Owner type Corporation
Year built 1981
Type Rotorcraft
Engine Turbo-shaft
Airworthiness Standard, transport
Airworthiness date January 23, 1981
Certificate issued March 16, 2018
Expires March 31, 2028 From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming LTS-101 model are included below.
On this page Registration Potential ADs 62 Information bulletins 0 NTSB investigations 1 FAA incident reports 1 Difficulty reports 5 Potential STCs 86 Related links Airworthiness directives that may apply · 62 Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
1979 2026 ADs by the year they took effect: 69 ADs 1979 1 1980 1 1982 2 1983 2 1984 3 1986 1 1987 2 1988 3 1989 4 1992 1 1993 1 1994 2 1995 3 1996 6 1999 2 2000 2 2001 4 2002 5 2003 2 2004 1 2005 3 2006 1 2007 1 2008 3 2009 1 2010 3 2011 3 2013 1 2016 1 2021 2 2023 1 2026 1
See all 70 ADs Information bulletins that may apply Advisory, not mandatory.
No bulletins matched this aircraft’s models NTSB investigations · 1 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 5 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MDR01KH2005 Bolt · sheared UPON INSPECTION AND MAINTENANCE OF MAIN ROTOR CONTROLS, INSPECTION REVEALED SHEARED BOLT (PN 20-057-10-45D) AT BOLT HEAD AT THE M/R SWASH PLATE COLLECTIVE LEVER IDLER LINK. (ATTACH BOLTS) MFG A- NR 28 BOLT, MFG U-NR 28 BOLT. THIS CONDITION HAS BEEN REPORTED Oct 10, 2005 · N29KH · Bell 222 · Main Rotor Head SDR UNF2001F00001 Bolt · loose FOUND METAL TO METAL FRETTING WEAR AND MAKING MUD ON BOTTOM SIDE OF WING (22-031-800-101). BOLTS LOOSE ENOUGH TO ALLOW LOWER SKIN ON WING TO CAUSE SEVERE CHAFING DAMAGE BETWEEN LOWER WING SKINS (222-030-812-135/812-136) AND FUSELAGE STRUCTURAL SKINS (222-030- Nov 5, 2001 · N29KH · Bell 222 · Fuselage Miscellaneous Structure SDR UNF2001F00000 Bolt · worn FOUND METAL TO METAL FRETTING WEAR AND MAKING MUD ON BOTTOM SIDE OF WING (222-031-800-101). BOLTS LOOSE ENOUGH TO ALLOW LOWER SKIN ON WING TO CAUSE SEVERE CHAFING DAMAGE BETWEEN LOWER WING SKINS (222-030-812-135/812-136) AND FUSELAGE STRUCTURAL SKINS (222-030 Nov 5, 2001 · N29KH · Bell 222 · Fuselage Miscellaneous Structure SDR 99ZZZX3897 Ring · worn DURING C/W BELL SB ASB 222-99-84, DRIVE PIN TORQUE CHECK. ROTATIONAL TORQUE OF DRIVE PINS WAS FOUND TO BE BELOW MINIMUMS. NO REPAIR IS APPROVED AT THIS TIME. INSTALLED NEW PART. Sep 7, 1999 · N29KH · Bell 222 · Main Rotor Mast/Swashplate SDR 96ZZZX1029 Bearing · defective ENGINE REMOVED FOR PT WHEEL REPLACEMENT. DURING DISASSEMBLY, SPUR GEAR PLAY FOUND EXCESSIVE. GEARBOX DISASSEMBLED AND SPUR GEAR ASSY REMOVED. THE NR 19 BEARING HAD BEEN SPINNING IN ITS BORE, WEARING AND ELONGATING BORE. SUBMITTER RECOMMENDS PINNING OR SECU Feb 1, 1996 · N29KH · Bell 222 · Turbine Engine Accessory Drive STCs that may be installed · 86 Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 86 STCs