N925EV

Service difficulty reports · 191

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 = 'N925EV' 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 ASOA201001444Attach Fitting · corrodedCLIP AT FS 322 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21. SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.Sep 24, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001443Attach Fitting · corrodedCLIP AT FS 336 ON BOTTOM OF PAX DOOR IS CORRODED. R & R CORRODED CLIP IAW SRM 51-40-11, 51-42-06, AND 51-42-21 SEE FORM 412 FOR FABRICATION AND INSTALLATION DETAILS.Sep 24, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001427Intercostal · crackedRT SIDE INTERCOSTAL LOCATED BETWEEN THE 621 BULKHEAD AND 625 IS CRACKED. REMOVED CRACKED PART RT SIDE INTERCOSTAL BETWEEN 621 BULKHEAD AND 625 IAW SRM 51-41-02. FABRICATED PART IAW SRM 53-61-17 PG. 3 FIG 1. TREATED AND PRIMED AND APPLIED TOPCOAT IAW SRM 51-2Sep 20, 2010 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001426Isolator · crackedAFT PRESSURE BULKHEAD HAS 5 ISOLATORS WITH CRACKS. REMOVED UNSERVICEABLE NR5 ISOLATORS FROM 621AFT PRESSURE BULKHEAD AND INSTALLED SERVICEABLE 5 EA ISOLATORS IAW SRM 51-42-06.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001425Seat Track · corrodedRT NR 1 FLOOR SEAT TRACK HAS FLAKING CORROSION. REMOVED DAMAGED SEAT FLOOR TRACK LOCATED DRILLED AND INSTALLED SERVICABLE FLOOR TRACK RT NR1 IAW SRM 51-40-11 AND AMM 53-01-11.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001424Rib · crackedBATTERY RIB IN RT W/W IS CRACKED. REPAIRED BATTERY BIB RT IAW REO 601R-57-51-046, REV B. AND EC/TC 601R-57-51-046.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001423Rib · crackedBATTERY RIB IN LT W/W IS CRACKED. REPAIRED BATTERY RIB IN LT W/W WHICH WAS CRACKED IAW REO 601R-57-51-046, REPAIR NR 2.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001422Skin · crackedPAX DOOR INNER SKIN TO STAIR SUPPORT AFT DRAG ANGLE IS CRACKED. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-513. C/W ASA EC/TC REO 601R-52-11-513.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001421Structure · crackedFOUND CRACK INDICATION APPROX .2500" IN LENGTH AT WL 58.7 AND RBL 9. COMPLIED WITH EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260 REV E AND COMPLIED WITH EC/TC REO 601R-53-41-609 OR AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV B (SHEET 3 TO 11 REV Sep 20, 2010 · N925EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001330Handle · out of adjustPAX DOOR FAILED FUNCTIONAL TEST ON HANDLE FORCE AND OPENING TIME. ADJUSTED PAX DOOR INNER HANDLE IAW AMM SUBTASK 52-11-25-820-003, STEPS AC.1 THRU 7 AND REACCOMPLISHED FUNCTIONAL TEST IAW AMM 52-11-00-720-802. NO DEFECTS NOTED.Sep 13, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001329Skin · corrodedEXTERIOR SKIN AT LOWER AFT CORNER OF PAX DOOR CUTOUT HAS CORROSION. REPAIRED EXTERIOR SKIN AT LOWER AFT CORNER OF PAX DOOR CUTOUT, BLENDED TO WITHIN SERVICEABLE LIMITS IAW SRM 51-21-06 AND SRM 53-00-31.Sep 13, 2010 · N925EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001087Placard · deterioratedPAX DOOR EXIT PLACARD DETERIORATED. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC. (CLOSED)Aug 7, 2010 · N925EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001086Bulb · burned outLT 2 EXTERNAL EMERGENCY LIGHT INOP. R & R LT NR 2 EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD. ITEM: 1 R & R LT NR 2 EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD.Aug 7, 2010 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000694Light · inoperativeLEFT OVERWING NR 4 EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT OVERWING NR 4 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.May 7, 2010 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200901304Flashlight · inoperativeF/O FLASHLIGHT INOP.Nov 14, 2009 · N925EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA200901139Anchor Fitting · crackedPAX DOOR FWD ANCHOR FITTING CRACKED. INSTALLED NEW PAX DOOR FWD ANCHOR FITTING IAW EC/TC EO600-52-66 C/W. REMOVED PAX DOOR FWD ANCHOR FITTING IAW AMM 52-11-17. INSTALLED NEW PAX DOOR FWD ANCHOR FITTING IAW EC/TC EO600-52-66 C/W.Oct 15, 2009 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900509Bulkhead · crackedFOUND CRACK ON 202 PRESS BULKHEAD AT PARKING BRAKE CABLE. REPAIRED IAW EC/TC EO600-53-217.Apr 30, 2009 · N925EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200900057Light · malfunctionedWITH THE EMERGENCY LIGHTS SWITCH IN THE OFF POS SOME OF THE EMERGENCY LIGHTS STAY ON WHEN POWER IS TURNED OFF.Jan 11, 2009 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200801689Support Beam · crackedCARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.3 INCH IN LENGTH.Dec 2, 2008 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200801590Angle · crackedPAX DOOR INNER HANDLE MEET STRUCTURE HAS CRACKED ANGLE. REMOVED THE PAX DOOR INNER HANDLE STRUCTURAL ANGLE. LOCATED, SEALED AND INSTALLED A NEW ANGLE IAW SRM 51-40-11 AND 51-42-06.Dec 1, 2008 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200700972Light · inoperativeRIGHT WING EMERGENCY LIGHT IS INOP.Jul 8, 2007 · N925EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200700100Unknown · unknownFOUND BIRDSTRIKE ON NOSE GEAR, EMERGENCY DECLARED.Jan 14, 2007 · N925EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR TRAX200600915Pump · failedHYD SYSTEM 2 QTY READS 5 PERCENT LOST HYD 2A PUMP IN FLIGHT (EMERGENCY DECLARED).Oct 24, 2006 · N925EV · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR TRAX200600731Attach Fitting · crackedI/B CLIP CRACKED @ FS280 RBL9Sep 10, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600730Attach Fitting · crackedIB AND OB CLIPS AT FS280 LBL 9 CRACKED.Sep 10, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600729Floorbeam · crackedAFT ANGLE CRACKED AT FS 280 FLOORBEAM JUST OB OF RBL 9.Sep 10, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200600728Floorbeam · crackedAFT ANGLE CRACKED AT FS 280 FLOORBEAM JUST OB OF LBL 9.Sep 10, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200600720Intercostal · crackedRT OB FS 484 INTERCOSTAL CRACKED.Sep 9, 2006 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600719Intercostal · crackedLT OB FS 484 INTERCOSTAL CRACKED.Sep 9, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600716Stringer Clip · crackedRIGHT SIDE FS 625 CLIP CRACKED (MARKED).Sep 8, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600285Handle · crackedASD HANDLE CRACKED.May 27, 2006 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05797Light · brokenFLT 4287 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT THE PASSENGER DOOR WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVISep 23, 2005 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05265Apu · overservicedFLT 4151 - DURING FINAL APPROACH TO ATL FROM FPO, THE CREW RECEIVED A SMOKE TOILET CAUTION MESSAGE. THE MESSAGE OCCURRED SIMULTANEOUSLY WHEN SHIFTING THE BLEEDS FROM THE ENG TO THE APU. A MILD ACRID ODOR WAS PRESENT BRIEFLY WITH NO HARD INDICATIONS OF SMOKE Mar 23, 2005 · N925EV · Cndair CL6002B19 · APU Oil SystemSDR ASOA05241Clip · crackedDURING A C-CHECK IN MCN, THE FS 625 LEFT CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 625 LT CLIP IAW CRJ-200 SRM 51-42. (M)Mar 16, 2005 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05242Angle · crackedDURING A C-CHECK IN MCN, THE FS 621 LT/RT FLOOR SUPPORT ANGLES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 621 LT/RT FLOOR SUPPORT ANGLES IAW ASA EO 600-53-0105. (M)Mar 16, 2005 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05235Clip · crackedDURING A C-CHECK IN MCN, THE RIGHT OUTBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT OUTBOARD FS 280 CLIP. (M)Mar 15, 2005 · N925EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04525Valve · failedFLT 4390 - DURING DESCENT INTO MSP FROM DFW, THE AUXILIARY POWER UNIT PERFORMED AN AUTOMATIC SHUTDOWN WITH NO WARNING MESSAGE, ACCOMPANIED BY A HEAVY FUEL ODOR UPON SHUTDOWN. THE AIRCRAFT LANDED SAFELY IN MSP. MAINTENANCE REMOVED AND REPLACED THE FUEL SOLENOJul 23, 2004 · N925EV · Cndair CL6002B19 · APU Engine Fuel and ControlSDR ASOA04479Light · odorDURING CRUISE, THE CREW NOTICED A HOT PLASTIC TYPE SMELL FROM THE LAVATORY AREA. UPON INVESTIGATION THE CREW DETERMINED THE LAVATORY OCCUPIED LIGHT WOULD NOT EXTINGUISH WHICH WAS CAUSING THE SMELL. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LAVATJul 1, 2004 · N925EV · Cndair CL6002B19 · Passenger Compartment LightingSDR ASOA04392Wire · brokenDURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHT POWER CABLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.May 30, 2004 · N925EV · Cndair CL6002B19 · Emergency LightingSDR ASOA04284Window · crackedFLT 4266 - DURING DESCENT INTO DFW FROM CAE, AT APPROXIMATELY 20,000 FT THE INTERIOR PANE ON THE FIRST OFFICERS RIGHT WINDOW CRACKED. THE CRACK CONTINUED TO PROPAGATE AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. NO PRESSURIZATION OR OTHER PROBLEMS OCCURREDApr 19, 2004 · N925EV · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA04157O-Ring · leakingFLT 4768 - DURING DESCENT AND APPROACH INTO ATL FROM GTR, THE CREW SMELLED FUMES AFTER SELECTING THE BLEEDS TO THE APU. SMOKE FILLED THE COCKPIT AND CABIN ACCOMPANIED BY A SMOKE LAVATORY MESSAGE. THE CREW SWITCHED THE BLEEDS BACK TO THE ENGINES AND THE SMOKEFeb 27, 2004 · N925EV · Cndair CL6002B19 · APU Oil System
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