N27532

CESSNA A185F · 1979 · Valid Registration

Registered owner: SHADOW AVIATION INC, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
SHADOW AVIATION INC (QS9A)Certificate holderMatched by certificate designator

Accident & incident history

Accident · 1992-07-30 Unresolved
Cessna A-185-F None injuryoperator not yet resolved
Source: NTSB case ANC92LA117

Maintenance disclosures

O · 2006-05-11 Unresolved
ATA 2742

MAINTENANCE PERSONNEL WERE ADVISED BY THE PILOT THE HORIZONTAL STABILIZER TRIM QUIT WORKING. INSPECTION FOUND THE BARREL SIDE OF THE TRIM SCREW JACK HAD STRIPPED OUT. THE SYSTEM INCLUDES 2 TRIM SCREW JACKS THE OTHER TRIM SCREW JACK TOOK ALL OF THE LOAD AND JAMMED UP. INSPECTION OF SECOND TRIM SCREW JACK BARREL FOUND THE UPPER THIRD OF THE THREADS WERE STRIPPED IN THE SECOND TRIM SCREW BARREL. MFG DOES NOT SPECIFY ANY INSPECTION CRITERIA FOR WEAR OF THE JACK SCREW THREADS OR THE BARREL THREADS. RECOMMEND EITHER MANDATORY INSPECTION CRITERIA FOR THE BARRELS AND THREADS OR AN AIRWORTHINESS DIRECTIVE TO PRECLUDE LOSS OF CONTROL OF THE TAIL OF THE AIRCRAFT. (K)

Source: SDR 2006FA0000485 · FAA SDRS
O · 1998-05-13 Unresolved
ATA 5510

AT ANNUAL INSPECTION, FOUND LEFT AND RIGHT STABILIZER HINGE REINFORCEMENTS CRACKED. LEFT FITTING CRACKED FROM AFT EDGE TO BOLT HOLE AT INBOARD LOWER TAB. RIGHT FITTING HAD SIMILAR CRACKS IN BOTH LOWER TABS. NOT SO OBVIOUS WAS A CRACK ALONG 90 PERCENT OF THE LOWER FLANGE BEND RADIUS ON THE RIGHT FITTING. SUGGEST CAREFUL INSPECTION OF THIS AREA DURING ROUTINE INSPECTIONS ESPECIALLY HIGHER TIME AIRCRAFT. PART TIS: 5,272 HOURS.

Source: SDR 98ZZZX2282 · FAA SDRS