N506AE

Service difficulty reports · 179

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 = 'N506AE' 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 VNAA20260726417Seat Track · corrodedRIGHT SIDE WALL SEAT TRACK IS CORRODED BETWEEN BS 785.15 TO 863. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801(CONFIGA02).Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726416Seat Track · corrodedRBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 581 TO 677. REMOVED DAMAGED SEAT TRACK SEGMENT IAW AMM 53-00-49-000-801(CONFIGA02). INSTALLED A NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801(CONFIGA02).Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726415Stringer · corrodedSTRINGER 21L IS CORRODED BETWEEN BS 485 TO 501. REPAIRED STRINGER 21L IAW REO 670-53-31-1206, REV --,Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260726414Stringer · corrodedSTRINGER 21R CORRODED BETWEEN BS 469 TO 517. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03-201-001-A01, SOLUTION II, FIGURE 53-00-03-991-804.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260726413Seat Track · corrodedLBL 9 SEAT TRACK CORRODED BETWEEN BS 581 TO 677. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026072412Seat Track · corrodedRBL 9 SEAT TRACK WAS CORRODED AND GOUGED AT BS 849, 862, 923, AND 953. REMOVED DAMAGED SEAT TRACK FOR RBL 9 BTWN BS 8490 AND BS. 953 FOR REPLACMENT IAW AMM 53-00-49-000-801 CONFIGA02. INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK IAW AMM 53-00-49-400-801,CONFIGJul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026072411Seat Track · corrodedLEFT FLOOR SEAT TRACK, LBL 9 HAS CORROSION AND GOUGES AT BS 863, 893, 906, 923, AND 953. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02 AND AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026072410Intercostal · chafedPASSENGER DOOR INTERCOSTAL DD7A IS CORRODED. NEW SERVICEABLE PAX DOOR INTERCOSTAL DD7A HAS BEEN LOCATED AND DRILLED IAW SRM 51-40-11-001-001-A01. INSTALLED PAX DOOR INTERCOSTAL DD7A IAW SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026072409Striker · chafedPASSENGER DOOR SURROUND STRUCTURE LOWER SEAL STRIKER HAS CHAFING DAMAGE AT SEVERAL SPOTS BETWEEN BS 310 - 349. REMOVED THE DOOR LOWER SEAL STRIKER IAW SRM 51-42-21-001-001-A01. LOCATED AND DRILL NEW SERVICEABLE DOOR LOWER SEAL STRIKER IAW SRM 51-40-11-001-00Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026072407Angle · corrodedPASSENGER DOOR LOWER SILL MID CAP ANGLE HAS CORROSION AROUND SEVERAL FASTENER HOLES. REMOVED PASSENGER DOOR LOWER SILL MID CAP ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE LOWER SILL MID CAP ANGLE PN: SH670-31825-9 IJul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026072406Skin · gougedFUSELAGE EXTERNAL SKIN IS GOUGED UNDER THE TOP AFT VHF (NR 3) ANTENNA. COMPLIED WITH REPAIR OF FUSELAGE EXTERNAL SKIN IS GOUGE UNDER THE TOP AFT VHF (NR 3) ANTENNA IAW REO 670-53-31-1185, REV--.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20260726404Stringer · corrodedSTRINGER 21R IS CORRODED BETWEEN BS 295 TO 310. REMOVED AND REPLACED STRINGER 21R IAW SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2026072403Floorbeam · crackedWHILE ACCESSING LT BS 280 FLOORBEAM FOUND CRACKED AT LOWER CORNER. REPAIRED THE LT COCKPIT FLOORBEAM IAW REO 670-53-11-896 REV-.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20260726402Channel · damagedFOUND RIVET HOLES ON LT COCKPIT POST UPPER CHANNEL TO BE DAMAGED. REPAIRED LT COCKPIT POST UPPER CHANNEL IAW REO 670-53-11-2301, REV-,Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2026072401Floorbeam · crackedWHILE ACCESSING RT, BS 280 CROSSBEAM FOUND CO-PILOTS SIDE RT COCKPIT FLOORBEAM TO BE CRACKED AT LOWER CORNER. PERFORMED REPAIR TO RT FLIGHT DECK FLOORBEAM AT BL12 IAW REO 670-11-896, REV-.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2025042511101Skin · ground damageBAG CART HIT SIDE OF PLANE BETWEEN FS549 AND FS565 AND STGR16L AND STGR17L. DENT/GOUGE 2.5" LONG BY 1 5/8" WIDE .187" DEEP. / PERMANENT REPAIR COMPLETED IAW REO 670-53-31-1024.Apr 23, 2025 · N506AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20231130012Plate · corrodedHN 122920 DISCREPANCY: AFT KEEL BEAM LOWER PLATE REQUIRES REPAIR DUE TO EXTENSIVE CORROSION. CORRECTIVE ACTION: REPAIRED AFT KEEL BEAM LOWER CLOSING PLATE (P/N: SH670-37291-1) IAW MHIRJ REO 670-53-41-644 REV—DATED 2023-11-16 AND MHIRJ REO 670-53-41-646 REV—DATNov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231130011Strap · corrodedHN 118212 DISCREPANCY: BELLY FAIRING STRAPS & ANGLE @ FS 879 FROM STRINGER 24L TO 24R CORRODED. CORRECTIVE ACTION: REMOVED CORRODED STRAPS AND INSTALLED NEW STRAPS IAW CRJ 700 SRM 51-42-06-001-001-A01.Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231130010Doubler · corrodedHN 118176 DISCREPANCY: LOWER WIFI ANTENNA INTERNAL DOUBLER FOUND TO BE CORRODED BETWEEN FS1000 - FS1015. CORRECTIVE ACTION: REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER P/N 601-2365-01-400-17 IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06-00Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20231130009Drain · corrodedHN 117589 DISCREPANCY FOUND AFT LAV LOWER DRAIN ASSEMBLY TO BE HEAVILY CORRODED. CORRECTIVE ACTION: REPLACED AFT LAV DRAIN VALVE P/N: BA670-43202-3 IAW CRJ700 AMM 38-31-20-400-801 (CONFIG A01)Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA20231130008Stringer · corrodedHN 117362 DISCREPANCY: FOUND CORROSION ON STRINGER 25R BETWEEN FS 847 AND FS 863. CORRECTIVE ACTION: REMOVED CORRODED SECTION OF STRINGER AND SPLICED IN A NEW SECTION IAW CRJ 700 SRM 53-00-03-201-001-A01Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20231130007Bolt · corrodedHN00115399 DISCREPANCY: DESCRIPTION: FLAP PDU REQUIRES REMOVAL FOR ACCESS FOR STRUCTURE REPAIRS. CORRECTIVE ACTION: FLAP PDU ATTACHING HARDWARE FOUND TO BE CORRODED AND REQUIRES REPLACEMENT. NEW SERVICEABLE HARDWARE INSTALLED IAW CRJ 700 AMM 27-52-37-400-801-ANov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20231130006Support Bracket · corrodedHN00115398 DISCREPANCY: FS 847 LOWER FAIRING SUPPORT BRACKET BETWEEN LBL AND RBL 18 IS CORRODED. CORRECTIVE ACTION: FOUND THE FS 847 LOWER FAIRING SUPPORT BRACKET TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-82-55-101-002-A01. LOCATED, DRILLED AND INSTALLED LOWER FANov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20231130005Frame · corrodedHN 115322 DISCREPANCY: CORROSION FOUND UNDER CARGO COMPARTMENT FLOOR ON LOWER SKIN FRAME AT FS1000.00 FWD OF WIFI ANTENNA. CORRECTIVE ACTION: REPAIRED FS1000 FRAME (P/N MM670-36112-003) BETWEEN STGR27 AND STGR25R IAW OLIVER WYMAN EA 23-C7-53-1453 REV IR DATEDNov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20231130004Keelbeam · corrodedHN 115321 DISCREPANCY: FOUND CORROSION ON AFT KEEL BEAM AT FS847 INSIDE LH WHEEL BIN AREA. CORRECTIVE ACTION: REPAIRED AFT RH KEEL BEAM PN SH670-37282-2 BTWN FS797.31 AND FS923 IAW MHIRJ REO 670-53-41-645 REV—DATED 2023-11-10Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, KeelSDR VNAA20231130003Keelbeam · corrodedHN 115321 DISCREPANCY: FOUND CORROSION ON AFT KEEL BEAM AT FS847 INSIDE LH WHEEL BIN AREA. CORRECTIVE ACTION: REPAIRED AFT LH KEEL BEAM PN SH670-37282-1 BTWN FS797.31 AND FS923 IAW MHIRJ REO 670-53-41-645 REV—DATED 2023-11-10Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, KeelSDR VNAA20231130002Stringer · corrodedHN 117591 DISCREPANCY: STRINGER 23R BETWEEN FS953 - FS969 FOUND TO BE CORRODED. CORRECTIVE ACTION: UPON FURTHER INVESTIGATION, FOUND STGR23R BETWEEN FS953 - FS969 TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED . REPAIRED STRINGER 23R BETWEEN FS953 - FS969 IAW CRNov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20231130001Strap · corroded"C.O. PSA384D HN 118212 DISCREPANCY: BELLY FAIRING STRAPS & ANGLE @ FS 879 FROM STRINGER 24L TO 24R CORRODED. CORRECTIVE ACTION: REMOVED CORRODED STRAPS AND INSTALLED NEW STRAPS"Nov 30, 2023 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202210241111Acm · odorR PACK AUTOFAIL CAUTION MSG RECIEVED AFTER LANDING, FA REPORTED A LIGHT HAZE AND RUBBER SMELL IN THE CABIN. REMOVED AND INSTALLED RH AIR CYCLE MACHINE IAW CRJ 700 AMM 21-51-08-400-801-A01. OPS CHECK GOOD. LEAK CHECK GOOD.Oct 20, 2022 · N506AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA202108069994Frame · corrodedAVIONICS BAY FRAME AT FS 319.70 CORRODED AT STR 26 L TO STR 26 R.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2021080699916Stringer Clip · corrodedAFT CARGO BAY UNDERFLOOR AT FS 1031 STR 23L ANGLE CLIP IS CORRODED.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2021080699915Hinge · corrodedPAX DOOR HINGE (FUSELAGE SIDE) HAS MULTIPLE CHAFED LUG LANDINGS.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA2021080699914Seat Track · corrodedALL SIDE SEAT RAILS FROM FS 379.00 TO FS 669.40 HAVE CORROSION ON LH SIDE.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2021080699913Seat Track · corrodedALL SIDE SEAT RAILS FROM FS 669.40 TO FS 977.00 HAVE CORROSION ON RH SIDE.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2021080699912Seat Track · corrodedALL SIDE SEAT RAILS FROM FS 669.40 TO FS 977.00 HAVE CORROSION ON LH SIDE.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2021080699911Cleat · corrodedPAX DOOR CLEAT CORRODED AT DD6 AND FRAME FS 320.00Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2021080699910Cleat · corrodedPAX DOOR CLEAT CORRODED BETWEEN DD4 AND DD5 AT FRAME FS 320.00Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202108069999Angle · corrodedFWD CARGO BAY ANGLE AT STR 26L BETWEEN FS 581.00 AND 597.00 FASTENERS GOING THROUGH EXTERNAL SKIN CORRODED.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202108069998Door Sill · corrodedAFT CARGO BAY DOOR SILL CORRODED AT FS 1008.00 TO FS 1020.00Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202108069997Floor Support · corrodedAFT CARGO AREA FLOOR BEAM AT LBL 9 CORRODED AT FS 1051.30 TO FS 1069.75.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202108069996Floor Support · corrodedAFT CARGO AREA FLOOR BEAM AT LBL 27 CORRODED AT FS 1000.00 TO FS 1040.00.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202108069995Intercostal · corrodedAVIONICS BAY INTERCOSTALS AT FS 364.00 STR27 LEFT AND RIGHT ARE CORRODEDAug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202108069993Frame · corrodedMAIN AVIONICS BAY FS 295.00 FRAME CORRODED AT STR 27 TO STR 26R.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202108069992Stringer · corrodedAVIONICS BAY FRAME 297.00 STRINGER 25R HAS LIGHT SURFACE CORROSION.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202108069991Buttstrap · corrodedFS 280 CIRCUMFERENTIAL SPLICE HAS CORROSION AT STR L26 AND STR R25.Aug 6, 2021 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020012321102Circuit Breaker · smokeAFTER PARKING AT THE GATE EXTENAL POWER WAS ATTACHED & AVAILABLE. SELECTED EXTERNAL POWER AND TURNED OFF THE APU. THE AIRCRAFT TOOK EXTERNAL POWER FOR AROUND 5 SECONDS & THEN STARTED FLICKERING. EXTERNAL POWER SWITCH WAS DESELECTED AND THE FLICKERING CONTINJan 22, 2020 · N506AE · Cndair CL6002C10 · Electrical Power SystemSDR VNAA201908021103Handle · unsecureDURING CLIMB THE FA ALERTED THE CREW THAT THE PASSENGER DOOR HANDLE WOULD NOT STAY LOCKED. PASSENGER DOOR WARNING LIGHT ILLUMINATED MULTIPLE TIMES IN FLIGHT. THE CREW RETURNED THE AIRCRAFT TO CLT. THE FLIGHT LANDED WITHOUT INCIDENT AND IS CURRENTLY IN MAINTENAug 1, 2019 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2019072911101Door · out of rigEMERGENCY LANDING / COCKPIT CREW BASE: CLT CABIN CREW BASE: CLT AT 10,000 FEET THE CREW RECEIVED A PASSENGER DOOR WARNING MESSAGE. THEY FOLLOWED THE QRH AND DECLARED FOR PRIORITY HANDLING. PAX DID NOT BRACE. THE AIRCRAFT DID NOT LOSE PRESSURIZATION. MAJul 29, 2019 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2019051111101Battery · dischargedEMER LIGHTS INOP DURING TEST. FERRIED AIRCRAFT TO CLT. REMOVED AND REPLACE ALL EMERGENCY POWER SUPPLY BATTERIES.May 11, 2019 · N506AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2018121611101Sensor · defectiveTHE CREW RECEIVED A BRAKE OVERHEAT CAUTION MESSAGE AT FL290 AND DIVERTED DECLARING AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED #1 BRAKE TEMP SENSOR. OPS CHECK GOOD.Dec 16, 2018 · N506AE · Cndair CL6002C10 · Landing Gear Brake System
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