# Service difficulty reports: N702PS

A list on [N702PS](https://openairdocs.org/aircraft/N702PS.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 · 127 reports

- [SDR VNAA2026070220601](https://openairdocs.org/sdr/VNAA2026070220601.md): Uplock · unserviceable · Jun 29, 2026 · N702PS · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > STATUS MESSAGE PROX SYS FAULT 1, LANDING GEAR INDICATION ON R MAIN DASHED OUT AND YELLOW ALSO INTERMITTENT, GEAR DISAGREE WARNING MSG, WITH GEAR UP. REMOVED AND INSTALLED THE RT MLG UPLOCK IAW AMM 32-32-01-000/400-801. OCF COMPLETED SUCCESSFULLY.
- [SDR VNAA2026062920202](https://openairdocs.org/sdr/VNAA2026062920202.md): Terminal Block · faulted · Jun 25, 2026 · N702PS · Cndair CL6002C10 · Landing Gear System Wiring
  > APPR 20 MINS INTO OCF RECEIVED PROX SYS 1 FAULT STATUS MSG FOLLOWED BY GEAR AND FLAP ICONS THEN COULD HEAR GEAR TRYING TO EXTEND. PROBLEM PROGRESSIVELY BECAME MORE FREQUENT THROUGH REST OF FLIGHT AND RIGHT MLG GEAR STARTED SHOWING IN TRANSIT ON EICAS. COMMANDE
- [SDR VNAA2026062519401](https://openairdocs.org/sdr/VNAA2026062519401.md): Selector Valve · unserviceable · Jun 21, 2026 · N702PS · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > UNCOMMANDED RELEASE OF MLG, HYDS REPRESSURIZED AND RETRACTED, RAN QRC FOR GEAR DISAGREE FOR APPROACH SUCCESSFULLY. DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-01-2. REMOVED AND REPLACED SELECTOR VALVE IAW AMM 32€“32€“10€“000/400€“801. OPS CHECK
- [SDR VNAA202510020003](https://openairdocs.org/sdr/VNAA202510020003.md): Helicoil · missing · Oct 3, 2025 · N702PS · Cndair CL6002C10 · Wing Main, Frame Structure
  > RH WING JACK POINT MISSING HELI-COIL AND NYLON PLUG. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-57-22-155, REV -- DATED 2025-09-22 - TEMPORARY DISPOSITION FOR REMAINING THREADS AFTER REAMING RH WING JACKING FITTING BORE (DEVIATION TO GENERIC REO 670-57-22-
- [SDR VNAA202510020002](https://openairdocs.org/sdr/VNAA202510020002.md): Bracket · broken · Oct 3, 2025 · N702PS · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 2-3 LOWER BRACKET IS BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET ASSEMBLY IAW CRJ-700 AMM 20-21-00-910-801-A01. CC670-12065-1
- [SDR VNAA202510020001](https://openairdocs.org/sdr/VNAA202510020001.md): Skin · chafed · Oct 3, 2025 · N702PS · Cndair CL6002C10 · Ailerons
  > R/H AILERON UPPER LEADING EDGE IS CHAFED IN SEVERAL AREAS. CORRECTIVE ACTION: PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-57-61-194 REV -C DATED 2019-01-07. CC670-1305-1,-2,-3,-4
- [SDR VNAA2025091411102](https://openairdocs.org/sdr/VNAA2025091411102.md): Windshield · cracked · Sep 10, 2025 · N702PS · Cndair CL6002C10 · Flight Compartment Windows
  > CA WINDSHIELD OUTER LAYER MULTIPLE CRACKS DURING FLIGHT. PERFORMED INSTALLATION OF LH SIDE WINDOW IAW AMM 56-12-01-400-801-A01-PSA.
- [SDR VNAA2025062511102](https://openairdocs.org/sdr/VNAA2025062511102.md): Pseu · faulted · Jun 23, 2025 · N702PS · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG ON DECENT. / REMOVED AND REPLACED THE PSEU IAW AMM 32-61-01-00-801-A01,PERFORMED FUNCTIONAL TEST OF THE NOSE WHEEL STEERING AND OPERATIONAL TEST OF THE NOSE WHEEL STEERING IAW AMM 32-51-00-720-801-A01 AND 32-51-00-710-801-A01 RESPECT
- [SDR VNAA2024080611102](https://openairdocs.org/sdr/VNAA2024080611102.md): Control Lever · intermittent · Jul 30, 2024 · N702PS · Cndair CL6002C10 · Landing Gear Selector
  > DURING CRUISE ABOUT 1HR 20MIN INTO FLIGHT AT FL330 PROS SYS FAULT 1 STATUS MSG AND RIGHT LNDING GEAR YELLOW ON LANDING GEAR DISPLAY. SLOWED TO 220KTS AND BELOW MSG WAS INTERMITTENT. FELT SHUDDERING / REMOVED AND REPLACED LANDING GEAR LEVER CONTROL IAW CRJ700 A
- [SDR VNAA202318040001](https://openairdocs.org/sdr/VNAA202318040001.md): Unknown · gouged · Apr 18, 2023 · N702PS · Cndair CL6002C10 · Wing Spar
  > FOUND THE L/H WING INBOARD LEADING EDGE SKIN TO HAVE GOUGE DAMAGE ON THE OUTBOARD END AT WS 144.94
- [SDR VNAA202318040002](https://openairdocs.org/sdr/VNAA202318040002.md): Slat · gouged · Apr 18, 2023 · N702PS · Cndair CL6002C10 · Leading Edge Devices
  > FOUND LH SLAT #1 TO HAVE GOUGE NEAR MIDDLE ON BOTTOM SIDE.
- [SDR VNAA202302011111](https://openairdocs.org/sdr/VNAA202302011111.md): None · unserviceable · Jan 30, 2023 · N702PS · Cndair CL6002C10 · Fuel Quantity Indicator
  > TOTAL FUEL INDICATION DECREASED RAPIDLY DURING CLIMB / C/W EXTERNAL ZONAL INSPECTION OF A/C IAW CRJ700 AMM 05-21-00-210-802-A01. NO FUEL LEAKS NOTED. C/W OPS. TEST OF FUEL QTY. GAUGING COMPUTER IAW CRJ700 AMM 28-41-22-710-801-A01.. NO DEFECTS NOTED. DEFE
- [SDR VNAA202212151111](https://openairdocs.org/sdr/VNAA202212151111.md): Door · damaged · Dec 12, 2022 · N702PS · Cndair CL6002C10 · Landing Gear Doors
  > LOUD RUMBLING SOUND/VIBRATION FROM UNDER NOSE DURING FLIGHT SUSPECT NOSE GEAR DOORS NOT SEATING PROPERLY. REPLACED RH NLG DOOR AND ASSOCIATED HARDWARE IAW CRJ 700 AMM 32-22-01-000/400-801.
- [SDR VNAA202207051112](https://openairdocs.org/sdr/VNAA202207051112.md): Gcu · unserviceable · Jul 4, 2022 · N702PS · Cndair CL6002C10 · Alternator-Generator Drive
  > IN CRUISE FLIGHT AT FL310 CREW GOT GEN2 CAUTION MESSAGE. CA TOOK OVER THE CONTROLS AND FO RAN THROUGH ( QRC/QRH) BUT THE MESSAGE WAS STILL THERE. APU WAS ALREADY DIFFERED SO CREW DECLARED MECHANICAL EMERGENCY. CREW DID A NORMAL LANDING IN CLT ( NO OVERWEIGHT A
- [SDR VNAA202206099921](https://openairdocs.org/sdr/VNAA202206099921.md): Hinge Fitting · gouged · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Service Doors
  > EA 12-2020-258 (PERMANENT REPAIR OF SERVICE DOOR HINGE ASSEMBLY) ACCOMPLISH PERMANENT REPAIR PER EA 12-2020-258.
- [SDR VNAA202206099920](https://openairdocs.org/sdr/VNAA202206099920.md): Hinge Arm · gouged · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR, AFT HINGE ARM HAS CHAFFING AND GOUGING
- [SDR VNAA202206099919](https://openairdocs.org/sdr/VNAA202206099919.md): Former · loose · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PREVIOUS REPAIR ON PAX DOOR FORMER AND PULLEY HINGE BRACKET AT FS 347.25, DATUM 4 HAS WORKING/LOOSE FASTENERS.
- [SDR VNAA202206099918](https://openairdocs.org/sdr/VNAA202206099918.md): Slat Track · worn · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Wing, Control Surfaces
  > L/H SLAT TRACK 3-3 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
- [SDR VNAA202206099917](https://openairdocs.org/sdr/VNAA202206099917.md): Slat Track · worn · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Wing, Control Surfaces
  > L/H SLAT TRACK 3-1 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
- [SDR VNAA202206099916](https://openairdocs.org/sdr/VNAA202206099916.md): Slat Track · worn · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Wing, Control Surfaces
  > L/H SLAT TRACK 2-1HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
- [SDR VNAA202206099915](https://openairdocs.org/sdr/VNAA202206099915.md): Slat Track · worn · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Wing, Control Surfaces
  > L/H SLAT TRACK 1-3 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
- [SDR VNAA202206099914](https://openairdocs.org/sdr/VNAA202206099914.md): Slat Track · worn · Jun 12, 2022 · N702PS · Cndair CL6002C10 · Wing, Control Surfaces
  > L/H SLAT TRACK 1-2 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
- [SDR VNAA202206099913](https://openairdocs.org/sdr/VNAA202206099913.md): Slat Track · worn · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Flight Control System
  > L/H SLAT TRACK 1-1 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
- [SDR VNAA202206099912](https://openairdocs.org/sdr/VNAA202206099912.md): Fitting · damaged · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Vertical Stabilizer
  > RH HSTA SCREW JACK MOUNT FITTING HAS BURRS AND SIGNS OF TOOLING DAMAGE NEAR UPPER MOUNT BOLT ATTACH POINTS.
- [SDR VNAA202206099911](https://openairdocs.org/sdr/VNAA202206099911.md): Fitting · damaged · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Horizontal Stabilizer Structure
  > HSTA JACK SCREW MOUNT FITTING HAS SIGNS OF TOOLING MARK DAMAGE NEAR RH OUTBOARD UPPER MOUNT HOLE
- [SDR VNAA202206099910](https://openairdocs.org/sdr/VNAA202206099910.md): Rib · cracked · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Spoilers
  > R/H OUTBD GROUND SPOILER CENTER HINGE UPPER SURFACE LEADING EDGE CRACKED.
- [SDR VNAA202206099999](https://openairdocs.org/sdr/VNAA202206099999.md): Frame · corroded · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Fuselage Main, Frame
  > LOWER FRAME SEGMENT FS 364 (FWD SIDE) IS CORRODED SEVERAL LOCATIONS BETWEEN STRG 25L AND STRG 25R.
- [SDR VNAA202206099998](https://openairdocs.org/sdr/VNAA202206099998.md): Fitting · chafed · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Trailing Edge Flaps
  > LH O/B FLAP AT WS 178 AFT HINGE POINT FITTING ON WING HAS CHAFING ON METAL
- [SDR VNAA202206099997](https://openairdocs.org/sdr/VNAA202206099997.md): Skin · gouged · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > GOUGE ON PREVIOUS REPAIR BETWEEN FS 977 - FS 985 STGR 27
- [SDR VNAA202206099996](https://openairdocs.org/sdr/VNAA202206099996.md): Floorbeam · corroded · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088
- [SDR VNAA202206099995](https://openairdocs.org/sdr/VNAA202206099995.md): Floorbeam · corroded · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM AT LBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088
- [SDR VNAA202206099994](https://openairdocs.org/sdr/VNAA202206099994.md): Floorbeam · corroded · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM AT RBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088.
- [SDR VNAA202206099993](https://openairdocs.org/sdr/VNAA202206099993.md): Floorbeam · corroded · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088
- [SDR VNAA202206099992](https://openairdocs.org/sdr/VNAA202206099992.md): Skin · chafed · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Trailing Edge Flaps
  > L/H INBD FLAP INNER SKIN IS CHAFFED UNDER PANEL 584DB
- [SDR VNAA202206099991](https://openairdocs.org/sdr/VNAA202206099991.md): Arm · gouged · Jun 9, 2022 · N702PS · Cndair CL6002C10 · Cargo/Baggage Doors
  > REO 670-52-35-448(PERMANENT REPAIR) BLENDED GOUGE DAMAGE ON FWD CARGO DOOR FWD INNER ARM.
- [SDR VNAA202112011111](https://openairdocs.org/sdr/VNAA202112011111.md): Window · arced · Nov 27, 2021 · N702PS · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > CA SIDE WINDOW ARCING AT BOTTOM, APPROX 8-10 INCHES FROM PILLAR, CYCLED LH WINDOW HEAT, ARCING LESS INTENSE, ARCING STOPPED ONCE UNDER 15K FEET / DEFERRED LH SIDE WINDOW HEATING SYSTEM PER MEL 30-41-02 CAT A. DEACTIVATED LH SIDE WINDOW HEAT CONTROLLER BY PULLI
- [SDR VNAA202107131112](https://openairdocs.org/sdr/VNAA202107131112.md): Control Unit · failed · Jul 9, 2021 · N702PS · Cndair CL6002C10 · Stabilizer Control System
  > STAB TRIM RUNAWAY TOWARDS NOSE DOWN ON SHORT FINAL / PERFORMED DFDR DOWNLOAD IAW CRJ 700 AMM 31-33-01-970-802-A01. R&R OF THE HORIZONTAL STABLIZER MOTOR CONTROL UNIT IAW CRJ700 AMM 27-42-07-000/400-801-A01, & C/W SELF TEST OF THE SSCU IAW CRJ700 AMM 27-61-05-7
- [SDR VNAA202105311111](https://openairdocs.org/sdr/VNAA202105311111.md): Warning Message · illuminated · May 28, 2021 · N702PS · Cndair CL6002C10 · Drag Control System
  > EMERGENCY DECLARED GOING INTO PWM DUE TO IB FLIGHT SPOILER MESSAGE. NO TRUCKS WERE ROLLED AND NO NEED TO BRACE. FLIGHT LANDED SAFELY AND IS ON THE PHONE WITH MX NOW / CYCLED SYSTEM CBS AND PERFORMED SPOST2 TEST IAW CRJ700 AMM 27ˆ’61ˆ’05ˆ’740ˆ’801-A03 FAULT
- [SDR VNAA202103241111](https://openairdocs.org/sdr/VNAA202103241111.md): Selector Valve · malfunctioned · Mar 20, 2021 · N702PS · Cndair CL6002C10 · Landing Gear Steering System
  > DUE TO NOSEWHEEL STEERING INOP MESSAGE CAPTAIN INFORMED OPS AND ATC OF ISSUE AND ATC DECLARED AN EMERGENCY FOR THE FLIGHT. R/R LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA202103041111](https://openairdocs.org/sdr/VNAA202103041111.md): Wire Harness · damaged · Mar 2, 2021 · N702PS · Cndair CL6002C10 · Landing Gear System Wiring
  > ON TAKEOFF OUT OF TLH, CREW REPORTED A STEERING INOP MESSAGE, CREW RAN QRH. CREW THEN DECLARED AN EMERGENCY IN ORDER TO GET PRIORITY HANDLING AND THE LONG RWY (36C) IN CLT. UPON LANDING MAINTENANCE TOWED AIRCRAFT OFF TO SAFETY. CREW WAS ABLE TO RESET AND TAXI
- [SDR VNAA2020090299914](https://openairdocs.org/sdr/VNAA2020090299914.md): Stringer · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R IS CORRODED BETWEEN FS319.70 AND FS333 AT NUMEROUS LOCATIONS. INSTALLED NEW STRINGER 25R, IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR VNAA2020090299913](https://openairdocs.org/sdr/VNAA2020090299913.md): Stringer · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R IS CORRODED BETWEEN FS 1051-1098. REPAIRED IAW SRM 53-00-03-201-001-A01.
- [SDR VNAA2020090299912](https://openairdocs.org/sdr/VNAA2020090299912.md): Frame · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 1051 FRAME IS CORRODED BETWEEN STRINGER 25L AND STRINGER 25R. REPAIRED IAW STS EA 79-2020-009 REV P2 DATED 8/19/2020.
- [SDR VNAA2020090299911](https://openairdocs.org/sdr/VNAA2020090299911.md): Frame · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 1047 FRAME IS CORRODED BETWEEN STRINGER 27 AND STRINGER 26L. REPAIRED FRAME SEGMENT.
- [SDR VNAA2020090299910](https://openairdocs.org/sdr/VNAA2020090299910.md): Handle · cracked · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Passenger/Crew Doors
  > INNER PASSENGER DOOR HANDLE CRACKED AT INNER TAPGER PIN HOLE, P/N 600-31887-15. INSTALLED NEW HANDLE IAW CRJ700 SRM 51-40-11-001-001-A01.
- [SDR VNAA202009029999](https://openairdocs.org/sdr/VNAA202009029999.md): Frame · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 349.00 HAS CORROSION ON THE FLANGE AT STRINGER 26R. REMOVED AND REPLACED FRAME P/N SH670-31357-5 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR VNAA202009029998](https://openairdocs.org/sdr/VNAA202009029998.md): Stringer · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R BETWEEN FS863 TO FS879 HAS CORROSION AT RIVET. REPAIRED IAW EA: 80-2020-004 REV-P4, DATED 08/25/20.
- [SDR VNAA202009029997](https://openairdocs.org/sdr/VNAA202009029997.md): Angle · cracked · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR STEPS AFT WEB IS CRACKED AT LOWER STEP CORNER. COMPLIED WITH EO CL-600-2C10-52-LO6535 DATED 8-19-20 STEPS A(1-13) AND B(1-7).
- [SDR VNAA202009029996](https://openairdocs.org/sdr/VNAA202009029996.md): Web · cracked · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR STEPS AFT WEB REPAIR HAS MULTIPLE CRACKS AROUND ORIGINAL SKIN FASTENER HOLES. MULTIPLE DEFORMED FASTENER HOLES, AND MULTIPLE RIVET SHOP HEADS ARE MISFORMED. REPAIRED IAW EO CL-600-2C10-52-LO0537 DATED 8-19-2020.
- [SDR VNAA202009029995](https://openairdocs.org/sdr/VNAA202009029995.md): Skin · corroded · Sep 2, 2020 · N702PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INNER SKIN IS CORRODED BETWEEN DATUM AND DD1A FS313-FS320. INSTALLED NEW INNER SKIN P/N 601R318024-7 IAW CRJ 700/900 SRM 51-42-06-001-001-A01,51-42-13-001-001-A01,51-42-15-001-001-A01,51-42-21-001-001-A01,51-42-22-001-001-A01.

Next page: https://openairdocs.org/aircraft/N702PS/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 = 'N702PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N702PS/reports

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