# N5736J: 1980 Bell 212, registration cancelled 2019-11-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 4, 2019 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Bell 212](https://openairdocs.org/model/bell-212) (registry code 1181420) - Engine: [Pratt & Whitney PT6T-3B](https://openairdocs.org/engine/pratt-whitney-pt6t-3b) (registry code 51522) - Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW), [TCDS E22EA](https://openairdocs.org/tcds/E22EA) (OpenAirDocs) - Serial number: 31140 - Year built: 1980 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: August 22, 2006 - Certificate issued: September 5, 2019 - Last registry action: September 5, 2019 - Mode S code: A75CC1 - Owner when cancelled: [Phi Aviation LLC](https://openairdocs.org/faa-owner/PHI%20AVIATION%20LLC) - Location: [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette) - Owner type: LLC - Owner's area on the map: 30.1552° N, 92.0282° W: Placed by OpenAirDocs at the center of ZIP code 70508, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N5736J - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5736J - Page: https://openairdocs.org/deregistered/N5736J-2019-11-04 From the FAA registry file of November 5, 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 Bell 212: https://openairdocs.org/model/bell-212.md ## Service difficulty reports (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HEEA107314](https://openairdocs.org/sdr/HEEA107314), Nov 9, 2005: PACKING. INOPERATIVE. ON CLIMB-OUT HEARD A LOUD WHINNING NOISE, HYDRAULIC CAUTION LIGHT CAME ON AND NR 1 HYDRAULIC PRESSURE WENT TO ZERO. STARTED EMERGENCY CHECK LIST AND NOISE STOPP - [SDR HEEA108771](https://openairdocs.org/sdr/HEEA108771), Dec 8, 2004: WINDOW. DEPARTED. LH CARGO DOOR FWD WINDOW DEPARTED IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE AND INSTALLED A NEW WINDOW. - [SDR HEEA086675](https://openairdocs.org/sdr/HEEA086675), May 22, 2003: HANGER ASSY. CORRODED. PITTING ON OUTPUT FLANGE. REPLACED 4 EACH CLAMPS 204-040-811-001 DUE TO CORROSION. REPAIRED. - [SDR HEEA086610](https://openairdocs.org/sdr/HEEA086610), May 21, 2003: BEARING. WORN. BELLCRANK ASSY HAS WORN BEARINGS. REPLACED BEARING DW-4 DUE TO WORN AND SLEEVE 120-015-4KA DUE TO WORN. REPAIRED. - [SDR HEEA086597](https://openairdocs.org/sdr/HEEA086597), May 21, 2003: BUSHING. WORN. GUIDE BUSHINGS WORN. REPLACED 2 EACH 204-001-036-001 GUIDES DUE TO WORN AND BEARING MS27643-4 DUE TO WORN. REPAIRED. - [SDR HEEA080114](https://openairdocs.org/sdr/HEEA080114), Jun 25, 2002: DIAPHRAGM. DAMAGED. INCREASE OF 75 DEGREES ITT AND 4.5 PERCENT N1 IN CRUISE FLIGHT. FOUND HOLE IN DIAPHRAGM. REPLACED. - [SDR HEEA080109](https://openairdocs.org/sdr/HEEA080109), Jun 25, 2002: QUILL. LEAKING. QUILL ASSY LEAKING. WORN SPACER P/N 212-040-156-001. REPLACED SPACER. - [SDR HEEA079740](https://openairdocs.org/sdr/HEEA079740), May 31, 2002: TRANSCEIVER. INOPERATIVE. VHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. REPLACED WITH SERVICEABLE PART. - [SDR HEEA079089](https://openairdocs.org/sdr/HEEA079089), May 16, 2002: TRANSCEIVER. INOPERATIVE. DME/TACAN TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. REPLACED WITH SERVICEABLE UNIT. - [SDR HEEA078542](https://openairdocs.org/sdr/HEEA078542), Apr 1, 2002: CROSSTUBE. FAILED. DURING PASSENGER LOADING (ENGINES SECURED) AFT CROSSTUBE FAILED ONE INCH OUTBOARD OF RIGHT HAND ATTACHMENT POINT (STRESS MARKS ON TUBE INDICATES FAILURE STARTED - [SDR HEEA076985](https://openairdocs.org/sdr/HEEA076985), Oct 31, 2001: INDICATOR. FAILED. UNIT READ ZERO. PENDING VENDOR REPAIR. - [SDR HEEA076294](https://openairdocs.org/sdr/HEEA076294), Oct 1, 2001: OIL COOLER. CONTAMINATED. METAL CONTAMINATION. - [SDR HEEA072618](https://openairdocs.org/sdr/HEEA072618), Apr 17, 2001: TRANSCEIVER. FAILED. ON INITIAL INSTALLATION UNIT WOULD NOT TRANSMIT DURING FUNCTIONAL TEST. FOUND MODULATION WEAK WHEN UNIT WAS COOL AND WOULD GO UP AS UNIT WARMED UP. REPLACED CR3 - [SDR HEEA065220](https://openairdocs.org/sdr/HEEA065220), Nov 17, 1999: INDICATOR. FAILED. TRIPLE TACHOMETER'S NR 2 NEEDLE WILL NOT MOVE. STAYS ON ZERO. - [SDR HEEA065209](https://openairdocs.org/sdr/HEEA065209), Nov 17, 1999: WARNING BOX. FAILED. ENGINE OUT LIGHTS AND HORN BLINK INTERMITTENTLY. - [SDR HEEA065195](https://openairdocs.org/sdr/HEEA065195), Nov 17, 1999: INVERTER. INTERMITTENT. INVERTER HAD INTERMITTENT OPERATIONS. - [SDR HEEA063377](https://openairdocs.org/sdr/HEEA063377), Aug 13, 1999: TRIM COMPENSATOR. OUT OF ADJUST. TRIM COMPENSATOR OUT OF ADJUSTMENT. (INCREASE). - [SDR HEEA0016416](https://openairdocs.org/sdr/HEEA0016416), Oct 23, 1998: CONTROL UNIT. FAILED. TORQUE CONTROL UNIT CAUSES TORQUE OSCILLATION ON NR 2 ENGINE. - [SDR HEEA0016413](https://openairdocs.org/sdr/HEEA0016413), Oct 23, 1998: FLUX VALVE. INOPERATIVE. COMPASS IS INOPERATIVE, IT HAS ERRATIC OUTPUT. - [SDR HEEA0016406](https://openairdocs.org/sdr/HEEA0016406), Oct 23, 1998: INDICATOR. STICKING. N1 NEEDLE ERRATIC AND STICKS. - [SDR HEEA0016404](https://openairdocs.org/sdr/HEEA0016404), Oct 23, 1998: DETECTOR. MALFUNCTIONED. RPM INDICATOR ACTIVATES ALARM AT RANDOM. - [SDR HEEA0016402](https://openairdocs.org/sdr/HEEA0016402), Oct 23, 1998: DUAL AMMETER. STICKING. DUAL AMMETER NEEDLE STICKING. - [SDR HEEA0016401](https://openairdocs.org/sdr/HEEA0016401), Oct 23, 1998: INDICATOR. MALFUNCTIONED. ENGINE OIL TEMPERATURE STAYS AT ZERO. - [SDR HEEA0015896](https://openairdocs.org/sdr/HEEA0015896), Aug 27, 1998: TRANSPONDER. FAILED. TRANSPONDER A/C CODE STAYS AT 0000. - [SDR HEEA0015822](https://openairdocs.org/sdr/HEEA0015822), Aug 27, 1998: ELT. MALFUNCTIONED. ELT ACTIVATES IN ARMED POSITION. - [SDR HEEA0015731](https://openairdocs.org/sdr/HEEA0015731), Aug 20, 1998: INDICATOR. INACCURATE. RATE-OF CLIMB INDICATOR NEEDLE IS OFF. - [SDR HEEA0015520](https://openairdocs.org/sdr/HEEA0015520), Aug 13, 1998: INDICATOR. ERRATIC. TRIPLE TACHOMETER , ALL NEEDLES HAVE ERRATIC MOVEMENT. - [SDR HEEA0015145](https://openairdocs.org/sdr/HEEA0015145), Jul 1, 1998: PROBE. FAILED. FUEL SYSTEM PROBE DID NOT PASS CAPACITANCE TEST. - [SDR HEEA0014789](https://openairdocs.org/sdr/HEEA0014789), Jun 17, 1998: TUBE. MISMANUFACTURED. TUBE IS PART OF COLLECTIVE SYSTEM. MUST BE DRILLED IN A FIXTURE. THIS NEW TUBE HAS NO HOLES. - [SDR HEEA0014777](https://openairdocs.org/sdr/HEEA0014777), Jun 11, 1998: SHAFT. CORRODED. TRANSMISSION SHAFT IS CORRODED AND FRETTED ON MOUNTING SURFACE. - [SDR HEEA0014694](https://openairdocs.org/sdr/HEEA0014694), Jun 10, 1998: OIL COOLER. LEAKING. OIL COOLER LEAKING IN FIN AREA. - [SDR HEEA0014659](https://openairdocs.org/sdr/HEEA0014659), Jun 8, 1998: ENCODER. OUT OF TOLERANCE. ENCODER NEEDLE STICKS AND ENCODER READS OUT OF TOLERANCE. - [SDR HEEA0014608](https://openairdocs.org/sdr/HEEA0014608), Jun 5, 1998: BAFFLE. UNBONDED. FUEL CELL UNBONDED IN BAFFLE. - [SDR HEEA0014058](https://openairdocs.org/sdr/HEEA0014058), Apr 29, 1998: RECEIVER. FAILED. ADF RECEIVER WEAK RECEIVE AND NOT POINTING CORRECTLY IN ADF MODE. INSPECTED AND FOUND ADF MODE SIGNAL WEAK AND NOT POINTING. TRIED ALIGNING RECEIVER. NO HELP. - [SDR HEEA0013949](https://openairdocs.org/sdr/HEEA0013949), Apr 16, 1998: TRANSCEIVER. FAILED. TRANSCEIVER DISPLAY 50,250,400 AND 1200 LED'S GO OUT. - [SDR HEEA0013690](https://openairdocs.org/sdr/HEEA0013690), Apr 2, 1998: INDICATOR. FAILED. ITT INDICATOR DOES NOT WORK. - [SDR HEEA0013636](https://openairdocs.org/sdr/HEEA0013636), Mar 26, 1998: INDICATOR. FAILED. ATTITUDE INDICATOR LEFT KNOB WILL NOT ADJUST. - [SDR HEEA0013597](https://openairdocs.org/sdr/HEEA0013597), Mar 26, 1998: INVERTER. FAILED. INVERTER INOPERATIVE. - [SDR HEEA0013490](https://openairdocs.org/sdr/HEEA0013490), Mar 19, 1998: COMPENSATOR. FAILED. COMPENSATOR WILL NOT ADJUST. - [SDR HEEA0013484](https://openairdocs.org/sdr/HEEA0013484), Mar 19, 1998: TRANSMITTER. ERRATIC. FLUX VALVE HAS ERRATIC READINGS. - [SDR HEEA0012228](https://openairdocs.org/sdr/HEEA0012228), Dec 3, 1997: TRIM COMPENSATOR. DEFECTIVE. TRIM COMPENSATOR FLUCTUATING ITT INDICATION. - [SDR HEEA0011983](https://openairdocs.org/sdr/HEEA0011983), Nov 13, 1997: CVR. FAILED. CVR WILL NOT TEST. ALSO REMOVED PINGER P/N DK100, S/N DL8982 WITH CVR. REPLACEMENT PINGER S/N S9081 RECEIVED WITH CVR. - [SDR HEEA0011680](https://openairdocs.org/sdr/HEEA0011680), Oct 22, 1997: TRANSMITTER. ERRATIC. ENGINE OIL TRANSMITTER TRANSMITS ERRATIC. - [SDR HEEA0011289](https://openairdocs.org/sdr/HEEA0011289), Oct 8, 1997: INDICATOR. STICKS. NR2 NEEDLE STICKS THROUGHOUT SCALE. - [SDR HEEA0010834](https://openairdocs.org/sdr/HEEA0010834), Aug 21, 1997: TRANSCEIVER. MALFUNCTION. TRANSCEIVER UNIT HAS POPPING NOISE AT -101DB. TWO EACH FLEX CABLES MISSING ON SERIAL LOGIC ASSY. PIN ON CONNECTOR GOING TO J9055 IS BROKEN. - [SDR HEEA0010450](https://openairdocs.org/sdr/HEEA0010450), Jul 10, 1997: TARSYN. DEFECTIVE. TARSYN DEFECTIVE ADI PRECESSES IN ROLL. - [SDR HEEA0010446](https://openairdocs.org/sdr/HEEA0010446), Jul 10, 1997: MOTOR. WORN SHAFT. MOTOR AND CONVERTER HAS WORN SHAFT. - [SDR HAIHEEA9828](https://openairdocs.org/sdr/HAIHEEA9828), May 7, 1997: TRANSCEIVER. DEFECTIVE. TRANSCEIVER WON'T KEY UP. - [SDR HEEA968467](https://openairdocs.org/sdr/HEEA968467), Nov 6, 1996: BLADE. DEFECTIVE. TOO LIGHT TO BALANCE. BLADE BOLT HOLE WAS MAX. OUT, STILL WITH NO SUCCESS. - [SDR HEEA968377](https://openairdocs.org/sdr/HEEA968377), Oct 15, 1996: INDICATOR. METER INOP. GLIDE SCOPE METER INOPERATIVE. All 68: https://openairdocs.org/deregistered/N5736J-2019-11-04/reports.md ## FAA accident and incident reports (3) 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 20000318018669I](https://openairdocs.org/incident/20000318018669I), Mar 18, 2000: Bell 212 (N5736J), Cabine, AO. (-23)During takeoff, pilot attempted to move the collective up but it would not move. A second try was made, but the collective would not move. Mechanics fund… - [Incident 19950804034729I](https://openairdocs.org/incident/19950804034729I), Aug 4, 1995: Bell 212 (N5736J), Venice, LA. Torque split at cruise over gulf. Returned to Venice. Low side governor failure. Replaced unit. - [Incident 19801124086759I](https://openairdocs.org/incident/19801124086759I), Nov 24, 1980: Bell 212 (N5736J), LA, Minor damage. Tail rotor contacted guy cable while positioning for landing on rig. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.