# N707LP: Bell 222 - Status: Valid registration - Airframe: [Bell 222](https://openairdocs.org/model/bell-222) (registry code 1182122, 10 seats) - Engine: [Lycoming LTS-101 series](https://openairdocs.org/engine/lycoming-lts-101-series) (registry code 41560) - Data sheets: [TCDS H9SW](https://openairdocs.org/tcds/H9SW) (Bell Textron Canada Limited), [TCDS E5NE](https://openairdocs.org/tcds/E5NE) (Intermountain Turbine Services Inc.) (OpenAirDocs) - Serial number: 47072 - Type: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: December 11, 2002 - Certificate issued: February 18, 2025 - Expires: February 29, 2032 - Mode S code: A96F97 - Registered owner: [N-707lp Inc](https://openairdocs.org/faa-owner/N-707LP%20INC) - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Corporation - Owner's area on the map: 29.7482° N, 95.4689° W: Placed by OpenAirDocs at the center of ZIP code 77056, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=707LP - Page: https://openairdocs.org/aircraft/N707LP From the FAA registry file of October 21, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Lycoming LTS-101 model are included. ## ADs that may apply (OpenAirDocs): 62 in force ### Matched by airframe (Bell 222) - [AD 2026-17-51](https://openairdocs.org/ad/2026-17-51): Tail rotor system · Bell Textron Canada 222. Effective Sep 14, 2026 - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2021-19-01](https://openairdocs.org/ad/2021-19-01): Cabin Equipment/Furnishings · Shoulder harness restraint system (Bell Helicopter Textron STC SH2073SO or SH2751SO). Effective Oct 13, 2021 - [AD 2016-08-17](https://openairdocs.org/ad/2016-08-17): Rotorcraft Servo System · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective May 31, 2016 - [AD 2013-18-06](https://openairdocs.org/ad/2013-18-06): Main Rotor Control · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Oct 17, 2013 - [AD 2010-26-51](https://openairdocs.org/ad/2010-26-51): Tail rotor blade · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Mar 25, 2011 - [AD 2010-10-12](https://openairdocs.org/ad/2010-10-12): Blades · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Jul 16, 2010 - [AD 2008-19-02](https://openairdocs.org/ad/2008-19-02): Main rotor hydraulic actuator support (support) · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Oct 16, 2008 - [AD 2008-16-04](https://openairdocs.org/ad/2008-16-04): Tail rotor pedal · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Sep 15, 2008 - [AD 2008-14-01](https://openairdocs.org/ad/2008-14-01): Fuel valve switch · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Aug 14, 2008 - [AD 2006-13-14](https://openairdocs.org/ad/2006-13-14): Tail rotor counterweight bellcrank (bellcrank) · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Jul 11, 2006 - [AD 2005-03-10](https://openairdocs.org/ad/2005-03-10): Main rotor grip (grip) · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective Mar 18, 2005 - [AD 2004-20-07](https://openairdocs.org/ad/2004-20-07): Main rotor yoke (yoke) · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective Nov 9, 2004 - [AD 2003-13-13](https://openairdocs.org/ad/2003-13-13): Magnetic brake assembly · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Aug 12, 2003 - [AD 2003-08-07](https://openairdocs.org/ad/2003-08-07): main rotor pendulum · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective May 1, 2003 - [AD 2002-20-05](https://openairdocs.org/ad/2002-20-05): Rescue hoists · Agusta A109, A109A, A109A II and 31 more. Effective Nov 7, 2002 - [AD 2002-20-02](https://openairdocs.org/ad/2002-20-02): Right-hand upper fuel enclosure area · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Nov 7, 2002 - [AD 2001-19-52](https://openairdocs.org/ad/2001-19-52): Main Rotor Pendulum Weight Supports · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective Oct 30, 2001 - [AD 2001-01-51](https://openairdocs.org/ad/2001-01-51): Main Rotor Hydraulic Actuator Support · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Mar 2, 2001 - [AD 2000-10-14](https://openairdocs.org/ad/2000-10-14): Yoke Attachment Bolt · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective Jun 26, 2000 - [AD 2000-04-15](https://openairdocs.org/ad/2000-04-15): Drive Pin · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective Mar 14, 2000 - [AD 99-23-04](https://openairdocs.org/ad/99-23-04): Torque Of Vertical Fin Attachment Bolts Inspection · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Nov 19, 1999 - [AD 99-09-20](https://openairdocs.org/ad/99-09-20): Main Rotor Flapping Bearing Assembly · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective May 14, 1999 - [AD 96-18-15](https://openairdocs.org/ad/96-18-15): Tail Rotor Blade · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 1 more. Effective Sep 23, 1996 - [AD 93-08-14](https://openairdocs.org/ad/93-08-14): Main Rotor Flapping Bearings · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Apr 6, 1994 - [AD 87-09-02 R2](https://openairdocs.org/ad/87-09-02-R2): Drive Hub Assembly · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Dec 22, 1989 - [AD 89-25-04](https://openairdocs.org/ad/89-25-04): Tail Rotor Support Bracket Bulkhead · Bell Helicopter Textron, A Division of Textron Canada 222 and 222B. Effective Dec 20, 1989 - [AD 88-02-03](https://openairdocs.org/ad/88-02-03): Main Rotor Yoke · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Nov 28, 1989 - [AD 89-17-05](https://openairdocs.org/ad/89-17-05): Horizontal Stabilizers · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Aug 28, 1989 - [AD 87-13-01](https://openairdocs.org/ad/87-13-01): Rfm Changes - Engine · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective May 27, 1988 - [AD 85-14-11](https://openairdocs.org/ad/85-14-11): Linkage Rivets · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Feb 9, 1988 - [AD 87-19-01](https://openairdocs.org/ad/87-19-01): Stc Sh479gl Labels · Lubrication oil scavenge filter is installed in the existing… (Facet Filter Products STC SH1853SO or 3 others). Effective Dec 18, 1987 - [AD 87-15-07](https://openairdocs.org/ad/87-15-07): M/R Flapping Bearing · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Aug 7, 1987 - [AD 84-12-02](https://openairdocs.org/ad/84-12-02): Support Fittings · Bell Helicopter Textron, A Division of Textron Canada 222. Effective Jul 11, 1984 - [AD 83-02-51](https://openairdocs.org/ad/83-02-51): Walking Beam Assemblies · Bell Helicopter Textron, A Division of Textron Canada 222 and 222B. Effective May 15, 1984 - [AD 83-09-03](https://openairdocs.org/ad/83-09-03): Main Rotor Trunnion, Torquemeter · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective May 23, 1983 - [AD 82-09-53](https://openairdocs.org/ad/82-09-53): Swashplate Drive Links · Bell Helicopter Textron, A Division of Textron Canada 222. Effective Aug 19, 1982 - [AD 82-16-06](https://openairdocs.org/ad/82-16-06): Main Rotor Spar Doublers · Bell Helicopter Textron, A Division of Textron Canada 222, 222B and 222U. Effective Jul 30, 1982 ### Matched by engine (Lycoming LTS-101 series) - [AD 2011-23-13](https://openairdocs.org/ad/2011-23-13): Power turbine governors (PTG) · Honeywell International LTS101-600A-2, LTS101-600A-3, LTS101-600A-3A and 1 more. Effective Nov 29, 2011 - [AD 2011-08-06](https://openairdocs.org/ad/2011-08-06): Power turbine rotors · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 10 more. Effective May 17, 2011 - [AD 2009-24-12](https://openairdocs.org/ad/2009-24-12): Gas generator · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 12 more. Effective Jan 4, 2010 - [AD 2002-03-09 R1](https://openairdocs.org/ad/2002-03-09-R1): Impellers · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Mar 27, 2002 - [AD 2001-25-04](https://openairdocs.org/ad/2001-25-04): Fuel Controls · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 1 more. Effective Jan 23, 2002 - [AD 2001-22-07](https://openairdocs.org/ad/2001-22-07): Rigid Tube Fuel Manifold Assemblies · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Nov 30, 2001 - [AD 2001-17-15](https://openairdocs.org/ad/2001-17-15): Engine Fuel Pumps · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 2 more. Effective Oct 1, 2001 - [AD 96-12-27](https://openairdocs.org/ad/96-12-27): Gas Generator Turbine Disk · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Aug 19, 1996 - [AD 96-12-05](https://openairdocs.org/ad/96-12-05): Turbine rotors · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Aug 12, 1996 - [AD 96-10-04](https://openairdocs.org/ad/96-10-04): Fuel control · Honeywell International LTS101-600A-2 and LTS101-600A-3. Effective Jun 13, 1996 - [AD 96-06-10](https://openairdocs.org/ad/96-06-10): Power turbine (PT) disk · Honeywell International LTS101-600A-2, LTS101-600A-3 and LTS101-750B-2. Effective May 28, 1996 - [AD 95-26-01](https://openairdocs.org/ad/95-26-01): Power Turbine · Honeywell International LTS101-650B-1, LTS101-650C, LTS101-750B-1 and 1 more. Effective Apr 22, 1996 - [AD 95-16-04](https://openairdocs.org/ad/95-16-04): Axial Compressor Rotors · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Oct 2, 1995 - [AD 95-08-14](https://openairdocs.org/ad/95-08-14): Electronic Overspeed Protection System · Honeywell International LTS101-650B-1, LTS101-650C-3, LTS101-650C-3A and 2 more. Effective May 9, 1995 - [AD 94-18-06](https://openairdocs.org/ad/94-18-06): Bearings · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Sep 26, 1994 - [AD 93-13-11](https://openairdocs.org/ad/93-13-11): Gas Generator Turbine Rotor Disk · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 22 more. Effective Nov 8, 1993 - [AD 92-15-07](https://openairdocs.org/ad/92-15-07): Integrally Cast Power Turbine (PT) Rotor Blade · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Sep 2, 1992 - [AD 88-14-01](https://openairdocs.org/ad/88-14-01): Power Turbine Disk · Honeywell International LTS101-600A, LTS101-600A-1, LTS101-600A-2 and 17 more. Effective Jul 6, 1988 - [AD 86-10-04](https://openairdocs.org/ad/86-10-04): Gas Producer (G.P.) Blade · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 11 more. Effective May 16, 1986 - [AD 84-02-07](https://openairdocs.org/ad/84-02-07): Output Gear Assembly and Torquemeter Gear Assembly · Honeywell International LTS101-600A-2. Effective May 7, 1984 - [AD 83-16-03](https://openairdocs.org/ad/83-16-03): Install Overspeed Limiter · Honeywell International LTS101-600A-2. Effective Aug 25, 1983 - [AD 79-06-06 R2](https://openairdocs.org/ad/79-06-06-R2): Lubrication System Contamination · Honeywell International LTP 101-600, LTP 101-600A, LTS101-600A and 3 more. Effective Jun 2, 1980 - [AD 79-20-03](https://openairdocs.org/ad/79-20-03): Fuel Control, Fuel Pump And Oil Pump Drive Gears · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 5 more. Effective Sep 26, 1979 - [AD 84-14-01](https://openairdocs.org/ad/84-14-01): T4 Indicator System Check · Honeywell International LTS101-600A-2 ### Historical (superseded or no longer in force) - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 - [AD 2010-19-51](https://openairdocs.org/ad/2010-19-51) (historical): Corrosion or a nonconforming piston rod · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Dec 9, 2010 - [AD 2009-08-03](https://openairdocs.org/ad/2009-08-03) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Apr 24, 2009 - [AD 2007-19-52](https://openairdocs.org/ad/2007-19-52) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Dec 5, 2007 - [AD 2005-04-09](https://openairdocs.org/ad/2005-04-09) (historical): Tail rotor blades · 222, 222B, 222U and 2 more. Effective Mar 4, 2005 - [AD 2004-26-11](https://openairdocs.org/ad/2004-26-11) (historical): Tail Rotor Blades · 222, 222B, 222U and 2 more. Effective Jan 18, 2005 - [AD 2002-08-54](https://openairdocs.org/ad/2002-08-54) (historical): Main rotor grip assembly · 222, 222B, 222U and 1 more. Effective Aug 21, 2002 - [AD 95-09-02](https://openairdocs.org/ad/95-09-02) (historical): Fuel Pumps · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 12 more. Effective May 10, 1995 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N707LP. ## FAA accident and incident reports None matched to N707LP. ## Service difficulty reports None filed for this aircraft. ## Related - Other Bell 222 aircraft: https://openairdocs.org/model/bell-222/aircraft.md - STCs for the Bell 222: https://openairdocs.org/model/bell-222/stcs.md - The Lycoming LTS-101 series engine: https://openairdocs.org/engine/lycoming-lts-101-series.md --- 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.