Boeing 737-2L9
Service difficulty reports · 593
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 = '7372L9' 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 = '7372L9' 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 CA010924005Computer · failed(CAN) ON CLIMB OUT AUTO PILOT DISENGAGED, TCAS, GROUND PROXIMITY, MACH TRIM, ALTITUDE ALERT, TOTAL AIR TEMPERATURE AND ENGINE PRESSURE RATIO GAUGES FAILED. CENTRAL AIR DATA COMPUTER (CADC) RESET BUT DID NOT FIX PROBLEM AIRCRAFT RETURNED TO YYZ. CADC REPLACED ASDR F3LA200100101Control Cable · brokenON WALKAROUND PRIOR TO FLIGHT, MAINTENANCE REPORTED LT SPOILER CABLE BROKEN. FABRICATED AND INSTALLED REPLACEMENT SPOILER CABLE PER MM 27-09-111 AND MM 20-10-91. ADJUSTED AND TESTED SYSTEM PER MM 27-61-00.SDR F3LA200100100B-Nut · looseAIR TURNBACK, FLIGHT CREW REPORTED LOSS OF A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. TIGHTENED NR 1 ENGINE SUPPLY LINE B-NUT, REPLACED NR 1 ENGINE CASE DRAIN FILTER. PERFORMED LEAK CHECK AND OPERATIONAL CHECK AND CHECKED OKAY.SDR F3LA200100099BatteryPRIOR TO DEPARTURE, MAINTENANCE REPORTED OVERHEAD EXIT LOCATOR SIGN FOR OVERWING EMERGENCY EXITS, FIXED EXIT LIGHTS ON SIDE OF EMERGENCY EXITS AND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. FERRIED AIRCRAFT TO DEN. REPLACED BATTERIES, PERFORMED OPERATIONASDR AT0100214Socket · missingFOUND E-PATH LAMP HOLDER ASSEMBLY MISSING AT SEAT ROW 28. REPLACED HOLDER IAW MM 33-21-27.SDR F3LA200100093Web · crackedDURING C-1 CHECK, FLIGHT CREW REPORTED SEVERAL CRACKS FROM RIVET HOLE BEHIND THE 178 BULKHEAD IN THE FLOOR STRUCTURE AT BS 180, WL 207. MAINTENANCE REMOVED CRACKS FROM RIVET HOLE AND INSTALLED REPAIR PARTS PER SRM 51-40-02.SDR 2001F00066Transmitter · inoperativeSJO - FLT 610 - DURING TAKEOFF, THE CAPTAIN REPORTED RADAR INOPERATIVE. THE AIRCRAFT RETURNED TO SJO STATION FOR MAINTENANCE. AFTER LANDING MAINTENANCE PERSONNEL REMOVED AND REPLACED THE WEATHER RADAR TRANSMITTER, ACCORDING TO AMM 34-41-00. PERFORMED OPERATSDR SOK2001F00000Helicoil · faultyCCS - FLT LR611 - DURING LANDING, ENGINE NR 2 WAS SHUTDOWN DUE TO LOSS OF OIL AND LOW OIL PRESSURE LIGHT. AT CCS STATION, FOUND THAT AN OIL PRESSURE FITTING CORRESPONDING TO THE OIL BYPASS PRESSURE SWITCH WAS LEAKING, CHANGED HELICOIL AT THIS FITTING AS PER PSDR F3LA200100056Aileron · delaminatedPRIOR TO DEPARTURE, MAINTENANCE REPORTED OTBD SIDE OF RT AILERON DELAMINATED. REPLACED AILERONS IN LT AND RT POSITIONS PER MM 27-11-11, RIGGED AILERONS, AND PERFORMED OPERATIONAL CHECK PER MM 27-11-11.SDR AT0100106Connector · damagedFOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPAIRED BENT PIN AT BATTERY PACK CONNECTOR IAW 737WDM 33-51-01.SDR CA010322005Line · leaking(CAN) AIRCRAFT WAS CLIMBING THROUGH 8000 FEET WHEN NR 1 A SYSTEM HYDRAULIC PUMP FAILED, FOLLOWED SHORTLY BY THE NR 2 PUMP FAILURE. QUANTITY WAS DECREASING RAPIDLY. AIRCRAFT RETURNED. INSPECTION FOUND A SYSTEM FLEX LINE, LOCATED FORWARD OF L/H GEAR LEAKING. REPSDR F3LA200100042Control Unit · malfunctionedAIR TURNBACK. FLIGHT CREW REPORTED PRESSURIZATION SYSTEM WARNING HORN SOUNDED AT 14000 FT AND OXYGEN MASKS DROPPED. AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM PER MM 21-31-0 AND FOUND NO DISCREPANCSDR F3LA200100040Control Unit · failedPRIOR TO DEPARTURE, FLIGHT CREW REPORTED ALL PASSENGER OXYGEN MASKS DEPLOYED AFTER OXYGEN SYSTEM WAS SERVICED. REPLACED PASSENGER OXYGEN CONTINUOUS FLOW CONTROL UNIT PER MM 35-21-21, RESTOWED OXYGEN MASKS, PERFORMED OPERATIONAL TEST AND LEAK CHECK, AND SYSTEMSDR F3LA200100034Fairing · damagedAIRCRAFT DIVERTED TO GRAND JUNCTION, COLORADO DUE TO WEATHER. UPON WALKAROUND, FLIGHT CREW REPORTED DAMAGE TO RT INBD WING-TO-BODY FAIRING ELEPHANT EAR SCUFF PLATES DAMAGED. AIRCRAFT WAS FERRIED TO DEN FOR REPAIR. MAINTENANCE REPLACED RT INBD WING-TO-BODY FSDR CA010301025Control Unit · leaking(CAN) AT FL350 IN CRUISE, NR 2 B HYDRAULIC PUMP OVERHEAT LIGHT CAME ON. PUMP WAS SELECTED OFF. 30 SECONDS LATER THE NR 1 B HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON. PUMP WAS SELECTED OFF, B HYDRAULIC SYSTEM QUANTITY DROPPED TO 1.2 GALLONS. AIRCRAFT RETURNED WSDR F3LA200100035Indicator · inoperativeFLIGHT CREW REPORTED STICK SHAKER ACTIVATED ON TAKEOFF FOR APPROXIMATELY 3 SECONDS. REPLACED RT TRAILING EDGE FLAP POSITION INDICATOR PER MM 27-58-01.SDR AT0100076Power Supply · dischargedFOUND FORWARD ESCAPE SLIDE LIGHT AT L1 AND R1 FAILED TO ILLUMINATE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY ASSEMBLY IAW B737 MM33-51-71.SDR AT0100073Floorbeam · corrodedFOUND FLOORBEAM AT BS 1016 UPPER FORWARD FLANGE CORRODED. REMOVED, FABRICATED AND INSTALLED REPAIR BEAM IAW REO-L00367 REV D.SDR F3LA200100008Engine · vibrationAIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE VIBRATION ON CLIMBOUT AT 20,000 FT. NR 1 ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO PHX WITHOUT INCIDENT. THE NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. AN ADDENDUM WILL BESDR AT0100052Floorboard · delaminatedFOUND CABIN FLOOR PANEL RBL 45 BS 430 DELAMINATED. REMOVED, FABRICATED, AND INSTALLED REPLACMENT IAW REO L-00363 AND SRM 53-20-1.SDR AT0100053Seat Track · corrodedFOUND SEAT TRACK WAS CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF SEAT TRACK IAW B737 SRM 73-10-5 FIGURE 2, 53-20-1.SDR AT0100071Floor Panel · tornFOUND CABIN FLOOR SKIN TORN AT BS 767 - 827. REMOVED, FABRICATED AND INSTALLED REPAIR PANEL IAW B737 SRM 53-20-1, 53-20-2, 51-10-1 AND BCMM 25-00-66.SDR AT0100070Floor Panel · delaminatedFOUND CABIN FLOOR DELAMINATED AT BS 767 - 727. REMOVED, FABRICATED AND INSTALLED REPAIR PANEL IAW B737 SRM 53-20-1, 53-20-2, 51-10-1, BCMM 25-00-66.SDR AT0100014Floor Support · corrodedFOUND CORRODED FLOOR SUPPORT AT RBL 12 BS 344 - 360. REMOVED, FABRICATED, AND INSTALLED REPAIR IAW B737 SRM 51-40-4.SDR AT0100013Floor Panel · tornFOUND CABIN FLOOR PANEL METAL SKIN TORN, GOUGED, CRACKED, AND PUNCTURED AT SEVERAL PLACES. REMOVED, FABRICATED, AND INSTALLED NEW FLOORBOARD IAW B737 SRM 53-20-1, 53-20-2, 51-10-1, CMM 25-00-66.SDR AT0100012Floor Panel · damagedFOUND CABIN CENTER FLOOR PANEL SPONGY IN SEVERAL PLACES. REMOVED, FABRICATED AND INSTALLED NEW FLOOR PANEL IAW B737 SRM 53-20-1, 51-10-1 AND CMM 25-00-66.SDR F3LA200100005Teleflex Cable · out of adjAIR TURN BACK. FLIGHT CREW REPORTED GEAR HANDLE WOULD NOT MOVE TO "UP" POSITION AFTER TAKEOFF AND LANDING GEAR WARNING HORN WOULD NOT SILENCE AFTER FLAPS WERE RETRACTED. REPLACED LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY PER MM 32-07-100. ADJUSTED GROUND SDR AT0100065R1Seat Track · corrodedFOUND LEFT INBOARD SEAT TRACK CORRODED AT BS 500B-52D. REMOVED AND REPLACED SEAT TRACK IAW B737 SRM 53-10-5 FIGURE 1.SDR AT0100069Seat Track · corrodedFOUND LEFT OUTBOARD SEAT TRACK HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW B737 SRM 53-10-5 FIGURE 1.SDR AT0100057Floor Panel · delaminatedFOUND CABIN FLOOR PANEL AT BS 430 DELAMINATED AND METAL SKIN CRACKED. REMOVED, FABRICATED AND INSTALLED PANEL IAW B737 SRM 53-21-0, 51-40-8, 51-10-1, 53-20-1, 51-10-1, AND REO-L00363.SDR AT0100011Seat Track · corrodedFOUND LEFT IN BOARD SEAT TRACK HAS CORROSION BEYOND LIMITS BS 727. REMOVED AND REPLACED SECTION OF SEAT TRACK IAW B737 SRM 51-30-2, 53-10-5.SDR AT0100075Floorboard · puncturedFOUND FLOORBOARD AT BS 520 - 540 HAS PUNCTURES AND CRACKS ON METAL SKIN. REMOVED, FABRICATED AND INSTALLED REPAIR FLOORBOARD IAW REO-L00363.SDR AT0100074Floorboard · puncturedFOUND FLOORBOARD AT BS 540 - 616 HAS TWO PUNCTURES AND IS MISSING HARDWARE. REMOVED, FABRICATED, AND INSTALLED REPAIR FLOORBOARD IAW REO-00363.SDR AT0100068Structure · corrodedFOUND LAVATORY WALL SUPPORT AT BS 308 CORRODED AT FLANGE. REMOVED CORRODED LAVATORY WALL, FABRICATED AND INSTALLED REPAIR IAW B737 SRM 51-40-4.SDR AT0100061Floor Panel · delaminatedFOUND CABIN FLOOR PANEL IN COCKPIT ENTRY AT BS 295, MUSHY. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL IAW B737 SRM 53-20-2, 53-20-1, 51-10-1 AND CMM 25-00-66 AND REO-L000363IR.SDR F3LA200100004Fire Detector · malfunctionedFLIGHT CREW REPORTED APU FIRE WARNING ILLUMINATED IN FLIGHT FROM PHX TO DEN. THE APU FIRE BOTTLE WAS DISCHARGED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT.AN INSPECTION REVEALED NO SIGNS OF OVERHEATING OR FIRESDR AT0100067Panel · corrodedFOUND SIDE WALL PANEL BEHIND G1 GALLEY IS CORRODED. REMOVED CORROSION, FABRICATED REPLACEMENT PANEL IAW B737 SRM 53-00, 51-40-3, 51-10-2, 51-30-2.SDR AT0100066Skin · corrodedFOUND AT LEFT WHEEL WELL, CORROSION ON CUT OUT SKIN AROUND FASTENERS. FABRICATED DOUBLERS AND INSTALLED IAW B737 SRM 51-10-6, 51-10-2, 51-30-2.SDR AT0100062Panel · crackedFOUND FORWARD PIT CEILING PANEL AT BS 380 - 420 HAS SEVERAL TORN AND CRACKED AREAS. REMOVED, FABRICATED, AND INSTALLED PANEL IAW REO-L00361 REV A.SDR AT0100058Floorboard · tornFOUND CABIN FLOORBOARD AT BS 295 - 360 AFT SIDE WALL METAL SKIN TORN. REMOVED AND REPLACED FLOORBOARD IAW B737 SRM 53-20-2, 51-10-1, CMM25-00-66 AND RE0-L00363IR.SDR AT0100051Skin Panel · gougedFOUND RIGHT ELEVATOR LEADING EDGE GOUGED AT OUTBOARD END FROM OUTBOARD SEAL HARDWARE. REMOVED AND REPLACED LEADING EDGE SECTION, REPLACED SEAL ATTACH FASTENERS IAW TIMCO SERVICE ORDER 151151-23696.SDR AT0100072Floor Support · corrodedFOUND CORROSION IN AFT CARGO PIT AREA ON SUPPORT BEAM AT BS 857. REMOVED CORROSION, FORMED L ANGLE REPAIR, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-30-2, 53-10-1, 51-20-11, 51-40-3.SDR AT0100064Floor Support · corrodedFOUND AFT CARGO PIT AREA WAS CORRODED AT SUPPORT BEAMS AT BS 947 - 987. REMOVED CORROSION, TREATED, PRIMED, FABRICATED AND INSTALLED REPAIR SUPPORT BEAMS IAW B737 SRM 51-21-31, 53-10-9 AND TIMCO SERVICE ORDER 151151-23634.SDR AT0100059Floorbeam · corrodedFOUND AFT CABIN FLOORBEAM CORRODED AT UPPER AND LOWER EDGE AT BS 986. MECHANICALLY REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-10-9, 53-30-2.SDR AT0100050Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM AT BS 294 RBL 15 RBL 50. REMOVED CORROSION, REPLACED SECTION OF UPPER END CAP IAW TIMCO SERVICE ORDER 151151-23626.SDR AT0100049Floorbeam · corrodedFOUND CORROSION ON FLOORBEAMS AT BS 277 - 344. REMOVED CORROSION, TREATED, PRIMED AND REPAIRED FLOOR PANEL IAW B737 SRM 51-10-2, 51-10-6, 53-10-01.SDR AT0100016Floor Support · corrodedFOUND FLOOR SUPPORT FROM BS 984 - 1016 IS CORRODED. REMOVED CORRODED FLOOR SUPPORT AT BS 984 - 1016. FABRICATED AND INSTALLED REPAIRS IAW B737 SRM 51-40-4 AND 51-40-3.SDR AT0100015Seat Track · corrodedFOUND LEFT INBOARD SEAT TRACK HAS SURFACE CORROSION AT BS 344 - 967. REMOVED CORROSION, CHECK LIMITS, TREATED, PRIMED AND REPLACED SECTIONS OF SEAT TRACK IAW B737 SRM 51-10-6, 53-10-1 FIGURE 4.SDR AT0100010Seat Track · corrodedFOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK AT BS 1006. MECHANICALLY REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IAW B737 SRM 53-10-5, 51-30-2, 51-10-2.SDR AT0100063Structure · corrodedFOUND LEFT AFT LAVATORY VANITY SINK CORRODED ABOVE AND BELOW SOAP DISPENSER. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR USING WELDED METHOD IAW TIMCO REO L00727 REV A.
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