As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*LH ENGINE AFT BLEED LOOP ON TOP OF ENGINE FORWARD OF EXHAUST FRAME HAS CLAMP CUSHION TORN (MARKED) C (C-CHECK) RO:1/29/2020REMOVED AND INSTALLED A NEW CLAMP TO L/H ENGINE AFT BLEED LOOP ON TOP OF THE ENGINE FORWARD OF EXHAUST FRAME REF CRJ200 SRM.