# Service difficulty reports: N438AW

A list on [N438AW](https://openairdocs.org/aircraft/N438AW.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 · 217 reports

- [SDR A6WA202609018912](https://openairdocs.org/sdr/A6WA202609018912.md): Landing Gear · faulted · Sep 1, 2026 · N438AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > DURING CLIMB OUT AFTER GEAR RETRACTION AT A BOUGHT 8,000 FT, BEGAN HEARING A THUD NOISE COMING FROM NOISE AREA OF ACFT. LOWERED MLG & NOISE WENT AWAY, NOISE CAME BACK AFTER RETRACTED. MLG F/O NOTICED SLIGHT YAW MOTION AFTER LOWERING MLG FOR LANDING NOISE DID
- [SDR A6WA202608138907](https://openairdocs.org/sdr/A6WA202608138907.md): Flap System · failed · Aug 13, 2026 · N438AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION ON APPROACH C/W QRH. FLAPS FAILED AT 20 DEGREES. C/W FIM RESET PER AWA SUP 98-018I. MESSAGE REMAINS. AIRCRAFT REMOVED FROM SERVICE. REF 357150-1 FOR CORRECTIVE ACTION RESET FDU OPS TEST GOOD AND FLAPS OPS TEST GOOD.
- [SDR A6WA202606058893](https://openairdocs.org/sdr/A6WA202606058893.md): Proximity Sensor · false activation · Jun 12, 2026 · N438AW · Cndair CL6002B19 · Door Warning System
  > RIGHT EMERGENCY DOOR CAUTION MESSAGE AFTER TAKE OFF INTERMITTENTLY. DELTA P 1.4. AIRCRAFT REMOVED FROM SERVICE. VERIFIED EMERGENCY DOOR PUSH PLATE IS FLUSH AND THE DOOR IS CLOSED LATCHED AND LOCKED. REF 357128/2 FOR MEL. CLEANED RIGHT EMERGENCY DOOR PROXIM
- [SDR A6WA202501198853](https://openairdocs.org/sdr/A6WA202501198853.md): Pdu · failed · Jan 19, 2025 · N438AW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > RECEIVED FLAP FAIL CAUTION MSG ON APPROACH TO LAND WHEN SELECTING FLAPS 30 FROM 20. FLAPS FAILED AT 20. FLAPS WER ON MEL. AIRCRAFT REMOVED FROM SERVICE. R & R FLAP PDU IAW AMM 27-52-01 FLAP PDU OPS TEST GOOD.
- [SDR A6WA202501098851](https://openairdocs.org/sdr/A6WA202501098851.md): Wheel · unknown · Jan 9, 2025 · N438AW · Cndair CL6002B19 · Wheel/Ski/Float
  > UPON APPLYING TAKE-OFF POWER, AIRCRAFT YAWED HARD TO THE RIGHT, FULL LEFT RUDDER WOULD NOT COUNTERACT YAW. REJECTED TO PERFORMED. ON TAXI BACK TO HANGAR AC YAWED RIGHT WITH NO RUDDER / TILLER INPUT. BTMS SHOWED 2,1,1,1. AIRCRAFT REMOVED FROM SERVICE. REF LP
- [SDR A6WA202407308784](https://openairdocs.org/sdr/A6WA202407308784.md): Idg · faulted · Jul 30, 2024 · N438AW · Cndair CL6002B19 · AC Generator-Alternator
  > ABORTED TAKE OFF DUE TO IDG 2 CAUTION MSG. CAUTION MSG CLEARED WHEN POWER BROUGHT BACK TO IDLE. QRH NOT PERFORMED. AIRCRAFT REMOVED FROM SERVICE. C/W M ACTION FOR MEL 24-11-01-01. REF 365898-3 FOR MEL IN WORK. REFERENCE WORK ORDER 337826 MAINTENANCE WORKC
- [SDR A6WA2024031198724](https://openairdocs.org/sdr/A6WA2024031198724.md): Skin · dented · Mar 8, 2024 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENTS ON RH FUSELAGE LOW PRESSURE GROUND AIR CONDITIONING CONNECTION. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED REPAIR OF AFT LOWER FUSELAGE SKIN AT FS 574.0 TO FS621 BETWEEN STR 20R TO 24L IAW REO 601R-53-61-8143. REV DATED 2024-03-06. HFEC ACCOMPLISHED,
- [SDR A6WA202403088723](https://openairdocs.org/sdr/A6WA202403088723.md): Skin · dented · Mar 7, 2024 · N438AW · Cndair CL6002B19 · Wing, Plate/Skin
  > DENTS ON R/H WING OUTBOARD LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED R/H WING OUTBOARD LEADING EDGE ASSY REF AMM 57-41-01 REV 66. REMOVED AND REPLACED LEADING EDGE SKIN REF CRJ200 SRM 51-40-11 REV 39.
- [SDR A6WA202402098714](https://openairdocs.org/sdr/A6WA202402098714.md): Doubler · cracked · Feb 9, 2024 · N438AW · Cndair CL6002B19 · Passenger/Crew Doors
  > 50033 334403 452-830-606 - 70HRS PAX DOOR AFT ANGLE IS CRACKED AT PULL IN CAN AREA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DOUBLER PULL IN CAN WITH PN 601R318094-2. IAW CRJ200 SRM 51-42-00, AND 51-42-13 REV 39 WORK PERFORMED UNDER AERSALE
- [SDR A6WA202203108128](https://openairdocs.org/sdr/A6WA202203108128.md): Strut · discharged · Mar 10, 2022 · N438AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > INFLIGHT RECV'D GEAR DISAGREE AND NOSE DOOR WARNING MESSAGES. ALSO RECV'D WOW INPUT AND NOSE WHEEL STEERING CAUTION MESSAGES. ALONG WITH WOW OUTPUT STATUS MESSAGE. NOSE GEAR DID NOT RETRACT. C/W QRH. LANDING GEAR EXTENDED AND ALL MESSAGES EXTINGUISHED. *** A
- [SDR A6WA202202168104](https://openairdocs.org/sdr/A6WA202202168104.md): Bracket · none · Feb 2, 2022 · N438AW · Cndair CL6002B19 · Nacelle/Pylon Structure
  > NUMBER 1 ENGINE (ESN801422) NOSE COWL SUPPORT BRACKET IS LOOSE INBOARD SIDE OF ENGINE. ***AIRCRAFT REMOVED FROM SERVICE*** INTERIM REPAIR - VERIFIED NUMBER 1 ENGINE NOSE COWL SUPPORT BRACKET P/N 228-50082-145 HAS NOT CAUSED DAMAGE TO SURROUNDING STRUCTURE.
- [SDR A6WA202202218112](https://openairdocs.org/sdr/A6WA202202218112.md): Aileron · corroded · Jan 17, 2022 · N438AW · Cndair CL6002B19 · Aileron Tab Control System
  > LH WING AILERON PN CC670-13000-1 HAS INTERNAL STRUCTURE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH WING AILERON PN CC670-13000-1, SN 7693. PERFORMED RIGGING CHECK AND OPERATIONAL TESTS OF THE FLIGHT CONTROL SYSTEM. ALL WORK WITHI
- [SDR A6WA202201168110](https://openairdocs.org/sdr/A6WA202201168110.md): Beam · damaged · Jan 16, 2022 · N438AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > CABIN FLOOR BEAM SUPPORT P/N 601R31118-127 AT FS559.00 AND BL0.0 HAS TOOL SET MARKS ON UPPER HORIZONTAL SURFACE. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY DAMAGED SECTION OF BEAM AT FS559.00 AND BL0.0 AND REPLACED WITH FLOOR BEAM SUPPORT P/N 601R31118-12
- [SDR A6WA202202178105](https://openairdocs.org/sdr/A6WA202202178105.md): None · corroded · Jan 15, 2022 · N438AW · Cndair CL6002B19 · Wing Structure
  > PITTING CORROSION ON LH WING UPPER SKIN LANDING FOR PANEL 540AT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE ON LH WING UPPER SKIN LANDING P/N 601R10042-7 FOR PANEL 540AT. PERFORMED HFEC WITH NO INDICATIONS. PERFORMED ROTO PEEN TO REWORKED AREAS. R
- [SDR A6WA202202148101](https://openairdocs.org/sdr/A6WA202202148101.md): Fitting · gouged · Jan 15, 2022 · N438AW · Cndair CL6002B19 · Elevator, Plate/Skin
  > LH HORIZONTAL STABILIZER HINGE FITTING HAS DAMAGE IN TWO PLACES AT LBL55.8865. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE ON LH STABILIZER HINGE FITTING DIMENSION P1- L= 0.700Ï¿½ X W= 0.200Ï¿½ X D= 0.012Ï¿½, P2- L= 1.100Ï¿½ X W= 0.200Ï¿½ X D= 0
- [SDR A6WA202202148100](https://openairdocs.org/sdr/A6WA202202148100.md): Fitting · gouged · Jan 15, 2022 · N438AW · Cndair CL6002B19 · Elevator, Plate/Skin
  > LH ELEVATOR HINGE FITTING HAVE DAMAGE ON INBOARD AND OUTBOARD HALVES AT LBL55.88 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE DIMENSION L=1.500Ï¿½ X W= 0.300Ï¿½ X W D= 0.010Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. AL
- [SDR A6WA202202218113](https://openairdocs.org/sdr/A6WA202202218113.md): None · damaged · Jan 14, 2022 · N438AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR LOWER SILL SEAL STRIKER AT FS349.00 IS DAMAGED. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PAX DOOR LOWER SILL SEAL STRIKER AT FS349.00 PN 600-31535. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMI
- [SDR A6WA202202148098](https://openairdocs.org/sdr/A6WA202202148098.md): Doubler · corroded · Jan 14, 2022 · N438AW · Cndair CL6002B19 · Fuselage Floor Panel
  > SERVICE DOOR LOWER SURROUND STRUCTURE DOUBLER AND BRACKETS AT FS319.00 AND FS349.00 HAVE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SERVICE DOOR LOWER SURROUND STRUCTURE DOUBLER P/N 601R38669-49 AT FS309.00 Ï¿½ FS319.00 AND BRACKET
- [SDR A6WA202202168103](https://openairdocs.org/sdr/A6WA202202168103.md): Angle · corroded · Jan 11, 2022 · N438AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION ON CABIN FLOOR SILL RHS AT FS349.00 AND RBL41, WL73.5. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FLOOR SILL SECTION AND REPLACED WITH REPAIR ANGLE P/N 601R31148-1355 TO MATCH ORIGINAL FLOOR SILL CUTOUT AT FS349.00 Ï¿½ FS375.00 AND RBL 41.
- [SDR A6WA202202118097](https://openairdocs.org/sdr/A6WA202202118097.md): Shroud · cracked · Jan 11, 2022 · N438AW · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > LH WING LEADING EDGE PANEL P/N 601R12076 HAS A CRACK MEASURES L= 0.700 X W= 0.010Ï¿½ THE LOWER FLANGE OF INNER SHROUD AT INBOARD END AT WS149.58. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE ON LOWER FLANGE AND FABRICATED AND INSTALLED A REPAIR ANGLE
- [SDR A6WA202202218114](https://openairdocs.org/sdr/A6WA202202218114.md): Web · none · Jan 6, 2022 · N438AW · Cndair CL6002B19 · Fuselage Structure (General)
  > REAR SKIN PANEL OF AFT PRESSURE BULKHEAD IS MISSING ALL REINFORCEMENT ANGLES (7 EA) -59, -61, -62, -65, -66, -69, & -70 REF BOMBARDIER REO 601R-53-61-1240 REV D DTD 2016-10- 13 ***AIRCRAFT REMOVED FROM SERVICE*** GENERAL AND DETAILED INSPECTION C/W, WITH N
- [SDR A6WA202202158102](https://openairdocs.org/sdr/A6WA202202158102.md): Doubler · dented · Jan 6, 2022 · N438AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD HAS A DENT LOCATED AT FS621.00 AND RBL6.0, WL80.0. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY EXISTING UPPER DOUBLERS P/N 601R-53-61-1240-3 AND -4 AND EXISTING LOWER DOUBLERS P/N 601R-53-61-1240-1 AND -2. REMOVED DENT DAMAGE. FAB
- [SDR A6WA202202218111](https://openairdocs.org/sdr/A6WA202202218111.md): Seat Track · corroded · Jan 4, 2022 · N438AW · Cndair CL6002B19 · Fuselage Structure (General)
  > LH SIDEWALL SEAT TRACK FROM FS409.00 TO FS559.00 +112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 TO FS559.00 +112. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS
- [SDR A6WA202102038094](https://openairdocs.org/sdr/A6WA202102038094.md): Seat Track · corroded · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > R/H SIDEWALL SEAT TRACKS FROM FS 364.00 TO FS 559.79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364.00 TO FS 559.00+80 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. ****
- [SDR A6WA202102028093](https://openairdocs.org/sdr/A6WA202102028093.md): Angle · gouged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > L/H WING I/B LE PANEL UPPER MOUNT LANDING HAS A GOUGE ON ANGLE DWG #600-12031. GOUGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-00-00 REV 38. *************AIRCRAFT REMOVED FROM SERVICE************************ EDGE TRIMMED THE CHAFED AREA DIMENSIONS: 1.
- [SDR A6WA202102018092](https://openairdocs.org/sdr/A6WA202102018092.md): None · damaged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STABILIZER SPLICE AT CLOSING RIB #9 HAS DAMAGE FROM LIGHTNING STRIKE. PREVIOUS TEMPORARY REPAIR COMPLIED WITH IAW MHIRJ REO 601R-55-11-677 REV A. PERMANENT REPAIR REQUIRED. *************AIRCRAFT REMOVED FROM SERVICE************************ CUT
- [SDR A6WA202102018091](https://openairdocs.org/sdr/A6WA202102018091.md): Channel · gouged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CARGO DOOR UPPER FWD SUPPORT CHANNEL P/N: 601R35050-129 HAS A GOUGE ON FLANGE. DIMENSIONS ARE: (P1) 1.900L X.063W X.190D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***
- [SDR A6WA202102018090](https://openairdocs.org/sdr/A6WA202102018090.md): Bulkhead · none · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD REAR WEB HAS 2 EACH RIVETS INSTALLED AT THE EDGE OF CHEM MILL I/B OF Z STIFFENER AT LBL 17 WL 140.5 AND 141.5. ******************AIRCRAFT REMOVED FROM SERVICE********************** REMOVED 2 EACH RIVETS AT THE EDGE OF CHEM MILL ON AFT P
- [SDR A6WA202102018089](https://openairdocs.org/sdr/A6WA202102018089.md): Fitting · gouged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > R/H H STAB FITTING #2 HAS 2 EACH GOUGES AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 1.00L X 0.200W X.006D (P2) 1.100L X 0.200W X.015D. BOTH GOUGES ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SE
- [SDR A6WA202102018088](https://openairdocs.org/sdr/A6WA202102018088.md): None · gouged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > R/H ELEVATOR I/B AND O/B FITTING HAS GOUGE ON FITTING ASSY AT ES60.525 (RBL55.8865). DIMENSIONS ARE: (P1) 2.100L X 0.300W X.005D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SE
- [SDR A6WA202101318084](https://openairdocs.org/sdr/A6WA202101318084.md): Skin · dented · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 235+5" AND S19R. DENT DIMENSIONS ARE: (P1) 1.950L X 1.50W X.011D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***********
- [SDR A6WA202101318085](https://openairdocs.org/sdr/A6WA202101318085.md): Skin · dented · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > AIRCRAFT L/H SKIN AT PAX DOOR CUTOUT HAS 1 EACH DENT AT FS 310.00+1" AND S13L+1.5". DENT DIMENSIONS ARE: (P1).400L X.300W X.032D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM S
- [SDR A6WA202101318086](https://openairdocs.org/sdr/A6WA202101318086.md): None · gouged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > L/H LEADING EDGE PANEL 331AL HAS TOOL MARKS ON I/B FASTENER HOLES. DIMENSIONS ARE: (P1) 7.100L X 1.00W X.018D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-00-00 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***************
- [SDR A6WA202101318087](https://openairdocs.org/sdr/A6WA202101318087.md): Bracket · gouged · Dec 15, 2021 · N438AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > L/H HORIZONTAL STABILIZER JACKSCREW FITTING HAS GOUGE ON I/B FASTENER BRACKET. DIMENSIONS ARE: (P1) 2.150L X 1.650W X.010D. EVALUATED GOUGE AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-11-27 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**
- [SDR A6WA202111037951](https://openairdocs.org/sdr/A6WA202111037951.md): None · none · Nov 3, 2021 · N438AW · Cndair CL6002B19 · Window/Windshield System
  > CAPTS WS CRACKED SPIDERWEB ACROSS ENTIRE PANEL ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 309800 WC 6,7,8,9, & 11 FOR R&R OF CAPT WINDSHIELD IAW CRJ AMM 56-11-01.
- [SDR A6WA202101227560](https://openairdocs.org/sdr/A6WA202101227560.md): Control Unit · faulted · Jan 21, 2021 · N438AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH, WHILE SELECTING FLAPS TO 8 DEGREES, RECEIVED FLAP FAIL MESSAGE. C/W QRH. PERFORMED ZERO FLAP LANDING. LANDED AT 41,000LBS. MAX BRAKE TEMP DURING TAXI WAS "4". PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPP 98-18I BOX 12. FLAPS RESET. PLACARDE
- [SDR A6WA202010057308](https://openairdocs.org/sdr/A6WA202010057308.md): Bulkhead Web · cracked · Oct 4, 2020 · N438AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > SDI OF THE AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. ACCOMPLISHED UT INSPECTION ON AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM PART 4, 53-61-153 REV 41 NO INDICATIONS NOTED. ACCOMPLISHED HFEC INSPECTION ON AFT PRESSURE BULKHEAD FWD
- [SDR A6WA202010057307](https://openairdocs.org/sdr/A6WA202010057307.md): Bulkhead Web · cracked · Oct 3, 2020 · N438AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > NDT-3 INDICATION FOUND COMING FROM UNDER MACHINED FITTING OF THE BAGGAGE BAY DOOR (LINTEL AREA) FOUND 3 EACH CRACKS AT FS 621.00. NR 1 VERTICAL CRACK THAT MEASURES 1.7'' UPPER HORIZONTAL CRACK THAT MEASURES.5'' AND LOWER HORIZONTAL CRACK THAT MEASURES.5''
- [SDR A6WA202009189287](https://openairdocs.org/sdr/A6WA202009189287.md): Pressure Deck · corroded · Sep 9, 2020 · N438AW · Cndair CL6002B19 · Fuselage Main, Structure
  > LT PRESS FLOOR SILL PANEL HAS CORROSION AROUND FASTENER HOLE AT FS 452.35 & BL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FLOOR SILL PANEL AT FS 452.35 & BL 43 WITH A REWORK AREA THAT MEASURES L=1.88 X W=1.134 X D=.003" ORIGINAL THICKNESS.080"
- [SDR A6WA202009187290](https://openairdocs.org/sdr/A6WA202009187290.md): Skin · damaged · Sep 8, 2020 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH.001" MATERIAL REMOVED WITHIN REMAINING.054" MINIMUM SKIN THICKNESS CHECK. WITHIN ALLOWABLE LIMITS, REF AIR WISCONS
- [SDR A6WA202009187289](https://openairdocs.org/sdr/A6WA202009187289.md): Skin · damaged · Sep 8, 2020 · N438AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT DME ANTENNA CUTOUT HAS SCRATCHES ON ANTENNA PAD AREA OF FUSELAGE SKIN. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND BLENDED OUT DAMAGE WITH.002" MATERIAL LOSS AND A MINIMUM REMAINING MATERIAL THICKNESS OF.054" WITHIN ALLOWABLE LIMITS, REF AIR WISCONSIN SU
- [SDR A6WA2018042500784](https://openairdocs.org/sdr/A6WA2018042500784.md): Doubler · cracked · Apr 24, 2018 · N438AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR EXISTING REPAIR DOUBLER ON AFT RISER UNDER COUNTER BALANCE CRACKED.
- [SDR A6WA2018042500783](https://openairdocs.org/sdr/A6WA2018042500783.md): Fitting · cracked · Apr 24, 2018 · N438AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 460 RBL BATH TUB FITTING CRACKED.
- [SDR A6WA2018042500781](https://openairdocs.org/sdr/A6WA2018042500781.md): Stiffener · cracked · Apr 24, 2018 · N438AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR ASSIST MOTOR LOWER STIFFNER CRACKED
- [SDR A6WA2018042500782](https://openairdocs.org/sdr/A6WA2018042500782.md): Angle · cracked · Apr 24, 2018 · N438AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE IS CRACKED ON THE OTBD SIDE OF RBL 9 AND JUST AFT OF THE FLOORBEAM BS 280.
- [SDR A6WA2018042445780](https://openairdocs.org/sdr/A6WA2018042445780.md): Angle · cracked · Apr 18, 2018 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 AFT SIDE RBL 9 CLIP CRACKED. REPLACED
- [SDR A6WA2018042445776](https://openairdocs.org/sdr/A6WA2018042445776.md): Seat Track · damaged · Apr 14, 2018 · N438AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PILOT SEAT TRACKS HAVE GROVES WORN INTO TRACKS. REPAIRED THE SEAT TRACK IAW SRM 53-11-49, AND 51-12-00.
- [SDR A6WA201845600](https://openairdocs.org/sdr/A6WA201845600.md): Bulkhead Web · cracked · Jan 26, 2018 · N438AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE PERFORMING NDT ON THE AFT PRESSURE BULKHEAD, BS 621. FOUND DISCONTINUITY INDICATION AT LBL 36.2. 5 INCHES ABOVE WL 73.50. INDICATION IS APPROX. 3/4 INCHES IN LENGTH.
- [SDR A6WA2017082245214](https://openairdocs.org/sdr/A6WA2017082245214.md): Crossbeam · chafed · Aug 21, 2017 · N438AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR CROSS BEAM LOWER OUTBOARD CHANNEL CHAFED BY THE CABLES.
- [SDR A6WA201644176](https://openairdocs.org/sdr/A6WA201644176.md): Door Seal · lack of lube · Aug 2, 2016 · N438AW · Cndair CL6002B19 · Service Doors
  > UNABLE TO OPEN SERVICE DOOR FROM EXTERIOR. LUBRICATED SERVICE DOOR SEAL, HANDLE, AS REQUIRED. OPS CHECK NORMAL. DOOR OPENS FROM OUTSIDE, ACFT OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N438AW/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 = 'N438AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N438AW/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.