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 ASAA2023022242609Battery Pack · failedEMERGENCY LIGHT SYSTEM BATTERY PACK FAILED CAPACITY CHECK FOR BATTERIES M1670, M1671, M1672, M1673. GROUNDED - YES. REPLACED BATTERY PACKS M1670, M1671, M1672 AND M1673 IAW ASA B737NG MM 33-51-06-960-805, OP CHECK GOOD ASA B737NG MM 33-51-06-960-805.SDR ASAA2023022242235Battery Pack · failedEMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK GROUNDED - YES. REPLACED FOUR BATTERY PACKS S/N 162201, 202540, 211441, 211447.SDR ASAA2023022242053Power Supply · inoperativeR1 DOOR EMERGENCY LIGHTS BOTH EXTERIOR AND INTERIOR INOP. GROUNDED - YES. REMOVED REPLACED AND OPS CHECKED R1 DOOR EMERGENCY LIGHT POWER SUPPLY S/N 131987 IAW B737-800 AMM 33-51-06-960-806.SDR ASAA2023022242052Sign · detachedFWD GALLEY EXIT SIGN FELL OFF MOUNTING BRACKET. GROUNDED - YES. REMOVED AND REPLACED FWD GALLEY EXIT SIGN EMERGENCY LIGHT SYSTEM OP'S CK IS GOOD.SDR ASAA2023022242049Processing Unit · faultyLEFT FUEL QUANTITY AND TOTAL FUEL QUANTITY INDICATORS CONTINUOUSLY BLANK OUT FOR ABOUT 11 SECONDS THEN REAPPEAR. GROUNDED - YES. 8 FLIGHT LEGS OF FQIS PROCESSOR FAULURE CODE 28-41109. RMVD & RPLCD FUEL QTY PROCESSOR UNIT REF B737-800 AMM 28-41-81. OPS NORMAL PSDR ASAA2023022242041Filter · cloggedAPU OIL FILTER DELTA P INDICATOR EXTENDED. GROUNDED - YES. ACCOMPLISHED B737-800 AMM TASK 49-91-13-600-801. REPLACED OIL FILTER ELEMENT. AND OIL FILTER INDICATOR REF AMM 49-91-13-000-802. LEAK CK GOOD.SDR ASAA2023022242036Bulb · inoperativeEMERGENCY EXIT AREA LT AT ROW 16-17 DEF INOP. GROUNDED - YES. RELAMPED EMERGENCY EXIT AREA LT AT ROW 16-17 DEF, OPS CHECKS OK. REF B737-800 AMM 33-51-03.SDR ASAA2023022242022Inverter · faultyELEC LIGHT FAULTS. GROUNDED - YES. REPLACED STATIC INVERTER PER B737-800 AMM 24-34-21/401. OPS GOOD.SDR ASAA2023022142473Intercostal · crackedAFT CARGO DOOR CUTOUT, LOWER SILL, IBRD EDGE INTERCOSTAL HAS EVIDENCE OF A CRACK AT THE RADUIS, LOCATED ABOVE A VERT STIFENER AT BS 818, RBL20.TIPR833K. GROUNDED - YES. GAINED ACCESS TO REPAIR AREA AFT CARGO DOOR CUTOUT STA 818 RBL20. CUTOUT DAMAGED AREA. PERFSDR ASAA2023022142330Bracket · crackedFWD CARGO FLOOR STRUCTURE @ STA. 500G UNDER R/H TRANSITION PANEL, FWD SIDE OF FRAME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500G .LOCATED AND DRILLED NEW CLIP @ STA 500G IAW B737-800 SRM 51-40-02 AND DWG #1SDR ASAA2023022142339Crease Beam · corrodedWING CENTER SECTION R/H SIDE AT STA. 639 STR.17R HAS CORROSIONON SILL ANGLE. GROUNDED - YES. REMOVED CORROSION ORIG .071, REMAIN .058 LOSS OF .013 WITH CORROSION STILL EVIDENT. FOUND OUT OF LIMITS IAW B737-800 SRM 53-40-13. REMOVED SILL ANGLE IAW B737-800 SRM SDR ASAA2023022142338Track · corrodedFWD CARGO FLOOR STRUCTURE BETWEEN STA.500H AND 500I, APPROX.LBL18 FLOOR PANEL LONGITUDINAL SUPPORT HAS CORROSION ON TOP SURFACE AS MARKED. GROUNDED - YES. REMOVED AND REPLACED PREVIOUSLY REPAIRED FLOOR SUPPORT IAW B737-800 SRM 53-00-53-1A-2, SRM 51-40-02, SRM SDR ASAA2023022142337Transition Panel · corrodedFWD CARGO FLOOR STRUCTURE BETWEEN STA.500A AND 500H, RBL24 TRANSITION PANEL THROUGHOUT HAS CORROSION AROUND NUMEROUS FASTENER HOLES AS MARKED. GROUNDED - YES. EVALUATED NOTED AREA ORG. THICKNESS IS .040" REMOVED .010" REMAINING IS .030" IAW B737-800 AMM 53-00-SDR ASAA2023022142332Unknown · corrodedINTERNAL PASSENGER FLOOR STRUCTURE WET AREA HAS CORROSION BELOW FASTENER HOLE AT FRAME STA 967, RBL 18. GROUNDED - YES. REMOVED CORROSION ORIG .125, REMAIN .098 LOSS OF .027.FOUND OUT OF LIMITS IAW B737-800 SRM 53-70-51 CUTOUT DAMAGE, FABBED REPAIR PARTS, ALODSDR ASAA2023022142331Shear Tie · crackedFWD CARGO FLOOR STRUCTURE @ STA. 500G UNDER R/H TRANSITION PANEL, FWD SIDE OF FRAME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500G .LOCATED AND DRILLED NEW CLIP @ STA 500G IAW B737-800 SRM 51-40-02 AND DWG #1SDR ASAA2023022142329Shear Tie · crackedFWD CARGO DLOOR STRUCTURE @ SAT.500H UNDER R/H TRANSITION PANEL, FWD SIDE OF FRAME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500H LOCATED AND DRILLED NEW CLIP @ STA 500H IAW B737-800 SRM 51-40-02 AND DWG# 143SDR ASAA2023022142328Shear Tie · crackedFWD CARGO DLOOR STRUCTURE @ STA .500H UNDER R/H TRANSITION PANEL, AFT SIDE OF FREME TO INTERCOSTAL ATTACH SHEAR TIE CRACKED AS MARKED. GROUNDED - YES. REMOVED DAMAGED CLIP @ STA 500H,LOCATED AND DRILLED NEW CLIP @ STA 500H IAW B737-800 SRM 51-40-02 AND DWG # 1SDR ASAA2023022142159Transition Panel · corrodedAFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727E+10 - 767 (MARKED). GROUNDED - YES. REMOVED CORROSION ON AFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES FROM STA 727E+10 - 767. ORG MAT .040. MAT REMOVED .016. MAT REMAININGSDR ASAA2023022142158Transition Panel · corrodedAFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727B+10 - 727E+10 (MARKED). GROUNDED - YES. REMOVED CORROSION ON AFT PIT RH TRANSITION PANEL UPPER AND LOWER SURFACES FROM STA 727B+10 - 727E+10. ORG MAT. .040. MAT REMOVED .013. MAT SDR ASAA2023022142156Transition Panel · corrodedAFT PIT LH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727G+10 - 787 (MARKED). GROUNDED - YES. REMOVED CORROSION AT AFT PIT LH TRANSITION PANEL STA 727G+10. ORIGINAL THICKNESS .040". REMOVED .010", REMAINING MATERIAL THICKNESS IS .030". FSDR ASAA2023022142155Transition Panel · corrodedAFT PIT LH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727C+10 - 727G+10 (MARKED). GROUNDED - YES. REMOVED CORROSION AT AFT PIT LH TRANSITION PANEL FROM STA 727C+10 - 727G+10. ORIGINAL THICKNESS .040". REMOVED .013". REMAINING .027". FOUNSDR ASAA2023022142148Transition Panel · corrodedAFT PIT LH TRANSITION PANEL UPPER AND LOWER SURFACES HAVE CORROSION FROM STA 727A+10 - 727C+10 (MARKED). GROUNDED - YES. REMOVED CORROSION AT AFT PIT LH TRANSITION PANEL FROM STA 727A+10 - 727C+10. ORIGINAL THICKNESS .040". REMOVED .006". REMAINING .034". FOUNSDR ASAA2023022142132Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CRACKED AT APPROX STA 780, LBL 22 (MARKED). GROUNDED - YES. EVALUATED DAMAGE AT AFT PIT LH TRANSITION PNL AT STA 780, LBL 22. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. PANEL TO BE REPLACED ON TASK CARD G1774079 OPSDR ASAA2023022142131Shield · corrodedFWD CARGO FLOOR STRUCTURE BETWEEN STA. 500 AND 500A, RBL24 HAS TRANSITION PANEL CORRODED AS MARKED. GROUNDED - YES. EVALUATED SHIELD & FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVENREMOVED OLD SHIELD, LOCATED & DRILLED NEW SHIELD P/N 143A8126-29 PO 1054152.1SDR ASAA2023022142044Starter · inoperativeUNABLE TO START ENG #1, NO N2 ROTATION. GROUNDED - YES. REMOVED AND REPLACED #1 ENG STARTER PER B737-800 AMM 80-11-01. OPS CHECK GOOD. ENG STARTS GOOD WITH N2 ROTATION. NO OTHER DEFECTS NOTED.SDR ASAA2023022142035Panel · faultyAUTO PILOT-A WILL NOT ENGAGE. GROUNDED - YES. C/W DFCS BITE PROCEDURE, B737-800 FIM 22-11 TASK 801, BITE GRP #20 FAULT REVIEW, FOUND LEG 6 HAD MULTIPLE FAULTS FOR BOTH ENGAGE ATTEMPT AND A/P DISC FAULTS. MCP AIL ENG DISAGREE, FC 22-11625, MCP ELV ENG DISAGREE SDR ASAA2023022042129Floorboard · delaminatedFLOOR PANEL #147A5810-28 HAS 1EA INSERT PULLED THROUGH. AREA MARKED. GROUNDED - YES. REPAIRED FLOOR PANEL #147A5810-28 IAW B737-800 SRM 53-00-50-2R-0 AND 53-00-50-2R-1.SDR ASAA2023022042055Pump · faultyON START ENGINE #1 AUTOSHUTDOWN. GROUNDED - YES. REPLACED #1 ENG FUEL PUMP & HMU REF ASA T/C N8473000, N8473001N, N8473002N, AND N8473003 (REF TSR713881).SDR ASAA2023022042034Battery Pack · dischargedEXIT LIGHT INOP GROUNDED - YES. REPLACED BATTERY PACK M1695 S/N 58339 AW B737-800 AMM 33-51-06SDR ASAA2023022042025Unknown · unknownSINGLE FMC MESSAGE AFTER LANDING. GROUNDED - YES. PERFORMED BITE PROCEDURE OF FLIGHT MANAGEMENT COMPUTER SYS PER B737-800 FIM 34-61 TASK 801 FOR BOTH FMC'S. ALL SENSORS READ OK . NO ACTIVE FAULTS CURRENTLY IN SYS.SDR ASAA2023022042024Valve · faulty#2 ENG ANTI-ICE VALVE DISAGREEMENT LIGHT CAME ON DESPITE REPEATED ATTEMPTS AT DIFFERENT POWER SETTINGS. GROUNDED - YES. PERFORMED B737-800 FIM 30-21 TASK 805 FOUND ENG ANTI ICE VALVE TO BE BAD. REMOVED AND REPLACED #2 ENGINE ANTI ICE VALVE REF B737-800 AMM 30-SDR ASAA2023022042020Switch · stickingCAPT AUTO-PILOT DISENGAGE BUTTON STICKS. GROUNDED - YES. REPLACED CAPT'S A/P DISCONNECT SWITCH PER B737-800 AMM 22-11-41, SYS OPS CKS NML PER SAME.SDR ASAA2023022042018Unknown · unknownAFTER ENGINE START, BOTH LEFT & RIGHT PACK LIGHTS ILLUMINATED ON MASTER CAUTION RECALL. PACK LIGHTS EXTINGUISHED ON MASTER RESET. DURING PERFORMANCE OF QRH PROCEDURE, FLIGHT CREW OBSERVED THE FORWARD AND AFT SUPPLY DUCT TEMPERATURES WERE NOT ABLE TO BE LOWEREDSDR ASAA2023022042017Bulb · faultyRIGHT PACK TRIP LIGHT ILLUMINATES ON RECALL. RIGHT PACK TEMP INDICATES 22 DEGREES. LEFT PACK TEMP INDICATES LESS THAN ZERO. GROUNDED - YES. PERFORMED B737-800 FIM 21-53 TASK 821, FOUND R/H PZTC "RAM AIR ACT" FAULTED ON BIT, PASSED ON "PREV FLT" AND "VERIFY". RSDR ASAA2023022042009Bulb · burned outR2 DOOR EXTERNAL EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR EXTERNAL LIGHT LAMP IAW B737-800 AMM 33-51-04 LIGHT TEST GOOD.SDR ASAA2023021942027Igniter · inoperativeENG #1 DID NOT START WITH L IGN. GROUNDED - YES. REMOVED AND REPLACED LH IGNITER PER B737-800 AMM 74-21-02 OPS CHECK OK.SDR ASAA2023021842030Cover · leakingREF ASA T/C 78472000 DURING INSPECTION FOUND #1 ENG S/N 895405 OIL LEAKAGE AND COKE AT OIL SCAVENGE TUBE TO TRF INTERFACE. GROUNDED - YES. REMOVED AND REPLACED TURBINE REAR FRAME (TRF) OIL INLET COVER REF B737-800 AMM 72-56-00.SDR ASAA2023021842023Indicator · inoperativeRIGHT WING #2 TANK INDICATOR ON RE-FUELING PANEL IS NOT FUNCTIONING. GROUNDED - YES. REMOVED AND REPLACED #2 REFUEL QUANTITY INDICATOR. IAW B737-800 AMM 28-41-61. OPS CHECK GOOD.SDR ASAA2023021841988Unknown · unknownRIGHT WING, #2 FUEL TANK RE-FUELING PANEL INDICATOR IS NOT FUNCTIONING. GROUNDED - YES. FOUND RIGHT WING #2 FUEL TANK REFUELING PANEL INDICATOR BLANK NOT DISPLAYING. PERFORMED RESET OF #2 FUEL TANK INDICATION REF B737-800 AMM 28-00-00. OPS CK GOOD.SDR ASAA2023021841987Unknown · unknownPILOT REPORTS #2 ENGINE LOOP "A" INOP. GROUNDED - YES. ACCOMPLISHED ENG FIRE DETECTION CONTROL MODULE BITE PROCEDURE-SHOWED #2 ENG LOOP A RIGHT CORE DETECTOR FAULT REF B737-800 FIM TASK 26-10-00-810-801. CK'D AND FOUND WIRE BROKEN AT LUG ON LOOP A DETECTOR. INSDR ASAA2023021841983Unknown · unknownSPEED TRIM FAIL LIGHT ILLUMINATED ON RECALL. RESETS ON MASTER CAUTION PUSH TO RESET. GROUNDED - YES. CREW REPORTED TEST FLIGHT PROBABLE CAUSE OF SPEED TRIM LIGHT DUE TO MANUAL REVERSION PORTION OF FLIGHT. ACCOMPLISHED B737-800 FIM 22-11 TASK 849. MULTIPLE COLUSDR ASAA2023021841981Relay · faultyWHILE IN CRUISE AT FL340, AUTOPILOT B DISCONNECTED, COMPLIED WITH QRH, WOULD NOT STAY ENGAGED, TRIED AUTOPILOT A AND IT DISCONNECTED AS WELL, AND WOULD NOT STAY ENGAGED. THEN NEITHER AUTO PILOT WOULD ENGAGE AT ALL. NO OTHER ANORMALIES, NO CIRCUIT BREAKERS POPPSDR ASAA2023021742010Unknown · unknownLOWER CARGO FWD A SIDE INOP DETECTOR LOOP. GROUNDED - YES. OPS TEST OF CARGO BAY SMOKE DETECTION OPS CHECKS OK. CLEANED ALL FWD CARGO BAY SMOKE DETECTORS. OPS TEST CARGO BAY SMOKE DETECTION SYSTEM, AGAIN, OPS TEST OK. REF B737-800 AMM 26-16-00 & 26-16-01. ETOPSDR ASAA2023021741989Compensator · faultyAFTER CENTER TANK EMPTY & CENTER FUEL PUMPS OFF APPROX 10 MINS LATER RT TANK FUEL QTY 1060 LB LESS THAN LT. BECAUSE TOTAL FUEL QTY REFLECTED AS PLANNED, FUEL LEAK WAS NOT SUSPECTED & BALANCED FUEL VIA CROSSFEED. RT QTY CONTINUED TO DECREASE 100 LB OVER 25 MINSDR ASAA2023021742005Skin · dentedREF L/P 60246073, DENT LOCATED 9" FWD OF STA 787 & 4" ABOVE STR 22L. GROUNDED - YES. REPAIRED REF REF B737-800 SRM 53-00-01-2R-3 & EA 800-53EA-25281. THIS CAT B REPAIR WAS SUBMITTED TO ENGINEERING FOR TRACKING.SDR ASAA2023021741980Unknown · unknownCONT CAB ZONE TEMP ILLUMINATES ON RECALL & RESETS WITH MC RESET. GROUNDED - YES. ACCOMPLISHED BITE CK ON TEMP CONTROLLERS, FOUND FLT DECK TRIM VALVE FAULT, RESET FAULT. ACCOMPLISHED TEMP CONTROLLER OP CK NO FAULTS NOTED, REF B737-800 AMM 21-61-00-700-506-002 ASDR ASAA2023021741979Valve · inoperativeAT 10,000 FA CALLED TO REPORT EXTREME HEAT. WE COULD NOT CONTROL TEMP IN CABIN. RAN QRH 2.7. TEMP RETURNED TO NORMAL IN CABIN BUT WAS NOT CONTROLLABLE IN FLIGHT DECK. TEMP BECAME VERY COLD. NO COMBINATION OF TRIM AIR OR PACK POSITION ALLOWED US TO CONTROL TEMPSDR ASAA2023021642145Valve · faultyCFM REPORTS #2 ENGINE GRADUAL INCREASE IN DELTA EGT AND DELTA FUEL FLOW AND DECREASE IN DELTA CORE SPEED. GROUNDED - YES. REMOVED AND REPLACED HPTACC ACTUATOR ASSY PER B737-800 AMM 756-25-05.SDR ASAA2023021642003Exciter · faulty#1 ENG HAS NO EGT RISE AFTER START LEVER TO IDLE WITH IGN R. #1 ENG STARTS OK WITH IGN L. GROUNDED - YES. REMOVED AND REPLACED MAIN IGNITER PLUG #1 ENGINE REFB737-800 AMM 74-21-02. OPS CHECK OOD. NO DEFECTS NOTED. REMOVED AND REPLACED #1 ENGINE TOP IGNITION ESDR ASAA2023021641998Engine · damagedWHILE PERFORMING T/C SBCFM 56-7B-72-1074-1 , FOUND STAGE 3 AFT L-HOOK TO BE WORN THROUGH COMPLETELY AT 12 O'CLOCK POSITION ENGINE REMOVED REQUIRED WITH IN 10 CYCLE S/N 896963. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE. TRANSFERRED DEFECT TO SHOP W/O # 194
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