N72821, cancelled May 17, 2005

Service difficulty reports · 29

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 = 'N72821' AND deregistration_id = 'N72821-2005-05-17'
  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 CALA0400628Beam · corrodedINSPECTION FOUND BULKHEAD BEAM WEB CORRODED AT STA 110, S30L. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387.Sep 4, 2004 · N72821 · Doug DC982 · Fuselage Main, BulkheadSDR CALA0300697Beam · corrodedINSPECTION FOUND STA 110 BULKHEAD BEAM WEB CORRODED AT MAIN BATTERY GROUND STUD HOLE. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387.Nov 20, 2003 · N72821 · Doug DC982 · Fuselage Main, BulkheadSDR CALA0200438Seat Track · corrodedINSPECTION FOUND L/H CENTER SEAT TRACK CORRODED BETWEEN STA 1079 AND 1136. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5.Aug 9, 2002 · N72821 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200437Web · corrodedINSPECTION FOUND E&E COMPARTMENT SUBFLOOR CORRODED AT VENTRAL STAIR MECHANISM, STA 162-168, X = 54.000. A DOUBLER WAS INSTALLED IAW SRM 51-70-4.Aug 9, 2002 · N72821 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0200436Seat Track · corrodedINSPECTION FOUND R/H CENTER AND R/H I/B SEAT TRACKS CORRODED AT STA 228. THE CORRODED SEAT TRACK SECTIONS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW SRM 53-05, FIGURE 4F AND 51-30-0.Aug 7, 2002 · N72821 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100757Skin · dentedTHE R/H FUSELAGE SKIN WAS DENTED BETWEEN FORWARD CARGO DOOR AND RIGHT TURN OFF LIGHT AT STA 435-510 BETWEEN LONGERONS 20R AND 21R. A FLUSH SKIN PANEL REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12C.Aug 10, 2001 · N72821 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100756Longeron · crackedINSPECTION FOUND A 10" CRACK AT END OF LONGERON 2L AT STA 1418. A HAT SECTION REPAIR SPLICE WAS INSTALLED IAW SRM 53-02, FIGURE 18.Aug 10, 2001 · N72821 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0100755Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN TAIL COMPARTMENT LEFT VENTRAL BOX SUPPORT ANGLE AT CANTED FRAME STA 1474. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05.Aug 10, 2001 · N72821 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100753Fitting · crackedINSPECTION FOUND A 2 INCH CRACK IN TAIL COMPARTMENT SUPPORT FITTING BETWEEN CANTED FRAMES 1463 AND 1485 AT LOWER AFT SIDE. THE SUPPORT FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4.Aug 9, 2001 · N72821 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100752Plate · corrodedINSPECTION FOUND HORIZONTAL STABILIZER PIVOT PLATE CORRODED AT LEFT I/B LUG BORES. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW EA 5530-01238.Aug 9, 2001 · N72821 · Doug DC982 · Horizontal Stabilizer StructureSDR CALA0100751Plate · corrodedINSPECTION FOUND HORIZONTAL STABILIZER PIVOT PLATES CORRODED AT RIGHT O/B AND RIGHT I/B LUG BORES. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW EA 5530-01238.Aug 9, 2001 · N72821 · Doug DC982 · Horizontal Stabilizer StructureSDR CALA0100750Frame · crackedINSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1474, LEFT LOWER SIDE, BY VENT BOX DRAIN HOSE. REPAIRED IAW ECRA 5310-04173.Aug 9, 2001 · N72821 · Doug DC982 · Fuselage Main, FrameSDR CALA0100747Attach Angle · crackedINSPECTION FOUND A 3/4" CRACK COMING FROM RIVET HOLE IN R/H SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463. THE CRACKED AREA WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23.Aug 8, 2001 · N72821 · Doug DC982 · Fuselage, Stabilizer Attach FittingsSDR CALA0100743Pan · crackedINSPECTION FOUND A 1" CRACK IN L/H MLG I/B DOOR PAN AT LEADING EDGE. THE DOOR PAN WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-3, 51-30-8, AND 51-10-2.Aug 7, 2001 · N72821 · Doug DC982 · Landing Gear DoorsSDR CALA9901487Skin · crackedINSPECTION FOUND A 3 CRACK IN RT WING LEADING EDGE UPPER SKIN AT STA XOS 286. A DOUBLER WAS INSTALLED IAW ECRA 5720-01773 AND A DIP WAS INITIATED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 14 DAYS AND TO INSTALL A PERMANENT REPAIR WITHIN 12 MONTHS.Nov 12, 1999 · N72821 · Doug DC982 · Wing, Plate/SkinSDR CALA9900245Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT SERVICE DOOR SKIN AT TOP AFT EDGE OF HOLD OPEN HOOK CUTOUT. REPAIRED IAW ECRA 5205-01008.Mar 11, 1999 · N72821 · Doug DC982 · Service DoorsSDR CALA9900243Bayonet · wornTHE FORCE REQUIRED TO RELEASE TAIL CONE USING EXTERNAL HANDLE WAS LOW. THE LEFT LOWER TAIL CONE BAYONET WAS REMOVED AND REPLACED DUE TO WEAR. AN ADJUSTMENT/TEST OF THE TAIL CONE RELEASE MECHANISM WAS PERFORMED IAW MM 53-53-00.Mar 10, 1999 · N72821 · Doug DC982 · Aerodynamic FairingsSDR CALA9900236Pan · crackedINSPECTION FOUND A 2.25 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD HOLD OPEN LATCH AND A .75 INCH CRACK IN AFT CARGO DOOR PAN AT AFT HOLD OPEN LATCH. INSTALLED REPAIRS IAW ECRA 5321-01010.Mar 9, 1999 · N72821 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9900228Beam · crackedINSPECTION FOUND TWO CRACKS IN THE NR 1 BEAM OF MAIN CABIN DOOR. THE BEAM HAD A .75 INCH CRACK ON AFT END AND A .375 INCH CRACK ON FORWARD END.Mar 6, 1999 · N72821 · Doug DC982 · Passenger/Crew DoorsSDR CALA9900227Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AROUND SCREW HOLES AT LT I/B POSITION, STA 1117-1174 AFT GALLEY AREA. NEW SEAT TRACK SECTIONS WERE INSTALLED IAW SRM 53-05.Mar 5, 1999 · N72821 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900224Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 ABOVE CUSP. A NEW SKIN SECTION WAS INSTALLED BETWEEN LONGERON 15L AND 18L IAW ECRA 5330-02445.Mar 5, 1999 · N72821 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900221Pan · crackedINSPECTION FOUND A 1.5 INCH CRACK IN MID CARGO BIN DOOR PAN. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 26A.Mar 4, 1999 · N72821 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9900220Seat Track · corrodedINSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AROUND SCREW HOLES FROM GALLEY NR 3 TO GALLEY NR 4 AREA, STA 1117 TO 1174. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.Mar 4, 1999 · N72821 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900212Angle · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63 AND 51-30-5.Mar 3, 1999 · N72821 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800659Sensor · inoperativeTHE AIRCRAFT HAD A BRIEF HISTORY OF THE NOSE GEAR UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. CYCLING THE GEAR WOULD EXTINGUISH THE LIGHT. THE NOSE GEAR LOCK SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-05, PAGES 216-220. THE NOSE GEAR WAS SWUNG WITH OApr 15, 1998 · N72821 · Doug DC982 · Landing Gear Position and WarningSDR CALA9700365Skin · damagedFINGER DOUBLERS WERE INSTALLED TO FUSELAGE SKIN AT STA 427 TO 507, LONGERON 20L IAW SRM 53-04, FIGURE 12B. THE SKIN DAMAGE HAD BEEN REPAIRED PREVIOUSLY AND DEFERRED PER DIP NR D16874.Mar 12, 1997 · N72821 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9700363Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN RT MLG INBOARD DOOR FORWARD JAMB CHANNEL. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.Mar 12, 1997 · N72821 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL950872Skin · tornTUS - FLT 0425 - INSPECTION FOUND A 1.5 INCH TEAR IN FUSELAGE SKIN AND DAMAGE TO TWO SKIN CLIPS DUE TO GROUND DAMAGE. THE DAMAGE WAS LOCATED AT STA 427-STA 507 AND LONGERONS 19L AND 20L. THE SKIN TEAR WAS REPAIRED IAW ECRA 5330-02317 AND SRM 53-04, FIGURE 12Sep 25, 1995 · N72821 · Doug DC982 · Fuselage Main, Plate/SkinSDR CAL950464Eel Pwr Supply · inoperativeFLT NR 0305 - EWR - BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE POWER SUPPLY WAS REPLACED AND OPERATION OF THE OVERWING EMERGENCY EXIT LIGHTS WAS RESTORED. (M)Jun 7, 1995 · N72821 · Doug DC982 · Emergency Lighting
Back to N72821, cancelled May 17, 2005