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 CA970226006Bearing · broken(CAN) ON ARRIVAL FLAPS REQUIRED 1 UNIT LEFT AILERON TIRM. HAD TENDENCY TO ROLL RIGHT WITH FLAPS SELECTED. ONE OF THE FOREFLAPS TOGGLE ASSEMBLY'S BEARING BROKEN AND MISSING WHICH CAUSED THE FLAPS TO SHIFT AND WHEN SELECTED UP PUNCHED A HOLE INTO THE MID FLAP FRSDR CA970213002Window · overheated(CAN) #1 LEFT HAND WINDOW OVERHEATING. REPEAT PROBLEM. MOVED WIRES TO SECONDARY SENSOR.SDR AWXA9700071Control Panel · malfunctionedNUMEROUS UNCOMMANDED ROLLS WITH AUTOPILOT ENGAGED AND HEADING SELECT IN USE OR NOT. REMOVED AND REPLACED AUTO PILOT CONTROL PANEL. OPS CHECK GOOD. REMOVED AND REPLACED YAW DAMPER COUPLER PER MM 22-11-141. OPS CHECK GOOD. REMOVED AND REPLACED AILERON POWERSDR CA970210005Switch · intermittent(CAN) AFTER TAKEOFF INFLIGHT 'THRUST REVERSER ISOLATION LIGHT' ILLUMINATED. LIGHT REMAINED ON UNTIL GEAR SELECTED DOWN THEN LIGHT OUT. UNABLE TO DUPLICATE, REPLACED HYDRAULIC PRESSURE SWITCHES.SDR CA970109008Collar · broken(CAN) ON TAXI NOSE WHEEL FROZE IN FULL LEFT TURN. TOWED TO BLOCKS. STEERING COLLAR FORWARD BEARING, BOTH LUGS ON RH SIDE OF COLLAR FOUND BROKEN. BEARING AND STEERING COLLAR REPLACED.SDR CA970109004Clip · broken(CAN) SLIDE ASSEMBLY GIRT BAR RETAINER CLIP BROKEN OFF. REPLACED.SDR AWXA9600742Linkage · brokenON GEAR RETRACTION, BANG HEARD IN NOSE WHEEL WELL WITH VIBRATION. REPLACED BROKEN LT NOSE GEAR DOOR LINKAGE, CHECKED AND ADJUSTED DOORS PER BMM 32-22-11, PAGE 407, STEP L. NOSE GEAR EXT/RET PER 32-33-0, PAGE 101.SDR AWXA9600682Battery · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND R-1 AND R-2 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT. REMOVED AND REPLACED BATTERY, OPERATIONS CHECK GOOD. POWER SUPPLY UNIT INOP CABIN.SDR AWXA9600658Battery · dischargedFOUND EMERGENCY EXIT SIGN ABOVE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY. OPERATIONS CHECK GOOD. (M)SDR CA961104004Turbine Section · failure(CAN) NR 2 ENGINE COMPRESSOR STALLED FOLLOWED BY VIBRATION WHEN APPLYING TAKEOF F POWER. TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO THE RAMP. INSPECTION FOUND A MAJOR FAILURE OF THE TURBINE SECTION. THE NR 2 ENGINE WAS REPLACED.SDR CA961113003Fan · seized(CAN) ON FINAL APPROACH CABIN CREW REPORTED STRONG SMELL OF SMOKE IN AFT PASSENGERS CABIN. GASPER FAN CB PULLED. FAN REPLACED.SDR CA960924011Indicator · no picture(CAN) AIRCRAT HAD NO PICTURE ON WEATHER PPI. REPLACED PPI AND TRANSCEIVER. PPI REPLACED SECOND TIME.SDR CA960924010Line · split(CAN) NOSE GEAR UNSAFE LIGHT ON WITH GEAR SELECTED UP. HYDRAULIC LINE TO UPLOCK ACTUATOR SPLIT, REPLACED.SDR CA960925004Battery · overheat(CAN) APU START UP MAIN AIRCRAFT BATTERY OVERTEMP/THERMAL RUNAWAY. SMOKE IN PASSENGER CABIN. CFR CALLED. REPLACED.SDR CA960925006Valve · sticking(CAN) ON CLIMB #1 ENGINE OIL TEMPERATURE INCREASED TO 126 DEGREES CELSIUS. BY INCREASING POWER TO MAX CONTINUOUS IT CAME TO 120 DEGREES CELSIUS. DURING DESCENT FUEL FLOW AT 7500 PPH TEMPERATURE REMAINED AT 120 DEGREES CELSIUS. OIL TEMPERATURE BULB AND PLUG CHESDR CA960826014Valve · open(CAN) AIRCRAFT RETURNED TO GATE AFTER OIL TEMPERATURE INDICATION IN CLIMB OUT. FOUND FUEL HEAT VALVE PARTIALLY OPEN. REPLACED.SDR AWXA960436Sign · inoperativePHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND CENTER AISLE EMERGENCY LIGHT SIGN INOPERATIVE AT ROW 2. REPLACED CARTRIDGE ASSEMBLY. OPS CHECK GOOD. (X)SDR AWXA960399Standby Act · inoperativePHX - FLT 98 - FLT CREW REPORTED, A RUDDER FLUTTER WHEN CHECKING THE STANDBY RUDDER. PERFORMED RIGHT CHECKS ON NORMAL RUDDER SYSTEM, ALL CHECKS NORMAL. STANDBY SYSTEM CHECKS OK. FOUND STANDBY ACTUATOR DEAD BAND CHECK OUT OF LIMITS. COULD NOT RIG ACTUATOR. SDR CA960826001Boss Nut · loose(CAN) ENGINE OIL PRESSURE LOSS IN FLIGHT. ENGINE SHUTDOWN AND AIRCRAFT DIVERTED. POST FLIGHT INSPECITON FOUND BANJO BOLT LOOSE ON THE OIL BYPASS BOSS. BANJO BOLT TIGHTENED AND ENGINE GROUND RUN SERVICEABLE.SDR CA960827007Bulb · burnt(CAN) AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF. FOUND E & E DOOR OPEN, DOOR CLOSED. FOUND DOOR INDICATION LIGHT ON FLIGHT DECK BRUNED OUT. REPLACED.SDR CA960808106Fuel Control · faulty(CAN) ON TAKEOFF, ADVANCED THRUST LEVERS TO NORMAL SPOOL UP POSITION, ENGINE ACCELERATION NORMAL, CONTINUED TO ADVANCE THRUST LEVERS, #2 ENGINE ACCELERATION WAS A LITTLE SLOWER THAN #1 ENGINE, THEN AS THRUST LEVERS ADVANCED, #2 ENGINE ASSUMED CONTINUOUS POWER SDR AWXA960366Door Frame · crackedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK ON FWD SIDE OF AFT CARGO DOOR FRAME, BS 794, STRINGER 24R. FABRICATED REPAIR PARTS AFTER CONTAINMENT OF CRACK. INSTALLED REPAIR APRTS PER SRM 53-10-4. (M)SDR AWXA960365Flow Contl Unit · inoperativePAE - FLT NR 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, WHILE WORKING PASSENGER OXYGEN SYSTEM CHECK, FOUND ELECTRO-PNEUMATIC CONTINUOUS FLOW CONTROL UNIT AND FUNCTIONAL TEST GOOD IAW MM 35-21-21, 35-21-0. (M)SDR CA960801002Eye End · sheared(CAN) EYE END OF MAIN GARGO DOOR ACTUATOR FAILED WHILE CLOSING DOOR FROM FULLY OPEN. DOOR CLOSED CAUSING DAMAGE TO ONE LOCK ASSEMBLY.SDR AWXA960364Flap Track · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND RIGHT WING OUTBOARD FLAP, INBOARD TRACK NR 7 VERY CORRODED WHERE FLAP TRACK ATTACHES TO LOWER WING PANEL REAR SPAR. REMOVED AND REPLACED NR 7 FLAP TRACK PER CARD R3R27004. (M)SDR AWXA960363Flap Track · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION EMITTING FROM AFT MOUNT OF NR 1 FLAP TRACK. REMOVED AND REPLACED NR 1 FLAP TRACK PER R3L27002. (M)SDR AWXA960362Flap Track · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION EMITTING FROM AFT MOUNT OF NR 2 FLAP TRACK. REMOVED AND REPLACED NR 2 FLAP TRACK PER CARD R3L27003. (M)SDR AWXA960361Stringer · crackedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACKED LWR FLANGE OF STRINGER 27L AT BS 360. REMOVED DAMAGED HAT CHANNEL AT BS 360, STRINGER 27L, FABRICATED NEW CHANNEL, TREATED, PRIMED AND INSTALLED PER SRM 51-10-03. (M)SDR CA960729003Hinge · cracked(CAN) ON COMPLIANCE WITH AD 96-10-06, A 12 INCH CRACK WAS DETECTED ON THE FORWARD LOWER GALLEY LOWER HINGE. REPLACED.SDR CA960725102Capacitor · burnt(CAN) DURING FLIGHT CREW REPORTED LEFT SIDE WINDOW HEATER DID NOT WORK . WORKED AFTER CB RESETTHIRTY MINUTES AFTER ARRIVAL CREW REPORTED ELECTRICAL SMOKE AND SMELLL ON THE FLIGHT DECK LH SIDE WINDOW HEATER WIRE BROKEN AT THE LOWER WINDOW TERMINAL STRIP. LH SISDR AWXA960498Battery Pack · dischargedPHX - FLT 2455 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONS CHECK OK. (X)SDR CA960711008Breaker · burnt(CAN) AIRCRAFT RETURNED AFTER ENGINE START DUE #1 GENERATOR WOULD NOT GO ON LINE. REPLACED BUS TIE BREAKER.SDR CA960711006Switch Oil Press · defective(CAN) #2 ENGINE WAS SHUTDOWN IN FLIGHT, AIRCRAFT DIVERTED, DUE TO ENGINE OIL FILTER BYPASS LIGHT ON. OIL BYPASS PRESSURE SWITCH REPLACED. FURTHER TROUBLESHOOTING TO BE CARRIED OUT AS FILTER BYPASS LIGHT DID NOT GO OUT ON ENGINE START UP.SDR AWXA960360Mop Seal · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON AFT SERVICE DOOR MOP SEAL AT PREVIOUS REWORK AREAS, BS 967 TO BS 987, WL 208, RBL 53. REMOVED AND REPLACED MOP SEAL PER SRM 53-10-1. (M)SDR AWXA960359Seat Track · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK OF BS 987 TO 1016, WL 208, RBL 38. REMOVED AND FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-10-1. (M)SDR AWXA960358Floor Beam · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD UPPER SURFACE BS 947.5, WL 208, LBL 4 TO LBL 8. REMOVED DAMAGED AREA AT BS 947.5, WL 208, LBL 4 - LBL 8. FABRICATED AND INSTALLED REPAIR PARTS FROM BS SDR AWXA960357Floor Beam · corrodedPAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 987.5, WL 208, LBL 41-45. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-1. (M)SDR CA960719101Cells · melted(CAN) ON WALKAROUND CREW REPORTED HOT PLASTIC BURNING SMELL IN CABIN. FOUND BATTERY OVERHEATED. REPLACED.SDR AWXA960322Actuator · damagedICT/PHX - FLT 1103 - LOSS OF A-SYSTEM HYDRAULIC FLUID. CONTRACT MAINTENANCE FOUND NR 2 LEADING EDGE SLAT ACTUATOR DAMAGED. REMOVED AND REPLACED ACTUATOR PER R3M27020. OP CHECK NORMAL. INSPECTED HYDRAULIC FILTERS PER MM 2911-0. NO CONTAMINATION FOUND. PHXSDR AWXA960295Actuator · malfunctionedTUS - FLT 2606 - UNCOMMMANDED ROLL EXPERIENCED ON CLIMB-OUT OF TUSCON, CAUSED BY YAW DAMPER. YAW DAMPER COUPLER FAILS STEP 4 OF BITE, NEW COUPLER NO HELP. INSTALLED MEL 22-03. YAW DAMPER BITE CHECK GOOD AT THIS TIME PER MM 22-11-00, PAGES 543, 544. MEL 22-SDR CA960624002Wire · misinstalled(CAN) ON GROUND AND BOTH GENERATORS TRIPPED OFF WITH STANDBY POWER AS WELL, THEN ALL RETURNED TO NORMAL. ON TAXI SAME THING HAPPENED. ON DESCENT NEXT FLIGHT SAME, LOSS POWER BETWEEN 500' AND 200' BEFORE ALL POWER RETURNED TO NROMAL. REPLACED GENERATOR POWER CSDR AWXA960258Actuator · failedPHX/OAK - FLT 0577 - AIR TURNBACK. NR 2 SLAT EXTENDED ABOUT 2 INCHES EN ROUTE. REMOVED AND REPLACED NR 2 ACTUATOR PER R3M27020. OPERATION AND LEAK CHECK GOOD. PART TOTAL CYCLES, 35,841. (X)SDR CA960514102Tube Assembly · chafed(CAN)AFTER DEPARTURE AIRCRAFT EXPERIENCED LOSS OF "A" SYSTEM HYDRAULICS AND RETURNED TO BLOCKS. "A" SYSTEM HYDRAULIC LINE ABOVE THE L/H MAIN LANDING GEAR CHAFED THROUGH AND WEARING INTO THE 13TH STAGE RESERVOIR PRESSURE LINE. TEMPORARY REPAIR. LINE TO BE REPLASDR AWXA960207Floor Beam · crackedPAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FLOOR BEAM BS 669, LBL 28, WL 208, (LBL 25 LONGITUDINAL BEAM CRACKS EMANATING FROM OVER CUTOUTS BS 665 TO BS 678). STOP DRILLED CRACK TIPS AND REPAIRED IAW, AWA ER NR 2-57-12-10, SDR AWXA960206Door Frame · crackedPAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR, AFT FRAME CRACKED AT STRINGER 14. REMOVED AND REPLACED AFT DOOR FRAME BS 492, STRINGER R18R TO 26R, IAW SRM 51-20-04. (M)SDR AWXA960205Door Frame · crackedPAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR, FORWARD FRAME CRACKED AT STRINGER 21R AND 23R. REMOVED AND REPLACED FORWARD DOOR FRAME BS 440, STRINGER 18R TO 26R, IAW SRM 51-20-04. (M)SDR AWXA960194Service Door · out of adjustPAE - FLT 3710 - AIR TURNBACK. R-2 AFT SERVICE DOOR LIGHT CAME ON CLIMBING OUT OF 29,500 FEET. REMOVED LINER, ADJUSTED UPPER AND LOWER GATES, ADJUSTED TIMING PER MM 52-41-0. REINSTALLED LINER, PRESSURIZED AIRCRAFT. OPS CHECK GOOD. ACFT TT: 60,705 HRS. ASDR AWXA960204Floor Beam · crackedPAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON LONGITUDINAL FLOOR BEAM BS 708, BL 07, WL 202. REMOVED FASTENERS AND CUT DAMAGED SEALANT FROM LONGITUDINAL BEAM. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02. (M)SDR AWXA960196Floor Beam · crackedPAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FLOOR BEAM BS 669, LBL 25, WL 205. REPLACED CHANNEL PER SB 727-57-1139. (M)SDR CA960423107Pump · inoperative(CAN)LOST CONTROL OF POWER SETTINGS ON #1 ENGINE DURING DESCENT, SHUTDOWN BEFORE LANDING. #1 FCU REPLACED, NO CHANGE. ORIGINAL FCU REINSTALLED WITH A NEW FUEL PUMP, OPERATION NORMAL.
Back to Boeing 737-275