# Service difficulty reports: N411ZW

A list on [N411ZW](https://openairdocs.org/aircraft/N411ZW.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 · 234 reports

- [SDR A6WA202610098917](https://openairdocs.org/sdr/A6WA202610098917.md): Downlock · faulted · Oct 9, 2026 · N411ZW · Cndair CL6002B19 · Landing Gear Position and Warning
  > WHILE CLIMBING RECEIVED GEAR DISAGREE WARNING FOR APOX 10 SECONDS. NOSE GEAR DID NOT DISPLAY STATUS. OCCURRED WHEN GEAR WAS ALREADY RETRACTED. AIRCRAFT REMOVED FROM SERVICE. R & R NLG HARNESS DOWNLOCK NR1 IAW 32-61. OPS CHECKED GOOD.
- [SDR A6WA202501318855](https://openairdocs.org/sdr/A6WA202501318855.md): Driver Unit · faulted · Jan 31, 2025 · N411ZW · Cndair CL6002B19 · Central Computers
  > AFTER ARRIVE A/C, BURNING SMELL ON EXT AC POWER. SWITCHED TO APU GEN. OVERHEAD PANEL LIGHTS FLICKERING AND BURNING SMELL CONTINUED NEAR 1 & 2 BREAKER PANELS. AIRCRAFT REMOVED FROM SERVICE. FOUND LAMP TEST #1 TO NOT BE WORKING AND PBA FLICKERING R&R LAMP DRI
- [SDR A6WA202409308830](https://openairdocs.org/sdr/A6WA202409308830.md): Seat Track · corroded · Sep 30, 2024 · N411ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 16 EA BLENDED AREAS P11 TO P26 FOUND OUT OF LIMITS ON FLOOR BEAM RAIL AT FS559+121 TO FS621 LBL27. REMOVED AND REPLACED 1EA FLOOR BEAM RAIL (P/N; N126-1577-56830), 4EA BEAM (P/N; 600-35031-307, 600-35031-308, 600-35031-309, AND 600-35031-310), AND 1EA BEA
- [SDR A6WA202409298832](https://openairdocs.org/sdr/A6WA202409298832.md): Floor Support · corroded · Sep 29, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE HAS SEVERAL AREAS WITH CORROSION BETWEEN FS559+80 AND FS621 LBL9. AIRCRAFT REMOVED FROM SERVICE. BLENDED AND EVALUATED 28 AREAS OF CORROSION BETWEEN FS559 TO FS621 LBL8 TO LBL10 FOUND TO BE STRUCTURALLY ACCEPTABLE IAW REO 601R-53-00-0
- [SDR A6WA202409298831](https://openairdocs.org/sdr/A6WA202409298831.md): Skin · eroded · Sep 29, 2024 · N411ZW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH OUTBOARD LEADING EDGE SKIN P/N 601R12074-4 OUT OF LIMITS AFTER EROSION REMOVAL. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RH OUTBOARD LEADING EDGE P/N 601R12074-4 AT WS350.348 TO WS389.00. REF CRJ-200 SRM 51-42-06, AND 51-42-13 REV 39. UPPER EDG
- [SDR A6WA202409238822](https://openairdocs.org/sdr/A6WA202409238822.md): Floor Support · damaged · Sep 23, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 20144 327672 453-170-500 Ï¿½ MFG50317. 74.45MHRS FLOOR SILL AT FS513+9 LBL42 TOOL MARK ON PRESSURE FLOOR SILL PANEL AT FS513+9 LBL42. AIRCRAFT REMOVED FROM SERVICE PERFORMED REPAIR ON PRESSURE FLOOR SILL PANEL AT FS513+9 AND LBL42. ALL WORK WAS PERFORMED
- [SDR A6WA202409238820](https://openairdocs.org/sdr/A6WA202409238820.md): Floor Support · corroded · Sep 23, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BLENDED AREA FOUND OUT OF LIMITS ON FLOOR SUPPORT AT FS559 RBL9. AIRCRAFT REMOVED FROM SERVICE REPAIRED AREA ON FLOOR SUPPORT STRUCTURE AT FS559 AND RBL9 IAW MHIRJ REO 601R-53-41-3255 REV--. DATED 2024-09-18.
- [SDR A6WA202409238813](https://openairdocs.org/sdr/A6WA202409238813.md): Trim Panel · cracked · Sep 18, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRIM EDGE FOUND BROKEN AND CORRODED ON WARDROBE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED TRIM EDGE ON WARDROBE IAW CMM 25-20-52 REV 8, AND CRJ200 SRM 51-22-00 REV 39.
- [SDR A6WA202409178809](https://openairdocs.org/sdr/A6WA202409178809.md): Seat Track · damaged · Sep 17, 2024 · N411ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PILOTS SEAT TRACK LH FWD SECTION MISSING HI-LITE FASTENERS REMOVED AND REPLACED PILOT SEAT TRACK P/N 601R41082-11 REF CRJ200 SRM 51-41-02 REV39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004393 CARD NO. 20078. TT: 44,686:36, TC: 42,772 AIRCRAFT REMOVED
- [SDR A6WA202409168808](https://openairdocs.org/sdr/A6WA202409168808.md): Floor Support · corroded · Sep 16, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL AT FS559+14 RBL42 BLEND AREA P3 ON RH FLOOR SILL AT FS559+14 RBL42 OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL P/N 601R38842-3 AT FS559.00 TO FS559+16 RBL42. ALL WORK WAS PERFORMED IAW SRM 51-42-06 REV 39, CRJ200 SRM 51-40-20 REV 39. ALL W
- [SDR A6WA202409048803](https://openairdocs.org/sdr/A6WA202409048803.md): Floor Support · cracked · Sep 4, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR STRUCTURE AT FS153 LBL30 AND WL79.50. AIRCRAFT REMOVED FROM SERVICE. REMOVED ANGLE P/N 601R75251-13.CUT AWAY CRACKED PORTION OF FLOOR PANEL 601R33101-117. & LOWER FLANGE BRACKET P/N 601R75251-13.BETWEEN FS559-621 LBL27 FABRICATED AND INSTALLED
- [SDR A6WA202409038802](https://openairdocs.org/sdr/A6WA202409038802.md): Floorbeam · corroded · Sep 3, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND RBL27 - 36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND RBL27 - 36 WITH FABRICATED NEW STRAP WITH MATERIAL 7075-T6, THI
- [SDR A6WA202409038801](https://openairdocs.org/sdr/A6WA202409038801.md): Seat Track · corroded · Sep 3, 2024 · N411ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK PN 20276-288-0-0 AT FS364.00 TO 559.00 +80 LHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS544.00 TO FS599.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 5
- [SDR A6WA202408278797](https://openairdocs.org/sdr/A6WA202408278797.md): Strap · corroded · Aug 27, 2024 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR STRAP L/H AT FS559.00 AND LBL27-36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 1EA STRAP PN 601R31025-29 ON FLOOR STRAP L/H AT FS559.00 AND LBL27 TO 36. IAW CRJ-200 SRM 51-42-06 REV 36.. PERFORMED HFEC WITH NO INDICATIONS. RESTO
- [SDR A6WA202409038800](https://openairdocs.org/sdr/A6WA202409038800.md): Seat Track · corroded · Aug 26, 2024 · N411ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK PN 20276-288-0-0 AT FS544.00 TO 559.00 RHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS544.00 TO FS599.00 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01
- [SDR A6WA202309268655](https://openairdocs.org/sdr/A6WA202309268655.md): Control Lever · failed · Sep 26, 2023 · N411ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH RECEIVED FLAP FAIL AT 20 DEGREES. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT PER FIM SUPP. 98-018I. REMOVED AND REPLACED FLAP CONTROL LEVER IAW AMM SUPP. 09-038A. OPS CHECKS GOOD. REMOVED PLACARD + FROM MEL.
- [SDR A6WA202304038539](https://openairdocs.org/sdr/A6WA202304038539.md): Drive Unit · unknown · Apr 3, 2023 · N411ZW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > RECIEVED FLAPS FAIL CAUTION MSG FLAPS FAIL AT 20* IN FLIGHT. PERFORMED FLAP RESET PROCEDURES IAW AWAC SUP 09-018I BOX 12 FLAPS RESET ********AIRCRAFT REMOVED FROM SERVICE******** R&R FLAP PDU
- [SDR A6WA202302098460](https://openairdocs.org/sdr/A6WA202302098460.md): Proximity Sensor · none · Feb 9, 2023 · N411ZW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER DROPPING LDG GEAR 5MIN LATER NOSE DOOR OPEN WARN MSG ANTI SKID IB/OB CAU MSG AND PARK BRAKE SOV/ PROX SYS CAU MSGS. C/W QRH LANDED NORMAL. TAXIED OFF RUNWAY. GOT TOWED TO GATE. HAD 3 GREENS BUT PULLED EMER GEAR RELASE HANDLE PER QRH. ******AIRCRAFT REM
- [SDR A6WA202112228031](https://openairdocs.org/sdr/A6WA202112228031.md): None · none · Dec 22, 2021 · N411ZW · Cndair CL6002B19 · Doors
  > ON CLIMB OUT, HEARD LOUD SQUEAL FROM PAX DOOR AREA. ABOVE 11,000' COULD NOT MAINTAIN CABIN PRESSURE. PACKS NORMAL, DOOR INDICATIONS NORMAL. DIVERTED TO MKE. ***AIRCRAFT REMOVED FROM SERVICE*** R/R PAX DOOR SEAL PER AWA SUP 21-023 AND AMM 52-11-10 OPS AND
- [SDR A6WA2019121847057](https://openairdocs.org/sdr/A6WA2019121847057.md): Skin · dented · Dec 14, 2019 · N411ZW · Cndair CL6002B19 · Spoilers
  > LEFT WING, I/B GROUND SPOILER LOWER SURFACE HAS ROCK DAMAGE. AIRCRAFT REMOVED FROM SERVICE REPAIRED LEFT WING I/B GROUND SPOILER IAW EA# AWAC-CRJ257-01402 REV-IR.
- [SDR A6WA2019121247055](https://openairdocs.org/sdr/A6WA2019121247055.md): Floor Support · damaged · Dec 11, 2019 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SILL AT CARGO DOOR HAS SEVERAL ELONGATED HOLES AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLOOR SILL AT CARGO DOOR IAW BOMB. REO 601R-53-61-690 REV. D
- [SDR A6WA2019121147053](https://openairdocs.org/sdr/A6WA2019121147053.md): Post · cracked · Dec 11, 2019 · N411ZW · Cndair CL6002B19 · Fuselage Main, Structure
  > BS 409+128 VERTICLE POST AT RBL 18 WAS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE VERTICLE POST IAW REO 601R-53-41-889.
- [SDR A6WA2019121247056](https://openairdocs.org/sdr/A6WA2019121247056.md): Angle · damaged · Dec 10, 2019 · N411ZW · Cndair CL6002B19 · Service Doors
  > SUPPLEMENTAL INFORMATION, INSIDE OF SERVICE DOOR HAS SEVERAL IMPROPERLY INSTALLED AND MISSING FASTENERS AND DAMAGED ANGLES AT FS 342.00, WL 73.50 TO WL 93.50. AIRCRAFT REMOVED FROM SERVICE. REPAIRED SERVICE DOOR IAW SRM 51-42-06, 51-42-10, 51-42-21 AND 51-42
- [SDR A6WA2019121147050](https://openairdocs.org/sdr/A6WA2019121147050.md): Angle · damaged · Dec 10, 2019 · N411ZW · Cndair CL6002B19 · Galley Doors
  > INSIDE SERVICE DOOR HAS SEVERAL IMPROPERLY INSTALLED AND MISSING FASTENERS AND DAMAGE ANGLE AT FS 342.00 WL 73.5 AND WL93.50 AIRCRAFT REMOVED FROM SERVICE REPAIRED SERVICE DOOR IAW CRJ 200 SRM 51-42-06 51-42-10 51-42-21 AND 51-42-22
- [SDR A6WA2019121147049](https://openairdocs.org/sdr/A6WA2019121147049.md): Structure · cracked · Dec 10, 2019 · N411ZW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR EDGE MEMBER CRACKED ON FWD SIDE OF DOOR AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED EDGE MEMBER IAW CRJ-200 SRM 51-42-06 AND 51-42-10
- [SDR A6WA2019121047048](https://openairdocs.org/sdr/A6WA2019121047048.md): Doubler · cracked · Dec 7, 2019 · N411ZW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > 436AL HAS CRACKED DOUBLER AT MOUNTING HOLE PANEL AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED DOUBLER AT MOUNTING HOLE ON PANEL 436AL IAW BOMB. CMM 20-42-06
- [SDR A6WA2019121047044](https://openairdocs.org/sdr/A6WA2019121047044.md): Floor Support · corroded · Dec 4, 2019 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL CORRODED AT FS 319.00. AIRCRAFT REMOVED FROM SERVICE REPLACED FLOOR SILL IAW CRJ200 SRM 51-42-06.
- [SDR A6WA2019120647041](https://openairdocs.org/sdr/A6WA2019120647041.md): Doubler · corroded · Dec 4, 2019 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL GALLEY SHOOT BOLT MOUNT BETWEEN FS310 AND FS319 HAS CORROSION AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H FLOOR SILL GALLEY MOUNT IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2019112647037](https://openairdocs.org/sdr/A6WA2019112647037.md): Skin · cracked · Nov 24, 2019 · N411ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PANEL 435AB HAS CRACKED AREA ON INSODE SKIN PANEL, AIRCRAFT REMOVED FROM SERVICE, REPAIR INNER SKIN IAW BOMBARDIER CMM 71-12-01 SRS0460
- [SDR A6WA2019112647036](https://openairdocs.org/sdr/A6WA2019112647036.md): Retainer · cracked · Nov 22, 2019 · N411ZW · Cndair CL6002B19 · Passenger/Crew Doors
  > SUPPLEMENTAL INFORMATION, PASSENGER DOOR LOWER CENTER SEAL RETAINER DAMAGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PASSENGER DOOR SEAL RETAINER IAW SUPP 18-014A.
- [SDR A6WA2019112647038](https://openairdocs.org/sdr/A6WA2019112647038.md): Attach Angle · cracked · Nov 22, 2019 · N411ZW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO BEAM MEMBER AFT ATTACH ANGLE CRACKED, AIRCRAFT REMOVED FROM SERVICE, REMOVED AND REPLACED CRACKED ANGLE ON CARGO BEAM MEMBER IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2019112047023](https://openairdocs.org/sdr/A6WA2019112047023.md): Seal · chafed · Nov 18, 2019 · N411ZW · Cndair CL6002B19 · Engine Cowling System
  > SUPPLEMENTAL INFORMATION, PANEL 432AT ACCESS COWL HAS CHAFED AFT SEAL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT EDGE STRIP IAW CMM 71-14-01.
- [SDR A6WA2019112047017](https://openairdocs.org/sdr/A6WA2019112047017.md): Bracket · cracked · Nov 15, 2019 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BRACKET FOR EXTERNAL SERVICE BOX CRACKED INSIDE PANEL 122CR AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-06 AND SRM 51-41-02
- [SDR A6WA2018081645986](https://openairdocs.org/sdr/A6WA2018081645986.md): Windshield · failed · Aug 14, 2018 · N411ZW · Cndair CL6002B19 · Flight Compartment Windows
  > FIRST OFFICER`S WINDSHIELD SHATTERED IN FLIGHT. COMPLIED WITH QRH.
- [SDR A6WA2017112745448](https://openairdocs.org/sdr/A6WA2017112745448.md): Plug · missing · Nov 26, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CUT OUT AT BS 222, STRINGER 22L HAS MISSING FREEZE PLUG FOR CHEEK PANEL 131AL.
- [SDR A6WA2017112745449](https://openairdocs.org/sdr/A6WA2017112745449.md): Angle · cracked · Nov 26, 2017 · N411ZW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR ASSIST MOTOR LOWER ANGLE CRACKED.
- [SDR A6WA2017112745447](https://openairdocs.org/sdr/A6WA2017112745447.md): Retainer · cracked · Nov 26, 2017 · N411ZW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER FWD SEAL RETAINER CRACKED.
- [SDR A6WA2017113045444](https://openairdocs.org/sdr/A6WA2017113045444.md): Skin · torn · Nov 25, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PAX DOOR CUTOUT FWD LOWER CORNER SKIN TORN.
- [SDR A6WA2017112045440](https://openairdocs.org/sdr/A6WA2017112045440.md): Seal · cracked · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Spoilers
  > RIGHT FLT SPOILER CENTER SPRING SEAL IS CRACKED.
- [SDR A6WA2017112045443](https://openairdocs.org/sdr/A6WA2017112045443.md): Bracket · cracked · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT ACCESSORY BAY, HYDRAULIC SYSTEM NR 2 PRESSURE AND RETURN MANIFOLD MOUNT BRACKET CRACKED.
- [SDR A6WA2017112045441](https://openairdocs.org/sdr/A6WA2017112045441.md): Seal · cracked · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Spoilers
  > LEFT FLT SPOILER INBD SPRING SEAL IS CRACKED.
- [SDR A6WA2017112045439](https://openairdocs.org/sdr/A6WA2017112045439.md): Angle · cracked · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT THE INBD SIDE OF STRINGER 14L IN THE AFT EQUIPMENT BAY.
- [SDR A6WA2017112045438](https://openairdocs.org/sdr/A6WA2017112045438.md): Angle · cracked · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT THE INBD SIDE OF FRAME BS 625.3, STRINGER 13R IN THE AFT EQUIPMENT BAY, JUST AFT OF 621 BULKHEAD.
- [SDR A6WA2017112045442](https://openairdocs.org/sdr/A6WA2017112045442.md): Bracket · broken · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING BRACKET BROKEN IN THE R/H MLG WHEEL WELL FS530 AND RBL23.
- [SDR A6WA2017112045437](https://openairdocs.org/sdr/A6WA2017112045437.md): Angle · cracked · Nov 19, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT THE INBD SIDE OF BS 625.3, STRINGER 13L IN THE AFT EQUIPMENT BAY AFT OF PRESSURE BULKHEAD.
- [SDR A6WA2017112045434](https://openairdocs.org/sdr/A6WA2017112045434.md): Intercostal · cracked · Nov 18, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY BAY INTERCOSTAL AT BS 621 - 625, STRINGER 14L CRACKED.
- [SDR A6WA2017112045435](https://openairdocs.org/sdr/A6WA2017112045435.md): Intercostal · cracked · Nov 18, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT ACCESSORY BAY INTERCOSTAL AT BS 621 - 625, STRINGER 15L IS CRACKED
- [SDR A6WA2017112045436](https://openairdocs.org/sdr/A6WA2017112045436.md): Intercostal · cracked · Nov 18, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 1014984 3000-0026 - AFT ACCESSORY BAY INTERCOSTAL AT FS621-FS625 AT STRL13L CRACKED
- [SDR A6WA2017112045431](https://openairdocs.org/sdr/A6WA2017112045431.md): Static Wick · cracked · Nov 17, 2017 · N411ZW · Cndair CL6002B19 · Pitot/Static System
  > RIGHT AILERON STATIC WICK BASE IS CRACKED.
- [SDR A6WA2017112045433](https://openairdocs.org/sdr/A6WA2017112045433.md): Floorbeam · corroded · Nov 17, 2017 · N411ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE AT BS 621 HAS CORROSION BETWEEN LBL 9 AND LBL 27 IN THE CARGO BAY.

Next page: https://openairdocs.org/aircraft/N411ZW/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 = 'N411ZW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N411ZW/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.