# Service difficulty reports: N796FT, cancelled Oct 27, 2004 A list on [N796FT, cancelled Oct 27, 2004](https://openairdocs.org/deregistered/N796FT-2004-10-27.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 · 83 reports - [SDR RRXA010020](https://openairdocs.org/sdr/RRXA010020.md): Fire Loop · malfunctioned · Mar 15, 2001 · N796FT · Doug DC873F · Fire Detection > SHORTLY AFTER DEPARTURE FROM IAH, EB127/796FT AIR RETURNED TO IAH DUE TO NR 4 FIRE WARNING. REPLACED O/B LOOP ASSY ON LOWER FAN CASE, ADJUSTED WIRE BUNDLES NEXT TO START VALVE DUCT. RAN ENGINE NO MALFUNCTION FOUND. DID BLEED AIR LEAK CHECK. NO LEAK NOTED. - [SDR RRXA010023](https://openairdocs.org/sdr/RRXA010023.md): Fire Loop · intermittent · Feb 16, 2001 · N796FT · Doug DC873F · Fire Detection > INTERMITTENT SHORT AND FIRE INDICATION ON NR 4 ENGINE, SHUTDOWN NR 4 ENG PER QRH 1 BOTTLE DISCHARGED. REMOVED AND REPLACED ALL 5 FIRE LOOPS. OPS CKS NORMAL IAW 26-10-1. - [SDR RRXA002864](https://openairdocs.org/sdr/RRXA002864.md): Structure · corroded · Jul 12, 2000 · N796FT · Doug DC873F · Ailerons > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND SHEARED FASTENERS ON THE LWR SURFACE AT THE I/B SIDE ON THE LT WING O/B AILERON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW - [SDR RRXA002863](https://openairdocs.org/sdr/RRXA002863.md): Skin · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING LWR SKIN AT A FASTENER HOLE AT STA XFS 435, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SERVICE REWORK DWG 08570013 AN - [SDR RRXA002862](https://openairdocs.org/sdr/RRXA002862.md): Skin · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK AT A FASTENER HOLE AT THE LWR L/E CAP AT THE FWD SPAR ATTACHMENT ON THE RT WING L/E 6 INCHES I/B OF STA XFS 710, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A - [SDR RRXA002861](https://openairdocs.org/sdr/RRXA002861.md): Skin · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM OF THE FUSELAGE WHERE THE NR 1 ADF ANTENNA MOUNTS, 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 RRXA002860](https://openairdocs.org/sdr/RRXA002860.md): Floorbeam · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM AT FS 920 AND LBL 48 - 53, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DALFORT AEROSPACE LP XEA X8-53-880 REV - [SDR RRXA002859](https://openairdocs.org/sdr/RRXA002859.md): Floorboard · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PLANK AT FS 41 - 58 AND LBL 31 - LBL 44, 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. (CORROSI - [SDR RRXA002858](https://openairdocs.org/sdr/RRXA002858.md): Frame · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AT FS 25 AND STR 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 51-1-20D. (CORROSION DAMA - [SDR RRXA002857](https://openairdocs.org/sdr/RRXA002857.md): Skin · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Engine Thrust Reverser > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INNER SKIN OF THE NR 2 ENGINE I/B THRUST REVERSER, 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 78-31-10. - [SDR RRXA002856](https://openairdocs.org/sdr/RRXA002856.md): Floorboard · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER SIDE OF THE FLOOR WEB AT FS 25 - 55 AND LBL 57, 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 RRXA002855](https://openairdocs.org/sdr/RRXA002855.md): Shear Tie · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SHEAR TIE AT FS 640 AND STR 27R, 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 RRXA002854](https://openairdocs.org/sdr/RRXA002854.md): Angle · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ATTACH ANGLE AT THE LT WING T/E FLAP WELL PANEL AT STA XCW 69.5, 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 51-1-4 A - [SDR RRXA002853](https://openairdocs.org/sdr/RRXA002853.md): Shear Tie · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SHEAR TIE AT FS 640 AND STR 27L, 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 RRXA002852](https://openairdocs.org/sdr/RRXA002852.md): Frame · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE WEB AT FS 70 AND STR 21R, 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 RRXA002851](https://openairdocs.org/sdr/RRXA002851.md): Floorboard · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE FLOOR PLANK AT FS 1020 - 1023 AND RBL 17, 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 RRXA002850](https://openairdocs.org/sdr/RRXA002850.md): Floorbeam · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM ON THE FWD AND AFT FLANGES AT FS 940 AND RBL 53, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DALFORT AEROSPAC - [SDR RRXA002849](https://openairdocs.org/sdr/RRXA002849.md): Lever · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Power Lever > DURING A MAINTENANCE VISIT FOUND A CRACK AT THE NECK DOWN AREA WITH HFEC ON THE NR 1 THROTTLE LEVER, 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. - [SDR RRXA002848](https://openairdocs.org/sdr/RRXA002848.md): Angle · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Spoilers > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SUPPORT ANGLE IN THE LT W/W FOR THE SPOILER MIXER ASSY, 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. - [SDR RRXA002847](https://openairdocs.org/sdr/RRXA002847.md): Fitting · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND A CRACK ON THE LT WING FLAP HINGE SUPPORT FITTING ASSY ON O/B SIDE OF FITTING AT STA XF 409.667, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PART IAW - [SDR RRXA002846](https://openairdocs.org/sdr/RRXA002846.md): Fitting · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON END FITTING AT FS 8 AND L30R, 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 51-1-20D. - [SDR RRXA002845](https://openairdocs.org/sdr/RRXA002845.md): Frame · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A CRACK ON THE FRAME AT FS 260 AND STR 33R, 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 RRXA002844](https://openairdocs.org/sdr/RRXA002844.md): Lever · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Power Lever > DURING A MAINTENANCE VISIT FOUND A CRACK AT THE NECK DOWN AREA WITH HFEC ON THE NR 1 THROTTLE LEVER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21. - [SDR RRXA002843](https://openairdocs.org/sdr/RRXA002843.md): Angle · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Spoilers > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SUPPORT ANGLE IN THE LT W/W FOR THE SPOILER MIXER ASSY, 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 51-1-21. - [SDR RRXA002842](https://openairdocs.org/sdr/RRXA002842.md): Fitting · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING FLAP HINGE SUPPORT FITTING ASSY ON THE O/B SIDE OF FITTING AT STA XF 409.667, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW - [SDR RRXA002841](https://openairdocs.org/sdr/RRXA002841.md): Fitting · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE END FITTING OF LONGERON 30R AT FS 8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8S RM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. - [SDR RRXA002840](https://openairdocs.org/sdr/RRXA002840.md): Floorboard · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE FLOOR PLANK AT FS 1260 AND LBL 17, 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 RRXA002839](https://openairdocs.org/sdr/RRXA002839.md): Seat Track · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK AT FS 770 AND BL 0, 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 53-2-3. (CORROSION DAMAGE RECORD - [SDR RRXA002838](https://openairdocs.org/sdr/RRXA002838.md): Skin · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND A CRACK AT FASTENER HOLE ON THE RT WING L/E LWR SURFACE AT STA XFS 301.888, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DALFORT AEROSPACE LP XE - [SDR RRXA002837](https://openairdocs.org/sdr/RRXA002837.md): Pressure Panel · corroded · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WHEEL WELL PRESSURE FLOOR AT FS 930 - 943 AND RBL 56 - 64 WL-1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DALFORT - [SDR RRXA002836](https://openairdocs.org/sdr/RRXA002836.md): Frame · cracked · Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME AT FS 260 AND STR 33R, 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 RRXA003414](https://openairdocs.org/sdr/RRXA003414.md): Floor Panel · corroded · Jun 22, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT FWD LAV AREA BETWEEN STA'S 35.000 AND 55.000 AND X-44 AND -66, 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 51-20-01 - [SDR RRXA003415](https://openairdocs.org/sdr/RRXA003415.md): Stringer · corroded · Jun 8, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD AND AFT END OF STRINGER AT STA 35 TO 55 AND STR 26R, 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 51-1-20 - [SDR RRXA003452](https://openairdocs.org/sdr/RRXA003452.md): Floorboard · corroded · May 30, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBOARD PLANKS NEAR LAVATORY AT FS 41-57, X-31 TO -44, 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 DC-8 S - [SDR RRXA003450](https://openairdocs.org/sdr/RRXA003450.md): Skin · corroded · May 25, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER 'A' BIN CROSSSLIDE DOOR BILGE AREA AT FS 280-360, X54-X30, Z-34 TO -50 AND L27L TO L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. - [SDR RRXA003459](https://openairdocs.org/sdr/RRXA003459.md): Doubler · corroded · May 24, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE BOTTOM OF FUSELAGE WHERE NR 2 ADF ANTENNA IS MOUNTED AT FS 136 TO 160 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. - [SDR RRXA003458](https://openairdocs.org/sdr/RRXA003458.md): Doubler · corroded · May 24, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATC TRANSPONDER ANTENNA PLATE AND RING AT FS370.5 TO 379.5 AND L35.8L TO 35.8R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARTS AND - [SDR RRXA003457](https://openairdocs.org/sdr/RRXA003457.md): Skin · corroded · May 24, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM SIDE OF FUSELAGE WHERE NR 1 ADF ANTENNA MOUNTS AT FS X360 TO 380, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INST - [SDR RRXA003456](https://openairdocs.org/sdr/RRXA003456.md): Skin · corroded · May 23, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT THE AFT LWR BAG BIN AT CROSSSLIDE BILGE AREA AT STA 1214 TO 1220, X6 TO -6 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WI - [SDR RRXA003455](https://openairdocs.org/sdr/RRXA003455.md): Shear Tie · corroded · May 23, 2000 · N796FT · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT PIT INTERCOSTAL STR 31L O/B FACE BETWEEN STA'S 1340-1360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIN LIMITS. - [SDR RRXA003454](https://openairdocs.org/sdr/RRXA003454.md): Frame · corroded · May 23, 2000 · N796FT · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT PIT LOWER CAP OF FRAME FWD AT FS 1020-1040 AND STR 35R-35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC - [SDR RRXA003453](https://openairdocs.org/sdr/RRXA003453.md): Floorbeam · corroded · May 22, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER PORTION OF FLOOR BEAM AT STA 920, X-48 TO -53 AND Z-4 TO -7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED. - [SDR RRXA003416](https://openairdocs.org/sdr/RRXA003416.md): Stringer · corroded · May 21, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON STRINGER AND PNEUMATIC DUCT SUPPORT AT STA 25 TO 35, STR 25R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. MATERIAL LOSS WAS WITHIN LIMITS IAW DC-8 SRM 53-2-0 - [SDR RRXA003449](https://openairdocs.org/sdr/RRXA003449.md): Skin · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INNER SKIN AT STA 30 AND STR 27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. MATERIAL LOSS WITHIN LIMITS. (CORR - [SDR RRXA003448](https://openairdocs.org/sdr/RRXA003448.md): Floor Panel · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR SIDE OF FLOOR AT STA 25-55 AND LBL 51, 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 51-3-0. - [SDR RRXA003447](https://openairdocs.org/sdr/RRXA003447.md): Stringer · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD AND AFT END OF STRINGER REPAIR AT STA 35-55 AND STR 26R, 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 RRXA003446](https://openairdocs.org/sdr/RRXA003446.md): Floorbeam · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD UPPER FLANGE OF FLOOR BEAM AND LOWER SIDE OF FLOOR AT STA 45-55 AND LBL15-30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. MATERIAL LOSS WI - [SDR RRXA003445](https://openairdocs.org/sdr/RRXA003445.md): Floorbeam · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD UPPER FLANGE OF FLOOR BEAM AND LOWER SIDE OF FLOOR AT STA 55-57 AND LBL10 TO RBL10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. - [SDR RRXA003444](https://openairdocs.org/sdr/RRXA003444.md): Stringer · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER 25R AND PNEUMATIC DUCT SUPPORT AT STA 25 TO 35 AND STR 25R, DAMAGE EXCEEDEDN LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIN LIMITS. - [SDR RRXA003443](https://openairdocs.org/sdr/RRXA003443.md): Stringer · corroded · May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER 31R AT STA 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIN LIMITS. Next page: https://openairdocs.org/deregistered/N796FT-2004-10-27/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 = 'N796FT' AND deregistration_id = 'N796FT-2004-10-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N796FT-2004-10-27/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.