# Service difficulty reports: N436AW

A list on [N436AW](https://openairdocs.org/aircraft/N436AW.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 4 · 177 reports

- [SDR A6WA202401158698](https://openairdocs.org/sdr/A6WA202401158698.md): Proximity Sensor · out of adjust · Jan 15, 2024 · N436AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > WHEN SELECTING LANDING GEAR UP RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE WARNING MSG APPEARED IN 2-3 SECONDS C/W QRH MSG CLEARED NORMAL SMOOTH LANDING. LANDING WT 34,750LBS. AIRCRAFT REMOVED FROM SERVICE. READJUSTED GAP ON NLG CENTERED/EXTENDED PROXIMITY SE
- [SDR A6WA202301048689](https://openairdocs.org/sdr/A6WA202301048689.md): Unknown · unknown · Jan 4, 2024 · N436AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > AFTER T/O RECEIVED GEAR DISAGREE WARN MSG, C/W QRH DIVERTED TO MKE. MSG APPEARED IMMEDIATELY AFTER SELECTING GEAR UP. NOSE DOOR WARNING ALSO PRESENT. CONT BLK 4 WAS NOSE GEAR INDICATED GREEN, MAIN GEAR INDICATED AMBER. PULLED EMERGENCY GEAR HANDLE, ALL INDICA
- [SDR A6WA202306308634](https://openairdocs.org/sdr/A6WA202306308634.md): Control Unit · unknown · Jun 30, 2023 · N436AW · Cndair CL6002B19 · Ice/Rain Protection System
  > WHILE IN CRUSE RECIEVED RIGHT ANTI DUCT WARNING, C/W QRH MSG CLEARED. MSG CLEARED WHE 14TH STAGE SOV CLOSED. MSG OCCURED WHEN ANTI ICE SELECTED OFF. MOC NOTE CREW DECLAIRED AN EMERGENCY DUE TO THE FACT THAT THE TR'S WOULD NOT BE AVAILABEL DURING LANDING.
- [SDR A6WA202303138499](https://openairdocs.org/sdr/A6WA202303138499.md): Bulkhead · cracked · Mar 13, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > E17/003/453 - FS621 PRESS BULKHD WEB MOD ********AIRCRAFT REMOVED FROM SERVICE********** COMPLIED WITH 601R-53-1240 REV D DATED 10-31-2016, REPAIR AND MODIFICATION TO F.S.621.00 PRESSURE BULKHEAD WEB.
- [SDR A6WA202303138497](https://openairdocs.org/sdr/A6WA202303138497.md): Support · cracked · Mar 13, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > WHILE REMOVING FS 621 LINTEL SUPPORT, FOUND 1EA "BUILD UP" LEG, P/N: 601R35212-103 TO BE CRACKED. ********AIRCRAFT REMOVED FROM SERVICE********** LOCATED AND DRILLED 1EA NEW "BUILD UP" LEG, P/N: 601R35212-103 FOR FS 621 LINTEL SUPPORT IAW CRJ 200 SRM 51-40-11.
- [SDR A6WA202303138496](https://openairdocs.org/sdr/A6WA202303138496.md): Fitting · cracked · Mar 13, 2023 · N436AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RH WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED IN THE UPPER AFT RADIUS. FAILED DETAILED VISUAL INSPECTION. *********AIRCRAFT REMOVED FROM SERVICE********* REMOVED CRACKED R/H SIDE POST LOWER FITTING AT WL 110.00 PN 601R33235-4 IAW AIR WISCONSIN CRJ 200 S
- [SDR A6WA202303128495](https://openairdocs.org/sdr/A6WA202303128495.md): Fitting · none · Mar 12, 2023 · N436AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > NEW CENTER POST LOWER R/H FITTING MISDRILLED. ******AIRCRAFT REMOVED FROM SERVICE******** REPAIRED CENTER POST LOWER RH FITTING IAW MHIRJ REO 601R-53-11-3832 REV-A DATED 2023-03-03
- [SDR A6WA202303118494](https://openairdocs.org/sdr/A6WA202303118494.md): Angle · corroded · Mar 11, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX DOOR LOWER SILL ANGLE CORRODED. *******AIRCRAFT REMOVED FROM SERVICE******** REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE (P/N 601R31527-221S) IAW CRJ 200 SRM 51-41-06, 51-42-13, 51-42-21.
- [SDR A6WA202303098517](https://openairdocs.org/sdr/A6WA202303098517.md): Unknown · unknown · Mar 9, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > ON FWD SIDE OF FS 621 BULKHEAD ABOVE AFT BAGGAGE BAY DOOR FOR LINTEL REPAIR ACCESS FOUND RIV-NUT TO BE FREE SPINNING *********AIRCRAFT REMOVED FROM SERVICE*********** COMPLIED WITH MHIRJ REO 601R-53-61-7980 REV-- DATED 2023-03-10.
- [SDR A6WA202302198504](https://openairdocs.org/sdr/A6WA202302198504.md): Floor Skin · gouged · Feb 19, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > PRESSURE FLOOR SKIN IS GOUGED AT FS 499 BETWEEN BL 0 AND LBL 9 APPROXIMATELY 0.75" LONG AND.005" DEEP. ******AIRCRAFT REMOVED FROM SERVICE********** COMPLIED WITH MHIRJ REO 601R-53-41-3123 REV -- DATED 2023-03-06.
- [SDR A6WA202302198508](https://openairdocs.org/sdr/A6WA202302198508.md): Unknown · unknown · Feb 19, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DURING INCORPORATION OF BOMBARDIER REO 601R-53-61-1240 REV -D FOUND PREVIOUS REPAIR BOMBARDIER REO 601R-53-61-1541 ON RBL 27.50 TO BE INSTALLED INCORRECTLY. DEVIATION FOR 601R-53-61-1240 OR REACCOMPLISH REO 601R-53-61-1541 TO CORRECTLY INCORPORATE BOMBARDIER R
- [SDR A6WA202302178505](https://openairdocs.org/sdr/A6WA202302178505.md): Door · cracked · Feb 17, 2023 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > INDICATION FOUND ON FWD SIDE RPB WEB FS 621 CARGO DOOR LINTEL APPROXIMATELY.200" LONG. FAILING NDT. ********AIRCRAFT REMOVED FROM SERVICE******** COMPLIED WITH MHIRJ REO 601R-53-6-7973 REV -- DATED 2023-03-09 AND BOMBARDIER REO 601R-53-61-1230 REV. -F DATED 2
- [SDR A6WA202205188185](https://openairdocs.org/sdr/A6WA202205188185.md): Steering Sys · warning light · May 29, 2022 · N436AW · Cndair CL6002B19 · Steering Unit
  > RECEIVED STEERING INOP CAUTION MSG IN FLIGHT. C/W QRH MSG PERSISTED. C/W FIM RESET MSG REMAINED. ***AIRCRAFT REMOVED FROM SERVICE **** R&R RT FEEDBACK RVDT IAW AMM 32-51-20. REQ ADJUSTMENT. OPS CHECK GOOD P/N OFF: 16735-109, S/N OFF: 4520
- [SDR A6WA202202088160](https://openairdocs.org/sdr/A6WA202202088160.md): Fitting · corroded · Feb 8, 2022 · N436AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR FORWARD COUNTER BALANCE ANCHOR FITTING ASSEMBLY AT FS310.00 IS CORRODED. ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED PAX DOOR FORWARD COUNTER BALANCE ANCHOR FITTING ASSEMBLY PN 601R38075-4 AT FS310.00. RESTORED PROTECTIVE FINISH. ALL W
- [SDR A6WA202202028159](https://openairdocs.org/sdr/A6WA202202028159.md): Fitting · corroded · Feb 2, 2022 · N436AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT TRACK FROM FS559.00 + 48 TO FS559.00 + 64 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS559.00 + 48 TO FS559.00 + 64. RESTORED PROTECTIVE FINISH. ALL WORK WI
- [SDR A6WA202201088168](https://openairdocs.org/sdr/A6WA202201088168.md): None · cracked · Jan 8, 2022 · N436AW · Cndair CL6002B19 · Fuselage Structure (General)
  > TWO EACH CRACKS FOUND AT PRESSURE FLOOR SUPPORT STRUCTURE AT FS 484.00 & RBL 36 AS FOLLOW: (P1) 1.00"L CRACK ON LOWER O/B CORNER OF INTERCOSTAL DWG #601R31171-15 AND (P2).400"L CRACK ON UPPER SIDE OF BEND RADIUS ON CLIP DWG #601R31171-09. **************AIRC
- [SDR A6WA202201088167](https://openairdocs.org/sdr/A6WA202201088167.md): Winglet · dented · Jan 8, 2022 · N436AW · Cndair CL6002B19 · Wing Structure
  > AIRCRAFT L/H WINGLET O/B SKIN HAS 1 EACH DENT AT WS 12.5 TO WS 19.00 & WINGLET F/S AND R/S. DENT DIMENSION IS: (P1) 2.6"L X.900"W X.015"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-31-31 REV 38 FIG 1 SHT 1. ****************AIR
- [SDR A6WA202201088150](https://openairdocs.org/sdr/A6WA202201088150.md): None · none · Jan 8, 2022 · N436AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > DAMAGED HOLES (4 EACH) FOUND UNDER PASSENGER DOOR HINGE (FUSELAGE SIDE) AT SKIN PANEL, DOUBLER, AND LONGERON WITH DIMENSIONS AS FOLLOW: (H1) =.267"L X.170"W AT FS 317.70 STR 17L-18L; (H2) =.295"L X.176"W AT FS 331.2 STR 17L-18L; (H3) =.236"L X.164"W AT FS
- [SDR A6WA202201088149](https://openairdocs.org/sdr/A6WA202201088149.md): None · none · Jan 8, 2022 · N436AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) IS WORN BEYOND ALLOWABLE LIMITS IAW CRJ 200 AMM 52-11-00 REV 64. ************AIRCRAFT REMOVED FROM SERVICE************************** REMOVED AND REPLACED PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) IAW CRJ200 SRM 53-
- [SDR A6WA202102167634](https://openairdocs.org/sdr/A6WA202102167634.md): Shutoff Valve · malfunctioned · Feb 14, 2021 · N436AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > 306717/1- WHILE CLIMBING RECEIVED RH WING ANTI-ICE CAUTION MESSGAE. CW QRH AND MESSAGE CLEARED. INCREASED POWER ON RH SIDE. OPENED 14 STAGE ISOL VALVE. MESSAGE CLEARED AFTER OPENING VALVE. 306717/2- RECEIVED LEFT COWL ANTI-ICE CAUTION MESSAGE WITH COWL SWITC
- [SDR A6WA202102167633](https://openairdocs.org/sdr/A6WA202102167633.md): Fmc · malfunctioned · Feb 14, 2021 · N436AW · Cndair CL6002B19 · Flight Management Computing Hardware System
  > LOST FMS ON APPROACH INTO CHICAGO. RECEIVED RED FMS FLAG ON BOTH PFDS. FMS DISPLAY SHOWS NO INPUT DATA, FMS. ***AIRCRAFT REMOVED FROM SERVICE*** NOTED BY MAINTENANCE COMPLIED WITH BOMBARDIER/MHI FIM RESET, MESSAGE CLEARED AND FMS OPERATES NORMALLY.
- [SDR A6WA202101047508](https://openairdocs.org/sdr/A6WA202101047508.md): Skin · gouged · Jan 3, 2021 · N436AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DAMAGED HOLE FOUND AT FS 621-105'' AND BETWEEN STRG 16L TO STRG 17L. AIRCRAFT REMOVED FROM SERVICE. REMOVED NUT PLATE AT FS 621-105'' AND BETWEEN STRG 16L TO STRG 17L, REF CRJ-200 SRM 51-45-00 REV 38. OPENED ELONGATED HOLE TO A NEW DIAMETER OF 0.284'', REF:
- [SDR A6WA202101047503](https://openairdocs.org/sdr/A6WA202101047503.md): Floor Support · corroded · Jan 2, 2021 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION SPOT ON RT PRESSURE FLOOR SILL PNL FS 409+133 AND RBL 34. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR SILL PNL FS 409+133 AND RBL 34 BY BLENDING. BLENDED AREA MEASURED 1.100''L X 0.900''W, REF BOMBARDIER REO 601R-53-41-666
- [SDR A6WA202101047504](https://openairdocs.org/sdr/A6WA202101047504.md): Floor Support · corroded · Jan 2, 2021 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION SPOT ON RT PRESSURE FLOOR ANGLE FS 474.15 AND RBL 34. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 474.15 AND RBL 34 BY BLENDING. BLENDED AREA MEASURED 2.600''L X 2.00''W, REF BOMBARDIER REO 601R-53-41-666 REV C DA
- [SDR A6WA202101047505](https://openairdocs.org/sdr/A6WA202101047505.md): Floor Support · corroded · Jan 2, 2021 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION SPOT ON RT PRESSURE FLOOR ANGLE FS 474.15 AND RBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 476.15 AND RBL 27 BY BLENDING. BLENDED AREA MEASURED 2.038''L X 1.400''W, REF BOMBARDIER REO 601R-53-41-666 REV C D
- [SDR A6WA202101047507](https://openairdocs.org/sdr/A6WA202101047507.md): Floor Support · corroded · Jan 2, 2021 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON 3 SPOTS WITHIN 1.5'' OF EACH OTHER ON RT PRESSURE FLOOR ANGLE FS 474.15 AND RBL 33 TO RBL 34. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE 3 SPOTS FS 474.15 AND RBL 33 TO RBL 34. BY BLENDING P1 OF BLENDED AREA FS47
- [SDR A6WA202101047506](https://openairdocs.org/sdr/A6WA202101047506.md): Floor Support · corroded · Jan 2, 2021 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION SPOT ON RT PRESSURE FLOOR ANGLE FS 518 AND RBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 518 AND RBL 27 BY BLENDING. BLENDED AREA MEASURED 1.342''L X 0.897''W, REF BOMBARDIER REO 601R-53-41-666 REV C DATED 2
- [SDR A6WA202101257562](https://openairdocs.org/sdr/A6WA202101257562.md): Channel · corroded · Dec 29, 2020 · N436AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LT WING HAS CORROSION AT WS 50 UPON FURTHER INSPECTION, CHANNEL, ANGLE, AND LOWER SKIN PANEL HAS CORROSION, REF CRJ200 51-11-00, (REV 38). AIRCRAFT REMOVED FROM SERVICE. REMOVED LOWER SKIN PANEL, REF CRJ200 SRM 51-42-21, (REV 38). REMOVED CORROSION ON LOWER
- [SDR A6WA202012167461](https://openairdocs.org/sdr/A6WA202012167461.md): Shim · damaged · Dec 14, 2020 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK ATTACH BRACKET AT 2 EA RIVETS JUST BELOW FED LOWER DOOR STOPS. AIRCRAFT REMOVED FROM SERVICE. REMOVED LOWER ATTACH BRACKET AT CARGO DOOR FABRICATED NEW CHANNEL FROM 2024T-3.050" ALODINE, PRIME, AND TOPCOAT INSTALLED, REF CRJ 200 SRM 51-
- [SDR A6WA202012187465](https://openairdocs.org/sdr/A6WA202012187465.md): Skin · gouged · Dec 11, 2020 · N436AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE SKIN AT ADF ANTENNA MATING SURFACE HAS SCRIBE MARKS AROUND OUTER EDGE. AIRCRAFT REMOVED FROM SERVICE. BLENDED AREA TO SMOOTH CONTOUR AT FS 409+64 TO FS 409+80, STR 1L TO STR 1R. REMOVED AND REPLACED SOLID FASTENER AT BLENDED AREA, REF ASAP EA
- [SDR A6WA202012187464](https://openairdocs.org/sdr/A6WA202012187464.md): Skin · corroded · Dec 11, 2020 · N436AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE ADF ANTENNA HAS PITTING CORROSION AROUND OUTER EDGES. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON UPPER SKIN FS 409+64 TO FS 409+80, STR 1L AND STR 1R. REMOVED AND REPLACED SOLID FASTENER AT BLENDED AREA, REF ASAP EA: AWAC-CRJ253-0154
- [SDR A6WA202101187547](https://openairdocs.org/sdr/A6WA202101187547.md): Angle · cracked · Dec 5, 2020 · N436AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > CRACKED ANGLE AT LT HAND WHEEL WELL TOP OF INTERCOSTAL WS 48.3. AIRCRAFT REMOVED FROM SERVICE. REMOVED CRACKED ANGLE AT LT HAND WING STATION 48.3, REF AIRWIS SUPPLEMENT NR 15-287A DATE ISSUED: AUG 23, 2016. DRILLED AND DEBURRED NEW ANGLE DRAWING NR 600-1020
- [SDR A6WA2019061046650](https://openairdocs.org/sdr/A6WA2019061046650.md): Warning Message · illuminated · Jun 7, 2019 · N436AW · Cndair CL6002B19 · Trailing Edge Flaps
  > DURING APPROACH, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY, COORDINATED WITH DISPATCH, COMPLETED THE NECESSARY CHECKLISTS AND LANDED WITHOUT INCIDENT. ONCE ON THE GATE FLAPS WERE SUCCESSFULLY RESET AND PLACED ON MEL.
- [SDR A6WA2017101345358](https://openairdocs.org/sdr/A6WA2017101345358.md): Warning Message · illuminated · Oct 12, 2017 · N436AW · Cndair CL6002B19 · Overheat Detection
  > INFLIGHT APROX 6000', PRIOR TO LANDING IAD, RECEIVED RIGHT 14TH. DUCT OVERHEAT WARNING WITH ASSOCIATED CHIME AND MASTER WARNING. C/W QRH, MESSAGE EXTINGUISHED APROX 4-5 MIN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT.
- [SDR A6WA201744919](https://openairdocs.org/sdr/A6WA201744919.md): Ballast · failed · Apr 11, 2017 · N436AW · Cndair CL6002B19 · Passenger Compartment Lighting
  > ELECTRICAL BURNING ODOR IN CABIN, POWERED AIRCRAFT DOWN. FOUND CEILING LIGHT BALLAST ABOVE ROW 11AC DISCOLORED. DISCCONNECTED THE BALLAST IAW AMM 33-21-10.
- [SDR A6WA201644112](https://openairdocs.org/sdr/A6WA201644112.md): Unknown · malfunctioned · Jul 18, 2016 · N436AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR WILL NOT OPEN FROM OUTSIDE.
- [SDR A6WA201644062](https://openairdocs.org/sdr/A6WA201644062.md): Fms · dislodged · Jul 2, 2016 · N436AW · Cndair CL6002B19 · Flight Management Computing Hardware System
  > FMS UNIT FELL OUT DURING TAKEOFF. ABORTED TAKEOFF AT APPROX 60 KNTS. BRAKE TEMPS NORMAL 3-2-3-3.
- [SDR A6WA201644014](https://openairdocs.org/sdr/A6WA201644014.md): Handle · stuck · Jun 17, 2016 · N436AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR OUTER HANDLE WILL NOT RELEASE FROM OUTSIDE.
- [SDR A6WA201643986](https://openairdocs.org/sdr/A6WA201643986.md): Handle · obstructed · Jun 9, 2016 · N436AW · Cndair CL6002B19 · Service Doors
  > UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. CLEANED AND LUBED SERVICE DOOR OUTER HANDLE. REMOVED DEBRIS FROM SERVICE DOOR OUTER HANDLE OUTER LATCH. OPS CHECK GOOD IAW AMM 52-40-0.
- [SDR A6WA201643963](https://openairdocs.org/sdr/A6WA201643963.md): Service Door · stuck · Jun 1, 2016 · N436AW · Cndair CL6002B19 · Service Doors
  > UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE.
- [SDR A6WA2016060243963](https://openairdocs.org/sdr/A6WA2016060243963.md): Handle · lack of lube · Jun 1, 2016 · N436AW · Cndair CL6002B19 · Service Doors
  > UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. LUBED SERVICE DOOR HANDLE & OPERATIONS CHECKED GOOD IAW 52-41-00.
- [SDR A6WA201643908](https://openairdocs.org/sdr/A6WA201643908.md): Jam-Nut · unsecure · May 19, 2016 · N436AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR DIFFICULT TO OPEN, UNLATCHES NORMAL, DIFFICULT TO PUSH OPEN. CLEANED & INSPECTION SERVICE DOOR SEAL. DOOR INSPECTION FOUND DOOR STOP ADJUSTMENT SCREW JAM NUT SAFETY CABLE DAMAGED. RE-SAFETIED JAM NUT AS REQUIRED. OPERATIONS CHECKED GOOD ALSO
- [SDR A6WA201643789](https://openairdocs.org/sdr/A6WA201643789.md): Plug · loose · Apr 14, 2016 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 131AL HAS A LOOSE FREEZE PLUG. REPLACED FREEZE PLUG IAW REO 601R-53-11-2886 REV C.
- [SDR A6WA201643787](https://openairdocs.org/sdr/A6WA201643787.md): Torque Box · cracked · Apr 14, 2016 · N436AW · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER TORQUE BOX CRACKED AT THE 5 O`CLOCK POSITION. REPAIRED RT ENG THRUST REVERSER TORQUE BOX IAW REO 601R-78-34-2527 REV B.
- [SDR A6WA201643788](https://openairdocs.org/sdr/A6WA201643788.md): Rib · damaged · Apr 14, 2016 · N436AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > UPON OK TO INSTALL FAIRING, DISCOVERED LT HORIZONTAL STAB OTBD TE RIB, LOWER FLANGE CUT OUT & MISSING NUTPLATE. R & R LT OTBD TE RIB IAW SRM 51-42-06 & 51-42-21.
- [SDR A6WA201643785](https://openairdocs.org/sdr/A6WA201643785.md): Door Sill · corroded · Apr 13, 2016 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING CORROSION REMOVAL FROM RT FLOOR SILL, FOUND EXISTING REPAIR AT FS 580 THAT IS CORRODED, REPAIRED.
- [SDR A6WA201643784](https://openairdocs.org/sdr/A6WA201643784.md): Door Sill · corroded · Apr 13, 2016 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL, BETWEEN FS 559+112 & 621, TOP & BOTTOM SIDES HAVE SEVERAL AREAS OF CORROSION, REPAIRED.
- [SDR A6WA201643779](https://openairdocs.org/sdr/A6WA201643779.md): Skin · chafed · Apr 12, 2016 · N436AW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON UPPER FIXED LE SKIN CHAFED, REPLACED.
- [SDR A6WA201643778](https://openairdocs.org/sdr/A6WA201643778.md): Skin · chafed · Apr 12, 2016 · N436AW · Cndair CL6002B19 · Ailerons
  > TWO EACH RT AILERON FIXED LE SKINS ARE CHAFED, REPLACED.
- [SDR A6WA201643777](https://openairdocs.org/sdr/A6WA201643777.md): Web · cracked · Apr 12, 2016 · N436AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FORWARD HYD NOSE COMPARTMENT CEILING AT FS 193 CRACKED, REPAIRED.

Next page: https://openairdocs.org/aircraft/N436AW/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 = 'N436AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N436AW/reports

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