N600BP
Service difficulty reports · 126
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 = 'N600BP' 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 = 'N600BP' 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 HNAA2021050300164Tat Probe · malfunctionedIN CRUISE TAT 2 INOPERATIVE IN EICAS. NO NOTED INDICATION ISSUES. R & R TAT 2 SENSOR IAW AMM 34 15 03. OPS CHECKED GOOD. R & R RELAY K0494 PER AMM 20 13 02. OPS CHECK GOOD. OK FOR SERVICESDR HNAA2020090900254Wheel · failedABNORMAL NOISE AND ODOR FROM NOSE WHEEL AREA DURING TAKEOFF ROLL. MAINTENANCE R& R LT AND RT NOSE WHEEL ASSY, I/A/W 32-49-05. OK FOR SERVICE, PCS.SDR HNAA2020080300241Duct · blownON TAKE OFF 2 LOUD POPS WERE HEARD IN CABIN BETWEEN RIGHT E-EXIT AND AFT BULKHEAD, FOLLOWED BY A BLEED 1 LEAK ON EICAS. AT 10,000 FT CABIN WAS LOSING PRESSURIZATION. MAINTENANCE: UPON INSPECTION OF PACK 2 DUCTS, FOUND BLOWN OFF LINE. REPLACED RUBBER SEAL AND CSDR HNAA2020022600079Trim System · inoperativePITCH TRIM MAIN INOP. BACK-UP OPS NORMAL.....FIX: TRANSCRIBED TO WORK PACKAGE SEQ 1 DATED 22FEB20. R&RD HSA(HORIZ STAB ACTUATOR) IAW AMM 27-40-02. PERFORMED HSA ADJ/TEST IAW 27-40-02-700-801-A. OKAY FOR SERVICE.SDR HNAA2020021700066Trim System · malfunctionedPDIS 600 27-41 2110041 15FEB20 PHL CLOSE
PITCH TRIM MAIN INOP ON EICAS DURING CLIMB WITH AUTO
PILOT ENGAGED
FACT 15FEB20 14:27 PHL
RESET PITCH TRIM 1/ PITCH TRIM 2 CB PER FIM 27-43-00-810-801-A BLOCK 1. PERFORMED HORIZONSDR HNAA2020011700019Pump · leakingHYD SYS 1 FLUID LOSS IN FLIGHT....FIX:FOUND #1ENG DRIVEN HYD PUMP LEAKING OUT DRAIN TUBE. R&RD #1ENG DRIVEN HYD PUMP IAW 29-10-03-000-801-A AND 29-10-03-400-801A,OPS CHECK LEAK CHECK GOOD.OK FOR SERVICESDR HNAA2018081300190Display · malfunctionedFIRST OFFICER`S ALTITUDE INDICATOR ON THE PFD SHOWED A RED X AND SPEED BUGS ON SPEED TAPE. DISAPPEARED AT VR SELECTED ADC 1 ON THE FIRST OFFICER`S REV PNL, ALL INDICATIONS NORMAL. R & R THE PFD 2 IAW AMM 34-22-01. OPS CHECKED GOOD. PERFORMED ADC SELF TEST SDR HNAA2018072000161Window · openCAPT DV WINDOW OPENED IN FLIGHT SHORTLY AFTER TAKEOFF. WINDOW WOULD NOT REMAIN CLOSED WITHOUT ASSISTANCE. INSPECTED CAPTAINS STORM WINDOW TRACK AND SEALS. NO DEFECTS NOTED. PERFORMED OPS CHECK IAW AMM TASK 56-11-00-700-801-A. OPS CHECK GOOD REQUIRES EVAL FLIGHSDR HNAA2018052500113Unknown · odorACRID SMOKE ODOR IN THE FLIGHT DECK AND FORWARD CABIN. NO VISUAL SIGNS OF SMOKE. VISUALLY INSPECTED AVIONICS NOSE BAY AND AROUND WINDSHIELDS, FOUND NO EVIDENCE OF BURNING. DURING GROUND RUN FOR RADAR, NO EVIDENCE OF SMOKE. OK FOR SERVICE.SDR HNAA2018041100080Unknown · odorPASSENGER REPORTED POSSIBLE ELECTRICAL ODOR IN CABIN. MX UNABLE TO DUPLICATE DISCREPANCY. NO ELECTRICAL ODOR PRESENT IN ACFT AT THIS TIME. NO OBVIOUS DEFECTS NOTED, OK FOR SERVICE.SDR HNAA2017101600350Engine · fireGROUND CREW REPORTED A NR 1 ENGINE FIRE AT EXHAUST NOZZLE DURING TAXI. CREW REPORTED THE ENGINE WAS JUST PREVIOUSLY SHUTDOWN AND NO ABNORMAL INDICATIONS OR MESSAGE VIEWED. INSPECTED FOR FIRE EVIDENCE AND DAMAGE. NONE FOUND. GROUND RAN THE ENGINE. SHUTDOSDR HNAA2017100200343Unknown · unknownAT 100 KNOTS DURING TAKE OFF, AIRCRAFT ABRUPTLY YAWED TO THE LEFT. COMPLIED WITH GVI ON NLG AND MLG. NO DEFECTS FOUND. ALL TIRE PRESSURES WERE GOOD. OK FOR SERVICE.SDR HNAA2017090700301Light · inoperativeEMERGENCY LIGHT AT ROW 17 INOPERATIVE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-50-08-000/400-802-A, OPS CHECKED GOOD.SDR HNAA2017082100279Engine · fireGATE AGENT NOTICED FLAMES AND SMOKE EMINATING FROM THE NR 1 ENGINE WHILE ENGINE WAS SHUTDOWN. INSPECTED AND NO DAMAGE NOTED. GVI ENGINE INLET AND EXIT AND NACELLE AREA. NO DAMAGE NOTED IAW MM 05-50-00. OK FOR SERVICE.SDR HNAA2016120900381Warning System · false activationHS VLV CAUTION ILLUMINATED AFTER ENGINE START. GROUND RAN BOTH ENGINE. PERFORMED 1 AND 2 ENGINE HSV FUNCTION TEST IN ACCORDANCE WITH MM 36-11-02. OPS CHECKED GOOD. OK FOR SERVICE.SDR HNAA2016121200387Valve · failedAFTER ENGINE START, HS VALVE 1 FAILED. R & R THE NR 1 HSV AND PRESSURE SWITCH IAW AMM 36-11-02. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR HNAA2016112100354Warning Light · false activationDURING TAKEOFF, EICAS CAUTION MESSAGE HS VALVE ILLUMINATED, NR 1 ENGINE N2 WAS ABOVE 80%. MESSAGE EXTINGUISHED AFTER REJECTED TAKEOFF AND THRUST LEVERS AT IDLE. GROUND RAN AIRCRAFT. PERFORMED HIGH STAGE VALVE FUNCTION TEST IAW MM 36-11-02-700-801-A/500. OPSDR HNAA2016101400318Warning Light · false activationDURING ICE PROTECTION TEST IN FLIGHT, STAB ANTI-ICE FAILED APPEARS ON EICAS. TROUBLESHOT IAW FIM 30-12-00-810-805-A. PERFORMED OPS CHECKED ON ANTI-ICE SYSTEM IAW MM 30-00-00 OPS CHECKED GOOD. FOUND TO BE TRANSITORY CONDITION.SDR SIMA20160725005Valve · corrodedTOILET WASTE VALVE SUPPORT BUCKET IS CORRODED. REMOVED AND REPLACED TOILET WASTE VALVE SUPPORT BUCKET IAW SRM 51-40-02SDR SIMA20160720006Wire · brokenNR 1 EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.SDR SIMA20160720004Floor Support · crackedLEFT OMEGA BEAM IS CRACKED AT NUTPLATE HOLE ABOVE FRAME 69. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2199SDR SIMA20160720007Wire · brokenLEFT NR 1 EMERGENCY LIGHT CONNECTION BROKEN. REPAIRED THE WIRE IAW SWPM 20-50-00SDR SIMA20160720005Skin · damagedRUDDER LOWER RT SIDE TRAILING EDGE SKIN HAS A BLEND-OUT AREA. ACCOMPLISHED PERMANENT REPAIR OF THE RUDDER IAW ERS-EM-55MR-441SDR SIMA20160712002Frame · corrodedFRAME 65 IS CORRODED BELOW CARGO DOOR GUIDE PLATE. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.SDR SIMA20160417002Inverter · inoperativeTHREE AFT EMER FLOOR LIGHT STRIPS INOPERATIVE. R & R NR 6 EMER LIGHT DC & AC INVERTER. OPERATIONS CHECKED GOOD FOR ALL EMER FLOOR LIGHT STRIPS IAW AMM 33-50-11.SDR SIMA20160414005Light · inoperativeEMERGENCY FLOOR PROXIMITY LIGHT STRIP, FOURTH FROM FRONT INOPERATIVE. DEFERRED IAW MEL 33-30. R & R EMER FLOOR PROXIMITY LIGHT STRIP, 4TH FROM FRONT IAW AMM 33-50-12. OPERATIONS CHECKED GOOD. MEL ITEM RESTORED.SDR SIMA20160401003Transducer · failedABORTED TAKEOFF AT 80KTS. BRAKE DEGRADED MSG & AT THE SAME TIME ACFT SWERVED TO THE LEFT. R & R NR 4 WHEEL SPEED TRANSDUCER IAW AMM 32-41-03. PERFORMED FUNCTIONAL CHECK OF THE MAIN BRAKE SYS IAW AMM TASK 32-41-00-700-801. CHECK IS GOOD.SDR SIMA20160215002Door · lack of lubeFLIGHT ATTENDANTS REPORTS THE MAIN CABIN DOOR NOT OPEN OR CLOSE EASILY. CLEANED & LUBRICATED MAIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20160120007Structure · crackedCRACK AT RIVET BELOW ACCESS PANEL 113AZ. MARKED WITH MX INFO TAG. PERFORMED PERMANENT REPAIR TO CRACK AT RIVET BELOW ACCESS PANEL 114AZ IAW ERS-EM-53MR-1880.SDR SIMA20160120006Structure · crackedCRACK AT RIVET BELOW ACCESS PANEL 114AZ. MARKED WITH MX INFO TAG. PERFORMED PERMANENT REPAIR TO CRACK AT RIVET BELOW ACCESS PANEL 114AZ IAW ERS-EM-53MR-1880.SDR SIMA20160120005Uplock · failedUNUSUAL THUMPING NOISE COMING FROM UNDERNEATH COCKPIT AREA. HAPPENED ON TWO SEPARATE TIMES WITH VIBRATION FELT BY BOTH PILOTS. REMOVED AND REPLACED NLG UPLOCK BOX IAW AMM 32-33-07. REMOVED AND REPLACED HARNESS TO NLG UPLOCK BOX FOR INTERNAL SHORT IAW SWPM 2SDR SIMA20160107002Inverter · inoperativeFOUND FLOOR STRIPS NR 2 AT NR 3 NOT WORKING. R & R NR 3 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.SDR SIMA20151225003Regulator Valve · failedANTI-ICE FAIL FOLLOWED BY ANTI-ICE COND. ANTI-ICE INOPERATIVE, BUT ALL VLVS INDICATED OPEN. MSG CLEARED & SYS WORKED MANUALLY WITHOUT FURTHER ISSUES. TRANSFERRED TO NRWC 600-ORD-02595, REF NRWC 600-ORD-02595. R & R RT PRESS REGULATOR VLV IAW AMM 21-31-05. SDR SIMA20151103002Unknown · odorSTRONG ELEC BURNING ODOR THROUGHOUT ACFT, WHILE TAXING UP TO GATE. PERFORMED GVI OF ALL AVIONICS COMPARTMENTS, GVI OF MAIN CABIN AREA, GVI OF MAIN CABIN LIGHTS, GVI OF GALLEY AREA, GVI OF COCKPIT AREA & OPERATED BOTH PACKS IAW AMM 21-51-00. RAN ENG AT IDLE WSDR SIMA20151001002Flashlight · inoperativeCAPTAINS FLASH LIGHT QUIT WORKING. R & R CAPTAINS FLASH LIGHT ASSEMBLY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.SDR SIMA20150915001Light · inoperativeRIGHT FWD OVERWING EMER LIGHT INOPERATIVE. R & R RT FWD OVERWING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.SDR SIMA20150822001Radio Altimeter · failedON CLIMB OUT RA SHOWED 25 FT GREEN WITH MIN BOX SHOWING & GND INDICATION UNDER ALTITUDE. NUMEROUS AURAL WARNINGS & MASTER CAUTIONS INCLUDING BANK ANGLE, PULL UP, LG, SINK RATE GND PROX, HOWEVER NO MSG ON EICAS. TRANSFERRED TO NRWC 600-DFW-02420. REFERENCE NSDR SIMA20150819004Light · inoperativeRIGHT FWD EMER WING LIGHT INOPERATIVE. R & R FWD WING EMER LIGHT IAW AMM 33-50-07.SDR SIMA20150330002Mechanism · lack of lubeMAIN CABIN DOOR EXCEPTIONALLY DIFFICULT TO OPEN & CLOSE. LUBRICATED ACTUATING & LOCKING MECHANISM ON MAIN CABIN DOOR IAW AMM 52-18-00. OPENING & CLOSING GOOD IAW AMM 52-18-00-820-801A.SDR SIMA20150319004Door · scratchedPASSENGER DOOR SCRATCHED & GOUGED ON LOWER TE. TRANSFERRED TO AML PAGE 3740390 ITEM 1. SATISFACTORILY ACCOMPLISHED ERS-EM-52MR-308.SDR SIMA20141221003Engine · power lossNUMBER 2 ENG UNABLE TO PRODUCE COMMANDED THRUST IN DETENT DURING CRUISE & NR 2 N1 ABOUT 1% BELOW COMMANDED THRUST. NR 2 ITT WAS ON BORDER OF AMBER A FEW TIMES. NR 2 ITT 50 + WARMER COMPARED TO NR 1 ENG ITT. NR 2 N2 APPROX 4% HIGHER THAN NR 1. RETURNED & AFSDR SIMA20141117004Light · inoperativeSERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD. CHARGER ASSEMBLY BATTERY PN BA5-0933-901 SN C01608.SDR SIMA20141013002Rib · chafedLEFT WING AILERON PCA HYDRAULIC LINES CHAFING INTERNAL RIBS OF WING. COMPLIED WITH REPAIR OF LT WING RIB 21 IAW ERS-EM-57MR-260.SDR SIMA20141009002Rib · gougedLEFT WING RIB 21 GOUGED. COMPLIED WITH LT WING RIB 21 REPAIR IAW ERS-EM-57MR-260.SDR SIMA20141008012Rib · crackedRIGHT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IS CRACKED LOWER OTBD CORNER. R & R RT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IAW SRM 51-40-02.SDR SIMA20141008010Gusset · crackedGALLEY FLOOR GUSSET HAS A CRACK AT FRAME 18. INSTALLED NEW GALLEY FLOOR GUSSET IAW SRM 51-40-02.SDR SIMA20141005008Support Bracket · crackedFOUND SUPPORT BRACKET FOR THE BLEED AIR DUCT, JUST AFT OF APU CHECK VLV IN THE AFT AVIONICS TO BE CRACKED. R & R RT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IAW SRM 51-40-02.SDR SIMA20141001008Support · crackedLEFT OVERWING PANEL SUPPORT FLANGE IS CRACKED AT FRAME 48. REPAIRED LT OVERWING PANEL SUPPORT FLANGE AT FRAME 48 IAW SRM 53-23-12.SDR SIMA20141001007Bracket · crackedRIGHT OVERWING PANEL SUPPORT FLANGE HAS A CRACKED BRACKET AT FRAME 48. R & R RT OVERWING SUPPORT FLANGE BRACKET IAW SRM CH 51-40-02.SDR SIMA20141001006Support Angle · crackedSUPPORT ANGLE CRACKED, AFT OF THE RT MLG WELL FOR THE AFT BELLY FAIRING. R & R BRACKET IAW SRM CH 51-40-02.
Back to N600BP