# Service difficulty reports: N467AW

A list on [N467AW](https://openairdocs.org/aircraft/N467AW.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 · 166 reports

- [SDR A6WA202401318710](https://openairdocs.org/sdr/A6WA202401318710.md): Skin · dented · Jan 31, 2024 · N467AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN ON FUSELAGE HAS 3 DENTS WITH CREASE AT FS 589 TO FS621 BETWEEN STRG21R AND STRG22R. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REPAIRED FWD AND AFT FUSELAGE SKIN AT FS 589.00 STR17R REF REO 601R-53-61-8146 REV -- DATED 2024-01-25.
- [SDR A6WA202401318709](https://openairdocs.org/sdr/A6WA202401318709.md): Skin · dented · Jan 31, 2024 · N467AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REF WO 332477 MXWC #4 DAMAGE TO FUSELAGE AT FS587 BETWEEN STR17R-STR18R DENT MEASURES 3" X 3.2" X.045 DEPTH. DAMAGE TO UNDERLYING FRAME SECTOR AT FS589 AND STRINGER 17R ALSO NOTED. TROUBLE SHOOT AND REPAIR AS REQUIRED. AIRCRAFT HAS BEEN REMOVED FROM SERVICE.
- [SDR A6WA202401318708](https://openairdocs.org/sdr/A6WA202401318708.md): Frame · corroded · Jan 31, 2024 · N467AW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME AT FS589 R/H BETWEEN STRINGER 22R-24R ***** AIRCRAFT REMOVED FROM SERVICE ***** LOCATED AND DRILLED NEW FRAME SECTION AT FS 589 SEE JOB HN00131220 FOR INSTALL
- [SDR A6WA202304028531](https://openairdocs.org/sdr/A6WA202304028531.md): Unknown · unknown · Apr 2, 2023 · N467AW · Cndair CL6002B19 · Air Conditioning System
  > INFLIGHT RECEIVED DISPLAY COOL CAUTION MESSAGE. MESSAGE BECAME INTERMITTENT. EXTINGUISHED AND REMAINED OUT BELOW FL140. *****AIRCRAFT REMOVED FROM SERVICE******** FOUND DUCT TO DISPAY COOL PLENUM OFF. REATTACEHD DUCT IN REF TO AMM 21-24 OPS CHECK GOOD.
- [SDR A6WA202301298509](https://openairdocs.org/sdr/A6WA202301298509.md): Doubler · dented · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Standard Practices/Structures
  > DENT ON AFT FUSELAGE SKIN AT FS589-605 AND BETWEEN S22R -25R. ADDITIONAL DAMAGE TO FS574-589 AND S22R TO 25R. FASTENERS INSTALLED FOUND CLOSE TO RADIUS OF STRINGER & WEAR DAMAGE TO STRINGER FLANGE DUE TO DOOR. LATCH WEAR. PERFORMED TEMPORARY REPAIR TO SKIN,
- [SDR A6WA202301298498](https://openairdocs.org/sdr/A6WA202301298498.md): Unknown · unknown · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Fuselage Structure (General)
  > COMPLY WITH EO E17/003/453 AFT FUSELAGE MODIFICATION TO FS621.00 PRESSURE BULKHEAD WEB. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH EO E17/003/453 AFT FUSELAGE MODIFICATION TO FS621.00 PRESSURE BULKHEAD WEB. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTE
- [SDR A6WA202301298482](https://openairdocs.org/sdr/A6WA202301298482.md): Angle · corroded · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN FLOOR SUPPORT STRUCTURE AT FS349 AND RBL27 TO RBL 42. *****AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED CABIN FLOOR SUPPORT ANGLE PN 601R38783-13 AT FS349 AND RBL27 TO RBL 42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMIT
- [SDR A6WA202301298474](https://openairdocs.org/sdr/A6WA202301298474.md): Seat Track · corroded · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > CORROSION ON CABIN LH SIDE SEAT TRACK PN 20276-288-0-0 AT FS449.85 TO FS499.0. P7 - L= 0.800Ï¿½ X W= 0.400Ï¿½ X D= 0.023Ï¿½, REMAINING THICKNESS 0.077Ï¿½, CENTER OF SEAT TRACK AT FS449.85+2.0Ï¿½. *****AIRCRAFT REMOVED FROM SERVICE******* REPLACED WITH A NEW
- [SDR A6WA202301298469](https://openairdocs.org/sdr/A6WA202301298469.md): Skin · chafed · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Aileron Tabs
  > RH INBOARD FLAP VANE HAS WEAR MARK AT CENTER OF LEADING EDGE SKIN PN 601R14303-52. WEAR DIMENSIONS FOR P2 ARE - L = 2.300Ï¿½ X W = 0.500Ï¿½ X D = 0.012Ï¿½, WS 97.009+6.5 TO WS 106.352+1.0. *********AIRCRAFT REMOVED FROM SERVICE********** BLENDED DAMAGE OF RH I
- [SDR A6WA202301298470](https://openairdocs.org/sdr/A6WA202301298470.md): Skin · chafed · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Aileron Tabs
  > RH INBOARD FLAP VANE HAS WEAR MARK AT INBD END OF LEADING EDGE SKIN PN 601R14303-54. WEAR DIMENSIONS FOR P1 ARE - L = 2.100Ï¿½ X W = 0.700Ï¿½ X D = 0.018Ï¿½, WS 50.448+5.0 TO WS 54.848+1.5. *******AIRCRAFT REMOVED FROM SERVICE********** BLENDED DAMAGE OF RH IN
- [SDR A6WA202301298471](https://openairdocs.org/sdr/A6WA202301298471.md): None · none · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STABILIZER SHROUD UPPER FLANGE HAS 1 ELONGATED HOLE BETWEEN FSS 110.63 AND FSS 118.63. ****AIRCRAFT REMOVED FROM SERVICE******* TEMPORARY REPAIR DISPOSITION FOR RH HORIZONTAL STABILIZER SHROUD UPPER FLANGE, 1 ELONGATED HOLE BETWEEN FSS 110.63 AND
- [SDR A6WA202301298468](https://openairdocs.org/sdr/A6WA202301298468.md): Skin · chafed · Jan 29, 2023 · N467AW · Cndair CL6002B19 · Aileron Tabs
  > RH INBOARD FLAP VANE HAS WEAR MARK AT OUTBOARD END OF LEADING EDGE SKIN PN 601R14303-44. WEAR DIMENSIONS FOR P3 ARE - L = 1.800Ï¿½ X W = 0.650Ï¿½ X D = 0.014Ï¿½, WS 135.513+3.5 TO WS 142.512+0.50. ******AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OF
- [SDR A6WA202201108059](https://openairdocs.org/sdr/A6WA202201108059.md): None · none · Jan 5, 2022 · N467AW · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > WHILE CLIMBING OUT OF KHPN AND GOING THROUGH 10,000', THE CABIN ALT CAUTION MESSAGE INDICATED. THE FO LEVELED OFF AND RETURNED TO 10,000' WHICH I COORDINATED WITH DEPARTURE CONTROL. THE CABIN WAS INDICATING AN ALTITUDE OF 9,300 AT THAT TIME. WE RAN THE QRH FO
- [SDR A6WA202110137899](https://openairdocs.org/sdr/A6WA202110137899.md): Skin · dented · Sep 29, 2021 · N467AW · Cndair CL6002B19 · Fuselage Structure (General)
  > MULTIPLE DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24 AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION P1- L = 7
- [SDR A6WA202110137898](https://openairdocs.org/sdr/A6WA202110137898.md): Skin · dented · Sep 29, 2021 · N467AW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 5.300Ï¿½ X W = 0
- [SDR A6WA202110127897](https://openairdocs.org/sdr/A6WA202110127897.md): None · dented · Sep 19, 2021 · N467AW · Cndair CL6002B19 · Wing Structure
  > RIGHT HAND OUTBOARD FLAP CENTER HINGE BOX AT WS220.00 HAS A GOUGE DAMAGE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE ON RIGHT HAND OUTBOARD FLAP CENTER HINGE BOX AT WS220.00. ROTO PEENED REWORKED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFA
- [SDR A6WA2019091846874](https://openairdocs.org/sdr/A6WA2019091846874.md): Stiffener · cracked · Sep 14, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 BULKHEAD RBL 18 POST OUTBD SIDE HAS A CRACK INDICATION ON THE LOWER RADIUS. REPLACED.
- [SDR A6WA2019091846873](https://openairdocs.org/sdr/A6WA2019091846873.md): Skin · chafed · Sep 14, 2019 · N467AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT I/B FLAP VANE SKIN OB OF CENTER VANE ACT CHAFED. REMOVED AND REPLACED RT IB FLAP VANE SKIN OUTBOARD INSTALLED NEW FLAP VANE LEADING EDGE IAW SRM 51-42-13.
- [SDR A6WA2019091846872](https://openairdocs.org/sdr/A6WA2019091846872.md): Beam · damaged · Sep 13, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR BEAM MEMBER 601R35050-64 HAS CUT MARKS FWD AND AFT FROM CABLE ASSIST. REPLACED DAMAGED BEAM IAW SRM 51-42-06, 51-40-11.
- [SDR A6WA2019091846871](https://openairdocs.org/sdr/A6WA2019091846871.md): Attach Angle · cracked · Sep 13, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ATTACH ANGLE CRACKED ON BOTTOM AFT CARGO DOOR BEAM, FS621.00. REPLACED ANGLE IAW SRM 51-42-06, 51-40-11-00, TR51-42, 51-42-21.
- [SDR A6WA2019091846869](https://openairdocs.org/sdr/A6WA2019091846869.md): Post · cracked · Sep 12, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 409+128 VERTICAL POST @ LBL18 CRACKED. REPLACED VERTICAL POST @ FS409+128, LBL18 IAW REO 601R-53-41889 REV-D.
- [SDR A6WA2019091846870](https://openairdocs.org/sdr/A6WA2019091846870.md): Angle · cracked · Sep 12, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT FS 409+128, BL0 CRACKED ON BOTH LEFT AND RIGHT AFT ANGLES. REPLACED LEFT AND RIGHT AFT ANGLES IAW SRM 51-42-06, REO601R-53-41-889 REV-D.
- [SDR A6WA2019091746867](https://openairdocs.org/sdr/A6WA2019091746867.md): Panel · cracked · Sep 12, 2019 · N467AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 446AL HAS CRACKED STIFFENER RING. REPLACED STIFFENER RING IAW CMM 20-42-06, 20-40-11.
- [SDR A6WA2019091746868](https://openairdocs.org/sdr/A6WA2019091746868.md): Retainer · corroded · Sep 11, 2019 · N467AW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR SEAL RETAINER CORRODED. REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR A6WA2019091146865](https://openairdocs.org/sdr/A6WA2019091146865.md): Doubler · gouged · Sep 10, 2019 · N467AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD RBL 18 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.
- [SDR A6WA2019091146862](https://openairdocs.org/sdr/A6WA2019091146862.md): Doubler · gouged · Sep 10, 2019 · N467AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD RBL 36 PREVIOUS REPAIR HAS SCREW MARKS. REMOVE AND REPLACED DOUBLED IAW REO# 601R-53-61-1285 REV E.
- [SDR A6WA2019091146864](https://openairdocs.org/sdr/A6WA2019091146864.md): Doubler · gouged · Sep 10, 2019 · N467AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD RBL 27 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.
- [SDR A6WA2019091146861](https://openairdocs.org/sdr/A6WA2019091146861.md): Landing · cracked · Sep 10, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT AFT TRU LAND LATCH IS CRACKED. REPAIRED TRU LAND LATCH AREA IAW SUPPLEMENT 19-016B.
- [SDR A6WA2019091146863](https://openairdocs.org/sdr/A6WA2019091146863.md): Doubler · gouged · Sep 9, 2019 · N467AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD WL 103.5 AT LBL 18 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.
- [SDR A6WA2019091046860](https://openairdocs.org/sdr/A6WA2019091046860.md): Support Channel · cracked · Sep 9, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK LOWER SUPPORT CHANNEL IS CRACKED. REPLACED SUPPORT CHANNEL IAW SRM 51-42-06, 51-41-02.
- [SDR A6WA2019090946856](https://openairdocs.org/sdr/A6WA2019090946856.md): Intercostal · cracked · Sep 7, 2019 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD FS621.00 ON THE LEFT SIDE STR13L, INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.
- [SDR A6WA2019090946855](https://openairdocs.org/sdr/A6WA2019090946855.md): Retainer · cracked · Sep 7, 2019 · N467AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR LOWER CENTER SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW REO 601R-52-11-915 AND SRM 51-42-13.
- [SDR A6WA2019090946854](https://openairdocs.org/sdr/A6WA2019090946854.md): Divider · chafed · Sep 5, 2019 · N467AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PYON PANEL 422DB HAS 2 CHAFED DIVIDER PANELS. REPLACED DIVIDERS IAW SRM 51-42-06.
- [SDR A6WA2019090946853](https://openairdocs.org/sdr/A6WA2019090946853.md): Retainer · cracked · Sep 5, 2019 · N467AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PYLON PANEL 422 DB HAD CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR A6WA2019090946852](https://openairdocs.org/sdr/A6WA2019090946852.md): Divider · chafed · Sep 5, 2019 · N467AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > PYLON PANEL 412DB HAS 2 EACH DIVIDER PANELS KNIFE EDGED. REPLACED DIVIDER PANELS IAW SRM 51-42-06, 51-42-13.
- [SDR A6WA2019073046741](https://openairdocs.org/sdr/A6WA2019073046741.md): Warning System · activated · Jul 28, 2019 · N467AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER SELECTING GEAR DOWN ON FINAL APPROACH, RECIEVED GEAR DIS WRNING AFTER 6 SECONDS FROM DOWN SELECTION. RT MAIN GEAR SHOWED RED BOX UP. HYD TEMPS AND PRESSURE NORMAL NO OTHER ASSOCIATED MSGS DISPLAYED CONDUCTED GO AROUND, BROUGHT FLAPS TO 8 DEGREES LEFT GE
- [SDR A6WA201845610](https://openairdocs.org/sdr/A6WA201845610.md): Rvdt · failed · Feb 2, 2018 · N467AW · Cndair CL6002B19 · Landing Gear Steering System
  > DURING CRUISE, RECEIVED A STEERING INOPERATIVE MESSAGE, RAN QRH. LANDING WITH NOSE WHEEL STEERING IN OFF POSITION. AFTER LANDING REARMED NOSE WHEEL STEERING, MESSAGE PERSISTED. REMOVED AND REPLACED LEFT RVDT IAW AMM 32-51. OPS CHECKED GOOD.
- [SDR A6WA201745416](https://openairdocs.org/sdr/A6WA201745416.md): Proximity Sensor · malfunctioned · Nov 15, 2017 · N467AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES AFTER LANDING GEAR HANDLE SELECTED UP. MLG SHOWED UP AND LOCKED AND NLG SHOWED DOWN AND GREEN. MANUALLY LOWERED GEAR, LANDING SMOOTH AND UNEVENTFUL. ADJUSTED NOSE LANDING GEAR OLEO CENTERED/EXTENDED PR
- [SDR A6WA2017102045365](https://openairdocs.org/sdr/A6WA2017102045365.md): Frame · cracked · Oct 17, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 333 ABOVE MAIN ENTRY DOOR IS CRACKED AT EWIS SUPPORT ATTACH POINT.
- [SDR A6WA2017101645362](https://openairdocs.org/sdr/A6WA2017101645362.md): Heat Shield · cracked · Oct 9, 2017 · N467AW · Cndair CL6002B19 · APU Core Engine
  > APU EXHAUST HEAT SHIELD PREVIOUS REPAIR WELD CRACKED. REPAIRED APU HEAT SHIELD IAW REO 601R-49-81-003 REV-B.
- [SDR A6WA2017101145352](https://openairdocs.org/sdr/A6WA2017101145352.md): Attach Bracket · cracked · Oct 8, 2017 · N467AW · Cndair CL6002B19 · Vertical Stabilizer, Attach Fittings
  > FWD ATTACH BRACKET FOR VERTICAL STAB ACCESS PANEL 326CR IS CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-20.
- [SDR A6WA2017101145344](https://openairdocs.org/sdr/A6WA2017101145344.md): Drag Angle · cracked · Oct 6, 2017 · N467AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER DRAG ANGLE CRACKED.
- [SDR A6WA201745340](https://openairdocs.org/sdr/A6WA201745340.md): Angle · cracked · Oct 5, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD, STRINGER 14R OBLIQUE ANGLE CRACKED.
- [SDR A6WA2017101145353](https://openairdocs.org/sdr/A6WA2017101145353.md): Fitting · cracked · Oct 5, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FLIGHT DECK WINDSHIELD CENTER POST LEFT LOWER FITTING IS CRACKED. REPLACED THE FITTING IAW SRM 51-42-21.
- [SDR A6WA2017101145339](https://openairdocs.org/sdr/A6WA2017101145339.md): Angle · cracked · Oct 5, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD AT STRINGER 14L OBLIQUE ANGLE IS CRACKED.
- [SDR A6WA2017101145347](https://openairdocs.org/sdr/A6WA2017101145347.md): Floor Support · corroded · Oct 4, 2017 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AT BS 574 TO 621, LBL 27. REPAIRED THE FLOOR SUPPORT IAW EA 15-2013-442.
- [SDR A6WA2017101145355](https://openairdocs.org/sdr/A6WA2017101145355.md): Angle · cracked · Oct 4, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE CRACKED AT BS 280, LBL 9 OTBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, AND 51-40-11.
- [SDR A6WA2017101145348](https://openairdocs.org/sdr/A6WA2017101145348.md): Angle · cracked · Oct 3, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE IS CRACKED. REPLACED THE IAW SRM 51-42-21.
- [SDR A6WA2017101145342](https://openairdocs.org/sdr/A6WA2017101145342.md): Angle · cracked · Oct 3, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ANGLE CRACKED AT BS 484, LBL 27. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.
- [SDR A6WA2017101145341](https://openairdocs.org/sdr/A6WA2017101145341.md): Angle · cracked · Oct 3, 2017 · N467AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ANGLE CRACKED AT BS 484, LBL 36 ON INBD SIDE. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.

Next page: https://openairdocs.org/aircraft/N467AW/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 = 'N467AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N467AW/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.