N452AW
Service difficulty reports · 202
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 = 'N452AW' 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.
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 = 'N452AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR A6WA201140100Rib · crackedLT BATT RIB CRACKED CUT OUT DAMAGED AND INSTALLED FILLER AND DOUBLER.SDR A6WA201140264Skin · chafedLT AILERON UPPER L/E SKIN HAS CHAFING DAMAGE IN SEVERAL AREAS. REPAIRED LT AILERON UPPER L/E SKIN IAW REO 601R-57-60-013.SDR A6WA201140263Skin · chafedLT AILERON LWR SKIN HAS CHAFING DAMAGE ON L/E IN 2 EA AREAS. REPAIRED DAMAGED AREAS IAW REO 601R-57-60-020.SDR A6WA201140265Skin · chafedRT INBD FLAP VANE L/E SKIN HAS CHAFING DAMAGE IN (3 EA) AREAS FROM STOPS. REPAIRED RT INBD FLAP L/E IAW REO 601R-57-52-004.SDR A6WA201140256Angle · crackedLT FS 621.00 OBLIQUE ANGLE CRACKED. R & R WITH SERVICEABLE OBLIQUE ANGLE, PN 601-35012-51 IAW SRM 51-42-06 AND REO 601R-53-61-422, REV NC.SDR A6WA201140106Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AFT CRACKED DRAG ANGLE SECTION, THEN SPLICED IN NEW SECTION USING PN 601R31772-5 AND IAW BA REO 601R-52-11-513, REV A.SDR A6WA201140259Beam · chafedLT INBD FLAP VANE CENTER ACTUATOR BEAM HAS WEAR FROM LOWER ROLLERS. REMOVED CHAFING DAMAGE ON LT INBD FLAP VANE CENTER ACTUATOR BEAM IAW REO 601R-51-52-1683.SDR A6WA201140258Beam · chafedLT INBD FLAP VANE INBD ACTUATOR SEAM HAS WEAR FROM LOWER ROLLERS. REMOVED CHAFING DAMAGE ON LT INBD FLAP VANE INBD ACTUATOR BEAM IAW REO 601R-51-52-1683.SDR A6WA201140261Fitting · chafedLT WING OTBD FLAP ROLLER FITTING HAS CHAFING DAMAGE. REPAIR CHAFING DAMAGE ON LT WING OTBD FLAP ROLLER FITTING IAW REO 601R-57-53-850.SDR A6WA201140267Skin · damagedRT OTBD FLAP HAS 2 LOOSE RIVETS ON TOP SKIN IN THE CENTER OF THE FLAP. REMOVED UNSERVICEABLE LOOSE RIVETS ON RT OTBD FLAP TOP SKIN IN THE CENTER OF THE FLAP AND INSTALLED SERVICEABLE RIVETS IAW REO 601R-57-53-849.SDR A6WA201140091Bulkhead · crackedBULKHEAD FS 202 CRACKED AROUND PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, WL 69.684 IAW REO 601R-53-11-563.SDR A6WA201140262Fitting · chafedLT WING OTBD FLAP ROLLER GUIDE FITTING HAS CHAFING DAMAGE. REPAIRED LT OTBD FLAP ROLLER GUIDE FITTING IAW REO 601R-57-51-143.SDR A6WA201140266Skin · chafedL/E OF RT INBD FLAP VANE JAS CHAFE DAMAGE. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN.SDR A6WA201140268Skin · chafedRT AILERON LOWER L/E IS CHAFED IN 2 PLACES. REPAIRED CHAFED AREAS ON RT LOWER L/E 2 PLACES IAW 601R-57-60-020, REV NC.SDR A6WA201140257Track · chafedRT T/R LOWER OTBD AND INBD MAIN TRACKS CHAFED. REPAIRED CHAFE ON RT T/R LOWER OTBD AND INBD MAIN TRACK.SDR A6WA201140260Skin · chafedLT INBD FLAP VANE SKIN L/E HAS CHAFING DAMAGE FROM STOPS IN 3 EA AREAS. REPAIR LT INBD FLAP VANE IAW REO 601R-57-52-004.SDR A6WA201140083Bracket · crackedAFT FACE OF RT NOSE INLET HAS CRACKED BRACKET AT 4 O`CLOCK POSITION. R & R BRACKET IAW SRM 51-42-06, 51-21-11, 51-25-16.SDR A6WA201140088Skin · chafedRT MLG DOOR L/ECHAFED. REMOVED DAMAGE, INSTALLED DOUBLER AND FILLER.SDR A6WA201140269Handle · crackedPAX DOOR EXTERNAL HANDLE CRACKED. REMOVED CRACKED HANDLE THEN INSTALLED NEW HANDLE PN 601252-119.SDR A6WA200940782Pin · installedRT MAIN GEAR WOULD NOT COME UP AFTER T/O. RETURNED AND LANDED. REMOVED RT MLG DOWNLOCK PIN AS REQUIRED. (K)SDR A6WA2000940544Computer · inoperativeAFTER TAKEOFF WITH 2600 LBS PER SIDE, FUEL IMBALANCE ON ED1, QTY 3000 IN LT, 2000 IN RT. RT WING LOWERING AND CENTER TANK WAS INCREASING. REMOVED AND REPLACED FUEL SYS COMPUTER IAW AMM 28-41-16. OPS CHECK GOOD. (K)SDR A6WA200940198Floorbeam · damagedTOOL DAMAGE ON FLOORBEAM AT FS 484, RBL 36.00, WL 72.00 AND INTERCOSTAL AT FS 484.00 BTW RBL 36 AND RBL 45, WL 72.00. FLOORBEAM AT FS 484.00, RBL 36.00, WL 72 AND INTERCOSTAL FS 484.00, RBL 36-45 WL 72 REPAIRED IAW REO 601R-53-41-916. (K)SDR A6WA200940196Flap · crackedPAX DOOR OUTER HANDLE FLAP IS CRACKED. PAX DOOR OUTER HANDLE REPLACED IAW SRM 51-42-06. (K)SDR A6WA200940195Floor Support · crackedMID CABIN FLOOR STRUCTURE, ANGLE CRACKED (.500 LENGTH) AT FS 484 AND RBL 28. MID CABIN FLOOR STRUCTURE, ANGLE REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)SDR A6WA200940194Intercostal · crackedMWC 132399-121 - MID CABIN FLOOR STRUCTURE, INTERCOSTAL CRACKED AT FS 484, RBL 35. MID CABIN FLOOR STRUCTURE INTERCOSTAL AT FS 484, RBL 35, REPAIRED IAW REO 601R-53-41-059, REV A. (K)SDR A6WA200940192Floor Support · crackedMWC 132399-119- MID CABIN FLOOR STRUCTURE, ANGLE CRACKED (.400 INCH LENGTH) AT FS 484, LBL 28. MID CABIN FLOOR STRUCTURE, ANGLE REPLACED AT FS 484, LBL 28 IAW SRM 51-42-06 AND 51-42-21. (K)SDR A6WA200940189Floorbeam · crackedMWC 132400-69- UPPER ANGLE ALONG CROSSBEAM AT FS 280.00, LBL 10.00, WL 72 IS CRACKED. UPPER ANGLE ALONG CROSSBEAM AT FS 280.00 LBL 10.00, WL 72.00 REPAIRED IAW REO 601R-53-11-138. (K)SDR A6WA200940193Intercostal · crackedMWC 132399-120 - INTERCOSTAL AT FS 484 LBL 36.00, WL 70.00 IS CRACKED. INTERCOSTAL AT FS 484.00, LBL 36.00, WL 70.00 REPAIRED IAW REO 601R-53-41-059, REV A. (K)SDR A6WA200940197Floorbeam · crackedOTBD ANGLES CRACKED AT FS 280.00, LBL 9.0, WL 72.00 (L+.200 INCH AND .300 INCH) OTBD + INBD ANGLES AT FS 280.00, LBL 9.0, WL 72, INSTALLED IAW SRM 51-42-21. (K)SDR A6WA200940190Floorbeam · crackedMWC 132400-83 - RT INBD ANGLE AT FS 280.00, RBL 8.00, WL 72.00 CRACKED, CRACK LENGTH .350 INCH RT INBD ANGLE AT FS 280.00, RBL 8.00, WL 72.00. REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)SDR A6WA200940188Skin · damagedMWC 132399-41 - FWD FUSELAGE ASSESS PANEL DOOR SURROUND SKIN QTY (2) ELONGATED FASTENER HOLES AT FS 228.00 BTW STR 19-20 RT SIDE FWD FUSELAGE ACCESS PANEL DOOR SURROUND SKIN QTY (2) ELONGATED FASTENER HOLES AT FS 228.00 BTW STR 19-20. REPAIRED IAW REO 601R-53SDR A6WA200940138Flap System · malfunctionedFLAP FAIL MSG ON TAXI OUT WHEN FLAPS SELECTION TO FLAPS 8 DEGREES. COMPLIED WITH RESET PROCEDURE FOR SDS AND FLAP SYS IAW FIM 27-00. OPS CHECK GOOD. (K)SDR A6WA200940035Control Lever · faultyFLAPS FAILED WHEN SELECTING FROM 8 DEGREES TO 20 DEGREES, AIRSPEED 180 KNOTS. OAT APPROXIMATELY 5 DEGREES CELSIUS. CW FIM 27-50 FOUND FLAP CONTROL LEVER FAULT ON FECU. REPLACED FLAP CONTROL LEVER IAW AMM 27-50. RESET FLAP SYSTEM IAW AWAC SUP 98-018B. OPS SDR A6WA200840618Ecu · malfunctionedLOG 192018/1 ON APPROACH HAD FLAPS FAIL MSG. WHEN FLAPS SELECTED TO 8 FLAP INOPERATIVE CAUTION MSG DISPLAYED. COMPLIED WITH FIM 27-50-00. FAULTS FOUND LEAD TO INTERNAL FECU/BPSU MISS RIG. R&R FECU IAW AMM 27-51-05. OPS CHECK GOOD. RIG CHECK GOOD AT THIS SDR A6WA200840606Actuator · failedLOG 192011/1 PAX DOOR WILL NOT LOWER COMPLETELY. HELD DOOR DOWN TO UNLOAD PASSENGERS, POWER ASSIST MOTOR FAILED. ASSIST SPRINGS ALSO BAD. R&R PAX DOOR ACTUATOR IAW AMM 52-10-00, OPS CHECK OK.SDR A6WA200840403Warning System · false activationUPON ENGINE START GROUND SPOILER DEPLOY ADVISORY MESSAGE. ALL SPOLERS CONFIRMED UP VISUALLY AND ON FLIGHT CONTROL PAGE. INTERROGATED LT AND RT SECU`S FOR FAULTS, NO FAULTS FOUND. CHECKED MDC FOR FAULTS/DIAGNOSTICS, NO FAULTS FOUND GROUND RAN AIRCRAFT, RE CHECKSDR A6WA200840229Landing Gear · malfunctionedAFTER SELECTING GEAR DOWN GOT GEAR DISAGREE MESSAGE, RT MLG DID NOT EXTEND. COMPLIED WITH QRH, ALL THREE GEAR EXTENDED DOWN AND LOCKED AND ALL GREEN. DURING GEARDOWN SELECTION, HEAVY SIDE WIND GUST. (M)SDR A6WA200840055Handle · unsecureON CLIMBOUT AFTER TAKEOFF, APROX 600 MSL, CARGO DOOR MESSAGE ED1 AND CAUTION LIGHT ILLUMINATED. CABIN CLIMBING APPROX 1400 FT PER MIN. C/W QRH. AFTER LANDING NOTED CARGO DOOR HANDLE POPPED. FOUND CARGO DOOR HANDLE EXTENDED UPON ARRIVAL AT GATE. STOWED CARSDR A6WA200740233Floorbeam · crackedRT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE REPAIRED IAW BOMBARDIER AEROSPACE REO 601R-53-61-117. (M)SDR A6WA200740232Floorbeam · crackedLT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R53-61-117 REV C. (M)SDR A6WA200740231Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX .5 INCHES LONG AT DOOR ASSIST CABLE PULLEY BRACKET. (K) [07-17-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R52-11-513 REV A. (M)SDR A6WA200640371Heater · failedSTRONG BURNING SMELL IN GALLEY AREA. SMELL LESSENS WHEN GALLEY HEATERS TURNED OFF. PERFORMED SELF TEST OF GALLEY HEATING SYSTEM, FOUND SYSTEM ONE FAILED. PERFORMED SELF TEST OF GALLEY HEAT SYSTEM, FOUND SYSTEM ONE FAILED. COMPLIED WITH CM ACTION, REF 14228SDR A6WA200640372Warning Light · activatedRIGHT REVERSER UNLOCKED CAS MESSAGE IN FLIGHT FOLLOWED QRH PROCEDURE. COMPLIED WITH MAINTENANCE ACTION AND DEACTIVATION OF THRUST REVERSER REF 142277/4 FOR MEL. PERFORMED OPS CHECK OF RT REVERSER SYSTEM PER MM 78-30-00, OK FOR SERVICE REMOVED FROM MEL. (M)SDR A6WA200640351Beam · crackedTRANSVERSE BEAM AT FS 250, RBL 30, NEAR STRINGER 16 IS BENT AND CRACKED .3 INCH INBOARD OF STRINGER 16. MAINTENANCE REPAIRED TRANSVERSE BEAM IAW EO 601R-53-9822. (M)SDR A6WA200640350Skin · damagedAIRCRAFT BLOWN INTO FUEL TRUCK. DAMAGED ON RIGHT FUSELAGE BELOW F/O`S WINDOW. MAINTENANCE REPAIRED DAMAGE TO FWD FUSELAGE STRUCTURE FS 235 TO FS 280, STRINGER 17 TO 23, REO 601R-53-11-1062. (M)SDR A6WA200540175Skin · dentedRT IB FLAP LOWER SKIN HAS A DENT 2 INCHES X 2.5 INCHES AND .077 INCH DEEP. DENT IS 24 INCHES FROM IB EDGE AND 2 INCHES FROM TRAILING EDGE. REPAIRED RT IB FLAP LOWER SKIN BY INSTALLING FLUSH REPAIR IAW BRAS EO. (K)SDR A6WA200540176Skin · dentedRT AFT FUSELAGE SKIN AT FS 590, 11 INCHES BELOW LOW PRESSURE EXT AIR DOOR HAS DENT AND GOUGE. REPAIRED LOWER AFT FUSELAGE SKIN AT FS 590 BETWEEN STRINGERS 21L AND 25R BY REMOVING EXISTING REPAIR AND INSTALLING A LARGER EXTERNAL DOUBLER IAW BRAS EO. (K)SDR A6WA200540150Seal · damagedDOOR SEAL IS LOUD ABOVE 6 DP. VIBRATION NOISE STARTS AT 270 KNOTS IAS. REMOVED AND REPLACED PASSENGER DOOR SEAL. PRESSURE CHECK GOOD. (M)SDR A6WA200440113Engine · vibrationENGINE 2 VIBRATION EXCEEDED LIMITS AT V1 WITH CONSTANT AIRFRAME VIBRATION INDICATION GOT OVER 3. REMOVED AND REPLACED NR 2 ENGINE DUE TO HIGH VIBRATION IAW AMM 72-10. (M)SDR A6WA200340170Frame · damagedFOUND FRAME AT FS 589 SKIN FLANGE BETWEEN STRINGERS 24L AND 25L IS DAMAGED AND FLANGE BETWEEN STRINGERS 25L AND 26L IS DAMAGED. REMOVED FLANGE, FABRICATED REPAIR FLANGES FROM 2024 T3 .050 INCH WVAC PO NR 29699/1, FABRICATED FILLER SHIMS FROM 2024 T3 .090 INCH
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