N926EV

Service difficulty reports · 195

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 = 'N926EV' 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 ASOA201001136Floor Support · corrodedFLOOR SUPPORT HAS MINOR CORROSION AROUND NUTPLATES ON INBD ROW OF CARGO FLOOR PANEL 281LLF. REMOVED NUT PLATES ON FLOOR SUPPORT CAP AT LBL 27 STA 585-615 BLENDED CORRODED AREAS ON LBL 27 FLOOR SUPPORT CAP AT STA 615, 609, 603, 597, 591, 585 REF SEM 51-21-06. Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001135Seat Track · corrodedSEAT TRACK HAS MINOR CORROSION LBL 9.00 AT FS 559 + 80. REMOVED OLD SEAT TRACK AT LBL 9 AT FS 559+80 & INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001109Seat Track · corrodedSEAT TRACK HAS MINOR CORROSION RBL9.00 AT FS 559 + 92. (APPX). REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-004.Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001108Seat Track · corrodedSEAT TRACK HAS MINOR CORROSION, RBL 9.00 AT FS 559+80. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00-910-004.Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001091Skin · corrodedBELLY CORROSION JUST AFT FRAME 310 AT LT SIDE OF 27 NEXT TO WATER DRAIN. REMOVED WATER DRAIN LEFT OF STR 27 REMOVED 5EA FASTNERS FROM LEFT SIDE OF STR 27 IAW SRM 51-42-06 REMOVED CORROSION LEFT OF STR 27 & AFT OF 310 NEXT TO WATER DRAIN IAW SRM 51-21-06. AREAAug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001090Frame · corrodedCORROSION ON FWD AND AFT SIDE OF 349 FRAME AND LOWER LEG BETWEEN STRINGERS 26L TO 26R BELLY. REMOVED FASTENERS THROUGH SKIN, DRILLED OUT FASTENERS THROUGH TOP OF FRAME FROM STR25L TO 25R, REMOVED GUSSETE & TRACK SUPPORT. REMOVED FASTENERS THROUGH TIE STRAP Aug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201001089Floor Support · crackedFLOOR SUPPORT CRACKED IN CARGO COMPARTMENT AT AFT PRESSURE BULKHEAD UNDER PANEL 281LLF. REMOVED LT FS 621 FLOOR SUPPORT ANGLE LT SIDE REF SRM 51-42-06 AND 51-42-21. DRILLED COUNTERSUNK AND TRIMMED NEW FLOOR SUPPORT ANGLE REF SRM 51-40-11. STARTED INSTALLINGAug 9, 2010 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201000967Lamp · burned outNR 1 CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED NR 1 CEILING EMERGENCY LIGHT IAW AMM 33-51-16 OPS CHECK GOOD. RELAMPED NR 1 CEILING EMERGENCY LIGHT IAW AMM 33-51-16 OPS CHECK GOOD.Jun 29, 2010 · N926EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000311Seal · lack of lubeCATERING PERSONEL AND F/A REPORT SERVICE DOOR BEING DIFFICULT TO CLOSE AND OPEN. CLEANED AND LUBRICATED DOOR SEAL AND STRIKER IAW MM 12-20-52. OPS CK GOOD IAW MM 52-41-00.Feb 23, 2010 · N926EV · Cndair CL6002B19 · Service DoorsSDR ASOA200900603Door · stuckCABIN SVC REPORTS SERVICE DOOR EXTREMELY DIFFICULT TO OPEN AND CLOSE. FLT 5603 DEL 35 MINS.May 31, 2009 · N926EV · Cndair CL6002B19 · Service DoorsSDR ASOA200900355Flap · failedAFTER TAKEOFF FLAPS FAILED AT 8FT, LANDED CVG. NOT AN OVERWEIGHT LANDING. EMERGENCY DECLARED. A/C RETURNED TO CVG AFTER T/O. FLT 4972 DEL 138 MINS.Mar 27, 2009 · N926EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA200801444Step · brokenPAX DOOR BOTTOM STEP BROKEN.Nov 3, 2008 · N926EV · Cndair CL6002B19 · Entrance StairsSDR TRAX200800948Skin · corrodedRT WING LOWER PLANK ACCESS HOLE 650BB HAS CORROSION AROUND ENTIRE LANDING IN CRITICAL AND NON-CRITICAL AREAS. FAILED NDT INSPECTION 60% FULL SCREEN HEIGHT. REPAIRED RT WING LOWER PLANK ACCESS HOLE NR10 650BB IAW REO 601R-57-21-030. COMPLIED WITH EC/TC EO 6Jul 30, 2008 · N926EV · Cndair CL6002B19 · Wing, Plate/SkinSDR TRAX200800947Support Beam · crackedCARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH IN RADIUS. REMOVED AND REPLACED CARGO DOOR SUUPPORT BEAM ANGLE IAW SRM 51-42-21. PRESSURE CHECK DUE. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801. NO DISCREPANCIES NOTED AT THIS TIME. (S)Jul 30, 2008 · N926EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR TRAX3200800943Sill · crackedJUST OUTBOARD LBL 9, FS 280 UPPER SILL CRACKED APPROX 1 INCH LONG AT MLG EMERGENCY RELEASE CABLE BRACKET. REMOVED MLG EMERGENCY RELEASE CABLE BRACKET IAW SRM 51-41-02. REPAIRED LBL 9 FS 280 UPPER SILL IAW REO 601R-53-11-138-NC AND DEVIATION REO 601R-53-11-14Jul 28, 2008 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800943Sill · crackedJUST OUTBOARD LBL 9, FL 280 UPPER SILL CRACKED APPROX 1 INCH LONG AT MLG EMERGENCY RELEASE CABLE BRACKET. (S)Jul 28, 2008 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800938Intercostal · crackedFS 484.0, RBL 36.0 INTERCOSTAL CRACKED (NOT PREVIOUSLY REPAIRED). REPAIRED INTERCOSTAL AT FS 484.0 RBL 36.0 IAW REO 601R-53-41-059. COMPLIED WITH REO 601R-53-41-059. PRESSURE CHECK DUE. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801. NO DISCREPANCIES NJul 28, 2008 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800937Channel · crackedCARGO DOOR FWD, LOWER "C" CHANNEL IS CRACKED. REMOVED AND REPLACED CHANNEL IAW SRM 51-42-06. (S)Jul 28, 2008 · N926EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR TRAX200800936Angle · crackedRT SIDE FUSELAGE STATION 621 OBLIQUE ANGLE CRACKED. REFERENCE MWC JOB 8784311, OP 48 FOR REPLACEMENT OF OBLIQUE ANGLES. REMOVED LT/RT FS 625 OBLIQUE ANGLES IAW SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE OBLIQUE ANGLES IAW SRM 51-40-11. INSTALLED NEW SEJul 27, 2008 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800935Angle · crackedLT SIDE FUSELAGE STATION 621 OBLIQUE ANGLE CRACKED. REPLACEMENT OF OBLIQUE ANGLES. REMOVED LT/RT FS 625 OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11. INSTALLED NEW SERVICEABLE FS 625 OBLIQJul 27, 2008 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX0800933APin · not seatedJOB 8783411 OPERATION 37. RT OVERWING EMERGENCY EXIT (EYE LEVEL) LIGHT DOES NOT WORK FROM BATTERY PACK NR 4. TROUBLESHOT USING CRJ 200 WDM 33-51-00 AND 33-52-00 AND FOUND WIRE LY10D22 CONTACT PIN NOT SEATED IN TB105-3. SECURED WIRE CONTACT INTO TERMINAL MODJul 25, 2008 · N926EV · Cndair CL6002B19 · Light System WiringSDR TRAX200800931Pin · not seatedRT OVERWING EMERGENCY EXIT (EYE LEVEL) LIGHT DOES NOT WORK FROM BATTERY PACK NR 4. TROUBLESHOT USING CRJ 200 WDM 33-51-00 AND 33-52-00 AND FOUND WIRE LY10D22 CONTACT PIN NOT SEATED IN TB105-3. SECURED WIRE CONTACT INTO TERMINAL MODULE IAW EESPM 20-18-00. RTJul 25, 2008 · N926EV · Cndair CL6002B19 · Light System WiringSDR TRAX200800932Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR SPLICE. COMPLIED WITH REO 601R-52-11-513 AND ASA ECTC 601R-52-11-513. SUPPLEMENTAL SDR CLOSED 7/31/08. (A)Jul 25, 2008 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200800933Angle · crackedLT AND RT FS 625 OBLIQUE ANGLES ARE CRACKED. OPEN. (S)Jul 25, 2008 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200800586Light · damagedFLOOR EMERGENCY FLOODLIGHT DAMAGED.Apr 30, 2008 · N926EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200800466Flap · failedFLAP FAIL AT ZERO WHEN SELECTING 8 AT 200 KTS. EMERGENCY EQUIPMENT REQUESTED TO BE ON STANDBY AS A PRECAUTION. FLT4656 DEL 171 MINS.Mar 24, 2008 · N926EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200800357Flap System · failedFLAPS FAILED AT 0 AFTER TAKEOFF IN ATL RETURNED FOR LANDING IN ATL, EMERGENCY DECLARED. AIRCRAFT RETURNED TO ATL AFTER T/O.Feb 29, 2008 · N926EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200701736Flap System · malfunctionedFLAPS FAIL AT 0 DEGREES ON APPROACH WHEN SELECTED TO 8 DEGREES. EMERGENCY EQUIPMENT ON STANDBY.Nov 14, 2007 · N926EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200701395Step · brokenASD LOWER STEP BROKEN.Sep 24, 2007 · N926EV · Cndair CL6002B19 · Entrance StairsSDR TRAX200701031Door · stuckSERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE.Jul 20, 2007 · N926EV · Cndair CL6002B19 · Service DoorsSDR TRAX200600864Sign · inoperativeEMERGENCY EXIT SIGN NEXT TO SERVICE DOOR INOP.Oct 13, 2006 · N926EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600704Angle · crackedRANRC 244, PAX DOOR AFT DRAG ANGLE CRACKED.Sep 5, 2006 · N926EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200600703Intercostal · crackedRANRC 231, RIGHT RBL 27 AT FS 484 INTERCOSTAL CRACKED.Sep 4, 2006 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600702Attach Fitting · crackedRANRC 216, RBL 9, FS 280 O/B CLIP CRACKED. REMOVED AND DUPLICATED CLIPS USING 2024-T3, .050, PO# 8398-1. PRIMED AND TOPCOATED. ALL WORK DONE IAW CRJ SRM 51-24-26, 51-25-16. (EMP 302) OK TO INSTALL. (INSP RA313) COMPLETED INSTALLATION IAW CRJ SRM 51-24-26, 51Sep 4, 2006 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600701Attach Fitting · crackedRANRC 215, LBL 9, FS 280 CLIPS I/B AND O/B CRACKED. REMOVED AND DUPLICATED CLIPS USING 2024-T3, .050, PO 8398-1. PRIMED AND TOPCOATED. ALL WORK DONE IAW CRJ SRM 51-24-26, 51-25-16. (EMP 302) OK TO INSTALL. (INSP RA313) COMPLETED INSTALLATION IAW CRJ SRM 51-2Sep 4, 2006 · N926EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600700Intercostal · crackedRANRC 211, LEFT FS 484 OUTBOARD OF LBL 36, BRACKET AND INTERCOSTAL CRACKED.REMOVED DAMAGED ANGLE AT O/B SIDE OF LBL 27 & CUT-OUT DAMAGED SECTION OF INTERCOSTAL AT I/B SIDE OF LBL 36 AS REQUIRED IAW REO. HAD LPI OF INTERCOSTAL CUTLINE PERFORMED REFER TO W/C 28Sep 4, 2006 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600699Floor Support · crackedRANRC 207, LT 621 FLOOR SUPPORT ANGLE CRACKED. ACCOMPLISHED ASA EO CARD NO. REO 601R-53-61-117 STEPS 1-7 JP929 09-05-06 OK TO INSTALL REPAIR ANGLE RA313 INSTALLED REPAIR IAW ASA TASK CARD REO 601R-53-61-117. TS1050 090606 RA313 REQ'S TOP COAT. TOP COSep 4, 2006 · N926EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600578Light · inoperativeEMERGENCY EXIT FLOOR LIGHTING INOP AT SEAT 1CD.Aug 4, 2006 · N926EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600205Light · intermittentEMERG FLOOR LIGHTING FLICKERS INTERMITTENTLY WHEN SWITCH IS IN THE "ON" POSITION, FLT 4897 DEL 38 MINS.May 11, 2006 · N926EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600133Placard · unsecureEXIT PLACARD ON PAX DOOR FADED AND NOT SECURED.Apr 24, 2006 · N926EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA05335Control Panel · malfunctionedDURING CLIMB OUT, AT APPROX 5,000 FT THE CREW RECEIVED A CARGO SMOKE WARNING. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. AFTER THE CREW DISCHARGED THE FIRE BOTTLES, THE WARNING WENT OUT. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY. AApr 14, 2005 · N926EV · Cndair CL6002B19 · Fire DetectionSDR ASOA05234Power Supply · dischargedFLT 4500 - DURING A GROUND INSPECTION IN ATL, LEFT EXTERIOR EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY UNIT AT ROW 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 20, 2005 · N926EV · Cndair CL6002B19 · Emergency LightingSDR ASOA04380Windshield · brokenDURING DESCENT, OUT OF 25,000 FT, THE F/O`S WINDSHIELD SHATTERED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY.May 24, 2004 · N926EV · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA03564Bpsu · failedDURING TAKEOFF, AT APPROX 1,000 FEET AFTER SELECTING THE FLAPS FROM EIGHT DEGREES TO ZERO DEGREES THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW REQUESTED EMERGENCY EQUIPMENT STANDBY AS A PRECAUTION AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. Nov 3, 2003 · N926EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA03553Control Unit · malfunctionedDURING CLIMB-OUT, WHEN FLAPS WERE SELECTED TO ZERO DEGREES, THEY STAYED AT EIGHT DEGREES AND THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW LEVELED OFF THE AIRCRAFT AND MAINTAINED A SPEED OF 200 KNOTS WHILE COMPLYING WITH THE QRH. UPON NOTIFYING THNov 1, 2003 · N926EV · Cndair CL6002B19 · Trailing Edge Flap Control System
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