Type Record · As of May 3, 2026
BRITISH AIRCRAFT CORP BAC 1-11 419/EP
Fixed Wing Multi Engine · ROLLS-ROYC SPEY MK 511SR
Registered
1
Year Range
1967–1967
NTSB Events
1
Airworthiness Directives
0
01 / Distribution
Where the fleet lives and was built
Counts of currently-registered BRITISH AIRCRAFT CORP BAC 1-11 419/EP aircraft by US state and decade of manufacture, sourced from the FAA Aircraft Registry.
By State (top 10)
- MO 100.0% 1
By Decade of Manufacture
- 1960s 100.0% 1
02 / NTSB Records
Events involving BRITISH AIRCRAFT CORP BAC 1-11 419/EP aircraft
1 event(s) on file. Showing the most recent 1.
-
Oct 23, 1994
N999BWNEWVILLE, Alabama Fatal
NTSB Docket →
03 / Airworthiness Directives
FAA directives applicable to BRITISH AIRCRAFT CORP BAC 1-11 419/EP
No matching airworthiness directives are on file for this make and model in the Federal Register.
04 / Type Certificate Data Sheets
FAA TCDS for BRITISH AIRCRAFT CORP BAC 1-11 419/EP
The TCDS is the legal certification document — weight limits, performance, equipment, AD compliance times, operating limitations. 1 match in the FAA catalog.
- A5EU Current Rev 29 · 08/31/2011
Airbus SAS
Models: BAC 1-11 200 Series, BAC 1-11 400 Series
06 / Supplemental Type Certificates
Modifications approved for BRITISH AIRCRAFT CORP BAC 1-11 419/EP
18 STCs on file — every FAA-approved modification, alteration, or installation for this aircraft. STOL kits, avionics, fuel systems, floats, engine swaps, you name it.
-
03/06/2026
STC SA2622NM
Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)
Precise Flight Inc.
-
03/19/2009
STC SA2289NM-D
Installation of dual Universal Navigation System UNS-1 Flight Management System.
Hollingsead International
-
03/19/2009
STC SA2532NM-D
Installation of Collins Model EFIS 85a, 4 Tube Electronic Flight Instrument System and dual Collins Model FD-109 Flight Director System. (1-11, Series 401AK)
Hollingsead International
-
11/12/2008
STC ST01854SE
Non-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM).
AeroMech Incorporated
-
06/12/2008
STC SA3170NM
Installation of Floor Proximity Emergency Escape Path Marking System
Bruce Aerospace Inc.
-
02/04/2008
STC SA1626WE
ONE-ONLY STC: Installation of auxiliary fuel tanks in the forward and aft cargo compartments for model number 419/EP, serial number 120.
Rogerson ATS
-
04/30/2007
STC SA3819WE
Installation of 1478 gallon auxiliary fuel tank system in the forward and aft cargo compartments. (1-11 SERIES 414/EG)
Rogerson ATS
-
04/30/2007
STC SA1626WE
ONE-ONLY STC: Installation of auxiliary fuel tanks in the forward and aft cargo compartments for model number 419/EP, serial number 120.
Rogerson ATS
-
04/30/2007
STC SA1995WE
Installation of auxiliary fuel tanks in forward and aft cargo compartments. (1-11 SERIES 401/AK, 410/AQ, 419/EP, 412A/EB, 422/EQ, 414EG)
Rogerson ATS
-
12/13/2006
STC ST01723SE
ONE-ONLY: Non-group (individual aircraft) approval for Reduced Vertical Separation Minimum (RVSM), S/N BAC 120. (BAC 1-11 419/EP)
AeroMech Incorporated
-
10/23/2006
STC ST10504SC
Installation of a Honeywell GNS-XLS Enhanced Flight Management System.
West Star Aviation Inc
-
07/31/2006
STC SA2289NM-D
Installation of dual Universal Navigation System UNS-1 Flight Management System.
Hollingsead International
-
07/31/2006
STC SA2532NM-D
Installation of Collins Model EFIS 85a, 4 Tube Electronic Flight Instrument System and dual Collins Model FD-109 Flight Director System. (1-11, Series 401AK)
Hollingsead International
-
04/24/2006
STC ST10504SC
Installation of a Honeywell GNS-XLS Enhanced Flight Management System.
McKinney Aerospace
-
08/29/2005
STC ST10440SC
Installation of a Sandel Class A Terrain Awareness and Warning System.
Aircraft Systems & Mfg
-
11/07/2003
STC SA2622NM
Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)
Precise Flight Inc.
-
04/19/1991
STC SA1626WE
ONE-ONLY STC: Installation of auxiliary fuel tanks in the forward and aft cargo compartments for model number 419/EP, serial number 120.
Rogerson ATS
-
09/17/1971
STC SA2421WE
Installation of 600 gallon extended range fuel tankage in forward freight hold.
Qualitron Inc
07 / PMA replacement parts
FAA-approved replacement parts for BRITISH AIRCRAFT CORP BAC 1-11 419/EP
9 parts on file from the FAA Parts Manufacturer Approval database. Each is a non-OEM part the FAA has authorized for use as a replacement on this aircraft type.
-
Parts as Listed in Dwg 4900#https://drs.faa.gov/browse/excelExternalWindow/F9B8BFC99EE9A10D8625828600522244.0001##
Auxiliary Fuel Tanks
ROGERSON AIRCRAFT EQUIPMENT GROUP replaces Modification, Part
PMA holder → -
CFAK-1#https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161841938520220509143713.0001##
First Aid Kit Assy
Astronics - LSI replaces DME Corporation Model CFAK-1
PMA holder → -
AFAK-1#https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185491784120220509143706.0001##
First Aid Kit Assy
Astronics - LSI replaces DME Corporation Model AFAK-1
PMA holder → -
K5657-0000-00#https://drs.faa.gov/browse/excelExternalWindow/20859677A5A645FA86257CDD00586FBC.0001##
Sandel Avionics Terrain Awareness and Warning System (TAWS) Installation Kit
Aircraft Systems and Manufacturing replaces Modification Part
PMA holder → -
K5657-0000-00#https://drs.faa.gov/browse/excelExternalWindow/87B2F462CFF11411862570C8006E6313.0001##
Sandel Avionics Terrain Awareness and Warning System (TAWS) Installation Kit
Aircraft Systems and Manufacturing replaces Modification Part
PMA holder → -
309623WE#https://drs.faa.gov/browse/excelExternalWindow/DF42F3055ED7F22B862576240072A87A.0001##
Ring-Rear Cover Molded
Wencor LLC replaces 309623
PMA holder → -
NAK27-A315 DRAWING NO. NAK27-A315 SHT 1 OF 1 REV N/C DATED 2/29/77, OR LATER FAA APPROVED REVISION#https://drs.faa.gov/browse/excelExternalWindow/E1E8CAE1E2C36BC68625734C006FDDF3.0001##
CABIN WINDOW OUTER PANEL
Nordam Group Inc, Transparency Division, The replaces BOEINGP/N AK27-A315
PMA holder → -
Parts as Listed in Dwg. 4900#https://drs.faa.gov/browse/excelExternalWindow/A51DB8B49746F260862572AD0056889C.0001##
Auxiliary Fuel Tank
ROGERSON AIRCRAFT EQUIPMENT GROUP replaces Modification Part
PMA holder → -
Parts as Listed in Dwg.: 2500#https://drs.faa.gov/browse/excelExternalWindow/0130775B86A140A8862572AD00568810.0001##
Auxiliary Fuel Tanks
ROGERSON AIRCRAFT EQUIPMENT GROUP replaces Modification Part
PMA holder →
04 / Regulations watching this type
Advisory Circulars and Federal Register activity for BRITISH AIRCRAFT CORP BAC 1-11 419/EP
Advisory Circulars
No ACs explicitly mention this type. Showing universal operating-rule ACs that apply to all aircraft.
Recent Federal Register activity
Latest rulemakings touching general operating rules (Part 91) and maintenance rules (Part 43).
- 2026-04-17 Settlement Policy for Small Unmanned Aircraft System (UAS) Cases FR ↗
- 2026-02-10 Normalizing Unmanned Aircraft Systems Beyond Visual Line of Sight Operations; Reopening of Comment Period; Denial of Extension FR ↗
- 2026-02-02 25-Hour Cockpit Voice Recorder (CVR) Requirement, New Aircraft Production FR ↗
- 2026-01-28 Normalizing Unmanned Aircraft Systems Beyond Visual Line of Sight Operations; Reopening of Comment Period FR ↗
- 2026-01-07 Requirements for Interference-Tolerant Radio Altimeter Systems FR ↗
05 / Aircraft of this type
All 1 registered N-numbers
Every tail currently on the FAA registry for this make/model. Click an N-number to query the FAA Aircraft Inquiry; rows flagged ● have NTSB events on file. Tails seeded with full TallyAero pages link directly.
| N-number | St | Year | NTSB | FAA |
|---|---|---|---|---|
| N999BW | MO | 1967 | ● | Look up ↗ |
Source — FAA Aircraft Registry · click "Look up" to query the live registry record (owner, address, last airworthiness)
05 / Sources & Methodology
Every count traces back to a primary US-government source
- FAA Aircraft Registry →
Refreshed Apr 27, 2026
Available
- NTSB CAROL →
Refreshed Apr 27, 2026
Available
- Federal Register (FAA Airworthiness Directives) →
Refreshed Apr 27, 2026
Available
We render counts and lists as the agency publishes them. Read the methodology →