N796FT, cancelled Oct 27, 2004

Service difficulty reports · 83

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR RRXA010020Fire Loop · malfunctionedSHORTLY 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. Mar 15, 2001 · N796FT · Doug DC873F · Fire DetectionSDR RRXA010023Fire Loop · intermittentINTERMITTENT 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.Feb 16, 2001 · N796FT · Doug DC873F · Fire DetectionSDR RRXA002864Structure · corrodedDURING 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 IAWJul 12, 2000 · N796FT · Doug DC873F · AileronsSDR RRXA002863Skin · crackedDURING 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 ANJul 10, 2000 · N796FT · Doug DC873F · Wing, Plate/SkinSDR RRXA002862Skin · crackedDURING 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 AJul 10, 2000 · N796FT · Doug DC873F · Wing, Plate/SkinSDR RRXA002861Skin · corrodedDURING 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 53-2-0Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA002860Floorbeam · corrodedDURING 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 REVJul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA002859Floorboard · corrodedDURING 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. (CORROSIJul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA002858Frame · corrodedDURING 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 DAMAJul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002857Skin · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Engine Thrust ReverserSDR RRXA002856Floorboard · corrodedDURING 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. (Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA002855Shear Tie · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, StructureSDR RRXA002854Angle · crackedDURING 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 AJul 10, 2000 · N796FT · Doug DC873F · Trailing Edge FlapsSDR RRXA002853Shear Tie · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002852Frame · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002851Floorboard · crackedDURING 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. (Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA002850Floorbeam · corrodedDURING 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 AEROSPACJul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA002849Lever · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Power LeverSDR RRXA002848Angle · corrodedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · SpoilersSDR RRXA002847Fitting · crackedDURING 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 Jul 10, 2000 · N796FT · Doug DC873F · Trailing Edge FlapsSDR RRXA002846Fitting · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002845Frame · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR RRXA002844Lever · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Power LeverSDR RRXA002843Angle · corrodedDURING 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. Jul 10, 2000 · N796FT · Doug DC873F · SpoilersSDR RRXA002842Fitting · crackedDURING 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 Jul 10, 2000 · N796FT · Doug DC873F · Trailing Edge FlapsSDR RRXA002841Fitting · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002840Floorboard · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA002839Seat Track · corrodedDURING 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 RECORDJul 10, 2000 · N796FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA002838Skin · crackedDURING 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 XEJul 10, 2000 · N796FT · Doug DC873F · Wing, Plate/SkinSDR RRXA002837Pressure Panel · corrodedDURING 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 Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA002836Frame · crackedDURING 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.Jul 10, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR RRXA003414Floor Panel · corrodedDURING 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 Jun 22, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA003415Stringer · corrodedDURING 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 51-1-20Jun 8, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003452Floorboard · corrodedDURING 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 SMay 30, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA003450Skin · corrodedDURING 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.May 25, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003459Doubler · corrodedDURING 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.May 24, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003458Doubler · corrodedDURING 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 ANDMay 24, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003457Skin · corrodedDURING 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 INSTMay 24, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003456Skin · corrodedDURING 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 WIMay 23, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003455Shear Tie · corrodedDURING 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.May 23, 2000 · N796FT · Doug DC873F · Fuselage Main, StructureSDR RRXA003454Frame · corrodedDURING 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 DCMay 23, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR RRXA003453Floorbeam · corrodedDURING 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.May 22, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003416Stringer · corrodedDURING 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 53-2-0May 21, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003449Skin · corrodedDURING 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. (CORRMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003448Floor Panel · corrodedDURING 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.May 19, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA003447Stringer · corrodedDURING 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 DMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003446Floorbeam · corrodedDURING 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 WIMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003445Floorbeam · corrodedDURING 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.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003444Stringer · corrodedDURING 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.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003443Stringer · corrodedDURING 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.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/Stringer
Back to N796FT, cancelled Oct 27, 2004