# N389UA: Xag P100 PRO - Status: Valid registration - Airframe: [Xag P100 PRO](https://openairdocs.org/model/xag-p100-pro) (registry code 06102FP) - Serial number: 8219423CA089 - Type: Rotorcraft - Engine type: Electric - Certificate issued: April 14, 2025 - Expires: April 30, 2032 - Mode S code: A47E7C - Registered owner: [Airstrike Ag LLC](https://openairdocs.org/faa-owner/AIRSTRIKE%20AG%20LLC) - Location: [Barnum, IA](https://openairdocs.org/faa-place/IA/Barnum) - Owner type: LLC - Owner's area on the map: 42.5121° N, 94.3824° W: Placed by OpenAirDocs at the center of ZIP code 50518, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=389UA - Page: https://openairdocs.org/aircraft/N389UA 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 P100 PRO) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N389UA. ## FAA accident and incident reports None matched to N389UA. ## 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 N389UA not matched to an aircraft (15) They name N389UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2006FA0000240](https://openairdocs.org/sdr/2006FA0000240), Feb 8, 2006: SLIDE. OUT OF ALIGNMENT. THE ESCAPE SLIDE FOR DOOR R-2 WAS DEPLOYED FOR A SAMPLE INSPECTION. THE SLIDE DID NOT DEPLOY CORRECTLY, THE SLIDE INFLATED TO THE FULL LENGTH, STRAIGHT OUT FROM - [SDR 2004UALA00219](https://openairdocs.org/sdr/2004UALA00219), Mar 9, 2004: SKIN. DAMAGED. RIGHT HORIZONTAL L/E HAS A TEMPORARY REPAIR 82 INCHES FROM I/B END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2004UALA00194](https://openairdocs.org/sdr/2004UALA00194), Mar 4, 2004: SUPPORT FITTING. CRACKED. LEFT MLG BEAM SUPPORT FITTING AFT SIDE 2 CRACK INDICATIONS AT HOLE C-AREA ON E AT 9 O`CLOCK POS UNDER WASHER RUNNING RADIALLY AT HOLE EDGE. ONE CRACK AT 12 O`CL - [SDR 2004UALA00169](https://openairdocs.org/sdr/2004UALA00169), Feb 25, 2004: SKIN. DENTED. LEFT FUSELAGE SKIN HAS 3 EA SMALL DENTS BETWEEN STA 1010 AND 1016 AND STR 12L &13L. MAJOR REPAIR ACCOMPLISHED. REPLACED FUSELAGE SKIN. - [SDR 2004UALA00165](https://openairdocs.org/sdr/2004UALA00165), Feb 24, 2004: FLOORBEAM. CORRODED. STA 947 RBL 45.5 FLOORBEAM UPPER CAP HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND REPAIR ANGLE. - [SDR 2001UALA00772](https://openairdocs.org/sdr/2001UALA00772), May 18, 2001: LANDING GEAR. MALFUNCTIONED. GEAR WOULD NOT RETRACT AFTER TAKEOFF. *S/D* MAINTENANCE ACCOMPLISHED MAIN LANDING GEAR OPERATIONAL CHECK PER THE MAINTENANCE MANUAL. ACCOMPLISHED INSPECTION OF - [SDR 2000UALA00267](https://openairdocs.org/sdr/2000UALA00267), May 17, 2000: BLADE. BIRD STRIKE. RETURNED TO TUS DUE TO A NR 1 ENGINE BIRD STRIKE. *S/D* INSPECTION REVEALED 3 DAMAGED FAN BLADES AND MIDSPAN SHROUD OVERLAP ON THE FAN BLADES. BORESCOPE INSPECT - [SDR 2000UALA00739](https://openairdocs.org/sdr/2000UALA00739), May 11, 2000: BULKHEAD. CRACKED. CRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08. - [SDR 2000UALA00136](https://openairdocs.org/sdr/2000UALA00136), Mar 15, 2000: SENSOR. CONTAMINATED. THE NOSE LANDING GEAR AMBER LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. *S/D* FOUND LANDING GEAR HAD HEAVY ACCUMULATION OF ICE. CLEANED GEAR AND SENSOR. JACKED AI - [SDR 99UAL900583](https://openairdocs.org/sdr/99UAL900583), Nov 9, 1999: COMPUTER. FAILED. ON TAKEOFF, ALL ENGINE FAN SPEED INDICATIONS WERE LOST ON THE FLIGHT MANAGEMENT COMPUTER. *S/D* REPLACED THE FLIGHT MANAGEMENT COMPUTER. THE DIGITAL FLIGHT COMP - [SDR 99UAL900175](https://openairdocs.org/sdr/99UAL900175), Mar 25, 1999: FIRE WARNING. MALFUNCTIONED. ABORTED TAKEOFF OF 100 KNOTS DUE TO A FALSE ENGINE FIRE WARNING INDICATION. *S/D* REPLACED ENGINE AND APU FIRE DETECTION ACCESSORY UNIT (M279). OPS CHECK OK. - [SDR 98UAL900407](https://openairdocs.org/sdr/98UAL900407), Aug 23, 1998: CONTROL CABLE. LOOSE. AIRPLANE AIR-GROUND SWITCH STUCK IN GROUND MODE. *S/D* SECURED GROUND SPOILER INTERLOCK CABLE TO TORSION LINK. - [SDR 95UAL900159](https://openairdocs.org/sdr/95UAL900159), Sep 28, 1995: CONNECTOR. LOOSE. ABORTED TAKEOFF AT 80 KNOTS DUE TO A REVERSER LIGHT. FOUND LOOSE CONNECTOR, RESET THE ENGINE ACCESSORY UNIT, AND REPLACED THE CONTROL VALVE MODULE. - [SDR 95UAL900156](https://openairdocs.org/sdr/95UAL900156), Sep 27, 1995: EEL BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS AT RIGHT HAND OVER WING EXIT AND AT CLASS DIVIDER ARE INOP. REPLACED BATTERY PACK. - [SDR 95UAL737038](https://openairdocs.org/sdr/95UAL737038), Mar 30, 1995: TR LIGHT. ILLUMINATED. RIGHT ENGINE REVERSER LIGHT ON OVERHEAD PANEL CAME ON AT 95 KNOTS ON TAKEOFF. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Xag P100 PRO aircraft: https://openairdocs.org/model/xag-p100-pro/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.