# N328AW: DJI AGRAS T30 - Status: Valid registration - Airframe: [DJI AGRAS T30](https://openairdocs.org/model/dji-agras-t30) (registry code 06102BX) - Serial number: 527BJAL001002X - Type: Rotorcraft - Engine type: Electric - Certificate issued: August 27, 2025 - Expires: August 31, 2032 - Mode S code: A38C1D - Registered owner: [Steele Michael W](https://openairdocs.org/faa-owner/STEELE%20MICHAEL%20W) - Location: [El Paso, TX](https://openairdocs.org/faa-place/TX/El%20Paso) - Owner type: Individual - Owner's area on the map: 31.7849° N, 106.4969° W: Placed by OpenAirDocs at the center of ZIP code 79902, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=328AW - Page: https://openairdocs.org/aircraft/N328AW 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 (DJI AGRAS T30) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N328AW. ## NTSB investigations on N328AW 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 LAX99LA050](https://openairdocs.org/ntsb/LAX99LA050), Dec 14, 1998: Boeing 737-300 (N328AW), Sacramento, CA, no damage. Probable cause: The failure of the second and third flight attendants to comply with instructions to remain seated in anticipation of turbulence. ## FAA accident and incident reports None matched to N328AW. ## Reports on N328AW not matched to an aircraft (2) They name N328AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20020329013099I](https://openairdocs.org/incident/20020329013099I), Mar 29, 2002: Boeing 7373B7 (N328AW), Omaha, NE. (-23) America west flight 332 departed Omaha, NE, enroute to phoenix, AZ. The aircraft encountered turbulence during climb and the crew received a number two… - [Accident 19981213041989A](https://openairdocs.org/incident/19981213041989A), Dec 13, 1998: Boeing 7373B7 (N328AW), Sacramento, CA. (-23) During descent into smf on flight for sna, aircraft encountered moderate to severe turbulence. Two flight attendents at aft galley area were thrown to… ## 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 N328AW not matched to an aircraft (125, newest 50) They name N328AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AWXA200600353](https://openairdocs.org/sdr/AWXA200600353), Feb 20, 2006: SKIN. CRACKED. MCN - DURING C24 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT BS 943 AND STR 24L. MAINTENANCE REPAIRED SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5360 - [SDR AWXA200600345](https://openairdocs.org/sdr/AWXA200600345), Feb 20, 2006: SKIN. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION BULGE ON FUSELAGE EXTERIOR SKIN AT BS 1006 AND STR 27R. MAINTENANCE REPAIRED IAW AMERICA WEST AIRLINES ENGINEERING R - [SDR AWXA200600380](https://openairdocs.org/sdr/AWXA200600380), Jan 19, 2006: SHEAR TIE. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE UPPER SURFACE OF SHEAR TIE AT BS 967 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW REPLACEMENT SH - [SDR AWXA200600312](https://openairdocs.org/sdr/AWXA200600312), Jan 19, 2006: SHEAR TIE. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION ON SHEAR TIE AT BS 987 AND BL 6R ON LOWER SURFACE. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 987 AND BL - [SDR AWXA200600393](https://openairdocs.org/sdr/AWXA200600393), Jan 18, 2006: STRINGER. CORRODED. MCN - MAJOR REPAIR - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON STR 25R AT BS 960 TO BS 1020. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 7 - [SDR AWXA200600313](https://openairdocs.org/sdr/AWXA200600313), Jan 17, 2006: SHEAR TIE. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION ON SHEAR TIE AT BS 986 AND BL 16R ON LOWER SURFACE. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 986 AND BL - [SDR AWXA200600392](https://openairdocs.org/sdr/AWXA200600392), Jan 15, 2006: BULKHEAD. CANNING. MCN - DURING C24 CHECK, DISCOVERED THE AFT PRESSURE BULKHEAD OIL CANNING JUST ABOVE STR 24L AT BS 1016, END FITTING BELOW APU DUCT. MAINTENANCE FABRICATED REPAI - [SDR AWXA200600391](https://openairdocs.org/sdr/AWXA200600391), Jan 14, 2006: DOOR FRAME. CRACKED. MCN - DURING C24 CHECK DISCOVERED 2 CRACKS, .5 INCHES IN LENGTH EACH, ON THE L1 DOOR FRAME ADJACENT TO THE 7TH FROM THE TOP AFT STOP FITTING AND ON THE INTERIOR - [SDR AWXA200600318](https://openairdocs.org/sdr/AWXA200600318), Jan 14, 2006: ANGLE. CRACKED. MCN - DURING C24 CHECK DISCOVERED L1 DOOR FRAME ANGLE CRACKED, .5 INCHES, AT 7TH FROM TOP AFT STOP FITTING. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLAC - [SDR AWXA200600315](https://openairdocs.org/sdr/AWXA200600315), Jan 14, 2006: SHEAR TIE. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON SHEAR TIE AT BS 1006, BL 0 AND BETWEEN STR 27L AND STR 27R. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR T - [SDR AWXA200600307](https://openairdocs.org/sdr/AWXA200600307), Jan 13, 2006: SKIN. CRACKED. MCN - DURING C24 CHECK DISCOVERED 6 CRACKS, .189 INCHES LONG, ON THE BOTTOM OF THE NR 4 SLAT SKIN BELOW THE OUTBOARD AUXILIARY TRACK FROM SS 80R TO SS 100R. MAI - [SDR AWXA200600306](https://openairdocs.org/sdr/AWXA200600306), Jan 13, 2006: CHANNEL. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON STR 26L CHANNEL AT BS 540. MAINTENANCE REMOVED FABRICATED AND REPLACED STR 26L CHANNEL AT BS 540 IAW B737 - [SDR AWXA200600379](https://openairdocs.org/sdr/AWXA200600379), Jan 12, 2006: FRAME. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON FRAME AT BS 1006 AND BL 0. MAINTENANCE REMOVED DAMAGE FROM FRAME AT BS 1006 IAW BOEING 737-300 SRM 53-00- - [SDR AWXA200600327](https://openairdocs.org/sdr/AWXA200600327), Jan 12, 2006: SILL. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE UPPER SURFACE OF THE R1 LOWER SILL WEB AT BS 294.5 TO BS 332.1, BL 60R AND WL 208. MAINTENANCE REMOVE - [SDR AWXA200600325](https://openairdocs.org/sdr/AWXA200600325), Jan 12, 2006: WEB. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION ON WEB LOCATED AT BS 794 TO BS 821 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW WEB FROM BS 794 TO BS 821 AND B - [SDR AWXA200600321](https://openairdocs.org/sdr/AWXA200600321), Jan 12, 2006: STIFFENER. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON 3 ZEE STIFFENERS SUPPORTS FOR THE R1 DOOR THRESHOLD PLATE, FROM BS 312 TO BS 328, WL 208 AND BL 62R. MAIN - [SDR AWXA200600320](https://openairdocs.org/sdr/AWXA200600320), Jan 12, 2006: SILL. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON MOD REPAIR ANGLE BELOW THE R1 LOWER SILL, AFT SIDE OF FRAME AT BS 294.5, WL 208 AND FROM BL 43R TO BL 60R - [SDR AWXA200600319](https://openairdocs.org/sdr/AWXA200600319), Jan 12, 2006: STRAP. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION AROUND NUT PLATE HOLES ON STRAP FROM BS 799 TO BS 835, BL 0R AND BENT AT BS 821. CORROSION WAS FOUND OUT OF - [SDR AWXA200600316](https://openairdocs.org/sdr/AWXA200600316), Jan 12, 2006: ATTACH ANGLE. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION ON WEB ATTACH ANGLE AT BS 847, WL 157 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW WEB ATTACH ANGLE AT BS 847, - [SDR AWXA200600305](https://openairdocs.org/sdr/AWXA200600305), Jan 12, 2006: DOUBLER. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON DOUBLER ON UPPER SIDE OF B/S FRAME 294.5, BL 57R AND RT OUTBOARD END AT CIRCUMFERENTIAL. MAINTENANCE REMO - [SDR AWXA200600389](https://openairdocs.org/sdr/AWXA200600389), Jan 10, 2006: FLOORBEAM. CRACKED. MCN - DURING C24 CHECK DISCOVERED FLOORBEAM CRACKED, .25 INCHES, AT BS 663 AND BL 24L. MAINTENANCE STOP DRILLED CRACK IAW AMERICA WEST AIRLINES (AWA) ENGINEERIN - [SDR AWXA200600376](https://openairdocs.org/sdr/AWXA200600376), Jan 10, 2006: CLIP. CRACKED. MCN - DURING C24 CHECK DISCOVERED INTERCOSTAL SUPPORT CLIP CRACKED. 500 INCHES IN LENGTH, AT BS 693.75, WL 207 AND BL. 25L. MAINTENANCE REMOVED, FABRICATED AND - [SDR AWXA200600372](https://openairdocs.org/sdr/AWXA200600372), Jan 10, 2006: ANGLE. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE R1 INNER CHORD AT BS 294 TO BS 300 AND BS 333 AT BL 59R AND WL 208. MAINTENANCE REMOVED AND INSTALLED - [SDR AWXA200600332](https://openairdocs.org/sdr/AWXA200600332), Jan 10, 2006: STRINGER CLIP. CRACKED. MCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .125 INCHES IN LENGTH, AT BS 847 AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS - [SDR AWXA200600330](https://openairdocs.org/sdr/AWXA200600330), Jan 10, 2006: STRINGER CLIP. CRACKED. MCN - DURING C24 CHECK DISCOVERED TWO INTERCOSTAL SUPPORT CLIPS CRACKED, .4 INCHES, AT BS 693.75 AND BL .25R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPL - [SDR AWXA200600326](https://openairdocs.org/sdr/AWXA200600326), Jan 10, 2006: SILL. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE BOTTOM SURFACE OF THE R1 LOWER SILL WEB AT BS 297, BL 60R AND WL 208. MAINTENANCE REMOVED, FABRICATED - [SDR AWXA200600322](https://openairdocs.org/sdr/AWXA200600322), Jan 10, 2006: ANGLE. CRACKED. MCN - DURING C24 CHECK DISCOVERED STIFFENER ANGLE CRACKED, .25 INCHES, AT BS 277 AND STR 12R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENE - [SDR AWXA200600311](https://openairdocs.org/sdr/AWXA200600311), Jan 10, 2006: SKIN. DEBONDED. MCN - DURING C24 CHECK DISCOVERED DISBOND AREA ON THE RT OUTBOARD AFT FLAP TRAILING EDGE, SEPERATING 8" AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND - [SDR AWXA200600309](https://openairdocs.org/sdr/AWXA200600309), Jan 10, 2006: SKIN. DEBONDED. MCN - DURING C24 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD AFT CORNER OF THE RT INBOARD AFT FLAP, UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DISBOND SKIN - [SDR AWXA200600378](https://openairdocs.org/sdr/AWXA200600378), Jan 9, 2006: FRAME. CRACKED. MCN - DURING C24 CHECK DISCOVERED MAIN CABIN FRAME AT BS 663 CRACKED .5 INCHES IN LENGTH AT STR 2R. MAINTENANCE ROUTED OUT DAMAGED AREA IAW BOEING 737-300 SRM 5 - [SDR AWXA200600334](https://openairdocs.org/sdr/AWXA200600334), Jan 9, 2006: ATTACH ANGLE. CORRODED. DURING C24 CHECK DISCOVERED CORROSION ON THE R1 LOWER SILL, INBOARD ATTACH ANGLE FROM BS 304 TO BS 324, BL 62R AND WL 209. CORROSION WAS FOUND TO BE OUT OF LIMI - [SDR AWXA200600333](https://openairdocs.org/sdr/AWXA200600333), Jan 9, 2006: STRINGER CLIP. CRACKED. MCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .125 INCHES IN LENGTH, AT BS 616 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS - [SDR AWXA200600331](https://openairdocs.org/sdr/AWXA200600331), Jan 9, 2006: STRINGER CLIP. CRACKED. MCN - DURING C24 CHECK DISCOVERED TWO STRINGER CLIPS CRACKED, .125 INCHES IN LENGTH EACH, AT BS 639 STR 2L AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW STR - [SDR AWXA200600329](https://openairdocs.org/sdr/AWXA200600329), Jan 9, 2006: STRINGER CLIP. CRACKED. MCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES, AT BS 663 AND STR 10L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER T - [SDR AWXA200600323](https://openairdocs.org/sdr/AWXA200600323), Jan 9, 2006: FRAME. CRACKED. MCN - DURING C24 CHECK DISCOVERED MAIN CABIN FRAME AT BS 616 CRACKED, 2.2 INCHES, AT RT SIDE BOTTOM END, UNDER MAIN CABIN FLOOR AT BL 60R AND WL 200. MAINTENANC - [SDR AWXA200600314](https://openairdocs.org/sdr/AWXA200600314), Jan 9, 2006: SHEAR TIE. CRACKED. MCN - DURING C24 CHECK DISCOVERED BS 328 FRAME SHEAR TIE CRACKED, .25 INCHES, OUTBOARD SIDE OF STRINGER 28L. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT - [SDR AWXA200600374](https://openairdocs.org/sdr/AWXA200600374), Jan 8, 2006: SPAR. CRACKED. MCN - DURING C24 CHECK DISCOVERED RT HORIZONTAL STAB LEADING EDGE SPAR WEB CRACKED, .890 INCHES IN LENGTH, AT THE THIRD LIGHTENING HOLE FROM THE OUTBOARD END AT - [SDR AWXA200600328](https://openairdocs.org/sdr/AWXA200600328), Jan 8, 2006: DOOR FRAME. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION ON THE AFT CARGO COMPARTMENT DOOR, LOWER DOOR SURROUND STRUCTURE WEB FROM BS 800 TO BS 847, WL 158 AND FROM BL 17R T - [SDR AWXA200600324](https://openairdocs.org/sdr/AWXA200600324), Jan 8, 2006: FRAME. CORRODED. MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOOR FRAME, LOWER ATTACH AND FORWARD SIDE AT BS 727C AND STR 26L. MAINTENANCE CUT OUT DAMAGED PORTION OF - [SDR AWXA200600308](https://openairdocs.org/sdr/AWXA200600308), Jan 8, 2006: STRINGER. CORRODED. MCN - DURING C24 CHECK DISCOVERED CORROSION ON STRINGER 26R FROM BS 1006 TO BS 1012. MAINTENANCE REMOVED STRINGER AND FABRICATED REPLACEMENT STRINGER IAW BOEING - [SDR AWXA200600317](https://openairdocs.org/sdr/AWXA200600317), Jan 7, 2006: ATTACH ANGLE. CRACKED. MCN - DURING C24 CHECK DISCOVERED CRACK, 1.1 INCHES LONG, ON THE R1 DOOR LOWER FORWARD TORQUE BOX FLOOR WEB ATTACH ANGLE AT BS 298, WL 208 AND BL 53R. MAINTENAN - [SDR AWXA200600310](https://openairdocs.org/sdr/AWXA200600310), Jan 6, 2006: WEDGE. DEBONDED. MCN - DURING C24 CHECK DISCOVERED DISBOND AREA ON THE LT INBOARD AFT FLAP AT THE OUTBOARD CORNER, UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DISBOND SKIN AND - [SDR AWXA200600390](https://openairdocs.org/sdr/AWXA200600390), Jan 5, 2006: WIRE HARNESS. DAMAGED. MCN - EEL - DURING C34 CHECK, DISCOVERED ESCAPE PATH WIRING HARNESS WITH MULTIPLE DAMAGED CONNECTORS FROM BS 344 TO BS 947 AT WL 208. MAINTENANCE REPAIRED THE E - [SDR AWXA200501496](https://openairdocs.org/sdr/AWXA200501496), Dec 11, 2005: SKIN. CRACKED. PHX - DURING INSPECTION DISCOVERED FUSELAGE SKIN CRACK, 1.0 INCHES LONG, ON THE LT SIDE OF THE AIRCRAFT JUST AFT OF WING TO BODY FAIRING BELOW STRINGER 23L AND - [SDR AWXA200501480](https://openairdocs.org/sdr/AWXA200501480), Dec 3, 2005: LIGHT. INOPERATIVE. EEL - DURING INSPECTION DISCOVERED EMERGENCY LIGHT AT ROW 5, LT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. - [SDR AWXA200600254](https://openairdocs.org/sdr/AWXA200600254), Oct 10, 2005: DOOR. DAMAGED. PHX - DISCOVERED PREVIOUS BLEND OUT AT STA 1088, ABOVE THE FORWARD RT CORNER OF THE APU DOOR. WAS DETERMINED TO BE CHAFFING DAMAGE ABOUT 6" AFT OF STA 1088 AT S - [SDR AWXA200501089](https://openairdocs.org/sdr/AWXA200501089), Sep 21, 2005: BATTERY. INOPERATIVE. PHX - EEL - CREW REPORTED TO MAINTENANCE THE FORWARD GALLEY FLASH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGH - [SDR AWXA200500765](https://openairdocs.org/sdr/AWXA200500765), Jun 28, 2005: STIFFENER. CORRODED. DURING C-13 CHECK FOUND CORROSION PRESENT ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD FORWARD SIDE AT BS 1016, WL 155, BL 0. CORROSION REMOVED AND FOU - [SDR AWXA200500730](https://openairdocs.org/sdr/AWXA200500730), Jun 17, 2005: THRESHOLD. CORRODED. DURING C-13 CHECK, FOUND CORROSION IN FORWARD CARGO PIT ON 20 NUT PLATES LOCATED ON THRESHOLD WEB FROM STA 450 TO STA 490. MX FOUND CORROSION TO BE OUT OF LIMIT - [SDR AWXA200500754](https://openairdocs.org/sdr/AWXA200500754), Jun 16, 2005: INTERCOSTAL. CRACKED. DURING C-13 CHECK FOUND INTERCOSTAL CRACKED, .25 INCHES IN LENGTH INSIDE FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, All 125: https://openairdocs.org/aircraft/N328AW/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other DJI AGRAS T30 aircraft: https://openairdocs.org/model/dji-agras-t30/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.