# Service difficulty reports: N435AW

A list on [N435AW](https://openairdocs.org/aircraft/N435AW.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 · 248 reports

- [SDR A6WA202610098918](https://openairdocs.org/sdr/A6WA202610098918.md): Outflow Valve · faulted · Oct 9, 2026 · N435AW · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > DURING CLIMB RECEIVED CABIN ALT CAUTION MESSAGE AT ABOUT 11,000 FT THEN RECEIVED CABIN ALT WARNING SOON AFTER. DESCENDED TO 8,000 FT PRESSURIZATION STABILIZED. AIRCRAFT REMOVED FROM SERVICE. FOUND OVERBD AND INBD EXHAUST VALVES DEACTIVATED INCORRECTLY. SECUR
- [SDR A6WA202609018914](https://openairdocs.org/sdr/A6WA202609018914.md): O-Ring · leaking · Sep 9, 2026 · N435AW · Cndair CL6002B19 · Fuel Storage
  > AFTER DEPARTURE TOWER REPORTED MIST COMING FROM RIGHT WING AS WE WERE RETURNING STARTED HAVING A FUEL IMBALANCE DECLARED AN EMERGENCY RETURNED TO YAM ON FINALE TOWER REPORTED POSSIBLE STILL TRAILING FUEL, AFTER LANDING FIRE DEPARTMENT DID SEE FUEL LEAKING BUT
- [SDR A6WA202410148836](https://openairdocs.org/sdr/A6WA202410148836.md): A/C Pack · smoke · Oct 14, 2024 · N435AW · Cndair CL6002B19 · Cabin Cooling System
  > WHILE AT GATE PRIOR TO PUSHBACK, CREW NOTICED SMOKE/HAZE COMING FROM REAR OF THE CABIN NEAR LAVATORY WHICH BEGAN TO FILL THE CABIN. SHUTDOWN AIRCRAFT, & BEGAN TO ORDERLY DEPLANE. ARFF & EMS WERE REQUESTED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED LAVATORY, NO
- [SDR A6WA202406038758](https://openairdocs.org/sdr/A6WA202406038758.md): Selector Valve · faulted · Jun 3, 2024 · N435AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > 6158 - AFTER RAISING THE LANDING GEAR ON TAKEOFF RECEIVED A GEAR DISAGREE WARNING MESSAGE AND DOOR WARNING MESSAGE. C/W BOTH QRH'S BOTH MESSAGE CLEARED. MESSAGE'S APPEARED. 6 SECOND AFTER SELECTION AT APPROX 165 IAS. NO OTHER ASSOCIATED MESSAGED, NOSE GEAR IND
- [SDR A6WA202307308644](https://openairdocs.org/sdr/A6WA202307308644.md): Pump · faulted · Jul 30, 2023 · N435AW · Cndair CL6002B19 · Hydraulic System, Main
  > ON CLIMB AT FL290, RECV'D "HYD 2 LO PSI" CAUTION. SYS PAGE SHOWED HYD 2 QUANTITY @ 5%. EDP2 WAS IN YELLOW WITH NO FLOW LINE. C/W QRH. EDP2 OPERATED FOR 57 MINS WITHOUT FLUID. AIRCRAFT REMOVED FROM SERVICE. R&R ACMP #2B IAW AMM TASK 29-11-03-100-801 P/N:
- [SDR A6WA202307298643](https://openairdocs.org/sdr/A6WA202307298643.md): Relief Valve · unknown · Jul 29, 2023 · N435AW · Cndair CL6002B19 · Hydraulic System, Main
  > HYD 2 LOW PRESS CAUTION MSG SHORTLY AFTER LANDING, OUTBD BRAKE PRESS CAUTION MSG. BRAKING ACTION LIMITED. QTY IS 5 PERCENT. FLUID IS DRIPPING FROM ECS BAY. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND HYD #2 RESERVOIR PRESSURE RELIEF VALVE LEAKING. R
- [SDR A6WA202301028424](https://openairdocs.org/sdr/A6WA202301028424.md): Bpsu · failed · Jan 2, 2023 · N435AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH WHEN EXTENDING FLAPS FROM 0 TO 8 DEGREES, RECEIVED FLAPS FAIL. FLAPS FAILED AT 6 DEGREES. DECLARED EMERGENCY. NORMAL LANDING AND BRAKING. MAX BTMS WAS 5. AIRCRAFT REMOVED FROM SERVICE. R & R RT FLAPS BPSU IAW AMM 27-51-10 OPS TESTED GOOD.
- [SDR A6WA202204278177](https://openairdocs.org/sdr/A6WA202204278177.md): None · gouged · Apr 27, 2022 · N435AW · Cndair CL6002B19 · Doors
  > CARGO DOOR OUTER SKIN GOUGE DAMAGE FROM INCORRECT SCREWS INSTALLED IN CARGO BAY LINERS ABOVE THE DOOR OPENING. MX DISCOVERED ON RON WALKAROUND. A****AIRCRAFT REMOVED FROM SERVICE ***** CARGO DOOR OUTER SKIN WAS REPAIRED PER REO 601R-52-31-370. CORRECT SCRE
- [SDR A6WA202204028161](https://openairdocs.org/sdr/A6WA202204028161.md): Harness · inoperative · Apr 2, 2022 · N435AW · Cndair CL6002B19 · Nose/Tail Landing Gear Attach Section
  > AFTER TAKE OFF APROX 13 SECONDS RECIEVED GEAR DISAGREE WARNING MSG AND NOSE GEAR DOOR MSG. MANUAL RELEASE USED TO EXTEND GEAR.ALL HYD SYSTEMS IN AUTO POSITION. NO ICEING CONDITIONS DURING EVENT. EMERGENCY WAS DECLARED. ***AIRCRAFT REMOVED FROM SERVICE*** C/
- [SDR A6WA202203128127](https://openairdocs.org/sdr/A6WA202203128127.md): Warning Message · illuminated · Mar 12, 2022 · N435AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE - NOSE LANDING GEAR DID NOT RETRACT DURING TAKEOFF *** AIRCRAFT REMOVED FROM SERVICE *** C/W LANDING GEAR EXTENSION AND RETRACTION SEVERAL TIMES WITH NO FAULTS FOUND IAW AMM 32-30-00. REMOVED PLACARD AND FROM MEL
- [SDR A6WA202201238080](https://openairdocs.org/sdr/A6WA202201238080.md): None · none · Jan 23, 2022 · N435AW · Cndair CL6002B19 · Landing Gear System
  > ON TAKE OFF,RECEIVED GEAR DISAGREE NOSE WHEEL DID NOT RETRACT. C/W QRH MANUALLY LOWERED GEAR, GEAR WAS DOWN AND LOCKED AND LANDED WITHOUT ANY FURTHER INCIDENTS. USED MANUAL HANDLE AND STOWED WHEN GEAR WAS LOWERED. NO ABNORMAL HYD MESSAGES. 3A WAS ON AND 3B S
- [SDR A6WA202201058050](https://openairdocs.org/sdr/A6WA202201058050.md): None · none · Jan 2, 2022 · N435AW · Cndair CL6002B19 · Ice/Rain Protection System
  > ON CLIMBOUT RECIEVED R COWL ANTI ICE MESSAGE. C/W QRH AND MESSAGE CLEARED. ***AIRCRAFT REMOVED FROM SERVICE*** C/W OPERATIONAL CHECK OF RH COWL ANTI ICE SYSTEM IAW 32-20-00 AC OK FOR SERVICE. FOUND RH TURKEY POPPER OUT. REF 218827/2 FOR MEL R&R RT ENGINE TUR
- [SDR A6WA202110238046](https://openairdocs.org/sdr/A6WA202110238046.md): Bulkhead · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD AT FS 621 LBL 25 HAS A DENT ON PREVIOUSLY INSTALLED DOUBLER 3.400"L X.800"W X.028"D AND A SETMARK AT DENT MEASURING.250"L ON FORWARD SIDE OF BULKHEAD AT LBL 24.75 TO LBL 25.75 AND WL 130 TO WL 133.400. ************AIRCRAFT REMOVED F
- [SDR A6WA202112238042](https://openairdocs.org/sdr/A6WA202112238042.md): None · corroded · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > CORROSION DAMAGE LOCATED ON R/H FLOOR SILL WEB AT FS 349 TO FS 349+12.5" AND RBL 42 TO RBL 44. DIMENSIONS ARE: (P1) = FS 349+1" - FS 349+6" & RBL 42 = 5.40"L X 2.80"W X.019"D (P2) = FS 349+9 - FS 349+12.5" & RBL 42 = 3.60"L X 1.80"W X.003"D **************
- [SDR A6WA202112238044](https://openairdocs.org/sdr/A6WA202112238044.md): None · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > MAINTENANCE FOUND 4 EACH SCRATCHES ON VERTICAL STABILIZER R/H SIDE COMMON TO ACCESS PANEL 325CR. DIMENSIONS OF SCRATCHES ARE: (P1) = 2.500"L X 0.800"W X 0.006"D AND (P2) = 3.00"L X 1.400"W X.007"D (P3) = 1.500"L X 1.300"W X.004"D (P4) = 1.500"L X.500"W X.
- [SDR A6WA202112238043](https://openairdocs.org/sdr/A6WA202112238043.md): Skin · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > MAINTENANCE FOUND 2 EACH SCRATCHES ON VERTICAL STABILIZER R/H SIDE COMMON TO ACCESS PANEL 325DR. DIMENSIONS OF SCRATCHES ARE: (P1) = 3.00"L X 0.500"W X 0.004"D AND (P2) = 4.00"L X 0.300"W X.004"D ************AIRCRAFT REMOVED FROM SERVICE********************
- [SDR A6WA202112238038](https://openairdocs.org/sdr/A6WA202112238038.md): Skin · dented · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT SKIN R/H EXTERIOR HAS 1 EACH DENT AT FS 193.00+7 AND S13R+3. DENT DIMENSIONS ARE: (P1) 2.100L X 1.500W X.016D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE******
- [SDR A6WA202112238041](https://openairdocs.org/sdr/A6WA202112238041.md): None · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT RBL 6. DIMENSIONS OF SCRATCH ARE:.900"L X 0.600"W X 0.002"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH
- [SDR A6WA202112238039](https://openairdocs.org/sdr/A6WA202112238039.md): None · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR AT RBL 6. DIMENSIONS OF SCRATCH ARE: 38.00"L X 0.70"W X 0.005"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH CONTOUR. DIMEN
- [SDR A6WA202112238040](https://openairdocs.org/sdr/A6WA202112238040.md): None · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON R/H HORIZONTAL STABILIZER ATTACHMENT VISOR SUPPORT ANGLE AT RBL 6. DIMENSIONS OF SCRATCH ARE: 4.20"L X 0.70"W X 0.005"D. ************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED DAMAGED AREA TO A SMOOTH
- [SDR A6WA202112238035](https://openairdocs.org/sdr/A6WA202112238035.md): Bulkhead · dented · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD AT FS 621 LBL 21.00 TO LBL 23.30 HAS A DENT 1.250"L X 1.00"W.020"D AND A PREVIOUS BLEND AT DENT MEASURING 1.10"L X.850"W X.028"D ON FWD SIDE OF BULKHEAD AT WL 75.95 TO WL 78.60. ************AIRCRAFT REMOVED FROM SERVICE**************
- [SDR A6WA202112238032](https://openairdocs.org/sdr/A6WA202112238032.md): Bulkhead · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD AT FS 621 RBL 14.75 HAS SETMARK IN DOUBLER COMMON TO FWD SIDE OF BULKHEAD. DIMENSIONS ARE:.300"L X.040"W X.007"D. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGED AREA TO A SMOOTH CONTOUR WITH DIME
- [SDR A6WA202112238037](https://openairdocs.org/sdr/A6WA202112238037.md): Skin · dented · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT SKIN R/H EXTERIOR HAS 1 EACH DENT AT FS 409.00+64+4 AND S23R+3. DENT DIMENSIONS ARE: (P1).375L X.340W X.004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*****
- [SDR A6WA202112238034](https://openairdocs.org/sdr/A6WA202112238034.md): Bulkhead · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD AT FS 621 LBL 9.50 TO LBL 18 AT WL 77.4 HAS A PREVIOUSLY BLENDED AREA ON FWD SIDE. DIMENSIONS ARE: 1.40"L X 1.00"W X.029"D. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGED AREA TO A SMOOTH CONTOUR W
- [SDR A6WA202112238033](https://openairdocs.org/sdr/A6WA202112238033.md): Bulkhead · dented · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD AT FS 621 LBL 30.00 TO LBL 32.80 HAS A DENT 2.80"L X 2.20"W.045"D AND A GOUGE AT DENTED AREA MEASURING 1.40"L X 1.00"W X.029"D ON FWD SIDE OF BULKHEAD AT WL 111.63 TO WL 114.43. ************AIRCRAFT REMOVED FROM SERVICE***************
- [SDR A6WA202112238036](https://openairdocs.org/sdr/A6WA202112238036.md): None · gouged · Dec 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT PRESSURE BULKHEAD AT FS 621 LBL 21.00 TO LBL 23.30 HAS A PREVIOUS BLENDED AREA MEASURING 0.075"L X 0.550"W X 0.031"D ON FWD SIDE OF BULKHEAD AT WL 76.1 TO WL 76.9. ************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED DAMAGED AREA
- [SDR A6WA202111297994](https://openairdocs.org/sdr/A6WA202111297994.md): None · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 449.85+9 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 1 EACH AREA ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT F
- [SDR A6WA202111297993](https://openairdocs.org/sdr/A6WA202111297993.md): None · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 473.15+6 TO FS 484.00+2 AND RBL 39 TO RBL 42 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140 AND PRESSURE FLOOR ANGLE P/N: 601R31145-220. ***************AIRCRAFT REMOVED FROM SERVICE***************************
- [SDR A6WA202111297995](https://openairdocs.org/sdr/A6WA202111297995.md): None · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 439.00+8 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140 AND PRESSURE FLOOR ANGLE P/N: 601R31145-218. ****************AIRCRAFT REMOVED FROM SERVICE************************ BLENDED 5 EACH AREAS: PR
- [SDR A6WA202111297996](https://openairdocs.org/sdr/A6WA202111297996.md): None · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 439.00+2 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 1 EACH AREA ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT F
- [SDR A6WA202111297991](https://openairdocs.org/sdr/A6WA202111297991.md): None · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 513.00+5 TO FS 513.00+8 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 2 EACH AREAS ON PRESSURE FLOOR SILL P/N: 60
- [SDR A6WA202111297992](https://openairdocs.org/sdr/A6WA202111297992.md): None · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 484.00 +8 AND RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140. ***************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED 1 EACH AREA ON PRESSURE FLOOR SILL P/N: 601R31145-140 AT
- [SDR A6WA202111297989](https://openairdocs.org/sdr/A6WA202111297989.md): Angle · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Stabilizer Attach Fittings
  > CORROSION COMMON TO PRESSURE FLOOR ANGLE AT FS 513.00 TO FS 513.00+4 AND LBL 40 TO LBL 43. ****************AIRCRAFT REMOVED FROM SERVICE************************** BLENDED 2 EACH AREAS: FS 513.00 AT LBL 41 (P1) 1.20"L X.800"W X.004"D; FS 513.00+4 AT LBL 43
- [SDR A6WA202111297990](https://openairdocs.org/sdr/A6WA202111297990.md): Angle · corroded · Nov 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE PRESSURE FLOOR SILL HAS CORROSION AT FS 549.00+13 TO FS 559.00 AND RBL 30 TO RBL 40 COMMON TO PRESSURE FLOOR SILL P/N: 601R31145-140, PRESSURE FLOOR ANGLE P/N: 601R31145-222, AND PRESSURE FLOOR CROSS MEMBER STRAP. ***************AIRCRAFT REMOVED FROM
- [SDR A6WA202112178029](https://openairdocs.org/sdr/A6WA202112178029.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT LOWER BELLY SKIN EXTERIOR HAS 3 EACH DENTS AT FS 654.50+10-FS 654.50+16 AND S25R+1 S26L+4. DENT DIMENSIONS ARE AS FOLLOW: (P1) = FS654.50+12 & S26L+4 =.500"L X.455"W X.016"D (P2) = FS654.50+10 & S26R+4 =.550"L X.450"W X.007"D (P3) = FS654.50+16
- [SDR A6WA202112138025](https://openairdocs.org/sdr/A6WA202112138025.md): None · none · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > PRIOR TO INSTALLATION OF HSTA PINS & TRUNNION INSTALLATION OF THE UPPER PIN FOUND ATTACH HOLES IN AIRCRAFT STRUCTURE BELOW SERVICE BULLETIN NOMINAL SIZE (.189" -.195"). PRIOR TO INSTALLATION OF HSTA PINS & TRUNNION INSTALLATION OF THE LOWER PIN FOUND ATTACH H
- [SDR A6WA202112138026](https://openairdocs.org/sdr/A6WA202112138026.md): None · gouged · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Window/Windshield System
  > TOOL MARKS COMMON TO AFT SIDE OF PILOT'S WINDSHIELD SIDE WINDOW POST AT FS 250. DIMENSIONS ARE: (P1) =.900"L X.600"W X.015"D. *************AIRCRAFT REMOVED FROM SERVICE************************ BLENDED DAMAGE TO A SMOOTH CONTOUR AT AREA (P1). VERIFIED REP
- [SDR A6WA202112108023](https://openairdocs.org/sdr/A6WA202112108023.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT SKIN L/H EXTERIOR HAS 1 EACH DENT AT FS 409.00+15" AND S18L+3.80". DENT DIMENSIONS ARE: (P1).500L X.450W X.002D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**
- [SDR A6WA202112108024](https://openairdocs.org/sdr/A6WA202112108024.md): Door · gouged · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Doors
  > PASSENGER DOOR UPPER SILL P/N: 601R31522 HAS SEVERAL GOUGES/ABRASIONS BETWEEN FS 295.00 - FS 364.00 AT S3L. DAMAGE LOCATIONS AND MEASUREMENTS ARE: (P1) FS 310+2 & S3L =.450"L X.250"W X.002"D (P2) FS 319.70+1 & S3L =.850"L X.500"W X.003"D (P3) FS 319.70+6
- [SDR A6WA202112108020](https://openairdocs.org/sdr/A6WA202112108020.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > AIRCRAFT SKIN L/H EXTERIOR HAS 1 EACH DENT AT FS 280.00+1 AND S14L. DENT DIMENSIONS ARE: (P1) 1.200L X 1.00W X.008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********
- [SDR A6WA202112108022](https://openairdocs.org/sdr/A6WA202112108022.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT SKIN UPPER CROWN EXTERIOR HAS 1 EACH DENT AT FS 672.20+5.2" AND S3R+4". DENT DIMENSIONS ARE: (P1) 1.900L X.900W X.008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SER
- [SDR A6WA202112098018](https://openairdocs.org/sdr/A6WA202112098018.md): Angle · gouged · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > MAINTENANCE FOUND SCRATCH DAMAGE ON L/H HORIZONTAL STABILIZER FAIRING ATTACHMENT VISOR ANGLE P/N: 600-23072 AT LBL 6 FROM FWD TO AFT END MEASURING: 38.00"L X.700"W X.005"D. VISOR IS FORMED FROM PA21068.075" 2024-T3511. ***************AIRCRAFT REMOVED FROM
- [SDR A6WA202112098019](https://openairdocs.org/sdr/A6WA202112098019.md): Angle · corroded · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Galley Doors
  > MAINTENANCE FOUND CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N: 601R38303-253 AT FS 319.70 TO FS 349 AND RBL 38 TO RBL 39. **************AIRCRAFT REMOVED FROM SERVICE************************ BLENDED 3 EACH AREAS ON SERVICE DOOR LOWER SILL ANGLE AS FOLLOW:
- [SDR A6WA202112088017](https://openairdocs.org/sdr/A6WA202112088017.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 625.30+11 AND S24L+2. DENT DIMENSIONS ARE: (P1).700L X.600W X.015D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******
- [SDR A6WA202112088016](https://openairdocs.org/sdr/A6WA202112088016.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Internal Stairs
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+8 AND S22R+4. DENT DIMENSIONS ARE: (P1) 1.00L X 1.00W X.001D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE********
- [SDR A6WA202112088014](https://openairdocs.org/sdr/A6WA202112088014.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+11 AND S24L+3. DENT DIMENSIONS ARE: (P1).600L X.600W X.013D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******
- [SDR A6WA202112088013](https://openairdocs.org/sdr/A6WA202112088013.md): None · gouged · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > MAINTENANCE FOUND 2 EACH SCRATCHES COMMON TO FWD SIDE OF AFT PRESSURE BULKHEAD AT FS 621 AND RBL 29.75 AT WL 137.18-137.95. DAMAGE MEASURES: (P1) =.350"L X.010"X.005" AND (P2) =.500"L X.010"W X.005"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CR
- [SDR A6WA202112088015](https://openairdocs.org/sdr/A6WA202112088015.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT SKIN EXTERIOR HAS 1 EACH DENT AT FS 559.00+7 AND S8L. DENT DIMENSIONS ARE: (P1).800L X.650W X.004D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***************
- [SDR A6WA202112078008](https://openairdocs.org/sdr/A6WA202112078008.md): Skin · gouged · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > MAINTENANCE FOUND 1 EACH SCRATCH AT FS 409+48 AND S25L+4 ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1).600"L X.500"W X.005"D. SCRATCH WAS FOUND NOT TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE****
- [SDR A6WA202112078009](https://openairdocs.org/sdr/A6WA202112078009.md): Skin · dented · Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 559+80 AND S7R+3. DENT DIMENSIONS ARE: (P1).600L X.350W X.005D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***********

Next page: https://openairdocs.org/aircraft/N435AW/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 = 'N435AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N435AW/reports

---
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.