# Bell 222B

- Type: Aircraft model (FAA registry)
- Registry code: 1182124
- Manufacturer (registry): BELL
- Model: 222B
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 10
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS H9SW](https://openairdocs.org/tcds/H9SW) (OpenAirDocs)
- Holder: Bell Textron Canada Limited
- Registered aircraft: 3
- Page: https://openairdocs.org/model/bell-222b

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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 87-15-06](https://openairdocs.org/ad/87-15-06): Tail Boom Assembly · Bell Helicopter Textron, A Division of Textron Canada 222B and 222U. Effective Aug 7, 1987
- [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 82-16-06](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

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

## Registered aircraft (3)

- [N16UA](https://openairdocs.org/aircraft/N16UA): [E D Santos & Associates LLC Trustee](https://openairdocs.org/faa-owner/E%20D%20SANTOS%20%26%20ASSOCIATES%20LLC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1984, S/N 47141
- [N322AW](https://openairdocs.org/aircraft/N322AW): [541 East Liberty LLC](https://openairdocs.org/faa-owner/541%20EAST%20LIBERTY%20LLC), [Savannah, GA](https://openairdocs.org/faa-place/GA/Savannah), built 1987, S/N 47151
- [N4VE](https://openairdocs.org/aircraft/N4VE): [Greenway Avia Inc](https://openairdocs.org/faa-owner/GREENWAY%20AVIA%20INC), [Leesburg, FL](https://openairdocs.org/faa-place/FL/Leesburg), S/N 47142

## STCs approved for it (80, first 50)

- [STC SA00680SE (2 OF 6](https://openairdocs.org/stc/SA00680SE%20(2%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International
- [STC SA1626NM PAGE 1](https://openairdocs.org/stc/SA1626NM%20PAGE%201): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc.
- [STC SA324NE](https://openairdocs.org/stc/SA324NE): Installation of two reinforcing plates P/N TSA-101-1 on Bell P/N 222-062-216-101 exhaust ejector.. Tri-State Aviation
- [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International
- [STC SH132NE](https://openairdocs.org/stc/SH132NE): Removal of height-velocity limita- tions and diagram from Limitations Section of RFM and placing in in Performance Section of RFM.. Pittston Co Coal Group
- [STC SH1879SO](https://openairdocs.org/stc/SH1879SO): Install lubrication oil scavenge filter.. Facet Filter Products
- [STC SH2252NM](https://openairdocs.org/stc/SH2252NM): Installation of Silver Instruments Fueltron IIIPT-IGS, IIIPT-IPS, IIIPT-ILS, IIIPT-IKS digital fuel flow indicating system.. Arnav Systems Inc
- [STC SH2697SO](https://openairdocs.org/stc/SH2697SO): Installation of a Wire Strike Protection System Kit.. Bristol Aerospace Ltd
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the
Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SH3613SW](https://openairdocs.org/stc/SH3613SW): Installation of a pivoting, tracking litter assembly.. RSG Products
- [STC SH3621SW](https://openairdocs.org/stc/SH3621SW): Installation of a defibrillator container.. RSG Products
- [STC SH3623SW](https://openairdocs.org/stc/SH3623SW): Installation of a medical stowage cabinet in aft cabin bulkhead.. RSG Products
- [STC SH3624SW](https://openairdocs.org/stc/SH3624SW): Installation of a litter/ stretcher attachment bracket.. RSG Products
- [STC SH3625SW](https://openairdocs.org/stc/SH3625SW): Installation of oxygen bottle rack in baggage compartment.. RSG Products
- [STC SH3727NM](https://openairdocs.org/stc/SH3727NM): Installation of ARNAV Systems FC-10/FT-10 digital fuel flow indicating system.. Arnav Systems
- [STC SH3784SW](https://openairdocs.org/stc/SH3784SW): Installation of an emergency exit and camera opening window.. Bell Helicopter Textron Inc.
- [STC SH424NE](https://openairdocs.org/stc/SH424NE): Installation of two reinforcing plates P/N TSA-101-1 on Bell P/N 222-062-216-101 exhaust ejector assembly.  Eligible for installation on serial numbers up to and including S/N 47146.. Helicopter Support Inc Services Div
- [STC SH442NE](https://openairdocs.org/stc/SH442NE): Installation of 'Zapper' pulsed chip detector system Model No. 1K1310.. TEDECO Division
- [STC SH4593SW](https://openairdocs.org/stc/SH4593SW): Installation of tail rotor floodlight system.. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SH4793NM](https://openairdocs.org/stc/SH4793NM): Fabrication of Onboard Systems Model E-73 Cargo Hook Load Cell System. Onboard Systems International
- [STC SH5225NM](https://openairdocs.org/stc/SH5225NM): Installation of a freon air conditioning system.. Air Comm Corporation
- [STC SH5226NM](https://openairdocs.org/stc/SH5226NM): Installation of a bleed air cabin heating system.. Air Comm Corporation
- [STC SH5255NM](https://openairdocs.org/stc/SH5255NM): Installation of a right side maintenance step.. Air Methods Corporation
- [STC SH569NE](https://openairdocs.org/stc/SH569NE): Installation of an engine inlet screen assembly, Tri-State Aviation P/N TSA001M.. Helicopter Support Inc Services Div
- [STC SH5789SW](https://openairdocs.org/stc/SH5789SW): Installation of SFENA automatic flight control system(AFCS).. Sextant Avionique, Inc
- [STC SH5880SW](https://openairdocs.org/stc/SH5880SW): Installation of Sperry digital automatic flight control system SPZ-7000.. RSG Products
- [STC SH5903SW](https://openairdocs.org/stc/SH5903SW): Installation of forward facing recognition lights under fuselage.. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SH5995SW](https://openairdocs.org/stc/SH5995SW): Installation of Synergetics retractable passenger door step.. Synergetics, Inc
- [STC SH7853SW](https://openairdocs.org/stc/SH7853SW): Installation of two Allison Model250-C30G engines.. World Wide Helicopters Inc.
- [STC SH7937SW](https://openairdocs.org/stc/SH7937SW): Installation of an observer/attendant seat.. RSG Products
- [STC SH7938SW](https://openairdocs.org/stc/SH7938SW): Installation of a stowable attendant seat.. RSG Products
- [STC SH7939SW](https://openairdocs.org/stc/SH7939SW): Installation of a secondary stretcher.. RSG Products
- [STC SH7940SW](https://openairdocs.org/stc/SH7940SW): Installation of a primary litter carriage and stowage cabinet.. Fort Worth
- [STC SH7941SW](https://openairdocs.org/stc/SH7941SW): Installation of a secondary attendant seat.. RSG Products
- [STC SH8036SW](https://openairdocs.org/stc/SH8036SW): Installation of floor tracks for litter/equipment attachments.. RSG Products
- [STC SH8037SW](https://openairdocs.org/stc/SH8037SW): Installation of a tracking attendant seat.. RSG Products
- [STC SH8038SW](https://openairdocs.org/stc/SH8038SW): Installation of a dual pivot litter with cabinet.. RSG Products
- [STC SH8591SW](https://openairdocs.org/stc/SH8591SW): Installation of a Bendix King KLN 90 GPS navigation system.. Texas Aviation Services
- [STC SH8592SW](https://openairdocs.org/stc/SH8592SW): Installation of a Bendix King RDS 82VP color radar.. Heritage Aviation Ltd
- [STC SH8613SW](https://openairdocs.org/stc/SH8613SW): Installation of replacement roof skylight windows.. The NORDAM Group LLC
- [STC SH8614SW](https://openairdocs.org/stc/SH8614SW): Installation of replacement of opera picture windows.. The NORDAM Group LLC
- [STC SH8615SW](https://openairdocs.org/stc/SH8615SW): Installation of replacement passenger door windows.. The NORDAM Group LLC
- [STC SH8616SW](https://openairdocs.org/stc/SH8616SW): Installation of replacement chin bubble windows.. The NORDAM Group LLC
- [STC SH8632SW](https://openairdocs.org/stc/SH8632SW): Installation of replacement crew door windows.. The NORDAM Group LLC
- [STC SH8647SW](https://openairdocs.org/stc/SH8647SW): Installation of an airborne vibration monitoring system.. Rotor Dynamics Americas
- [STC SH8651SW](https://openairdocs.org/stc/SH8651SW): Approval to operate with crew doors removed.. Bell Helicopter Textron
- [STC SH8673SW](https://openairdocs.org/stc/SH8673SW): Tail skid modification.. RSG Products
- [STC SH8704SW](https://openairdocs.org/stc/SH8704SW): Installation of fuselage floodlights.. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SH935GL](https://openairdocs.org/stc/SH935GL): Installation of Shadin Company digital fuel flow indicator system.. Shadin Company Inc

All 80: https://openairdocs.org/model/bell-222b/stcs.md

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DFW06LA072](https://openairdocs.org/ntsb/DFW06LA072), Feb 19, 2006: Bell 222B (N306CH), Gulf of Mexico (Gulf of Mexico), destroyed. Probable cause: The flight crew's failure to maintain control of the helicopter, and the crew's diverted attention to secondary tasks while preparing for the night landing. A contributing factor was the dark night…
- [NTSB LAX98LA249](https://openairdocs.org/ntsb/LAX98LA249), Jul 30, 1998: Bell 222B (N911RA), Tranquility, CA, destroyed. Probable cause: The pilot's delayed initiation of a go-around when the severity of the dust condition first became apparent. Contributing factors were dark night conditions and the obscuration from the dust.

## FAA accident and incident reports (7)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20060219001399A](https://openairdocs.org/incident/20060219001399A), Feb 19, 2006: Bell 222B (N306CH), Galveston, TX, Destroyed. (-23) Helicopter N306CH a Bell 222-B departed houston hobby airport at 0100 local, VFR, enroute to an oil tanker moored in the sabine lightering area…
- [Incident 19990127010989I](https://openairdocs.org/incident/19990127010989I), Jan 27, 1999: Bell 222B (N406MA), Henderson, NV, Minor damage. The pilot was repositioning for takeoff. As he turned the helicopter by ground taxi from a westerly to a northerly heading, the main rotor blades struck the…
- [Accident 19980729018259A](https://openairdocs.org/incident/19980729018259A), Jul 29, 1998: Bell 222B (N911RA), Fresno, CA, Destroyed. (.19) On July 29, 1998, at 2248 hour pacific daylight time, a Bell 222B helicopter, N911RA, was destroyed when it landed hard, rolled over, and burned at…
- [Incident 19970919033399I](https://openairdocs.org/incident/19970919033399I), Sep 19, 1997: Snias AS350B (N8WU), Tyler, TX, Substantial damage. Narrative: conducting 4-5 foot ground hover, experience severe vibration. Landed, shut aircraft down. Inspection revealed skin on boom, at fuselage attach…
- [Incident 19910509038009I](https://openairdocs.org/incident/19910509038009I), May 9, 1991: Bell 222B (N222LB), Midland, TX, Minor damage. Unable to lock gear in down position. Gear collapsed on landing.
- [Incident 19820728066199I](https://openairdocs.org/incident/19820728066199I), Jul 28, 1982: Airbus A300B4203 (N222EA), San Francisco, CA. Pilot encountered moderate turbulence. Three passengers and three flight attendants received slight injuries.
- [Incident 19790929049739I](https://openairdocs.org/incident/19790929049739I), Sep 29, 1979: Cessna 500CESSNA (N222LB), Jacksonville, FL. Pressurization regulator malfunction allowed door seal to depressurize and pop out of its channel.

## Service difficulty reports (25)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA130314004](https://openairdocs.org/sdr/CA130314004), Mar 13, 2013: CASE. CRACKED. (CAN) TOP CASE RT INBD COLLECTIVE IDLER LUG FOUND CRACKED. BUSHING WORN BEYOND LIMIT. CASE REPLACED.
- [SDR QML3MR0241](https://openairdocs.org/sdr/QML3MR0241), Aug 9, 2010: BULKHEAD. CRACKED. DURING OTHER MX 1 CRACK WAS FOUND IN BULKHEAD 222-031-505-001 AT ATTACHMENT POINT OF BEAM SUPPORT PN 222-031-519-103.
- [SDR QML3MR0244](https://openairdocs.org/sdr/QML3MR0244), Aug 5, 2010: BLADE. DEBONDED. DURING INSP ROTOR BLADE FOUND APPROX 2" DEBONDING OF MIDDLE TRIM TAB LOWER SIDE AT BS 90.1-92.1 AND 1.25" TEAR IN LOWER BLADE SKIN AT BS 101.4
- [SDR QML3MR0243](https://openairdocs.org/sdr/QML3MR0243), Aug 5, 2010: SKIN. DELAMINATED. DURING INSP, FOUND DELAMINATION/PUNCTURE OF RT UPPER WING SKIN IN AREA OF A PREVIOUS REPAIR. DELAMINATION MEASURES APPROX 16" X 7". PUNCTURE IS SCREW HEAD USED 
- [SDR QML3MR0242](https://openairdocs.org/sdr/QML3MR0242), Aug 5, 2010: SKIN. PUNCTURED. DURING INSP, FOUND PUNCTURE/CRACK OF UPPER WING SKIN APPROX 1" IN LENGTH CAUSED BE IMPACT FROM ABOVE.
- [SDR ZES2007F00001](https://openairdocs.org/sdr/ZES2007F00001), Apr 27, 2007: FUEL CONTROL. MALFUNCTIONED. ON APPROACH, THE RT ENG LOST POWER AND WAS UNRESPONSIVE TO THROTTLE MOVEMENT. FUEL CONTROL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR N406MA0204](https://openairdocs.org/sdr/N406MA0204), Feb 27, 2004: WIRE. CHAFED. DURING FLIGHT TAIL ROTOR CAUTION LIGHT ILLUMINATED. RETURNED TO BASE. FOUND POWER WIRE TO CHIP DETECTOR WAS FOUND TO HAVE CHAFED THROUGH AND SHORTED. REPAIRED W
- [SDR N406MA](https://openairdocs.org/sdr/N406MA), Feb 18, 2004: DETECTOR. BROKEN. WHILE ENROUTE TO A SCENE CALL, CLIMBING THROUGH 3800 FT EAST OF ROMNA, CA. I NOTICED NR 2 ENGINE OIL TEMP PEGGED ABOVE MAX. TEMP HAD BEEN NORMAL ON LAUNCH AND T
- [SDR CA020228013](https://openairdocs.org/sdr/CA020228013), Feb 1, 2002: SLEEVE. WORN. (CAN) WHEN SWASH PLATE ASSY WAS REMOVED TO FACILITATE 7 YEAR MAST REMOVAL FOR INSPECTION AND RECALIBRATION, THE SLIDER BEARINGS (2OF) P/N 222-310-464-003 WERE F
- [SDR 99ZZZX2556](https://openairdocs.org/sdr/99ZZZX2556), Jun 22, 1999: BEAM. DAMAGED. WALKING BEAM REPLACED WITH NEW FROM BELL HELICOPTER.
- [SDR ERAA062393](https://openairdocs.org/sdr/ERAA062393), May 13, 1999: INDICATOR. FLUCTUATES. RIGHT NEEDLE FLUCTUATES TO HIGH SIDE. READS 104 PERCENT WHEN ROTOR IS AT 100 PERCENT.
- [SDR 97ZZZX2840](https://openairdocs.org/sdr/97ZZZX2840), May 12, 1997: FLEXTURE. DELAMINATED. INSPECTION FOUND FLEXTURES DELAMINATED. REPLACED WITH NEW FLEXTURES.
- [SDR 97ZZZX2839](https://openairdocs.org/sdr/97ZZZX2839), May 12, 1997: FLEXTURE. DELAMINATED. INSPECTION FOUND FLEXTURES DELAMINATED. REPLACED WITH NEW FLEXTURES.
- [SDR HAIW6HR0080](https://openairdocs.org/sdr/HAIW6HR0080), Apr 29, 1997: PUMP. WORN EXCESS. PART IS WORN EXCESSIVELY. PUMP LEAKS AT SHAFT SEAL.
- [SDR HAIW6HR0077](https://openairdocs.org/sdr/HAIW6HR0077), Mar 23, 1997: GENERATOR. ARCED. PART IS ARCED. COMMUTATOR APPEARS TO HAVE BURNED SPOTS. STATIC IS HEARD THRU ALL HEAD SETS. REQUEST WARRANTY REPAIR SINCE THIS UNIT HAS ONLY BEEN IN SERVICE 22.
- [SDR 97ZZZX906](https://openairdocs.org/sdr/97ZZZX906), Jan 28, 1997: PUMP. FAILED. PILOTS EXPERIENCED HYD CAUTION LIGHT, AND SLOWLY DECLINING PRESSURE INDICATION ON COCKPIT GAUGE. TOTAL LOSE OF HYDRAULIC PRESSURE FOLLOWED SHORTLY THEREAFTER.
- [SDR 97ZZZX406](https://openairdocs.org/sdr/97ZZZX406), Dec 16, 1996: TAIL BOOM. CRACKED. PILOT FOUND CRACK ON PRE-FLIGHT CHECK. CRACK WAS FOUND ON RIGHT HAND SIDE OF TAIL BOOM FORWARD OF HORIZ STAB AT BSTA 219.40, WL 75. CRACK RUNS FORE AND AFT AND 
- [SDR 96ZZZX5156](https://openairdocs.org/sdr/96ZZZX5156), Sep 23, 1996: BRACE. BROKEN. BRACE, P/N 222-080-134-102, WAS FOUND BROKEN TO NR 2 SYSTEM HYDRAULIC FILTER MANIFOLD. SUBMITTER STATED BRACE MANUFACTURING PROCEDURE NEEDS TO BE CHANGED. BRACE
- [SDR 96ZZZX5155](https://openairdocs.org/sdr/96ZZZX5155), Sep 23, 1996: TUBE ASSY. CRACKED. DURING FLIGHT, TUBE ASSY CRACKED CAUSING LOSS OF NR 2 HYDRAULIC SYSTEM PRESSURE. ALSO, FOUND BROKEN WAS BRACE P/N 222-080-134-102 THAT SUPPORTS FILTER MANIFOLD 
- [SDR 96ZZZX614](https://openairdocs.org/sdr/96ZZZX614), Dec 13, 1995: ROTOR. BLADE SHIFT. POWER TURBINE ROTOR INSPECTION, SB LT101-72-50-0153, COMPLIED WITH EARLY DUE TO ANNUAL INSPECTION FOUND UNSERVICEABLE. TIME SINCE INSTALLATION 40.3 HOURS. CYCLE
- [SDR 95ZZZX7037](https://openairdocs.org/sdr/95ZZZX7037), Nov 22, 1995: PT ROTOR. BLADE SHIFT. THIS PART WAS INSPECTED EARLY AT CONVENIENCE OF OPERATOR, TO MAINTAIN ACFT AVAILABILITY. DURING C/W ALLIED SIGNAL AEROSPACE (FORMERLY TEXTRON LYCOMING) SB LT-10
- [SDR 95ZZZX3169](https://openairdocs.org/sdr/95ZZZX3169), Jun 5, 1995: DIODE. FAILED. ACTT 1990.5. PILOT ATTEMPTED TO START NR 1 ENGINE AT 12 PERCENT NG. STARTER DROPPED OFF-LINE. ON SUBSEQUENT ATTEMPT, ONLY ENGINE IGNITER OPERATED. DURING TROUBL
- [SDR 95ZZZX2534](https://openairdocs.org/sdr/95ZZZX2534), May 2, 1995: SHAFT. CORRODED. INSPECTION FOUND SHAFTS CORRODED. W.P.H.S. REPLACED WITH NEW SHAFTS.
- [SDR 95ZZZX2533](https://openairdocs.org/sdr/95ZZZX2533), May 2, 1995: SHAFT. CORRODED. INSPECTION FOUND SHAFTS CORRODED. W.P.H.S. REPLACED WITH NEW SHAFTS.
- [SDR 95ZZZX2457](https://openairdocs.org/sdr/95ZZZX2457), May 2, 1995: FLEXTURE. DEBONDED. INSPECTION FOUND FLEXTURE DEBONDED. W.P.H.S. REPLACED WITH NEW FLEXTURE.

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