No. |
Date
MM/DD/YY |
Title |
Manufacturer/Model |
RDIMS # |
86-01 |
4/2/1986 |
Operation Above 41,000 ft Altitude up to and Including 51,000 ft |
Gulfstream G-1159C (G-IV) |
157409 |
86-02 |
8/19/1986 |
Conditional Use of Rated Take-Off Thrust up to 10 Minutes for One-Engine Inoperative Take-Off Climb Operations |
Boeing 747-133 and 747-233B |
137815 |
87-01 |
3/20/1987 |
Steep Approach and Short Landing Capability |
Shorts SD-330 |
153992 |
87-03 |
8/14/1987 |
Lightning Protection |
Airbus Industrie A310-300 |
153887 |
87-04 |
9/17/1987 |
Aircraft Conversion for the Fire Fighting Role |
CP-121 and CS2F (TRACKER) |
153876 |
88-01 |
2/26/1988 |
Pusher-Propeller Powerplant Installation |
Viking Air Trigull 330 |
154027 |
88-02 |
3/7/1988 |
Automatic Take-Off Power Control System (ATPCS) |
ATR 42 |
157539 |
88-03 |
6/10/1988 |
Operation Above 41,000 ft Altitude up to and Including 45,000 ft |
Boeing B757-200 |
157410 |
88-04 |
7/18/1988 |
Automatic Power Reserve System |
British Aerospace Jetstream 3200, Model 3212 |
157506 |
88-05 |
7/18/1988 |
Alcohol-Water Injection System |
British Aerospace Jetstream 3200, Model 3212 |
154189 |
88-06 |
7/21/1988 |
Lightning Protection - Indirect Effects |
Fokker F28-MK0100 |
138209 |
89-01 |
1/6/1989 |
Equipment Standards for Crew Oxygen Dispensing Units |
Piper PA-42-1000 |
154256 |
89-07 |
6/28/1989 |
Flight Characteristics and Performance |
Airbus Industrie A320 |
154318 |
89-08 |
11/14/1989 |
Improved Flammability Standards for Materials Used in the Cabin Interior |
Transport Category Aeroplanes (SCA used for A320 and B747-400) |
138279 |
90-04 |
6/20/1990 |
Evaluation of Bonded Structural Joints |
Piaggio P180 Avanti |
138299 |
90-06 |
8/3/1990 |
Aircraft Operation After Ground Cold Soak |
Piaggio P180 Avanti |
138305 |
90-07 |
8/27/1990 |
Evaluation of Composite Structure |
Slingsby T-67 |
138324 |
90-08 |
11/27/1990 |
Operation Above 41,000 ft Altitude up to and Including 45,000 ft |
Boeing B747-400 |
157453 |
90-09 |
11/27/1990 |
Flight Attendant View of Passenger Compartment |
Boeing B747-400 |
138345 |
91-03 |
3/22/1991 |
Main Deck Cargo Compartment Fire Protection |
Boeing B747-400 |
138382 |
91-04 |
5/15/1991 |
Operation Above 41,000 ft Altitude up to and Including 51,000 ft |
Learjet 31/31A |
157464 |
91-07 |
10/29/1991 |
Improved Flammability Standards for Materials Used in the Cabin Interior |
Avions de Transport Régional ATR 72 |
138508 |
91-08 |
12/10/1991 |
High Intensity Radiated Fields (HIRF) |
Canadair Regional Jet (RJ) |
138539 |
92-01 |
5/11/1992 |
Lightning Protection |
Canadair Regional Jet (RJ) |
138648 |
92-02 |
10/5/1992 |
Retractable Wheel Ski Installation |
De Havilland of Canada DHC-7 |
138715 |
92-05 |
11/1/1992 |
Retractable Wheel-Ski Installation - Load Requirements |
De Havilland of Canada DHC-7 |
138860 |
93-02 |
1/4/1993 |
High Intensity Radiated Fields (HIRF) |
Bell 430 |
138918 |
93-03 |
1/4/1993 |
Lightning Protection |
Bell 430 |
139056 |
93-04 |
4/5/1993 |
High Intensity Radiated Fields (HIRF) |
Canadair CL-415 |
139122 |
93-05 |
4/6/1993 |
Lightning Protection |
Canadair CL-415 |
139182 |
93-06 |
3/1/1993 |
Remote Switch |
Northern Airborne Technology Ltd. RS08-001 and RS08-350 |
140048 |
93-06
Rev. A |
8/22/2000 |
Remote Switch |
Northern Airborne Technology Ltd. RS08-001, RS08-350 and RS08-500 |
140227 |
93-09 |
8/27/1993 |
Folding Wings |
HOAC/DIMONA DV20 KATANA |
140271 |
93-10 |
9/1/1993 |
Airborne Satellite Communication Antenna Subsystem |
Canadian Marconi Company 2102 |
140287 |
93-10
Rev. A |
7/26/1999 |
Airborne Satellite Communication Antenna Subsystem |
Canadian Marconi Company 2102 |
140305 |
93-11 |
9/2/1993 |
L-Band Diplexer/Low Noise Amplifier |
Com Dev Atlantic |
140569 |
93-12 |
10/12/1993 |
High Altitude Operation Up to 51,000 feet |
Learjet 60 |
140629 |
94-01 |
1/11/1994 |
Flight Dynamics Headup Guidance System (HGS 2100) |
Canadair Regional Jet (CL-600-2B19) |
141170 |
94-02 |
1/11/1994 |
High Intensity Radiated Fields (HIRF) |
Canadair CL-600-2B19, CL-604 Variant |
141450 |
94-03 |
1/12/1994 |
Lightning Protection |
Canadair CL-600-2B19, CL-604 Variant |
141832 |
94-04 |
2/8/1994 |
Aircraft Operation After Ground Cold Soak |
Cessna 525 |
141844 |
94-05 |
2/8/1994 |
Crew Oxygen Dispensing Units |
Cessna 525 |
155728 |
94-06 |
3/7/1994 |
Evaluation of Composite Structure |
Extra-Flugzeugbau GmbH EA300 and EA300/S |
141975 |
94-07 |
3/7/1994 |
Structural Design and Loads Criteria |
Extra-Flugzeugbau GmbH EA300 and EA300/S |
142014 |
94-08 |
3/18/1994 |
Software Aspects of Certification |
Bell 430 |
142031 |
94-09 |
6/27/1994 |
Aircraft Conversion for the Aerial Fire Supression Role |
Lockheed L-188 (Electra) |
142045 |
94-10 |
11/28/1994 |
High Altitude Operation Up to 51,000 Feet |
Bombardier Canadair BD-700-1A10 (Global Express) |
142759 |
94-11 |
11/28/1994 |
High Intensity Radiated Fields (HIRF) |
Bombardier Canadair BD-700-1A10 (Global Express) |
143234 |
94-11
Rev. A |
2/28/1996 |
High Intensity Radiated Fields (HIRF) |
Bombardier Canadair BD-700-1A10 (Global Express) |
143240 |
94-12 |
12/28/1994 |
Operation on Narrow Runways |
De Havilland DHC-8 100/200/300 |
143341 |
94-13 |
11/28/1994 |
Software Aspects in Certification |
Bombardier Canadair BD-700-1A10 (Global Express) |
143555 |
95-01 |
4/25/1995 |
Aircraft Conversion for the Aerial Fire Supression Role |
Douglas DC-4 |
143582 |
95-02 |
4/26/1995 |
High Intensity Radiated Fields (HIRF) |
Bell 407 |
143655 |
95-03 |
4/26/1995 |
Lightning Protection |
Bell 407 |
143772 |
95-04 |
11/27/1995 |
Contaminant/Fluid Integrity Measuring System (Advisory System) |
Allied Signal |
152873 |
96-06 |
11/10/1995 |
High Altitude Operations (45,000 Feet) |
IAI Model 1125 Astra SPX Business Jet |
1750546 |
95-07 |
5/19/1999 |
High Intensity Radiated Fields (HIRF) |
De Havilland DHC-8-400 |
143832 |
95-08 |
12/19/1995 |
High Intensity Radiated Fields (HIRF) |
Pilatus PC-12 |
143874 |
95-10 |
12/19/1995 |
Aircraft Operation After Ground Cold Soak |
Pilatus PC-12 |
143894 |
96-03 |
4/24/1996 |
Emergency Avionics System |
SPAR EAS-3000 |
143999 |
96-03
Rev. 1 |
9/11/1997 |
Emergency Avionics System |
SPAR EAS-3000 |
144118 |
96-03
Rev. 2 |
12/1/1997 |
Emergency Avionics System |
DRS EAS-3000 |
144151 |
96-05 |
12/18/1996 |
Bird Ingestion |
Pratt & Whitney Canada PW150 |
144203 |
96-06 |
12/18/1996 |
Rain and Hail Ingestion |
Pratt & Whitney Canada PW150 |
155542 |
96-07 |
2/26/1996 |
Engine-Propeller Feather Test |
Pratt & Whitney Canada PW150 |
144530 |
96-08 |
12/4/1996 |
Rotor Integrity |
Pratt & Whitney Canada PW545A |
144583 |
96-09 |
12/4/1996 |
Engine Vibration |
Pratt & Whitney Canada PW545A |
144598 |
96-10 |
12/4/1996 |
Vibration Test |
Pratt & Whitney Canada PW545A |
144607 |
96-11 |
12/4/1996 |
Wind-Milling |
Pratt & Whitney Canada PW545A |
144665 |
96-12 |
12/4/1996 |
Bird Ingestion |
Pratt & Whitney Canada PW545A |
153413 |
96-13 |
12/4/1996 |
Water and Hail Ingestion |
Pratt & Whitney Canada PW545A |
145178 |
96-17 |
9/25/1996 |
Aeroplane Flight Characteristics and Performance |
Airbus Industrie A319 |
145299 |
96-18 |
9/27/1996 |
L-Band Diplexer/Low Noise Amplifier |
Phase Atlantic P/N AS 100697-01-201 |
145236 |
96-19 |
11/18/1996 |
Aircraft Cabin Humidifier |
Air Data Inc. LBFS 4229R25-00 |
145521 |
96-20 |
11/20/1996 |
Intermediate Gain Antenna |
Canadian Marconi Company CMA-2200 |
145282 |
97-01 |
1/6/1997 |
High Intensity Radiated Fields (HIRF) |
Bell 427 |
145875 |
97-04 |
4/8/1997 |
Bird Ingestion |
Pratt & Whitney Canada PW535A |
147367 |
97-05 |
4/8/1997 |
Water and Hail Ingestion |
Pratt & Whitney Canada PW535A |
147500 |
97-06 |
2/20/1997 |
Helicopter Passenger Transportation Suit System |
Meta Research Inc. MHSS01 |
146094 |
97-07 |
5/28/1997 |
VHF Data Link Receiver |
SED Systems Inc. VL-500 |
157494 |
97-10 |
12/30/1997 |
Satellite Communication System |
CAL Corporation CALQUEST |
146455 |
97-11 |
12/1/1997 |
Lightning Protection Indirect Effect |
Bell 427 |
146663 |
98-01 |
3/9/1998 |
Helicopter Rescue System Requirements for Human External Cargo (HEC) System |
Bell 206L - Parks Canada |
146974 |
98-02 |
5/31/1999 |
High Intensity Radiated Fields (HIRF) |
Bombardier Aerospace CL-600-2C10 |
146992 |
99-01 |
3/3/1999 |
Installation of a Single Flight Visions Head-Up Display (FV 2000) |
Gulfstream G-1159A |
148045 |
99-02 |
6/14/1999 |
30 Second OEI Limits - Limit Over-ride Feature |
Bell Helicopter Textron Canada 427 |
148068 |
99-03 |
6/23/1999 |
Obstacle Awareness System |
Amphitech International HRD 1200 |
154550 |
99-03
Rev. A |
8/21/2000 |
Obstacle Awareness System |
Amphitech International HRD 1200 |
148085 |
99-03
Rev. B |
7/18/2003 |
Obstacle Awareness System |
Amphitech International Model AI-130 |
443623 |
1999-04 |
7/23/1999 |
Operation on Narrow Runways |
De Havilland DHC-7-102/103 |
148108 |
99-05 |
10/14/1999 |
Remote Switch |
Northern Airborne Technology Ltd. RS |
148329 |
99-07 |
11/17/1999 |
Emergency Avionics System |
DRS Technologies Canada EAS-3000 (121.5/406 MHz) |
148654 |
2000-01 |
2/7/2000 |
Aircraft Conversion for the Aerial Fire Supression Role |
Convair 580 |
148699 |
2000-01
Rev. A |
3/9/2000 |
Aircraft Conversion for the Aerial Fire Supression Role |
Convair 580 |
148908 |
2000-02 |
2/22/2000 |
High Intensity Radiated Fields (HIRF) |
Bombardier Aerospace BD-100-1A10 |
148946 |
2000-03 |
4/10/2000 |
Mechanical Tests for the Twin-Pac Configuration |
Pratt & Whitney Canada PT6T-9 |
148960 |
2000-04 |
3/13/2000 |
Helicopter Rescue System for Human External Cargo (HEC) System |
Aero Design Ltd. Bell 206L |
148998 |
2000-04
Rev. A |
6/2/2000 |
Helicopter Rescue System for Human External Cargo (HEC) System |
Aero Design Ltd. Bell 206B, Bell 206L, L-1, L-3 and L-4, Bell 407; McDonnell Douglas 369D and E, 500N; Eurocopter AS350B, BA, B1, B2, B3, D and F, AS355F1 and F2. |
149214 |
2000-05 |
5/3/2000 |
L-Band Diplexer/Low Noise Amplifier |
Com Dev Wireless Group Aero-1, P/N 102618 |
157473 |
2000-05
Rev. A |
10/27/2000 |
L-Band Diplexer/Low Noise Amplifier |
Com Dev Wireless Group Aero-1, P/N 102618 |
157480 |
2000-06 |
4/18/2000 |
Installation of a Single Head-Up Display (HUD) System |
Bombardier Aerospace BD-700-1A10 Global Express |
150987 |
2000-07 |
5/3/2000 |
High Intensity Radiated Fields (HIRF) |
De Havilland DHC-7 |
151037 |
2000-08 |
10/6/2000 |
Automatic Performance Reset |
Bombardier CL-600-2C10 (RJ-700) |
151122 |
2000-09 |
12/22/2000 |
Performance Standards for Public Address (PA) Systems |
Bombardier BD-700-1A10 Global Express |
151287 |
2000-10 |
12/20/2000 |
Installation of a Single Flight Dynamics HGS 2860 Head Up Display (HUD) |
Dassault Falcon 900 EX |
151312 |
2001-01 |
2/22/2001 |
Approval of Steep Approach Landing Capability |
Bombardier Aerospace DHC-8-400 |
151386 |
H2001-02 |
4/24/2001 |
Automatic Overwing Emergency Exits |
Boeing B737-600/-700/-800 |
151413 |
H2001-02
Rev. A |
5/17/2001 |
Automatic Overwing Emergency Exits |
Boeing B737-600/-700/-800 |
151423 |
H2001-02
Rev. B |
5/23/2001 |
Automatic Overwing Emergency Exits |
Boeing B737-600/-700/-800 |
151460 |
H2001-02
Rev. C |
5/25/2001 |
Automatic Overwing Emergency Exits |
Boeing B737-600/-700/-800 |
151477 |
2001-03 |
8/20/2001 |
Aeroplane Flight Characteristics and Performance |
Airbus Industrie A321-100/200 |
188395 |
2001-04 |
11/19/2001 |
Passenger Seat Front Row Inflatable Lapbelt System |
Bombardier CL-600-2C10, Regional Jet (CRJ-700) |
151555 |
2001-04
Rev. A |
12/6/2001 |
Passenger Seat Front Row Inflatable Lapbelt System |
Bombardier CL-600-2C10, Regional Jet (CRJ-700) |
151587 |
H2002-01 |
2/8/2002 |
Automatic Performance Reserve |
Bombardier BD-100-1A10 |
151668 |
H2002-02 |
3/1/2002 |
Crew Rest Compartment |
Bombardier BD-700-1A10 - Global Express |
151700 |
H2002-03 |
8/19/2002 |
Fuel Tank System Safety – Ignition Prevention |
Bombardier CL-600-2D24, Regional Jet (CRJ-900) |
190609 |
H2002-04 |
8/19/2002 |
Automatic Performance Reset |
Bombardier CL-600-2D24, Regional Jet (CRJ-900) |
190614 |
H2002-05 |
8/19/2002 |
High Intensity Radiated Fields |
Bombardier CL-600-2D24, Regional Jet (CRJ-900) |
190615 |
H2002-06 |
12/6/2002 |
Passenger Seat Inflatable Lapbelt System |
Airbus Industrie Models A319/A320/A321 |
239550 |
H2003-01 |
03/21/2003 |
Inflatable Restraint System |
Zenair Model CH-2000 |
335903 |
2003-02 |
05/09/2003 |
High Intensity Radiated Fields |
SeaWind 300C Amphibian |
393287 |
2003-03 |
06/02/2003 |
Enhanced Vision System (EVS) |
Bombardier Global Express and Global 5000 Aeroplanes |
391686 |
2004-01 |
03/18/2004 |
Infrared Sensor Unit (ISU) |
CMC Electronics Inc. Model CMA-2600 |
686440 |
2004-02 |
11/12/2004 |
Single-Occupancy Side-Facing Seat |
Bombardier Aerospace Model BD100-1A10 |
917351 |
2005-01 |
01/28/2005 |
Continued Engine Operation During Transient Loss of Engine Control System Activity |
Pratt and Whitney Canada PW610F-A Engine |
973956 |
2005-02 |
03/24/2005 |
Helicopter Passenger Transportation Suit System |
DSS Marine Incorporated DS-HPTS-V01 HPTSS |
1078620 |
2005-02A |
10/05/05 |
Life Preserving Helicopter Passenger Transportation Suit System |
DSS Marine Incorporated DS-HPTS-V01 |
1350189 |
2005-03 |
03/24/2005 |
Aircraft Conversion for the Aerial Fire Suppression Role (Not Signed Yet) |
Cascade Dash 8-400 |
823774 |
2005-04 |
08/05/2005 |
Life Preserving Helicopter Passenger Transportation Suit System |
Whites Mfg. Ltd. Model 5A-S620 |
1281692 |
2005-05 |
08/05/2005 |
Life Preserving Helicopter Passenger Transportation Suit System |
Mustang Survival Model MHSS01 |
1283606 |
2005-06 |
10/24/2005 |
High Intensity Radiated Fields |
Bell Helicopter Textron Canada Lt d. Model Bell 429 |
1291301 |
2005-07 |
03/09/2006 |
30-Second One-Engine-Inoperative Power Limits – Limit Override Feature |
Bell Helicopter Textron Canada Limited Model 429 |
1314885 |
2006-01 |
03/28/2006 |
Single-Occupancy Side-facing Seats Equipped With Inflatable Lapbelts |
Boeing Model 767 |
1394217 |
2006-02 |
04/04/2006 |
Aircraft Operation after Ground Cold Soak |
Pilatus Models PC-12/45 and PC-12/47 |
1760373 |
2006-03 |
04/04/2006 |
High Intensity Radiated Fields (HIRF) |
Pilatus Models PC-12/45 and PC-12/47 |
1755894 |
2006-04 |
10/5/2006 |
High Intensity Radiated Fields (HIRF) |
Agusta Model AB 139 Helicopter |
1415397 |
2006-05 |
26/09/2006 |
High Intensity Radiated Fields (HIRF) |
Symphony Model SA 160 with Avionics Update (S/N S-10001 and subsequent) |
1952152 |
2006-06 |
17/11/2006 |
High Altitude Operation up to 41,000 Feet. |
Boeing Model 777-200LR/-300ER Series Aeroplanes |
1979028 |
2006-07 |
08/12/2006 |
Life Preserving Helicopter Passenger Transportation Suit System |
Helly Hansen Canada Limited Model E-452 |
2109404 |
2007-01 |
01/29/2007 |
Approval of Steep Approach and Landing Capability. |
Bombardier Model CL-600-2B18 (606 and 605 Variants) |
2203909 |
2007-02 |
05/11/2007 |
Engine Operation in Auxiliary Power Unit (APU) Mode |
Pratt & Whitney Canada Model PA210S Engine |
2319024 V1 |
2007-03 |
09/14/2007 |
Rejected Takeoff Performance |
Diamond Model D-Jet Aeroplane |
2284204 V1 |
2007-04 |
09/14/2007 |
Emergency Landing Conditions – Engine Retention |
Diamond Model D-Jet Aeroplane |
2287516 V1 |
2007-05 |
09/14/2007 |
High Intensity Radiated Fields (HIRF) |
Diamond Model D-Jet Aeroplane |
2010173 V1 |
2007-06 |
09/14/2007 |
Fire Extinguishing for Aft Fuselage Mounted Engines |
Diamond Model D-Jet Aeroplane |
2285282 V1 |
2007-07 |
09/14/2007 |
Full Authority Digital Engine Control |
Diamond Model D-Jet Aeroplane |
2305410 V3 |
2007-08 |
10/26/2007 |
Retractable Wheel-Ski Installation – Load Requirements |
Amtech Aeronautical Ltd., Douglas Model DC3C with Basler PT6A-67R Conversion |
3653839 V4 |
2007-09 |
11/06/2007 |
New Engine Rating: 30-Minute Hovering Power |
Pratt & Whitney Canada Model PW210S Engine |
2526443 V2 |
For further information, please contact the Manager, Domestic Regulations,
Regulatory Standards, Aircraft Certification, at (613) 990-5213 or
email aardh-d@tc.gc.ca.