# N777AU: 2022 Diamond Aircraft Ind DA 62

- Status: Valid registration
- Airframe: [Diamond Aircraft Ind DA 62](https://openairdocs.org/model/diamond-aircraft-ind-da-62) (registry code 2990106, 7 seats)
- Engine: [Austro E4P(SERIES)](https://openairdocs.org/engine/austro-e4p-series) (registry code 06405)
- Data sheets: [TCDS E00081EN](https://openairdocs.org/tcds/E00081EN) (Austro Engine GmbH) (OpenAirDocs)
- Serial number: 62.199
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: 4 cycle
- Airworthiness: Standard, normal
- Airworthiness date: July 8, 2022
- Certificate issued: September 14, 2022
- Expires: September 30, 2029
- Mode S code: AA831B
- Registered owner: [777au LLC](https://openairdocs.org/faa-owner/777AU%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: LLC
- Owner's area on the map: 25.9660° N, 80.1399° W: Placed by OpenAirDocs at the center of ZIP code 33180, 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=777AU
- Page: https://openairdocs.org/aircraft/N777AU

From the FAA registry file of October 27, 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): 11 in force

### Matched by airframe (Diamond Aircraft Ind DA 62)

- [AD 2024-07-03](https://openairdocs.org/ad/2024-07-03): Horizontal Stabilizer Structure · Diamond Aircraft Industries DA 62. Effective Apr 24, 2024
- [AD 2023-22-18](https://openairdocs.org/ad/2023-22-18): Cargo Compartments · Diamond Aircraft Industries DA 62. Effective Jan 19, 2024

### Matched by engine (Austro E4P(SERIES))

- [AD 2025-02-12](https://openairdocs.org/ad/2025-02-12): Reciprocating Engine Cylinder Section; Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Apr 1, 2025
- [AD 2024-19-10](https://openairdocs.org/ad/2024-19-10): Engine (Reciprocating) · Austro Engine E4 and E4P. Effective Oct 9, 2024
- [AD 2024-05-01](https://openairdocs.org/ad/2024-05-01): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Mar 11, 2024
- [AD 2022-03-03](https://openairdocs.org/ad/2022-03-03): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Feb 14, 2022
- [AD 2021-24-10](https://openairdocs.org/ad/2021-24-10): Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Dec 27, 2021
- [AD 2021-17-01](https://openairdocs.org/ad/2021-17-01): Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Aug 23, 2021
- [AD 2020-22-14](https://openairdocs.org/ad/2020-22-14): Reciprocating Engine Supercharger · Austro Engine E4 and E4P. Effective Dec 10, 2020
- [AD 2020-15-05](https://openairdocs.org/ad/2020-15-05): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Aug 31, 2020
- [AD 2020-14-07](https://openairdocs.org/ad/2020-14-07): Fuel Control/Reciprocating Engines and Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Aug 25, 2020

### Historical (superseded or no longer in force)

- [AD 2023-20-03](https://openairdocs.org/ad/2023-20-03) (historical): Reciprocating Engine Cylinder Section, Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Dec 11, 2023
- [AD 2021-22-20](https://openairdocs.org/ad/2021-22-20) (historical): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Nov 16, 2021
- [AD 2021-09-04](https://openairdocs.org/ad/2021-09-04) (historical): Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective May 10, 2021
- [AD 2018-18-02](https://openairdocs.org/ad/2018-18-02) (historical): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Nov 29, 2018
- [AD 2018-07-16](https://openairdocs.org/ad/2018-07-16) (historical): Reciprocating Engine Supercharger · Austro Engine E4 and E4P. Effective Apr 27, 2018

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N777AU.

## FAA accident and incident reports

None matched to N777AU.

## Reports on N777AU not matched to an aircraft (2)

They name N777AU, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19920709027759I](https://openairdocs.org/incident/19920709027759I), Jul 9, 1992: Boeing 7374B7 (N777AU), Syracuse, NY. Severe turbulence on descent. Flight attendant injured. Taken to hospital. Aircraft released for service.
- [Incident 19911003049889I](https://openairdocs.org/incident/19911003049889I), Oct 3, 1991: Boeing 7374B7 (N777AU), Baltimore, MD, Minor damage. Pilot landed on displaced threshold of runway. Aircraft hit concrete blocks. Runway notamed closed.

## 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 N777AU not matched to an aircraft (48)

They name N777AU, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR USAA060582](https://openairdocs.org/sdr/USAA060582), Apr 10, 2006: WEDGE. DEBONDED. UPPER SURFACE T/E WEDGE OUTBOARD END DISBOND. PREVIOUSLY INSTALLED DOUBLER IAW SRM 51-70-10 AND TYP 57-42-02, DEFECT SIZE: 1.5 X 2 INCH.
- [SDR USAA060583](https://openairdocs.org/sdr/USAA060583), Apr 10, 2006: STRUCTURE. DAMAGED. INBOARD T/E UPPER SURFACE OF NR 5 SLAT COMPOSITE. REPAIRED PER T/R 57-42-02/04, DEFECT SIZE: 5 X 7 INCH.
- [SDR USAA060557](https://openairdocs.org/sdr/USAA060557), Apr 3, 2006: HINGE. DAMAGED. STAB FASTENER HOLE AT NR 6 BEARING HINGE ELONGATED. OVERSIZED HOLES AND TREATED AREA IAW TR 55-50-01A, DEFECT SIZE: .031 INCH.
- [SDR USAA060556](https://openairdocs.org/sdr/USAA060556), Apr 3, 2006: SKATE ANGLE. WORN. RT VERT STAB SKATE ANGLE HAS WEAR. REMOVED DAMAGE, INSTALLED FABRICATED REPAIR PARTS IAW TR 53-20-05, DEFECT SIZE: 3 X 1 INCH.
- [SDR USAA060555](https://openairdocs.org/sdr/USAA060555), Apr 3, 2006: SKATE ANGLE. WORN. RT VERT STAB SKATE ANGLE WEAR. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 53-20-05, DEFECT SIZE: 3 X 1 INCH.
- [SDR USAA060554](https://openairdocs.org/sdr/USAA060554), Apr 3, 2006: HINGE. DAMAGED. STAB FASTENER HOLE AT NR 6 BEARING HINGE ELONGATED. OVERSIZED HOLES AND TREATED AREA IAW TR 55-50-01A, DEFECT SIZE: .0312 INCH.
- [SDR USAA060553](https://openairdocs.org/sdr/USAA060553), Apr 3, 2006: SKIN. DEBONDED. SLAT LOWER SIDE INBOARD EDGE DISBOND. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 X 3 INCH.
- [SDR USAA060540](https://openairdocs.org/sdr/USAA060540), Apr 3, 2006: CARGO TRACK. CORRODED. STA 787-847 RT TRACK CORROSION. FAB NEW TRACK AND INSTALL IAW SRM 53-60-53, DEFECT SIZE: 1.0 INCH.
- [SDR USAA060539](https://openairdocs.org/sdr/USAA060539), Apr 3, 2006: SKIN. DENTED. STA 480 S26R DENTED. REMOVED DAMAGE, INSTALLED DOUBLER AND TRIPLER REPAIR PARTS IAW EA 97535, DEFECT SIZE: 3.0"X1.25"X.095".
- [SDR USAA060549](https://openairdocs.org/sdr/USAA060549), Apr 3, 2006: SKIN. DEBONDED. SLAT LOWER SIDE INBOARD EDGE DISBOND. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 X 3 INCHES.
- [SDR USAA060541](https://openairdocs.org/sdr/USAA060541), Apr 3, 2006: ANGLE. CRACKED. RT WING 135.5 RIB LOWER CHORD ANGLE AT AFT END IN VERTICAL LEG CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EA 97533, DEFECT SIZE: .50
- [SDR USAA060542](https://openairdocs.org/sdr/USAA060542), Apr 3, 2006: WEDGE. DELAMINATED. T/E WEDGE OUTBOARD END DELAMINATED. INSTALLED REPAIR IAW EA 97548, DEFECT SIZE: 11.0" X 6.5".
- [SDR USAA060543](https://openairdocs.org/sdr/USAA060543), Apr 3, 2006: SKIN. WORN. BS 879-887 WL 306.5 RBL 3 SKIN HAS FRETTING WEAR. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-60-01 EA 97537, DEFECT SIZE: 9" X .250" X .010".
- [SDR USAA060547](https://openairdocs.org/sdr/USAA060547), Apr 3, 2006: FRAME. DENTED. BS 767 S-24L FRAME DENTED. DOUBLER INSTALLED PER TR 53-60-07, DEFECT SIZE: .500 X .500 INCH.
- [SDR USAA060538](https://openairdocs.org/sdr/USAA060538), Apr 3, 2006: ANGLE. CORRODED. STA 303-360 LBL 55 CORROSION. REMOVED AND REPLACED Z-ANGLE IAW SRM 53-10-15, DEFECT SIZE: 58 INCHES.
- [SDR USAA060515](https://openairdocs.org/sdr/USAA060515), Mar 24, 2006: FRAME. CRACKED. BS 400 BETWEEN S8R AND 9R CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20D, DEFECT SIZE: .5 INCH.
- [SDR USAA060516](https://openairdocs.org/sdr/USAA060516), Mar 24, 2006: FRAME. CRACKED. BS 440 BETWEEN STRINGERS 8R AND 9R CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20D, DEFECT SIZE: .5 INCH.
- [SDR USAA060484](https://openairdocs.org/sdr/USAA060484), Mar 22, 2006: FRAME. CRACKED. STA 294, S10R CRACKED. REMOVE AND REPLACE CHORD IAW SRM 51-10-02, DEFECT SIZE: .750 INCH.
- [SDR USAA060477](https://openairdocs.org/sdr/USAA060477), Mar 22, 2006: SPLICE. CRACKED. STRINGER 4L AT LAP SPLICE, STA 907 CRACKED. PART REPLACED WITH IDENTICAL PART, REPLACED SPLICE IAW SRM 51-40-02, DEFECT SIZE: .25" X .50".
- [SDR USAA060478](https://openairdocs.org/sdr/USAA060478), Mar 22, 2006: SPLICE. CRACKED. THE 4R AT LAP SPLICE , STA 907 CRACKED. DEFECTIVE PART, REPLACED WITH IDENTICAL PART, INSTALLED NEW SPLICE IAW SRM 51-40-02, DEFECT SIZE: .250 INCH.
- [SDR USAA060479](https://openairdocs.org/sdr/USAA060479), Mar 22, 2006: STRINGER CLIP. CRACKED. STA 294, S11L CRACKED. MFG NEW TIE CLIP AND INSTALLED IAW DWG 65-45808, DEFECT SIZE: 1 INCH.
- [SDR USAA060480](https://openairdocs.org/sdr/USAA060480), Mar 22, 2006: INTERCOSTAL. CRACKED. CRACK IN RADIUS OF INTERCOSTAL FWD LEFT SIDE AT STA 294.5 STR 11L. FABRICATED NEW INTERCOSTAL AND INSTALLED IAW DWG 65-1768, DEFECT SIZE: .025 INCH.
- [SDR USAA060481](https://openairdocs.org/sdr/USAA060481), Mar 22, 2006: ATTACH ANGLE. CRACKED. STA 360 STR 8L CRACKED. REMOVED ANGLE, FABRICATED AND INSTALLED NEW PART IAW DWG 90-7813, DEFECT SIZE: 1 INCH.
- [SDR USAA060483](https://openairdocs.org/sdr/USAA060483), Mar 22, 2006: FRAME. CRACKED. STA 294 S11R CRACKED. REMOVED DAMAGED PART, INSTALLED REPAIR PART IAW SRM 51-10-02, DEFECT SIZE: .500.
- [SDR USAA060482](https://openairdocs.org/sdr/USAA060482), Mar 22, 2006: SILL. CORRODED. SILL WEB STA 794.3 TO 847 CORROSION. REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: 12" X 2".
- [SDR USAA060452](https://openairdocs.org/sdr/USAA060452), Mar 15, 2006: ANGLE. CORRODED. STA 961 TO 997.5 AFT ENTRY DOOR CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REPLACED Z-ANGLE IAW 51-10-2.
- [SDR USAA060451](https://openairdocs.org/sdr/USAA060451), Mar 14, 2006: SKIN. WORN. BS 879 TO BS 887 WL 306.5 RBL 3 UNDER DORSAL FIN FAIRING HAS WEAR. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-60-01, DEFECT SIZE: 9 X .250 X .010 INCH DEE
- [SDR USAA060450](https://openairdocs.org/sdr/USAA060450), Mar 13, 2006: CLIP. CRACKED. STA 727C S4L CRACK. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.0 INCH.
- [SDR SB05137](https://openairdocs.org/sdr/SB05137), Oct 26, 2005: CHARGER. INOPERATIVE. MCO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 23 AND 24ABC AND AT THE AFT SERVICE DOOR EXTERIOR. MAINTENANCE REMOVED AND REPLACED T
- [SDR SB05096](https://openairdocs.org/sdr/SB05096), Aug 21, 2005: WIRE. BROKEN. MAINTENANCE REPORTED THE LAST 2 ROWS OF FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-SPLICED POWER WIRE IAW WPM 20-10-13. OPS CHECK GOOD.
- [SDR SB05021](https://openairdocs.org/sdr/SB05021), Jan 31, 2005: POWER SUPPLY. DISCHARGED. CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ON SEATS 24L AND 25L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1137 EMERGENCY LIGHT POWER SUPPLY. 
- [SDR SB05007](https://openairdocs.org/sdr/SB05007), Jan 18, 2005: FUSE. BLOWN. PIT - MAINTENANCE REPORTED THE AFT SERVICE DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 5 AMP FUSE (E-1) AT POWE
- [SDR SB04155](https://openairdocs.org/sdr/SB04155), Nov 17, 2004: CHARGER. INOPERATIVE. MAINTENANCE REPORTED AN EMERGENCY LIGHT IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR SB04151](https://openairdocs.org/sdr/SB04151), Oct 29, 2004: CHARGER. INOPERATIVE. PIT - MAINTENANCE REPORTED THE MID-CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY PACK AT SEA
- [SDR USAA040773](https://openairdocs.org/sdr/USAA040773), Oct 24, 2004: BULKHEAD. CRACKED. PIT - C2, BULKHEAD SKIN, 1 INCH CRACK, FWD PRESSURE BULKHEAD RBL 57, WL 210. INSTALLED DOUBLER IAW SRM 53-10-08 FIG 211.
- [SDR USAASB04123](https://openairdocs.org/sdr/USAASB04123), Sep 11, 2004: FUEL CONTROL. MALFUNCTIONED. MIA - FLT 724 - FLIGHT DEPARTED MIA WITH THE NR 1 ENGINE CSD ON MEL FOR AN OIL LEAK. CON CLIMB-OUT, EN ROUTE TO CLT, THE APU GENERATOR DROPPED OFF LINE AT 700 F
- [SDR USAASB04118](https://openairdocs.org/sdr/USAASB04118), Sep 6, 2004: CHARGER. FAILED. CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHTS IN THE AFT GALLEY ARE BLINKING AND WON'T ILLUMINATE AND STAY ON WHEN SELECTED. MAINTENANCE REMOVED AND REPLACED T
- [SDR USAASB04075](https://openairdocs.org/sdr/USAASB04075), Jun 23, 2004: BATTERY PACK. DISCHARGED. BOS - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT BATTERY WAS LOW. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA040013](https://openairdocs.org/sdr/USAA040013), Feb 8, 2004: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED 3.5 TO 4 INCHES LONG, STATION 1138 STRINGER 5A RIGHT SIDE. REPLACED STRINGER 5A LOWER CHORD PER TR 53-80-04, EA 77840, SRM 53-00-01
- [SDR USAA040010](https://openairdocs.org/sdr/USAA040010), Feb 1, 2004: SKIN. CHAFED. PIT - FOUND FLAP DEEP CHAFED 4 INCHES BY .125 INCH BY .025 INCH DEEP, LEFT OUTBOARD MID FLAP INBOARD LEADING EDGE. INSTALLED SKIN REPLACEMENT DOUBLER PER SRM 57
- [SDR USAASB03036](https://openairdocs.org/sdr/USAASB03036), Mar 5, 2003: SENSOR. MALFUNCTIONED. DURING CLIMB-OUT, WHEN FLAPS WERE RETRACTED TO THE FULL UP POSITION, THE LEADING FLAPS TRANSIT LIGHT AND THE NR 3 SLAT FULL EXTEND LIGHT REMAINED ILLUMINATED. N
- [SDR USAASB02052](https://openairdocs.org/sdr/USAASB02052), Mar 17, 2002: ODOR. DETECTED. DCA - FLT 716 - EN ROUTE FROM PIT-DCA, FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMELL IN TH AFT CABIN AREA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R
- [SDR USAASB00320](https://openairdocs.org/sdr/USAASB00320), Nov 20, 2000: BATTERY. DISCHARGED. EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 12 THROUGH 19ABC, RIGHT AFT OVERWING AND AFT EXTERIOR LIGHTS. MAINTENANCE REPAIRED WIRING 
- [SDR USAASB00319](https://openairdocs.org/sdr/USAASB00319), Nov 18, 2000: CHARGER. FAILED. PHL - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS FOR SEAT ROWS 12 THROUGH 18 AND 20 THROUGH 23 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY 
- [SDR USAA000581](https://openairdocs.org/sdr/USAA000581), Apr 18, 2000: CARGO TRACK. CORRODED. TPA - FOUND CARGO TRACK CORRODED, 12 FEET, STATION 740 TO STATION 900, RBL 14 AFT CARGO TRACK. INSTALLED CARGO TRACK PER SRM 53-00-53 FIG 202. (M)
- [SDR USAA000580](https://openairdocs.org/sdr/USAA000580), Apr 18, 2000: FLOOR SUPPORT. CORRODED. TPA - FOUND FLOOR PANEL SUPPORT CORRODED 40 INCHES, AFT CARGO LBL 20, STATION 727E PLUS 8 TO 727F PLUS 8, RBL 20. INSTALLED NEW SECTION PER SRM 53-60-53 FIG 204
- [SDR USAASB98093](https://openairdocs.org/sdr/USAASB98093), Apr 11, 1998: LIGHT. INOPERATIVE. PVD - DURING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND THE LOWER LEFT, FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AN
- [SDR USAASB96189](https://openairdocs.org/sdr/USAASB96189), Aug 2, 1996: BATTERY PACK. DISCHARGED. ORD - MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHTS AND MISCELLANEOUS CABIN EMERGENCY LIGHTS INOP DURING SYSTEM TEST ON OVERNIGHT CHECK. MAINTENANCE REPLA

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Austro E4P(SERIES))

- [STC SE03232CH](https://openairdocs.org/stc/SE03232CH): Installation of Engine Preheat Kit p/n TA2925-1 for 115 volt application. Hartzell Propeller Inc

## Related

- Other Diamond Aircraft Ind DA 62 aircraft: https://openairdocs.org/model/diamond-aircraft-ind-da-62/aircraft.md
- The Austro E4P(SERIES) engine: https://openairdocs.org/engine/austro-e4p-series.md

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