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N622AM

2003 Aircraft Mfg & Development CH 2000 · Lycoming 0-235 series

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Registered owner: Kv Aviation LLC
Location: Louisville, KY
Owner type: LLC
Serial number: 20-1023
Year built: 2003
Type: Fixed wing single engine
Engine: 4 cycle
Airworthiness: Standard, normal
Airworthiness date: November 17, 2003
Certificate issued: July 6, 2023
Expires: July 31, 2030
Mode S code: A81DB7

Aircraft Mfg & Development CH 2000Airframe model · 2 seats · 1 engine · 38 registered TCDS TA5CHAirframe · Aircraft Mfg & Development CH 2000 TCDS E-223Engine · Lycoming 0-235 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming 0-235 model are included below.

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Airworthiness directives that may apply · 23

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1969In forceSuperseded2026

Airframe · Aircraft Mfg & Development CH 2000

AD 2022-03-15Fuel Quantity IndicatorEffective Mar 21, 2022 AD 2005-01-19Mode S transpondersEffective Feb 23, 2005 · Supersedes AD 2004-10-15

Engine · Lycoming 0-235 series

AD 2026-17-10Reciprocating Engine Cylinder SectionEffective Sep 14, 2026

Information bulletins that may apply · 10

Advisory, not mandatory.

Airframe · Aircraft Mfg & Development CH 2000

SAIB SW-18-31Navigation, Attitude, and Direction Data SystemIssued Nov 21, 2018 SAIB CE-11-58Landing Gear, Nose: Zenair CH2000 Nose Landing Gear Weld CrackingIssued Sep 27, 2011 SAIB CE-04-29Issued Dec 9, 2003 SAIB CE-04-28Issued Dec 8, 2003 SAIB CE-03-37Issued May 20, 2003

Engine · Lycoming 0-235 series

SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersIssued May 2, 2019 SAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsIssued Mar 24, 2014 SAIB NE-06-32R1Reciprocating Engine - CrankshaftIssued Sep 10, 2008 SAIB NE-05-89Issued Sep 30, 2005 SAIB NE-01-22Issued May 11, 2001

NTSB investigations

No NTSB investigations matched to N622AMMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Aircraft Mfg & Development CH 2000 aircraft

FAA incident reports

No FAA accident or incident reports matched to N622AMMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Aircraft Mfg & Development CH 2000 aircraft

Service difficulty reports · 11

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2004FA0000245Placard · missingDOES NOT INDICATE TAKEOFF POSITION, PLACARD MISSING. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Placards and Markings SDR 2004FA0000244Audio Panel · inoperativeSTEREO INPUT INTO AIRCRAFT DOES NOT WORK. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Communications System SDR 2004FA0000243Bracket · brokenCARB HEAT BRACKET BROKE LOOSE IN FLIGHT.Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Fuselage Miscellaneous Structure SDR 2004FA0000242Fuel Tank · leakingWITH FULL FUEL TANKS AND THE AIRCRAFT ON THE GROUND AN AMOUNT OF FUEL (.5 GALLON +) WILL DRAIN FROM THE VENT OF THE LT FUEL TANK AFTER A FORWARD OR AFT MOVEMENT OF THE AIRCRAFT. (GL13200305339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Fuel Storage SDR 2004FA0000241Step · looseRT ENTRANCE STEP IS EXTREMELY LOOSE. (GL200305339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Entrance Stairs SDR 2004FA0000240Indicator · inaccurateNEWLY INSTALLED VORS INDICATORS 6-10 DEGREES DIFFERENCE. NAV 1 G430 W G5, NAV 2 BK W G5 KX 155. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Visual Omnirange (VOR) System SDR 2004FA0000239Bungee Cylinder · stiffNOSE WHEEL STEERING BUNGEES ARE EXTREMELY STIFF, CAUSES THE RUDDER TO REQUIRE EXTREMELY HIGH RUDDER INPUTS IN FLIGHT. PILOT CAN FEEL A BREAKOVER POINT. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Landing Gear Steering System SDR 2004FA0000238Rudder · misinstalledRUDDER CONTACTS FUSELAGE BEFORE REACHING STOPS. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Rudder Structure SDR 2004FA0000237Spinner · chafedPROP SPINNER RUBS AGAINST COWL, INCH LONG AND GOING THOUGH FIBERGLASS COWL. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Propeller Spinner Section SDR 2004FA0000236Fastener · chafedDEFLECTION OF LT AILERON UP CAUSES IT TO RUB AGAINST AN EXPOSED RIVET. DEFLECTION OF RT AILERON UP CAUSES IT TO RUB AGAINST TWO EXPOSED RIVETS POSSIBLY HINDERING TRAVEL. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Fasteners SDR 2004FA0000235Structure · chafedSTABILATOR RUBS AGAINST FUSELAGE SCREW. .5 INCH GAP ON LT SIDE, .2500 INCH GAP ON RT SIDE. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2T · Flight Control System

STCs that may be installed · 115

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

Airframe · Aircraft Mfg & Development CH 2000

STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).Garmin International Inc.STC SA12428CHInstallation of the Lycoming Engines Electronic Ignition System (EIS)Lycoming Engines, An Operating Division of AVCO Corporation STC SA12406WIInstallation of a Garmin AXIS Flight Display SystemGarmin International Inc.

See all 115 STCs