# TCDS T00005NY: Bombardier Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Bombardier Inc.
- Revision: 12
- Revised: July 2, 2019
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Registered aircraft: 878, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/74/6c/746c8f8deb808820baa77231f592f9b65b426fd08d167d1b9aa6c2bf9ce3b805
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/16C9267B2E0010B98625843100611BB5.0001
- Page: https://openairdocs.org/tcds/T00005NY

## Models (1)

As the data sheet lists them.

- BD-100-1A10

## What the data sheet says

Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

```text
Page No. 1 2 3 4 5 6 7 8 9 10 
Rev No. 11 12 7 7 11 9 11 12 7 7 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
T00005NY 
Revision No. 12 
Bombardier  Inc. 
BD-100-1A10 
July 2, 2019 
 
TYPE CERTIFICATE DATA SHEET NO. T00005NY 
  
This data sheet which is part of Type Certificate No. T00005NY, prescribes conditions and limitations under 
which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal 
Aviation Regulations (FAR). 
 
Type Certificate Holder: Bombardier Inc. 
800 boul. René Lévesque West 
Montreal, Quebec, Canada  
H3B1Y8 
 
I - Model BD-100-1A10,  (Transport Category), Approved June 4, 2003 by the FAA and May 30, 2003, by 
Transport Canada Civil Aviation with Canadian type certificate number A-234 
  
 
ENGINES Two Honeywell AS907-1-1A for S/N 20002 to 20500, or  
two Honeywell AS907-2-1A for S/N 20501 and subsequent, engine type certificate number 
E00010LA 
  
 
FUEL Type  Specifications   
  Canada U.S.A. U.K.  
 Jet A CAN2-3.23 ASTM D1655 D. Eng RD2494  
 Jet A-1 CAN2-3.23 ASTM D1655 D. Eng RD2494  
  
 
OIL Engine, APU: Refer to Aircraft Maintenance Manual, Bombardier Publication BD 100 AMM, 
Chapter 12. 
  
 
AS907-1-1A ENGINE 
LIMITS CONDITIONS  
Refer to Limits Table in the AFM (CH 300 AFM)  
 
AS907-2-1A ENGINE 
LIMITS CONDITIONS 
Refer to Limits Table in the AFM (CH 350 AFM)  
         
 
OIL TEMPERATURE  °C °F 
 Minimum for Starting (ground)  -40 -40 
 Minimum before accelerating above idle N/A N/A 
 Maximum Continuous 138 280 
 Maximum Permissible (transient, 2 minutes)  154 309

Page 2 of 11 T00005NY  
   
OIL PRESSURE Take-off Power (minimum) * 
 Steady State Idle (minimum) 28 psi 
  * Oil pressure is not regulated and pressure limits varies with N 2 speeds 
    
APU  Honeywell 36-150[BD] 
      
APU LIMITS Maximum RPM: 110%    
  Maximum EGT: °C °F   
   Starting 512-1024 954-1875   
   Running 594-714 1101-1317   
 
    
 
AIRSPEED LIMITS (IAS) S/N 20002 - 20500 S/N above 20501 
S/N 20813 and subsequent & 
20501 to 20812, incorporating 
SB 350−27−008, Rudder Travel 
Increase (See Flight Manual 
Supplement 11, SFO, for 
additional limitations) 
VMO and MMO 
(Maximum Operating): m.p.h. knots Mach m.p.h. knots Mach m.p.h. knots Mach 
Sea Level to 8000 ft. 345 300 - 345 300 - 345 300 - 
8001 ft. to 29475 ft. 368 320 - 368 320 - 368 320 - 
Above 29475 ft. - - 0.83 - - 0.83 - - 0.83 
VFE                                                                 
10° 242 210 - 242 210 - 242 210 - 
20° 242 210 - 242 210 - 242 210 - 
30° 201 175 - 201 175 - 201 175 - 
VD and MD          
Sea Level to 25525 ft. 437 380 - 437 380 - 437 380 - 
Above 25525 ft. - - 0.90 - - 0.90 - - 0.90 
See Flight Manual for variation of Va with altitude and aircraft weight  
VMCA                                
Flap 10° 122 106 - 127 110 - 127 110 - 
Flap 20° 117 102 - 125 109 - 125 109 - 
VMCG                                
Flap 10° 128 111 - 132 115 - 132 115 - 
Flap 20° 128 111 - 131 114 - 125 109 - 
VLO (EXT) 288 250 - 288 250 - 288 250 - 
VLO (RET) 230 200 - 230 200 - 230 200 - 
VLE 288 250 - 288 250 - 288 250 - 
 
 
C. G. RANGE See Figure 1.0, Longitudinal C.G. Envelope  
MRW=Maximum Ramp Weight 
MTOW= Maximum Takeoff Weight 
MLW=Maximum Landing Weight 
MZFW=Maximum Zero Fuel Weight 
MFW=Minimum Fuel Weight 
  
DATUM FS 0.0 located at 195 in. Fwd of the aircraft nose

Page 3 of 11 T00005NY  
MEAN AERO-
DYNAMIC CHORD 
112.2 in (MAC leading edge at fuselage station 556.67 in.)  
  
LEVELING MEANS Plumb bob and target in the aft equipment bay at FS 755.5 and RBL 1.0  
 
 
 
MAXIMUM 
WEIGHTS 
(S/Ns up to 20500) 
(See Figure 1) 
(See Note 1) 
 lb. kg.   
Max. Taxi and Ramp 38 650 17 530   
Max. Takeoff 38 500 17 460   
Max. Landing 33 750 15 310   
Max. Zero Fuel 26 100 11 840   
  
 
INCREASED 
MAXIMUM WEIGHT 
WITH M.S.100T010126 
BB100T010126 & S.B. 
100-11-01 (See Figure 
2)(See Note 1) 
 lb. Kg.   
Max. Taxi and Ramp 39 000 17 690   
Max. Takeoff 38 850 17 622   
Max. Landing 33 750 15 310   
Max. Zero Fuel 27 000 12 247   
 
 
MAXIMUM 
WEIGHTS 
(S/N 20501 and subs) 
(See Figure 3) 
(See Note 1) 
 lb. Kg.  
Max. Taxi and Ramp 40 750 18 484  
Max. Takeoff 40 600 18 416  
Max. Landing 34 150 15 490  
Max. Zero Fuel 28 200 12 791  
  
MINIMUM CREW Two (Pilot and Co-pilot) 
  
MAXIMUM 
OCCUPANTS 
19 (including the crew and no more than 16 passengers)  
See Note 4 
 
  
FUEL CAPACITY  Load Weight** 
 Usable U.S. Gal. liters lb. kg 
 2 main tanks (each) 1 048 3 967 7 074 3 209 
 Total 2 096 7 934 14 150 6 418 
* Total Unusable 
(drainable) 
7.5 28.2 50.4 22.8 
*  Total Undrainable 6.4 24.3 43.4 19.7 
 * See NOTE 3 
** Assuming a fuel density of 6.75 lbs/U.S. Gal. 
 
OIL CAPACITY  Load Weight 
  U.S. Qts. liters lb. kg. 
 Left Engine 6.0 5.7 12.6 5.7 
 Right Engine 5.0 4.7 10.4 4.7 
 Total 11.0 10.4 23.0 10.4 
 Usable per Engine 1.7 1.6 3.5 1.6 
  
MAX. OPERATING Take off and landing:   10 000 ft

Page 4 of 11 T00005NY  
ALTITUDE En route:           45 000 ft 
  
CONTROL SURFACE Rudder 30° Left 30° Right  
MOVEMENTS Horizontal Stabilizer 2° LE Up 12° LE Down 
 Aileron 18° TE Up 18° TE Down 
 Elevator 24° TE Up 18° TE Down 
 Ground spoilers 60° Up - 
 Multi-function spoilers  
(Inboard to Outboard) 
45 ° Up - 
  
TYPE CERTIFICATION 
APPLICATION DATE 
28 June 1999 
  
SERIAL NUMBERS 
ELIGIBLE 
20002 and subsequent 
  
SERVICE INFORMATION Service Bulletins, structural repair manuals, vendor manuals, overhaul and 
maintenance manuals, and aircraft flight manuals which contain a statement 
that the document is Transport Canada approved or Transport Canada 
approved through the Manufacturers Design Approval Representative are 
accepted by the FAA and are considered FAA approved.  (These approvals 
pertain to the design data only). 
  
APPROVED 
PUBLICATIONS 
  
S/N 20002 to 20500 (a) 
 
Airplane Flight Manual (AFM), Bombardier Publication CSP 100 -1, dated 
May 30, 2003 and subsequent approved revisions. 
(b) Drawing List, Bombardier Publication RAL-100-0001, Issue A and 
subsequent approved revisions. 
(c) Time Limits/Maintenance Checks Manual, Bombardier Publication CH 300 
TLMC and subsequent approved revisions contains the Certification 
Maintenance Tasks, Life Limited Parts and Damage Tolerant Inspections.  
See NOTE 3  
(d) Structural Repair Manual (SRM), Bombardier Publication CH 300 SRM and 
subsequent approved revisions. 
See NOTE 3 
  
S/N 20501 and subs (a) 
 
Airplane Flight Manual (AFM), Bombardier Publication CH 350 AFM, dated 
June 24, 2014 and subsequent approved revisions. 
(b) Drawing List, Bombardier Publication RAL-100-0001, Issue A and 
subsequent approved revisions. 
(c) Time Limits/Maintenance Checks Manual, Bombardier Publication CH 350 
TLMC and subsequent approved revisions contains the Certification 
Maintenance Tasks, Life Limited Parts and Damage Tolerant Inspections.  
See NOTE 3  
(d) Structural Repair Manual (SRM), Bombardier Publication CH 350 SRM and 
subsequent approved revisions. 
See NOTE 3 
  
  
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:

Page 5 of 11 T00005NY  
  
 "This certifies that the aircraft described below has been manufactured in 
conformity with data forming the basis for the Transport Canada Type 
Certificate No. A-234 and includes the minimum type design defined in 
document RAZ-BA100-124 Issue A or subsequent approved revisions and 
RAL-100-0001 Issue A or subsequent approved revisions as being required to 
comply with the basis for the U.S. Type Certificate No. T00005NY, and is in a 
condition for safe operation. " 
  
 The approved type design appropriate to the "as delivered" configuration of a 
particular BD-100-1A10 airplane is defined in the document RAL-100-
XXXX.  (XXXX represents the Serial Number for the airplane concerned).  
  
 The U.S. airworthiness certification basis for aircraft type certificated under 
FAR 21.29 and exported by the country of manufacture is FAR 21.183(c) or 
FAR 21.185(c) 
  
 The U.S. airworthiness certification basis for aircraft type certificated under 
FAR 21.29 and exported from countries other than the country of manufacture 
(e.g. third party country) is FAR 21.183(d) or FAR 21.185(b)  
  
 The U.S. airworthiness certification basis for the issuance of an airworthiness 
certificate for aircraft type certificated under FAR 21.21 and manufactured in 
a foreign country under a licensing arrangement is FAR 21 .183(d) or FAR 
21.183(b) 
  
 The U.S. airworthiness certification basis for  an aircraft originally type 
certificated under FAR 21.21 but transferred outside the U.S. is 21.183(d) 
  
 Additional guidance is contained in FAA AC 21 -23A, or subsequent revision,  
Airworthiness Certification of Civil Aircraft, Engines, Propellers and Related 
Products Imported into the United States. 
  
CERTIFICATION BASIS FAR Part 25, including: 
Amendments 25-1 through 25-101, 
Amendment 25-103 and Amendment 25-105. 
 
There are no exceptions. 
  
 Exemptions: 
 (1) Static testing requirements of FAR 25.1435(b)(1), Hydraulic System 
Proof Pressure Testing, Exemption No. 7508, Regulatory Docket No. 
FAA-2001-9034, issued April 18, 2001. 
 (2) 
 
 
(3) 
General Occupant Protection of FAR 25.785(b), Multi-Place Side Facing 
Divans, Exemption No. 7884A, Regulatory Docket No. FAA-2002-
11998, issued September 2, 2003. 
Exemption No. 11013 , FAR 25.901(c) Uncontrollable High Thrust (See 
Note 8 and Note 9) 
  
 Additional FAA Requirements: 
 (1) FAR Part 36 dated February 3, 2006,  
as amended through Amendment 36 -28 inclusive. 
 (2)  Applicable portions of FAR 34 dated November 5, 2002, 
as amended through Amendment 34 -3 inclusive.

Page 6 of 11 T00005NY  
 (3) Special Conditions: 
High Intensity Radiated Fields (HIRF), Docket No. NM243, Special 
Condition No. 25-226-SC, effective date 1/9/2003. 
 
Approach and Go-around use of Automatic Power Reserve, Docket No. 
NM255, Special Conditon  No. 25-03-04-SC, effective date May 28, 
2003 
 
Limit Engine Torque Loads for Sudden Engine Stoppage, Docket No. 
NM245, Special Condition No. 25-229-SC, effective date March 6, 2003  
 
Side Facing Single Occupancy Seats, Docket No. NM259, Special 
Condition No. 25-249-SC, effective October 6, 2003 
 
No. 25-659-SC, Non-Rechargeable Lithium Batteries, effective to design 
changes applied for after May 12, 2017.  See the applicability section of 
this special condition for more information on which design changes 
must meet it. 
  
 Equivalent safety has been established for the following requirements:  
 (1) FAR 25.103 and several other FAR’s for the use of 1-g stall speed and 
reduced reference speeds 
(documented in Transport Airplane Directorate Equivalent Level of 
Safety (ELOS) Memo No. TC2500NY-T-F-1) 
 (2) FAR 25.933(a)(1)(ii) Capability of Continued Safe Flight and Landing 
under any possible position of the Thrust Reverser System (documented 
in Transport Airplane Directorate ELOS Memo No. TC2500NY -T-P-1) 
 (3) FAR 25.1203, FAR 25.1207 Engine Thrust Reverser Zone Fire Detection 
(documented in Transport Airplane Directorate ELOS Memo No. 
TC2500NY-T-P-3) 
 (4)  FAR 25.177(c) Static lateral-directional stability, (documented in 
Transport Airplane Directorate (TAD) ELOS Memo No. TC2500NY-T-
F-2) 
 (5) FAR 25.811(d)(1) and 25.812(b)(1)(i) Emergency Exit Marking and 
Locator Signs (documented in Transport Airplane Directorate 
Equivalent Level of Safety (ELOS) Memo No. ANM-113-04-01) 
 (6) FAR 25.813(e) Lavatory Door (documented in Transport Airplane 
Directorate Equivalent Level of Safety (ELOS) Memo No. ST4805NY-
SE-1) 
  
 Compliance with the following optional requirements has been established: 
 (1) Ditching provisions of FAR 25.801 when the safety equipment 
requirements of FAR 25.1411 and the ditching equipment requirements 
of FAR 25.1415 are satisfied. 
  
EQUIPMENT The basic equipment as prescribed in the applicable airworthiness 
requirements (see Certification Basis) must be installed in the aircraft for 
certification. 
  
   
NOTE 1 (a) A current weight and balance report including the list of equipment 
included in the certificated empty weight, and loading instructions when 
necessary, must be provided for each aircraft at the time of original 
certification.

Page 7 of 11 T00005NY  
   
 (b) System fuel, which must be included in the empty weight, is the amount 
of fuel required to fill the system plumbing and tanks to the undrainable 
level plus unusable fuel in the fuel tanks.  The weight of undrainable and 
unsuable fuel defined in the Fuel Capacity section must be included in 
the empty weight of the airplane. 
  
NOTE 2 All placards must be installed in accordance with Bombardier Drawings:   
1001100001, 1001100002, 1001100003 and 1001100004. 
  
NOTE 3 The airplane life limits and repetitive inspections for components and 
equipment and information essential for proper maintenance, ar e listed in 
Bombardier Publication BD 100 TLMC.  These limitations may not be 
changed without FAA Engineering approval.  
 
Instructions for Continued Airworthiness consist of the following Publications: 
a) BD 100 AMM, Aircraft Maintenance Manual (Publication s No. 
CH300 AMM and CH350 AMM) 
b) BD100 TLMC, Time Limits/Maintenance Checks Manual 
(Publications No. CH300 TLMC and CH350 TLMC) 
c) BD 100 SRM, Structural Repair Manual  
(Publications No. CH300 SRM and CH350 SRM) 
d) BD 100 NDT, Non-Destructive Testing Manual (Publications No. 
CH300 NDTM and CH350 NDTM) 
 
  
NOTE 4 
 
The green aircraft type design configuration does not include passenger 
provisions.  Carriage of persons in the cabin is permitted when an approved 
seating arrangement and related required passenger provisio ns are 
incorporated in accordance with the Type Certificate Basis. 
  
NOTE 5 Bombardier Aerospace report RAZ-BA-100 provides guidance to completion 
centers regarding compliance with the basis of certification for the BD-100-
1A10 Challenger 300 with a completed interior. 
  
NOTE 6 Compliance with FAR 25.105(c)(1) and 25.125(b), associated with Takeoff and 
Landing Performance on Unpaved Runways, has not been demonstrated. 
  
NOTE 7 “Challenger 300” is a marketing designation for the BD -100-1A10 up to 
aircraft S/N 20500. “Challenger 350” is a marketing designation for the BD -
100-1A10 starting at aircraft S/N 20501.  
  
NOTE 8 The FAA has concluded that the occurrence of any uncontrollable high -thrust 
failure conditions, or any of the associated causal failures listed in Section 05-
10-00 of the CH350 TLMC, Time Limits/Maintenance Checks Manual may 
endanger the safe operation of an airplane , and hence are reportable under 
FAR 121.703(c), 125.409(c), and 135.415(c).

Page 8 of 11 T00005NY  
NOTE 9 Bombardier has complied with the conditions in TLE 11013 with the 
incorporation of Modification Summary 100T010874.  TLE 11013 
permanently exempts the Model BD-100-1A10 airplane from single failures 
within the Airplane Throttle System (ATS) and single failures on approach 
below 400 feet from full compliance with 25.901(c) as it pertains to UHT. No 
retrofit is required.  
  
The FAA has concluded that the occurrence of any uncontrollable high-thrust 
failure conditions, or any of the associated causal failures listed in Section 05-
10-00 of the CH350 TLMC, Time Limits/Maintenance Checks Manual may 
endanger the safe operation of an airplane.   Consequently, the FAA 
recommends that operators report any such failures in accordance with title 14, 
Code of Federal Regulation 121.703(c), 125.409(c), and 135.415(c).

Page 9 of 11  T00005NY
Figure 1.0
LONGITUDINAL C.G. ENVELOPE
40000
- 17980
MRW 38 650 lb (17 530 kg)
MTOW 38 500 Ib (17 465 kg)
38000
- 16980
36000
- 15980
34000
MLW 33 750 Ib (15 310 kg)
14980
Aircraft Weight (Ib)  32000  Aircraft Weight (kg)
13980
30000
- 12980
28000
MZFW 26 100 lb (11 840 kg)  - 11980
26000
- 10980
24000
MFW 23 100 lb (10 480 kg)
22000 +  + 9980
20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45
% MAC

Page 10 of 11 T00005NY  
 
Figure 2.0 
LONGITUDINAL C.G. ENVELOPE 
(A/Cs with M.S.100T010126, BB100T010126 
& S.B. 100-11-01) 
 
 
22000
24000
26000
28000
30000
32000
34000
36000
38000
40000
20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45
% MAC
Aircraft Weight (lb)
10000
11000
12000
13000
14000
15000
16000
17000
18000
Aircraft Weight (kg)
MRW 39 000 lb (17 690 kg)
MTOW 38 850 lb (17 622 kg)
MLW 33 750 lb (15 309 kg)
MZFW 27 000 lb (12 247 kg)
MFW 23 100 lb (10 478 kg)

Page 11 of 11  T00005NY
Figure 3.0
LONGITUDINAL C.G. ENVELOPE
(S/N 20501 and subsequents)
42000  19000
MRW 40 750 Ib (18 484 kg)
MTOW 40 600 Ib (18 416 kg)
40000
- 18000
38000
- 17000
36000
16000
MLW 34 150 lb (15 490 kg)
34000
Aircraft Weight (Ib)  32000  - 15000  Aircraft Weight (kg)
14000
30000
MZFW 28 200 Ib (12 791 kg)  - 13000
28000
- 12000
00092
MFW 24 800 lb (11 249 kg)
- 11000
0O0+Z
0002Z  00001 +
20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45
% MAC
```

## ADs (60, 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 2026-02-06](https://openairdocs.org/ad/2026-02-06): Flight controls · Bombardier BD-100-1A10. Effective Feb 25, 2026
- [AD 2026-01-07](https://openairdocs.org/ad/2026-01-07): Time Limits/Maintenance Checks · Bombardier BD-100-1A10. Effective Feb 20, 2026
- [AD 2025-02-01](https://openairdocs.org/ad/2025-02-01): Flight controls · Bombardier BD-100-1A10. Effective Mar 17, 2025
- [AD 2024-21-04](https://openairdocs.org/ad/2024-21-04): Electrical Power · Bombardier BD-100-1A10. Effective Dec 17, 2024
- [AD 2024-18-03](https://openairdocs.org/ad/2024-18-03): Electrical Power · Bombardier BD-100-1A10. Effective Nov 12, 2024
- [AD 2024-16-18](https://openairdocs.org/ad/2024-16-18): Nacelles/Pylons · Bombardier BD-100-1A10. Effective Oct 30, 2024
- [AD 2024-16-13](https://openairdocs.org/ad/2024-16-13): Ice and Rain Protection · Bombardier BD-100-1A10. Effective Oct 29, 2024
- [AD 2024-16-04](https://openairdocs.org/ad/2024-16-04): Equipment/Furnishings · Bombardier BD-100-1A10. Effective Oct 23, 2024
- [AD 2024-11-02](https://openairdocs.org/ad/2024-11-02): Stabilizer · Bombardier BD-100-1A10. Effective Aug 26, 2024
- [AD 2024-01-09](https://openairdocs.org/ad/2024-01-09): Landing gear · Bombardier BD-100-1A10. Effective Mar 21, 2024
- [AD 2023-26-02](https://openairdocs.org/ad/2023-26-02): Pneumatic · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 27, 2024
- [AD 2023-23-05](https://openairdocs.org/ad/2023-23-05): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 14, 2023
- [AD 2023-13-06](https://openairdocs.org/ad/2023-13-06): Time limits/maintenance checks, Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective Sep 1, 2023
- [AD 2023-14-11](https://openairdocs.org/ad/2023-14-11): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 10, 2023
- [AD 2023-12-06](https://openairdocs.org/ad/2023-12-06): Auto flight · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 7, 2023
- [AD 2023-11-04](https://openairdocs.org/ad/2023-11-04): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 21, 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 2023-03-18](https://openairdocs.org/ad/2023-03-18): Fuselage · Bombardier BD-100-1A10 (Challenger 300). Effective Apr 4, 2023
- [AD 2023-02-01](https://openairdocs.org/ad/2023-02-01): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 14, 2023
- [AD 2022-12-02](https://openairdocs.org/ad/2022-12-02): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 21, 2022
- [AD 2022-09-02](https://openairdocs.org/ad/2022-09-02): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 16, 2022
- [AD 2022-03-11](https://openairdocs.org/ad/2022-03-11): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 17, 2022
- [AD 2021-25-07](https://openairdocs.org/ad/2021-25-07): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 15, 2022
- [AD 2021-23-14](https://openairdocs.org/ad/2021-23-14): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Jan 10, 2022
- [AD 2021-14-01](https://openairdocs.org/ad/2021-14-01): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 24, 2021
- [AD 2021-10-26](https://openairdocs.org/ad/2021-10-26): Hydraulic power · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 6, 2021
- [AD 2021-09-17](https://openairdocs.org/ad/2021-09-17): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 23, 2021
- [AD 2021-09-16](https://openairdocs.org/ad/2021-09-16): Pneumatic; Engine Fuel and Control · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 1, 2021
- [AD 2021-03-10](https://openairdocs.org/ad/2021-03-10): Fire protection · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 31, 2021
- [AD 2020-25-06](https://openairdocs.org/ad/2020-25-06): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jan 27, 2021
- [AD 2020-11-14](https://openairdocs.org/ad/2020-11-14): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 21, 2020
- [AD 2020-11-10](https://openairdocs.org/ad/2020-11-10): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 14, 2020
- [AD 2019-15-04](https://openairdocs.org/ad/2019-15-04): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 23, 2019
- [AD 2019-03-29](https://openairdocs.org/ad/2019-03-29): Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 6, 2019
- [AD 2019-07-06](https://openairdocs.org/ad/2019-07-06): Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective May 28, 2019
- [AD 2018-20-16](https://openairdocs.org/ad/2018-20-16): Hydraulic Power · Bombardier BD-100-1A10 (Challenger 300). Effective Nov 23, 2018
- [AD 2018-14-05](https://openairdocs.org/ad/2018-14-05): SUMMARY: We are adopting a new airworthiness directive (AD) for certain  
 Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by reports  
 of fire incidents of the auxiliary power unit (APU) inlet, which caused tail  
 cone damage after an initial failed APU start followed by two or more in-flight  
 APU start attempts. This AD requires modification of the APU electronic control  
 unit (ECU) wiring harness. We are issuing this AD to address the unsafe · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 13, 2018
- [AD 2018-13-04](https://openairdocs.org/ad/2018-13-04): Oxygen · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 25, 2018
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017
- [AD 2017-17-13](https://openairdocs.org/ad/2017-17-13): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Oct 2, 2017
- [AD 2017-14-16](https://openairdocs.org/ad/2017-14-16): Fuselage · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 1, 2017
- [AD 2017-12-11](https://openairdocs.org/ad/2017-12-11): Equipment/ Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 20, 2017
- [AD 2017-11-12](https://openairdocs.org/ad/2017-11-12): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 11, 2017
- [AD 2016-02-05](https://openairdocs.org/ad/2016-02-05): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 8, 2016
- [AD 2015-26-03](https://openairdocs.org/ad/2015-26-03): Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 2, 2016
- [AD 2015-23-07](https://openairdocs.org/ad/2015-23-07): Electrical Power · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 22, 2015
- [AD 2015-15-08](https://openairdocs.org/ad/2015-15-08): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 28, 2015
- [AD 2014-05-23](https://openairdocs.org/ad/2014-05-23): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Apr 15, 2014
- [AD 2012-12-17](https://openairdocs.org/ad/2012-12-17): Oxygen · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 30, 2012

All 60: https://openairdocs.org/tcds/T00005NY/ads.md

## Registered aircraft by registry model (OpenAirDocs)

- [Bombardier BD-100-1A10](https://openairdocs.org/model/bombardier-bd-100-1a10): 874 aircraft (registry code 1390044)
- [Bombardier Aerospace BD-100-1A10](https://openairdocs.org/model/bombardier-aerospace-bd-100-1a10): 4 aircraft (registry code 1390050)

## STCs approved under this data sheet (141, first 50)

- [STC ST11935CH](https://openairdocs.org/stc/ST11935CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [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 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 ST12288IB](https://openairdocs.org/stc/ST12288IB): Demonstration of TPED Tolerance. Bombardier Inc.
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc.
- [STC ST12036WI](https://openairdocs.org/stc/ST12036WI): Installation of Gogo Business Aviation Galileo Half-Duplex (HDX). Gogo Business Aviation LLC
- [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc.
- [STC ST04560AT](https://openairdocs.org/stc/ST04560AT): Replacement of the existing Honeywell HTF7000 engine upper and lower thrust reverser door assemblies with Quiet Technology Aerospace modified upper and lower thrust reverser door assemblies. Quiet Technology Aerospace
- [STC ST01569LA](https://openairdocs.org/stc/ST01569LA): Installation of Floor Proximity Emergency Escape Path Marking System. Bruce Aerospace 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 ST02691SE](https://openairdocs.org/stc/ST02691SE): Installation of Head-up Display System (HUD) Model 6650 and Enhance Vision System (EVS) Model 3600. Rockwell Collins Inc.
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1.. Peregrine
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc.
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST00200IB](https://openairdocs.org/stc/ST00200IB): Installation of Gogo AVANCE L5 System. Sky Service F.B.O. Inc.
- [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 ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc.
- [STC ST01970WI](https://openairdocs.org/stc/ST01970WI): Installation of an Aircraft Health Management System (AHMS). Learjet Inc.
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02765LA](https://openairdocs.org/stc/ST02765LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc
- [STC ST04544CH](https://openairdocs.org/stc/ST04544CH): Installation of a Viasat Business Aviation Router (VBR) P/N 1371388. StandardAero Business Aviation Services LLC
- [STC ST04327CH](https://openairdocs.org/stc/ST04327CH): Installation of High Speed Internet System and Wireless Activation. Nextant Aerospace LLC
- [STC ST01991WI](https://openairdocs.org/stc/ST01991WI): Installation of Switch Bezels. Duncan Aviation Inc.
- [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and
upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25.. BHE & Associates Ltd.
- [STC ST04490CH](https://openairdocs.org/stc/ST04490CH): Installation of a Viasat Business Aviation Router (VBR) P/N 1371388 in accordance with StandardAero Master Data List 1039044, Revision (B), dated November 13, 2020 or later FAA approved revision.. Learjet Inc
- [STC ST02293SE](https://openairdocs.org/stc/ST02293SE): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Aerospace Corp.
- [STC ST04508CH](https://openairdocs.org/stc/ST04508CH): Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM System and a KuKa Radome in
accordance with Master Data List (MDL), 1039410, Revision (F), dated November 05, 2021, or later
FAA Approved Revision.. StandardAero Business Aviation Services LLC
- [STC ST02047NY](https://openairdocs.org/stc/ST02047NY): Modification of Complete Custom Aircraft Interior to be completed. Bombardier Aerospace
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc.
- [STC ST04455CH](https://openairdocs.org/stc/ST04455CH): Installation of a Viasat Ka Radome in accordance with StandardAero Master Data List 1038145, Revision (E), dated November 13, 2020 or later FAA approved revision.. Learjet Inc
- [STC ST04457CH](https://openairdocs.org/stc/ST04457CH): Installation of a Viasat Ka Terminal in accordance with StandardAero Master Data List 1038079, Revision (B), dated November 14, 2020 or later FAA approved revision.. Learjet Inc
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS).  This approval is limited to specifically idenitfied aircraft.. Duncan Aviation Inc
- [STC ST04352NY](https://openairdocs.org/stc/ST04352NY): Installation of Fire Extinguishers with Halocarbon Clean Extinguishing Agents. Bombardier Inc
- [STC ST04391NY](https://openairdocs.org/stc/ST04391NY): Installation of Galley with Compartment for Commercial-off-the-shelf (COTS) Appliances or Equipment. Bombardier Inc
- [STC ST00923DE](https://openairdocs.org/stc/ST00923DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00395BO](https://openairdocs.org/stc/ST00395BO): Installation of a Honeywell GoDirect Router. Pro Star Aviation, LLC
- [STC ST04236NY](https://openairdocs.org/stc/ST04236NY): Installation of Lavatory Glass Mirror. Bombardier Inc
- [STC ST00267BO](https://openairdocs.org/stc/ST00267BO): Installation of a Honeywell HD-710 High Speed Data Receiver, EMS AMT-50 High Gain Antenna System, and EMS CNX-200 Cabin Network Router in accordance with Pro Star Aviation Master Document List 20674-MDL-02, Revision D, dated March 17, 2008, or later FAA-approved revision.. Pro Star Aviation, LLC
- [STC ST00268BO](https://openairdocs.org/stc/ST00268BO): Installation of an EMS Satcom AMT-50 High Gain Antenna System. Pro Star Aviation, LLC
- [STC ST02130LA](https://openairdocs.org/stc/ST02130LA): Installation of Honeywell MKV Enhanced Ground Proximity Warning System (EGPWS) with Runway Awareness and Advisory System (RAAS).. Pro Star Aviation, LLC
- [STC ST04148NY](https://openairdocs.org/stc/ST04148NY): Installation of the Rockwell Collins TDR-94D ADS-B Out Upgrade. Mid Canada Mod Center
- [STC ST02976NY](https://openairdocs.org/stc/ST02976NY): Installation of ADS-B Out System in the Bombardier BD-100-1A10 (CH 300) aircraft with Rockwell Collins Pro Line 21 Series Avionics System. Flying Colours Corp.
- [STC ST04123NY](https://openairdocs.org/stc/ST04123NY): Installation of Bleed Air Leak Detection System Loop Element Shell and Insert Assembly Replacement. Bombardier Inc
- [STC ST04290CH](https://openairdocs.org/stc/ST04290CH): Wireless Local Area Network (WLAN) Cabin Router and Aircraft Transmitting Portable Electronic Device (TPED) Compatibility. Comlux America LLC
- [STC ST00896DE](https://openairdocs.org/stc/ST00896DE): Installation of a 3-Place Side-Facing Divan. Lee Products Engineering Services, Inc.

All 141: https://openairdocs.org/tcds/T00005NY/stcs.md

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