# TCDS A13NM: De Havilland Aircraft of Canada Limited

- Type: Type certificate data sheet
- Status: Current
- Holder: De Havilland Aircraft of Canada Limited
- Revision: 24
- Revised: October 19, 2026
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Registered aircraft: 95, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/b4/60/b460c540db154966d7311ecd26861748737b641a0db4660574e9a7dbebb18f50
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131623639720261019134058.0001
- Page: https://openairdocs.org/tcds/A13NM

## Models (16)

As the data sheet lists them.

- DHC-8-300 Series
- DHC-8-200 Series
- DHC-8-100 Series
- DHC-8-400 Series
- DHC-8-101
- DHC-8-102
- DHC-8-103
- DHC-8-106
- DHC-8-201
- DHC-8-202
- DHC-8-301
- DHC-8-311
- DHC-8-315
- DHC-8-400
- DHC-8-401
- DHC-8-402

## 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 8 9 10 11 12 13 14 
Rev. No. 24 15 18 18 13 22 15 13 18 19 23 21 20 23 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
                           A13NM 
             Revision 24 
 De Havilland Aircraft of 
Canada Limited 
 DHC-8-100 Series 
 DHC-8-200 Series 
 DHC-8-300 Series 
DHC-8-400 Series 
 
October 19, 2026  
  
TYPE CERTIFICATE DATA SHEET NO. A13NM 
 
This data sheet, which is a part of Type Certificate No. A13NM, 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 De Havilland Aircraft of Canada Limited 
 4100 Westwinds Drive NE 
 Calgary, Alberta 
 Canada T3J 4L2 
 
Type Certificate Holder Record         Bombardier Inc. 
 123 Garratt Boulevard 
 Downsview, Ontario 
 Canada M3K 1Y5 
 
1. DHC-8-100 Series      (see Note 5) 
 Model -101 - Approved Dec. 11, 1984, by the FAA and Sept . 28, 1984, by the Canadian Department of Transport 
 
 Model -102 - Approved Aug. 7, 1986, by the FAA and June . 12, 1986, by the Canadian Department of Transport 
 
 Model -103 - Approved Nov. 30, 1988, by the FAA and July . 20, 1987, by the Canadian Department of Transport 
 
 Model -106 - Approved Dec. 10, 1993, by the FAA and Nov.  20, 1992, by the Canadian Department of  Transport 
 
Data Pertinent to all Models Except as Indicated 
 
Engines 2-Pratt & Whitney Canada, Inc., PW120 or PW120A (-101) 
 2-Pratt & Whitney Canada, Inc., PW120A or PW121 (-102)  
 2-Pratt & Whitney Canada, Inc., PW121           (-103)  
 2-Pratt & Whitney Canada, Inc., PW121           (-106) 
 (See Data Pertinent to All Models Except as Indicated) 
 
Fuel ASTM D1655 Jet A, Jet A1, Jet B, MIL-DTL-5624 JP-4 & JP-5, and MIL-DTL-83133   JP-
8 conforming to Pratt and Whitney Canada, Inc. Specification No. CPW 204 
 
Oil Oils conforming to Pratt and Whitney Canada, Inc. 
 Specification No. PWA 521 Type II (MIL-L-23699). 
 
Engine Limits See AFM as listed under Approved Publications

A13NM Page 2 of 14 
Propeller and Propeller Limits 2-Hamilton Standard Model 14SF-7 
 Blade     SFA13( )-0A 
 Diameter  3.96M (13 Ft) 
 
 Pitch settings at 0.75 radius: 
   Feather 77.5 o 
   Flight fine 10.5 o 
   Ground fine -5.5 o 
   Full reverse -18.5 o 
 
 Propeller (Np) - Takeoff 1212 r.p.m.         
  Max Continuous 1212 r.p.m. 
 (See Data Pertinent to All Models Except as Indicated) 
 
 Knots m.p.h. 
Airspeed Limits V MO(Maximum operating)  0 to 14000 ft 242 279 
(IAS) 15000 ft 239 275 
 20000 ft 223 257 
 25000 ft 207 238 
 
 V FE (Flaps extended) Flaps  5 o 148 170 
 Flaps 15 o 148 170 
 Flaps 35 o 130 150 
 
 V A (Maneuvering) (-101, -102, -103) 163 188  
 V A (Maneuvering)(-106) 164 189  
 V LO (Landing gear operation) 158 182 
 V LE (Landing gear extended) 172 198 
 V B (Rough Air) 180 207 
 Landing Gear Doors Open Operative 140 161 
 Speed (Max. speed for operation 
 following an alternate landing gear 
 extension) 
 V MCA (Minimum control speed) Flaps 5 o 79 91 
 15 o 75 86 
 
Maximum Weight DHC-8-101 Take-off weight 14,970 kg (33,000 lb) 
(Mass) DHC-8-102 Take-off weight 15,649 kg (34,500 lb)  
 DHC-8-103 Take-off weight 15,649 kg (34,500 lb) 
                              15,966 kg (35,200 lb) 
                               (With MODSUM 8Q420649 incorporated)  
 DHC-8-106 Take-off weight 16,466 kg (36,300 lb) 
 
 (For other weights see AFM as listed under Approved Publications) 
 
CG Limits See AFM as listed under Approved Publications 
 
Maximum Baggage  454 kg (1000 lb) (See Weight and Balance Manual for mixed passenger cargo 
 configuration) 907 kg (2000 lb) with Mod 8/0063 or 8/0083

Page 3 of 14 A13NM 
 
2. DHC-8-200 Series   
   Model -201 - Approved January 4, 1996, by the FAA and A ugust_24, 1995, by the Canadian Department of Transport  
   Model -202 - Approved April 19, 1995, by the FAA and Marc h 9, 1995, by the Canadian Department of Transport  
  
Engines   2-Pratt & Whitney Canada, Inc., PW123C (201) 
  2-Pratt & Whitney Canada, Inc., PW123D (202) 
 (See Data Pertinent to All Models Except as Indicated) 
  
Fuel  ASTM D1655 Jet A, Jet A1, Jet B, MIL-DTL-5624 JP-4 & JP-5, and           
MIL-DTL-83133 JP-8 conforming to Pratt and Whitney Canada, Inc. 
Specification No. CPW 204 
  
Oil  Oils conforming to Pratt and Whitney Canada, Inc. Specification No. PWA 521  
 Type II (MIL-L-23699).  
  
Engine Limits  See AFM as listed under Approved Publications  
  
Propeller and Propeller Limits 2-Hamilton Standard Model 14SF-23  
  Blade     SFA13( )-0A 
  Diameter  3.96M (13 Ft) 
  Pitch settings at 0.75 radius: 
    Feather 77.5 o 
    Flight fine 10.5 o 
    Ground fine -5.5 o 
    Full reverse -18.5 o 
  Propeller (Np) - Takeoff 1212 r.p.m. 
    Max Continuous 1212 r.p.m. 
 (See Data Pertinent to All Models Except as Indicated) 
 
  Knots m.p.h.  
Airspeed Limits V MO(Maximum operating)      0 to 14000 ft 242  279 
(IAS) 15000 ft 239  275 
 20000 ft 223  257 
 25000 ft 207  238 
  
  V FE (Flaps extended) Flaps     5 o 148 170 
  Flaps 15 o 148 170 
  Flaps  35 o 130 150 
 
 V A (Maneuvering) 164  188  
 V LO (Landing gear operation) 158  182 
 V LE (Landing gear extended) 172  198 
 V B (Rough Air) 180  207 
 Landing Gear Doors Open Operative 140  161 
 Speed (Max. speed for operation  
 following an alternate landing gear extension)  
 V MCA (Minimum control speed) Flaps 5 o 80  91  
  15 o 74  86  
  
Maximum Weight (Mass) All Models, Take-off weight 16,466 kg (36,300 lb)  
   (For other weights see AFM as listed under Approved Publications)  
  
CG Limits   See AFM as listed under Approved Publications  
  
Maximum Baggage  907 kg (2000 lb) (See Weight and Balance Manual for mixed passenger cargo configuration)

A13NM Page 4 of 14 
3. DHC-8-300 Series  
 
 Model -301- Approved June 8, 1989, by the FAA and Feb. 14, 1989, by the Canadian Department of 
Transport 
 Model -311- Approved September 14, 1990, by the FAA and July 31, 1990, by the Canadian 
Department of Transport 
  Model -315- Approved June 28, 1995, by the FAA and June 2, 1995, by the Canadian Department of 
Transport  
 
Engines 2-Pratt & Whitney Canada, Inc., PW123  (-301 and -311) 
 2-Pratt & Whitney Canada, Inc., PW123E (-315)  
 (See Data Pertinent to All Models Except as Indicated) 
 
Fuel ASTM D1655 Jet A, Jet A1, Jet B, MIL-DTL-5624 JP-4 & JP-5, and           
MIL-DTL-83133 JP-8 conforming to Pratt and Whitney Canada, Inc. 
Specification No. CPW 204 
 
Oil  Oils conforming to Pratt and Whitney Canada, Inc. Specification No. PWA 521  
  Type II (MIL-L-23699). 
 
Engine Limits  See AFM as listed under Approved Publications 
 
Propeller and 2-Hamilton Standa rd Model 14SF-15 or 14SF-23 
Propeller Limits 
 Blade SFA13 ( )-0A 
 Diameter 3.96M (13 Ft) 
 
 Pitch settings at 0.75 radius: 
 Feather 77.5 o 
 Flight fine 11.5 o 
 Ground fine -7.5 o 
 Full reverse -18.5 o 
 
 Propeller (Np) - Takeoff 1212 r.p.m. 
  Max Continuous 1212 r.p.m. 
 (See Data Pertinent to All Models Except as Indicated) 
 
 Knots m.p.h. 
Airspeed Limits V MO (Maximum operating)       0 to 17000 ft 243 280 
(IAS) 20000 ft 232 267 
 25000 ft 214 246 
 
 DHC-8-301 
 V FE (Flaps extended) Flaps  5 o 160 184 
 Flaps 10 o 149 171 
 Flaps 15 o 149 171 
 Flaps 35 o 127 155  
 
 V A (Maneuvering) 176 203 
 V LO (Landing gear operation) 158 182 
 V LE (Landing gear extended) 173 199 
 V B (Rough Air) 188 216

Page 5 of 14 A13NM 
 
3. DHC-8-300 Series   (cont’d) 
 Knots m.p.h. 
 Landing Gear Doors Open Operative 140 161 
 Speed (Max. speed for operation 
 following an alternate landing gear extension) 
 V MCA (Minimum control speed) Flaps 5 o 83 96 
 Flaps 15 o 78 89  
 
 DHC-8-311 and 315 
 V FE (Flaps extended) Flaps  5 o 163 187 
 Flaps 10 o 154 177 
 Flaps 15 o 150 173 
 Flaps 35 o 138 159 
 V A (Maneuvering) 177 204 
 V LO (Landing gear operation) 163 187 
 V LE (Landing gear extended) 173 199 
 V B (Rough Air) 190 219 
 Landing Gear Doors Open Operative  140  161 
 Speed (Max. speed for operation 
 following an alternate landing gear 
 extension) 
 V MCA (Minimum control speed) Flaps 15 o 78 90 
 Flaps 10 o 80 92 
 Flaps 5 o 83 95 
 Flaps 0 o 94 109  
 
Maximum Weight DHC-8-301  Take-off weight 18,643 kg (41,100 lb)  
(Mass) DHC-8-311 and 315  Take-off weight 18,643 kg (41,100 lb)  
   18,997 kg (41,880 lb)  
   (with CR803SO00001 incorporated) 
   19,505 kg (43,000 lb)  
   (with CR803SO00002 incorporated) 
  (For other weights see AFM as listed under Approved Publications) 
 
CG Limits See AFM as listed under Approved Publications 
 
Maximum Baggage  1,130 kg (2500 lb) for standard baggage compartment (See Weight and Balance  
  Manual for other configurations) 
 
Cargo/Combi   All cargo, 20, 40 or 48 passenger configurations with a moveable passenger/ 
(DHC-8-311)   cargo bulkhead located at station 197.0, 354.0, 515.0 or 579.0 respectively

A13NM Page 6 of 14 
4. DHC-8-400 Series  
 
 Model 400 Approved January 24, 2000 by the FAA and July 30, 1999 by the Canadian Department 
of Transport 
 Model 401 Approved January 25, 2000 by the FAA and August 3, 1999 by the Canadian  
Department of Transport 
 Model 402 Approved January 26, 2000 by the FAA and August 4, 1999 by the Canadian  
Department of Transport 
 
 Engines  2 Pratt & Whitney Aircraft of Canada engines as follows: 
   DHC-8-400, 401 and 402, PW150A 
 
 Fuel  Kerosene Type: 
   ASTM D1655 JET A, ASTM D1655 JET A1 
   MIL-DTL-5624 JP-5, MIL-T-83133 JP-8 
 
   Wide Cut Type: 
   A S T M  D 1 6 5 5  J E T  B ,  MIL-DTL-5624 JP-4 
 
   conforming to Pratt & Whitney Canada, Inc. Specification No. CPW 204 
    
 
 Oil  Oils conforming to specification MI L-L-23699 (See AFM as listed in Approved  
Publications.) 
 
 Engine Limits  See AFM as listed in Approved Publications. 
 Propeller and  Dowty Aero space Model R408/6-123-F/17 
 Propeller Limits  
     
    Blade     4.11 M (13.5 ft.) nominal 
    Diameter 
 
    Pitch setting at 0.70 radius: 
    F e a t h e r      8 4 . 5 o 
    Flight fine (Electronic)   16.5  o 
    Flight fine (Hydraulic)   16.0  o 
    G r o u n d  f i n e     - 3 . 5  o 
 Full reverse -19.0 o  
 
    Propeller (NP) - Take-off   1020 rpm 
    M a x .  c o n t i n u o u s     1 0 2 0  r p m  
 
A i r s p e e d  L i m i t s          K n o t s   m . p . h  
(IAS)   V MO (Maximum Operating) 0 to 8,000 ft  245  282 
        1 0 , 0 0 0  f t  2 8 2   3 2 5  
        1 8 , 0 0 0  f t  2 8 6   3 2 9  
        2 0 , 0 0 0  f t  2 7 5   3 1 6  
        2 5 , 0 0 0  f t  2 4 8   2 8 5  
 
   V FE (Flaps extended)   Flap 5 o  200  230 
        F l a p  1 0  o  181  208 
        F l a p  1 5  o  172  198 
        F l a p  3 5  o  158  182

Page 7 of 14 A13NM 
 
 
 V A (Maneuvering) 204 235  
   V LO (Landing gear operation)    200  230 
   V LE (Landing gear extended)    215  247 
   V B (Rough Air)      210  242 
   Landing Gear Door Open Operative Speed   185  213 
   (Max. Speed for operation following an alternate 
   landing gear extension)  
VMCA (Minimum control speed)  Flap 15  o  91  105 
        F l a p  1 0  o  95  109 
        F l a p   5  o   98  113 
        F l a p  0  o   113  130 
 
 
    (Refer to AFM for airspeed limits)    
 
 
 Maximum Weight Take-off weight:   
    Models 400, 401 and 402   
    (With Modsum 4-201539 incorporated) 27,987 Kg (61,700 lb) 
    (With Modsum 4-308807 incorporated) 28,998 Kg (63,930 lb) 
    (With Modsum 4-308907 incorporated) 29,257 Kg (64,500 lb) 
    (With Modsum 4-309238 incorporated) 29,574 Kg (65,200 lb) 
 
 
C.G. Limits  See AFM as lis ted in Approved Publications. 
 
 Maximum Baggage For standard baggage compartments 
Aft baggage compartment: 1669 Kg (3680 lb)   
Fwd baggage compartment: 413 Kg  (910 lb)   
See Weight and Balance Manual for other configurations 
 
DATA PERTINENT TO ALL MODELS EXCEPT AS INDICATED: 
 
Series 100, 200 and 300: 
Propeller and Propeller Limits 
 
The following Hamilton Standard Propeller combinations are approved. 
  
Basic Aircraft 
Model 
101 
Models 
102, 103 & 106 
Models 
201 & 202 
Models 
301, 311, & 315 
14SF-7 & -7 14SF-7 & -7 14SF-23 & -23 14SF-15 & 15 
14SF-23 & -23 
 
Modification 8/2579 allows the following additional Hamilton Standard Propeller combinations. 
  
Models 102, 103, & 106 Models 20 1 & 202 Models 301, 311, & 315 
14SF-15 & 14SF-15 14SF-15 & 14SF-15 14SF-15 & 14SF-23 
14SF-15 & 14SF-7 14 SF-15 & 14SF-23  
14SF-15 & 14SF-23   
14SF-23 & 14SF-23   
14SF-23 & 14SF-7

A13NM Page 8 of 14 
 
Engines The following Pratt & Whitney Aircraft of Canada engine combinations are approved. 
Any combination of original engines and/or optional engines within each aircraft model 
is permitted. For series 200 and 300 aircraft, optional engines must incorporate 
modification 8/2735 
 
Approved Engine Combinations 
Aircraft Model Ori ginal Engine Optional En gine 
102 PW120A PW121 
201 PW123C PW123 
PW123B 
PW123D 
PW123E 
202 PW123D PW123 
PW123B 
PW123E 
301 and 311 PW123 PW123B 
PW123E 
 
The following P&WC Service Bulletin matrix lists the service bulletins which must be incorporated to change 
an optional engine to the rating of an original engine. The cancelling derate service bulletin is also shown. 
 
P&WC Service Bulletin Matrix 
Optional Engine Original Engine 
Rating 
P&WC S.B. 
Derate 
P&WC S.B. 
Cancel Derate 
PW123 PW123C 
PW123D 
21501 21502 
 
PW123B 
PW123 
PW123C 
PW123D 
 
21499 
 
21500 
PW123D PW123C 21503 21504 
 
PW123E 
PW123 
PW123C 
PW123D 
 
21497 
 
21498 
 
Reference Datum   
 
(Series 100, 200, 300)  Plate located  on centerline at Station 423.0 in. (1074.4 cm) on underside of  
  fuselage. 
(Series 400)   Plate located on centerline at “Station 428.0 in” (1087.1 cm) on underside of  
  fuselage. 
 
Leveling Means  Plum bob and target in RH emergency exit opening. 
 
Minimum Crew  2 (Pilot and Copilot) 
 
Maximum   Series 100 and 200 
Occupants  Not to exceed 44, including 2 p ilots, 1 attendants and 1 check pilot (40  
  passengers when fitted with an approved interior) 
 
   Series 300 
  Not to exceed 61, including 2 pilo ts, 2 attendants and 1 check pilot  
  (56 passengers when fitted with an approved interior)

Page 9 of 14 A13NM 
 
  Series 400 
 Model 400:  
Not to exceed 74, including 2 pilots, maximum 3 attendants, minimum 2   
attendants and 1 check pilot (68 passengers when fitted with an approved  
interior) 
Model 401: 
Not to exceed 76, including 2 pilots, maximum 3 attendants, minimum 2   
attendants and 1 check pilot (70 passengers when fitted with an approved  
interior) 
Model 402: 
Not to exceed 86, including 2 pilots, maximum 3 attendants, minimum 2   
attendants and 1 check pilot (80 passengers when fitted with an approved 
interior) 
 
Flight Load  Flaps Up +2.5g; -1.0g. 
Factors  Flaps extended +2.0g; 0.0g. 
 
Fuel Capacity    kg   lb US Gal Imp Gal 
(Series 100, 200, 300) Usable  2575 5678  835    695 
  Unusable      40     87    13      11 
  Total  2615 5765    848    706 
 
 (Series 400) Usable 5318 11724 1724 1436  
 Unusable 73 160 24 20  
 Total 5391 11884 1748 1456  
 
Oil Capacity   US Gal Imp Gal 
Per Engine 
  PW120/120A/121   Usable 1.0    0.83 
   Total  4.7    3.9 
 
   PW123/123B/123E   Usable 1.9    1.6 
   Total  5.5  4.57 
 
(Series 400) PW150A Usable 1.48 1.23 
  Total 6.58 5.48 
 
Maximum Operating Altitude Take-off and landing 10,000 feet 
 Enroute 25,000 feet 
 
Outside Air Temperature See AFM, as listed under Approved Publications 
  Limits 
 
Control Surface See Maintenance Manual: Series 100  PSM 1-8-2  
  Series 200  PSM 1-82-2  
 Series 300  PSM 1-83-2  
 Series 400  PSM 1-84-2 
 
Import Eligibility  A U.S Airworthiness certificate may be issued on the basis of the Canadian  
  Department of Transport "Certificate of Airworthiness for Export" signed by the 
Minister of Transport.  This form must contain the following statement: "This 
certifies that the aircraft described above has been manufactured in conformity 
with the data forming the basis for the DOT Aircraft Type Approval No. A-142 
as modified in accordance with the requirements for U.S. registered airplanes 
FAA Type Certificate No. A13NM defined in AEROC 8.1.AC.1."

A13NM Page 10 of 14 
Certification Basis  Series 100, 200 and 300:  
  FAR Part 25 dated February 1, 1965 including Amendments 25-1 through  
  25-51; FAR 25.832, Amendment 25-56; FAR 36 dated December 1, 1969  
 including Amendments 36-1 through 36-12; SFAR 27 dated December 12, 1973 
including Amendments 27-1  through 27-5.  
 
  Application for Type Certificate:  March 31, 1980 (Series 100) 
 
   Series 200 Additional Requirements: 
   FAR Part 25, Amendments 25-52 through 25-66; FAR 25.963(e), 
   Amendment 25-69; FAR 25.361, Amendment 25-72; FAR 25.729(e), 
   Amendment 25-75; FAR Part 34 date d September 10, 1990 (Replaces SFAR  
  27); FAR Part 36, Amendments 36-1 through 36-20   
  
   With the following exceptions (See Note 6) 
    FAR 25.365(e), Amendment 25-54; FAR 25.561, Amendment 25-64; 
  FAR 25.562, Amendment 25-64; FAR 25.783, Amendment 25-54; 
  FAR 25.785, Amendment 25-64; FAR 25.904, Amendment 25-62; 
   FAR 25.1091(e), Amendment 25-57 
  
    Series 300 Additional Requirements: 
     All Models; 
   FAR 25.812, Amendment 25-58 
 
   DHC-8-301; 
   FAR 25.853, Amendment 25-59 
  
   DHC-8-311 and 315; 
   FAR 25.853, Amendment 25-66 
  
   DHC-8-315; 
   FAR Part 34 dated September 10, 1 990 (Replaces SFAR 27); FAR Part 36,  
  Amendments 36-1 through 36-20  
 
   Series 100, 200 and 300 
 
  Items of Equivalent Safety 
 
   1. Pilot compartment view FAR 25.773(b)(2). 
 
  2. Ditching emergency exits FAR 25.807(d)(2) Amdt. 25-55. (DHC-8-311  
   and 315 with CR803SO 00001 or CR803SO00002  incorporated) 
 
  3. Cargo compartment classification FAR 25.857(b)&(d) Amdt. 25-60, for the 
20, 40 & 48 passenger configurations. DHC-8-311 Flight Manual Suppl. 42, 
Iss. 3, Cargo Loading Manual PSM 1-83-8A, Suppl. 1, Iss. 3 and Weight & 
Balance Manual PSM 1-83-8C are required. (S/N 230 & 242) 
 
  Special Conditions 
  1. Automatic take-off power control system (ATPCS) (ref. FAA Special  
   Conditions No. 25.-ANM-3). 
 
  2. Special Condition No. 25-394-SC, Passenger seats with non-traditional, 
large, non-metallic panels.

Page 11 of 14 A13NM 
 
  3. Special Condition No. 25-660-SC, Non-Rechargeable Lithium Batteries, 
effective to design changes applied for after May 1, 2017. See the 
applicability section of this special condition for more information on which 
design changes must meet it. 
 
  Exemptions 
  1. FAR 25.571(e)(2)  Propeller Debris (ref. FAA exemption No. NM-102) 
 
  2. FAR 25.807(c)(1)  40 passenger configuration Series 100 and 200 (ref.  
   FAA exemption No. 4723 dated October 24, 1986) 
 
  Compliance with the following additional optional requirements has been  
  established: 
 
  Ice Protection - FAR 25.1419 
 
   Compliance with FAR 25.801 has been established when the safety equipment  
   requirements of FAR 25.1411 and the ditching equipment requirements of FAR  
   25.1415 are satisfied. 
 
 
Part 26 – Continued Airworthiness and Safety Improvements for Transport Category Airplanes: 
   Based on § 21.101(g) for changes to TCs, applicable provisions 
   of Part 26 are included in th e certification basis. For any future 
   Part 26 amendments, the holder of  this TC must demonstrate compliance  
   with the applicable sections. 
 
  Compliance has been found for the following regulations 14 CFR § 26.11, 
26.43, 26.45 and 26.49. (Amdt.No.26-0, through 26-1) 
 
Certification Basis Series 400: 
 
Federal Aviation Regulations (FAR) Part 25, Airworthiness Standards: Transport 
Category Airplanes, dated 01 February 1965, Amendments 25-1 through 25-83 
Federal Aviation Regulations (FAR) Part 34, Fuel Venting and Exhaust Emission 
Requirements for Turbine Engine Powered Airplanes, effective 10 September, 1990, 
including Amendment 34-3 effective February 3, 1999. 
 
US Code of Federal Aviation Regulation (CFR) Title 14 part 36, effective 1 
December, 1969, including Amendment 36-1 through 36-21, Stage 3. 
 
US Code of Federal Aviation Regulation (CFR) Title 14 part 36, effective 1 
December, 1969, including Amendment 36-1 through 36-28, Stage 4, when De 
Havilland Aircraft of Canada Limited AFM Revision 185, dated 24 September 2007 
is installed. 
 
US Code of Federal Aviation Regulation (CFR) Title 14 part 36, effective 1 
December, 1969, including Amendment 36-1 through 36-31, Stage 5, when De 
Havilland Aircraft of Canada Limited AFM Revision 401.1, dated 17 June 2021 is 
installed.    
 
 Additional Requirements: 
 
Federal Aviation Regulations (FAR) Part 25, Airworthiness Standards: Transport 
Category Airplanes, dated 01 February 1965, Amendments 25-84 through 25-86, and 
25-92.

A13NM Page 12 of 14 
 
 
 Items of Equivalent Safety: 
1. FAA Issue Paper F-1. “Use of 1-g Stall Speed Criteria Instead of Minimum 
Speed in the Stall” 
 
2. Equivalent Level of Safety has been made for the following regulation: 
14 CFR § 25.815, Width of Aisle, documented in ELOS Memo # AT7055NY-
T-CS-1. (See Note 8) 
 
 Special Conditions: 
1. Special Condition No. 25-ANM-121, High Intensity Radiated Fields (HIRF) 
 
2. Special Condition No. 25-154-SC, Automatic take-off power control system 
(ATPCS) 
 
3. Special Condition No. 25-394-SC, Passenger seats with non-traditional, large, 
non-metallic panels. 
 
4. Special Condition No. 25-660-SC, Non-Rechargeable Lithium Batteries, 
effective to design changes applied for after May 1, 2017. See the applicability 
section of this special condition for more information on which design changes 
must meet it. 
 
 Exemptions: 
1. Exemption No. 6790 to FAR 25.571(e)(1) “Damage Tolerance (Discrete 
Source) Evaluation at Amendment 25-72” 
 
2. Exemption No. 6833 to FAR 36 Appendix C, Section C36.3c. “Definition of 
noise Sideline Point [compliance will be shown with ICAO Annex 16, Vol. 1, 
Iss. 3, Amendment 5, Chapter 3, Section 3.3.1(a)(2)] 
 
3. Exemption No. 6864 to FAR 25.1435(b)(1) “Hydraulic System – Test and 
Analysis, at Amendment 25-72” 
 
Part 26 – Continued Airworthiness and Safety Improvements for Transport Category Airplanes: 
   Based on § 21.101(g) for changes to TCs, applicable provisions 
   of Part 26 are included in th e certification basis. For any future 
   Part 26 amendments, the holder of  this TC must demonstrate compliance  
   with the applicable sections. 
 
  Compliance has been found for the following regulations 14 CFR § 26.11, 
26.43, 26.45 and 26.49. (Amdt.No.26-0, through 26-1) 
 
Optional Requirements: 
 1. Ice Protection: FAR 25.1419 
 
2. Ditching: Compliance with FAR 25.801 has been established when the safety 
requirements of FAR 25.1411 and the ditching equipment requirements of FAR 
25.1415 are satisfied 
 
Serial Numbers Eligible  Series 100 
  Serial number 2 and subsequent 
   Series 200 
   Serial number 391 and subsequent 
  Series 300 
  Serial number 100 and subsequent

Page 13 of 14 A13NM 
 
  Series 400 
  Serial 4001 and subsequent 
 
Equipment  The basic required equipment as prescribed in the applicable airworthiness  
  requirements (See Certif ication Basis) must be installed in the aircraft. 
 
Approved Publications Flight Manual 
  Series 100: PSM 1-81-1A (Models 101, 102, 103 and 106) 
  Series 200: PSM 1-82-1A (Model 201, 202)  
  Series 300: PSM 1-83-1A (Models 301, 311 and 315)  
  Series 400: PSM 1-84-1A (Models 400, 401 and 402) 
  
   Airworthiness Limitations (Part 2) an d MRB Report (Sections 2 and 3) of the  
  Maintenance Program  
   Series 100: PSM 1-8-7 
   Series 200: PSM 1-82-7 
   Series 300: PSM 1-83-7 
 Maintenance Requirements Manual, MRM (Section 1, MRB report and Section 
2, Airworthiness Limitation Items 
  Series 400: PSM 1-84-7 
 
  Definition Report AEROC 8.1.AC.1 
 
Service Information  Service Bulletins, structural re pair manuals, and aircraft flight manuals which  
  contain a statement that the docume nt is Transport Canada approved or  
  Transport Canada approved through the Manufacturers Design Approval  
  Representative are accepted by the FA A and are considered FAA approved.  
  These approvals pertain to the type design only. 
 
Life Limited Parts  Components wh ich are life limited are listed in the "Airworthiness Limitations"  
  section of the Maintenance  Program.   (See Note 3).  
 
Note 1. A current weight and balance report including list of equipment included in certificated empty 
weight, and loading instructions must be in each aircraft at the time of original certification and 
at all times there after except in the case of operators having an approved weight control system.  
The aircraft total system fuel must be included in the empty weight.  System fuel is the amount of 
fuel required to fill the system plumbing and tanks to the undrainable level plus unusable fuel in 
the tanks established under FAR 25.959. 
 The aircraft must be loaded so that the C.G. is within specified limits at all times, considering fuel 
loading and usage, gear retraction, and movement of crew and passengers from their assigned 
positions. 
 
Note 2. The aircraft must be operated in accordance with the FAA Approved Airplane Flight Manual. 
 
Note 3. Compliance with the frequencies for "Threshold" and "Repeat" inspection specified in the 
"Airworthiness Limitations", Volume 1, Part 2 of the Maintenance Program (PSM 1-8-7, PSM  1-
82-7 and PSM 1-83-7) and MRB report Volume 1, Part 1 of the  same document, are required to 
ensure continuing compliance  with the type certification basis. For Series 400, the “Threshold” 
and “Repeat” inspections are specified in Part 2 of the MRM (Airworthiness Limitations) and 
Part 1 of the MRM (MRB report). 
 
Note 4. For mixed passenger/cargo configurations see weight and balance manual.

A13NM Page 14 of 14 
Note 5. Modifications required to convert a Model DHC-8-101 to a 102, a 102 to a 103, a 102/103 to a 
106, and a 311 to a 315 are identified in Bombardier Definition Report AEROC 8.1.AC.1 listed in 
Approved Publications. 
 
Note 6. The DHC-8 Series 200 was certificated as a derivative of the  Series 100 aircraft.  The applicable 
basis of certification is the same as the Series 100, but the manufacturer elected to demonstrate 
compliance with FAR Part 25, up to Amendment 25-66, less the exceptions shown under the Series 
200 Certification Basis.  
 
Note 7. Deleted.   
 
Note 8. The Equivalent Safety Finding is applicable to DHC-8 Series 400 incorporating a post 
certification design change that introduces a business class section (dual class configuration), 
whereby the left side overhead bin intrudes into the passenger aisle of the aircraft. 
 
 
-- END --
```

## ADs (353, first 50, in force first)

- [AD 2026-11-06](https://openairdocs.org/ad/2026-11-06): Hardware; Standard practices/structures · De Havilland Aircraft of Canada DHC-8-101, DHC-8-102, DHC-8-103 and 9 more. Effective Jul 9, 2026
- [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 2026-08-07](https://openairdocs.org/ad/2026-08-07): Stabilizers · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jun 3, 2026
- [AD 2025-19-05](https://openairdocs.org/ad/2025-19-05): Flight controls · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Oct 31, 2025
- [AD 2025-05-06](https://openairdocs.org/ad/2025-05-06): Nacelles/pylons · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Apr 16, 2025
- [AD 2024-22-07](https://openairdocs.org/ad/2024-22-07): Landing Gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Dec 31, 2024
- [AD 2024-12-05](https://openairdocs.org/ad/2024-12-05): Landing Gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Aug 21, 2024
- [AD 2024-12-06](https://openairdocs.org/ad/2024-12-06): Fuselage · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Aug 21, 2024
- [AD 2024-08-04](https://openairdocs.org/ad/2024-08-04): Time Limits/Maintenance Checks · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jun 20, 2024
- [AD 2024-02-02](https://openairdocs.org/ad/2024-02-02): Stabilizers · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Mar 21, 2024
- [AD 2023-16-05](https://openairdocs.org/ad/2023-16-05): Landing Gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Sep 25, 2023
- [AD 2023-07-06](https://openairdocs.org/ad/2023-07-06): Stabilizers · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jun 20, 2023
- [AD 2023-06-03](https://openairdocs.org/ad/2023-06-03): Landing Gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective May 18, 2023
- [AD 2023-05-01](https://openairdocs.org/ad/2023-05-01): Flight Controls · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Apr 18, 2023
- [AD 2023-01-09](https://openairdocs.org/ad/2023-01-09): Fuel System · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Mar 13, 2023
- [AD 2022-25-06](https://openairdocs.org/ad/2022-25-06): Air Conditioning System · De Havilland Aircraft of Canada DHC-8-402. Effective Jan 23, 2023
- [AD 2022-23-01](https://openairdocs.org/ad/2022-23-01): Fuel · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Dec 13, 2022
- [AD 2022-17-04](https://openairdocs.org/ad/2022-17-04): Fuel System, Time Limits/Maintenance Checks · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Nov 1, 2022
- [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022
- [AD 2022-13-08](https://openairdocs.org/ad/2022-13-08): Landing gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Aug 10, 2022
- [AD 2022-11-11](https://openairdocs.org/ad/2022-11-11): Landing gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jul 8, 2022
- [AD 2022-11-14](https://openairdocs.org/ad/2022-11-14): Landing gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jun 21, 2022
- [AD 2022-06-15](https://openairdocs.org/ad/2022-06-15): Pneumatic · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective May 10, 2022
- [AD 2022-03-02](https://openairdocs.org/ad/2022-03-02): Wings · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Mar 17, 2022
- [AD 2021-23-02](https://openairdocs.org/ad/2021-23-02): Fire protection · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jan 5, 2022
- [AD 2021-23-03](https://openairdocs.org/ad/2021-23-03): Landing Gear · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Dec 6, 2021
- [AD 2021-19-11](https://openairdocs.org/ad/2021-19-11): Flight controls · De Havilland Aircraft of Canada DHC-8-102, DHC-8-103, DHC-8-106 and 8 more. Effective Nov 18, 2021
- [AD 2021-12-02](https://openairdocs.org/ad/2021-12-02): Nacelles/pylons · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Jul 20, 2021
- [AD 2021-11-04](https://openairdocs.org/ad/2021-11-04): Landing Gear · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Jul 9, 2021
- [AD 2021-10-13](https://openairdocs.org/ad/2021-10-13): Landing gear · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Jul 1, 2021
- [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020
- [AD 2020-21-03](https://openairdocs.org/ad/2020-21-03): Doors · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Nov 18, 2020
- [AD 2020-11-13](https://openairdocs.org/ad/2020-11-13): Nacelles/pylons · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Jul 14, 2020
- [AD 2020-09-12](https://openairdocs.org/ad/2020-09-12): Stabilizers · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Jun 24, 2020
- [AD 2020-02-10](https://openairdocs.org/ad/2020-02-10): Fire protection · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Mar 12, 2020
- [AD 2019-24-12](https://openairdocs.org/ad/2019-24-12): Fuselage · De Havilland Aircraft of Canada DHC-8-401 and DHC-8-402. Effective Feb 3, 2020
- [AD 2019-22-11](https://openairdocs.org/ad/2019-22-11): Main landing gear · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Jan 9, 2020
- [AD 2019-20-09](https://openairdocs.org/ad/2019-20-09): Wings · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Nov 27, 2019
- [AD 2019-18-05](https://openairdocs.org/ad/2019-18-05): Landing gear · De Havilland Aircraft of Canada DHC-8-400, DHC-8-401 and DHC-8-402. Effective Oct 31, 2019
- [AD 2019-15-09](https://openairdocs.org/ad/2019-15-09): Wings · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Sep 19, 2019
- [AD 2019-12-17](https://openairdocs.org/ad/2019-12-17): Stabilizers · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Aug 12, 2019
- [AD 2018-23-04](https://openairdocs.org/ad/2018-23-04): Engine Controls · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Mar 15, 2019
- [AD 2018-22-03](https://openairdocs.org/ad/2018-22-03): Stabilizers · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Nov 28, 2018
- [AD 2018-20-11](https://openairdocs.org/ad/2018-20-11): Doors · Bombardier DHC-8-301, DHC-8-311 and DHC-8-315. Effective Nov 23, 2018
- [AD 2018-20-12](https://openairdocs.org/ad/2018-20-12): Ice and rain protection · Bombardier DHC-8-102, DHC-8-103, DHC-8-106 and 5 more. Effective Nov 23, 2018
- [AD 2018-20-18](https://openairdocs.org/ad/2018-20-18): Flight Controls · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Nov 20, 2018
- [AD 2018-17-17](https://openairdocs.org/ad/2018-17-17): Ice and Rain Protection · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Oct 2, 2018
- [AD 2018-17-09](https://openairdocs.org/ad/2018-17-09): Landing gear · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Sep 25, 2018
- [AD 2018-02-16](https://openairdocs.org/ad/2018-02-16): Doors · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Mar 5, 2018
- [AD 2017-23-01](https://openairdocs.org/ad/2017-23-01): Landing gear · Bombardier DHC-8-400, DHC-8-401 and DHC-8-402. Effective Dec 19, 2017

All 353: https://openairdocs.org/tcds/A13NM/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Bombardier DHC-8-402](https://openairdocs.org/model/bombardier-dhc-8-402): 26 aircraft (registry code 1390042)
- [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202): 17 aircraft (registry code 2809007)
- [Bombardier DHC-8-315](https://openairdocs.org/model/bombardier-dhc-8-315): 15 aircraft (registry code 1390043)
- [Bombardier DHC-8-202](https://openairdocs.org/model/bombardier-dhc-8-202): 14 aircraft (registry code 1390007)
- [Dehavilland DHC-8-106](https://openairdocs.org/model/dehavilland-dhc-8-106): 4 aircraft (registry code 2809020)
- [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102): 3 aircraft (registry code 1386002)
- [Boeing Of Canada/Dehav Div DHC-8-311](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-311): 3 aircraft (registry code 1386006)
- [Boeing Of Canada/Dehav Div DHC-8-106](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-106): 2 aircraft (registry code 1386020)
- [Bombardier DHC-8-201](https://openairdocs.org/model/bombardier-dhc-8-201): 2 aircraft (registry code 1390004)
- [Dehavilland DHC-8-103](https://openairdocs.org/model/dehavilland-dhc-8-103): 2 aircraft (registry code 2809006)
- [Dehavilland DHC-8-201](https://openairdocs.org/model/dehavilland-dhc-8-201): 2 aircraft (registry code 2809001)
- [Dehavilland DHC-8-315](https://openairdocs.org/model/dehavilland-dhc-8-315): 2 aircraft (registry code 2809010)
- [Boeing Of Canada/Dehav Div DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-102): 1 aircraft (registry code 1385303)
- [Bombardier DHC-8-300](https://openairdocs.org/model/bombardier-dhc-8-300): 1 aircraft (registry code 1390011)
- [Dehavilland DHC-8-102](https://openairdocs.org/model/dehavilland-dhc-8-102): 1 aircraft (registry code 2809003)
- [Boeing / Dehavilland DHC-8-103](https://openairdocs.org/model/boeing-dehavilland-dhc-8-103): 0 aircraft (registry code 1386005)
- [Boeing DHC-8-301](https://openairdocs.org/model/boeing-dhc-8-301): 0 aircraft (registry code 1386003)
- [Boeing Of Canada DHC-8-102](https://openairdocs.org/model/boeing-of-canada-dhc-8-102): 0 aircraft (registry code 1385305)
- [Boeing Of Canada/Dehav Div DHC-8-315](https://openairdocs.org/model/boeing-of-canada-dehav-div-dhc-8-315): 0 aircraft (registry code 1386107)
- [Boeing/Canada DHC-8-301](https://openairdocs.org/model/boeing-canada-dhc-8-301): 0 aircraft (registry code 1386007)
- [Bombardier DHC-8-100 SER](https://openairdocs.org/model/bombardier-dhc-8-100-ser): 0 aircraft (registry code 1390000)
- [Bombardier DHC-8-101](https://openairdocs.org/model/bombardier-dhc-8-101): 0 aircraft (registry code 1390001)
- [Bombardier DHC-8-102](https://openairdocs.org/model/bombardier-dhc-8-102): 0 aircraft (registry code 1390002)
- [Bombardier DHC-8-103](https://openairdocs.org/model/bombardier-dhc-8-103): 0 aircraft (registry code 1390003)
- [Bombardier DHC-8-106](https://openairdocs.org/model/bombardier-dhc-8-106): 0 aircraft (registry code 1390012)
- [Bombardier DHC-8-311](https://openairdocs.org/model/bombardier-dhc-8-311): 0 aircraft (registry code 1390010)
- [Bombardier DHC-8-401](https://openairdocs.org/model/bombardier-dhc-8-401): 0 aircraft (registry code 1390041)
- [Dehavilland Acft Of Canada DHC-8-402](https://openairdocs.org/model/dehavilland-acft-of-canada-dhc-8-402): 0 aircraft (registry code 2805090)
- [Dehavilland DHC 8 200](https://openairdocs.org/model/dehavilland-dhc-8-200): 0 aircraft (registry code 2809004)
- [Dehavilland DHC-8-100 SERIES](https://openairdocs.org/model/dehavilland-dhc-8-100-series): 0 aircraft (registry code 2802602)
- [Dehavilland DHC-8-101](https://openairdocs.org/model/dehavilland-dhc-8-101): 0 aircraft (registry code 2809002)
- [Dehavilland DHC-8-300 SERIES](https://openairdocs.org/model/dehavilland-dhc-8-300-series): 0 aircraft (registry code 2809008)
- [Dehavilland DHC-8-301](https://openairdocs.org/model/dehavilland-dhc-8-301): 0 aircraft (registry code 2809011)
- [Dehavilland DHC-8-311](https://openairdocs.org/model/dehavilland-dhc-8-311): 0 aircraft (registry code 2809005)
- [Dehavilland DHC-8-400](https://openairdocs.org/model/dehavilland-dhc-8-400): 0 aircraft (registry code 2802413)
- [Dehavilland DHC-8-401](https://openairdocs.org/model/dehavilland-dhc-8-401): 0 aircraft (registry code 2809041)
- [Dehavilland DHC-8-402](https://openairdocs.org/model/dehavilland-dhc-8-402): 0 aircraft (registry code 2800942)

## STCs approved under this data sheet (355, first 50)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.. Rockwell Collins Inc
- [STC ST12511IB](https://openairdocs.org/stc/ST12511IB): Installation of the Emergency Locator Transmitter (ELT) 4000/4000M Upgrade. Avmax Aviation Services Inc.
- [STC ST00153IB](https://openairdocs.org/stc/ST00153IB): Installation of Static Line Provisions. Voyageur Aviation Corp.
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc.
- [STC ST01902AT-D](https://openairdocs.org/stc/ST01902AT-D): Installation of expanded flight data parameters for Teledyne DF DAU.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST01929AT-D](https://openairdocs.org/stc/ST01929AT-D): Installation of flight data recorder expanded parameters with a Plessey FDAU.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02240AT-D](https://openairdocs.org/stc/ST02240AT-D): Bombardier DHC-8 BAE Systems (Plessey) Digital Flight Data Acquisition Unit Upgrade.. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON LLC d/b/a MASS Systems
- [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 ST04762NY](https://openairdocs.org/stc/ST04762NY): Installation of Cobham Remote Control Audio Unit (RCAU). LB Aircraft Engineering
- [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 ST12331IB](https://openairdocs.org/stc/ST12331IB): Installation and maintenance of the Slip Ring De-Icer Harness. Avmax Aviation Services Inc.
- [STC ST03220CH](https://openairdocs.org/stc/ST03220CH): Installation of an advertisement container on the bottom of a seat back tray table. Atin OOH LLC
- [STC ST03308CH](https://openairdocs.org/stc/ST03308CH): Installation of Printed Advertising onto cabin interior surfaces. Atin OOH LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC ST12076CH](https://openairdocs.org/stc/ST12076CH): Installation of FMS Software Upgrade and Solid State Data Transfer Unit Plus (SSDTU+). Canard Aerospace Corporation
- [STC ST01460LA](https://openairdocs.org/stc/ST01460LA): Installation of a reinforced cockpit door.. Safran Cabin Inc.
- [STC ST04559CH](https://openairdocs.org/stc/ST04559CH): Installation of L3Harris Aviation Products SRVIVR25 Model 7100 Cockpit Voice Recorder (CVR) System. Acron Aviation Inc.
- [STC ST04560CH](https://openairdocs.org/stc/ST04560CH): INSTALL L3HARRIS AVIATION PRODUCTS SRVIVR25 MODEL 7100 COCKPIT VOICE RECORDER SYSTEM. Acron Aviation Inc.
- [STC ST12032IB](https://openairdocs.org/stc/ST12032IB): Installation of the Center Console Extension. Avmax Aviation Services Inc.
- [STC ST02783SE](https://openairdocs.org/stc/ST02783SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST03472NY](https://openairdocs.org/stc/ST03472NY): Installation of the Cabin LED Lighting. Avmax Aviation Services Inc
- [STC ST11980IB](https://openairdocs.org/stc/ST11980IB): Installation of the Cockpit USB Charger. Avmax Aviation Services Inc.
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc.
- [STC ST01255SE](https://openairdocs.org/stc/ST01255SE): Installation of a center console extended fairing. Metal Innovations Inc. dba MII Aero
- [STC ST03224NY](https://openairdocs.org/stc/ST03224NY): Replacement of existing flight data recording systems with new Mini Flight Data Acquisition Unit (MFDAU) and Flight Data Recorder, sensors and wiring capable of recording 57 parameters. KGB Aviation Solutions LLC
- [STC ST00193IB](https://openairdocs.org/stc/ST00193IB): Installation of the Universal Avionics Kapture CVR. Avmax Aviation Services Inc.
- [STC ST00658DE](https://openairdocs.org/stc/ST00658DE): Installation of Electronic Flight Bag (EFB) provisions and XM Weather Receiver.. Amphenol Cable and Interconnect Technologies Inc.
- [STC ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc.
- [STC ST02050NY](https://openairdocs.org/stc/ST02050NY): Installation of U.S. Customs Special Mission Modifications. Field Aviation East Limited
- [STC ST03795NY](https://openairdocs.org/stc/ST03795NY): Installation of the TB44 Lithium-Ion Battery System. Avmax Aviation Services Inc.
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01909NY](https://openairdocs.org/stc/ST01909NY): Installation of Hawker 9750W0370-6 (24V 43Ah) sealed lead-acid batteries.. Securaplane Technologies Inc
- [STC ST02028WI](https://openairdocs.org/stc/ST02028WI): Installation of Bighorn CASEVAC Interior System. Bighorn Airways Inc.
- [STC ST00226IB](https://openairdocs.org/stc/ST00226IB): Installation of the Battery Access Kit. Avmax Aviation Services Inc.
- [STC ST03065NY](https://openairdocs.org/stc/ST03065NY): The installation of Dual Universal UNS-1F Flight Management System WAAS Up-grade. Field Aviation East Limited
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00388BO](https://openairdocs.org/stc/ST00388BO): Installation of a Night Vision Imaging System (NVIS). ATI Engineering Services LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST00188IB](https://openairdocs.org/stc/ST00188IB): Installation of the Collins TCAS 4000. Mid Canada Mod Center
- [STC ST01969WI](https://openairdocs.org/stc/ST01969WI): Operation of Air Operable Baggage Door at 25,000 ft.. Bighorn Airways Inc.
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc.
- [STC ST02311AT](https://openairdocs.org/stc/ST02311AT): Installation of Saf-T-Glo Inc photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc.
- [STC ST00213MC](https://openairdocs.org/stc/ST00213MC): Installation of means to disable ADS-B Out. Sierra Nevada Corporation
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00109IB](https://openairdocs.org/stc/ST00109IB): Installation of the Flight Compartment Stowage Box. Infinion Certification Engineering Inc.
- [STC ST04809NY](https://openairdocs.org/stc/ST04809NY): Conversion of a DHC-8-402 aircraft into a Airtanker for the aerial dispensing of liquids with the addition
of an external retardant tank system operated under the restricted category. Conair Group Inc.

All 355: https://openairdocs.org/tcds/A13NM/stcs.md

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