000 · N8085U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP LT WING AFT OF NR 2 ENGINE CENTER SPAR AT STA 252.351, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW PDO8-57-018. - [SDR RRXA003434](https://openairdocs.org/sdr/RRXA003434.md): Fitting · corroded · Feb 24, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING TO THE MAIN CABIN R/S AT STA 440 AND L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2 - [SDR RRXA002190](https://openairdocs.org/sdr/RRXA002190.md): Fitting · corroded · Feb 24, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN R/S AT STA 440 AND L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FITTING IAW EA PD 08-53-040 AND SRM 51-2-0. - [SDR RRXA002185](https://openairdocs.org/sdr/RRXA002185.md): Seat Track · corroded · Feb 24, 2000 · N8085U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN SEAT TRACK AT STA 840 TO 990 AND RBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED TRACK IAW DC-8 SRM 53-2-3 FIG 7. - [SDR RRXA002184](https://openairdocs.org/sdr/RRXA002184.md): Longeron · corroded · Feb 23, 2000 · N8085U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CABIN AT STA 1260 TO 1280 AND L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-20 FIG 45. - [SDR RRXA002181](https://openairdocs.org/sdr/RRXA002181.md): Frame · corroded · Feb 23, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD CARGO COMPARTMENT AT STA 620 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FRAME IAW DC-8 SRM 51-1-0 FIG F - [SDR RRXA002180](https://openairdocs.org/sdr/RRXA002180.md): Splice · corroded · Feb 23, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD CARGO COMPARTMENT FRAME AT STA 560 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED SPLICE IAW DC-8 SRM 53-4-0 FIG 1B. - [SDR RRXA002182](https://openairdocs.org/sdr/RRXA002182.md): Frame · corroded · Feb 22, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CABIN INT BELOW FLOOR LEVEL AT STA 879 AND L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED FRAME IAW DC-8 SRM 51-1-20D FIG 1D. - [SDR RRXA002179](https://openairdocs.org/sdr/RRXA002179.md): Frame · corroded · Feb 19, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT FWD FRAME IN THE COCKPIT AT STA 117, 223 AND 220 30 IN LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME IAW DC-8 SRM - [SDR RRXA002183](https://openairdocs.org/sdr/RRXA002183.md): Floorbeam · corroded · Feb 7, 2000 · N8085U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CABIN INT FLOOR LEVEL AROUND CLIP NUT HOLES AT STA 1000 AND RBL 25 THROUGH 44, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW CAP - [SDR RRXA002178](https://openairdocs.org/sdr/RRXA002178.md): Frame · corroded · Feb 7, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LOWER CARGO COMPARTMENT FRAME AT STA 491 AND LONGERON 29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED FRAME IAW DC-8 SRM 53-4 - [SDR RRXA002177](https://openairdocs.org/sdr/RRXA002177.md): Longeron · corroded · Feb 7, 2000 · N8085U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT AT STA 1420 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 51-20-1 FIG 42 AND 53- - [SDR RRXA003435](https://openairdocs.org/sdr/RRXA003435.md): Frame · corroded · Feb 5, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SIDE OF FRAME IN THE AFT CARGO COMPT AT FS 1340 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IA - [SDR RRXA002176](https://openairdocs.org/sdr/RRXA002176.md): Splice · corroded · Feb 5, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT AT FS 1500 TO 1520 AND LONGER SPLICE 26R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED SPLICE IAW DC-8 SRM 53 - [SDR RRXA002175](https://openairdocs.org/sdr/RRXA002175.md): Doubler · corroded · Feb 5, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT AT STA 1510 AND L27R TO L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4 AND 51 - [SDR RRXA002174](https://openairdocs.org/sdr/RRXA002174.md): Longeron · corroded · Feb 5, 2000 · N8085U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT IN CENTER ROW OF FASTENERS AT FS 1416 TO 1410 AND L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED I - [SDR RRXA002172](https://openairdocs.org/sdr/RRXA002172.md): Doubler · corroded · Feb 4, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD CARGO COMPARTMENT DOOR CUTOUT UPPER JAMB RT SIDE SKIN AT STA 284 - 325, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER - [SDR RRXA002171](https://openairdocs.org/sdr/RRXA002171.md): Doubler · corroded · Feb 4, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LOWER CARGO COMPARTMENT AT FS 119 THROUGH 204 AND LONGERON 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED DOUBLER IAW DC-8 S - [SDR RRXA002168](https://openairdocs.org/sdr/RRXA002168.md): Clip · corroded · Feb 4, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LOWER CARGO COMPARTMENT AT STA 198 AND LONGERON 31 RT TO FRAME CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED CLIP IAW DC-8 - [SDR RRXA002170](https://openairdocs.org/sdr/RRXA002170.md): Frame · corroded · Feb 3, 2000 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT CARGO COMPARTMENT TOP SIDE OF FRAME LEG AT FS 1140, 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 51-1-21 FI - [SDR RRXA002169](https://openairdocs.org/sdr/RRXA002169.md): Strap · corroded · Feb 3, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT BAGGAGE COMPARTMENT AT FS 1086 - 1100 AND LONGERON 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW STRAP IAW DC-8 SRM 53- - [SDR RRXA991289](https://openairdocs.org/sdr/RRXA991289.md): Finger Doubler · corroded · Feb 11, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER AT LT CUSP LINE STA -32. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 53-2-0. (CORROSION - [SDR RRXA991032](https://openairdocs.org/sdr/RRXA991032.md): Frame · corroded · Feb 11, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, FWD PIT AT STA 160, LOWER CAP, BETWEEN LONGERONS 34 RIGHT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER - [SDR RRXA991028](https://openairdocs.org/sdr/RRXA991028.md): Frame · corroded · Feb 10, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, FWD ACCESSORY COMPARTMENT FRAME AT STA 70, BETWEEN LONGERONS 33 LEFT AND LONGERON 31 LEFT, FRAME LOWER CHORD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 S - [SDR RRXA991036](https://openairdocs.org/sdr/RRXA991036.md): Frame · corroded · Feb 5, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, BILGE CORROSION UNDER NUT PLATES TOP CAP AND AFT FACE OF WEB FRAME AT STA 1260 BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED - [SDR RRXA991019](https://openairdocs.org/sdr/RRXA991019.md): Frame · corroded · Feb 4, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, LT FRAME STA 1843 TW0 FEET ABOVE HORIZ STAB. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE T - [SDR RRXA991368](https://openairdocs.org/sdr/RRXA991368.md): Frame · corrosion · Feb 3, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 500, LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 AND 51-1-20. (CORRO - [SDR RRXA991301](https://openairdocs.org/sdr/RRXA991301.md): Frame · corroded · Jan 30, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME AT STA 420, BETWEEN LONGERONS 36 AND LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW D - [SDR RRXA991300](https://openairdocs.org/sdr/RRXA991300.md): Frame · corroded · Jan 30, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME AT STA 480, BETWEEN LONGERONS 35 LEFT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC - [SDR RRXA991027](https://openairdocs.org/sdr/RRXA991027.md): Web · corroded · Jan 29, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, UPPER CUSP MEMBRANE, AT STA 560. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS AND INSTALLED IAW FAA APPROVED TENNESSEE TECH DER ENGI - [SDR RRXA991030](https://openairdocs.org/sdr/RRXA991030.md): Frame · corroded · Jan 26, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, BILGE CORROSION FRAME AT STA 1040 BETWEEN LONGERONS 28 LEFT AND LONGERON 33 LEFT AT NUT PLATES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED - [SDR RRXA991021](https://openairdocs.org/sdr/RRXA991021.md): Skin · corroded · Jan 26, 1999 · N8085U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, SKIN/PLATING, MARKER BEACON ON MOUNTING SKIN BETWEEN STA 640 AND STA 660, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC - [SDR RRXA991315](https://openairdocs.org/sdr/RRXA991315.md): Floor Panel · corroded · Jan 21, 1999 · N8085U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ENTRANCE AND LAV FLOOR, BETWEEN STA -8.0 AND STA 80. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL SKINS ON 9 EA PANELS IAW DC8 SR - [SDR RRXA991025](https://openairdocs.org/sdr/RRXA991025.md): Frame · corroded · Jan 21, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, FWD PIT, AT STA 120, BETWEEN LONGERONS 33 RIGHT AND LONGERON 30 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLE DOUBLER AND I - [SDR RRXA991024](https://openairdocs.org/sdr/RRXA991024.md): Channel · corroded · Jan 21, 1999 · N8085U · Doug DC871F · Engine Cowling System > DURING A MAINTENANCE VISIT, FOUND CORROSION, NOSE COWL CHANNEL 5:30 POSITION AFT SIDE OF CANTED BULKHEAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED U CHANNEL IAW FAA APPROVED TENNESSEE - [SDR RRXA991023](https://openairdocs.org/sdr/RRXA991023.md): Bulkhead · cracked · Jan 21, 1999 · N8085U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT, FOUND CRACK, CENTER FUSELAGE, SHIELD BULKHEAD, C-PIT FWD BULKHEAD, BENT, CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PARTITION AND ATTACH ANGLE IAW FAA - [SDR RRXA991018](https://openairdocs.org/sdr/RRXA991018.md): Skin · damaged · Jan 18, 1999 · N8085U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT, FOUND SCRAPE, CENTER FUSELAGE, SKIN/PLATE, AT STA 1360, LONGERON 23 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA IAW DC8 SRM 51-1-0, TREATED AND PRIMED IAW DC8 SRM 51 - [SDR RRXA991299](https://openairdocs.org/sdr/RRXA991299.md): Frame · corroded · Jan 15, 1999 · N8085U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, BETWEEN STA 280 AND STA 287, AND BETWEEN LONGERONS 28 LEFT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED R - [SDR RRXA991026](https://openairdocs.org/sdr/RRXA991026.md): Angle · corroded · Jan 15, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME ATTACH ANGLE, FWD PIT, AT STA 140, LONGERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACH ANGLE IAW DC8 SR - [SDR RRXA991033](https://openairdocs.org/sdr/RRXA991033.md): Skin · corroded · Jan 14, 1999 · N8085U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT, FOUND CORROSION, WING, L/E SKIN, UNDER FASTENER RIGHT WING L/E UPPER SURFACE AT STA XFS 13.750 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLE Next page: https://openairdocs.org/deregistered/N8085U-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 = 'N8085U' AND deregistration_id = 'N8085U-2006-05-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8085U-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.