# N293AS: Ea Vision EA J100

- Status: Registration pending
- Airframe: Ea Vision EA J100 (registry code 06102JZ)
- Serial number: EAVUAV502585876
- Type: Rotorcraft
- Mode S code: A300B0
- Registered owner: Registration Pending
- Location: Great Falls, MT
- Owner's area on the map: 47.5025° N, 111.3000° W: Placed by OpenAirDocs: center of Great Falls, MT, within about 3 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N293AS

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 matched by airframe (Ea Vision EA J100) (OpenAirDocs)

None matched.

## Earlier aircraft with N293AS

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N293AS before.

- [Cancelled 2011-09-07](https://openairdocs.org/deregistered/N293AS-2011-09-07): Boeing 727-212, S/N 21348, built 1978. Exported to Mexico. Owner: Broken Wing LLC, Webster Groves, MO

## Service difficulty reports (95)

- [SDR C1HA200893001](https://openairdocs.org/sdr/C1HA200893001), Jan 30, 2008: FLAP SYSTEM. UPON FLAP RETRACTION, THE INBOARD TRAILING EDGE LEFT WING REMAINED AT 1 DEG OF EXTENSION.  COMPLIED WITH COM 2.27.16.  DUMPED FUEL COM 228.4.  INSPECTED INBD T/
- [SDR C1HA200793006](https://openairdocs.org/sdr/C1HA200793006), Jan 31, 2007: STRINGER. AFT CARGO COMPT BS 1160 STR 30 AND SPLICE REPAIR CORRODED.  REPAIRED STR 30 AT BS 1160 IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200793005](https://openairdocs.org/sdr/C1HA200793005), Jan 31, 2007: SILL. C2 - DOOR SILL ON FUSELAGE FRAME HAS CORROSION.  REPAIRED AREA AS REQUIRED IAW CHAMPION AIR EO 727-5314-02
- [SDR C1HA200793004](https://openairdocs.org/sdr/C1HA200793004), Jan 31, 2007: STRINGER. FOUND CORROSION ON STR 27L AT BS 737 FWD PIT.  REPAIRED AREA AS REQUIRED IAW CHAMPION AIR EO 727-5331-18.
- [SDR C1HA200793003](https://openairdocs.org/sdr/C1HA200793003), Jan 30, 2007: WEB. NOSE WHEEL WELL HAS WEB CORRODED BEHIND NLG LOCK ACTUATOR SUPPORT BRACKET AT BS 351.2.  REPAIRED NWW WEB AT BS 351.2 IAW B727 SRM 51-40-2 FIG 1 AND 53-10-2 FIG 
- [SDR C1HA200793002](https://openairdocs.org/sdr/C1HA200793002), Jan 29, 2007: STRINGER. FOUND CORROSION ON STR 27R AT BS 737 FWD PIT.  REPAIRED STR 27R AT BS 737 - 740 IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200593005](https://openairdocs.org/sdr/C1HA200593005), Dec 22, 2005: ATTACH ANGLE. WHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON CORD ANGLE CRACKED FWD PYLON FIREWALL P/N 69-16977-1.  REMOVED CRACKED ATTACH ANGLE AND INSTALLED NEW ATTAC
- [SDR C1HA200593004](https://openairdocs.org/sdr/C1HA200593004), May 29, 2005: POWER LEVER. UPON APPLICATION OF T/O THRUST, NR 3 ENGINE POWER LEVER TO FORWARD STOP AND EPR ONLY 2.05 FULL T/O EPR = 2.13 T/O ABORTED IAW CHAMPION PROCEDURES.  SOC, MX CONT
- [SDR C1HA200593003](https://openairdocs.org/sdr/C1HA200593003), May 29, 2005: ROD. UPON APPLICATION OF FULL T/O THRUST NR 3 ENGINE POWER LEVER WENT TO FORWARD STOP AND EPR ONLY 2.00 (T/O EPR 2.09) T/O ABORTED IAW CHAMPION PROCEDURES.  SOC, MX 
- [SDR C1HA200593002](https://openairdocs.org/sdr/C1HA200593002), Mar 16, 2005: ENGINE. ON TAKEOFF AFTER V1 THE NUMBER 1 ENGINE HAD SEVERE FLUCTUATIONS IN ALL INSTRUMENTS WITH VIBRATIONS ON NUMBER ONE SIDE.  HEARD THREE LOUD POPS NR 1 EGT WENT TO 7

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.