Lockheed P2V-5F
Service difficulty reports · 31
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'P2V5F' ORDER BY difficulty_date 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.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'P2V5F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR NI6R201708260046Warning Light · false activationDURING CLIMB OUT FROM FIREFIGHTING DROP, THE CREW NOTICED A REAR OIL SYSTEM CHIP LIGHT ON THE RT RADIAL ENGINE. THE ENGINE WAS SHUTDOWN AND SECURED AND A IFE DECLARED. THE AIRCRAFT RETURNED TO BASE WITH AN UNEVENTFUL LANDING. UPON EXAMINING THE CHIP DETECTSDR NI6R201708230045Oil System · low pressureIN LOADED CRUISE FLIGHT, RIGHT RADIAL ENGINE LOST MANIFOLD PRESSURE FOLLOWED BY A REAR OIL SYSTEM CHIP LIGHT. ENGINE WAS SHUT DOWN, JETTISONED THE LOAD, AND RETURNED TO BASE WITH AN UNEVENTFUL LANDING. IFE WAS DECLARED.SDR NI6R201708050044Trim System · twistedIMMEDIATELY AFTER LIFT OFF, AT APPROXIMATLEY 500 FT AGL, THE CAPTAIN NOTICED THE NOSE WAS INCREASING INTO AN UNCOMMANDED PITCH UP. THE CREW ATTEMPTED TO TRIM THE AIRCRAFT USING THE ELEVATOR TRIM SYSTEM BUT THE INDICATOR DID NOT MOVE. TRIED TO USE THE THE TRSDR NI6R201707250043Chip Detector · malfunctionedIN CRUISE FLIGHT, THE LT RADIAL ENGINE OIL SYSTEM REAR CHIP LIGHT ILLUMINATED INTERMITTENTLY, THEN WENT TO STEADY ON. NO OTHER ABNORMAL INDICATIONS WERE NOTED. ENGINE WAS SHUTDOWN AND SECURED AS A PRECAUTIONARY MEASURE AND CREW RETURNED TO BASE, JETTISONED THESDR NI6R201707220042Governor · faultedON TAKE OFF ROLL, CAPTAIN SAW THE RT RADIAL ENGINE RPM INDICATING HIGH. ATTEMPTED TO MANUALLY TOGGLE THE PROPELLER TO DECREASE THE ENGINE RPM. WHEN NO RPM DROP OCCURRED, ELECTED TO ABORT THE TAKE OFF. AS THE CREW HELD REVERSE PROPPELLER LONGER THAN NORMAL WSDR NI6R201707180041Exhaust Pipe · leakingNORMAL LOADED TAKE-OFF & ROTATION. RECIP NR 2 FIRE LIGHT ILLUMINATED WITH THE AIRCRAFT AIRBORNE OVER THE END OF THE RUNWAY AND ENGINE POWER AT TAKE-OFF POWER. POWER WAS REDUCED TO CLIMB POWER SETTING AND THE LIGHT EXTINGUISHED IMMEDIATELY. LOAD WAS JETTISONSDR NI6R201706110039Rocker Shaft · failedAFTER RETARDANT DROP, THE FLIGHT CREW NOTICED OIL STREAMING DOWN THE SIDE OF THE RH RADIAL ENGINE. THE ENGINE WAS SHUT DOWN, AND AN IFE DECLARED. AIRCRAFT RETURNED TO BASE AND PERFORMED AN UNEVENTFUL LANDING. UPON INVESTIGATION, THE ROCKER ARM FOR NR 12 CYLSDR NI6R201606090034Tire · rupturedON DESCENT FOR LANDING, THE CREW RECEIVED AN UNSAFE RT MLG INDICATION UPON LOWERING GEAR. THE CREW VISUALLY CHECKED THE GEAR AND SAW THAT IT SHOWED DOWN AND LOCKED. THE CAPTAIN RAN THE EMERGENCY CHECKLIST AND PROCEEDED TO LAND. UPON TOUCHDOWN, HE ELECTED TOSDR NI6R201603270032Cylinder · inoperativeLEFT RADIAL ENGINE BEGAN POPPING AND BANGING. FLIGHT CREW CHECKED ENGINE ANALYZER AND FOUND A DEAD CYLINDER INDICATION. ENGINE WAS SHUTDOWN AND SECURED. UNEVENTFUL LANDING.SDR NI6R201508160031Warning Light · illuminatedFORWARD OIL SYSTEM CHIP LIGHT FLICKERED ON AND OFF AFTER RETARDANT DROP, THEN REMAINED OFF. ENGINE WAS SHUTDOWN AND SECURED FOR REMAINDER OF FLIGHT ON A PRECAUTIONARY BASIS. CHIP WARNING LIGHT CAME BACK ON AGAIN ON FINAL APPROACH TO LANDING WITH ENGINE SHUTDSDR NI6R201507120029Position Sensor · out of adjustIMMEDIATELY AFTER TAKE OFF IN CLIMB THE NOSE LANDING GEAR WOULD NOT RAISE. IFE WAS DECLARED, EMERGENCY CHECKLIST WAS COMPLETED, AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED.SDR NI6R201507060028Sequence Valve · bindingDURING RETURN LEG THE LT RADIAL ENGINE OIL SYSTEM BEGAN INDICATING OVER TEMP READINGS. OTHER ENGINE INDICATIONS APPEARED NORMAL. ENGINE WAS SHUTDOWN AND SECURED FOR REMAINDER OF FLIGHT TO BASE. IFE WAS NOT DECLARED, LANDING WAS UNEVENTFUL.SDR NI6R201503080026Oil System · leakingDURING CRUISE FLIGHT, THE CAPTAIN NOTICED OIL STREAMING FROM THE LT RADIAL ENGINE. FLIGHT DIVERTED TO NEAREST BASE WITH AN UNEVENTFUL LANDING.SDR NI6R201503060025Chip Detector · warning lightLT RADIAL ENGINE REAR OIL SUMP CHIP DETECTOR LIGHT ILLUMINATED AFTER T/O ON CLIMB AT METO POWER SETTING. ENGINE WAS SHUTDOWN AND THE ACFT RETURNED TO BASE WITH AN UNEVENTFUL LANDING.SDR NI6R201409060019Warning Light · illuminatedNR 2 RADIAL ENGINE FRONT OIL SUMP CHIP DETECTOR LIGHT ILLUMINATED IN CRUISE FLIGHT. ENGINE WAS SHUTDOWN AND RETARDANT LOAD JETTISONED. AIRCRAFT RETURNED TO BASE WITH AN UNEVENTFUL LANDING.SDR NI6R201409050018Engine · malfunctionedDURING A POST INSPECTION FCF, IN CRUISE FLIGHT, THE NR 2 RADIAL ENGINE BACKFIRED WITH A CORRESPONDING FUEL FLOW FLUCTUATION INDICATED. ENGINE WAS SHUTDOWN AND AN IFE DECLARED. ACFT LANDED UNEVENTFULLY.SDR NI6R201408100017Engine · making metalDURING DEPARTURE, THE NR 1 RADIAL ENGINE REAR SUMP METAL CONTAMINATION LIGHT ILLUMINATED ON CLIMBOUT. NO OTHER ABNORMAL INDICATIONS WERE NOTED. THE ENGINE WAS SECURED, THE ACFT RETURNED TO BASE AND LANDED WITHOUT FURTHER INCIDENCE. AN IFE WAS NOT DECLAREDSDR NI6R201408100016Turbine · failedDURING CRUISE RETURNING TO BASE, WHEN THE NR 2 RADIAL ENGINE REAR SUMP METAL CONTAMINATION LIGHT ILLUMINATED, FOLLOWED BY A DEGRADATION OF TORQUE REQUIRING ADDITIONAL MANIFOLD PRESSURE TO MAINTAIN CRUISE POWER, WHITE SMOKE OBSERVED FROM THE INBD POWER RECOVERSDR NI6R201407200014Engine · making metalDURING CLIMB, THE NR 1 RADIAL ENGINE FRONT CHIP DETECT LIGHT ILLUMINATED. NO OTHER ABNORMAL INDICATIONS WERE PRESENT. THE DECISION WAS MADE TO JETTISON THE RETARDANT LOAD AND SECURE THE ENGINE. BOTH JETS AND NR 2 RADIAL ENGINE WERE OPERATING NORMALLY. AN ESDR NI6R201306190012Line · rupturedDURING RETURN FLIGHT FROM A RETARDANT DROP MISSION, THE MAIN HYD SYSTEM ACCUMULATOR AIR LINE RUPTURED, RESULTING IN LOSS OF MAIN HYD SYSTEM PRESSURE INDICATION IN THE COCKPIT. THE HYD SYSTEM PRESSURE REMAINED AT NORMAL LEVELS WITH NO LOSS OF CONTROL OR SYS ACSDR NI6R20121220011Skin · crackedDURING ANNUAL INSPECTION, DAMAGE WAS DISCOVERED ON THE LT LOWER WING SKIN AT WS 114.5, CONSISTING OF A CRACK MEASURING 0.90" IN LENGTH AND EXTENDING INTO A FASTENER. THE AFFECTED AREA FALLS WITHIN THE AREA COVERED BY THE ORIGINAL AMOC FOR AD2002-19-13. ON-SISDR NI6R20121220010Skin · crackedDURING ANNUAL INSPECTION, DAMAGE WAS DISCOVERED ON LT LOWER WING SKIN AT FUEL SUMP ACCESS PANEL LOCATED AT WS 102.25. ONE MINOR CRACK IN FWD INBD CORNER AND MEASURES .200" IN LENGTH AND IS .050" FROM THE CLOSEST FASTENER. ANOTHER MINOR CRACK IS IN THE AFT OSDR NI6R20121105008Downlock Sensor · out of adjustDURING CLIMB, LANDING GEAR HANDLE WAS PLACED INTO RETRACT. BOTH MLG RETRACTED NORMALLY, NLG DID NOT. AFTER SEVERAL ATTEMPTS, CREW DECLARED AND IN-FLIGHT EMERGENCY, JETTISONED THE RETARDANT LOAD, AND LANDED WITHOUT INCIDENT. CAUSE WAS FOUND TO BE AN OUT-OF-RSDR NI6R20120913007Cylinder · failedDURING CRUISE FLIGHT, THE LT RADIAL ENGINE NR 2 CYLINDER SUFFERED A CATASTROPHIC FAILURE. BOTH FRONT AND REAR OIL SUMP CHIP DETECTOR WARNING LIGHTS ILLUMINATED SIMULTANEOUSLY AND THE ENGINE EXPERIENCED SUDDEN STOPPAGE. THE CREW COMPLETED THE EMERGENCY SHUTDOSDR NI6R20120814004Skin · looseFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP, RT WS 120, RUNNING FOR APPROX 4.25 INCHES TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .005. NO ADDITIONAL STRUCTURES WERE FOUND TO BE DISCREPANT BY VISUAL INSPECTION ANDSDR NI6R20120814003Wing · crackedAT LEFT WING STATION 40, A CRACK IN THE WING SKIN, JUST OUTBOARD OF THE FUSELAGE SKIN, APPROXIMATELY 4 INCHES LONG WAS DISCOVERED UNDER AN EXISTING REPAIR USING EDDY CURRENT INSPECTION. THE CRACK RUNS FORE AND AFT BETWEEN STRINGERS 17 AND 18. NO OTHER DAMAGE HSDR NI6R20120814005Skin · looseFOUND WING SKIN AT THE ATTACHING FASTENERS AT THE RT LOWER FWD SPAR CAP, R WS 120, RUNNING FOR APPROX 5.0 INCHES TO HAVE WORKED LOOSE. SKIN CAN BE PUSHED UP AND DOWN APPROX .005. NO ADDITIONAL STRUCTURES WERE FOUND TO BE DISCREPANT BY VISUAL INSPECTION AND NSDR NI6R20110817001Filter Housing · rupturedAFTER DROPPING RETARDANT ON A FIRE, WHILE AT CRUISE RETURNING TO BASE, MAIN HYDRAULIC SYSTEM FAILURE OCCURRED WITH ASSOCIATED VAPORS IN THE COCKPIT. VISUAL INSPECTION SHOWED NO FLUID PRESENT WITH MAIN SYSTEM PRESSURE READING ONLY ACCUMULATOR PRESSURE. DIVERSSDR 2010FA0001060Regulator Valve · worn(NI6R) ON APPROACH FOR LANDING, THE AIRCREW DISCOVERED THE MAIN HYD SYS WOULD NOT BUILD PRESSURE ABOVE 1,000 PSI. NORMAL IN-FLIGHT OPERATING RANGE IS 1,400 - 1,725 PSI. AN IN-FLIGHT EMERGENCY WAS DECLARED, THE ACFT LANDED SAFELY, AND WAS TOWED FROM THE ACTIVE SDR 2010FA0001058Regulator Valve · out of toleranceMAIN HYD SYS UNLOADER VALVE PN HC5520, SN 235 WAS REMOVED FROM THE ACFT POST-INCIDENT AND WAS BENCH TESTED FOR FUNCTION. NORMAL VALVE PRESSURE RANGE UNLOADS AT 1,675 - 1,725 PSI AND LOADS AT 1,400 - 1,500 PSI. SUBJECT VALVE WAS FOUND TO UNLOAD PRESSURE AT APPSDR 97ZZZX4661Casting · crackedWHILE ACCOMPLISHING A FLEET-WIDE INSPECTION OF AIRCRAFT, A CASTING CRACK WAS FOUND ON A SECOND UNIT WITHIN FLEET.
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