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Feb 14, 2015 · The AD1403 and AD1403A are improved three-terminal, low cost, temperature compensated, bandgap voltage referenced that provide a fixed 2.5V output voltage for inputs between 4.5V and 40V. A unique combination of advanced circuit design and laser-wafer-trimmed thin-film resistors provides the AD1403/AD1403A with an initial tolerance of ±10mV ...
Jul 18, 2019 · This AD was posted on 13 May 2019 as PAD 19-083 for consultation until 10 June 2019. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD 3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information ...
- 2019-08-01
- Europe
- 2019-07-18
- 2019-0173
Council Implementing Regulation (EU) 2019-1403 of 12 September 2019 implementing Regulation (EU) No 269-2014 concerning restrictive measures in respect of actions undermining or threatening the territorial integrity, sovereignty and independence of Ukraine
FEATURES. Improved, Lower Cost, Replacements for Standard 1403, 1403A. 3-Terminal Device: Voltage In/Voltage Out. Laser Trimmed to High Accuracy: 2.500 V 6 10 mV (AD1403A) Excellent Temperature Stability: 25 ppm/8C (AD1403A) Low Quiescent Current: 1.5 mA max. 10 mA Current Output Capability. Low Cost.
Compliance for this AD. 2. This AD was posted on 13 May 2019 as PAD 19-083 for consultation until 10 June 2019. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD 3. Enquiries regarding this AD should be referred to the EASA Programming and Continued
- Summary
- Dates
- Addresses
- For Further Information Contact
- Supplementary Information
- List of Subjects in 14 CFR Part 39
- Part 39—Airworthiness Directives
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 737–8 and –9 airplanes. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires revising certificate limitations and operating procedures of the airplane flight manual (AFM) to provide the flight crew with ru...
This AD is effective December 21, 2018 to all persons except those persons to whom it was made immediately effective by Emergency AD 2018–23–51, issued on November 7, 2018, which contained the requirements of this amendment. We must receive comments on this AD by January 22, 2019.
You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. • Fax:202–493–2251. • Mail:U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140...
Douglas Tsuji, Senior Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206–231–3548; email: Douglas.Tsuji@faa.gov.
Discussion
On November 7, 2018, we issued Emergency AD 2018–23–51, which requires revising certificate limitations and operating procedures of the AFM to provide the flight crew with runaway horizontal stabilizer trim procedures to follow under certain conditions. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This action was prompted by analysis performed by the manufacturer showing that if an erroneously high single AOA sensor input is received by the...
FAA's Determination
We are issuing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design.
AD Requirements
This AD requires revising certificate limitations and operating procedures of the AFM to provide the flight crew with runaway horizontal stabilizer trim procedures to follow under certain conditions.
Air transportationAircraftAviation safetyIncorporation by reference1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): 2018–23–51 The Boeing Company:Amendment 39–19512; Docket No. FAA–2018–0960; Product Identifier 2018–NM–151–AD.
AD1403 Datasheet. Part #: AD1403. Datasheet: 80Kb/4P. Manufacturer: Analog Devices. Description: Low Cost, Precision 2.5 V IC References. 5 Results. Datasheet: 84Kb/4P.
