# TCDS A14EA: De Havilland Aircraft of Canada Limited

- Type: Type certificate data sheet
- Status: Current
- Holder: De Havilland Aircraft of Canada Limited
- Revision: 15
- Revised: October 19, 2026
- Product: Aircraft, Large Airplane
- Certification basis: Part 25, Part 21
- Registered aircraft: 12, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/4e/4e/4e4e6559bf8b183fc5e3934814953bd2271d33f5e6e7fae683d5a3e8410c4588
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153742859520261019135821.0001
- Page: https://openairdocs.org/tcds/A14EA

## Models (3)

As the data sheet lists them.

- CL-215-1A10
- CL-215-6B11 (CL-415 Variant)
- CL-215-6B11 (CL-215T Variant)

## What the data sheet says

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

```text
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
 
 
 
 
 
 
TYPE CERTIFICATE DATA SHEET NO. A14EA 
 
This data sheet which is a part of Type Certificate No. A14EA, 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 
 
 
 
Type Certificate Holder Record 
De Havilland Aircraft of Canada Limited 
4100 Westwinds Drive NE  
Calgary, Alberta  
Canada T3J 4L2 
 
Viking Air Limited transferred TC A14EA to De Havilland Aircraft of Canada 
Limited on August 1, 2024 
Bombardier Inc. transferred TC A14EA to Viking Air Limited on October 1, 2016 
Canadair Limited transferred Type Certificate A14EA to Bombardier Inc. On March 
6, 1998 
 
I. MODEL CL-215-1A10 Amphibious Flying Boat (Restricted Category) Approved May 15, 1969 by the FAA and 
March 7, 1969 by the Canadian Department of Transport. 
 
The CL-215-1A10 has been produced in five groups: Serial Numbers 1001 to 1030, 
1031 to 1050, 1051 to 1065, 1066 to 1080, and 1081 and subsequent. Data in this Type 
Approval that contains no specific reference to any group of serial numbers applies to 
all groups.  (See NOTE 4). 
 
Engines Two Pratt and Whitney Double Wasp CA3. 
 
Fuel Avgas Grade 100/130 minimum to CAN 2-3.25-M77 or MIL-G-5572. 
Avgas Grade 100 LL to ASTM Specification D910. 
 
Oil Engine:  All dispersant oils listed in Pr att & Whitney Aircraft Service Bulletin No. 1183 
P or subsequent issue. 
 
Engine Limits See AFM as list ed in Approved Publications. 
 
GPU-2 Type:   Andover Motors, Model 204 
Fuel same as Aircraft. 
Oil MIL-0-6082 grade 1065 or SAE 10W30 Automotive Oil 
Oil Quantity: U. S. gal. Imp. gal. 
0.9 0.75 
 
Propeller and Propeller Limits Ma nufacturer  Hamilton Sundstrand 
On aircraft 1001 to 1030 and 1039 and subsequent: Intermix in any combination of four 
types listed below: 
Propeller Types 
43E60-581 P1 
43E60-581 P2 
43E60-701 
43E60-583 
 
 
Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 
Rev. No. 15 10 5 5 9 10 12 14 12 13 12 13 14 
A14EA 
Revision No. 15 
De Havilland 
CL-215-1A10 
CL-215-6B11 (CL-215T Variant) 
CL-215-6B11 (CL-415 Variant) 
October 19, 2026

Blades  - Number and Type 
Three 6093A-10S (for -581P1 or P2) 
or Three 6901S-10 (for -701) 
or Three 6903A-10 (for -583) 
 
On aircraft 1031 to 1038: 
Propeller Type 
43E60-581 P3 
 
Blades - Number and Type 
Three 6903B-10S (for -581 P3) 
 
Diameter Limits Maximum 14 ft. 3 in (4.34 m) 
Minimum 13 ft. 11 1/2 in. (4.25 m) 
Pitch setting at 72-inch station 
For Propeller Type 43E60-581P1, 43E 60-581P2, 43E60-581P3 or 43E60-701: 
Low pitch stop 9.5 degrees ( 0.2 degrees) 
Constant speed range 9.5 degrees to 30 degrees  
Feathered 81 degrees ( 0.5 degrees) 
 
For Propeller Type 43E60-583: 
Low pitch stop 9.0 degrees ( 0.2 degrees) 
Constant speed range 9.0 degrees to 30 degrees  
Feathered 81 degrees ( 0.5 degrees) 
 
Except for transients, propeller must not be operated in the 1550 to 1750 RPM range. 
 
Airspeed Limits 
IAS CAS 
 knots m.p.h. km/h knots m.p.h. km/h 
VMO (Maximum Operating)       
S.L. to 12,000 ft. 188 216 348 190 219 352 
12,000 ft to 20,000 158 182 293 160 184 296 
VFE (Flaps Extended)       
10 138 159 255 140 161 259 
25 Land and       
Water Operation 110 127 204 112 129 207 
*25 Water Operation 114 131 211 116 133 215 
*Refers to aircraft 1056 & subsequent 
VA (Maneuvering Speed)       
 
 
 
 
Restricted Category 
      
A/C at 36000 lb.       
16329 kg MTOW.       
Water operation only 126 145 234 127 146 235 
**A/C at 37700 lb.       
17100 kg MTOW.       
Water operation only 128 147 237 129 148 239

3 A14EA 
   
IAS 
   
CAS 
 
 knots m.p.h. km/h knots m.p.h. km/h 
A/C at 43500 lb.       
19731 kg MTOW.       
Land operation only 149 171 276 150 173 278 
A/C at 93500 lb.       
19731 kg Lift-off and 15 
flap 
      
Water operation only 131 151 243 133 153 246 
VLE (Maximum Speed       
Landing Gear Extended) 129 148 239 130 150 241 
VLO (Maximum Speed       
Landing Gear Operation) 129 148 239 130 150 241 
VMCA (Minimum Control       
Speed with Automatic       
Propeller Feathering) 86 99 159 85 98 157 
VLL (Maximum speed at       
which landing lights may       
be extended or used) Not       
applicable to aircraft       
1081 and subsequent. 129 148 239 130 150 241 
**Refers to Serial Numbers 1003, 1007, 1008, 1009, 1012, 1017, 1018, 1020, 1031 and 
subsequent, and aircraft Serial Number 1001 through 1030 fitted with additional 
buoyancy compartment in accordance with Canadair Service Bulletin Number CL215- 
124. 
 
Restricted Category (water Bomber, including Chemical Foam, Configuration) 
  IAS   CAS  
 knots m.p.h. km/h knots m.p.h. km/h 
VFE (Maximum speed with       
flaps extended) 15 138 159 255 140 161 259 
VWD (Maximum airspeed at       
which water doors may       
be opened or operated       
in flight) 129 148 239 130 150 241 
Maximum speed on water 
with probes extended (water
      
speed) 80 92 148    
 *90 104 167    
*Refers to aircraft 1051 and subsequent and aircraft which embody Service Bulletin 
CL215-203. 
Restricted Category, Liquid Sprayer Configuration Only 
  IAS   CAS  
 knots m.p.h. km/h knots m.p.h. km/h 
VMO (Maximum Operating)       
S.L. to 20,000 ft 158 182 293 160 184 296 
VJD (Maximum airspeed at       
which jettison doors may       
be opened or operated in       
flight) 158 182 293 160 184 296

Maximum Weight (Water or Chemical/Water Mix Tanks in use)  
(See NOTE 1) 
 Lb. 
 (Kg) 
Ramp 43500 
(Land Operation) (19731) 
(Water Operation) 36300 
 (16465) 
*1* 38000 
*1* (17236) 
Take-off 43500 
(Land Operation) (19731) 
(Water Operation) 36000 
 (16329) 
*1* 37700 
*1* (17100) 
Landing 34400 
(Land Operation) (15604) 
*3* 37000 
*3* (16783) 
 
  Lb. 
  (Kg) 
(Water Operation)  35500 
  (16103) 
 *5* 37000 
 *5* (16783) 
Zero Fuel *4* 39000 
(Land Operation) *4* (17690) 
  41000 
  (18597) 
(Water Operation)  41000 
  (18597) 
 
Water Bomber, including Chemical Foam, Configuration only 
Touch-down for water 33500 
Pick-up (15195) 
*2* 35500 
*2* (16103) 
Lift-off following 43500 
Water Pick-up (19731) 
*1*  Refers to Serial Numbers 1003, 1007, 1008, 1009, 1012, 1017, 1018, 1020, 
1031 and subsequent, and aircraft Serial Number 1001 through 1030 fitted with 
additional buoyancy compartment in accordance with Canadair Service Bulletin 
Number CL215-124. 
*2* Refers to aircraft Serial Numbers 1051 and subsequent, and aircraft which 
incorporate New Probe System to Canadair Service Bulletin CL215-203. 
*3* Refers to aircraft 1056 to 1125 which incorporate Canadian Service Bulletin 
CL-215-376. 
*4*  Refers to aircraft in the Liquid Sprayer Configuration. 
*5*  Refers to aircraft 1056 and subsequent.

5 A14EA 
C.G. Limits See AFM as listed in Approved Publications. 
 
Maximum Occupants Ten (including two crew).  Limite d by approved seating arrangements. In particular, 
see (See NOTE 2) 
 
Maximum Cargo General Cargo 
Load distribution must not exceed 150 lb./sq. ft. (732.36 kg/m2), nor 500 lbs. (226.8 
kg) per running foot. For compartment limitations, refer to the following Canadair 
Reports: 
RAW-215-110 for S/N 1001 to 1030. 
RAW-215-144 for S/N 1001 to 1030 (Liquid Sprayer). 
RAW-215-146 for S/N 1031 to 1055. 
RAW-215-145 for SAR Aircraft S/N 1031 to 1038. 
RAW-215-172 for SAR Aircraft S/N 1058 to 1059. 
RAW-215-174 for S/N 1062 and 1063. 
RAW-215-190 for S/N 1056 and subsequent. 
 
Jettisonable Liquid Cargo: 
Water Bomber Configuration: Two tanks at Station 403.8, maximum water load of 
6000 lb. (2722 kg) each.  Volume 706 gallons (588 Imp. gallons) each. 
 
Liquid Sprayer Configuration: Five cabin installed tanks with total maximum 
chemical/water load of 10,500 lb. (4763 kg).  Volume 1400 gallons (1166 Imp. gallons). 
 
Chemical Foam Configuration: Two tanks at Station 403.8, maximum load, water or 
chemical/water mix, of 6000 lb. (2722 kg) each. Volume 706 gallons (588 Imp. 
gallons) each. 
 
Non Jettisonable Liquid Cargo 
Chemical concentrate for Chemical Foam operations. Four cabin installed storage tanks 
with total maximum chemical load of 1,566 lb. (710 kg). Volume 158 US gallons (132 
Imp). 
 
Additional Cargo Limitations 
(a) Carriage of general cargo in the cabin is prohibited when the water or chemical 
concentrate or chemical/water mix tanks are in use. 
(b) Landing with jettisonable water or chemical/water load in the tanks is prohibited. 
(c) All chemicals to be used in Liquid Spraying Operations must be approved by the 
local environmental authorities prior to commencement of spraying. 
(d) All chemicals to be used in Chemical Foam operations must comply with Canadair 
Material Specification CMS560-01 and be approved by the local environmental 
authorities prior to commencement of foam fire fighting operations. 
 
Fuel Capacity Usable Fuel 
U.S. gal. Imp. gal. 
S/N 1001 to 1030 1146 954 
S/N 1031 and Sub. 1562 1301 
Oil Capacity Engines: (eac h) U.S. gal. Imp. gal. 
Total  36.0  30.0 
Usable* 30.7 25.6 
* Excluding propeller feathering reserve of 2.0 gallons (1.7 Imp. gal.) each engine. 
 
Control Surface Movements Controls to be rigged in  accordance with the following Canadair Drawings: 
(a) P215-90014 Diagram Aileron Controls. 
(b) P215-90015 Diagram Elevator Controls. 
(c) P215-90016 Diagram Rudder Controls.

Maximum Operating Altitude Take-off and landing 8000 feet 
(Pressure Altitude) Enroute 20,000 feet 
Maximum altitude for water pick-up 5000 feet* 
* 8000 feet for water pick-up on A/C S/N 1051 and subsequent and aircraft 
incorporating Canadair Service Bulletin CL215-203. 
 
Additional Limitations Dispatch into known icing condit ions is prohibited unless aircraft is modified in 
accordance with Canadair Modification Summary SC-21002 and operated in accordance 
with Supplement II of the DOT Approved Flight Manual PSP 291. 
 
Serial Numbers Eligible Serial Number 1001 to 1125. (See NOTE 4). 
 
Placards Placards are listed in the following Canadair Drawings: 
215-40053, 215-40440, 215-40443, 215-51004, 215-51137, 215-51311,  215-51312, 
215-51314, 215-51317, 215-51387, 215-51402, 215-66000, (See NOTE 3). 
 
Approved Publications D.O.T. Approve d Airplane Flight Manual, Canadair Product Support Publication No. 
191 for S/N 1001 to 1030 and Publication No. 291 for S/N 1031 and subsequent. 
 
D.O.T. Approved Maintenance Specification, Canadair Product Support Publication No. 
295. 
 
D.O.T. Approved Drawing List, Canadair Report No. RAL-215-101. 
 
D.O.T. Approved Loading Instructions.  (See NOTE 6). 
 
Life Limited Parts Required retirement times for life- limited components are as prescribed in the D.O.T. 
Approved Maintenance Specification, Canadair Product Support Publication No. 295. 
 
II. Model CL-215-6B11 (CL-215T Variant), Restricted Category, Amphibious Flying Boat 
Restricted Category, Approved March 30, 1993 by the FAA and March 28, 1991 by the Canadian Department of Transport 
(DOT) 
 
III. Model CL-215-6B11 (CL-415 Variant), Restricted Category 
Approved October 14, 1994 by the FAA and June 24, 1994 by the Canadian Department of Transport (DOT) 
 
DATA PERTINENT TO CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant) 
Engines Two Pratt & Whitney Canada 
(See NOTE 7) PW123AF (Turboprop) w ith P&WC SB 21211 incorporated. 
 
Fuel Fuels conforming to any of the follo wing specifications are approved for use. 
 
Mixing of fuels is permitted. 
 
TYPE SPECIFICATION 
 
Kerosene 
CANADA USA UK 
 
Jet A, A-1 
 
CGSB 3.23 
 
ASTM D1655 
 
DERD 2494 
JP8 3-GP-23 MIL-T-83133 DERD 2453 
Wide Cut*    
Jet B CGSB 3.22 ASTM D1655 DERD 2486 
JP4 CGSB 3.22 MIL-T-5624 DERD 2486 
High Flash  
3-GP-24 
 
MIL-T-5624 
 
DERD 2452 JP5 
 
*NOTE: Refer to Flight Manual Limitations Section for operating limits for JP4/Jet B 
fuel.

7  A14EA 
Oil Engine:   All MIL-L-23699, type II oils and Castrol 4000   
Engine Limits See AFM as list ed in Approved Publications.   
Airspeed Limits    
 IAS  CAS 
 knots m.p.h. km/h knots m.p.h. km/h 
 VMO (maximum Operating) 187 215 347  190 219 260 
 S.L. to 20,000 feet   
 VFE (Flaps Extended) 10 138 159 256  140 161 260 
 15 138 159 256  140 161 260 
 25 114 131 211  116 134 215 
 25* 116 134 215  117 135 217 
 25** 119 137        220  120 138        222 
 
VA (Maneuvering Speed) 
 
See Flight Manual for variation of VA with aircraft weight. 
 
* For CL-215-6B11 (CL-215T Variant) Refer to A/C 1056 and subsequent incorporating 
Canadair S.B. 215-376 
** For CL-215-6B11 (CL-415 Variant). 
VLE (Maximum Speed-Landing 
Gear Extended) 129 148 239 130 150 241 
 
VLO (Maximum Speed-Landing 
Gear Operation) 129 148 239 130 150 241 
 
VMCA (Minimum Control Speed 
in the air with Automatic 
Propeller Feathering 
Operative) 84 97 155 84 97 155 
 
VLL (Maximum speed at which 
Landing lights may be 
extended or used)** 129 148 239 130 150 241 
** not applicable to A/C 1081 and subsequent 
VWD (Maximum Speed at which 
water doors may be opened or 
operated in flight) 129 148 239 130 150 241 
 
Maximum speed on  
Water with Probes 80 92 148 
extended (water speed) *90 104 167 
 
* Refers to aircraft 1051 and subsequent and aircraft which embody Service bulletin 
CL215-203. 
 
C.G. Limits See AFM as listed in Approved Publications. 
 
Maximum Cargo Additional Cargo Limitations 
(a) Carriage of general cargo in the cabin is prohibited when water tanks are in use. 
(b) Landing with jettisonable water load in the tanks is prohibited.

Fuel Capacity Usable Fuel 
Pressure refueling: 1530 gallons (1275 Imperial Gallons) (Total Capacity) 
Gravity refueling: 1562 gallons (1301 Imperial Gallons) (Total Capacity) 
Maximum refuel pressure:  50 psig. 
 
Oil Capacity Engines: (Each) 
Total 
U.S. Gal. 
5.1 
Imp. Gal. 
4.3 
 Usable 0.9 0.8 
Control Surface Movements Rudder 
Elevator 
Aileron 
30R 
23L 
Up 22 
Down 20 
Up 20  
Down 13.75 
 0.5 
 0.5 
 0.5 
 0.5 
 0.5 
 0.5 
Neutral 2  TE up 
Additional Limitations Dispatch into kn own icing conditions is prohibited 
DATA PERTINENT TO CL-215-6B11 (CL215T Variant) 
The data in this Type Approval apply to Aircraft model CL-215-1A10 retrofitted with 
the Canadair Modification Kit described in: 
- Report RAD-215T-103 (Kit Specification for the Retrofit of CL-215-piston aircraft 
with turboprop engines) for A/C with S/Ns 1056, 1057, 1061, 1080, 1109, 1113, to 
1122, 1124, 1125. 
 
- Report RAL-K215T-0001 Rev. A or later approved revision (K215T Engineering 
Configuration Statement), as amended by Modification Summaries, for A/C with S/Ns 
1081 to 1090, 1092 to 1108, 1110 to 1112, and 1123. 
 
After embodiment of the kit, affected A/C shall be redesignated as model CL-215-6B11 
(CL-215T Variant). 
 
Propeller and Manufacturer: Hamilton Sundstrand 
Propeller Limits Propeller Type: Two 14SF-17 (four-bladed) or  
Two 14SF-19 (four-bladed) 
Diameter:13 feet, 1/4 inch (3.97m) 
 
Pitch setting at 42-inch station: 
Reverse: -10  1.17 (dynamic conditions) 
-13.6 to -15.6 reverse pitch stop position 
Feathered: 86.0 

Maximum Weight Restricted Category 
(Mass) 
 
(See NOTE 1) Take-Off  lb.  kg 
Land Operation 43,500 19,731 
Water Operation 37,850 17,168 
 
(For other weights see AFM as listed in Approved Publications). 
 
Maximum Occupants (a)   Ten (including two crew).  Limited by approved seating arrangements. In 
particular, see NOTE 2. 
 
 
Maximum Cargo General Cargo 
Load distribution must not exceed 150 lb./sq.ft. (732.36 kg/m2), nor 500 lbs. (226.8 kg) 
per running foot. For compartment limitations, refer to the following Canadair Report: 
RAW-215T-102

9 A14EA 
Jettisonable Liquid Cargo: 
Water Bomber Configuration: Two tanks at Station 403.8, maximum water load of 6000 
lb. (2722 kg) each.  Volume 706 gallons (588 Imp. gallons) each. 
 
Maximum Operating Take-off and Landing: 10000 feet 
Altitude Enroute: 20000 feet 
(Pressure Altitude) Water Pick-up: 5000 feet 
8000 feet (1) 
(1) A/C incorporating Canadair SB CL215-203 
Serial Numbers Eligible Serial Numbers 1056, 1057, 106 1, 1080, 1109, 1113 to 1122, 1124, 1125 retrofitted per 
RAD-215T-103 and Serial Numbers 1081 to 1090, 1092 to 1108, 1110 to 1112 and 1123 
in retrofit per RAL-K215T-0001. 
 
Placards Substitution and/or removal of existing placards on CL-215-1A10 in addition to new 
(See NOTE 3) placards, as  specified in Canadair Report MBS-215T-111 required to achieve model 
CL-215-6B11 aircraft (refer to Approved Publications). 
 
Approved Publications CL-215-6B11 (S/N 1056,  1057, 1061, 1080, 1109, 1113 to 1122, 1124, 1125 
 
D.O.T. Approved Airplane Flight Manual, Product Support Publication No. 391 
 
D.O.T. Approved Airworthiness Limitations, scheduled inspections and 
maintenance intervals sections of D.O.T. Approved Standard Maintenance 
Specifications, Product Support Publication No. 395. 
 
D.O.T. Approved Drawing List, Canadair Report No. RAL-215-xxx (for each individual 
aircraft) (CL-215-1A10) in addition to the following Canadair Modification Summaries 
(to achieve model CL-215-6B11): 
215T001A, 215T001B, 215T001C, 215T001D, 215T003, 215T004, 215T011, 215T012, 
215T013, 215T016, 215T017, 215T020A, 215T020B, 215T020C, 215T020D, 215T021, 
215T024, 215T025, 215T026. 
 
D.O.T. Approved Loading Instructions (see NOTE 6). 
 
CL-215-6B11 (S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 1123 
 
D.O.T. Approved Airplane Flight Manual, Product Support Publication No. 391-1 
 
D.O.T. Approved Airworthiness Limitations, scheduled inspections and 
maintenance intervals sections of D.O.T. Approved Standard Maintenance 
Specifications, Product Support Publication No. 395-1. 
 
D.O.T. Approved Drawing List, Canadair Report No. RAL-215-xxx (for each individual 
aircraft) (CL-215-1A10) in addition to th e following Canadair Modification Summary 
(to achieve model CL-215-6B11): 
215T60010 
 
D.O.T. Approved Loading Instructions (see NOTE 6). 
 
Airworthiness CL-215-6B11 (S/N 1056, 1057, 1061, 1080, 1109, 1113 to 1122, 1124, 1125 
Limitations The Airworthiness Limitations are prescribed in the D.O.T. Approved Standard 
Maintenance Specification, Product Support Publication No. 395, Airworthiness 
Limitation Section. 
 
 CL-215-6B11 (S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 1123 
The Airworthiness Limitations are prescribed in the D.O.T. Approved Standard 
Maintenance Specification, Product Support Publication No. 395-1, Airworthiness 
Limitation Section.

DATA PERTINENT TO CL-215-6B11 (CL-415 Variant) 
The data in this Type Approval applies to Aircraft Model CL-215-6B11 described by 
Report RAL-415-101 Issue NC plus Mod. Sums. 
 
Propeller and Manufacturer: Hamilton Sun dstrand 
Propeller Limits Propeller Type: Two 14SF-19 (four-bladed) 
 Diameter: 
 
Pitch setting at 42-inch station: 
13 feet, 1/4 inch (3.97m) 
Reverse: -10  1.17 (dynamic conditions) 
-13.6 to -15.6 reverse pitch stop position 
Feathered: 86.0 

Maximum Weight Take-Off Re stricted Category  lb.  kg 
(Mass) Land Operation 43,850 19,890 
(See NOTE 1) Water Operation 37,850 17,169 
(For other weights see AFM as listed in Approved Publications). 
 
Maximum Occupants (a)   Ten (including two crew).   Limited by approved seating arrangements. 
(See NOTE 2) 
 
Maximum Cargo General Cargo 
Load distribution must not exceed 150 lb./sq. ft. (732.36 kg/m2), nor 500 lbs. (226.8 
kg) per running foot. For compartment limitations, refer to the following Canadair 
Report:   RAW-415-102 
 
Maximum Water Tank Capacity: (Water Bomber Configuration:) 
 
 VOLUME WEIGHT 
Gallons Imp Gal lb. kg 
Inboard tanks (2) 838 698 6980 3167 
Outboard tanks  (2) 783 652 6520 2957 
All tanks (4) 1621 1350 13500 6124 
 
Maximum Operating Take-off and Landing: 10000 feet 
Altitude Enroute: 20000 feet 
(Pressure Altitude) Water Pick-up: 8000 feet 
Serial Numbers Eligible Serial Number 2001 to 2999 
Placards Required placards are specified in Canadair report MBS-215T-105 
 
Approved D.O.T. Approved Airplane Flight Ma nual Canadair Product Support Publication No. 
491 Publications D.O.T. Approved Airworthiness limitations, scheduled inspections and 
maintenance intervals sections of Canadair Product Support Publication No. 495. 
 
D.O.T. Approved Drawing List and Modification Summary listed in Canadair Report 
No. RAL-415-101 which defines the build standard of the production CL-415. 
 
D.O.T. Approved Loading Instructions (See NOTE 6) 
 
Airworthiness The Airworthiness Limitations ar e prescribed in the Standard Maintenance 
Specification, Limitations Canadair Product Support Publication No. 495, 
Airworthiness Limitations Section. 
 
DATA PERTINENT TO ALL MODELS EXCEPT AS INDICATED 
Datum The reference datum is located 300 inches  (762 cm) forward of the keyhole slot in the 
chine angle on both sides of the fuselage at station 300.0. 
 
Leveling Means Longitudinal:  Lugs  on left hand nose wheel well sidewall at stations 170.0 and 182.5. 
Lateral:  Lugs on front face of nose wheel well rear bulkhead, station 222.50.

11 A14EA  
Mean Aerodynamic The leading edge of the MAC is  366.57 inches (931.08 cm) aft of the reference 
datum. Chord (MAC) The length of the MAC is 139.4 inches (354.07 cm). 
 
Minimum Crew Two (Pilot and Co-Pilot) 
 
Certification Basis CL-215-1A10 S/N 1001 to 1030 
FAR 21.29(a)(1)(ii), FAR Part 25, dated February 1, 1965 plus amendment 25-18 dated 
September 29, 1968 with the deviations recorded in the following documents. 
 
Canadair Report No. RAO-215-100, Issue 2, dated 15 January 1966, including Revision 
"A" dated 28 February, 1969, and Revision "B" dated 21 May, 1970, and modified by 
D.O.T. letter dated 26 February, 1971. 
 
CL-215-1A10 S/N 1031 to 1125* 
FAR 21.29(a)(1)(ii), FAR Part 25, dated February 1, 1965 plus amendment 25-18 dated 
September 29, 1968 with the deviations recorded in the following documents. 
 
Canadair Report No. RAO-215-100, Issue 2, dated 15 January 1966, including Revision 
"A" dated 28 February 1969, Revision "B" dated 21 May, 1970, Revision "C" dated 13 
September, 1973 and Revision "C", Addendum 1 dated 27 May, 1974, modified by 
DOT letter dated 23 April 1974, and by DOT letter dated 9 December 1981. 
 
*  For Aircraft S/N 1058, 1059, 1062 and 1063, see NOTE 4. 
 
CL-215-6B11 (CL-215T Variant), and CL-215-6B11 (CL-415 Variant) 
FAR 21.29(a)(1)(ii), FAR Part 25, dated February 1, 1965 plus amendment 25-18 dated 
September 29, 1968 and selected requirements of FAR Part 25 including amendments 
25-1 through 25-61 and of Airworthiness Manual Chapters 525 and 516, as specified in, 
and including the deviations recorded in, the following document: 
 
Canadair Report RAO-215-100, Issue 2, Revision H, dated September 19, 1991 for 
CL-215-6B11 (CL-215T Variant) with S/N 1056, 1057, 1061, 1080, 1109, 1113 to 
1122, 1124, 1125. 
 
Canadair Report RAO-215-100, Revision I-1, CL-215-6B11 (CL-215T Variant) with S/N   
1081 to 1090, 1092 to 1108, 1110 to 1112, 1123. 
 
Canadair Report RAO-215-100, Issue 2 Revision I, for CL-215-6B11 (CL-415 Variant) 
Compliance with the following requirements has been established: 
SFAR 27-2, Environmental Protection Agency Final Venting and Exhaust Emission 
Requirements For Turbine Powered Aircraft. 
 
Noise requirements of FAR Part 36 with Amendments 36-1 through 36-17, change 22 
Appendices A, B, and C. 
 
Findings of Equivalent Safety: 
 
a) FAR Part 25.901(b)(1)(i) Installation 
b) FAR Part 25.1045(e) Cooling Test Procedures 
 
CL-215-1A10, and CL-215-6B11 (CL-215T & CL-415 Variants) 
Compliance with the following requirements has been established: 
 
Ditching provisions of FAR Part 25.801(b) through (e), and 25.807(d). (The 
requirements of 25.1415(a) through (d) are not applicable, per Report RAO-215-100, 
Appendix 11, item RU.801).

CL-215-6B11 (CL-215T Variant) with S/N 1081 to 1090, 1092 to 1108, 1110 to 
1112, 1123 
 
ELOS Memo Requirement Title 
AT09323NY-
T-P-1 
14 CFR 25.1549(a)(b)(c) Digital Only Display of the Turbine 
Engine Required Parameters 
 
CL-215-6B11 (CL-415 Variant) 
Transport Canada Special Conditions (Airworthiness) 
SCA 93-4 High Intensity Radiated Fields (HIRF) (Ref FAA Issue Paper 
SE-3) SCA 93-5 Lighting Protection (Ref FAA Issue Paper SE-2) 
 
Import requirements  A Restricted U.S. Airworthiness Certificate may be issued for the aerial dispensing 
of liquids approved under the special purpose of forest and wildlife conservation on 
the basis of the Canadian Department of Transport "Certificate of Airworthiness 
for Export" signed by or for the Minister of Transport. This form must contain the 
following statement: "The aircraft covered by this certificate has been examined 
and found to comply with the provisions of the following: 
 
CL-215-1A10 
Canadair Ltd. Report No. RAO-215-100, Issue 2 dated January 15, 1966, 
including Revision "A" dated February 28, 1969, and Revision "B" dated May 
21, 1970, plus FAA's "additional requireme nts" presented in Attachment "A" 
to FAA's minutes of November 10, 1966 meeting, as amended by FAA's letter 
dated December 5, 1968. 
 
CL-215-6B11 (CL-215T Variant) with S/N 1056, 1057, 1061, 1080, 1109, 1113 to 1122, 
1124, 1125 Canadair Report RAO-215-100, Issue 2, Revision H, dated September 19, 
1991. 
 
CL-215-6B11 (CL-215T Variant) with S/N 1081 to 1090, 1092 to 1108, 1110 to 1112, 
1123 Canadair Report RAO-215-100, Revision I-1. 
 
CL-215-6B11 (CL-415 Variant) 
Canadair Report RAO-215-100, Issue 2, Revision I. 
 
Reference Canadian D.O.T. Type Approval No. A-86, Issue 25, dated October 1, 
2016, FAA Type Certificate A14EA. 
 
Production Basis "Does not apply

13 A14EA 
NOTE 1 Definitions:  For the purposes of th is Type Certification and with reference to information on aircraft weight 
and C.G., the following definitions apply: 
 
Restricted Category Aircraft configured such that water or Chemical/Water Mix may be loaded and 
promptly jettisoned. 
 
NOTE 2 Carriage of Persons 
The carriage of persons in the cabin of Restricted Category Aircraft is only permitted when: 
i. Such persons are Cargo Handlers or persons employed in support of the operation; and 
ii. The water tanks are not in use. 
 
NOTE 3 All required Placards must be installed in the specified locations. 
 
NOTE 4 Aircraft S/N 1058 and 1059 are not eligible for a U.S. Certificate of Airworthiness until compliance has 
been shown with requirements FAR 25.813(a) and 25.815. (Reference DOT Telex LIAE 120 dated 17 June 
1978). 
 
Aircraft S/N 1062 and 1063 are not eligible for a U.S. Certificate of Airworthiness until compliance has 
been shown with requirements FAR 25.803, 25.809, 25.813(a) and 25.875(b). (Reference DOT Telex 
LIAE 10 dated 22 January 1979). 
 
NOTE 5 The aircraft must be operated in accordance with all sections of the Approved Flight Manual as listed in the 
Approved Publications. 
 
NOTE 6 The current Weight and Balance Report, containing the list of equipment included in the approved empty 
weight and loading instructions, must be provided for each aircraft. 
 
NOTE 7 Every CL415 manufactured and every CL215T conve rsion after June 1994 must have PW123AF engines 
with SB 21211 incorporated or later superseding SB. For CL215T converted before June 1994 if SB 21211 
is not incorporated on both engines then both engines must have SB 21113 and the aircraft must have SB 
215-A3030 until both engines incorporate SB 21211 or later superseding SB. 
 
NOTE 8 REMOVED 
 
...END....
```

## ADs (51, first 50, in force first)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025
- [AD 2023-07-10](https://openairdocs.org/ad/2023-07-10): Equipment/furnishings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 20, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2019-25-11](https://openairdocs.org/ad/2019-25-11): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Feb 10, 2020
- [AD 2019-08-12](https://openairdocs.org/ad/2019-08-12): Flight controls · Viking Air CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 13, 2019
- [AD 2019-02-05](https://openairdocs.org/ad/2019-02-05): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Mar 22, 2019
- [AD 2017-17-17](https://openairdocs.org/ad/2017-17-17): Hydraulic power · Viking Air CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 11, 2017
- [AD 2017-15-14](https://openairdocs.org/ad/2017-15-14): Equipment/ Furnishings · Viking Air CL-215-6B11 (CL-415 Variant). Effective Sep 5, 2017
- [AD 2015-02-02](https://openairdocs.org/ad/2015-02-02): Flight Controls · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 11, 2015
- [AD 2014-16-08](https://openairdocs.org/ad/2014-16-08): Nacelles/Pylons · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Sep 23, 2014
- [AD 2013-20-09](https://openairdocs.org/ad/2013-20-09): ATA Code 53, Fuselage · Bombardier CL-215-6B11 (CL-415 Variant). Effective Oct 18, 2013
- [AD 2012-11-04](https://openairdocs.org/ad/2012-11-04): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jul 9, 2012
- [AD 2012-05-05](https://openairdocs.org/ad/2012-05-05): Equipment/Furnishings · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Apr 24, 2012
- [AD 2011-22-06](https://openairdocs.org/ad/2011-22-06): Landing Gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 14, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2009-05-04](https://openairdocs.org/ad/2009-05-04): Rudder lower torque tube · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 16, 2009
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 2005
- [AD 2004-26-08](https://openairdocs.org/ad/2004-26-08): Mounting Pad Studs of the Auxiliary Feather Pump · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Feb 9, 2005
- [AD 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 2004-10-04](https://openairdocs.org/ad/2004-10-04): Rear engine mount struts · Bombardier CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 21, 2004
- [AD 2004-03-13](https://openairdocs.org/ad/2004-03-13): Main landing gear (MLG) axles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 17, 2004
- [AD 2002-12-12](https://openairdocs.org/ad/2002-12-12): Wing-to-Fuselage Frame Angles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jul 25, 2002
- [AD 98-05-11](https://openairdocs.org/ad/98-05-11): Switching Valve-to-Rear Inlet Case Sealing Air Tube Assembly · Bombardier CL-215-6B11 (CL-215T Variant). Effective Mar 23, 1998
- [AD 97-11-09](https://openairdocs.org/ad/97-11-09): AFM - Limitation Section - Power Levers · Bombardier CL-215-6B11 (CL-215T Variant). Effective Jun 12, 1997
- [AD 97-11-08](https://openairdocs.org/ad/97-11-08): AFM - Limitation Section - Power Levers · Bombardier CL-215-6B11 (CL-415 Variant). Effective Jun 6, 1997
- [AD 96-23-13](https://openairdocs.org/ad/96-23-13): DC Generators · Bombardier CL-215-1A10. Effective Dec 5, 1996
- [AD 96-05-06](https://openairdocs.org/ad/96-05-06): Inspect Main Distribution Center and Electrical Components · Bombardier CL-215-1A10. Effective Mar 22, 1996
- [AD 93-16-06 R2](https://openairdocs.org/ad/93-16-06-R2): Rudder-Aileron Interconnect Tab · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 25, 1995
- [AD 78-08-02](https://openairdocs.org/ad/78-08-02): Water Door Hinge Plates · Bombardier CL-215-1A10. Effective Apr 14, 1978
- [AD 77-17-13](https://openairdocs.org/ad/77-17-13): Nose Landing Gear Doors · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Aug 30, 1977
- [AD 77-15-03](https://openairdocs.org/ad/77-15-03): Elevator Torque Tube Quadrant · Bombardier CL-215-1A10. Effective Jul 27, 1977
- [AD 77-13-05](https://openairdocs.org/ad/77-13-05): Missing Rivets In Bulkhead · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 29, 1977
- [AD 77-10-14](https://openairdocs.org/ad/77-10-14): Main Landing Gear Actuator · Bombardier CL-215-1A10. Effective May 26, 1977
- [AD 77-09-04](https://openairdocs.org/ad/77-09-04): Main Landing Gear Wheel Well · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 77-09-05](https://openairdocs.org/ad/77-09-05): Nose Landing Gear · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 77-09-06](https://openairdocs.org/ad/77-09-06): Lower Rudder Bearing · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 75-12-02](https://openairdocs.org/ad/75-12-02): Engine Fire Bottles · Bombardier CL-215-1A10. Effective May 30, 1975
- [AD 72-15-04](https://openairdocs.org/ad/72-15-04): Flame Propagation In Engine Fire Zone · Bombardier CL-215-1A10. Effective Jul 25, 1972
- [AD 71-04-04](https://openairdocs.org/ad/71-04-04): Failure Water Door Tension Rod · Bombardier CL-215-1A10. Effective Feb 25, 1971
- [AD 70-01-05](https://openairdocs.org/ad/70-01-05): Chine Spray Strips · Bombardier CL-215-1A10. Effective Dec 8, 1970
- [AD 2013-11-03](https://openairdocs.org/ad/2013-11-03) (historical): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 14, 2013
- [AD 2011-03-08](https://openairdocs.org/ad/2011-03-08) (historical): Landing gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 14, 2011
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2005-18-05](https://openairdocs.org/ad/2005-18-05) (historical): Lower caps of the wing front spar and rear spar · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 6, 2005
- [AD 99-16-04](https://openairdocs.org/ad/99-16-04) (historical): Inspect Fuselage Frame-Angles · Bombardier CL-215-1A10. Effective Sep 7, 1999
- [AD 98-04-08](https://openairdocs.org/ad/98-04-08) (historical): Inspect Lower Cap of Wing Front & Rear Spars · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 4, 1998
- [AD 96-12-11](https://openairdocs.org/ad/96-12-11) (historical): Water Door Actuator Microswitches · Bombardier CL-215-1A10. Effective Jun 21, 1996
- [AD 95-22-04](https://openairdocs.org/ad/95-22-04) (historical): Main Landing Gear Axle · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 8, 1995

All 51: https://openairdocs.org/tcds/A14EA/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Canadair CL-215-6B11(CL-215T)](https://openairdocs.org/model/canadair-cl-215-6b11-cl-215t): 6 aircraft (registry code 1900321)
- [Bombardier CL-215-6B11 (CL-415)](https://openairdocs.org/model/bombardier-cl-215-6b11-cl-415): 4 aircraft (registry code 1390019)
- [Canadair CL215 1A10](https://openairdocs.org/model/canadair-cl215-1a10): 2 aircraft (registry codes 1900111, 1900320)

## STCs approved under this data sheet (27)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc.
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc.
- [STC ST00164IB](https://openairdocs.org/stc/ST00164IB): Manufacture and Installation of Foam Injection System. Cascade Aerospace Inc.
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC ST00045IB](https://openairdocs.org/stc/ST00045IB): Installation of the NAT N301A Audio Panel. Avionics Design Services Ltd.
- [STC ST00040IB](https://openairdocs.org/stc/ST00040IB): Installation of the NAT N301A-021 Audio Panel. Avionics Design Services Ltd.
- [STC ST04490NY](https://openairdocs.org/stc/ST04490NY): Installation of the Audio System. Cascade Aerospace Inc.
- [STC ST04689NY](https://openairdocs.org/stc/ST04689NY): Installation of the Artex Emergency Locator Transmitter (ELT). Genesys Certification Services Inc.
- [STC ST04653NY](https://openairdocs.org/stc/ST04653NY): Installation of the Collins Aerospace Angle of Attack Indicating System. B/E Aerospace Limited
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc.
- [STC ST04603NY](https://openairdocs.org/stc/ST04603NY): Installation of NAT N301A-021 Audio Panel. Avionics Design Services Ltd.
- [STC ST04482NY](https://openairdocs.org/stc/ST04482NY): Installation of the Avionics Modifications. Aerocorp Avionic Solutions Inc
- [STC ST04424NY](https://openairdocs.org/stc/ST04424NY): Installation of a NAT N301A-021 Audio Panel. Avionics Design Services Ltd.
- [STC ST04432NY](https://openairdocs.org/stc/ST04432NY): Installation of a NAT N301A-021 Audio Panel. Avionics Design Services Ltd.
- [STC ST04398NY](https://openairdocs.org/stc/ST04398NY): Installation of the NAT N301A-021 Audio Panel. Avionics Design Services Ltd.
- [STC ST00813DE](https://openairdocs.org/stc/ST00813DE): Replacement of Honeywell (formerly Sperry) ED-800 cathode ray tube (CRT) display, part number 7003110-90 I or 7003110-902, with Esterline CMC Electronics CMA-6800 multi-purpose liquid crystal display (LCD),. Peregrine
- [STC SA00944CH](https://openairdocs.org/stc/SA00944CH): Replace Janitrol combustion heater Model 81D94-X (XX) with C&D Associates combustion heater Model CD25K, CD35K, and CD45K. Hartzell Engine Technologies, LLC
- [STC SA571NE](https://openairdocs.org/stc/SA571NE): Installation of cockpit vapor cycle air conditioning system kit No. 215-CCA-001.. Rilpa Enterprises, Ltd
- [STC ST01425NY](https://openairdocs.org/stc/ST01425NY): Installation of a Flight Deck Cooling System.. ACS-NAI Limited
- [STC ST01824NY](https://openairdocs.org/stc/ST01824NY): Installation of Northern Airborne Technology Satphone.. Northern Airborne Technology Ltd
- [STC ST02248NY](https://openairdocs.org/stc/ST02248NY): Installation of EMS HSD-64, HSD-128, HSD-HCM, and HSD-X. EMS Technologies Canada Ltd
- [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models.. SMR Technologies
- [STC ST01101NY](https://openairdocs.org/stc/ST01101NY): Installation of Sundstrand T-20G-10C3A auxiliary power unit for ground and water use only.. PATS Aircraft LLC
- [STC SQ00643NY](https://openairdocs.org/stc/SQ00643NY): Installation of spinners and balancing weights for dynamic propeller balancing.. Airworthiness Resources Corporation
- [STC SA2178WE](https://openairdocs.org/stc/SA2178WE): Installation of liquid spray system.. Aviation Specialties Inc

---
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