N415AW
Service difficulty reports · 215
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 = 'N415AW' 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 = 'N415AW' 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 A6WA201140418Floor Support · corrodedFLOORBEAM CAP FS 589 TO FS 620.00, LBL 9 HAS CORROSION AT NUT PLATE HOLES. REMOVED CORROSION FROM NUT PLATE HOLES IAW SRM 51-12-00 AND REO 601R-53-00-005, REV B.SDR A6WA201140421Angle · crackedFS 625, RT OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM FS 625 RT AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-61-422, REV NC.SDR A6WA201140422Angle · crackedFS 625 LT OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM FS 625 LT AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-61-422, REV NC.SDR A6WA201140291Strip · chafedT/E STRIP ON RT UPPER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT UPPER NOSE COWL IAW CMM 71-14-01.SDR A6WA201140292Floorbeam · corrodedFLOORBEAM AT FS 589.00 OTBD NEXT TO FLOOR LEDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-12-00 AND SRM 51-11-00 ALODINED, PRIMED, TOPCOATED.SDR A6WA201140293Structure · chafedT/E OF RT LOWER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT LOWER NOSE COWL IAW CMM 71-14-01.SDR A6WA201140168Selector Valve · inoperativeON GEAR EXTENSION RECEIVED "GEAR DISAGREE" MSG FOLLOWED WITH DOWN INDICATION OF THE NLG. FOLLOWED QRH MSG CLEARED AND RECEIVED NORMAL DOWN INDICATION AFTER PULLING THE EMERGENCY EXTEND HANDLE. R & R NLG SELECTOR VALVE IAW AMM 32-33-10.SDR A6WA201040974Adg · unwanted deployADG INADVERTANT DEPLOYMENT AT FL310 COMPLIED WITH QRH ALL SYS POWERED NORMALLY PRIOR TO ADG DEPLOYMENT. COMPLIED WITH RETRACTION OF ADG IAW AMM 24-23-01. OPS CK GOOD.SDR A6WA201040758Pcu · malfunctionedINFLIGHT RECEIVED "OTBD GRND SPLR FAULT" AND "FLIGHT SPOILER FAULT" MESSAGES. INFLIGHT AND ON THE GROUND, FLIGHT CONTROL SYNOPTIC PAGE INDICATION FOR BOTH OTBD GRND SPOILERS AND FLIGHT SPOILERS INTEWRMITTENTLY CHANGING COLORS FROM GREEN, WHITE OR YELLOW. DURSDR A6WA201040389Skin · damagedACFT STRUCK BY TUG ON TAIL ON RT SIDE BETWEEN VS 55.625-VS 67.50. REMOVED DAMAGED SKIN IN SECTION STR 13R AND BUTT SPLICE STRAP. REPAIRED IAW 601R-53-71-116.SDR A6WA201040190Control Panel · failedAUTO CROSSFLOW INHIBIT MESSAGE ON ED2, NO POWER ON FUEL, DEFUEL PANEL. R & R FUEL/DEFUEL CONTROL PANEL AND HARNESS IAW AMM 28-25-16, PERFORMED OPS TEST IAW AMM 28-25-00. OPS TEST GOOD.SDR A6WA200940757Pressure Switch · malfunctioned2 INDICATION OF RT ENGINE LOW OIL PRESSURE WARNING. ENG OIL INDICATION NORMAL. PERFORMED HIGH POWER ENGINE RUN A T/O PWR FOR APPROX 10 MINUTES. OPERATION NORMAL. OIL PRESSURE INDICATION GOOD. INSPECTED LOP SWITCH CONNECTOR AND HARNESS. R & R LOP SWITCH ISDR A6WA200940756Fcu · failedON APPROACH, FLAPS FAILED WHEN SELECTED TO 30 DEGREES. AIRSPEED WAS 170 KIAS WITH GEAR DOWN. FLAPS FAILED AT 19 DEGREES. FOND NUMEROUS CODES FOR FLAP CONTROL IN FECU, REPLACED FLAP CONTROL LEVER IAW AMM 27-51-01. OPS CK GOOD AT THIS TIME.SDR A6WA200940637Connector · looseON CLIMB-OUT, RECEIVED RT ENG OIL PRESS WARNING MSG WITH AURAL WARNING. C/W QRH. REDUCED POWER AND MSG WENT OUT. MSG CAME ON AT 90 PERCENT N1, APPROX 70 PSI. NO OTHER CAS MSGS. FOUND OIL PRESSURE TRANSDUCER CONNECTOR PLUG TO BE VERY LOOSE AT BACKSHELL ANDSDR A6WA200940451Unknown · odorBURNING ODOR NOTICED AT MID SECTION OF CABIN, STRONGEST AROUND ROW 8. IT HAS BEEN DETERMINED THAT THIS WAS A RESIDUAL ODOR FROM A PREVIOUS DISCREPANCY CABIN AREA WAS OZONE CLEARED, NO FURTHER SMOKE ODOR EXISTS. (K)SDR A6WA200940450Battery Pack · failedSTRONG BURING ODOR AT MID CABIN OVERHEAD. FOUND ODOR TO BE VERY STRONG AT CEILING PANEL 7CA. REMOVED CEILING PANE LS AND PAX SERV UNIT PANELS FROM 5AD-8AC FOR T/S. FOUND NO ODOR UNDER PSU`S REMOVED CEILING INSULATION AND VERIVIED THAT NO CHAFED WIRES ON CEISDR A6WA200940449Ballast · odorSTRONG BURNING ODOR IN CABIN REQUEST INSPECTION. REMOVED AND REPLACED OVERHEAD BIN LIGHT BALLAST OVER ROW 7CA. OPS CHECK GOOD AT THIS TIME IAW AMM 33-20-00. (K)SDR A6WA200940373Idg · making metalCLIMBING THRU FL 200, FELT A THUD AND HAD A NR 1 GEN CAUTION APPEARED, C/W QRH MSG CLEARED. 2 THUD HEARD IDG 1 FAULT CAUTION, RAN QRH DISCONNECTED IDG. FOUND LT IDG OIL SCAVENGE FILTER TO BE CONTAMINATED WITH METAL C/W ACTION FOR MEL 24-11-01-01, REF 192748/SDR A6WA200940351Pressure Switch · malfunctionedRECEIVED RT ENGINE OIL PRESSURE MASTER WARNING ON DESCENT, 3 TIMES COMPLIED WITH QRH OIL PRESSURE INDICATED 63 PSI. REMOVED AND REPLACED RT ENGINE LOW OIL PRESSURE SWITCH IAW AMM 79-31-03. OPS CHECK LEAK CHECK GOOD. RAN ENGINE AT ALL POWER SETTINGS. NO FAUSDR A6WA200940288Fire Loop · shortedAFTER DEPARTURE SELECTED GEAR UP, AFTERWARD RECEIVED GEAR BAY OVERHEAT WARNING AURAL ON ED1 MSG, RAN QRH, MSG REMAINED, AND SOUNDED REPEATEDLY, RETURNED TO DEPARTURE. INS AND FOUND LOOP INSULATOR BRACKET MISSING RUBBER, INSULATION MIGRATED INBD, REPLACED FASTSDR A6WA200940128Skin Panel · corrodedLT WING PLANK ACCESS HOLE 510AB CORRODED. LT WING PLANK ACCESS HOLE 510AB. CORROSION REMOVED IAW REO 601R-57-21-030 REV G. EDDY CURRENT PERFORMED IAW REO 601R-57-21-030 REV G. ROTO PEEN PERFORMED AND ALODINE TREATMENT IAW REO 601R-57-21-03, REV G. (K)SDR A6WA200940199Handle · corrodedCREW ESCAPE HATCH OUTER HANDLE IS CORRODED. CREW ESCAPE HATCH OUTER HANDLE REPLACED IAW AMM TASK 52-22-03-400-801 AND OPS CHECK FOUND SERVICEABLE IAW CRJ200 52-22-02-710-801. (K)SDR A6WA200940127Sill · corrodedPAX DOOR LOWER SILL LONGERON INNER AND OUTER SURFACE CORRODED. PAX DOOR LOWER SILL LONGERON REPLACED IAW SRM 51-42-06. (K)SDR A6WA200940126Sill · crackedCARGO DOOR SILL CRACKED AT OTBD FASTENERS FS 589-605. CARGO DOOR SILL. REPAIRED IAW REO 601R-53-61-433. (K)SDR A6WA200940119Crossbeam · crackedCROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00 IS CRACKED IN THE LOWER RADIUS, CRACK LENGTH IS .600 INCH LONG. CROSSBEAM REPAIRED IAW REO 601R-53-11-171, SCHEME A. (K)SDR A6WA200940118Crossbeam · crackedCROSSBEAM AT FS 280.00, RBL 9.00, WL 72.00 IS CRACKED IN LOWER RADIUS. CRACK LENGTH IS .700 INCH LONG. CROSSBEAM AT FS 280.00, RBL 9.00, WL 72.00 IN LOWER RADIUS REPAIRED IAW REO 601R-53-11-171. REV D REPAIR SCHEME A. (K)SDR A6WA200940125Fitting · crackedCRACK FOUND ON MACHINED FITTING, FS 461, RBL 9, OTBD MACHINED FLOOR SUPPORT FITTING AT FS 461, RBL 9, WL 72.00. REPLACED IAW SRM 51-42-21 AND DWG 601R31118. (K)SDR A6WA200940120Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75 AT BL 23.71 AROUND PARKING BRAKE CABLE. CUTOUT CARRIED/OUT NDT PERFORMED, DOUBLER AND SHIMS FABRICATED AND WET INSTALLED, FITTING REPLACED AND WET INSTALLED. IAW REO 601R-53-11-563. (K)SDR A6WA200840644Bulkhead · crackedMWC 17. FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING, INSTALLING REPAIR PARTS IAW REO 601R-53-61-1230 REV D.SDR A6WA200840593Coalescer Bag · odorNOTICED OILY ODOR COMING FROM AIR CONDITIONING, BOTH PACS IN ENGINE OR APU AS AIR SOURCE, STRONGER WHEN DUCT TEMP IS HOTTER. REMOVED AND REPLACED RT ACM WATER SEPARATOR COALESCER BAG, REACTIVATED LT AND RT PACKS AND OVERBOARD EXHAUST SOV, OPS CHECK GOOD IAW AMSDR A6WA200840594Apu · odorRT PAC HAS OIL SMELL WHILE ON APU AIR. OILY SMELL DISSIPATES WHILE ON 10TH STAGE BLEED AIR. REMOVED AND REPLACED APU IAW AMM 49-10-00, OPS CHECK GOOD. (K)SDR A6WA200740258Sensor · malfunctionedFLAPS FAIL MASTER CAUTION OCCURRED 15 MINUTS AFTER DEPARTURE. QRH WAS ACCOMPLISHED. FLAPS FAILED AT ZERO DEGREES. EMERGENCY LANDING DECLARED FOR PRECAUTIONARY MEASURES. INTERROGATED FECU, FOUND L-BPSU MISRIGGED, NO EVIDENCE OF TWISTING OR ABNORMAL DEFORMATSDR A6WA200740136Skin · corrodedRT WING PLANK ACCESS HOLE AT FUEL PANEL 650CB HAS MINOR CORROSION AROUND APPROX 90 PERCENT OF BONDING AREA. (K) [SUP 06-05-07] MAINTENANCE SANDED CORRODED AREA TO REMOVE DAMAGE MAX BLEND .004 IAW BSC EO NR 601R-57-11217. (M)SDR A6WA200740135Skin · corrodedRT WING PLANK ACCESS HOLE AT 640 AB HAS MINOR PITTING IN CRITICAL AND NON-CRITICAL AREA. (K) [SUP 06-05-07] MAINTENANCE CLEANED EDGE OF FUEL TANK ACCESS DOOR SKIN CUTOUT. BLENDED CORROSION IN DETAIL AREA I AND IV TO DEPTH OF .002 IAW STEPS 1-4 OF BOMBARDISDR A6WA200740134Fitting · crackedFS 280.0 FLOOR SUPPORT CLIPS PN 601R31113-57 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE LBL 9.0. (K) [SUP 06-05-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 LBL 9 IAW CRJ 200 SRM 51-40-11, 51-42-02, 51-42-21. (M)SDR A6WA200740133Fitting · crackedFS 280.0 FLOOR SUPPORT CLIPS PN 601R3113-58 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 RBL9 IAW CRJ SRM 51-40-11, 52-42-06 AND 51-42-21. (M)SDR A6WA200740132Floor Support · crackedFS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE DAMAGED SECTION DRILLED NEW SECTION OF ANGLE AND SPLICES IAW BOMBARDIER REO 601R-53-11-136. (M)SDR A6WA200740131Floor Support · crackedFS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF LBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPAIRED DAMAGED SECTION, DRILLED NEW SECTION OF ANGLE AND SPLICES IAW REO 601R-53-11-136 STEPS 1-6 ANGLE P/N 600-SDR A6WA200740147Channel · crackedHYDRAULIC TRANSDUCER HOT CHANNEL PN 601R75262-159 CRACKED APPROX .1 INCH LONG IN CEILING OF LT MLG WHEEL WELL. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M)SDR A6WA200740146Bracket · crackedHYDRAULIC TRANSDUCER BRACKET PN 601R75262-157 CRACKED APPROX .1 INCH LONG IN CEILING OF RT MLG WHEEL WELL. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-06. (M)SDR A6WA200740145Support Bracket · crackedHYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) JUST FWD OF TRANSDUCER IN CEILING OF RT MLG WHEEL WELL CRACKED APROX .1 INCH LONG. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-153 IAW CRJ SSDR A6WA200740158Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED AT PAX DOOR ASST PULLEY BRACKET. (K) [SUP 06-05-07] CUTOUT DAMAGED SECTION AND REPAIRED IAW BOMBARDIER REO 601R-52-11-513 REV A AND BSC EO 601R-52-11280. (M)SDR A6WA200740149Angle · crackedRT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE NEW SERVICEABLE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11207. (M)SDR A6WA200740148Angle · crackedLT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCHES LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11218. (M)SDR A6WA200640312Warning System · false activationOUTER PASSENGER DOOR HANDLE MESSAGE ON DEPARTURE OUT OF DCA. COMPLIED WITH QRH FLIGHT ATTENDANT SAID THERE WAS UNLOCK INDICATION ON DOOR, DIVERTED TO IAD. TROUBLESHOOT IAW FIM 52-70-00. NO DEFECTS NOTED. OPS CHECK GOOD IAW CRJ AMM 52-11-00, NO DEFECTS NOTSDR A6WA200640140Carbon Seal · defectiveRT OIL PRESSURE DROPPED BELOW 25 PSI ON CLIMB-OUT AND CONTINUED TO CYCLE BETWEEN 25-35 PSI (AIR RETURN). NO INFLIGHT ENGINE SHUTDOWN. FOUND EDP NR 2 AGB CARBON SEAL LEAKING, REMOVED AND REPLACED HYD PUMP NR 2 AGB CARBON SEAL IAW AMM, COMPLIED WITH OIL CONSUMSDR A6WA200540173Shutoff Valve · faultyL-PACK HIGH PRESS WHINE, XFERRED TO ENGINE BLEED. WHEN DUCT PRESS 60 PSI OR GREATER. REMOVED AND REPLACED L-PRSOV IAW AMM 2-151-43. FUNCTIONAL TEST OF PRSOV GOOD IAW AMM 21-51-43. (M)SDR A6WA200540124Skin · scratched2 SCRATCHES IN FUSELAGE AT CARGO DOOR CUT-OUT, (APPROX 1 INCH LONG AND .5 INCH LONG.) PERFORMED A MAJOR REPAIR AT FS 549, STR 14-16 IAW EO. (K)SDR A6WA200540117Bushing · migratedRT MLG AFT TRUNNION BUSHING IS MIGRATED 0.15 INCH. REMOVED BUSHING, REAMED BARE AND INSTALLED 1ST OVERSIZE BUSHING IAW MFG REO. (K)SDR A6WA200540107Access Panel · corrodedRT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 50.54 AND WS 66.2 HAS MINOR FRETTING AND FAYING SURFACE LESS THAT .006 INCH DEEP. (K) BLEED MINOR FRETTING ON RT LOWER WING PLANK BETWEEN WS 50-54 AND 66.2 IAW REO. (K)
Back to N415AW