This N-number isn't registered right now. Below is its last known registration, canceled Dec 5, 2020.
Safety record in brief:1 NTSB incident (Sep 2010)18 ADs may apply7 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
Failure of the air traffic controller to exercise positive control of the situation by issuing clear and timely control instructions to the helicopter pilot. Contributing to the incident was delay by the helicopter pilot in responding to instructions issued by the controller.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for OPS10IA538)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2016-08-17 | Bell Helicopter Textron Canada Helicopters | May 31, 2016 | Airframe (222U)Only with: Main rotor hydraulic servo actuator P/N 222-382-001-107 installed. |
| 2013-18-06 | Bell Helicopter Textron Canada Limited (Bell) Helicopters | Oct 17, 2013 | Airframe (222U)Only with: Applies only to helicopters with specified flight control bellcrank, link, idler, bearing, swashplate link, or engine bipod mount fitting assemblies (various P/Ns by model) installed. |
| 2010-26-51 | Bell Helicopter Textron Canada Limited (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3… | Mar 25, 2011 | Airframe (222U)Serial numbers per RBI document attached to Bell Helicopter Textron ASBs 206-07-116, 206L-07-148, 222-07-106, 222U-07-77, 230-07-38, 407-07-81, 427-07-18, 430-07-41. Only with: Tail rotor blade with part number and serial number listed in the RBI document attached to the Bell ASBs installed. |
| 2010-10-12 | Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters | Jul 16, 2010 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038; 430 49001–49107. Only with: Tail rotor blade P/N 222-016-001-123, -123M, -127, -127M, -131, -135, -139M, or -141M installed (per model), except blades with S/Ns listed in Exceptions 1 and 2 or marked with an "R" code. |
| 2009-08-03 | Bell Helicopter Textron Canada Limited Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4… | Apr 24, 2009 | Airframe (222U)Serial numbers per Rotor Blades, Inc. (RBI) document attached to Bell Helicopter Textron ASBs 206-07-116, 206L-07-148, 222-07-106, 222U-07-77, 230-07-38, 407-07-81, 427-07-18, 430-07-41. Only with: Tail rotor blade installed with a part number and serial number listed in the RBI document attached to the applicable Bell ASB. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2008-19-02 | Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters | Oct 16, 2008 | Airframe (222U)Only with: Main rotor hydraulic actuator support P/N 222-040-125-001 installed. |
| 2008-16-04 | Bell Helicopter Textron Canada (BHTC) Model 222, 222B, and 222U Helicopters | Sep 15, 2008 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156 |
| 2008-14-01 | Bell Helicopter Textron Canada Model 222, 222B, 222U, 230 and 430 Helicopters | Aug 14, 2008 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038; 430 49001–49101 |
| 2004-20-07 | Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters | Nov 9, 2004 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038. Only with: With main rotor hub assembly P/N 222-011-101-ALL or 222-012-101-ALL installed (Model 230: P/N 222-012-101-ALL only). |
| 2003-13-13 | Bell Helicopter Textron Canada Model 222, 222B, and 222U Helicopters | Aug 12, 2003 | Airframe (222U)Only with: Magnetic brake P/N 204-001-376-105 or -107 installed, manufactured by Memcor Truohm, Inc. as P/N MP498-105 or -107. |
| 2003-08-07 | Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters | May 1, 2003 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038. Only with: With main rotor pendulum weight support P/N 222-011-114-101 or -103 installed, except pendulum weight supports with S/N prefix FN and numbers 363 through 409. |
| 2001-22-07 | Honeywell International, Inc. LTP 101 Series Turboprop and LTS101 Series Turboshaft… | Nov 30, 2001 | Engine (LTS 101 600A)Only with: Rigid tube fuel manifolds P/N 4-301-042-02, -04, -05, -06, 4-301-236-01, -02, -03, -04, 4-301-286-01, -02, or 4-301-376-01 installed. |
| 2001-19-52 | Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters | Oct 30, 2001 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038 |
| 2000-10-14 | Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, and 230 Helicopters | May 22, 2000 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038 |
| 2000-04-15 | Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters | Mar 14, 2000 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574; 230 23001–23038. Only with: Swashplate drive pin P/N 222-010-455-003 installed. |
| 99-23-04 | Bell Helicopter Textron Canada Model 222, 222B, and 222U Helicopters | Nov 19, 1999 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574 |
| 99-09-20 | Bell Helicopter Textron Canada (BHTC) Model 222, 222B, and 222U Helicopters | May 14, 1999 | Airframe (222U)Certain serial numbers: 222 47006–47089; 222B 47131–47156; 222U 47501–47574 |
| 96-12-27 | AlliedSignal Inc. (formerly Textron Lycoming) LTS 101 Series Turboshaft and LTP 101… | Aug 19, 1996 | Engine (LTS 101 600A) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
WHILE IN CRUISE FLIGHT, THE NR 1 ENG BEGAN RUNNING ERRATICALLY & THE NP WAS ATTEMPTING TO OVER SPEED. THE PILOT WAS ABLE TO ARREST THE ENG POWER BY MANUALLY RETARDING THE NG CONTROL TWIST GRIP. MADE AN UNEVENTFUL LANDING AT KBVU. MADE AN INITIAL VISUAL INSPECTION OF THE NR 1 ENG & FOUND THAT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MAINTENANCE FOUND CRACK .7 IN LONG IN LOWER LEFT BELLY SKIN TRAILING EDGE AT FS 245.3-246 BL -16 WL 25.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MAINTENANCE, FOUND CRACK IN BELLY SKIN APPROX, .7".
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MAINTENANCE FOUND .7 INCH CRACK IN BELLY SKIN AT FS 245.3, BL -16, WL 25.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON A ROUTINE ENGINE OVERSPEED SYS CHECK, WANTED TO INCREASE THE ENGINE RPM SLIGHTLY WITH THE TRIM SWITCH. FOUND UNABLE TO GET THE SWITCH TO DO ANYTHING. ON INSPECTION, MECHANIC FOUND THAT THE LINEAR ACTUATOR WAS INOPERATIVE AND SUBSEQUENTLY REPLACED THAT PART WHICH RESTORED SYS TO WORKING ORDER.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL SKID BRACKET ON BOTTOM OF VERTICAL FIN CRACKED AT TAIL STINGER AND TAIL ROTOR GUARD ATTACHMENT POINT. REMOVED VERTICAL FIN TO FACILITATE REMOVAL OF CRACKED BRACKET. REPLACED BRACKET WITH NEW TAIL SKID BRACKET AND REINSTALLED VERTICAL FIN.
From FAA Service Difficulty Reports; matched by N-number and serial number.SPIRAL BEVEL COLLECTOR GEAR FAIL APART, (DRIVE TOOTH/GEAR BOKE AWAY/SEPARATED FROM THE BEVEL GEAR BODY) WITH IN THE MAIN ROTOR GEARBOX/TRANSMISSION.
From FAA Service Difficulty Reports; matched by N-number and serial number.