N722EV

Service difficulty reports · 314

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 = 'N722EV' 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 SWIA2020072751431Former · corrodedCORROSION FOUND ON PASSENGER DOOR FORMER AT FS311.75 P/N# 601R318031-3. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FWD Jun 17, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020072751430Intercostal · corrodedCORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD2 P/N# 601R318053-3. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 40 % OF LENGTH OF THE PART . OUT OF LIMITS REF CRJ200 SRM AND REO.REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOJun 17, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020072751429Intercostal · corrodedCORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD4 P/N# 601R318081-1. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSJun 17, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020072751428Former · corrodedCORROSION FOUND ON PASSENGER DOOR FORMER FS329.41 BETWEEN DD5 AND DD6 P/N# 601R318078-3. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PAJun 17, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020072751427Intercostal · corrodedCORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD6 P/N# 601R318057-1. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSJun 17, 2020 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020072751426Structure · damaged2EA LH PYLON UPPER LOCK FASTENER HOLES, LOCATIONS 5 AND 7 COUNTING FROM FWD TO AFT, WERE FOUND OVERSIZED AND WITH DEFECTS UPON INCORPORATION OF SB 670BA-54-007 (MARKED) (C-CHECK) RO 7/23/2020 REPAIRED LH PYLON OVERSIZED AND DEFECTIVE HOLES REF. MHIRJ REO.Jun 16, 2020 · N722EV · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA2020072751425Skin · dented* THE RUDDER'S TRAILING EDGE IS DENTED. REPAIRED RUDDER TRAILING EDGE DENT TO REF MHIRJ REO.Jun 16, 2020 · N722EV · Cndair CL6002C10 · Rudder, Plate/SkinSDR SWIA2020072751457Hinge · crackedPASSENGER DOOR AFT HINGE COVER ON FUSELAGE SIDE IS CRACK. REMOVED AND REPLACED WITH NEW PN# 601R31895-12PP, PASSENGER DOOR AFT HINGE COVER FAIRING REF CRJ700 AMM PRESSURE CHECKS GOODJun 15, 2020 · N722EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2020072751423Doubler · chafedAPPROX. F.S 969 LOWER FUSELAGE DOUBLER HAS TWO CHAFES AT STGR 27. PERFORMED DOUBLER REPAIR AT APPROX. F.S 969 STRINGER 27 REF. REO . COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.Jun 15, 2020 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2020072751422Structure · chafed* THE CENTER WING FRONT SPAR'S LOWER ANGLE IS CHAFED ON ITS UPPER SURFACE AT BL0.00. BLENDED CENTER WING FRONT SPAR REF MHIRJ REO. WITHIN LIMITS.Jun 14, 2020 · N722EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2020072751421Skin · gougedRH AILERON UPPER SURFACE LEADING EDGE GOUGED. (C-CHECK) RO 7/23/2020 REMOVED DAMAGE TO R/H AILERON UPPER SURFACE LEADING EDGE, PART IS OUT OF LIMITS PER BOMBARDIER REO. REPLACED R/H AILERON UPPLER SURFACE LEADING EDGE WITH NEW REF CRJ 700 SRM AND BOMBARJun 13, 2020 · N722EV · Cndair CL6002C10 · AileronsSDR SWIA2020072751420Skin · wornLEFT ENGINE UPPER TRANS COWL HAS COWL SLIDER WEAR AND RIDGES WORN. (C-CHECK) RO 7/23/2020 REPAIRED LEFT SIDE ENGINE UPPER TRANS COWL SLIDER REF MHI REO AND REO. . SEE CONTINUATION FOR DETAILS.Jun 13, 2020 · N722EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWIA2020072751419Support Fitting · damagedL/H INBOARD FLAP INBOARD SUPPORT FITTING HAS VISIBLE TOOLING MARK. (C-CHECK) RO 7/23/2020 REMOVED DAMAGE ON THE L/H INBOARD FLAP INBOARD SUPPORT FITTING REF CRJ700 SRM. REPAIRED FITTING REF MHI RJ REO. COMPLETED SKYWEST ST ATTACHED. SEE CONTINUATION FOR DJun 12, 2020 · N722EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2020072751456Web · crackedWEB AT FS939.00 - LOWER/AFT BOTTOM CORNER IS CRACKED. AFT FAIRING ATTACHMENT. CRACK IS VERIFIED TO BE ON WEB AT FS909.00 LOWER/AFT BOTTOM CORNER. COMPLIED WITH ALL STEPS (1-13) IN THE BOMBARDIER REO SEE CONTINUE CARD FOR DETAILSJun 11, 2020 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020072751455Attach Bracket · cracked* AFT CARGO DOOR, AFT TRACK LOWER ATTACH BRACKET IS CRACKED. MARKED. INSTALLED NEW BRACKET ASSY COMMON TO LINTEL PN MM670-35699-029. REF CRJ700 SRM.Jun 11, 2020 · N722EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2020072751418Slat Track · wornR/H SIDE LEADING EDGE SLAT DRIVEN TRACK 1-1 HAS WEAR MARKS ON OUTER SECTION OF TRACK.(MARKED) (C-CHECK) RO 7/23/2020 REPAIRED RH SIDE LEADING EDGE SLAT DRIVE TRACK 1-1 PER MHIRJ REO. ALL CHECKS AND RIGS ARE GOOD AT THIS TIME.Jun 11, 2020 · N722EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2020072751417Skin · scratched* R/H SIDE EXTERNAL FUSELAGE ARE VARIOUS SMALL SCRATCHES JUST AFT AND BELOW A/C SERVICE CONNECTION FS 1031.0 (C-CHECK) RO 7/23/2020 BLENDED VARIOUS SCRATCHES ON RH SIDE EXTERNAL FUSELAGE SKIN JUST AFT AND BELOW A/C CONNECTION AT FS 1031.0. REF CRJ 700 SRMJun 11, 2020 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2020072751416Skin · dentedDENT ON FUSELAGE SKIN FWD OF FS 265.00 BETWEEN STGR 24R - 25R (C-CHECK) RO 7/23/2020 REPAIRED FUSELAGE SKIN DENT FWD OF F.S 265 BETWEEN STGR 24R - 25R REF. MHIRJ REO. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.Jun 10, 2020 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2020072751415Bearing · damagedROUTE LT AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON LH AILERON PER AMM (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS REF,CRJ 700 AMM FOR BEARINGS AND REO FOR BUSHJun 9, 2020 · N722EV · Cndair CL6002C10 · AileronsSDR SWIA2020072751414Skin · dentedRH SIDE FUSELAGE BETWEEN FS 985 AND FS1000 IN BETWEEN STGR12 AND 13 HAS A SCRATCH/GOUGE MEASURING 6 IN X 1.3 IN AND A MAX DEPTH OF .007 IN. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-61-1475 REV A. PERMANENT REPAIR DUE WITHIN 6700 FH FROM ORIGINAL ISSUE OF Jun 2, 2020 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA201945690Control Panel · failedEXPERIENCED FULL LEFT RUDDER DEFLECTION DURING DESCENT. RUDDER TRIM FOUND TO BE ALMOST FULL NL POSITION. RESET RUDDER TRIM TO CENTER AND LANDED WITH NO FURTHER ISSUES. (FLT#3290) CLOSED REMOVED AND REPLACED RUDDER TRIM/AILERON TRIM PANEL. PERFORMED OP CHECK OFApr 1, 2019 · N722EV · Cndair CL6002C10 · Rudder Tab Control SystemSDR SWIA2018070944874Vane · chafedRT INBOARD FLAP VANE MIDDLE LEADING EDGE PANEL HAS CHAFE DAMAGE. (C-CHECK) 07/08/2018 REPAIRED RT INBOARD FLAP VANE, MIDDLE LEADING EDGE CAP IAW REO.Jun 16, 2018 · N722EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2018070944873Vane · chafedLT INBOARD FLAP VANE MIDDLE LEADING EDGE PANEL HAS CHAFE DAMAGE. (C-CHECK) 07/08/2018 REPAIRED LT INBOARD FLAP VANE, MIDDLE LEADING EDGE IAW REO.Jun 16, 2018 · N722EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2018070944872Not Reported · dentedTHERE IS A DENT ABOVE FWD POT WATER DOOR CUTOUT. (C-CHECK) 07/08/2018 REPAIRED DENT ABOVE FWD POT WATER DOOR CUTOUT IAW REO.Jun 14, 2018 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018070944871Not Reported · dentedTHERE IS A DENT BELOW THE PAX DOOR CUTOUT. (C-CHECK) 07/08/2018 REPAIRED DENT BELOW THE PAX DOOR CUTOUT IAW REO.Jun 14, 2018 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201801025017Connector · not seatedPILOT REPORTED THAT DURING ARROACH AT 4000FT, RECEIVED A SMOKE MASTER WARNING FOR THE AFT LAVATORY. STAYED ON EVEN AFTER LANDING, COMPLIED WITH QRH. RESET THE CONNECTOR AND PERFORMED AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 2, 2018 · N722EV · Cndair CL6002C10 · Fire Protection System WiringSDR ASOA201708281881Bulkhead · corrodedINSIDE AVIONICS BAY BULKHEAD AT FS 235.00 HAS (1) EA FASTENER CORRODED AND POSSIBLE STRUCTURE AROUND FASTENER CORRODED AT RBL3, APPOX 6"HIGH FROM LOWER SKIN. COMPLIED WITH EC/TC REO 670-53-11-1307 AND REO 670-53-11-1307.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201708281880Floor Support · corrodedCRAWLWAY FLOOR SUPPORT ANGLE CORRODED AT FS 280.00. REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT FS 280.00 PER SRM 51-40-11-001-001-A01. P/N-CC670-35256-3 DRAWING CC670-3525.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201708281879Floor Support · corrodedCRAWLWAY FLOOR SUPPORT ANGLE CORRODED AT FS 280.00. REMOVED AND REPLACED FLOOR SUPPORT ANGLE FS 280.00 PER SRM 51-40-11-001-001-A01. P/N-CC670-35256-3 DRAWING CC670-35256.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201708281876Stringer Splice · corrodedSTRINGER SPLICE 25R CORRODED BS 328 - 338. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-32429.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201708281875Stringer · corrodedSTRINGER 26R CORRODED AT BS 363. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201708281871Frame · corrodedFRAME 310 CORRODED FWD SIDE BTW STGRS 25L-25R. REPAIRED FRAME AT 310 FWD SIDE BTW STGRS 25L-25R IAW EC/TC REO 670-53-21-799 01 AND REO 670-53-21-799 01.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201708281866Stringer · corrodedSTG 26L CORRODED 363.00. REMOVED AND REPLACED CORRODED STG 26L BTW FRAMES 363.00 IAW SRM 51-42-06-001-001-A01. ALL DEFECTS CORRECTED. P/N-SH670-31372-3 DRAWING SH670-31372-3.Aug 28, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201708271874Frame · corrodedFRAME BS 333 CORRODED FWD & AFT SIDES BETWEEN STRINGERS 24R - 25L. COMPLIED WITH EC/TC REO 670-53-21-799-03, AND REO 670-53-21-799-03.Aug 27, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201708271873Frame · corrodedFRAME BS 295 CORRODED FWD & AFT SIDES BETWEEN STRINGERS 24R - 25L. COMPLIED WITH EC/TC REO 670-53-21-799, AND REO 670-53-21-799 .Aug 27, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201708271872Frame · corrodedFRAME 364 CORRODED FWD & AFT SIDES BTW STGRS 25R-25L. COMPLIED WITH EC/TC REO 670-53-21-687 AND REO 670-53-21-687.Aug 27, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201708271865Stringer Splice · corrodedSTR 26R SPLICE JOINT SEGMENT CORRODED BTW FS 328-338. REMOVED AND REPLACED STR SPLICE SEGMENT PER SRM 51-42-06-001-001-A01 AND 51-25-00-001-001 A01 P/N-SH670-32429-4 DRAWING SH670-32429Aug 27, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201708261877Handle · chafedSERVICE DOOR OUTER HANDLE HOUSING CHAFED AT THE FWD UPPER CORNER. REMOVED AND REPLACED HANDLE ASSEMBLY IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, DRAWINGS CC670-38171, AND CC670-38255.Aug 26, 2017 · N722EV · Cndair CL6002C10 · Service DoorsSDR ASOA201708251878Intercostal · corrodedPAX DOOR ICE BREAKER DOOR CUTOUT INTERCOSTALS CORRODED. REPAIRED THE INTERCOSTALS IAW EC/TC EA 43-2017-128 &129, AND EA 43-2017-128-29,Aug 25, 2017 · N722EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201708231864Wire · meltedLEFT ENGINE IDG SHRINK WRAP MELTED. REPAIRED THE LT IDG CABLE IAW EC/TC REO 670-24-21-001 AND REO 670-24-21-001.Aug 23, 2017 · N722EV · Cndair CL6002C10 · Electrical Power System WiringSDR ASOA201708211857Frame · corrodedFRAME BS 319.7 CORRODED FWD SIDE BETWEEN STINGERS 25L-25R. REPAIRED THE FRAME IAW EC/TC REO 670-53-21-799-02, AND REO 670-53-21-799-02.Aug 21, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201708201858Skin · corrodedMAIN AVIONICS DOOR SURROUND HAS CORRISION.. REMOVED AND REPLACED IAW MODSUM IS67053210097, EC/TC REO 670-53-21-242, AND REO 670-53-21-242.Aug 20, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201708191860Floor Support · corrodedCORRODED FLOOR SUPPORT BETWEEN BS 349 - 364, RBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.Aug 19, 2017 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201708191859Floor Support · corrodedCORRODED FLOOR SUPPORT BETWEEN BS 349 - 364, LBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01Aug 19, 2017 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201708161852Frame · corrodedFRAME 349 FWD & AFT SIDES CORRODED BTW STR 24R-25L. REMOVED AND REPLACED FRAME 349.00 IAW SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01 AND DRAWING SH670-31357.Aug 16, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201708161851Door Sill · corrodedRT CABIN FLOOR SILL CORRODED AT FS 282.00 RBL 42. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390.Aug 16, 2017 · N722EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201708151849Stringer · corrodedSTRINGER 27, BS 280 - 300 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, AND DRAWING SH670-31642.Aug 15, 2017 · N722EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201708151848Seat Track · corrodedLEFT SIDE SEAT TRACK CORRODED AT BS 581 AND 613. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.Aug 15, 2017 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708151847Seat Track · corrodedLEFT SIDE SEAT TRACK BS 785.15 - 853 CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, ECTC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801-A17.Aug 15, 2017 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708151846Seat Track · corrodedRIGHT SIDE SEAT TRACK WAS CORRODED AT BS 736.05. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, ECTC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801-A17.Aug 15, 2017 · N722EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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