NTSB investigations: Rockwell International S-2R, 2001

6 cases on aircraft the registry lists as Rockwell International S-2R. Aircraft are matched to the registry by N-number and event date, checked against the reported serial number, make and model, so older matches can be wrong.

Cases per year

19742026
NTSB investigations: Rockwell International S-2R, 2001 per year, 1974–2026: 276 cases
19742
19755
197613
19778
197817
197917
198012
198114
198210
19839
19848
19856
19866
19877
19889
19898
19909
19916
19925
19934
19947
19954
19966
19974
19989
19997
20003
20016
20022
20034
20044
20057
20062
20084
20102
20113
20127
20133
20142
20151
20162
20173
20192
20202
20211
20221
20232
20261

Latest cases

Query with SQL
duckdb -csv -c "SELECT c.\"ntsbNumber\", c.\"eventDate\", c.\"eventType\", c.\"eventCity\", c.\"eventStateOrRegion\", a.n_number, a.\"aircraftMake\", a.\"aircraftModel\", c.\"highestInjuryLevel\", c.\"totalFatal\", c.\"completionStatus\", c.report_url
  FROM 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c LEFT JOIN 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a ON a.case_mkey = c.\"mKey\" AND a.position = 1
  WHERE year(c.\"eventDate\") = 2001
    AND c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('7630202', '7630205'))
  ORDER BY c.\"eventDate\" DESC, c.\"ntsbNumber\" DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

NTSB ATL01LA100Accident · No injuriesLimited investigationFinal reportRockwell S2R · Bentonia, MSThe loss of engine power due to the loss of throttle cable continunity. The throttle cable linkage was worn beyond servicable limits. A factor was uneven terrain at the emergency landing site.Aug 29, 2001 · N8438V · Substantial damageNTSB FTW01LA184Accident · No injuriesLimited investigationFinal reportRockwell S-2R · Fabens, TXthe pilot's inadequate preflight resulting in loss of engine power due to fuel exhaustion. A contributing factor was the power line.Aug 17, 2001 · N4890X · Substantial damageNTSB SEA01LA146Accident · No injuriesLimited investigationFinal reportRockwell S-2R · Latah, WAthe failure of a cylinder head exhaust rocker shaft boss while the aircraft was performing aerial application. Factors include soft terrain and a drop-off in the field where the emergency landing took place.Aug 4, 2001 · N4237X · Substantial damageNTSB SEA01LA131Accident · 1 fatalLimited investigationFinal reportRockwell International S-2R · Nez Perce, IDThe pilot's failure to maintain terrain clearance for undetermined reasons.Jul 14, 2001 · N5011X · Substantial damageNTSB SEA01FA127Accident · 1 fatalField investigationFinal reportRockwell S-2R-1200 · Cottonwood, IDFailure to maintain adequate clearance from terrain while dropping fire retardant. Factors include low visibility with smoke.Jul 10, 2001 · N4947X · DestroyedNTSB FTW01LA156Accident · Minor injuriesLimited investigationFinal reportRockwell International S-2R · Sabinal, TXa loss of engine power due to a crack in the #9 cylinder, which result in the failure of the connecting rod during the aerial application flight. A contributing factor was the lack of suitable terrain for the forced landing.Jun 28, 2001 · N4888X · Substantial damage