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ATA 52 Information Group EASA 2022-0090 Date 18-05-2022
Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism –
Inspection
Applicability : A321 aero planes
Affected Part : Doors – Airbus Cabin Flex / Over wing Emergency Exit Slide
Back Ground :
During an emergency slide deployment test on an A321NEO Airbus Cabin Flex (ACF) over wing
emergency exit, the slide did not deploy. Investigation identified that the slide release mechanism cable
junction was disconnected inside the surrounding collets and knurled sleeve nut.
The mushroom head connector was not inserted into the T-slot cable joint. This condition, if not
detected and corrected, could prevent emergency slide deployment, possibly resulting in injury to
occupants during an emergency evacuation.
ATA 52 Information Group EASA 2022-0090 Date 18-05-2022
Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism –
Inspection
To address this potential unsafe condition, Airbus issued the AOT, providing instructions to inspect
the slide release mechanism cable lock wire and junction and the associated corrective actions.
For the reasons described above, this AD requires a one-time detailed inspection (DET) of the
installation of the ACF over wing emergency exit slide release mechanism on both left-hand (LH)
and right-hand (RH) sides of the fuselage.
Applicability:
For all A321 aero planes, within 4 months after 01 June 2022, accomplish a DET of the slide
release mechanism cable lock wire and junction of each ACF over wing emergency exit, on both
LH and RH sides, in accordance with the instructions of the AOT.
ATA 52 Information Group EASA 2022-0090 Date 18-05-2022
Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism –
Inspection
Objective/Action:
During the DET, if any discrepancies are detected, as defined in the AOT, accomplish the applicable
corrective action(s) within the compliance time as defined in, and in accordance with the
instructions of, the AOT.
Ref. Publications: Airbus AOT A52N014-22 original issue dated 21 March 2022, or Revision 01 dated 19
April 2022.

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EASA 2022-0090.pptx

  • 1. ATA 52 Information Group EASA 2022-0090 Date 18-05-2022 Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism – Inspection Applicability : A321 aero planes Affected Part : Doors – Airbus Cabin Flex / Over wing Emergency Exit Slide Back Ground : During an emergency slide deployment test on an A321NEO Airbus Cabin Flex (ACF) over wing emergency exit, the slide did not deploy. Investigation identified that the slide release mechanism cable junction was disconnected inside the surrounding collets and knurled sleeve nut. The mushroom head connector was not inserted into the T-slot cable joint. This condition, if not detected and corrected, could prevent emergency slide deployment, possibly resulting in injury to occupants during an emergency evacuation.
  • 2. ATA 52 Information Group EASA 2022-0090 Date 18-05-2022 Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism – Inspection To address this potential unsafe condition, Airbus issued the AOT, providing instructions to inspect the slide release mechanism cable lock wire and junction and the associated corrective actions. For the reasons described above, this AD requires a one-time detailed inspection (DET) of the installation of the ACF over wing emergency exit slide release mechanism on both left-hand (LH) and right-hand (RH) sides of the fuselage. Applicability: For all A321 aero planes, within 4 months after 01 June 2022, accomplish a DET of the slide release mechanism cable lock wire and junction of each ACF over wing emergency exit, on both LH and RH sides, in accordance with the instructions of the AOT.
  • 3. ATA 52 Information Group EASA 2022-0090 Date 18-05-2022 Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism – Inspection Objective/Action: During the DET, if any discrepancies are detected, as defined in the AOT, accomplish the applicable corrective action(s) within the compliance time as defined in, and in accordance with the instructions of, the AOT. Ref. Publications: Airbus AOT A52N014-22 original issue dated 21 March 2022, or Revision 01 dated 19 April 2022.