N709BR
Service difficulty reports · 206
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 = 'N709BR' 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 = 'N709BR' 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 SWIA2020032649405Seat Track · corroded* CORROSION ON RH SIDE SEAT TRACK BETWEEN FS513 AND FS544 (MARKED). (C-CHECK) RO 3/25/2020 REMOVED THE CORROSION FROM THE RH SIDE SEAT TRACK, FOUND TO BE OUT OF LIMITS REFERENCE CRJ200 SRM. REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN FS513 AND FS544 WSDR SWIA2020032649404Support Angle · corroded* FLIGHT DECK FLOOR SUPPORT ANGLE AT FS280, LBL9 TO RBL9 IS CORRODED. (C-CHECK) RO 3/25/2020 BLENDED OUT CORRSION ON COCKPIT FLOOR SUPPORT ANGLE FS280.00 LBL9.0 TO RBL9.0. REF: CRJ-200 SRM 51-21-06. BLENDED AREA FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. SDR SWIA2020032649379Post · defectiveF.S 409+128 BL 0.0 LH AFT VERTICAL POST RADIUS DEFECT NOTED. (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW L/H AFT VERTICAL POSTAND CLIP REF BOMBARDIER REO, BOMBARDIER DWG, CRJ 200 SRM, BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649378Floorbeam · corroded* THE FLOORBEAM AT LBL27.00 FROM APPROX. FS559.00+80 TO FS574.00 HAS CORROSION. (MARKED) (C-CHECK) RO 3/25/2020 BLENDED CORROSION FROM FLOOR BEAM AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE FLOOR BEAM AT LBL27.00 FS559+10 TO FS569.00 REF CRJ200 SRM. REPSDR SWIA2020032649377Door Sill · corroded* THE RH FLOOR SILL HAS CORROSION FROM APPROX. FS559.00+80 TO FS559.00+112. (MARKED) (C-CHECK) RO 3/25/2020 BLENDED OUT DAMAGE ON RH FLOOR SILL FROM FS559.00+80 TO FS559.00+112. REF: REO. THE REWORKED AREA IS OUT OF LIMITS REF REO. REMOVED AND REPLACED THSDR SWIA2020032649376Seat Track · corroded* THE SEAT TRACK AT RBL9.00 FROM APPROX FS559.00+80 TO FS559.00+96 HAS CORROSION. (MARKED) (C-CHECK) RO 3/25/2020 REMOVED THE CORROSION FROM THE SEAT TRACK AT RBL9.00 FROM APPROX FS559.00+80 TO FS559.00+96 REFERENCE CRJ200 SRM. EVALUATED AND FOUND TO BE OSDR SWIA2020032649375Seat Track · corroded* THE SEAT TRACK ON THE FLOOR ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT LBL9.00 HAS CORROSION. (MARKED) (C-CHECK) RO 3/25/2020 BLENDED OUT CORROSION ON SEAT TRACK, NEAR THE REAR PRESSURE BULKHEAD(FS621) LBL9.0. REF CRJ 200 SRM. BLEND OUT OF LIMITS ON SESDR SWIA2020032649374Attach Fitting · corroded* THE FLOORBEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT LBL9.00 HAS CORROSION. (MARKED) (C-CHECK) RO 3/25/2020 REMOVED CORROSION FROM FLOORBEAM ATTACHMENT TO THE REAR BULKHEAD AT LBL9. FOUND TO BE OUT OF LIMITS. REPAIRED BLENDED AREA. COMPLIED WITH ALSDR SWIA2020032649373Bracket · cracked* FLOOR BEAM BRACKET AT FS461, LBL27, INBOARD, IS CRACKED (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW FLOOR BEAM BRACKET AT FS.461 INBD OF LBL.27 REF CRJ 200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649372Support Fitting · cracked* PRESSURE FLOOR SUPPORT CLIP AT FS484, LBL27 IS CRACKED. (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED PRESSURE FLOOR SUPPORT CLIP AT FS484, LBL27 WITH NEW FABRICATED CLIP REF PREVIOUSLY INCORPERATED REO, SRM. SEE CONTINUATION CARD FOR DETAILSDR SWIA2020032649371Support Fitting · cracked* PRESSURE FLOOR SUPPORT CLIP AT FS484, LBL36 IS CRACKED. (C-CHECK) RO 3/25/2020 INSTALLED NEW PRESSURE FLOOR SUPPORT CLIP AT FS484, LBL36 REO. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649370Cup · corroded* FORWARD PAX DOOR HANDRAIL CUP IS CORRODED. (C-CHECK) RO 3/25/2020 REMOVED CORROSION FROM PAX DOOR FWD HANDRAIL CUP, EVALUATED AND FOUND TO BE OUT OF ALLOWABLE LIMITS, REF CRJ 200 SRM. REMOVED AND REPLACED HANDRAIL CUP WITH NEW P/N 601R31527-217, REF BOMSDR SWIA2020032649369Floorbeam · corroded* THE FLOORBEAM AT RBL 9.00 FROM FS559.00+48 TO FS559.00+80 APPROX. HAS CORROSION IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK) RO 3/25/2020 REPAIRED FLOORBEAM AT RBL 9.00 FROM FS559.00+48 TO FS559.00+80 REF CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649368Seat Track · corroded* THE SEAT TRACK AT RBL 9.00 FROM FS559.00 TO FS559.00+80 APPROX. HAS CORROSION. (MARKED) (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FLOOR SEAT RAIL FROM RBL 9.00 FROM FS559.00 TO FS559.00+80. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK REFERENCSDR SWIA2020032649367Floorbeam · corroded* FS280 FLOOR BEAM IS CORRODED BETWEEN LBL9 AND RBL9, MARKED. (C-CHECK) RO 3/25/2020 REPAIRED FS280 BULKHEAD WEB BETWEEN LBL20.75 AND RB20.75 AND INSTALLED NEW RECEPTABLE , REF REO. SEE CONTINUATION CARD FOR DETAILSDR SWIA2020032649366Angle · corroded* L/H PRESSURE FLOOR SILL ANGLES ARE CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK) RO 3/25/2020 REPAIRED L/H PRESSURE FLOOR SILL ANGLES REF BOMBARDIER REO. SEE CONTINUTION CARD FOR DETAILSSDR SWIA2020032649365Panel · corroded* L/H PRESSURE FLOOR SILL PANEL IS CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK) RO 3/25/2020 REPAIRED L/H PRESSURE FLOOR SILL PANEL REF BOMBARDIER REO. SEE CONTINUTION CARD FOR DETAILSSDR SWIA2020032649364Plate · corroded* R/H PRESSURE FLOOR SILL PLATE IS CORRODED IN MULTIPLE SPOTS, MARKED. (C-CHECK) RO 3/25/2020 REPAIRED R/H PRESSURE FLOOR SILL PLATE REF BOMBARDIER REO. SEE CONTINUTION CARD FOR DETAILSSDR SWIA2020032649363Frame · corroded* FRAME AT FS333 FORWARD AND AFT SIDES CORRODED BETWEEN STR26L AND STR26R. (C-CHECK) RO 3/25/2020 REPAIRED FRAME AT FS333 BETWEEN STR26L AND STR26R REF BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649413Pin · chafed* THE PAX DOOR LOWER FWD LATCH PIN IS CHAFFED. (MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED THE PASSENGER DOOR LOWER FWD LATCH PIN REF CRJ-200 AMM. OP CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649412Pin · chafed* THE PAX DOOR UPPER FWD LATCH PIN IS CHAFFED. (MARKED) (C-CHECK) RO 3/25/2020 INSTALLED SERVICEABLE PASSENGER DOOR UPPER FWD LATCH PIN(1EACH P/N 601R38380-11) AND NEW WASHER(1EACH) REF CRJ-200 AMM. TORQUE WRENCH TUC4822, DUE 4/30/20. OP OP TEST GOODSDR SWIA2020032649411Flap · chafed* THE PAX DOOR PRESSURE VENT FLAP ON THE INSIDE IS CHAFFED. (MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED PRESSURE VENT FLAP ON THE PAX DOOR REF CRJ 200 AMM. PERFORMED OPERATIONAL TEST OF THE PAX DOOR PRESSURE VALVE. REF CRJ 200 AMM. NO DEFECTS NOTSDR SWIA2020032649403Skin · corroded* CORROSION ON FUSELAGE SKIN BETWEEN APPROXIMATELYFS559+32 AND FS559+64 AND BETWEEN STR 26R AND STR 26L (AREA MARKED). (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FUSELAGE SKIN APPROX. FS 559+32" AND FS 559+64" AND BETWEEN STR 26R AND STR 26L. REF:L CRJ 20SDR SWIA2020032649402Panel · corroded* CORROSION ON FUSELAGE AT MULTIPLE FASTENER LOCATIONS FOR PANELS 191BB AND 192BB BETWEEN APPROXIMATELY FS 409+64 AND FS409+100 BELOW STR20L AND STR20R (MARKED). (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FUSELAGE AT MULTIPLE FASTENER LOCATIONS FOR PANELSSDR SWIA2020032649401Web · corroded* THE PAX DOOR FWD WEB HAS CORROSION ON THE UPPER INNER SIDE. (MARKED). (C-CHECK) RO 3/25/2020 FOUND MULTIPLE AREAS OF CORROSION ON PAX DOOR FWD STAIR WEB, PART FOUND TO BE OUT OF ALLOWABLE LIMITS, REMOVED AND REPLACED PAX DOOR FWD WEB WITH NEW WEB (P/N 6SDR SWIA2020032649399Pulley · cracked* THE PAX DOOR SUPPPORT WHEEL PIVOT FITTING PULLEY IS CRACKED. (MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED THE PAX DOOR SUPPPORT WHEEL PIVOT FITTING PULLEY IAW BOMBARDIER CMM PASSANGER DOOR P/N CC670-38601 52-11-00, REMOVAL STEP 1A(9) PG 3011, RESDR SWIA2020032649362Hinge · nicked* PASSENGER DOOR HINGE FUSELAGE SIDE FLANGE ATTACHED TO THE SILL HAS NICKS IN AREA OF 7TH AND 8TH LUGS FROM AFT END (MARKED WITH BLACK GREASE PENCIL). (C-CHECK) RO 3/25/2020 FURTHER INSPECTION FOUND HINGE LUGS 1-7 AND 12 FROM AFT END OF HINGE I.D. EXCEEDEDSDR SWIA2020032649361Skin · chafed* LH WING LOWER PLANK CHAFED AT APPROXIMATELY LBL 45 (MARKED). (C-CHECK) RO 3/25/2020 REPAIRED L/H WING LOWER PLANK AT APPROXIMATELY LBL 45 REF REO. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649360Skin · chafed* RH WING LOWER PLANK CHAFED AT APPROXIMATELY RBL 45 (MARKED). (C-CHECK) RO 3/25/2020 REPAIRED R/H WING LOWER PLANK AT APPROXIMATELY LBL 45 REF REO. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020032649359Skin · corroded* CORROSION ON FUSELAGE SKIN BETWEEN APPROXIMATELY FS559+8 AND FS559+32 AND BETWEEN STR 26R AND STR 26L (AREA MARKED). (C-CHECK) RO 3/25/2020 REPAIRED FUSELAGE SKIN BETWEEN APPROXIMATELY FS559+8 AND FS559+32 AND BETWEEN STR 26R AND STR 26L REF BOMBARDIER SDR SWIA2020032649358Fitting · cracked* RIGHT SIDE LOWER OUTBD WINDSHIELD POST CLIP CRACKED (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED THE RH LOWER OUTBD WINDSHIELD POST CLIP WITH NEW PART REFERENCE CRJ200 SRM & BOMBARDIER DWG. APPLIED CIC AS REQUIRED.SDR SWIA2020032649400Rib · corroded* L/H BATT RIB AT WS53-60, FORWARD SECTION IS CORRODED AROUND CANON PLUGS, MARKED IN RED. (C-CHECK) RO 3/25/2020 BLENDED CORROSION FROM L/H BATT RIB AT WS53-60, FORWARD SECTION AROUND CANON PLUGS, REF CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS ON L/H BATT RSDR SWIA2020032649357Angle · cracked* R/H BATT RIB AT WS48.30 TOP ANGLE IS CRACKED, MARKED IN RED. (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED NEW R/H BATT RIB AT WS48.30 TOP ANGLE P/N 600-10389-2 REF BOMBARDIER DWG AND CRJ200 SRM. RESTORED FINISH CRJ200 SRM.SDR SWIA2020032649356Angle · cracked* L/H BATT RIB AT WS48.30, TOP ANGLE IS CRACKED, MARKED IN RED. (C-CHECK) RO 3/25/2020 REMOVED CRACKED LH BATT RIB TOP AFT ANGLE AND REPLACED WITH NEW L/H BATT RIB TOP AFT ANGLE AT WS.48.30 WITH NEW FASTENERS PER CRJ200 SRM AND BOMBARD. DWG. COMPLIED WISDR SWIA2020032649355Hinge Arm · gouged* RH INBOARD FLAP INBOARD HINGE ARM GOUGED AT ATTACHMENT TO HINGE BOX (MARKED). (C-CHECK) RO 3/25/2020 BLENDED GOUGE ON RH INBOARD FLAP INBOARD HINGE ARM AT ATTACHMENT TO HINGE BOX REF CRJ-200 SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. RSDR SWIA2020032649354Stop Fitting · chafed* L/H AFT AVIONICS DOOR STOP FITTING ON FUSELAGE IS CHAFED. (C-CHECK) RO 3/25/2020 REPLACED L/H AFT AVIONICS DOOR STOP FITTING ON FUSELAGE. REF CRJ200 SRM AND BOMBARDIER ENG. DWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)SDR SWIA2020032649353Stop Fitting · chafed* R/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE IS CHAFED. (C-CHECK) RO 3/25/2020 REPLACED R/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE. REF CRJ200 SRM AND BOMBARDIER ENG. DWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**).SDR SWIA2020032649352Stop Fitting · chafed* L/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE IS CHAFED. (C-CHECK) RO 3/25/2020 REPLACED L/H FORWARD AVIONICS DOOR STOP FITTING ON FUSELAGE. REF CRJ200 SRM AND BOMBARDIER ENG. DWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)SDR SWIA2020032649351Skin · gouged*NICKS AND GOUGES ON EXTERNAL SKIN SURROUNDING CARGO DOOR HANDLE(MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED WITH NEW CARGO DOOR HANDLE HOUSING REF CRJ200 SRM AND BOMBARDIER DWG OPERATIONAL AND PRESSURE CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARSDR SWIA2020032649350Skin · gougedD: GOUGE DAMAGE SINGLE DENT TO LHS FUSELAGE SKIN, FS333.00-FS349.00, STR 19L - STR 22L COMPLIED WITH TEMPORARY REPAIR PER REO. PERMANENT REPAIR WITHIN 3400 FLIGHT HOURS PER REO 601R-53-21-3124 REV B DUE BY TAT 39961.2. C: MCI RA# 48096 NOTE: BUILT MX CODE SDR SWIA2020032649349Skin · scratchedCOMPLY WITH SCHEDULED MAINTENANCE CODE: FOUND PAINT SCRAPED DOWN TO THE SKIN BELOW THE CARGO BAY DOOR. BETWEEN FS605.00 AND FS589.00 AND BETWEEN STGR19L STGR20L. COMPLIED WITH TEMP REPAIR PER REO. PERFORMED NDT LPI. NO CRACKS FOUND. PRIMERED THE AREA AS REQUSDR SWIA2020032649348Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB ASDR SWIA2018071644883Warning System · false activationGEAR DISAGREE ON FINAL. BOTH CLEARED WITHOUT RECYCLING GEAR. FLIGHT 3114. HYDRAULICS INDICATE NORMAL WITH GOOD QUANTITY AND PRESSURES, PERFORMED A NOSE GEAR SWING SEVERAL TIMES, WITHIN LIMITS PER FIM 32-60,32-60-08 AND AMM 32-00-00 ALL CHECKS GOOD OK FOR CONTSDR SWIA2018030144340Cover Plate · chafedLEFT AND RIGHT REAR SPAR WEB COVER PANELS ARE CHAFED AND HAVE MULTIPLE POINTS OF CORROSION. REPLACED THE SPAR WEB COVER PLATES IAW SRM.SDR SWIA2018030144339Frame · crackedBS 333 FRAME CRACKED BETWEEN STRINGERS 0 AND 1L. PERFORMED A CUT-OUT OF DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW SRM AND REO.SDR SWIA2018030144338Floorbeam · corrodedCABIN FLOORBEAM AT BS 349 CORRODED BETWEEN LBL 27 AND LBL 42. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM.SDR SWIA2018030144337Floorbeam · corrodedCORROSION ON THE FLOORBEAM BS 589, LBL 9- LBL 27. REMOVED AND REPLACED THE FLOORBEAM IAW SRM.SDR SWIA2018030144336Door Sill · corrodedCORROSION ON THE CARGO DOOR SILL AT BS 568. REPLACED THE CARGO DOOR SILL IAW REO.SDR SWIA2018030144335Strap · corrodedRT SIDE BS 559 FLOORBEAM STRAP HAS CORROSION BETWEEN RBL 27 TO RBL 36. REMOVED AND REPLACED THE STRAP IAW SRM.SDR SWIA2018030144334Inlet · dentedLH ENG. - NOSE INLET-COWL - L/E DENTED. (C-CHECK) RO: 02/28/2017 REMOVED AND REPLACED L/H ENGINE NOSE INLET COWL IAW AMM. OPS CHECKS SATISFACTORY.
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