Epstein Secrets

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

2 $1.69 $338 832#4 NASII49D0163K WASHER 2 50.23 $0.46 832#5 202-16126-41 NUT, SELF LOCKING 2 $23.62 $47.24 832 #6 MS24665-153 PIN, COTTER 2 $0.22 $0.44 832 #7 MS24665-86 COTTER PIN 6 $0.23 $138 Discrepancy: 833 FUI I #5 Flap pillow block assembly is worn and making a loud gri

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

R 2 $1.69 $338 832#4 NASI149D0463K WASHER 2 $0.23 $0.46 832#5 202-16I26-4L NUT, SELF LOCKING 2 $23.62 $47.24 832#6 NIS24665-153 PIN, COTTER 2 $0.22 S0.44 832 #7 MS24665-86 COTTER PIN 6 $0.23 5138 Discrepancy: 833 R/I1 #5 Flap pillow block assembly is worn and making a loud grin

'. Doc. Apvd: Discrepancy: GIV_240160_EMERGENCY POWER SYSTEM - OPERATIONAL CHECK Resolution: COMPLIED

ARING, FLAP, TRACK ROLLER, 1 IN DIA 1.000 $788.64 $788.64 MS17826-5 NUT, SLF LKG,HEX,THD: 5/16-24, CDPS 6.000 $2.98 $17.88 MS24665-I55 PIN, COTTER 6.000 $0.60 $3.60 NAS1580C3T10 BOLT,SHEAR,100 DEG FL HEAD,OFS CRUC,DVTL 10.000 $2.87 $28.70 NAS1580C3T10 BOLT,SHEAR,100 DEG FL HEAD,OFS CRU

f. Doc. Apvd: Discrepancy: GIV_240160_EMERGENCY POWER SYSTEM - OPERATIONAL CHECK Resolution: COMPLIED

ARING, FLAP, TRACK ROLLER, 1 IN DIA 1.000 3788.64 $788.64 MS17826-5 NUT, SLF LKG,HEX,THD: 5/16-24, CDPS 6.000 $2.98 $17.88 MS24665-I55 PIN, COTTER 6.000 $0.60 $3.60 NAS1580C3T10 BOLT,SHEAR,100 DEG FL HEAD,OFS CRUC,DVTL 10.000 $2.87 $28.70 NAS1580C3T10 BOLT,SHEAR,100 DEG FL HEAD,OFS CRU

Prepare the Airplane for the Installation of the Power Plant, as per AMM Task 71-00-02-400-801-F00, Par

move the nut [3]. NOTE: You can use the thread protector, a metal or hard plastic tube, or another nut to hold the pawl in. ii) PAWL PINS WITH A COTTER PIN; Remove the cotter pin before you remove the nut (3). C. Remove the pawl pin (5] and washer [4] from the forward end of thrust link. OwDleWnD

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

ervice Information Report Date: 05-Aug-2014 Task No. Description Unit Interval Compliance Next Due Disposition MOC SL 737-SL-32-094 REV. 8 COTTER PINS MISSING FROM RUDDER PEDAL STEERING INTERCONNECT MECHANISM, SERVICE LETTER I6-AUG-2000 MOS - Is) St 737-SL-32-095 PROXIMITY SENSOR 10-61226