# N371AA: Xag P100 PRO

- Status: Valid registration
- Airframe: [Xag P100 PRO](https://openairdocs.org/model/xag-p100-pro) (registry code 06102FP)
- Serial number: 8219425YY149
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: April 22, 2025
- Expires: April 30, 2032
- Mode S code: A43783
- 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=371AA
- Page: https://openairdocs.org/aircraft/N371AA

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 N371AA.

## FAA accident and incident reports

None matched to N371AA.

## 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 N371AA not matched to an aircraft (80, newest 50)

They name N371AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MK1Y20170602001](https://openairdocs.org/sdr/MK1Y20170602001), Jun 2, 2017: FRAME. CRACKED. FOUND A .236 INCH CRACK ON THE FRAME INNER TRANSITION RADIUS, BS 883.5, RBL 89.
- [SDR MK1Y20170604005](https://openairdocs.org/sdr/MK1Y20170604005), May 18, 2017: FRAME. CRACKED. CRACK AT BS 883.5, LBL 89 FRAME.
- [SDR MK1Y20170604004](https://openairdocs.org/sdr/MK1Y20170604004), May 18, 2017: FRAME. CRACKED. CRACK AT BS 859.5, RBL 89 RT FRAME.
- [SDR MK1Y20170604003](https://openairdocs.org/sdr/MK1Y20170604003), May 18, 2017: SKIN. CRACKED. CRACK FOUND ON THE LT WING SKIN AT AFT PITCH LOAD FITTING, REPAIRED IAW DRAWING 112T7001.
- [SDR MK1Y20170604001](https://openairdocs.org/sdr/MK1Y20170604001), May 18, 2017: FRAME. CRACKED. DURING PERFORMANCE OF AD 2012-22-17, FOUND A CRACK, 0.236 INCHES IN LENGTH AT THE FRAME IN THE TRANSITION RADIUS BS 903.5, RBL 89.
- [SDR AALA20150821013](https://openairdocs.org/sdr/AALA20150821013), Aug 21, 2015: WINDOW. OPEN. ABORTED TAKEOFF BETWEEN 70 & 75 KNOTS FOR COCKPIT SLIDING WINDOW OPENED ON TAKEOFF ROLL. NO DEFECTS NOTED WITH THE WINDOW, OPERATES NORMALLY. PERFORMED HIGH ENE
- [SDR AALA20150223005](https://openairdocs.org/sdr/AALA20150223005), Feb 21, 2015: O-RING. TORN. EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. AT TOP OF DESCENT RECEIVED, C HYD QTY EICAS MSG. QTY CONTINUED TO DECREASE TO .15 DURING FINAL APP
- [SDR AALA20150119004](https://openairdocs.org/sdr/AALA20150119004), Jan 19, 2015: COMPUTER. FAILED. AIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB BOTH FLIGHT MANAGEMENT COMPUTERS FAILED. R & R LT FLIGHT MAN
- [SDR AALA20150101006](https://openairdocs.org/sdr/AALA20150101006), Jan 1, 2015: PSEU. FAULTY. LEADING EDGE SLAT ASSYM MSG ON CLIMB OUT. FLAP NEEDLES FLUCTUATED BETWEEN 0 & 1. ON ARRIVAL AT JFK, BITE OF PSEU SHOWS CARD FAULT 10 & LE SLAT TARGET FAULT 297.
- [SDR AALA20141209010](https://openairdocs.org/sdr/AALA20141209010), Dec 7, 2014: WARNING SYSTEM. FALSE ACTIVATION. EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. LE SLAT ASYMMETRY MSG ILLUMINATED AFTER TAKEOFF. LANDED 20 DEGREE FLAPS USING FLAP HANDLE. ACCOMPL
- [SDR AALA20140910001](https://openairdocs.org/sdr/AALA20140910001), Sep 8, 2014: LIGHT. INOPERATIVE. LEFT NR 2 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140531005](https://openairdocs.org/sdr/AALA20140531005), May 31, 2014: SKIN. DAMAGED. FUSELAGE SKIN AT STATION 1460 & STRINGER 28 RT DAMAGED. ACCOMPLISHED REPAIR IAW EA B767-53-035130.
- [SDR AALA20140530015](https://openairdocs.org/sdr/AALA20140530015), May 30, 2014: STRUCTURE. CRACKED. CRACKS FOUND IN OUTER CORD AT RT STATION 1725.5. ACCOMPLISHED REPAIR IAW SRM 53-80-01 REPAIR 5, FIGURE 201 DETAIL 3 & EA B767-53-035085.
- [SDR AALA20140524006](https://openairdocs.org/sdr/AALA20140524006), May 24, 2014: FRAME. CRACKED. NUMBER 2 PYLON FRAME CHORD AT STATION 285.450 OTBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW SRM 51-10-02 & DWG 311T2400.
- [SDR AALA20140524005](https://openairdocs.org/sdr/AALA20140524005), May 24, 2014: FRAME. CRACKED. RIGHT PYLON FRAME CHORD AT STATION 285.450 INBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW B767-300 SRM 51-10-02 & DWG 311T2400.
- [SDR AALA20140524004](https://openairdocs.org/sdr/AALA20140524004), May 24, 2014: STIFFENER. CRACKED. RIGHT PYLON STIFFENER CRACKED 2 INCHES AFT OF INBD FRAME CHORD AT STATION 285.450. R & R STIFFENER IAW SRM 51-10-02-0G, 51-40-02-0G & DWG 311T2400.
- [SDR AALA20140516009](https://openairdocs.org/sdr/AALA20140516009), May 15, 2014: SOCKET. DIRTY. EXTERIOR EMERGENCY LIGHT AFT OF LT NR 4 DOOR INOPERATIVE. CLEANED LIGHT SOCKET & REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140401002](https://openairdocs.org/sdr/AALA20140401002), Apr 1, 2014: SKIN. DAMAGED. FUSELAGE SKIN DAMAGED FROM BS 1390 - 1480 BETWEEN STRINGERS 27 & 28 RT. INSTALLED EXTERNAL REPAIR IAW EA B767-53-034141.
- [SDR AALA20140131006](https://openairdocs.org/sdr/AALA20140131006), Jan 31, 2014: LIGHT. DEFECTIVE. OVERWING LIGHT WAS DIM. REPLACED LAMP FOR OVERWING LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140131005](https://openairdocs.org/sdr/AALA20140131005), Jan 31, 2014: LIGHT. INOPERATIVE. LT NR 4 EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 EXIT EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20131123008](https://openairdocs.org/sdr/AALA20131123008), Nov 23, 2013: CONTROLLER. INOPERATIVE. GIG CREW REPORTED DUAL BLEED FAULTS & RT HIGH PRESSURE SHUTOFF VLV EICAS MESSAGE WITH WARNING LIGHT & LT PRESSURE RELIEF VLV MESSAGE DISPLAYED. EMERGENCY DECLAR
- [SDR AALA20130604010](https://openairdocs.org/sdr/AALA20130604010), Jun 4, 2013: CHARGER. FAILED. CREW REPORTED MULTIPLE ELECTRICAL FAULTS AND MAIN BATTERY CHARGER MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE
- [SDR AALA20130223002](https://openairdocs.org/sdr/AALA20130223002), Feb 23, 2013: WIRE HARNESS. FAULTY. JFK - INFLIGHT ORD-LHR. CREW REPORTED RIGHT ENGINE HP BLEED AIR *HPSOV* LIGHT ILLUMINATED DURING FLIGHT. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT R
- [SDR AALA20121116004](https://openairdocs.org/sdr/AALA20121116004), Nov 16, 2012: STRUCTURE. CORRODED. CORROSION FOUND ON TOP OF HORIZONTAL STABILIZER BOX. REPAIRED CORROSION ON STABILIZER BOX PER EA B767-55-026959.
- [SDR AALA20121116003](https://openairdocs.org/sdr/AALA20121116003), Nov 16, 2012: SKIN. CORRODED. HORIZONTAL STABILIZER CENTER BOX UPPER SKIN FROM STRINGER 1 TO REAR SPAR, RIGHT BUTTLINE 2.75. INSTALLED DOUBLER PER EA B767-55-027021.
- [SDR AALA20121116002](https://openairdocs.org/sdr/AALA20121116002), Nov 16, 2012: SKIN. CORRODED. HORIZONTAL STABILIZER CENTER BOX UPPER SKIN FROM STRINGERS 3 TO 2, LEFT BUTTLINE 1.75. INSTALLED DOUBLER PER EA B767-55-027021.
- [SDR AALA20121116001](https://openairdocs.org/sdr/AALA20121116001), Nov 16, 2012: STRUCTURE. CRACKED. RIGHT STATION 1809.5 OUTER CHORD CRACK. ACCOMPLISHED SPLICE REPAIR PER ECO C1945DN.
- [SDR AALA20121116013](https://openairdocs.org/sdr/AALA20121116013), Nov 16, 2012: ANGLE. CRACKED. RIGHT PYLON CLOSE OUT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-00-05-1.
- [SDR AALA20121106005](https://openairdocs.org/sdr/AALA20121106005), Nov 6, 2012: SLAT. DEBONDED. NUMBER 5 LEADING SLAT STARTING TO DISBOND. ACCOMPLISHED BONDED REPAIR PER SRM 57-43-02-01.
- [SDR AALA20121106004](https://openairdocs.org/sdr/AALA20121106004), Nov 6, 2012: SKIN. DELAMINATED. RIGHT WING OUTBOARD FLAP LOWER SKIN SURFACE DELAMINATED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.
- [SDR AALA20120403009](https://openairdocs.org/sdr/AALA20120403009), Apr 2, 2012: LAMP. BURNED OUT. L2 DOOR EMERGENCY EXIT LIGHT. REPLACED LAMP FOR L2 EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.
- [SDR AALA20120403008](https://openairdocs.org/sdr/AALA20120403008), Apr 2, 2012: LAMP. BURNED OUT. RIGHT NUMBER 2 DOOR EMERGENCY EXIT LIGHT UPPER INTERIOR LOWER SECTION INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY EXIT LIGHT. OPS CHECKED NORMA
- [SDR AALA20120403007](https://openairdocs.org/sdr/AALA20120403007), Apr 2, 2012: LAMP. BURNED OUT. RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.
- [SDR AALA20120403006](https://openairdocs.org/sdr/AALA20120403006), Apr 2, 2012: LAMP. BURNED OUT. OVERHEAD EMERGENCY LIGHT AT SEAT 43C INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 43C. OPS CHECKED NORMAL.
- [SDR AALA20120403005](https://openairdocs.org/sdr/AALA20120403005), Apr 2, 2012: LAMP. BURNED OUT. OVERHEAD EMERGENCY LIGHT AT SEAT 34B INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 34B. OPS CHECKED NORMAL.
- [SDR AALA20120403004](https://openairdocs.org/sdr/AALA20120403004), Apr 2, 2012: LAMP. BURNED OUT. SEAT 37H OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 37H OVERHEAD LIGHT. OPS CHECKED NORMAL.
- [SDR AALA20120403003](https://openairdocs.org/sdr/AALA20120403003), Apr 2, 2012: LAMP. BURNED OUT. MID GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR MID GALLEY OVERHEAD EMERGENCY LIGHT. OPS CHECKED NORMAL.
- [SDR AALA20120403002](https://openairdocs.org/sdr/AALA20120403002), Apr 2, 2012: LAMP. BURNED OUT. FORWARD GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.
- [SDR AALA20120209MIA01](https://openairdocs.org/sdr/AALA20120209MIA01), Feb 9, 2012: LENS. LOOSE. EMERGENCY EXIT LIGHT LENS COVER AT RIGHT NUMBER 4 DOOR LOOSE. SECURED LENS COVER FOR RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.
- [SDR AALA20120125TUL05](https://openairdocs.org/sdr/AALA20120125TUL05), Jan 24, 2012: LIGHT. INOPERATIVE. RIGHT EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO DOOR. OPS CHECK NORMAL.
- [SDR AALA20120125SFO02](https://openairdocs.org/sdr/AALA20120125SFO02), Jan 24, 2012: LIGHT. INOPERATIVE. LEFT AFT EXTERIOR EMERGENCY LIGHT NEAR LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED LAMP FOR LEFT AFT EXTERIOR EMERGENCY NEAR LEFT NUMBER 2 DOOR. OPS CHECK NORMAL.
- [SDR AALA20110402DFW01](https://openairdocs.org/sdr/AALA20110402DFW01), Apr 2, 2011: BRAKE. OVERHEATED. DFW - CREW REPORTED TAIL STRIKE ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. BRAKES OVERHEATED UPON LANDING CAUSING ALL MAIN LAND
- [SDR AALA20110302LHR01](https://openairdocs.org/sdr/AALA20110302LHR01), Mar 2, 2011: SMOKE DETECTOR. FAULTY. UPON LANDING RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF. NO GREEN LIGHT ON. CHECKED LAVATORY FOR SMOKE AND FIRE NONE NOTED. REPLACED SMOKE DETECTOR. OPS CHECK N
- [SDR AALA20110228LHR03](https://openairdocs.org/sdr/AALA20110228LHR03), Feb 27, 2011: TRANSFORMER. FAILED. LHR - INFLIGHT CDG-JFK. CREW REPORTED RIGHT AC BUSS OFF LIGHT WITH CORRESPONDING ELECTRICAL BUS FAILURE. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT I
- [SDR AALA20100224TUL12](https://openairdocs.org/sdr/AALA20100224TUL12), Jan 18, 2010: FRAME. CRACKED. FRAME AT STATION 522 IN THE FORWARD CARGO BETWEEN STRINGER 30 LEFT AND 31 LEFT WERE FOUND DAMAGED. THE SUBJECT DAMAGE IS LIMITED TO THE FRAME INNER CHORD BETWEE
- [SDR AALA20100224TUL10](https://openairdocs.org/sdr/AALA20100224TUL10), Jan 18, 2010: STRUCTURE. CRACKED. FOUND CRACK INDICATION AT STATION 1809.5 RIGHT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2782 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEI
- [SDR AALA20100118AFW03](https://openairdocs.org/sdr/AALA20100118AFW03), Jan 18, 2010: FRAME. CRACKED. FRAME AT STATION 500 IN THE FORWARD CARGO BETWEEN STRINGER 30 LEFT AND 31 LEFT WERE FOUND DAMAGED. THE SUBJECT DAMAGE IS LIMITED TO THE FRAME INNER CHORD BETWEE
- [SDR AALA20100118AFW02](https://openairdocs.org/sdr/AALA20100118AFW02), Jan 18, 2010: TORQUE BOX. CRACKED. FOUND SEVERAL CRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-54-008424
- [SDR AALA20100118AFW01](https://openairdocs.org/sdr/AALA20100118AFW01), Jan 18, 2010: STRUCTURE. CRACKED. FOUND CRACK INDICATION AT STATION 1809.5 LEFT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2636 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEIN
- [SDR AALA20100224TUL08](https://openairdocs.org/sdr/AALA20100224TUL08), Jan 15, 2010: SKIN. DAMAGED. ONE UPPER SKIN PANEL 666JT FASTENER HOLE ON THE RIGHT OUTBOARD LEADING EDGE FLAP WAS DAMAGED DURING MAINTENANCE. REPAIRED UNDER EA COMP-57-008495.

All 80: https://openairdocs.org/aircraft/N371AA/unmatched-reports.md

## 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

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