N216PS, cancelled Dec 31, 2022

Service difficulty reports · 85

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2018100999906Bulkhead · crackedFS 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.Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018100999905Bulkhead · crackedFS 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.Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018100999904Bulkhead · crackedFS 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 Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018100999903Bulkhead · crackedFS 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 AOct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018100999902Bulkhead · crackedFS 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 FOct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018100999901Door Sill · corrodedRT 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.Oct 9, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018100599904Fitting · crackedPRESSURE 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.Oct 5, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018100599903Fitting · crackedPRESSURE 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 2009-09-16Oct 5, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018100599902Structure · crackedPAX DOOR ASSIST MOTOR LOWER "2" MEMBER IS CRACKED. C/A: 1. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-13.Oct 5, 2018 · N216PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2018100599901Intercostal · cracked621-625 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.Oct 5, 2018 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018081321101Lever · malfunctionedFLAP 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.Aug 12, 2018 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2018053111101Bpsu · out of rigDURING 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. THISMay 31, 2018 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2018021611101Warning Message · activatedTHE CREW RECEIVED A FLAPS FAIL MESSAGE AT 20 DEGREES. THE CREW RAN THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. OPEN.Feb 16, 2018 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2017040500004Unknown · smokeSMOKE IN LAVATORY, AN EMERGENCY WAS DECLARED.Apr 5, 2017 · N216PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2017032300014Unknown · smokeSMOKE IN LAVATORY AFTER TAKEOFF.Mar 23, 2017 · N216PS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2017031900010Smoke Warning · activatedSMOKE IN TOILET CAUTION MESSAGE.Mar 19, 2017 · N216PS · Cndair CL6002B19 · Smoke DetectionSDR VNAA2017013100042Coalescer Bag · saturatedAFTER 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.Jan 31, 2017 · N216PS · Cndair CL6002B19 · Humidity Control SystemSDR VNAA2016122000037Yaw Damper · malfunctionedUNCOMMANDED 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.Dec 20, 2016 · N216PS · Cndair CL6002B19 · Auto Flight SystemSDR VNAA2016100600008Control Unit · malfunctionedFLAPS 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.Oct 6, 2016 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2016092500043Skin Panel · crackedNOSE 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.Sep 25, 2016 · N216PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2016081600023Skin · damagedDURING 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.Aug 16, 2016 · N216PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2016081600022Panel · missingDURING POST FLIGHT INSPECTION, CREW FOUND THE UPPER ACCESS COWL MISSING. MAINTENANCE INSPECTED, REPLACED THE UPPER ACCESS COWL AND PERFORMED CHECKS IAW THE AMM.Aug 16, 2016 · N216PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2016080500004Battery Pack · inoperativeOVERHEAD EMERGENCY EXIT LIGHT OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, REPLACED THE LAMP IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 5, 2016 · N216PS · Cndair CL6002B19 · Emergency LightingSDR VNAA2016050800006Smoke Detector · faultySMOKE 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.May 8, 2016 · N216PS · Cndair CL6002B19 · Smoke DetectionSDR VNAA2016042000020Position Sensor · failedFLAPS 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 FORApr 20, 2016 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2016041400016Position Sensor · out of adjustFLAPS 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 RApr 14, 2016 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2016022400031Sensor · failedCREW 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.Feb 24, 2016 · N216PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2016022300030Warning Message · false activationCREW 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.Feb 23, 2016 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2016021500019Pitot Tube · contaminatedCREW 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. MAINTFeb 15, 2016 · N216PS · Cndair CL6002B19 · Pitot/Static SystemSDR VNAA2016021300015Heater · malfunctionedCREW 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.Feb 13, 2016 · N216PS · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR VNAA2015080700010Wire Harness · shortedCREW 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.Aug 7, 2015 · N216PS · Cndair CL6002B19 · Landing Gear System WiringSDR VNAA2015072300028Tire · failedRIGHT 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 Jul 23, 2015 · N216PS · Cndair CL6002B19 · TireSDR VNAA2015071200011Control Unit · out of adjustCREW 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 RIJul 12, 2015 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2014103100014Seat Track · corrodedRT SIDE SEAT TRACK NR 5 HAS CORROSION AT BS 536. REPLACED DAMAGED SEAT TRACK IAW AMM 53-01-11-400-802.Oct 31, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014102700013Seat Track · corrodedRIGHT SIDE SEAT TRACK NR 6 HAS CORROSION BS 559+39 AND 559+56. REMOVED AND REPLACED IAW AMM 53-01-11-400-802.Oct 27, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014102700012Stiffener · crackedBS 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.Oct 27, 2014 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2014102700011Stringer · crackedBS 379 STRINGER 3L IS CRACKED. REPAIRED THE STRINGER IAW REO601R-53-21-2574 AND SRM 53-00-03.Oct 27, 2014 · N216PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR VNAA2014101500010Seat Track · corrodedLT SEAT TRACK NR 6 HAS CORROSION BETWEEN BS 559+48 AND BS 559.80. R & R THE SEAT TRACK IAW AMM.Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014101500009Seat Track · corrodedLEFT SIDE SEAT TRACK NR 4 HAS CORROSION BETWEEN BS 449+85 AND FS 484. R & R THE SEAT TRACK IAW AMM.Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014101500008Floor Support · corrodedLEFT FLOOR SUPPORT HAS CORROSION BETWEEN BS 349 - 364. REPAIRED THE FLOOR SUPPORT IAW SRM 51-21-06.Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2014101500007Seat Track · corrodedRIGHT SIDE SEAT TRACK NR 3 CORRODED BETWEEN BS 409+112 AND 449.85. INSTALLED NEW SEAT TRACK IAW AMM.Oct 15, 2014 · N216PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2014101500006Plate · corrodedPAX DOOR AFT ANCHOR FITTING SERRATED PLATE IS CORRODED. R & R SERRATED PLATE IAW SRM 51-41-02.Oct 15, 2014 · N216PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA2014093000015Ejector · malfunctionedAT 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 PERFOSep 30, 2014 · N216PS · Cndair CL6002B19 · Cabin Pressure Control SystemSDR VNAA2014040300002Fire Bottle · dischargedCREW 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.Apr 3, 2014 · N216PS · Cndair CL6002B19 · Fire Bottle, FixedSDR VNAA2013110600004Position Sensor · failedCREW 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.Nov 6, 2013 · N216PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2013082300015Ground Stud · looseCREW 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.Aug 23, 2013 · N216PS · Cndair CL6002B19 · Light System WiringSDR VNAA2013041000004Engine · malfunctionedCREW 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 PROApr 10, 2013 · N216PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2013022400015Fastener · looseCREW 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.Feb 24, 2013 · N216PS · Cndair CL6002B19 · Flight Compartment LightingSDR VNAA2012110500003Windshield · crackedCREW 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 SERVICNov 5, 2012 · N216PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2012070300006Light · inoperativeCREW 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.Jul 3, 2012 · N216PS · Cndair CL6002B19 · Emergency Lighting
Back to N216PS, cancelled Dec 31, 2022