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Airworthiness directives › 2025-12-01

AD 2025-12-01 Airworthiness Directives; Bombardier Inc. Airplanes

2025-07-17
2025-06-12
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Airframe
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Models named: BD-700-1A10, BD-700-1A11. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Bombardier Inc. Model BD-700-1A10 and BD-700-1A11 airplanes, certificated in any category, having serial numbers 9002 through 60086 inclusive, 60088 through 60091 inclusive, 60098, 60100, 60105, 60107, and 60111.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within 30 days after the effective date of this AD, revise the existing AFM to incorporate the information in the applicable sections of the applicable AFMs identified in table 1 to paragraph (g) of this AD. Table 1 to Paragraph ( g )—AFM References Bombardier airplane model (marketing designation) AFM AFM section AFM supplement, if applicable AFM revision and issue date BD-700-1A10 (Global Express) Bombardier Global Express AFM, Publication No. CSP 700-1  1 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures Jammed or Inoperative Slat/Flap Control Lever procedure and Slat-Flap Fail procedure, Landing Distance Factors subsection of Non-Normal Procedures section of Chapter 7—Supplement 20—Operations at Airport Elevations Above 10,000 Feet Revision 119, dated May 22, 2024. BD-700-1A10 (Global Express XRS) Bombardier Global Express AFM, Publication No. CSP 700-1A  2 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures Jammed or Inoperative Slat/Flap Control Lever procedure and Slat-Flap Fail procedure, Landing Distance Factors subsection of Non-Normal Procedures section of Chapter 7—Supplement 20—Operations at Airport Elevations Above 10,000 Feet Revision 119, dated May 22, 2024. BD-700-1A10 (Global 6000) Bombardier Global 6000 AFM, Publication No. CSP 700-1V  3 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures Jammed or Inoperative Slat/Flap Control Lever procedure and Slat-Flap Fail procedure, Landing Distance Factors subsection of Non-Normal Procedures section of Chapter 7—Supplement 20—Operations at Airport Elevations Above 10,000 Feet Revision 49, dated May 22, 2024. BD-700-1A10 (Global 6500) Bombardier Global 6500 AFM, Publication No. CSP-700-6500-1  4 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures None Revision 21, dated May 22, 2024. BD-700-1A11 (Global 5000) Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1  5 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures Jammed or Inoperative Slat/Flap Control Lever procedure and Slat-Flap Fail procedure, Landing Distance Factors subsection of Non-Normal Procedures section of Chapter 7—Supplement 20—Operations at Airport Elevations Above 10,000 Feet Revision 80, dated May 22, 2024. BD-700-1A11 (Global 5000 Featuring Global Vision Flight Deck) Bombardier Global 5000 Featuring Global Vision Flight Deck AFM, Publication No. CSP 700-5000-1V  6 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures Jammed or Inoperative Slat/Flap Control Lever procedure and Slat-Flap Fail procedure, Landing Distance Factors subsection of Non-Normal Procedures section of Chapter 7—Supplement 20—Operations at Airport Elevations Above 10,000 Feet Revision 49, dated May 22, 2024. BD-700-1A11 (Global 5500) Bombardier Global 5500 AFM, Publication No. CSP 700-5500-1  7 Jammed or Inoperative Slat/Flap Control Lever Procedure and Slat-Flap Fail (Caution) procedure, Slat and Flap Control Systems subsection, Section 05-10 Flight Controls, of Chapter 5—Non-Normal Procedures None Revision 21, dated May 22, 2024. 1  For obtaining the procedures for Bombardier Global Express AFM, Publication No. CSP 700-1, use Document Identification No. GL 700 AFM-1. 2  For obtaining the procedures for Bombardier Global Express AFM, Publication No. CSP 700-1A, use Document Identification No. GL 700 AFM-1A. 3  For obtaining the procedures for Bombardier Global 6000 AFM, Publication No. CSP 700-1V, use Document Identification No. GL 6000 AFM. 4  For obtaining the procedures for Bombardier Global 6500 AFM, Publication No. CSP 700-6500-1, use Document Identification No. GL 6500 AFM. 5  For obtaining the procedures for Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1, use Document Identification No. GL 5000 AFM. 6  For obtaining the procedures for Bombardier Global 5000 Featuring Global Vision Flight Deck AFM, Publication No. CSP 700-5000-1V, use Document Identification No. GL 5000 GVFD AFM. 7  For obtaining the procedures for Bombardier Global 5500 AFM, Publication No. CSP 700-5500-1, use Document Identification No. GL 5500 AFM.

Unsafe condition

This AD was prompted by a report that incorrect information was found in certain calculation tables in a section of the airplane flight manual (AFM) that addresses certain slat-flap conditions. The FAA is issuing this AD to address incorrect speed adders and landing distance factors in AFM tables. The unsafe condition, if not addressed, could lead to increased workload for the flightcrew, possible stick shaker activation (stall warning) due to a need to increase speed beyond the published AFM speed adder, and increased landing distance beyond published non-normal landing distance factors.

Affected ADs

None.

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