N439AW

Service difficulty reports · 186

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 = 'N439AW' 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 A6WA202502058858Skin · dentedRH AFT FUSELAGE HAS DENTS. AIRCRAFT REMOVED FROM SERVICE. PERFORMED REPAIR ON RH FUSELAGE SKIN BETWEEN FS 625.30 TO FS672.20 STR 20-23R IAW MHIRJ REO 601R-53-61-8276 REV -- DATED 2025-02-04.Feb 5, 2025 · N439AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202412178846Shutoff Valve · malfunctionedWHILE PERFORMING APPENDIX D PROCEDURE AFTER T/O, RT 10TH STAGE SOV WOULD NOT OPEN. LH PACK ON MEL AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BLEED AIR SOV IAW AWAC SUPP 19-036 AND AMM AMM 36-11-04, PERFORMED OPS CHECK, BLEED LEAK CHECK IAW AWAC Dec 17, 2024 · N439AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA202407058774Bracket · damaged6060 - AFTER TO GEAR UP NLG WOULD NOT RETRACT RAN QRH GEAR DOWN IN GREEN . NO ASSOC MSG, NO MAN RELEASE. HYDS ON. ATC DECLARED EMER, NO HARD. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND NLG TOW GUARD COLLAR MIGRATED UP AND DAMAGED NLG PROX SENSOR AND Jul 4, 2024 · N439AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA202405088743Strut · low pressureGEAR DISAGREE AFTER TAKEOFF, AIRCRAFT REMOVED FROM SERVICE. PERFORMED SERVICING OF NOSE LANDING GEAR SHOCK STRUT IAW AMM 12-12-32 AND AWAC SUP 16-250A. OPSERATIONAL AND FUNCTIONAL TEST ARE GOOD.May 8, 2024 · N439AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA202310228662Unknown · unknownGEAR DISAGREE ON TAKEOFF ******AIRCRAFT REMOVED FROM SERVICE******** C/W M ACTION FOR MEL 32-30-01 REF 362977/3 FOR MEL. R&R NLG S/A BRACKET IAW CMM 32-20-04 AND AMM 32-61-00-05. OPS CHECK GOOD, REMOVED PLACARD AND REMOVED FROM MELOct 22, 2023 · N439AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202308238649Wheel · damagedON TAXI INTO GATE, HIT POTHOLE RESULTING TO BOTH RIGHT TIRES BLOWN ON. TAXI WAY A ABEAM A14. BTMS INDICATIONS 4,3,3,3. AIRCRAFT REMOVED FROM SERVICE. CW TIRE BURST INSPECTION OF #3 AND #4 TIRE AIW AMM 05-51-29 NO DEFECTS NOTED. REF 362958-4 AND 362599-1 FOR Aug 23, 2023 · N439AW · Cndair CL6002B19 · TireSDR A6WA202307108638Unknown · unknownON CLIMB OUT GEAR UP GEAR DISAGREE WARNING. MESSAGE CLEARED CONTINUED CLIMB RECEIVED GEAR DISAGREE AGAIN. RAN QRH MESSAGE CLEARED WITH B PUMPS ON. NO ISSUES LOWERING GEAR FOR LANDING. NOSE GEAR DISPLAYED WHITE. MANUAL RELEASE NOT USED, NO OTHER ASSOCIATED MJul 10, 2023 · N439AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202306128630Sensor · unknownFLAPS FAILED AT 30' ON APPROACH, WHEN SELECTING FLAPS 45', LANDED WITH 1400 LBS FUEL. AIRCRAFT REMOVED FROM SERVICE. R&R RH BPSU OPS CHECK GOOD AT THIS TIME. REF AMM 27-51-10.Jun 12, 2023 · N439AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA202212158415Connector · brokenWHILE ON APPROACH WITH FLAPS 20 FLAP FAIL CAUTION WITH FLAPS 14 DEG. RAN QRH. AIRCRAFT REMOVED FROM SERVICE. WHEN RECONNECTING SKEW DETECTION SYSTEM FOUND BACK SHELL ON P11CE BROKE. R & R BACK SHELL. OPS CHECK GOOD.Dec 15, 2022 · N439AW · Cndair CL6002B19 · Flight Control System WiringSDR A6WA202210258411Detector · faultedLAP FAIL CAUTION AT 15 DEG. AIRCRAFT REMOVED FROM SERVICE. REF 351843/4, 351844/1,2,3,4 AND 351845/1 FOR CORRECTIVE ACTIONS AND MEL. SDU WAS DETERMINED TO BE THE CAUSE OF THE FLAP FAIL.Dec 14, 2022 · N439AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA202111227983Wire · failedDURING CLIMB, AT ABOUT 10,000 FEET THE CREW RECEIVED MULTIPLE CAUTION MESSAGES. CREW RAN THE QRH BASED ON THE MESSAGES AND WERE LEAD TO BELIEVE IT WAS A POSSIBLE ELECTRICAL ISSUE. THE FLIGHT ATTENDANT KNOCKED ON COCKPIT DOOR TO NOTIFY CREW THAT THE CHIMES ANDNov 21, 2021 · N439AW · Cndair CL6002B19 · Instrument System WiringSDR A6WA202109307929None · corrodedFLIGHT DECK DOOR LOWER TRIM SURFACE HAS CORROSION AND IS DELAMINATED REMOVED AND REPAIRED FLIGHT DECK DOOR LOWER TRIM IAW C&D ZODIAC RPM 25-6000-1 REV 1 DATE 2-18-06 AND SRM 51-26-00 REV 38. ACCOMPLISHED REINSTALL OF FLIGHT DECK DOOR. ALL WORK PERFORMED ATSep 30, 2021 · N439AW · Cndair CL6002B19 · DoorsSDR A6WA202110227926None · corroded16 AREAS ON THE L/H FLOOR SILL AND FLOOR ANGLE FROM FS450 TO FS559 FOUND TO HAVE CORROSION. ALL 16 AREAS WERE BLENDED IAW REO# 601R-53-41-666 AND THE MEASUREMENT ARE LISTED BELOW. 1. FS 424 + 3Ï¿½ L= 1.3Ï¿½ X W= 1Ï¿½ X D= .005Ï¿½ FLOOR SILL 2. FS 424 + 9Sep 30, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202110227925None · corroded2 SPOTS OF CORROSION ON R/H FLOOR SILL PANEL WITHIN 2.50IN OF EACH OTHER FROM FS438.0 TO FS443.0. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED BOTH SPOTS IAW REO 601R-53-41-666 REV C. DATE 2012-11-06. DIMENSIONS #1 L=1.025IN X W=.900IN X D=.005IN #2 L=1.0IN Sep 30, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202110217922None · dentedDENT WITH SCRATCH ON SKIN OF RH HORIZONTAL STABILIZER LE PANEL 341AR ON UPPER OUTBOARD END BETWEEN STABILIZER BL96.26 AND BL112.00. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AND REMOVED SCRATCH BY BLENDING ON SKIN OF RH HORIZONTAL STABILIZER LE Sep 30, 2021 · N439AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR A6WA202109297928None · corrodedCORROSION AT 3 AREAS ON RH FLOOR SILL PANEL AROUND FASTENER HOLES BETWEEN FS441.00 TO FS459.00 AND RBL41. BLENDED CORROSION AT 3 AREAS ON RH FLOOR SILL PANEL AROUND FASTENER HOLES BETWEEN FS441.00 TO FS459.00 AND RBL41. DIMENSIONS P1 - L= 1.025Ï¿½ X W= 0.900ÏSep 29, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202111037950None · noneCRACK INDICATIONS (2 TOTAL) AT FS 621 AFT PRESSURE BULKHEAD. CRACKS AT THE FOLLOWING LOCATIONS: FS 621 WL 107-WL 110 AT BL 0 CRACK IS 3"LENGTH; FS 621 WL 112.5-WL 115.5 AT LBL 27.5 CRACK IS 3" LENGTH. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON SSep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111017947Seat Track · corrodedSEAT TRACK P/N: 20276-144-0-0 AT FS 364.00 TO FS 409+18 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N 20276-144-0-0 FS 364.00 TO FS 409+18 L/H SIDE. ALL WORK WITHIN LIMITS WAS PERFORSep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Fixed PartitionsSDR A6WA202111017948Seat Track · corrodedSEAT TRACK P/N: 20276-144-0-0 AT FS 546 TO FS 559+80 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N: 20276-144-0-0 AT FS 546 TO FS 559+80 L/H SIDE. ALL WORK WITHIN LIMITS IAW CRJ200 ASep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202111017949Seat Track · corrodedSEAT TRACK P/N: 20276-144-0-0 AT FS 449.83 TO FS 546 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK P/N: 20276-144-0-0 AT FS 449.83 TO FS 546 L/H SIDE. ALL WORK WITHIN LIMITS IAW CRJ200 ASep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110197914Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS546.00 Ï¿½ FS599.00 + 80 RHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS546.00 Ï¿½ FS599.00 + 80 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IASep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202110197912Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 18 - FS409.00 + 110 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 18 - FS409.00 + 110 LHS. ALL WORK WITHIN LIMITS WAS PESep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110197913Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 110 - FS449.83 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS409.00 + 110 - FS449.83 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110187911Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 10Ï¿½ Ï¿½ FS449.83 HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFORMED IAW Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110187910Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS409.00 + 16Ï¿½ Ï¿½ FS409.00 + 112Ï¿½ HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFSep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110187909Seat Track · corrodedSEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½ HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½. ALL WORK WITHIN LIMITS WAS PERFORMED IAWSep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Fixed PartitionsSDR A6WA202110187908None · corrodedSEAT TRACK PN 20276-144-0-0 AT FS449.83 Ï¿½ FS546.00 HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED WITH A NEW SEAT TRACK PN 20276-144-0-0 AT FS449.83 Ï¿½ FS546.00. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202110157902Fitting · gougedPAX DOOR SUPPORT WHEEL FITTING PN 601R317092-3 HAS A GOUGE BELOW SPRING FS345.00. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED PAX DOOR SUPPORT WHEEL FITTING GOUGE BELOW SPRING FS345.00. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORSep 25, 2021 · N439AW · Cndair CL6002B19 · DoorsSDR A6WA202110067895None · corrodedCORROSION ON FLOOR SILL STRAP P/N 601R31025-29 AT FS559 AND LBL28.00". ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED FLOOR SILL STRAP WITH A NEW FABRICATED STRAP P/N 601R31025-29 AT FS559 AND LBL28.00. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PSep 25, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202111017946None · gougedGOUGE FOUND ON FWD SIDE OF I/B FLANGE OF FRAME SPLICE ANGLE AT FS 559.00 + 80 AT STR 6R. GOUGE DIMENSIONS ARE: .200"L X .200" W X .032"D. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND OUT ON FRAME SPLICE ANGLE AT FS 559.00 + 80 AT STR 6R. BLEND DIMENSSep 24, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202109227935Antenna · corrodedGPS ANTENNA RH HAS CORROSION ON MATING SURFACE, FS409.00+32, STR 0.0. REMOVED AND REPLACED WITH A NEW GPS ANTENNA AT FS409.00+32, STR 0.0. PN S67-1575-52 / SN 512-32090. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 34-58-400-801, REV 64. WORK PERFORSep 22, 2021 · N439AW · Cndair CL6002B19 · Navigation SystemSDR A6WA202110217920Fitting · gougedGOUGE ON RH ELEVATOR MID HINGE NO. 2 BL55.88 LOWER SIDE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE ON RH ELEVATOR MID HINGE NO. 2 BL55.88 LOWER SIDE. PN 600-23046. FITTING DIMENSION L= 0.500Ï¿½ X W= 0.100Ï¿½ X D= 0.010Ï¿½, PLATE DIMENSION L= 0.700Sep 20, 2021 · N439AW · Cndair CL6002B19 · Elevator, Spar/RibSDR A6WA202110217921Skin · dentedAFT FUSELAGE SKIN HAS 3 DENTS AT FS640.00 + 8Ï¿½ RH STR24 + 1.75Ï¿½, FS640.00 + 9Ï¿½ RH STR24 + 1.25Ï¿½ AND FS640.00 + 10Ï¿½ RH STR24 + 2.70Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN HAS 3 DENTS AT FS640.00 + Sep 20, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110187907None · gougedRH ELEVATOR HAS A GOUGE AT INBOARD PCU FORWARD ATTACHMENT FITTING LOWER SIDE BETWEEN 1 AND RIB 2 RHS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE AT INBOARD PCU, FORWARD ATTACHMENT FITTING LOWER SIDE BETWEEN 1 AND RIB 2 RHS. GOUGE DIMENSION L = 0.40Sep 20, 2021 · N439AW · Cndair CL6002B19 · Elevator, Plate/SkinSDR A6WA202110187906Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS605.00 +2Ï¿½ AND LH STR23+2.5Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 +2Ï¿½ AND LH STR23+2.5Ï¿½. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 1.200Ï¿½ X W = 1.100Ï¿½ X DSep 20, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110187903Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS589.00 AND LH STR20+3Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS589.00 AND LH STR20+3Ï¿½. AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 9.00Ï¿½ X W = 0.600Ï¿½ X D = 0.016Ï¿½. PERFSep 20, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110187904Skin · corrodedCORROSION AND PITTING ON LH WING UPPER ACCESS FOR PANEL 540AT AT WS65.75. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION DAMAGE AT TWO PLACES ON LH WING UPPER ACCESS FOR PANEL 540AT AT WS65.75. DIMENSION P1- L = 3.800Ï¿½ X W = 0.4.0Ï¿½ X D = 0.194Ï¿½,Sep 19, 2021 · N439AW · Cndair CL6002B19 · Wing StructureSDR A6WA202110227924Skin · dentedTWO DENTS ON AFT FUSELAGE SKIN FS755.00 - 67.50 DATUM AND STR26L AND STR26R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED TWO DOUBLER REPAIRS TO THE AFT FUSELAGE SKIN AT FS755.00 - 67.50 DATUM AND STR26L AND STR26R. DENT DIMENSION LH S26 L= 2.300Ï¿½ X W = Sep 16, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202109017866Warning Message · false activationRECEIVED PAX DR WARNING CLIMBING THRU FL 330 PRESSURIZATION REMAINED NORMAL THROUGH FLIGHC/Q QRH DESCENDED TO 11,000 FT MSG CLEARED ON ITS OWN. AIRCRAFT REMOVED FROM SERVICE. INSPECTED PAX DOOR WIRING, CONNECTORS AND SPLICES FOUND ALL TO BE TIGHT AND NO DEAug 31, 2021 · N439AW · Cndair CL6002B19 · Door Warning SystemSDR A6WA202110297941None · noneH/STAB PCU ACCESS PANEL #332AB (P/N: 601R23052-11) HAS 3EACH DAMAGED HOLES. DIMENSIONS: HOLE #1: .195" X .258"; HOLE #2: .310" X .220"; HOLE #3: .195" DIA ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLES TO FOLLOWING DIMENSIONS: HOLE #1: .3685"; HOLE #2: .37Aug 27, 2021 · N439AW · Cndair CL6002B19 · Horizontal Stabilizer, Tab StructureSDR A6WA202110297942None · noneELONGATED HOLE COMMON TO H/STAB LHS LOWER DOUBLER (DWG 600-23044) AND RIB (DWG 601R23030) AT PCU ACCESS DOOR. HOLE DIMENSIONS AT DOUBLER ARE (P2) = .370" X .250. HOLE DIMENSIONS AT RIB ARE (P1) = .370" X .370. ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLAug 27, 2021 · N439AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR A6WA202103027672Rvdt · faultedRECIEVED STEERING INOP CAUTION MSG IN FLIGHT C/W QRH AND MSG PERSISTS. ***AIRCRAFT REMOVED FROM SERVICE*** R&R LFT NLG RVDT IAW AWAC SUP 15-177A OPS TEST OF NWS GOOD P/N OFF:16735-109,S/N OFF:NSN/447/1,P/N ON:3A1252D,S/N ON:D0796. Feb 25, 2021 · N439AW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA2020022547201Bulkhead Web · crackedAFT PRESSURE BULKHEAD AT FS 621.00 & LBL 27.5 WL 133-135 HAS A FAILED INDICATION APPROXIMATELY 2" LONG IAW CRJ 200 NDT MANUAL PART 1 57-20-06 REV 41. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED DAMAGED AREA ON APB REF CRJ 200 REO 601-53-61-1541 REV F.Feb 18, 2020 · N439AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2020022647202Cable · damagedL/H VERTICAL AUTO PILOT SERVO CABLE IS RUSTED AROUND SERVO BOTTOM. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ELEVATOR SERVO P/N 822-0260-001 REF CRJ 200 AMM. REMOVED AND REPLACE L/H ELEVATOR FUSELAGE CABLE P/N 601R90020-79 FOR BROKEN STRANDS REF Feb 16, 2020 · N439AW · Cndair CL6002B19 · Autopilot ComputerSDR A6WA2019083046811Warning Message · illuminatedDURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW NOTIFIED DISPATCH, DECLARED AN EMERGENCY AND DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO INJURIES OR ADVERSE PASSENGER REACTION.Aug 29, 2019 · N439AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2019082746805Warning Message · illuminatedCLIMBING OUT OF 17,000 FLAP FAIL CAUTION MESSAGE, C/W QRH, MESSAGE REMAINED, LANDED FLAPS 0, NORMAL T/D, NORMAL LANDING, PERFORED FLAP RESET PROCEDURE IAW 98-18G BOX 12,Aug 25, 2019 · N439AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201908146790Warning Message · illuminatedFLAP FAIL CAUTION MESSAGE IN FLIGHT FLAPS INDICATED 0 DEGREES PERFORMED FLAP REST PROCEDURE IAW AWAC SUP 98-18G BOX 12 ABOUT 20 MINS AFTER DEPARTURE, ABOUT 17000 FEET, THE PLANE SHOWED A FLAPS FAIL CAUTION MESSAGE. THE FO WAS FLYING AT THE TIME. WE PERFORMED Aug 2, 2019 · N439AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2019073046760Warning System · activatedON APPROACH TO GSO THE FLIGHT RECEIVED AN ANTI-SKID OUTBOARD CAUTION MESSAGE. THE CREW DID A GO-A-ROUND AND HAD THE EQUIPMENT STANDING BY BUT DID NOT DECLARE AN EMERGENCY. FLIGHT LANDED AND TAXIED TO THE GATE WITH OUT INCIDENT. 3869 - RECEIVED ANTI-SKID OUTBOJul 27, 2019 · N439AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA2019060646646Unknown · malfunctioned3884 STAB AND MACH TRIM WOULD NOT STAY ENGAGED. FAILED 8 TIMES. RAN QRH EACH TIME. WOULD STAY ENGAGED ABOUT 25 SECONDS.Jun 4, 2019 · N439AW · Cndair CL6002B19 · Speed-Attitude Correction SystemSDR A6WA2018021645632Skin · dentedDENT ON LOWER FUSELAGE SKIN AT FS605.00, STGR24L.Feb 15, 2018 · N439AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
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