# Incident 19880509022589I: Lkheed 188C, Detroit, MI, May 9, 1988

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: May 9, 1988, 11:40 local time
- Place: Detroit, MI
- Airport: Willow Run
- Phase of flight: Practice Training Manuevers
- Operating rules: General operating rules (Part 91)
- Operator: ZIAA
- Location: 42.2403° N, 83.5315° W: Placed by OpenAirDocs at WILLOW RUN (YIP), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=42.2403&lon=-83.5315&mi=10
- Aircraft: N284F, a cancelled registration (https://openairdocs.org/deregistered/N284F-2012-08-27) (OpenAirDocs)
- Registry model: Lockheed 188C (registry code 5262604, https://openairdocs.org/model/lockheed-188c) (OpenAirDocs)
- Registry engine: Allison 501-D13 series (registry code 03004, https://openairdocs.org/engine/allison-501-d13-series) (OpenAirDocs)
- Reported make and model: LKHEED 188C
- People aboard: 3
- Fatal injuries: 0
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19880509022589I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

FLAP ASYMMETRY OCCURRED ON FLAP RETRACTION ON RECOVERY FROM A STALL.MADE SAFE LANDING. SAFETY LETTER RECOMMENDATION

## Other reports on N284F (3)

Matched to the same aircraft by N-number and date.

- [Incident 19900929059459I](https://openairdocs.org/incident/19900929059459I), Sep 29, 1990: Lkheed 188C (N284F), Buffalo, NY. NR2 engine problem on approach. Shut down and landed. Replaced negative torque sensing valve.
- [Incident 19900722042049I](https://openairdocs.org/incident/19900722042049I), Jul 22, 1990: Lkheed 188C (N284F), Odgen, UT. NR1 engine flamed out on climb. Returned. Found NR1 engine driven fuel pump had failed.
- [Incident 19781110049939I](https://openairdocs.org/incident/19781110049939I), Nov 10, 1978: Lkheed 188C (N284F), Ypsilanti, MI, Minor damage. Tire exploded during inflation. No rim, wheel or tire defect. Cause was overpressurzation. Used wrong equipment.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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