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March 30, 2026 at 9:45 AM
snsproductreview.bsky.social
Safety Razor Holder Stand, Safety Razor Stand for Men, Razor and Shaving Brush Holder Stand, Metal Base for Added Stability and Long-Lasting Use

Price: (as of - Details) Upgradingthe Shaving Ritual: Nfijnlt zinc alloy razor stand combines practical functionwith exquisite design, redefining daily…
Safety Razor Holder Stand, Safety Razor Stand for Men, Razor and Shaving Brush Holder Stand, Metal Base for Added Stability and Long-Lasting Use
Price: (as of - Details) Upgradingthe Shaving Ritual: Nfijnlt zinc alloy razor stand combines practical functionwith exquisite design, redefining daily shaving for the modern gentleman - nolonger a rushed chore, but an “exclusive time” to be enjoyed, making every everymorning is full of ease.Compatiblewith Most Tools: Thoughtfully sized to easily accommodate most shaving tools:brush opening is just over 1 inch, razor opening is about 1/2 inch, compatiblewith 99% of shaving brushes and razors, we recommend you measure your brush andrazor before purchasing.Durableand Detailed: Made of rust-resistant zinc alloy, it is sturdy and durable, andremains beautiful even after long-term use; the weighted non-slip base holdsthe tools securely in place, preventing them from slipping off accidentally,and letting the countertop stop being cluttered; the elevated design alsopromotes air circulation, helping the brushes to dry more quickly andprolonging their lifespan.
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January 31, 2026 at 1:15 PM
epsteinweb.bsky.social
Parts 1-2/2 — EFTA00278240.jpg
#epsteinweb #efta00278240
https://epsteinweb.org
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https://apps.apple.com/us/app/epstein-web/id6758880661
EFTA00278135 | EFTA00278240 NOTICE Weight and balance or operating limitation changes shall be entered m the appropnate aircraft`record. An alteration must be compatibleWith all previous alterations to assure continued conformity with the applicable airworthiness requirements:8. Description of Work Accomplished • (Ifmore spaceis required, attach additional sheets. Identify with aircraft nationality and registration mark and date work complete d) Aircraft: Gulfstream, Type: G-1159, SIN 151, Date: 03119/98, W.O. 12307 Page 1 oft Removed the existing Universal Avionics model UNS-1A FMS systems and Canadian Marconi VLF/Omega sensor, and installed new Universal Avionics UNS-D FMS systems. The existing Universal Radio Ttining Unit, Database Transfer Unit and the Universal Loran C sensor were retained. This installation was accomplished using Jet Aviation drawings, FIVIS98001, FMS98002 and IPB98001, Rev. IR, dated 01/20/98 are substantiated by FAA Forms 8110-3, dated 03/11/98 submitted by FAA D.E.R. Mr. Norman J. Curran, FAA D.E.R. No. SO-780. The structural installation of 'the GPS antennas was accomplished using Jet Aviation Drawing HPA98001, Rev. A, dated 03/02/98 and is _structurally substantiated by FAA Form 8110-3, dated 03/12/98 submitted by Lauren Napier, D.E.R. No. SO-815. -The CDU's replaced the removed units at the same station using the existing DZUZ rails installed by the airframe manufacture. The Navigation Computer Units replaced the existing UNS-1A NCU's using the same mounting technique and hardware. The required annunciators were furnished and installed. The following annunciators were installed: MSG (message) annunciator, color amber WPT (wayoint) annuciator, color amber APPR (approach), color white SX (parallel track), color amber HDG (heading), color blue INTEG (integrity) color amber This system, the Universal Avionics UNS-1D FMS system has been previously installed and 'has obtained a STC approval in another type of aircraft, which qualifies this installation as a follow on installation per AC 20-130A and is qualified for FAA Form 337 Field Approval. • • ''sv- The existing No. 4 airdata computer was interfaced to provide the required airspeed input and barocorrected altitude. The existing Honeywell Laser-ref INS system was interfaced as a blended sensor as well as the existing Loran C sensor. The No. 1 compass system is interfaced to the No. 1 FMS and the No. 2 compass system is interfaced to the No. 2 FMS. c. The above annunciators were installed in each instrument panel for their associated system. The Static Loading of the installed equipment meets the requirements of AC 43.13-2A, Chapter 1, Paragraph 3 and was found to meet the requirements of Paragraph 2. Materials and practices comply with Paragraphs 4 through 12. The Electrical Load Analysis was performed in accordance with 43.13-1A, Chapter 11, Section 2, Paragraph 424 and was found to meet the requirements of paragraph 424, 426 and 428. Aircraft Metal Work involving metal repair or alteration complies with AC 43.13-1A, Chapter 2, Section 1 and 3, Chapter 6, Paragraphs 248 and 249. Hardware and materials used the installation conform to AC 43.13-1A, Chapter 5 and 7, Sections 1, 4 and 5 as applicable. Circuit Breakers, switches and connectors are of the type recommended by the aircraft manufacture or are MIL SPEC approved for aircraft use and meet the requirements of AC 43.13-1A, Chapter 11, Paragraphs 429 and 430. Electrical/electronic wiring was selected and installed lAW AC 43.13-1A, Chapter 11 and AC 43.13-2A Chapter 2, Paragraph 21, 22 & 27. Routing, lacing and tying complies with AC 43.13-1A, Chapter 11, Section 7. Wire marking complies with Section 4. Electronic equipment installation complies with yj Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012160157 EFTA00278240
April 26, 2026 at 2:11 AM