N534AE

Service difficulty reports · 81

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 = 'N534AE' 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 VNAA202603130001Structure · elongatedLH PRESSURE BOX AT FS 847 HAS MULTIPLE ELONGATED HOLES COMMON TO LBL 18 FLOOR BEAM SH670-35834-3 PRESSURE BOXMar 13, 2026 · N534AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2025041511102Skin · dentedLH SIDE FWD FUSELAGE DENT (REO) 670-53-11-2108 / C/W REO 670-53-11-2108 REPAIR FOR DENT DAMAGE TO UPPER FUSELAGE SKIN PANEL BETWEEN FS 220.00 - FS250.00 AND STR12L - STR15LApr 13, 2025 · N534AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2025041511101Skin · damaged(RH) NOSE SKIN DAMAGED AFT OF TRU ACCESS PANEL / C/W REO 670-53-11-815 REPAIR TO UPPER SECTOR FS193.00.Apr 13, 2025 · N534AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20231014025Frame · chafedFRAME @ F.S 319 STR 25 R HAS CORROSION. REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20231014029Skin · chafedR/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1291 REV IR DATED 09/19/2023.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA20231014028Skin · chafedR/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, MIDDLE HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1290 REV IR DATED 09/19/2023.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA20231014027Skin · chafedR/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, INBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1245 REV IR DATED 09/19/2023.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA20231014026Stringer Splice · corrodedCORROSION FOUND ON STR 25R @ MULTIPLE LOCATIONS FROM F.S 280 THRU F.S 333. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20231014023Skin · chafedL/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF OUTBOARD FLAP, MID HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1297 REV IR DATED 09/20/2023.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA20231014022Skin · chafed/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF INBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1251 REV IR DATED 09/20/2023.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA20231014024Skin · chafedL/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF OUTBOARD FLAP, MID HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX. REPAIRED IAW OLIVER WYMAN EA 23-C7-57-1297 REV IR DATED 09/20/2023.Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA20231014013Seat Track · corrodedREMOVED AND REPLACED IAW CRJ 700 AMM 53-00-49-000/400-801-A01 AND CRJ 700 SRM 51-40-11-001-001-A01.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231014020Angle · corrodedPAX DOOR SILL ANGLE IS CORRODED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231014015Stiffener · crackedFWD PAX DOOR WEB STIFFENER IS CRACKED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20231014012Seat Track · corroded.LH #2 SEAT TRACK IS CORRODED AT LBL 9Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231014011Former · corrodedREMOVED AND REPLACED IAW CRJ700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA20231014021Cleat · corrodedPAX DOOR CLIPS THAT ATTACH TO THE FWD AND AFT ENDS OF "ANGLE C" LOCATED ON INNER PORTION OF OUTER HANDLE BOX BELOW HINGE ARE CORRODED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20231014010Angle · corrodedGALLEY SERVICE DOOR SILL ANGLE IS CORRODED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231014009Intercostal · corrodedSTRINGER 27 RH INTERCOSTAL IS CORRODED BETWEEN FS 349.00 AND 364.00.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231014008Intercostal · corrodedSTRINGER 20R INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND 349.00.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231014007Skin · crackedFOUND CRACK ON PAX DOOR INNER SKIN AT PANEL CUTOUT.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20231014030Joint · chafedFS 280.00 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STRINGER 27 AND 26R.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20231014005Frame · corrodedF.S. 310.00 FRAME IS CORRODED BETWEEN STRINGER 26L AND STRINGER 26R.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20231014004Stringer · corrodedSTRINGER 26R AT F.S. 300.00 HAS CORROSION AROUND FASTENER HOLE.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20231014003Stringer Splice · corrodedSTRINGER 26R SPLICE AT F.S. 333.00 IS CORRODEDOct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20231014017Floor Support · corrodedRH FLOOR SILL IS CORRODED BETWEEN FS 280.00 AND 319.70.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231014016Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODED BEYOND REPAIRABLE LIMITSOct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231014018Coaming · chafedRH UPPER TRANSCOWL FWD HOOK LATCH (INNER DOUBLER) IS CHAFED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR VNAA20231014002Strap · corroded670-57-21-867_REV-A (PERM REPAIR-LOWER SKIN ASSY AND INSTL WINGBOX) REPAIR IAW REO-670-57-21-867 WITHIN 8000 FH OR NEXT "C" CHECK.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Wing Miscellaneous StructureSDR VNAA20231014001Skin · damagedLH I/B FLAP PANEL 584KB & UNDERLYING STRUCTURE HAS 1EA ELONGATED HOLE.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20231014006Stiffener · crackedFWD PAX DOOR WEB STIFFENER IS CRACKED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20231014014Seat Track · corrodedLH #5 SEAT TRACK IS CORRODED AT LBL 9.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231014019Angle · corrodedPAX DOOR LOWER SILL MID CAP ANGLE IS CORRODED.Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202301201111Selector Valve · faultedONCE IN GEAR UP POSITION GOT GEAR DISAGREE WITH IND. THREE GREEN WHILE HANDLE IN UP POSITION. ALSO GOT NWS INOP CAUT MSG. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801-A01 OPS CHECK GOOD, GEAR SWING GOOD.Jan 17, 2023 · N534AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2020031311102Warning System · false activationSLATS FAIL CAUTION WHEN DEPLOYING FLAPS FOR LANDING. FLAPS 45 SLATS 0. PERFORMED SELF TEST OF SFECU IAW CRJ 700 AMM 27-51-05-740-801. TEST PASSED. PERFORMED OPS TEST OF FLAPS / SLATS SYSTEM IAW 27-50-00-710-801. OPS TEST GOOD.Mar 9, 2020 · N534AE · Cndair CL6002C10 · Leading Edge Slat Position Indicating SystemSDR VNAA2020022061103Slat System · malfunctioned20 MIN OUT OF DCA THE CREW RECEIVED A SLAT FAIL MSG. THEY DIVERTED TO IAD FOR THE RW LENGTH. AC LANDED, AND TAXIED TO THE GATE SAFE. CLEARED SFECU INHIBITS IAW CRJ 700 AMM. PERFOMED SELF TEST OF SFECU AND OPS TEST OF SLATS AND FLAPS SYSTEM IAW CRJ 700 AMM. TESFeb 16, 2020 · N534AE · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR VNAA2019082199907Seat Track · corrodedLBL 9 SEAT RAIL, 3RD FROM FRONT, STARTING AT APPROX FS581.00 GOUGED/CORRODED IN MULTIPLE LOCATIONS. FABRICATED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK AMM 53-00-49-400-801-A03 SEAT TRACK LBL 9 FROM FS 581-FS 677 SRM 53-00-49-201-002-A01.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019082199906Seat Track · corrodedRBL 9 SEAT RAIL, 3RD FROM FRONT, STARTING AT APPROX FS581.00 CORRODED. FABRICATED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK AMM 53-00-49-400-801-A03 SEAT TRACK RBL 9 FROM FS 581-FS 677 SRM 53-00-49-201-002-A01.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019082199905Floor Support · corrodedAFT CARGO DOOR FLOOR SILL ANGLE IS CORRODED BETWEEN FS 1000 AND FS 1047.00. REPAIRED AFT CARGO DOOR FLOOR SILL ANGLE BETWEEN FS 1000 TO FS 1047 IAW BOMBARDIER REO #670-53-61-913 REV A DATE 2012-11-02.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019082199904Frame · corrodedFS 349 FRAME IS CORRODED ON AFT SIDE BETWEEN STR27 & 26R. REPAIRED FS 349 AFT SIDE BETWEEN STR 27 AND 26R IAW REO 670-53-21-1308.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA2019082199903Frame · corrodedFS333 FRAME IS CORRODED ON AFT SIDE BETWEEN STR 27 & 26R. REPAIRED FS 333 ON AFT SIDE BETWEEN STR 27 AND STR 26L AND STR 27 AND STR 26L IAW REO 670-53-21-1308.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA2019082199902Stringer · crackedAFT OF FS280 AT STR 3L, LINTEL IS CRACKED APPROX 1" LONG. REPAIRED PAX DOOR LINTEL (STR 3LZ) IAW REO 670-53-21-493 REV D DATE 2015-07-10 AND SB#670BA-53-040 PART B.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA2019082199901Drag Angle · crackedLEFT AFT FUSELAGE AFT DRAG ANGLE CRACKED. INSTALLED NEW L/H AFT FUSELAGE AFT DRAG ANGLE IAW CRJ700 SRM 51-42-10-001-001-A01, 51-42-21-001-A01.Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019062861102Shutoff Valve · failedDURING CRUISE AT 35,800 FEET THE CREW RECEIVED A BLEED DUCT WARNING MESSAGE. THE OXYGEN MASKS DEPLOYED AND THE CREW FOLLOWED THE INSTRUCTIONS OF THE QRH AND LANDED AT THE NEAREST SUITABLE AIRPORT USING A DESCENT RATE OF 4200-4500 FPM. THE FLIGHT LANDED WITHOUJun 26, 2019 · N534AE · Cndair CL6002C10 · Pneumatic Indicating SystemSDR VNAA2019061761102Controller · failedR BLEED DUCT (W/C) AND L BLEED DUCT (W/C) ALONG WITH RH/LH COWL A/I CAUTIONS. AS A RESULT BLEED VALVES CLOSED AND CABIN PRESSURE WAS LOST AIRCRAFT DIVERTED TO PITTSBURGH. GROUND RAN AIRCRAFT AND C/W LEAK CHECKS OF BLEED DUCTS AND A/C UNITS, NO LEAKS FOUND. FERJun 16, 2019 · N534AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2018010211101Smoke Detector · false activationTHE CREW REPORTED AN AFT LAVATORY WARNING MESSAGE. THERE WAS NO PHYSICAL SMOKE OR ODOR OF SMOKE. THE SMOKE DETECTOR ALARM WILL NOT TURN OFF. MX R & R THE LAVATORY SMOKE DETECTOR. OPS CHECKED GOOD.Jan 2, 2018 · N534AE · Cndair CL6002C10 · Smoke DetectionSDR VNAA2017101711101Bpsu · warning messageCREW RECEIVED FLAPS FAIL MESSAGE ON RETRACTION. RAN CHECKLIST AND DECLARED EMERGENCY. R & R THE LT BPSU, OPS CHECKED GOOD.Oct 17, 2017 · N534AE · Cndair CL6002C10 · Trailing Flap Position Indicating SystemSDR VNAA2017070411103Fadec · failedFLIGHT DIVERTED DUE TO AN AMBER LEFT FADEC CAUTION MESSAGE. WAS ABLE TO TAXI TO A GATE. MX REPLACED THE FADEC.Jul 4, 2017 · N534AE · Cndair CL6002C10 · Fuel Controlling SystemSDR VNAA2017070399904Doubler · crackedPAX DOOR PULL IN CAM DOUBLER CRACKED. REPLACED THE DOUBLER.Jul 2, 2017 · N534AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170510001Stiffener · crackedFUSELAGE BULKHEAD AT BS 202.75 STIFFENER AT RBL 30 LOWER END FOUND BENT AND CRACKED. REPAIRED IAW ERS-CR-53MR-2412.May 10, 2017 · N534AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
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