Boeing 737-800
Service difficulty reports · 843
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 = '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 29EA201701110001Warning Light · false activationLEFT AFT OVERWING LIGHT CAME ON WHEN APPLYING TAKE-OFF POWER. TROUBLESHOT IAW FIM 52-20 TASK 801 AND FOUND FAULT DURING PSEU BITE PROCEDURE. CLEARED FAULT AND LIGHT EXTINGUISHED IAW TASK 801. PERFORMED EMERGENCY EXIT DOOR SYSTEM TEST IAW AMM 52-22-00 SYSTEM TESDR AALA20161229016Indicator · faultyAIRCRAFT NOT GROUNDED. EMERGENCY DECLARED. BOS-ORD FLIGHT RETURNED TO BOS ACCOUNT LEADING EDGE FLAP TRANSMITTER INDICATION. FLAPS STUCK AT 1/2 DEGREE, HANDLE 0. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW AMM 27-58-02-000-80SDR ASMF201612017Solenoid · failedAIRCRAFT REJECTED TAKEOFF AT 45 KNOTS DUE TO RIGHT FORWARD EMERGENCY OVERWING DOOR WARNING ANNUNCIATOR ILLUMINATED. MAINTENANCE PERFORMED REVISION IAW AMM 52-20-00. THE RIGHT FORWARD EMERGENCY OVERWING WARNING DOOR SOLENOID WAS REPLACED IAW AMM 52-22-41 AND TSDR ASMF201612015B-Nut · looseDURING TRANSIT CHECK, DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR WW. MAINTENANCE PERFORMED FOUND THE HYDRAULIC LEAK IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE NUT. THE HYDRAULIC PRESSURE LINE WAS TIGHTENED IAW ASDR AALA20161125006Battery · dischargedFLIGHT ATTENDANT FLASHLIGHT AFT RIGHT OUTBOARD IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.SDR ASMF201612012Skin · dentedDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED THE INBOARD TRAILING EDGE FLAP AND INBOARD AFT FLAP WITH DAMAGES BY FOD. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING A DENT OF 25.0” LENGTH, 55.0” WIDTH, 0.625” DEPTH BETWEEN ITEF 112.55 AND ITEF 138.05SDR ASMF201612011Shutoff Valve · malfunctionedDURING FUELING, A FUEL SPILLAGE IN THE LEFT TANK WAS DETECTED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN AND MAINTENANCE PERSONNEL CLOSED THE VALVE MANUALLY AND THE REFUELING SHUTOFF VALVE WAS DEFERRED BY MEL 28-10-2 CAT C. AT SDR ASMF20161216009Contactor · failedDURING TRANSIT CHECK, THE TRANSFER BUSS OFF LIGHT TURNED ON WITH APU AND EXTERNAL POWER. MAINTENANCE PERSONNEL PERFORMED BITE TO GCU AND BPCU IAW FIM 24-41 TASK 801 PROCEDURE, DETECTING THAT TRANSFER BAR DID NOT FEED ELECTRIC CURRENT DUE TO THE LEFT GENERATOR SDR ASMF201612008Fan · distortedDURING TRANSIT CHECK, IT WAS DETECTED IN THE RIGHT ENGINE DISTORTION AT FAN BLADE LEADING EDGE POSITION 2. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING DISTORTION AT FAN BLADE LEADING EDGE POSITION 2 IN THE RIGHT ENGINE WITH 2.0” OF RADIAL DISPLACEMENT, SDR AALA20161107038Bracket · out of adjustAIRCRAFT NOT GROUNDED. R1 DOOR EVACUATION SLIDE GIRT BAR IS DIFFICULT TO ARM/DISARM. ADJUSTED DOOR SLIDE BRACKET IAW AMM 25-61-00. OPERATIONAL CHECK GOOD.SDR ASMF20161216005Pitot Tube · damagedAIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO EICAS MESSAGE IAS DISAGREE AND A DIFFERENCE OF 12 KNOTS BETWEEN SPEEDOMETERS BEING BIGGEST LEFT SIDE. MAINTENANCE PERSONNEL PERFORMED FIM 31-62 TASK 876 PROCEDURE, DETECTING THE RIGHT STATIC PITOT TUBE DAMAGED; SO TSDR 29EA2016102400001Power Supply · faultyDURING DAILY CHECK FOUND L1 DOOR ENTRY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOOTING FOUND EMERGENCY POWER SUPPLY FAULTY. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-06 OPS CHECKED NORMAL.SDR ASMF20161216001Hmu · failedAIRCRAFT REJECTED TAKEOFF AT 70 KNOTS DUE TO RIGHT EICAS MESSAGE MASTER CAUTION AND ENGINE CONTROL LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 7.14 PROCEDURE, CONFIRMING THE FAILURE. MAINTENANCE PERSONNEL PERFORM THE FIM 73-06 TASK 801 PROCEDURE, DETECTSDR ASMF201611024Shutoff Valve · malfunctionedDURING FUELING, A FUEL SPILLAGE IN THE RIGHT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED AND MAINTENANCE CLEANED THE SELECTOR. THE SHUTOFF VALVE WAS RESEATED AND TESTED SEVERAL TIMES IAW MM 28-21-00, NO LEAKS WERE DETECTED SDR 2016FA0000472Lens · missingEMERGENCY AISLE LIGHT LENS MISSING AT POSITION 15C. LIGHT IS OPERATIVE.SDR ASMF201611017Wire Harness · damagedDURING TRANSIT CHECK, THE RIGHT ENGINE FIRE HANDLE LIGHT WAS NOT ILLUMINATED DURING FIRE DETECTION TEST AND LOOP B OF RIGHT ENGINE WITH FAULT. MAINTENANCE PERSONNEL PERFORMED RIGHT ENGINE FIRE DETECTION TEST IAW AMM 26-10-00, DETECTING LINE OPEN AT MW0326 WIRSDR ASMF201611009Tire · deflatedAIRCRAFT REJECTED TAKE OFF AT 110 KNOTS, DUE TO FWD ENTRY DOOR LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE MLG TIRES NUMBERS 3 AND 4 THAT BEGIN TO DEFLATE; SO THE MLG WHEEL NUMBERS 3 AND 4 WERE REPLACED IAW AMM 32-45-11. AIRCRAFT WASDR ASMF201610018Tire · deflatedAIRCRAFT REJECTED TAKE OFF AT 110 KNOTS, DUE TO FWD ENTRY DOOR LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE MLG TIRES NUMBERS 3 AND 4 THAT BEGIN TO DEFLATE; SO THE MLG WHEEL NUMBERS 3 AND 4 WERE REPLACED IAW AMM 32-45-11. AIRCRAFT WASDR ASMF201611005Pump · failedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFSDR ASMF201610014Pump · failedAIRCRAFT RETURNED DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFT WAS SENT TO THSDR ASMF201611003Skin · dentedDURING TRANSIT CHECK, DETECTED A HIT ON THE RIGHT INBOARD FLAP NUMBER 3. MAINTENANCE PERSONNEL PERFORMED REVISION TO RIGHT FLAP NUMBER 3 IAW SRM 57-53-01, DETECTING A DENT OF 11 INCHES IN LENGTH, 2 INCHES WIDE. INSPECTION PERSONNEL EVALUATED THE DAMAGE AND FOSDR ASMF201610012Skin · dentedDURING TRANSIT CHECK, IT WAS DETECTED A HIT ON THE RIGHT INBOARD FLAP NUMBER 3. MAINTENANCE PERSONNEL PERFORMED REVISION TO RIGHT FLAP NUMBER 3 IAW SRM 57-53-01, DETECTING A DENT OF 11 LENGTH, 2 WIDE. INSPECTION PERSONNEL EVALUATED THE DAMAGE AND FOUND IT OUT SDR ASMF201610009Skin · damagedCAPTAIN REPORTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN DURING DESCENT. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING SEVERAL LIGHTNING STRIKES ON LEFT WINDOW FRAME NUMBERS 2 AND 3 AT D-F SILL AND E-F, G-H POSTS. INSSDR FOTR20160722076Door Sill · corrodedAFT CARGO DOOR SILL SKIN UPPER SURFACE HAS NUMEROUS SPOTS OF CORROSION. REPLACED.SDR FOTR20160711075Floorbeam · corrodedAFT CABIN BS 980, RBL 36-56, FLOOR SUPPORT BEAM UPPER FLANGE & PAN HAVE SURFACE CORROSION. REPAIRED ON FAS NR 83223, W/O N364AG-01-01.SDR FOTR20160711074Floor Support · corrodedAFT CABIN BS 980, LBL 36-LBL +56 FLOOR SUPPORT BEAM UPPER FLANGE AND ADJACENT PAN HAVE CORROSION. REPLACED ON FAS NR 83224, W/O N364AG-01-01.SDR FOTR20160711073Floor Support · corrodedCABIN BS 992 FLOOR SUPPORT, ZEE-ANGLE, RBL 36-56 HAS CORROSION AT FASTENER HOLES. REPLACED ON FAS NR 83290 W/O N364AG-01-01.SDR FOTR20160711072Web · corrodedAFT CABIN BS 986, RBL 36 FLOOR WEB HAS CORROSION. REPLACED ON FAS NR 83374, W/O N364AG-01-01.SDR FOTR20160711071Floorbeam · corrodedCABIN BS 992 FLOORBEAM ANGLE LBL 36-46 HAS CORROSION AT THE FASTENER HOLES. REPLACED ON FAS NR 83292 W/O N364AG-01-01.SDR FOTR20160712070Floor Support · corrodedAFT CABIN BS 980-1010, RBL 36 AFT GALLEY FLOOR SUPPORT HAS CORROSION. REPLACED ON FAS NR 83221 W/O N364AG-01-01.SDR FOTR20160708069Skin · dentedSKIN BS 1007 BETWEEN STRINGERS 13 & 14R, HAS A SHARP DENT. REPAIRED ON FAS NR 83006, REF: FAS EA 16215 REV IR, W/O N364AG-01-01.SDR ASMF201608006Engine · damagedIAW REMOTE DIAGNOSTIC SYSTEM, THE RT ENGINE HAD A SHARP DECREASE IN TAKEOFF, EGT MARGIN AND CORE SPEED AS WELL AS IN INCREASE IN EGT AND FUEL FLOW. MAINTENANCE PERSONNEL PERFORMED THE RT BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTIONSDR ASMF201608005Transmitter · failedCAPTAIN REPORTED THAT DURING APPROACH, T/E FLAP DISAGREE AND FLAP ASYMMETRY, SO FLIGHT CREW ACCOMPLISHED THE QRH 9.28 PROCEDURE, BEING NECESSARY A MISSED APPROACH. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-51, TASK 801 PROCEDURE, SHOWING FAILURE CODE 27-5226SDR BJNA20160711001Lamp · inoperativeDOOR 2 RIGHT EMERGENCY EXIT LIGHT HAD ONE LAMP INOPERATIVE.SDR ASMF2016072600014Actuator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINES START, THE LEFT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO LEFT EEC IAW FIM 73-10 TASK 801 PROCEDURE, SHOWING THE MESSAGES L REVERSER SLEEVE POSITION SIGNAL OUT OF RANGE; SO THE LSDR ASMF2016072600006Window · openAIRCRAFT REJECTED TAKEOFF AT 75 KNOTS WITH 74,600 KG WEIGHT DUE TO LEFT WINDOW NUMBER 2 OPENING. MAINTENANCE PERSONNEL PERFORMED TO LEFT NUMBER 2 THE OPERABLE WINDOW OPERATIONAL CHECK IAW AMM 56-12-11-720-803 AND OPERABLE WINDOW FUNCTIONAL CHECK IAW AMM 56-12-SDR ASMF20160620010Engine · damagedIAW REMOTE DIAGNOSTIC SYSTEM, THE LT ENGINE HAD A SHARP DECREASE OF EGT HOT DAY MARGIN, AS WELL AS AN INCREASE OF EGT AND FUEL CONSUMPTION. MAINTENANCE PERSONNEL PERFORMED THE LT ENGINE BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTION SDR SAJF2016041905008Controller · malfunctionedB-18609 ATB DUE TO OUTFLOW VLV CAN'T CONTROL. AT FL370 CABIN ALT CONTINUED TO CLIMB 500 FT PER MIN, EMER DESCENT INITIATED. CABIN ALT WARNING HORN & LIGHT ON. GND BITE FOUND FAULT CODE 007 ON CPCS. IAW AMM 21-31-03 REPLACED OUTFLOW VLV & CHECKED AUTO & MANSDR 29EA20160415001Oxygen Gen · swollenEMERGENCY O2 GEN EXPANDED DURING MX SEAT ROW 23DEF. R & R O2 GEN IAW AMM 35-22-11.SDR BJNA20160412001Light · inoperativeDURING PHASE INSPECTION, CHECK FOUND AFT RT SECTION OF EMERGENCY LIGHTS NOT ILLUMINATING.SDR Z6WR20160405007Panel · 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, REVEALED EIGHT AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION C/T THE 174 BONDED PANSDR 29EA20160406001Trim Motor · faultySTABILIZER FAILS TO TRIM NOSE UP & NOSE DOWN. TROUBLESHOOT STAB TRIM MOTOR IAW FIM 27-41 TASK 802 & 803. FOUND FAULTY STAB TRIM MOTOR. REMOVED STAB TRIM MOTOR. INSTALLED SERVICEABLE STAB TRIM MOTOR TAKEN FROM ACFT N276EA. PERFORMED OPERATIONS CHECK OF STASDR ASMF201605003Warning Light · false activationAIRCRAFT REJECTED TAKEOFF DUE TO FWD OVERWING DOOR LIGHT TURNED ON BEFORE RESIZING 80% OF N1. DEFERRED THE FWD OVERWING DOOR LIGHT IAW MEL 52-3 2 CAT C. HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-51-07, NO DAMAGES WERE FOUND. THE FIM 52-20 TASK 801SDR SAJFCAL105004Control Panel · malfunctionedAT BUNTA 1224Z FL330 MCP INOPERATIVE, AUTOPILOT INOPERATIVE, REVERT TO MANUAL UNABLE RVSM DES FL270 B4 LEVEL OFF, OPERATIONS NORMAL ACTION TAKEN. REPLACED MCP & PFM INSTALLATION TESTED NORMALLY.SDR Z6WR20160219006Panel · degradedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B REVEALED 3 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION. CT THE 174 BONDED PANEL ASSDR Z6WR20160219005Panel · degradedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2102-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 45B, REVEALED 3 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION. CT THE 174 BONDED PANEL ASDR Z6WR20160219004Panel · degradedUPON REMOVAL OF THE 315A2130 BLANKET INSTALLATION, VISUAL & ULTRASONIC INSPECTION OF THE 315A2101-174 BONDED PANEL ASSEMBLY, CMM 78-31-26 FIGURE 6 ITEM 40B, REVEALED 3 AREAS OF THERMAL DEGRADATION RESULTING IN DISBOND & DELAMINATION CT THE 174 BONDED PANEL ASSSDR 29EA2016020900001Bulb · inoperative16 DEF EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-51-03. OPS CHECK NORMAL. LEFT OVERWING AFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM 33-51-04. OPS CHECK NORMAL.SDR BJNA20160204001Power Supply · failedTHE LEFT AFT OVERWING EXIT EGRESS LIGHT WILL NOT ILLUMINATE. THE RIGHT AFT OVERWING EXIT EGRESS LIGHT WILL NOT ILLUMINATE. REPLACED THE POWER SUPPLY.SDR 29EA1601143380001Battery Pack · dischargedSEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE ON THE AFT LT AREA OF THE AIRCRAFT. R & R AFT LT POWER SUPPLY BATTERY PACK IAW AMM 33-51-01. OPS CHECK NORMAL IAW AMM 33-51-00.
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