# Bell 214B - Type: Aircraft model (FAA registry) - Registry code: 1182100 - Manufacturer (registry): BELL - Model: 214B - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Turbo-shaft - Seats: 16 - Weight class: Up to 12,499 lb - Cruise speed: 112 mph - Certification: Type certificated - Data sheet: [TCDS H6SW](https://openairdocs.org/tcds/H6SW) (OpenAirDocs) - Holder: McDermott 214 Holdings, LLC - Registered aircraft: 2 - Page: https://openairdocs.org/model/bell-214b 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 2022-22-12](https://openairdocs.org/ad/2022-22-12): Nose/Tail Landing Gear Structure/Axle · Replacement crosstubes P/N D212-664 (Dart Aerospace STC SR01298NY). Effective Nov 22, 2022 - [AD 2020-16-10](https://openairdocs.org/ad/2020-16-10): Cabin Equipment/Furnishings · Bell Textron 204B, 205A, 205A-1 and 7 more. Effective Sep 3, 2020 - [AD 2014-12-01](https://openairdocs.org/ad/2014-12-01): Tail Rotor Drive Bearing · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Jul 14, 2014 - [AD 2013-19-05](https://openairdocs.org/ad/2013-19-05): JASC Code: 6330, Transmission Mount · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Nov 5, 2013 - [AD 2013-06-51](https://openairdocs.org/ad/2013-06-51): Equipment/Furnishings · Agusta A109, A109A, A109A II and 43 more. Effective Jul 15, 2013 - [AD 2002-22-14](https://openairdocs.org/ad/2002-22-14): Main rotor tension-torsion (TT) straps · Bell Helicopter Textron 204B, 205A, 205A-1 and 4 more. Effective Dec 13, 2002 - [AD 2001-03-03](https://openairdocs.org/ad/2001-03-03): Main Rotor Outboard Strip Fitting Assemblies · Bell Helicopter Textron 214B and 214B-1. Effective Feb 28, 2001 - [AD 99-05-07](https://openairdocs.org/ad/99-05-07): Pillow Block Bearing Bolts · Bell Helicopter Textron 214B and 214B-1. Effective May 3, 1999 - [AD 99-02-17](https://openairdocs.org/ad/99-02-17): Tail Rotor Yoke Assembly · Bell Helicopter Textron 214B and 214B-1. Effective Feb 10, 1999 - [AD 98-23-18](https://openairdocs.org/ad/98-23-18): Kaynar Tech. Manufactured Barrel Nut · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Nov 30, 1998 - [AD 98-18-01](https://openairdocs.org/ad/98-18-01): Main Rotor Trunnion · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Sep 29, 1998 - [AD 97-15-04](https://openairdocs.org/ad/97-15-04): Main Transmission Upper Planetary Carrier · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Aug 19, 1997 - [AD 97-06-02](https://openairdocs.org/ad/97-06-02): Lower Planetary Spider · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Apr 16, 1997 - [AD 93-21-10](https://openairdocs.org/ad/93-21-10): Main Rotor Yoke Assembly · Bell Helicopter Textron 214B and 214B-1. Effective Jan 18, 1994 - [AD 87-11-06](https://openairdocs.org/ad/87-11-06): Locking Plates · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective May 26, 1987 - [AD 85-18-06](https://openairdocs.org/ad/85-18-06): Main Rotor Drag Brae Assembly · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Apr 20, 1987 - [AD 86-20-06](https://openairdocs.org/ad/86-20-06): Main Rotor Drag Brace Assembly · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Oct 18, 1986 - [AD 82-06-07](https://openairdocs.org/ad/82-06-07): Tail Rotor Yoke · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Apr 12, 1982 - [AD 81-12-03](https://openairdocs.org/ad/81-12-03): Spindle Retention Bolts · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Jun 11, 1981 - [AD 81-02-10](https://openairdocs.org/ad/81-02-10): Clutch Assembly · Bell Helicopter Textron 214B and 214B-1. Effective Jan 26, 1981 - [AD 77-17-05](https://openairdocs.org/ad/77-17-05): Emergency Exit Latch Pin · Bell Helicopter Textron 204B, 205A-1, 212 and 2 more. Effective Jul 17, 1978 - [AD 78-08-08](https://openairdocs.org/ad/78-08-08): Tail Fin Spar · Bell Helicopter Textron 214B and 214B-1. Effective Apr 21, 1978 - [AD 77-03-04](https://openairdocs.org/ad/77-03-04): Fuselage Splice Fitting · Bell Helicopter Textron 214B and 214B-1. Effective Feb 14, 1977 - [AD 85-23-05](https://openairdocs.org/ad/85-23-05): Collective Sleeve · Bell Helicopter Textron 214B, 214B-1 and 214ST - [AD 84-05-51](https://openairdocs.org/ad/84-05-51): Collective Sleeves · Bell Helicopter Textron 214B, 214B-1 and 214ST Historical (superseded or no longer in force): - [AD 2013-11-05](https://openairdocs.org/ad/2013-11-05) (historical): Tail rotor hanger bearing · Bell Helicopter Textron 214B, 214B-1 and 214ST. Effective Jun 19, 2013 - [AD 80-17-09](https://openairdocs.org/ad/80-17-09) (historical): Main Rotor Straps · Bell Helicopter Textron 204B, 205A-1, 212 and 16 more. Effective Sep 15, 1980 ## Registered aircraft (2) - [N216PJ](https://openairdocs.org/aircraft/N216PJ): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1981, S/N 28069 - [N217PJ](https://openairdocs.org/aircraft/N217PJ): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1979, S/N 28032 ## 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 SA04465NY](https://openairdocs.org/stc/SA04465NY): Installation of the iPad Mount. Avio Design Group Inc - [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 SA2662NM](https://openairdocs.org/stc/SA2662NM): Installation of a Simples Model7300 spray system.. Simplex Manufacturing Company - [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc. - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SH2149NM](https://openairdocs.org/stc/SH2149NM): Removal of five seats. TransWestern Helicopters Inc. - [STC SH2298SW](https://openairdocs.org/stc/SH2298SW): Interior arrangement and installation.. Associated Air Center - [STC SH261WE](https://openairdocs.org/stc/SH261WE): Installation of an external load attachment mechanism in accordance with FAA Approved USDA Forest Service Master Drawing List and Rotorcraft Flight Manual Supplements, per Approved Model List SH261WE, and all subsequent FAA approved revisions to these documents.. USDA Forest Service - [STC SH2778NM](https://openairdocs.org/stc/SH2778NM): Removal passenger seats. Air Methods Corporation - [STC SH3312SO](https://openairdocs.org/stc/SH3312SO): Manufacture of replacement windows.. Bell Helicopter Textron Inc. - [STC SH3314SO](https://openairdocs.org/stc/SH3314SO): Installation of pushout window assembly.. Bell Helicopter Textron Inc. - [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 SH3712SW](https://openairdocs.org/stc/SH3712SW): Installation of replacement windshield.. Bell Helicopter Textron Inc. - [STC SH3722NM](https://openairdocs.org/stc/SH3722NM): Installation of closed circuit refueling reciever P/N 750000-5.. H R Textron Inc - [STC SH400NW](https://openairdocs.org/stc/SH400NW): Installation of left hand bubble door with or without duplicate engine instruments. WSH, LLC - [STC SH4331NM](https://openairdocs.org/stc/SH4331NM): Installing a Model 7700 Modular Electrical System.. Simplex Manufacturing Company - [STC SH464NW](https://openairdocs.org/stc/SH464NW): Incorporation of a weighing system for external load operations.. Measurement Systems Intl Inc - [STC SH46NW](https://openairdocs.org/stc/SH46NW): Installation of an electronic weighing system, for monitoring cargo hook weight, in accordance with Measurement Systems International, Inc., Installation drawing No. D00409, Rev. A, or Drawing D00471, Rev. IR.. Measurement Systems Intl Inc - [STC SH5236NM](https://openairdocs.org/stc/SH5236NM): Installation of passenger grab bars. Air Methods Corporation - [STC SH897NE](https://openairdocs.org/stc/SH897NE): Installation of passenger access step.. Dart Aerospace Limited - [STC SH975NE](https://openairdocs.org/stc/SH975NE): Installation of Dart Aerospace Ltd. Cargo Mirror in accordance with FAA Approved Model List (AML) SH975NE. Dart Aerospace Limited - [STC SR00145IB](https://openairdocs.org/stc/SR00145IB): Installation of LH and RH Vertical Reference Door(s). Transwest Helicopters Ltd. - [STC SR00180AT](https://openairdocs.org/stc/SR00180AT): Installation of replacement door handle.. Bell Helicopter Textron Inc. - [STC SR00213IB](https://openairdocs.org/stc/SR00213IB): Modification of Swashplate Inner Ring Assembly. McDermott Aviation Ltd. - [STC SR00408SE](https://openairdocs.org/stc/SR00408SE): Fabrication of Onboard Systems Model E-62 Cargo Hook Load Weigh System. Onboard Systems International LLC - [STC SR00488DE](https://openairdocs.org/stc/SR00488DE): Reconfigure aircraft to a maximum seating of 9 passengers.. Central Copters Inc. - [STC SR00513NY](https://openairdocs.org/stc/SR00513NY): Installation of HeliRappel.. Dart Aerospace Limited - [STC SR00563NY](https://openairdocs.org/stc/SR00563NY): Installation of Skidtubes and associated saddles. Dart Aerospace Limited - [STC SR00571NY](https://openairdocs.org/stc/SR00571NY): Installation of Bearpaws.. Dart Aerospace Limited - [STC SR00592NY](https://openairdocs.org/stc/SR00592NY): Installation of Dart Aerospace fixed step.. Dart Aerospace Limited - [STC SR00597NY](https://openairdocs.org/stc/SR00597NY): Installation of folding cabin step.. Dart Aerospace Limited - [STC SR00696NY](https://openairdocs.org/stc/SR00696NY): Installation of external utility basket.. Dart Aerospace Limited - [STC SR00798DE](https://openairdocs.org/stc/SR00798DE): Installation of Torque Meter Junction Box Relocation. Erickson Incorporated - [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models.. Technisonic Industries Limited - [STC SR00939NY](https://openairdocs.org/stc/SR00939NY): Installation of Vertical Reference Door with left seat operation provisions.. Dart Aerospace Ltd. - [STC SR00957NY](https://openairdocs.org/stc/SR00957NY): Installation of external cargo hook release system for co-pilot position.. Dart Aerospace Ltd. - [STC SR01298NY](https://openairdocs.org/stc/SR01298NY): Installation of replacement crosstubes P/N D212-664.. Dart Aerospace Limited - [STC SR01446NY](https://openairdocs.org/stc/SR01446NY): Installation of Serviceability Kit: Auxiliary cowl latches, cockpit door wear pads and cabin door handle.. Dart Aerospace Ltd. - [STC SR01742NY](https://openairdocs.org/stc/SR01742NY): Installation of extended height landing gear.. Dart Aerospace Limited - [STC SR01787LA](https://openairdocs.org/stc/SR01787LA): Installation of Nine Passenger Or Less Seating.. Helimax Aviation Inc - [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System.. Atlantic Avionics Inc. - [STC SR01903NY](https://openairdocs.org/stc/SR01903NY): Installation of a modified co-pilot seat.. Transwest Helicopters Ltd - [STC SR01997NY](https://openairdocs.org/stc/SR01997NY): Manufacture of Shoulder Harness Kits.. Dart Aerospace Limited - [STC SR02055NY](https://openairdocs.org/stc/SR02055NY): Installation of Fuel Purge Canister to be done in accordance with Transport Canada approved DART Aerospace Ltd. Installation Instructions, IIN-D412-706, Revision A, dated November 30, 2004, or later Transport Canada approved revision.. Dart Aerospace Limited - [STC SR02058NY](https://openairdocs.org/stc/SR02058NY): The installation of replacement window kits in accordance with Dart Aerospace Ltd. Installation Instructions IIN-D412-709, Rev. A dated December 5, 2003 on Bell models 205A, 205A-1, 205B, 212, 412, 412CF, 412EP, 214B and 214B-1 aircraft.. Dart Aerospace Limited - [STC SR02086NY](https://openairdocs.org/stc/SR02086NY): Installation of a Spacedoor.. Dart Aerospace Limited - [STC SR02091NY](https://openairdocs.org/stc/SR02091NY): Installation of a D212-722 avionics riser console in the cockpit as a replacement for the center console.. Dart Aerospace Limited - [STC SR02094NY](https://openairdocs.org/stc/SR02094NY): Installation of GPS Receiver and Gimbal Mount System.. Dart Aerospace Ltd. - [STC SR02270SE](https://openairdocs.org/stc/SR02270SE): Fabrication and installation of Geneva Aviation Audio System. AEM USA Inc. All 80: https://openairdocs.org/model/bell-214b/stcs.md ## NTSB investigations (4) 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 ANC93FA033](https://openairdocs.org/ntsb/ANC93FA033), Feb 19, 1993: Bell 214B1 (N114CR), Ketchikan, AK, destroyed, 2 fatal. Probable cause: INADEQUATE MAINTENANCE OF THE HYDRAULIC SERVO ACTUATOR WHICH LED TO THE FATIGUE FAILURE AND LOSS OF FLIGHT CONTROL. IN ADDITION, THE FLIGHTCREW DID NOT, OR WAS UNABLE TO, JETTISON THE EXTERNAL LOAD.… - [NTSB CHI91LA082](https://openairdocs.org/ntsb/CHI91LA082), Jan 26, 1991: Cessna 170B (N4414B), Rochester, IN, substantial damage. Probable cause: THE PILOT-IN-COMMAND'S INADEQUATE COMPENSATION FOR WIND CONDITIONS. A FACTOR CONTRIBUTING TO THE ACCIDENT WAS THE CROSSWIND. - [NTSB SEA89LA016](https://openairdocs.org/ntsb/SEA89LA016), Nov 4, 1988: Bell 214B-1 (N514RM), Ketchikan, AK, substantial damage - [NTSB SEA83FA033](https://openairdocs.org/ntsb/SEA83FA033), Dec 18, 1982: Bell 214B (N244PH), Near Randle, WA, destroyed, 2 fatal ## FAA accident and incident reports (5) 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 19930219002899A](https://openairdocs.org/incident/19930219002899A), Feb 19, 1993: Bell 214B1 (N114CR), Ketchikan, AK, Destroyed, 2 fatal. Hovering with logs on long line. Lost control. Log load not released. Crashed. Rotor cylic hydraulic servo failed. - [Accident 19910126001039A](https://openairdocs.org/incident/19910126001039A), Jan 26, 1991: Cessna 170B (N4414B), Rochester, IN, Substantial damage. Reported wind gust on landing veered aircraft off runway. Tried to go around but hit brush across railroad bed. - [Accident 19881104049589A](https://openairdocs.org/incident/19881104049589A), Nov 4, 1988: Bell 214B1 (N514RM), Ketchikan, AK, Substantial damage. Main rotor blade delaminated while in a hover with a long line attached. Was able to make a safe landing. - [Incident 19870411033419I](https://openairdocs.org/incident/19870411033419I), Apr 11, 1987: Bell 214B (N514RM), Mancos, CO. Helicopter settled due to a wind gust while setting a bridge unit on a powerline tower. Tower crewman injured. - [Accident 19821218064369A](https://openairdocs.org/incident/19821218064369A), Dec 18, 1982: Bell 214B (N244PH), Randle, WA, Destroyed. Flew into a fogbank shortly after a night takeoff. Impacted a fog-obscured mountainside. Misjudged rising terrain. ## Service difficulty reports (13) As reported by operators and repair stations, by the model named in the report. - [SDR XJ2R201609120001](https://openairdocs.org/sdr/XJ2R201609120001), Sep 12, 2016: CYLINDER. LEAKING. SERVO 214-076-146-101 REMOVED FOR EXTERNAL LEAKAGE FOR REPAIR, DISCOVERED UPPER CYLINDER CRACKED DURING TEST. - [SDR JYDR20150910002](https://openairdocs.org/sdr/JYDR20150910002), Sep 10, 2015: CONTROL HORN. CRACKED. CRACK FOUND ON RT EAR OF CONTROL HORN DURING NDT. - [SDR JYDR20150910001](https://openairdocs.org/sdr/JYDR20150910001), Sep 10, 2015: CONTROL HORN. CRACKED. CRACK FOUND ON RT EAR OF CONTROL HORN DURING NDT. - [SDR CA120504004](https://openairdocs.org/sdr/CA120504004), May 1, 2012: TURBINE WHEEL. DAMAGED. (CAN) OPERATOR IS IMPROPERLY MARKING PARTS THAT THEY MFG, PURSUANT TO A LICENSING AGREEMENT WITH OEM MFG. REF: MFG AO 230-91 IAW CHAPTER 561 AERONAUTICAL PRODUC - [SDR CA060524008](https://openairdocs.org/sdr/CA060524008), May 24, 2006: SPINDLE. BROKEN. DONT HAVE ANY OTHER INFO AT THIS TIME, AS THIS INCIDENT JUST OCCURRED THIS MORNING. WILL ADD INFORMATION AS IT COMES IN. THIS INCIDENT SEEMS VERY SIMILAR TO ONE - [SDR CA021108017](https://openairdocs.org/sdr/CA021108017), May 28, 2002: WIRE. CHAFED. (CAN) WHILE HOVERING DURING HELI-LOGGING OPERATIONS, PILOT NOTICED SMOKE AND SPARKS ORIGINATING FROM THE LT OVERHEAD CCT BREAKER PANEL. THE PILOT INITIATED AN U - [SDR 20010508CW013](https://openairdocs.org/sdr/20010508CW013), Apr 16, 2001: HOUSING. GOUGED. GOUGE PLUS LINER IND. BELOW GOUGE. - [SDR 20010419CW008](https://openairdocs.org/sdr/20010419CW008), Mar 19, 2001: LEVER. CRACKED. CRACKING DETECTED ON TANG EDGE OF LEVER ASSEMBLY. - [SDR 20010413CW007](https://openairdocs.org/sdr/20010413CW007), Mar 19, 2001: HOUSING. CRACKED. CRACKS DETECTED ON FLANGE MOUNTS. REPLACED SERVO UNIT FROM SURPLUS. - [SDR 20010206CW013](https://openairdocs.org/sdr/20010206CW013), Oct 27, 2000: BEARING. CRACKED. CRACKS DETECTED DURING OVERHAUL. - [SDR CA010921003](https://openairdocs.org/sdr/CA010921003), Sep 26, 1999: HOSE. DETERIORATED. (CAN) OIL SOAKED HOSE CLAMP CAUSED RUBBER TO DETERIORATE ON THE HOSE CLAMP WHICH CAUSED THE STEEL BRADING AROUND THE HOSE TO ERODE, THUS CAUSING THE HOSE TO LEA - [SDR 99ZZZX4186](https://openairdocs.org/sdr/99ZZZX4186), Sep 17, 1999: CYLINDER. DAMAGED. CYLINDER ON SERVO ACTUATOR IS DAMAGED. - [SDR 99ZZZX4185](https://openairdocs.org/sdr/99ZZZX4185), Sep 17, 1999: BEARING. DAMAGED. BEARING DAMAGED IN THE SERVO ACTUATOR. --- From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.