N8506C
Service difficulty reports · 34
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 = 'N8506C' 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 = 'N8506C' 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 REXA2014102801081Door Seal · dirtyGEAR DISAGREE WARNING AFTER TAKEOFF. CLEANED DEBRIS FROM DOOR SEAL & PERFORMED VISUAL INSPECTION OF SEAL IAW AMM 52-11-10. NO DEFECTS NOTED AT THIS TIME.SDR REXA2014070600673Pbe · unserviceableFLIGHT DECK, GALLEY & CABIN PBE'S HAVE LOST THEIR SEAL SOFT. REPLACED FLIGHT DECK, GALLEY & CABIN PBE'S IAW AMM 25-61-10.SDR REXA2014030400253Cover · unsecureLEFT EMERGENCY LIFE LINE COVER WILL NOT STAY ON. SECURED EMERGENCY ROPE COVER IAW AMM 25-63-04.SDR REXA2014030100246Shaft · lack of lubeFLAP FAIL AFTER LANDING, STUCK AT 45. CYCLED FLAPS 5 TIMES, NO DEFECTS NOTED. REPLACED NR 1 LT FLAP SHAFT & LUBED LT & RT FLEX SHAFTS. ALL CHECKED GOOD.SDR REXA2014021000014Skin · damagedA GOUGE & DENT IN THE SKIN JUST AFT OF FS 394 & STRINGER 16R. THE GOUGE DAMAGE WAS REMOVED BY BLENDING WITH A MINIMUM REMAINING THICKNESS OF 0.013”. REPAIRED IAW EA CRJ253-02295.SDR REXA2013120502287Selector Valve · malfunctionedGEAR DISAGREE, DOWN, BOTH MAINS REMAINED UP, NOSE GEAR WAS DOWN. QRH REQUIRED GEAR SELECT UP WAIT THEN DOWN THAT DID NOT WORK HAD TO USE MANUAL EXTENSION IAW QRH. COMPLIED WITH PA 05-018 REV K SCENARIO, R & R MLG SELECTOR VLV IAW AMM 32-32-10. OPC & LEAK CHESDR REXA2013120302307Floorbeam · damagedMAINTENANCE FOUND AN ELONGATED HOLE IN THE CTR FLOOR BEAM AT FS 589.00 BETWEEN LBL 9 & RBL 9. THE HOLE MEASURES .355 INCHES X .270 INCHES. REPAIRED IAW EA CRJ253-02117 AS APPROVED BY CORRESPONDING DER SIGNED 8110-3.SDR REXA2013112902305Attach Angle · crackedPASSENGER DOOR LINTEL ATTACH ANGLES AT FS 280 CRACKED. REPAIRED IAW SRM 51-40-11 51-42-00 51-42-21.SDR REXA2013112502304Skin · crackedLEFT WING TE LOWER PLANK JUST AFT OF REAR SPAR AT APPROXIMATELY WS 147 IS CRACKED. REPAIRED IAW REO 601R-57-21-030, 601R-57-21-131 & 601R-57-21-470.SDR REXA2013112402303Bulkhead · chafedAFT SIDE AFT PRESS BULKHEAD HAS BEEN CHAFED BY 10TH STAGE ISOLATION VLV. REPAIRED IAW REO 601R-52-61-1523.SDR REXA2013112402302Skin · corrodedRIGHT WING FUEL ACCESS PANEL 640BB CORRODED AT NUMEROUS LOCATIONS IN THE NON-CRITICAL REGION 0.003 INCHES TO 0.005 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.SDR REXA2013112402301Skin · corrodedLEFT WING FUEL ACCESS PANEL 540BB CORRODED AT NUMEROUS LOCATIONS IN THE NON-CRITICAL REGION 0.003 INCHES TO 0.005 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.SDR REXA2013112402300Skin · corrodedLEFT WING FUEL PANEL ACCESS 510AB HAS CORROSION AROUND PERIMETER AT 2 LOCATIONS IN NON-CRITICAL REGIONS 0.008 INCHES & 0.010 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.SDR REXA2013111801175Floor Support · corrodedLEFT UPPER PRESSURE FLOOR SUPPORT BS 500-508, LBL 44 HAS CORROSION AROUND FASTENER HEADS 8.4" X1.6" X 0.003" DEEP. REPAIRED IAW REO 601R-53-41-666.SDR REXA2013012100180Actuator · malfunctionedON FLIGHT 3814 (DLH TO MSP) RECEIVED FLAPS FAIL AT 20 AFTER TAKEOFF. CAPTAIN STATED THAT AFTER TAKEOFF WHEN HE WENT TO RETRACT THE FLAPS THEY DID NOT MOVE. AIRTURN BACK WAS PERFORMED BACK TO DLH AND THE AIRCRAFT LANDED SAFELY. PERFORMED TROUBLESHOOTING PER SDR REXA2013012100164Bolt · dirtyMAIN CABIN DOOR BINDS AND DIFFICULT TO OPEN. CLEANED AND LUBED PASSENGER DOOR BOLTS. OPS CHECK GOOD IAW AMM 52-11-00. OK FOR SERVICE.SDR REXA2012072601187Coalescer Bag · failedCONDENSATION FROM AIR CONDITIONING CREATES A THICK FOG IN FLIGHT (FLIGHT 3906). THE FOG IS BAD ENOUGH TO OBSCURE THE FLIGHT INSTRUMENTS. FOG COMPLETELY OBSCURES THE CABIN SO THE FLIGHT ATTENDANT CANNOT SEE THE PASSENGERS. REMOVED AND REPLACED LEFT AND RIGHTSDR REXA2012071801062Bulkhead Web · chafedMAINTENANCE FOUND THE FS 280 BULKHEAD WEB TO BE CHAFED 0.725 INCH BY 0.092 INCH BY 0.022 INCH DEEP AT LBL 13 AND WL 83.5. REPAIRED IAW EA CRJ253-00709 AND ASSOCIATED 8110-3.SDR REXA2012062301007Power Lever · bindingLEFT ENGINE THRUST LEVER BUCKLES. DOES NOT GO FULL/MAX POWER AT ALTITUDE. VERY UNEVEN THRUST ADVANCE AND RESEND BETWEEN LEVERS. COULD NOT DUPLICATE PROBLEM AT THIS TIME. OK FOR SERVICE, CREW NOTIFIED AND OK WITH IT.SDR REXA2012030400331Trim Switch · dirtyAILERON TRIM DIFFICULT TO OPERATE TO THE RIGHT. CLEANED AILERON TRIM SWITCH IAW AMM 27-12-00. OPS CHECKS GOOD.SDR REXA201100925Beam · crackedFS 280.00 TRASVERSE BEAM CRACKED IN WEB OUTBOARD OF LBL 9 AFT UPPER J ANGLE CRACKED OUTBOARD OF LBL 9 AND OUTBOARD RBL 9 CLIPS CRACKED ON INBOARD AND OUTBOARD SIDES OF LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORSDR REXA201100924Post · damagedINDICATION NOTED AT FS 409+128 VERTICAL POST AT RBL 18 WL 69.0 IN THE AFT RADIUS OF THE INBD CHANNEL APPROX .10 LONG AND 53 FULL SCREEN HEIGHT FAILED NDT. REPAIRED IAW SRM 51-42-06,51-40-11.SDR REXA201100202Warning System · activatedCREW REPORTED GEAR DISAGREE ON APPROACH, DECLARE EMERGENCY. STILL IN WORK FOR P/A COMPLIANCE.SDR REXA201100182Landing Gear · slowGEAR DISAGREE ON LANDING. NOSE LANDING GEAR DIDN'T EXTEND ON 1ST ATTEMPT. AFTER 3 MINUTES GEAR EXTENDED. CREW DECLARED AN EMERGENCY. CW PA 05-018A. NO DEFECTS NOTED.SDR REXA201000284Pan · damagedTHE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE BEING PULLED FROM THE INSTALLED POSITION IN THE RECESSED PAN AREA. TEMPORARY REPAIR IAW STS EA 1-2010-207. REPEAT INSPECT DAILY, FLY ON FOR 10 DAYS WISDR REXA201000236Bulkhead Web · crackedFS 559.00 BULKHEAD WEB CRACK DETECTED DURING INSPECTION AND REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B DEVIATION C.SDR REXA201000182Bpsu · malfunctionedFLAP FAILURE AT 13 DEGREES. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I), AMOC DATED MARCH 27, 2009, TR 27-012 PER AMOC DATED DEC 18, 2009 AND PA AD27-052G MEGGED RT WING HARNESS AND RT BPSU. REMOVED AND REPLACSDR REXA201000134Idg · underservicedTR GEN CAUTION AFTER T/O IDG 2 CAUTION ALSO INTERMITTENT. PERFORMED AIR RETURN. ELECTRICAL SYSTEM OPERATED NORMAL AT LOW THRUST SETTINGS. SERVICED RT ENG IDG IAW AMM 12-13-24. OP CHECK IAW AMM 24-11-01 GOOD. OK FOR SERVICE.SDR REXA200900114Throttle Cable · brokenFLIGHT 4107 MOT/MSP ATC REQUESTED A DESCENT TO BEGIN APPROACH INTO MSP, WHEN THROTTLES RETARDED THE LEFT WAS FOUND TO BE INOPERATIVE, NO ENGINE CHANGE WITH THROTTLE MOVEMENT. QRH FOLLOWED FOR "STUCK THROTTLE" AND ENGINE SHUTDOWN. EMERGENCY DECLARED AND LANDESDR REX2008F00054Wire Harness · faultyON APPROACH, RECEIVED GEAR OVERHEAT WARNING WHEN GEAR EXTENDED, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT AND RT MLG BAY DETECTION LOOP HARNESS IAW AMM. (K)SDR REX2008F00053Wire Harness · faultyON APPROACH, RECEIVED GEAR OVERHEAT WARNING WHEN GEAR EXTENDED. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT AND RT MLG BAY DETECTION LOOP HARNESS IAW AMM. (K)SDR REX2008F00046Bpsu · malfunctionedON APPROACH WHEN SELECTING FLAPS 8 RECEIVED FLAP FAIL WHEN FLAPS REACHED 8 QRH FOLLOWED EMERGENCY DECLARED WITH UNEVENTFUL LANDING. TROUBLESHOT FLAP SYSTEM PER BOMBARDIER FAULT ISOLATION MANUAL (FIM) R&R THE LT BPSU (BRAKE POSITION SENSING UNIT) IAW BOMBARDIESDR REX2005F00010Fcu · failed(REF NR: 05-097) FLAP FAILURE AT 30, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K)SDR REX02020O-Ring · cutENROUTE, IN CRUISE CONFIGURATION AT FL290, AT A POSITION 80 MILES NORTH, THE RT ENG OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 28 AND 42 PSI, FOLLOWED BY INTERMITTENT ILLUMINATION OF LOW OIL PRESSURE WARNING. FLIGHT CREW DECLARED EMERGENCY AND SHUT DOWN THE ENGI
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