N6816, cancelled Oct 11, 2012
Service difficulty reports · 19
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 = 'N6816' AND deregistration_id = 'N6816-2012-10-11' 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 = 'N6816' AND deregistration_id = 'N6816-2012-10-11' 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 GAIA01306OPLight · inoperativeDURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA01241OPSConnector · dirtyFLT 718 - ELP - ON CLIMB-OUT, FLAPS RETRACTED NORMALLY. THEN AMBER 'L/E FLAPS' LIGHT ILLUMINATED AT 8,000 FT CONFIRMED DOWN L/E NR 6 ON FE PANEL. LOWERED FLAPS AT 230 KIAS TO 2 DEGREES WITH NORMAL GREEN LIGHT AN NO AMBER. RETRACTED AND 'L/E FLAPS' REMAINED SDR GAIA01007BDump Valve · inoperativeFLT 202 - BIL - RIGHT FUEL DUMP NOZZLE VALVE WOULD NOT OPEN TO DUMP. AIRCRAFT MADE AN UNEVENTFUL RETURN TO BIL. REMOVED AND REPLACED NR 4 FUEL DUMP VALVE IAW B727 MM 28-31-1. AIRCRAFT RETURNED TO SERVICE. (M)SDR GAIA01006BFuel Door · damagedFLT 202 - BIL - NR 5 TRAILING EDGE FLAP WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL RETURN TO BIL. UPON INSPECTION OF AIRCRAFT, FOUND FUEL DOOR OPEN AND DAMAGED. ALSO FOUND NR 6 LEADING EDGE SLAT DAMAGED. REMOVED AND REPLACED NR 6 SLAT PERSDR GAIA00365Controller · misinstalledFLT 727 - MHR - LOSS OF HYDRAULIC FLUID, THEN PRESSURE (HYDRAULIC SYSTEM A). ALTERNATE FLAPS OPERATION REVERSED. AIRCRAFT RETURNED AND MADE UNEVENTFUL LANDING AT MHR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT SWITCH. SYSTEM TEST GOOD AND AIRCRAFT WAS RETURSDR GAIA00365APump · failedFLT 727 - MHR - LOSS OF HYDRAULIC FLUID, THEN PRESSURE (HYDRAULIC SYSTEM A). ALTERNATE FLAPS OPERATION REVERSED. AIRCRAFT RETURNED AND MADE UNEVENTFUL LANDING AT MHR. VERIFIED PROPER OPERATION OF I/N AND OUTBOARD ALTERNATE FLAPS. FOUND CONNECTORS TO INDICASDR GAIA99271Light · inoperativeNO FLIGHT FOUND DURING GROUND MX AT DFW, MAIN ENTRY DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED MAIN ENTRY EMERGENCY EXIT LIGHT. SYSTEM TEST GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA99236Frame · corroded'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). FRAME WEB AT BS 227.8 WL 208.1 TO WL 224 CORRODED OUT OF SRM LIMITS. CUT OUT CORROSION DAMAGED AREAS IAW ENGINEERING DEVIATION REQUEST B2-07307. APPLIED PSDR GAIA99235Spar · corroded'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). VERTICAL STABILIZER FORWARD SPAR CORRODED AT FS 55R. REMOVED DAMAGED AREA IAW ENGINEERING DEVIATION REQUEST B2-07305. PERFORMED HFEC AND LIGHT INSPECTION SDR GAIA99234Tee · worn'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). VERTICAL STABLIZER LEFT SIDE T-CHORD WORN AT PANEL NR 9601. REMOVED DAMAGE IAW ENGINEERING DEVIATION REQUEST (EDR B2-07298). PERFORMED HFEC IAW B 727 NDT SDR GAIA99233Floorbeam · cracked'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). FLOOR BEAM UPPER CHORD AFT FLANGE CORRODED AND CRACKED AT FASTENER HOLE. (BS 950F, RBL 62.0). REMOVED DAMAGED AREA IAW B 727 SRM 53-10-8. FABRICATED DOUSDR GAIA99232Web · cracked'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). WEB CRACKED AT FLOOR SUPPORT, BS 848.0, RBL 50.0. STOP DRILLED CRACK IAW B727 SRM 51-10-1. PERFORMED HFEC IAW 727 NDT MANUAL PART 651-00-00 FIG 11 AND FIGSDR GAIA9977Air Dist · odorFLT 1756 - HUF-CLT - AT FLT LVL 290 SMELLED ODOR FROM CARGO COMPARTMENT. EMERGENCY WAS DECLARED AND CHECKLIST COMPLETED. NORMAL LANDING AT CLT. PERFORMED HAZ MAT INSPECTION FOR POSSIBLE HAZ WASTE SPILLAGE IAW THE KHA GMM CHAPTER 18. NO DEFECTS NOTED. AIRCSDR CKSA97616Bushing · badDURING CRUISE AT FL290, .78 MACH WITH LIGHT TURBULENCE, NOSE GEAR DOOR LIGHT CAME ON INTERMITTENTLY ALONG WITH LOUD BANGING FROM NOSE GEAR DOORS. RAISING GEAR HANDLE TO UP POSITION NO HELP. HAD TO SLOW TO 270 KNOTS FOR REMAINDER OF FLIGHT. FOUND AFT BRACKETSDR CKSA97588Switch · bindingNOSE GEAR DOORS FLUTTER IN FLIGHT, ACCOMPANIED BY RED DOORS LIGHT ON FORWARD PANEL. INSPECTED AND CHECKED NOSE GEAR DOORS FOLLOW UP LINKAGE. NO DEFECTS NOTED. LUBED GEAR DOOR F0LLOW UP LINKAGE. FOUND RT NOSE GEAR DOOR SWITCH BINDING. CLEANED SWITCH FROM CSDR CKSA97182Retract Mech · out of adjustNOSE GEAR DOOR ANNUNCIATOR LIGHT ILLUMINATED AND NOSE GEAR DOORS CHATTERING WITH AIRSPEED AT APPROXIMATELY 310 KNOTS. ADJUSTED NOSE WHEEL GEAR WELL DOORS IAW BMM CHAPTER 32-22-1.SDR CKSA97180Switch · corrodedNOSE GEAR DOORS VIBRATE IN FLIGHT AND DOOR LIGHTS ILLUMINATE. PLACED GEAR HANDLE IN UP POSITION, VIBRATION STOPPED. FOUND LOOSE AND CORRODED TERMINAL ON SWITCH. CLEANED AND TIGHTENED AS REQUIRED, CHECKS GOOD.SDR CKSA95084Connections · dirtyCVG - ON GEAR RETRACTION WITH THE GEAR LEVER IN THE UP POSITION LEFT MAIN GEAR RED AND GREEN LIGHTS STAYED ON. ALL OTHER INDICATIONS WERE NORMAL. GEAR EXTENSION AND RETRACTION OPERATED NORMAL. CLEANED CONNECTIONS ON LANDING GEAR ACCESSORY UNIT. OPS CHECKEDSDR CKSA95001Angle · crackedOSC - CRACK IN ANGLE AND WEB FORWARD OF APU LT GEAR WELL, FORWARD OF APU. REPLACED ANGLE AND REPAIRED WEB IAW 727 SRM CHAPTER 51, FIGURE 51-40-2, FIGURE 1. REPLACED APU FORWARD WEB VERTICAL STIFFENER, STA 870, LT GEAR WELL, FORWARD OF APU. (X)
Back to N6816, cancelled Oct 11, 2012