# TCDS R00003RD: Bell Textron Canada Limited

- Type: Type certificate data sheet
- Status: Current
- Holder: Bell Textron Canada Limited
- Revision: 5
- Revised: June 11, 2021
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27, Part 36
- Registered aircraft: 174, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/4d/0f/4d0fc8ba3ea576d8f9e8f7b48de80095affff3f41dee61ed5fa44fa1671b2c31
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/35F5323C150F634B862586F5006DE823.0001
- Page: https://openairdocs.org/tcds/R00003RD

## Models (1)

As the data sheet lists them.

- 429

## What the data sheet says

Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

```text
Page No. 1 2 3 4 5 6 
Rev. No. 4 5 0 0 5 4 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
R00003RD 
Revision 5 
Bell 
429 
June 11, 2021 
 
TYPE CERTIFICATE DATA SHEET NO. R00003RD 
 
This data sheet, which is part of type certificate No. R00003RD prescribes conditions and limitations under which the product for 
which type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. 
 
Type Certificate Holder Bell Textron Canada Limited 
 12800 rue de l’Avenir 
 Mirabel, Quebec 
 J7J 1R4 Canada 
 
Type Certificate Holder Record:  Bell Helicopter Textron Canada Limited was the previous name of TC holder. 
The company name history is presented below. 
 
Type Certificate Holder Period 
Bell Helicopter Textron Canada Limited 
Mirabel Quebec 
Prior to 16 December 2019 
Bell Textron Canada Limited 
Mirabel Quebec 
16 December 2019 
Present 
 
I. Model 429 (Normal Category; Category A), Approved June 30, 2009. 
 
Engine   2 Pratt and Whitney Canada PW207D1 or D2 engines (See NOTE 4) 
   FAA Engine Type Certificate Data Sheet E42NE 
 
Fuel ASTM-D-1655, Type Jet A, Jet A-1, and Jet B; MIL-DTL-5624 Grade JP-4 and Grade JP-5; and 
MIL-DTL-83133 Grade JP-8. 
 
 See Rotorcraft Flight Manual for fuel mixture and fuel temperature limitations. 
 
 Anti-icing fuel additive is required for operations at fuel temperatures below 4°C (39.2°F).  The 
maximum allowed concentration of fuel additives is 0.15% by volume. 
 
Oil Engine: MIL-PRF-23699; Transmission and Tail Rotor Gearbox: DOD-PRF-85734. For approved 
engine oil types, prohibition against mixing brands and for approved transmission and gearbox oil 
types refer to Maintenance Manual BHT-429-MM-01. 
 
Installed Engine Limits 
 Torque 
(%) Lb-ft 
Turbine Temperature 
oC  (oF) 
Gas Generator Speed 
% (RPM) 
Twin Engine Operation    
Take-Off (5 Min) (54.3) 523 900 (1652) 99.8 (57900) 
Max. Continuous (53.3) 513 850 (1562) 97.2 (56400) 
One Engine Inoperative    
30 sec. OEI (66.3) 638 990 (1814) 104.3 (60500) 
2 min. OEI (63.8) 614 950 (1742) 102.2 (59300) 
30 min OEI (60.2) 580 925 (1697) 101.2 (58700) 
Continuous OEI (59.5) 573 900 (1652) 99.8 (57900) 
 
 See Rotorcraft Flight Manual for transient limits 
 Output shaft speed limit is 104.5% (6271 RPM) 
 
Rotor Limits  
Power Off Power On 
Maximum 423 RPM 
107% 
Maximum 411 RPM 
104% 
Minimum 336 RPM 85% Minimum 391 RPM 99%

R00003RD Page 2 of 7 Revision 5 
 
Transmission Torque    
Limits 
Both Engines Operation Torque Limits % 
Take Off 100 
Maximum Continuous 100 
Transient 105 
 
One Engine Inoperative OEI 
 
30 Seconds OEI 66.3 
2 Minute OEI 59.1 
Continuous OEI 50.0 
 
Airspeed Limits Basic VNE (never exceed) is 155 KIAS. Decrease VNE for ambient conditions in accordance with 
the Airspeed Limitations placard in the Rotorcraft Flight Manual. 
 
C.G. Limits  Refer to approved Rotorcraft Flight Manual (See NOTE 3). 
 
Empty Weight CG Range See Maintenance Manual. 
 
Datum   Station 0 datum is 183.6 cm (72.3 in.) forward of the nose of the helicopter. 
 
Leveling Means Protractor or level placed on the crew or passenger floor or seat rails, both longitudinally and 
laterally. 
 
Maximum Weight  3175 kg (7000 lb.) Internal Loading 
(Mass)   3629 kg (8000 lb.) External Loading 
 
Altitude limits  Maximum altitude to 6096 m (20000 ft.) pressure altitude. 
 
OAT Limits Minimum -40°C (-40°F)    Maximum 51.7°C (125°F), decreasing with pressure altitude at a 
standard lapse rate of 2°C (3.6°F) per 1,0000 feet.  
 
Minimum crew  1 pilot (right seat). 
 
Maximum occupants 8 (includes crew). 
 
Maximum Baggage Refer to approved Rotorcraft Flight Manual for loading schedule. 
 
Fuel capacity  Refer to 429 Maintenance Manual for Fuel Capacity. 
 
Oil capacity  Refer to 429 Maintenance Manual for Oil Capacity. 
 
Rotor blade and   For rigging information refer to the 429 Maintenance Manual. 
Control movement 
 
Serial numbers eligible 57001 and subsequent.  
 
Import Requirements “Refer to the applicable bilateral agreement to verify eligibility for import into the United States of 
both new and used aircraft based on the scope of the agreement, to identify any required statements 
by the exporting authority on the export certificate of airworthiness (or equivalent document), and 
for procedures for coordinating exceptions to conformity statements on these documents. Refer to 
FAA Order 8130.2, Airworthiness Certification of Aircraft, for requirements for issuance of an 
airworthiness certificate for imported aircraft.” 
  
To be considered eligible for operation in the United States, each aircraft manufactured under this 
Type Certificate must have a U.S. Airworthiness Certificate that may be issued on the basis of the 
Canadian Department of Transport Certificate of Airworthiness for Export signed by the Minister 
of Transport containing the following statement: 
 
 “The rotorcraft covered by this certificate has been examined, tested and found to comply with the 
type design approved under Type Certificate R00003RD and to be in condition for safe operation.” 
 
 The approved type design for the model 429 consists of data listed on Bell top drawing 429-100-
001, Revision CG, or later approved revision for serial numbers 57001 and subsequent.

R00003RD Page 3 of 7 Revision 5 
 
 The U.S. airworthiness certification basis for aircraft certificated under 14 CFR 21.29 and exported 
by the country of manufacture is 14 CFR 21.183(c) or 21.185(c). 
 
Production Basis  None. See Import Requirements.

R00003RD  Page 4 of 7  Revision 5
Longitudinal Gross Weight / CG Envelope
FUSELAGE STATION - MILLIMETERS
5850  5900  5950
7800
7600
7400
3300
7200
7000  • 3200
6800  3100
o at Stn 5634 mr  (3175 Kg at Stn 5828 mm)
6600  3000
6400  2900
6200  2800
6000  2700
5800
700 lb at Sth 233.0 inch  2600
586 Kg at Stn 5918 ml
5600
2500
5400
2400
5200
2300
5000
4800  2100 b at Str  3 Kg at sin 5634 m  2200
4600  2100
4400  2000
4200  Ub at Sth 255.U inc  1900
96 Kg at Stn 5918 r
4000  1800
3800  T
220  222  224  226  228  230  232  234
FUSELAGE STATION - INCHES

R00003RD  Page 5 of 7  Revision 5
Lateral Gross Weight / CG Envelope
FUSELAGE STATION - MILLIMETERS
-75  -50  -25  25  50  75
7800
3500
7600
3400
7400
3300
7200
3200
7000
6800  3100
o bat at-1.9 inche  7000 lb at 1.9 inches
OR A-40 T  (3175 Kg at 48 mm)
6600  3000  GROSS WEIGHT - KILOGRAMS
GROSS WEIGHT - POUNDS  6400  2900
6200  2800
6000  2700
5800
2600
5600
5500 lb at -2.5 inches  5500 lb at 2.5 inches  2500
(2495 Kg at -64 mm)  (2495 Kg at 64 mm)
5400
2400
5200
2300
5000
2200
4800
4600  2100
4400  2000
4200  1900
4000
-3  -2  -1  2
LATERAL CG - INCHES

R00003RD Page 6 of 7 Revision 5 
 
 
Certification Basis  For approved MGW configuration of 3175 kg (7000 lb.) 
 
a) Title 14 part 27, dated October 2, 1964, amendment 27-1 through 27-40 including 
Appendix B criteria for instrument flight and Appendix C criteria for Category A 
performance, plus 
Compliance with the following additional requirements has been established: 
14 CFR part 27, Amendment 27-44 
 
b) Title 14 part 36 Amendment 36-1 through 36-28 
 
 c) Equivalent Safety Findings: 
 
  Number TC2486RD-R/A-2 
  14 CFR part 27.307(b)(5) Proof of Structure Landing Gear Drop Test 
  14 CFR part 27.723 Landing Gear Shock Absorption Tests 
  14 CFR part 27.725 Landing Gear Limit Drop Test 
  14 CFR part 27.727 Landing Gear Reserve Energy Absorption Drop Test 
 
  Number TC2486RD-R/S-2 
  14 CFR part 27 Appendix B VIII (b)(5)(i) Equipment, systems, and installations 
  14 CFR part 27 Appendix B VIII (b)(5)(ii) Equipment, systems, and installations 
 
  Number TC2486RD-R/F-2 
  14 CFR part 27.1545(b)(2) Airspeed Indicator 
 
  Number TC2486RD-R/P-1 
14 CFR part 29.903(b) as required by 14 CFR part 27 Appendix C, Category A Engine 
Isolation 
   
d) Special Condition made in accordance with FAR part 21.16 is as follows: 
 No. 27-017-SC Bell Helicopter Textron Canada Limited Model 429 Helicopters High 
Intensity Radiated Fields (HIRF), dated December 28, 2007. 
 
 e) Special Condition made in accordance with FAR part 21.16 is as follows: 
 SCA 2016-01; Rechargeable Lithium Batteries and Battery Systems, dated February 12, 
2016. 
 
 
Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see 
Certification Basis) must be installed in the helicopter for certification. 
 
In addition, the following items of equipment are required: 
 
Transport Canada approved Rotorcraft Flight Manual BHT-429-FM-1 dated June 19, 2009 or later 
approved revision. 
 
Refer to approved Rotorcraft Flight Manual for other approved mandatory and optional equipment. 
 
Service Information Bell Canada Service bulletins, structural repair manuals, vendor manuals, aircraft flight manuals, 
and overhaul and maintenance manuals, which contain a statement that the document is (Transport 
Canada) approved, are accepted by the FAA and are considered FAA approved.  These approvals 
pertain to the approved type design only. 
 
NOTE 1   This type certificate is for a Day/Night VFR operation (Single or Dual Pilot); Instrument Flight 
Rules (IFR) Operations (Single or Dual) Pilot: Category A, Normal Category Rotorcraft with 
engine isolation. 
 
NOTE 2 Certification Noise Levels are detailed in the approved Rotorcraft Flight Manual. 
 
NOTE 3 Current weight and balance report including list of required equipment and list of equipment 
included in certificated empty weight, and loading instructions when necessary must be provided 
for each helicopter at the time of original certification.  
 
NOTE 4 PW207D1 is a derivative of the PW207D with increased mechanical power and without fuel heater.

R00003RD Page 7 of 7 Revision 5 
 
The PW207D2 is identical to the PW207D1 but has a fuel heater installed. 
 
NOTE 5 The following placard must be displayed in front of and in clear view of the pilot: “THIS 
HELICOPTER MUST BE OPERATED IN COMPLIANCE WITH OPERATING LIMITATIONS 
SPECIFIED IN THE APPROVED FLIGHT MANUAL”.  
 
All placards listed in the approved flight manual must be installed in the specified locations. 
 
NOTE 6 Information essential to the proper maintenance of the helicopter is contained in the Manufacturer’s 
Maintenance Manual provided with each helicopter.  The approved service lives, mandatory 
inspections and other approved supplemental procedures of components are listed in approved 
Chapter 4, Airworthiness Limitations Section of the Maintenance Manual BHT-429-MM-01, dated 
June 19, 2009 or later approved revision.  
 
NOTE 7 The Bell 429 rotorcraft employs electronic engine controls, commonly named Full Authority 
Digital Engine Controls (FADEC) that are recognized to be more susceptible to Electromagnetic 
Interference (EMI) than rotorcraft that have manual (non-electronic) controls. EMI may be the 
result of radiated or conducted interference. For this reason, modifications that add or change 
systems that have the potential for EMI, must either be qualified to a standard acceptable to the 
FAA or tested at the time of installation for interference to the FADEC. This type of testing must 
employ the particular FADEC diagnostic techniques and external diagnostic techniques. The test 
procedure must be approved. 
 
NOTE 8 Deleted. 
 
NOTE 9 The model 429 incorporates an emergency OEI limit override function. When this feature is 
selected, damage to the engine and transmission is experienced and continued flight is not 
permitted. Use of this emergency power invalidates the airworthiness of the aircraft.  Maintenance 
in accordance with the model 429 Maintenance Manual is required to return the aircraft to an 
airworthy condition.  
 
NOTE 10 Effective December 16, 2019 the name Bell Helicopter Textron Canada Limited was revised to Bell Textron 
Canada Limited. 
  
 
 
….END….
```

## ADs (38, in force first)

- [AD 2026-08-10](https://openairdocs.org/ad/2026-08-10): Passenger compartment equipment · B/E Aerospace Fischer Medical Seat 230/305, EC135P1, EC135T1 and 19 more. Effective May 11, 2026
- [AD 2026-06-02](https://openairdocs.org/ad/2026-06-02): Rotorcraft flight control · Bell Textron Canada 429. Effective Apr 24, 2026
- [AD 2024-07-51](https://openairdocs.org/ad/2024-07-51): Tail Rotor Blades · Bell Textron Canada 429. Effective Jun 10, 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 2022-20-11](https://openairdocs.org/ad/2022-20-11): Rotorcraft tailboom · Bell Textron Canada 429. Effective Nov 28, 2022
- [AD 2022-09-07](https://openairdocs.org/ad/2022-09-07): Tail Rotor Control System · Bell Textron Canada 429. Effective May 31, 2022
- [AD 2022-08-11](https://openairdocs.org/ad/2022-08-11): Indicating/Recording System · Bell Textron Canada 429. Effective May 27, 2022
- [AD 2022-06-20](https://openairdocs.org/ad/2022-06-20): Flight Control System · Bell Textron Canada 429. Effective Apr 26, 2022
- [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 2021-20-11](https://openairdocs.org/ad/2021-20-11): Rotorcraft Flight Control · Bell Textron Canada 429. Effective Nov 22, 2021
- [AD 2021-18-16](https://openairdocs.org/ad/2021-18-16): Tail Rotor Drive System, Tail Rotor Gearbox · Bell Textron Canada 429. Effective Nov 1, 2021
- [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 2021-18-10](https://openairdocs.org/ad/2021-18-10): Tail Rotor Control System · Bell Textron Canada 429. Effective Oct 12, 2021
- [AD 2021-13-15](https://openairdocs.org/ad/2021-13-15): Landing Gear Systems, Emergency Equipment · Bell Textron Canada 429. Effective Jul 29, 2021
- [AD 2021-11-13](https://openairdocs.org/ad/2021-11-13): Emergency Flotation System (EFS) · Bell Textron Canada 429. Effective Jul 15, 2021
- [AD 2021-03-13](https://openairdocs.org/ad/2021-03-13): Main rotor system · Bell Textron Canada 429. Effective Apr 1, 2021
- [AD 2020-17-10](https://openairdocs.org/ad/2020-17-10): Tail Rotor System · Bell Helicopter Textron Canada 429. Effective Sep 21, 2020
- [AD 2020-04-21](https://openairdocs.org/ad/2020-04-21): Tail Rotor System · Bell Helicopter Textron Canada 429. Effective Mar 31, 2020
- [AD 2019-06-04](https://openairdocs.org/ad/2019-06-04): Main Rotor System · Bell Helicopter Textron Canada 429. Effective May 7, 2019
- [AD 2019-03-05](https://openairdocs.org/ad/2019-03-05): Landing Gear System · Bell Helicopter Textron Canada 429. Effective Mar 26, 2019
- [AD 2018-21-15](https://openairdocs.org/ad/2018-21-15): Standard Practices/Structures · Bell Helicopter Textron Canada 429. Effective Nov 27, 2018
- [AD 2018-16-51](https://openairdocs.org/ad/2018-16-51): Tail Rotor Gearbox · Bell Helicopter Textron Canada 429. Effective Nov 6, 2018
- [AD 2018-14-07](https://openairdocs.org/ad/2018-14-07): Placards and Markings · Bell Helicopter Textron Canada 429. Effective Aug 16, 2018
- [AD 2017-15-13](https://openairdocs.org/ad/2017-15-13): Landing Gear System · Bell Helicopter Textron Canada 429. Effective Aug 31, 2017
- [AD 2017-05-51](https://openairdocs.org/ad/2017-05-51): Cabin Cooling System · Bell Helicopter Textron Canada 429. Effective Apr 25, 2017
- [AD 2016-20-01](https://openairdocs.org/ad/2016-20-01): Engine and Transmission Lubrication System · Bell Helicopter Textron Canada 427 and 429. Effective Oct 17, 2016
- [AD 2015-17-02](https://openairdocs.org/ad/2015-17-02): Main Rotor Drive System · Bell Helicopter Textron Canada 206L-4, 407, 427 and 1 more. Effective Sep 24, 2015
- [AD 2012-26-15 R1](https://openairdocs.org/ad/2012-26-15-R1): Navigation · Agusta AW139, A318-111, A318-112 and 70 more. Effective Dec 3, 2014
- [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 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 2020-20-06](https://openairdocs.org/ad/2020-20-06) (historical): Flight Control System · Bell Helicopter Textron Canada 429. Effective Oct 30, 2020
- [AD 2019-11-05](https://openairdocs.org/ad/2019-11-05) (historical): Tail Rotor Control System · Bell Helicopter Textron Canada 429. Effective Jul 12, 2019
- [AD 2017-13-03](https://openairdocs.org/ad/2017-13-03) (historical): Standard Practices/Structures · Bell Helicopter Textron Canada 429. Effective Jul 27, 2017
- [AD 2016-02-06](https://openairdocs.org/ad/2016-02-06) (historical): Tail Rotor System · Bell Helicopter Textron Canada 429. Effective Feb 2, 2016
- [AD 2015-22-02](https://openairdocs.org/ad/2015-22-02) (historical): Tail Rotor Control System · Bell Helicopter Textron Canada 429. Effective Nov 12, 2015
- [AD 2012-26-15](https://openairdocs.org/ad/2012-26-15) (historical): Navigation · Agusta AW139, A318-111, A318-112 and 71 more. Effective Jan 24, 2013
- [AD 2015-16-51](https://openairdocs.org/ad/2015-16-51) (historical): Tail Rotor Control System · Bell Helicopter Textron Canada 429
- [AD 2018-15-51](https://openairdocs.org/ad/2018-15-51) (historical): Tail Rotor Gearbox · Bell Helicopter Textron Canada 429

## Registered aircraft by registry model (OpenAirDocs)

- [Bell Helicopter Textron Canada 429](https://openairdocs.org/model/bell-helicopter-textron-canada-429): 102 aircraft (registry code 1182158)
- [Bell Textron Canada 429](https://openairdocs.org/model/bell-textron-canada-429): 72 aircraft (registry code 1182220)

## STCs approved under this data sheet (60, first 50)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC SR03168CH](https://openairdocs.org/stc/SR03168CH): Installation of Heli-Preheat System, P/N TA2584-1 for 115 volt application. Hartzell Propeller LLC
- [STC SR12063AK](https://openairdocs.org/stc/SR12063AK): Installation of JJASPP Engineering Services Six Place Seating. JJASPP Engineering Services – Alaska LLC
- [STC SR04262AT](https://openairdocs.org/stc/SR04262AT): Installation of Aerolite Emergency Medical System (EMS) interior P/N 429-0036800-501. Aerolite America LLC
- [STC SR04711NY](https://openairdocs.org/stc/SR04711NY): Replacement of Luminator LS400 LED searchlight (steerable landing light). Sterling Helicopter
- [STC SR00532SE](https://openairdocs.org/stc/SR00532SE): Installation of Certified Technology quick release door pins.. Certified Technology
- [STC SR02806SE](https://openairdocs.org/stc/SR02806SE): Installation of dual hook cargo system for carrying Human External Cargo (HEC) and Non-human External Cargo
(NHEC) loads,. Onboard Systems International LLC
- [STC SR00782DE](https://openairdocs.org/stc/SR00782DE): Approval of a seating configuration to allow flight operations with the left hand pilot seat removed. Bell Textron Inc.
- [STC SR00791DE](https://openairdocs.org/stc/SR00791DE): Installation of the skid-gear mounted step to assist in external hoist operations. Bell Textron Inc.
- [STC SR00829DE](https://openairdocs.org/stc/SR00829DE): Installation of Baggage Pallet. Bell Textron Inc.
- [STC SR04705NY](https://openairdocs.org/stc/SR04705NY): Installation of Astronics (Max-Viz) Model 1400 Enhanced Vision System (EVS). Avio Design Group Inc
- [STC SR04213AT](https://openairdocs.org/stc/SR04213AT): Installation of a barrier net. Bell Helicopter Textron Inc.
- [STC SR04643NY](https://openairdocs.org/stc/SR04643NY): Installation of the Floor Protection Kit. Alpine Aerotech LP
- [STC SR01079DE](https://openairdocs.org/stc/SR01079DE): Installation of the Green Power Monitoring Systems (GPMS) Foresight MX Condition Monitoring System. Green Power Monitoring Systems
- [STC SR01068DE](https://openairdocs.org/stc/SR01068DE): Installation of External Equipment Mounting Provisions. Fulcrum Concepts LLC
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR11247DS](https://openairdocs.org/stc/SR11247DS): Installation of Connected Aircraft Interface Residing On-board (CAIRO) System. Bell Helicopter Textron Inc.
- [STC SR04489CH](https://openairdocs.org/stc/SR04489CH): EMS conversion in accordance with Spectrum Aeromed Master Drawing List 7015DL, Revision: - (Initial), dated June 17, 2020, or later FAA approved revisions.. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SR00708DE-D](https://openairdocs.org/stc/SR00708DE-D): Installation of Enhanced Cockpit Avionics Systems.. Air Methods Corporation
- [STC SR03317NY](https://openairdocs.org/stc/SR03317NY): Fixed Cabin Step Installation. Dart Aerospace Limited
- [STC SR03470NY](https://openairdocs.org/stc/SR03470NY): Installation of EMS Equipment P/N 429-0029300-501 in the Cabin. Aerolite AG
- [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SR04321NY](https://openairdocs.org/stc/SR04321NY): Installation of Deep Snow Kit. Alpine Aerotech LP
- [STC SR04174NY](https://openairdocs.org/stc/SR04174NY): Installation of the Wearplate Kits. Dart Aerospace Limited
- [STC SR02600SE](https://openairdocs.org/stc/SR02600SE): Installation of a Supplemental Lighting System manufactured and installed. Aviation Specialties Unlimited Inc.
- [STC SR00704DE-D](https://openairdocs.org/stc/SR00704DE-D): Installation of Emergency Medical Services Interior and Systems. Air Methods Corporation
- [STC SR00812DE](https://openairdocs.org/stc/SR00812DE): Installation of Honeywell Sky Connect Tracker III system. Cert Works LLC
- [STC SR04029NY](https://openairdocs.org/stc/SR04029NY): Installation of Aspire 200 IG SATCOM with Cabin Wi-fi System. EMS Technologies Canada Ltd
- [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC
- [STC SR02943NY](https://openairdocs.org/stc/SR02943NY): Installation of EMS Equipment P/N 429020-501 & 429020-502 must be in accordance with Aerolite Max Bucher GMBH Master Document List MDL-10-006, Rev. B dated April 29, 2011.  This modification is required to be maintained in accordance with Aerolite Operations Manuals OPM-429020-501, Rev. A, dated March 1, 2011 & OPM-429020-502, dated January 19, 2011, respectively. EASA approved Rotorcraft Flight Manual Supplement FMS-429020-501, Rev. A & FMS429020-502, Rev. 0, respectively, are required with these installation.. Aerolite AG
- [STC SR03696NY](https://openairdocs.org/stc/SR03696NY): Installation of VIP Cabin Interiors, P/N 6B420000X001-001, consisting of seats layout, entertainment system and life vest provision for P/N 6B422522A004-(XXX). Mecaer Aviation Group S.p.A.
- [STC SR04091CH](https://openairdocs.org/stc/SR04091CH): Installation of an air ambulance conversion kit. Med-Pac Inc.
- [STC SR03997AT](https://openairdocs.org/stc/SR03997AT): Installation of  Locking Fuel Cap. Bell Helicopter Textron Inc.
- [STC SR04210AT](https://openairdocs.org/stc/SR04210AT): Installation of a locking hinge on the baggage door. Turbine Kinetics
- [STC SR02377LA](https://openairdocs.org/stc/SR02377LA): Airfilm Nose Utility Mount. Airfilm Camera Systems
- [STC SR02376LA](https://openairdocs.org/stc/SR02376LA): Installation of Airfilm Tail Utility Mount. Airfilm Camera Systems
- [STC SR04187AT](https://openairdocs.org/stc/SR04187AT): Installation of L-3 Communications Micro Quick Access Recorder (QAR) that records the Flight Data Recorder echo line on flash memory; QAR data can be downloaded via the USB port, or the QAR unit can be removed for flight data analysis. Skybooks, Inc.
- [STC SR00692DE](https://openairdocs.org/stc/SR00692DE): Installation of a Cabin Heater System Provisions. Air Comm Corporation
- [STC SR00693DE](https://openairdocs.org/stc/SR00693DE): Installation of a Cabin Air Conditioning System Provisions. Air Comm Corporation
- [STC SR03489NY](https://openairdocs.org/stc/SR03489NY): Installation of Bear Paw Kit. Alpine Aerotech LP
- [STC SR00780DE](https://openairdocs.org/stc/SR00780DE): Installation of  Tail Rotor Pedal Removal Kit. Laz-Tec, LLC
- [STC SR09566RC](https://openairdocs.org/stc/SR09566RC): Installation of Night Vision Goggle Compatible Lighting System. Aero Dynamix Inc.
- [STC SR02452LA](https://openairdocs.org/stc/SR02452LA): Installation of Airfilm Nose Utility Mount Light Kit. Airfilm Camera Systems
- [STC SR00716DE](https://openairdocs.org/stc/SR00716DE): Installation of Crew Door Assist Handle in accordance with Aeronautical Accessories Drawing List, Report No   AA-10134, Revision A, dated February 09, 2011, FAA approved February 16, 2011, or later FAA approved revision.. Bell Helicopter Textron Inc.
- [STC SR00739DE](https://openairdocs.org/stc/SR00739DE): Installation of Sliding Door Push-out Windows in accordance with Laz-Tec Drawing List, Report No. AA-11062, Revision B, dated November 23, 2011, FAA approved December 19, 2011, or later FAA approved revision.. Bell Helicopter Textron Inc.
- [STC SR00740DE](https://openairdocs.org/stc/SR00740DE): Installation of Aft Cabin Floor Protectors in accordance with Laz-Tec Drawing List, Report No. AA-11059, Revision B, dated December 07, 2011, FAA approved December 16, 2011, or later FAA approved revision.. Bell Helicopter Textron Inc.
- [STC SR00741DE](https://openairdocs.org/stc/SR00741DE): Installation of Removable Crew Doors. Bell Helicopter Textron Inc.
- [STC SR00743DE](https://openairdocs.org/stc/SR00743DE): Installation of structural provisions for a blade fold kit. Paravion Technology Inc
- [STC SR02810NY](https://openairdocs.org/stc/SR02810NY): The Installation of Hardpoint and Spotter Fixtures. Bell Helicopter Textron Inc.

All 60: https://openairdocs.org/tcds/R00003RD/stcs.md

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