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FAA orders · airworthiness directive · historical

2019-12-09: Navigation

FAA order 2019-12-09 is an airworthiness directive in force since July 23, 2019. The FAA's subject line: Navigation. It names Beechcraft B200 King Air B200, Beechcraft B300 King Air 350, Beechcraft C90 King Air C90, Bombardier CL-600 Challenger and CRJ, Cessna 525 CitationJet (CJ series): about 5,734 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: instruments and avionics.

What it applies to as the FAA lists it

Kind of product
Appliance
Makes
Bombardier Inc.; Rockwell Collins, Inc.; Textron Aviation Inc.
Models
CL-600-2B16 (CL-604), Flight Display System Application FDSA-6500, 525B, B200, B200C, B200C (C-12F), B200C (C-12R), B200C (UC-12F), B200C (UC-12M), B200CGT, B200GT, B300, B300C, B300C (MC-12W), B300C (UC-12W), C90GTi
On this site
Beechcraft B200 King Air B200 718 registered
Beechcraft B300 King Air 350 784 registered
Beechcraft C90 King Air C90 607 registered
Bombardier CL-600 Challenger and CRJ 1,657 registered
Cessna 525 CitationJet (CJ series) 1,968 registered

Dates and paperwork

In force since
July 23, 2019
Published
July 8, 2019 (signed June 28, 2019)
Docket
FAA-2019-0469
Replaced by
2021-05-17
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain part-numbered Rockwell Collins, Inc. (Rockwell Collins) FDSA- 6500 flight display system applications installed on airplanes. This AD imposes operating limitations on the traffic collision avoidance system (TCAS) by revising the Limitations section of the airplane flight manual (AFM) or AFM supplement (AFMS) and installing a placard on each aircraft primary flight display. This AD was prompted by a conflict between the TCAS display indications and aural alerts that may occur during a resolution advisory (RA) scenario. The FAA is issuing this AD to require actions that address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (5,246 characters)
Adoption of the Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): \n\n2019-12-09 Rockwell Collins, Inc.: Amendment 39-19664 ; Docket No. FAA-2019-0469 Product Identifier 2019-CE-028-AD. \n\n(a) Effective Date \n\n\n\tThis AD is effective July 23, 2019. \n\n(b) Affected ADs \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to Rockwell Collins, Inc. (Rockwell Collins) Flight Display System Application FDSA-6500 part numbers 810-0234- 1H0001, 810-0234-1H0002, 810-0234-1H0003, 810-0234-2H0001, 810-0234- 2C0001, 810-0234-2C0002, and 810-0234-4B0001. These appliances are installed on, but not limited to, Bombardier Inc. Model CL-600-2B16 (604 variant) airplanes and Textron Aviation Inc. Models 525B, B200, B200C, B200CGT, B200GT, B300, B300C, and \n\n((Page 32262)) \n\nC90GTi airplanes, certificated in any category. \n\n\n\tNote 1 to paragraph (c) of this AD: Rockwell Collins Operator Bulletin OPSB 0193-19R1, Revision 1, dated April 3, 2019, contains additional information related to the Applicability of this AD. \n\n\n\t(d) Subject \n\n\n\tJoint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 34; Navigation. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by a conflict between the traffic collision avoidance system (TCAS) primary display indications and aural alerts during a resolution advisory (RA) scenario. The FAA is issuing this AD to prevent conflicting TCAS information. The unsafe condition, if not addressed, could result in the pilot under-correcting or over- correcting and may lead to inadequate aircraft separation and a mid- air collision. \n\n(f) ComplianceComply with this AD within 30 days after July 23, 2019 (the effective date of this AD), unless already done. \n\n(g) Operating Limitations \n\n\n\t(1) Revise the airplane flight manual (AFM) or AFM supplement (AFMS) by adding the following text to the Limitations section: For TCAS II installations, during flight, do not operate TCAS in the ''TA/RA'' mode; TCAS may only be operated in ''TA Only'' mode. \n\n\n\tNote 2 to paragraphs (g) and (h) of this AD: In ''TA/RA'' mode, the TA stands for traffic advisory and RA stands for resolution advisory. \n\n\n\t(2) Fabricate a placard for each aircraft primary flight display, using at least \1/8\ inch letters, with the following text: TCAS Flight Ops--TA Only mode (TA/RA mode prohibited). \n\t(3) Install the placard on the bottom of each aircraft primary flight display bezel in the area depicted in figure 1 to paragraph (g)(3) of this AD. (GRAPHIC) (TIFF OMITTED) TR08JY19.001 \n\n\n\t(4) In addition to the provisions of 14 CFR 43.3 and 43.7, the actions required by paragraph (g)(1) through (3) of this AD may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417. This authority is not applicable to aircraft being operated under 14 CFR part 119. \n\n(h) Special Flight Permit \n\n\n\tA special flight permit may be issued with the following limitation: Flight operation with the TCAS II in ''TA/RA'' mode is prohibited. Flight operation with the TCAS is only permitted in ''TA Only'' mode. \n\n(i) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The Manager, Wichita ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (j). \n\t(2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. \n\n(j) Related Information \n\n\n\t(1) For more information about this AD, contact Nhien Hoang, Aerospace Engineer, Wichita ACO Branch, FAA, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4157; fax: (316) 946-4107; email: nhien.hoang@faa.gov or Wichita-COS@faa.gov. \n\t(2) Rockwell Collins Operator Bulletin OPSB 0193-19R1, Revision 1, dated April 3, 2019, contains additional information related to this AD. You may obtain copies of this service information by contacting Rockwell Collins, Inc. at Collins Aviation Services, 400 Collins Road NE, M/S 164-100, Cedar Rapids, IA 52498-0001; telephone: 888-265-5467 (U.S.) or 319-265-5467; fax: 319-295-4941 (outside U.S.); email: techmanuals@rockwellcollins.com; internet: http://www.rockwellcollins.com/Services_and_Support/Publications.aspx. \n\n\n\n((Page 32263))

Related safety bulletins advice on the same designs, not orders

2021-09-16AIR-21-15R1 · Navigation System
2021-08-26AIR-21-15 · Navigation System
2020-03-18NM-20-03 · Landing Gear: Brake Control Valve
2019-02-19NE-19-03 · Escape Slide Maintenance Tasks and Intervals - JASC 2565
2015-04-20CE-15-15 · Empennage Horizontal & Vertical Stabilizer Structure

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2019-12-09.json · aircraft systems.