# Accident 20010527009189A: Cessna 182P, Hondo, TX, May 27, 2001 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: May 27, 2001, 11:40 local time - Place: Hondo, TX - Airport: Hondo Municipal Airport - Damage: Substantial damage - Phase of flight: Fcd/Prec Ldg From Cruise - Operating rules: General operating rules (Part 91) - Location: 29.3594° N, 99.1767° W: From the FAA - Nearby events: https://openairdocs.org/map.md?lat=29.3594&lon=-99.1767&mi=10 - Aircraft: N9875E, a cancelled registration (https://openairdocs.org/deregistered/N9875E-2021-07-03) (OpenAirDocs) - Registry model: Cessna 182P (registry code 2075816, https://openairdocs.org/model/cessna-182p) (OpenAirDocs) - Registry engine: Continental O-470 series (registry code 17026, https://openairdocs.org/engine/continental-o-470-series) (OpenAirDocs) - Reported make and model: CESSNA 182P - Reported engine: CONT O470S - Fatal injuries: 0 - Pilot flight hours: 369 total, 67 in this make and model - NTSB investigation: [NTSB FTW01LA130](https://openairdocs.org/ntsb/FTW01LA130) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/20010527009189A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (.19)ON MAY 27, 2001, AT 1132 CENTRAL DAYLIGHT TIME, A CESSNA 182P, SINGLE-ENGINE AIRPLANE, N9875E, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING FOLLOWING A LOSS OF ENGINE POWER DURING THE CLIMB TO CRUISE NEAR HONDO, TEXAS. THE AIRPLANE WAS OWNED AND OPERATED BY THE PILOT UNDER 14 CODE OF FEDERAL REGULATIONS PART 91. THE PRIVATE PILOT, SOLE OCCUPANT, RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PLANNED CROSS-COUNTRY FLIGHT TO WHARTON, TEXAS. IT IS UNKNOWN AT THIS TIME IF A FLIGHT PLAN WAS FILED FOR THE PERSONAL FLIGHT WHICH DEPARTED HONDO MUNICIPAL AIRPORT APPROXIMATELY 10 MINUTES BEFORE THE ACCIDENT. (-23)ON MAY 27, 2001, AT 1133 HOURS, CST, A CESSNA 182P AIRPLANE, N9875E, INCURRED SUBSTANTIAL DAMAGE DURING LANDING IN A FIELD THREE MILES EAST OF HONDO, TX (HDO) AIRPORT. THE PRIVATE PILOT, WHO WAS THE SOLE OCCUPANT, RECEIVED MINOR INJURIES. DAY VMC PREVAILED FOR THE FAR PART 91 FLIGHT. THE FLIGHT ORIGINATED FROM HDO. THE PILOT STATED AFTER DEPARTURE FROM HDO, HE WAS ESTABLISHED IN CRUISE FLIGHT AT APPROXIMATELY 2500 FEET MSL WHEN THE ENGINE LOST POWER TO IDLE (800 RPM). HE TURNED THE AIRCRAFT BACK TO HDO AND LAN DED IN A WHEAT FIELD. THE AIRCRAFT SKIDDED APPROXIMATELY 100 FEET, RIPPING THE NOSE GEAR OFF, ROLLED OVER THE NOSE AND CAME TO REST INVERTED. FURTHER INVESTIGATION OF THE FUEL SYSTEM DISCLOSED WATER AND DEBRIS CONTAMINATION IN THE FUEL. THERE WAS NO ELT INSTALLED. THERE WERE NO SHOULDER HARNESSES INSTALLED. THERE WAS NO NMAC. THERE WAS NO POST-CRASH FIRE. (.4) ON MAY 27, 2001, AT 1140 DAYLIGHT TIME, A CESSNA 182P, SINGLE-ENGINE AIRPLANE, N9875E, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING FOLLOWING A LOSS OF ENGINE POWER DURING CRUISE FLIGHT NEAR HONDO, TEXAS. THE AIRPLANE WAS OWNED AN OPERATED BY A PRIVATE INDIVIDUAL UNDER 14 CODE OF FEDERAL REGULATIONS PART 91. THE PRIVATE PILOT, SOLE OCCUPANT, RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PLANNED CROSS-COUNTRY FLIGHT TO WHARTON, TEXAS. A FLIGHT PALAN WAS NOT FILED FOR THE PERSONAL FLIGHT WHICH DEPARTED HONDO MUNICIPAL AIRPORT AT 1120. THE PILOT REPORTED THAT HE PERFORMED THE PREFLIGHT AND FOUND "NO WATER IN [THE] FUEL." THE AIPLANE WAS TOPPED WITH 25.2 GALLONS OF FUEL FOR THE PLANNED FLIGHT, AND THE PILOT VERIFIED THAT THE FUEL TANKS WERE FULL. FOLLOWING A SATISFACTORY PRE-TAK EOFF, THE FLIGHT DEPARTED RUNWAY 17. SEVERAL MINUTES AFTER THE AIRPLANE WAS IN CRUISE FLIGHT AT 2,500 FEET MSL, THE ENGINE POWER DECREASED TO 900 RPM. THE PILOT PERFORMED THE EMERGENCY CHECKLIST; HOWEVER, THE ENGINE DID NOT REGAIN CRUISE POWER. DURING THE OFF AIRPORT LANDING, THE NOSE GEAR DUG INTO THE SOFT TERRAIN, AND THE AIRPLANE CAME TO REST IN THE INVERTED POSITION. THE FAA INSPECTOR, WHO RESPONDED TO THE SITE, FOUND THE VERTICAL STABILIZER BENT, UPPER RUDDER AREA CRUSHED, RIGHT WING STRUT BENT, AND THE LEFT WING BUCKLED OUTBOARD OF THE WING STRUT. THE FUSELAGE WAS WRINKLED AND BUCKLED. ON MAY 29, 2001, AN FAA INSPECTOR EXAMINED THE AIRPLANE AT RUSTY'S FLYING SERVICE, HONDO, TEXAS. WATER CAME OUT OF THE CARBURETOR WHEN THE THROTTLE WAS OPERATED. WATER AND DEBRIS WERE FOUND MIXED WITH THE FUEL DRAINED FROM THE GASCOLATOR. A FUEL SAMPLE FROM THE FUEL TRUCK LOOKED "CLEAR WITH SOME MINUTE FIBERS FLOATING IN IT," AND THE FUEL COLOR WAS CONSISTENT WITH 100 LOW LEAD AVIATION FUEL. MAINTENANCE RECORDS, REVIEWED BY THE FAA INSPECTOR, INDICATED THE LAST ANNUAL INSPECTION WAS PERFORMED ON MARCH 10, 2001. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB FTW01LA130](https://openairdocs.org/ntsb/FTW01LA130), May 27, 2001: Cessna 182P (N9875E), Hondo, TX, substantial damage. Probable cause: the pilot's inadequate preflight of the airplane, which resulted in a loss of engine power in cruise flight due to water in the fuel. A contributing factor was the soft terrain encountered during the… ## Other reports on N9875E (1) Matched to the same aircraft by N-number and date. - [Accident 19860410010829A](https://openairdocs.org/incident/19860410010829A), Apr 10, 1986: Cessna 182P (N9875E), Jackson, CA, Substantial damage. Inadequate compensation for the crosswind on the landing roll. Veered off the runway side and collided with a ditch. 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. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.