N416AW

Service difficulty reports · 183

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 = 'N416AW' 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 A6WA200840649Bulkhead · crackedMWC 15 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-1230 REV D.Dec 17, 2008 · N416AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740163Access Panel · corrodedLT LOWER WING PLANK FUEL ACCESS PANEL CUTOUT FOR FUEL PNL 540 CB HAS CORROSION IN NON-CRITICAL AREA APPROX 6.0 INCHES DEEP AND .020 WIDE. (K) [SUP 05-17-07] MAINTENANCE REPAIRED CORROSION BY BLENDING OUT CORROSION. PERFORMED NDT, ROTO PEENED AREA, SANDED RMar 28, 2007 · N416AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740159Frame · crackedFOUND FRAME CLIP AT FS 617 AT LBL 9 IS CRACKED .25 INCH CRACK IN RADIUS. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)Mar 27, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200740161Support · crackedINTERCOSTAL SUPPORT FOR THE NR 2 HYDRAULIC PRESSURE/RETURN FILTERS IS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. (K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT DAMAGE, LPI TO ENSURE CRACK REMOVED, PRIME AND PAINMar 27, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740160Support · crackedINTERCOSTAL SUPPORT FOR THE NR 1 HYDRAULIC PRESSURE/RETURN FILTERS AS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. (K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT CRACK, LPI TO ENSURE CRACK REMOVED, PRIME AND PAINTMar 27, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740209Support Beam · crackedCARGO DOOR SUPPORT BEAM LOWER ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED .4 INCH IN LENGTH. MAINTENANCE REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE IAW CRJ 200 SRM 51-42-21. (M)Mar 24, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200740162Vertical Beam · crackedFS 409.0 + 128.0 VERTICAL BEAM AT RBL 27.0 IS CRACKED .4 INCH. (K) [SUP 05-09-07] MAINTENANCE TRIMMED OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABRICATED REPAIR ANGLE AND INSTALLED IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R-53-11286. (M)Mar 24, 2007 · N416AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200740150Channel · crackedCARGO DOOR FWD TRUCK BOTTOM U-CHANNEL CRACKED APPROX .1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED CARGO DOOR FORWARD U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)Mar 20, 2007 · N416AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740144Channel · crackedHYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-159) CRACKED APPROX .1 INCH LONG IN CEILING LT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW BSC STANDARD REPAIR 601R-53-004Mar 19, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740143Channel · crackedHYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-157) CRACKED APPROX 1 INCH LONG IN CEILING RT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW BSC STANDARD REPAIR 601R-53-0044Mar 19, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740142Support Bracket · crackedHYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN CEILING RT WHEEL WELL FWD OF TRANSDUCER BRACKET. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-153 IAW CRJ 200Mar 19, 2007 · N416AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740141Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED LEFT FS 625 INTERCOSTAL AT STRINGER 14L IAW CRJ200 SRM 51-42-06. (M)Mar 18, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740140Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .8 INCHES LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED RIGHT FS 625 INTERCOSTAL AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)Mar 18, 2007 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640053Brake Assy · damagedNR 3 BRAKE LOCKED UP AFTER EXITING RUNWAY BTMS INDICATES 13. INSPECTED AND FOUND HYDRAULIC BRAKE COUPLING NR 3 LOOSE AND THREADS DAMAGED. C/W INSP OF MLG, TIRE, BRAKES, AND AXLE IAW AMM. REMOVED AND REPLACED NR3 HYD BRAKE COUPLING AND NR 3 BRAKE ASSY. (K)Jan 30, 2006 · N416AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA200540156Skin · damagedLEFT SIDE AFT FUSELAGE SKIN DAMAGED BETWEEN FS 574-621, STRINGERS 17L-19L. MEASURES 2 INCH LONG BY 1 INCH WIDE BY .096 INCH DEEP. INSTALLED EXTERNAL DOUBLER AND TRIPLER TO DAMAGED FUSELAGE SKIN IAW BOMBARDIER, INCH REO 601R-53-61-1039. (M)Apr 12, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540159Clip · crackedFLOORBEAM CLIP AT FS 280, LBL 9, INBOARD IS CRACKED IN RADIUS APPROX 33 INCHES. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW SRJ SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540135Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 LHS IS CRACKED AT LBL 41.5 APPROX 1 INCH. REPAIRED BY REMOVING DAMAGE, FABRICATING STRAP, INSTALLING STRAP AND ANGLES P/N 601R-53-61-117-1 AND 601R-53-61-117-3 IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540136Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 RT IS CRACKED AT RBL 41 APPROX 70 INCHES. REPAIRED BY REMOVING DAMAGE, FABRICATING STRAP, INSTALLING STRAP AND ANGLES P/N 601R-53-61-117-2 AND 601R-53-61-117-4 IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540133Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS484, LBL 36, IS CRACKED FROM TOP RIVET HOLE TO EDGE APPROX. (0.30 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540132Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 OB IS CRACKED IN RADIUS APPROX 0.52 INCH. (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540131Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 IB IS CRACKED IN RADIUS APPROX ( 0.50 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540130Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9, IB IS CRACKED IN RADIUS APPROX (0.33 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540128Clip · crackedFLOOR SUPPORT BEAM CLIP AS FS280, LBL 9.0, OB IS CRACKED IN RADIUS APPROX 0.30. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540129Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED 1 INCH LONG AT THE MOTOR CABLE PULLEY BRACKET. PERFORMED REPAIR TO PASSENGER DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 REV A. (M)Apr 3, 2005 · N416AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540137Angle · crackedRIGHT FS 625.0 OBLIQUE ANGLE CRACKED .5 INCH LONG. S/D - INSTALLED NEW ANGLE AT FS 625 RT P/N 601-35012-52. (M)Apr 2, 2005 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540138Angle · crackedLEFT FS 625 OBLIQUE ANGLE CRACKED .5 INCH LONG. S/D - INSTALL NEW ANGLE P/N 601-35012-51 AT LEFT FS 625 IAW CRJ 200 SRM 51-42-06. (M)Apr 2, 2005 · N416AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440189Control Unit · failedIN-FLIGHT RECEIVED SPOILERON CASS MESSAGE. REMOVED AND REPLACED NR 1 SECU, OPS CHECK GOOD IAW 27-61-00.Nov 18, 2004 · N416AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200440161Bracket · damagedNOSE GEAR DOOR/ DISAGREE ON WITH GEAR HANDLE UP. NOSE GEAR DOWN, MAINS UP. REPLACED NOSE GEAR BRACKET WITH NOSE GEAR EXT AND PROXIMITY SENSOR IAW CMM 32-61-05 PERFORMED NOSE GEAR SWING. OPS CHECK GOOD.Oct 22, 2004 · N416AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200440122Warning Light · false indicationIN FLIGHT RIGHT AOA HEAT CAUTION, COMPLIED WITH QRH. COMPLIED WITH OPS CHECK OF RIGHT AOA HEAT CONFIRMED THAT VANE IS HEATING AND CHECKED WIRING TO HEAT CONTROLLER. COULD NOT DUPLICATE IAW AMM 30-30-00. (M)Aug 29, 2004 · N416AW · Cndair CL6002B19 · Ice/Rain Protection SystemSDR A6WA200340123Control Unit · malfunctionedSTAB TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PER QRH. MACH TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PRE QRH. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW 27-41-01, GROUND OPS CHECK GOOD. (M)Aug 13, 2003 · N416AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200340119Warning System · activatedFOUND STAB TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET FOR QRH. MACH TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PER QRH. (M)Aug 13, 2003 · N416AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200340108Control Unit · malfunctionedSTAB TRIM CHANNEL 1 DISCONNECT WHEN YOKE TRIM SWITCH ENGAGED FROM EITHER SIDE. FERRIED TO DEN. REMOVED AND REPLACED HORIZ STAB P/N 8396-2 S/N 827, AND MCU P/N 7062-3 P/N 849, IAW AMM 27-42-01. OPS CHECK GOOD. REPORT CONFIRMED FAULT REMOVED REPLACED CH1 RVDJul 15, 2003 · N416AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200340106Idg · intermittentINTERMITTENT IDG 2 CAS MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF MESSAGE CLEARED. BRAKE TEMP REMAIN IN NORMAL RANGE. COMPLIED WITH 'CM' ACTION. PLACARDED AND PLACED ON MEL. SERVICED NR 2 IDG AND RECONNECTED, CHECKS OK. REMOED FROM MEL. (M)Jun 24, 2003 · N416AW · Cndair CL6002B19 · AC Generation System
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