# Service difficulty reports: N8091U, cancelled Apr 13, 2006 A list on [N8091U, cancelled Apr 13, 2006](https://openairdocs.org/deregistered/N8091U-2006-04-13.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 6 · 257 reports - [SDR RRXA010045](https://openairdocs.org/sdr/RRXA010045.md): Frame · corroded · May 2, 2001 · N8091U · Doug DC871F · Fuselage Main, Frame > COMPLY WITH FCD A53-4R1 INSPECTION FOR LOWER FUSELAGE CORROSION. INSPECTED LOWER FUSELAGE FOR CORROSION. FOUND CORROSION AT STA 100 L36 LEVEL 2 CORROSION. BLENDED CORROSION, BEYOND LIMITS. AIRCRAFT FERRIED TO TENNESSEE TECHNICAL SERVICES, LLC. INSPECTED T - [SDR RRXA10771](https://openairdocs.org/sdr/RRXA10771.md): Switch · failed · Apr 16, 2001 · N8091U · Doug DC871F · Landing Gear Position and Warning > DURING A MAINTENANCE VISIT FOUND UNSAFE LIGHT DAMAGE TO LT MLG UNSAFE LIGHT (RED) STAYS ON & NO L/H MLG GREEN LIGHT AFTER SEVERAL GEAR CYLES, GOT GREEN LIGHT ONLY AFTER STEEP BANKS AT LT. SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED - [SDR RRXA10759](https://openairdocs.org/sdr/RRXA10759.md): Floor Panel · corroded · Mar 28, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER FWD. FLOOR PANEL AT COCKPIT PANEL #676, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 - [SDR RRXA10764](https://openairdocs.org/sdr/RRXA10764.md): Stringer · cracked · Mar 26, 2001 · N8091U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING STR.53 AT STA. 495 AND AFT HORZ. LEG, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O. #01- - [SDR RRXA10763](https://openairdocs.org/sdr/RRXA10763.md): Fitting · gouged · Mar 26, 2001 · N8091U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND GOUGE DAMAGE TO LT. WING CANOE FITTING AT STA.340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/23/01 - [SDR RRXA10767](https://openairdocs.org/sdr/RRXA10767.md): Skin · damaged · Mar 22, 2001 · N8091U · Doug DC871F · Horizontal Stabilizer, Tab Structure > DURING A MAINTENCE VISIT FOUND HOLE DAMAGE TO HORZ STAB RT. ELEVATOR AT STA. XE 228.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 02/ - [SDR RRXA10765](https://openairdocs.org/sdr/RRXA10765.md): Door Frame · cracked · Mar 22, 2001 · N8091U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. MLG BODY DOOR AT AFT O/B CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED - [SDR RRXA10760](https://openairdocs.org/sdr/RRXA10760.md): Panel · corroded · Mar 22, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LAV. FLOOR PANEL AT STA. 46-66, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND - [SDR RRXA10766](https://openairdocs.org/sdr/RRXA10766.md): Spar · corroded · Mar 20, 2001 · N8091U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BOTTOM OF SPAR AT STA. 781 AND INSIDE L/H CENTER TANK THUR MID-SPAR ACCESS HOLE560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. F - [SDR RRXA10762](https://openairdocs.org/sdr/RRXA10762.md): Skin · damaged · Mar 20, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO TAIL CONE SKIN AT STA.1902 AND RT 14 INCHES O/B AND 8 INCHES AFT OF ACCESS DOOR NR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW PART AND INSTALLE - [SDR RRXA10761](https://openairdocs.org/sdr/RRXA10761.md): Bushing · elongated · Mar 20, 2001 · N8091U · Doug DC871F · Trailing Edge Flap Control System > DURING A MAINTENANCE VISIT FOUND ELONGATED BUSHING DAMAGE TO #3 LT. FLAP 2ND FROM O/B VANE AT 2ND O/B VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED I - [SDR RRXA10770](https://openairdocs.org/sdr/RRXA10770.md): Skin · cracked · Mar 19, 2001 · N8091U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND CRACK DAMAGED TO A-PIT DOOR SEAL FRAME WORN/CRACKED OUT INCLUDING SKIN--LOC CENTER SECTION OF DOOR AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INS - [SDR RRXA10769](https://openairdocs.org/sdr/RRXA10769.md): Bracket · worn · Mar 19, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO A-PIT DOOR SEAL FRAME AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 01-024 WITH APPROVED 8110-3 DATED 03/13/01. - [SDR RRXA10768](https://openairdocs.org/sdr/RRXA10768.md): Skin · gouged · Mar 19, 2001 · N8091U · Doug DC871F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO A-PIT DOOR SEAL FRAME & DOOR SKIN AT THE A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 - [SDR RRXA10773](https://openairdocs.org/sdr/RRXA10773.md): Skin · tool damage · Mar 17, 2001 · N8091U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND TOOLING MARK DAMAGE TO LWR. WING SKIN UPPER SURFACE AT STA. XRS 507.625 AND STR. 54, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 W - [SDR RRXA10861](https://openairdocs.org/sdr/RRXA10861.md): Frame · corroded · Mar 14, 2001 · N8091U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BRACKET AT STA. 1140-1160 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D - [SDR RRXA10744](https://openairdocs.org/sdr/RRXA10744.md): Skin · corroded · Mar 14, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OUTER SKIN L35L AT STA.705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROS - [SDR RRXA10743](https://openairdocs.org/sdr/RRXA10743.md): Panel · corroded · Mar 12, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H STRESS PANEL AT KEEL BEAM, AT STA 740, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. - [SDR RRXA10742](https://openairdocs.org/sdr/RRXA10742.md): Fitting · gouged · Mar 12, 2001 · N8091U · Doug DC871F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT FOUND GOUGING DAMAGE TO RT. CANOE FITTING TOP FWD 3 INCHES AT RT. STA 340, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 811 - [SDR RRXA10860](https://openairdocs.org/sdr/RRXA10860.md): Skin · corroded · Mar 9, 2001 · N8091U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FILLET ATTACH HOLES AT STA. 640-610 AND L31L TO L28L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED I - [SDR RRXA10772](https://openairdocs.org/sdr/RRXA10772.md): Bulkhead · cracked · Mar 8, 2001 · N8091U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE INSPECTION FOUND CRACK DAMAGE TO C & D PIT R/H BULKHEAD AT C & D PIT, DAMAGE EXCEEDS LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WIT - [SDR RRXA10749](https://openairdocs.org/sdr/RRXA10749.md): Skin · corroded · Mar 8, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA. 772-721 AND L35L-L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#01-024 WITH - [SDR RRXA10748](https://openairdocs.org/sdr/RRXA10748.md): Skin · gouged · Mar 1, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND GOUGED AND DENTED DAMAGE TO SKIN AT STA.1890 AND TAIL POST SUPPORT, DAMAGE EXCEEDED LIMITAIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-2-1 AND DC-8 SRM - [SDR RRXA10747](https://openairdocs.org/sdr/RRXA10747.md): Skin · damaged · Mar 1, 2001 · N8091U · Doug DC871F · Rudder, Plate/Skin > DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO SKIN AT HOLE 62 AND RUDDER POWER PACK LEDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND ISTALLED IAW SRM 51-1-4 AND DC-8 SRM 51-1-21. - [SDR RRXA10746](https://openairdocs.org/sdr/RRXA10746.md): Brace · cracked · Mar 1, 2001 · N8091U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENACE VISIT FOUND CRACK DAMAGE TO HORZ. BRACE AT STA. 1916 AND DOOR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 A - [SDR RRXA10745](https://openairdocs.org/sdr/RRXA10745.md): Skin · damaged · Mar 1, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VIST FOUND ELONGATED HOLE DAMAGE TO SKIN AT FWD OF MLG DOORS, DAMAGE ECXEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 51-3-0. - [SDR RRXA10862](https://openairdocs.org/sdr/RRXA10862.md): Skin · corroded · Feb 28, 2001 · N8091U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN LT WW AT STA. 857-879 AND LBL 0-68.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0 & 53-2-0 FI - [SDR RRXA010687](https://openairdocs.org/sdr/RRXA010687.md): Angle · broken · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND THE "C-PIT" ANGLE BROKEN IN HALF (AFT R/H), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SR - [SDR RRXA010686](https://openairdocs.org/sdr/RRXA010686.md): Fitting · cracked · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR BEAM SUPPORT FITTING AT STA 300 AND RBL -24", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SR - [SDR RRXA010685](https://openairdocs.org/sdr/RRXA010685.md): Hand Rail · cracked · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SIDE RAIL AT STA 90-220 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-1-4. - [SDR RRXA010684](https://openairdocs.org/sdr/RRXA010684.md): Panel · corroded · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE GALLEY FLOOR PANEL AT TOP SURFACE PANEL #329, DAMAGE EXCEEDED LIMITATIONS IAAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC - [SDR RRXA010683](https://openairdocs.org/sdr/RRXA010683.md): Panel · cracked · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP LINE PANEL AT STA 1540-1620 L/H, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. - [SDR RRXA010682](https://openairdocs.org/sdr/RRXA010682.md): Structure · cracked · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP RAIL AT STA 210-380 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21. - [SDR RRXA010681](https://openairdocs.org/sdr/RRXA010681.md): Fitting · cracked · Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK INSIDE BATH TUB FITTING LWR HORIZ. SURFACE TO LT LONGERON 24 STA 860, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53 - [SDR RRXA010680](https://openairdocs.org/sdr/RRXA010680.md): Skin · corroded · Feb 28, 2001 · N8091U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUEL TANK PANEL LAND 506B AT STA XRS 110 TO 125 S-69 TO S-71, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 - [SDR RRXA10868](https://openairdocs.org/sdr/RRXA10868.md): Fitting · corroded · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION TO BATH TUBE FITTING AT STA. 1690 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51 - [SDR RRXA010679](https://openairdocs.org/sdr/RRXA010679.md): Fitting · corroded · Feb 27, 2001 · N8091U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING SKIN AT STA 960-980 X+45", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & 53-2-0 FIG. 1F. - [SDR RRXA010678](https://openairdocs.org/sdr/RRXA010678.md): Guard · cracked · Feb 27, 2001 · N8091U · Doug DC871F · Emergency Exits > DURING A MAINTENANCE VISIT FOUND A CRACK IN 2 PLACES TO THE R-1 DOOR SILL GUARD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/15/01. - [SDR RRXA010677](https://openairdocs.org/sdr/RRXA010677.md): Floorbeam · cracked · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FLOOR BEAM AT STA 857 X+60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/26/ - [SDR RRXA010676](https://openairdocs.org/sdr/RRXA010676.md): Flange · cracked · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT FWD TYPE I DOOR FRAME SEAL FLANGE LWR END, DAMAGE EXCEEDED LIMITATIONS IAAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 53-2-0 - [SDR RRXA010675](https://openairdocs.org/sdr/RRXA010675.md): Frame · gouged · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE FWD SIDE OF FRAME ON THE R/H FWD TYPE I DOOR FRAME SEAL AT STA 370, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-2 - [SDR RRXA010674](https://openairdocs.org/sdr/RRXA010674.md): Floor Panel · misrepaired · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE MAIN CARGO FLOOR PANEL AT STA 80 TO 340E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-9 SRM - [SDR RRXA010673](https://openairdocs.org/sdr/RRXA010673.md): Doubler · bent · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A BENT TO THE UPPER FWD CORNER ON THE DOUBLER FOR "A-PIT" CUTOUT AT STA 320-333, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA - [SDR RRXA010672](https://openairdocs.org/sdr/RRXA010672.md): Doubler · bent · Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A BENT UPPER FWD CORNER TO THE DOUBLER FOR "A-PIT" CUTOUT AT STA 292, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW D - [SDR RRXA10507](https://openairdocs.org/sdr/RRXA10507.md): Seat Track · damaged · Feb 22, 2001 · N8091U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES ON THE FE'S FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREAIAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0. - [SDR RRXA010510](https://openairdocs.org/sdr/RRXA010510.md): Panel · cracked · Feb 22, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE EDGES OF THE FLOOR PANEL CAPT'S SIDE PANEL #676D, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SR - [SDR RRXA010509](https://openairdocs.org/sdr/RRXA010509.md): Panel · corroded · Feb 22, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL #661 AND CRACKED SCREW HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IA - [SDR RRXA010508](https://openairdocs.org/sdr/RRXA010508.md): Panel · corroded · Feb 22, 2001 · N8091U · Doug DC871F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND PERIMETER TOP & BOTTOM EDGES OF CENTER COCKPIT FLOOR PANEL #677 CHAFF STRIP BROKEN, ELONGATED HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IA - [SDR RRXA010506](https://openairdocs.org/sdr/RRXA010506.md): Skin · corroded · Feb 22, 2001 · N8091U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND DISCOLORATION TO THE SKIN ON INSIDE TANK AT LT LWR WING FUEL VENT BOX UPPER SKIN BETWEEN STRINGERS NR 1 & 2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTA - [SDR RRXA10863](https://openairdocs.org/sdr/RRXA10863.md): Door Frame · corroded · Feb 20, 2001 · N8091U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ACCESS HOLE 60 DOOR FRAME AT STA. 1793-1766 AND L34L-L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51 Next page: https://openairdocs.org/deregistered/N8091U-2006-04-13/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 = 'N8091U' AND deregistration_id = 'N8091U-2006-04-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8091U-2006-04-13/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.