N383HA
Service difficulty reports · 228
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 = 'N383HA' 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 = 'N383HA' 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 HALA2016111500514Fire Loop · faultyENG 2 FIRE LOOP A FAULT, TSM 26-12-00 CKED LOSS OF DETECTOR ENG 2 LOOP A. REPLACED DET FIRE, PYLON PER AMM 26-12-00. OPS CK OK.SDR HALA2016080800322Indicator · malfunctionedPOWER INTERRUPTION, DOUBLE AMBER BARS THRU FUEL USED COUNTERS REPORTED BY FLT CREW. RESET BFCMC. PERFORMED BITE TEST IAW AMM 28-51-00-740-801A OK. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2016072600146Valve · leakingAIR TURNBACK TO DEPARTURE DUE TO FUEL LEAK FROM RIGHT JETTISON VALVE. REPLACED THE JETTISON VALVE ASSEMBLY IAW AMM 28-31-41.SDR HALA2016072400301Valve · unknownAIR TURNBACK DUE TO FUEL LEAK FROM RIGHT JETTISON VALVE. REMOVED AND REPLACED THE VALVE JETTISON ASSY IAW AMM 28-31-41. OPS & LEAK CHECKED GOOD.SDR HALA2016072400299Plunger · lack of lubeRAT WILL NOT STOW. LUBRICATED TURBINE LOCK PLUNGER CABLE. OPS CHECKED GOOD.SDR HALA2016072300300Flow Divider · malfunctionedAIR TURNBACK, APU FAILED TO START THREE TIMES FL390 TEMP -55 EGT OVERTEMP 950 DEG C. PERFORMED APU BITE IAW AMM 49-62 FAULTS APU FUEL FLOW
DIVIDER. R & R THE FUEL FLOW DIVIDER IAW AMM 49-31. OPS CHECKED NORMAL.SDR HALA2016062900264Unknown · odorON INBOUND FLIGHT ON T/O F/A'S NOTICED AN UNKNOWN ODOR FROM THE AFT OF ACFT THRU FWD OF ACFT INCLUDING FLT DECK, DISSIPATED DURING CRUISE,
THEN ODOR APPEARED AGAIN ON DESCENT. RAN ENGINES 1 AND 2 AND APU NO ODOR NOTED. PERFORMED AMM 12-33-21-618-801-402SDR HALA2016030300063Unknown · odorDURING T/O ROLL, STRONG , FOUL MUSTY ODOR CAME OUT OF VENTS, BOTH IN COCKPIT AND THROUGHOUT ACFT. CAUSED CONCERN TO BOTH F/A AND PASSENGERS, DISSIPATED DURING CLIMB. DEBRIEFED CREW. ODOR ALSO PRESENT ON DECENT AT THROTTLE BACK. APU NOT RUNNING. PERFORMED SDR HALA2016010200001Igniter · failedAPU FAILED TO START AFTER THREE ATTEMPTS. REPLACED APU IGNITER IAW AMM 49-41. OPS CHECKED NORMAL. APU STARTS AND RUNS NORMAL. ACFT OK FOR SERVICE.SDR HALA2015112305037Unknown · odorAIRCRAFT DIVERTED, DUE TO STRONG CHEMICAL SMELL IN COCKPIT WHILE IN FLIGHT. PERFORMED TSM 71-00-81-810-805-A, BOROSCOPED NR 1 AND 2 ENGINES-NO TROUBLE FOUND. REMOVED MCDU'S AND INSPECTED, NO TROUBLE FOUND, RE-INSTALLED MCDU'S LP 8054092. ACFT RELEASED FOR ESDR HALA2015112200240Unknown · odorSTRONG CHEMICAL SMELL IN COCKPIT WHILE IN FLIGHT. PERFORMED TSM71-00-81-810-805-A THRU STEP4.A, 3, L HAS BEEN COMPLETED THE FIRST 4 ITEMS-NO TROUBLE NOTED. BOROSCOPE OF IP OVERPRESSURE HAS BEEN ACCOMPLISHED ON 1 AND 2 ENGINES-WAITING FOR RESULTS AFTER PICTURSDR HALA201506250116Isolation Valve · abnormalBULK CARGO VENT FAULT ON SHUTDOWN. R & R BULK CARGO VENT VALVE IAW AMM 21-28-56, SYSTEM TEST C/W IAW AMM 21-28-710-802-A, VENT VALVE OPS CHECK GOOD.SDR HALA2015031805007Valve · malfunctionedAIRCRAFT RETURNED TO DEPARTURE DUE TO AIR NR 1 ENGINE BLEED FAULT PRIOR TO ENTERING ETOPS AIR SPACE. REPLACED NR 1 ENGINE PRV.SDR HALA2015031600039Bleed Valve · malfunctionedDURING CLIMBOUT ECAM AIR ENGINE BLEED FAULT. R & R NR 1 ENGINE, INTERMEDIATE BLEED VALVE IAW AMM36-11-52. LEAK & OPS CHECK GOOD IAW AMM 36-11-52-790-807A. OK FOR SERVICE.SDR HALA2014120700203Fmu · failedECAM ON TAKEOFF ROLL AT 80KTS, ENG 1 SYS CTL FAULT. ABORTED T/O, RETURNED TO GATE. REMOVED NR 1 ENG FMU IAW AMM 73-21-52-000-802A. INSTALLED FMU IAW AMM 73-21-52-400-802A. OPS AND LEAK CHECK GOOD. REF LP 6094691 FOR VERIFICATION FLIGHT.SDR HALA2014092500154Skin · damagedAFT CARGO DOOR INNER PANEL SKIN DAMAGED BETWEEN FRAME 62 & FRAME 62A, BEAM 5 FROM CARGO LOCK. BLENDED DAMAGED AREA. DIMENSIONS AFTER BLEND ARE 0.5" X 0.5". DEPTH OF DENT IS .095 AND .032 REMAINING THICKNESS. NO CRACK INDICATION. CUT OUT DAMAGE AREA IAW SRMSDR HALA2013052600073Igniter · malfunctionedAPU SHUTDOWN ON START. SYS REPORT SHOWS IGNITOR PLUG (59KA31), IGNITOR EXCITER (59KA10), CLASS 1 FAULT. R & R IGNITOR PLUGS IAW TSM 49-41. RAN APU & OPS CHECK NORMAL.SDR HALA2013052600072Igniter · faultedAPU SHUTDOWN ON START. SYS REPORT SHOWS IGNITOR PLUG (59KA31), IGNITOR EXCITER (59KA10) CLASS 1 FAULT. R & R IGNITOR PLUGS IAW TSM 49-41. RAN APU & OPS CHECK NORMAL.SDR HALA2013052000064Apu · unknownAPU AUTO SHUTDOWN ON START UP. PERFORMED OPS TEST OF THE APU IAW AMM 49-00-00-710-801. TESTED OK.SDR HALA2013051300058Warning Message · false activationAFTER STARTING ENGINE RECEIVED NR 1 ENGINE OVERSPEED PROT FAULT. TROUBLESHOT IAW TSM 73-21-72-810-925-A. RAN BOTH ENGINES FOR FIVE MINUTES, NO FAULTS, ON START,ON SHUTDOWN, INTERMITTENT FAULT, IAW TSM. OK FOR SERVICE.SDR HALA2013042800047Blade · bentNR 1 ENGINE HAS BENT BLADE, 7.5 INCHES FROM FILLET ON NR 9 FAN BLADE. PERFORMED AMM 72-31-41-200-801-A, FOUND WITHIN LIMITS IAW AMM.SDR HALA2013031900030Lavatory · cloggedAIR TURNBACK, LAVATORY 3L OVERFLOWING INTO CABIN AND GALLEY. REMOVED CLOG OPS CHECKS OK.SDR HALA2012091600207Unknown · odorAPP 3 HRS FLT F/A & PAX IN MID CABIN DETECTED ODOR OR BURNING ELECTRONICS. F/A'S POWERED DOWN CABIN FOR 15 MIN & SLOWLY BEGAN POWERING THINGS BACK ON. ODOR DISSIPATED & DID NOT RETURN. NOTIFIED DISPATCH ABOUT ODOR & INOPERATIVE RADAR. MID CABIN GALLEY OVEN SDR HALA2011101700463Unknown · unknownETOPS SIGNIFICANT SYS - LINE SERVICE REPORTED NO FUELING ON ACFT. BITE FCMC 1 & 2 TEST OK. NO FAULTS NOTED. REFUEL OK.SDR HALA2011072800338Fms · malfunctionedETOPS SIGNIFICANT SYS - "FMS1/FMS2 SPD TGT DIFF" ON SCRATCH PAD BOTH FMS'S IN WHITE. ACFT WOULD NOT FLY PROGRAMED SPEEDS IN THE BOX ON THE REEF 3 ARRIVAL. PERFORMED TSM 22-83-00. NO FAULTS NOTED. PERFORMED AMM 22-97-00. NO FAULTS NOTED. TEST PASSES.SDR HALA2011070700318Apu · shutdownETOPS SIGNIFICANT SYS - APU AUTO SHUTDOWN AND NO RESTART. BLED APU FUEL LINE. GRD OPS CHECK OK IAW AMM, 28-22-00.SDR HALA2011060800249Light · malfunctionedEXIT LIGHT ABOVE 1L DOOR REMAINS LIT ENTIRE FLIGHT. CREW REPORTS LIGHT EXTINGUISHED AFTER LANDING. PERFORMED CIDS TEST AND NO FAULTS SHOWN. ACFT OK FOR SVC.SDR HALA2011060100248Light · malfunctionedEXIT LIGHT ABOVE 1L DOOR REMAINS ILLUMINATED ENTIRE FLIGHT. CREW REPORTED LIGHT EXTINGUISHED AFTER LANDING. PERFORMED CIDS TEST AND NO FAULTS SHOWN. ACFT OK FOR SVC.
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