# Service difficulty reports: N706PS

A list on [N706PS](https://openairdocs.org/aircraft/N706PS.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 3 · 108 reports

- [SDR 1Q2R2026093020063](https://openairdocs.org/sdr/1Q2R2026093020063.md): Latch · gouged · Sep 28, 2026 · N706PS · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > R/H ENGINE LATCH, BEAM LATCH, STRUCTURE IS GOUGED. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-131113 REV. 0, AND REO 670-54-14-1357 REV. -.
- [SDR 1Q2R2026092420074](https://openairdocs.org/sdr/1Q2R2026092420074.md): Skin · gouged · Sep 24, 2026 · N706PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS-985.00 STGR HAS GOUGE AND DENTS.
- [SDR 1Q2R2026092920061](https://openairdocs.org/sdr/1Q2R2026092920061.md): Door · chafed · Sep 23, 2026 · N706PS · Cndair CL6002C10 · Landing Gear Doors
  > CHAFFING ALONG OUTER SKIN OF OUTER R/H MLG DOOR. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130952 REV. 0, DATED SEPTEMBER 23, 2026, AND MHI RJ REO 670-52-82-457 REV. --, DATED SEPTEMBER 23, 2026.
- [SDR 1Q2R2026092020074](https://openairdocs.org/sdr/1Q2R2026092020074.md): Skin · gouged · Sep 20, 2026 · N706PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > BS 9850 STGR HAS GOUGE AND DENTS.
- [SDR 1Q2R2026092120236](https://openairdocs.org/sdr/1Q2R2026092120236.md): Support Fitting · gouged · Sep 14, 2026 · N706PS · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > TWO GOUGES, LOCATED ON UPPER, FWD, CENTER OF HORIZONTAL STAB. PERFORMED PERMANENT REPAIR IAW REO 670-55-11-415, REV. --.
- [SDR 1Q2R2026091450062](https://openairdocs.org/sdr/1Q2R2026091450062.md): Skin · dented · Sep 14, 2026 · N706PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENT FS 497 AND S17L.
- [SDR 1Q2R2026092020076](https://openairdocs.org/sdr/1Q2R2026092020076.md): Diaphragm · cracked · Sep 8, 2026 · N706PS · Cndair CL6002C10 · Aerodynamic Fairings
  > LEFT LOWER WING-TO-FUSELAGE FAIRING AT FS909.00 DIAPHRAGM IS CRACKED 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130787 REV. 0, DATED SEPTEMBER 08, 2026, AND MHI RJ REO 670-53-82-478 REV. -A, DATED NOVEMBER 12, 2014.
- [SDR VNAA202504150005](https://openairdocs.org/sdr/VNAA202504150005.md): Fitting · worn · Apr 7, 2025 · N706PS · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > SECONDARY NRC OF TRFKE001WDWE: AFTER REMOVAL RH WISHBONE FITTING, WEAR ON UPPER EXTERNAL FACES OF FITTING PCU 2 WAS FOUND. WEAR ON UPPER EXTERNAL FACES OF FITTING PCU 2 WAS REPAIRED PER REO 670-55-21-113 REV - -.
- [SDR VNAA202504150003](https://openairdocs.org/sdr/VNAA202504150003.md): Intercostal · worn · Apr 5, 2025 · N706PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > IN REFERENCE TO JOB CARD TRFKE003NWAG DURING INSPECTION OF STGR 7RH: EXCESSIVE WEAR ON INTERCOSTAL ATTACHED TO STGR 9RH BTWN FS 1144.00 TO 1162 AND BROKEN BRACKET ATTACHED TO SAME INTERCOSTAL. WEAR ON INTERCOSTAL ATTACHED TO STGR 9RH BTWN FS 1144.00 TO 1162.0
- [SDR VNAA202504150002](https://openairdocs.org/sdr/VNAA202504150002.md): Skin Panel · dented · Apr 4, 2025 · N706PS · Cndair CL6002C10 · Cargo/Baggage Doors
  > DENT ON UPPER EDGE OF EXTERNAL SKIN AT AFT CARGO DOOR. UPPER EDGE OF EXTERNAL SKIN AT AFT CARGO DOOR. WAS REPAIRED PER REO 670-51-00-085 REV. - A AND REO 670-52-31-170 REV --.
- [SDR VNAA202504150001](https://openairdocs.org/sdr/VNAA202504150001.md): Retainer · cracked · Apr 3, 2025 · N706PS · Cndair CL6002C10 · Cargo/Baggage Doors
  > DAMAGE TO FORWARD BAGGAGE DOOR($) LOWER SEAL RETAINER WITHIN 800FH, PERFORM A PERMANENT REPAIR OR REPLACE PART IAW APPROVED PROCEDURES. LOWER SEAL RETAINER WAS REPAIRED PER CRJ-700 SRM 52-35-07-201-001-A01
- [SDR VNAA202504150004](https://openairdocs.org/sdr/VNAA202504150004.md): Hinge · corroded · Mar 5, 2025 · N706PS · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSON ON HINGE AT PASSENGER ACCESS PANEL 832ET EVALUATED, FOR EXCESSIVE DAMAGE ON HINGE AT PASSENGER ACCESS PANEL 832ET PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER AMM 52-11-04.
- [SDR VNAA2024052111101](https://openairdocs.org/sdr/VNAA2024052111101.md): Wire Harness · damaged · May 19, 2024 · N706PS · Cndair CL6002C10 · Flight Control System Wiring
  > RUDDER LIMITER CAUTION MSG IN FLIGHT RAN QRH LANDED AT FLAPS 20 / INTERROGATED MDC FOUND B1 CODE 233326, TROUBLESHOT IAW CRJ 700 FIM 27-61-05-810-852-A01. POSSIBLE CAUSES HAVE ALREADY BEEN RULED OUT, PERFORMED INSULATION WIRE CHECKS IAW CRJ 700 FIM 27-61-05-81
- [SDR VNAA2023102611101](https://openairdocs.org/sdr/VNAA2023102611101.md): Unknown · unknown · Oct 25, 2023 · N706PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CRACKS ZONE 2 - FWD SIDE OF PAX DOOR / PERFORMED PERM REPAIR IAW REO 670-52-11-1336.
- [SDR VNAA202309261111](https://openairdocs.org/sdr/VNAA202309261111.md): Transducer · unserviceable · Sep 24, 2023 · N706PS · Cndair CL6002C10 · Landing Gear Brake System
  > UPON TAKEOFF ROTATION THE A/SKID OUTBD CAUTION MSG AND OB GND SPLR FAULT S MSG POSTED / REMOVED AND REPALCED L/H OUT BOARD WHEEL TRANSDUCER IAW CRJ 900 AMM 32-44-01-000/400-801-A01. ( OPS CHECK GOOD AT THIS TIME)
- [SDR VNAA202307101111](https://openairdocs.org/sdr/VNAA202307101111.md): Windshield · unserviceable · Jul 8, 2023 · N706PS · Cndair CL6002C10 · Flight Compartment Windows
  > RH WINDSHIELD HEAT CAUTION MSG, ELECTRICAL BURNING ODOR SHORTLY AFTER SWITCH TURNED ON / REMOVED AND INSTALLED RH WINDSHIELD IAW CRJ 700 AMM 56-11-01-400-801-A01-PSA. OPS AND LEAK CHECK GOOD.
- [SDR VNAA202210299920](https://openairdocs.org/sdr/VNAA202210299920.md): Intercostal · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > INTERCOSTAL IS CORRODED RIGHT OF STGR 27 BETWEEN FS 394.00 AND 409.00 CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL IAW CRJ700 SRM TASKS 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR VNAA202210299919](https://openairdocs.org/sdr/VNAA202210299919.md): Intercostal · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > INTERCOSTAL IS CORRODED LEFT OF STGR 27 BETWEEN FS 394.00 AND 409.00 CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL IAW CRJ700 SRM TASKS 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR VNAA202210299918](https://openairdocs.org/sdr/VNAA202210299918.md): Angle · cracked · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > RH VERTICAL STAB FWD DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: PERFORMED A MAJOR REPAIR TO VERTICAL STAB RHS FWD DRAG ANGLE IAW CRJ700 SRM TASK 55-31-00-201-001-A01.
- [SDR VNAA202210299917](https://openairdocs.org/sdr/VNAA202210299917.md): Former · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FOUND PAX DOOR AFT FORMER TO BE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED PASSENGER DOOR AFT FORMER IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR VNAA202210299916](https://openairdocs.org/sdr/VNAA202210299916.md): Track · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > SEAT TRACK ON RBL9 FROM F.S.985 TO F.S.1000 IS CORRODED. CORRECTIVE ACTION: FABRICATED NEW SEAT TRACK PN:BA670-45073-3 IAW CRJ-700 SRM 53-00-49-101-001-A01, 51-40-11-001-001-A01 AND 51-24-36-001-001-A01. INSTALLED NEW SEAT TRACK
- [SDR VNAA202210299915](https://openairdocs.org/sdr/VNAA202210299915.md): Rail · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FLOOR SEAT RAIL AT LBL9 BETWEEN FS 364+10 AND 485.00 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK @ LBL 9 FS. 374.00 - 485.00 IAW CRJ700 AMM 53-00-49-000-801 (CONFIG A03) AND AMM 53-00-49-400-801 (CONFIG A03).
- [SDR VNAA202210299914](https://openairdocs.org/sdr/VNAA202210299914.md): Seat Track · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H SIDE SEAT RAIL FROM 863 - FS 969 IS CORRODED CORRECTIVE ACTION:. REMOVED AND REPLACED SEAT TRACK @ LH SIDE SEAT TRACK FS. 863-969 IAW CRJ700 AMM 53-00-49-000-801 (CONFIG A03) AND 53-00-49-400-801 (CONFIG A03)
- [SDR VNAA202210299913](https://openairdocs.org/sdr/VNAA202210299913.md): Angle · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > MINOR CORROSION FOUND ON LH FLOOR SILL BETWEEN FS 785.15-792.15. CORRECTIVE ACTION: UPON FURTHER INVESTIGATION FOUND CORROSION TO BE ON RH FLOOR SILL ANGLE. PERFORMED A MAJOR REPAIR TO THE RH FLOOR SILL ANGLE BETWEEN FS 761.85 AND FS 785.15
- [SDR VNAA202210299912](https://openairdocs.org/sdr/VNAA202210299912.md): Intercostal · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > INTERCOSTAL IS CORRODED LEFT OF STGR 27 BETWEEN FS 349.00 AND 364.00 CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL IAW CRJ700 SRM TASKS 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR VNAA202210299911](https://openairdocs.org/sdr/VNAA202210299911.md): Longeron · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > STRINGER 25L IS CORRODED BETWEEN FS 333.00 AND 349.00. CORRECTIVE ACTION: REPLACED LONGERON AT STGR 25L FROM FS 333.00 TO FS 364.00 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202210299910](https://openairdocs.org/sdr/VNAA202210299910.md): Rail · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > RH SIDE SEAT TRACK FROM F.S. 573 TO F.S. 669 TO BE CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED SEAT TRACK FROM FS573 TO FS 669 RH SIDE IAW CRJ 700 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK FROM FS 573 TO FS669 RHS ISDE IAW CRJ 700-AMM
- [SDR VNAA202210299999](https://openairdocs.org/sdr/VNAA202210299999.md): Angle · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > F.S.280 J ANGLE IS CORRODED BETWEEN RBL 11 AND LBL 11 CORRECTIVE ACTION: REMOVED AND REPLACED F.S. 280 J ANGLE IAW CRJ700 SRM TASKS 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01.
- [SDR VNAA202210299998](https://openairdocs.org/sdr/VNAA202210299998.md): Intercostal · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FOUND INTERCOSTAL STGR 27R BETWEEN F.S 349-364 TO BE HEAVILY CORRODED. CORRECTIVE ACTION: REMOVED UNSERVICEABLE INTERCOSTAL AT STGR 27R BETWEEN F.S 349-364 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTA
- [SDR VNAA202210299997](https://openairdocs.org/sdr/VNAA202210299997.md): Doubler · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > DOUBLER @ FS536, STGR 25L IS CORRODED CORRECTIVE ACTION: REMOVED UNSERVICEABLE DOUBLER AT FS536, STGR25L IAW CRJ700 SRM 51-42-21-001-001-A01, 51-42-27-001-001-A01. INSTALLED NEW SERVICEABLE DOUBLER AT FS536, STGR25L IAW CRJ700 SRM 51-42-21-001-001-A01, 51-
- [SDR VNAA202210299996](https://openairdocs.org/sdr/VNAA202210299996.md): Longeron · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > STRINGER 25L IS CORRODED BETWEEN FS 333.00 AND 349.00. CORRECTIVE ACTION: REMOVED UNSERVICEABLE F.S 349 FRAME BETWEEN STGR 24R TO STGR 23L FOR ACCESS IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE F.S 349 FRAME IAW CR
- [SDR VNAA202210299995](https://openairdocs.org/sdr/VNAA202210299995.md): Stringer · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > STRINGER 26L IS CORRODED BETWEEN FS 319.00 AND 349.00. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW SERVICEABLE STGR 26L F.S. 280-333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202210299994](https://openairdocs.org/sdr/VNAA202210299994.md): Stringer · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > STRINGER 25R IS CORRODED BETWEEN FS 295.00 AND 310.00 CORRECTIVE ACTION:. INSTALLED NEW SERVICEABLE STRINGER 25R F.S. 280-333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 41-42-21-001-001-A01.
- [SDR VNAA202210299993](https://openairdocs.org/sdr/VNAA202210299993.md): Frame · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FRAME AT FS 319.00 IS CORRODED BETWEEN STGR 25L ANS 23R. CORRECTIVE ACTION:. REPAIRED F.S. 295 FRAME BETWEEN STGR 25L TO 23R IAW CRJ 700 SRM 53-00-06-201-006-A01.
- [SDR VNAA202210299992](https://openairdocs.org/sdr/VNAA202210299992.md): Frame · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FRAME AT FS 295.00 IS CORRODED BETWEEN STGR 25L ANS 25R. CORRECTIVE ACTION:. REPAIRED F.S. 295 FRAME BETWEEN STGR 25L TO 25R IAW CRJ 700 SRM 53-00-06-201-006-A01.
- [SDR VNAA202210299991](https://openairdocs.org/sdr/VNAA202210299991.md): None · corroded · Oct 29, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 280.00 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 26R AND 25R.. CORRECTIVE ACTION:. REPAIRED F.S. 280 CIRCUMFERENTIAL JOINT BETWEEN STGR 26R AND 25R
- [SDR VNAA202209209999](https://openairdocs.org/sdr/VNAA202209209999.md): None · corroded · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL FROM F.S.860 TO F.S.969 IS CORRODED.
- [SDR VNAA202209209998](https://openairdocs.org/sdr/VNAA202209209998.md): Former · corroded · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER FS329.50, DD2 PN: 601R318092-1 IS CORRODED.
- [SDR VNAA202209209997](https://openairdocs.org/sdr/VNAA202209209997.md): None · corroded · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT RAIL FROM FS 969 - FS 985 IS CORRODED
- [SDR VNAA202209209996](https://openairdocs.org/sdr/VNAA202209209996.md): None · corroded · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R IS CORRODED COMPLETELY THROUGH AT F.S 319 COMMON TO GROUND STUD BRACKET.
- [SDR VNAA202209209995](https://openairdocs.org/sdr/VNAA202209209995.md): None · cracked · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Wing, Control Surfaces
  > RH SLAT PANEL #1 LOWER SKIN BENT/ CRACKED AROUND 622GZ CUTOUT AND SLAT DISCONNECT SENSOR FUSE IS BROKEN DUE TO SLAT INADVERTENTLY RETRACTED WITH SLAT DISCONNECT SENSOR LAYING IN 622GZ CUTOUT.
- [SDR VNAA202209209994](https://openairdocs.org/sdr/VNAA202209209994.md): None · corroded · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT RBL9 BETWEEN FS 485 AND 581.00 IS CORRODED.
- [SDR VNAA202209209993](https://openairdocs.org/sdr/VNAA202209209993.md): None · corroded · Sep 20, 2022 · N706PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT RBL9 BETWEEN FS 349.00 AND 485.00 IS CORRODED
- [SDR VNAA2021021311110](https://openairdocs.org/sdr/VNAA2021021311110.md): Controller · malfunctioned · Feb 9, 2021 · N706PS · Cndair CL6002C10 · Cabin Cooling System
  > LEFT PACK FAULT STATUS DURING TAKEOFF ROLL. REMOVED AND REPLACED LEFT PACK DISCHARGE TEMP SENSOR IAW CRJ 700 AMM 21-51-22-000/400-801-A01 SENSOR CHECKED GOOD ON BOTH CHANNELS. REMOVED AND REPLACED NO. 1 ACSC IAW CRJ 700 AMM 21-61-04-000/400-801-A01. COMPLIED W
- [SDR VNAA2020080911103](https://openairdocs.org/sdr/VNAA2020080911103.md): Windshield · cracked · Aug 6, 2020 · N706PS · Cndair CL6002C10 · Flight Compartment Windows
  > UPON ARRIVAL, THE CREW NOTICED THE RT WINDSHIELD WAS CRACKED. THE CREW DID NOT DECLARE A EMERGENCY, ATC DID. REMOVED THE RT WINDSHIELD IAW AMM 56-11-01-000-801-A01. INSTALLED A NEW RT WINDSHIELD IAW AMM 56-11-01-400-801-A01-PSA. OPS AND LEAK CHECKED GOOD.
- [SDR VNAA2020031111102](https://openairdocs.org/sdr/VNAA2020031111102.md): Torque Tube · disconnected · Mar 8, 2020 · N706PS · Cndair CL6002C10 · Trailing Edge Flap Control System
  > FLAP FAIL ASYMMETRICALLY. MAINTENANCE FOUND TORQUE TUBE FROM WS0.00 TO WS54.55 DISCONNECTED, MAINTENANCE RECONNECTED TUBE, RIGGED AND OPS CHECKED GOOD.
- [SDR VNAA2019110761101](https://openairdocs.org/sdr/VNAA2019110761101.md): Wire · broken · Nov 6, 2019 · N706PS · Cndair CL6002C10 · Light System Wiring
  > #4 CABIN EMERGENCY LIGHT WILL NOT ILLUMINATE (CEILING). MX FOUND BROKEN WIRE AT CONNECTOR P358. REPLACED CONTACT. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2019091111101](https://openairdocs.org/sdr/VNAA2019091111101.md): Actuator · failed · Sep 11, 2019 · N706PS · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > THIS WAS A MAINTENANCE OCF TEST FLIGHT. THE AIRCRAFT HAD BEEN IN MX OVERNIGHT FOR A FLAP FAIL CAUTION MESSAGE. AN OCF TEST FLIGHT WAS REQUIRED. DURING CLIMB THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE, COMPLIED WITH THE QRH, DECLARED AN EMERGENCY WITH ATC
- [SDR VNAA2019091011101](https://openairdocs.org/sdr/VNAA2019091011101.md): Indicator · tripped · Sep 10, 2019 · N706PS · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > DURING CLIMB THE CREW RECEIVED A FLAPS FAIL MESSAGE. INSTEAD OF RETURNING TO DCA THEY ARE DIVERTING TO IAD FOR RUNWAY LENGTH. RECEIVED FLAP FAIL MSG ON CLIMB OUT WHEN SEL SECT TO 0 DEG FROM 8 DEG POS RAN QRH MSG PERSISTED. FERRIED TO CVG FOR FURTHER TROUBLESHO
- [SDR VNAA2019090211101](https://openairdocs.org/sdr/VNAA2019090211101.md): Computer · failed · Sep 2, 2019 · N706PS · Cndair CL6002C10 · Fuel Quantity Sensor
  > ENROUTE TO DCA THE EICAS FUEL QUANTITY READOUTS GAVE AN AMBER MESSAGE ON THE LEFT TANK MAKING THE TOTAL QUANTITY ALSO UNKNOWN. THE CREW WAS ADVISED TO TRY AND RETURN TO CVG, BUT AFTER FOLLOWING THE QRH DECLARED AN EMERGENCY AND DIVERTED TO CRW. THE AIRCRAFT LA

Next page: https://openairdocs.org/aircraft/N706PS/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 = 'N706PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N706PS/reports

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