Airworthiness directives › 2025-09-04
AD 2025-09-04 Airworthiness Directives; Bombardier Inc. Airplanes
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 (S/Ns) 9002 through 9879 inclusive, 9998, and 60001 through 60065 inclusive.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 60 days after the effective date of this AD, revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in the tasks identified in table 1 to paragraph (g) of this AD, of Part 2, “Airworthiness Limitations,” of the applicable time limits/maintenance checks (TLMC) manual identified in table 2 of this AD. The initial compliance time for doing the tasks is at the time specified in the applicable TLMC manual identified in table 2 to paragraph (g) of this AD, or within 60 days after the effective date of this AD, whichever occurs later, except as provided by paragraph (h) of this AD. Table 1 to Paragraph ( g )—New or Revised Tasks Applicable airplane model (marketing designation) Chapter 5 task No. Task title Affected section All airplanes 27-41-09-107 Restoration of the Pitch Trim Actuator, Part No. GT412-4001-7 5-10-20, “Time Limits—Supplementary Limitations”. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-11-17-106 Discard the Main Landing Gear (MLG) Side-Stay Upper-Pin, Part No. GM227-1725 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes 32-21-01-101 Discard the Nose Landing Gear (NLG) Shock Strut Axle, Part No. 1286-0201/-0203/-0204 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-21-01-103 Discard the Nose Landing Gear (NLG) Shock Strut Main Fitting, Part No. 1286-0101/-0109 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-21-01-107 Discard the Nose Landing Gear (NLG) Shock Strut Retraction Actuator Bolt, Part No. 1285-0007/-0041 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-21-01-108 Discard the Nose Landing Gear (NLG) Shock Strut Steering Actuator Bolt, Part No. 1285-0010 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-21-05-107 Discard the Nose Landing Gear (NLG) Drag Brace Forward Stabilizer Link, Part No. 22580 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-21-05-108 Discard the Nose Landing Gear (NLG) Drag Brace Aft Stabilizer Link, Part No. 22585 5-10-10, “Life Limits (Structures),” or 5-10-90, “Life Limits (Structures),” as applicable. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-32-01-105 Discard the Main Landing Gear (MLG) Retraction Actuator Assembly, Part No. 21600 5-10-90, “Life Limits (Structures)”. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-32-05-107 Discard the Main Landing Gear (MLG) Uplock Assembly, Part No. 21900 5-10-90, “Life Limits (Structures)”. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-33-01-105 Discard the Nose Landing Gear (NLG) Retraction Actuator Assembly, Part No. 22400-101/-103 5-10-90, “Life Limits (Structures)”. Model BD-700-1A10 (Global Express and Global Express XRS) airplanes 32-33-01-111 Restoration of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (Post SB 700-32-035 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A10 (Global 6000) airplanes 32-33-01-111 Restoration of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (A/C 9640 and Subs or A/C Post SB 700-32-6011 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-33-01-111 Restoration of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A11 (Global 5000) airplanes 32-33-01-111 Restoration of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (Post SB 700-1A11-32-022 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A11 (Global 5000 featuring Global Vision Flight Deck (GVFD)) airplanes 32-33-01-111 Restoration of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (A/C 9639 and Subs or A/C Post SB 700-32-5011 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. All airplanes except Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-33-05-106 Discard the Nose Landing Gear (NLG) Uplock Assembly, Part No. 22600-101/-103 5-10-90, “Life Limits (Structures)”. Model BD-700-1A10 (Global Express and Global Express XRS) airplanes 32-33-01-112 Detailed Inspection of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (Post SB 700-32-035 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A10 (Global 6000) airplanes 32-33-01-112 Detailed Inspection of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (A/C 9640 and Subs or A/C Post SB 700-32-6011 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A10 (Global 6500) airplanes and Model BD-700-1A11 (Global 5500) airplanes 32-33-01-112 Detailed Inspection of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A11 (Global 5000) airplanes 32-33-01-112 Detailed Inspection of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (Post SB 700-1A11-32-022 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A11 (Global 5000 featuring GVFD) airplanes 32-33-01-112 Detailed Inspection of the Nose Landing Gear (NLG) Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint (A/C 9639 and Subs or A/C Post SB 700-32-5011 Part C) 5-10-20, “Time Limits—Supplementary Limitations”. Model BD-700-1A10 (Global Express, Global Express XRS, Global 6000, and Global 6500) airplanes 53-20-00-122 Detailed Inspection of the Machined Fittings and Skin Around the Service Door, FS295.00 to FS310.00 and STR22R to STR24R 5-10-30, “Airworthiness Limitation Items”. All Model BD-700-1A11 (Global 5000, Global 5500, and Global 5000 featuring GVFD) airplanes 53-20-00-122 Detailed Inspection of the Machined Fittings and Skin Around the Service Door, FS295.00+32.00 to FS310.00+32.00 and STR22R to STR24R 5-10-30, “Airworthiness Limitation Items”. Model BD-700-1A10 (Global Express, Global Express XRS, Global 6000, and Global 6500) airplanes 53-20-00-140 Detailed Inspection of the External Skin Around the Service Door Cutout, FS295.00 to FS310.00 and STR22R to STR24R 5-10-50, “High Altitude Special Conditions Requirements”. Model BD-700-1A11 (Global 5000, Global 5500, and Global 5000 featuring GVFD) airplanes 53-20-00-140 Detailed Inspection of the External Skin Around the Service Door Cutout, FS295.00+32.00 to FS310.00+32.00 and STR22R to STR24R 5-10-50, “High Altitude Special Conditions Requirements”. Table 2 to Paragraph ( g )—Applicable TLMC Manual Airplane model (marketing designation) Title Revision Date Model BD-700-1A10 (Global Express) Bombardier Global Express TLMC, Publication No. BD-700 TLMC 1 35 December 19, 2023. Model BD-700-1A10 (Global Express XRS) Bombardier Global Express XRS TLMC, Publication No. BD-700 XRS TLMC 2 22 December 19, 2023. Model BD-700-1A10 (Global 6000) Bombardier Global 6000 TLMC, Publication No. GL 6000 TLMC 16 December 19, 2023. Model BD-700-1A10 (Global 6500) Bombardier Global 6500 TLMC, Publication No. GL 6500 TLMC 5 December 19, 2023. Model BD-700-1A11 (Global 5000) Bombardier Global 5000 TLMC, Publication No. BD-700 TLMC 3 26 December 19, 2023. Model BD-700-1A11 (Global 5500) Bombardier Global 5500 TLMC, Publication No. GL 5500 TLMC 5 December 19, 2023. Model BD-700-1A11 (Global 5000 featuring GVFD) Bombardier Global 5000 Featuring Global Vision Flight Deck TLMC, Publication No. GL 5000 GVFD TLMC 16 December 19, 2023. 1 For obtaining the tasks specified in Bombardier Global Express TLMC, Publication No. BD-700 TLMC, use Document Identification No. GL 700 TLMC. 2 For obtaining the tasks specified in Bombardier Global Express XRS TLMC, Publication No. BD-700 XRS TLMC, use Document Identification No. GL XRS TLMC. 3 For obtaining the tasks specified in Bombardier Global 5000 TLMC, Publication No. BD-700 TLMC, use Document Identification No. GL 5000 TLMC.
Unsafe condition
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address new or more restrictive airworthiness limitations. Failure to adhere to the specified airworthiness limitations could adversely affect the stability and controllability of the airplane on landing and could result in damage to the airplane.
Affected ADs
None.
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1