# N16892: Yuneec TYPHOON H - Status: Valid registration - Airframe: [Yuneec TYPHOON H](https://openairdocs.org/model/yuneec-typhoon-h) (registry code 06101WR) - Serial number: YU16321261B08A01 - Type: Rotorcraft - Engine type: Electric - Certificate issued: December 30, 2020 - Expires: December 31, 2027 - Mode S code: A11314 - Registered owner: [Digital Aeroimaging Services LLC](https://openairdocs.org/faa-owner/DIGITAL%20AEROIMAGING%20SERVICES%20LLC) - Location: [Las Cruces, NM](https://openairdocs.org/faa-place/NM/Las%20Cruces) - Owner type: LLC - Owner's area on the map: 32.3788° N, 106.5762° W: Placed by OpenAirDocs at the center of ZIP code 88011, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16892 - Page: https://openairdocs.org/aircraft/N16892 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 (Yuneec TYPHOON H) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N16892. ## FAA accident and incident reports None matched to N16892. ## 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 N16892 not matched to an aircraft (28) They name N16892, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR GTIA020277](https://openairdocs.org/sdr/GTIA020277), Apr 30, 2002: DOOR. OUT OF ADJUST. FLT 909 - LGA - LEFT MAIN GEAR INDICATES UNLOCK WITH DOOR LIGHT OUT. COMPLIED WITH QRH PROCEDURES. ADJUSTED LEFT MLG FLYAWAY DOOR. (M) - [SDR GTIA020391](https://openairdocs.org/sdr/GTIA020391), Apr 26, 2002: BATTERY. DISCHARGED. FLL - FLT 197 - FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROW 1 TO ROW 6. REPLACED EMERGENCY BATTERY FOR CEILING EMERGENCY LIGHTS SEAT ROW 1 TO ROW 6. OPS - [SDR GTIA020390](https://openairdocs.org/sdr/GTIA020390), Apr 26, 2002: LIGHT. INOPERATIVE. FLL - FLT 197 - FOUND FORWARD ENTRY DOOR WALK AROUND EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY DOOR WALK AROUND EMERGENCY LIGHT ASSEMBLY. - [SDR GTIA020299](https://openairdocs.org/sdr/GTIA020299), Apr 18, 2002: SENSOR. DIRTY. LAX - FLT 906 - ON DEPARTURE FROM DTW, GOT LEFT GEAR UNSAFE LIGHT ALL OTHER LIGHTS OUT PASSING THROUGH 20,000 FEET GOT GEAR DOOR OPEN LIGHT. APPEARS MECH LATCH - [SDR GTIA020289](https://openairdocs.org/sdr/GTIA020289), Apr 11, 2002: PROXIMITY SWITCH. FAILED. LGA - FLT 1774 - AFTER GEAR RETRACTION LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED QRH PROCEDURES. RED LIGHT REMAINED ILLUMINATED NO VIBRATION, SUSPE - [SDR GTIA020271](https://openairdocs.org/sdr/GTIA020271), Apr 2, 2002: CONNECTOR. CONTAMINATED. DTW - FLT 906 - CLIMBING OUT AT 14,000 FEET GEAR DOOR OPEN LIGHT CAME ON AND LEFT MAIN GEAR LIGHT CAME ON. HYDRAULIC PUMP TO HI, DOOR LIGHT WENT OUT. RECYCLED G - [SDR GTIA020247](https://openairdocs.org/sdr/GTIA020247), Mar 23, 2002: PROXIMITY SENSOR. DIRTY. DTW - FOUND AFTER DEPARTURE DURING GEAR RETRACTION, GOT A RED UNSAFE LIGHT ON THE LEFT MAIN. RECYCLED THE GEAR AND HAD NORMAL INDICATIONS. CLEAN PROXIMITY SENSO - [SDR GTIA020248](https://openairdocs.org/sdr/GTIA020248), Mar 23, 2002: SWITCH. FAULTY. DTW - FLT 909 - ALTERNATE TRIM MOTO TRIMS WHEN RIGHT SWITCH IS MOVED. LEFT SWITCH IN CENTER POSITION, RIGHT SWITCH ALONE WILL MOVE TRIM IN BOTH DIRECTIONS. REMO - [SDR GTIA020249](https://openairdocs.org/sdr/GTIA020249), Mar 22, 2002: LIGHT. OUT OF POSITION. DTW - SAFETY GLOW FLOOR PATH LIGHTING HAS NO BREAKS AT LEFT OVERWING EXITS. REPOSITIONED SAFETY GLOW FLOOR PATH LIGHTING AT LEFT OVERWING EXITS IAW SPIRIT AIRLI - [SDR CALA9901534](https://openairdocs.org/sdr/CALA9901534), Nov 24, 1999: LONGERON. CRACKED. INSPECTION FOUND A 1.125 CRACK IN LONGERON 2L AT BELTFRAME 1418. REPAIRED IAW ECRA 5310-03950. - [SDR CALA9901533](https://openairdocs.org/sdr/CALA9901533), Nov 24, 1999: LONGERON. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R AT BELTFRAME 1418. REPAIRED IAW SRM 53-02, FIGURE 18. - [SDR CALA9901530](https://openairdocs.org/sdr/CALA9901530), Nov 23, 1999: DOOR PAN. WORN. INSPECTION FOUND MAIN BAGGAGE BIN DOOR INNER PAN WORN THROUGH AT AFT LOCKING CAM. A DOUBLER WAS INSTALLED IAW ECRA 5230-01502. - [SDR CALA9901510](https://openairdocs.org/sdr/CALA9901510), Nov 17, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND CAPTAIN'S RT AFT SEAT TRACK I/B SIDE CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. - [SDR CALA9901508](https://openairdocs.org/sdr/CALA9901508), Nov 17, 1999: CABLES. OUT OF ADJUST. THE INTERIOR AND EXTERIOR TAIL CONE RELEASE HANDLES REQUIRED EXCESS FORCE TO DEPLOY TAIL CONE. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-01. - [SDR CALA9901507](https://openairdocs.org/sdr/CALA9901507), Nov 16, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 229-237. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F. - [SDR CALA9901501](https://openairdocs.org/sdr/CALA9901501), Nov 15, 1999: JAMB. CORRODED. INSPECTION FOUND FORWARD BAGGAGE BIN DOOR JAMB PAN CORRODED AT STA 370-427. THE CORRODED PAN SECTION WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, - [SDR CALA9901495](https://openairdocs.org/sdr/CALA9901495), Nov 12, 1999: BEAM. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31. - [SDR CALA9900124](https://openairdocs.org/sdr/CALA9900124), Feb 10, 1999: BATTERIES. DISCHARGED. INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHT IDENTIFIERS INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9800189](https://openairdocs.org/sdr/CALA9800189), Feb 5, 1998: RETRACT MECH. ICED UP. THE LANDING GEAR HANDLE WOULD NOT GO DOWN UPON GEAR EXTENSION ON APPROACH TO DEN. THE GEAR WAS EXTENDED USING THE EMERGENCY GEAR EXTENSION HANDLE. THE REGULAR G - [SDR CALA9701641](https://openairdocs.org/sdr/CALA9701641), Nov 19, 1997: CABLE. OUT OF ADJ. THE TAIL CONE DROP TEST USING EXTERIOR RELEASE HANDLE WAS BELOW 25 MINIMUM PULL. THE TAIL CONE RELEASE SYSTEM WAS ADJUSTED IAW MM 53-53-00. THE TAIL CONE RELEAS - [SDR CALA9701158](https://openairdocs.org/sdr/CALA9701158), Jul 24, 1997: BRAKE ROD. BROKEN. THE CAPTAIN'S LEFT BRAKE/RUDDER PEDAL SNAPPED DURING TAXI OUT. THERE WAS NO BRAKE CONTROL FROM THAT PEDAL, BUT OPERATION WAS GOOD FROM FIRST OFFICER'S SEAT. THE - [SDR CALA9700585](https://openairdocs.org/sdr/CALA9700585), Apr 21, 1997: SKIN. BIRD STRIKE. CREW ADVISED OF BIRD STRIKE, INSPECTION FOUND STRIKE AT LS FWD FUSELAGE ON PRESSURIZED NOSE REGION. EXTERNAL REPAIR AS PER SRM 53-04 FIG 12B SHEET 14. REQUESTED - [SDR CALA9601137](https://openairdocs.org/sdr/CALA9601137), Aug 7, 1996: T3 BLADE. BROKEN. A LOUD BANG WAS HEARD AND THE AIRCRAFT EXPERIENCED VIBRATION DURING CLIMBOUT.T HE NR 1 ENGINE N1 AND N2 BOTH SPOOLED DOWN AND EGT ROSE TO APPROXIMATELY 630 DEGR - [SDR CALA9601015](https://openairdocs.org/sdr/CALA9601015), Jul 13, 1996: DUCT. BLOWN. THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF. THE BELL WAS SILENCED AND WHEN THE NR 1 ENGINE THROTTLE WAS RETARDED, THE LIGHT EXTINGUISHE - [SDR CAL951155](https://openairdocs.org/sdr/CAL951155), Dec 1, 1995: BRACKET. CRACKED. HOU - INSPECTION FOUND A 3 INCH CRACK IN BRACKET AT LT OUTBOARD END OF FLOOR BEAM, STA 845, LONGERON 18. THE BRACKET WAS REMOVED AND REPLACED. (X) - [SDR CAL951156](https://openairdocs.org/sdr/CAL951156), Nov 28, 1995: DOOR JAMB. CRACKED. HOU - INSPECTION FOUND A .50 INCH CRACK AT INBOARD END OF LT WHEELWELL FORWARD DOOR JAMB, STA 946. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SR - [SDR CAL951153](https://openairdocs.org/sdr/CAL951153), Nov 28, 1995: BRACKET. CRACKED. HOU - INSPECTION F0UND A .75 INCH CRACK IN LT KEEL BEAM BRACKET AT STA 946. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5. (X) - [SDR CAL951062](https://openairdocs.org/sdr/CAL951062), Nov 21, 1995: HYD PUMP. LEAKING. FLT 0545 - IAH - THE RIGHT HYDRAULIC QUANTITY DROPPED WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N16892 The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N16892 before. - [Cancelled 1969-08-19](https://openairdocs.org/deregistered/N16892-1969-08-19): Douglas C-47, S/N 27129. Exported to Indonesia. Owner: [Stan Air Inc](https://openairdocs.org/faa-owner/STAN%20AIR%20INC), [Fresno, CA](https://openairdocs.org/faa-place/CA/Fresno) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N16892-undated): Bell 206B, S/N 2265. N-number assigned, not yet registered ## Related - Other Yuneec TYPHOON H aircraft: https://openairdocs.org/model/yuneec-typhoon-h/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.