N475HA
Service difficulty reports · 84
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 = 'N475HA' AND registry_match = 'registration' 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 = 'N475HA' AND registry_match = 'registration' 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 HALA2010031200101Via · failedATB - FUEL QTY SYS FAIL, AIR DATA 1 FAIL, BLEED AIR L FAIL APU FAULT, PCU FAULT, GPWS FAIL SEL CABIN PRESS MAN, GPSY FAIL, LT AIR SENS FAIL DISPLAYED. TROUBLESHOT SYSTEMS AND FOUND NR 2 VIA CAUSING ASSOCIATED FAILS. REMOVED AND REPLACED NR 2 VIA PER AMM 31-SDR HALA2010020300050Compressor · damagedDURING EXTERNAL AIR START, ABORTED START ATTEMPT DUE TO HIGH EGT (680 DEGREES). R & R LT EEC IAW AMM 73-21-01, CONDITION SAME. ACCOMPLSHED BOROSCOPE INSP IAW AMM 72-50-00. FOUND HPC STAGES 9 & 20 AND STATOR DAMAGED DUE TO FOD. R & R NR 1 ENGINE. OPS AND LEASDR HALA2010010400010Skin · crackedFUSELAGE CRACKED AT STA 1022, 1.1/2" ABOVE LT LONGERON 8R. CRACK LENGTH 5/8". CRACK VERIFIED WITH EDDY CURRENT. ENDS OF CRACK MARKED. REPAIR IN WORK.SDR HALA201001040001AStructure · crackedOPEN - FUSELAGE CRACKED AT STA 1022, 3 1/2" ABOVE LT PYLON. CRACK LENGTH 3/4". REPAIR IN WORK.SDR HALA2010010400009Structure · crackedFUSELAGE CRACKED AT STA 1022, 3 1/2" ABOVE LT PYLON. CRACK LENGTH 3/4". REPAIR IN WORK. OPENSDR HALA2009102500484Connector · damagedSEAT MOUNTED EXIT PATH EMERGENCY LT INOP ROW 8. REPAIRED BROKEN PIN LUG CONNECTOR OPS CHECK GOOD.SDR HALA2009090100397Fire Detector · failed"FIRE DET L FAIL" ALERT INFLIGHT. REPLACED LT ENG GEARBOX FIRE DETECTION ASSY IAW AMM 26-11-02. OPS TEST OK.SDR HALA2009040100119Door · damagedMETAL SEPARATION NEAR AFT CARGO DOOR. RUBBER DEPOSIT LEFT BELOW DOOR FROM BELT LOADER. REPAIR PER M105 FILE R0018 INSPECTED AREA NO DEFECTS NOTED EDDY CURRENT CHECKS OK OK FOR SERVICE.SDR HALA2009021100045Position Sensor · out of adjustATB - AFTER TAKEOFF ELEV SPLIT ANNUNCIATED, RETURN TO GND. RE-ADJUSTED ELEVATOR POSITION SENSOR PER AMM 27-34-01. OPS CHECKED OK. CLEAR MIC SHEET. PLACARD REMOVED.SDR HALA2008102300826Battery · failedBATTERY CHARGER FAIL LIGHT ON CLIMBOUT. REPLACED ALL 3 BATTERIES PER AMM 24-34-01.SDR HALA0800822Valve · faultedBTB - NR 2 ENGINE HOT START, MAX TGT 700 DEG. INTERROGATED NR 2 EEC FOUND STARTER AIR VLV FAULT. START TEMP WITHIN LIMITS PER MM 71-00-05. REPLACED START VLV PER M/M 80-11-03, OPS CHECK LEAK CHECK GOOD. P/N 3291678-2, S/N ON 182C OFF 378.SDR HALA0800544Door · damagedRT MLG OUTBOARD DOOR AFT STAINLESS STEEL EDGE DENTED BETWEEN 6" AND 14" FROM TOP EDGE. ALL LDG GEAR PINS INSTALLED AND SAFETY WIRED. REMOVED AND REPLACED RT MLG OUTBD DOOR SEAL. INSTALLED NOSE LANDING GEAR DOOR PER AMM TASK 32-14-0-400-801. ADJUSTMENT ACCOSDR HALA0800542Skin · dentedUNDER SIDE OF WING PANEL P/N 5912161-4512 ABOVE NR 3 MLG TIRE AREA HAS DENT APPROX 1.5 INCH DIAMETER AND .25 DEEP. OK TO CONTINUE PER GMM43.1. OK TO CONTINUE PER HAL M105 FILE NR 475127 INSPECTION FIRST FLIGHT EACH DAY, TAP TEST MARKED BOUNDARY OF DENT ENSURSDR HALA0800541Tire · failedNEED TO REPLACE NR 4 MLG TIRE DUE TO RECAP SEPARATION. REPLACED NR 4 MLG TIRE PER AMM 32-41-01, SPIN CK GOOD.SDR HALA0800369Relay · failedEMERGENCY POWER TEST FAILED. REMOVED AND REPLACED EMERGENCY POWER RELAY, OPS CHECK OK IAW BOEING AMM 24-24-00.SDR HALA0700341Connector · unknown"ENG L SYS FAIL" ANNUNCIATED ON TAXI IN. PERF EEC-1 BITE, FOUND CURRENT FAULT 732102 ENG POSITION ID CIRCUIT CH-A, T/S PER FIM 73-21-00-810-804, RESEATED CONNECTOR P1-8204, EEC-1 FAULTS CLEARED, RTS PASSED, GRD ENG RUN CHECK GOOD.SDR HALA0700340Eec · faultedFIM 732102 "LEFT ENG SYS FAIL" CAME ON AFTER ENGINE START. FOUND NR 1 ENG EEC1 FAULT. REPLACED NR 1 ENG EEC PER 73-21-01-741-801. RTS CK OK.SDR HALA0700249Actuator · leakingON TAXI CHECKS, RUDDER CONTROL CHECK REQUIRED APPROX TWICE THE EFFORT TO DEFLECT THE RUDDER. HYD PRESSURE = 3000 PSI. TROUBLE SHOT AND FOUND RUDDER PEDALS STIFF, FOUND POWER PACK BYPASSING. REMOVED RUDDER HYDRAULIC ACTUATOR PER AMM 27-28-02. INSTALLED RUDDSDR HALA07000247Control Cable · out of rigDURING FLIGHT CONTROL CHECK RUDDER PEDAL TRAVEL IS STIFF. FOUND RUDDER CONTROL CABLE OUT OF RIG. ADJUSTED RUDDER CONTROL CABLE SYSTEM PER BOEING 717 AMM 27-20-00. PERFORMED OPS CHECK OF RUDDER PEDAL PER AMM 27-20-00. CHECKED OK. INSPECTED CABLE RUN AFT OFSDR HALA0700047Proximity Sensor · malfunctionedFOUND LEFT LANDING GEAR RED IN TRANSIT LIGHT ON. QRH PROCEDURE FOLLOWED. RED LIGHT STILL ON INFLIGHT. NO VIBRATION OR NO NOISE. BITE CHECKED PROX BOX, NO FAULTS NOTED. CHECKED UPLOCK SENSOR PER 32-61-00. NO FAULTS NOTED, GEAR SWING ACCOMPLISHED. READINGSDR HALA0600858Controller · malfunctionedFOUND SMOKE IN CABIN. FOUND FWD PLASTIC DUCT AND GRILL MELTED. VISUALLY INSPECTED WIRING AROUND FWD DUCT/GRILL. NO DEFECTS FOUND. REMOVED AND REPLACED BOTH TEMP ANTICIPATOR SW PER AMM 21-52-03. OPS CK OK. REPLACED THERMAL SW 190 DEG SHUTDOWN FOR BOTH LT SDR HALA0600730Battery · dischargedFWD ENTRYWAY EMERGENCY LIGHT FLICKERS THEN DIES OUT. REMOVED AND REPLACED FWD ENTRYWAY EMERGENCY LIGHT BATTERY PER AMM 33-51-03, OPS CHECK GOOD. CONDITION AND SECURITY GOOD.SDR HALA0600696Frame · crackedL FUSELAGE L END OF FRAME STA237 L18LT - L19LT 2" CRACK. OK TO CONTINUE PER M105 NR 475090.SDR HALA0600695Skin · dentedIMPACT DAMAGE ON LT FUSELAGE 3' AFT OF MED AND 5" BELOW CASP DENT IN ACFT SKIN BETWEEN LONG 18 AND 19 LT SIDE AT APP STA 215 .016 BY 2 BY 2.5 STA 222 .049 BY 3.5 BY 3. OK TO CONTINUE PER GMM4-3.2SDR HALA0600640Control Module · unknownAILERON TRIM IS INTERMITTENT TO THE RIGHT-TRIM GETS STUCK OCCASIONALLY. REMOVED AND REPLACED CAPT AILERON/RUDDER TRIM CONTROL MODULE IAW AMM 27-10-07. OPS CHECK GOOD.SDR HALA0600538Warning Light · illuminatedBTB - LT AFT FUEL PUMP LOW LITE ON AFTER ENGINE START. OK TO CONTINUE PER C 28-22-01SDR HALA0600492Panel · crackedFOUND THRUST REVERSER PANEL CRACKED. INBOARD SIDE AFT OF (NR 2 ENG) REPLACED LEFT SIDE BEAM FAIRING, SECURITY CHECK OK, P/N 715-0320-501/715, PANEL NR 424GR RT ENG.SDR HALA0600444Smoke Detector · malfunctionedCARGO SMOKE FAIL TEST. PERFORMED SELF TEST. TEST PASSED, NO FAULTS NOTED.SDR HALA0600385Structure · corrodedRT WING TOP 5 AREAS OF MODERATE CORROSION JUST AFT OF NR 4 SLAT (MARKED). REMOVED CORROSION AT 5 AREAS PER SRM 51-10-04. BLENDED AREAS OK PER HALM105 NR 475086.SDR HALA0600384Fastener · corrodedRT WING TOP MODERATE CORROSION 3 FT INBOARDD OF OVERWING FUEL CAP APPROX 2 X .75 INCHES. REMOVED CORROSION GROUND HI-LOK PIN PER SRM 51-10-04. REMOVED & REPLACED HI-LOK PIN AT APPROX STA XRS 399 8 INCHES FROM FWD SPAR. BLEND OK PER HALM105 NR 475086. LEAK SDR HALA0300700Support Fitting · crackedHNL - FOUND LEFT WING INBOARD SPOILER HAS A CRACK ON THE OUTBOARD SPOILER ACTUATOR SUPPORT FITTING. REPAIR IN WORK. (M)SDR HALA0200464Inlet · crackedHNL - FOUND 4 INCH CRACK ON APU INLET BOX, APU INOPERATIVE. OK TO CONTINUE PER MEL 49-10-01. (M)SDR HALA0200110Rotor · inoperativeDURING CLIMBOUT RIGHT ENGINE SYSTEM FAULT ALERT ON . CREW UNABLE TO CONFIRM FAULT CODE NUMBER. ON ARRIVAL HNL OIL PRESSURE DROPPED TO 2PSI OIL TEMP RISING TO 102 DEGREES. OIL QUANTITY DROPPED TO 2PSI OIL TEMP RISING TO 102 DEGREES. OIL QUANTITY DROPPED TO SDR HALA0100176Control Column · disconnectedFLT 345 - OGG - DURING FLIGHT CONTROL CHECK, THE LEFT AND RIGHT COLUMNS DISCONNECTED DURING ELEVATOR CHECK. RE-SET CONTROL COLUMN PER MM 27-31-10-44-801. OPS CHECK OK. (M)
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