What was found
AIR BLEED MSG - DUE TO HISTORY OF AIR BLEED MSG, AVIATAR IS SHOWING L WING LOOP A 36-22-16 DURING CRUISE FLT DO THE FAULT ISOLATION PER TSM 36-22-00-810-825-A TO CHK L-WING LOOP A FOR DISCREPANCIES. VERIFY NO BLEED LEAKS ARE PRESENT. CHK LOOP RESISTANCE AND IMPEDANCE READINGS ARE WITHIN LIMITS. THE CWR SHOULD BE 15-25 OHMS REF AMM 36-22-00-760-803-A. LOOP IMPEDA NCE SHOULD BE >10K OHMS AMM 36-22-00-760-804-A. CORRECT DISCREPA NCIES FOUND. REPORT ALL FINDINGS, SFOLM LEE 650-874-5101.CARRIED BY ELB PER TSM TASK 36-22-00-810-825-A. BMC 1 BITE TEST OK, WILL NEED TO OPEN ACCESS PANELS TO PERFORM DUCT LK INSPECTION REF AMM 36-11-00-720-809. PROFORMED LEAK CHECK FOUND LEAK AT DUCT NR 2 & 28 CONNATION IAW AMM 30-11-42. ALSO REMOVE ANTI-ICE VALVE AND DUCT NR 2 TO INSPECT FOR DAMAGE AND WEAR. REPLACED WORN SEALS INSIDE DUCTS 2, 28, AND 78 IAW AMM 30-11-42/401 CONFIG 00 ILLUSTRATIONS. TORQUED CLAMP 44 INSULATION SLEEVE STILL NEEDS TO BE INSTALLED OVER CLAMP ALL WORK REF AMM 30-11-42. TESTED OVER HEAT LOOPS FROM BMC 1 FOR LEFT WING, CHANNEL A, NO FAULTS FOUND REF TSM 36-22-00-810-807-A AND WDM 36-22-01. REINSTALLED DUCT #2 IAW TASK 30-11-42-400-001-A UP TO AND INCLUDING PARA 4 STEP 13. ANTI ICE CONTROL VALL CBS HAVE BEEN CLOSED AND OPPS CHECKS AND LEAK CHECK GOOD REF AMM TASK 30-11-42-400-001-A PARAGRAPH C TO AND THUR SUBTASK 30-11-42-410-050-A PARAGRAPH A COMPLETED.