N438AW

Service difficulty reports · 217

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 = 'N438AW' 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 A6WA200640176Case · crackedLT ENGINE LOW PRESSURE TURBINE CASE IS CRACKED 1.5 INCHES LONG AT 9 O`CLOCK POSTION .75 INCH AFT OF FORWARD FLANGE. CLEANED SUSPECT AREA AND PERFORMED LPI IAW CRJ NDTM 51-20-08. FOUND 1 CRACK LIKE INDICATION APPROXIMATELY 1.5 INCH LONG AT 9 O`CLOCK POSITION.May 6, 2006 · N438AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200640180Bracket · crackedHYDRAULIC PRESSURE TRANSDUCER BRACKET P/N 601R75262-157 IN RT WHEEL WELL CEILING CRACKED. REMOVED AND REPLACED BRACKET P/N 601R75262-157 IAW CRJ SRM 51-40-11. (M)May 5, 2006 · N438AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640179Support Bracket · crackedHYDRAULIC PRESSURE TRANSDUCER LINE SUPPORT BRACKET, P/N 601R75262-153 IN RT WHEEL WELL CEILING CRACKED. REMOVED AND REPLACED HYDRAULIC PRESSURE TRANSDUCER LINE SUPPORT BRACKET P/N 601R75262-153 IN RT WHEEL WELL IAW CRJ 200 SRM 51-42-06. (M)May 5, 2006 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640178Bracket · crackedHYDRAULIC PRESSURE TRANSDUCER BRACKET P/N 601R75262-159 CRACKED IN LEFT WHEEL WELL CEILING. REMOVED AND REPLACED BRACKET, P/N 601R75262-159, IAW CRJ SRM 51-40-11. (M)May 5, 2006 · N438AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640172Floor Support · crackedFOUND RT FS 621 FLOOR SUPPORT ANGLE CRACKED .5 INCH LONG IN OUTBOARD RADIUS. REPAIRED FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV C. (M)May 2, 2006 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640171Intercostal · crackedFOUND LEFT FS 484 INTERCOSTAL HAS A .25 INCH CRACK AT LBL 36 ANGLE. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)May 2, 2006 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640170Intercostal · crackedFOUND RIGHT FS 484 INTERCOSTAL HAS A .25 INCH CRACK AT RBL 36 ANGLE. REPAIRED ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)May 2, 2006 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640169Support Channel · crackedFOUND FS 574 BAGGAGE DOOR CAM TRACK LOWER SUPPORT CHANNEL P/N 601R-35050-25 IS CRACKED .75 INCH LONG. REMOVED AND REPLACED CHANNEL, P/N 601R35050-25 IAW CRJ SRM 51-42-06. (M)May 1, 2006 · N438AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200640168Intercostal · crackedRT UPPER FS 621 TO FS 625 INTERCOSTAL/OBLIQUE ANGLE P/N 601-35012-52 IS CRACKED 1.5 INCHES LONG IN AFT RADIUS. REMOVED RT UPPER 621 TO 625 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (M)May 1, 2006 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640167Intercostal · crackedFOUND LEFT UPPER FS 621 TO FS 625 INTERCOSTAL/OBLIQUE ANGLE IS CRACKED 1.5 INCHES LONG IN THE AFT RADIUS P/N 601-35012-51. REMOVED LEFT UPPER FS 621 TO 625 OBLIQUE ANGLE CRJ 200 SRM 51-42-06. INSTALLED NEW INTERCOSTAL/OBLIQUE ANGLE AT LBL 45 AT STRINGER 14L May 1, 2006 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540126Warning Light · illuminatedAT 32,000 FT, A FUEL IMBALANCE CAS MESSAGE APPEARED ON EICAS. THE PROBLEM WAS NOT CORRECTABLE USING AUTO, MANUAL OR GRAVITY CROSSFLOW. LT WING HEAVY AT LANDING AN IMBALANCE 1700 LBS C/W QRH. SHUTDOWN ENG NR 2, LANDING WEIGHT WAS NOT EXCEEDED. PERFORMED SYSMar 25, 2005 · N438AW · Cndair CL6002B19 · Fuel Indicating SystemSDR A6WA200540084Relief Valve · failedDURING DESCENT WITH POWER AT IDLE BOTH PACKS DROP OFF LINE. REMOVED AND REPLACED RT AND LT PRESSURE RELIEF VALVES IAW 21-51-43. (M)Mar 3, 2005 · N438AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200440134Skin · lightning strikeMWC 122, LIGHTNING STRIKE DAMAGE AT FS 235.00, STR 15R. BLENDED DAMAGE AND ENSURED ARE IS CRACK FREE IAW REO 601R-53-11-814.Sep 9, 2004 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440133Skin · lightning strikeMWC 121, LIGHTNING STRIKE DAMAGE AT FS 202.75, STR 22R. BLEND DAMAGED AND ENSURED AREA IS CRACK FREE IAW REO 601R-53-11-814.Sep 9, 2004 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440127Skin · lightning strikeWHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 24R-25R AT FS 220-235 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLESep 9, 2004 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440125Skin · lightning strikeWHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 27R-26R AT FS 257 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER ANSep 9, 2004 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440126Skin · lightning strikeDURING LIGHTNING STRIKE DAMAGE INSPECTION OF RIGHT FUSELAGE FOUND AREA BETWEEN STRINGER 26R-27R AT FS 243 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .007 INCH. CUT OUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLESep 8, 2004 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
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