Boeing 737-275
Service difficulty reports · 290
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 = '737275' 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 = '737275' 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 CA980406015Pitot Heat · failed(CAN) AIRCRAFT RETURNED DUE TO LT ELEVATOR PITOT HEAT INOPERATIVE. REPLACED.SDR CA980325013Pitot Head · failed(CAN) AIRCRAFT RETURNED TO BLOCKS DUE LT ELEVATOR PITOT PROBE HEAT INOP, REPLACED.SDR 98ZZZX1380Skin · crackedFUSELAGE SKIN CRACKED AT THE FOLLOWING LOCATIONS, BUTT JOINT 1016 STR 14L AND STR 10R. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-204 DATED 2-18-98, AND 737 SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 2-25-98.SDR 98ZZZX1379Skin · crackedNUMEROUS FASTENER HOLES CRACKED IN FUSELAGE SKIN, STA 1016, STR 4L. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-212 REV 1, DATED 3-20-98, AND SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 3-20-98.SDR 98ZZZX1378Skin · crackedFUSELAGE SKIN IS CRACKED AROUND SEVERAL FASTENER HOLES IN THE LAP JOINT LOWER ROW AT STR 14R FROM STA 927 TO STA 951. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-211 REV 1, DATED 3-16-98, AND BOEING SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 3-11-98SDR 98ZZZX1377Skin · crackedCRACKS WERE FOUND IN THE FUSELAGE SKIN LAP LOWER ROW BETWEEN STA 992 AND STA 1016, STR 14R. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-208 REV 1, DATED 3-6-98, AND 737 SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 3-12-98.SDR 98ZZZX1376Skin · crackedTHE LOWER FUSELAGE WAS CRACKED AT STA 272, STR 19L. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-203 REV 1, DATED 2-24-98, AND 737 SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 2-25-98.SDR 98ZZZX1375Skin · crackedCRACKS IN FUSELAGE SKIN AT STA 300, STR 24L. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-202 DATED 2-12-98, AND 737 SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 2-23-98.SDR CA980317037Washer · worn(CAN) A/C RETURNED DUE TO FLAPS WOULD NOT LOWER PAST 10 UNITS ON APPROACH. FOUND WASHER RETAINING WASHER AND NUT P/N 69-52435-1, BACKED OFF OF DRIVE SHAFT. TRANSMISSION REPLACED.SDR CA980317035Washer · worn(CAN) AIRCRAFT RETURNED DUE FLAPS WOULD NOT LOWER PAST 10 UNITS ON APPROACH. RETAINING WASHERS BACKED OFF OF DRIVE SHAFT. TR REPLACED.SDR CA980317034Lines · leaking(CAN) A/C RETURNED DUE LT MLG WOULD NOT RETRACT. HEAVY HYD FLUID LOSS ON RETURN. REPLACED HYD LINES, LEAK CHECK. A/C RETURNED TO SERVICE.SDR CA980317026Air Data Compute · failed(CAN) AIRCRAFT RETURNED TO BLOCKS DUE TO CAPT'S ALTIMETER FLAG, MACK TRIM FAIL FLAG. C.A.D.C REPLACED.SDR CA980317025Ivsi · failed(CAN) AIRCRAFT RETUREND TO GATE DUE TO CAPTAIN'S IVSI FAILURE ON CLIMB OUT. REPLACED.SDR CA980317022Drive Gear · stripped(CAN) NR 1 ENGINE ON WATCH FOR EXCESSIVE OIL CONSUMPTION. DURING TROUBLESHOOTING THE DRIVE GEAR (SPUR GEAR) FOR THE ENGINE OIL PUMP WERE FOUND STRIPPED. THE ENGINE WAS REPLACED.SDR CA980128005Light Assembly · defective(CAN) AFTER TAKEOFF,RIGHT HAND MASTER CAUTION LIGHT WOULD NOT CANCEL. AIR TURNBACK. OVERWEIGHT LANDING. MASTER CAUTION LIGHT REPLACED.SDR AWXA9700679Wire · looseDURING ROUTINE MAINTENANCE CHECK, FOUND R-2 DOOR INTERIOR EMERGENCY EXIT LIGHT INOP. RESECURED WIRE, OPS CHECK GOOD.SDR CA971216020Bus Tie Breaker · failed(CAN) NR 2 CONSTANT SPEED DRIVE (CSD) FAILURE, APU WOULD NOT TAKE LOAD. BUS TIE BREAKER (BTB) AND CSD REPLACED.SDR CA971216019Csd · failed(CAN) AIR TURNBACK DUE TO NR 2 CONSTANT SPEED DRIVE (CSD) FAILURE, APU WOULD NOT TAKE LOAD, CSD REPLACED AND THE AIRCRAFT WAS RETURNED TO SRVICE.SDR CA971113021Transciever · intermittent(CAN) AIRCRAFT RETURNED DUE TO UNSERVICEABLE WEATHER RADAR, TEST NORMAL. 2ND UNIT INSTALLED. ANTENNA REPLACED.SDR AWXA9700618Battery · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND MID-CABIN OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID-CABIN OVERHEAD EMERGENCY LIGHT BATTERY, OPS CHECK GOOD. STC - BOEING STANDARD.SDR CA971015018Mask · separated(CAN) TWO EXAMPLES OF BAG SEPARATION AT THE ULTRASONIC BOND BETWEEN THE INLET CHECK RING AND THE BASE. THIS ALLOWED THE INHALATION BAG TO SEPARATE FROM THE UNIT. FOUND DURING DEPLOYMENT WHEN PULLED ON THE BAG TO OPEN THE FLOW VALVE.SDR CA971015017Computer · failed(CAN) IN CRUISE AT 35,000 AUTO PILOT TRIPPED OFF FOLLOWED BY MACH TRIM FAIL LIGHT ON. CAPTAIN ALTIMETER RED FLAG CAME IN VIEW, ALTIMETER ALERT FLAG ON GPWS INOPERATIVE LIGHT ON. TCAS FAILED, SHORTLY THEREAFTER CABIN ALERT HORN SOUNDED, O2 MASKS DEPLOYED, EMERGSDR CA971015015Valve · failed(CAN) TAKEOFF WAS ABORTED AT 100 KNOTS DUE TO BOOM HEARD AND A PARAMETER SHIFT WITH A YAW OF THE AIRCRAFT. VISUAL AND BORESCOPE INSPECTION CARRIED OUT. PRBC (PRESSURE RELIEF BLEED CONTROL) VALVE REPLACED. HIGH ENERGY STOP INSPECTION CARRIED OUT AND AIRCRAFT RESDR CA970922004Module · failed(CAN) AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT LOCK UP. RED LIGHT ON, RECYCLED TWICE STILL NO LOCK UP. HELD UP BY HYDRAULIC PRESSURE, AIRCRAFT RETURNED. NOSE LANDING GEAR HYDRAULIC MODULE REPLACED. NOSE LANDING GEAR UPLOCK ACTUATOR REPLACED, GEAR LUBRICATED.SDR CA970918001Transmitter · failed(CAN) CREW REPORTED EPR GAUGE UNRELIABLE DURING CLIMB. EPR TANSMITTER REPLACED AND TESTED IN ACCORDANCE WITH 77-11-0. ON TAKEOFF ROLL EPR GAUGE AGAIN FAILED. ANOTHER EPR TRANSMITTER WAS INSTALLED, TESTED SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE.SDR AWXA9700489Light · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND THE CEILING MOUNTED OVERWING EMERGENCY EXIT LIGHT INOP. INSTALLED NEW TERMINALS FOR LIGHT ASSEMBLY. REMOVED AND REPLACED FWD LIGHT ASSEMBLY. REMOVED AND REPLACED BATTERY PACK. RELAMPED LIGHTS, OPS CHECK GOOD. STC - SDR CA970922015Indicator · inoperative(CAN) AFTER TAKEOFF UNABLE TO RETRACT FLAPS OR OTHER LEADING EDGE DEVICES. UNABLE TO EXTEND BY NORMAL MEANS. USED ALTERNATE FLAP EXTENSION, AIRCRAFT RETURNED. REPLACED TRAILING EDGE FLAP POSITION INDICATOR.SDR CA970922014Plug · broken(CAN) NR1 ENGINE OIL TEMPERATURE GAUGE NEEDLE BOUNCES IN FLIGHT. NR1 ENGINE SHUTDOWN 20 MINUTES PRIOR TO LANDING. INSPECTION FOUND OIL TEMPERATURE BULB CONNECTOR SOCKET "A" WIRE BROKEN AND "B" LOCK BROKEN AND PUSHED BACK. HARNESS RESECURED AND CONNECTOR SOCKETSDR AWXA9700483Hyd Qty Ind · inoperativeAIR TURNBACK, 'A' SYSTEM HYDRAULIC QUANTITY LIGHT CAME ON AFTER TAKEOFF. QUANTITY DROPPED TO LESS THAN 1.5 GALLONS. ON APPROACH, WITH GEAR AND FLAPS DOWN, QUANTITY CAME BACK TO R/F LINE. CHECKED FOR VISIBLE LEAKS, NO LEAKS NOTED. SERVICED HYDRAULIC SYSTEM SDR AWXA9700447Battery · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND CEILING EMERGENCY LIGHT AT ROW 9 INOP. REPLACED BATTERY PACK, OPS CHECK GOOD. STC - BOEING STANDARDSDR AWXA9700436Light · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL SECTIONS OF FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED 2 SECTIONS OF ESCAPE PATH LIGHTING. OPS CHECK GOOD.SDR CA970807003Indicator · inoperative(CAN) ON TAXI NR1 ENGINE OIL PRESSURE INDICATOR PEGGED FULL SCALE. REPLACED.SDR AWXA9700423Light · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND L-1 DOOR EXIT LIGHT BATTERY DEAD. REMOVED AND REPLACED LIGHT ASSEMBLY STC - BOEING STANDARD.SDR CA970722003Sensor Switch · intermittent(CAN) AIRCRAFT RETURNED DUE TO NR3 LEADING EDGE. TRANSIT LIGHT ON P2 FORWARD PANEL AND NR3 FLAP AMBER LIGHT REMAINED ON AFTER 2 ATTEMPTS AT RE-CYCLING FLAPS. REPLACED RETRACT PROXIMITY SWITCH.SDR CA970715007Epr Transmitter · faulty(CAN) TAKEOFF REJECTED AT 60 KNOTS DUE TO #2 EPR FLUCTUATING AND THROTTLE STAGGER. #2 EPR TRANSMITTER REPLACED AND ENGINE RUN AT FULL POWER CARRIED OUT SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.SDR CA970618006Indicator · fading(CAN) LEFT SIDE OF RADAR SCREEN WENT BLANK. RADAR TURNED OFF FOR A FEW MINUTES, BACK ON AND SAME. TRANSCEIVER REPLACED, NO GOOD. PPI REPLACED AND FUNCTIONED OK.SDR CA970603007Spring · broken(CAN) AIRCRAFT TURNBACK DUE TO INABILITY TO PRESSURIZE. BYPASS VALVE SPRING IN THE WATER SEPARATOR BROKEN, REPLACED.SDR CA970603006Blade · damaged(CAN) #2 ENGINE HAD SLIGHT COMPRESSOR STALL AND DROP IN EPR OF .05, EPR REGAINED AFTER STALL. AIRCRAFT LANDED AS SCHEDULED. INSPECTION FOUND DAMAGE TO A FIRST STAGE COMPRESSOR BLADE BEYOND LIMITS. #2 ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR AWXA9700314Hyd Syst · reqd serviceAFTER GEAR RETRACTION 'A' SYSTEM LOW QUANTITY LIGHT ILLUMINATED AND QUANTITY DROPPED TO ABOUT 1.5 GAL. CYCLED GEAR DOWN AND QUANTITY CAME BACK UP TO NORMAL. LIGHT WENT OUT.'A' SYSTEM HYDRAULIC QUANTITY READING AT REFILL. RESERVICED HYDRAULIC SYSTEM FULL.SDR AWXA9700236Battery · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND CABIN FLOOR EMERGENCY EXIT LIGHT CENTER SECTION OUT. REMOVED AND REPLACED BATTERY AND CABLE SECTION SEAT ROW 8 TO 12.SDR AWXA9700229Fire Warning · soundedON SHORT FINAL AT APPROXIMATLEY 2300 FEET, DURING APU START SEQUENCE, APU FIRE LIGHT ILLUMINATED AND FIRE BELL SOUNDED. FIRE HANDLE PULLED AND ROTATED. LIGHT WENT OUT. APU SHUTDOWN, FIRE SYSTEM TESTED OK. INSPECTED APU ASSEMBLY SECTION. NO EVIDENCE OF FIRSDR CA970421017Sensor · damaged(CAN) DURING CLIMB STALL WARNING SYSTEM ACTIVATED AND CONTINUED TO ACTIVATE UNTIL TOUCHDOWN. STALL WARNING SENSOR DAMAGED BY BRIDGE, REPLACED.SDR AWXA9700221Fire Loop · wornAPU FIRE WARNING ACTIVATED ON FINAL APPROACH. SECURED APU AS PER QRH. FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED TAIL AND DONUT LOOP. REMOVED AND REPLACED FIRE BOTTLE.SDR AWXA9700192Fire Warning · activatedAPU FIRE WARNING ACTIVATED ON FINAL APPROACH. SECURED APU AS PER QRH. FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED TAIL AND DOUGHNUT LOOP.SDR AWXA9700220Element · wornAPU FIRE LIGHT ILLUMINATED DURING APU START. QRH PROCEDURE ACCOMPLISHED, AGENT DISCHARGED, LIGHT EXTINGUISHED AFTER APPROXIMATELY 15 TO 20 SECONDS. REMOVED AND REPLACED APU FIRE BOTTLE IAW R6D26001 AND APU FIRE LOOP ELEMENT, OPS CHECKED GOOD.SDR AWXA9700219Terminal · brokenDURING APU START INFLIGHT, APU FIRE BELL/LIGHT ILLUMINATED. FIRE HANDLE PULLED, BOTTLE FIRED, LIGHT AND BELL OUT WITHIN 10 SECONDS AND MAXIMUM TEMPERATURE DURING START 430 DEGREEES. INSPECTED APU, NO SIGNS OF FIRE NOTED. FOUND TERMINAL END BROKEN ON TAILPIPSDR CA970327006Electronic Contr · faulty(CAN) AIRCRAFT RETURN TO DEPARTURE POINT WITH BOTH EPR GAUGES UNSERVICEABLE. CIRCUIT BREAKERS CHECKED AND FOUND TRIPPED. ELECTRONIC CONTROL UNIT REPLACED, FAILURE NOT CONFIRMED IN THE SHOP.SDR AWXA9700157Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND AFT CENTER AISLE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK STC - BOEING STANDARD.SDR CA970312005Engine Accessory · faulty(CAN) FAILURE OF BOTH #1 AND #2 ENGINE EPR GAUGES ON TAKEOFF. RESET BOTH EPR AND LG CIRCUIT BREAKERS. REPLACED ENGINE ACCESSORY UNIT AS PER WORK CARD.SDR CA970312004Bracket · loose nuts(CAN) CREW REPORTED LOW FREQUENCY AIRFRAME VIBRATIONS AT VARIOUS SPEEDS. AIRCRAFT GROUNDED. ELEVATOR TAB ACTUATOR RODS ATTACHMENT BRACKET WAS LOOSE. RETAINED BY SIX NUTS AND BOLTS AND WAS LOOSE TO THE EXTENT THAT A 1/2 INCH PLAY WAS POSSIBLE BETWEEN BRACKET AN
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