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 VNAA2026072467Web · corrodedRIGHT BS 280 LOWER WEB FOUND TO BE CORRODED, REQUIRES REPLACEMENT. REPLACED RT BS 280 LOWER WEB IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, & 53-11-10-201-004-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2026072466Web · corrodedLEFT BS 280 LOWER WEB FOUND TO BE CORRODED REQUIRES REPLACEMENT. REPLACED LT BS 280 LOWER WEB CC670-34170 IAW SRM 51-42-06-001-001-A01, & 51-42-13-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260726465Pulley Bracket · damagedWHILE ACCESSING BS 280 RT CROSSBEAM AND WEB IT WAS FOUND THAT PULLEY BRACKET WAS EXCESSIVELY OVERSIZED FASTENER HOLES. R & R REQUIRED. LOCATED & DRILLED NEW SERVICEABLE PULLEY BRACKET IAW SRM 51-40-11-001-001-A01. REPLACED THE PULLEY BRACKET AT RT BS 280 CROJul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260726464Frame · corrodedFWD SIDE OF FRAME BS 319 CORRODED BETWEEN STR 24L-25L. REPLACED FRAME SECTION IAW SRM 53-00-06-201-006-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260726463Frame · corrodedFWD SIDE OF FRAME BS 319 CORRODED BETWEEN STR 24L-25L. REPLACED FRAME SECTION IAW SRM 53-00-06-201-006-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260726462Stringer Splice · corrodedSTRINGER 21R CORRODED BETWEEN BS 295 TO 310. INSTALLED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2026072461Attach Fitting · corrodedPAX DOOR FWD AND AFT HANDRAIL FITTING ARE CORRODED ON THE FUSELAGE SIDE. REPLACED PAX DOOR FWD AND AFT HANDRAIL FITTINGS IAW SRM 51-42-21-001-001-A01. REF TASK CARD FOR WORK PEFORMED.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20260726460Angle · crackedWHILE APPLYING PAINT TOUCH UP TO BACKSIDE OF FS.280 BULKHEAD REPAIR IT WAS NOTED THAT ITEM 81A BULKHEAD ANGLE FS.280 , BL 26.00 CRACKED UPON INSTALLATION AND REQUIRES REPLACEMENT. REPLACED ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260726459Seat Track · corrodedSEAT TRACK AT LBL 27, FS 923-969 CORRODED. REMOVED DAMAGED SEAT TRACK IAW AMM 53-00-49-000-801-A02, AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726458Seat Track · gougedLEFT SEAT TRACK FROM BS 683 - 836 GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026072457Seat Track · gougedRIGHT SEAT TRACK FROM BS 683 - 836 AT RBL 9 GOUGED. REMOVED AND REPLACED RT SEAT TRACK. FABRICATED ON HN00315720 IAW AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726456Skin · damagedRUDDER LT SIDE HAS A DENT AT APPROXIMATELY 6 INCHES FROM THE LEADING EDGE BETWEEN RS 66.76 AND RS 72.79. REPAIRED THE RUDDER SKIN IAW REO 670-55-41-184, REV --.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Rudder, Plate/SkinSDR VNAA2026072455Bulkhead · corrodedDURING INSTALLATION OF FLOORBOARD 131ALF FOUND AFT SIDE OF BS 235 BULKHEAD HAS CORROSION AND MISSING COLLAR ON LOWER RT SIDE, ADJACENT TO ELECTRICAL CONNECTOR J110. PERFORMED A MAJOR REPAIR TO BS 235 FRAME IAW REO 670-53-11-2344 REV--.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2026072454Stringer · corrodedSTRINGER 20R IS CORRODED BETWEEN BS 581 TO 597, REPAIRED STRINGER 20R IAW SRM 53-00-03-201-001-A01 AND REO 670-53-31-1182, REV-.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260726453Skin · damagedDCA IS REPORTING A DENT AFT OF GALLEY SERVICE DOOR ABOUT AIRPLANE FLOOR LEVEL. BS 379, STRINGER 17R. REPORTED DIMENSIONS ARE W: 0.60”, L: 0.65” BY D: 0.0001. PERMANENT REPAIR IAW REO 670-53-21-2382.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2026072452Drag Angle · corrodedPAX DOOR AFT DRAG ANGLE HAS CORROSION BESIDE LOWER REPAIR. REMOVED DAMAGED DRAG ANGLE AND INSTALLED A SERVICABLE DRAG ANGLE.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026072451Hinge · damagedPAX DOOR HINGE (FUSELAGE SIDE) REQUIRES REPLACEMENT. REMOVED PAX DOOR HINGE IAW SRM 51-42-21-001-001-A01. LOCATED AND DRILL NEW SERVICEABLE PAX DOOR HINGE IAW SRM 51-40-11-001-001-A01. INSTALLED SERVICEABLE PAX DOOR HINGE IAW SRM 51-42-21-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA2026072450Intercostal · corrodedPAX DOOR AFT DD7 INTERCOSTAL FOUND TO BE CRACKED REQUIRES REPLACEMENT. REMOVED DAMAGED DD7 AFT INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD7 IAW SRM 51-40-11-001-001-A01AND 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20260726449Former · corrodedPAX DOOR AFT FORMER FOUND TO BE CORRODED REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20260726448Intercostal · corrodedPAX DOOR MID DD6 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT. REMOVED DAMAGED DD 6 MID INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-AJul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR `VNAA20260726447Window Post · crackedDURING SEALANT REMOVAL FOUND THE RH SIDEPOST CRACKED AT THE TOP FASTENER HOLE AND REQUIRES REPLACEMENT. REMOVED DAMAGED RT WINDSHIELD SIDEPOST IAW SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE RT WINDSHIELD SIDEPOST IAW SRM 51-42-21-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260726446Intercostal · damagedPAX DOOR AFT INTERCOSTAL DD4 FOUND (2EA) LARGE HOLE FROM PREVIOUS REPAIR REQUIRE REPLACEMENT. REMOVED DAMAGED DD 4 AFT INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD4 IAW SRM TASK 51-40-11-001-001-A01, & 51-42-06-001-Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20260726445Slat Track · wornLEFT SLAT TRACK 3-3 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. PERFORMED REPAIR TO LT SLAT TRACK3-3 IAW REO 670-57-42-2433 REV -.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260726444Former · gougedFORWARD CARGO DOOR, LOWER DOOR FRAME FORMER HAS SEVERAL AREAS OF CORROSION. REPAIRED FWD CARGO DOOR, LOWER DOOR FRAME FORMER IAW REO 670-52-35-607 REV --. REINSPECTION REQUIREMENTS ARE BEING TRACKED UNDER RFTS-127775.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026072443Support Fitting · gougedRIGHT WING OTBD FLAP HINGE BOX AFT SUPPORT FITTING AT WS 264 HAD ALL 4 ATTACH LUGS GOUGED. REPAIRED FLAP SUPPORT FITTING IAW REO 670-57-21-11-21, REV -.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2026072442Stringer Clip · corrodedSTRINGER CLIP CORRODED AT STR 27 FWD SIDE OF BS 265. REMOVED UNSERVICEABLE BS 265 STRINGER CLIP 27 IAW SRM 51-42-06-001-001-A01. INSTALLED A NEW STRINGER CLIP IAW SRM 51-42-21-001-001-A01, AND SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2026072441Frame · corrodedBS 549 FRAME IS CORRODED BETWEEN STR 18L - 19L. REPAIRED IAW REO 670-53-31-1189, REV-.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2026072440Shear Tie · corrodedBS 549 FRAME ATTACH ANGLE IS CORRODED BETWEEN STR 18L - STR 19L. REMOVED AND INSTALLED NEW SERVICEABLE FRAME CLEAT IAW SRM 51-42-13-001-001-A01M, AND 51-42-21-001-001-A01 AND REPAIRED THE FRAME SECTION AT BS 549 LT FROM STR 16L TO STR 18L IAW REO 670-53-31-1Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR VNAA2026072439Frame · corrodedBS 565 FRAME IS CORRODED BETWEEN STR 18L - 16L. REPAIRED IAW REO 670-53-31-1189, REV--, AND REO 670-53-31-1189, REV-.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260726438Attach Angle · corrodedBS 565 FRAME ATTACH ANGLE IS CORRODED BETWEEN STR 18L TO STR 19L. REMOVED AND INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW SRM 51-42-10-001-001-A01, AND 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20260726437Floorbeam · corrodedRIGHT BS. 280 FLOORBEAM APPEARS TO BE CORRODED AROUND SCREW HOLES. INSTALLED NEW SERVICEABLE RT BS 280 FLOORBEAM IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-13-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026072436Post · corrodedLBL 9 FLIGHT COMPARTMENT ENTRY POST IS CORRODED AT BS 280. ININSTALLED NEW REPAIR PARTS FLIGHT COMPARTMENT ENTRY POST LOWER SECTION IAW SRM 51-42-13-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260726435Door Frame · corrodedRBL 9 FLIGHT COMPARTMENT ENTRY POST IS CORRODED AT F.S. 280 CORRECTIVE ACTION: ININSTALLED NEW REPAIR PARTS @ RBL 9 FLIGHT COMPARTMENT ENTRY POST LOWER SECTION FS. 280 IAW CRJ700 SRM 51-42-13-001-001-A01. CC670-34142-2Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026072434Angle · corrodedBS 280, FWD J ANGLE CORRODED. REMOVED AND REPLACED WITH NEW SERVICEABLE J ANGLE, CROSSBEAM IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026072433Mount Fitting · corrodedGALLEY MOUNT FITTING IS CORRODED AT BS 295 JUST INBD OF RBL 9. INSTALLED A NEW GALLEY MOUNT FITTING IAW SRM 51-42-20-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Equipment Attach FittingsSDR VNAA2026072432Seat Track · corrodedRBL 9 SEAT TRACK CORRODED BETWEEN BS 394 - 485. INSTALLED NEW SERVICEABLE SEAT TRACK IAW REO 670-53-21-2875, REV-.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026072431Seat Track · corrodedLBL 9 SEAT TRACK CORRODED BETWEEN BS 394 TO 485. REMOVED UNSERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A02). 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 VNAA20260726430Stringer · corrodedSTRINGER 20R IS CORRODED BETWEEN FS 295 AND FS 310. REMOVED AND REPLACED STRINGER 20R IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260726429Stringer · corrodedSTRINGER 22R IS CORRODED BETWEEN BS 333 TO 349. REPLACED STRINGER 22R.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260726428Stringer · corrodedSTRINGER 21L IS CORRODED BETWEEN BS 437 TO 453. REMOVED AND REPLACED STRINGER 21L IAW SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2026072427Angle · corrodedPAX DOOR FWD SEAL ANGLE IS CORRODED. REMOVED AND REPLACED FWD AND AFT SEAL STRIKER ANGLES IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026072426Support Bracket · corrodedPAX DOOR FWD AND AFT HANDRAIL SUPPORT BRACKETS ARE CORRODED ON THE FUSELAGE SIDE. INSTALLED NEW SERVICEABLE FWD HANDRAIL SUPPORT BRACKET IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE AFT HANDRAIL SUPPORT BRACKET IAW SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026072425Door Sill · corrodedSERVICE DOOR SILL IS CORRODED BETWEEN BS 319 TO 349. REMOVED SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01. REF TASKS 1Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026072424Striker · corrodedAFT SIDE OF SERVICE DOOR SEAL STRIKER IS CORRODED AROUND SCREW HOLES BETWEEN BS 319 TO 333. REPLACED STRIKER ANGLE IAW SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Service DoorsSDR VNAA2026072423Frame · corrodedBS 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STR 20L TO 21L. UPON REVIEW OF UT MEASUREMENTS FOUND .064 REMAINING ORIGINAL THICKNESS IS .080 REMOVED .016 FOUND DAMAGE TO BE OUT OF LIMITS OF SRM 53-00-00-101-001-A01. REPAIRED BS 280 CIRCUMFERENTIAL JOINT IAJul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2026072422Stringer · corrodedSTRINGER 21R CORRODED BETWEEN BS 364 TO BS 379. REMOVED AND REPLACED THE STRINGER 21R BETWEEN BS 333 TO BS 379 IAW SRM 51-42-06-001-001-A01.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260726421Seat Track · corrodedLEFT SIDE WALL SEAT TRACK IS CORRODED BETWEEN BS 708 TO 761.85. REMOVED DAMAGED SEAT TRACK IAW SRM 53-41-49-101-001A01. INSTALLED A NEW SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801 (CONFIGA02).Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726420Seat Track · corrodedLEFT SIDE WALL SEAT TRACK IS CORRODED BETWEEN BS 785.15 - 863. REPLACED THE SEAT RAIL IAW AMM 53-00-49-000/400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726419Seat Track · corrodedLEFT SIDE WALL SEAT TRACK IS CORRODED BETWEEN BS 863 TO 969. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260726418Seat Track · corrodedRIGHT SIDE WALL SEAT TRACK GOUGED & CORRODED BTWN BS 677 TO 708. INSTALLED RT SIDE WALL SEAT TRACK IAW AMM 53-00-49-400-801-A02.Jul 24, 2026 · N506AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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