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 ASAA2023031242359Floor Panel · delaminatedAFT WET AREA FLOOR PANEL147A5810-28 HAS CORRODED INSERTS. GROUNDED - YES. CLEANED, SANDED AND REMOVED DAMAGE AND DAMAGE INSERTS ON AFT WET AREA FLOOR PANEL 147A5810-28 AND REPAIRED IAW B37-800 SRM 55-00-50-2R.SDR ASAA2023031242323Fmc · faultedAFTER LANDING CAPTAIN ND DISPLAYED VTK FLAG. MCDU MENU PAGE FMC PROMPT BLANKED. THIS SEQUENCE REPEATED ITSELF NUMEROUS TIMES. FLAG WOULD APPEAR, THEN DISAPPEAR. GROUNDED - YES. REMOVED AND REPLACED #1 FMC PER B737-800 AMM 34-61-02. OPS CHECK NORMAL.SDR ASAA2023031242343Unknown · unknownRH PACK LIGHT ILLUMINATES, ON M/C RESET IT EXTINGUISHES. GROUNDED - YES. PERFORMED B737-800 FIM 21-62 TASK 801. PREVIOUS FLY INDICATED R/H RAM AIR ACTUATOR FAULT. RAN VERIFICATION TEST. TEST PASSED RAN PACKS, OPS CHECK GOOD.SDR ASAA2023031242306Light · detachedR-2 DOOR EXIT SIGN FELL OFF. GROUNDED - YES. REPLACED EXIT SIGN AT R-2 DOOR WITH SERVICEABLE UNIT. OK FOR SERVICE.SDR ASAA2023031242297Unknown · unknownLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL AT TOP OF DESCENT. LIGHT DOES AWAY WHEN RESET. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE REF B737-800 FIM 21-62 TASK 801. RAM AIR LIGHT ILLUMINATES UPON BITE TEST AND PREVIOUS LEG ON NO.1 PACK/ZONSDR ASAA2023031142654Skin · dentedRH SIDE UPPER CROWN SKIN HAS A DENT AT APPROXIMATELY STA 440. STREAMER ATTACHED. GROUNDED - YES. EVALUATED DENT - DEPTH OF DENT IS .012, MAX DEPTH OF DENT ALLOWED OVER A STRINGER IS .010, FOUND TO BE OUT OF LIMITSIAW B737-800 SRM 53-00-01-1A-1.ACCOMPLISHED DOUSDR ASAA2023031142626Web · corrodedFORWARD CARGO DOOR CUTOUT THRESHOLD SILL PLATE HAS SURFACE CORROSION AT SEEM AND AROUND FASTENERS HOLES. GROUNDED - YES. REMOVED CORROSION FROM WEB:ORIG MAT.0.056; REMOVED 0.012; RENAUBUBG 0.044 AND FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-30-15REMVOED ANSDR ASAA2023031142625Threshold Web · corrodedAFT CARGO DOOR CUTOUT- THRESHOLD SILL PLATE HAS SURFACE CORROSION LENGTH WISE ALONG SEEM AND FASTENER HOLES/. GROUNDED - YES. REMOVED CORROSION FROM AFT CARGO LOWER SILL WEB,ORIG THICKNESS 0.050;REMOVED 0.006;REMAINING 0.044 AND FOUND TO BE OUT OF LIMITS PER BSDR ASAA2023031142536Intercostal · wornMAIN CABIN AFT WET AREA R/H SIDE AREA, INTERCOSTAL HAS 2 EACH WEAR MARKS AT THE UPPER FLANGE LOWER SURFACE BETWEEN BS 1006 AND BS 1016 APPROX. RBL-17. MARKED GROUNDED - YES. REMOVED DAMAGE, ORIGINAL THICKNESS 0.063. REMOVED 0.008 REMAINING THICKNESS 0.055. FOUSDR ASAA2023031142357Bleed Valve · faultedCLIMB OUT OF 9000' LEFT DUCT PRESSURE WAS 38PSI. RIGHT DUCT 26PSI. FL 360 CRUISE FLT L DUCT 38 RIGHT DUCT 28PSI FL 360 N1 89%. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023031142356Indicator · faultedFUELER REPORTS REFUEL PANEL CENTER TANK QTY INDICATOR NOT TESTING WHEN SELECTED. GROUNDED - YES. REMOVED AND REPLACED CENTER FUEL QUANTITY INDICATOR. PERFORMED GOOD INSTALLATION TEST REF B737-800 AMM 28-41-61/401.SDR ASAA2023031142355Harness · faultedON FIRE TEST # 2 FIRE SWITCH DOES NOT ILLUMINATED AND HAS ASSOCIATED FAULT LIGHT. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 26-10 TASK 801, NO FAULTS FOUND. REMOVED AND INSTALLED NEW #2 ENGINE CORE FIRE DETECTION HARNESS (MW0325), OPS NORMAL. GROUND VERIFICATSDR ASAA2023031042688Skin · corrodedLH WING UPPER SURFACE HAS CORROSION IN SEVERAL SPOTS ALONG THE BLACK PAINTED LINE ACROSS FROM SPOILERS 3,4 AND 5. MARKED IN RED. GROUNDED - YES. REMOVED FASTENERS IN AFFECTED AREA, CORROSION DAMAGE REMOVED BY BLENDING, HFEC INSP WERE PERFORMED WITH NO ADDITIONSDR ASAA2023031042524Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA 986 HAS CORROSION AT RH END AROUND GIRT BAR FITTING NUTPLATE. GROUNDED - YES. PREFORMED SURFACE BLEND AND REMOVED DAMAGE ON FLOOR BEAM 986 RH FASTNER HOLE FOUND TO BE OUT OF LIMITS REPAIRED FLOOR BEAM IAW B737-800 SRM 53-70-51-2R-6WSDR ASAA2023031042452Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA 986 HAS CORROSION AT LH END AROUND GIRTBAR FITTING NUTPLATE. GROUNDED - YES. PREFORMED SURFACE BLEND REMOVED CORROSION ON FLOOR BEM STA 986 LH FASTNER HOLE FOUND TO BE OUT OF LIMITS INSTALLED REPAIR PARTS RESTORED FINISH IAW B737-80SDR ASAA2023031042312Bolt · unknownFO SIDE FLIGHT DECK EMERGENCY ESCAPE WINDOW IS VERY DIFFICULT TO OPEN. GROUNDED - YES. STARTED FO WINDOW ADJUSTMENT PER B737-800 AMM 56-12-11-820-801(12) REPLACED FWD BOTTOM SPECIAL BOLT THREADS RUINED. NEEDS TO BE RETHREADED. REPLACED FWD LOWER ROLLER AND BOLSDR ASAA2023031042308Unknown · unknownTHE "EXIT SALIDA" SIGN OVER THE OVER WING EXIT FELL OFF. GROUNDED - YES. REINSTALLED OVERWING EXIT " EMERG" SIGN " OPS CHECKS OK.SDR ASAA2023031042305Unknown · unknownDOOR L2 EXIT SIGN FELL OFF. GROUNDED - YES. RESECURED EXIT SIGN COVER,OP CK NORMAL,NO DEFECTS NOTED. IAW B737-800 AMM 33-51-01.SDR ASAA2023031042298Unknown · unknownCPDLC LOGGING OFF. GROUNDED - YES. ACCOMPLISHED QRH SATCOM LOCKUP PROCEDURESDR ASAA2023031042289Unknown · unknownAFTER PUSHBACK AND ENGINE START ZONE TEMP CONT CAB ILLUMINATED ON RECALL. PERFORMED QRH PROCEDURE. ZONE TEMP LIGHT DID NOT GO OUT, LIGHT REMAINED AFTER RECALL. GROUNDED - YES. PERFORMED ZONE CONT. BITE CHECKED FAULTS NOTED. FLT DECK TRIM VALVE. RESET ZONE CONTSDR ASAA2023030942525Track · corrodedAFT PIT RH CARGO TRACK IS CORRODED BETWEEN STA 787-807. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED CARGO TRACK FROM STA 887 TO STA 767 IAW B737-800 SRM 53-00-53-2R-3W=1 O=.072 R=.059 L=2 D=.033.SDR ASAA2023030942541Baffle · crackedBAFFLE CLIP STA 500H FWD SIDE AT L/H TRANSITION PANEL CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP STA 500H FWD SIDE AT L/H TRANSITION PANEL IAW B737-900 SRM 51-40-02-0G-0.SDR ASAA2023030942526Support · corrodedR/H TRANSITION PANEL STA 500C TO 500E HAS CORROSION. GROUNDED - YES. CORROSION FOUND TO BE BEYOND LIMITS IAW B737-800 SRM 53-00-53-1A-2 FIG 103 CUTOUT DAMAGED SECTION AND PERFORMED SIDEPLATE REPAIR IAW B737-800 SRM 53-00-53-2R-5W- .4 O- .040 R- 0 L- .5 D- .040SDR ASAA2023030942523Cargo Track · corrodedAFT PIT RH CARGO TRACK IS CORRODED BETWEEN STA 787-807. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED CARGO TRACK FROM STA 887 TO STA 767 IAW B737-800 SRM 53-00-53-2R-3W=1 O=.072 R=.059 L=2 D=.033.SDR ASAA2023030942453Floor Support · corrodedAFT WET AREA FLOOR SUPPORT STA 947 TO 947 LBL 32 IS CORRODED. GROUNDED - YES. PERFORMED SURFACE BLEND REMOVED CORROSION ON FLOOR SUPPORT AT LBL 32 STA 647-967 FOUND TO BE OUT OF LIMITS REPLACED FLOOR SUPPORT IAQW B737-800 SRM 53-70-51-1A-1, SRM 51-40-02-0G-0W=SDR ASAA2023030942291Valve · uncontrollableHISTORY OF R/H PACK TEMP UNCONTROLLABLE. GROUNDED - YES. PERFORMED BITE TEST OF RH PACK TEMP CONTROLLER (M1443) AND TORQUE CHECK OF THE RH PACK ACM REF B737-800 FIM 21-62 TASK 849. BITE TEST RESULTED IN A "THIS PACK -TCV" LIGHT ON BIT AND PREV FLT. DISPLAYED GSDR ASAA2023030842451Web · corrodedAFT CARGO THRESHOLD SILL WEB IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO THRESHOLD SILL WEB IAW B737-800 SRM 51-40-02-0G-0, 51-40-05-0G-0.SDR ASAA2023030842296Modulating Valve · faulted"ZONE TEMP" MASTER CAUTION ON CONT. CAB. RESETS WITH MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED FLIGHT COMPARTMENT ZONE TRIM AIR MODULATING VALVE REF B737-800 AMM 21-61-21OPS CHECK GOOD, BITE CHECK GOOD. NO DEFECTS NOTED.SDR ASAA2023030842264Unknown · unknownR2 DOOR WOULD NOT CLOSE PROPERLY- LARGE GAP. GROUNDED - YES. CYCLED R2 DOOR TO ENSURE PROPER OPERATION. PFMD CABIN PRESS LEAK TEST REF B737-800 AMM 05-51-94. NO LEAKS FND.SDR ASAA2023030842261Unknown · unknownCRZ ALT. HF1 CHANNELIZED. FREQ CHANGE AND CHANNELIZED. HF1 DOES NOT TRANSMIT ON CAPT OR FO SIDE. HF1 RECEIVES 5X5 AND GOOD SELCAL. GROUNDED - YES. PERFORMED GOOD HF #1 BITE PROCEDURE PER B737-800 FIM 23-11 TASK 801. PERFORMED FIM 23-11 TASK 806 AND HF #1 RECEISDR ASAA2023030842252Transmitter · leakingWHILE ACCOMPLISHING LEAK CHECK (REF ASA W/O 1944385 TSR) FOUND #1 ENG FUEL FLOW TRANSMITTER LEAKING AT IDLE. GROUNDED - YES. REPLACED #1 ENG FUEL FLOW TRANSMITTER REF B737-800 AMM 73-31-01.SDR ASAA2023030842247Indicator · faultyWHILE WORKING MEL 28-12B- FOUND #1 REFUEL TANK IND. NOT GOING INTO TESTS MODE. GROUNDED - YES. RMVD AND INSTALLED NEW REFUEL #1 TANK IND. REF 28-21-00-211-801. NO DEFECTS FOUND. ACCOMPLISHED INSTALL TES PER STEP G. REF 28-41-61-400-801. ALL TESTS PASSED.SDR ASAA2023030742449Web · corrodedFWD CARGO THRESHOLD PAN IS CORRODED IN SEVERAL SPOTS. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND THRESHOLD WEB (PANS) OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED WEB IAW B737-800 SRM 51-40-02-06-0W- 1.0 O- .045 R- .039 L-SDR ASAA2023030742336Baffle · crackedFWD PIT FLOOR SUPPORT (BAFFLE) BETWEEN STA 500C-STA 500D RBL24 IS CRACKED. GROUNDED - YES. REMOVED AND INSTALLED NEW BAFFLE (FLOOR SUPPORT) BETWEEN STA 500C-500D IN FWD PIT. IAW B737-800 SRM 51-40-02 AND BAC DWG #143A7505 REV A.SDR ASAA2023030742246Control Panel · faultyALTITUDE SELECTOR ON MCP MISSES THE ALTITUDE SELECTION AND ADDS BACK A FEW HUNDRED FEET OCCASIONALLY. GROUNDED - YES. DUPLICATED PROBLEM, R & RD DFCS MODE CONT PNL PER B737-800 AMM 22-11-34.SDR ASAA2023030742245Unknown · unknownINNER HEADING KNOB LOOSE. GROUNDED - YES. RE-SECURED MODE CONTROL PANEL HEADING KNOB AS REQUIRED IAW B737-800 AMM 22-11-34,SDR ASAA2023030642266Wire · abnormalRIGHT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATES WITH FUEL IN CTR TANK. GROUNDED - YES. R & R BOOST PUMP IAW AMM 28-22-41, OPS CHECK FAILED. CB AT THE P92, D5 POPPED AS SOON AS PUMP IS TURNED ON. FOUND WIRE W1126-3601Y-18 BROKEN AT CONNECTOR D804. WIRESDR ASAA2023030642230Unknown · unknownRIGHT HAND CENTER FUEL PUMP LIGHT ILLUMINATED WITH MORE THAN 2000 LBS FUEL IN CTR TANK. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 28-22 TASK 802, FOUND CENTER RIGHT LOW PRESSURE SWITCH (S155) CONNECTOR LOOSE. SECURED CENTER RIGHT LOW PRESSURE SWITCH (S155) CONSDR ASAA2023030642210Indicator · faultyCENTER FUEL TANK INDICATION DISPLAY IS SHOWING FAIL INTERMITTENTLY ON RE FUEL PANEL. GAUGE IN COCKPIT OPS NORMALLY. GROUNDED - YES. REMOVED AND INSTALLED NEW CENTER TANK REFUEL INDICATOR. PERFORMED WIRING INSPECTION REF B737-800 WDM 28-21-00-211801. NO DEFECTSSDR ASAA2023030642215Packing · leaking#2 ENG AGB DRIVE-PAD LEAKING. GROUNDED - YES. REMOVED AND REPLACED O-RINGS UP UNTIL REF B737-800 AMM 72-63-01-400-801 F00 STEP F (2)(A-E) 1. LEAK CK GOOD.SDR ASAA2023030642212Unknown · unknown#1 ENGINE COWL VALVE FAILED IN CLOSED POSITION. BLUE LIGHT STAYS ON IN ON POSITION OF SWITCH. GROUNDED - YES. FLT CREW REPORTS #1 ENG COWL VALVE STARTED WORKING ON SEVERAL CYCLES OF VALVE, DID NOT FAIL. PERFORMED B737-800 FIM 30-21 TASK 805. OPS CK GOOD.SDR ASAA2023030642205Valve · faultyRIGHT PACK RUNS WITH SWITCH SET TO 'OFF". GROUNDED - YES. REMOVED AND REPLACED THE R/H FLOW CONTROL SHUTOFF VALVE PER B737-800 AMM 21-51-01-000/400-801.SDR ASAA2023030542211Probe · out of limits3 HOURS INTO FLT #2 MAIN FUEL INDICATED 800LBS > THAN #1 MAIN FUEL, ALL PUMPS ON & FUEL X-FEED VALVE WAS CLOSED. AFTER TURNING CTR PUMPS OFF WHEN ALL CTR TANK FUEL INDICATED ZERO, GOT A FUEL IMBALANCE LIGHT WITH 1.1 LB DIFFERENCE 1 HR AFTER ESTABLISHING BALANCSDR ASAA2023030542207Unknown · unknownAUTO PILOT B DISCONNECTS AFTER 4-5 SECONDS. GROUNDED - YES. ACCOMPLISHED FLIGHT FAULT REVIEW. FOUND FAULT IN HISTORY 22-11132, 22-11149. PERFORMED DFCS BITE TEST REF B737-800 FIM 22-11 TASK 801. NO FAULTS FOUND. PERFORMED AUTO PILOT A&B CURRENT STATUS. ALL TESSDR ASAA2023030542214Transceiver · faultyWEATHER RADAR DEPICTED CELLS WHERE THERE WERE NONE AND DEPICTED NOTHING WHEN THERE WERE CELLS. USED IN AUTO AND MANUAL BOTH. AUTO SEEMED MORE INACCURATE. GROUNDED - YES. REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER IAW B737-800 AMM 34-43-41.SDR ASAA2023030442827Valve · out of range75-10591 FAULT CODE FOUND UPON TASK CARD 78273000, TBV POSITION SIGNAL IS OUT OF RANGE, LONG TIME FAULT, ENGINE #1. GROUNDED - YES. REMOVED & INSTALLED LPTACC VALVE #1 ENGINE PER AMM 75-22-04-400-802-F00SDR ASAA2023030442744Start Valve · faulty#1 ENGINE WOULD NOT START. GOOD DUCT PRESSURE AT 38 PSI BUT NO ROTATION WHEN STARTER WAS ENGAGED. GROUNDED - YES. REMOVED AND REPLACED #1 ENG START VALVE REF IAW B737-800 AMM 80-11-03.SDR ASAA2023030442181Unknown · unknownR2 WINDOW OVERHEAT: RAN QRH, LIGHT REMAINS ILLUMINATED. GROUNDED - YES. FOUND C/B OPEN - INSP C/B & PANEL AREA, NO DEFECTS NOTED, RESET SAME. SYS OPS CKS NML REF B737-800 AMM 30-41-00, GND VERIFICATION SUCCESSFUL.SDR ASAA2023030442179Unknown · unknownAFTER START #1 ENGINE ANTI-ICE COWL VALVE LIGHT ILLUMINATED BRIGHT WITH AMBER TAI INDICATION. CYCLED SWITCH AT TAXI POWER 30% N1 AND 50% N1. NO CHANGE. FOLLOWED QRH. GROUNDED - YES. REFERENCE B737-800 WDM 30-21-11, FOUND #1 ENGINE COWL ANTI-ICE VALVE CONNECTORSDR ASAA2023030342641Battery Pack · dischargedEMREGENCY LIGHTS BATTERY PACK FOR EXTERIOR FWD LH OVERWING ESCAPE LIGHT FAILS CAP CHECK. GROUNDED - YES. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805 CH E 33-51-06-960-006 5J6.
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