N17812, cancelled Apr 1, 2004

Service difficulty reports · 89

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 = 'N17812' AND deregistration_id = 'N17812-2004-04-01'
  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 CALA0300159Skin · dentedMAINTENANCE FOUND A CREASE IN THE AFT UPPER CORNER OF THE OUTER SKIN OF THE AFT CARGO DOOR. THE CREASED AREA OF DOOR SKIN WAS REPAIRED IAW ECRA 5232-01023. A DIP WAS ISSUED TO PERFORM INSPECTION OF THE REPAIR IAW ECRA 5232-01023 BEGINNING AT OR BEFORE 45,815 CMar 11, 2003 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0300108Frame · corrodedINSPECTION FOUND BELTFRAME LOWER CHANNEL AND WEB CORRODED AT STA 1309 FROM LONGERON 28L TO 28R. REPAIRED IAW SRM 53-03, PAGE 04A, FIGURE 2A.Mar 8, 2003 · N17812 · Doug DC982 · Fuselage Main, FrameSDR CALA0300107Cable · out of rigTHE TAILCONE FAILED TO DROP WITHIN SPECIFICATIONS AT ALL THREE POSITIONS DURING FUNCTIONAL TEST. THE PULL EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW 53-53-00.Mar 8, 2003 · N17812 · Doug DC982 · Aerodynamic FairingsSDR CALA0300106Light · inoperativeTHE TAILCONE SLIDE LIGHT FAILED BATTERY TEST. THE SLIDE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 25-62-01.Mar 8, 2003 · N17812 · Doug DC982 · Escape SlideSDR CALA0300101Frame · crackedINSPECTION FOUND A 1" CRACK IN FRAME RADIUS AT STA 1418, LONGERON 2L AND 2R. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-04332.Mar 7, 2003 · N17812 · Doug DC982 · Fuselage Main, FrameSDR CALA0300100Web · corrodedINSPECTION FOUND WEB AT STA 1338 AFT PRESSURE BULKHEAD T-CAP CORRODED. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-4, FIGURE 1.Mar 6, 2003 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0300093Frame · crackedINSPECTION FOUND A 3/4" CRACK IN FRAME AT STA 1418, LONGERON 1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 4.Mar 3, 2003 · N17812 · Doug DC982 · Fuselage Main, FrameSDR CALA0300089Casting · crackedINSPECTION FOUND A 1/2" CRACK IN AFT ENTRY DOOR LEFT LOWER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-0.Mar 3, 2003 · N17812 · Doug DC982 · Passenger/Crew DoorsSDR CALA0100630Battery · dischargedTHE EMERGENCY CEILING LIGHTS WERE FOUND INOPERATIVE AT ROW 15. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Jul 2, 2001 · N17812 · Doug DC982 · Emergency LightingSDR CALA0000744Skin · crackedINSPECTION FOUND CABIN LT SUBFLOOR SKIN CRACKED AT FS 218. THE SUBFLOOR PANEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW SUBFLOOR WAS INSTALLED IAW SRM 53-14-1, 51-10-4, AND 51-30-1.May 25, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000743Cargo Track · corrodedINSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED FROM STA 1003 - 1212. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.May 25, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000304Clip · crackedINSPECTION FOUND A 2.3 INCH CRACK IN AFT CARGO FORWARD BULKHEAD FRAME CLIP AT STA 1003, LONGERON 28R. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-5, 51-10-3, 51-10-4, AND 51-30-2.Mar 13, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000303Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN PREVIOUS DOUBLER REPAIR OF UPPER FORWARD CORNER RT MLG DOOR. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Mar 13, 2000 · N17812 · Doug DC982 · Landing Gear DoorsSDR CALA0000301Floorbeam · gougedINSPECTION FOUND AFT CARGO CEILING FLOORBEAM GOUGED AT FS 1174, RBL 2. A DOUBLER AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 86, 51-10-2, 51-10-3, AND 53-04, FIGURE 36.Mar 11, 2000 · N17812 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000300Cargo Track · corrodedINSPECTION FOUND MID PIT RT CARGO TIE DOWN TRACK CORRODED FROM STA 427-636. THE TRACK WAS REMOVED AND NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.Mar 11, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000299Skin · dentedINSPECTION FOUND RUDDER SKIN DENTED AT UPPER LEFT SIDE. THE DENTED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 55-03 AND 51-10-3.Mar 11, 2000 · N17812 · Doug DC982 · Rudder, Plate/SkinSDR CALA0000298Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 133 BETWEEN LONGERONS 18L AND 19L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3.Mar 11, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000297Skin · dentedINSPECTION FOUND RIGHT EXTERNAL FUSELAGE SKIN DENTED AT STA 560 BETWEEN LONGERON 21R AND 22R. THE DOUBLER WAS REMOVED AND THE AREA WAS COLD WORKED IAW ECRA 5330-01856. A REPAIR WAS INSTALLED IAW SRM 51-10-3, 53-04, FIGURE 38, AND ECRA 5330-01856.Mar 11, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000296Stop · gougedINSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-2, 51-10-3, AND 51-30-2.Mar 11, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000295Skin · gougedINSPECTION FOUND LEFT AILERON LOWER SURFACE SKIN GOUGED. THE AILERON WAS REPAIRED IAW ECRA 5750-03367.Mar 11, 2000 · N17812 · Doug DC982 · AileronsSDR CALA0000294Pan · crackedINSPECTION FOUND SEVERAL .125 INCH CRACKS AROUND DOOR SEAL RIVET HOLE AT AFT CARGO DOOR UPPER AFT CORNER. THE FASTENERS WERE REMOVED IAW SRM 52-03, FIGURE 8. DOUBLERS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 52-03, FIGURE 8.Mar 11, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000291Bracket · crackedINSPECTION FOUND NR 2 T/R UPPER DOOR I/B SIDE WING FAIRING SUPPORT BRACKET AND ANGLE CLIP CRACKED. THE CRACKS WERE 1 AND 1/8 LONG. THE I/B SIDE SUPPORT BRACKET AND ANGLE CLIP WERE REMOVED IAW SRM 51-30-2. REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30Mar 10, 2000 · N17812 · Doug DC982 · Engine Thrust ReverserSDR CALA0000290Stop · gougedINSPECTION FOUND MID CARGO DOOR STOPS GOUGED IN TWO PLACES. DOUBLERS WERE INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5, AND ECRA 5330-02819.Mar 10, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000289Cargo Track · corrodedINSPECTION FOUND AFT CARGO TIE DOWN TRACK CORRODED FROM STA 1003 TO 1212. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.Mar 10, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000288Stop · gougedINSPECTION FOUND AFT CARGO DOOR STOPS GOUGED IN THREE PLACES. REPAIRS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND ECRA 5330-02819.Mar 10, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000287Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN NEXT TO TOP RT RADOME HINGE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 7.Mar 9, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000286Stop · wornINSPECTION FOUND MID CARGO DOOR STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2.Mar 9, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000285Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 200, LBL 12 TO LBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4.Mar 9, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000284Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AND DENTED AT FS 280 BETWEEN LONGERONS 22L AND 23L. THE AREA WAS COLD WORKED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 38 AND 51-10-3.Mar 9, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000283Cargo Track · corrodedINSPECTION FOUND AFT CARGO AFT RT TIE DOWN TRACK CORRODED AROUND FASTENER HOLES. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.Mar 9, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000282Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT FS 1309-1331, LONGERON 29R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Mar 8, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000281Floor Panel · corrodedINSPECTION FOUND COCKPIT FLOOR SKIN CORRODED AT FS 160, LBL 6. THE CORROSION WAS REMOVED IAW SRM 53-01, FIGURE 2 AND 51-10-3. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-04, 51-30-02.Mar 8, 2000 · N17812 · Doug DC982 · Fuselage Floor PanelSDR CALA0000280Stop · wornINSPECTION FOUND TWO MID CARGO DOOR STOPS WORN. REPAIRED STOPS IAW ECRA 5330-02819.Mar 8, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000279Stop · wornINSPECTION FOUND TWO AFT CARGO DOOR STOPS WORN. THE AREAS WERE REPAIRED IAW SRM 52-03, FIGURE 8, 51-30-2, 52-30-7, 51-10-3, AND ECRA 5330-02819.Mar 8, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000272Stop · gougedINSPECTION FOUND MID CARGO DOOR STOP GOUGED.. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.Mar 6, 2000 · N17812 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000271Angle · crackedINSPECTION FOUND FILLET PANEL SUPPORT ANGLE CRACKED AT STA 945, LONGERON 30. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-04, 51-10-3, AND 51-30-1.Mar 6, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000258Stop · gougedINSPECTION FOUND FORWARD CARGO DOOR STOP GOUGED. THE DOOR STOP WAS REPAIRED IAW ECRA 5330-02819.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000257Flange · corrodedINSPECTION FOUND ANTENNA FLANGE CORRODED IN MID PIT AT STA 600, LONGERON 29L TO 30. THE ANTENNA FLANGE WAS REMOVED AND A NEW FLANGE AND DOUBLER WERE INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000256Floorbeam · corrodedINSPECTION FOUND L-1 DOOR THRESHOLD LOWER SUB FLOOR WEB CORRODED AND ATTACH ANGLE CRACKED. THE SUB FLOOR WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUB FLOOR WEB WAS INSTALLED IAW SRM 53-14-1, FIGURE 1 AND 53-01, FIGURE 4. THE ATTACH ANGLE WAS REMOVED AND REPLAMar 3, 2000 · N17812 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000255Web · corrodedINSPECTION FOUND LEFT CUSP WEB ON FORWARD SIDE OF FRAME AT STA 237, LONGERON 18L CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. A DOUBLER, PLATE, TEE ANGLE, AND BRACKET WERE INSTALLED IAW SRM 53-01, 53-10-2, 51-30-3, AND 51-30-2.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000254Web · crackedINSPECTION FOUND A 3 INCH CRACK IN MAIN ENRTY DOOR AFT TORQUE BOX UPPER WEB TENSION LEG AT FS 208, LONGERON 11L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000253Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000252Intercostal · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO INTERCOSTAL AFT SUPPORT ANGLE AT STA 237 BETWEEN LONGERON 27R AND 28R. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000251Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 465 AND 484 AT LONGERON 21R AND 22R. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 8, CONDITION 2. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-3, 51-30-02, AND 53-04, FIGURE 38, VIEW P.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000250Seat Track · corrodedINSPECTION FOUND LEFT I/B SET TRACK CORRODED AT FS 1030-1300. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 5F.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000249Floorbeam · crackedINSPECTION FOUND A 3 INCH CRACK IN R-1 DOOR THRESHOLD FLOOR SUPPORT WEB AT FORWARD EDGE OF DOOR CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-30-2, AND 51-30-6.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000248Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER RUDDER FAIRING AT STIFFENER ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-4.Mar 3, 2000 · N17812 · Doug DC982 · Rudder StructureSDR CALA0000247Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 30 FILLET PANEL SUPPORT ANGLE AT STA 970. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-4.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000246Seat Track · corrodedINSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AT FS 1030-1100, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.Mar 3, 2000 · N17812 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000245Stop · wornINSPECTION FOUND FORWARD CARGO DOOR STOP WORN. REPAIRED IAW ECRA 5330-02819.Mar 3, 2000 · N17812 · Doug DC982 · Cargo/Baggage Doors
Back to N17812, cancelled Apr 1, 2004