Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA980154Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK .125 INCH AFT ENTRY DOOR CUTOUT UPPER HINGE STATION 953 SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21A. (M)SDR USAA980153Skin · creaseINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 5 INCH CREASE IN SKIN BS 927-947 AND 933-943, STRINGER 17L-19L. REMOVED PREVIOUS DOUBLER AND CUTOUT DAMAGED AREA, INSTALLED DOUBLER AND FILLERS, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAA980152Strap · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS, BS 312 LOWER CHORD STABILIZER STRAP. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA980151Keel Beam · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORRODED AREA TWO LEFT KEEL BEAMS BS 727 AND 722. INSTALLED REPAIR STRAP, REPAIRED PER EA 43828. (M)SDR USAASB98086Connector · failedCLT - MAINTENANCE FOUND 50 PERCENT OF THE EMERGENCY LOW LEVEL LIGHTING INOP. MAINTENANCE FOUND A LOW LEVEL LIGHTING CANNON PLUG BAD. WHEN CANNON PLUG WAS HANDLED AND SHAKEN, LIGHTS FLICKERED. WIRES WERE PULLED AND APPEARED TO BE OVERCRIMPED WHEN INSTALLED. SDR USAASB98081Filter · dirtyMCO - FLT 254 - THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED OVER MCO AT 25,000 FEET. CREW REDUCED POER AND LIGHT WENT OUT, BUT THEN REILLUMINATED AND REMAINED ON EVEN AT IDLE. CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED TO MCO WHERE THE FLIGHT LANDEDSDR USAASB98082Power Supply · inoperativeCMH - MAINTENANCE FOUND ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE FOUND ALL EMERGENCY LIGHT BATTERIES DEAD. CHARGED ALL BATTERIES FOR FIVE HOURS, THEN REMOVED AND REPLACED BATTERY PACKS FOR THE INTERIOR LIGHTS ABOVE THE MAIN ENTRANCE DOOR SDR USAASB98079Switch · defectiveLGA - UPON TESTING EMERGENCY LIGHTING SYSTEM, WITH SWITCH IN ARMED POSITION, ALL LIGHTS BEGAN TO ILLUMINATE INTERMITTENTLY OFF AND ON, ON THEIR OWN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK. OPERATIONAL CHECK GOOD. (M)SDR USAASB98061Light Assy · failedALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB98055Light · failedCLT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB98049Wire · brokenPIT - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9 INOP. MAINTENANCE REPAIRED A BROKEN WIRE NEAR SEAT ROW 9. OPERATIONAL CHECK GOOD. (M)SDR USAA980106Skin · crackedROA - DURING 'CX-2' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK FORWARD ENTRY DOOR CUT OUT LOWER HINGE CUT OUT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIG 31. (M)SDR USAASB98041Tr Unit · inopMCO - FLT 508, EN ROUTE FROM FLL TO PIT, THE NR 1 GEN SHOWED OVERLOAD WITH A HIGH AMP READING OF 90 AMPS. THE NR 2 GEN WAS 50 AMPS. WHEN THE CREW TRIED TO DOWNLOAD, THE NR 1 GENERATOR DROPPED OFF LINE ALONG WITH FOUR CIRCUIT BREAKERS IN SEQUENCE. NR 1 MAIN SDR USAA980059Stringer · corrodedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORROSION BS 967 TO 1006 STRINGER 27L. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAASB98036Uplock Sensor · failedATL - FLT 1243 - AFTER TAKEOFF FROM PHL, THE LEFT MAIN LANDING GEAR TRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR AND LIGHT WENT OUT, THEN IT FLICKERED FOR REMAINDER OF FLIGHT. FLIGHT LANDED IN ATL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND RESDR USAASB98030Epr Indication · malfunctionedMCI - FLT 878 - FLT RETURNED FIELD AT MCI DUE TO NR 2 ENGINE APPEARED TO LOSE POWER. INDICATION SHOWED INCREASING EGT AND DECREASING EPR. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE VISUALLY INSPECSDR USAASB98026Battery Pack · dischargedCLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAA980046Stringer · corrodedROA - DURING CX-4 CHECK, FOUND 2 INCH BY 6 INCH CORROSION AT BS 967 STRINGER 26 LEFT. REMOVED CORROSION AND INSTALLED STRINGER SPLICE PER SRM 53-10-3 PAGE 3. (M)SDR USAASB98029Power Supply · inoperativeROA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. (M)SDR 98ZZZM290Battery Pack · dischargedROA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB98023Battery Pack · dischargedCLT - MAINTENANCE FOUND THE FORWARD, CENTER AND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE THREE BATTERY PACKS AT EACH INDIVIDUAL OVERHEAD LIGHT. OPERATIONAL CHECK GOOD. (M)SDR USAASB98017Door · failedLGA - FLT 324 - DURING CLIMB-OUT OF LGA, AT APPROXIMATELY 17,200 FEET, A LOUD BANG WAS HEARD AROUND THE LEFT FORWARD ENTRY DOOR. PRESSURIZATION COULD NOT KEEP UP WITH THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERSDR USAASB98013Battery Pack · dischargedPHL - DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB97353Anti-Ice Duct · crackedPIT - FL 1223 - DURING CLIMB-OUT OF PIT AT APPROX 12,9000 FT, THE START VALVE OPEN LIGHT ILLUMINATED ON THE NR 2 ENGINE. CREW FOLLOWED CHECKLIST AND SHUT DOWN THE NR 2 ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT PIT WHERE IT LANDED SDR USAASB97350Shutoff Vlv · failedPIT - FLT 1090 - FLT DIVERTED TO PIT DUE TO A NR 2 ENGINE START VALVE INDICATOR LIGHT ILLUMINATING. CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED AND EMERGENCY. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. SDR 98ZZZM142Switch · failedPIT - FLT 1090 - FLT DIVERTED TO PIT DUE TO A NR 2 ENGINE START VALVE INDICATOR LIGHT ILLUMINATING. CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED AND EMERGENCY. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. SDR 98ZZZM141Shutoff Vlv · failedPIT - FLT 1090 - FLT DIVERTED TO PIT DUE TO A NR 2 ENGINE START VALVE INDICATOR LIGHT ILLUMINATING. CREW SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED AND EMERGENCY. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. SDR USAASB97345Power Supply · failedCMH - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHT AISLE SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY. OPS CHECK GOOD. (M)SDR USAASB97340Pitot Probe · malfunctionedCLT - FLT 8026 - FLIGHT DIVERTED TO CLT DUE TO A 10 KNOT DIFFERENCE BETWEEN CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS. INDICATED AIRSPEED APPEARS TO BE 10 KNOTS HIGHER ON FIRST OFFICERS SIDE BETWEEN 70-150 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR 98ZZZM111Adc · malfunctionedCLT - FLT 8026 - FLIGHT DIVERTED TO CLT DUE TO A 10 KNOT DIFFERENCE BETWEEN CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS. INDICATED AIRSPEED APPEARS TO BE 10 KNOTS HIGHER ON FIRST OFFICERS SIDE BETWEEN 70-150 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR USAASB97332Battery Pack · dischargedCLT - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY ESCAPE SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB97326Battery Pack · dischargedROA - MAINTENANCE FOUND THE FORWARD ENTRY AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD CARGO COMPT. OPS CHECK GOOD. (M)SDR USAASB97322Brakes · failedPIT - FL159 PILOT REPORTED NO RIGHT BRAKING WHEN LANDING AND WHILE TAXIING. ONCE FULL PRESSURE WAS APPLIED TO RIGHT BRAKE PEDAL, BRAKE WOULD THEN SUDDENLY GRAB. MAINTENANCE FOUND INSPECTION OF BRAKES NORMAL. NO FLUID LEAKS WERE FOUND. PRESSURES WERE NORMALSDR USAASB97313Power Supply · inoperativeBWI - MAINTENANCE FOUND THE FORWARD CENTER AISLE EMERGENCY LIGHT INOP IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPS CHECK GOOD. (M)SDR USAA970336Frame · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK DOOR FRAME AT BOTTOM FORWARD CORNER OF FORWARD CARGO DOOR FRAME. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 51-40-3 FIG 1. (M)SDR USAA970335Skin · crackedINT - DURING Q-1 CHECK EDDY CURRENT INSPECTION, FOUND CRACK .5 INCH FORWARD SERVICE DOOR SKIN LOWER AFT CORNER. DOUBLER AND TRIPLERS INSTALLED, REPAIRED PER SRM 43-30-3, FIG 6. (M)SDR USAA970334Frame · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .25 IINCH CRACK BS 616 WL 201 LBL 63 FRAME. INSTALLED DOUBLER, REPAIRED PER EA 43250. (M)SDR USAA970333Stringer · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 10 INCHES CORROSION AT BS 1016 AT STRINGER 26R FUSELAGE STRINGER. REMOVED CORRODED SECTION AND SPLICED IN NEW STRINGER. REPAIRED PER BOEING DRAWING 65-45776. (M)SDR USAA970332Skin · scratchedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 8 INCH SCRATCH, BLENDED BEYOND SRM LIMITS, BS 877 BETWEEN STRINGER 18L AND STRINGER 19L FUSELAGE SKIN. FABRICATED AND INSTALLED DUOBLER REPAIR, REPAIRED PER SRM 53-30-1, FIG 1. (M)SDR USAA970331Skin · scratchedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND BURNISHED OUT SCRATCHES BEYOND LIMITS 2 INCHES BY 19 INCHES BETWEEN STRINGERS 2 - 3 LT, BS 987-1006 (UNDER DORSEL FIN) FUSELAGE SKIN. CUT OUT DAMAGE AND INSTALLED 23.5 INCH BY 8 INCH DOUBLER PER SRM SRM 53-30-3 SDR USAA970330Keel Beam · wornINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FLANGE WORN AT SCREW HOLES FORWARD OF BS 727 RIGHT SIDE KEEL BEAM LOWER CHORD. BLENDED DAMAGE AREAS AND INSTALLED FABRICATED REPAIR, REPAIRED PER EA 4329. (M)SDR USAASB97307Power Supply · failedCLE - MAINTENANCE FOUND THE AFT ENTRANCE DOOR AND AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY M571. OPS CHECK GOOD. (M)SDR USAASB97304Bulbs · failedBWI - FL1721 - ON DESCENT INTO DCA, CAPT DID NOT RECEIVE THREE GREEN LIGHTS WHEN THE GEAR WAS EXTENDED. LIGHTS TESTED GOOD. CAPT DID A FLYBY AND THE TOWER CONFIRMED GEAR WAS DOWN. FIRST OFFICER WENT TO THE CABIN AND CONFIRMED THAT THE MAIN GEAR WAS DOWN. CSDR USAASB97303Battery Charger · failedORD - MAINTENANCE FOUND THE AFT LEFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP AND THE AFT LEFT EMERGENCY LIGHT BATTERY SUPPLY WITH LOW CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER UNIT FOR THE AFT LEFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT ASDR 97ZZZM1204Battery Pack · dischargedORD - MAINTENANCE FOUND THE AFT LEFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP AND THE AFT LEFT EMERGENCY LIGHT BATTERY SUPPLY WITH LOW CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER UNIT FOR THE AFT LEFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT ASDR USAASB97305Wire · brokenROC - MAINTENANCE FOUND THE EMERGENCY EXIT FLOOR LIGHT INOP AT ROW 13, MID CABIN. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. (M)SDR USAA970320Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK NOSE WHEEL WELL 5 INCHES AFT OF 227 BULKHEAD 1 INCH BELOW W/W CEILING WEB. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA970319Beam · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLE ON FLOORBOARD BEAM BS 328 LBL 54. INSTALLED NUTPLATE REPAIR, REPAIRED PER TR 53-10-13. (M)SDR USAASB97291Windshield · failedCLT - FLT 200 - THE AIRCRAFT WAS OVER (SDF) EN ROUTE TO (DFW) WHEN THE CAPTAINS NR 1 WINDSHIELD BEGAN ARCING. THE WINDOW HEAT WAS SWITCHED OFF BUT A FEW MINUTES LATER THE OUTER PANE CRACKED. THE CREW DECIDED TO DIVERT TO (CLT). NO EMERGENCY WAS DECLARED ANDSDR 97ZZZM1100Heat Controller · failedCLT - FLT 200 - THE AIRCRAFT WAS OVER (SDF) EN ROUTE TO (DFW) WHEN THE CAPTAINS NR 1 WINDSHIELD BEGAN ARCING. THE WINDOW HEAT WAS SWITCHED OFF BUT A FEW MINUTES LATER THE OUTER PANE CRACKED. THE CREW DECIDED TO DIVERT TO (CLT). NO EMERGENCY WAS DECLARED AND
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