# N170LS: Learjet 45, registration cancelled 2023-08-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 28, 2023
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Learjet 45](https://openairdocs.org/model/learjet-45) (registry code 5170805)
- Data sheets: [TCDS T00008WI](https://openairdocs.org/tcds/T00008WI) (OpenAirDocs)
- Serial number: 029
- Type of aircraft: Fixed wing multi engine
- Certificate issued: July 12, 2023
- Last registry action: July 12, 2023
- Mode S code: A11A38
- Owner when cancelled: [Airtrade Aviation Corp](https://openairdocs.org/faa-owner/AIRTRADE%20AVIATION%20CORP)
- Location: [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes)
- Owner type: Corporation
- Owner's area on the map: 38.7287° N, 75.1685° W: Placed by OpenAirDocs at the center of ZIP code 19958, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N170LS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=170LS
- Page: https://openairdocs.org/deregistered/N170LS-2023-08-28

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Learjet 45: https://openairdocs.org/model/learjet-45.md

## Service difficulty reports (13)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR V6NA2023041001](https://openairdocs.org/sdr/V6NA2023041001), Apr 10, 2023: SKIN SPLICE. CORRODED. AT SCHEDULED INSPECTION, UPON REMOVAL OF LOWER FORWARD WING ACCESS PANEL, DISCOVERED LOWER FORWARD WING SPLICE CORRODED AT F.S 384, B.L. 10L-10R BEYOND ALLOWABL
- [SDR V6NA20201013001](https://openairdocs.org/sdr/V6NA20201013001), Oct 9, 2020: SKIN. CHAFED. AT SCHEDULED INSPECTION DISCOVERED RIGHT WING LEADING EDGE TO HAVE CHAFE DAMAGE, SCUFF MARKS BLENDED OUT. REMAINING MATERIAL THICKNESS DETERMINED TO BE APPROVED
- [SDR V6NA202007286001](https://openairdocs.org/sdr/V6NA202007286001), Jul 26, 2020: WINDSHIELD. CRACKED. SHORTLY AFTER CLIMBING THROUGH 10,000 FEET THE RIGHT WINDSHIELD CRACKED. LEVELED OFF AT 10,800 FEET AND REQUESTED DESCEND TO 10,000 FEET. THE INNER LAYER WAS ST
- [SDR V6NA20190410003](https://openairdocs.org/sdr/V6NA20190410003), Apr 10, 2019: SKIN. CORRODED. AT PAINT POST STRIPPING INSPECTION DETERMINED THE BELOW LISTED AREAS ON SKINS WERE CORRODED. CORROSION REMOVED AND DETERMINED BEYOND MANUFACTURES RECOMMENDATION
- [SDR V6NA201904100002](https://openairdocs.org/sdr/V6NA201904100002), Apr 10, 2019: SKIN. CORRODED. AT PAINT POST STRIPPING INSPECTION DETERMINED THE BELOW LISTED AREAS WERE CORRODED. CORROSION REMOVED AND DETERMINED BEYOND MANUFACTURES RECOMMENDATION.
- [SDR V6NA20190411005](https://openairdocs.org/sdr/V6NA20190411005), Apr 10, 2019: SKIN. CORRODED. AT PAINT POST STRIPPING INSPECTION, DETERMINED RIGHT THRUST REVERSER UPPER SKIN TO BE CORRODED. SKIN REPLACED WITH ONE FABRICATED PER APPROVED DATA IN FAA DER D
- [SDR V6NA20190411003](https://openairdocs.org/sdr/V6NA20190411003), Apr 10, 2019: SKIN. CORRODED. AT POST PAINT INSPECTION, DETERMINED RIGHT THRUST REVERSER LOWER SKIN TO BE CORRODED. SKIN REPLACED WITH ONE FABRICATED PER APPROVED FAA DER DRAWING.
- [SDR V6NA201904100001](https://openairdocs.org/sdr/V6NA201904100001), Apr 10, 2019: FAIRING. CORRODED. AFTER PAINT STRIPPING PROCESS DETERMINED VERTICAL STABILIZER TOP AFT FAIRING TO BE CORRODED. CORROSION WAS REMOVED AND DOUBLER REPAIR INSTALLED PER APPROVED DAT
- [SDR V6NA2018050701](https://openairdocs.org/sdr/V6NA2018050701), May 7, 2018: SKIN. CORRODED. CORROSION WAS DISCOVERED AT THE FOLLOWING LOCATIONS. CORROSION WAS MECHANICALLY CLEANED. CORROSION WAS BEYOND. MANUFACTURE ACCEPTED STRUCTURAL REPAIR MANUAL.
- [SDR V6NA20180214001](https://openairdocs.org/sdr/V6NA20180214001), Feb 14, 2018: ANGLE. CORRODED. WHILE PERFORMING 9600 HOUR INSPECTION DISCOVERED LAND ANGLE AT BS 520 TO BE CORRODED. CORROSION WAS ON AFT SURFACE LOWER POSITION AND DETERMINED TO BE OUT OF LI
- [SDR V6NA20180103002](https://openairdocs.org/sdr/V6NA20180103002), Jan 3, 2018: SKIN. CORRODED. WHILE PERFORMING 9600 HOUR INSPECTION, DETERMINED RIGHT WING OUTBOARD LOWER SKIN UPPER SURFACE TO HAVE CORROSION AT WS 260 AT COVE SURFACE INTERFACE. CORROSION 
- [SDR V6NA20150629001](https://openairdocs.org/sdr/V6NA20150629001), Jun 23, 2015: WINDSHIELD. CRACKED. ENROUTE AT APPROX FL 220 THE RT COCKPIT WINDSCREEN SHATTERED, ACCOMPANIED WITH A LOUD BANG NOISE. WE ADVISED ATC THAT WE NEEDED TO DIVERT & REQUESTED A LOWER AL
- [SDR EXO2006F00000](https://openairdocs.org/sdr/EXO2006F00000), May 17, 2006: ADC. FAILED. 30 MIN INTO FLIGHT, AC EXP MULTIPLE FAILURES, WITH LOSS OF NR 1 ADC, LOSS OF CABIN PRESS WITH CABIN EXCEEDING 10,000 BUT NO MORE THAN 11,000 FT, CABIN O2 MASKS 

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