# Service difficulty reports: N719PS

A list on [N719PS](https://openairdocs.org/aircraft/N719PS.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 · 102 reports

- [SDR VNAA2025092911101](https://openairdocs.org/sdr/VNAA2025092911101.md): Control Lever · inoperative · Sep 23, 2025 · N719PS · Cndair CL6002C10 · Landing Gear Selector
  > GEAR DISAGREE / STEERING INOP / GEAR WOULD NOT EXTEND WITH GEAR HANDLE. / REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW CRJ 700 AMM 32-31-01-000/400-802. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-00
- [SDR VNAA2024090411103](https://openairdocs.org/sdr/VNAA2024090411103.md): Manifold · faulted · Sep 1, 2024 · N719PS · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP AFTER ROTATION IN ALB, CAUTION MSG. / REMOVED AND INSTALLED NEW NLG STEERING MANIFOLD IAWCRJ 700 AMM 32-51-50-400-801-A01. LEAK, BITE AND OPS TEST GOOD AT THIS TIME. BLED SYSTEM 3 AND SERVICED SYSTEM 3. NO LEAK FOUND AT THIS TIME.
- [SDR VNAA2024082711107](https://openairdocs.org/sdr/VNAA2024082711107.md): Pcu · low pressure · Aug 16, 2024 · N719PS · Cndair CL6002C10 · Drag Control Actuator
  > WHILE DESCENDING INTO ICT AT FL280 WE RECEIVED A HYD 1 LOW PRESSURE EICAS CAUTION. REMOVED AND REPLACED THE RHOB GROUND SPOILER PCU IAW CRJ 700 AMM 27-63-01-000/400-801-A01.
- [SDR VNAA202408070029](https://openairdocs.org/sdr/VNAA202408070029.md): Transcowl · cracked · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Nacelle/Pylon Structure
  > UPON REMOVAL OF THE RH UPPER TRANSCOWL LATCH COAMING, FOUND THE UNDERLYING STRUCTURE TO BE CRACKED. REPAIRED R/H UPPER TRANSCOWL FWD DISHING IAW MHIRJ REO 670-54-21-1647 REV. A DATED 2024-06-17.
- [SDR VNAA202408070028](https://openairdocs.org/sdr/VNAA202408070028.md): Diaphragm · cracked · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Aerodynamic Fairings
  > CRACK FOUND COMMON TO WING TO BODY FAIRING DIAPHRAGM AT F.S 913, RBL 17.3 ON P/N SH670-39241-3. REPAIRED CRACK IAW BOMBARDIER REO 670-53-82-478 REV-A DATED 2014-11-12.
- [SDR VNAA202408070027](https://openairdocs.org/sdr/VNAA202408070027.md): Retainer · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR LOWER AFT CORNER SEAL RETAINER IS SEVERELY CORRODED. REMOVED DAMAGED AFT BAGGAGE BAY DOOR LOWER AFT CORNER SEAL RETAINER PN: CC670-38746-1 IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE AFT BAGGAGE BAY DOOR LOWER AFT CO
- [SDR VNAA202408070026](https://openairdocs.org/sdr/VNAA202408070026.md): Bracket · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR LOWER FWD CORNER SEAL RETAINER IS SEVERELY CORRODED. REMOVED DAMAGED AFT BAGGAGE BAY DOOR LOWER FWD CORNER SEAL RETAINER PN: CC670-38744-1 IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE AFT BAGGAGE BAY DOOR LOWER FWD COR
- [SDR VNAA202408070025](https://openairdocs.org/sdr/VNAA202408070025.md): Door Sill · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY DOOR SILL IS CORRODED. REMOVED AFT CARGO DOOR LOWER SILL BETWEEN FS 1000 TO FS1047 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW SERVICEABLE AFT CARGO DOOR LOWER SILL PN: MM670-35655-003 IAW
- [SDR VNAA202408070024](https://openairdocs.org/sdr/VNAA202408070024.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK LBL 27 CORRODED BETWEEN FS 1033 AND FS 1061. CORRECTIVE ACTION: REPLACED LBL 27 SEAT TRACK FROM FS 1033 AND FS 1061 IAW CRJ-700 SRM 53-00-49-201-002-A01."
- [SDR VNAA202408070023](https://openairdocs.org/sdr/VNAA202408070023.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE REMOVING SEAT TRACK FOR ACCESS TO FLOOR BEAM REPAIR @ APPROX F.S 1031-1061 LBL 9, FOUND SEAT TRACK TO BE CORRODED. FABRICATED NEW SERVICEABLE SEAT TRACK FROM F.S. 1031 -1061 LBL 9 IAW CRJ700 SRM 53-00-49-201-002-A01. REFERENCE BARCODE: HN00163768 FOR IN
- [SDR VNAA202408070022](https://openairdocs.org/sdr/VNAA202408070022.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE REMOVING SEAT TRACK FOR ACCESS TO FLOOR BEAM REPAIR @ APPROX F.S 975-1005 RBL 9, FOUND SEAT TRACK TO BE CORRODED. FABRICATED NEW SERVICEABLE SEAT TRACK FROM F.S. 975 -1005 RBL 9 IAW CRJ700 SRM 53-00-49-201-002-A01. NEWLY FABRICATED SEAT TRACK WAS INSTA
- [SDR VNAA202408070021](https://openairdocs.org/sdr/VNAA202408070021.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE REMOVING SEAT TRACK FOR ACCESS TO FLOOR BEAM REPAIR @ APPROX F.S 975-1005 LBL 27, FOUND SEAT TRACK TO BE CORRODED. FABRICATED NEW SERVICEABLE SEAT TRACK FROM F.S. 975 -1005 LBL 27 IAW CRJ700 SRM 53-00-49-201-002-A01. NEWLY FABRICATED SEAT TRACK WAS INS
- [SDR VNAA202408070020](https://openairdocs.org/sdr/VNAA202408070020.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > "HN00165852 DISCREPANCY: WHILE REMOVING SEAT TRACK FOR ACCESS TO FLOOR BEAM REPAIR @APPROX F.S 1033-1061 RBL 9, FOUND SEAT TO BE CORRODED CORRECTIVE ACTION: FABRICATED NEW SERVICEABLE SEAT TRACK FROM F.S. 1033-1061 RBL 9 IAW CRJ700 SRM 53-00-49-201-002-A01.
- [SDR VNAA202408070019](https://openairdocs.org/sdr/VNAA202408070019.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE REMOVING SEAT TRACK @ APPROX F.S 975 TO 1005 RBL 9 FOR ACCESS TO FLOOR BEAM REPAIR, FOUND SEAT TRACK TO BE CORRODED. RECEIVED NEW SERVICEABLE SEAT TRACK PART NUMBER BA670-45073-3. REFERENCE BARCODE# HN00166084 FOR INSTALLATION OF NEW RBL 9 SEAT TRACK B
- [SDR VNAA202408070018](https://openairdocs.org/sdr/VNAA202408070018.md): Frame · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND CORROSION ON FS 1000 FRAME BETWEEN STRINGER 25R AND STRINGER 25L. REPAIRED CORRODED FRAME IAW MHIRJ REO 670-53-61-2311 REV.—DATED 2024-07-02.
- [SDR VNAA202408070017](https://openairdocs.org/sdr/VNAA202408070017.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE REMOVING SEAT TRACK @ APPROX F.S 975 TO 1005 RBL 27 FOR ACCESS TO FLOOR BEAM REPAIR, FOUND SEAT TRACK TO BE CORRODED. INSTALLED NEW SERVICEABLE SEAT TRACK P/N: BA670-45073-3 AT APPROX F.S. 975 TO 1005 RBL27 IAW CRJ700 AMM 53-00-49-400-802-A03.
- [SDR VNAA202408070016](https://openairdocs.org/sdr/VNAA202408070016.md): Seat Track · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE REMOVING SEAT TRACK FOR ACCESS TO FLOOR BEAM REPAIR @APPROX F.S 1033-1061 RBL 27, FOUND SEAT TO BE CORRODED. FABRICATED NEW SERVICEABLE SEAT TRACK FROM F.S. 1033-1061 RBL 27 IAW CRJ700 SRM 53-00-49-201-002-A01.
- [SDR VNAA202408070015](https://openairdocs.org/sdr/VNAA202408070015.md): Floor Support · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR BEAM AT RBL 9 AT FS 1031. REPAIRED CORRODED FLOORBEAM AT RBL 9 FROM FS 1031 TO 1051.30 IAW MHIRJ REO 670-53-62-2290 REV. – DATED 2024-06-07 AND CRJ 700 AMM 53-00-49-000-802-A03."
- [SDR VNAA202408070014](https://openairdocs.org/sdr/VNAA202408070014.md): Floorbeam · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOOR BEAM AT RBL 27 AT FS 1031. REPAIRED FLOOR BEAM AT RBL 27 FS 1031 IAW MHI RJ REO 670-53-61-2290 REV – DATED 2024-06-07 AND CRJ 700 SRM 53-00-41-201-001-A01 -830, CRJ 700 SRM 51-25-16-001-001-A01. "
- [SDR VNAA202408070013](https://openairdocs.org/sdr/VNAA202408070013.md): Floor Support · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR BEAM AT LBL 9 AT FS 1031. REPAIRED CORRODED FLOORBEAM AT RBL 9 FROM FS 1031 TO 1051.30 IAW MHIRJ REO 670-53-62-2290 REV. – DATED 2024-06-07 AND CRJ 700 AMM 53-00-49-000-802-A03.
- [SDR VNAA202408070012](https://openairdocs.org/sdr/VNAA202408070012.md): Floorbeam · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOOR BEAM AT LBL 27 AT FS 1031. REPAIRED CORRODED FLOORBEAM AT LBL 27 FROM FS 1031 TO 1051.30 IAW MHIRJ REO 670-53-62-2290 REV. – DATED 2024-06-07 AND CRJ 700 AMM 53-00-49-000-802-A03"
- [SDR VNAA202408070011](https://openairdocs.org/sdr/VNAA202408070011.md): Post · cracked · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Main, Structure
  > RH WINDSHIELD SIDE POST IS CRACKED AT THE TOP. REMOVED AND REPLACED RH WINDSHIELD SIDE POST IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01."
- [SDR VNAA202408070010](https://openairdocs.org/sdr/VNAA202408070010.md): Doubler · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR SURROUND STRUCTURE SILL PLATE AND ""H"" DOUBLER BETWEEN F.S.533 TO F.S.549 ARE CORRODED. REMOVED DAMAGED JOINT PLATE (H DOUBLER) IAW CRJ-700 SRM 51-42-22-001-001-A01. INSTALLED NEW SERVICEABLE JOINT PLATE PN: SH670-33793-4 IAW CRJ-700 SRM 51-4
- [SDR VNAA202408070009](https://openairdocs.org/sdr/VNAA202408070009.md): Stringer · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STGR 26 BETWEEN FS 1015.00 AND FS 1051.30. REPAIRED CORRODED STRINGER IAW CRJ 700 SRM 53-00-03-201-A01."
- [SDR VNAA202408070008](https://openairdocs.org/sdr/VNAA202408070008.md): Intercostal · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD6 AFT CLEAT FOUND TO BE CORRODED REQUIRE REPLACEMENT. REMOVED PAX DOOR MID INTERCOSTAL DD6 AFT CLEAT P/N # 600-31902-269 IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD6 AFT CLEAT P/N #
- [SDR VNAA202408070007](https://openairdocs.org/sdr/VNAA202408070007.md): Coaming · cracked · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Engine Exhaust System
  > RH UPPER TRANSCOWL LATCH COAMING IS CRACKED. REMOVED AND REPLACED COAMING IAW MHIRJ REO 670-54-21-1647 REV -A DATED 2024-06-17."
- [SDR VNAA202408070006](https://openairdocs.org/sdr/VNAA202408070006.md): Intercostal · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD6 IS CORRODED. REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01."
- [SDR VNAA202408070005](https://openairdocs.org/sdr/VNAA202408070005.md): Angle · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND SERVICE DOOR MOUNTING ANGLE TO BE CORRODED. REPLACED DAMAGED MOUNTING ANGLE P/N SH670-31996-3S WITH NEW SERVICEABLE MOUNTING ANGLE P/N SH670-31996-3S IAW CRJ 700 SRM 51-42-06-001-001-A01"
- [SDR VNAA202408070004](https://openairdocs.org/sdr/VNAA202408070004.md): Intercostal · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 MIDDLE IS CORRODED AND REQUIRES REPLACEMENT. (INSIDE OF PAX DOOR). REMOVED PAX DOOR INTERCOSTAL DD4 MIDDLE IAW CRJ 700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DO
- [SDR VNAA202408070003](https://openairdocs.org/sdr/VNAA202408070003.md): Former · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER @ FS311.75 CORRODED, REQUIRES REPLACEMENT. REMOVED CORRODED PAX DOOR FORMER IAWCRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FORMER FS311.75 P/N# 601R318315S IAW CRJ 700 SRM 51-42-06-001-00-A01."
- [SDR VNAA202408070002](https://openairdocs.org/sdr/VNAA202408070002.md): Intercostal · cracked · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 AFT IS CRACKED. REQUIRES REPLACEMENT. (INSIDE PAX DOOR). INSTALLED NEW SERVICEABLE DD1 INTERCOSTAL PN 601R31902-318 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. "
- [SDR VNAA202408070001](https://openairdocs.org/sdr/VNAA202408070001.md): Web · corroded · Aug 7, 2024 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD WEB CORRODED, REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE FWD STAIR WEB PN 601R317071-12 IAW CRJ 700 SRM 51-40-11-001-001-A01. REFERENCE HN 00160606 FOR INSTALLATION OF FWD WEB ONTO PAX DOOR"
- [SDR VNAA202208041111](https://openairdocs.org/sdr/VNAA202208041111.md): Yoke · out of position · Aug 2, 2022 · N719PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MOTOR ASSIST YOKE ASSEMBLY PULLING FROM DOOR STRUCTURE / C/W PERM REPAIR FOR PAX DOOR STRUCTURE AT PAX MOTOR YOKE IAW REO 670-52-11-130 STEPS 6 THRU COMPLETION SDIR ASSESSMENT DUE WITHIN 12 MONTHS FORM 337 ON FILE WEIGHT AND BALANCE REVISION COMPLETED
- [SDR VNAA202203141111](https://openairdocs.org/sdr/VNAA202203141111.md): None · none · Mar 10, 2022 · N719PS · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > SUPPLEMENTAL RECORD CORRECTION
- [SDR VNAA202008069993](https://openairdocs.org/sdr/VNAA202008069993.md): Tee Fitting · cracked · Aug 6, 2020 · N719PS · Bombdr CL6002D15 · Fuselage Main, Attach Fittings
  > LEFT TEE FITTING AT ATTACHMENT OF BS 280 CROSSBEAM TO LONGITUDINAL FLOOR SUPPORT AT LBL 9. REMOVED AND REPLACED THE TEE FITTING.
- [SDR VNAA202008069992](https://openairdocs.org/sdr/VNAA202008069992.md): Door · cracked · Aug 6, 2020 · N719PS · Bombdr CL6002D15 · Landing Gear Doors
  > LEFT MLG INBOARD DOOR HAD A CRACK ON FORWARD MEMBER. REMOVED AND REPLACED THE LT MLG INBOARD DOOR.
- [SDR VNAA202008069991](https://openairdocs.org/sdr/VNAA202008069991.md): Tee Fitting · cracked · Aug 6, 2020 · N719PS · Bombdr CL6002D15 · Fuselage Main, Attach Fittings
  > DURING A HEAVY CHECK INSPECTION, FOUND EVIDENCE CRACKING ON THE RT TEE FITTING AT ATTACHMENT OF FS 280 CROSSBEAM TO LONGITUDINAL FLOOR SUPPORT AT RBL 9. REMOVED AND REPLACED THE TEE FITTING.
- [SDR VNAA2020012321101](https://openairdocs.org/sdr/VNAA2020012321101.md): Acm · failed · Jan 22, 2020 · N719PS · Cndair CL6002C10 · Cabin Cooling System
  > CREW REPORTED SMOKE IN THE CABIN WITH THE APU RUNNING. THIS WAS THE FIRST FLIGHT OF THE DAY WITH NO PASSENGERS ON BOARD. MX DEFERRED RH PACK.MX REMOVED AND REPLACED THE RH ACM. OPS AND LEAK CHECK GOOD. CLEARED MEL.
- [SDR VNAA2020010741101](https://openairdocs.org/sdr/VNAA2020010741101.md): Battery Pack · discharged · Jan 4, 2020 · N719PS · Cndair CL6002C10 · Emergency Lighting
  > CREW REPORTED ALL EMERGENCY LIGHTS WOULD SHUT OFF AFTER 4 SECONDS. MX REMOVED AND REPLACED ALL 4 EMERGENCY LIGHT BATTERIES AND THE LIGHTS OPERATED NORMALLY. PART NUMBER / SERIAL NUMBER LISTED IN THE PARTS SECTION IS POSITION 1. POSITION 2 P/N AD2013-1A S/N 205
- [SDR VNAA2019092511101](https://openairdocs.org/sdr/VNAA2019092511101.md): Blade · damaged · Sep 25, 2019 · N719PS · Cndair CL6002C10 · Turbine Engine Compressor Section
  > DURING TAKE OFF FROM RUNWAY 36R AT 100 KNOTS THE CREW BELIEVED THEY BLEW A TIRE AND REJECTED THE TAKE OFF. THE AIRCRAFT TAXIED BACK TO THE GATE UNDER IT'S OWN POWER. MX INSPECTED AND FOUND DAMAGE TO RT ENGINE FAN BLADES. BORESCOPE INSPECTION REVEALED ENGINE
- [SDR VNAA2018083111102](https://openairdocs.org/sdr/VNAA2018083111102.md): Smoke Detector · false activation · Aug 31, 2018 · N719PS · Cndair CL6002C10 · Smoke Detection
  > ABORTED TAKEOFF DUE TO A LAV SMOKE WARNING. LAVATORY WAS INSPECTED BY THE FIRE DEPARTMENT WITH THERMAL SENSORS. NO EVIDENCE OF FIRE OR SMOKE FOUND. DEFERRED LAV SMOKE DETECTION SYSTEM. R&R LAV SMOKE DETECTOR IAW AMM 26-11-01-000/400-801, OPS CHECK GOOD.
- [SDR VNAA2018083041101](https://openairdocs.org/sdr/VNAA2018083041101.md): Control Valve · leaking · Aug 24, 2018 · N719PS · Cndair CL6002C10 · Cabin Pressure Control System
  > DIVERTED DUE TO A BLEED DUCT WARNING, THAT CUASED THE AIRCRAFT TO LOOSE PRESSURIZATION AND DEPLOY THE CREW AND PAX OXYGEN MASKS. MAINTENANCE REPLACED THE RT FLOW CONTROL VALVE DUE TO LEAKING ON THE LOOPS, CAUSING THE MESSAGE.
- [SDR VNAA2017111699903](https://openairdocs.org/sdr/VNAA2017111699903.md): Door Sill · corroded · Nov 16, 2017 · N719PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL IS CORRODED FROM BS 310 TO 349. INSTALLED PAX DOOR LOWER SILL IAW SRM 51-42-02-001-001-A01, AND SRM 51-42-21-001-001-A01.
- [SDR VNAA2017111699902](https://openairdocs.org/sdr/VNAA2017111699902.md): Floorbeam · cracked · Nov 16, 2017 · N719PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > WHILE PERFORMING REO 670-53-11-745, REV A, FOUND LEFT AND RIGHT FLIGHT DECK CENTER FLOORBEAM ANGLES CRACKED AT THE AFT END, BS 280. LOCATED AND DRILLED A NEW FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01. LOCATED AND DRILLED A NEW FLOORBEAM ANGLE IAW SRM 51-4
- [SDR VNAA2017111699901](https://openairdocs.org/sdr/VNAA2017111699901.md): Floorbeam · corroded · Nov 16, 2017 · N719PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM FORWARD ANGLE IS CORRODED. LOCATED AND DRILLED A NEW ANGLE IAW IAW SRM 57-40-11-001-001-A01.
- [SDR VNAA2017111599901](https://openairdocs.org/sdr/VNAA2017111599901.md): Rib · cracked · Nov 15, 2017 · N719PS · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > BAT RIB WS 24.50 ON LT OUTER WING IS CRACKED. INSTALLED A NEW BAT RIB IAW SRM 51-42-21-001-001-A01, & 51-42-22-001-001-A01.
- [SDR VNAA2017091611101](https://openairdocs.org/sdr/VNAA2017091611101.md): Fan · failed · Sep 16, 2017 · N719PS · Cndair CL6002C10 · Air Distribution Fan
  > THE CREW REPORTED A BURNING ODOR WHILE THE AIRCRAFT WAS AT THE GATE. IT WAS DISCOVERED THAT THE DISPLAY FAN NR 2 WAS THE CAUSE.
- [SDR VNAA2016121800035](https://openairdocs.org/sdr/VNAA2016121800035.md): Wire Harness · damaged · Dec 18, 2016 · N719PS · Cndair CL6002C10 · Landing Gear System Wiring
  > BRAKE OVERHEAT WARNING DURING TAKE OFF. REMOVED AND REPLACED THE MAIN LANDING GEAR LEFT OUTBOARD HARNESS.
- [SDR VNAA2016081000007](https://openairdocs.org/sdr/VNAA2016081000007.md): Acm · seized · Aug 10, 2016 · N719PS · Cndair CL6002C10 · Cabin Cooling System
  > CABIN TEMPERATURE CONTROL SYSTEM INOPERATIVE, SMOKE IN MID CABIN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE AIR CYCLE MACHINE AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FO
- [SDR VNAA2016032700033](https://openairdocs.org/sdr/VNAA2016032700033.md): Light · inoperative · Mar 27, 2016 · N719PS · Cndair CL6002C10 · Emergency Lighting
  > CREW REPORTED RT EMERGENCY EXIT LIGHT ON FORWARD CABIN BULKHEAD INOPERATIVE. MAINTENANCE TROUBLESHOT. R & R THE EMERGENCY EXIT LIGHT HOUSING ASSY AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N719PS/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 = 'N719PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N719PS/reports

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