# Service difficulty reports: N437AW

A list on [N437AW](https://openairdocs.org/aircraft/N437AW.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 5 · 234 reports

- [SDR A6WA202406038759](https://openairdocs.org/sdr/A6WA202406038759.md): Ecu · unknown · Jun 3, 2024 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAP FAIL CAUTION MSG FLAPS WERE AT 0, AIRCRAFT REMOVED FROM SERVICE. R&R FECU IAW AMM 27-51 OPS CHECK GOOD
- [SDR A6WA202406028757](https://openairdocs.org/sdr/A6WA202406028757.md): Control Unit · faulted · Jun 2, 2024 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL AT FL190. RAN QRH PROCEDURE. AND MSG REMAINED. PREFOREMD FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE REF LP 353462-1, R&R OF FECU. OPS CHECK GOOD. REMOVED PLACARD AND FROM M
- [SDR A6WA202311138670](https://openairdocs.org/sdr/A6WA202311138670.md): Unknown · unknown · Nov 13, 2023 · N437AW · Cndair CL6002B19 · Accessory Compartment Doors
  > AFTER T/O OUT OF ORD, HEARD LOUD NOISE FROM NOSE OF AIRCRAFT. RH SIDE. ******AIRCRAFT REMOVED FROM SERVICE********* FOUND CREW O2 SERVICING DOOR OPEN ON ARRIVAL. VISUALLY INSPECTED DOOR AND LATCHES, NO DEFECTS AT THIS TIME. DOOR SECURES CLOSED.
- [SDR A6WA202308208648](https://openairdocs.org/sdr/A6WA202308208648.md): Unknown · unknown · Aug 20, 2023 · N437AW · Cndair CL6002B19 · Aircraft Fuel System
  > ON CLIMBOUT, RECEIVED FUEL IMBALANCED CAUTION MSG WITH LH QTY EXCEEDING RH QTY BY 800+LBS AUTO CROSSFLOW WOULD NOT COMMENCE INITIALLY, BUT LATER WORKED NORMAL RETURNED AC TO A BALANCED CONDITION. SINGLE ENGINE TAXI PRIOR TO TAKEOFF ON RH ENGINE WITH LH BOOST P
- [SDR A6WA202307158641](https://openairdocs.org/sdr/A6WA202307158641.md): Unknown · unknown · Jul 15, 2023 · N437AW · Cndair CL6002B19 · Landing Gear System
  > ON DEPARTURE UPON SELECTING GEAR UP RECIEVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING MSGS C/W QRH EXTENDED GEAR GEAR MSGS WENT AWAY AIRCRAFT REMOVED FROM SERVICE. INSTALLED NOSE AND MAIN GEAR LOCK PINS PER AMM SUP. 11-054A FOR M ACTION OF MEL 32-30-01. SEE
- [SDR A6WA202204068165](https://openairdocs.org/sdr/A6WA202204068165.md): Bulkhead · none · Apr 6, 2022 · N437AW · Cndair CL6002B19 · Aerodynamic Fairings
  > REAR PRESSURE BULKHEAD WEB REQUIRES MODIFICATION PER E17/003/453 ****AIRCRAFT REMOVED FROM SERVICE**** MODIFIED THE REAR PRESSURE BULKHEAD WEB FS 621.00 IAW GREO 601-53-61-1240 REV D
- [SDR A6WA202204068166](https://openairdocs.org/sdr/A6WA202204068166.md): Bulkhead · gouged · Apr 6, 2022 · N437AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD Z-MEMBER AT FS 621.00, CENTER, SHOWS DEEP GAUGE LOCATED AT THE TOP END. ****AIRCRAFT REMOVED FROM SERVICE**** REPAIRED BULKHEAD AFT VERTICAL STIFFENER AT FS 621.00 IAW EA# AWAC-CRJ253-01806
- [SDR A6WA202204058162](https://openairdocs.org/sdr/A6WA202204058162.md): Stiffener · cracked · Apr 5, 2022 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ANGLE STIFFENER AT FS 516, ON RH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE**** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON RH BL 45.00 IAW ED# AWAC-CRJ 253-01816
- [SDR A6WA202204058163](https://openairdocs.org/sdr/A6WA202204058163.md): Stiffener · cracked · Apr 5, 2022 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ANGLE STIFFENER AT FS 516, ON LH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE**** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON LH BL 45.00 IAW ED# AWAC-CRJ253-01817
- [SDR A6WA202105127774](https://openairdocs.org/sdr/A6WA202105127774.md): Bpsu · warning message · May 10, 2021 · N437AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION ON TAKEOFF, PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I BOX 12 FLAP RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. FOUND RT WING BRAKE AND POSITION SENSOR OUT OF RIG, AND RT WING POSITION 10 FLEX DRIVE WORN,
- [SDR A6WA202101287570](https://openairdocs.org/sdr/A6WA202101287570.md): Clamp · loose · Jan 27, 2021 · N437AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > JUST AFTER VR RECEIVED WING OVERHEAT WARNING MESSAGE, FOLLOWED BY ANTI-ICE DUCT WARNING MESSAGE. CW QRH MESSAGES CLEARED. RETURNED TO MKE. 14TH STAGE SOVS AND WING AND COWL AI VALVES WERE ALL SELECED ON. THE 10TH STAGE SOVS WERE CLOSED AT THE TIME. QRH AC
- [SDR A6WA202101227561](https://openairdocs.org/sdr/A6WA202101227561.md): Skin · corroded · Jan 20, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE TCAS ANTENNA MATING SURFACE FS 310, STGR 1R TO STGR 1L HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. BLENDED OUT DAMAGE ON TCAS ANTENNA MATING SURFACE FS 310, STGR 1R TO STGR 1L, P(1) 1.0L X 0.70W, P(2) 1.2L X 0.60W, P(3) 0.8L X 0.95W, P(4) 1.
- [SDR A6WA202101257564](https://openairdocs.org/sdr/A6WA202101257564.md): Flange · gouged · Jan 16, 2021 · N437AW · Cndair CL6002B19 · Aircraft Fuel System
  > FUEL PRESSURE BOX AFT UPPER FLANGE, INBOARD AND OUTBOARD CORNERS GOUGED BLEND OUT DAMAGE ON FUEL PRESSURE BOX AFT UPPER RT FLANGE, 0.390 L X 0.120 W X 0.045 D, REF REO 601R-28-20-044, REV A DATE: 2021-01-21. BLENDED OUT DAMAGE ON FUEL PRESSURE BOX AFT UPPER L
- [SDR A6WA202101217559](https://openairdocs.org/sdr/A6WA202101217559.md): Skin · dented · Jan 16, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPPER SURFACE OF FUSELAGE HAS DENT AT FS 596.00, STGR 3R AND STGR 4R. AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENT AT FS 596.00, STGR 3R AND STGR 4R, 1.7 L X 1.6 W X 0.057 D, FOUND TO BE OUT OF LIMITS FOR SHARP CREASES. IAW CRJ200 SRM 53-00-31, (REV 38). A
- [SDR A6WA202101257565](https://openairdocs.org/sdr/A6WA202101257565.md): Access Panel · cracked · Jan 15, 2021 · N437AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER PANEL 326AL AFT END BENT AND 1 EA DENT. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND MEASURED 1 (EA) DENT ON VERTICAL STABILIZER PANEL 326AL, 0.700 L X 0.500 W X 0.007 D, DENT FOUND TO BE WITHIN LIMITS, REF CRJ200 SRM 55-00-31 AND A.W. SU
- [SDR A6WA202101217558](https://openairdocs.org/sdr/A6WA202101217558.md): Channel · corroded · Jan 14, 2021 · N437AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT HAND WING AFT CHANNEL AT WS 53.60 HAS POSSIBLE CORROSION AROUND UPPER LIGHTNING HOLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT LT WS.53.60, REF CRJ200 SRM 51-21-06, (REV 38). REWORKED AREA MEASURES 1.7L X 1.0W, REF CRJ200 SRM 51-21-06, (REV
- [SDR A6WA202101217557](https://openairdocs.org/sdr/A6WA202101217557.md): Channel · corroded · Jan 14, 2021 · N437AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT HAND WING AFT CHANNEL AT WS 53.60 HAS POSSIBLE CORROSION ON INBOARD SURFACE. AIRCRAFT REMOVED FROM SERVICE. REMOVED ANGLE SUPPORT AND NUTPLATE AT RT WS 53.60, REF CRJ200 SRM 51-42-21 AND CRJ 200 SRM 51-45-00, (REV.38). REMOVED CORROSION AT (2 EA) LOCA
- [SDR A6WA202101217556](https://openairdocs.org/sdr/A6WA202101217556.md): Channel · corroded · Jan 14, 2021 · N437AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT HAND WING AFT CHANNEL AT WS 48.30 HAS POSSIBLE CORROSION ON INBOARD SURFACE. AIRCRAFT REMOVED FROM SERVICE. REMOVED NUTPLATE AT WS 48.30, REF CRJ200 SRM 51-45-00, (REV 38). REMOVED CORROSION AT (2 EA) LOCATIONS ON CHANNEL AT WS 48.30, REF CRJ200 SRM 5
- [SDR A6WA202101087520](https://openairdocs.org/sdr/A6WA202101087520.md): Bulkhead Web · cracked · Jan 8, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 103.43 TO WL 114.93 LENGTH 11.5'' BL 0.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM. L=12.0'' W=1.8'', REF BOMBARDIER REO 601R-53-61-1285 REV E DATED 2016-10-31. PERFORMED HFEC INSPECTI
- [SDR A6WA202101087516](https://openairdocs.org/sdr/A6WA202101087516.md): Bulkhead Web · cracked · Jan 8, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 126.88 TO WL 136.18 LENGTH 9.5'' BL 0.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM L=10.0'' W=1.85''. CUT OUT ON STRAP FOR REPAIR DIM L=7.0'' W=2.50'', REF BOMBARDIER REO 601R-53-61-128
- [SDR A6WA202101087519](https://openairdocs.org/sdr/A6WA202101087519.md): Bulkhead Web · cracked · Jan 8, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 131.98 TO WL 135.93 LENGTH 5.0'' RBL 18.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM L=4.9'' W=1.7''. CUT OUT ON STRAP FOR REPAIR DIM L=8.2'' W=2.5'', REF BOMBARDIER REO 601R-53-61-1285
- [SDR A6WA202101157546](https://openairdocs.org/sdr/A6WA202101157546.md): Floorbeam · corroded · Jan 7, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT STRUCTURES AT FS 599, LBL 28 TO LBL 42, AND RBL 28 TO RBL 42 HAND AND RT HAND BLENDED OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED RT HAND AND LT HAND FLOOR SUPPORT AT FS 599, LBL 28 TO LBL 42, AND RBL 28 TO RBL 42, IAW CRJ 200 SRM 51
- [SDR A6WA202101257566](https://openairdocs.org/sdr/A6WA202101257566.md): Angle · cracked · Jan 2, 2021 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR CROSS MEMBER GAPPED DUE TO FASTENER SWOLLEN BETWEEN STRUCTURES AT FUSELAGE STATION 559.00, LBL 8. AIRCRAFT REMOVED FROM SERVICE. UPON EVALUATION OF DAMAGE OF CROSS MEMBER AT FUSELAGE STATION 559.00, LBL 8. DAMAGE FOUND TO MEASURE 1.78 L X 0.620 W X 0.0
- [SDR A6WA202101157543](https://openairdocs.org/sdr/A6WA202101157543.md): Pressure Deck · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR PANEL AT FS 484.00 +9, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT FS 484.00 +9, LBL 429, LBL 42. REWORKED DIMENSIONS P(1) 0.5 L X 0.34 W, P(2) 1.0 L X 1.0 W, P(3) 0.59 L X 0.45 W, REF
- [SDR A6WA202012297521](https://openairdocs.org/sdr/A6WA202012297521.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 439.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE POSITIONS AT FS 439.00, LBL 42. REWORKED DIMENSIONS 2.2 L X 1.8 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORM
- [SDR A6WA202001137530](https://openairdocs.org/sdr/A6WA202001137530.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 461.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 461.00, LBL 42. REWORKED DIMENSIONS 0.6 L X 0.3 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMED HFEC IN
- [SDR A6WA202001137526](https://openairdocs.org/sdr/A6WA202001137526.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 409.00 +128 +11, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 409.00 +128 +11, LBL 42. REWORKED DIMENSIONS 0.720 L X 0.420 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-
- [SDR A6WA202001137535](https://openairdocs.org/sdr/A6WA202001137535.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 544.00, RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 544.00, RBL 42. REWORKED DIMENSIONS 1.1 L X 0.7 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMED HFEC PR
- [SDR A6WA202101137536](https://openairdocs.org/sdr/A6WA202101137536.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 473.15 TO FS 473.15 +5 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 473.15 TO FS 473.15 + 5 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.070'' L X
- [SDR A6WA202001137537](https://openairdocs.org/sdr/A6WA202001137537.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS. 484.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 484.00, LBL 42. REWORKED DIMENSIONS P(1) 1.260 L X 0.640 W, P(2) 1.220 L X 0.710 W, REF REO 601R-53-41-666 REV (C) DA
- [SDR A6WA202101137533](https://openairdocs.org/sdr/A6WA202101137533.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 461.00 + 9 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 + 9 AND LBL 36 TO LBL 42. BY BLENDING. BLENDED AREA MEASURED (P1) 2.330''L X 0.950''W (P2) 1.160''L X 0
- [SDR A6WA202101137523](https://openairdocs.org/sdr/A6WA202101137523.md): Floor Support · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PRESSURE FLOOR ANGLE FS 499.00 TO FS 513 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 499.00 TO FS 513 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 2.64''L X 1.11''W (P2) 1.
- [SDR A6WA202101137529](https://openairdocs.org/sdr/A6WA202101137529.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 449.85 AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 449.85 AND LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 2.780''L X 1.530''W (P2) 0.920''L X 0.340''W TOOL USED DIGITAL C
- [SDR A6WA202001137534](https://openairdocs.org/sdr/A6WA202001137534.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS. 513.00 TO FS. 513.00 + 5, RBL 36 TO RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513.00 TO FS 513.00 +5, RBL 36 TO RBL 42. REWORKED DIMENSIONS P(1) 3.0 L X 1.0 W, P(2) 1.
- [SDR A6WA202101137540](https://openairdocs.org/sdr/A6WA202101137540.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 439.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 439.00 RBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.00'' L X 0.720'' W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03/
- [SDR A6WA202101137539](https://openairdocs.org/sdr/A6WA202101137539.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 484.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 484.00 RBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.250'' L X 0.800'' W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03
- [SDR A6WA202101137525](https://openairdocs.org/sdr/A6WA202101137525.md): Floor Support · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON PRESSURE FLOOR ANGLE FS 544.00 +11 TO FS 559 +2 AND LBL 41 TO LBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 544.00 +11 TO FS 559 + 2 AND LBL 41 TO LBL 43. BY BLENDING. BLENDED AREA MEASURED 2.480'' L X 0.
- [SDR A6WA202101137527](https://openairdocs.org/sdr/A6WA202101137527.md): Pressure Deck · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON PRESSURE FLOOR PANEL AT NUT-PLATE FS 529.00 +10 AND LBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR PANEL AT NUT-PLATE FS 529.00 +10 AND LBL 43 BY BLENDING. BLENDED AREA MEASURED (P1) 1.530'' L X 0.630'' W (P2) 1.17
- [SDR A6WA202001137538](https://openairdocs.org/sdr/A6WA202001137538.md): Floor Support · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS 544 +11 TO FS 599, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 544 +11 TO FS 599, LBL 42. REWORKED DIMENSIONS 2.7 L X 1.5 W, REF REO 601R-53-41-666. REV (C) DATED 2012-1
- [SDR A6WA202101137531](https://openairdocs.org/sdr/A6WA202101137531.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 513.00 TO FS 513.00 +5 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 513.00 TO FS 513.00 +5 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.180'' L X 0
- [SDR A6WA202001137532](https://openairdocs.org/sdr/A6WA202001137532.md): Floor Support · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR ANGLE AT FS 499.00 TO FS 513.00, RBL 36 TO RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 499.00 TO FS 513.00, RBL 36 TO RBL 42. REWORKED DIMENSIONS P(1) 1.7 L X 1.0 W, P(2) 2.0 L X 0.6
- [SDR A6WA202101137542](https://openairdocs.org/sdr/A6WA202101137542.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 461.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 RBL 42.BY BLENDING. BLENDED AREA MEASURED (P1) 1.00''L X 1.700''W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03/20
- [SDR A6WA202101137541](https://openairdocs.org/sdr/A6WA202101137541.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON PRESSURE FLOOR ANGLE FS 461.00 +9 RBL 36 TO RBL 38. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 + 9 RBL 36 TO RBL 38 BY BLENDING. BLENDED AREA MEASURED (P1) 1.20''L X 0.796''W TOOL USED DIGITAL CALIPER S
- [SDR A6WA202001137524](https://openairdocs.org/sdr/A6WA202001137524.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 424.00+4, LBL 38 TO LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 424.00+4, LBL 38 TO LBL 42. REWORKED DIMENSIONS P (1) 0.4 L X 2.7 W, P(2) 0.76 L X 0.5, W P(3) 0.4 L X 0.3
- [SDR A6WA202001137528](https://openairdocs.org/sdr/A6WA202001137528.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 473.15 +5, RBL 36 TO RBL 38, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 473.15 +5, RBL 36 TO RBL 38. REWORKED DIMENSIONS 1.45 L X 0.55 W, REF REO 601R-53-41-666 REV (C) DATED 20
- [SDR A6WA202001137521](https://openairdocs.org/sdr/A6WA202001137521.md): Floorbeam · corroded · Dec 29, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR ANGLE AT FS 439.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE POSITIONS AT FS 439.00, LBL 42. REWORKED DIMENSIONS 2.2 L X 1.8 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORM
- [SDR A6WA202101257563](https://openairdocs.org/sdr/A6WA202101257563.md): Pressure Blkhd · cracked · Dec 1, 2020 · N437AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD SURFACE FS 621.00, WL 130.93 TO WL 133.93 CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED SPRING BRACKET AND CARGO DOOR TRACK AT REPAIR AREA, REF CRJ200 SRM 51-40-11, (REV 38) AND BOMBARDIER REO 601R-53-61-1541 DATED: 2020-12-06, (R
- [SDR A6WA2019121847064](https://openairdocs.org/sdr/A6WA2019121847064.md): Display · failed · Dec 16, 2019 · N437AW · Cndair CL6002B19 · Central Display
  > BOTH MFD FAILED AT 1000 FT AGL AIRCRAFT REMOVED FROM SERVICE REPLACED L MFD IAW AMM 31-61-01. OPS CK GOOD
- [SDR A6WA2019082846809](https://openairdocs.org/sdr/A6WA2019082846809.md): Warning Message · false activation · Aug 27, 2019 · N437AW · Cndair CL6002B19 · Brake Anti-Skid Section
  > THE CREW RECEIVED AN OUTBOARD ANTI SKID MESSAGE UPON LOWERING LANDING GEAR. THE CREW OPTED TO DIVERT TO MKE FOR A LONGER RUNWAY. FLIGHT LANDED NORMALLY, NO EMERGENCY DECLARED AND NO ADVERSE REACTION FROM PASSENGERS. SYSTEM WAS SUCCESSFULLY RESET ONCE THE AIRCR
- [SDR A6WA201904126552](https://openairdocs.org/sdr/A6WA201904126552.md): Warning Message · illuminated · Apr 10, 2019 · N437AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > INFLIGHT WITH WING ANTIICE ON IN NORMAL MODE, RECEIVED WING OVERHEAT WARNING. SUSPECT LEFT WING. C/W'D QRH & SELECTED WING ANTI-ICE OFF. MESSAGE CLEARED IMMEDIATELY. PER QRH, SELECTED WING ANTI-ICE TO STBY, THEN RECEIVED LEFT WING ANTI-ICE CAUTION & SYNOPTIC S

Next page: https://openairdocs.org/aircraft/N437AW/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 = 'N437AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N437AW/reports

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