# N304AW: Xag P100 PRO

- Status: Valid registration
- Airframe: [Xag P100 PRO](https://openairdocs.org/model/xag-p100-pro) (registry code 06102FP)
- Serial number: 8219345M3639
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: September 20, 2024
- Expires: September 30, 2031
- Mode S code: A32E43
- Registered owner: [Wilson Joshua Howard](https://openairdocs.org/faa-owner/WILSON%20JOSHUA%20HOWARD)
- Location: [Garland, NC](https://openairdocs.org/faa-place/NC/Garland)
- Owner type: Individual
- Owner's area on the map: 34.8115° N, 78.4274° W: Placed by OpenAirDocs at the center of ZIP code 28441, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=304AW
- Page: https://openairdocs.org/aircraft/N304AW

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 N304AW.

## NTSB investigations on N304AW not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA91LA126](https://openairdocs.org/ntsb/SEA91LA126), Jun 6, 1991: Boeing 737-3G7 (N304AW), Elko, NV, no damage. Probable cause: AN UNSECURED CART. THE FACTORS TO THE ACCIDENT WERE: TURBULENT WEATHER CONDITIONS, AND POOR JUDGEMENT BY THE FLIGHT ATTENDANT.

## FAA accident and incident reports

None matched to N304AW.

## Reports on N304AW not matched to an aircraft (2)

They name N304AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19980719023409I](https://openairdocs.org/incident/19980719023409I), Jul 19, 1998: Boeing 737300 (N304AW), Kansas City, MO. Left pack tripped during climb thru FL120. Unable reset 390 degree temp sens or bad. Overnight ldg check.
- [Accident 19910605027549A](https://openairdocs.org/incident/19910605027549A), Jun 5, 1991: Boeing 7373G7 (N304AW), Elko, NV. Flight attendant left beverage cart unattended. Spilled hot coffee on a passenger causing second degree burns.

## 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 N304AW not matched to an aircraft (55, newest 50)

They name N304AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 304AW0008](https://openairdocs.org/sdr/304AW0008), Jun 17, 2004: BATTERY PACK. INOPERATIVE. ROWS 1-4 OF EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED FUSES IN BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-51.
- [SDR 304AW0007](https://openairdocs.org/sdr/304AW0007), May 19, 2004: SKIN. LIGHTNING STRIKE. SEVERAL LIGHTENING STRIKES IN THE CROWN OF THE FUSELAGE SKIN NEAR STATION 259 BETWEEN STR 2 AND 3 LEFT. REPAIRED IAW SRM 53-00-01 AND EA NR 53-171.
- [SDR 304AW0006](https://openairdocs.org/sdr/304AW0006), Apr 25, 2004: PANEL. MALFUNCTIONED. MODE CONTROL PANEL SWITCHES, N1, SPD, VNAV, LNAV, ALT HLD & V/S INDICATORS INOP. PLACED ON MEL 22-15-8. NOTE: MAINTENANCE INDUCED PROBLEM WHILE REPLACING ONE LI
- [SDR 304AW0005](https://openairdocs.org/sdr/304AW0005), Apr 18, 2004: COUPLER. DAMAGED. YAW DAMPER POPS DC CIRCUIT BREAKER. PLACED ON MEL 22-3-1 AND PERFORMED RUDDER PRESSURE REDUCER SYSTEM TEST PER MM 22-12-01. 04/22/2004: REPLACED YAW DAMPER COUP
- [SDR 304AW0004](https://openairdocs.org/sdr/304AW0004), Mar 18, 2004: BATTERY. INOPERATIVE. MID CABIN EMERGENCY ESCAPE LIGHTS ALONG SEAT BOTTOMS INOP. ALSO AFT EMERGENCY FLASHLIGHT INOP. REPLACED 1 FUSE ON BATTERY PACK LOCATED ON RIGHT AFT DOOR. CABIN 
- [SDR 304AW0003](https://openairdocs.org/sdr/304AW0003), Feb 8, 2004: RELAY. STICKING. CREW REPORTED THAT THE AUTOPILOT COMMAND-A WILL NOT ENGAGE UNLESS COMMAND-B IS ENGAGED FIRST. REPLACED AILERON FORCE LIMITER CLUTCH RELAY DUE TO STICKING. CHECK
- [SDR 304AW0002](https://openairdocs.org/sdr/304AW0002), Nov 14, 2003: CONNECTOR. DIRTY. SPEED TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. PLACED ON MEL 22-10. CLEANED AND RESECURED CANNON PLUG ON FCC PER MM 22-11-33. PERFORMED BITE TEST PER MM 22-11
- [SDR 304AW0001](https://openairdocs.org/sdr/304AW0001), May 11, 2003: COMPUTER. MALFUNCTIONED. AUTO THROTTLE DISCONNECTED ON TAKEOFF ROLL. REMOVED AUTO THROTTLE COMPUTER AFTER TROUBLESHOOTING. REINSTALLED AUTO THROTTLE COMPUTER AND PERFORMED BITE TEST PER
- [SDR AWXA200200280](https://openairdocs.org/sdr/AWXA200200280), Apr 3, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT CARGO COMPARTMENT AT BS 727+6, LBL 2.5. MAINTENANCE RE
- [SDR AWXA200200271](https://openairdocs.org/sdr/AWXA200200271), Mar 21, 2002: SKIN. DENTED. LCQ - MAJOR REPAIR - DURING C-15 CHECK A DENT WAS FOUND ON RT HORIZONTAL STABILIZER AT STAB STA 144 MID SPAN. FABRICATED A DOUBLER, FILLER AND INSTALLED REPAIR 
- [SDR AWXA200200295](https://openairdocs.org/sdr/AWXA200200295), Mar 11, 2002: FLOOR SUPPORT. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AND NUTPLATES IN THE AFT CARGO PIT AT BS 773, LBL 2.5. MAINTENANCE REMOVED 
- [SDR AWXA200200294](https://openairdocs.org/sdr/AWXA200200294), Mar 11, 2002: STRAP. CORRODED. MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON THE RT FLOOR SUPPORT LOWER STRAP IN THE AFT CARGO COMPARTMENT AT BS 849, RBL 19. MAINTENANCE REMOVED COR
- [SDR AWXA200200292](https://openairdocs.org/sdr/AWXA200200292), Mar 11, 2002: FLOORBEAM. CORRODED. MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON THE TOP OF FLOORBEAM AT BS 986.5, LBL 58. MAINTENANCE CLEANED CORROSION OFF FLOORBEAM AND FOUND MATERIAL
- [SDR AWXA200200279](https://openairdocs.org/sdr/AWXA200200279), Mar 11, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT CARGO COMPARTMENT AT BS 727D+6, LBL 7.5. MAINTENANCE R
- [SDR AWXA200200278](https://openairdocs.org/sdr/AWXA200200278), Mar 11, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT ACRGO COMPARTMENT AT BS 860, LBL 7.5. MAIN
- [SDR AWXA200200277](https://openairdocs.org/sdr/AWXA200200277), Mar 11, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM IN THE AFT CARGO COMPARTMENT AT BS 860, RBL 7.5. MAINTENANCE FABRIC
- [SDR AWXA200200276](https://openairdocs.org/sdr/AWXA200200276), Mar 11, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATE IN THE AFT CARGO COMPARTMENT AT BS 860, LBL 2.5. MAINTENANCE REMOV
- [SDR AWXA200200275](https://openairdocs.org/sdr/AWXA200200275), Mar 11, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM IN THE AFT CARGO COMPARTMENT AT BS 773, RBL 2.5. MAINTENANCE CLEANED CORROSION 
- [SDR AWXA200200274](https://openairdocs.org/sdr/AWXA200200274), Mar 11, 2002: FLOORBEAM. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO PIT RT FLOOR SUPPORT BEAM BS 727D+6, RBL 7.5. MAINTENANCE REMOVED CORROSION AND MATERAIL
- [SDR AWXA200200273](https://openairdocs.org/sdr/AWXA200200273), Mar 11, 2002: FLOOR SUPPORT. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO PIT FLOOR SUPPORT NUT PLATE BS 860, RBL 2.5. MAINTENANCE REMOVED NUT PLATE AND CORROSION
- [SDR AWXA200200272](https://openairdocs.org/sdr/AWXA200200272), Mar 11, 2002: FLOOR SUPPORT. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATED CORROSION WAS FOUND ON AFT PIT FLOOR SUPPORT AT BS 860, LBL 12.5. MAINTENANCE CLEANED CORROSION AND FOUND MATE
- [SDR AWXA200200270](https://openairdocs.org/sdr/AWXA200200270), Mar 11, 2002: FLOORBEAM. CRACKED. LCQ - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND RUNNING FROM SEAT TRACK FLOORBEAM TEE CAP LOWER EDGE TO A FASTENER HOLE ON INBOARD SIDE, BS 663.75, RBL
- [SDR AWXA200200268](https://openairdocs.org/sdr/AWXA200200268), Mar 11, 2002: FRAME. CRACKED. LCQ - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND ON CABIN SIDE WALL FRAME ATTACHED TO FLOORBEAM AT BS 616, LBL 66, WL 208, LOCATED JUST BELOW F
- [SDR AWXA200200293](https://openairdocs.org/sdr/AWXA200200293), Mar 10, 2002: STRINGER. CORRODED. LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER IN THE AFT CARGO COMPARTMENT BS 1010, STR 27 R/H. MAINTENANCE REMOVED CORRODE
- [SDR AWXA200200269](https://openairdocs.org/sdr/AWXA200200269), Mar 10, 2002: SKIN. CRACKED. LCQ - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .300" CRACKS WERE FOUND ON LOWER AFT RADIUS RIVET PATTERN OF R1 DOOR CUTOUT. MAINTENANCE CUTOUT CRACKED AREA OF SK
- [SDR AWXA200200267](https://openairdocs.org/sdr/AWXA200200267), Mar 10, 2002: SKIN. CRACKED. LCQ - MAJOR REPAIR - DURING C-15 CHECK A .250 INCH CRACK WAS FOUND ON THE SKIN OF THE L2 DOOR CUTOUT AT BS 986.5, STR 8 LT. FABRICATED REPAIR DOUBLERS AND INSTA
- [SDR AWXA200200078](https://openairdocs.org/sdr/AWXA200200078), Jan 24, 2002: POWER SUPPLY. FAILED. AFT EMERGENCY EXIT LIGHTS FROM ROW 18 LT, ALL THE WAY AFT WILL NOT ILLUMINATE DURING TEST. MAINTENANCE TROUBLESHOT AND FOUND THE AFT POWER SUPPLY INOPERATIVE AT
- [SDR AWXA0001952](https://openairdocs.org/sdr/AWXA0001952), Jul 9, 2001: CREASE BEAM. CORRODED. BS 767-787 LT CREASE BEAM PANEL IS CORRODED. SHEAR WEB MADE AND INSTALLED AS PER DWG 65-55885-3, PART PAINTED AS PER MM 51-21-10 PG 701.
- [SDR AWXA0001951](https://openairdocs.org/sdr/AWXA0001951), Jul 9, 2001: TEE CHORD. CRACKED. CRACK INDICATION ON AFT CARGO DOOR LOWER AFT CORNER, LOWER WEB TO SKIN ATTACH ANGLE, CRACK, LOCATED BETWEEN TWO AFT RIVETS WEB. AFT LOWER WEB T-CHORD REPAIRED P
- [SDR AWXA0001950](https://openairdocs.org/sdr/AWXA0001950), Jul 9, 2001: SKIN. DAMAGED. FUSELAGE SKIN HAS A NON STANDARD REPAIR AT RIVET LOCATION BS 727C AND 2 INCHES BELOW STRINGER 17L. FUSELAGE SKIN REPAIRED AT BS 727C AND 2 INCHES BELOW STR 17L 
- [SDR AWXA0001949](https://openairdocs.org/sdr/AWXA0001949), Jul 9, 2001: STRINGER. CRACKED. D: Stringer crack at STA 178. WL 207. RBL 28C: fabricated repair parts per SRM 51-70-12 Fig 1 detail 7. Installed repair parts per SRM 51-70-12 Fig 1
- [SDR AWXA0001948](https://openairdocs.org/sdr/AWXA0001948), Jul 9, 2001: FRAME. CRACKED. FUSELAGE RT SIDE CHORD AT WL 207, STA 178 CRACKED. INSTALLED NEW SIDE CHORD P/N 65-16300-87 AS PER DWG 65-16300 SHEET 4 FRAME 1-8.
- [SDR AWXA0001947](https://openairdocs.org/sdr/AWXA0001947), Jul 9, 2001: FRAME. CRACKED. FUSELAGE LT SIDE CHORD AT WL 207 STA 178 CRACKED. INSTALLED NEW 65-16300-86 SIDE CHORD AS PER DWG 65-16300 SHEET 4 FRAME 1 TO 8.
- [SDR AWXA0001946](https://openairdocs.org/sdr/AWXA0001946), Jul 9, 2001: WEB. CRACKED. D: Center Bulkhead Web Crack At Body STA .178 . WL 187. BLO.C: Remove Crack Per SRM 53-10-08 Fig 203. NDT Checked For Crack Containment. Frabricate Repair Parts
- [SDR AWXA0001945](https://openairdocs.org/sdr/AWXA0001945), Jul 9, 2001: BULKHEAD. CRACKED. WEB CRACKS AT STA 178 LBL 5.7. REMOVED FASTENERS PER SRM 51-40-2 AT REPAIR AREA. REPAIRED CRACKS PER SRM 53-10-08 FIG 209. NDT CHECKED CRACKS CONTAINMENT. FABRI
- [SDR AWXA0001944](https://openairdocs.org/sdr/AWXA0001944), Jul 9, 2001: WEB. CRACKED. D: Web Crack on Floor Level (WL 207) At STA .178 on R/H Side RBL 28C: Removed Cracked Web, Fabricated New Web P/N 65-45833-40 Per REF DWG 65-45833, install Web 
- [SDR AWXA0000365](https://openairdocs.org/sdr/AWXA0000365), Jun 5, 2000: BLEED VALVE. FAILED. AIR TURNBACK, NR 1 ENGINE BLEED AIR VALVE W/N CLOSE, CURCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 ENGINE BLEED AIR REGULATOR. TT 0049297 M+E=03-3611-9-0001
- [SDR AWXA0000329](https://openairdocs.org/sdr/AWXA0000329), May 23, 2000: STRUCTURE. CRACKED. C-CHECK, VERT STAB UPPER RUDDER HINGE POINT RT STRUCTURE HAS CRACK AT CORNER. REMOVED DAMAGED CORNER COVER, FABRICATED REPAIR COVER IAW 737 SRM 51-30-30, 51-20-
- [SDR AWXA0000328](https://openairdocs.org/sdr/AWXA0000328), May 23, 2000: SKIN. CRACKED. C-CHECK, CRACKS IN LOWER SKIN OF THE LEADING EDGE OF NR 2 AND NR 3 SLATS. REMOVED DAMAGED AREA IAW ER NR 3-57-55-17E, FABRICATED FILLERS FROM MAT SHT 77075 T6 X
- [SDR AWXA0000327](https://openairdocs.org/sdr/AWXA0000327), May 23, 2000: FLOORBEAM. CORRODED. C-CHECK, CORROSION OUT OF LIMITS ON T-CAP AT FS 986.5 RBL 18. REMOVED DAMAGED T CAP IAW 737 SRM 51-40-02, FABRICATED T CAP FROM BAC 1505 100617/7077, IAW 737 SR
- [SDR AWXA9900253](https://openairdocs.org/sdr/AWXA9900253), Aug 3, 1999: MODULE. INOP. NML OPS, ELECTRICAL SMELL IN COCKPIT. UNKNOWN ELECTRICAL SMELL IN COCKPIT. INSPECTED COCKPIT, RAN ENGINES ISOLATED ODOR TO P5-9 WINDOW, PITOT HEAT MODULE. REPLA
- [SDR AWXA9900157](https://openairdocs.org/sdr/AWXA9900157), Mar 26, 1999: FLOORBEAM. CORRODED. FLOORBEAM UPPER CHORD CORRODED RBL 6 TO RBL 52 AT STA 294.5. FABRICATED T-CHORDS AND REPAIRED AS PER AWA ER 3-53-1529 INSTRUCTIONS.
- [SDR AWXA9900156](https://openairdocs.org/sdr/AWXA9900156), Mar 26, 1999: FLOORBEAM. CORRODED. CORROSION AROUND SCREW HOLES TOP AND BOTTOM OF UPPER TEE CHORD RBL 21-56, FRAME STA 328 RT. FABRICATED T-CHORD AND REPAIR AS PER AWA ER 3-53-1529 INSTRUCTIONS.
- [SDR AWXA9900158](https://openairdocs.org/sdr/AWXA9900158), Mar 16, 1999: FLOORBEAM. CORRODED. FLOORBEAM 986.5 REQUIRES REPAIR SPLICES IAW AWA ER 3-53-1529 DUE TO CORROSION ON T-CAP. FABRICATED T-CHORDS AND REPAIRED ANGLES PER AWA ER 3-53-1529 INSTRUCTION
- [SDR AWXA9700691](https://openairdocs.org/sdr/AWXA9700691), Dec 8, 1997: CONTROLLER. FAILED. SMOKE CAME OUT OF THE AFT PORTION OF THE COPILOTS FORWARD WINDOW, NEAR THE DRAIN HOSE. THE WINDOW HEAT WAS TURNED OFF AND THE SMOKE WENT AWAY. REMOVED AND REPLA
- [SDR AWXA9600787](https://openairdocs.org/sdr/AWXA9600787), Dec 31, 1996: SKIN. DENTED. DURING ROUTINE MAINTENANCE CHECK, FOUND C-2 DOOR AFT CARGO OUTER SKIN DENTED AND CREASED IN SEVERAL PLACES. REMOVED AND REPLACED C-2 DOOR OUTER SKIN IAW B737, S
- [SDR AWXA960020](https://openairdocs.org/sdr/AWXA960020), Jan 20, 1996: SKIN. DENTED. PHX - FLT NR 842 - DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENTED ACROSS STRINGER 25R, 4 FEET FORWARD OF AFT CARGO DOOR CUTOUT. OPENED UP INTERIOR
- [SDR AWXA960011](https://openairdocs.org/sdr/AWXA960011), Jan 9, 1996: OUTFLOW VALVE. FAILED. PHX/BUR - FLT 0484 - AUTOPRESSURE INOPERATIVE AT 280 FEET CABIN ALTITUDE AT 3,000 FEET, DIFFERENTIAL PRESSURE 8.4. REMOVED AND REPLACED REAR OUTFLOW VALVE. OPS 
- [SDR 96ZZZX565](https://openairdocs.org/sdr/96ZZZX565), Jan 9, 1996: CONTROLLER. FAILED. PHX/BUR - FLT 0484 - AUTOPRESSURE INOPERATIVE AT 280 FEET CABIN ALTITUDE AT 3,000 FEET, DIFFERENTIAL PRESSURE 8.4. REMOVED AND REPLACED REAR OUTFLOW VALVE. OPS 
- [SDR AWXA9500820](https://openairdocs.org/sdr/AWXA9500820), Dec 22, 1995: COVER. LOOSE. LAS - FLT 1512 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT COVER IN FORWARD GALLEY LOOSE. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. 

All 55: https://openairdocs.org/aircraft/N304AW/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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