N103WP

Cancelled 2004

Deregistered aircraft · 1991 Schweizer 269C · Lycoming HIO-360 series

Cancelled
August 10, 2004
Exported to
Sweden
Status when cancelled
Registration pending
Serial number
S1573
Year built
1991
Type
Rotorcraft
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
November 1, 1991
Last registry action
August 9, 2004
Mode S code
A011DB
Owner when cancelled
Registration Pending
Location
Alva, FL
Owner type
Individual

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N103WP and the event date: up to this one’s cancellation.

Service difficulty reports · 6

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

SDR COW2003F00001Servo · inoperativeON INITIAL TEST FLIGHT, AFTER INSTALLING ENGINE RECEIVED FROM OVERHAULER, ENGINE HAD UNUSUALLY HIGH CYLINDER HEAD TEMPERATURES AND RAN ROUGH. REMOVED AND REPLACED FUEL SERVEO (PRECISION AIRMOTIVE) WITH SERVICEABLE UNIT AND ENGINE POWER AND TEMPS FOUND NORMAL.May 29, 2003 · N103WP · Scwzer 269D · Fuel Controlling SystemSDR 2003FA0000694Magneto · failedMAGNETO WAS REPLACED ON 5-27-03 WITH THIS MAGNETO. ON 5-28-03, WHILE PERFORMING MAGNETO CHECK, LEFT MAGNETO WAS DEAD. VERIFIED BY REMOING PRIMARY LEAD. CHECKED NEXT DAY AND STILL WAS NOT FUNCTION ING. REMOVED AND REPLACED MAGNETO.May 29, 2003 · N103WP · Scwzer 269D · Magneto/DistributorSDR COW2003F00000Support · failedON 5/2/03, WHILE ON FINAL APPROACH TO AIRPORT, PILOT HEARD A LOAD EXPLOSION, FOLLOWED BY A LOSS OF ENGINE TACH. PILOT INITIATED AUTOROTATION TO OPEN FIELD ON AIRPORT PROPERTY. ON 5/3/03, DISCOVERED CLUTCH CONTROL SPRING HANGING OVER EXHAUST AND IDLER PULLEY May 2, 2003 · N103WP · Scwzer 269D · Main Rotor ControlSDR 99ZZZX239Bearing · failedWHILE IN-FLIGHT, PILOT NOTICED SLIGHT VIBRATION COMING FROM THE ENGINE AND A DROP IN OIL PRESSURE STARTING TO OCCUR. PILOT OPTED FOR A PRECAUTIONARY LANDING. UPON COMPLETION, OIL PRESSURE NOTED TO BE AT 15 PSI WITH A LOUD SQUEAL COMING FROM THE ENGINE. PILONov 12, 1998 · N103WP · Hughes 269C · Reciprocating Engine Oil SystemSDR 95ZZZX3867Switch · failedMAIN ROTOR TRANSMISSION OIL TEMP/PRESSURE LIGHT ILLUMINATED IN-FLIGHT. INVESTIGATION FOUND THE SWITCH WOULD OPEN AT A LOWER TEMPERATURE THAN NORMAL. INSTALLED NEW SWITCH, OPERATIONAL CHECK NORMAL.Jun 21, 1995 · N103WP · Hughes 269C · Main Rotor GearboxSDR 95ZZZX1499Bearing · failedWHILE PERFORMING A 400-HOUR INSPECTION OF THIS AIRCAFT, THE INNER RACE OF THE FLAPPING HINGE BEARING WAS FOUND BRINNELLED IN TWO AREAS BEYOND THE ACCEPTABLE LIMITS. THIS BEARING WAS NEW AT THE LAST 400-HOUR INSPECTION. SUSPECT CONTAMINATION INTRODUCED DURINGMar 9, 1995 · N103WP · Hughes 269C · Main Rotor Blades

The same airframe elsewhere in the registry · 1

Matched by serial number S1573 and the registry’s model code.

Other aircraft with N103WP · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N103WP now.