# TCDS A00007SE: Daher Aircraft Design LLC

- Type: Type certificate data sheet
- Status: Current
- Holder: Daher Aircraft Design LLC
- Revision: 28
- Revised: November 6, 2025
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Registered aircraft: 254, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/87/44/8744909d823f3e3146da0c77a2aca1eab34521e478bd5eb6f51b7ee09380649f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128562299920251125193447.0001
- Page: https://openairdocs.org/tcds/A00007SE

## Models (2)

As the data sheet lists them.

- Kodiak 200
- Kodiak 100

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
A00007SE 1  
Page No. 1 2 3 4 5 6 
Rev. No. 27 26 26 28 26 26 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A00007SE 
Revision 28 
DAHER 
Kodiak 100 
Kodiak 200 
November 6, 2025  
 
 
TYPE CERTIFICATE DATA SHEET A00007SE 
This data sheet, which is part of Type Certificate No. A00007SE, prescribes conditions and limitations under which the produc t 
for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. 
TC Holder:  Daher Aircraft Design, LLC 
   1200 Turbine Drive 
   Sandpoint, Idaho 83864 
 
TC Holder Record:  Quest Aircraft Design, LLC. Transferred to Daher Aircraft Design, LLC on November 7, 2019 
 
I - Model Kodiak 100 (Normal Category), Approved May 31, 2007 
Engine: Engine Manufacturer: Pratt and Whitney Canada, Inc. 
Number of Engines: One (1) 
Engine TC Number: E4EA 
Engine Model Designation: PT6A-34 
Fuel: Primary Fuel: Jet A 
Alternate Fuels: Jet A-1, JP-1, JP-5, JP-8,  
 No. 3 Jet Fuel (People’s Republic of China) 
Note that all fuels must conform to Pratt and Whitney Canada Specification CPW204 
Engine Limits: Maximum Takeoff Power: 750 horsepower at 2,200 rpm, subject to ambient temperature 
and pressure conditions. 
See the latest approved revision of the Kodiak 100 “Pilot’s Operating Handbook &  FAA Approved 
Airplane Flight Manual” and Engine TC Data Sheet E4EA for additional details and limitations. 
Propeller and Propeller Manufacturer: Hartzell 
Propeller Limits: Number of Propellers: One (1) 
Propeller TC Number: P10NE 
Propeller Model Designation: HC-E4N-3P(Y)/D9511FSB 
Diameter Limits: 95" minimum, 96" maximum; no further tolerance permitted 
High Pitch Angle: 86.1° ± 0.5° 
Low Pitch Angle: 17.5° ± 0.5° 
Reverse Pitch Angle: -10.0 ± 0.5° 
Static RPM Limits: Stabilized ground operation prohibited from 
 between 450 rpm and 1,050 rpm 
Pitch angle limits to be measured at 30” radial distance.  See Propeller TC Data Sheet P10NE for 
additional details and limitations. 
Airspeed Limits: VO: 143 kcas  (142 kias) 
VFE (10°): 139 kcas  (138 kias) 
VFE (20°): 120 kcas  (120 kias) 
VFE (35°): 108 kcas  (108 kias) 
VMO: 180 kcas  (182 kias)

A00007SE 2  
Page No. 1 2 3 4 5 6 
Rev. No. 27 26 26 28 26 26 
 
 
Center of Gravity 
(C.G.) Range: 
Serial Numbers 100-0001 thru  
100-0034 without Quest Service 
Notice SN-025 compliance: 
Aft Limits:  
Forward Limits:   
80.8" aft of datum (3,620 lb to 6,750 lb) 
63.9" aft of datum (3,620 lb to 5,000 lb) 
69.4" aft of datum at 6,750 lb 
 Straight-line variation between points 
 
  
 Serial Numbers 100-0035 and 
above and Serial Numbers  
100-0001 thru 100-0034 with 
Quest Service Notice SN-025 
compliance: 
Takeoff and flight 
   Aft Limits:  
   Forward Limits:   
 
80.8" aft of datum (4,070 lb to 7,255 lb) 
63.9" aft of datum (4070 lb to 5,000 lb) 
71.0" aft of datum at 7,255 lb 
  Landing (Standard) 
   Aft Limits:  
   Forward Limits:   
 
80.8" aft of datum (4,070 lb to 6,690 lb) 
63.9" aft of datum (4070 lb to 5,000 lb) 
69.3" aft of datum at 6,690 lb 
  Landing (Optional) 
   Aft Limits:  
   Forward Limits:   
 
80.8" aft of datum (4,070 lb to 7,255 lb) 
63.9" aft of datum (4070 lb to 5,000 lb) 
69.3" aft of datum at 6,690 lb 
72.6" aft of datum at 7,255 lb 
    
Straight-line variation between points 
 
Optional landing weight allowed only when the aircraft is operated per, and the required tires and 
vortex generators(VGs) are installed per the limitations section of the latest FAA approved Kodiak 
100 POH/AFM Supplement “Oversized Tires and Landing Weight” and the supplement is 
incorporated into the aircraft POH/AFM. 
Empty Weight None 
C.G. Range: 
Datum: The forward face of the firewall represents datum 0.0 inches. 
Leveling Means: Place a level on the seat tracks in the aft cabin next to the cargo door forward post. 
See the latest approved revision of the Kodiak 100 “Pilot’s Operating Handbook &  FAA Approved 
Airplane Flight Manual” for additional details. 
 
Maximum Weights: Serial Numbers 100-0001 thru 
100-0034 without Quest Service 
Notice SN-025 compliance: 
Maximum Ramp:  
Maximum Landing:  
Maximum Takeoff:  
Design Minimum Flying Weight:  
6,800 lb 
6,690 lb 
6,750 lb 
3,620 lb 
 Serial Numbers 100-0035 and 
above and Serial Numbers 100-
0001 thru 100-0034 with Quest 
Service Notice SN-025 
compliance: 
Maximum Ramp:  
Maximum Landing 
                    Standard: 
                    Optional: 
Maximum Takeoff:  
Maximum Zero-Fuel:  
Design Minimum Flying Weight:  
7,305 lb 
 
6,690 lb 
7,255 lb 
7,255 lb 
7,071 lb 
4,070 lb 
 
Optional landing weight allowed only when the aircraft is operated per, and the required tires and 
VGs are installed per the limitations section of the latest FAA approved Kodiak 100 POH/AFM 
Supplement “Oversized Tires and Landing Weight” and the supplement is incorporated into the 
aircraft Pilot’s Operating Handbook & FAA Approved Airplane Flight Manual. 
Minimum Crew: 1 Pilot 
Number of Seats: Up to 10 seats total, including 2 seats located at 40" aft of datum and up to 8 additional seats located 
in accordance with latest approved revision of the Kodiak 100 “Pilot’s Operating Handbook and FAA 
Approved Flight Manual” 
Maximum Compartment As defined in latest approved revision of the Kodiak 100 “Pilot’s Operating Handbook & FAA 
Weights: Approved Airplane Flight Manual”.

A00007SE 3  
Page No. 1 2 3 4 5 6 
Rev. No. 27 26 26 28 26 26 
 
Fuel Capacity: One 160 gallon tank in each wing at 83.4" aft of datum; 157.5 gallons usable, 2.5 gallons unusable 
(320 gallons total; 315 gallons usable, 5 gallons unusable) 
Note: add weight of unusable fuel to the certificated empty weight. 
 
Oil Capacity:            13 qt total at 18.9" forward of datum; 9 qt drainable, 4 qt undrainable 
Note:  Add the weight if oil to the certificated empty weight of the aircraft. 
See Pratt and Whitney Canada Service Bulletin Number 1001 for approved oil. 
 
Maximum Operating 14,000 feet without FAA approved oxygen system installed. 
Altitude: 25,000 feet with FAA approved oxygen system installed. 
Control Surface Wing Flaps: 0° 10° +1°/-2° 20° ±2° 35° ±2° 
Movements: Ailerons: Up: 28° ±1° Down: 15° ±1° 
Aileron Trim Tab: Up: 30° ±2° Down: 30° ±2° 
Elevator: Up: 30° ±1° Down: 22° ±1° 
Elevator trim tab: Up: 15° ±2° Down: 12° ±1° 
Rudder: Right: 26° ±1° Left: 26° ±1° 
 
See the latest FAA approved revision of the Kodiak 100 “Airplane Maintenance Manual”, or other 
FAA approved data, for flap rigging instructions and setting Flaps up (0°) configuration. 
Manufacturer’s The information contained herein is applicable to Serial Numbers 100-0001 and up. 
Serial Numbers: 
Certification Basis: Certification Basis: Part 23 of the Federal Aviation Regulations (FAR) effective February 1, 1965, 
as amended by 23-1 through 23-55; FAR 34 as amended through 34-3, FAR 23.1306 for Lightning 
Protection, per Amdt 23-61, and FAR 36 as amended through 36-28. 
Special Condition 23-207-SC for high intensity radiated fields (HIRF) protection, effective January 
31, 2007. 
For aircraft equipped with the Garmin GFC 700 Automatic Flight Control System:  FAR 23.1308(a), 
at amendment 23-57 for HIRF protection of the GFC 700 system and associated systems performing 
functions whose failure would prevent continued safe flight and landing.  
For aircraft serial number 100-0354 and up and aircraft serial numbers 100-0001 through 100-0353 
that are equipped with the Mid-Continent MD302 standby attitude module and MD32 magnetometer:  
FAR 23.1303(c) at amendment 23-62 for flight and navigation instruments and FAR 23.1331(c) at 
amendment 23-62 for instruments using a power source. 
 
II - Model Kodiak 200 (Normal Category), Approved August 30, 2022 (See NOTE 5) 
Engine: Engine Manufacturer: Pratt and Whitney Canada, Inc. 
Number of Engines: One (1) 
Engine TC Number: E4EA 
Engine Model Designation: PT6A-140A 
Fuel: Primary Fuel: Jet A 
Alternate Fuels: Jet A-1, JP-5, JP-8,  
 No. 3 Jet Fuel (People’s Republic of China) 
Note that all fuels must conform to Pratt and Whitney Canada Specification CPW204 
Engine Limits: Maximum Takeoff Power: 900 horsepower at 1,900 rpm, subject to ambient temperature 
and pressure conditions. 
See the latest a pproved revision of the Kodiak  900 “Pilot’s Operating Handbook &  FAA Approved 
Airplane Flight Manual” and Engine TC Data Sheet E4EA for additional details and limitations.   See 
NOTE 5. 
Propeller and Propeller Manufacturer: Hartzell 
Propeller Limits: Number of Propellers: One (1) 
Propeller TC Number: P20NE 
Propeller Model Designation: HC-E5W-3/NC9405B 
Diameter Limits: 97"; no further tolerance permitted 
High Pitch Angle: 88.6°±0.5° 
Low Pitch Angle: 18.5°±0.5° 
Reverse Pitch Angle: -10.0°±0.5° 
Static RPM Limits: Maximum 1900 rpm.  Stabilized ground operation prohibited                   
from between 400 rpm and 1,150 rpm.

A00007SE 4  
Page No. 1 2 3 4 5 6 
Rev. No. 27 26 26 28 26 26 
 
Pitch angle limits to be measur ed at 30” radial distance.  See Propeller TC Data Sheet P20NE for 
additional details and limitations. 
Airspeed Limits: VO (at 8,000 lb): 153 kcas  (152 kias) 
VFE (10°): 139 kcas  (137 kias) 
VFE (20°): 125 kcas  (123 kias) 
VFE (35°): 120 kcas  (118 kias) 
VMO: 190 kcas  (187 kias) 
  
Center of Gravity 
(C.G.) Range: 
Serial Numbers K2-0002 and up.   
 
Forward limits: 
 
 
Aft Limits: 
 
   
78.8” aft of datum at 4,840 lb 
78.8” aft of datum at 6,250 lb 
84.4” aft of datum at 8,000 lb 
92.5” aft of datum at 4,840 lb 
92.5” aft of datum at 8,000 lb 
Straight-line variation between points 
Empty Weight None 
C.G. Range: 
Datum: The forward face of the firewall represents datum 0.0 inches. 
Leveling Means: Place a level on the seat tracks in the aft cabin next to the cargo door forward post . 
See the latest a pproved revision of the Kodiak  900 “Pilot’s Operating Handbook &  FAA Approved 
Airplane Flight Manual” for additional details.  See NOTE 5. 
 
Maximum Weights: Serial Numbers K2-0002 and up: Maximum Ramp:  
Maximum Landing:  
Maximum Takeoff:  
Maximum Zero Fuel: 
Design Minimum Flying Weight:  
8,100 lb 
7,800 lb 
8,000 lb 
7,210 lb 
4,840 lb 
 
See the latest approved revision of the Kodiak 900 “Pilot’s Operating Handbook and FAA Approved 
Airplane Flight Manual” for additional details.  See NOTE 5. 
 
Minimum Crew: 1 Pilot 
Number of Seats: Up to 10 seats total, including 2 seats located  at 41" aft of datum and up to 8 additional seats located 
in accordance with latest approved revision of the K odiak 900 “Pilot’s Operating Handbook &  FAA 
Approved Airplane Flight Manual”.  See NOTE 5. 
Maximum Compartment As defined in latest approved revision of the Kodiak 900 “Pilot’s Operating Handbook & FAA 
Weights: Approved Airplane Flight Manual”.  See NOTE 5. 
 
Fuel Capacity: Wing Tanks:  One 1 59 gallon tank in each wing at 94.2 " aft of datum; 155. 5 gallons usable, 3. 5 
gallons unusable (318 gallons total; 311 gallons total usable, 7 gallons total unusable). 
Header Tank:  One 4.1 gallon header tank at 93.5” aft of datum, 4.1 gallons unusable. 
Note: add weight of unusable fuel to the certificated empty weight. 
Oil Capacity:             14.4 qt total at 22.3" forward of datum; 14 qt drainable, 0.4 qt undrainable 
 Note:  Add the weight if oil to the certificated empty weight of the aircraft. 
See Pratt and Whitney Canada Service Bulletin Number 1001 for approved oil. 
Maximum Operating 25,000 feet with FAA approved oxygen system installed. 
Altitude: 14,000 feet without FAA approved oxygen system installed. 
20,000 feet in icing conditions or any flight conditions with ice on the airplane. 
Control Surface Wing Flaps: 0°        10° +1°/-2° 20° ±2° 35° ±2° 
Movements: Ailerons: Up: 28° ±1° Down: 15° ±1° 
Aileron Trim Tab: Up: 30° ±2° Down: 30° ±2° 
Elevator: Up: 30° ±1° Down: 22° ±1° 
Elevator trim tab: Up: 18° +1°/-0° Down: 12° ±1° 
Rudder: Right: 20° ±1° Left: 20° ±1° 
See the latest FAA approved revision of the Kodiak 900 “Airplane Maintenance Manual”, or other 
FAA approved data, for flap rigging instructions and setting Flaps up (0°) configuration.See NOTE 5. 
Manufacturer’s The information contained herein is applicable to Serial Numbers K2-0002 and up. 
Serial Numbers:

A00007SE 5  
Page No. 1 2 3 4 5 6 
Rev. No. 27 26 26 28 26 26 
 
 
Certification Basis:   14 CFR Part 23, as amended through 23-63. 
 14 CFR 23.2010 Accepted means of compliance and 14 CFR 23.2150 Stall characteristics, stall 
warning, and spins, as amended by 23-64. 
 Project Specific Policy Memorandum (PSPM) for correction of Amendment 23-62 and prior 
amendment errors, as described in an FAA Memorandum, under the subject, “Project Specific Policy 
Memorandum for 14 CFR Part 23, up to and including Amdt 62.”  
 ELOS Finding for Quest, Project No. AT13028SE-A, “Equivalent Level of Safety Finding for 14 
CFR §23.1353(h), Storage Battery Design and Installation: in the event of a complete loss of the 
primary electrical generating system.” dated August 31, 2020. 
14 CFR Part 34, as amended through 34-6.  
14 CFR Part 36, as amended through 36-31.  
 
DATA PERTINENT TO ALL MODELS: 
TC Number: A00007SE 
TC Issuance Date: May 30, 2007 
TC Application Date: April 7, 2005 
TC Amendment Date August 30, 2022 
 
Operational Restrictions: Day-Night, Visual Flight Rules (VFR) and Instrument Flight Rules (IFR).  
Flight into known icing conditions allowed when the required equipment listed in the latest FAA 
approved revision of the Kodiak 100 POH/AFM Supplement, “TKS Ice Protection System,” or 
Kodiak 900 POH/AFM Supplement, “TKS Ice Protection System,” as applicable, is installed. For 
Kodiak 100 only: installation may have been accomplished when the airplane was produced (may 
have required system activation in accordance with Quest Service Notice SN-043), or may have been 
installed in accordance with the latest FAA approved revision of Quest Field Service Instruction FSI-
013.  See NOTE 5. 
Minimum Operating OAT -25°C for Kodiak 100 models Serial Numbers 100-0001 thru 100-0017 
without Quest Service Bulletin SB-016 compliance. 
Minimum Operating OAT -55°C for Kodiak 100 models Serial Numbers 100-0018 and up and Serial 
Numbers 100-0001 thru 100-0017 with Quest Service Bulletin SB-016 compliance. 
Minimum Operating OAT -55°C for Kodiak 200 models Serial Numbers K2-0002 and up. 
Production Basis: Production Certificate 728NM. 
Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (see 
Certification Basis) must be installed in the aircraft for airworthiness certification. 
Additional Equipment The latest FAA Approved Revision of the Kodiak 100 “Pilot’s 
Necessary for Type Operating Handbook & FAA Approved Airplane Flight Manual.” 
Certification: or the Kodiak 900 “Pilot’s Operating Handbook and FAA Approved 
Flight Manual,” as applicable.  See NOTE 5. 
     -         
 
NOTE 1: A current weight and balance report, including a list of equipment included in the certificated empty 
weight, and loading instructions when necessary must be provided for each aircraft at the time of 
original certification. 
NOTE 2: The placards specified in the latest FAA approved revision of the Kodiak 100 “Pilot’s Operating 
Handbook & FAA Approved Airplane Flight Manual” or the Kodiak 900 “Pilot’s Operating 
Handbook & FAA Approved Airplane Flight Manual”, as applicable, are required.  See NOTE 5. 
NOTE 3: The airplane must be subsequently maintained in accordance with the Instructions for Continued 
Airworthiness, and Airworthiness Limitations section, as contained in the latest FAA approved 
revision of the Kodiak 100 “Airplane Maintenance Manual” or the Kodiak 900 “Airplane 
Maintenance Manual”, as applicable, or other FAA approved data.  See NOTE 5. 
For Kodiak 100 serial numbers 100-0354 and up use document AM902.0, Kodiak 100 Airplane 
Maintenance Manual, Revision 32 or later FAA-approved revision. 
For Kodiak 200 serial numbers K2-0020 and up use document AM922.0. Kodiak 900 Airplane 
Maintenance Manual, Revision 03 or later FAA-approved revision.  See NOTE 5.

A00007SE 6  
Page No. 1 2 3 4 5 6 
Rev. No. 27 26 26 28 26 26 
 
NOTE 4: The airplane shall be manufactured in accordance with the latest FAA approved revision of the 
Kodiak 100 “Master Drawing List” or the Kodiak 200 “Master Drawing List”, as applicable, or 
other FAA approved data.   
 
NOTE 5: The marketing name for the model Kodiak 200 is the “Kodiak 900”.  Some documents that apply to 
the Kodiak 200 model such as the Airplane flight manual and Airplane maintenance manual are 
labeled with the Kodiak 900 trade name.  Documents that are entitled with Kodiak 900 are applicable 
to the Kodiak 200 model.   
 
.....END.....
```

## ADs (5, in force first)

- [AD 2020-13-01](https://openairdocs.org/ad/2020-13-01): Landing Gear · Daher Aircraft Design Kodiak 100. Effective Aug 17, 2020
- [AD 2020-04-13](https://openairdocs.org/ad/2020-04-13): Charts · Daher Aircraft Design Kodiak 100. Effective Apr 1, 2020
- [AD 2016-06-06](https://openairdocs.org/ad/2016-06-06): Elevator Control System · Quest Aircraft Design Kodiak 100. Effective Apr 22, 2016
- [AD 2015-02-15](https://openairdocs.org/ad/2015-02-15): Elevator skins · Quest Aircraft Design Kodiak 100. Effective Feb 19, 2015
- [AD 2011-25-04](https://openairdocs.org/ad/2011-25-04): Engine Air Intake System · Quest Aircraft Design Kodiak 100. Effective Dec 19, 2011

## Registered aircraft by registry model (OpenAirDocs)

- [Quest KODIAK 100](https://openairdocs.org/model/quest-kodiak-100): 140 aircraft (registry codes 7320001, 7320005, 05622SV)
- [Kodiak KODIAK 100](https://openairdocs.org/model/kodiak-kodiak-100): 79 aircraft (registry code 7320010)
- [Kodiak KODIAK 200](https://openairdocs.org/model/kodiak-kodiak-200): 34 aircraft (registry codes 7320201, 056408O)
- [Quest Aircraft Design KODIAK 100](https://openairdocs.org/model/quest-aircraft-design-kodiak-100): 1 aircraft (registry code 7320015)
- [Kodiak KODIAK 900](https://openairdocs.org/model/kodiak-kodiak-900): 0 aircraft (registry code 7320901)

## STCs approved under this data sheet (38)

- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12420IB](https://openairdocs.org/stc/SA12420IB): Battery Installation. AEROSPACE COMPOSITES GmbH
- [STC SA12329AT](https://openairdocs.org/stc/SA12329AT): Installation of Teledyne Star SAFIRE 380-HDc FLIR Imaging System with Class 1M Eye Safe Laser Range Finder (ESLRF) & Class 3B Laser Pointer (LP). IOMAX USA LLC
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc.
- [STC SA04589CH](https://openairdocs.org/stc/SA04589CH): Installation of Hartzell Propeller model 5D3-NK366A1(Y)( )/91D17(B). Hartzell Propeller LLC
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS  (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc.
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc.
- [STC SA04114CH](https://openairdocs.org/stc/SA04114CH): Installation of Engine Preheat Kit, P/N TA3123-1 for 115 volt application. Hartzell Propeller LLC
- [STC SA04554CH](https://openairdocs.org/stc/SA04554CH): Install Emergency Medical System. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc.
- [STC SA04567CH](https://openairdocs.org/stc/SA04567CH): Installation of a Retractable Camera Mount System in accordance with Fargo Jet Center LLC's Installation Data List, Doc. No. FJC 1810023, Revision A, dated May 9, 2022, or later FAA-approved revisions.. Fargo Jet Center
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA01031DE](https://openairdocs.org/stc/SA01031DE): Installation of the Garmin GSR 56 SATCOM transceiver and Flightstream 210 transceiver. Daher Aircraft Design LLC
- [STC SA04450NY](https://openairdocs.org/stc/SA04450NY): Installation of MTV-27-1-E-C-F-R(P)/CFR240-55() propeller and spinner. MT- Propeller Entwicklung GmbH
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit.. Med-Pac Inc.
- [STC SA04345CH](https://openairdocs.org/stc/SA04345CH): Installation of Wipaire Fuel Handles, Steps and Mirrors. Wipaire Inc
- [STC SA01871WI](https://openairdocs.org/stc/SA01871WI): Installation of a Single Point Pressure Refueling System. AO Aviation LLC
- [STC SA02452SE](https://openairdocs.org/stc/SA02452SE): Installation of Aerocet Model 6650 Amphibious Twin Floats. Aerocet Inc
- [STC SA02477AK](https://openairdocs.org/stc/SA02477AK): Installation of the Aero Twin, Inc. External Oxygen Service Port, Kit No. QX-100. Aero Twin Inc
- [STC SA01761WI](https://openairdocs.org/stc/SA01761WI): Executive Style Interior Installation.. Millennium Concepts Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01711WI](https://openairdocs.org/stc/SA01711WI): Installation of an interior upgrade.. Quest Aircraft Design LLC
- [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA03237CH](https://openairdocs.org/stc/SA03237CH): External Cargo Compartment and Cabin Interior Modifications. Standard Aero
- [STC SA02412AK](https://openairdocs.org/stc/SA02412AK): Installation of Aero Twin, Inc. extended crew door steps. Aero Twin Inc
- [STC SA03098CH](https://openairdocs.org/stc/SA03098CH): Installation of a wing mounted weather radar system. Quest Aircraft Design LLC
- [STC SA02991CH](https://openairdocs.org/stc/SA02991CH): Installation of Hartzell Propeller Model HC-B3TN-3DY/T10282NS in accordance with Wipaire , Inc. Drawing No. 1005338, Revision A, dated June 3, 2011, or later FAA approved revisions.. Wipaire Inc
- [STC SA02391AK](https://openairdocs.org/stc/SA02391AK): Installation of a Nose Gear Gravel Deflector, P/N NGDQ-100. Aero Twin Inc
- [STC SA02848CH](https://openairdocs.org/stc/SA02848CH): Installation of Wipaire Model 7000 Amphibious Floats. Wipaire Inc
- [STC SA00059WI](https://openairdocs.org/stc/SA00059WI): Installation of Single Point Refueling System in accordance with Wipaire, Inc. Installation Drawing as listed on AML No. SA00059WI, issued February 25, 2011, or later FAA approved revisions.. Wipaire Inc
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc.
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [STC SA02337AK](https://openairdocs.org/stc/SA02337AK): Installation of up to eight (8) seats, Aero Twin, P/N DFS2T-L/R in loading zones two through five.. Aero Twin Inc
- [STC SA02339AK](https://openairdocs.org/stc/SA02339AK): Installation of main gear gravel deflectors, PN GDQ-100, on the main landing gear of the Quest Kodiak 100.. Aero Twin Inc
- [STC SA02344AK](https://openairdocs.org/stc/SA02344AK): Manufacture and installation of nose gear tire scraper, on the nose landing gear of the Quest Kodiak 100.. Aero Twin Inc
- [STC SA12425IB](https://openairdocs.org/stc/SA12425IB): Installation of Single Hatch. AEROSPACE COMPOSITES GmbH

---
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