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.
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
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 A6WA202609018912Landing Gear · faultedDURING CLIMB OUT AFTER GEAR RETRACTION AT A BOUGHT 8,000 FT, BEGAN HEARING A THUD NOISE COMING FROM NOISE AREA OF ACFT. LOWERED MLG & NOISE WENT AWAY, NOISE CAME BACK AFTER RETRACTED. MLG F/O NOTICED SLIGHT YAW MOTION AFTER LOWERING MLG FOR LANDING NOISE DID SDR A6WA202608138907Flap System · failedFLAP FAIL CAUTION ON APPROACH C/W QRH. FLAPS FAILED AT 20 DEGREES. C/W FIM RESET PER AWA SUP 98-018I. MESSAGE REMAINS. AIRCRAFT REMOVED FROM SERVICE. REF 357150-1 FOR CORRECTIVE ACTION RESET FDU OPS TEST GOOD AND FLAPS OPS TEST GOOD.SDR A6WA202606058893Proximity Sensor · false activationRIGHT EMERGENCY DOOR CAUTION MESSAGE AFTER TAKE OFF INTERMITTENTLY. DELTA P 1.4. AIRCRAFT REMOVED FROM SERVICE. VERIFIED EMERGENCY DOOR PUSH PLATE IS FLUSH AND THE DOOR IS CLOSED LATCHED AND LOCKED. REF 357128/2 FOR MEL. CLEANED RIGHT EMERGENCY DOOR PROXIMSDR A6WA202501198853Pdu · failedRECEIVED FLAP FAIL CAUTION MSG ON APPROACH TO LAND WHEN SELECTING FLAPS 30 FROM 20. FLAPS FAILED AT 20. FLAPS WER ON MEL. AIRCRAFT REMOVED FROM SERVICE. R & R FLAP PDU IAW AMM 27-52-01 FLAP PDU OPS TEST GOOD.SDR A6WA202501098851Wheel · unknownUPON APPLYING TAKE-OFF POWER, AIRCRAFT YAWED HARD TO THE RIGHT, FULL LEFT RUDDER WOULD NOT COUNTERACT YAW. REJECTED TO PERFORMED. ON TAXI BACK TO HANGAR AC YAWED RIGHT WITH NO RUDDER / TILLER INPUT. BTMS SHOWED 2,1,1,1. AIRCRAFT REMOVED FROM SERVICE. REF LPSDR A6WA202407308784Idg · faultedABORTED TAKE OFF DUE TO IDG 2 CAUTION MSG. CAUTION MSG CLEARED WHEN POWER BROUGHT BACK TO IDLE. QRH NOT PERFORMED. AIRCRAFT REMOVED FROM SERVICE. C/W M ACTION FOR MEL 24-11-01-01. REF 365898-3 FOR MEL IN WORK. REFERENCE WORK ORDER 337826 MAINTENANCE WORKCSDR A6WA2024031198724Skin · dentedDENTS ON RH FUSELAGE LOW PRESSURE GROUND AIR CONDITIONING CONNECTION. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR OF AFT LOWER FUSELAGE SKIN AT FS 574.0 TO FS621 BETWEEN STR 20R TO 24L IAW REO 601R-53-61-8143. REV DATED 2024-03-06. HFEC ACCOMPLISHED,SDR A6WA202403088723Skin · dentedDENTS ON R/H WING OUTBOARD LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED R/H WING OUTBOARD LEADING EDGE ASSY REF AMM 57-41-01 REV 66. REMOVED AND REPLACED LEADING EDGE SKIN REF CRJ200 SRM 51-40-11 REV 39.SDR A6WA202402098714Doubler · cracked50033 334403 452-830-606 - 70HRS PAX DOOR AFT ANGLE IS CRACKED AT PULL IN CAN AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DOUBLER PULL IN CAN WITH PN 601R318094-2. IAW CRJ200 SRM 51-42-00, AND 51-42-13 REV 39 WORK PERFORMED UNDER AERSALESDR A6WA202203108128Strut · dischargedINFLIGHT RECV'D GEAR DISAGREE AND NOSE DOOR WARNING MESSAGES. ALSO RECV'D WOW INPUT AND NOSE WHEEL STEERING CAUTION MESSAGES. ALONG WITH WOW OUTPUT STATUS MESSAGE. NOSE GEAR DID NOT RETRACT. C/W QRH. LANDING GEAR EXTENDED AND ALL MESSAGES EXTINGUISHED. *** ASDR A6WA202202168104Bracket · noneNUMBER 1 ENGINE (ESN801422) NOSE COWL SUPPORT BRACKET IS LOOSE INBOARD SIDE OF ENGINE. ***AIRCRAFT REMOVED FROM SERVICE*** INTERIM REPAIR - VERIFIED NUMBER 1 ENGINE NOSE COWL SUPPORT BRACKET P/N 228-50082-145 HAS NOT CAUSED DAMAGE TO SURROUNDING STRUCTURE. SDR A6WA202202218112Aileron · corrodedLH WING AILERON PN CC670-13000-1 HAS INTERNAL STRUCTURE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH WING AILERON PN CC670-13000-1, SN 7693. PERFORMED RIGGING CHECK AND OPERATIONAL TESTS OF THE FLIGHT CONTROL SYSTEM. ALL WORK WITHISDR A6WA202201168110Beam · damagedCABIN FLOOR BEAM SUPPORT P/N 601R31118-127 AT FS559.00 AND BL0.0 HAS TOOL SET MARKS ON UPPER HORIZONTAL SURFACE. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY DAMAGED SECTION OF BEAM AT FS559.00 AND BL0.0 AND REPLACED WITH FLOOR BEAM SUPPORT P/N 601R31118-12SDR A6WA202202178105None · corrodedPITTING CORROSION ON LH WING UPPER SKIN LANDING FOR PANEL 540AT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE ON LH WING UPPER SKIN LANDING P/N 601R10042-7 FOR PANEL 540AT. PERFORMED HFEC WITH NO INDICATIONS. PERFORMED ROTO PEEN TO REWORKED AREAS. RSDR A6WA202202148101Fitting · gougedLH HORIZONTAL STABILIZER HINGE FITTING HAS DAMAGE IN TWO PLACES AT LBL55.8865. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE ON LH STABILIZER HINGE FITTING DIMENSION P1- L= 0.700Ï¿½ X W= 0.200Ï¿½ X D= 0.012Ï¿½, P2- L= 1.100Ï¿½ X W= 0.200Ï¿½ X D= 0SDR A6WA202202148100Fitting · gougedLH ELEVATOR HINGE FITTING HAVE DAMAGE ON INBOARD AND OUTBOARD HALVES AT LBL55.88 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE DIMENSION L=1.500Ï¿½ X W= 0.300Ï¿½ X W D= 0.010Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALSDR A6WA202202218113None · damagedPAX DOOR LOWER SILL SEAL STRIKER AT FS349.00 IS DAMAGED. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PAX DOOR LOWER SILL SEAL STRIKER AT FS349.00 PN 600-31535. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMISDR A6WA202202148098Doubler · corrodedSERVICE DOOR LOWER SURROUND STRUCTURE DOUBLER AND BRACKETS AT FS319.00 AND FS349.00 HAVE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SERVICE DOOR LOWER SURROUND STRUCTURE DOUBLER P/N 601R38669-49 AT FS309.00 Ï¿½ FS319.00 AND BRACKET SDR A6WA202202168103Angle · corrodedCORROSION ON CABIN FLOOR SILL RHS AT FS349.00 AND RBL41, WL73.5. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FLOOR SILL SECTION AND REPLACED WITH REPAIR ANGLE P/N 601R31148-1355 TO MATCH ORIGINAL FLOOR SILL CUTOUT AT FS349.00 Ï¿½ FS375.00 AND RBL 41.SDR A6WA202202118097Shroud · crackedLH WING LEADING EDGE PANEL P/N 601R12076 HAS A CRACK MEASURES L= 0.700 X W= 0.010Ï¿½ THE LOWER FLANGE OF INNER SHROUD AT INBOARD END AT WS149.58. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE ON LOWER FLANGE AND FABRICATED AND INSTALLED A REPAIR ANGLESDR A6WA202202218114Web · noneREAR SKIN PANEL OF AFT PRESSURE BULKHEAD IS MISSING ALL REINFORCEMENT ANGLES (7 EA) -59, -61, -62, -65, -66, -69, & -70 REF BOMBARDIER REO 601R-53-61-1240 REV D DTD 2016-10- 13 ***AIRCRAFT REMOVED FROM SERVICE*** GENERAL AND DETAILED INSPECTION C/W, WITH NSDR A6WA202202158102Doubler · dentedAFT PRESSURE BULKHEAD HAS A DENT LOCATED AT FS621.00 AND RBL6.0, WL80.0. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY EXISTING UPPER DOUBLERS P/N 601R-53-61-1240-3 AND -4 AND EXISTING LOWER DOUBLERS P/N 601R-53-61-1240-1 AND -2. REMOVED DENT DAMAGE. FABSDR A6WA202202218111Seat Track · corrodedLH SIDEWALL SEAT TRACK FROM FS409.00 TO FS559.00 +112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 TO FS559.00 +112. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS SDR A6WA202102038094Seat Track · corrodedR/H SIDEWALL SEAT TRACKS FROM FS 364.00 TO FS 559.79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364.00 TO FS 559.00+80 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. ****SDR A6WA202102028093Angle · gougedL/H WING I/B LE PANEL UPPER MOUNT LANDING HAS A GOUGE ON ANGLE DWG #600-12031. GOUGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-00-00 REV 38. *************AIRCRAFT REMOVED FROM SERVICE************************ EDGE TRIMMED THE CHAFED AREA DIMENSIONS: 1.SDR A6WA202102018092None · damagedL/H HORIZONTAL STABILIZER SPLICE AT CLOSING RIB #9 HAS DAMAGE FROM LIGHTNING STRIKE. PREVIOUS TEMPORARY REPAIR COMPLIED WITH IAW MHIRJ REO 601R-55-11-677 REV A. PERMANENT REPAIR REQUIRED. *************AIRCRAFT REMOVED FROM SERVICE************************ CUTSDR A6WA202102018091Channel · gougedCARGO DOOR UPPER FWD SUPPORT CHANNEL P/N: 601R35050-129 HAS A GOUGE ON FLANGE. DIMENSIONS ARE: (P1) 1.900L X .063W X .190D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***SDR A6WA202102018090Bulkhead · noneAFT PRESSURE BULKHEAD REAR WEB HAS 2 EACH RIVETS INSTALLED AT THE EDGE OF CHEM MILL I/B OF Z STIFFENER AT LBL 17 WL 140.5 AND 141.5. ******************AIRCRAFT REMOVED FROM SERVICE********************** REMOVED 2 EACH RIVETS AT THE EDGE OF CHEM MILL ON AFT PSDR A6WA202102018089Fitting · gougedR/H H STAB FITTING #2 HAS 2 EACH GOUGES AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 1.00L X 0.200W X .006D (P2) 1.100L X 0.200W X .015D. BOTH GOUGES ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SESDR A6WA202102018088None · gougedR/H ELEVATOR I/B AND O/B FITTING HAS GOUGE ON FITTING ASSY AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 2.100L X 0.300W X .005D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SESDR A6WA202101318084Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 235+5" AND S19R. DENT DIMENSIONS ARE: (P1) 1.950L X 1.50W X .011D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***********SDR A6WA202101318085Skin · dentedAIRCRAFT L/H SKIN AT PAX DOOR CUTOUT HAS 1 EACH DENT AT FS 310.00+1" AND S13L+1.5". DENT DIMENSIONS ARE: (P1) .400L X .300W X .032D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SSDR A6WA202101318086None · gougedL/H LEADING EDGE PANEL 331AL HAS TOOL MARKS ON I/B FASTENER HOLES. DIMENSIONS ARE: (P1) 7.100L X 1.00W X .018D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***************SDR A6WA202101318087Bracket · gougedL/H HORIZONTAL STABILIZER JACKSCREW FITTING HAS GOUGE ON I/B FASTENER BRACKET. DIMENSIONS ARE: (P1) 2.150L X 1.650W X .010D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**SDR A6WA202111037951None · noneCAPTS WS CRACKED SPIDERWEB ACROSS ENTIRE PANEL ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 309800 WC 6,7,8,9, & 11 FOR R&R OF CAPT WINDSHIELD IAW CRJ AMM 56-11-01.SDR A6WA202101227560Control Unit · faultedON APPROACH, WHILE SELECTING FLAPS TO 8 DEGREES, RECEIVED FLAP FAIL MESSAGE. C/W QRH. PERFORMED ZERO FLAP LANDING. LANDED AT 41,000LBS. MAX BRAKE TEMP DURING TAXI WAS "4". PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPP 98-18I BOX 12. FLAPS RESET. PLACARDESDR A6WA202010057308Bulkhead Web · crackedSDI OF THE AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. ACCOMPLISHED UT INSPECTION ON AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM PART 4, 53-61-153 REV 41 NO INDICATIONS NOTED. ACCOMPLISHED HFEC INSPECTION ON AFT PRESSURE BULKHEAD FWDSDR A6WA202010057307Bulkhead Web · crackedNDT-3 INDICATION FOUND COMING FROM UNDER MACHINED FITTING OF THE BAGGAGE BAY DOOR (LINTEL AREA) FOUND 3 EACH CRACKS AT FS 621.00. NR 1 VERTICAL CRACK THAT MEASURES 1.7'' UPPER HORIZONTAL CRACK THAT MEASURES .5'' AND LOWER HORIZONTAL CRACK THAT MEASURES .5'' SDR A6WA202009189287Pressure Deck · corrodedLT PRESS FLOOR SILL PANEL HAS CORROSION AROUND FASTENER HOLE AT FS 452.35 & BL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FLOOR SILL PANEL AT FS 452.35 & BL 43 WITH A REWORK AREA THAT MEASURES L=1.88 X W=1.134 X D=.003" ORIGINAL THICKNESS .080" SDR A6WA202009187290Skin · damagedRT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH .001" MATERIAL REMOVED WITHIN REMAINING .054" MINIMUM SKIN THICKNESS CHECK. WITHIN ALLOWABLE LIMITS, REF AIR WISCONSSDR A6WA202009187289Skin · damagedLT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH .002" MATERIAL LOSS AND A MINIMUM REMAINING MATERIAL THICKNESS OF .054" WITHIN ALLOWABLE LIMITS, REF AIR WISCONSIN SUSDR A6WA2018042500784Doubler · crackedPAX DOOR EXISTING REPAIR DOUBLER ON AFT RISER UNDER COUNTER BALANCE CRACKED.SDR A6WA2018042500783Fitting · crackedBS 460 RBL BATH TUB FITTING CRACKED.SDR A6WA2018042500781Stiffener · crackedPAX DOOR ASSIST MOTOR LOWER STIFFNER CRACKEDSDR A6WA2018042500782Angle · crackedANGLE IS CRACKED ON THE OTBD SIDE OF RBL 9 AND JUST AFT OF THE FLOORBEAM BS 280.SDR A6WA2018042445780Angle · crackedFS 280 AFT SIDE RBL 9 CLIP CRACKED. REPLACEDSDR A6WA2018042445776Seat Track · damagedPILOT SEAT TRACKS HAVE GROVES WORN INTO TRACKS. REPAIRED THE SEAT TRACK IAW SRM 53-11-49, AND 51-12-00.SDR A6WA201845600Bulkhead Web · crackedWHILE PERFORMING NDT ON THE AFT PRESSURE BULKHEAD, BS 621. FOUND DISCONTINUITY INDICATION AT LBL 36.2. 5 INCHES ABOVE WL 73.50. INDICATION IS APPROX. 3/4 INCHES IN LENGTH.SDR A6WA2017082245214Crossbeam · chafedCARGO DOOR CROSS BEAM LOWER OUTBOARD CHANNEL CHAFED BY THE CABLES.SDR A6WA201644176Door Seal · lack of lubeUNABLE TO OPEN SERVICE DOOR FROM EXTERIOR. LUBRICATED SERVICE DOOR SEAL, HANDLE, AS REQUIRED. OPS CHECK NORMAL. DOOR OPENS FROM OUTSIDE, ACFT OK FOR SERVICE.
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