ING 1159WM2005 I REV L STEP: 2 MATCHED DRILLED P/N I I 59WM20051-110 FLAP TRACK B TO ORIGINAL FLAP TRACK B THAT WAS TAKEN OFF PLANE. WORK WAS DONE I.A.W. DWG I 159WM2 0051 REV. L For detailed description of the work complied with see the Work Order Detail report Unless otherwise indicated, all financ

unction Test, reference item SC13300.6.2 Resolution: COMPLIED WITH CMP GIV 213086 Pressure Ground Delta P-Function Test. No defects noted. Work done I.A.W. GIV M. chap. 21.02.00. For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financi

IED WITH CMP CHB 271311 Rudder Actuator and Forward Attach Fitting - Inspection as required. No discrepancies found at this time. All work performed I.A.W. (NIB M.M. 27-03-00 For detail description of the work complied with see the Work Order Detail report. Unless otherwise indicated, all financial val

. ILS Receivers, 2ea. racks, and lea. ILS controller. The ILS system was originally installed at the factory. The ILS system was previously disabled I.A.W. AD 89.02-12 R1 dated March 21, 1994. #1 and #2 ILS circuit breakers were previously removed. Connectors are capped, bagged, and stowed. Removed th

cumented on Pro Star Aviation, DER approved drawing 2649 *GMX 200 MFD MOD WIRING DIAGRAM", Rev. IR dated 04/11/11. Performed post installation test I.A.W. the applicable sections of the post installation test document 20677-PTP-01. Rev. D dated 11/24/08 with no faults noted Removed the existing Sikors

tal Cycles: 2086 DURING ENGINE CHANGE (REF WON15766 DT: Category: AD 737-71A1462-1 26-MAY-2011) SB HANGAR FITTING WAS MARKED Status: TERMINATED I.A.W. SB 737-71A1462 R3 Rev: 3 EARLIEST Reason Frog: 1 REFER THE ENGINE AD STATUS COMMENT E/C: 2011.20-07 737-28Al201 FUEL PUMP CONTROL GROUND FAU