# TCDS A47EU: Polskie Zakłady Lotnicze Sp. z o.o.

- Type: Type certificate data sheet
- Status: Current
- Holder: Polskie Zakłady Lotnicze Sp. z o.o.
- Revision: 11
- Revised: July 30, 2021
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 21, Part 23
- Registered aircraft: 2, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/d5/ae/d5ae2169efc4485076646c7ae063f2c27a707356d98ce3361673abaf8463574e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177436605120230605133656.0001
- Page: https://openairdocs.org/tcds/A47EU

## Models (3)

As the data sheet lists them.

- PZL M18
- PZL M18A
- PZL M18B

## What the data sheet says

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

```text
Page No. 1 2 3 4 5 6 7 
Rev. No. 11 8 6 6 10 11 10 
 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A47EU 
Revision 11 
Polskie Zaklady Lotnicze Spolka. 
PZL M18 
PZL M18A 
PZL M18B 
 
July 30, 2021 
 
TYPE CERTIFICATE DATA SHEET No. A47EU 
 
This data sheet which is part of Type Certificate No. A47EU prescribes conditions and limitations under which the product for 
which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. 
 
Type Certificate Holder.  Polskie Zaklady Lotnicze Spolka zo.o. 
     Wojska Polskiego 3 
     39-300 Mielec 
     Poland 
 
Type Certificate Ownership Record       Wytwornia Sprzetu Komunikacyjnegc,“PZL Mielec” transferred ownership of  
type certificate A47EU to Polskie Zaklady Lotnicze Spolka zo.o. on January 2000. 
      
 
I. Model PZL M18 (Restricted Category), approved January 23, 1981. 
 
Engine.    1 PZL-KALISZ ASz-62IR-M18 nine cylinder air cooled radial. 
     Reduction gear ratio: 0.687:1 
 
Fuel.    91 (Minimum grade aviation fuel). 
 
Oil.     Aeroshell 100W. 
 
Engine Limits.       Manifold       Cyl. 
         Pressure  Altitude             Head Temp. 
     Rating         S.H.P.        R.P.M.        (Inch of Hg)    (ft)  (°C) 
          Takeoff (5 min)         967           2200    41.3       0  245 
          Max. continuous       793           2100    35.4       0  215 
              812           2100    35.4  5,000  215 
 
Propeller.    PZL-Warszawa AW-2-30, four blade constant speed. 
     Diameter:129.9 inches. 
 
Airspeed Limits (CAS).  VA (Maneuvering)  123 knots      VFE (Flap operating)  108 knots      VNE (Never exceed)  151 knots      See GICA Polish-approved AFM for airspeed limits when agricultural spraying  
     equipment is installed.

Page 2 of 7 A47EU 
 
C.G. Range.    
2 3  2  7 2 8
6160
7950
92 60
20.8 24.2 2 5.1 27.9 inches
aft of datum
% M .A .C .
pounds
3 1
 
    Straight line varation between points. 
 
Empty Weight C.G. Range.  None 
 
M.A.C.    1/6 inches aft of datum. 
 
Maximum Weight.   Takeoff  9260 lb. 
     Landing  9260 lb. 
 
Number of Seats.   1 - for operating flights (100 inches aft of datum) 
     2 - for other flights, pilot plus one person in mechanic's cabin 
          (1st  - 100 inches aft of datum, 
           2nd - 118 inches aft of datum). 
 
Maximum Baggage.  66 lb. (154 inches aft of datum). 
      (See AFM Section 2) 
 
Hopper Capacity.   3300 lb. (32.7 inches aft of datum). 
      (See AFM Section 2) 
 
Fuel Capacity.   Usable - LH tank 94; RH tank 94 
     Total - 188 per tank (moment arm 37.6 in. aft of datum) 
     (See NOTE 1) 
 
Oil Capacity (U.S. Gal.).  Total - 20.6 (moment arm 19.4 in. fwd of datum) 
     See NOTE 1 for data on system oil. 
 
Control Surface Movements.  Aileron   Up 21° (± 1°)  Down  17° (± 1°) 
     Elevator  Up 27° (± 1°)  Down  17° (± 1°) 
     Elevator trim tab  Up 13° (- 1°)   Down  15° (- 1°) 
          Rudder  Left 23° (± 1°)  Right 23° (± 1°) 
     Flaps  0° to 30° (± 1°) 
 
 
 
II.  Model PZL M18A (Restricted Category), approved September 8, 1987. 
 
 
Engine.    PZL-Kalisz 1 ASz-62IR-M18 nine cylinder air cooled radial. 
     Reduction gear ratio: 0.687:1 
 
Fuel.    91 (Minimum grade aviation fuel). 
 
Oil.     Aeroshell 100W.

Page 3 of 7 A47EU 
Engine Limits.       Manifold       Cyl. 
         Pressure  Altitude             Head Temp. 
     Rating         S.H.P.        R.P.M.        (Inch of Hg)    (ft)  (°C) 
          Takeoff (5 min)         967           2200    41.3       0  245 
          Max. continuous       793           2100    35.4       0  215 
              812           2100    35.4  5,000  215 
 
Propeller.    PZL-Warszawa AW-2-30, four blade constant speed. 
     Diameter:129.9 inches. 
 
Airspeed Limits (CAS).  VA (Maneuvering)  123 knots      VFE (Flap operating)  108 knots      VNE (Never exceed)  151 knots  
     See GICA Polish-approved AFM for airspeed limits when agricultural spraying  
     equipment is installed. 
 
Center of Gravity (C.G.) Range. 
2 3 2 7 3 1
6160
9260
20.8 24.2 27.9 inches
aft of datum
% M.A.C.
pounds
 
 
     Straight line variation between points. 
 
Empty Weight C.G. Range.  None 
 
M.A.C.    1/6 inches aft of datum. 
 
Maximum Weight.   Takeoff  9260 lb. 
     Landing  9260 lb. 
 
Number of Seats.   1 - for operating flights (100 inches aft of datum) 
     2 - for other flights, pilot plus one person in mechanic's cabin  
          (1 st - 100 inches aft of datum, 
           2 nd - 118 inches aft of datum). 
 
Maximum Baggage.  66 lb. (154 inches aft of datum). 
      (See AFM Section 2) 
 
Hopper Capacity.   3300 lb. (32.7 inches aft of datum). 
      (See AFM Section 2)

Page 4 of 7 A47EU 
Fuel Capacity (U.S. Gal.).  Usable  - LH tank 53; RH tank 53 
  - Standard  Total  - 106 per tank (moment arm 37.6 in. aft of datum) 
 
  - With enlarged tanks Usable  - LH tank 94, RH tank 94 
     Total  - 188 per tank/moment arm 37.6 in. (aft of datum) 
 
Oil Capacity (U.S. Gal.).  Total  - 20.6 (moment arm 19.4 in. fwd of datum) 
     See NOTE 1 for data on system oil. 
 
Control Surface Movements.  Aileron   Up 21° (± 1°)  Down  17° (± 1°) 
     Elevator  Up 27° (± 1°)  Down  17° (± 1°) 
     Elevator trim tab  Up 10° (± 1°)  Down  17° (± 1°) 
     Rudder  Left 23° (± 1°)  Right 23° (± 1°) 
     Flaps  0° to 15° (± 1°) 
 
III.  Model PZL M18B (Restricted Category), approved December 19, 1995. 
 
Engine.    PZL-KALISZ ASz-62IR-M18 nine cylinder air cooled radial. 
     Reduction gear ratio: 0.687:1 
 
Fuel.    91 (Minimum grade aviation fuel). 
 
Oil.     Aeroshell 100W. 
Engine Limits.       Manifold       Cyl. 
         Pressure  Altitude             Head Temp. 
     Rating         S.H.P.        R.P.M.        (Inch of Hg)    (ft)  (°C) 
          Takeoff (5 min)         967           2200    41.3       0  245 
          Max. continuous       793           2100    35.4       0  215 
              812           2100    35.4  5,000  215 
 
Propeller.    PZL-Warszawa AW-2-30, four blade constant speed. 
     Diameter:129.9 inches. 
     Low Pitch (30 in station): 18° 
 
Airspeed Limits (CAS).  VA (Maneuvering)  123 knots      VFE (Flap operating)  108 knots      VNE (Never exceed)  151 knots  
     See GICA Polish-approved AFM for airspeed limits when agricultural spraying  
     equipment is installed. 
 
 
Center of Gravity (C.G.) Range. 
 
2 3 2 7 3 1
6160
9260
20.8 24.2 27.9 inches
aft of datum
% M.A.C.
pounds
28.7
3 2
Rear C.G. position
for spraying version
(atomizers)
for other
operational
versions
 
     Straight line variation between points.

Page 5 of 7 A47EU 
Empty Weight C.G. Range.  None 
 
M.A.C.    1/6 inches aft of datum. 
 
Maximum Weight.   Takeoff  9260 lb. 
     Landing  9260 lb. 
 
Number of Seats.   1 - for operating flights (100 inches aft of datum) 
     2 - for other flights, pilot plus one person in mechanic's cabin 
          (1st  - 100 inches aft of datum, 
           2nd - 118 inches aft of datum). 
 
Maximum Baggage.  66 lb. (154 inches aft of datum). 
      (See AFM Section 2) 
 
Hopper Capacity.   3300 lb. (32.7 inches aft of datum). 
      (See AFM Section 2) 
 
Fuel Capacity.   Usable - LH tank 94; RH tank 94 
     Total - 188 per tank (moment arm 37.6 in. aft of datum) 
     (See NOTE 1) 
 
Oil Capacity (U.S. Gal.).  Total - 20.6 (moment arm 19.4 in. fwd of datum) 
     See NOTE 1 for data on system oil. 
Control Surface Movements.  Aileron   Up 21° (± 1°)  Down  17° (± 1°) 
     Elevator  Up 27° (± 1°)  Down  17° (± 1°) 
     Elevator trim tab  Up 13° (- 1°)   Down  15° (- 1°) 
          Rudder  Left 23° (± 1°)  Right 23° (± 1°) 
     Flaps  0° to 30° (± 1°) 
 
DATA PERTINENT TO ALL MODELS 
 
Datum.    Wing leading edge. 
 
Leveling Means.   Longitudinal - Place a level on foot step. 
     Lateral          - Place a level on top of main wing spar, center wing. 
 
Serial Numbers Eligible. Each individual aircraft manufactured under this type certificate must be accompanied by 
an Export Certificate of Airworthiness as noted below under "Import Requirements" 
when an application for a U.S. airworthiness certificate is made. (NOTE 5) 
 
     Model M18: 
     1Z005-01, 02, 03, 04, 05, 06, 07, 11, 12 (S/B U/16/81 required) 
     1Z006-06, 14, 15, 19, 20, 
     1Z007-03, 04, 05, 07, 08, 14, 15, 
     1Z008-01, 02, 03, 04, 05, 06, 07, 08, 09, 10, 15, 16, 17, 18, 19, 
     1Z011-04, 05, 
     1Z012-07, 08, 09, 10, 27, 28, 29, 30, 31, 32, 33 
 
     Model M18A: 
     1Z013-43, 44, 45, 46, 47, 48, 50, 
     1Z014-13, 14, 15, 16, 
     1Z015-25, 
     1Z016-01, 03, 04, 05, 06, 08, 09, 10, 14, 15, 16, 17, 18, 19, 20, 26, 27, 
     1Z017-09, 
     1Z018-18, 19, 20, 21, 
     1Z019-05, 06, 07, 08, 10, 19, 20, 
     1Z020-03, 04, 05, 06, 07, 08, 09, 10, 11, 12, 16, 17, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30 
     1Z021-01, 02, 
     1Z022-06, 07, 08, 09, 10, 11, 12, 19, 
     1Z023-01, 02, 03, 04, 06, 07, 08, 09, 29, 
     1Z024-01, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 
     1Z025-01, 02, 03, 04, 05, 06, 07, 08, 09, 10, 11, 12, 18, 19, 20, 21, 22, 23, 24, 25, 26, 
     1Z026-01, 02, 03, 
      
     Model M18B: 
     1Z026-01 and subsequent

Page 6 of 7 A47EU 
Import Requirements The FAA can issue a U.S. airworthiness certificate based on an NAA Export Certificate 
of Airworthiness (Export C of A) signed by a representative of the Civil Aviation Office 
(CAO) of Poland on behalf of the European Community. The Export C of A should 
contain the following statement: ‘The aircraft covered by this certificate has been 
examined, tested, and found to comply with U.S. airworthiness regulations 14 CFR  
Federal Aviation Regulations Part 21.25, U.S. Type Certificate No. A47EU and to be in a 
condition for safe operation.’  
 
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. 
 
      
Certification Basis. FAR 21.17 and FAR 21.25, FAR 23 dated February 1, 1965 as amended through 
Amendment 23-16, effective, February 14, 1975; except for the following exclusions 
considered inappropriate for FAR 21.25 the Restricted Category, Agricultural and 
Forest/Wildlife Conservation (Fire Fighting)  
     Special Purposes: Paragraphs:  
     23.45(c); 23.155; 23.175(b); 23.221; 23.253; 23.335(a)(1), (a)(4), (b)(1), (b)(4); 
23.629(f); 23.677(b); 23.771(b); 23.773(a)(3); 23.781(b); 23.785(m); 23.807(a)(3); 
23.867; 23.929; 23.1141(e); 23.1303(e); 23.1321(d); 23.1325(b)(3); 23.1415; 23.1416; 
23.1419; 23.1441; 23.1443; 23.1449; 23.1450; 23.1457; 23.1459; 23.1505(c); 23.1523(c); 
23.1524; 23.1545(d); 23.1599(a) and 23.1581(e). 
 
The Civil Aviation Office (CAO) of Poland originally type certificated these aircraft 
models under its type certificate Number BB-120/1. The FAA validated this product 
under U.S. Type Certificate Number A47EU. Effective October 24, 2005, the European 
Aviation Safety Agency (EASA) began oversight of this product on behalf of Poland. 
The EASA TCDS number is EASA.A.056. 
 
 
Validation Basis. Type Certificate A47EU was issued pursuant to FAR 21.29 in validation of the General 
Inspectorate of Civil Aviation Certification of compliance with the aforementioned 
certification basis, and in accordance with the restricted category airworthiness certificate 
provisions of 21.185(c). 
 
Equipment. The basic required equipment as prescribed in the applicable airworthiness 
regulations(see Certification Basis) must be installed in the aircraft for airworthiness 
certification.  In addition, the following items of equipment are required: 
Model M18 - CACA approved Airplane Flight Manual dated October 4, 1979, or later 
CACA/GICA approved revision. 
 
Model M18A - CACA approved Airplane Flight Manual dated May 30, 1987, or later 
CACA/GICA approved revisions. 
 
Model M18B - GICA approved Airplane Flight Manual dated July 30, 1994, or later 
GICA approved revisions. 
 
     The equipment described below may be installed: 
1. For agricultural aircraft equipment operations: 
- Spray system - Dwg. No. D98.000/01.0 or D98.100.00.0 or D98.000/11.0 
 
- Atomizing Equipment - Dwg. No. D98.000/03.0 or D98.200.00.0   and 
 
- Spreading Equipment - Dwg. No. D98.000/05.0 or   D98.300.00.0 or 
D.98.000/13.0 
 
     2. For despersing fire fighting materials: 
- Fire Bombing Equipment - Dwg. No. 98.000/07.0 or D99.100.00.0

Page 7 of 7 A47EU 
  Service Information Each of the documents listed below must state that it is approved by the European 
Aviation Safety Agency (EASA) or – for approvals made before October 24, 2005 – by 
the Civil Aviation Office (CAO) of Poland. (See Note 4) 
 
  • Service bulletins,  
   • Structural repair manuals,  
   • Vendor manuals,  
   • Aircraft flight manuals, and  
   • Overhaul and maintenance manuals.  
 
The FAA accepts such documents and considers them FAA-approved for type design 
data only unless one of the following conditions exists: 
 
• The documents change the limitations, performance, or procedures of the FAA 
approved manuals; or 
 
•The documents make an acoustical or emissions changes to this product’s U.S. type 
certificate as defined in 14 CFR § 21.93.  
 
The FAA uses the post type validation procedures to approve these documents.  The FAA 
may delegate on case-by-case to EASA to approve on behalf of the FAA for the U.S. type 
certificate.  If this is the case it will be noted on the document.  
 
 
NOTES: 
 
 
NOTE 1.  A current weight and balance report including list of equipment in certificated empty weight, and loading 
instructions, must be provided with each aircraft at the time of original airworthiness certification, and at all 
times thereafter. 
 
The certificated empty weight and corresponding center of gravity location must include undrainable oil (3.7 
lbs. at 53 inches) forward of datum, and unusable fuel (22.2 lbs. at 60 inches) aft of datum. 
 
NOTE 2.  Placards (Refer to Manufacturer's Specifications for a complete listing):  All required placards as listed in the 
approved Airplane Flight Manual must be installed in the appropriate locations. 
 
   Refer to the Airplane Flight Manual, Section 2, Limitations for a listing of required placards. 
 
NOTE 3.  Instructions for Continued Airworthiness and Service Life Limits of components include the  
Maintenance Manual (Section 8 of Airplane Description and Service Manual).  Revisions to Airworthiness 
Limitations must be GICA approved for the FAA.  The maximum service life of the models M-18 and M-
18A can be extended to a maximum of 6000 hours by compliance with service bulletins K/02-142/91 and 
E?02.152/94.  
 
All manufacturer's service bulletins (and other manual material) which contain a statement that the document 
is approved by the exporting airworthiness authority (GICA)  may be interpreted as FAA Approved.  These 
approvals pertain to the type design only. 
All service bulletins classified as Mandatory by the General Inspectorate Civil Aviation Authority are 
identified to that effect and are subject to an Airworthiness directive issued by the FAA. 
 
   Service documents required: 
   1. Airplane Description and Service Manual issued December 1979. 
 
NOTE 4. The national airworthiness authority (NAA) for this airplane is the Civil Aviation Office (CAO) of Poland. The CAO 
was previously known as CAIB, CACA and General Inspectorate of Civil Aviation (GICA).     
  
 
NOTE 5.                 Other serial numbers are also eligible on condition that modifications are performed according to service  
                                Bulletin issued by aircraft manufacturer. Service Bulletin no. E/02.187/2003 was issued to allow  
                                M18 airplanes S/N 1Z010-12, 1Z010-13, 1Z012-34, 1Z012-40, 1Z013-36 to be eligible for certificate  
                               A47EU.  
 
 
_…..END…..
```

## ADs (12, in force first)

- [AD 2000-18-12](https://openairdocs.org/ad/2000-18-12): Wing Attach Joints · Polskie Zaklady Lotnieze Spolka zo.o PZL M18, PZL M18A and PZL M18B. Effective Sep 27, 2000
- [AD 91-12-07](https://openairdocs.org/ad/91-12-07): Agriculture Equipment Electro-Hydraulic Control System · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Jul 5, 1991
- [AD 90-20-03](https://openairdocs.org/ad/90-20-03): Aileron Hinge · Polskie Zaklady Lotnieze Spolka zo.o PZL M18 and PZL M18A. Effective Oct 17, 1990
- [AD 90-20-04](https://openairdocs.org/ad/90-20-04): Engine Push-Pull Cables · Polskie Zaklady Lotnieze Spolka zo.o PZL M18 and PZL M18A. Effective Oct 17, 1990
- [AD 90-17-15](https://openairdocs.org/ad/90-17-15): Vertical Fin and Rib · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Sep 17, 1990
- [AD 87-03-09](https://openairdocs.org/ad/87-03-09): Engine Mount Nuts · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Mar 1, 1987
- [AD 86-13-01](https://openairdocs.org/ad/86-13-01): Check for Cracks · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Jul 19, 1986
- [AD 83-07-11](https://openairdocs.org/ad/83-07-11): Left and Right Braking Levers · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Apr 14, 1983
- [AD 83-07-02](https://openairdocs.org/ad/83-07-02): Counterweights Reinforcement · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Apr 7, 1983
- [AD 83-06-07](https://openairdocs.org/ad/83-06-07): Yaw Axis Flight Control · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Apr 4, 1983
- [AD 83-06-09](https://openairdocs.org/ad/83-06-09): Inflight Engine Shut-down Prevention · Polskie Zaklady Lotnieze Spolka zo.o PZL M18. Effective Apr 4, 1983
- [AD 83-07-19](https://openairdocs.org/ad/83-07-19): Primary Flight Control · Polskie Zaklady Lotnieze Spolka zo.o PZL M18

## Registered aircraft by registry model (OpenAirDocs)

- [WSK PZL Mielec PZL M18B](https://openairdocs.org/model/wsk-pzl-mielec-pzl-m18b): 1 aircraft (registry code 9810127)
- [WSK PZL Mielec PZL-M18A](https://openairdocs.org/model/wsk-pzl-mielec-pzl-m18a): 1 aircraft (registry code 9810126)

## STCs approved under this data sheet (28)

- [STC SA5783NM](https://openairdocs.org/stc/SA5783NM): Fabrication of Onboard Systems Model 7 CROPHAWK spray flow measuring system.. Onboard Systems International
- [STC SA01323CH](https://openairdocs.org/stc/SA01323CH): Installation of a ground single point fueling system.. Turbine Conversions Ltd
- [STC SA01406NY](https://openairdocs.org/stc/SA01406NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and
rotary wing. Airwolf Filter Corporation
- [STC ST03554CH](https://openairdocs.org/stc/ST03554CH): Installation of Rotary Gatekeeper and provisions equipment. Turbine Conversions Ltd
- [STC SA5154NM](https://openairdocs.org/stc/SA5154NM): Installation of a Lycoming T53-L7 turbine engine equipped with a Hamilton Standard 53C51 propeller.. Mr. Andrew Donohue
- [STC SA5155NM](https://openairdocs.org/stc/SA5155NM): Installation of a Cleveland wheel and brake assembly.. Mr. Andrew Donohue
- [STC SA01361SE](https://openairdocs.org/stc/SA01361SE): Installation of a Honeywell TPE331-10, -10U, -10UF, -10UG, -10UGR, -10UR engine in combination with Hartzell Propeller Model HC-B4TN-5NL/LT10890N, or HC-B4TN-5PL/LT10890N, or Honeywell TPE331-11U or -11UA engine in combination with a Hartzell HC-B5MP-5BL/LM11692N propeller.. Turbine Dromaders LLC
- [STC SA09063SC](https://openairdocs.org/stc/SA09063SC): Installation of geared tabs on ailerons, elevator, and vertical tail.. Turbine Installation LLC
- [STC SA01276AT](https://openairdocs.org/stc/SA01276AT): Increase in the Maximum Take off Gross Weight from 9260 lbs. To 11700 lbs.. Dromader USA LLC
- [STC SA09039SC](https://openairdocs.org/stc/SA09039SC): Installation of the AlliedSignal TPE331-10U engine with the Hartzell Model HC-B4TN-5NL/LT10890N propeller, or the installation of the AlliedSignal TPE331-10UA engine with either the Hartzell Model HC-B3TN-5/T10282 or HC-B3TN-5U/T10290N propeller;  or the installation of either the AlliedSignal TPE331-11U-612G or TPE331-12UA-701G engine with the Hartzell Model HC-B5MP-5BL/LM11692N propeller.. Delta Turbines Inc.
- [STC SA00946SE](https://openairdocs.org/stc/SA00946SE): ONE-ONLY: Installation of a Honeywell TPE331-10 engine and Hartzell propeller Model HCB4TN-5NL/LT10890N, serial number 1Z024-15.. Turbine Dromaders LLC
- [STC SA01216SE](https://openairdocs.org/stc/SA01216SE): ONE-ONLY: Installation of a Honeywell TPE331-10UG engine and Hartzell Propeller Model HC-B4TN-5NL/LT10890N, serial number 1Z023-06.. Turbine Dromaders LLC
- [STC SA00961CH](https://openairdocs.org/stc/SA00961CH): Installation of hydraulically driven material dispersal gate for fire fighting applications.. Turbine Conversions Ltd
- [STC SA01249SE](https://openairdocs.org/stc/SA01249SE): ONE-ONLY: Installation of a Honeywell TPE331-10UF engine and Hartzell Propeller Model HC-B4TN-5NL/LT10890N, serial number 1Z027-08.. Turbine Dromaders LLC
- [STC SA01737CH](https://openairdocs.org/stc/SA01737CH): Installation of a Wytwornia Sprzetu Komunikacyjnego (WSK) PZL-KALISZ ASz-62IR-M18/K9-
BB or/K9-BA model engine.. Dromader USA LLC
- [STC SA01473NY](https://openairdocs.org/stc/SA01473NY): Installation of Hamilton Standard model 23E50 propeller and 4G10 governor. Required limitations: Hub 23E50. Eligible blades 6477A-0 or 7149A-0 or 6277-0. Diameter 138.375 inches, no reduction. Pitch stops 15 degrees low, 35 degrees high. New Sioux Enterprises Ltd.
- [STC SA1014GL](https://openairdocs.org/stc/SA1014GL): Installation of Pratt and Whitney Canada PT6A-45A, -65B, -65R, -65AG, or -65AR engine, Hartzell HC-B5MP-3C/M10876 propeller, and related changed.. Turbine Conversions Ltd
- [STC SA01379CH](https://openairdocs.org/stc/SA01379CH): Installation of a fiberglass pressure cowling.. Turbine Conversions Ltd
- [STC SA00567WI](https://openairdocs.org/stc/SA00567WI): Installation of a Compro Aviation Driftfinder DFS-10 system which injects oil into engine exhaust to produce to determine wind speed and direction.. Compro Aviation Inc
- [STC SA00443SE](https://openairdocs.org/stc/SA00443SE): Installation of vortex generators on wings, installation of fuselage strakes, and removal of stall strips.. Micro AeroDynamics Inc
- [STC SA00278SE](https://openairdocs.org/stc/SA00278SE): Fabrication and Installation of vortex generators and 'delta wings' mounted on airplane wings, and strakes mounted above left and right-hand wing/fuselage junctions.. Aeronautical Testing Service Inc.
- [STC SA09027SC](https://openairdocs.org/stc/SA09027SC): Installation of Garrett TPE 331-10 turboprop engine and Hartzell propeller, P/N HC-B4TN-5JL/ LT10282N+4.. Hansen Air Activities
- [STC SA200CH](https://openairdocs.org/stc/SA200CH): Increase material hopper volume from 660 gallons to 780 gallons.. Turbine Conversions Ltd
- [STC SA3550SW](https://openairdocs.org/stc/SA3550SW): Installaton of electrically powered auxiliary hydraulic pump.. Southeast Arkansas Avn Co
- [STC SA00153AT](https://openairdocs.org/stc/SA00153AT): Installation of chemical evacuation system to remove residue from the agricultural spray dispersal system. (PZL M18 restricted category). Paul S Woods
- [STC ST00009AT](https://openairdocs.org/stc/ST00009AT): Installation of a chemical rinsing system.. Paul S Woods
- [STC SA1198GL](https://openairdocs.org/stc/SA1198GL): Extend M18 cockpit aft installing a second pilot's seat.. Turbines Inc
- [STC SA1735CE](https://openairdocs.org/stc/SA1735CE): Increase capacity of main fuel tanks from 53 to 112 U.S. gallons each.. Javelin Aircraft Co Inc

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