N228PS
Service difficulty reports · 98
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 = 'N228PS' 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 = 'N228PS' 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 SWIA202162686None · corrodedR/H AILERON PCU'S (BOTH) SHOW SIGNS OF CORROSION ON CLEVIS SUBASSEMBLIES. REMOVE & INSPECT, REPLACE IF NECESSARY (FILED CLOSED) REMOVED AND REPLACED WITH SERVICIABLE UNITS BOTH I/B AND O/B R/H AILERON PCU'S IAW CRJ 200 AMM 27-14-01. RIGGING CHECK GOOD. LSDR SWIA202162682None · corrodedFLOOR SILL BETWEEN FS 559.00 TO FS FS 559.00+80 L/H SIDE CORRODED (FILED CLOSED) REMOVED AND REPLACED FLOOR SILL BETWEEN FS 559.00 TO FS 559+80 LH SIDE IAW CRJ200 SRM 51-42-06 AND SRM 51-42-21SDR SWIA202162679None · corrodedCROSSBEAM @ FS349 RBL 39 TOP SURFACE CORRODED (FILED CLOSED) CORROSION FOUND TO BE OUT OF LIMITS REPAIRED CROSSBEAM AT FS 349 RBL39 IAW REO 601R-53-21-2745 BOMBARDIER REV-- 2016-11-18 CRJ200 SRM 51-42-21 SRM SRM 51-23-00 SRM 51-42-10 SRM 51-42-13 SRM 51-SDR SWIA202162681None · corrodedTOP OF INTERCOSTAL BETWEEN RBL 9.0 & RBL 27.0 CORRODED IN MULTIPLE PLACES (FS 559+96) (FILED CLOSED) FOUND CORROSION TO BE OUT LIMITS IAW CRJ200 SRM 53-00-00 REMOVED CROSSBEAM CAP AT FS559+96 RBL9 TO RBL27 IAW CRJ200 SRM 51-42-06 FABRICATED REPLACEMENTSDR SWIA202162678None · corrodedSTRAP ON TOP OF RBL 9 FROM ROUGHLY 409.00+6 TO 409+120 CORRODED IN MULTIPLE SPOTS (MARKED) (FILED CLOSED) CORROSION FOUND ON RBL 9 AT FS 409.00 +6 TO FSS 409 +120 IS OUT OF LIMITS. IAW CRJ 200 SRM 53-00-00. REMOVED AND REPLACED FLOORBEAM CAP IAW CRJ 200 SDR SWIA202162677None · corrodedFLOOR BEAMON LBL 9.0 FROM ROUGHLY FS 409.00 +120 TO 559+8 CORRODED IN MULTIPLE PLACES (MARKED) & HAS 3 LOOSE/WRONG FASTENERS (FILED CLOSED) CORROSION FOUND ON FLOORBEAM CAP FOUND TO BE OUT OF LIMITS IAW BOMBARDIER REO 601R-53-41-2962 REV.-A 2021-09-22 RSDR SWIA202162676None · corrodedFLOOR BEAM ON RBL 9.0 FROM FS 409.00 +120 TO FS 559+8 CORRODED IN MULTIPLE PLACES ( MARKED) (FILED CLOSED) CORROSION ON RBL 9 FLOORBEAM FROM FS 409.00+ 120 TO FS 559+8 WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM CAP. IAW BOMBARDIER REO 6SDR SWIA202162675None · corrodedSTRAP ON TOP OF LBL 9.0 FROM ABOUT FS 559.0+8 TO FS 570.0 CORRODED IN MULTIPLE PLACES (MARKED) (FILED CLOSED) REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-00-00 REMOVED AND REPLACED BEAM CAP FROM FS 559+8 TO FS 570 IAW CRJ200 SRM 51-42-0SDR SWIA202162674None · corrodedSTRAP ON TOP OF LBL 9.0 FROM ROUGHLY FS 409.00+6 TO 409.00+120 CORRODED IN MULTIPLE SPOTS (MARKED) (FILED CLOSED) CORROSION FOUND ON FLOOR BEAM CAP FOUND TO BE OUT OF LIMITS. IAW CRJ 200 SRM 53-00-00. REMOVED AND REPLACED FLOOR BEAM CAP AT FS 409+6 TO FS SDR SWIA202162685None · corrodedF/S 314 & F/S 343 LBL 36 WL 73.50 CORROSION ON 2 EACH FLOOR SUPPORT FITTINGS (PAX) DOOR AREA (FILED CLOSED) REMOVED AND REPLACED (2) FLOOR SUPPORT FITTINGS ON PAX DOOR SILL IAW CRJ200 SRM 51-24-00 SRM 51-40-00 SRM 51-25-00 SRM 51-23-00 AND SRM 51-4SDR SWIA202162673None · corrodedCORROSION ON FRAME AT FS 409+16 AT STR 27 (FILED CLOSED) CORROSION TO BE FOUND OUT OF LIMITS. REPAIRED FRAME AT FS 409+16 STR 25L TO STR 26R WITH FRAME SPLICE REPAIR IAW CRJ200 SRM 53-00-15 SRM 51-23-00 SRM 51-25-00 SRM 51-42-06 SRM 51-42-21 / CALIBRATESDR SWIA202162672None · corrodedCORROSION ON FRAME AT FS 349.00 AT STR 27 (FILED CLOSED) EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED NEW FRAME SECTION FROM STGR 23L TO STGR 23R FS 349 BACKDRILLED AND INSTALLED NEW FRAME SECTION IAW CRJ200 SRM 51-40-11, SRM 51-42SDR SWIA202162671None · corrodedCORROSION ON FRAME AT FS 333.00 ST STR 27 (FILED CLOSED) EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED NEW FRAME SECTION FROM STGR 18L TO STGR 23R FS 333 BACKDRILLED AND INSTALLED NEW FRAME SECTION IAW CRJ200 SRM 51-40-11, SRM 51-42-SDR SWIA202162670None · corrodedCORROSION ON FRAME AT FS 319.70 ST STR 27 (FILED CLOSED) EVALUATED CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-00-00 REMOVED AND DRILLED NEW FRAME AT FS 319.70 STR 23L TO 23R AND INSTALLED FRAME IAW CRJ200 SRM 51-42-06, SRM 51-42-21, SRM 51-25-SDR SWIA202162684None · corrodedR/H AILERON 5 EACH HINGE BOLT KEEPERS HAVE CORRODED HARDWARE (FILED CLOSED) REPLACED HARDWARE .INSTALLED NEW HARDWARE REF.CRJ 200 AMM 27-15-01 & CRJ 200 AMM 20-21-00 / CALIBRATED TOOL: TORQUE WRENCH AV 6522 CAL DUE AUG 22SDR SWIA202162683None · corrodedL/H AILERON ALL HINGE BOLT RETAINERS HAVE CORRODED HARDWARE (FILED CLOSED) REMOVED AND REPLACED CORRODED HARDWARE ON L/H AILERON WITH NEW HARDWARE IAW CRJ 200 AMM 27-15-01 / CALIBRATED TOOL: TORQUE WRENCH AV7327 CAL DUE DEC 21SDR SWIA202162680None · damagedALL PAX SEAT TRACKS REQUIRE REPLACEMENT (EXCEPT FOR SEAT TRACK AT STA 559.32 TO STA 559.80 RBL9) (FILED CLOSED) REPLACED ALL SEAT TRACK EXCEPT SEAT TRACK AT STA 559+32 TO STA 559+80 RBL9. REF. CRJ200 AMM 53-01-11-400-802.SDR VNAA202008119995Floor Support · corrodedFLOOR BEAM CAP CORRODED AT LBL 27 FS 617 TO 621. REMOVED LBL 27 FLOORBEAM FITTING AT FS 617 - 621 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. PN 601R35289-1. INSTALLED NEW SERVICEABLE LBL 27 FLOORBEAM FITTING IAW REO 601R-53-61-3778 REV B DATED 12/19/16.SDR VNAA202008119994Floor Support · crackedFLOOR BEAM CAP CORRODED AND CRACKED AT LBL 27 BETWEEN FS 574.00 TO FS 621.00. INSTALLED NEW SERVICEABLE FLOOR BEAM CAP IAW REO 601R-53-61-3778 REV B DATED 12/19/16.SDR VNAA202008119993Floorbeam · corrodedFLOOR BEAM CAP CORRODED AT RBL 9.00 BETWEEN FS 559+80 TO FS 559+96. FABRICATED, LOCATED, DRILLED AND INSTALLED, FABRICATED FLOORBEAM CAP IAW CRJ 200 SRM 51-24-36 AND 51-40-11.SDR VNAA202008119992Floorbeam · corrodedFLOOR BEAM CAP CORRODED AT RBL 27 BETWEEN FS 559+80 TO FS 559+96. LOCATED,DRILLED, AND INSTALLED FLOORBEAM CAP AT RBL27 ON FS 559+80-559+96 IAW CRJ 200 SRM 51-40-11 AND 51-42-21 AND S+SEA 72-2020-163 REV P1 DATED 03/06/20.SDR VNAA202008119991Bracket · crackedPAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET IS CRACKED. REMOVED DAMAGED PAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE. IAW CRJ200 SRM 51-40-11, 51-42-06, AND 51-42-13.SDR VNAA202001311101Pump · leakingHYD 2 LOW PRESS IN FLIGHT 0PSI. - AT FL2200, CREW RECEIVED A HYDRAULIC PUMP #2 LOW PRESSURE CAUTION MESSAGE FOLLOWED BY THE HYDRAULIC GAUGE SHOWING 0 PSI. CREW RAN QRH, DECLARED EMERGENCY AND LANDED RDU WITHOUT ISSUE. R&R #2 EDP IAW AMM. PERFORMED OPS CHECK ANSDR VNAA2019080171101Control Unit · failedON TAKEOFF CREW SELECTED FLAPS 20. ONCE AIRBORNE SELECTED FLAPS 8 AND RECEIVED A FLAPS FAIL CAUTION MSG. CREW CONTINUED CLIMB TO 7000. RAN QRH, DECLARED AN EMERGENCY AND LANDED NORMALLY. MX REMOVED AND REPLACED FECU. OPS CHECK GOOD.SDR VNAA2019050699901Skin · crackedCORROSION AND CRACK AROUND RT WING LOWER PLANK AROUND DRAIN HOLE AT WS 85.5 BETWEEN STRINGER14R-15R. CA ACCOMPLISHED REPAIR IAW REO 601R-57-21-3024.SDR VNAA2018101511101Flap System · malfunctionedDURING LANDING THE CREW DECIDED TO DO A GO AROUND DUE TO WINDS AND SELECTED THE FLAPS UP AND RECEIVED A FLAP FAIL AT 8 DEGREES. THE AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX C/W TO 27-050-004-09 REV Q,IAW TO INST. FLAPS SYS OPS CHECKS GOOD IASDR VNAA2018101111101Flap · malfunctionedON SHORT FINAL CREW RECEIVED A FLAPS FAIL CAUTION MSG. CREW THEN DECLARED AND EMERGENCY AND LANDED WITHOUT INCIDENT. ONCE AT THE GATE THEY WERE ABLE TO RESET THE SYSTEM, RUN THE FLAPS THROUGH 5 FULL CYCLES AND DEFER THE FLAP SYSTEM.SDR VNAA2018092941101Control Unit · failedDURING CLIMB THE CREW RECEIVED A FLAPS FAIL 20-8 FAIL MESSAGE. THE AIRCRAFT WAS AROUND 160 KNOTS. THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY AND LANDEDWITHOUT FURTHUR INCIDENT. THE AIRCRAFT FERRIED TO A MAINTENANCE BASE AND REPLACED THE FLAP ECTRONIC CONTSDR VNAA2018092111101Bpsu · malfunctionedAFTER DEPARTURE AT 17000 FEET THE CREW RECEIVED A FLAPS FAIL MESSAGE AT ZERO. THE CREW RETURNED TO FIELD AND DECLARED AN EMERGENCY AND LANDED ON THE LONGEST RUNWAY. MAINTENANCE REMOVED AND REPLACED LEFT HAND BRAKE POSITION SENSING UNIT AND WAS RETURNED TO REVESDR VNAA2018091711102Warning System · false activationON CLIMBOUT THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE AT FLIGHT LEVEL 190. THE FLAPS CURRENT POSITION WAS ZERO SETTING. ONCE ON THE GROUND THE CREW PERFORMED FIVE FULL EXTENSION/RETRACTION OF THE FLAPS WITH NO FAILURES. THE CAT II SYSTEM WAS DEFERRED.SDR VNAA2018090611101Ecu · failedTHE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE ON CLIMB OUT. THE CREW RAN THE QUICK REFERENCE HANDBOOK AND RETURNED TO FIELD. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY AND TAXIED TO THE GATE. MX REPLACED THE FECU. OPS CHECK GOOD.SDR VNAA2018073111103Controller · failedDURING CRUISE FLIGHT AT FLIGHT LEVEL 260, THE CREW RECEIVED A RIGHT HAND WINDSHIELD HEAT CAUTION MESSAGE. THE CREW CYCLED THE WINDHIELD TOGGLE SWITCH AND WHEN SELECTED BACK ON, THE FIRST OFFICER WINDSHIELD SHATTERED. THE CREW DECLARED AN EMERGECNY AND DIVERTEDSDR VNAA2018062599911Window · scratchedLEFT EMERGENCY EXIT WINDOW SEVERLY SCRATCHED AND HAS TWO POSSIBLE CRACKS. INSTALLED A NEW OUTER PLY & SEAL WINDOW ASSY IAW CMM 56-20-00.SDR VNAA2018062599910Bulkhead · crackedBS 621 PRESSURE BULKHEAD WEB WAS CRACKED. REPAIRED THE PRESSURE BULKHEAD IAW REO 601R-53-61-1240, REV D.SDR VNAA2018062599909Floor Support · crackedWHILE PERFORMING EA 45-2018-109 P1, STEP 6, AND NDTM PART 1, 51-20-06, FOUND MULTIPLE CRACK INDICATIONS APPROXIMATELY .15 INCH LONG FROM CUTOUT HOLE. REPAIRED THE LT PRESSURE FLOOR SILL IAW EA 45-2018-109.SDR VNAA2018062599908Strap · corrodedFLOORBEAM STRAP AT BS 559, LBL 38 WAS CORRODED. LOCATED, AND DRILLED A NEW FLOORBEAM STRAP IAW SRM 51-40-11.SDR VNAA2018062599907Seat Track · gougedLEFT SEAT TRACK, BS 559+56, LBL 9, WAS HEAVILY GOUGED. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-1-400-802.SDR VNAA2018062599905Fitting · crackedHORIZONTAL STABILIZER ANTI-ROTATION FITTING WAS CRACKED. INSTALLED A NEW ANTI-ROTATION FITTING IAW SB 601R-55-007.SDR VNAA2018062599005Angle · corrodedSERVICE DOOR FLOORBEAM ANGLE BS 349 WAS CORRODED. LOCATED, DRILLED, AND INSTALLED A NEW FLOORBEAM ANGLE IAW SRM 51-42-06, 51-42-21, AND 51-40-11.SDR VNAA2018062599904Mount · corrodedFLOOR SUPPORT STRUCTURE BS 310 WAS CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11, AND 51-42-13.SDR VNAA2018062599903Angle · crackedLH WING, WING TO FUSE ATTACHMENT ANGLE IS CRACKED AT FS 449.85. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE LH WING TO FUSELAGE ANGLE IAW SRM 51-42-06, 51-42-15, AND 51-45-00.SDR VNAA2018062599902Angle · crackedRIGHT WING TO FUSE ATTACH ANGLE WAS CRACKED AT BS 439. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, 51-42-15, AND 51-45-00.SDR VNAA2018062599901Intercostal · corrodedPASSENGER DOOR INTERCOSTAL INSIDE DOOR BELOW THE LOCK, LATCH BOX WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.SDR VNAA2017092311101Unknown · odorBURNING SMELL COMING FROM LT PACK ON TAXI OUT. A/C RETURNED TO GATE FOR MAINTENANCE INSPECTION. CLT MX RAN PACK FOR 30 MINUTES. INSPECTED PACK AND FOUND NO DEFECTS.SDR VNAA2017071000006Release Pin · brokenPASSENGER DOOR HANDLE RELEASE PIN BROKEN. REMOVED AND REPLACED RELEASE PIN.SDR VNAA2016080200002Door Seal · damagedSERVICE DOOR SQUEALED AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FERRIED ACFT TO NEAREST MAINTENANCE FACILITY. MAINTENANCE INSPECTED AND REPAIRED THE SERVICE DOOR SEAL. OPS CHECK GOOD. CLEARED FERRY AND CW O/SDR VNAA2016060900014Cargo Track · corrodedBS 559+91 TO FS 559+96 , 559+110 TO 569, 583, 600 AND 612 TO 617 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT LBL 9. MAINTENANCE. R & R CARGO COMPARTMENT RAIL FITTINGS AT LBL 9 IAW AMM 20-21-00-910-801.SDR VNAA2016060922214Fitting · corrodedBS 559+91 TO 559+96 , 559+110 TO 569, 583, 600 AND 612 TO 617 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT LBL 9. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTINGS AT LBL 9 IAW AMM 20-21-00-910-801.SDR VNAA2016060900013Cargo Track · corrodedBS 559+80 TO 559+96 , 559+104 , 559+110 AND 567 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT LBL 27. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTINGS AT LBL 27 IAW AMM 20-21-00-910-801.SDR VNAA2016060900012Cargo Track · corrodedBS 559+91 TO 559+96 AND BS 559+110 TO 569 CARGO COMPARTMENT RAIL FITTINGS ARE CORRODED AT RBL 9. MAINTENANCE R & R CARGO COMPARTMENT RAIL FITTINGS AT RBL 9 IAW AMM 20-21-00-910-801.
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