# N216PS: 2003 Bombardier CL-600-2B19, registration cancelled 2022-12-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 31, 2022
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7882
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 18, 2003
- Certificate issued: September 3, 2019
- Last registry action: September 3, 2019
- Mode S code: A1D122
- Owner when cancelled: [Psa Airlines Inc](https://openairdocs.org/faa-owner/PSA%20AIRLINES%20INC)
- Location: [Vandalia, OH](https://openairdocs.org/faa-place/OH/Vandalia)
- Owner type: Corporation
- Owner's area on the map: 39.9040° N, 84.2181° W: Placed by OpenAirDocs at the center of ZIP code 45377, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N216PS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=216PS
- Page: https://openairdocs.org/deregistered/N216PS-2022-12-31

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (85, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR VNAA2018100999906](https://openairdocs.org/sdr/VNAA2018100999906), Oct 9, 2018: BULKHEAD. CRACKED. 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 
- [SDR VNAA2018100999905](https://openairdocs.org/sdr/VNAA2018100999905), Oct 9, 2018: BULKHEAD. CRACKED. 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 R
- [SDR VNAA2018100999904](https://openairdocs.org/sdr/VNAA2018100999904), Oct 9, 2018: BULKHEAD. CRACKED. 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. B
- [SDR VNAA2018100999903](https://openairdocs.org/sdr/VNAA2018100999903), Oct 9, 2018: BULKHEAD. CRACKED. 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 M
- [SDR VNAA2018100999902](https://openairdocs.org/sdr/VNAA2018100999902), Oct 9, 2018: BULKHEAD. CRACKED. 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 DO
- [SDR VNAA2018100999901](https://openairdocs.org/sdr/VNAA2018100999901), Oct 9, 2018: DOOR SILL. CORRODED. 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), Oct 5, 2018: FITTING. CRACKED. 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 
- [SDR VNAA2018100599903](https://openairdocs.org/sdr/VNAA2018100599903), Oct 5, 2018: FITTING. CRACKED. 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 CO
- [SDR VNAA2018100599902](https://openairdocs.org/sdr/VNAA2018100599902), Oct 5, 2018: STRUCTURE. CRACKED. 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), Oct 5, 2018: INTERCOSTAL. CRACKED. 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. WVAC704
- [SDR VNAA2018081321101](https://openairdocs.org/sdr/VNAA2018081321101), Aug 12, 2018: LEVER. MALFUNCTIONED. 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. 
- [SDR VNAA2018053111101](https://openairdocs.org/sdr/VNAA2018053111101), May 31, 2018: BPSU. OUT OF RIG. 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 INCID
- [SDR VNAA2018021611101](https://openairdocs.org/sdr/VNAA2018021611101), Feb 16, 2018: WARNING MESSAGE. ACTIVATED. 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), Apr 5, 2017: UNKNOWN. SMOKE. SMOKE IN LAVATORY, AN EMERGENCY WAS DECLARED.
- [SDR VNAA2017032300014](https://openairdocs.org/sdr/VNAA2017032300014), Mar 23, 2017: UNKNOWN. SMOKE. SMOKE IN LAVATORY AFTER TAKEOFF.
- [SDR VNAA2017031900010](https://openairdocs.org/sdr/VNAA2017031900010), Mar 19, 2017: SMOKE WARNING. ACTIVATED. SMOKE IN TOILET CAUTION MESSAGE.
- [SDR VNAA2017013100042](https://openairdocs.org/sdr/VNAA2017013100042), Jan 31, 2017: COALESCER BAG. SATURATED. 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 
- [SDR VNAA2016122000037](https://openairdocs.org/sdr/VNAA2016122000037), Dec 20, 2016: YAW DAMPER. MALFUNCTIONED. 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
- [SDR VNAA2016100600008](https://openairdocs.org/sdr/VNAA2016100600008), Oct 6, 2016: CONTROL UNIT. MALFUNCTIONED. FLAPS FAILED AT 20 DEGREES WHEN SELECTING FLAPS 30 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLAP ELECTR
- [SDR VNAA2016092500043](https://openairdocs.org/sdr/VNAA2016092500043), Sep 25, 2016: SKIN PANEL. CRACKED. 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
- [SDR VNAA2016081600023](https://openairdocs.org/sdr/VNAA2016081600023), Aug 16, 2016: SKIN. DAMAGED. DURING POST FLIGHT INSPECTION, CREW FOUND THE LOWER ACCESS COWL MISSING. MAINTENANCE INSPECTED, REPLACED THE LOWER ACCESS COWL AND PERFORMED CHECKS IAW THE AMM.
- [SDR VNAA2016081600022](https://openairdocs.org/sdr/VNAA2016081600022), Aug 16, 2016: PANEL. MISSING. 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), Aug 5, 2016: BATTERY PACK. INOPERATIVE. 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), May 8, 2016: SMOKE DETECTOR. FAULTY. SMOKE TOILET CAUTION MESSAGE ON DEPARTURE. THE CREW DECLARED AN EMERGENCY, RETURNED TO FIELD, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R THE LAVA
- [SDR VNAA2016042000020](https://openairdocs.org/sdr/VNAA2016042000020), Apr 20, 2016: POSITION SENSOR. FAILED. FLAPS FAIL CAUTION AND FLAPS FAIL ON FINAL APPROACH. THE CREW DECLARED AND EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R 
- [SDR VNAA2016041400016](https://openairdocs.org/sdr/VNAA2016041400016), Apr 14, 2016: POSITION SENSOR. OUT OF ADJUST. FLAPS FAIL "C" MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS IAW THE AMM
- [SDR VNAA2016022400031](https://openairdocs.org/sdr/VNAA2016022400031), Feb 24, 2016: SENSOR. FAILED. CREW REPORTED FLAPS FAIL CAUTION ON APPROACH. THE CREW LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE TROUBLESHOT, R & R THE LT BRAKE AND POSITION SENSOR UNIT. M
- [SDR VNAA2016022300030](https://openairdocs.org/sdr/VNAA2016022300030), Feb 23, 2016: WARNING MESSAGE. FALSE ACTIVATION. CREW REPORTED RECEIVING A TAT CAUTION MESSAGE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED, RECYCLED CI
- [SDR VNAA2016021500019](https://openairdocs.org/sdr/VNAA2016021500019), Feb 15, 2016: PITOT TUBE. CONTAMINATED. 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 DECLA
- [SDR VNAA2016021300015](https://openairdocs.org/sdr/VNAA2016021300015), Feb 13, 2016: HEATER. MALFUNCTIONED. 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 REL
- [SDR VNAA2015080700010](https://openairdocs.org/sdr/VNAA2015080700010), Aug 7, 2015: WIRE HARNESS. SHORTED. CREW REPORTED GEAR WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT OTBD MLG HARNESS AND PERFORMED CHECK
- [SDR VNAA2015072300028](https://openairdocs.org/sdr/VNAA2015072300028), Jul 23, 2015: TIRE. FAILED. 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 F
- [SDR VNAA2015071200011](https://openairdocs.org/sdr/VNAA2015071200011), Jul 12, 2015: CONTROL UNIT. OUT OF ADJUST. 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
- [SDR VNAA2014103100014](https://openairdocs.org/sdr/VNAA2014103100014), Oct 31, 2014: SEAT TRACK. CORRODED. 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), Oct 27, 2014: SEAT TRACK. CORRODED. 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), Oct 27, 2014: STIFFENER. CRACKED. 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), Oct 27, 2014: STRINGER. CRACKED. 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), Oct 15, 2014: SEAT TRACK. CORRODED. 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), Oct 15, 2014: SEAT TRACK. CORRODED. 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), Oct 15, 2014: FLOOR SUPPORT. CORRODED. 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), Oct 15, 2014: SEAT TRACK. CORRODED. 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), Oct 15, 2014: PLATE. CORRODED. 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), Sep 30, 2014: EJECTOR. MALFUNCTIONED. 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 
- [SDR VNAA2014040300002](https://openairdocs.org/sdr/VNAA2014040300002), Apr 3, 2014: FIRE BOTTLE. DISCHARGED. CREW REPORTED CARGO BOTTLE LOW AMBER MESSAGE. CREW COMPLETED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT CARGO FIRE BOTTLE A3HL A
- [SDR VNAA2013110600004](https://openairdocs.org/sdr/VNAA2013110600004), Nov 6, 2013: POSITION SENSOR. FAILED. CREW REPORTED FLAPS FAIL MESSAGE AT ZERO DEGREES DURING EXTENSION ON DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT FLAP SYS IA
- [SDR VNAA2013082300015](https://openairdocs.org/sdr/VNAA2013082300015), Aug 23, 2013: GROUND STUD. LOOSE. 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 RE
- [SDR VNAA2013041000004](https://openairdocs.org/sdr/VNAA2013041000004), Apr 10, 2013: ENGINE. MALFUNCTIONED. CREW REPORTED HIGH ITT ON LEFT ENGINE WHEN THROTTLES ADVANCED AND BRAKES RELEASED FOR TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED 
- [SDR VNAA2013022400015](https://openairdocs.org/sdr/VNAA2013022400015), Feb 24, 2013: FASTENER. LOOSE. 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 AN
- [SDR VNAA2012110500003](https://openairdocs.org/sdr/VNAA2012110500003), Nov 5, 2012: WINDSHIELD. CRACKED. CREW REPORTED RIGHT WINDSHIELD CRACKED IN FLIGHT AT FL 340. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT
- [SDR VNAA2012070300006](https://openairdocs.org/sdr/VNAA2012070300006), Jul 3, 2012: LIGHT. INOPERATIVE. CREW REPORTED OVERHEAD EMERGENCY LIGHT (CEILING) OUTSIDE LAV DOES NOT ILLUMINATE. MAINTENANCE INSPECTED, RELAMPED AFT OVERHEAD EMERGENCY CEILING FLOOD LIGHT AND

All 85: https://openairdocs.org/deregistered/N216PS-2022-12-31/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20160816014519I](https://openairdocs.org/incident/20160816014519I), Aug 16, 2016: Bombardier Inc CL-600-2B19 (N216PS), Dayton, OH, Minor damage. On 08/16/2016 psa flight 5517, aircraft N216PS, phl-day, reported a birdstrike to the nose of the aircraft and the LH engine on approach into day. The aircraft…

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