N163YV, cancelled Jun 9, 2010
Service difficulty reports · 51
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N163YV' AND deregistration_id = 'N163YV-2010-06-09' 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 n_number = 'N163YV' AND deregistration_id = 'N163YV-2010-06-09' 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 AMWA88898Master Cylinder · weakDURING TAXI INTO GATE, THE PILOT'S LT BRAKE PEDAL LOST PRESSURE. PRESSURE WAS REGAINED AFTER PUMPING PEDAL. MAINTENANCE BLED BRAKES AND CLEARED DISCREPANCY.SDR AMWA88571Brake · weakAFTER LANDING THE CAPTAIN REPORTED THAT THE LT BRAKE WAS SPONGY AND MUSHY. REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES AND CLEARED DISCREPANCY.SDR AMWA88211Annunciator · false indicationCABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AND MAINTENANCE VERIFIED DOOR WAS SECURED AND PROBLEM WAS A FAULTY ANNUNCIATOR. ANNUNCIATOR PLACED IN DEFERRED STATUS. REMAINS DEFERRED AS OF 10/29/07.SDR AMWA86756BCBattery · false activationBATTERY CHARGE ANNUNCIATOR ILLUMINATED WHEN GEAR WAS EXTENDED AND THEN EXTINGUISHED. AC LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE WRITEUP AND DISTRACTION TO THE CREW. COULD NOT DUPLICATE ON GROUND, OPS CHECKS NORSDR AMWA86499Rod · brokenON APPROACH TO GRI, CAPT PEDALS LOST RUDDER CONTROL. CAPT TRANSFERRED CONTROL OF THE ACFT TO THE FO. FO PEDALS HAD RUDDER CONTROL. FO LANDED WITH NO FURTHER INCIDENT. OCCURENCE REPORT FILED. REMOVED AND REPLACED RUDDER INTERCONNECT ROD (ROD END), RIGGED RSDR AMWA06032EFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032DFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032CFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032UFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032HFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032GFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING INC. REPORT 6799-1 REV 1R.SDR AMWA06032BStructure · chafedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.SDR AMWA06032AStructure · chafedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.SDR AMWA06032VFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032TFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032SFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032RFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032MFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032QFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032PFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032OFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032NFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032LFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032KFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032JFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032FFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032IFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06002Spar Cap · corrodedBIO CORROSION LT SPAR, ALT SPAR FLANGE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW ENGINEERING REPORT 6799-3 REV 1R.SDR AMWA84592Brake · bindingDURING ROLLING TAKEOFF, CAPT HAD EXCESSIVE BRAKE DRAG AND ABORTED TAKEOFF. RETURNED TO GATE W/O FURTHER INCIDENT. ADJUSTED PARKING BRAKE HANDLE AND VALVES.SDR AMW1070010901Skin Panel · crackedDISCOVERED DURING MAINTENANCE INSPECTION FOR PRESSURIZATION PROBLEM. MAINTENANCE FOUND THE FUSELAGE SKIN TO BE CRACKED ALONG THE RT SIDE OF THE NR 1 COMM ANTENNA. THE CRACK WAS 7 IN LONG, EXTENDING FROM APPROX FS 213.00 TO FS 220.750 RUNNING PARALLEL TO THE ASDR AMWA078434Actuator · wornUPON GEAR EXTENSION CREW OBSERVED THE GEAR TRANSIT LIGHT WOULD NOT GO OUT. CREW ACCOMPLISHED REQUIRED PROCEDURES AND LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE WAS CALLED AND REMOVED AND REPLACED LT. MAIN GEAR ACTUATOR, THE (CR110) DIODE, LOWER LEGENSDR 71813Brake Assy · malfunctionedUPON TAXI INTO DUJ, CREW EXPERIENCED RIGHT BRAKE SPONGY. PARKED AND CHOCKED AIRCRAFT WITH NO FURTHER INCIDENT. MAINTENANCE BLED BRAKES. THEREFORE THERE WERE NO PARTS USED.SDR 70891Connector · dirtyRT PROP WILL ONLY MAKE 1550 UNDER POWER. MAINTENANCE CLEANED OVERSPEED GOVERNOR CONNECTOR PLUG. THEREFORE NO PARTS WERE USED.SDR 69476Brake · malfunctionedAFTER TAXI OUT LEFT BRAKE WILL NOT RELEASE. PASSENGERS DEPLANED ON TAXIWAY. MTC DETERMINED PARKING BRAKE WAS NOT RELEASING COMPLETELY. A/C RETURNED TO GATE AND PARKING BRAKE DEFERRED PER MEL 32-7. A/C RETURNED TO SERVICE. INSTALLED PARKING BRAKE KNOB.SDR 67556Brake Assy · weakCREW EXPERIENCED WEAK BRAKING ACTION ON RIGHT SIDE ON TAXI IN WITH NO FURTHER INCIDENT. BLED BRAKES.SDR 60212Door · stuckUPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THRU THE EMERGENCY EXIT AT 6A. REMOVED & REINSTALLED EMERGENCY EX/DOORSDR 60211Cable · damagedUPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR TO OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THUR EMERGENCY EXIT AT SEAT 6A ALL WERE DEPLANED WITH NO FURTHER INCIDENT. REINSTALLED PASS/DOOR FWD CABLE ON UPPER END.SDR 60146Airstair · damagedAIRCRAFT DOOR WOULD NOT LOCK PROPERLY FROM THE INSIDE. MAINTENANCE CALL AND AIRCRAFT WAS MOVED TO THE HANGAR FOR REPAIRS. PERFORMED AIRSTAIR DOOR HONYECOMB INSERT. REPAIR AND SERVICE BULLENTIN 52-3099. RIGGED DOOR. P/N MS2469AS71SDR AMWA35Rib · crackedRIB AT CSS 39.289 AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 ON RH SIDE AND STRG P/N 101-640000-39 STRG P/N 101-640000-37 (4EA CRACKS ON THIS RIB)SDR AMWA34Rib · crackedRIB AT CSS 54.026 CRACKED AT STRG. 101-640000-47 STRG. P/N 101-640000-42 RT SIDE AND STRG 101-640000-43 STRG P/N 101-640000-39 STRG P/N 10164000041 5 EA CRACKS ON THIS RIB)SDR AMWA30Rib · crackedWHILE PERFORMING INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM MANUAL P/N 114-590021-9, 51-70-03.SDR AMWA29Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03.SDR AMWA28Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021-9, 51-70-03.SDR AMWA20Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB, STA 39.289 AND STAB 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL REPAIR MANUAL P/N 114-590021-9, 51-70-03.SDR AMW2002F00001Hose · leakingENROUTE, THE CREW NOTICED THAT THE OIL PRESSURE LOW LIGHT FLICKERED AND THE OIL PRESSURE INDICATED LOW. THE CREW REDUCED POWER ON THE LEFT ENGINE AND LANDED WITHOUT INCIDENT.SDR 98ZZZM898Skin · crackedOVERNIGHT MAINTENANCE IN ICT, FOUND A SMALL CRACK ON THE RT OUTBOARD FLAP LOWER SKIN TE 10 INCH FROM INBOARD END. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)SDR 97ZZZM966Valve · normalLEFT ENGINE WAS SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMP. EN ROUTE FROM FYV TO MCI. REPLACED OIL FILTER HOUSING O-RINGS. SUSPECT OIL TANK PRESSURIZING VALVE MAY HAVE BEEN STUCK CLOSED. UNABLE TO CONFIRM RELIEF VALVE PROBLEM. VALVE MAY HAVE FREED ITSELF DUSDR 97ZZZX4245Flap · crackedICT - OVERNIGHT MAINTENANCE FOUND 1 INCH CRACK ON TE TOP SKIN OF RIGHT INBOARD FLAP 31 INCHES INBOARD EDGE. STOP-DRILLED CRACK WITH A NR 45 DRILL BIT. FABRICATED A 2 INCH BY 3 INCH PATCH FROM FLAP SKIN STOCK. INSTALLED PATCH USING REFERENCES SRM'S 51-00, 5SDR 97ZZZM947Flap · crackedDURING ROUTINE MAINTENANCE A 2 INCH CRACK WAS FOUND ON THE LEFT O/D FLAP, 30 INCHES FROM OUTBOARD EDGE AND 16 INCHES FORWARD OF T/E. REPAIRED WITH DOUBLER IAW AMWA T.O. AND SRM. (M)SDR 96ZZZX115Gas Shock · bentWHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK.
Back to N163YV, cancelled Jun 9, 2010