N306PQ

Service difficulty reports · 52

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 = 'N306PQ' 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 REXA2024102901127Floorbeam · crackedR/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED RIGHT COCKPIT FLOOR BEAM AT RBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08Apr 11, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2024102901126Floorbeam · crackedL/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED LEFT COCKPIT FLOOR BEAM AT LBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08Apr 11, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2024102901125Drag Angle · deformedAFTER REMOVAL OF PAX DOOR DRAG ANGLE FOUND HOLES ON WEB COMMON TO BE ENLARGE AND FOUND 1EA DOUBLE DRILL HOLE. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16330 REV-A DATED 4/5/2024.Mar 31, 2024 · N306PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024102801069Lug · deformed"FOUND BOTH LUGS LABELED ""C"" & ""F"" ON THE R/H AILERON ARE PREVIOUSLY OVERSIZED. FABRICATION OF O/S BUSHINGS (QTY. 2) IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV-- DATE 2017-07-25. "Mar 31, 2024 · N306PQ · Cndair CL6002D24 · AileronsSDR REXA2024061400436Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. INSTALLED PAX DOOR AFT DRAG ANGLE WITH PN 601R311772-5 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01 AND 51-42-15-001-001-A01.Mar 31, 2024 · N306PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024102801068Attach Fitting · corrodedCORROSION FOUND ON GALLEY ATTACHMENT FITTING BETWEEN FS 280-295 AT RBL 27. GALLEY MOUNTING BRACKET AT RBL 27 F.S. 280 - F.S. 295 IS IDENTIFIED AS P/N SH670-32149-3 AND HAS CORROSION PRESENT BOTH AROUND AND INSIDE OF BOLT HOLE AND IS FOUND TO BE OUT OFMar 28, 2024 · N306PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2024040900346Fitting · corrodedCORROSION FOUND ON GALLEY ATTACHMENT FITTING BETWEEN FS 280-295 AT RBL 18. GALLEY MOUNTING BRACKET AT RBL 18 F.S. 280 - F.S. 295 IS IDENTIFIED AS P/N SH670-32149-3 AND HAS CORROSION PRESENT BOTH AROUND AND INSIDE OF BOLT HOLE AND IS FOUND TO BE OUT OF LMar 28, 2024 · N306PQ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2024040900345Crossbeam · corrodedR/H FS280 CROSSBEAM CORRODED BETWEEN BL0 AND RBL 11. REPAIRED R/H FS280 CROSSBEAM CORRODED BETWEEN BL0 AND RBL 11 IN ACCORDANCE WITH MHIRJ REO 690-53-11-1717 DATE 2024-03-29 REV (--). SEE SHEET 2 FOR DTI REQUIREMENTSMar 28, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024102901122Floorbeam · corrodedFS 280 FWD J-ANGLE IS CORRODED INSTALLED J-ANGLE PN: CC670-34095-1 AT FS 280 BETWEEN RBL 11 TO LBL 11 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Mar 26, 2024 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2024102801066Lug · deformed"FOUND BOTH LUGS LABELED ""C"" & ""F"" ON THE L/H AILERON ARE PREVIOUSLY OVERSIZED. FABRICATION OF O/S BUSHINGS (QTY. 2) IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV-- DATE 2017-07-25. "Mar 26, 2024 · N306PQ · Cndair CL6002D24 · AileronsSDR REXA2024040900343Lug · crackedRH FWD EMERGENCY EXIT DOOR FORMER CRACKED AT UPPER ALIGNMENT LUG REPAIRED BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16266 REV IR DATED 4 APR 2024Mar 25, 2024 · N306PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2024040900342Lug · crackedL/H FWD EMERGENCY EXIT DOOR FORMER CRACKED AT UPPER ALIGNMENT LUG. REPAIRED LH FWD EMERGENCY EXIT DOOR UPPER ALIGNMENT LUG BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16265 REV IR DATED 4 APR 2024Mar 25, 2024 · N306PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2024040900340Bracket · crackedL/H AFT EMERGENCY EXIT DOOR UPPER FWD DOOR ALIGNMENT BRACKET IS CRACKED AT BASE OF BRACKET, REPAIRED LH AFT EMERGENCY EXIT DOOR UPPER FWD DOOR ALIGNMENT BRACKET BY COMPLYING WITH ENDEAVOR AIR EA CRJ952-16264 REV IR DATED 4 APR 2024Mar 25, 2024 · N306PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2024011800089Engine · fluctuatesWHILE CLIMBING OUT OF ORF THROUGH 13,000' PILOT HEARD A LOUD NOISE. LH ENG N1 WAS FLUCTUATING BETWEEN 30%-60% AND RUNNING ROUGH. FOLLOWED SEVERE ENGINE DAMAGE CHECKLIST AND SHUT DOWN LH ENG. AIRCRAFT CURRENTLY AOS WITH ENGINE CHANGE.Jan 14, 2024 · N306PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2022020100209Pseu · noneLEVELED OFF AT FL250 AT 290 KTS. HEARD A NOISE IN THE NOSE GEAR BAY ALONG WITH A SLIGHT SHUDDER, FOLLOWED BY A GEAR DISAGREE WARNING. NOISE AND SHUDDER REOCCURRED AS WARNING EXTINGUISHED. INSUFFICIENT TIME BEFORE WARNING EXTINGUISHED TO PERFORM QRH ITEMS. REMOJan 29, 2023 · N306PQ · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR REXA2020122300847Hinge · damagedRUDDER CENTER HINGE BEARINGS 2 EA HAVE EXCESSIVE PLAY. FOUND BOTH CENTER HINGE FITTINGS TO HAVE BORE DAMAGE. REMOVED, DRILLED UP, & INSTALLED 2 EA HINGE FITTINGS P/N: AV67021081-015 & AV67021081- 013, IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-ADec 11, 2020 · N306PQ · Cndair CL6002D24 · Rudder StructureSDR REXA2020122300844Hinge · damagedRUDDER CENTER HINGE BEARINGS 2 EA HAVE EXCESSIVE PLAY. FOUND BOTH CENTER HINGE FITTINGS TO HAVE BORE DAMAGE. REMOVED, DRILLED UP, & INSTALLED 2 EA HINGE FITTINGS P/N: AV67021081-015 & AV67021081-013, IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A0Dec 11, 2020 · N306PQ · Cndair CL6002D24 · Rudder StructureSDR REXA2020122300843Channel · gougedVERTICAL STAB LEADING EDGE, PUNCTURE ON CHANNEL 1.5 INCH, MARKED WITH ORANGE TAPE. FABRICATED CHANNEL, IAW CRJ 900 SRM 51-24-21-001-001-A01 REV 38 DATED 72-25-20 AND SRM 51-24-36-001-001-A01 AND 51-40-11-001-001-A01 AND INSTALLED PER SRM 51-42-06-001-001-A01.Dec 11, 2020 · N306PQ · Cndair CL6002D24 · Vertical StabilizerSDR REXA2020122300850Angle · corrodedFS 280 FWD J-ANGLE IS CORRODED. MAINTENANCE PERFORMED CORRECTIVE ACTION NR 1, IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.Dec 10, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020122300841Door Sill · corrodedAFT BAGGAGE BAY DOOR CUTOUT LOWER THRESHOLD CORROSION INDICATIONS FS 1020 TO FS 1045, FOUR PLACES AS MARKED. REMOVED & REPLACED AFT CARGO DOOR SILL P/N MM670-35655-003, IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-21-001-001-A01, 51-40-11Dec 7, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020122300846Door Frame · corrodedFS 280.00 BULKHEAD, LT DOOR FRAME SKIN IS CORRODED AT FLOOR LEVEL. REPAIRED FS 280.00 BULKHEAD LT DOOR FRAME SKIN, IAW REO 670-53-11-745 REV-A DATED 2016/10/28.Dec 6, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2020122300849Bracket · corrodedFWD CARGO BAY BRACKET IS CORRODED BETWEEN FS 565 TO FS 580 AT STGR 27. LOCATED AND INSTALLED BRACKET PN SH670-33389-2 AT FS 565-580 STRINGER 27, IAW CRJ 900 SRM 51-42-21-001-001-A01 AND IAW CRJ 900 SRM 51-42-22- 001-001-A01.Dec 5, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020122300848Floor Support · corrodedPAX DOOR SURROUND STRUCTURE HAS CORROSION ON MID FLOOR SUPPORT ANGLE. REMOVED AND REPLACED ANGLE, IAW CRJ 900 SRM 51-42-06-001-A01.Dec 4, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020122300845Angle · corrodedPAX DOOR SURROUND STRUCTURE HAS CORROSION ON SILL ANGLE. REMOVED AND REPLACED PAX DOOR SILL ANGLE, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Dec 4, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020122300842Angle · corrodedCORROSION FOUND ACROSS SERVICE DOOR LOWER SILL. REMOVED & REPLACED SERVICE DOOR LOWER SILL P/N: SH670-31996-3, IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.Dec 4, 2020 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019101021395Lens · crackedPAX DOOR EXTERNAL EMERGENCY LIGHT LENS IS CRACKED. REMOVED AND REPLACED PAX DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-15.Oct 2, 2019 · N306PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2019060740813Battery Pack · inoperativeDURING PRE FLIGHT INSPECTION EMERGENCY EXIT LIGHTING ON THE LOWER SIDE WALL AT ROW 13 FOUND TO BE INOP ON BOTH SIDES. REPLACED BATTERY PACK (EMERGENCYLIGHTS) AT PS 38 IAW CRJ 900 AMM 33-51-17 OPS TEST GOOD THIS CLEARS MEL MM02 UPDATED PLACARD REMOVED MOC NOTIJun 4, 2019 · N306PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2018082970725Oxygen Mask · no testFIRST OFFICER`S OXYGEN MASK WILL NOT SHUT OFF DURING TEST. R & R THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED NORMAL.Aug 27, 2018 · N306PQ · Cndair CL6002D24 · Crew Oxygen SystemSDR REXA2018082180708Flashlight · inoperativeFA FLASHLIGHT NOT CHARGING, NO CHARGE LIGHT SHOWN. REPLACED THE FLASHLIGH BATTERY IAW AMMAug 18, 2018 · N306PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017092901044Oxygen Mask · unwanted deployOXYGEN MASK ON FA JUMPSEAT DEPLOYED AFTER LANDING. STOWED THE FLT ATTENDANT OXYGEN MASK IAW AMM 35-11-12. OK FOR SERVICESep 29, 2017 · N306PQ · Cndair CL6002D24 · Passenger Oxygen SystemSDR REXA2017092001017Seal · brokenRED SEAL ON PBE IN COCKPIT BROKEN. INSTALLED THE SEAL IAW AMM 35-31-06.Sep 20, 2017 · N306PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017081200883Unknown · odorODOR OF AN OVERHEATING MOTOR WITH RECIRCULATION FAN ON, GOES AWAY WITH FAN OFF. PULLED AND COLARD CIRCUIT BREAKER 1 A5 , 2 A5. RAN RECIRCULATION FANS FOR TWO HOURS AND PERFORMED OPERERATIONAL TEST IAW AMM 21-22-10. ALL CHECKED GOOD NO ODOR NOTED AT THIS Aug 12, 2017 · N306PQ · Cndair CL6002D24 · Air Distribution SystemSDR REXA2017050800575Fan · inoperativeBOTH FA'S REPORTED HEAVY ELECTRICAL ODOR IN FWD PART OF CABIN BETWEEN ROW1 AND FA JUMPSEAT. OVEN NOT IN USE. NO SMOKE OBSERVED. ACCOMPLISHED + INSPECTED AREA FOR SMELL PER FIM 21-22-00. ISOLATED SMELL COMING FROM LEFT PACK. DEFERRED LEFT PACK PER MEL 21-51-1B.May 8, 2017 · N306PQ · Cndair CL6002D24 · Air Distribution FanSDR REXA2017040400440Stringer · corrodedSTR 27 HAS CORROSION SPOTS BETWEEN FRAMES 319.70 TO JUST FWD OF FRAME 310, IN THE FWD E & E BAY. OUT OF LIMITS. REPAIRED STR 27 IAW EA CRJ953-05486 REV IR.Apr 4, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2017040100430Channel · crackedDIAPHRAM JUST TO THE RIGHT OF STGR 27 HAS CORROSION BETWEEN FRAMES 364 AND 349, IN THE FWD E&E BAY. REMOVED AND REPLACED DIAPHRAM RIGHT OF STGR 27, FR 364-FR 349 IAW SRM 51-42-06 + 51-42-21 OPS TEST OF THE MAIN AVIONICS DOOR IS GOOD IAW AMM 52-42-00-710-801.Apr 1, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017040100439Handle · crackedMAIN AVINICS COMPT. DOOR OUTER HANDLE IS CRACKED. REMOVED AND REPLACED AVIONICS DOOR HANDLE IAW AMM 52-42-02. OPS TEST OF THE MAIN AVIONICS DOOR GOOD IAW AMM 52-42-00-710-801.Apr 1, 2017 · N306PQ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2017033100432Drag Angle · crackedMAIN ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED ENTRY DOOR AFT DRAG BRACE ANGLE IAW REO 670-52-11-072.Mar 31, 2017 · N306PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2017033100433Channel · corroded(OK TO INSTALL TCAS CHANNEL) STGR27 CORRODED AT FS295. REMOVED AND REPLACED STRINGER AND RESTORED FINISH IAW SRM 51-42-06, 51-42-21 AND 51-25-16.Mar 31, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017033000431Channel · crackedAFT WING TO BODY FAIRING SPLICE CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL ON AFT WING TO BODY FAIRING, AND REPLACED W/NEW SERV CHANNEL IAW SRM 51-42-13.Mar 30, 2017 · N306PQ · Cndair CL6002D24 · Aerodynamic FairingsSDR REXA2017032900436Crossbeam · corrodedRT 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED WITH NEW BEAM PER SRM 51-42-06, 51-42-13 AND 51-42-21.Mar 29, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017032900438Crossbeam · corrodedLT 280 CROSSBEAM IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED WITH NEW BEAM PER SRM 51-42-06, 51-42-13 AND 51-42-21.Mar 29, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017032800434Door Sill · corrodedRT FLOOR SILL AT FS 280 HAS CORROSION AT THE TOP AND BOTTOM SIDE IN CABIN. OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED PER SRM 53-21-43.Mar 28, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017032800435Diaphragm · corrodedDIAPHRAM JUST TO THE LEFT OF STGR 27 HAS CORROSION ON BOTH SIDES BETWEEN FRAMES 364 AND 349, IN THE FWD E & E BAY. OUT OF LIMITS. REMOVED AND REPLACED DIAPHRAM LEFT OF STGR 27 FR 364- FR 349 IAW SRM 51-42-06 + 51-42-21.Mar 28, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2017032800437Floorbeam · corrodedFWD ANGLE SIDE OF 280 BEAM HAS CORROSION BETWEEN LBL 12 AND RBL 12, IN FLT DECK BELOW FLOOR. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-42-06.Mar 28, 2017 · N306PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2016062701158Pbe · unserviceableCOCKPIT PBE VACUUM SEAL BROKEN. INSTALLED SERVICEABLE PBE IAW AMM 35-31-06.Jun 27, 2016 · N306PQ · Cndair CL6002D24 · Emergency EquipmentSDR REXA2015060600562Unknown · odorWITH APU ON & BOTH PACKS ON ENS OFF, INSTANT SMELL OF SMOLDERING PLASTIC & RUBBER. MOSTLY IN FLIGHT DECK BUT THROUGHOUT ACFT. NO FAULTS FOR ANY ASSOCIATED SYSTEMS NOTED IN MDC. INSPECTED AFT EQUIP BAY, NO DISCREPANCIES NOTED. PERFORMED APU BLEED AIR OPS CHJun 6, 2015 · N306PQ · Cndair CL6002D24 · Air Distribution SystemSDR REXA2015032600353Escape Hatch · out of adjustCREW HATCH LEAKING AT RT CORNER LOWER PART OF HATCH. INSPECTED FITS & CLEARANCES OF CREW ESCAPE HATCH AS WELL AS SEAL & HATCH LOCKING PINS & RECEPTACLES FOR SECURITY. FOUND HATCH TO BE OUT OF ADJUSTMENT & RIG LE DOWN MORE THAN .070"". SEAL OKAY IAW MM 52-22Mar 26, 2015 · N306PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2015030300278Seal · lack of lubeCREW ESCAPE HATCH LEAKING WATER. LUBRICATED THE CREW ESCAPE HATCH SEAL IAW AMM 12-20-52 PARA 4 STEP A 3.Mar 3, 2015 · N306PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2014122201199Light · unsecureEMERGENCY FLOOR PATH LIGHTING UNSECURE IN FWD GALLEY, LT SIDE & DIRECTLY BEHIND FWD LAVATORY ON RT SIDE. SECURED EMER FLOOR PATH IAW AMM 33-51-01.Dec 22, 2014 · N306PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2014102001057Light · unsecureFLOOR STRIP IN FRONT OF GALLEY CART B CAME UP IN FLIGHT. SECURED EMER FLOOR STRIP IAW AMM 33-51-01. NO OTHER DEFECTS NOTED AT THIS TIME.Oct 19, 2014 · N306PQ · Cndair CL6002D24 · Emergency Lighting
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