# Service difficulty reports: N432AW

A list on [N432AW](https://openairdocs.org/aircraft/N432AW.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 · 229 reports

- [SDR A6WA202206208193](https://openairdocs.org/sdr/A6WA202206208193.md): Engine · overtemp · Jun 20, 2022 · N432AW · Cndair CL6002B19 · Engine Temperature Indicating System
  > AT APROX 80 KTS THE RH ITT WENT RED LINE AT 900 DEG PLUS. REDUCED THROTTLE TO IDLE, ABORTED TO. RH ENG ITT RETURNED TO NORMAL IAT IDLE. BTMS READ 9557. INTERROGATED MDC NO EXCEEDANACES SHOWN THIS DATE. ***AIRCRAFT REMOVED FROM SERVICE *** C/W ENGINE INSPECT
- [SDR A6WA202203288156](https://openairdocs.org/sdr/A6WA202203288156.md): None · gouged · Mar 28, 2022 · N432AW · Cndair CL6002B19 · Doors
  > IAD MX FOUND TWO GOUGES IN THE CARGO DOOR OUTER SKIN UPPER EDGE. AIRCRAFT WAS FERRIED TO DAY FOR REPAIR. OUTER SKIN WAS REPAIRED WITH REO 601R-52-31-366. DAMAGE WAS MOST LIKELY CAUSED BY INCORRECT HARDWARE INSTALLED IN THE CARGO LINERS ABOVE THE DOOR. WHEN
- [SDR A6WA202111157968](https://openairdocs.org/sdr/A6WA202111157968.md): Doubler · damaged · Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > LH WINGLET DOUBLER PN 600-10380-59 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET DOUBLER PN 600-10380-59, REF CRJ200 SRM 57-31-31 REV 38, PG6, FIGURE 1, SHT 2, ITEM 33, MATERIAL 0.071Ï¿½ CLAD 202
- [SDR A6WA202111157964](https://openairdocs.org/sdr/A6WA202111157964.md): Strap · damaged · Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > LH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 6, MATERIAL 0.071Ï¿½ CLAD
- [SDR A6WA202111157965](https://openairdocs.org/sdr/A6WA202111157965.md): Strap · damaged · Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > LH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 3, MATERIAL 0.040Ï¿½ CLAD 20
- [SDR A6WA202111157966](https://openairdocs.org/sdr/A6WA202111157966.md): Strap · damaged · Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > LH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 8, MATERIAL 0.040Ï¿½ CLAD 20
- [SDR A6WA202111157967](https://openairdocs.org/sdr/A6WA202111157967.md): Doubler · damaged · Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > LH WINGLET DOUBLER PN 600-10380-63 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET DOUBLER PN 600-10380-63, REF CRJ200 SRM 57-31-31 REV 38, PG6, FIGURE 1, SHT 2, ITEM 34, MATERIAL 0.071Ï¿½ CLAD 202
- [SDR A6WA202111057975](https://openairdocs.org/sdr/A6WA202111057975.md): None · corroded · Nov 5, 2021 · N432AW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON BRACKET ASSEMBLY COMMON TO PASSENGER DOOR SURROUND STRUCTURE FS 318.00 LBL 40. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON BRACKET ASSY 601R31527-149 AT FS 318.00 AT 4 EACH LOCATIONS. (P1) 2.100L X 1.200W X.008D (P2) 2.5L X
- [SDR A6WA202111197974](https://openairdocs.org/sdr/A6WA202111197974.md): None · corroded · Nov 5, 2021 · N432AW · Cndair CL6002B19 · Doors
  > CORROSION FOUND ON FLOOR STRUCTURE COMMON TO PASSENGER DOOR SURROUND STRUCTURE AT FS 333.00 TO FS 349.00 LBL 36 TO LBL 40. ***AIRCRAFTY REMOVED FROM SERVICE*** BLENDED CORROSION ON BRACKET ASSY 601R31527-149 AT FS 333.00 AT 4 EACH LOCATIONS. (P1) 2.100L X 1.
- [SDR A6WA202111197977](https://openairdocs.org/sdr/A6WA202111197977.md): None · dented · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE.600"L X.500"W X.025"D AT FS 621, 3.7" O/B OF RBL 36.20, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES:.250"L X.050"W X.011"D. CUTOUT DAMAGED AREA
- [SDR A6WA202111227979](https://openairdocs.org/sdr/A6WA202111227979.md): None · corroded · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > CORROSION DAMAGE COMMON TO L/H WING ACCESS PANEL #540AT AT LOWER WING PLANK LAND AROUND ENTIRE AREA OF LAND. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON LOWER WING PLANK LAND COMMON TO L/H WING ACCESS PANEL #540AT. BLEND DIMENSIONS ARE 19.50"L X
- [SDR A6WA202111197978](https://openairdocs.org/sdr/A6WA202111197978.md): None · dented · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE.500"L X.300"W X.015"D AT FS 621, LBL 9.5 TO LBL 18.00, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES:.250"L X.050"W X.013"D. CUTOUT DAMAGED AREA
- [SDR A6WA202111197976](https://openairdocs.org/sdr/A6WA202111197976.md): None · dented · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD HAS DENT.400"L X.300"W X.010"D AT FS 621 IN BETWEEN LBL 27.50 AND LBL 36.20 AND 1.70" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** DRESSED BACK DENT ON AFT PRESSURE BULKHEAD TO ORIGINAL CONTOUR. HFEC WAS PERFORMED AT REWORK AR
- [SDR A6WA202111127963](https://openairdocs.org/sdr/A6WA202111127963.md): Doubler · damaged · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > RH WINGLET INNER SKIN LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET INNER SKIN LOWER STRAP PN 600-15108. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. A
- [SDR A6WA202111127962](https://openairdocs.org/sdr/A6WA202111127962.md): Doubler · damaged · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > RH WINGLET DOUBLER PN 600-10388-60 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET DOUBLER PN 600-10388-60. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS W
- [SDR A6WA202111127961](https://openairdocs.org/sdr/A6WA202111127961.md): Strap · damaged · Nov 4, 2021 · N432AW · Cndair CL6002B19 · Wing Structure
  > RH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** RH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388 HAS SEVERAL TOOL MARKS. BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET LOWER OUTBOARD FAIR
- [SDR A6WA202111227980](https://openairdocs.org/sdr/A6WA202111227980.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT HAS 2EA DENTS LOCATED ON R/H FUSELAGE SKIN EXTERIOR BETWEEN FS 589+5 TO FS 589+8 JUST BELOW S25R. DENT DIMENSIONS (D1) 1.100L X.900W X.003D (D2) 1.100L X.900W X.009D. (P1) AND (P2) ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38.
- [SDR A6WA202111227981](https://openairdocs.org/sdr/A6WA202111227981.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > AIRCRAFT HAS OUTWARD DENT ON R/H FUSELAGE SKIN EXTERIOR AT FS 379.00 +3 AT S18R+4. DIMENSIONS =.200"L X.100"W X.003"D. DENT NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ********AIRCRAFT REMOVED FROM SERVICE*********** PERFORMED CUTOUT (.400
- [SDR A6WA202111227982](https://openairdocs.org/sdr/A6WA202111227982.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT R/H SKIN EXTERIOR HAS 5 EACH DENTS AT FS 589.00 TO FS 605.00 AND S24R - S25R. DENT DIMENSIONS ARE: (P1).500L X.400W X.006D; (P2).450L X.400W X.004D; (P3).200L X.200W X.001D; (P4).350L X.200W X.001D; (P5).350L X.300W X.003D. EVALUATED DE
- [SDR A6WA202111517971](https://openairdocs.org/sdr/A6WA202111517971.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENTS (11 TOTAL) ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED 11 DENTS ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. DENTS DIMENSION: FS654.50 Ï¿½ FS672.2 AND S22R Ï¿½ S23R: P1= L =
- [SDR A6WA202111217960](https://openairdocs.org/sdr/A6WA202111217960.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R DENT DIMENSIONS P1- L = 1.200Ï¿½ X W = 0.900Ï¿½X D = 0.006Ï¿½. PERFORMED HFEC W
- [SDR A6WA202111117959](https://openairdocs.org/sdr/A6WA202111117959.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSIONS P1- L = 0.900Ï¿½ X W =
- [SDR A6WA202111107956](https://openairdocs.org/sdr/A6WA202111107956.md): Skin · dented · Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT TO RE-FORM ORIGINAL CONTOUR ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. DENT DIMENSION L = 0.500Ï¿½ X W = 0.400Ï¿½ X D = 0.008Ï¿½. P
- [SDR A6WA202110207987](https://openairdocs.org/sdr/A6WA202110207987.md): Web · cracked · Oct 20, 2021 · N432AW · Cndair CL6002B19 · Doors
  > PASSENGER DOOR HAS CRACK ON INNER WEB AT FS 338.9 DOOR HAS EXISTING REPAIR IAW GREO 601R-52-11-402 REV H. ********************AIRCRAFT REMOVED FROM SERVICE*********************** EXTENDED CUTOUT ON INNER WEB PN:601R31902-537 AT FS 338.9 TO 13.300"L X 6.800"W
- [SDR A6WA202110207986](https://openairdocs.org/sdr/A6WA202110207986.md): None · gouged · Oct 20, 2021 · N432AW · Cndair CL6002B19 · Doors
  > PASSENGER DOOR ROLLER BRACKET PN: 600-31471-9 HAS A GOUGE 0.400"L X 0.165"W X 0.020"D ON OUTSIDE EDGE OF BRACKET. ***************AIRCRAFT REMOVED FROM SERVICE******************* BLENDED THE DAMAGE TO A SMOOTH CONTOUR. HFEC PERFORMED WITH NO INDICATIONS. ROTO
- [SDR A6WA202111247985](https://openairdocs.org/sdr/A6WA202111247985.md): Web · cracked · Oct 20, 2021 · N432AW · Cndair CL6002B19 · Doors
  > PASSENGER DOOR HAS A CRACK.375"L ON INNER WEB P/N:601R31902-537 AT FS 320 AT UPPER FORWARD CORNER. **************AIRCRAFT REMOVED FROM SERVICE********************** DURING INCORPORATION OF GENERIC REO 601R-52-11-402 REV H, HFEC INSPECTION FOUND CRA
- [SDR A6WA202012087452](https://openairdocs.org/sdr/A6WA202012087452.md): Angle · corroded · Dec 2, 2020 · N432AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > T CAP CORRODED BEYOND LIMITS AT FS 621 TO FS 559+112 LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TCAP AT FS 559+112 TO FS 621, IAW CRJ SRM 51-42-21 AND BOMBARDIER DWG 601R35031.
- [SDR A6WA2020031047221](https://openairdocs.org/sdr/A6WA2020031047221.md): Wire Harness · defective · Mar 8, 2020 · N432AW · Cndair CL6002B19 · Landing Gear System Wiring
  > DURING TAKE OFF CLIMB, WHEN SELECTING GEAR UP, RECEIVED NOSE GEAR DISAGREE WITHIN 6 SECONDS OF SELECTION. LH+RH GEAR INDICATED GEAR UP AND LACKED. NOSE GEAR WHITE IN TRANSIT. DECLARED EMERGENCY. LANDING WAS BELOW MAX LANDING WEIGHT @ 146 KNOTS.
- [SDR A6WA2019122347077](https://openairdocs.org/sdr/A6WA2019122347077.md): Transducer · malfunctioned · Dec 20, 2019 · N432AW · Cndair CL6002B19 · Hydraulic System, Main
  > PRESSURE INDICATOR ON HYD 1 FROM 200-1800 PSI. C/W QRH. QTY AND TEMPS NORMAL AT 15-20 DEG AND 60% QTY. NEVER RECEIVED LOW PRESS CAUTION. AIRCRAFT REMOVED FROM SERVICE R&R HYD SYS #1 PRESSURE TRANSDUCER. OPS CHECK GOOD.
- [SDR A6WA2019121047046](https://openairdocs.org/sdr/A6WA2019121047046.md): Selector Valve · abnormal · Dec 7, 2019 · N432AW · Cndair CL6002B19 · Landing Gear Selector
  > SUPPLIMENTAL INFORMATION, AT 170 KTS APROX 2200 FT AGL RECEIVED GEAR DISSAGREE WARNING ON GEAR EXTENSION. NLG SHOWS DOWN AND LOCKED. MLG SHOW UP AND LOCKED. PER QRH CYCLED GEAR HANDLE CONDITION PERSISTS. PER QRH PULLED MANUAL GEAR EXTENSION. ALL SHOW DOWN AND
- [SDR A6WA2019120647040](https://openairdocs.org/sdr/A6WA2019120647040.md): Sealant · loose · Dec 3, 2019 · N432AW · Cndair CL6002B19 · Flight Compartment Windows
  > SUPPLEMENTAL INFORMATION, AFTER TAKE-OFF, FIRST OFFICER'S WINDSHIELD SEALANT CAME LOOSE. STARTED MAKING LOUD SOUNDS AGAINST FIRST OFFICER'S WINDSHIELD THEN DEPARTED AIRCRAFT. MX INSPECTED AND FOUND FIRST OFFICER'S WINDSHIELD MISSING APPROXIMATELY 18" OF MOIS
- [SDR A6WA2019112647034](https://openairdocs.org/sdr/A6WA2019112647034.md): Support Beam · cracked · Nov 20, 2019 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT FS 621 BAGGAGE DOOR UPPER SUPPORT BEAM IS CRACKED AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT ANGLE FROM 2024 T-3.040" AND INSTALLED REFERENCE CRJ 200 SRM 51-42-20, 51-24-21, AND 53-61-23 REV 37.
- [SDR A6WA2019112647032](https://openairdocs.org/sdr/A6WA2019112647032.md): Bracket · cracked · Nov 19, 2019 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BRACKET ASSY AT FS 574.00 & S6L HAS A CRACK AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT BRACKET FROM 2024 T-3.050" REF CRJ 200 SRM 51-24-21 AND 53-61-15 REV 37. AND INSTALLED REF CRJ 200 SRM 51-42-21 AND 51-23-00 REV 37.
- [SDR A6WA2019112647033](https://openairdocs.org/sdr/A6WA2019112647033.md): Bracket · cracked · Nov 19, 2019 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BRACKET ASSY AT FS 621.00 & S6L IS CRACKED. AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT BRACKET FROM 2014 T-3.050" REF CRJ 200 SRM -51-24-21 AND 53-61-15 REV 37 AND INSTALLED REF CRJ 200 SRM 51-42-21 AND 51-23-00 REV 37.
- [SDR A6WA2019112047022](https://openairdocs.org/sdr/A6WA2019112047022.md): Structure · damaged · Nov 13, 2019 · N432AW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H O/B FLAP T/E DAMAGED 14" O/B FROM I/B CORNER. DAMAGE WAS INDUCED DURING MAINTENANCE. AIRCRAFT REMOVED FROM SERVICE REPAIRED DAMAGE ON R/H O/B FLAP T/E AT APPROX 14" O/B FROM I/B CORNER WITH A REPAIR DOUBLER THAT MEASURES 5.6" X 3.1" REF CRJ 200 SRM 57-53
- [SDR A6WA2019112247029](https://openairdocs.org/sdr/A6WA2019112247029.md): Fitting · cracked · Nov 8, 2019 · N432AW · Cndair CL6002B19 · Service Doors
  > FOUND CRACK ON MICRO SWITCH MOUNTING BRACKET INSTALLED ON THE SERVICE DOOR. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MOUNTING BRACKET ON R1 SERVICE DOOR REF CRJ 200 SRM 51-42-20 REV 37.
- [SDR A6WA2019112147027](https://openairdocs.org/sdr/A6WA2019112147027.md): Fitting · chafed · Nov 7, 2019 · N432AW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H WING O/B FOREFLAP / AFT FLAP FITTING WORN DUE TO SEIZED ROLLER.AT FZ 189.57. AIRCRAFT REMOVED FROM SERVICE BLENDED CHAFE DAMAGE AREA ON R/H WING O/B FLAP O/B FOREFLAP FITTING AND AFT FLAP FITTING IN AN AREA OF 4.2"L X.20"W X.005"D WITHIN LIMITS REF ASA
- [SDR A6WA2019112647035](https://openairdocs.org/sdr/A6WA2019112647035.md): Panel · cracked · Nov 6, 2019 · N432AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PANEL 433AB HAS A CRACK AIRCRAFT REMOVED FROM SERVICE REPLACED WITH SERVICEABLE PANEL 433AB REF CRJ200 SRM 52-41-02 REV 37.
- [SDR A6WA2019112047024](https://openairdocs.org/sdr/A6WA2019112047024.md): Hinge Fitting · chafed · Nov 4, 2019 · N432AW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H WING O/B FLAP HINGE BOX AT WS 264.00 HAS 2 AREAS OF CHAFING DAMAGE. DAMAGE AREA 1 IS TO THE I/B FLAP HINE ARM FITTING DWG 601R10910 WITH DAMAGE DIMENSIONS OF.20"L X.15"W X.032"D. DAMAGE 2 IS TO THE AFT SIDE PLATE DWG 601R10180 WITH DAMAGE DIMENSIONS OF
- [SDR A6WA2019081446789](https://openairdocs.org/sdr/A6WA2019081446789.md): Spoiler Sys · malfunctioned · Aug 13, 2019 · N432AW · Cndair CL6002B19 · Drag Control System
  > GROUND LIFT DUMP SYSTEM DID NOT DEPLOY ON INITIAL TOUCHDOWN CAUSING BOUNCE. DEPLOYED ON 2ND TOUCHDOWN. NO ASSOCIATED MSGS.
- [SDR A6WA2019061246657](https://openairdocs.org/sdr/A6WA2019061246657.md): Cabin Pressure · malfunctioned · Jun 11, 2019 · N432AW · Cndair CL6002B19 · Cabin Pressure Control System
  > DURING CLIMB, THE CABIN WOULD NOT PRESSURIZE. THE FLIGHT LEVELED OFF AND THE CREW RAN THE QRH. THE FLIGHT RETURNED TO ORD AND LANDED WITHOUT FURTHER ISSUES.
- [SDR A6WA2019030146448](https://openairdocs.org/sdr/A6WA2019030146448.md): Warning System · false activation · Feb 19, 2019 · N432AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMBOUT, RECIEVED NOSE DOOR WARNING MESSAGE AND GEAR DISAGREE WARNING MESSAGES, C/W QRH, MESSAGE CLEARED, THEN DIVERTED.
- [SDR A6WA2018052945853](https://openairdocs.org/sdr/A6WA2018052945853.md): Connector · unsecure · May 27, 2018 · N432AW · Cndair CL6002B19 · Oxygen System Wiring
  > DURING OPERATIONAL TEST OF PAX O2, PSU AT ROW 6CD FAILED TO DEPLOY. RESECURED CONNECTOR TO DEPLOY SOLENOID. SUBSEQUENT OPS TEST OF PAX O2 SYSTEM, AMM 35-20-00 PROVES GOOD.
- [SDR A6WA2017101645361](https://openairdocs.org/sdr/A6WA2017101645361.md): Frame · cracked · Oct 12, 2017 · N432AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333, OTBD OF STRINGER 0, FOUND CRACKED. REPLACED THE FRAME.
- [SDR A6WA2017101345356](https://openairdocs.org/sdr/A6WA2017101345356.md): Skin · chafed · Oct 12, 2017 · N432AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT WING UPPER INBD AFT TE TO BODY (APRON SKIN) HAS LARGE CHAFE AREA. REPAIRED
- [SDR A6WA2017101345360](https://openairdocs.org/sdr/A6WA2017101345360.md): Angle · corroded · Oct 11, 2017 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT ANGLES AT BS 409+128 TO 559, LBL 36 - 47 CORRODED. REPAIRED.
- [SDR A6WA2017101345359](https://openairdocs.org/sdr/A6WA2017101345359.md): Frame · cracked · Oct 11, 2017 · N432AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26L AND 26R. A.14 INCH CRACK WAS DISCOVERED DURING CORROSION REMOVAL. REPLACED.
- [SDR A6WA2017101145350](https://openairdocs.org/sdr/A6WA2017101145350.md): Floor Support · corroded · Oct 9, 2017 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN CABIN L1 DOOR CUT OUT LOWER SILL VERTICAL FLOOR SUPPORT IS CORRODED BS 310 - 349, LBL 42
- [SDR A6WA2017101145343](https://openairdocs.org/sdr/A6WA2017101145343.md): Stiffener · cracked · Oct 6, 2017 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)
  > STIFFENER CRACKED BEHIND PANEL 326ER.
- [SDR A6WA2017101345337](https://openairdocs.org/sdr/A6WA2017101345337.md): Support Angle · cracked · Oct 4, 2017 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL SUPPORT ANGLE COMMON WITH SKIN CRACKED AT BS 621 TO 625.3, STRINGER 15L.

Next page: https://openairdocs.org/aircraft/N432AW/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 = 'N432AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N432AW/reports

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