# Service difficulty reports: N216PS, cancelled Dec 31, 2022

A list on [N216PS, cancelled Dec 31, 2022](https://openairdocs.org/deregistered/N216PS-2022-12-31.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 2 · 85 reports

- [SDR VNAA2018100999906](https://openairdocs.org/sdr/VNAA2018100999906.md): Bulkhead · cracked · Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 RPB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AT RBL 18 WL 100 1" LONG BY 50% FSH. REPAIRED FS 621 RPB WEB AT RBL 18 IAW REO 601R-53-61-1285 REV E.
- [SDR VNAA2018100999905](https://openairdocs.org/sdr/VNAA2018100999905.md): Bulkhead · cracked · Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 RPB WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AT RBL 9 WL 108 TO WL 110 BY 50% FSH. REPAIRED WEB AND Z MEMBER AT FS 621 RPB AT RBL 9 IAW REO 601R-53-61-1285 REV E.
- [SDR VNAA2018100999904](https://openairdocs.org/sdr/VNAA2018100999904.md): Bulkhead · cracked · Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 RPB WEB HAS 2 AREAS OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AT BL WL 126 TO WL 134 BY 60% FSH AND AT BL 0 WL110 TO WL 114 BY 70% FSH. BOTH AREAS FAILED NDT. REPLACED AND INSTALLED UPPER AND LOWER ENGINE BEAM SUPPORT ANGLES AT BL 0 IAW
- [SDR VNAA2018100999903](https://openairdocs.org/sdr/VNAA2018100999903.md): Bulkhead · cracked · Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 RPB WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AT LBL 18 - WL 106-110 BY 50% FSH. FAILED NDT. FS 621 PRESSURE BULKHEAD Z MEMBER AT LBL 18 WL 111 FOUND INDICATION APPROX 1/4 LONG 80% FCH. REPAIRED 621 RPB WEB AND Z MEMBER A
- [SDR VNAA2018100999902](https://openairdocs.org/sdr/VNAA2018100999902.md): Bulkhead · cracked · Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 RPB WEB HAS AN AREA OF CRACK INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AT LBL 27 WL 130-131.5 BY 100% FSH, EXTENDING UNDER THE TOP OF THE CARGO DOOR AFT TRACK. C/W REPAIR AT FS 621, LBL 27 WL 130-131.5 IAW REO 601R-53-61-1541 DATED 11/12/14 REV F
- [SDR VNAA2018100999901](https://openairdocs.org/sdr/VNAA2018100999901.md): Door Sill · corroded · Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL FROM FS.559+16 TO FS.559+32 HAS CORROSION. C/A: BLENDED CORROSION ON RT FLOOR SILL FROM FS.559+16 TO FS.559+32.
- [SDR VNAA2018100599904](https://openairdocs.org/sdr/VNAA2018100599904.md): Fitting · cracked · Oct 5, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT BEAM INTERCOSTAL CLIPS ARE CRACKED AT FS 484.00 RBL 27 AND RBL 36. C/A: REMOVED AND REPLACED CLIP AT RBL 27 IAW SRM 51-42-21. FOR RBL 36 COMPLIED WITH REO 601R-53-41-059 REV B 2009-09-16.
- [SDR VNAA2018100599903](https://openairdocs.org/sdr/VNAA2018100599903.md): Fitting · cracked · Oct 5, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT BEAM INTERCOSTAL CLIPS ARE CRACKED AT FS 484.00 LBL 27 AND LBL 36. C/A: REMOVED & REPLACED CLIP AT LBL 27 IAW SRM 51-42-21. FOR LBL 36 COMPLIED WITH REO 601R-53-41-059 REV B 2009-09-16
- [SDR VNAA2018100599902](https://openairdocs.org/sdr/VNAA2018100599902.md): Structure · cracked · Oct 5, 2018 · N216PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR ASSIST MOTOR LOWER "2" MEMBER IS CRACKED. C/A: 1. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13.
- [SDR VNAA2018100599901](https://openairdocs.org/sdr/VNAA2018100599901.md): Intercostal · cracked · Oct 5, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 621-625 OBLIQUE ANGLE AT RBL 36 IN CRACKED APPROX.5". C/A: LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE RT OBLIQUE ANGLE IAW SRM 51-40-11+ 51-42-21. WVAC704MTC 09/19/18 M/A.
- [SDR VNAA2018081321101](https://openairdocs.org/sdr/VNAA2018081321101.md): Lever · malfunctioned · Aug 12, 2018 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION MESSAGE AT 20 DEGRESS IN FLT. THE AIRCRAFT DIVERTED AND DECLARED EMERGENCY. RESET FLAP SYSTEM. MX TROUBLESHOT THE SYSTEM TO FLAP LEVER FAULT. COMPLIED WITH TAKEOFF AND A.D. OPS CHECKED GOOD.
- [SDR VNAA2018053111101](https://openairdocs.org/sdr/VNAA2018053111101.md): Bpsu · out of rig · May 31, 2018 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING FINAL APPROACH THE CREW SELECTED FLAPS 30 AND RECEIVED A FLAPS FAIL WARNING MESSAGE. THE CREW DECLARED AN EMERGENCY AND DIVERTED AND LANDED WITHOUT INCIDENT. MX C/W T.O. 27-050-004 ZERO RIGGED BPSU'S. RIG CHECKED GOOD AT THIS TIME. OPS CHECK GOOD. THIS
- [SDR VNAA2018021611101](https://openairdocs.org/sdr/VNAA2018021611101.md): Warning Message · activated · Feb 16, 2018 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > THE CREW RECEIVED A FLAPS FAIL MESSAGE AT 20 DEGREES. THE CREW RAN THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. OPEN.
- [SDR VNAA2017040500004](https://openairdocs.org/sdr/VNAA2017040500004.md): Unknown · smoke · Apr 5, 2017 · N216PS · Cndair CL6002B19 · Air Distribution System
  > SMOKE IN LAVATORY, AN EMERGENCY WAS DECLARED.
- [SDR VNAA2017032300014](https://openairdocs.org/sdr/VNAA2017032300014.md): Unknown · smoke · Mar 23, 2017 · N216PS · Cndair CL6002B19 · Air Distribution System
  > SMOKE IN LAVATORY AFTER TAKEOFF.
- [SDR VNAA2017031900010](https://openairdocs.org/sdr/VNAA2017031900010.md): Smoke Warning · activated · Mar 19, 2017 · N216PS · Cndair CL6002B19 · Smoke Detection
  > SMOKE IN TOILET CAUTION MESSAGE.
- [SDR VNAA2017013100042](https://openairdocs.org/sdr/VNAA2017013100042.md): Coalescer Bag · saturated · Jan 31, 2017 · N216PS · Cndair CL6002B19 · Humidity Control System
  > AFTER SWITCHING BLEEDS TO ENGINES, THE CABIN FILLED WITH SMOKE AND BURNT OIL SMELL. CLEANED LEFT AND RIGHT HAND COALESCERS, REMOVED AND REPLACED BOTH COALESCER BAGS AND SEALS. OPS CHECKED GOOD.
- [SDR VNAA2016122000037](https://openairdocs.org/sdr/VNAA2016122000037.md): Yaw Damper · malfunctioned · Dec 20, 2016 · N216PS · Cndair CL6002B19 · Auto Flight System
  > UNCOMMANDED YAW AT FL230, FOLLOWED BY A YAW DAMPER 1 DISCONNECT. PERFORMED TEST OF THE YAW DAMPER, OPS CHECKED GOOD. PERFORMED TEST OF THE YAW DAMPER PANEL, OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR VNAA2016100600008](https://openairdocs.org/sdr/VNAA2016100600008.md): Control Unit · malfunctioned · Oct 6, 2016 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 20 DEGREES WHEN SELECTING FLAPS 30 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016092500043](https://openairdocs.org/sdr/VNAA2016092500043.md): Skin Panel · cracked · Sep 25, 2016 · N216PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NOSE LANDING GEAR CUT-OUT AT FS 235 LBL 26 AND RBL 26 HAS CRACKS IN RADIUS. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT FS 235 BETWEEN STR 26L AND 26R AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016081600023](https://openairdocs.org/sdr/VNAA2016081600023.md): Skin · damaged · Aug 16, 2016 · N216PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > DURING POST FLIGHT INSPECTION, CREW FOUND THE LOWER ACCESS COWL MISSING. MAINTENANCE INSPECTED, REPLACED THE LOWER ACCESS COWL AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016081600022](https://openairdocs.org/sdr/VNAA2016081600022.md): Panel · missing · Aug 16, 2016 · N216PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > DURING POST FLIGHT INSPECTION, CREW FOUND THE UPPER ACCESS COWL MISSING. MAINTENANCE INSPECTED, REPLACED THE UPPER ACCESS COWL AND PERFORMED CHECKS IAW THE AMM.
- [SDR VNAA2016080500004](https://openairdocs.org/sdr/VNAA2016080500004.md): Battery Pack · inoperative · Aug 5, 2016 · N216PS · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT LIGHT OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, REPLACED THE LAMP IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016050800006](https://openairdocs.org/sdr/VNAA2016050800006.md): Smoke Detector · faulty · May 8, 2016 · N216PS · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAUTION MESSAGE ON DEPARTURE. THE CREW DECLARED AN EMERGENCY, RETURNED TO FIELD, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R THE LAVATORY SMOKE DETECTOR AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016042000020](https://openairdocs.org/sdr/VNAA2016042000020.md): Position Sensor · failed · Apr 20, 2016 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION AND FLAPS FAIL ON FINAL APPROACH. THE CREW DECLARED AND EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT BRAKE AND POSITION SENSOR, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR
- [SDR VNAA2016041400016](https://openairdocs.org/sdr/VNAA2016041400016.md): Position Sensor · out of adjust · Apr 14, 2016 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL "C" MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND DEFERRED THE FLAP SYS IAW MEL 90-10-02 CAT "A". MAINTENANCE CLEARED THE MEL BY RIGGING THE R
- [SDR VNAA2016022400031](https://openairdocs.org/sdr/VNAA2016022400031.md): Sensor · failed · Feb 24, 2016 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > CREW REPORTED FLAPS FAIL CAUTION ON APPROACH. THE CREW LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE TROUBLESHOT, R & R THE LT BRAKE AND POSITION SENSOR UNIT. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016022300030](https://openairdocs.org/sdr/VNAA2016022300030.md): Warning Message · false activation · Feb 23, 2016 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED RECEIVING A TAT CAUTION MESSAGE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED, RECYCLED CIRCUIT BREAKERS, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016021500019](https://openairdocs.org/sdr/VNAA2016021500019.md): Pitot Tube · contaminated · Feb 15, 2016 · N216PS · Cndair CL6002B19 · Pitot/Static System
  > CREW REPORTED THAT DURING CRUISE, AT 31,000 FT, THEY RECEIVED AN EFIS COMP MON MESSAGE THAT THE CAPTAIN’S SIDE INDICATED AIRSPEED WAS UNRELIABLE. THE CREW DECLARED AN EMERGENCY WITH ATC. THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINT
- [SDR VNAA2016021300015](https://openairdocs.org/sdr/VNAA2016021300015.md): Heater · malfunctioned · Feb 13, 2016 · N216PS · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > CREW REPORTED LT PITOT HEAT SYS FAIL IN FLIGHT. THE CREW RETURNED TO FIELD. MAINTENANCE OPS CHECK LT PITOT HEAT SYSTEM IAW AMM. OPS CHECK GOOD, THE ACFT WAS RELEASE FOR SERVICE.
- [SDR VNAA2015080700010](https://openairdocs.org/sdr/VNAA2015080700010.md): Wire Harness · shorted · Aug 7, 2015 · N216PS · Cndair CL6002B19 · Landing Gear System Wiring
  > CREW REPORTED GEAR WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT OTBD MLG HARNESS AND PERFORMED CHECKS IAW STC ST03239AT AND AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015072300028](https://openairdocs.org/sdr/VNAA2015072300028.md): Tire · failed · Jul 23, 2015 · N216PS · Cndair CL6002B19 · Tire
  > RIGHT OTBD MLG TIRE REPORTED TO HAVE TREAD SEPARATION. MAINTENANCE INSPECTED AND R & R NR 4 MAIN WHEEL AND TIRE ASSY. RIGHT MLG DOOR WAS REMOVED DUE TO DAMAGE FROM TIRE FAILURE AND LISTED ON CONFIGURATION DEVIATION LIST (CDL). RIGHT INBD FLAP WAS R & R DUE
- [SDR VNAA2015071200011](https://openairdocs.org/sdr/VNAA2015071200011.md): Control Unit · out of adjust · Jul 12, 2015 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL MESSAGE ON APPROACH. CREW INITIATED MISSED APPROACH PROCEDURES, DID A GO-AROUND AND LANDED SAFELY WITH FLAPS AT 20 DEGREES. MAINTENANCE TROUBLESHOT IAW ACFT FAULT ISOLATION MANUAL (FIM) AND FOUND POTENTIOMETERS OUT OF RANGE DURING RI
- [SDR VNAA2014103100014](https://openairdocs.org/sdr/VNAA2014103100014.md): Seat Track · corroded · Oct 31, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK NR 5 HAS CORROSION AT BS 536. REPLACED DAMAGED SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR VNAA2014102700013](https://openairdocs.org/sdr/VNAA2014102700013.md): Seat Track · corroded · Oct 27, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK NR 6 HAS CORROSION BS 559+39 AND 559+56. REMOVED AND REPLACED IAW AMM 53-01-11-400-802.
- [SDR VNAA2014102700012](https://openairdocs.org/sdr/VNAA2014102700012.md): Stiffener · cracked · Oct 27, 2014 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128, LBL 18 VERTICAL POST AND OTBD SIDES HAVE INDICATION NOTED IN AFT RADIUS AT WL 69 FAILED NDT INSPECTION. REPLACED IAW 51-40-11& 51-42-06.
- [SDR VNAA2014102700011](https://openairdocs.org/sdr/VNAA2014102700011.md): Stringer · cracked · Oct 27, 2014 · N216PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > BS 379 STRINGER 3L IS CRACKED. REPAIRED THE STRINGER IAW REO601R-53-21-2574 AND SRM 53-00-03.
- [SDR VNAA2014101500010](https://openairdocs.org/sdr/VNAA2014101500010.md): Seat Track · corroded · Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK NR 6 HAS CORROSION BETWEEN BS 559+48 AND BS 559.80. R & R THE SEAT TRACK IAW AMM.
- [SDR VNAA2014101500009](https://openairdocs.org/sdr/VNAA2014101500009.md): Seat Track · corroded · Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK NR 4 HAS CORROSION BETWEEN BS 449+85 AND FS 484. R & R THE SEAT TRACK IAW AMM.
- [SDR VNAA2014101500008](https://openairdocs.org/sdr/VNAA2014101500008.md): Floor Support · corroded · Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT HAS CORROSION BETWEEN BS 349 - 364. REPAIRED THE FLOOR SUPPORT IAW SRM 51-21-06.
- [SDR VNAA2014101500007](https://openairdocs.org/sdr/VNAA2014101500007.md): Seat Track · corroded · Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK NR 3 CORRODED BETWEEN BS 409+112 AND 449.85. INSTALLED NEW SEAT TRACK IAW AMM.
- [SDR VNAA2014101500006](https://openairdocs.org/sdr/VNAA2014101500006.md): Plate · corroded · Oct 15, 2014 · N216PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING SERRATED PLATE IS CORRODED. R & R SERRATED PLATE IAW SRM 51-41-02.
- [SDR VNAA2014093000015](https://openairdocs.org/sdr/VNAA2014093000015.md): Ejector · malfunctioned · Sep 30, 2014 · N216PS · Cndair CL6002B19 · Cabin Pressure Control System
  > AT 33,000 FT, CREW REPORTED DELTA-P OF 8.7 AND RISING IN RED. CREW INITIATED EMERGENCY DESCENT. DURING DESCENT, PRESSURE STABILIZED AT CABIN 300 TO 800 FT CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R JET PUMP EJECTOR AND PERFO
- [SDR VNAA2014040300002](https://openairdocs.org/sdr/VNAA2014040300002.md): Fire Bottle · discharged · Apr 3, 2014 · N216PS · Cndair CL6002B19 · Fire Bottle, Fixed
  > CREW REPORTED CARGO BOTTLE LOW AMBER MESSAGE. CREW COMPLETED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT CARGO FIRE BOTTLE A3HL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013110600004](https://openairdocs.org/sdr/VNAA2013110600004.md): Position Sensor · failed · Nov 6, 2013 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL MESSAGE AT ZERO DEGREES DURING EXTENSION ON DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT FLAP SYS IAW FAULT ISOLATION MANUAL. MX R & R RT BPSU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013082300015](https://openairdocs.org/sdr/VNAA2013082300015.md): Ground Stud · loose · Aug 23, 2013 · N216PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED A THE GALLEY EMERGENCY LIGHT DID NOT WORK. MX TROUBLESHOT, AND TIGHTENED THE GROUND STUD IAW AMM. CHECKS WERE PERFOMED IAW THE AMM AND ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013041000004](https://openairdocs.org/sdr/VNAA2013041000004.md): Engine · malfunctioned · Apr 10, 2013 · N216PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CREW REPORTED HIGH ITT ON LEFT ENGINE WHEN THROTTLES ADVANCED AND BRAKES RELEASED FOR TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND DETERMINED LEFT ENGINE REQUIRES REMOVAL AND REPLACEMENT. SUPPLEMENTAL INFORMATION WILL BE PRO
- [SDR VNAA2013022400015](https://openairdocs.org/sdr/VNAA2013022400015.md): Fastener · loose · Feb 24, 2013 · N216PS · Cndair CL6002B19 · Flight Compartment Lighting
  > CREW REPORTED CAPTAIN’S YOKE MAP LIGHT COMES ON EVEN THOUGH LIGHTS ARE TURNED OFF AND SHOCKED CAPTAIN TWICE. MAINTENANCE INSPECTED, RE-SECURED LOOSE HARDWARE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2012110500003](https://openairdocs.org/sdr/VNAA2012110500003.md): Windshield · cracked · Nov 5, 2012 · N216PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED RIGHT WINDSHIELD CRACKED IN FLIGHT AT FL 340. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT WINDSHIELD AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVIC
- [SDR VNAA2012070300006](https://openairdocs.org/sdr/VNAA2012070300006.md): Light · inoperative · Jul 3, 2012 · N216PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED OVERHEAD EMERGENCY LIGHT (CEILING) OUTSIDE LAV DOES NOT ILLUMINATE. MAINTENANCE INSPECTED, RELAMPED AFT OVERHEAD EMERGENCY CEILING FLOOD LIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N216PS-2022-12-31/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 = 'N216PS' AND deregistration_id = 'N216PS-2022-12-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N216PS-2022-12-31/reports

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