N267JB
Service difficulty reports · 92
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 = 'N267JB' 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 = 'N267JB' 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 YENA201812030818Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO COMPARTMENT, SHEAR CLIP AT FR 72 AND BTW STR 27L-28L. NOTE: NO ALLOWABLE OR DEFINED LIMITS IN THE SRM, THEREFORE THE PART IS TO BE REPLACED; NOTED SHEAR CLIP (P/N: 190-28351-001) REMOVED AND REPLASDR YENA201702170105Plate · lack of lubeR1 DOOR WOULD NOT DISARM. IT WAS FOUND THAT THE R1 DOOR GIRT BAR WAS CATCHING ON AFT GIRT BAR CLEAT SPRING PLATE. LUBRICATED SPRING PLATE WITH DRY RELEASE LUBRICANT. CYCLED, ARMED R1 DOOR 5 CYCLES. OP CHECKED NORMAL PER AMM 52-41-40.SDR YENA201701150031Power Supply · faultyFLT 2224, MCO-DCA, DIVERTED TO IAD. FLIGHT CREW RECEIVED A STEER FAIL MESSAGE ON EICAS. THEY FOLLOWED THE QRH RESET WITH NO POSITIVE RESULTS. CREW ELECTED TO DIVERT INTO IAD, SINCE THERE WAS HIGH FLIGHT VOLUME INTO DCA. AIRCRAFT LANDED WITHOUT INCIDENT. ; PERFSDR YENA20160829762Beam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON L1 DOOR LOWER BEAM UNDER AFT FLOOR FITTING. REPAIRED BEAM IAW ENGINEERING ISSUED EC E16-673-01.SDR YENA20160829761Beam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON R1 DOOR LOWER BEAM 10.75" AFT OF FRAME 16, RBL49. REPAIRED BEAM IAW ENGINEERING ISSUED EC16-660-01.SDR YENA20160829760Beam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON L1 DOOR LOWER BEAM 9.5 " AFT OF FRAME 18, LBL49. REPAIRED BEAM IAW ENGINEERING ISSUED EC E16-658-01 AND ETD 2016-190-072982.SDR YENA20160829759Fitting · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR CLIP AT FRAME 67 BETWEEN STR 27-STR 28. R & R SHEAR CLIP.SDR YENA20160829758Finger Doubler · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DOOR FINGER DOUBLER. R & R FINGER DOUBLER, PN 170-85070-001.SDR YENA20160829757Seal Rest · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FORWARD CARGO DOOR CUTOUT, CENTER SEAL REST. R & R SEAL REST, PN 170-66804-401.SDR YENA20160829756Seal Rest · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AFT CARGO DOOR LOWER CENTER SEAL REST. R & R SEAL REST, PN 170-85251-401.SDR YENA20160829755Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON PANEL SUPPORT SILL AT FRAME 90, LBL43. R & R PANEL SUPPORT, PN 170-86139-005.SDR YENA20160829754Seat Track · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON RT SEAT TRACK FROM FRAME 12-20, RBL12. R & R SEAT TRACK, PN 170-03263-001.SDR YENA20160829753Stringer · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FORWARD CARGO O2 BOX CUTOUT AT FRAME 23+6, STR 20R. R & R REPLACED STRINGER, PN 170-67342-001.SDR YENA20160829752Finger Doubler · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FORWARD CARGO LOWER BEAM AFT FINGER DOUBLER AT FRAME 25, RBL14. R & R FINGER DOUBLER, PN 170-67115-002.SDR YENA20160829751Finger Doubler · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO LOWER BEAM FWD FINGER DOUBLER AT FRAME 24; RBL16. R & R FINGER DOUBLER, PN 170-67115-001.SDR YENA20160829750Beam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO DOOR LOWER CUTOUT BEAM AT FRAME 26+9, RBL 17. R & R BEAM, PN 170-67118-003.SDR YENA20160422351Battery · failedEMERGENCY LIGHTS IN AISLE STAY ON EVEN WITH ACFT POWDERED DOWN AND WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION; FOUND EMERGENCY BATTERY FAULTED LOCATED ABOVE R1 DOOR. R & R IAW AMM 33-50-01.SDR YENA20150221027Circuit Card · failedCREW DECLARED AN EMERGENCY FAILED IN FLIGHT. R & R MAU1 NIC1 CARD IAW AMM 31-41-04. NO FAULTS NOTED.SDR YENA20140908190Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN STRINGER 21L BETWEEN FRAMES 88 - 89. CUTOUT THE STRINGER. PERFORMED HFEC IAW NDT PART 1, 51-00-00-916-803. INSTALLED NEW STRINGER BETWEEN FRAMES 88 - 91. FABRICATED REPAIR PARTS AND INSTALLESDR YENA20140908183Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON STRINGER 21L, FRAME 91. REPAIRED IAW E14-466-01 AND SRM 53-23-03, FIG 25, ITEM 80.SDR YENA20140908181Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT STRINGER 23L BETWEEN FRAMES 76-91. REPAIRED IAW E14-466-01. AND SRM 53-23-03 FIG 25, ITEM 80.SDR YENA20140830171Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED AT FORWARD GALLEY TRACK AT FRAME 16, LBL 11.75". ACCOMPLISH DVI TO ENSURE ALL CORROSION IS REMOVED. FABRICATED REPAIR STRAP, APPLIED A COAT OF INTERFACE SEALANT. TREAT THE REPAIR PARTS WITH A PROTECTIVE FINISDR YENA20140714133Warning Message · illuminatedBLEED 1 FAIL AT FL280. PERFORMED EMERGENCY DESCENT TO 10000 CABIN ALT REACHED 9300. ACFT DIVERTED IAW FIM 36-10-00-810-804-AA, NO CORRELATED OR ACTIVE MESSAGES, INSPECTED BLEED 1 PRESSURE SENSOR TUBE, NO DEFECTS NOTED. R & R NR 1 BLEED PRESSURE SENSOR IAW E1SDR YENA20140331068Wire · misinstalledAIR RETURN AND EMERGENCY EVACUATION DUE TO SMOKE IN COCKPIT AND CABIN. INSPECTION ACCOMPLISHED AND FOUND NR 1 ACM AT FAULT. REMOVED AND REPLACED ACM IAW AMM 21-51-05. ACCOMPLISHED EC E14-150-01. FURTHER INSPECTION FOUND LT PACK CONDENSER INLET TEMP SENSOR ASDR YENA20140302046Acm · failedCREW DECLARED AN EMERGENCY DUE TO SMOKE IN CABIN AND SMOKE STOPPED WHEN "CABIN IFE" WAS TURNED OFF. EXECUTED SMOKE CABIN SMOKE QRH TO IDENTIFY IFE, THEN EXECUTED SMOKE/FUME REMOVAL QRH TO DISIPATE SMOKE. SUSPECT SMOKE WAS FROM IFE BECAUSE IT STOPPED WHEN REMSDR YENA20121222683Acm · failedFLT 1736 SJU-FLL, CREW DECLARED EMERGENCY AND AIRCRAFT RETURN TO SJU DUE TO VISIBLE SMOKE IN COCKPIT AND CABIN DURING CLIMBOUT. SMOKE OF SOURCE COULD NOT BE IDENTIFIED. PERFORMED SMOKE AND ABNORMAL SMELL IN CABIN AND COCKPIT CHECK IAW FIM 21-20-00-810-801A FSDR YENA20121215668Crossbeam · corrodedFLT 6410 JFK-BNA, ON HEAVY MAINTENANCE CHECK FOUND FWD CABIN FR 17 CROSSBEAM CORRODED LBL 9 TO RBL 40. FABRICATED L SHAPED REPAIR ANGLES, BLENDED OUT GOUGE DAMAGE, HFEC INSPECTION PERFORMED AS PER EC E12-758-01.SDR YENA20120609524Controller · failedFLT 245 DFW-BOS, WHILE DESCENDING THROUGH FL 17000 FEET, THE F/O'S WINDSHIELD OUTER LAYER SHATTERED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW E190 AMM 30-42-01. OPS CHECK GOOD.SDR YENA20120609523Controller · failedFLT 254 DFW-BOS, WHILE DESCENDING THROUGH FLT 17000 FEET THE F/O'S WINDSHIELD OUTER LAYER SHATTERED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW E190 AMM 30-42-01. OPS CHECK GOOD.SDR YENA20120608522Windshield · crackedFLT 254 DFW-BOS, WHILE DESCENDING THROUGH FLT 17,000 FEET THE F/O'S WINDSHIELD OUTER LAYER SHATTERED. REMOVED AND REPLACED F/O WINDSHIELD IAW AMM 56-11-00. OPS CHECK NORMAL.SDR YENA20120602513Pressure Switch · failedFLT 1321 BOS-BWI, CREW DECLARED EMERGENCY DUE TO ENGINE 1 FUEL LO PRESSURE. PERFORMED FIM 73-31-00-810-801A. REMOVED AND REPLACED NR 1 ENGINE FUEL PRESSURE SWITCH IAW AMM 73-31-01. OPS AND LEAK CHECK OK.SDR YENA20120411476Amplifier · failedFLT 1731, AIR TURNBACK DUE TO HF TUNING FAILED, UNABLE TO TRANSMIT USING LOW, MED, HIGH TRANSMIT POWER. PERFORMED TROUBLESHOOTING, REMOVED AND REPLACED HF TRANSCEIVER AND HF ANTENNA COUPLER IAW AMM 23-11-03 AND AMM 23-11-01. OPS CHECKED NO HELP. IHF AMPLIFSDR YENA20101230173Rod · brokenFLT 1056 PIT-JFK, ON TAKE OFF NOTICED MODERATE TRIM/ROLL WITH FLAPS EXTENDED. OPPOSITE TRIM REQUIRED WHEN FLAPS RETRACTED. UPON LANDING SIGNIFICANT ROLL/TRIM REQUIRED WHEN FLAPS EXTENDED. REMOVED AND REPLACED NR 1 AND NR 2 LT AND RT MAIN FLAP CARRIAGE LOWERSDR YENA20101214168Floorbeam · corrodedFLT 6403 JFK-BNA, ON SCHEDULE MAINT CHECK FOUND LT FLOORBEAM AT Y=273.0L CORRODED BETWEEN FRAMES 16,17 & 18. REMOVED CORROSION REF SRM 51-12-00. REPAIRED DAMAGE AS PER JETBLUE EA E10-735-01 REVISION 12-9-10 REF EAMS H1908-2605. REPAIR WAS CLASSIFIED AS MAJOSDR YENA20100306028Acm · failedFLT JB1762 SJU-FLL AIR TURN BACK TO SJU, CREW REPORTED AT CLIMBOUT THROUGH 10000 FT SMELL AND VISIBLE INDICATION OF SMOKE IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO SJU AND ACCOMPLISHED EVACUATION L1, L2 R1 AND R2 DOOR SLIDES DEPLOYED. MX PERFORMED AMM FIM 2SDR YENA20091122160Control Lever · faultyFLT 1244 CLT-BOS - DECLARED AN EMERGENCY FOR "FLAP FAIL" EICAS MESSAGE WITH FLAPS ZERO ON LANDING. MX TROUBLESHOT FLAPS PER AMM 27-51-00-810-802-A FOUND FLAP SLAT CONTROL LEVER AT FAULT. REMOVED AND REPLACED SLAT FLAP CONTROL LEVER AND FUNCTIONAL CHECKED OK SDR YENA20091111154Electrical Sys · failedFLT JB624 - HOU-JFK "FLAP FAIL" EICAS MESSAGE ON APPROACH TO JFK FLAPS/SLATS 0 APPROACH. FL4000 AT 210 KTS SELECTED FLAPS 1 AND SLATS EXTENDED BUT FLAPS DID NOT, DID NOT RECEIVE "LO RATE" MESSAGE. CREW DECLARED EMERGENCY AIRCRAFT LANDED SAFELY. MX PERFORMEDSDR YENA2008089Acm · odorPACK 1 INOPERATIVE EICAS DISPLAYED IN FLIGHT. QRH RESET SUCCESSFUL. ON SHORT FINAL NOTICED BURNING ODOR, TURNED OFF PACK 1 AND ODOR WENT AWAY. REMOVED AND REPLACED NR 1 ACM IAW AMM 21-51-00. NO LEAKS NOTED OK TO CONTINUE SERVICE. (K)SDR YENA2008071Power Unit · failedON MX INSP, ROW 11, RT LOWER EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT CENTER EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECK GOOD. (S)SDR YENA2007044Strut · underservicedFLT 5102, AIR TURNBACK DUE LDG VOW SYS FAIL CAS, LANDING GEAR FAILED TO RETRACT. SERVICED NOSE LANDING GEAR SHOCK STRUT IAW AMM 32-21-04. PERFORMED OPS CHECK OF LANDING GEAR RETRACTION SYSTEM IAW 32-33-00-05. OPS TEST GOOD.SDR YENA2007026Acm · seizedFLT 1251, 1029Z, AIR RETURN, SMOKE IN COCKPIT, PACK NR 1 FAIL. PERFORMED TROUBLESHOOTING IAW FIM 21-51-00-810-833A, FOUND PACK NR 1 ACM SEIZED. REMOVED AND REPLACED NR 1 ACM IAW AMM 21-51-05, OPS CK GOOD.SDR YENA2007024Rudder · out of rigAFTER APPLICATION OF 40 PERCENT N1 ON TAKEOFF, AIRCRAFT RESPONDED OPPOSITE TO RUDDER INPUT. PRE-TAKEOFF FLIGHT CONTROL CHECK WAS GOOD. WITH ADDITIONAL INFORMATION FROM EMBRAER ENGINEERING REGARDING RUDT ALIGNMENT MARKINGS (INDEXES) ACCOMPLISHED RIGGING OF CA
Back to N267JB