# N22608: Bell 412, registration cancelled 2011-09-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 12, 2011 - Status when cancelled: Valid registration - Airframe: [Bell 412](https://openairdocs.org/model/bell-412) (registry code 1182202) - Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW) (OpenAirDocs) - Serial number: 33075 - Type of aircraft: Rotorcraft - Certificate issued: December 21, 2007 - Last registry action: May 19, 2010 - Mode S code: A1F9C4 - Owner when cancelled: [Ep Aviation LLC](https://openairdocs.org/faa-owner/EP%20AVIATION%20LLC) - Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale) - Owner type: Corporation - Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N22608 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=22608 - Page: https://openairdocs.org/deregistered/N22608-2011-09-12 From the FAA registry file of October 29, 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 412: https://openairdocs.org/model/bell-412.md ## Service difficulty reports (151, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P4YA2009051500001](https://openairdocs.org/sdr/P4YA2009051500001), May 15, 2009: ANGLE. CRACKED. DURING THE DAILY INSP IT WAS NOTED THAT THE UPPER LT CAP ANGLE HAS A CRACK IN THE VERTICAL LEG AT THE FWD END OF THE TAILBOOM ATTACH FITTING PN 212-030-159-001. - [SDR HEEA088501](https://openairdocs.org/sdr/HEEA088501), Jul 11, 2003: BATTERY. WILL NOT TEST. MASTER BATTERY WON'T TEST PROPERLY. - [SDR HEEA087981](https://openairdocs.org/sdr/HEEA087981), Jul 1, 2003: STARTER GEN. FAILED. STARTER GEN WILL NOT TURN OVER. SHOP REPAIR. - [SDR HEEA087808](https://openairdocs.org/sdr/HEEA087808), Jun 8, 2003: BLADE. SEPARATED. UPPER TRAILING EDGE FRETTING PAD IS SEPARATED. SENT FOR INSPECTION AND REPAIR. - [SDR HEEA088063](https://openairdocs.org/sdr/HEEA088063), Jun 8, 2003: BLADE. CRACKED. MAIN ROTOR BLADE FRETTING PAD ON THE LOWER SIDE HAS SOME SEPERATION. FIBERGLASS CRACKED NEAR THE INBOARD TRIM TAB. - [SDR HEEA0029439](https://openairdocs.org/sdr/HEEA0029439), May 21, 2003: VALVE. INOPERATIVE. PLATE LOOSE. REPLACED WITH SERVICEABLE PART. - [SDR HEEA084641](https://openairdocs.org/sdr/HEEA084641), Feb 14, 2003: TRANSPONDER. INOPERATIVE. TRANSPONDER WILL NOT COME ON. LOWER CHASSIS CORRODED. CLEANED CORROSION FROM UNIT. REPLACED Q104, Q501, Q502 TRANSISTORS, REPLACED 3 EACH WASHERS AND 3 EACH INS - [SDR HEEA084629](https://openairdocs.org/sdr/HEEA084629), Feb 14, 2003: TRANSCEIVER. NOISY. ADF TRANSCEIVER HAS CONTINUOUS NOISE IN BACKGROUND. REPAIRED. - [SDR HEEA084628](https://openairdocs.org/sdr/HEEA084628), Feb 14, 2003: TRANSCEIVER. WEAK. ADF TRANSCEIVER WEAK AND UNRELIABLE. REPAIRED. - [SDR HEEA084612](https://openairdocs.org/sdr/HEEA084612), Feb 14, 2003: TRANSCEIVER. INOPERATIVE. TRANSCEIVER INOPERATIVE. REPLACED BAD I309 IC CHIP. REPAIRED. ADJUSTED C/N SQUELCH, CARRIER SQUELCH, MIC GAIN, TRANSMIT COMPRESSOR AND SIDETONE. BENCH CHECK GOO - [SDR HEEA084610](https://openairdocs.org/sdr/HEEA084610), Feb 14, 2003: TRANSCEIVER. WEAK. TRANSCEIVER WEAK. REMOVED CORROSION FROM CHASSIS. ADJUSTED VCO VOLTAGE AND ALIGNED RECEIVER. REPAIRED WEAK RECEIVER. ADJUSTED MIC GAIN, TRANSMIT COMPRESSOR, POW - [SDR HEEA084555](https://openairdocs.org/sdr/HEEA084555), Feb 14, 2003: BLADE. CRACKED. MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS A CRACK NEAR THE SPLICE AREA. - [SDR HEEA084510](https://openairdocs.org/sdr/HEEA084510), Feb 14, 2003: ARM. STIFF. WINDSHIELD WIPER ARM STIFF, SPRING WILL NOT HOLD WIPER ON WINDOW. REPAIRED. - [SDR HEEA080629](https://openairdocs.org/sdr/HEEA080629), Jul 29, 2002: CONTROL BOX. FAILED. GENERATOR DROPS OFF LINE INTERMITTENTLY. - [SDR HEEA080595](https://openairdocs.org/sdr/HEEA080595), Jul 29, 2002: BEARING. WORN. MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. - [SDR HEEA080593](https://openairdocs.org/sdr/HEEA080593), Jul 29, 2002: BEARING. WORN. MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED. - [SDR HEEA080553](https://openairdocs.org/sdr/HEEA080553), Jul 29, 2002: BATTERY PACK. DISCHARGED. MAIN AIRCRAFT BATTERY PACK WEAK. REPAIRED. - [SDR HEEA080552](https://openairdocs.org/sdr/HEEA080552), Jul 29, 2002: BATTERY PACK. DISCHARGED. MAIN AIRCRAFT BATTERY PACK DEAD. REPAIRED. - [SDR HEEA080135](https://openairdocs.org/sdr/HEEA080135), Jun 26, 2002: TARSYN. MALFUNCTIONED. TARSYN 333 CAUSES YAW CHANNEL TO KICK. REPLACED WITH SERVICEABLE PART. - [SDR HEEA079669](https://openairdocs.org/sdr/HEEA079669), May 30, 2002: INDICATOR. READS LOW. TRIPLE TACH READS 3 PERCENT LOW. - [SDR HEEA079668](https://openairdocs.org/sdr/HEEA079668), May 30, 2002: INDICATOR. MALFUNCTIONED. TRIPLE TACH LIGHT INOPERATIVE. - [SDR HEEA079644](https://openairdocs.org/sdr/HEEA079644), May 30, 2002: COVER. TORN. EMERGENCY FLOAT BAG TORN. - [SDR HEEA079640](https://openairdocs.org/sdr/HEEA079640), May 30, 2002: COVER. WORN. EMERGENCY FLOAT COVER WORN. - [SDR HEEA079623](https://openairdocs.org/sdr/HEEA079623), May 30, 2002: FLOAT. LEAKING. EMERGENCY FLOAT BAG LEAKS. - [SDR HEEA079579](https://openairdocs.org/sdr/HEEA079579), May 30, 2002: GPS. FAILED. GPS LOST MEMORY. - [SDR HEEA079519](https://openairdocs.org/sdr/HEEA079519), May 28, 2002: FORCE GRADIENT. BINDING. CYCLIC FORCE GRADIENT IS BINDING AND HANGING UP. REPLACED WITH SERVICEABLE PART. - [SDR HEEA079436](https://openairdocs.org/sdr/HEEA079436), May 28, 2002: PUMP. MALFUNCTIONED. LT FUEL BOOST PUMP CAUSES NOISE IN ADF AUDIO. - [SDR HEEA079394](https://openairdocs.org/sdr/HEEA079394), May 28, 2002: LIGHT. MALFUNCTIONED. SEARCH LIGHT WILL NOT RETRACT. REPLACED WITH SERVICEABLE PART. - [SDR HEEA079237](https://openairdocs.org/sdr/HEEA079237), May 24, 2002: INDICATOR. FAILED. ATTITUDE INDICATOR WILL NOT TURN ON BOTH AXIS. - [SDR HEEA079214](https://openairdocs.org/sdr/HEEA079214), May 24, 2002: PLATE. LOOSE. PLATE LOOSE. REPLACED WITH SERVICEABLE PART. - [SDR HEEA079132](https://openairdocs.org/sdr/HEEA079132), May 22, 2002: INTERPHONE. MALFUNCTIONED. ADF SELECTOR SWITCH WILL NOT TURN IT'S AUDIO OFF (INTERMITTENTLY). FACEPLATE NEEDS REFURBISH. - [SDR HEEA079115](https://openairdocs.org/sdr/HEEA079115), May 21, 2002: CROSSTUBE. CORRODED. CROSSTUBE CORRODED BEYOND LIMITS IN SEVERAL AREAS. - [SDR HEEA076971](https://openairdocs.org/sdr/HEEA076971), Oct 30, 2001: VENT. LEAKING. HAD STRONG FUEL ODOR IN COCKPIT. FOUND A SMALL AMOUNT OF FUEL HAD SEEPED THROUGH THE RT EXTERNAL TANK VENT DUE TO HIGH FUEL LEVEL AND THE ATTITUDE OF THE AIRCRA - [SDR HEEA076820](https://openairdocs.org/sdr/HEEA076820), Oct 18, 2001: FUEL CONTROL. FLUCTUATES. AFTER DEPARTURE, NR 1 ENGINE STARTED TO HAVE N1 FLUCTUATIONS. REPLACED FUEL CONTROL. - [SDR HEEA072096](https://openairdocs.org/sdr/HEEA072096), Apr 5, 2001: EXHAUST STACK. CRACKED. EXHAUST STACK IS CRACKED AT SEAMS OF DUCT HALVES. REPLACED WITH SERVICEABLE PART. - [SDR HEEA065300](https://openairdocs.org/sdr/HEEA065300), Nov 29, 1999: ACTUATOR. SLOW. ACTUATOR MOVES VERY SLOW. TIME SINCE REPAIR 117:05 HOURS. - [SDR HEEA063246](https://openairdocs.org/sdr/HEEA063246), Aug 9, 1999: GPS. FAILED. RECEIVER FAILED. - [SDR HEEA063244](https://openairdocs.org/sdr/HEEA063244), Aug 9, 1999: TRANSCEIVER. MALFUNCTIONED. TRANSCEIVER TRANSMITS MUFFLED SIGNAL. TIME SINCE REPAIR 3:15 HOURS. - [SDR HEEA061711](https://openairdocs.org/sdr/HEEA061711), Apr 5, 1999: CONTROL UNIT. MALFUNCTIONED. SHOWS ONLY GENERATOR RESIDUAL VOLTAGE. WILL NOT EXCITE THE GENERATOR FIELD. CAUSES THE AIRCRAFT VOLTMETER TO BE DRIVEN DOWN BELOW ZERO WHEN THE GENERATOR SWITCH - [SDR HEEA060690](https://openairdocs.org/sdr/HEEA060690), Feb 22, 1999: RECEIVER. MALFUNCTIONED. TRANSCEIVER WILL NOT RECEIVE AND POINT TO STATION. - [SDR HEEA060687](https://openairdocs.org/sdr/HEEA060687), Feb 22, 1999: TRANSCEIVER. INTERMITTENT. TRANSCEIVER HAS INTERMITTENT OPERATION. - [SDR HEEA060686](https://openairdocs.org/sdr/HEEA060686), Feb 22, 1999: TRANSCEIVER. FAILED. TRANSCEIVER WILL NOT TRANSMIT O.D. RECEIVE. - [SDR HEEA060685](https://openairdocs.org/sdr/HEEA060685), Feb 22, 1999: TRANSCEIVER. WEAK. VERY WEAK AND FOUND WATER IN RADIO. - [SDR HEEA060645](https://openairdocs.org/sdr/HEEA060645), Feb 16, 1999: BEARING. WORN. LINK ASSEMBLY HAS WORN BEARING. REPLACED WITH SERVICEABLE BEARING. - [SDR HEEA060635](https://openairdocs.org/sdr/HEEA060635), Feb 16, 1999: BEARING. WORN. WORN BEARING. REPLACED WITH SERVICEABLE BEARING. - [SDR HEEA0016576](https://openairdocs.org/sdr/HEEA0016576), Oct 28, 1998: ENCODER. READS HIGH. ENCODER READOUTS ERRATIC AND INDICATES HIGH. - [SDR HEEA0016548](https://openairdocs.org/sdr/HEEA0016548), Oct 28, 1998: INDICATOR. MALFUNCTIONED. INDICATION CONSTANTLY FLUCTUATES 50 POUNDS ON TEST, LEFT TO RIGHT. - [SDR HEEA0016546](https://openairdocs.org/sdr/HEEA0016546), Oct 28, 1998: PROBE. READS HIGH. FUEL PROBE READS HIGH OUT OF TOLERANCE. - [SDR HEEA0016545](https://openairdocs.org/sdr/HEEA0016545), Oct 28, 1998: PROBE. READS HIGH. FUEL PROBE READS HIGH OUT OF TOLERANCE ON CAP METER. - [SDR HEEA0016520](https://openairdocs.org/sdr/HEEA0016520), Oct 28, 1998: DETECTOR. FAILED. RPM LIMIT DETECTOR NOT FUNCTIONING. All 151: https://openairdocs.org/deregistered/N22608-2011-09-12/reports.md ## FAA accident and incident reports (4) 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 19961005043079I](https://openairdocs.org/incident/19961005043079I), Oct 5, 1996: Bell 412 (N22608), Gulf Of Mexico, LA. Narrative: the pilot experienced a torque split; five minutes later, the no. 2 engine chip light came on. The pilot landed on the nearest platform. - [Incident 19950330013259I](https://openairdocs.org/incident/19950330013259I), Mar 30, 1995: Bell 412 (N22608), Venice, LA. During taxi for takeoff antitorque pedals failed. Returned. Yaw channel control transducer sticking. Cleaned lubed. - [Incident 19950104005849I](https://openairdocs.org/incident/19950104005849I), Jan 4, 1995: Bell 412 (N22608), Venice, LA. Narrative: after coming to a hover, while turning toward the landing pad, the no. 2 engine N1 surged momentarily to about 95 percent, a loud pop was heard, and… - [Incident 19880904062099I](https://openairdocs.org/incident/19880904062099I), Sep 4, 1988: Bell 412 (N22608), Gulf Of Mexico, LA, Minor damage. Sparks and fumes from windshield centerpost. Helicopter suffered minor damage. ## Other aircraft with N22608 - [Cancelled 1971-01-07](https://openairdocs.org/deregistered/N22608-1971-01-07): Taylorcraft BL, S/N 1255, built 1939. Owner: [Bennett Carl W](https://openairdocs.org/faa-owner/BENNETT%20CARL%20W), [Bastrop, LA](https://openairdocs.org/faa-place/LA/Bastrop) --- 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.