N63790

PIPER PA-23-250 · 1977 · Valid Registration

Registered owner: MCPHILLIPS FLYING SERVICE INC, MI (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
MCPHILLIPS FLYING SERVICE, INC. (ECLA)Certificate holderMatched by certificate designator

Accident & incident history

Accident · 2006-06-02 Matched by aircraft (N-number)
Piper PA-23-250 None injuryMCPHILLIPS FLYING SERVICE, INC.
Source: NTSB case CHI06LA146

Maintenance disclosures

R · 2008-12-30 Matched by certificate designator
ATA 8500

AFTER APPROX 30 MINUTES OF IFR FLIGHT AT 8000 FT WITH NO OUTSIDE EVIDENCE OF AIRFRAME ICING THE PILOT NOTICED LT ENG LOOSING FUEL PRESSURE AND MANIFOLD PRESSURE, PILOT FOLLOWED ENG FAILURE CHECKLIST AND ALTERNATE AIR, BOOST PUMPS AND FULL MIXTURE WERE APPLIED ON THAT ENG WITH NO EFFECT, ENGINE AT IDLE POWER SETTING ONLY, PILOT THEN CROSS FEED FROM RT WING TANK TO LT ENG AND SHORTLY AFTER BEGAN LOOSING FUEL PRESSURE AND MANIFOLD PRESSURE ON THE RT ENG THE PILOT THEN SWITCHED THE CROSS FEED OFF AND ADVANCED MIXTURE, BOOST PUMP AND ALTERNATE AIR WERE APPLIED TO THE RT ENGINE WITH NO EFFECT. AFTER MANEUVERING TOWARD AN ALTERNATE AIRPORT THE LT ENGINE CAME BACK UP ON POWER FOLLOWED SHORTLY AFTER BY THE RT ENGINE. THE PILOT THEN MADE AN UNEVENTFUL LANDING USING THE ILS. ALL FUEL TANKS WERE SUMPED PRIOR TO THE INITIAL DEPARTURE AND AFTER LANDING THE NEXT DAY AFTER A NIGHT IN HEATED HANGER AND NO EVIDENCE OF WATER FOUND EITHER TIME. FUEL TANKS WERE COMPLETELY DRAINED AND APPROX 82 GALS OF FUEL RECOVERED. NO MALFUNCTION OF ANY SYS COULD BE IDENTIFIED UPON INSP OF FUEL AND AIR INTAKE SYS. ACFT GROUND RUN AND FLOWN LOCALLY FOR 45 MINUTES ON ALL TANKS AND NO PROBLEM IDENTIFIED.

Source: SDR 2009F00005 · FAA SDRS
O · 2005-08-18 Matched by certificate designator
ATA 3210

PN 400-111 BOLT BROKE ON LANDING. BOLT IS IN LINK, PN 16240-5. GEAR FOLDED AFT AND MAIN TIRE RODE ON RT FLAP. (NM01200510571) (K)

Source: SDR 2005FA0001601 · FAA SDRS
O · 2005-05-23 Matched by certificate designator
ATA 7602

MIXTURE CABLE BROKE AT CONTROL LEVER END. 7 STRAND INNER CABLE PARTED .7500 INCH FROM PUSH/PULL SLIDER CABLE END. CABLE STRANDS APPEAR TO HAVE BEEN BALLONED FROM OVER COMPRESSION, OVER TRAVEL. CABLE PARTED AT ENGINE SHUT DOWN. THE REPLACEMENT CABLE IS PN 454-204 AND MAY AVE BEEN IMPROVED OVER THE ORIGINAL. (K)

Source: SDR 2005FA0001600 · FAA SDRS
O · 2005-05-23 Matched by certificate designator
ATA 5100

BOLT BROKEN. (K)

Source: SDR 2005FA0001608 · FAA SDRS