# N931NU: Xag P150 - Status: Valid registration - Airframe: [Xag P150](https://openairdocs.org/model/xag-p150) (registry code 06102JS) - Serial number: 186324P18223502H15Q8 - Type: Rotorcraft - Engine type: Electric - Certificate issued: April 15, 2026 - Expires: April 30, 2033 - Mode S code: ACEA9F - Registered owner: [Nutrien Ag Solutions Inc](https://openairdocs.org/faa-owner/NUTRIEN%20AG%20SOLUTIONS%20INC) - Location: [Loveland, CO](https://openairdocs.org/faa-place/CO/Loveland) - Owner type: Corporation - Owner's area on the map: 40.5446° N, 105.2451° W: Placed by OpenAirDocs at the center of ZIP code 80538, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=931NU - Page: https://openairdocs.org/aircraft/N931NU From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Xag P150) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N931NU. ## FAA accident and incident reports None matched to N931NU. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N931NU not matched to an aircraft (17) They name N931NU, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR HN6R0000546](https://openairdocs.org/sdr/HN6R0000546), May 16, 2001: FRAME. CRACKED. CRACK INDICATION NOTED AT RS 178 LEFT HAND SIDE CHORD WL 207. REMOVED AND REPLACED LEFT HAND 178 BULKHEAD SIDE CHORD. - [SDR HN6R0000372](https://openairdocs.org/sdr/HN6R0000372), May 16, 2001: SKIN. DEBONDED. DEBOND INDICATION NOTED AT RIGHT WING OUTBOARD AFT FLAP UPPER SURFACE. 46 INCHES FROM INBOARD END. -4 DEGREES FROM TRAINING EDGE APPROX 1.5 INCHES IN DIA. REPAI - [SDR HN6R0000371](https://openairdocs.org/sdr/HN6R0000371), May 16, 2001: SKIN. DEBONDED. DEBOND INDICATION NOTED AT RIGHT WING INBOARD AFT FLAP UPPER SURFACE. 22 INCHES FROM TRAILING EDGE APPROX 2 INCHES IN DIA. REPAIRED SURFACE OF FLAP. - [SDR HN6R0000370](https://openairdocs.org/sdr/HN6R0000370), May 16, 2001: SKIN. DEBONDED. DEBOND INDICATION NOTED: C LEFT WING INBOARD AFT FLAP LOWER SURFACE 11 INCHES FROM INBOARD END 1-6 INCHES FROM TRAILING EDGE APPROX 1.75 INCHES IN DIAMETER. REP - [SDR HN6R0000369](https://openairdocs.org/sdr/HN6R0000369), May 16, 2001: SKIN. DEBONDED. DEBOND INDICATION NOTED AT LEFT WING OUTBOARD AFT FLAP UPPER SURFACE 46 FROM INBOARD END AND 4 INCHES FROM TRAILING EDGE APPROX 1.75 INCHES IN DIA. REPAIRED UPP - [SDR HN6R0000252](https://openairdocs.org/sdr/HN6R0000252), May 16, 2001: SKIN. DELAMINATED. RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE DELAMINATED 92 INCHES FROM INBOARD END. REPAIRED UPPER SURFACE OF FLAP. - [SDR HN6R0000177](https://openairdocs.org/sdr/HN6R0000177), May 16, 2001: FLOORBEAM. CORRODED. CORROSION ON TOP FLANGE OF FLOOR BEAM. BS 328, WL208, RBL 10 FOR RBL 50. REMOVED AND REPLACED SECTION OF TOP FLANGE ER 01-0286. - [SDR HN6R0000172](https://openairdocs.org/sdr/HN6R0000172), May 16, 2001: FLOORBEAM. CORRODED. CORROSION ON TOP AND BOTTOM SIDE OF TOP FLANGE OF FLOOR BEAM. BS 312, WL 208, RBL 45 TO LBL 25. REMOVED , FABRICATED, AND REPLACED 25 T CHORD ON FLOOR BEAM ER 0 - [SDR HN6R0000151](https://openairdocs.org/sdr/HN6R0000151), May 16, 2001: SILL. CORRODED. BS 270 TO 344, WL 208, RBL51 TO 63 MOP SILL CORRODED. REMOVED AND REPLACED MOP SILL. - [SDR HN6R0000450](https://openairdocs.org/sdr/HN6R0000450), May 16, 2001: FRAME. CRACKED. HFEC FOUND CRACK INDICATION AT BS 663.75 STR 2L FORWARD HOLE, UNDER FRAME. - [SDR HN6R0000499](https://openairdocs.org/sdr/HN6R0000499), May 16, 2001: FLOORBEAM. CORRODED. FLOOR SPAR IS CORRODED AT BS 986, WL 208, RBL 43. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. - [SDR HN6R0000456](https://openairdocs.org/sdr/HN6R0000456), May 16, 2001: FRAME. CRACKED. HFEC FOUND CRACK INDICATION AT BS 663.75 STA 2R. FORWARD HOLE UNDER FRAME. CRACK RUNNING FORWARD. - [SDR HB6R0000329](https://openairdocs.org/sdr/HB6R0000329), May 16, 2001: FRAME. CRACKED. HFEC INSP EXHIBITS CRACK IN FRAME INNER CHORD RS 616 LOWEST HOLE APPROX WL 203, LBL 55. F/S 9, BS 616 WL 203, INSTALLED FASTENERS. - [SDR HN6R0000328](https://openairdocs.org/sdr/HN6R0000328), May 16, 2001: FRAME. CRACKED. HFEC INSP EXHIBITS CRACK IN FRAME INNER CHORD BS616 10 WEST HOLE APPROX WL 203 RBL 55. F/S 9 BS 616 WC 203 RBL 55. INSTALLED FASTENERS. - [SDR HN6R0000251](https://openairdocs.org/sdr/HN6R0000251), May 16, 2001: SKIN. DELAMINATED. R/W O/B FORE FLAP UPPER SURFACE DELAMINATED. 9 INCHES FROM THE I/B END.REPAIRED SURFACE OF FLAP. - [SDR HN6R0000150](https://openairdocs.org/sdr/HN6R0000150), May 16, 2001: SILL. CORRODED. BS 940 TO 991, WL 208, LBL 46 TO 51, MOP SILL CORRODED. REMOVED AND REPLACED MOP SILL. - [SDR HN6R0000180](https://openairdocs.org/sdr/HN6R0000180), May 15, 2001: FLOORBEAM. CORRODED. CORROSION ON TOP OF FLOORBEAM. BS 344, WL 208, LBL 65 TO RBL 15. FABRICATED AND REPLACED SECTION OF FLOORBEAM ER 01-0286 ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Xag P150 aircraft: https://openairdocs.org/model/xag-p150/aircraft.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.