N277EA
Service difficulty reports · 38
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 = 'N277EA' 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 = 'N277EA' 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 I5EA2023042000004Battery Pack · no testM1675 EMERGENCY BATTERY PACK FAILED CAPACITY FUNCTIONAL CHECK - REMOVED AND REPLACED M1675 STA 322L W/ SERVICEABLE UNIT AND TEST IAW B737-800 AMM 33-51-06, TEST OKSDR I5EA2023042000003Battery Pack · no testM1674 EMERGENCY BATTERY PACK FAILED CAPACITY FUNCTIONAL CHECK - REMOVED AND REPLACED M1674 STA 322R W/ SERVICEABLE UNIT AND TEST IAW B737-800 AMM 33-51-06, TEST OKSDR I5EA2022110300003Transducer · failedANTISKID LIGHT ILLUMINATED IN FLIGHT, EMERGENCY DECLARED INTO KIWA. REMOVED AND REPLACED #4 WHEEL TRANSDUCER AND ANTISKID CONTROL BOX IAW B737 AMM 32-42-11 AND 32-42-21, SYSTEM OPS CHECKS GOODSDR I5EA2021102000004Pump · failedINFLIGHT #2 ENGINE HYD. B SYSTEM LOW PRESSURE LIGHT ILLUMINATED RUN QRH AFTER A PERIOD OF TIME B SYSTEM QUANTITY DROPPED TO 0 RUN QRH. UPON INSPECTION FOUND EDP FAILED, REMOVED AND REPLACED #2 EDP IAW B737-800 AMM 29-11-11. OPS CHECK GOOD, LEAK CHECK GOOD , NSDR I5EA2021080400001Fseu · no testDURING CLIMB AURAL WARNING AND TAKE OFF CONFIGURATION WARNING LIGHTS CAME ON WHEN PASSING FL 310. CHECKLIST PERFORMED AND LIGHTS AND SOUND WENT OFF WHEN PASSING 10,000 FT DURING DESENT. REMOVED AND REPLACED FSEU IAW B737-800,OPS CHECK GOOD. CONFIDENT CHECK FLSDR I5EA2021032500009Pump · inoperative#2 EDP NO PRESSURE AND UPON ON APPROACH B SYSTEM HYDRAULIC QUANTITY LOW. REMOPVED AND REPLACED #2 ENG EDP PER AMM 29-11-11. OPS AND LEAK CHECK ARE GOOD.SDR I5EA201910110905Indicator · splitTRAILING EDGE FLAP INDICATOR SPLIT BETWEEN 0 UNIT RT, 3 UNIT LH DURING THE FLIGHT UNABLE TO OPERATE TRAILING EDGE FLAP FOR LANDING.SDR I5EA201910100904Indicator · splitTRAILING EDGE FLAP INDICATOR SPLIT BETWEEN 0RT AND 3"LH AFTER TAKE OFF. UNABLE TO OPERATED TRAILING EDGE FLAPS HIGH ENERGY CONDITION INSPECTION.SDR I5EA2019072909Pin · recessedDISCREPANCY: EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN THE ARMED POSITION. CORRECTIVE ACTION: TROUBLE SHOT THE EMERGANCY EXIT LIGHT SYSTEM IAW FIM 33-50-00 FOUND A RECESSED PIN ON THE BATTERY PAK ASSY TO THE R/H OVERWING INTERIOR LIGHTS. REPAIRED PER SWPMSDR I5EA20190705Power Supply · inoperativeDISCREPANCY: RT AFT EMERGANCY EXTERNAL LIGHT INOP. CORRECTIVE ACTION: TROUBLE SHOT EMERGANCY LIGHT SYSTEM PER WDM 33-51-14 FOUND THE EXTERNAL EMERGANCY LIGHT POWER SUPPLY ASSY INOP TO AFT EXTERNAL LIGHT. REMOVED AND REPLACED POWER ASSY IAW AMM 35-51-06. OPS TSDR I5EA2019071104Door · out of positionDISCREPANCY: AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT, PILOT RETURNED TO BASE AND CONDUCTED AN OVERWEIGHT LANDING ( LANDING WEIGHT 69.5 VREF 152+5=157). CORRECTIVE ACTION: PERFORMED FAULT ISOLATION OF PRIMARY LANDING GEAR TRANSFER VALVE. FOUND ALT EXSDR I5EA2019052800014Block · damagedDISCREPANCY: COMPLETE EO SWA-190203S, REV: IR, DATED: 02-15-2019. CORRRECTIVE ACTION: ACCOMPLISHED L/H AFT "D" LAVATORY REPAIR COMPOSITE EXTERIOR SURFACE AND FABRICATION ALUMINUME FLOOR FITTING BLOCKS PER EO SWA-190203S, REV: IR, DATED: 02-15-2019.SDR I5EA2019052800015Block · damagedDISCREPANCY: COMPLETE EO SWA-190203S, REV: IR, DATED: 02-15-2019. CORRRECTIVE ACTION: ACCOMPLISHED FWD "A" LAVATORY REPAIR COMPOSITE EXTERIOR SURFACE AND FABRICATION ALUMINUME FLOOR FITTING BLOCKS PER EO SWA-190203S, REV: IR, DATED: 02-15-2019.SDR I5EA2019052800013Block · damagedDISCREPANCY: COMPLETE EO SWA-190203S, REV: IR, DATED: 02-15-2019. CORRRECTIVE ACTION: ACCOMPLISHED RT AFT "E" LAVATORY REPAIR COMPOSITE EXTERIOR SURFACE AND FABRICATION ALUMINUME FLOOR FITTING BLOCKS PER EO SWA-190203S, REV: IR, DATED: 02-15-2019.SDR I5EA2019052800031Skin · crackedDISCREPANCY: FOUND CRACK AT FUSELAGE STA 787 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 787 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA20190530Skin · crackedDISCREPANCY: FOUND CRACK AT RT FUSELAGE STA: 867 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 867 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052800029Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 500A BETWEEN 8L AND 9L. CORRECTIVE ACTIONS: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 500A BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052800028Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 727D BTWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 727D BETWEEN 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052500027Skin · crackedDISCREPANCY: FOUND DAMAGE AT RT FUSELAGE STA 727D BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 727D BETWEEN STRINGERS 8R AND 9R PER AD 2001-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052500026Skin · crackedDISCREPANCY: FOUND CRACK AT RT FUSELAGE STA 460 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 460 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052400025Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 400 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 400 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052400024Skin · damagedDISCEPANCY: FOUND DAMAGE AT LT FUSELAGE STA 440 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIRS AT LT FUSELAGE STA 440 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052300022Skin · crackedCRACK FOUND AT STA 500 RT BETWEEN STRINGER 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 500 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052300020Skin · crackedDISCREPANCY: FOUND CRACK AT FUSELAGE SECTION 47 LOWER PLATING AROUND FUSELAGE STA LT 1016 BETWEEN STRINGERS 20 AND 23L. CORRECTIVE ACTION: ACCOMPLISHED CRACK REPAIR AT FUSELAGE SECTION 47 LOWER PLATING AROUND FUSELAGE STATION LT 1016, BETWEEN STRINGERS 20L ANSDR I5EA2019052100019Link · not reportedINSTALL NEW PIVOT LINK ASSEMBLYS BS 520 TO 540 IAW AD 2015-02-26 (G) 1 AND SB 737-53-12-44 R5 GROUP 4. CORRECTIVE ACTION: ACCOMPLISHED INSTALL NEW PIVOT LINK ASSEMBLYS STA 520 TO 540 PER AD 2015-02-26 (G) (1) AND SB 737-53-1244 R5 GROUP 4 INSTRUCTIONS.SDR I5EA2019052100018Skin · crackedDISCREPANCY: FOUND CRACK AT FUSELAGE STA. 867 RT BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 867 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052100017Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA. 460 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 460 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052100002Doubler · not reportedDISCREPANCY: ACCOMPLISHED DET VISUAL INSPECTION OF REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN LE STA 133.15 CORRECTIVE ACTION: ACCOMPLISHED PERMANENT EXTERNAL REPAIR ON LT HORIZONTAL STABILIZER LOWER SPAR SKIN STA 133.15 IAW SRM 55-10-01.SDR I5EA20190512Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STA. 500F BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA. 500F BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA20190511Skin · crackedDISCREPANCY: FOUND CRACK AT LT FUSELAGE STATION. 360 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STATION. 360 BETWEEN STRINGERS 8L AND 9L PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019052100001Skin · damagedDISCREPANCY: FOUND DAMAGE AT RT FUSELAGE STA. 400 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 400 BETWEEN STRINGERS 8R AND 9R AS PER AD 2009-01-02 AND SB 737-25-1544 INSTRUCTIONS.SDR I5EA2019040901Lamp · burned outROW 12 L/H SIDE EMERGANCY LIGHT INOP. REMOVED LAMP ROW 12 L/H SIDE AEREA LIGHT PER AMM 33-51-03. OPS TEST WAS GOOD.SDR I5EA201804060001Battery Pack · dischargedMID CABIN EMERGENCY LIGHTS M1670 INOP AT STA 727C+13. REMOVED AND REPLACED BATTERY PACK (M1670) AT STA. 727C+13, TEST GOOD IAW AMM 33-51-06.SDR 29EA20160523001Battery Pack · dischargedDURING INSPECTION FOUND THE EMER EXIT LIGHT BATTERY PACK NOT TESTING PROPERLY.SDR 29EA20160403003Light · inoperativeL1 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LAMP IAW THE AMM 33-51-04. OPERATIONS CHECKED NORMAL UNDER NR 500 038 WO SRO1857.SDR 29EA20160403002Light · inoperativeAFT LT WING EMER EXIT LIGHT INOPERATIVE. R & R LAMP IAW THE AMM 33-51-04. OPERATIONS CHECKED NORMAL UNDER NR 500 038 WO SR O1857.SDR 29EA20160403001Power Supply · inoperativeEMERGENCY POWER SUPPLY ON RT ROW 14 INOPERATIVE. R & R POWER SUPPLY IAW THE AMM 33-51-06. OPERATIONS CHECKED NORMAL UNDER NR 500 038 WO SRO1857.SDR 29EA2016F00037Circuit Board · burnedFOUND CIRCUIT BOARD BURNED AND SHORTED, CONNECTOR PLUG ALSO BURNED AND SHORTED.
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