Boeing 737-800
Service difficulty reports · 843
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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 = '737800' 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 = '737800' 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 ASMF201602005Shutoff Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED A LOW PRESS IN BOTH PNEUMATIC VENTS. PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE LT ENG PRSOV. THE LT ENG PRSOV WAS REPLACED IAW AMM 36-11-04, TESTED CORRECT.SDR ASMF201602004Gasket · damagedDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE LT SURGE TANK ACCESS PANEL. DETECTED A FUEL LEAK IN THE LT SURGE TANK ACCESS PANEL GASKET, SO THE LT SURGE TANK ACCESS DOOR GASKET WAS REPLACED IAW AMM 28-11-11, TESTED CORRECT.SDR Z6WR20151216009Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 8 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLSDR Z6WR20151216008Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 9 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLSDR Z6WR20151216007Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALS 9 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBLSDR Z6WR20151216006Panel · burnedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALS 11 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT -174 BONDED PANEL ASSEMBSDR 29EA2016F00037Circuit Board · burnedFOUND CIRCUIT BOARD BURNED AND SHORTED, CONNECTOR PLUG ALSO BURNED AND SHORTED.SDR 29EA2016F00036Megaphone · inoperativeFORWARD MEGAPHONE INOPERATIVE.SDR ASMF201601002Fuel Heater · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE LT ENG. PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER & HPTCC VLV LEAKING, SO THE LT FUEL SERVO HEATER & HPTCC VLV WERE REPLACED IAW AMM 73-11-07 & AMM 75-21-01, TESTED CORRECT.SDR ASMF201511011Transmitter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG OIL FILTER BY PASS LIGHT TURNED ON. PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. PERFORMED FIM 79-05 TASK 817 PROCEDURE, DETECTING THE SCAVENGE OIL FILTER SDR ASMF201510032Tube · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE RT WING INNER. PERFORMED REVISION DETECTING HYD LEAK IN THE PRESS TUBE OF THE SPOILER ACTUATOR NR 9 IAW AMM 29-10-00, SO THE PRESS TUBE WAS REPLACED IAW AMM 20-10-51-401, TESTED CORRECT.SDR ASMF201510029Warning System · false activationAIRCRAFT REJECTED TAKEOFF AT 30 KNOTS TO THE AFT SERVICE DOOR LIGHT TURNED ON. PERFORMED THE QRH 1.15 PROCEDURE, NO CONFIRMING THE FAILURE & INITIATING AGAIN SEQUENCE OF TAKEOFF. AS PRECAUTIONARY ACTION, PERFORMED AFT SERVICE DOOR CHECK IAW AMM 52-13-00, TESSDR ASMF201510018Sensor · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE PSEU LIGHT TURNED ON. PERFORMED BITE TO PSEU IAW FIM 32-61 TASK 804 PROCEDURE, SHOWING FAILURE CODES 32-61103, D10982 PIN 9, 2 & MSG NOSE LKD & S0846 FAIL SAFE, SO THE WIRING WAS VERIFIED IAW WDM 32-64-1SDR Z6WR20150828005Panel · burnedRECEIVED POST AIRWORTHINESS DIRECTIVE 2012-05-02 SERVICE BULLETIN 737-78-1079, REVISION 3 THRUST REVERSER PN 315A2295-699 78-31-40, FIGURE 1, ITEM 3G. UPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-165 BONDEDSDR ASMF201510011Skin · dentedDURING TRANSIT CHECK, IT WAS DETECTED A DENT IN FWD CARGO COMPARTMENT DOOR SKIN AT STATION 470.5 OF 1.373” LENGTH, 1.25” WIDE, 0.064” DEPTH. EVALUATED THE DAMAGE & FOUND IT OUT OF LIMITS IAW SRM 53-30-01. THE NON-ROUTINE CARD NR A0230328 WAS ISSUED TO REPAIRSDR Z6WR20150828004Panel · burnedRECEIVED POST AIRWORTHINESS DIRECTIVE 2012-05-02 SERVICE BULLETIN 737-78-1079, REVISION 3 THRUST REVERSER PN 315A2295-700 78-31-40 FIGURE 1 ITEM 7E. UPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-165 BONDED PSDR Z6WR20150828003Panel · burnedRECEIVED POST AIRWORTHINESS DIRECTIVE 2012-05-02 SERVICE BULLETIN 737-78-1079 REVISION 3 THRUST REVERSER PN 315A2295-702 78-31-40 FIGURE 1 ITEM 17F. UPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-165 BONDED PSDR ASMF201510010Starter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO THE LT ENG NOT STARTED. PERFORMED THE LT ENG START IAW MM 74-00-00 & ENG LEAKING INSPECTION IAW MM 73-21-00, DETECTING THE STARTER DAMAGED. THE STARTER WAS REPLACED IAW AMM 80-11-01, TESTED CORRECT.SDR ASMF201510009Sensor · failedDURING APPROACH, FLAPS DID NOT EXTEND. ACFT WAS SENT TO THE HANGAR & MX PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, SHOWING FAILURE CODE 27-53252 FLAP 3 SKEW, SO THE SENSOR T527 OF FLAP 3 WAS REPLACED IAW FIM 27-59 TASK 803 PROCEDURE, TESTED CORRSDR ASMF201510008Fan · lack of lubeDURING CLIMB, THE RT ENG VIBRATION REACHED 2.5 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. A BORESCOPE INSPECTION TO LPT STAGES 1 - 3 IAW AMM 72-00-00, NO DAMAGES WERE FOUND. LSDR CA150811002Duct · cracked(CAN) FLIGHT CREW REPORTED WING BODY OVERHEAT INDICATION LT AND RT CAME ON. LT WING - BODY OVERHEAT INDICATION EVENTUALLY EXTINGUISHED. LT WING BODY OVERHEAT INDICATION CAME ON AGAIN AFTER APPROXIMATELY 30 MINUTES AND RT PACK INDICATION ILLUMINATED. ALL 3 ISDR ASMF201510200001Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO, AFTER START ENGINES THE ILS & GLS LIGHTS TURNED ON IN THE IRS DISPLAY PANEL WHEN MASTER CAUTION PUSHED. PERFORMED THE FIM 34-31 TASK 801 PROCEDURE, NO CONFIRMING FAILURE, TESTED CORRECT.SDR CA150807008Coffeemaker · smoke(CAN) DURING FLIGHT, A STRONG ELECTRICAL BURNING ODOR DETECTED IN FWD GALLEY. GREY AND THIN SMOKE FOUND COMING FROM BREWER BELOW STOWAGE. BREWER POWER TURNED OFF AND CIRCUIT BREAKERS PULLED, SMOKE DISSIPATED VERY QUICKLY. BREWER REMOVED AND SENT FOR REPAIRSDR ASMF201509004Warning System · false activationCAPTAIN REPORTED THAT DURING CLIMB, THE LT ENG VIBRATION REACHED 4.2 UNITS. PERFORMED FIM 77-31 TASK 801 & FIM 78-01 TASK PROCEDURES, NO DAMAGES WERE FOUND, TESTED CORRECT. AS PRECAUTIONARY ACTION, REPLACED THE VIBRATION MONITOR IAW AMM 77-31-01. TRIM BALANSDR 2015FA0000645Water Heater · burnedTHE ACFT HAD BEEN UNDERGOING A BASE MAINTENANCE CHECK. AFTER ACCOMPLISHMENT OF A ROUTINE CLEANING TASK OF THE SINK CHAMBER UNIT, IAW TASK INSTRUCTIONS, LHT DOC A-00-11/006-MPD, A LEAK CHECK WAS REQUIRED TO BE CARRIED OUT. DURING THE ACCOMPLISHMENT OF THE LEAKSDR 29EA201506180001Slide · partial deployL1 DOOR SLIDE PARTIALLY DEPLOYED. SLIDE WAS SETTING ON THE DOOR FRAME & JET BRIDGE.SDR 2015F00087Slide · partial deployL1 DOOR PARTIALLY DEPLOYED. SLIDE WAS PARTIALLY ACTIVATED & RELEASED FROM THE L1 DOOR, COVER RESTING ON THE DOOR FRAME & JET BRIDGE.SDR ASMF201507009Wire Harness · damagedAIRCRAFT RETURNED TO PLATFORM, AFTER LT ENG START, THE BLEED DUCT PRESS INDICATOR SHOWED 5 PSI & IT WAS STABILIZED AT 10 PSI. PERFORMED REVISION, DETECTING THE ELEC HARNESS NR MW0311 DAMAGED. THE LT ELEC HARNESS NR MW0311, BLEED AIR REGULATOR & TUBE WERE REPSDR P7UR201506100001Diaphragm · swollenWHEN THE AUXILIARY FUEL TANKS WERE REMOVED FROM THE ACFT, THE 42060-3 DIAPHRAGMS, ASSEMBLY OF THE 42060-19/-29 SELF SEALING BREAKAWAY VALVES, WERE FOUND TO BE SWOLLEN.SDR ASMF201507001Skin Panel · dentedDURING TRANSIT CHECK, DETECTED SEVERAL DENTS ON LT & RT HORIZONTAL STAB LE SKIN. THE ACFT WAS SENT TO HANGAR & A HAIL STRIKE CONDITIONAL INSPECTION IAW MM 05-51-18, DETECTING DAMAGES ON BOTH SIDES OF HORIZONTAL STAB LE, SPOILERS PANELS UPPER SKIN NRS 4, 5, 8,SDR CA150427004Brake · seized(CAN) DURING THE REPLACEMENT OF NR 3 MAIN WHEEL CHANGE DUE TO TIRE WORN TO LIMITS, MATCHING BRAKE ASSY HAS BEEN FOUND SEIZED ONTO THE MAIN WHEEL ASSY. BOTH, MAIN WHEEL AND BRAKE ASSY WERE REMOVED TOGETHER AS 1 UNIT. AFTER REMOVAL IT WAS APPARENT THAT EITHER SDR EE4Y20150119Skin · dentedLOWER FUSELAGE FROM BS 1000 TO BS 1006 BETWEEN STR 20RT AND STR 24RT SKIN PANEL WITH DENT, CREASE AND SCRIBE LINE.SDR EE4Y20150118Skin · dentedLOWER FUSELAGE, BS 100, STR 24LT SKIN WITH SCRIBE LINE, AND BS 1006 BETWEEN STR 23LT AND 24LT SKIN WITH DENT.SDR EE4Y20150093Torque Tube · corrodedTAIL CONE COMPARTMENT, ELEVATOR INPUT TORQUE TUBE, PN 251A2345-11 WITH CORROSION.SDR EE4Y201503310121Skin · scratchedLOWER FUSELAGE, FROM STA 926 TO STA 976 BETWEEN STR 19R AND STR 22RT SKIN PANEL WITH SCRIBE LINES.SDR EE4Y20150111Skin · dentedLOWER FUSELAGE STA 918 STRINGER 23RH SKIN LAP JOINT WITH DENT.SDR EE4Y20150120Skin · scratchedLOWER FUSELAGE FROM STA 1012 TO STA 1020, BETWEEN STR 26RT AND 27LT SKIN PANEL WITH SCRIBE LINE.SDR EE4Y20150109Skin · dentedLOWER FUSELAGE FROM STA 395 TO STA 400 BETWEEN STRINGER 18RT AND STRINGER 20RT SKIN WITH DENT AND CREASE.SDR EE4Y20150094Flap Track · wornLEFT WING, T/E FLAP TRACK NR 1 INBD AND OTBD SIDE EDGES WITH WEARS.SDR EE4Y20150110Skin · dentedLOWER FUSELAGE AT BS 727+2 BETWEEN STRINGER 19 AND 20R SKIN WITH DENT.SDR EE4Y20150096Skin · dentedLOWER FUSELAGE BETWEEN BS 847 AND 867, AND BETWEEN STRINGERS 19 - 21R SKIN PANEL WITH DENTS.SDR ASMF201503022Hmu · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DIFFERENCE OF ONE INCH BETWEEN THRUST LEVERS AT IDLE & THE RT ENG WITH OSCILLATIONS. PERFORMED BITE TO RT EEC IAW FIM 73-00 TASK 801 PROCEDURE, NO FAILURE DETECTED. BOTH ENGS WERE STARTED DETECTING THE LT ENG WAS 67.9% ATSDR EE4Y20150095Skin · bentLEFT WING, SLAT, NR 1, WS 646 NOSE SKIN BENT.SDR Z6WR20150218001Panel · damagedAREAS OF DISCOLORATION DUE TO HEAT EXPOSURE ON BONDED PANEL ASSY. ULTRASONIC NDT INSPECTION ON BOND ASSY WAS PERFORMED IAW D6-37239, 78-30-02 PART 4 AND FOUND AN AREA OF HEAT DAMAGE/ DELAMINATION THAT MEASURES 2.1" X 2.3".SDR ASMF2015030400001Relay · failedAIRCRAFT REJECTED TAKE OFF AT 80 KNOTS DUE TO MASTER CAUTION & RT AFT OVERWING DOOR LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED REMOVAL & INSTALLATION OF THE RT EMER EXIT DOOR IAW AMM 52-22-00 & IT PERSDR ASMF201503008Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 60 KNOTS DUE TO MASTER CAUTION & RT AFT OVERWING DOOR LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED BITE TO PSEU & THE CB`S WERE RESEATED IAW FIM 32-09 TASK 801 PROCEDURE, NSDR ASMF201501028Battery Pack · damagedAIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CLIMB, ALL EMER LIGHTS TURNED ON & BURNED ODOR WITH NO EVIDENCE OF SMOKE WAS DETECTED. PERFORMED REVISION DETECTING IN THE M1671 BATTERY PACK THE CB P18-3 B-10 POPPED. O THE BATTERY PACK NR M1671 WAS DEFERRED IAW MSDR ASMF201501027Unknown · malfunctionedAIRCRAFT RETURNED FROM FLIGHT, DURING CLIMB, THE LT PNEUMATIC SYS INDICATOR SHOWED 5 PSI AT 1,000 FEET & IT WAS SHOWED 0 PSI AT 26,000 FEET WITH OSCILLATIONS. ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. DEFERRED THE LT PNEUMATIC SYS IAW MEL 3SDR ASMF201501024Radome · dentedDURING TRANSIT CHECK, IT WAS DETECTED A DENT IN RADOME BETWEEN 4:00 AND 5:00 HRS POSITION OF 4.0 INCHES IN LENGTH & 3.0 INCHES WIDE. EVALUATED THE DAMAGE & FOUND OUT OF LIMITS IAW SRM 53-52-00. ACFT WAS SENT TO THE HANGAR & ISSUED THE NON-ROUTINE CARDS A0223SDR ASMF201501022Solenoid · malfunctionedAIRCRAFT REJECTED TAKE OFF AT 60 KNOTS, DUE TO RT AFT OVERWING LIGHT TURNED ON. PERFORMED A REVISION AT THE AFT OVERWING DOOR IAW AMM 52-20-00 & BITE TO PSEU IAW FIM 52-20 TASK 801 PROCEDURE, SHOWING FAILURE MSG. R FL SW FAULT, & DETECTING FAILURE OF FLIGHT L
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