Boeing 737-890
Service difficulty reports · 23,038
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '737890' 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 aircraft_model_key = '737890' 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 ASAA2023050143067Unknown · unknownWHILE PERF ASA TC # 78273000 FOUND #1 ENG MSG # 73-20041 INTERNAL EEC LONG TIME FAULT. GROUNDED - YES. PER B737-800 FIM 73-21 TASK 801 PERFORMED EEC TEST FOR #1 ENG FAULT MSG 73-20041, NO FAULTS FOUND. THIS IS AN INTERMITTENT FAULT.SDR ASAA2023043043274Intercostal · corrodedSIDE WEB AT R2 DOOR FORWARD CORRODED STATION 945. GROUNDED - YES. REMOVED CORROSION FROM INTERCOSTAL WEB. ORIGINAL THICKNESS 0.150, REMAIINING THICKNESS 0.110, REMOVED 0.040. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A. REMOVED DAMAGED INTERCOSTAL IAW B737-800 SDR ASAA2023043043273Floorbeam · corrodedGALLEY MOUNT FITTING @ STATION 947 LEFT SIDE CORRODED. GROUNDED - YES. REMOVED CORROSION ON FLOOR BEAM UNDER GALLEY MOUNT. ORIGINAL THICKNESS 0.180 IAW B737-800 SRM 53-70-51-0I-1. REMAINING THICKNESS 0.100, REMOVED 0.080. OUT OF LIMITS IAW B737-800 SRM 53-70-5SDR ASAA2023043043083Unknown · unknownCON CAB ZONE TEMP LIGHT ON RECALL. GROUNDED - YES. FOUND PZTC #2 FLT DECK TRIM VALVE FAULT. REF B737-800 FIM 21-62 TASK 833 FAULT RESET, VERIFY TEST PASSED. NO RECENT HISTORY.SDR ASAA2023043043068Igniter · damagedNO "LIGHT OFF" #1 ENGINE. GROUNDED - YES. REMOVED AND REPLACED R/H IGNITER PLUG IAW ASA TASK CARD N8474000 AND REMOVED REPLACED L/H IGNITER PLUG DUE R/H CONDITION PERFORMED AUDIBLE IGNITER TEST FOR BOTH IGNITERS TEST OK.SDR ASAA2023043043064Control Unit · faultyRIGHT SIDE WINDOW OVERHEAT, AFTER SWITCH OFF 5 MINUTES AND TURNED BACK ON OVERHEAT LIGHT RETURNED. GROUNDED - YES. REMOVED & REPLACED NEW RIGHT SIDE WHCU & INSTALLATION TEST GOOD B737-800 AMM 30-41-11/401.SDR ASAA2023042943280Angle · corrodedFWD PIT, RH AFT BULKHEAD ANGLE HAS CORROSION ON BOTTOM SIDE. GROUNDED - YES. EVALUATED FWD PIT R/H AFT BULKHEAD ANGLE; MINIMUM THICKNESS: .056, REMOVED: .026, REMAINING .045 & IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-01. REMOVED, LOCATED & DRILLED, SDR ASAA2023042943272Transition Panel · corrodedAFT PIT, LH TRANSITION PANEL IS CORRODED AT STA 727A-727F+14. GROUNDED - YES. REPAIRED THE AFT PIT, L/H TRANSITION PANEL FROM STA 727-727F+14 USING MAT BAC1496-377 PER B737-800 SRM 53-00-53-2R-5. EVALUATED AFT PIT TRANSITION PANEL STA 727A-727F+14. ORIG THICKNSDR ASAA2023042943271Transition Panel · corrodedAFT PIT, LH TRANSITION PANEL IS CORRODED AT STA 758-808. GROUNDED - YES. EVALUATED AFT CARGO L/H TRANSITION PANEL FROM FR STA 758 TO FR STA 808. ORIGINAL MATERIAL THKS .040 PER BAC PROFILE DWG 1496-377 REMOVED .040, REMAINING .000 FOUND TO BE OUT OF LIMITS PERSDR ASAA2023042943270Transition Panel · corrodedAFT PIT, LH TRANSITION PANEL IS CORRODED AT STA 727H+14-757. GROUNDED - YES. EVALUATED AFT CARGO L/H TRANSITION PANEL FROM FR STA 727H +14 TO FR STA 757 ORIGINAL MATERIAL THKS .040 PER BAC PROFILE DWG 1496-377 REMOVED .005 REMAINING .035 FOUND TO BE OUT OF LIMSDR ASAA2023042943269Transition Panel · corrodedAFT PIT, RH TRANSITION PANEL IS CORRODED AT STA 727G-767. GROUNDED - YES. REPAIRED THE AFT PIT R/H TRANSITION PANEL FROM STA 727F+10-767 USING MAT BAC 1496-377 PER B737-800 SRM 53-00-53-2R-5. EVALUATED AFT PIT TRANSITION PANEL STA 727G-767. ORIG THICKNESS .040SDR ASAA2023042943266Transition Panel · corrodedAFT PIT, RH TRANSITION PANEL IS CORRODED AT STA 727A-727C+10. GROUNDED - YES. REPAIRED THE AFT PIT, R/H TRANSITION PANEL FROM STA 727-727D+10 USING MAT BAC 1496-377 PER B737-800 SRM 53-00-53-2R-5.EVALUATED THE CORROSION ON THE R/H TRANSITION PANELSTA 727A-727CSDR ASAA2023042943054Unknown · unknownFMC FAIL ON CAPTAIN AND FO SIDE, VTK FLAG ON CAPTAINS NAV DISPLAY. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 836. RESET AND CLOSED ALL C/B. OPS CHECK GOOD AT THIS TIME.SDR ASAA2023042943051Unknown · unknownEXIT SIGN COVER ABOVE R1 DOOR NOT ATTACHED. GROUNDED - YES. REATTACHED EXIT SIGN AT R1 DOOR PER B737-800 AMM 33-51-01.SDR ASAA2023042943040Modulating Valve · faulty"ZONE TEMP" AMBER ANNUNCIATOR ON OVERHEAD PANEL CONT CAB. EXTINGUISHES ON M.C RESET. GROUNDED - YES. R/R ZONE TRIM AIR MODULATING VALVE (V00143) IAW B737-800 AMM 21-61-21-400-801.SDR ASAA2023042843279Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL AT STA 500E+11-500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+11-500I PER B737-800 SRM 53-00-53-1A-2.2.D. 100% MATERIAL LOSS AND IS FOUND TO BE OUT OF LIMITS PER B737-800 SSDR ASAA2023042843278Transition Panel · corrodedFWD PIT L/H TRANSITION PANEL AT STA 500H-500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500H-500I PER B737-800 SRM 53-00-533-1A-2.2.D. ORIG THICKNESS IS .040" PER B737-800 SRM 53-30-53-0I-2 TABLE 2. REMOVEDSDR ASAA2023042843265Shield · corrodedFWD PIT, AFT SHIELD IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT AFT SHIELD PER B737-800 SRM 53-30-15-1A-1 2.A. 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-30-15-1A-1 REMOVED SHIELD PER B737-800 SRM 51-40-02. RECEIVED NEW SSDR ASAA2023042843063Idg · failedGEN 1 SOURCE OFF LIGHT ILLUMINATED UNABLE TO GET GEN 1 BACK ONLINE. GROUNDED - YES. REMOVED AND REPLACED #1 ENG IDG REF B737-800 AMM 24-11-11.SDR ASAA2023042843042Modulating Valve · faultyCONT CAB TEMP LIGHT. GROUNDED - YES. R&R CONTROL CABIN ZONE TRIM AIR MODULATING VALVE PER B737-800 AMM 21-61-21/401.SDR ASAA2023042743062Modulating Valve · faultedCONT CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL RESETS WITH MASTER CAUTION PRESSED. GROUNDED - YES. REMOVED AND REPLACED THE CONTROL CABIN ZONE TRIM AIR MODULATING VALVE ASSY. OPS AND BITE CK NORMAL, NO LEAKAGE FOUND. REF B737-800 AMM 21-61-21.SDR ASAA2023042743056Panel · delaminatedREF ASA T/C #78472000 #1 ENG. INLET AND FAN BLADES - DETAILED INSPT. FOUND #5 I/B AT 5 O'CLOCK POS. STRUT PANEL HAS 1 EACH FASTENER INSERT DELAMINATED FROM PANEL. (M) ALF AFT UPPER INSERT. GROUNDED - YES. REMOVED AND REPLACED #5 FAN DUCT PANEL REF B737-800 AMMSDR ASAA2023042743050Lens · missingFA REPORTS EXIT LIGHT COVER/LENS MISSING AT 17A. GROUNDED - YES. INSTALLED NEW EMERGENCY EXIT LIGHT LENS LOWER POSITION REF B737-800 AMM 33-51-01.SDR ASAA2023042743048Idg · failedGEN NO.1 CAME OFF LINE DURING DESCENT AND WOULD NOT RECONNECT TO THE BUS. APU WAS STARTED IAW QRH AND WAS CONNECTED TO THE L BUS. GROUNDED - YES. REMOVED AND REPLACED #1 ENG IDG IAW BOEING 737-800 AMM 24-11-11.SDR ASAA2023042643024Modulating Valve · faultyRIGHT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL. LIGHT GOES OUT ON MASTER CAUTION RESET. GROUNDED - YES. MSG ACTIVE ON RECALL, PZTC-2 SHOWS THIS PACK TCV ON CURRENT BIT REF B737-800 FIM 21-62 TASK 831. REMOVED AND REPLACED R/H TEMP CONTROL VALVE REF B737SDR ASAA2023042643007Pump · leaking#2 ENG (EDP) HYD PUMP LEAKING HYDRAULIC AT SUPPLY CASING. GROUNDED - YES. REMOVED AND REPLACED #2 ENG (EDP) HYD PUMP REF B737-800 AMM 29-11-11-400-801-001.SDR ASAA2023042543049Fire Detector · no testFIRE TEST ENG. #1 FAILED. GROUNDED - YES. REMOVED AND REPLACED LEFT CORE DETECTOR M1759 IAW B737-800 AMM 26-11-01. OPS CHECK GOOD.SDR ASAA2023042543028Sensor · faultyPER MAINT CONTROL SCOTT CSS FAIL START ATTEMPT AT FL 410 W/ FAULT LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED BITE CHECK OF APU REF B737-800 AMM 49-61-00 - FOUND STOPS CHECK NORMAL. PER TECH SERVICE REMOVED AND REPLACED INLET TEMP SENSOR REF B737-800 AMM 49-6SDR ASAA2023042543027Sensor · faultyFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL380. SUCCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED AT FL320. GROUNDED - YES. REF B737-800 FIM 49-40 TASK 801, REPLACED APU AIR INLET TEMP SENSOR (AMM 49-61-31)) AND AIR INLET PRESSURE SENSOR (ASDR ASAA2023042543008Unknown · unknownFAULT LIGHT ILLUMINATED DURING START ATTEMPS 1 AND 2, BOTH AT FL370 SUCCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED AT FL300 DURING DESCENT. GROUNDED - YES. FAULT HISTORY COMPLETED AND LAST 3 FAULTS LISTED: 1. MAINT MSG 49-41010 - NO ACCELERATION SHSDR ASAA2023042542998Processing Unit · faulty#1 FLIGHT DECK FUEL QUANTITY INDICATOR INTERMITTENTLY BLANKS AND THEN RETURNS. GROUNDED - YES. PERFORMED FQIS BITE FOUND NO FAULTS DUE TO HISTORY. REPLACED FQPU REF B737-800 AMM 28-41-81/401 ALL REQUIRED TESTS PASSED.SDR ASAA2023042443002Idg · leakingFOUND #1 ENG IDG SPLINE DRAIN LEAKING IN EXCESS OF 7 DROPS PER MINUTE. GROUNDED - YES. REMOVED #1 IDG AND GEAR BOX GARLOCK SEAL B737-800 AMM 24-11-11 AND AMM 72-60-00. INSTALLED NEW GARLOCK SEAL REF AMM 72-60-00 INSTALLED NEW IDG OPS CHECK GOOD REF AMM 24-11-1SDR ASAA2023042442997Motor · faultyDURING CLIMB THROUGH 17000 OBSERVED THE #2 MAIN FUEL TANK FWD LOW PRESSURE LIGHT ILLUMINATED. AT THE TIME THE ENGINES WERE FEEDING FROM CENTER TANK, THE #2 MAIN FUEL TANK WAS FULL AT 8.7. RAN FUEL PUMP LOW PRESSURE QRH. GROUNDED - YES. REMOVED AND REPLACED #2 SDR ASAA2023042442994Battery Pack · dischargedCUSTOMER WALK PER LONNIE- AFT GALLEY AREA EMERGENCY LIGHTS ARE INOP. GROUNDED - YES. REMOVED & REPLACED MIG72, MIG73, BATTERY PACKS, OPS CHECK GOOD REF B737 AMM 33-51-06.SDR ASAA2023042343001Window · faultyL1 WINDOW OVERHEAT ILLUMINATED AFTER ENGINE START/PUSHBACK. GROUNDED - YES. REMOVED AND REPLACED L1 WINDOW IAW B737-800 AMM 56-11-11-401. PERFORMED OPERATIONAL CHECK. CABIN PRESSURE LEAK TEST IAW AMM 05-51-91-790-801. NO LEAK FOUND, CHECK OKAY. WINDOW HEAT SYSSDR ASAA2023042342988Data Unit · faultyDURING APU TROUBLESHOOTING FOUND MESSAGE 49-72103 "DATA MEMORY MODULE CIRCUIT FAILURE". SUSPECT APU WIRING HARNESS. GROUNDED - YES. REF B737-800 FIM 49-70 TASK 806, REMOVED AND REPLACED APU WIRING HARNESS IAW B737-800 AMM 49-011-01. MAINT MSG 49-72103 STILL PRSDR ASAA2023042342986Unknown · unknownAPU FAULT LIGHT. GROUNDED - YES. PERFORMED B737-800 FIM 49-60 TASK 802 FOUND FAULT CODE 49-61116 ECU INTERNAL FAILURE TO BE INTERMITTENT FAULT NO HISTORY.SDR ASAA2023042342984Unknown · unknownL-SIDE WINDOW HEAT "OVERHEAT" LIGHT ILLUMINATED. COMPLIED WITH QRH. LIGHT DID NOT RE-ILLUMINATE. GROUNDED - YES. CHANGED THE WIRES FROM THE PRIMARY SENSOR TO THE SPARE SENSOR REF B737-800 AMM TASK 30-41-00-420-801. WHCU BITE TEST PASSED FOR THE L-SIDE WINDOW RSDR ASAA2023042342958Actuator · faultyDURING REPLACEMENT OF RIGHT PACK RAM AIR ACTUATOR ON DEFECT 60478284, FOUND RAM AIR ACTUATOR FAULT ON LEFT PACK/ZONE TEMPERATURE CONTROLLER. VERIFY TEST CONFIRMED LEFT PACK RAM AIR ACTUATOR FAULT. GROUNDED - YES. REMOVED AND REPLACED LH RAM AIR INLET ACTUATOR SDR ASAA2023042243004Unknown · unknownWHILE PERFORMING T/C 78273000 FOUND LONG TIME FAULT 73-20042 ON #2 ENGINE INTERNAL EEC FAULT. GROUNDED - YES. ACCOMPLISHED TASK CARD #7827300 NO CURRENT AND FAULT HISTORY FOR ENG #2. PER B737-800 FIM 73-21 TASK 801 THE FAULT WAS INTERMITENT FAULT. PERFORMED GOSDR ASAA2023042243003Unknown · unknownWHILE PERFORMING TASK CARD 78273000 FOUND SHORT TIME FAULT 73-20012 ON #2 ENGINE ENGINE INTERNAL EEC FAULT. GROUNDED - YES. ACCOMPLISHED TASK CARD #7827300 NO CURRENT AND FAULT HISTORY FOR ENG #2. PER B737-800 FIM 73-21 TASK 801 THE FAULT WAS INTERMITTENT FAULSDR ASAA2023042242967Unknown · unknownL2 WINDOW OVERHEAT LIGHT ILLUMINATED. CYCLED POWER TO L2 IAW QRH P36. OVERHEAT LIGHT REMAINED ON. GROUNDED - YES. FOUND PIN 3 PUSHED IN AT D10572 AND TOUCHING GROUND. RE-SEATED AND VERIFIED LOCKING. RESET C/B. L2 WINDOW HEAT OPS NORMAL. REF B737-800 AMM 30-41-SDR ASAA2023042242969Unknown · unknownCPDLC ALTERS ARE ABNORMAL. WHEN RECEIVING A MESSAGE FROM ATC INFLIGHT WE ONLY RECEIVE A SCRATCH PAD MESSAGE AND FMC P/RST LIGHT ON THE FORWARD PANEL. THERE IS NO AURAL HIGH/LOW ALTER TONE NOR IS. ATC DISPLAYED ON THE ENGINE DISPLAY. PRIOR TO DEPARTURE THE DCL SDR ASAA2023042242966Unknown · unknownENG #2 ANTI-ICE VALVE LIGHT (BLUE) ON W/ ANTI ICE SWITCH OFF. AMBER TAI LIGHT ON. RAN QRH. PULLED THRUST LEVER BACK < 80% N2, LIGHTS WENT OUT. GROUNDED - YES. PERFORMED B737-800 FIM 30-21 TASK 804. FOUND TO BE INTERMITTENT FAULT. TESTED OK.SDR ASAA2023042142987Fuel Control · faultyFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL 360 SUCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED. GROUNDED - YES. DURING APU BITE TEST FOUND MAINT MSG 49-31016 OVERTEMPERATURE SHUTDOWN IN FAULT HISTORY. NO FAULTS IN CURRENT STATUS. CONTINUESDR ASAA2023042043118Skin · crackedSUBTASK 839-004 ONE CRACK INDICATION FOUND APPROX 1/8"L. LOCATION IS ON THE 92.70 STAB STA AND 101.90 OFF THE 101.90 FASTENER SIDE, FWD OF PREVIOUS REPAIR. GROUNDED - YES. REPAIRED R/H LOWER HORIZONTAL SKIN WITH 2024-T3 IAW B737-800 SRM 55-10-01-2R-11THIS IS ASDR ASAA2023042042971Unknown · unknownL1 DOOR WOULD NOT CLOSE. GROUNDED - YES. ADJUSTED GUIDE ARM REF B737-800 AMM 52-11-21 OP CHECK GOOD.SDR ASAA2023042042963Processing Unit · faultyOGG TO SJC DURING CRUISE WITH CENTER TANK FUEL LEFT MAIN TANK DROPPED TO ABOUT 400LBS THAN THE RIGHT TANK FUEL FLOW WAS SLIGHTLY HIGHER ON THE # 1 ENGINE VS THE # 2 ENGINE. GROUNDED - YES. FQIS BITE PASSES BUT SYSTEM HAS HISTORY AND FAULT HISTORY SHOWS PROCESSSDR ASAA2023042042962Pressure Switch · intermittentRT INBOARD FUEL PUMP FORWARD LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY. GROUNDED - YES. VERIFIED RT FORWARD PUMP IS RUNNING WITH LOW PRESSURE LT OUT. DUE TO HISTORY REMOVED AND REPLACED TANK 2 FWD PRESSURE SWITCH REF B737-800 AMM 28-42-11. OPS CHECK GOOD.SDR ASAA2023042042961Harness · faultyNUMBER ONE ENGINE FIRE DETECT LIGHT INOP. GROUNDED - YES. PERFORMED B737-800 FIM 26-10 TASK 805 TO RESISTANCE CHK AT F(5) OUT OF LIMITS, M1759 B/2 TO DJ2601-1 = 13.4 OHM; DJ2601-2 13.2 OHM. REPLACED MW0326 WIRE HARNESS REF B737-800 AMM 26-11-02. OPS CHECKS GOO
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