# Service difficulty reports: N442AW

A list on [N442AW](https://openairdocs.org/aircraft/N442AW.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 · 225 reports

- [SDR A6WA202609028911](https://openairdocs.org/sdr/A6WA202609028911.md): Altimeter · malfunctioned · Sep 2, 2026 · N442AW · Cndair CL6002B19 · Ground Proximity System
  > ON TAKE OFF RADAR ALT ACTING ERRATIC, SETTING OFF TERRAIN GPWS WARNING. ABOVE 2500' RAD ALT CLEARED OFF OF PFD. RETURNED TO AEX. AIRCRAFT REMOVED FROM SERVICE. REF WO 348640 MWC #3&4. R&R RADIO ALTIMETER TRANSCEIVER. IAW AMM 34-44-07 & SUP 07-034H. OPS CHE
- [SDR A6WA202604138885](https://openairdocs.org/sdr/A6WA202604138885.md): Oil System · low pressure · Apr 13, 2026 · N442AW · Cndair CL6002B19 · Engine Oil Pressure
  > RECEIVED RIGHT ENGINE OIL PRESSURE WARNING AT 1000 FEET ON FINAL FULLY CONFIGURED OIL PRESSURE WAS APPROX. 30-35PSI AT 83% N2 PULLED RH ENGINE TO IDLE OIL PRESSURE REMAINED 30-35PSI, NO EXCEEDANCE IN MDC. AIRCRAFT REMOVED FROM SERVICE. REF W/O 347513 FOR R&R
- [SDR A6WA202604138884](https://openairdocs.org/sdr/A6WA202604138884.md): Idg · faulted · Apr 13, 2026 · N442AW · Cndair CL6002B19 · AC Generator-Alternator
  > ON TAKEOFF ROLL RECEIVED NR 2 IDG CAUTION FOLLOWED BY GEN 2 OFF ABORTED TAKEOFF PRIOR TO 80KTS. C/W CM ACTION PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. PLACED IDG NR 2 ON MEL, NO HOT BRAKES WERE NOTED DURING CALL. REF W/O 347513 FOR R&R
- [SDR A6WA202410108842](https://openairdocs.org/sdr/A6WA202410108842.md): Skin · corroded · Oct 10, 2024 · N442AW · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND EROSION DAMAGE TO THE RIGHT WING LEDAING EDGE SKIN BETWEEN WS350.348 AND WS386.348. THE DAMAGE IS REMOVED MEASURING A MATERIAL LOSS OF UP TO 0.018". THE SKIN IS FORMED FROM 0.080" 6013-T6 AL ALLOY LOCALLY CHEM-MILLED TO 0.042". MAINTENANCE CONTACTED ENGI
- [SDR A6WA202409108807](https://openairdocs.org/sdr/A6WA202409108807.md): Sealant · failed · Sep 10, 2024 · N442AW · Cndair CL6002B19 · Aerodynamic Fairings
  > DURING CLIMB ABOVE 10K AND SPEED 268KTS A/C BUFFETS. WAS NOT FELT IN YOKE, AP WAS DISENGAGED. BUFFETING NOT PRESENT ABOVE 270KTS AND BELOW 265KTS. FLIGHT CONTROLS OPERATE NORMALLY WHEN BUFFETING OCCURS. BUFFETING OCCURS AT APPROX 2* NOSE UP AND 2* NOSE DOWN.
- [SDR A6WA202406198767](https://openairdocs.org/sdr/A6WA202406198767.md): Water Separator · odor · Jun 19, 2024 · N442AW · Cndair CL6002B19 · Humidity Control System
  > AFTER LOW PRESSURE AIR WAS DISCONNECTED, ONCE APU LCV AND L PACK WAS TURNED ON, LIGHT HAZE SEEN AND SMELT IN COCKPIT. HAZE REPORTED FA IN CABIN AS WELL. INITIAL THOUGHT SMELT ELECTRICAL. AIRCRAFT REMOVED FROM SERVICE. CLEANED L AND R WATER SEPARATOR COAL
- [SDR A6WA202405078742](https://openairdocs.org/sdr/A6WA202405078742.md): Coalescer Bag · odor · May 7, 2024 · N442AW · Cndair CL6002B19 · Humidity Control System
  > DURING FLIGHT AFTER SWITCHING TO APU BLEED AIR, GOT SMOKE IN CABIN AND COCKPIT. SMOKE WAS BLUE WITH OILY SMELL. SMOKE CLEARED AFTER SWITCHING BLEEDS BACK TO ENGINES. AIRCRAFT REMOVED FROM SERVICE REMOVED AND CLEANED WATER SEPARATOR COALESCER THEN PUT IT IN
- [SDR A6WA202405087742](https://openairdocs.org/sdr/A6WA202405087742.md): Coalescer Bag · odor · May 7, 2024 · N442AW · Cndair CL6002B19 · Humidity Control System
  > DURING FLIGHT AFTER SWITCHING TO APU BLEED AIR, GOT SMOKE IN CABIN AND COCKPIT. SMOKE WAS BLUE WITH OILY SMELL. SMOKE CLEARED AFTER SWITCHING BLEEDS BACK TO ENGINES. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND CLEANED WATER SEPARATOR COALESCER THEN PUT IT IN
- [SDR A6WA202404288733](https://openairdocs.org/sdr/A6WA202404288733.md): Indicator · malfunctioned · Apr 28, 2024 · N442AW · Cndair CL6002B19 · Attitude Gyro and Indicating System
  > STANDBY ATTITUDE INDICATOR TUMBLED AFTER TAKE-OFF, INACCURATE DURING FLIGHT. STBY AI SHOWED LEVEL BEFORE TAKE-OFF AND AFTER LANDING. ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R STANDBY ATTITUDE IAW AMM 34-23-01. OPS CHECK GOOD AT THIS TIME. P/N 501-1567-10
- [SDR A6WA202311058668](https://openairdocs.org/sdr/A6WA202311058668.md): Sensor · faulted · Nov 5, 2023 · N442AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH INTO MHK, THE FLAPS FAILED AT 8 DEGREES. AN EMERGENCY HAS BEEN DECLARED AND THE FLIGHT WILL CONTINUE INTO MHK. R&R OF R/H BPSU IAW AMM 27-51-10
- [SDR A6WA202303208521](https://openairdocs.org/sdr/A6WA202303208521.md): Skin · dented · Mar 20, 2023 · N442AW · Cndair CL6002B19 · Fuselage Main, Frame
  > EXTERNAL FUSELAGE SKIN IS DENTED AT FS 265 BETWEEN STGR 24L AND 25L. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH MHIRJ REO 601R-53-11-3834 REV-- DATED 2023-03-12 REPAIRED FUSELAGE SKIN BETWEEN FS250-FS265 AND STR23L -24L
- [SDR A6WA202303168515](https://openairdocs.org/sdr/A6WA202303168515.md): Flap · dented · Mar 16, 2023 · N442AW · Cndair CL6002B19 · Wing Structure
  > LH INBD FLAP IS DENTED/PUNCTURED ON LOWER SKIN TRAILING EDGE AT APPROX. FLS 63.0. *******AIRCRAFT REMOVED FROM SERVICE********** REPAIRED LH IB FLAP LOWER SKIN IAW CRJ 200 AIRWIS SUPPLEMENT NO:15-230 AND MHIRJ ENGINEERING ORDER NO.: 600-2B19-57-L07424, DATE:
- [SDR A6WA202303118518](https://openairdocs.org/sdr/A6WA202303118518.md): Angle · cracked · Mar 11, 2023 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > STIFFENER ANGLE P/N 601R36008-51 LOCATED ON AFT SIDE OF FS621 PRESSURE BULKHEAD BETWEEN LBL36 AND STR 16B AT WL 79 IS CRACKED ON INBOARD END. *********AIRCRAFT REMOVED FROM SERVICE********** REPLACED STIFFENER ANGLE P/N 601R36008-51 AT AFT SIDE OF F.S. 621 BUL
- [SDR A6WA202302268507](https://openairdocs.org/sdr/A6WA202302268507.md): Bonding Plate · corroded · Feb 26, 2023 · N442AW · Cndair CL6002B19 · Nacelle/Pylon Structure
  > L/H UPPER PYLON TRAILING EDGE BONDING PLATES HAVE CORRODED FASTENERS. ******AIRCRAFT REMOVED FROM SERVICE********** REMOVED 12 RIVETS FROM LH UPPER PYLON BONDING PLATES IAW CRJ-200 SRM 51-42-13 INSTALLED 12 RIVETS IAW CRJ-200 SRM 51-42-13 REPLACED LH UPPER BON
- [SDR A6WA202302268492](https://openairdocs.org/sdr/A6WA202302268492.md): Retainer · corroded · Feb 26, 2023 · N442AW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > CORROSION FOUND ON ALL FOUR SEAL RETAINERS ON MAIN AVIONICS DOOR. ********AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED 4 EA. SEAL RETAINERS FOR MAIN AVIONICS DOOR IAW CRJ200 SRM 51-42-06
- [SDR A6WA202302268489](https://openairdocs.org/sdr/A6WA202302268489.md): Plate · corroded · Feb 26, 2023 · N442AW · Cndair CL6002B19 · Nacelle/Pylon Structure
  > L/H LOWER PYLON TRAILING EDGE BONDING PLATES HAVE CORRODED FASTENERS. ******AIRCRAFT REMOVED FROM SERVICE********** REMOVED AND REPLACED LH LOWER BONDING PLATE IAW AWAC SUPPLEMENT NO: 15-335.
- [SDR A6WA202302258516](https://openairdocs.org/sdr/A6WA202302258516.md): Panel · corroded · Feb 25, 2023 · N442AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > RH FLOOR SILL IS CORRODED BETWEEN FS 461 AND FS 473. *******AIRCRAFT REMOVED FROM SERVICE*********** REPAIRED RH PRESSURE FLOOR SILL PANEL BETWEEN FS461 AND FS 473 IAW MHIRJ REO 601R-53-41-3126 REV -- DATED 2023-03-14 AND BOMBARDIER REO NO. 601R-53-41-666, REV
- [SDR A6WA202302258506](https://openairdocs.org/sdr/A6WA202302258506.md): Angle · corroded · Feb 25, 2023 · N442AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > LH FLOOR SILL ANGLE IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 424 AND FS 513 *******AIRCRAFT REMOVED FROM SERVICE********** REMOVED CORROSION IN MULTIPLE SPOTS ON LH FLOOR SILL ANGLE BETWEEN FS 424 AND FS 513 IAW CRJ 200 SRM 51-21-06-00,REO 60
- [SDR A6WA202302258487](https://openairdocs.org/sdr/A6WA202302258487.md): Intercostal · cracked · Feb 25, 2023 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > ATTACHING CLIP CRACKED ON 3RD INTERCOSTAL ON R/H AFT SIDE OF AFT PRESSURE BULKHEAD. *********AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW ATTACH CLIP (PN: 601-35012-54) IAW CRJ200 SRM 51-42-21
- [SDR A6WA202302238519](https://openairdocs.org/sdr/A6WA202302238519.md): Hinge Arm · gouged · Feb 23, 2023 · N442AW · Cndair CL6002B19 · Leading Edge Devices
  > RH INBD FLAP HINGE ARM ASSY. AT WS 80.50 IS GOUGED ON LOWER MOUNT LUGS. *****AIRCRAFT REMOVED FROM SERVICE*********** REPAIRED RH IB FLAP HINGE ARM ASSY IAW MHIRJ REO 601R-57-54-358 REV -- DATED 2023-03-08
- [SDR A6WA202302228488](https://openairdocs.org/sdr/A6WA202302228488.md): Bracket · cracked · Feb 22, 2023 · N442AW · Cndair CL6002B19 · Spoilers
  > R/H FLAP STUB FAIRING HAS A BROKEN BRACKET THAT REQUIRES REPLACEMENT. ****AIRCRAFT REMOVED FROM SERVICE********** INSTALLED NEW R/H FLAP STUB FAIRING BRACKET AND RESTORED SURFACE FINISH IAW MHIRJ CRJ200 SRM 51-42-06-00 AND 51-21-16-00
- [SDR A6WA202301048425](https://openairdocs.org/sdr/A6WA202301048425.md): Sensor · failed · Jan 4, 2023 · N442AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAILED AT 20 DEGREES WHEN TRYING TO SET FLAP TO 30 DEGREES. GEAR WAS DOWN AND WERE IN ICING CONDITIONS. RAN QRH FLAP FAIL PROCEDURE. CW FIM RESET, FLAPS FAILED AT ZERO. AIRCRAFT REMOVED FROM SERVICE. R & R SKEW DETECTION UNIT IRW AMM 27-51-15-04. OPS C
- [SDR A6WA202211268390](https://openairdocs.org/sdr/A6WA202211268390.md): Transmitter · fault message · Nov 26, 2022 · N442AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FAULTY FLAP IND AND FLAPS DEGRADED MSG, FLUX BETWEEN 8-20 DEGREES @ 30,000' DOWN TO 3000' AND SET FLAPS 8 FOR LANDING- NORMAL IND AFTER THAT, BUT FLAPS DEGRADED MSG PERSISTED. WHEN INDICATION WAS FLUX AUTO PILOT PITCHED UP/DOWN. FLAPS SET 8 THRU 45 OPERATED NO
- [SDR A6WA202101118065](https://openairdocs.org/sdr/A6WA202101118065.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 233.27+3" AND S1R+2. DENT DIMENSIONS ARE: (P1) 1.700L X 1.700W X.016D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE******
- [SDR A6WA202101118061](https://openairdocs.org/sdr/A6WA202101118061.md): Angle · gouged · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT LBL 6. DIMENSIONS OF SCRATCH ARE: 4.100"L X 0.900"W X 0.004"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO
- [SDR A6WA202101118063](https://openairdocs.org/sdr/A6WA202101118063.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 394.00+10" AND S19R TO S20R. DENT DIMENSIONS ARE: (P1).500L X.500W X.007D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE
- [SDR A6WA202101118064](https://openairdocs.org/sdr/A6WA202101118064.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.50+15" AND S26L TO S27. DENT DIMENSIONS ARE: (P1).400"L X.350"W X.020"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVI
- [SDR A6WA202101118062](https://openairdocs.org/sdr/A6WA202101118062.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.00 AND S21R+3. DENT DIMENSIONS ARE: (P1) 1.00L X.800W X.008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**********
- [SDR A6WA202101118060](https://openairdocs.org/sdr/A6WA202101118060.md): Visor · gouged · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT LBL6. DIMENSIONS OF SCRATCH ARE: 35.00"L X 0.900"W X 0.004"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMEN
- [SDR A6WA202101108058](https://openairdocs.org/sdr/A6WA202101108058.md): Visor · gouged · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT RBL 6. DIMENSIONS OF SCRATCH ARE: (P1) = 4.300"L X.700"W X.006"D AND (P2) = 7.00"L X.200"W X.002"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLEND
- [SDR A6WA202101108057](https://openairdocs.org/sdr/A6WA202101108057.md): Visor · gouged · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT LBL6. DIMENSIONS OF SCRATCH ARE: 19.00"L X 0.800"W X 0.007"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMEN
- [SDR A6WA202101108052](https://openairdocs.org/sdr/A6WA202101108052.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.00 TO FS 672.00 AND S25R-26R. DENT DIMENSIONS ARE: (P1).600L X.300W X.008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SE
- [SDR A6WA202101108053](https://openairdocs.org/sdr/A6WA202101108053.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 736+15 AND S20R+2. S21R HAS EDGE DAMAGE AT SAME AREA ON SKIN INTERIOR MEASURING:.450"L X.050"W X.050"D. DENT DIMENSIONS ARE: (P1).600L X.300W X.008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IA
- [SDR A6WA202101108054](https://openairdocs.org/sdr/A6WA202101108054.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 310.00 AND S13L+5". DENT DIMENSIONS ARE: (P1).350L X.200W X.004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********
- [SDR A6WA202101108055](https://openairdocs.org/sdr/A6WA202101108055.md): Skin · dented · Jan 7, 2022 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 605.00 TO FS 621.00 AND S17L-19L. DENT DIMENSIONS ARE: (P1) 3.500"L X.800"W X.017"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FRO
- [SDR A6WA202101178076](https://openairdocs.org/sdr/A6WA202101178076.md): Rib · corroded · Dec 23, 2021 · N442AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STABILIZER TIP CLOSING RIB #9 P/N 600-23037-22 HAS TWO ELONGATED FASTENER HOLES CAUSED BY CORROSION. HORIZONTAL REAR SPAR AND LBL112.0. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED SECTIONS OF CLOSING RIB AT TWO LOCATIONS. MEASUREMENTS
- [SDR A6WA202101178069](https://openairdocs.org/sdr/A6WA202101178069.md): None · none · Dec 22, 2021 · N442AW · Cndair CL6002B19 · Fuselage Floor Panel
  > REMOVE AND REPLACE PAX DOOR HINGE PINHOLES WORN BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PAX DOOR HINGE ON DOOR HALF REF MHI RJ REO 601R-52-11-2912 REV -- DTD 2022-01-04 FOR DISPOSITION FOR FASTENER SUBSTITUTION DURING REPLACEME
- [SDR A6WA202101178077](https://openairdocs.org/sdr/A6WA202101178077.md): Skin · damaged · Dec 15, 2021 · N442AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > OUTER SKIN FS349.00 AT PAX DOOR CUTOUT P/N 601R31018-9 IS DAMAGED. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE BY EDGE BLENDING OUTER SKIN AT FS349.00. MEASUREMENT L= 1.180Ï¿½ X W= 0.113Ï¿½ X D= 0.060Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED P
- [SDR A6WA202101178074](https://openairdocs.org/sdr/A6WA202101178074.md): Door · cracked · Dec 15, 2021 · N442AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > MAIN ENTRY DOOR HAS A CRACK ON THE FORWARD SIDE PANEL OF UPPER STEP FS320.10. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE OF MAIN ENTRY DOOR FORWARD SIDE PANEL OF UPPER STEP FS320.10, DIMENSIONS L= 12.00Ï¿½ X W= 6.00Ï¿½. FABRICATED 1 WEB REPLACEMENT L
- [SDR A6WA202101178070](https://openairdocs.org/sdr/A6WA202101178070.md): Bracket · corroded · Dec 10, 2021 · N442AW · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION ON CONNECTOR BRACKET P/N 601R31771-1 LOCATED AT FS310.00+12 AND AND LBL42 UNDER FLOOR STRUCTURE AT PASSENGER ENTRY DOOR. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED CONNECTOR BRACKET P/N 601R31771-1 LOCATED AT FS310.00+12 AND LBL42.
- [SDR A6WA202101178073](https://openairdocs.org/sdr/A6WA202101178073.md): Plate · corroded · Dec 10, 2021 · N442AW · Cndair CL6002B19 · Standard Practices/Structures
  > REMOVED AND REPLACED 4 EACH BONDING PLATES P/N 601-37012-33. ***AIRCRAFT REMOVED FROM SERVICE*** RESTORED SURFACE FINISH. BOND CHECKED GOOD. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AWA SUPPLEMENT NO. 15-335 DATE OF ISSUE 12/22/2015. WORK PERFORMED UNDER A
- [SDR A6WA202101178075](https://openairdocs.org/sdr/A6WA202101178075.md): None · corroded · Dec 9, 2021 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FS 574.00+10 TO FS 589.00+8 & LBL 46 FRETTING CORROSION COMMON TO ANGLE AT LWR SIDE OF CARGO DOOR OPENING AT FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 5 OFF AREAS P1 THROUGH P5 OF BLENDED CORROSION DAMAGE AS: P1 1.60"L X 0.80"W X.068" MIN RE
- [SDR A6WA202101178071](https://openairdocs.org/sdr/A6WA202101178071.md): Strap · corroded · Dec 6, 2021 · N442AW · Cndair CL6002B19 · Fuselage, Stabilizer Attach Fittings
  > CORROSION ON PRESSURE FLOOR STRAP PN 601R31025-29 LOCATED AT FS559.00 AND RBL30 TO RBL44 PRESSURE FLOOR STRUCTURE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED PRESSURE FLOOR STRAP PN 601R31025-29 LOCATED AT FS559.00 AND RBL30 TO RBL44 WITH A N
- [SDR A6WA202101178067](https://openairdocs.org/sdr/A6WA202101178067.md): Skin · dented · Dec 5, 2021 · N442AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > DENT IN EXTERIOR SKIN C/T PAX DOOR OPENING AT F.S. 310.00 & S 14L+3" THAT MEASURES.750 "L X.300"W X.015"D. EVALUATED AND DETERMINED TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-00 REV 38. VERIFIED LOOSE OR PULLED FASTENERS IN THE SURROUNDING AREA REF ASAP EA
- [SDR A6WA202101178072](https://openairdocs.org/sdr/A6WA202101178072.md): Skin · dented · Dec 2, 2021 · N442AW · Cndair CL6002B19 · Fuselage Structure (General)
  > STRINGER HAS 4 OUTWARD DENTS COMMON TO EXTERIOR SKIN PN 601R35004-145 AT FS625.30 TO FS640.00 AND STR16R TO STR17R. ****AIRCRAFT REMOVED FROM SERVICE**** VERIFIED NO LOOSE OR PULLED FASTENERS IN THE SURROUNDING AREA AT STRINGER COMMON TO EXTERIOR SKIN AT FS
- [SDR A6WA202101178068](https://openairdocs.org/sdr/A6WA202101178068.md): Skin · cracked · Dec 1, 2021 · N442AW · Cndair CL6002B19 · Engine Cowl Flaps
  > R/H UPPER MAIN CORE COWL UPPER FWD I/B CORNER IS BENT AND DEBONDING.FOUND CRACK IN DEBONDING FWD I/B CORNER LENGTH IS 1.437" &.010"W. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUTOUT ON DAMAGE ON OUTER SKIN P/N 228-50142-607 THAT MEASURES 2.5"L X.77
- [SDR A6WA202108127855](https://openairdocs.org/sdr/A6WA202108127855.md): Seal · dirty · Aug 11, 2021 · N442AW · Cndair CL6002B19 · Passenger/Crew Doors
  > RECEIVED CABIN ALT CAUTION MESSAGE ON CLIMB-OUT; COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL PRESSURIZATION MODES. AIRCRAFT REMOVED FROM SERVICE. INSPECTED PAX DOOR SEAL AND CLEANED DEBRIS, NO OTHER DEFECTS NOTED, REF. AMM 52-11-00 PRESSURIZED A/C WITH
- [SDR A6WA202012297499](https://openairdocs.org/sdr/A6WA202012297499.md): Gcu · malfunctioned · Dec 26, 2020 · N442AW · Cndair CL6002B19 · AC Generation System
  > WHILE OPERATING WITH AN IDG 2 INOPERABLE MEL APPLIED, APU GCU DISABLED AND APU GEN WAS NO LONGER TO POWER AC BUS 2. SINGLE GEN OPERATIONS. ELECTED TO AIR RETRUN. APU GCU RE-ENABLED ITSELF PRIOR TO LANDING. AIRCRAFT REMOVED FROM SERVICE. R & R APU GCU, IAW
- [SDR A6WA202010147324](https://openairdocs.org/sdr/A6WA202010147324.md): Adg · unwanted deploy · Oct 14, 2020 · N442AW · Cndair CL6002B19 · AC Generator-Alternator
  > INADVERTENTLY DEPLOYED ADG DURING GEN 1 CAUTION. AROUND 220 KNOTS ADG RAN FOR APPROXIMATELY 20 MIN IN FLIGHT. APU GEN WAS ON MEL, PILOT CYCLED WRONG GEN SW. RETURNED DUE TO ADG DEPLOYED. IDG 1 CAUTION MSG ON T/O AND THEN MSG CLEARED, THEN RECEIVED GEN 1 CA
- [SDR A6WA202010077313](https://openairdocs.org/sdr/A6WA202010077313.md): Seat Track · corroded · Oct 6, 2020 · N442AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY SEAT TRACK SEGMENT FS 559-FS 559+80 RBL 9 HAS SURFACE CORROSION AND PITTING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CARGO BAY SEAT TRACK SEGMENT FS 559-559+80, IAW REO 601R-53-00-764 AND CRJ200 SRM 51-40-11.

Next page: https://openairdocs.org/aircraft/N442AW/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 = 'N442AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N442AW/reports

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