N16540, cancelled Dec 18, 2012
Service difficulty reports · 86
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 = 'N16540' AND deregistration_id = 'N16540-2012-12-18' 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 = 'N16540' AND deregistration_id = 'N16540-2012-12-18' 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 29GA94032083012Uplock Switch · out of adjustFLIGHT:4001 TLH/TPA GEAR UNSAFE LIGHT INTERMITTENTLY ILLUMINATES LIGHT AND HORN ACTIVATED IN CLIMBOUT WITH GEAR UP. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH, OPERATIONAL CHECK OK.SDR 29GA94032070712APowerpack · defectiveFLIGHT: 3979 PNS/PNS AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. REPLACED HYDRAULIC POWER PACK, OPERATIONAL CHECK SATISFACTORY.SDR 29GA201204110001Switch · dirtyIN FLIGHT, REDUCED POWER TO IDLE NO HORN NO GEAR LIGHTS. PERFORMED INSP OF LANDING GEAR HORN SYS AND INTRANSIT LIGHT SYS CLEANED DEBRIS FROM LANDING GEAR SWITCHES OPS CHECKED GOOD.SDR 29GA94052012612BHandle · lack of lubeDURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE OPERATIONAL CHECK NORMAL.SDR 29GA94052012612AHandle · lack of lubeREPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INNER AND OUTER HANDLE STIFF TO OPERATE. LUBRICATED RIGHT AFT EMERGENCY EXIT INNER AND OUTER HANDLE OPERATIONAL CHECK NORMAL.SDR 29GA94032121611APressure Switch · defectiveFLIGHT: 4017 FLL/GGT PILOT REPORTED LANDING GEAR "3 GREEN" ILLUMINATED WITH GEAR HANDLE IN "UP" POSITION AIRSPEED EXCEEDED 200 KTS. REPLACED LANDING GEAR POWERPACK GEAR UP PRESSURE SWITCH. LANDING GEAR OPERATIONAL CHECK SATISFACTORY.SDR 29GA94071081911ATruss · damagedREPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBES DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-4,8110-3, DERT-510208-CE.SDR 29GA94071081911Truss · damagedREPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBES DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-4,8110-3, DERT-510208-CE.SDR 29GA94061072811ASwitch · out of adjustFLIGHT 9185 FPO/FLL PILOT REPORTED AUTOFEATHER CYCLES ON AND OFF ON APPROACH TO LANDING WITH 1000 LBS OF TORQUE ON LEFT AND RIGHT ENGINES. ADJUSTED AUTOFEATHER ARMING SWITCHES OPERATIONAL CHECK GOOD.SDR GUUA94057050211CStringer · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED RT WING FWD LOWER BONDED J STRINGER HAS CORROSION BETWEEN WS 114.25 AND 124.25 . REMOVED CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA94057050211DSpar · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED RIGHT WING LOWER MAIN SPAR AREA OF CORROSION BETWEEN WS 124.25 TO WS 135.86. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA94057050211BSkin · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED LEFT WING FORWARD OF MAIN SPAR AREA OF CORROSION AT WS 124.25. REMOVED CORROSION FABRICATED AND INSTALLED EXTERNAL STRAP REPAIR.SDR GUUA94057050211AStringer · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED LEFT WING LOWER BONDED SKIN FORWARD J STRINGER CORRODED TWO SPOTS BETWEEN WS 114.25 AND 124.25. REMOVED CORROSION FABRICATED AND INSTALLED INTERNAL STRAP REPAIR.SDR GUUA94053041711BDoor Frame · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED AIRSTAIR DOOR FRAME CRACKED AT UPPER AND LOWER COUNTER BALANCE MOUNTS APPROXIMATELY FS 150.6 AND WL 105. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED NEW SECTION.SDR GUUA94053041711ASkin · corrodedDURING SCHEDULED ROUTINE STRUCTURAL INSP CORROSION FOUND BETWEEN FS 378.25 AND FS 393.25 BETWEEN STRINGERS 9AL AND 10L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.SDR GUUA94053032211ASkin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUSELAGE BELLY SKIN EXFOLIATED IN ONE SPOT AT FS 349.00 JUST AFT OF VCS SERVICE DOOR. REMOVED DAMAGE SKIN AND STRINGER AND INSTALLED STRINGER REPAIR AND AN EXTERNAL DOUBLER REPAIR.SDR GUUA94071121710ABracket · crackedDURING MAGNETIC PARTICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREAS CRACKED. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. FOUND DURING MAGNETIC PARTICLE INSP.SDR GUUA94032062410ABrake · faultedPILOT REPORTED AT TIMES WHEN APPLYING RT BRAKES PEDAL GOES ALL THE WAY TO THE FLOOR WITH NO BRAKE PRESSURE HAVE TO PUMP THE BRAKE TO GET PRESSURE. BLED BRAKES AND REMOVED TRAPPED AIR IN RT BRAKE SYS.SDR GUUA94057053110ASpar · damagedSPAR DAMAGED, ACFT REQUIRES D+ INSP ACFT COMPANY KIT 118-4014-0003. COMPLIED WITH D+ INSP COMPANY KIT 118-4014-0003.SDR GUUA94032043010ABrake Assy · weakPILOT REPORTED BRAKES ON LT SIDE OF ACFT SPONGY AND WEAK. REPLACED NR (1) BRAKE ASSY.SDR GUUA94032042910ABrake · weakPILOT REPORTED BRAKES FEEL WEAK. INSPECTED BRAKE SYS FOUND NO LEAKS. BLED BRAKE SYS TAXIED ACFT AND FOUND BRAKE SYS OPS CHECK GOOD NO DEFECTS NOTED.SDR GUUA94032042610ABrake Sys · contaminatedFLIGHT: 9168 MIA/TPA PILOT REPORTED BRAKES FEEL WEAK. BLED ALL FOUR BRAKES, OPERATIONAL CHECK NORMAL.SDR GUUA94027031410ATorque Tube · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LEFT ELEVATOR TORQUE TUBE.SDR GUUA94052022210ADoor · stuckDURING SCHEDULED ROUTINE MX DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. REPOSITIONED RT FWD EMERGENCY EXIT INTERIOR PANEL.SDR GUUA94053102309ASpar · damagedREPORT: DURING BELLY SKIN REPAIR DISCOVERED RIGHT MAIN SPAR HAS TWO ELONGATED FASTENER HOLES AT FS 288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERSSDR GUUA94057102309ASpar · damagedDURING BELLY SKIN REPAIR, DISCOVERED RT MAIN SPAR LWR FLANGE HAS 2 ELONGATED FASTENER HOLES AT FS288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERS. PREVIOUSLY SUBMITTED OPEN UNDER CONTROL NR GUUA94053102309A UPDATED TO GUUA94057102309ASDR GUUA94053102109ASkin · corrodedDISCOVERED CTR BELLY SKIN CORROSION AT FS 327.63 BETWEEN STR 16 TO 15R OUT OF LIMITS REQUIRES REPAIR. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA94053101309ASkin · corrodedDURING SCHEDULED ROUTINE INSP RT BELLY SKIN HAS SKIN DEBONDING AT FS 288.00. REMOVED SURFACE CORROSION FROM SKIN REQUIRES REPAIR. REMOVED DAMAGED SKIN AND INSTALLED SKIN FILLER AND EXTERNAL DOUBLER REPAIR.SDR GUUA94052101109AControl Cable · frayedDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD UPPER CONTROL CABLE FRAYED. REPLACED AIRSTAIR DOOR FWD UPPER CONTROL CABLE. ACFT DOWN FOR STRUCTURAL INSP.SDR GUUA94053100609ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT FUSELAGE HAS CORROSION BETWEEN STRINGERS 9L TO 10L AT F.S 408.25. REMOVED DAMAGED SKIN INSTALLED FILLERS AND SHIMS, FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA94053100509ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED SKIN BULGING AND SEVERAL RIVETS PULLED THROUGH SKIN AT LEFT EMERGENCY EXIT AFT CUT OUT FRAME. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN INTERNAL WEB REINFORCEMENT AND AN EXTERNAL DOUBLER REPAIR.SDR GUUA94057093009DStructure · corrodedDURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. CLEANED SURFACE CORROSION AT AREA 1 FOUND TO BE WITHIN ALLOWABLE LIMITS.SDR GUUA94057093009CSpar · corrodedDURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA94057093009BStringer · corrodedDURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. REMOVED CORROSION FROM RIGHT WING AREA 1 FORWARD BONDED STRINGER FOUND TO BE WITHIN ALLOWABLE LIMITS.SDR GUUA94057093009ASpar · corrodedDURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA94057092409ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 123.988 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.SDR GUUA94057060209ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN AREA EXFOLIATED AT RWS 136.86. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.SDR GUUA94052040409ADoor · stiffDURING SCHEDULED ROUTINE MX, DISCOVERED RT AFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLE.SDR GUUA94057030709ASkin · corrodedDURING FUTHER INSPECTION OF SURFACE CORROSION DISCOVERED SEVERE CORROSION EXTENDS FROM WS 140.00 TO 190.00 APROXIMATELY. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA94055030609DSpar Cap · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT HORIZONTAL STABILIZER UPPER REAR SPAR CAP HAS EXFOLIATION. REPLACED RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR CAP.SDR GUUA94055030609CHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED RT ELEVATOR OUTBOARD HINGE BRACKET.SDR GUUA94055030609BHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.SDR GUUA94055030609AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED LT ELEVATOR OUTBOARD HINGE BRACKET.SDR GUUA10200801Mechanism · dirtyDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED EMERGENCY EXIT DOOR 6A WILL NOT OPEN. CLEANED AND LUBRICATED EMERGENCY EXIT DOOR 6A LATCH MECHANISM. OPERATIONAL CHECK NORMAL.SDR GUU2008F00030Snubber · unknownFLIGHT 9237 GHB/FLL, PILOT REPORTED FORWARD DOOR HARD TO PULL. SERVICED AIRSTAIR DOOR SNUBBER. (S)SDR GUU2008F00001Hydraulic System · lowDURING APPROACH AFTER SELECTING THE LANDING GEAR DOWN THE "J" LOCK ENGAGED AND THE CIRCUIT BREAKER TRIPPED IMMEDIATELY. FOUND HYDRAULIC SYSTEM LOW SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECK NORMAL. (K)SDR GUU2008F00014Landing Gear · malfunctionedFLIGHT 9216, AFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPER WHEN GEAR SELECTED UP. INSPECTED MLG PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE. (A)SDR GUUA94053042208ASkin · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT THE LWR FUSELAGE SKIN AT FS 438.250. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA01230801Circuit Breaker · poppedFLIGHT: 9167, DURING APPROACH WHEN SELECTING THE LANDING GEAR DOWN THE LANDING GEAR CB FOR THE MOTOR POPPED. INSPECTED THE LANDING GEAR SYS, PERFORMED LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK NORMAL.SDR GUUA10110702Hinge · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LOWER RUDDER HINGE ASSEMBLY EXFOLIATED. REPLACED LOWER RUDDER HINGE ASSEMBLY.
Back to N16540, cancelled Dec 18, 2012