Accident · substantial damage
Oct 2, 2011 · Lincoln Park, NJThe pilot's improper landing flare.
- Damage
- Substantial
- Injuries
- None
- Report
- ERA12CA004
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA12CA004)
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Oct 2011)2 ADs may apply1 service difficulty report
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot's improper landing flare.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA12CA004)
The student pilot's improper power management during the short-field landing procedure, and the flight instructor's delayed remedial action.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for IAD03LA014)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (182P) |
| 2007-09-01 | Cessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R… | Apr 25, 2007 | Airframe (182P)Only with: Air Plains Services Corporation STC SA00152WI installed and a ground power receptacle mounted on the firewall (forward ground power receptacle). |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
ENGINE: 137 HOURS SOH (3-20-96). MODIFIED PER STC SE4985NM. NEW TCM CYLINDER ASSYS INSTALLED AT OVERHAUL AND MODIFICATION. COMP TEST: NR 1 - 55/80. NR 2 - 25/80. NR 3 - 75/80. NR 4 - 70/80. NR 5 - 75/80. NR 6 - 72/80. REMOVED ALL SIX CYLINDERS. ALL EXHAUST VALVES LOOSE IN GUIDES. VISUAL INSPECTION…
From FAA Service Difficulty Reports; matched by N-number and serial number.