# Service difficulty reports: N439AW

A list on [N439AW](https://openairdocs.org/aircraft/N439AW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 186 reports

- [SDR A6WA202502058858](https://openairdocs.org/sdr/A6WA202502058858.md): Skin · dented · Feb 5, 2025 · N439AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RH 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.
- [SDR A6WA202412178846](https://openairdocs.org/sdr/A6WA202412178846.md): Shutoff Valve · malfunctioned · Dec 17, 2024 · N439AW · Cndair CL6002B19 · Air Distribution System
  > WHILE 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
- [SDR A6WA202407058774](https://openairdocs.org/sdr/A6WA202407058774.md): Bracket · damaged · Jul 4, 2024 · N439AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > 6060 - 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
- [SDR A6WA202405088743](https://openairdocs.org/sdr/A6WA202405088743.md): Strut · low pressure · May 8, 2024 · N439AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR 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.
- [SDR A6WA202310228662](https://openairdocs.org/sdr/A6WA202310228662.md): Unknown · unknown · Oct 22, 2023 · N439AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR 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 MEL
- [SDR A6WA202308238649](https://openairdocs.org/sdr/A6WA202308238649.md): Wheel · damaged · Aug 23, 2023 · N439AW · Cndair CL6002B19 · Tire
  > ON 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
- [SDR A6WA202307108638](https://openairdocs.org/sdr/A6WA202307108638.md): Unknown · unknown · Jul 10, 2023 · N439AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON 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 M
- [SDR A6WA202306128630](https://openairdocs.org/sdr/A6WA202306128630.md): Sensor · unknown · Jun 12, 2023 · N439AW · Cndair CL6002B19 · Flight Control System
  > FLAPS 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.
- [SDR A6WA202212158415](https://openairdocs.org/sdr/A6WA202212158415.md): Connector · broken · Dec 15, 2022 · N439AW · Cndair CL6002B19 · Flight Control System Wiring
  > WHILE 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.
- [SDR A6WA202210258411](https://openairdocs.org/sdr/A6WA202210258411.md): Detector · faulted · Dec 14, 2022 · N439AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > LAP 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.
- [SDR A6WA202111227983](https://openairdocs.org/sdr/A6WA202111227983.md): Wire · failed · Nov 21, 2021 · N439AW · Cndair CL6002B19 · Instrument System Wiring
  > DURING 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 AND
- [SDR A6WA202109307929](https://openairdocs.org/sdr/A6WA202109307929.md): None · corroded · Sep 30, 2021 · N439AW · Cndair CL6002B19 · Doors
  > FLIGHT 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 AT
- [SDR A6WA202110227926](https://openairdocs.org/sdr/A6WA202110227926.md): None · corroded · Sep 30, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > 16 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 + 9
- [SDR A6WA202110227925](https://openairdocs.org/sdr/A6WA202110227925.md): None · corroded · Sep 30, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > 2 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
- [SDR A6WA202110217922](https://openairdocs.org/sdr/A6WA202110217922.md): None · dented · Sep 30, 2021 · N439AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > DENT 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
- [SDR A6WA202109297928](https://openairdocs.org/sdr/A6WA202109297928.md): None · corroded · Sep 29, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > CORROSION 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= 0.900Ï
- [SDR A6WA202111037950](https://openairdocs.org/sdr/A6WA202111037950.md): None · none · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CRACK 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 S
- [SDR A6WA202111017947](https://openairdocs.org/sdr/A6WA202111017947.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > SEAT 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 PERFOR
- [SDR A6WA202111017948](https://openairdocs.org/sdr/A6WA202111017948.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > SEAT 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 A
- [SDR A6WA202111017949](https://openairdocs.org/sdr/A6WA202111017949.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > SEAT 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 A
- [SDR A6WA202110197914](https://openairdocs.org/sdr/A6WA202110197914.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > SEAT 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 IA
- [SDR A6WA202110197912](https://openairdocs.org/sdr/A6WA202110197912.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > SEAT 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 PE
- [SDR A6WA202110197913](https://openairdocs.org/sdr/A6WA202110197913.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > SEAT 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
- [SDR A6WA202110187911](https://openairdocs.org/sdr/A6WA202110187911.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > SEAT 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
- [SDR A6WA202110187910](https://openairdocs.org/sdr/A6WA202110187910.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > SEAT 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 PERF
- [SDR A6WA202110187909](https://openairdocs.org/sdr/A6WA202110187909.md): Seat Track · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > SEAT 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 IAW
- [SDR A6WA202110187908](https://openairdocs.org/sdr/A6WA202110187908.md): None · corroded · Sep 27, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > SEAT 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-
- [SDR A6WA202110157902](https://openairdocs.org/sdr/A6WA202110157902.md): Fitting · gouged · Sep 25, 2021 · N439AW · Cndair CL6002B19 · Doors
  > PAX 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 WOR
- [SDR A6WA202110067895](https://openairdocs.org/sdr/A6WA202110067895.md): None · corroded · Sep 25, 2021 · N439AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > CORROSION 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 P
- [SDR A6WA202111017946](https://openairdocs.org/sdr/A6WA202111017946.md): None · gouged · Sep 24, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > GOUGE 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 DIMENS
- [SDR A6WA202109227935](https://openairdocs.org/sdr/A6WA202109227935.md): Antenna · corroded · Sep 22, 2021 · N439AW · Cndair CL6002B19 · Navigation System
  > GPS 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 PERFOR
- [SDR A6WA202110217920](https://openairdocs.org/sdr/A6WA202110217920.md): Fitting · gouged · Sep 20, 2021 · N439AW · Cndair CL6002B19 · Elevator, Spar/Rib
  > GOUGE 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= 0.700
- [SDR A6WA202110217921](https://openairdocs.org/sdr/A6WA202110217921.md): Skin · dented · Sep 20, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT 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 +
- [SDR A6WA202110187907](https://openairdocs.org/sdr/A6WA202110187907.md): None · gouged · Sep 20, 2021 · N439AW · Cndair CL6002B19 · Elevator, Plate/Skin
  > RH 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 = 0.40
- [SDR A6WA202110187906](https://openairdocs.org/sdr/A6WA202110187906.md): Skin · dented · Sep 20, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT 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 D
- [SDR A6WA202110187903](https://openairdocs.org/sdr/A6WA202110187903.md): Skin · dented · Sep 20, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT 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. PERF
- [SDR A6WA202110187904](https://openairdocs.org/sdr/A6WA202110187904.md): Skin · corroded · Sep 19, 2021 · N439AW · Cndair CL6002B19 · Wing Structure
  > CORROSION 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,
- [SDR A6WA202110227924](https://openairdocs.org/sdr/A6WA202110227924.md): Skin · dented · Sep 16, 2021 · N439AW · Cndair CL6002B19 · Fuselage Structure (General)
  > TWO 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 =
- [SDR A6WA202109017866](https://openairdocs.org/sdr/A6WA202109017866.md): Warning Message · false activation · Aug 31, 2021 · N439AW · Cndair CL6002B19 · Door Warning System
  > RECEIVED 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 DE
- [SDR A6WA202110297941](https://openairdocs.org/sdr/A6WA202110297941.md): None · none · Aug 27, 2021 · N439AW · Cndair CL6002B19 · Horizontal Stabilizer, Tab Structure
  > H/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:.37
- [SDR A6WA202110297942](https://openairdocs.org/sdr/A6WA202110297942.md): None · none · Aug 27, 2021 · N439AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > ELONGATED 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 HOL
- [SDR A6WA202103027672](https://openairdocs.org/sdr/A6WA202103027672.md): Rvdt · faulted · Feb 25, 2021 · N439AW · Cndair CL6002B19 · Landing Gear Steering System
  > RECIEVED 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.
- [SDR A6WA2020022547201](https://openairdocs.org/sdr/A6WA2020022547201.md): Bulkhead Web · cracked · Feb 18, 2020 · N439AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT 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.
- [SDR A6WA2020022647202](https://openairdocs.org/sdr/A6WA2020022647202.md): Cable · damaged · Feb 16, 2020 · N439AW · Cndair CL6002B19 · Autopilot Computer
  > L/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
- [SDR A6WA2019083046811](https://openairdocs.org/sdr/A6WA2019083046811.md): Warning Message · illuminated · Aug 29, 2019 · N439AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING 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.
- [SDR A6WA2019082746805](https://openairdocs.org/sdr/A6WA2019082746805.md): Warning Message · illuminated · Aug 25, 2019 · N439AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CLIMBING 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,
- [SDR A6WA201908146790](https://openairdocs.org/sdr/A6WA201908146790.md): Warning Message · illuminated · Aug 2, 2019 · N439AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP 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
- [SDR A6WA2019073046760](https://openairdocs.org/sdr/A6WA2019073046760.md): Warning System · activated · Jul 27, 2019 · N439AW · Cndair CL6002B19 · Brake Anti-Skid Section
  > ON 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 OUTBO
- [SDR A6WA2019060646646](https://openairdocs.org/sdr/A6WA2019060646646.md): Unknown · malfunctioned · Jun 4, 2019 · N439AW · Cndair CL6002B19 · Speed-Attitude Correction System
  > 3884 STAB AND MACH TRIM WOULD NOT STAY ENGAGED. FAILED 8 TIMES. RAN QRH EACH TIME. WOULD STAY ENGAGED ABOUT 25 SECONDS.
- [SDR A6WA2018021645632](https://openairdocs.org/sdr/A6WA2018021645632.md): Skin · dented · Feb 15, 2018 · N439AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON LOWER FUSELAGE SKIN AT FS605.00, STGR24L.

Next page: https://openairdocs.org/aircraft/N439AW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N439AW/reports

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