N363CM
Service difficulty reports · 85
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 = 'N363CM' AND registry_match = 'registration' 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.
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 = 'N363CM' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA202006250078Skin · corrodedRH WING UPPER SURFACE, EXFOLIATION ON SKIN APPROX. 45 FEET OUTBD OF FUSELAGE AND 2.2 FEET AFT OF FRONT SPAR. THE AIRPLANE WAS GROUNDED.SDR ABXA202006250076Skin · corrodedRIGHT WING UPPER SURFACE, EXFOLIATION ON SKIN APPROX. 18 FEET OUTBD OF FUSELAGE AND 6.8 FEET AFT OF FRONT SPAR. THE AIRPLANE WAS GROUNDED.SDR ABXA202006250075Skin · corrodedRH WING UPPER SURFACE, EXFOLIATION ON SKIN APPROX. 7 FEET OUTBD OF FUSELAGE AND 5 INCHES AFT OF FRONT SPAR. THE AIRPLANE WAS GROUNDED.SDR ABXA202006250074Scuff Plate · crackedL1 FWD ENTRY DOOR CTR SCUFF PLATE HAS 2 CRACKS EMANATING FROM CTR. THE AIRPLANE WAS GROUNDED.SDR ABXA20190104001Skin · damagedDAMAGE ON THE FUSELAGE SKIN AFT OF THE FORWARD LOWER CARGO DOOR AT STA 618, S31R. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20181211150Skin · damagedDAMAGE IN FUSELAGE SKIN AFT OF THE FORWARD LOWER CARGO DOOR AT BODY STATION 618, STRINGER 31 RIGHT. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201805219050Beam · corrodedCORROSION FOUND ON THE RIGHT WING NOSE BEAM WEB AT WS 500. THE NOSE BEAM WAS REPAIRED. THE ACFT WAS GROUNDED.SDR ABXA201808189049Support Angle · corrodedCORROSION ON THE SUPPORT ANGLE AT BS 1750, STRINGER 4R AT THE PERIMETER OF THE APU INLET BOX ASSEMBLY, UPPER AFT CORNER. THE ANGLE WAS REPLACED. THE ACFT WAS GROUNDED.SDR ABXA201805189048Angle · corrodedCORROSION FOUND ON THE KEEL BEAM ANGLE AT BS 782, RBL 9.5. THE ANGLE WAS REPAIRED. THE ACFT WAS GROUNDED.SDR ABXA201808189047Angle · corrodedCORROSION ON THE KEEL BEAM WEB ANGLE AT BS 1080, BL 0. THE ANGLE WAS REPLACED. THE ACFT WAS GROUNDED.SDR ABXA20180521046Skin · corrodedCORROSION ON THE INBOARD SKIN OF THE LEFT WING OUTBOARD AILERON OUTBOARD BALANCE ARM. THE SKIN WAS REPLACED. AIRPLANE WAS GROUNDED.SDR ABXA20160326075Skin · corrodedRIGHT WING UPPER TRAILING PANEL, ABOVE INBD AILERON INBD CORNER HAS SHEARED. FOUND CORROSION UNDER RT WING AT BULGED & SHEARED FASTENER LOCATION. REMOVED TE PANE CORROSION ON RT UPPER WING SKIN WS 433 - 448 AT REAR SPAR. THICK .210, MAT REMOVED .082, MAT RESDR ABXA20160323072Web · corrodedBULK CARGO DOOR CUT OUT LOWER WEB, LOWER SURFACE CORRODED. REMOVED FLOOR PANEL TO STATION 1417 - 1540, BL 0 - LBL 42. REMOVED CORROSION FROM WEB IAW SRM. CORROSION REMOVAL BEYOND LIMITS IAW SRM 53-00, THICKNESS 0.100 WITH 0.050 REMAINING, 0.050 MATERIAL REMSDR ABXA20160323071Plate · corrodedBULK CARGO DOOR CUT OUT LOWER WEB, UPPER SURFACE HAS CORROSION. REMOVED CORROSION FROM FLOOR PLATE WEB FROM STATION 1417 - 1461, DOOR SURROUND LOWER SILL, IAW SRM 51-10-02. CORRODED BEYOND LIMITS IAW SRM 53-00-15. ORIGINAL THICKNESS 0.050, REMAINING 03050 MSDR ABXA20160321074Skin · corrodedRIGHT WING NR 11 SLAT, LOWER SURFACE AT INBD AUXILIARY TRACK ATTACHMENT FASTENER. CLEANED AREA & REMOVED LIGHT SURFACE CORROSION AT RT WING NR 11. SURFACE AT INBD AUXILIARY TRACK ATTACHMENT FASTENER AREA. CHECKED TO BE OUT OF LIMITS IAW SRM 57-43-01. ALODISDR ABXA20160321073Skin · corrodedRIGHT WING NR 11 SLAT, LOWER SURFACE AT INBD ROTARY ARM ATTACHMENT FASTENER. REMOVED CORROSION & CHECKED LIMITS AT RT WING NR 11 SLAT, LOWER SURFACE ROTARY ARM ATTACHMENT FASTENER AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01. ALODINED AREA IAW SOPM 20-4SDR ABXA20160124001Latch · malfunctionedDURING DESCENT THROUGH FL250, THE LT FWD ENTRY DOOR LATCH RELEASED TO THE OPEN POSITION WITH ASSOCIATED, L FWD ENT DOOR, EICAS MSG. PRESSURIZATION HELD THROUGHOUT THE APPROACH. UPON TOUCHDOWN, THE DOOR RELEASED TO THE FULL OPEN POSITION. A GENERAL VISUAL INSDR ABXA20140812259Intercostal · corrodedCORROSION BETWEEN STATION 544 - 566 LBL45 AT BALL MAT NUTPLATE ATTACH POINT. REMOVED CORROSION IAW SRM 51-10-00, REPAIRED AREA AT LBL 45 BETWEEN 544 - 566 IAW SRM 51-70-11. CORRODED LEVEL 2, PN 143T5021, PART NAME INTERCOSTAL, SN NSN, FS & BS LOC FROM 544 TOSDR ABXA20140812257Frame · crackedFUSELAGE FRAME FAIL SAFE AT BS 904 LT IS CRACKED AT THE LOWEST FASTENER BELOW FLOOR. REPAIRED FUSELAGE FRAME CHORD AT BS 904 LT IAW JC EA 53000051-101. PN 691T0003T51, PART NAME INNER CHORD, SN NSN, CRACKED LENGTH 1.1, EXACT FS & BS LOC ON ACFT 904. ACFT WASDR ABXA20140810258Skin · crackedFUSELAGE SKIN CRACKED IN TWO PLACES AT FS 1658, STRINGER 12A LT. CUT OUT DAMAGED SKIN, FABRICATED DOUBLER & FILLER FROM 7075T6 .071 & .063 PO 0050971 & 0053815 & INSTALLED IAW SRM 53-00-01, REPAIR 1. TREATED, PRIMED & TOPCOAT IAW SRM 51-20-01. PN 148T3131-5SDR ABXR2012101900063Skin · crackedDENT ON EXISTING REPAIR AT STATION 618-635, STRINGERS S-26R AND S-30R. REPAIR REMOVED, CRACKS DISCOVERED IN 3 LOCATIONS ON THE SKIN. CUT OUT DAMAGE AND REPAIRED IAW EA B653-60359-MR, REV IR.SDR ABXR2012033100041Skin · crackedFUSELAGE SKIN CRACKED AT STA 1726. REPAIRED IAW SRM.SDR ABXR2012033100040Failsafe · corrodedFAILSAFE AREA CORRODED AT BS 955 S23-26L. REPAIRED IAW AMES REA 46938REA05.SDR ABXR2012033100039Skin · corrodedRIGHT WING UPPER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 350 AND WS 1021. REPAIRED IAW SRM AND REA 46938REA13.SDR ABXR2012033100038Skin · corrodedLEFT WING LOWER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 375 AND WS 992. REPAIRED IAW SRM AND AMES REA 46938REA10.SDR ABXR2012033100037Skin · corrodedLEFT WING UPPER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 344 AND WS 916. REPAIRED IAW SRM AND REA'S 46938REA09, 46938REA12, AND 46938REA24.SDR ABXR2012033100036Skin · damagedRT WING LOWER SURFACE HAS DAMAGE TO SEVERAL FASTENER HOLES BETWEEN WS 375 AND WS 1067. REPAIRED IAW SRM AND REA'S 46938REA11, 46938REA20, AND 46938REA26.SDR ABXR2012033100035Skin · corrodedRIGHT WING LOWER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 375 AND WS 1067. REPAIRED IAW SRM AND REA'S 46938REA11 AND 46938REA16.SDR ABXR2012033100034Fitting · damagedBS 1809 RT LOWER CHORD TENSION FITTING HAS HOLE DAMAGE. R & R TENSION FITTING IAW REA 46938REA22.SDR ABXR2012033100033Fitting · crackedRIGHT BS 1809 FWD SPLICE FITTING HAS CRACK INDICATION. R & R SPLICE FITTING IAW REA 46938REA28.SDR ABXR2012033100032Fitting · corrodedLEFT KICK FITTING CORRODED. R & R KICK FITTING IAW REA 46938REA21.SDR ABXR2012033100031Housing · debondedRIGHT OVERWING FILL HOUSING DID NOT BOND CHECK PROPERLY. REPAIRED IAW AMES REA 46938REA15.SDR ABXR2012033100029Skin · chafedFUSELAGE SKIN DAMAGED AT STA 1809, S12R. REPAIRED IAW SRM.SDR ABXR2012033100030Skin · corrodedFUSELAGE SKIN EXPOSED BY LT FAILSAFE STRAP CORRODED. REPAIRED IAW SRM AND REA 46938REA06.SDR ABXR2012033100028Structure · crackedBS 1809 RT/FWD UPPER CHORD CRACKED AT LWR/FWD FASTENER HOLE. R & R CHORD IAW AMES REA 46938REA19.
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