# Service difficulty reports: N429AW

A list on [N429AW](https://openairdocs.org/aircraft/N429AW.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 · 190 reports

- [SDR A6WA202501318856](https://openairdocs.org/sdr/A6WA202501318856.md): Warning Light · illuminated · Jan 31, 2025 · N429AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER SELECTING THE GEAR UP WITH THE FLAPS AT 0 DEGREES. RECEIVED MOMENTARY GEAR DISAGREE WARNING. MESSAGE CLEARED ON ITS OWN AND QRH REVIEWED. GEAR EXTENDED NORMALLY FOR LANDING. AIRCRAFT REMOVED FROM SERVICE. OPEN.
- [SDR A6WA202411158843](https://openairdocs.org/sdr/A6WA202411158843.md): Strut · underserviced · Nov 15, 2024 · N429AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > AFTER SELECTING GEAR LEVER UP NOSE GEAR REMAINED DOWN RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WRINGING MSGS C/W QRH ALL GEAR DOWN AND NORMAL LANDING. SMOOTH LANDING, LAND WEIGHT WAS 46,700. GEAR MESSAGES APPEARED, APPROX 10 SECONDS AFTER SELECTION. MANUAL RE
- [SDR A6WA202410158837](https://openairdocs.org/sdr/A6WA202410158837.md): Engine · faulted · Oct 15, 2024 · N429AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > IN CLIMB RIGHT ENGINE HAD SPIKE IN ITT AND REDUCTION IN N1 AND N2 AND WAS UNRESPONSIVE FOR 10-20 SECONDS. THEN RETURNED TO NORMAL. ON APPROACH RIGHT ENGINE AGAIN HAD SAME INDICATION AND AIRCRAFT HAD VIBRATIONS. DURING BOTH EVENTS THRUST WAS BEING REDUCED BY PI
- [SDR A6WA202401148697](https://openairdocs.org/sdr/A6WA202401148697.md): Bracket · bent · Jan 14, 2024 · N429AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > GEAR DISAGREE WARNING AFTER SELECTING GEAR UP DEPARTING ORD. NLG NEVER MOVED & ALSO RECEIVED NLG DOOR OPEN WARING AFTER MLG DISAGREE WARING ACFT REMOVED FROM SERVICE. INTERROGATED PSEU & FOUND CODES: NG0EXT FAR S23, S35 NEAR NGDLK2, S21 NGDLK01, S22 FAR NGU
- [SDR A6WA202209208308](https://openairdocs.org/sdr/A6WA202209208308.md): Bushing · wrong part · Sep 16, 2022 · N429AW · Cndair CL6002B19 · Ailerons
  > ELONGATED HOLE DUE TO WRONG BUSHING INSTALLED. WRONG BUSHING OUTSIDE DIAMETER.750, INSIDE DIAMETER.627 / AILERON HOLE.815" OUTSIDE DIAMETER,.611" INSIDE DIAMETER. ***AIRCRAFT REMOVED FROM SERVICE ***** RH AILERON PN: CC670-13000-2 SN: 7711 UPWARD PCU IB SI
- [SDR A6WA202206088192](https://openairdocs.org/sdr/A6WA202206088192.md): Oil System · warning message · Jun 15, 2022 · N429AW · Cndair CL6002B19 · Engine Oil Storage (Airframe Furnished)
  > ****SUPPLEMENTAL INFORMATION ******AT CRUISE NOTICED LH ENG OIL PRES FLUCTURATE BETWEEN 25-53 PSI NO MSG PRESENT. NORMAL DESCENT. ON SHORT FINAL RCVD LH ENG OIL PRES WARNING MSG INTERMIATELY. RAN QRH SHUTDOWN LH ENG. LANDED SAFELY.
- [SDR A6WA202202218115](https://openairdocs.org/sdr/A6WA202202218115.md): None · none · Feb 20, 2022 · N429AW · Cndair CL6002B19 · Flight Control System
  > RECEIVED STALL FAIL CAUTION AT 500'. C/W QRH. DIVERTED TO DAY. ON GROUND PERFORMED GPWS TEST, GPWS FAIL STATUS MSG POSTED. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED GPWS TEST TO CLEAR GPWS FAIL MESSAGE. IAW AWA SUP 20-137. ALSO PERFORMED TEST OF
- [SDR A6WA202201108056](https://openairdocs.org/sdr/A6WA202201108056.md): Trim Switch · faulted · Jan 9, 2022 · N429AW · Cndair CL6002B19 · Stabilizer Position Indicating
  > RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES AT CRUISE. QRH DIRECTED FLAPS 20 LANDING, WHICH WAS SUCCESSFUL WITH NO ISSUES. ATTEMPTED TO REENGAGE MULTIPLE TIMES WITHOUT SUCCESS. AIRCRAFT REMOVED FROM SERVICE. ACARS EMAILS REPORT FO STAB TRIM DISCONNE
- [SDR A6WA202201048048](https://openairdocs.org/sdr/A6WA202201048048.md): Warning Message · illuminated · Jan 4, 2022 · N429AW · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB TRIM CAUTION MSG IN FLT COULD NOT ENGAGE CHANNEL 1 OR 2 AT FLT LEVEL 340. CW QRH L.5 HRS LATER AT 6000 FT BOTH CHANNELS REENGAGED AND STAYED ENGAGED THE REMAINDER OF THE FLT. NORMAL LANDING FLAPS 20. AIRCRAFT REMOVED FROM SERVICE. PERFORMED SUP 05-0
- [SDR A6WA202111297997](https://openairdocs.org/sdr/A6WA202111297997.md): None · none · Nov 27, 2021 · N429AW · Cndair CL6002B19 · Auto Flight System
  > WHILE ENROUTE TO PWM THE CREW REPORTED RECEIVING A STAB TRIM AND MACH TRIM CAUTION. THEY DECLARED AND EMERGENCY AND WILL CONTINUE TO PWM. AT FL310 RECEIVED STAB & MACH TRIM CAUTIONS. C/W QRH, TRIM WOULD NOT RE-ENGAGE. ***AIRCRAFT REMOVED FROM SERVICE***
- [SDR A6WA202107227838](https://openairdocs.org/sdr/A6WA202107227838.md): Skin · dented · Jul 2, 2021 · N429AW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT HAND WING INBOARD LEADING EDGE HAS 3 DENTS AT WS96.134-WS101.00, WS101.00 Ï¿½ WS108.70 AND WS124.10 - 131.80. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DRESS BACK OF DENTS #1 AND #3 TO ORIGINAL CONTOUR PER GREO 601R-57-41-436 REV A DATED 2013-06-19.
- [SDR A6WA202107207828](https://openairdocs.org/sdr/A6WA202107207828.md): Rib · corroded · Jun 26, 2021 · N429AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH WING RIB CHANNEL IS PITTING CORROSION AT WS53.60 AND WHEEL WELL HYDRAULIC GUARD ACCESS PANEL AREA. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND RIB CHANNEL CORROSION TO BE OUT OF LIMITS CREATING A HOLE THROUGH RIB CHANNEL THICKNESS OF 0.050Ï¿½. REMOVED A
- [SDR A6WA202107087816](https://openairdocs.org/sdr/A6WA202107087816.md): Skin · corroded · Jun 25, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN AT UPPER TCAS ANTENNA AT TWO LOCATIONS BETWEEN FS295 TO FS310. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT TWO LOCATIONS ON SKIN AT UPPER TCAS ANTENNA LOCATION FS295 + 4Ï¿½, RH STR 0 + 2Ï¿½, DIMENSION L = 3.00Ï¿½ X W = 2.00Ï¿½
- [SDR A6WA202107027809](https://openairdocs.org/sdr/A6WA202107027809.md): Skin · scratched · Jun 22, 2021 · N429AW · Cndair CL6002B19 · Trailing Edge Flaps
  > SCRATCH ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED SRM 57-52-00 INBOARD FLAP REPAIR NO. 2 ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. CUTOUT DAMAGED SECTION OF UPPER SKIN INBOARD TRAILIN
- [SDR A6WA202107207830](https://openairdocs.org/sdr/A6WA202107207830.md): Frame · gouged · Jun 19, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS718 HAS TWO GOUGES; 1 AT STR26L AND ANOTHER AT STR25R. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE AT FS718 AND STR26L MEASURING.280"L X.200"W X.011"D AND GOUGE AT FS718 AND STR25R MEASURING.600"L X.200"W X.013"D IAW CRJ200
- [SDR A6WA202107097819](https://openairdocs.org/sdr/A6WA202107097819.md): Bulkhead Web · damaged · Jun 19, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THREE SCRATCH DAMAGES ON FORWARD FACE OF FS621 BULKHEAD WEB P/N 601R36008. #1 RBL23.875 TO RBL24.25 AT WL135.50 TO WL136.00, MEASURES L = 0.700Ï¿½ X W = 0.200Ï¿½ X D = 0.003Ï¿½ #2 RBL22.125 TO RBL22.325 AT WL134.25, MEASURES L = 0.400Ï¿½ X W = 0.200Ï¿½ X D = 0
- [SDR A6WA202107207829](https://openairdocs.org/sdr/A6WA202107207829.md): Skin · damaged · Jun 18, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ELONGATED FASTENER HOLE AND TOOLING DAMAGE LH AFT FUSELAGE SKIN AT FS559.00 + 64 Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A REPAIR AT LH AFT FUSELAGE SKIN AT FS559.00 + 64Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ELONGAT
- [SDR A6WA202107087817](https://openairdocs.org/sdr/A6WA202107087817.md): Plate · corroded · Jun 18, 2021 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON DOOR SILL PANEL ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SERVICE DOOR SILL PANEL P/N 601R38957-31 AND SHIM P/N 601R38695-19 AT FS319 TO FS349. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-40-1
- [SDR A6WA202107067811](https://openairdocs.org/sdr/A6WA202107067811.md): Angle · dented · Jun 18, 2021 · N429AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD: TRACK FRAME HAS 4 EACH DENTS ON FLANGE AND THE UPPER/LOWER SUPPORT CHANNELS HAVE DENTS AND ARE BENT. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED/REPLACED FWD CARGO DOOR CAM TRACK ANGLE P/N: 601R35050-15 (NSN) AT FS 574 FROM STR 8LH TO STR 17L
- [SDR A6WA202106177826](https://openairdocs.org/sdr/A6WA202106177826.md): Door · chafed · Jun 17, 2021 · N429AW · Cndair CL6002B19 · Wing Main, Frame Structure
  > RH BUTTE DOOR (694PB) HAS CHAFFING CONDITION ON LOWER SURFACE AT WS242. ****AIRCRAFT REMOVED FROM SERVICE****** BLENDED CHAFFING CONDITION ON RH BUTTE DOOR (694PB) LOWER SURFACE AT WS242. ORIGINAL MATERIAL THICKNESS 0.040Ï¿½, MATERIAL LOSS 0.006Ï¿½ WITH R
- [SDR A6WA202107097822](https://openairdocs.org/sdr/A6WA202107097822.md): Frame · dented · Jun 15, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Frame
  > DENTS AND GOUGES ON FUSELAGE AFT FRAME FS682.00Ï¿½ STR S26L TO S27. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE AND HAND DRESSED DENTS TO FUSELAGE FRAME AT FS682.00 STR S26L TO S27. DENT DAMAGE MEASURES L = 7.250Ï¿½ X W = 0.500Ï¿½ X D = 0.070Ï¿½
- [SDR A6WA202107097820](https://openairdocs.org/sdr/A6WA202107097820.md): Frame · dented · Jun 15, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE FRAME DENT FS672.20Ï¿½ STR26R-S27. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FRAME AT AFT FUSELAGE FS672.20Ï¿½ STR26R-S27. DAMAGE MEASURES L = 1.300Ï¿½ X W = 0.700Ï¿½ X D = 0.048Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECT
- [SDR A6WA202106307806](https://openairdocs.org/sdr/A6WA202106307806.md): Channel · dented · Jun 15, 2021 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT COMPARTMENT FUSELAGE FRAME CHANNEL FROM FS 689.5 TO FS 694.00 STR 24 LH HAS MULTIPLE DENTS. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FRAME CHANNEL AND REPLACED WITH FABRICATED FRAME CHANNEL AT FS 689.5 TO FS 694.00 STR 24 LH. NEW CHA
- [SDR A6WA202107097823](https://openairdocs.org/sdr/A6WA202107097823.md): Skin · dented · Jun 14, 2021 · N429AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS625.30 + 13.5Ï¿½ S24R AND S25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON SKIN AT FS625.30 + 13.5Ï¿½ AND S24R AND S25R. MEASURES L = 0.650Ï¿½ X W = 0.500Ï¿½ X D = 0.005Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED S
- [SDR A6WA202107227837](https://openairdocs.org/sdr/A6WA202107227837.md): Bushing · excess play · Jun 9, 2021 · N429AW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > REFERENCE 347219/1 HORIZONTAL STABILIZER EXCESSIVE PLAY. HORIZONTAL STABILIZER PIVOT BUSHING DIAMETER HOLES IN THE AIRCRAFT STRUCTURE ARE BELOW THE REQUIREMENTS AWA MAINTENANCE TASK CARD SUPPLEMENT NUMBER 19-154 REV B, DATED 07/16/2019. ***AIRCRAFT REMOVE
- [SDR A6WA202107097821](https://openairdocs.org/sdr/A6WA202107097821.md): Skin · dented · Jun 9, 2021 · N429AW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AFT EQUIPMENT BAY DOOR PERMANENT REPAIR FS712.00Ï¿½ STR 24R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A PERMANENT REPAIR TO AFT EQUIPMENT BAY DOOR OUTER SKIN FS712.00 AND STR 24R. DAMAGE MEASURES L = 1.200Ï¿½ X W = 0.500Ï¿½ X D = 0.024Ï¿½. PERFORMED HF
- [SDR A6WA202101057513](https://openairdocs.org/sdr/A6WA202101057513.md): Oil System · overheated · Jan 4, 2021 · N429AW · Cndair CL6002B19 · Turbine Engine Oil System
  > DURING CLIMB THROUGH FL220, NOTICED RT ENGINE OIL TEMP CLIMBING AND INDICATING IN THE RED AT 166. CW QRH FOR HIGH OIL TEMP. POWER LEVER ADJUSTMENTS DID NOT PREVENT OIL TEMP FROM CLIMBING. PERFORMED INFLIGHT ENGINE SHUTDOWN, AFTER SHUTDOWN, NEVER RECEIVED LO
- [SDR A6WA202002247192](https://openairdocs.org/sdr/A6WA202002247192.md): Cable · damaged · Feb 16, 2020 · N429AW · Cndair CL6002B19 · Autopilot System
  > L/H VERTICAL STABILIZER AUTO PILOT SERVO HAS RUST ON CABLE AT DRUM. FOUND AUTO PILOT SERVO SERVO CABLE P/N S 601R900200-79 AND 601R90020-131 WITH MULTIPLE BROKEN CABLE STRANDS. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED DAMAGED CABLES P/N S 601R900
- [SDR A6WA202002247193](https://openairdocs.org/sdr/A6WA202002247193.md): Fairing · damaged · Feb 12, 2020 · N429AW · Cndair CL6002B19 · Engine Thrust Reverser
  > L/H T/R DIFFICULT TO OPEN & HAD L/H REV UNLOCK CAUTION AFTER CLEARING RUNWAY AMBER ICON REV ICON ON N1 GAUGE LEVER WAS DIFFICULT TO MOVE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED UPPER STANG FAIRING THAT WAS FOUND TO BE DAMAGED. NO FURTHER DAMAGE
- [SDR A6WA2019121047047](https://openairdocs.org/sdr/A6WA2019121047047.md): Wire Harness · faulty · Dec 6, 2019 · N429AW · Cndair CL6002B19 · Landing Gear System Wiring
  > SUPPLEMENTAL INFORMATION, WOW INPUT CAUTION MSG RECEIVED INTERMITTENTLY SEVERAL TIMES AFTER T/O AND EARLY CLIMB. GEAR WAS STOWED IN UP POSITION WHEN MSG RECEIVED, MSG CLEARED WITHIN 10 MIN OF FLIGHT. AIRCRAFT REMOVED FROM SERVICE HISTORY OF A S02 CODE STORED
- [SDR A6WA2019062846683](https://openairdocs.org/sdr/A6WA2019062846683.md): A/C Pack · failed · Jun 27, 2019 · N429AW · Cndair CL6002B19 · Cabin Cooling System
  > AT APPROXIMATELY FL190, THE FLIGHT CREW NOTED THE FAILURE OF THE LEFT PACK, REDUCED AIRFLOW IN THE COCKPIT AND A CLIMBING CABIN PRESSURE. THE CREW INITIATED A DESCENT TO 10,000', DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. LOSS
- [SDR A6WA2018032245697](https://openairdocs.org/sdr/A6WA2018032245697.md): Bulkhead · cracked · Mar 13, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD SIDE OF APB IS CRACKED ABOVE AFT CARGO DOOR TRACK AT ITS END. FOUND ON HFEC INSP.
- [SDR A6WA2018031345693](https://openairdocs.org/sdr/A6WA2018031345693.md): Frame · cracked · Mar 12, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME ABOVE UPPER PAX DOOR SILL WAS FOUND CRACKED. REPLACED.
- [SDR A6WA2018031345692](https://openairdocs.org/sdr/A6WA2018031345692.md): Frame · cracked · Mar 11, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 IS CRACKED JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.
- [SDR A6WA2018031345691](https://openairdocs.org/sdr/A6WA2018031345691.md): Bracket · cracked · Mar 10, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT FUSELAGE BRACKET AT BS 461 FOUND CRACKED. REPLACED THE BRACKET.
- [SDR A6WA2018031345688](https://openairdocs.org/sdr/A6WA2018031345688.md): Drag Angle · cracked · Mar 10, 2018 · N429AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER DRAG ANGLE BY THE ASSIST MOTOR YOKE WAS CRACKED. REPLACED THE DRAG ANGLE.
- [SDR A6WA2018031345689](https://openairdocs.org/sdr/A6WA2018031345689.md): Bracket · cracked · Mar 10, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT FUSELAGE BRACKET AT BS 461 WAS FOUND CRACKED. REPLACED
- [SDR A6WA2018031345686](https://openairdocs.org/sdr/A6WA2018031345686.md): Bracket · cracked · Mar 10, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT FUSELAGE BRACKET AT BS 473 WAS FOUND CRACKED. REPLACED THE BRACKET.
- [SDR A6WA2018031345685](https://openairdocs.org/sdr/A6WA2018031345685.md): Angle · cracked · Mar 10, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Structure
  > BEAM AT BS 280 UPPER ANGLE IS CRACKED JUST OTBD OF THE MLG ALTERNATE CABLE EXTENSION PULLEY BRACKET, OTBD OF LBL 9.
- [SDR A6WA2018031345687](https://openairdocs.org/sdr/A6WA2018031345687.md): Bracket · cracked · Mar 10, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT FUSELAGE BRACKET AT BS 473 FOUND CRACKED. REPLACED THE BRAKCET.
- [SDR A6WA2018031345680](https://openairdocs.org/sdr/A6WA2018031345680.md): Skin · damaged · Mar 9, 2018 · N429AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP LOWER SKIN DENTED, 6 LOCATIONS AND PITTING IN TWO AREAS. REPLACED THE FLAP SKIN
- [SDR A6WA2018031345681](https://openairdocs.org/sdr/A6WA2018031345681.md): Mount Bracket · cracked · Mar 9, 2018 · N429AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET FOUND CRACKED. REPLACED THE MOUNT.
- [SDR A6WA2018031345682](https://openairdocs.org/sdr/A6WA2018031345682.md): Skin · cracked · Mar 7, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT FWD FUSELAGE SKIN IS CRACKED AT BS 202 BY FWD EQUIPMENT BAY AFT LATCH. REPLACED THE SKIN.
- [SDR A6WA2018031345684](https://openairdocs.org/sdr/A6WA2018031345684.md): Angle · cracked · Mar 6, 2018 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR BEAM AFT LOWER ANGLE AT BS 621 BULKHEAD IS CRACKED. REPLACED THE BEAM.
- [SDR A6WA2018031345683](https://openairdocs.org/sdr/A6WA2018031345683.md): Beam · gouged · Mar 6, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Structure
  > BEAM INBD OF CARGO DOOR, BS 618 - 621 HAS SEVERAL GOUGES. REPLACED THE BEAM.
- [SDR A6WA2018031345696](https://openairdocs.org/sdr/A6WA2018031345696.md): Riser · cracked · Mar 6, 2018 · N429AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER STEP RISER IS CRACKED. REPAIRED IAW AWAC 13-134.
- [SDR A6WA2018031345695](https://openairdocs.org/sdr/A6WA2018031345695.md): Stringer · cracked · Mar 3, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L AFT OF BS 364, PAX DOOR UPPER SILL IS CRACKED. REPAIRED THE STRINGER IAW SRM 53-00-03.
- [SDR A6WA2018031345694](https://openairdocs.org/sdr/A6WA2018031345694.md): Bracket · cracked · Feb 28, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT LOWER NOSE HYDRAULIC COMPARTMENT BRACKET ABOVE ACCUMULATOR IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.
- [SDR A6WA2018030845666](https://openairdocs.org/sdr/A6WA2018030845666.md): Fitting · cracked · Feb 28, 2018 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BATHTUB FITTING CRACKED AT FS 461, LBL9. REPLACED FITTING IAW SRM 51-42-06., 51-42-21.
- [SDR A6WA2018030845669](https://openairdocs.org/sdr/A6WA2018030845669.md): Floorbeam · corroded · Feb 26, 2018 · N429AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED AT FS574.00, RBL9 TO RBL27. REPLACED BEAM CAP IAW SRM5142-06, 53-00-00, 51-21-00, 51-41-11, 51-24-36.

Next page: https://openairdocs.org/aircraft/N429AW/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 = 'N429AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N429AW/reports

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