Epstein Secrets

00 Discrepancy: 40.56 CMP 6550 491301 Auxiliary Power Unit Turbine Plenum Drains - Operational Test Fo

r 7 days at room temperature, or 2-3 hours at room temperature followed by 2 hours at 130-140°F. Step: 29.2.2 Completed REMOVED PAINT/PRIMER FROM DISCREPANT FWD AREAS AND SOLVENT CLEANED. THEN FABRICATED AND INSTALLED 2 PLIES OF STYLE 181 FIBERGLASS WET USING EPON 828fDTA. VACUUM BAGGED AND CURED. REF

e IF frequencies to Ka-band frequencies. A High- Power Amplifier (IIPA) increases the signal strength fo

r 7 days at room temperature, or 2-3 hours at room temperature followed by 2 hours at 130-140°F. Step: 29.2.2 Completed REMOVED PAINT/PRIMER FROM DISCREPANT FWD AREAS AND SOLVENT CLEANED. THEN FABRICATED AND INSTALLED 2 PLIES OF STYLE 181 FIBERGLASS WET USING EPON 828fDTA. VACUUM BAGGED AND CURED. REF

IEST Freq: 1 E/C: 737-24A1150 B3-24A1150 INSP POWER SUPPLY VOLTAGE : CPT'S Manual Compliance 16/04/

3/2002, DELIVERY DOCUMENTS. REFER A6-DFR ESC: 737-27A1260 2002-19-51 FLIGHT CONTROLS HYDRAULIC MODULAR Cat egory: ASB PACKAGE - REPLACEMENT OF DISCREPANT COMPENSATORS Status: N/A Rev: 3 EARLIEST Reason Freq: 1 NOT AFFECTED BY SERIAL NUMBERS OF FLIGHT CONTROL MODULE. REFER LHT AD STATUS AT DELIV

ASTER CHANGE MOS MC 737-24-1196 RI ELECTRICAL POWER- STANDBY POWER SYSTEM - CHANGE THE ELECTRICAL POW

FT SIDE ELEVATOR TAB CONTROL MECHANISM AND DO DETAILED INSPECTION BEFORE AND AFTER INSTALLING IT ( IF ELEVATOR TAB CONTROL MECHANISM IS FOUND TO BE DISCREPANT OR REPLACEMENT ELEVATOR TAB CONTROL MECHANISM IS FOUND TO BE DISCREPANT) MOS BF(F SB 737-27A1297 RI DETAILED INSPECTION FLIGHT CONTROLS - ELEVA

MATIONAL SL 737-SL-33-049 ANTI-COLLISION LIGHT POWER SUPPLY BRACKET - FILLET SEAL APPLICATION (SUPERSE

-3. AND SPRING RETAINER. PN 3827074-4. SERVICE BULLETIN MOS MSC SB 49-8079 APU - AIRBORNE AUXILIARY POWER - GAS TURBINE ENGINE - REPLACEMENT OF DISCREPANT DATA MEMORY RECOMMENDED MODULE (DMM). PN 3876287-1. SERVICE BULLETIN MOS 20-JUN-2012 MSC SB 49-8079 RI APU - AIRBORNE AUXILIARY POWER- GAS TU