# N124EH: Messerschmitt-Boelkow-Blohm BO-105S

- Status: Valid registration
- Airframe: [Messerschmitt-Boelkow-Blohm BO-105S](https://openairdocs.org/model/messerschmitt-boelkow-blohm-bo-105s) (registry code 5626006, 5 seats)
- Engine: [Allison 250-C20 series](https://openairdocs.org/engine/allison-250-c20-series) (registry code 03020)
- Data sheets: [TCDS H3EU](https://openairdocs.org/tcds/H3EU) (Airbus Helicopters Deutschland GmbH (AHD)), [TCDS E4CE](https://openairdocs.org/tcds/E4CE) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: S559
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: July 8, 1999
- Certificate issued: March 11, 2026
- Expires: March 31, 2033
- Mode S code: A062FA
- Registered owner: [Jbp Aviation LLC](https://openairdocs.org/faa-owner/JBP%20AVIATION%20LLC)
- Location: [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson)
- Owner type: LLC
- Owner's area on the map: 35.9399° N, 115.0563° W: Placed by OpenAirDocs at the center of ZIP code 89044, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=124EH
- Page: https://openairdocs.org/aircraft/N124EH

From the FAA registry file of October 24, 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 Allison 250-C20 model are included.

## ADs that may apply (OpenAirDocs): 52 in force

### Matched by airframe (Messerschmitt-Boelkow-Blohm BO-105S)

- [AD 2025-25-05](https://openairdocs.org/ad/2025-25-05): Rotorcraft Flight Control · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105S and 6 more. Effective Dec 31, 2025
- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024
- [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 2023-03-01](https://openairdocs.org/ad/2023-03-01): Main Rotor System · ECD Superlifter Conversion Kit 105-800331 (Eurocopter Deutschland STC SR00043RD). Effective Feb 21, 2023
- [AD 2022-24-07](https://openairdocs.org/ad/2022-24-07): Main Rotor Drive System · ECD Superlifter Conversion Kit 105-800331 (Eurocopter Deutschland STC SR00043RD). Effective Jan 6, 2023
- [AD 2021-13-14](https://openairdocs.org/ad/2021-13-14): Cabin Equipment/Furnishings · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-3 and 1 more. Effective Aug 17, 2021
- [AD 2021-10-21](https://openairdocs.org/ad/2021-10-21): Main Rotor System · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-3 and 9 more. Effective Jul 7, 2021
- [AD 2021-07-08](https://openairdocs.org/ad/2021-07-08): Main Rotor Mast/Swashplate · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 2 more. Effective Apr 30, 2021
- [AD 2021-05-07](https://openairdocs.org/ad/2021-05-07): Electrical Power System Wiring · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105S and 6 more. Effective Apr 16, 2021
- [AD 2017-05-03](https://openairdocs.org/ad/2017-05-03): Main Rotor Blade · Airbus Helicopters Deutschland BO-105C, BO-105LS A-3 and BO-105S. Effective Mar 17, 2017
- [AD 2015-19-14](https://openairdocs.org/ad/2015-19-14): Main Gear Box · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Nov 3, 2015
- [AD 2013-20-17](https://openairdocs.org/ad/2013-20-17): Turbine Section · Airbus Helicopters Deutschland BO-105C and BO-105S. Effective Dec 13, 2013
- [AD 2013-16-13](https://openairdocs.org/ad/2013-16-13): Tail Rotor Head · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 8 more. Effective Sep 27, 2013
- [AD 2013-16-06](https://openairdocs.org/ad/2013-16-06): Main Rotor Blades · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 2 more. Effective Sep 13, 2013
- [AD 2013-11-15](https://openairdocs.org/ad/2013-11-15): Main Rotor Control · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 14 more. Effective Jul 26, 2013
- [AD 2011-25-01](https://openairdocs.org/ad/2011-25-01): Liferafts · Agusta AB412, AB412 EP, 206A and 23 more. Effective Jan 17, 2012
- [AD 2000-17-08](https://openairdocs.org/ad/2000-17-08): Tension-Torsion (TT) Strap · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 1 more. Effective Oct 2, 2000
- [AD 96-08-04](https://openairdocs.org/ad/96-08-04): Tandem Hydraulic System · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 1 more. Effective May 22, 1996
- [AD 90-23-08](https://openairdocs.org/ad/90-23-08): Continuous Ignition System · Airbus Helicopters Deutschland BO-105C and BO-105S. Effective Dec 3, 1990
- [AD 87-26-02 R1](https://openairdocs.org/ad/87-26-02-R1): Main Rotor Control Rods · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 2 more. Effective Sep 26, 1989
- [AD 87-09-03](https://openairdocs.org/ad/87-09-03): Rotor Blade Bolts · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 6 more. Effective Aug 26, 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 85-26-02](https://openairdocs.org/ad/85-26-02): Hydraulic Actuator · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Feb 25, 1986
- [AD 85-08-01](https://openairdocs.org/ad/85-08-01): Vertical Fin Spar And Skins · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Apr 26, 1985
- [AD 81-03-01](https://openairdocs.org/ad/81-03-01): Drive Shafts · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Jan 29, 1981
- [AD 80-16-01 R1](https://openairdocs.org/ad/80-16-01-R1): Engine Cowling Assemblies · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Sep 19, 1980
- [AD 80-10-02](https://openairdocs.org/ad/80-10-02): Tail Rotor System · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective May 1, 1980
- [AD 79-24-06](https://openairdocs.org/ad/79-24-06): Tail Rotor Blades · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Dec 10, 1979
- [AD 78-19-03](https://openairdocs.org/ad/78-19-03): Safety Belts · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Oct 18, 1978
- [AD 77-11-02](https://openairdocs.org/ad/77-11-02): Main Rotor · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S. Effective Jun 14, 1977
- [AD 84-16-01](https://openairdocs.org/ad/84-16-01): Tail Rotor Blade Inspection · Airbus Helicopters Deutschland BO-105A, BO-105C and BO-105S

### Matched by engine (Allison 250-C20 series)

- [AD 2022-10-06](https://openairdocs.org/ad/2022-10-06): Turbine Section · Rolls-Royce 250-C20, 250-C20B, 250-C20C (T63-A-720) and 9 more. Effective Jun 28, 2022
- [AD 2018-13-01](https://openairdocs.org/ad/2018-13-01): Turbine Governor · Rolls-Royce 250-C10 (T63-A-5), 250-C18, 250-C18A and 24 more. Effective Aug 16, 2018
- [AD 2006-16-04](https://openairdocs.org/ad/2006-16-04): Inspection of the fuel nozzle screen · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 43 more. Effective Sep 7, 2006
- [AD 2006-13-06](https://openairdocs.org/ad/2006-13-06): Gas producer rotor assembly tie bolts · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 16 more. Effective Jul 26, 2006
- [AD 2005-10-13](https://openairdocs.org/ad/2005-10-13): Turbine energy absorbing ring · Rolls-Royce 250-B17B, 250-B17C, 250-B17D and 7 more. Effective Jun 22, 2005
- [AD 2004-26-09](https://openairdocs.org/ad/2004-26-09): Compressor Adaptor Couplings · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 8 more. Effective Feb 8, 2005
- [AD 2001-24-12](https://openairdocs.org/ad/2001-24-12): Helical Torquemeter Gearshaft Assembly · Rolls-Royce 250-B17, 250-B17C, 250-B17D and 13 more. Effective Dec 19, 2001
- [AD 98-24-28](https://openairdocs.org/ad/98-24-28): Main Fuel Control Bellows · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 36 more. Effective Jan 7, 1999
- [AD 96-19-01](https://openairdocs.org/ad/96-19-01): Superior Air Parts Manufacture Approval (PMA) Bearings · Rolls-Royce 250-B15G, 250-B17F, 250-B17F/1 and 17 more. Effective Sep 26, 1996
- [AD 93-25-05](https://openairdocs.org/ad/93-25-05): Driveshaft Flex Coupling Bolts, Bushings, and Nuts · Rolls-Royce 250-C20S with STC SE2352NM. Effective Feb 22, 1994
- [AD 88-17-01](https://openairdocs.org/ad/88-17-01): Fuel Controls · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 26 more. Effective Mar 1, 1989
- [AD 83-03-02 R1](https://openairdocs.org/ad/83-03-02-R1): Slotted Third Stage Turbine Wheels · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 5 more. Effective Feb 28, 1984
- [AD 82-24-05](https://openairdocs.org/ad/82-24-05): Control Assembly and Power Turbine Governor Assembly · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 43 more. Effective Nov 26, 1982
- [AD 82-13-03](https://openairdocs.org/ad/82-13-03): Modify Engine High Pressure Fuel Control Filter Assembly · Rolls-Royce 250-C20 and 250-C20B. Effective Jul 1, 1982
- [AD 79-21-01 R1](https://openairdocs.org/ad/79-21-01-R1): Third Stage Turbine Wheel Blade · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 3 more. Effective Jun 3, 1981
- [AD 78-14-08](https://openairdocs.org/ad/78-14-08): Fuel Pump Drive Spline · Rolls-Royce 250-C18, 250-C18A, 250-C18B and 3 more. Effective Oct 24, 1979
- [AD 77-15-12](https://openairdocs.org/ad/77-15-12): Power Turbine Coupling Nut · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 23 more. Effective Sep 23, 1977
- [AD 77-09-08](https://openairdocs.org/ad/77-09-08): Bleed Valve Diaphragm · Rolls-Royce 250-B17, 250-B17B, 250-C20 and 2 more. Effective Jul 18, 1977
- [AD 74-14-03](https://openairdocs.org/ad/74-14-03): Fuel Control Rigging · Rolls-Royce 250-C20. Effective Jul 10, 1974
- [AD 73-19-07](https://openairdocs.org/ad/73-19-07): Turbine Governor-To-Fuel Control Tube · Rolls-Royce 250-C20. Effective Sep 14, 1973
- [AD 72-03-06](https://openairdocs.org/ad/72-03-06): Turbine Wheels · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 9 more. Effective Feb 8, 1972

### 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 2021-10-14](https://openairdocs.org/ad/2021-10-14) (historical): Main Rotor System · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-3 and 1 more. Effective Jun 24, 2021
- [AD 2019-07-07](https://openairdocs.org/ad/2019-07-07) (historical): Main Rotor System · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-3 and 9 more. Effective May 24, 2019
- [AD 2002-13-06](https://openairdocs.org/ad/2002-13-06) (historical): Tension-torsion (T-T) straps · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 1 more. Effective Jul 15, 2002
- [AD 99-19-22](https://openairdocs.org/ad/99-19-22) (historical): TT Strap · Eurocopter Deutschland BO-105A, BO-105C, BO-105LS A-1 and 1 more. Effective Oct 25, 1999
- [AD 97-26-02](https://openairdocs.org/ad/97-26-02) (historical): Main Rotor Mast Flange Crack Inspection · Airbus Helicopters Deutschland BO-105A, BO-105C, BO-105LS A-1 and 2 more. Effective Dec 31, 1997
- [AD 2017-18-14](https://openairdocs.org/ad/2017-18-14) (historical): Turbine Section · Rolls-Royce 250-C20, 250-C20B, 250-C20F and 8 more. Effective Oct 13, 2017
- [AD 2015-02-22](https://openairdocs.org/ad/2015-02-22) (historical): Repetitive visual inspections · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 15 more. Effective Mar 9, 2015
- [AD 2012-14-06](https://openairdocs.org/ad/2012-14-06) (historical): Released turbine blades and shrouds · Rolls-Royce 250-C20, 250-C20B and 250-C20R/2. Effective Aug 14, 2012
- [AD 2004-24-09](https://openairdocs.org/ad/2004-24-09) (historical): Fuel nozzle · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 40 more. Effective Jan 5, 2005
- [AD 2001-20-51](https://openairdocs.org/ad/2001-20-51) (historical): Helical Torquemeter Gearshaft Assembly · 250-B17, 250-B17C, 250-B17D and 12 more

## Information bulletins (advisory) (2 in force)

- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008
- [SAIB CE-01-10](https://openairdocs.org/saib/CE-01-10): . Issued Jan 24, 2001

## NTSB investigations

None matched to N124EH.

## FAA accident and incident reports

None matched to N124EH.

## Service difficulty reports (23)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ERAA097497](https://openairdocs.org/sdr/ERAA097497), Sep 14, 2004: COVER. MISOVERHAULED. SUMP COVER AIR HOLE IS BLOCKED. RETURNING ON ERA REPAIR ORDER NR RW-900461 REQUESTING WARRANTY REPAIR.
- [SDR ERAA098178](https://openairdocs.org/sdr/ERAA098178), Aug 19, 2004: GOVERNOR. MALFUNCTIONED. GOVERNOR DROPS OUT OF SERVICE LIMITS. COMPONENTS WORN INTERNALLY. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A.
- [SDR ERAA097536](https://openairdocs.org/sdr/ERAA097536), Dec 30, 2003: GUIDE. INOPERATIVE. GUIDE ASSY INOPERABLE ACTION TAKEN: DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, POTTED AND TESTED. INSPETED AND REPAIRED IAW MBB BO105 REM 405.
- [SDR ERAA097535](https://openairdocs.org/sdr/ERAA097535), Dec 30, 2003: GUIDE. INOPERATIVE. GUIDE ASSY IS INOPERABLE. FOUND BROKEN SOCKET AND SWITCHES. 2 SCREWS CORRODED. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SWITCHES, SCREWS AND TEST
- [SDR ERAA094451](https://openairdocs.org/sdr/ERAA094451), Nov 16, 2003: SHAFT. SCORED. TAILROTOR SHAFTS SCORED. SENT FOR REPAIR. SHAFT BEYOND LIMITS. SCRAPPED IAW BO-105 MM CHAPTER 33 FIG 33-12 ACTION TAKEN: REMOVED AND SCRAPPED TAIL ROTOR SHAFT 5
- [SDR ERAA085148](https://openairdocs.org/sdr/ERAA085148), Feb 13, 2003: WIRE. BROKEN. GUIDE ASSY WILL NOT RESET. FOUND BROKEN WIRE. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET AND POTTED AND TESTED. INSTALLED NEW SOCKET AND FLAT SPRING
- [SDR ERAA085146](https://openairdocs.org/sdr/ERAA085146), Feb 13, 2003: WIRE. BROKEN. GUIDE ASSY HAS BROKEN WIRE. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET AND TESTED & POTTED. INSTALLED NEW FLAT SPRING & SLIDE BLOCK. REPAIRED IAW M 
- [SDR ERAA082716](https://openairdocs.org/sdr/ERAA082716), Nov 20, 2002: GOVERNOR. MALFUNCTIONED. UNABLE TO ADJUST FOR TORQUE SPLITS. PC, PY FITTINGS LOOSE. LEVER CAM WORN, O LEVER. REPLACED WORN PARTS FOUND DURING INSPECTIN IAW CMM 73-20-25. FUNCTIONALLY TE
- [SDR ERAA081161](https://openairdocs.org/sdr/ERAA081161), Sep 26, 2002: FUEL CONTROL. MALFUNCTIONED. NR 2 ENGINE HANGS AT 50 PERCENT N1 FOR 3-5 SECONDS THEN RAPIDLY ACCELS TO 537 DEGREES N1. REPLACEMENT FIXED PROBLEM. FUEL CONTROL OVERHAULED, CLOSE TO TX REQUIR
- [SDR ERAA080339](https://openairdocs.org/sdr/ERAA080339), Jun 11, 2002: BEARING. MAKING METAL. ENGINE MAKING METAL. INITIAL INSPECTION FOUND COMPRESSOR ATTACHMENT HARDWARE LOOSE. 2 1/2 BEARING MAKING METAL. ACTION TAKEN: INSTALLED NEW 2 1/2 BEARING AND PT
- [SDR ERAA080338](https://openairdocs.org/sdr/ERAA080338), Jun 11, 2002: SHAFT. CORRODED. ENGINE MAKING METAL. FOUND GEARSHAFT TEETH DAMAGED GEARBOX HOUSING CORRODED. ACTION TAKEN: INSTALLED NEW GEARSHAFT & OVERHAULED GEARBOX.
- [SDR ERAA080337](https://openairdocs.org/sdr/ERAA080337), Jun 11, 2002: FUEL CONTROL. OUT OF ADJUST. FCU OUT OF CALIBRATION. METERING VALVE FUEL FLOW SETTING FOUND LOW
- [SDR ERAA077295](https://openairdocs.org/sdr/ERAA077295), Nov 16, 2001: GEARSHAFT. WORN. ENGINE IS MAKING METAL. . STARTER GENERATOR GEARSHAFT IS WORN. ACTION TAKEN: INSTALLED NEW GEARSHAFT AND BEARINGS. COMPLIED WITH CEB A-1374 PRESSURE PROBE INSPE
- [SDR ERAA065950](https://openairdocs.org/sdr/ERAA065950), Jan 10, 2000: COMBUSTION CASE. MISOVERHAULED. COMBUSTION CASE REPAIRED AND RETURNED WITH AIR TUBE BOSS RETAINING RING NOT BEING MACHINED. COULD NOT BE INSTALLED ON AIRCRAFT.
- [SDR ERAA96284](https://openairdocs.org/sdr/ERAA96284), Jul 19, 1996: SCROLL. DAMAGED. SCROLL OVERHAULED 6-13-96 AND HAS THREAD DAMAGE TO STUD AS MARKED.
- [SDR ERAA96281](https://openairdocs.org/sdr/ERAA96281), Jul 16, 1996: GEAR. PITTED. FUEL CONTROL/OIL PUMP GEAR WAS O/H AND RETURNED TO ERA 7/10/96 RECEIVED BACK WITH PITS IN GEAR TEETH.
- [SDR ERAA96278](https://openairdocs.org/sdr/ERAA96278), Jul 15, 1996: VANE ASSY. FAILED. VANE ASSY SENT FOR OVERHAUL ON STANDARD AERO WORK ORDER L127225 2-9-96. VANE ASSY HAS -0- TSO AND STUB BROKE OFF DURING INSTALLATION.
- [SDR ERAA96246](https://openairdocs.org/sdr/ERAA96246), Jun 14, 1996: SUMP COVER. DEFECTIVE. PART SENT FOR OVERHAUL AND RETURNED TO ERA 9-18-95. LARGE U-RING SEALING SURFACE NOT TRUE. U-RING WILL NOT CRUSH EVENLY AND LEAKS.
- [SDR ERAA96244](https://openairdocs.org/sdr/ERAA96244), Jun 10, 1996: EXHAUST COLLECTO. MIS REPAIR. EXHAUST COLLECTOR SENT FOR OVERHAUL 3-18-96 AND RETURNED WITH 4TH NOZZLE TIGHT FIT INTO COLLECTOR.
- [SDR ERAA9589](https://openairdocs.org/sdr/ERAA9589), Jun 14, 1995: NOZZLE. DELAMINATED. SENT TO D/AIRMOTIVE ON ERA P.O. G108376 FOR OVERHAUL ON D/A WORK ORDER C67743 4/24/95. NOZZLE HAS -0- T.S.O. AND PORTION OF METALIZED AREA OF #4 BLADE TIP PATH 
- [SDR ERAA9582](https://openairdocs.org/sdr/ERAA9582), Jun 6, 1995: NOZZLE. DEFECTIVE. NOZZLE WAS SENT TO DALLAS AIRMOTIVE FOR OVERHAUL ON ERA P.O. G108745 , D/AIRMOTIVE W/O C67772 . PART HAS -0- HRS TSO AND .007 -.009 SEAL RUNOUT ALL TANG LOCATIO
- [SDR ERAA9579](https://openairdocs.org/sdr/ERAA9579), Jun 5, 1995: COUPLING. DEFECTIVE. SHAFT INDENTIONS BETWEEN SEAL GROOVES AND BELOW SPLINE END (NOT SCALLOPED END) - OD OF SHAFT AT THESE POINTS DIFFER. 1.093" AND 1.104".
- [SDR ERAA9577](https://openairdocs.org/sdr/ERAA9577), May 17, 1995: INNER SHAFT. PITTED. NEW INNER SHAFT THAT HAS PITS ON BEARING RACE.

## STCs that may be installed (OpenAirDocs) (111, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Messerschmitt-Boelkow-Blohm BO-105S)

- [STC SR00643SE](https://openairdocs.org/stc/SR00643SE): Installation of Geneva Aviation Video System. Turbolyft USA Corporation
- [STC SR02301SE](https://openairdocs.org/stc/SR02301SE): Installation of Geneva Aviation 28 - 14 VDC Power Converter. AEM USA 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 SR00119BO](https://openairdocs.org/stc/SR00119BO): Installation of a Newcomb Communications, Inc. CP-2 Satcom System in accordance with Newcomb Communications, Inc., Master Document List No. D000-0058, Revision B, dated April 12, 2000, or later FAA-approved revision. Outerlink Corporation
- [STC SR00808SE](https://openairdocs.org/stc/SR00808SE): Fabrication of Onboard Systems Model 200-253-00 (without load weigh) and Model 200-254-00 (with load weigh) Big Mouth Hook Kit and Model 200-290-00 (without load weigh) and Model 200-291-00 (with load weigh) 3.5KK Cargo Hook Kit. Onboard Systems International
- [STC SR01694SE](https://openairdocs.org/stc/SR01694SE): Fabrication of Onboard Systems Models 200-302-00 and 200-387-00 Talon LC Hydraulic Cargo Hook Kits without Load Weigh and Models 200-303-00 and 200-388-00 Talon LC Hydraulic Cargo Hook Kits with Load Weigh. Onboard Systems International
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SR00910SE](https://openairdocs.org/stc/SR00910SE): Replacement of the original landing gear skid tubes with DART Model D105-674-011 skid tubes. Dart Aerospace USA Inc
- [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC
- [STC SR02475AK](https://openairdocs.org/stc/SR02475AK): Installation of the Lexavia Integrated Systems LFS3500 Enhanced Vision System (EVS) on Part 27 Airbus Helicopters equipped with a panel-mounted Multi-Function Display (MFD), primary navigational display or dedicated display with the ability to display video imagery. Lexavia Integrated Systems
- [STC SR02470AK](https://openairdocs.org/stc/SR02470AK): Installation of the L-3 Communications NGT -1000/2000/2500 ADS-B System. ADS-B Technologies, LLC
- [STC SR02471AK](https://openairdocs.org/stc/SR02471AK): Installation of the L-3 Communications NGT -9000/9000R ADS-B System. ADS-B Technologies, LLC
- [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC
- [STC SH664NE](https://openairdocs.org/stc/SH664NE): Installation of a medical interior and life support equipment. Sikorsky Aircraft Corporation
- [STC SH5485SW](https://openairdocs.org/stc/SH5485SW): Replace existing baggage door hinges with quick removal hinges. Apical Industries, Inc. dba Dart Aerospace
- [STC SH3526SW](https://openairdocs.org/stc/SH3526SW): Installation of an INSCO rotor speed warning unit. Apical Industries, Inc. dba Dart Aerospace
- [STC SH3541SW](https://openairdocs.org/stc/SH3541SW): Installation of a wet engine and transmission oil pressure indicating system. Apical Industries, Inc. dba Dart Aerospace
- [STC SH5555SW](https://openairdocs.org/stc/SH5555SW): Installation of Michigan Dynamics airframe fuel filter system. Apical Industries, Inc. dba Dart Aerospace
- [STC SH5916SW](https://openairdocs.org/stc/SH5916SW): Installation of fuel pressure gauge and fuel pressure transducer. Apical Industries, Inc. dba Dart Aerospace
- [STC SH7685SW](https://openairdocs.org/stc/SH7685SW): Replacement of the MBB oil cooler fairing, MBB P/N 105-61802. Apical Industries, Inc. dba Dart Aerospace
- [STC SH8123SW](https://openairdocs.org/stc/SH8123SW): Installation of a low fuel audio warning horn. Apical Industries, Inc. dba Dart Aerospace
- [STC SH8445SW](https://openairdocs.org/stc/SH8445SW): Replacement of linear actuator for Bendix fuel control system on the Allison 250 C20B engine. Apical Industries, Inc. dba Dart Aerospace
- [STC SH8977SW](https://openairdocs.org/stc/SH8977SW): Installation of Parker Hannifan Airborne fuel pump. Apical Industries, Inc. dba Dart Aerospace
- [STC SR00856LA](https://openairdocs.org/stc/SR00856LA): Installation of Apical emergency float kit, p/n 20430. Apical Industries, Inc. dba Dart Aerospace
- [STC SR09219RC](https://openairdocs.org/stc/SR09219RC): Installation of 2 ejector pumps. Apical Industries, Inc. dba Dart Aerospace
- [STC SR09221RC](https://openairdocs.org/stc/SR09221RC): Replacement of main, aft, and supply fuel tanks. Apical Industries, Inc. dba Dart Aerospace
- [STC SR03449NY](https://openairdocs.org/stc/SR03449NY): Installation of a Sky Trac ISAT-200 Airborne Position/Data Communicator. Sky Trac Systems Ltd
- [STC SR01546SE](https://openairdocs.org/stc/SR01546SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SH8417SW](https://openairdocs.org/stc/SH8417SW): Installation of Benz Part Number PCS-111A Continuity Sensor in the engine, tail rotor gearbox, intermediate gearbox, and main transmission chip detectors. Meggitt, Orange County, Inc
- [STC SH1770SO](https://openairdocs.org/stc/SH1770SO): Installation of a controllable belly-mounted searchlight. Bell Helicopter Textron Inc
- [STC SR03027CH](https://openairdocs.org/stc/SR03027CH): Installation of Air Ambulance Unit in accordance with Ocean Air Master Data List, Report AC-BO105, Revision Original, Dated February 1st 2011 or later FAA Approved Revision. Ocean Air Aviation
- [STC SH4856SW](https://openairdocs.org/stc/SH4856SW): Installation of two-place back-to-back seat. CALSTAR
- [STC SR01802AT](https://openairdocs.org/stc/SR01802AT): Manufacture of Replacements Windows and Windshields in accordance with Aeronautical Accessories, Inc. Drawing List Report No. AA-98155, no revision, dated October 21, 1998, or later FAA approved revisions, and installation per Installation Instructions listed in that report. Bell Helicopter Textron Inc
- [STC SH308NE](https://openairdocs.org/stc/SH308NE): Replace existing starter-generators and install Aicraft Parts Corp. starter-generators. Shurka Aerospace Inc
- [STC SR09549RC](https://openairdocs.org/stc/SR09549RC): Installation of Night Vision Goggle Compatible Interior Lighting System. Ahlers Aerospace Inc
- [STC SR02189NY](https://openairdocs.org/stc/SR02189NY): Iinstallation of SkyTrac ISAT-100 Airborne Position/Data Communicator System. SkyTrac Systems Ltd
- [STC SR09208RC](https://openairdocs.org/stc/SR09208RC): Installation of Night Vision Goggle (NVG) compatible equipment for operation of ITT AV4949 Night Vision Imaging Systems. Air Methods Corporation
- [STC SR00169BO](https://openairdocs.org/stc/SR00169BO): Installation of Altair Avionics Corporation SmartCycle monitoring and recording system. Pratt & Whitney Engine Services Inc
- [STC SH5847SW](https://openairdocs.org/stc/SH5847SW): Installation of manual anti-ice system. Apical Industries Inc
- [STC SH7354SW](https://openairdocs.org/stc/SH7354SW): Installation of cabin interior. Apical Industries Inc
- [STC SH7355SW](https://openairdocs.org/stc/SH7355SW): Installation of cargo interior. Apical Industries Inc
- [STC SH7893SW](https://openairdocs.org/stc/SH7893SW): Installation of shoulder harnesses to the aft three passenger seats. Apical Industries Inc
- [STC SH7970SW](https://openairdocs.org/stc/SH7970SW): Modification of the dual hydraulic booster 7VE, P/N 105-45023 to P/N 105-83011 configuration. Apical Industries Inc
- [STC SH1315GL](https://openairdocs.org/stc/SH1315GL): Installation of a Shadin Co. engine trend monitoring system. Shadin Avionics
- [STC SH752GL](https://openairdocs.org/stc/SH752GL): Installation of a fuel flow indicating system. Shadin Avionics
- [STC SH7353SW](https://openairdocs.org/stc/SH7353SW): Installation of seat back shroud. Era Helicopters LLC
- [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models. Technisonic Industries Limited
- [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System. Atlantic Avionics Inc
- [STC SH1031EA-D](https://openairdocs.org/stc/SH1031EA-D): Installation of Airesearch Manufacturing environmental control unit. Approval is also eligible with the modification approved under STC SH1025EA issued 11/24/1975 or latest FAA approved revision. American Eurocopter Corporation

All 111: https://openairdocs.org/aircraft/N124EH/stcs.md

## Related

- Other Messerschmitt-Boelkow-Blohm BO-105S aircraft: https://openairdocs.org/model/messerschmitt-boelkow-blohm-bo-105s/aircraft.md
- The Allison 250-C20 series engine: https://openairdocs.org/engine/allison-250-c20-series.md

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