# N340US: Xag P100 PRO

- Status: Valid registration
- Airframe: [Xag P100 PRO](https://openairdocs.org/model/xag-p100-pro) (registry code 06102FP)
- Serial number: 82193472N49X
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: December 10, 2024
- Expires: December 31, 2031
- Mode S code: A3BF21
- Registered owner: [Stratton Air And Ground LLC](https://openairdocs.org/faa-owner/STRATTON%20AIR%20AND%20GROUND%20LLC)
- Location: [Tulare, CA](https://openairdocs.org/faa-place/CA/Tulare)
- Owner type: LLC
- Owner's area on the map: 36.1779° N, 119.3800° W: Placed by OpenAirDocs at the center of ZIP code 93274, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=340US
- Page: https://openairdocs.org/aircraft/N340US

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 N340US.

## FAA accident and incident reports

None matched to N340US.

## Reports on N340US not matched to an aircraft (1)

They name N340US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19970626020729I](https://openairdocs.org/incident/19970626020729I), Jun 26, 1997: Boeing 737300 (N340US), Pittsburgh, PA. Uncommanded yaw FL310. Disconnected it and sautopilot. Turned off hyd system. Regained control. No defects found.

## 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 N340US not matched to an aircraft (95, newest 50)

They name N340US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR USAA060735](https://openairdocs.org/sdr/USAA060735), May 31, 2006: SKIN. DELAMINATED. INBOARD END OF RT AFT I/B FLAP DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-53-02, DEFECT SIZE: 2 X 3 INCH.
- [SDR USAA060736](https://openairdocs.org/sdr/USAA060736), May 31, 2006: SKIN. GOUGED. INBOARD SIDE OF RT INBOARD FOR FLAP GOUGED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-10. DEFECT SIZE: 5 X 1 INCH.
- [SDR USAA200605001](https://openairdocs.org/sdr/USAA200605001), May 2, 2006: SKIN. CRACKED. FOUND 1.5" CRACK AT STA 33 LBL, LT SIDE OF MAIN WHEEL WELL. REPAIRED PER TYPICAL REPAIR 53-60-04.
- [SDR SB06043](https://openairdocs.org/sdr/SB06043), Apr 29, 2006: GROUND WIRE. DISCONNECTED. BWI - MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED LIGHT WITH NO HELP. REQUIRES FURTHER TROUBLESHOOTING. PLACED ON MEL 3
- [SDR SB06037](https://openairdocs.org/sdr/SB06037), Apr 20, 2006: SIGN. BROKEN. THE RIGHT OVERWING EMERGENCY EXIT, LOWER VERTICAL SIGN, WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT SIGN ASSEMBLY. OPERATIONAL CHEC
- [SDR USAA200604001](https://openairdocs.org/sdr/USAA200604001), Apr 20, 2006: SKIN. CRACKED. FOUND SKIN CRACKED 2.75" AT STA 747 STRINGER 20L. TWO FILLERS AND TWO DOUBLERS INSTALLED PER SRM 53-00-01 FIG 201 DETAIL XIX.
- [SDR SB06023](https://openairdocs.org/sdr/SB06023), Mar 4, 2006: LIGHT. MALFUNCTIONED. DURING WEEKLY CHECK, MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT DOME LIGHT INOPERATIVE. MAINTENANCE COULD NOT DUPLICATE WRITE-UP. ARMED EMERGENCY LIGHT
- [SDR SB06010](https://openairdocs.org/sdr/SB06010), Jan 28, 2006: WARNING HORN. UNKNOWN. FLIGHT CREW REPORTED TO MOC VIA ACARS THAT THE CABIN ALTITUDE ALERT HORN SOUNDED WITH THE CPC IN AUTO MODE. CREW STATES, "AT CRUISE ALTITUDE 36,000 CABIN ALTITU
- [SDR SB05069](https://openairdocs.org/sdr/SB05069), Jun 12, 2005: INDICATOR. FAILED. EN ROUTE FROM PHL TO CUN, CREW REPORTED THE STANDBY ATTITUDE INDICATOR FAILED. DECISION WAS MADE TO DIVERT TO CLT FOR REPAIRS. FLIGHT LANDED WITHOUT FURTHER INC
- [SDR SB05026](https://openairdocs.org/sdr/SB05026), Feb 11, 2005: LIGHT. INOPERATIVE. PILOT REPORTED THE FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 9 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAA050152](https://openairdocs.org/sdr/USAA050152), Jan 26, 2005: SKIN. CRACKED. CLT - RON - SKIN, 1.750 INCH CRACK, STRINGER 23R STATION 727E; INSTALLED DOUBLER. (K)
- [SDR SB05005](https://openairdocs.org/sdr/SB05005), Jan 15, 2005: WIRE. FAULTY. PHL - MAINTENANCE REPORTED SEVERAL EMERGENCY EXIT ROW LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.
- [SDR USAA041029](https://openairdocs.org/sdr/USAA041029), Dec 5, 2004: SKIN. CHAFED. PIT - RON - L/E SKIN, .5 INCH X 4 INCH CHAFE MARK, LT OB MID FLAP L/E APPROX WBL 204 LT. INSTALLED REPAIR DOUBLER IAW SRM.
- [SDR USAA040410](https://openairdocs.org/sdr/USAA040410), Jul 31, 2004: SKIN. GOUGED. PIT - FOUND LEFT OUTBOARD FOREFLAP GOUGED, .3125 INCH WIDE BY .15 INCHE DEEP BY 2.5 INCH LONG, 30 INCHES FROM OUTBOARD END OF TOP SKIN, LEFT OUTBOARD FOREFLAP. 
- [SDR USAA040390](https://openairdocs.org/sdr/USAA040390), Jul 31, 2004: ROLLER. CHAFED. PIT - FOUND SUPPORT FLAP ROLLER CHAFED .5 INCH BY 1 INCH AREA, FT AFT FLAP NR 1 OUTBOARD ROLLER ARM. REPLACED WITH AFT FLAP PER MM 27-51-39. (M)
- [SDR USAA040346](https://openairdocs.org/sdr/USAA040346), Jul 15, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E, STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA040347](https://openairdocs.org/sdr/USAA040347), Jul 14, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .625 INCH, FS 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)
- [SDR USAA030323](https://openairdocs.org/sdr/USAA030323), Dec 19, 2003: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 3 INCHES, BS 727 D PLUS 13 INCHES S-24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAA030168](https://openairdocs.org/sdr/USAA030168), Aug 27, 2003: ANGLE. CORRODED. FOUND L-ANGLE WITH CORROSION 2 INCHES BY 2 INCHES, STATION 727 FORWARD BULKHEAD AFT FACE IN AFT CARGO, UNDER POTTING COMPOUND. FABRICATED AND INSTALLED NEW STRI
- [SDR USAA030155](https://openairdocs.org/sdr/USAA030155), Aug 19, 2003: BEAM. CRACKED. FOUND BEAM CRACKED 2 INCHES, WEB OF NLG ACTUATOR ATTACH BEAM, STATION 235 NLG WHEEL WELL. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-10-14 AND BOEING
- [SDR USAA030199](https://openairdocs.org/sdr/USAA030199), Aug 15, 2003: STRINGER. CRACKED. FOUND STRINGER CRACKED .75 INCH ON 18A SHELF IN L/RL WHEEL WELL. REPAIRED PER EA 65576. (M)
- [SDR USAA030141](https://openairdocs.org/sdr/USAA030141), Aug 14, 2003: SKIN. DELAMINATED. PIT - FOUND AFT FLAP EXTERIOR SKIN DELAMINATED, 6 INCHES - 11 INCHES FROM OUTBOARD END AND 5 INCHES FROM L/E. COMPOSITE DELAMINATED, RIGHT WING INBOARD AFT FLAP
- [SDR USAA030200](https://openairdocs.org/sdr/USAA030200), Aug 6, 2003: STRINGER. CRACKED. FOUND STRINGER CRACKED .75 INCH, ON 18A SHELF IN R/RL WHEEL WELL. REPAIRED PER EA 65576. (M)
- [SDR USAA030156](https://openairdocs.org/sdr/USAA030156), Aug 5, 2003: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED 1 INCH, BS 1138 S5R. CUT OUT DAMAGE AND SPLICED IN NEW PER TYPICAL REP 53-80-04. (M)
- [SDR USAA030142](https://openairdocs.org/sdr/USAA030142), Aug 4, 2003: ANGLE. CORRODED. PIT - FOUND L-ANGLE CORRODED 2 INCHES BY 2 INCHES, UNDER POTTING COMPOUNT, STATION 727 FORWARD BULKHEAD AFT FACE IN AFT CARGO. FABRICATED AND INSTALLED NEW STRI
- [SDR USAA030140](https://openairdocs.org/sdr/USAA030140), Aug 4, 2003: FRAME. CORRODED. PIT - FOUND CHORD CORRODED 8 INCHES BY 2 INCHES, BS 1016 BETWEEN STRINGERS 26L AND 26R. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-00-01 AND BOEING DWG 6
- [SDR USAASB03014](https://openairdocs.org/sdr/USAASB03014), Jan 25, 2003: ODOR. DETECTED. ATL - FLT 704 - DURING CRUISE, EN ROUTE FROM CLT TO ATL, CREW REPORTED A STRONG ODOR OF JET FUEL IN THE COCKPIT AT TWO DIFFERENT TIMES. ODOR APPEARED TO BE COMI
- [SDR USAASB02007](https://openairdocs.org/sdr/USAASB02007), Jan 11, 2002: CONTROLLER. MALFUNCTIONED. ROC - FLT 202 - EN ROUTE FROM CLT TO ROC, THE AIRCRAFT EXPERIENCED A GRADUAL DEPRESSURIZATION AT FL370 AS CABIN ALTITUDE ROSE TO 10,500 FEET. QUICK REFERENCE HA
- [SDR USAASB01357](https://openairdocs.org/sdr/USAASB01357), Dec 29, 2001: WIRE. DAMAGED. ORD - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT SEAT ROW 20. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA011177](https://openairdocs.org/sdr/USAA011177), Aug 30, 2001: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 1.3 INCHES, STATION 947.5 LOWER FORWARD CORNER OF HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 208. (M)
- [SDR USAA011136](https://openairdocs.org/sdr/USAA011136), Aug 21, 2001: KEELBEAM. CORRODED. CLT - FOUND 2 INCHES OF CORROSION, LEFT KEEL BEAM, VERTICAL LEG, INBOARD SURFACE BS 530. CORROSION LEVEL 2. CLEANED CORROSION, VERIFIED REMOVAL AND RESTORED FIN
- [SDR USAA011180](https://openairdocs.org/sdr/USAA011180), Aug 17, 2001: KEELBEAM. CRACKED. TPA - FOUND KEELBEAM CRACKED 2 INCHES, LEFT KEEL BEAM VERTICAL LEG INBOARD SURFACE STATION 530. CORROSION LEVEL 2. CLEANED CORROSION, VERIFIED REMOVAL AND RESTO
- [SDR USAA011178](https://openairdocs.org/sdr/USAA011178), Aug 16, 2001: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 1 INCH, STATION 947.5 UPPER FORWARD CORNER HINGE CUT OUT. INSTALLED DOUBLERS PER SRM 53-60-01 FIG 205. (M)
- [SDR USAASB01170](https://openairdocs.org/sdr/USAASB01170), Jun 10, 2001: TIRE. SEPARATED. PIT - FLT 1185 - CAPT REPORTED ON T/O FROM PIT, THE NR 3 MLG TIRE TREAD HAD SEPARATED AND CAUSED A RT MLG UNSAFE LIGHT TO ILLUMINATE. CREW RECYCLED GEAR AND REC
- [SDR USAA010391](https://openairdocs.org/sdr/USAA010391), Apr 16, 2001: FRAME. CRACKED. CLT - FOUND SIDE CHORD CRACKED, .5 INCH, BS 178, LBL 24, WL 207. CUT OUT DAMAGE, SPLICED IN NEW SIDECHORD, SRM 51-10-02, EO 5300V157. (M)
- [SDR USAA010390](https://openairdocs.org/sdr/USAA010390), Apr 16, 2001: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED 3 INCHES, WL 195, STATION 178, RBL 24. REMOVED AND REPLACED SRM 51-10-02, EO 5300V153. (M)
- [SDR USAA010388](https://openairdocs.org/sdr/USAA010388), Apr 16, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, FLOORWEBS STATION 179, LBL 28, WL 207. REMOVED AND REPLACED WEB, EO 5300V157. (M)
- [SDR USAA010387](https://openairdocs.org/sdr/USAA010387), Apr 16, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, BS 179, RBL 28, WL 207. REMOVED AND REPLACED WEB EO 5300V157. (M)
- [SDR USAASB00081](https://openairdocs.org/sdr/USAASB00081), Mar 23, 2000: FIRE LOOP. FAILED. BOS - FLT 6509 - ON CLIMB-OUT FROM BOS, AT 5,000 FEET, CREW RECEIVED A FLASHING FAULT LIGHT AND A NR 2 ENGINE OVERHEAT LIGHT. CLIMBING THROUGH 8,000 FEET, LIGHT
- [SDR USAA991130](https://openairdocs.org/sdr/USAA991130), Oct 18, 1999: FRAME. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AT STATION 867, RBL 13.80 FRAME. CORROSION LEVEL 1. CORROSION TASK NR C53-208-0
- [SDR USAA991129](https://openairdocs.org/sdr/USAA991129), Oct 18, 1999: FRAME. CORRODED. CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 2 INCH AT STATION 847 BETWEEN STRINGER 24R AND 25R FRAME. CORROSION LEVEL 1. CORROSION
- [SDR USAA991128](https://openairdocs.org/sdr/USAA991128), Oct 18, 1999: PAN. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AND A 2 INCH BY 2 INCH AT FORWARD AND AFT ENDS STATION 807 AND 847, RBBL 20 AFT
- [SDR USAA991092](https://openairdocs.org/sdr/USAA991092), Oct 18, 1999: ANGLE. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 540, STRINGER 22R SUPPORT ANGLE RAM AIR INLET SUPPORT. FABRICATED AND INSTALLED REPLACEME
- [SDR USAA991091](https://openairdocs.org/sdr/USAA991091), Oct 18, 1999: SKIN. CRACK. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF PANEL NR 5727L CUTOUT LEFT PYLON SKIN. INSTALLED DOUBLER PER EA 65815 AND T
- [SDR USAA991080](https://openairdocs.org/sdr/USAA991080), Oct 18, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 6, RBL 27, RBL 29 LWR SURFACE OF T-CAP BEAM. CORROSION LEVEL 2. CORRO
- [SDR USAA991079](https://openairdocs.org/sdr/USAA991079), Oct 18, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 1006, LBL 38 T-CAP BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. REMOV
- [SDR USAA991078](https://openairdocs.org/sdr/USAA991078), Oct 18, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AND 1 INCH UPPER CHORD STATION 328, LBL 28 BEAM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-0
- [SDR USAA991077](https://openairdocs.org/sdr/USAA991077), Oct 18, 1999: SKIN. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 379, LBS 3.5 SKIN. INSTALLED REPAIR DOUBLER PER TR-53-30-07 AND BAC DRWG 65C33930. (M)
- [SDR USAA991076](https://openairdocs.org/sdr/USAA991076), Oct 18, 1999: FRAME. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0125 INCH CRACK AT BS 827 STRINGER 9R AT FASTENER HOLE FRAME. INSTALLED DOUBLER PER EA 65542, SRM 53-00-07 AN
- [SDR USAA991075](https://openairdocs.org/sdr/USAA991075), Oct 18, 1999: FRAME. CRACKED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FORWARD SERVICE DOOR CUTOUT FRAME STATION 295.5, RBL 54, WL 208.5. FABRICATED REPAIR ANGLE PE

All 95: https://openairdocs.org/aircraft/N340US/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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