N412AW

Service difficulty reports · 200

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 = 'N412AW' 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 A6WA201302054666Structure · damagedELONGATED HOLES ON RIGHT ENGINE LOWER CORE COWL ALIGNMENT PIN HOLES. REPAIRED IAW CMM 71-12-01 REPAIR SRS109.Jan 25, 2013 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA2013020500667Bracket · brokenLEFT O/B FLAP O/B HINGE ARM HAS BROKEN MOUNT BRACKET FOR PANEL 597BB ON O/B SIDE. REMOVED AND REPLACED MOUNT BRACKET FOR PANEL 597BB.K.Jan 24, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA20134675Vane · chafedRIGHT I/B FLAP VANE LEADING EDGE I/B, CTR & O/B AREA CHAFED FROM STOPS. REMOVED AND REPLACED I/B LEADING EDGE & BLENDED & TREATED CTR & O/B LEADING EDGE IAW REO 601R-57-52-004.Jan 23, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201302050674Vane · chafedRIGHT INBD FLAP VANE HAS FOUR CHAFE SPOTS. NOT BUMP STOPS. BLENDED CHAFE SPOTS IAW SRM 51-12-00 FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004.Jan 23, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2013020500659Bracket · crackedIN THE NOSE HYD COMPARTMENT, UPPER ACCUMULATOR FWD UPPER MOUNT BRACKET IS CRACKED. REMOVED UNSERVICEABLE ACCUMULATOR FWD UPPER MOUNT BRACKET AND REPLACED WITH SERVICEABLE BRACKET IAW SRM 51-42-06 AND 51-42-21.Jan 23, 2013 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA20134M673Fitting · chafedRIGHT OTBD FLAP ROLLER GUIDE ALIGNMENT FITTING IS CHAFED. BLENDED CHAFE PER CRJ 200 SRM 51-12-00 DEPTH WAS .008 WITHIN LIMITS IAW REO 601R-57-51-143.Jan 22, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA20134672Fitting · chafedRIGHT OTBD FLAP ROLLER GUIDE FITTING IS CHAFED. BLENDED CHAFE ON CRJ 200 SRM 51-12-00 DEPTH OF CHAFE WAS .014 WITHIN LIMITS IAW REO 601R-57-53-039.Jan 22, 2013 · N412AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA20134671Seal · crackedRIGHT FLIGHT SPOILER OUTBD SEAL CRACKED AND BROKEN BY OUTBD SPOILER HINGE. REMOVED UNSERVCIEABLE SEAL ON RIGHT FLIGHT SPOILER O/B AND REPLACED WITH SERVICEABLE SEAL RIGHT P/N 601R10226-130 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.Jan 22, 2013 · N412AW · Cndair CL6002B19 · SpoilersSDR A6WA20134677Attach Angle · crackedPAX DOOR POWER ASSIST MOTOR UPPER ATTACH ANGLE CRACKED IN RADIUS. REMOVED AND REPLACED ANGLE P/N 601R317745-7.Jan 21, 2013 · N412AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA20134M678Fitting · crackedCRACKED CLIP FS 280 RBL 9 O/B. REMOVED AND REPLACED RBL 9 O/B CLIP AT FS 280 IAW CRJ 200 SRM 51-42-21 & 51-40-11.Jan 19, 2013 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA20130205661Angle · crackedCRACKED ANGLE AT FS 280 RBL 9 INBRD. REMOVED & REPLACED ANGLE IAW SRM 51-42-21 & 51-40-11.Jan 19, 2013 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013020500664Bulkhead · gougedAFT SIDE OF BULKHEAD FS 280 GOUGED. REPAIRED AFT SIDE FS 280 BULKHEAD IAW REO 601R-53-11-1727 REV F.Jan 17, 2013 · N412AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2013020500658Frame · damagedTWO FASTENER HOLES AROUND 132AL ACCESS HOLE ARE OBLONG. REPAIR PER REO 601R-53-11-162.Jan 17, 2013 · N412AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA20121001125Controller · failedDURING CRUISE HEARD CRACKING SOUND AND FLASH OF LIGHT BEHIND CBP1 LEFT WINDSHEILD HEAT AND LEFT WINDOW HEAT CAUTION MSG. REMOVED AND REPLACED AIHC WINDSHEILD CONTROLLER IAW AMM 30-41-01, OPS CHECK GOOD.Sep 28, 2012 · N412AW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR A6WA201140614Warning Message · illuminatedFLIAPS DEGRAGED, WHITE STATUS MESSAGE APPEARED. C/W FIM FAULT RESET PROCEDURE MESSAGE CLEARED.Jul 21, 2011 · N412AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA201140200Computer · malfunctionedEFIS COMP MON ROLL AND PITCH, F/O PFD WENT SIDEWAYS AND A/P KICKED OFF. ACFT RETURN TO DEPARTURE, NORMAL LANDING AND NORMAL BRAKING=WD 4460. R & R NR 2 AHRS COMPUTER IAW AMM 34-21-01. OPS CK GOOD.Mar 19, 2011 · N412AW · Cndair CL6002B19 · Attitude Gyro and Indicating SystemSDR A6WA201140117Cowling · chafedRT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED RT LOWER CORE COWL IAW CMM 228-50142, TASK 71-12-01-300-822-A01.Jan 27, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140118Cowling · chafedLT LOWER CORE COWL IS CHAFED AT FWD LATCHES. REPAIRED LT LOWER CORE COWL IAW CMM 228-50142 TASK 71-12-01-300-822 AOL.Jan 27, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140108Panel · damagedPANEL 132AL HAS DRILL STARTS AT SCREW HOLES. LOCATED HOLES IN FWD RT PRESSURE PANEL IAW SRM 51-40-11.Jan 27, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201140120Nut Plate · missingLT AILERON CTR BRACKET HAS MISSING NUTPLATE AND NUTPLATE HOLE IS DAMAGED. R & R LT AILERON CTR BRACKET IAW REO 601R-57-61-320.Jan 26, 2011 · N412AW · Cndair CL6002B19 · AileronsSDR A6WA201140119Structure · crackedUPPER OTBD CASCADE ON RT THRUST REVERSER CRACKED. REPAIRED RT T/R UPPER OTBD CASCADE IAW PROCESS SPEC 1 DWG AW-78-30-0711-04.Jan 25, 2011 · N412AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140055Skin · gougedCARGO BAY DOOR CUTOUT AFT LOWER CORNER DENTED. REPAIRED DAMAGED AREA IAW REO 601R-53-61-3965.Jan 25, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201140056Access Panel · crackedAPU ENCLOSURE COVER DOOR ACCESS PANEL HAS CRACK IN CORNER EXTENDING FROM WELD. REPAIRED APU ENCLOSURE DOOR 311B2 IAW REO 601R-49-11-070, REB B.Jan 25, 2011 · N412AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201140115Angle · crackedCLIP ANGLE CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD, LT SIDE. R & R CLIP IAW SRM 51-42-06 & SRM 51-42-21.Jan 22, 2011 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140114Angle · crackedCLIP ANGLE CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD. TEST RT SIDE, R & R CLIP ANGLE IAW SRM 51-42-06.Jan 22, 2011 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140113Sill · corrodedPAX DOOR SILL HAS CORROSION AS MARKED. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR SILL IAW SRM 51-42-06 & 51-42-21.Jan 21, 2011 · N412AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140110Attach Fitting · crackedCARGO BAY DOOR SEAL PLATE HAS CLIP CRACKED. REMOVED UNSERVICEABLE CARGO DOOR SEAL PLATE CLIP IAW SRM 51-40-11. INSTALLED SERVICEABLE CARGO DOOR SEAL PLATE CLIP SRM 51-40-11.Jan 21, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140121Skin · chafedRT AILERON L/E BUTTON SKIN CHAFE DAMAGE OTBD DEEP, RT AILERON L/E TOP SKIN CHAFE DAMAGE .006 DEEP. BLENDED CHAFE DAMAGE FROM BOTTOM SKIN BLENDED TOP SKIN WITHIN LIMITS, IAW REO 600R-57-60-020 IODIZED, PRIMED AND TOP COAT IAW SRM 51-25-16, 51-25-06.Jan 20, 2011 · N412AW · Cndair CL6002B19 · AileronsSDR A6WA201140109Attach Fitting · crackedFS 484 HAS CRACKED CLIP AT RBL 27 OTBD. R & R CLIP AT FS 484, RBL 27 IAW REO 601R-53-41-059.Jan 20, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140112Attach Fitting · crackedFS 484 CRACKED CLIP AT LBL 36 INBD. R & R FS484, LBL36 CLIP IAW REO 601R-53-41-059.Jan 20, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140111Attach Fitting · crackedFS 484 HAS CRACKED CLIP AT LBL 27 OB. R & R FS 484, LBL27 CLIP IAW REO 601R-53-41-059.Jan 20, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140065Bracket · crackedFWD LWR TRACK OF CARGO BAY DOOR HAS CRACKED BRACKET. R & R BRACKET IAW SRM 51-42-06.Jan 19, 2011 · N412AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140050Retainer · crackedBT HAS CRACKED SEAL RETAINER. R & R SEAL AND SEAL RETAINER IAW SRM 51-42-06.Jan 19, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140116Seal · chafedRT ENG UPPER NOSE COWL EDGE SEAL CHAFED. R & R EXISTING SPLICE IAW CMM 71-14-01.Jan 18, 2011 · N412AW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA201140046Attach Fitting · wornFWD AND AFT DIVIDER CLIP ARE DAMAGED ON PANEL 422BT. R & R WITH NEW FWD AND AFT DIVIDER CLIPS.Jan 18, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201140047Attach Fitting · worn100 PERCENT MATERIAL LOSS WORN ALL THE WAY THROUGH FWD DIVIDER CLIP ON PANEL 412BF. DAMAGE R & R WITH NEW CLIP.Jan 18, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201140045Skin · chafedLT MLG DOOR L/E CHOPPED. FABRICATED AND INSTALLED FILLER IAW REO 601R-52-82-034.Jan 17, 2011 · N412AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140048Skin · gougedRT LOWER COR COWL HAS (6EA) GOUGES IN NON FIRE SHIELD AREA (FWD INNERSKIN) BLENDED OUT (2EA) GOUGES IAW CMM 71-12-01. REPAIRED (2EA) GOUGES WHILE WAS OUT OF LIMITS IAW CMM 71-12-01-200-802-A01 (1EA) DENT WAS WITHIN LIMITS.Jan 17, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140049Skin · gougedLT LOWER CORE COWL HAS (5EA) GOUGES IN NON FIRE SHIELD AREAS (FWD INNERSKIN) BLENDED (2EA) GOUGES AND REPAIRED (2EA) GOUGES IAW CMM 71-12-01 (1 DENT) FOUND TO BE WITHIN LIMITS IAW CMM 71-12-01-200-802-401.Jan 17, 2011 · N412AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140057Skin · chafedMLG DOOR INNER SKIN CHAFING R & R PREVIOUS FILLER IAW REO 601R-52-82-034.Jan 10, 2011 · N412AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201040439Frame · crackedFS 559, RBL 9 HAS CRACK FROM BOTTOM OF LOWEST RIVET INCORPORATED REO 601R-53-41-260 REV D DATED 09/17/09 AND REO 601R-53-41-116, DATE 01/19/10.Jun 14, 2010 · N412AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201040403Isolator · crackedFS 621 BULKHEAD HAS 3 CRACKED ISOLATORS. R & R WITH SERVICEABLE 3 EA ISOLATORS PN SL2337-3, PO 961376 AT FS 621 BULKHEAD ALL WORN DOWN IAW SRM 51-42-06, 51-42-06, 51-25-06.Jun 2, 2010 · N412AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040185Flap System · malfunctionedFLAPS 45 DEGREES NORMAL APPROACH AIRSPEED (145 KNTS) ACFT REQUIRES ABOUT .5 INCH LT AILERON TRIM TO MAINTAIN LEVEL FLIGHT. ON CLIMB OUT ZERO FLAPS, NORMAL TRIM.Mar 3, 2010 · N412AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200940265Uplock Actuator · failed191172/3 - GEAR DISAGREE - WARNING ILLUMINATED APPROX 6-10 SECONDS AFTER RETRACTION SELECTION. LT MLG DID NOT RETRACT. COMPLIED WITH QRH. GEAR EXTENDED AND LOCKED NORMALLY. INSP LT MLG. FOUND NO VISUAL EVIDENCE OF HYD LK OF MECHANICAL FAILURE. INSTALLED May 22, 2009 · N412AW · Cndair CL6002B19 · Landing Gear ActuatorSDR A6WA200940261Uplock · inoperativeGEAR DISAGREE AFTER TAKEOFF, RED DASHES ON LT MAIN GEAR INDICATION. REMOVED AND REPLACED LT MLG UPLOCK ASSY IAW AMM 32-32-05. OPS AND LEAK CHECK GOOD. REMOVED PLACARD, REMOVED FROM MEL. RII I-160. (K)May 16, 2009 · N412AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200940242Landing Gear · malfunctioned"GEAR DISAGREE WARNING MESSAGE APPEARED APPROX 5-10 SECONDS AFTER COMMANDED NOSE AND RT MLG INDICATED "RED" , LT MLG SHOWED "YELLOW". QRH COMPLIED WITH GEAR EXTENDED NORMALLY. C/W MX ACTION FOR MEL 32-20-01. INSTALLED NLG SAFETY AND BOTH MLG PNS IAW AMM 10May 9, 2009 · N412AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200940209Line · leakingHYD LOW PRESSURE CAUTION INFLIGHT, COMPLIED WITH QRH WITH APPROX 17 MIN REMAINING IN FLIGHT. INSP AND FOUND NR 2 HYD SYS RESERVOIR SUCTION LINE LEAKING. REPAIRED HYD LINE WITH NEW FITTINGS IAW AMM 20-22-00. BLED NR HYD SYS OPS AND LEAK CHECK NORMAL IAW AMMApr 12, 2009 · N412AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200940068Floorbeam · crackedINBD AND OTBD CLIPS AT FS 280 AND JUNCTION OF RT FLOORBEAM 9.0 ARE CRACKED. INBD AND OTBD CLIPS AT FS 280 REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)Jan 26, 2009 · N412AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940041Skin · dentedMWC 131269/1 - 4DMI13275 REPAIR LT WING OTBD L/E AS REQUIRED DENT EXISTS IN L/E SKIN. 6.00 INCH L X 3.50 INCH W X .103 INCH DEEP. REO 601R-57-41-490 AND 601R-57-41-490 REV A LT WING OTBD L/E SKIN REPLACED IAW SRM 51-42-06 AND REO 601R-57-41-161, REV B AND DWGJan 25, 2009 · N412AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940040Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71 AT THE PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71 REPAIRED IAW REO 53-11-1571.Jan 23, 2009 · N412AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
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