N748EV

Service difficulty reports · 277

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 = 'N748EV' 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 ASOA201201495Angle · corrodedINTERNAL FWD JACKING FITTING ANGLE AT S26L IS CORRODED BETWEEN FS 265 & 280. REMOVED CORROSION IAW SRM 51-21-06-001-001.May 1, 2012 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201493Angle · corrodedANGLE AT S25R FWD OF FS 364.00 IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-01-001-001-A01, 51-42-21-001-001-A01 AND SWG SH670-32050.May 1, 2012 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201491Angle · corrodedANGLE AT S25L FWD OF FS 364.00 IS CORRODED. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.May 1, 2012 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201481Floor Panel · crackedFWD RIGHT EQUIPMENT BAY FLOOR CRACKED JUST AFT OF AFT DOOR FRAME STRUCTURE. REPAIRED.Apr 30, 2012 · N748EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA201201479Floor Panel · crackedFWD LEFT EQUIPMENT BAY FLOOR CRACKED JUST AFT OF AFT DOOR FRAME STRUCTURE. REPAIRED.Apr 30, 2012 · N748EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA201100851Megaphone · inoperativeAFT MEGAPHONE INOPERATIVE. R & R AFT MEGAPHONE IAW AMM 25-60-00.Apr 28, 2011 · N748EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201100418Cover · dislodgedEMERGENCY EXIT LIGHT COVER FELL OFF. REMOVED AND REPLACED EMERGENCY LIGHT FIXTURE IAW AMM 33-51-05. OPS CK GOOD.Mar 4, 2011 · N748EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100381Sign · dislodgedEMERGENCY EXIT LIGHT SIGN AT PAX DOOR HAS FALLEN OFF. LIGHT LENS/ COVERS, INCLUDING EMERGENCY LIGHT. R & R EMERGENCY LIGHT FIXTURE IAW AMM 33-51-05. OPS CHECKED GOOD.Feb 25, 2011 · N748EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201000884Angle · crackedSUPPORT ANGLE LT SIDE FOR COCKPIT PANEL 221ALF CRACKED. BEGAN REMOVING FASTENERS ON LT SIDE FLOOR SUPPORT ANGLE FOR COCKPIT PANEL 221ALF. IAW SRM 51-42-06-001-001-A01. R & R LT SIDE COCKPIT FLOOR SUPPORT ANGLE WITH SERVICEABLE PART ALL WORK DONE IAW SRM 51Jun 8, 2010 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000883Threshold · corrodedASD THRESHOLD MID CAP ANGLE CORRODED. BLENDED DAMAGED AREA OF MID CAP ANGLE FOUND TO BE OUT OF LIMITS REF SRM 51-21-06-001-001. RECEIVED SERVICEABLE ANGLE AND PICKED UP ALL EXISTING FASTENER HOLES FROM UNSERVICEABLE ANGLE IAW SRM 51-40-11-001-001-A01 AND 5Jun 7, 2010 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000872Floorbeam · corrodedBS 280 BEAM REQUIRES REPLACEMENT DUE TO CORROSION, REPAIRED. PRIMED AND PAINTED BARE AREAS AT CTR EATHING, INSTALLED NEW 280 CROSS BEAM IAW SRM 51-42-06, 51-42-20. 5. DRIP TRAYS AND FLOOR PANEL NUTPLATES REQUIRES INSTALLATION AND 280 BEAM NEEDS TO BE SEALED AJun 7, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201000857Bulkhead · corrodedFS 280.00, BULKHEAD RT SIDE LOWER WEB HAS CORROSION DAMAGE. REMOVED BULKHEAD LOWER IAW SRM 51-42-06-001-001-A01. FABRICATED LOWER WEB IAW REO 670-53-11-052. FABRICATED WEB PANEL. PERFORMED LPI, TYPE 1, METHOD C ON RT LOWER WEB IAW SRM 51-12-00-001-001 IAW MJun 1, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201000856Bulkhead · corrodedFS 280.00 BULKHEAD LT SIDE LOWER WEB HAS CORROSION DAMAGE. REMOVED LT SIDE FS280 BULKHEAD LOWER WEB IAW SRM 51-42-06-001-001-A01. DRILLED ALL HOLES IN LT SIDE 280 LOWER PANEL, FASTENER HOLES DRILLED IAW SRM 51-40-11-001-001-A01. INSTALLED ALL FASTENERS IN LJun 1, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201000852Angle · crackedUPON REMOVAL OF RT LOWER BULKHEAD WEB FS 280 FOUND ANGLE AT RBL 26 CRACKED AT BOTTOM HOLE. R & R RT LOWER WEB ANGLE IAW SRM 51-42-06-001-001-A01.May 30, 2010 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000826Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. REMOVED FS 280 BEAM, ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. PERFORMED LPI, TYPE1, METHOD C ON CUT LINE ON NEW FS 280.00 BEAM IAW SRM 52-12-00-001-001 IAW NDT INSP PROCEDURE PT-1. NO INDICATIONS NOTEDMay 26, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201000820Post · corrodedFLIGHT STA DOOR POST AT FS280 LBL 11.128 HAS SIGNS OF CORROSION AFT LOWER CORNER. COMPLIED WITH EC/TC REO 670-53-11-511 AND REO 670-53-11-511.May 25, 2010 · N748EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201000882Threshold · corrodedASD THRESHOLD FWD DRAIN AREA CORRODED MARKED. CORROSSION FOUND TO BE ON ANGLE AT ASD THRESHOLD AREA. R & R ANGLE REFER TO JOB 1, OP 169 FOR WORK ACCOMPLISHED.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000881Threshold · corrodedASD THRESHOLD CORRODED AT CTR JUST AFT OF DOOR HARNESS ADEL CLAMP. BLENDED ANGLE AT ASD THRESHOLD FOUND TO BE OUT OF LIMITS REF SRM 51-21-06-001-001, WA161715 6/4/10. RECEIVED & STARTED DRILLING NEW ANGLE AND INSTALLED NUT PLATES ON NEW ANGLE REF SRM 51-42-0May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000818Drag Angle · crackedPERFORMED EDDY CURRENT INSP OF RT VERT STAB TO FUSELAGE ATTACH DRAG ANGLE IAW MAC NDT INSP PROCEDURE ET-2. DRAG ANGLE IS CONFRIMED CRACKED AND END OF CRACK IS MARKED. REMOVED RT AFT DRAG ANGLE IAW SRM 51-42-27-001-001-A01, 51-42-21-001-A01 & 51-42-13-001-001-May 24, 2010 · N748EV · Cndair CL6002C10 · Vertical StabilizerSDR ASOA201000817Drag Angle · crackedPERFORMED EDDY CURRENT INSP OF LT VERTICAL STAB TO FUSELAGE ATTACH DRAG ANGLE IAW MAC NDT INSP PROCEDURE ET-2, DRAG ANGLE IS CONFIRMED CRACK AND END OF CRACK IS MARKED. REMOVED LT SIDE AFT DRAG ANGLE & LOCATED HOLES IN NEW DRAG ANGLE IAW SRM 51-42-27-001-001-May 24, 2010 · N748EV · Cndair CL6002C10 · Vertical StabilizerSDR ASOA201000816Wire · brokenNR 1 EMERGENCY CEILING FLOOD LIGHT CONNECTOR P355 (STN 409 RT) HAS A BROKEN WIRE. STRIPPED WIRE OF CONNECTOR P355 AND CRIMPED NEW CONTACT PN 350689-7 ON WIRE AND REINSERTED WIRE IN 9355 IAW ESPM CH 20-11-00-AND CH 20-16-00. PERFORM OPS TEST OF THE EMERGENCY May 24, 2010 · N748EV · Cndair CL6002C10 · Light System WiringSDR ASOA201000815Stringer · corrodedMAIN AVIONICS COMPARTMENT BETWEEN FS 319.70 & FS 333.00 S26R AROUND ATTACH FASTENERS HAS CORROSION. REMOVED RIVETS IN AREA OF CORROSION ON STR 26R AND BLENDED CORROSION IAW SRM CH 51-42-06-001-001- & 51-21-06-001-001. KC 161720 05/26/10. PERFORMED THICKNESSMay 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201000814Frame · noneMAIN AVIONICS COMPARTMENT FS 319.70 BETWEEN S26L & S27 FRAME AFT SIDE HAS CORROSION. AFTER FURTHER INVESTIGATION FOUND TO BE MISSING PAINT AND DIRT. CLEANED AREA NO CORROSION FOUND. ALODINED PRIMED AND PAINTED IAW SRM CH 51-25-00-001-001-A01.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201000813Intercostal · corrodedMAIN AVIONICS COMPARTMENT BETWEEN FS 349.00 & FS 364.00 AND BETWEEN S27 & S26R INTERCOSTAL AROUND ATTACH FASTENERS HAS CORROSION. R & R INTERCOSTAL IAW SRM CH 51-42-06-001-001-A01.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201000812Floorbeam · corrodedMAIN AVIONICS COMPARTMENT FS 280.00, 241ALF, FLOOR SUPPORT STRUCTURE UPPER SURFACE HAS CORROSION. FLOOR SUPPORT ANGLE WAS R & R FOR ALL WORK ACCOMPLISHED.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201000811Seat Track · corrodedCORROSION DAMAGE ON FLOOR SEAT RAIL FS 485.00 TO FS 581.00 AT RBL 9.0. R & R FLOOR SEAT RAIL IAW AMM TSK 53-00-49-400-801.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000810Seat Track · corrodedCORROSION DAMAGE ON FLOOR SEAT RAIL FS485.00 TO FS581.00 AT LBL 9.0. R & R MAIN CABIN FLOOR SEAT RAIL IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000809Seat Track · corrodedCORROSION DAMAGE ON FLOOR SEAT RAIL FS581.00 TO FS677.00 AT LBL 9.0. R & R FLOOR SEAT RAIL IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000808Seat Track · corrodedCORROSION DAMAGE ON FLOOR SEAT RAIL FS 581.00 TO FS 677.00 AT RBL 9.0. R & R RT SIDE FLOOR SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.May 24, 2010 · N748EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201000807Drag Angle · crackedPAX DOOR AFT DRAG ANGLE JUST ABOVE ASSIST MOTOR PULLEY MOUNT BRACKET CRACKED APPROX .5" L. COMPLIED WITH REO 670-52-11-072, STEPS 1 & 2 COMPLIED WITH FILLER IN STEP 5 IS CUT TRIMMED & DRILLED . PERFORMED ET INSP OF CUT LINES ON PAX DOOR AFT DRAG ANGLE IAW REOMay 24, 2010 · N748EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201000806Placard · crackedPAX DOOR INNER HANDLE "EXIT/PULL" SIGN CRACKED THRU BOTH ATTACH FASTENERS. R & R PAX DOOR INNER HANDLE BETA LIGHT IAW AMM 33-51-13-400-801.May 24, 2010 · N748EV · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201000805Placard · deterioratedPAX DOOR LOWER "EXIT" PLACARD DETERIORATED. R & R PAX DOOR LOWER "EXIT" PLACARD IAWAMM 51-22-81-340-802-A01.May 24, 2010 · N748EV · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201000804Lock · out of adjustGALLEY SERVICE DOOR FAILED FUNCTIONAL CHECK. FORCE REQUIRED TO COMPLETE THE UNLATCH CYCLE IS 48 LBF MAXIMUM IAW AMM IS 35 LBF. CLEANED AND LUBRICATED GALLEY SERVICE DOOR LOCKING MECHANISM AND CHECKED ADJUSTMENT IAW AMM 51-41-00-820-801. PERFORMED FUNCTIONAL May 24, 2010 · N748EV · Cndair CL6002C10 · Galley DoorsSDR ASOA201000643Circuit Breaker · trippedSTEERING INOP CAUTION MSG IN FLT. QRH RUN. EMERGENCY DECLARED. RESET CIRCUIT BREAKERS ON GROUND IAW MCC. STEERING INOP EXTINGUISHED. (EMERGENCY DECLARED -- EMERGENCY PERSONNEL WERE STANDING BY) PERFORMED OPS TEST OF NWS IAW AMM 32-51-00. NO DEFECTS NOTED ATApr 26, 2010 · N748EV · Cndair CL6002C10 · Landing Gear Steering SystemSDR ASOA200900989Unknown · smokeFLT 5578-SMOKE AFT LAV, AIR RETURN. EMERGENCY DECLARED-ACFT RETURNED TO DEPARTURE AFTER T/O.Sep 10, 2009 · N748EV · Cndair CL6002C10 · Air Distribution SystemSDR ASOA200900363Light · inoperativeRT EXTERIOR AFT OVERWING EMERGENCY EXIT LIGHT INOP.Mar 30, 2009 · N748EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200801552Megaphone · inoperativeCABIN MEGAPHONE INOP.Nov 23, 2008 · N748EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA200801378Light · missingEMERGENCY FLOOR PATH MARKING MISSING FWD LT STRIP BY GALLEY 3.Oct 21, 2008 · N748EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200800886Drag Angle · crackedRIGHT SIDE VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. REFER TO STEPS 2-9 ON M-234 FORM ATTACHED FOR WORK ACCOMPLISHED DK 7022603. REMOVED RT VERTICAL DRAG ANGLE PAINT IAW CRJ 700 SRM 51-26-00. (S)Jul 5, 2008 · N748EV · Cndair CL6002C10 · Vertical StabilizerSDR TRAX200800885Drag Angle · crackedSUSPECT CRACK ON LT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE. (B) REFER TO STEPS 3-9 ON M-234 FOR WORK ACCOMPLISHED DK 7022603. REFER TO STEP NUMBER THREE ON M-234 FOR WORK ACCOMPLISHED FOR THIS STEP.Jul 5, 2008 · N748EV · Cndair CL6002C10 · Vertical StabilizerSDR TRAX200800884Floorbeam · corrodedMAIN AVIONICS COMPARTMENT UNDER FLOOR CRAWLWAY, FLOORBEAM ANGLE IS CORRODED AT FS 280 STR 27. BLENDED OUT MINOR CORROSION IAW SRM 51-21-06. MATERAL REMOVED .003 IN OUT OF .006 IN MAX ALLOWED IAW SRM 53-22-55. (B)Jul 5, 2008 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR TRAX200800883Angle · corrodedCOCKPIT ENTRANCE PANEL 221ALF AFT ANGLE CORRODED. REMOVED ANGLE IAW SRM 51-42-06. (B)Jul 5, 2008 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200800882Floorbeam · corrodedLT FS 280 FLOORBEAM CORRODED. (B) BLENDED MINOR CORROSION AREAS (3 TOTAL) ON FLOORBEAM IAW REO 670-53-11-046. .004 MATERIAL REMOVED. BLENDED AREAS WITHIN LIMITS. PERFORMED CUTOUT OF DAMAGED AREA FLOORBEAM, AND FABRICATED FILLER PER REO 670-53-11-310. (SJul 5, 2008 · N748EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR TRAX200800881Web · corrodedLT FS280 WEB CORRODED. (B) REMOVED MINOR CORROSION ON LT 280 WEB, LOWER INBD CORNER (1X.8X.004 REMOVED). BLEND IS WITHIN LIMITS PER SRM 53-11-10. (S)Jul 5, 2008 · N748EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200800875Step · crackedASD LOWER STEP CRACKED. REMOVED AND REPLACED ASD LOWER STEP IAW AMM 52-11-04. (S)Jul 4, 2008 · N748EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR TRAX200800588Light · inoperativeRIGHT AFT EXTERIOR EMERGENCY LIGHT INOP.May 1, 2008 · N748EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200800540Light · inoperativeRIGHT AFT EXTERIOR EMERGENCY LIGHT INOP.Apr 15, 2008 · N748EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200800487Door · bindingSERVICE DOOR HARD TO OPEN. FLT 4484 DEL 36 MINS.Apr 5, 2008 · N748EV · Cndair CL6002C10 · Service DoorsSDR TRAX200800237Light · inoperativeRIGHT AFT MOST EXTERNAL EMERGENCY LIGHT INOP.Feb 8, 2008 · N748EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701688Flashlight · inoperativeCAPTAIN`S FLASHLIGHT INOP.Nov 5, 2007 · N748EV · Cndair CL6002C10 · Emergency Equipment
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