N186PQ

Service difficulty reports · 235

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 = 'N186PQ' 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.

SDR ASOA2014071410878Angle · corrodedSERVICE DOOR SILL ANGLE CORRODED IN SEVERAL AREAS. ON FURTHER EVALUATION FOUND THE SERVICE DOOR MOUNTING ANGLE HAD INTERGRANULAR CORROSION AND REMOVED MOUNTING ANGLE AND INSTALLED NEW ANGLE ASSY IAW SRM 53-21-23-001-002-A01 AND SRM 51-42-06-001-001-A01 AND SRJun 23, 2014 · N186PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014071410877Floorbeam · corrodedCRAWLWAY FWD FLOORBEAM ANGLE AT FS 280 CORRODED. R & R FLOORBEAM ANGLE IAW SRM 51-42-02-001-001-A01.Jun 23, 2014 · N186PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2014071410876Floor Support · corrodedRT CABIN FLOOR SUPPORT CORRODED FROM BS 280-349. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-21-00-001-001-A01 & 53-00-00-101-001. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW FLOOR SUPPORT IAW DWG SH6Jun 23, 2014 · N186PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014071410875Skin · chafedRT ENGINE LOWER COWLING CHAFED, INTERIOR, SKIN. COMPLIED WITH REO 670-54-23-959. MAJOR REPAIR.Jun 21, 2014 · N186PQ · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR ASOA2014071410874Floor Panel · crackedRT FWD EQUIPMENT BAY FLOOR CRACKED UNDER ADG STOW PUMP. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509, REV B.Jun 21, 2014 · N186PQ · Cndair CL6002D24 · Fuselage Floor PanelSDR ASOA2013102109239Light · inoperativeRT OVERWING EMERGENCY LIGHT INOPERATIVE (AFT). R & R RT AFT EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-15. OPS CHECKED GOOD.Oct 16, 2013 · N186PQ · Cndair CL6002D24 · Emergency LightingSDR ASOA2013062508504Skin · burnedBURNED SKIN FS 330 AND 349 AT S23L AND AT BS 453 AND 469 S21L. REPAIRED IAW REO 690-53-21-480 IAW NDTM PART 1, 51-20-006.Jun 18, 2013 · N186PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2013062508503Floor Support · corrodedCORROSION ON FLOOR SUPPORT RBL 45 AT FS 349 - 355. REPAIRED IAW SRM 51-21-06-001-001 & REO 690-53-21-477.Jun 14, 2013 · N186PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2013062508502Channel · crackedC CHANNEL AT SEAM BETWEEN 195DL AND 196DR IS CRACKED INTO. REMOVED C CHANNEL IAW SRM 51-42-10-001-001-A01. INSTALLED REPLACEMENT C CHANNEL IAW DWG CC690 -39302 AND 51-42-10-001-001-A01. REPAIR CLASSIFIED AS MINOR.Jun 13, 2013 · N186PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2013050903483Fitting · out of rigFORWARD CARGO DOOR IS HARD TO OPEN IAW AMM 52-35-00. OPS CHECKED GOOD RIGGED AFT UPPER ROLLER FITTING.May 5, 2013 · N186PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR ASOA2012122102702Sensor · inoperativeRECEIVED CAUTION "SLATS FAIL" WHEN SELECTIONG FLAPS 8 COMPLIED WITH QRH. EMERGENCY DECLARED. R & R RT SLAT BRAKE POSITION SENSOR UNIT IAW AMM 27-81-03. OPS CHECKED GOOD.Dec 20, 2012 · N186PQ · Cndair CL6002D24 · Leading Edge Slat Position Indicating SystemSDR REXA2012112001694Life Vest · unserviceableTWENTY THREE (23) PAX LIFE VEST UNSERVICEABLE. REMOVED AND REPLACED 23 PASSENGER LIFE VEST IAW AMM 25-61-03. SEE ATTACHED SHEET FOR PARTS REMOVAL / INSTALLATION PART NUMBER & SERIAL NUMBER LIST.Nov 20, 2012 · N186PQ · Cndair CL6002D24 · Life JacketSDR REXA2012111201673Life Vest · unserviceableCAPTAINS & FORWARD FLIGHT ATTENDANTS LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED CAPTAINS & FORWARD FLIGHT ATTENDANTS LIFE VEST IAW AMM 25-61-03. OPS CHECK GOOD.Nov 12, 2012 · N186PQ · Cndair CL6002D24 · Life JacketSDR REXA2012061800859Floorbeam · crackedRBL12 FLOORBEAM FS 272 CRACKED AT BACK-UP FITTING ATTACHMENT BOSS. REPAIRED IAW REO 690-53-11-383.May 31, 2012 · N186PQ · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012061800858Floorbeam · crackedLBL12 FLOORBEAM FS 272 CRACKED AT BACK-UP FITTING ATTACHMENT BOSS. REPAIRED IAW REO 690-53-11-382.May 31, 2012 · N186PQ · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA2012061300853Floorbeam · corrodedFS 280 CROSSBEAM SPLICE CORRODED. REMOVED AND REPLACED IAW SRM 53-00-00.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2012061300852Beam · damagedRIGHT FS 280 BEAM CORRODED. REMOVED AND REPLACED IAW SRM 53-00-00.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2012061300851Beam · damagedLEFT FS 280 BEAM CORRODED. REMOVED AND REPLACED IAW SRM 53-00-00.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2012061000696Stringer · corrodedMAIN AVIONICS BAY STRINGER 26L AT FS 280 TO FS 333 CORRODED. REMOVED AND REPLACED IAW SRM 51-40-11 AND 51-42-06.May 31, 2012 · N186PQ · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR REXA2012060900695Stringer · corrodedSTRINGER 26R AT FS 333-FS 364 CORRODED. REMOVED AND REPLACED IAW SRM 53-21-03.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2012060800686Skin · damagedRIGHT STABILIZER SKIN HAS LIGHTNING STRIKE DAMAGE. REPAIRED IAW REO 690-55-11-045.May 31, 2012 · N186PQ · Cndair CL6002D24 · Horizontal Stabilizer, Plate/SkinSDR REXA2012060100685Skin · damagedMAINTENANCE FOUND LIGHTNING DAMAGE TO THE FUSELAGE SKIN AT FS 469 BETWEEN S-6R. REPAIRED IAW EA CRJ953-00598C AND ASSOCIATED 8110-3.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2012060100684Structure · damagedMAINTENANCE FOUND LIGHTNING DAMAGE TO A FASTENER HOLE AT FS 543 S5R. THE DAMAGE WAS REMOVED BY BLENDING RESULTING IN A 0.12 BY 0.007 BY 0.004 DEEP BLENDOUT. REPAIRED IAW EA CRJ953-00563D AND ASSOCIATED 8110-3.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2012060100683Skin · damagedRIGHT ELEVATOR HAS LIGHTNING STRIKE DAMAGE. REPAIRED IAW REO 690-55-21-050.May 31, 2012 · N186PQ · Cndair CL6002D24 · Elevator, Plate/SkinSDR REXA2012060100682Skin · damagedMAINTENANCE FOUND DAMAGE TO THE SKIN AT BETWEEN S-24R AND S-25R. THE DAMAGE WAS REMOVED RESULTING IN A 1.1 BY 0.9 BY 0.022 DEEP BLEND OUT. REPAIRED IAW PINNACLE EA CRJ953-00597 REV B AND ASSOCIATED 8110-3 DATED MAY 25, 2012.May 31, 2012 · N186PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2012042900588Unknown · malfunctionedGLD - UNARMED CAUTION MSG AT 150 FT GLD FAILED TO DEPLOY ON LANDING. C/W CRJ900 FIM 27-64-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE PER CRJ900 AMM 27-64-00.Apr 29, 2012 · N186PQ · Cndair CL6002D24 · Drag Control SystemSDR REXA201200178Actuator · faultyAFTER T/O OUT OF HOU, RETRACTED LANDING GEAR, GOT 3 UP, INDICATIONS, THEN NOSE GEAR DROPPED SLIGHTLY AND GOT AMBER NOSE GEAR INDICATION. NOSE GEAR RETRACTED AGAIN WITH UP INDICATION. THAT REPEATED ONCE MORE, AND THEN WE GOT A PROX SYS FAULT 1 STATUS MSG. REFeb 4, 2012 · N186PQ · Cndair CL6002D24 · Landing Gear ActuatorSDR REXA201100846Battery · dischargedFWD F/A FLASHLIGHT INOP. DEFERRED PER MEL 25-61-04. R&R FA FLAHSLIGHT BATTERY IAW AMM 25-60-00. OPS CHK GOOD. THIS DEFER CLEARS. PART EFFECTIVITY VERIFIED.Nov 17, 2011 · N186PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA201100697Cartridge · inoperativeCROSSFLOW PUMP CAUTION MESSAGE ON TAXI-IN. RESET CIRCUT BREAKER N8 AND PERFORMED OPS TEST OF CROSSFLOW PUMP IAW AMM28-40-00. OK FOR SERVICE. CROSSFLOW PUMP CAUTION MESSAGE RETURNED. FOUND CIRCUIT BREAKER TRIPPED AGAIN. REMOVED & REPLACED CROSSFLOW PUMP CAOct 10, 2011 · N186PQ · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR REXA201100565Spoileron · malfunctionedRT I/B MULTIFUNCTION SPOILER DEPLOYED INFLIGHT ON SHORT FINAL WITH I/B FLT SPLRS AND I/B SPOILERONS CAUTION MESSAGES REMOVED AND REPLACED RT I/B MULTIFUNCTION SPOILERON IAW CRJ900 AMM 27-62-01 OPS AND LEAK CHECK GOOD AND THIS TIME MSG CLEARED NO FURTHER DEFECTSep 14, 2011 · N186PQ · Cndair CL6002D24 · Drag Control SystemSDR REXA201100433Unknown · malfunctionedA/C DIVERTED FROM ATL-CZM TO FLL DUE TO LOSING BOTH FMS IN FLIGHT. PERFORMED OPS CHECK OF FMS IAW CRJ900 AMM 34-61-01. CHECK GOOD. DM CLEARED. PLACARD REMOVED. OK FOR SERVICE.Jun 27, 2011 · N186PQ · Cndair CL6002D24 · Flight Management Computing Hardware SystemSDR REXA201100348Blades · dirtyAIR RETURN RT ENG VIBE 2.0 IN FLT. MTX WILL PERFORM ENG TANG BLADE LUBE BLADES HAVE BEEN REMOVED CLEANED AND LUBED WILL START THE INSTALL PROCESS NOW IAW AMM 72-20-00. Jun 6, 2011 · N186PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR REXA201000299Warning Light · false activationANTI-ICE WARN THEN L/R CAUTIONS OPS CHECK IAW AMM 30-10-00 AND OP CHECK AILC IAW AMM 30-12-12. NO DEFECTS NOTED.Dec 1, 2010 · N186PQ · Cndair CL6002D24 · Pneumatic Distribution SystemSDR REXA201000066Pin · installedGEAR DISAGREE, FOUND LANDING GEAR LOCK PINS INSTALLED. REMOVED LANDING GEAR PINS IAW AMM 10-11-00.May 3, 2010 · N186PQ · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR REXA201000025Warning System · malfunctionedSLATS FAIL CAUTION MESSAGE. CLEARED INHIBITS FROM SFECU AND PERFORMED OPS CHECK OF SLAT/FLAP SYSTEM IAW AMM 27-51-05. OPS CHECK GOOD, OK FOR SERVICE. MX PERFORMED AT OUTSTATION: BUF.Feb 17, 2010 · N186PQ · Cndair CL6002D24 · Leading Edge Slat Position Indicating System
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