N395HA
Service difficulty reports · 143
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 = 'N395HA' 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 = 'N395HA' 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 HALA2019020400039Warning System · false activationETOPS SIGNIFICANT SYSTEM - BTB - NAV ADR 2+3 FAULT. F/CTL ALTN LAW. RESET MMR1 PER AMM 34-36. 232582. PERFORMED BOTH ENG RUN TO SIMULATE FAULT AND NO FAULT FOUND. A/C OK FOR SVC, NO FURTHER FAULT OR ISSUE NOTED IAW AMM 71-00.SDR HALA2019020400038Adiru · faultedATB - NAV ADR 3 FAULT. SWAPPED ADIRU NR 2, S/N 56063186, W/FAILED ADIRU NR 3. DEFER BAD ADIRU NOW IN NR 2 RACK PER MEL 34-10-1B. NR 2 ADIRU REPLACED REF AIM 34-11 CHECKS AND TEST PASS.SDR HALA2019011500027Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 MINOR FAULT, AFTER ENG SHUTDOWN. NO FAULTS PRESENT AT THIS TIME.SDR HALA2019011500028Warning System · false activationETOPS SIGNIFICANT SYSTEM - "FUEL LEFT PUMP 2 LO PR" ECAM APPEARED FOR TWO MINUTES DURING CRUISE FLIGHT. TROUBLE SHOT PER TSM 28-21-00-810-852-A NO FAULT FOUND OP CHECK NORMAL.SDR HALA2019010800015Idg · unknownATB - ETOPS SIGNIFICANT SYSTEM - ECAM ELEC IDG (1) OIL LO PRES. REMOVED AND REPLACED NR 1 ENGINE IDG PER AMM 24-21-51. OPS CHECK OK. NO LEAKS NOTED.SDR HALA2018121700663Controller · malfunctionedETOPS SIGNIFICANT SYSTEM - COCKPIT TRIM AIR TEMPERATURE WAY TOO HOT. 125-130. TWICE RESET ZONE CONTROL WITHOUT EFFECT. RESET TEMP CONTROLLER PER A330 AMM 21-63. OPS CHECK GOOD. NO FAULTS. CLEANED TEMP SENSOR. OPS CHECK GOOD. OK FOR SERVICE.SDR HALA2018120500629Warning Message · false activationETOPS SIGNIFICANT SYSTEM - LEFT FUEL PUMP #1 LOW PRESSURE DESCENT.// PERFORMED FCMC BITE & FUEL PUMP L#1 OPE NORMAL PER A330 AMM 28-
51-00. OK FOR SVC.SDR HALA2018112600608Motor · inoperativeETOPS SIGNIFICANT SYSTEM - UNABLE TO START APU. // T/S PER A330 TSM 49-00-00-810-827-A AND REMOVED AND REPLACED FUSE 6KA1 REATTEMPTED START UP OF APU AFTER PRIMING APU FUEL
LINE, NO HELP. FUSE 6KA1 BLOW AGAIN. NEEDS FUSE. REMOVED AND REPLACED STARTER FUSSDR HALA2018102900550Structure · damagedLINE SVC REPORTS DAMAGE ON RH WINGLET. // RH WINGLET REPAIRED AND INSTALLED IAW AMM 57-31-22-400-801A. OK FOR SERVICE.SDR HALA2018090500417Filter · trippedAPU FAULT; SHUT DOWN MANUALLY. FOUND THE APU GENERATOR SCAVENGE OIL FILTER DPI TRIPPED. REMOVED THE FILTER AND NO REMNANTS WERE FOUND. REPLACED THE FILTER IAW AMM 49-91-41-960-801-A. OPS & LEAK CHECKED GOOD. NO FAULTS, TESTED OK.SDR HALA2018053000262Pin · brokenWHEN THE MAIN LANDING GEAR WAS EXTENDED FOR FINAL, ECAM WHEEL, NLG STEERING FAULT. WHEEL PAGE DISPLAYED NLG STEERING. AFTER LANDING UNABLE TO STEER ACFT TO
EXIT RUNWAY. SELECTOR VALVE FOR NLG STEERING 5113GC, BSCU 3GG, CLASS 1 HARD FAULT. TROUBLESHOT IAWSDR HALA2018030100063Warning Message · false activationDURING CRUISE, OBSERVED AN ECAM FOR THE FUEL TANK TRANSFER FAULT. PERFORMED A SITE TEST IAW TSM 28-46. TEST PASSED. FOR FMC 1 AND FMC 2. MESSAGE CLEARED. OK FOR SERVICE.SDR HALA2018022600051Warning Message · false activationECAM STATUS PAGE HAS APU INOPERATIVE, BUT APU IS OPERATING NORMALLY. LAST LEG REPORT INDICATED LUBE PUMP FILTER & GEN SCAV FILTER. TROUBLESHOT IAW TSM 49-62-00-810-916-A. PERFORMED APU BITE IAW AMM 49-00-00-740-802-A. TESTED OK. CHECKED DPI OF LUBE OIL FISDR HALA2018022600050Warning Message · false activationFUEL TANK TRANSFER FAULT DURING DESCENT, PASSING 16,000 FT. PERFORMED SYSTEM TEST OF FCMC 1 & FCMC 2 IAW AMM 28-51-00-740-801-A. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2018013000013Elevator System · faultedAIR TURNBACK DUE TO AN ELEVATOR SERVO FAULT AND PRIM 1 PITCH FAULT DURING CRUISE AT FL410. REPLACED THE FLIGHT CONTROL PRIMARY 1, REPLACED CONNECTOR B WITH CONTACT OF R G ELEVATOR SERVO, REPLACED PLU 5212VC-A AND CONTACTS R AND D, LP 4516199SDR HALA2018013000023Connector · damagedATB DURING FL410 CRUISE, RECEIVED A F/CT ELEVATOR SERVO FAULT ON ECAM. REMOVED AND REPLACED THE FLT CONTROL PRIM 1 PB IAW ESPM 20-45-11. OPS CHECKED GOOD IAW AMM 27-96-00 AND CONTINUITY CHECK. FOUND PIN C ON B CONNECTOR LOOSE TENSION. REMOVED AND REPLACEDSDR HALA2018012600015Transducer · malfunctionedELEVATOR SERVO FAULT DURING CRUISE, FOLLOWED BY F/CTL PRIM 1 PITCH FAULT FOR 30 SEC, THEN CLEARED 1MIN, FOLLOWED BY F/CTR ELEVATOR SERVO FAULT SHOWING LT ELEV B & RT ELEV G AMBER BOXED ON F.CTLPG. REPLACED THE LT ELEVATOR POS TRANSDUCER IAW AMM 27-98--17, SDR HALA2017122200314Warning Message · illuminatedDURING APPROACH, FUEL AFT TRANSFER ECAM MESSAGE. FAULT CLEARED AFTER LANDING. RESET FCMC 1 & 2. OK FOR SERVICE.SDR HALA2017121900303Warning Light · false activationAPPROXIMATELY 15 MILES FROM LANDING, THE FUEL AFT TRANSMITTER ECAM ILLUMINATED. CLEARED ITSELF AFTER ENGINE SHUTDOWN. NO ECAM MESSAGE. PERFORMED BITE IAW AMM 28-51-00. NO TROUBLE FOUND.SDR HALA20171800293Transfer Sys · malfunctionedDURING FINAL APPROACH, FUEL TANK TRANSFER FAULT. CHECKED CMC & CORRELATE FAULT MESSAGE FOUND. TROUBLESHOT IAW TSM 28-27-00. PERFORMED FCMC BITE TEST & TEST OK. OK FOR SERVICE.SDR HALA2017121900304Fire Loop · faultyETOPS SIGNIFICANT SYSTEM - ECAM:ENG1 LOOP B INOP. PERFORMED BITE TEST OF THE FDU1 PER AMM 26-12-00.FOUND CLASS 1 MESSAGE 261215 ENG 1 FIRE LOOP B/FDU1(1WD1). FOUND PYLON LP (6WD1) GAS LEAK. REPLACED PYLON LP DETECTOR (6WD1) PER AMM 26-12-16-400-808-A - CONTINUSDR HALA2017121800300Transfer Sys · malfunctionedFUEL T TANK XFER FAULT ECAM FOR 2 MIN FUEL 15880 0 FUEL IN T TANK. ACCOMPLISHED TSM 28-27-00-810-829-A.FCMS FUEL VALVES TEST OK IAW AMM 28-51-00-710-801.FCMS BITE TEST OK, IAW AMM 28-51-00-740-801. ACFT OK FOR SERVICE.SDR HALA20171800294Transfer Sys · malfunctionedFUEL T TANK TRANSFER FAULT ECAM FOR 2 MIN FUEL 15880 0 FUEL IN T TANK. ACCOMPLISHED TSM 28-27-00-810-829-A.FCMS FUEL VALVES TEST OK IAW AMM 28-51-00-710-801.FCMS BITE TEST OK, IAW AMM 28-51-00-740-801. ACFT OK FOR SERVICE.SDR HALA2017111308096Sign · detachedR3 DOOR EXIT SIGN DETACHED. SECURED THE SIGN.SDR HALA2017081500223Check Valve · crackedLT EMERGENCY RAM AIR CHECK VALVE CRACKED 3/4 THE WAY DOWN 1 SIDE OF VALVE. REMOVED & REPLACED LT RAM AIR CHECK VALVE PER MM 21-55-41.SDR HALA2017072400214Pump · unknownRIGHT FUEL PUMP 1 LOW PRESSURE IN CRUISE, TURNED OFF THE RIGHT PUMP 1, STANDBY OPERATED NORMALLY. PERFORMED OP CHECK OF RT 1 FUEL PUMP IAW FIM 28-21-00-810-852-A, AND AMM 28-21-00-710-801-A. ALL TEST NORMAL NO FAULTS NOTED. ACFT OK FOR SERVICE.SDR HALA2017071600198Warning Message · false activationAIRCRAFT ABORTED TAKEOFF BELOW 80 KNOTS DUE TO ECAM MESSAGE F/CTL PRIM 1 PITCH FAULT. RESET PRIMARY 1, 2, 3 AND SEC 1 AND 2.SDR HALA2017071700191Warning System · false activationON TAKEOFF ROLL, BELOW 80 KTS ECAM MSG "F/CTL PRIM 1 PITCH FAULT. DID EFCS 1 AND 2 BITE. DID AFS BITE RESET PRIM 1,2,3. SEC 1,2 OPS CHECK GOOD PER AMM 27-96-00. OK TO CONTINUE.SDR HALA2017010500002Skin · dentedA DENT WAS FOUND ON THE AFT CARGO DOOR INNER SKIN BETWEEN FRAMES 61 & 61A, BETWEEN BEAMS 4 & 5. TRIMMED OUT DAMAGE AREA, INSTALLED REPAIR FILLER AND REPAIR DOUBLER IAW ER/A 554066-14.SDR HALA2016082900339Warning Light · false activationFUEL RIGHT PUMP 1 LOW PRESSURE ILLUMINATED DURING CRUISE. TROUBLESHOT IAW TSM 28-21-00-810-855A, ACCOMPLISHED FAULT ISOLATION PROCEDURE & FCMS 1&2 BITE TEST,OK AS PER AMM 25-51-00-740-801A. PUMP OPS TEST ALSO NORMAL. ACFT OK FOR SERVICE.SDR HALA2016072000142Packing · damagedAIRCRAFT 395, AIR TURNBACK TO DEPARTURE DUE TO THE GREEN HYDRAULIC SYSTEM LOW ECAM MESSAGE APPEARED 45 MINUTES INTO THE FLIGHT AT FL370, RESERVOIR SHOWS HALF EMPTY, ALL GREEN PUMPS TURNED OFF. FOLLOWED MANUAL GEAR EXTENSION AND OTHER GREEN HYDRAULIC SYSTEM OUSDR HALA2016071700275Packing · damagedGREEN HYD SYS LOW ILLUMINATED 45 MINS INTO FLIGHT, RESERVOIR SHOWS HALF LOW. ALL GREEN PUMPS TURNED OFF. AIRCRAFT RETURNED TO THE DEPARTURE STATION. FOUND HYD LEAK GREEN SYS HP MANIFOLD PLUG CAP IAW IPC29-11-03-06, FIN5102JH. REPLACED PACKING AND LEAK CHECSDR HALA2016021900058Eec · malfunctionedDURING START OF ENGINE NR 2, ENGINE 2 CONTROL SYS FAULT, ECAM DISPLAYED. ENGINE NR 2 STARTED NORMALLY WITH NO ABNORMAL INDICATIONS. ACCOMPLISHED TSM 71-00-00-810-924A FOR ENGINE 2 CONTROL SYS FAULT MSG BITE TESTED ELECTRONIC ENGINE CONTROL 2 BITE PASSED NOSDR HALA2016021900057Eec · malfunctionedNR 2 ENGINE CONTROL SYS FAULT ON START, ACCOMPLISHED ECAM ACTIONS. RESTARTED NR 2 ENGINE NORMAL INDICATIONS. LAST LEG REPORT NO FAULT ON BOTH CHANNELS OF THE NR 2 ENGINE ELECTRONIC ENGINE CONTROL 2 SYSTEM TEST OK, IAW AMM 73-21-00-710-812-A.SDR HALA201512100245Servo Valve · malfunctionedFLIGHT CONTROL SEC 1 FAULT AFTER LANDING. FLIGHT CONTROL ELEVATOR SERVO FAULT WITH ASSOCIATED CLASS 1 R G ELEV SERVO CONTROL SERVICE. TROUBLESHOT IAW TSM. REPLACED RT GREEN SYS ELEVATOR SERVO VALVE IAW AMM. OPS CHECK OK. NO FAULTS FOUND. OK FOR SERVICE.SDR HALA2015110505035Apu · malfunctionedRETURNED TO DEPARTURE DUE TO APU T/R SHOWING 304A DURING CRUISE. REPLACED APU T/R.SDR HALA2015110500026Apu · faultedIN CRUISE FLT NOTED ELECT DC PAGE "APU TR" SHOWING 304A, NORMALLY 0, APU OFF FOUND APU TR INDICATING 30V/304A, GREEN. ACCOMPLISHED FWC SYS TEST, BLC BITE TEST AND MCDU APU TR RESET. NO FAULTS NOTED. CONDITION SAME. APU BATTERY COOL TO THE TOUCH. NO EVIDENCSDR HALA201510290023Control Valve · dirtyAIR PACK 2 REGULATOR FAULT. PACK 2 TEMP CONTROL VALVE, PACK 2 TEMP SENSOR. CLEANED UP NR 2 TEMP CONTROL VALVE IN NR 2 PACK SYS. OPS CHECKED AND BITE ECS PACK 2 SYS OK IAW AMM21-63-00.SDR HALA201508030147Actuator Valve · failedNR 1 FUEL LP VALVE FAULT DURING APPROACH. INDICATED VALVE DISAGREE ON EICAS. REPLACED THE NR 1 LP VALVE ACTUATOR. OPS CHECKED OK. SYSTEM TEST NORMAL IAW AMM 28-24-00.SDR HALA2015052005011Actuator · failedACCOMPLISHED AN AIR TURNBACK DUE TO FUEL JETTISON LIGHT ON ECAM. REPLACED FUEL JETTISON VALVE ACTUATOR. REPLACED RT JETTISON ACTUATOR. LP 6070619.SDR HALA2015051800088Actuator · malfunctionedFUEL JETTISON LIGHT ON, FUEL JETTISON IN PROCESS, ECAM LIGHT. VALVE LOCK AND DUMMY PLUGS INSTALLED IN RT JETTISON. REMOVED VALVE LOCK & DUMMY PLUGS. INSTALLED NEW ACTUATOR IN RT JETTISON IAW AMM 28-31-51. OPS TEST GOOD AT THIS TIME. PERFORMED FCMS BITE TESDR HALA2015020300019Pump · malfunctionedAPU AFT FUEL PUMP STATUS MESSAGE AND LOW FUEL PRESSURE ON APU PAGE DURING APU INITIAL OPERATION. TROUBLESHOT IAW TSM 49-00-00-810-816-A. R & R APU AFT FUEL FEED PUMP, LEAK AND OPS TEST GOOD, IAW AMM 28-22-52 AND 49-34-11. NO STATUS MESSAGES NOTED, OK FOR SSDR HALA2014112400196O-Ring · leakingAIR DIVERSION, HYD Y RESVOIR LOW LEVEL. IAW FLT CREW THEY SHUTOFF YELLOW HYD PUMP AND ENGINE PUMP. RESERVOIR NOT EMPTY. PUMPS DID NOT CAVITATE. FOUND ON YELLOW HP MANIFOLD. CAPPED OFF LINE, O-RING BAD, REPLACED O-RING IAW AMM 29-00-00, AND LEAK CHECKED IA
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