Boeing 737-705
Service difficulty reports · 449
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 = '737705' 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 = '737705' 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 SWAA2012073006305Battery · failedCENTER RIGHT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.SDR SWAA2012073006304Battery · failedAFT RIGHT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.SDR SWAA2012073006303Battery · failedAFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.SDR SWAA2012073006302Battery · failedFORWARD LEFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.SDR SWAA2012073006301Battery Pack · failedFORWARD RIGHT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL CAPACITY TEST. REMOVED AND REPLACED BATTERY PER AMM.SDR SWAA2012062105116Fseu · faultyDECLARED EMERGENCY -- LEADING EDGE TRANSIT LIGHT REMAINED ILLUMINATED WHEN FLAP 5 SELECTED. NO LEADING EDGE DEVICES INDICATED ANY EXTENSION. REPLACED LEADING EDGE FLAP AND SLAT HYD FUSE EXTEND AND FSEU PER MM.SDR SWAA2012061805046Skin · crackedRIGHT HORIZONTAL STABILIZER, LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN IAW PER SRM.SDR SWAA2012061104782Slide · out of positionR1 DOOR EMERGENCY EVAC SLIDE IN ADVERTANTLY FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MT.SDR SWAA2012040502833Light · inoperativeSIDEWALL LIGHT ABOVE RT OVERWING EXIT INOP. RELAMPED LIGHT ABOVE RT OVERWING EXIT PER MM.SDR SWAA2012032202477Light · inoperativeRT EMERGENCY EXIT OVERHEAD LIGHT INOP AT ROW 5. RELAMPED LIGHT PER MM.SDR SWAA2012031302132Slide · looseR2 DOOR EMERGENCY ESCAPE SLIDE LOOSE. SECURED SLIDE PER MT.SDR SWAA2012030501876Skin · puncturedRT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2012022001542Lamp · inoperativeFORWARD ENTRY EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT PER MM.SDR SWAA20111208481Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR ASMF201109011Motor · damagedACFT RETURNED, DURING CLIMB, THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MX PERSONNEL PERFORMED THE FIM 27-41-00, TASK 804 PROCEDURE, NOT CONFIRMING THE FAILURE. AS PRECAUTIONARY ACTION, THE STAB TRIM MOTOR WAS REPLACED IAW MM 27-41-71, TESTED CORRECT.SDR SWAA2012080806578Slide · out of adjustL1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER M/M.SDR SWAA115457Slide · out of adjustL1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.SDR SWAA2012080806579Slide · out of adjustR2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSED SLIDE PER MT.SDR SWAA115066Slide · out of adjustR2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.SDR ASMF201107004Skin · dentedDURING TRANSIT CHECK, MX DETECTED ONE DENT IN THE RT HORIZ STABILIZER L/E AT STATION 233.30 OF 5.50 X 2.00 INCHES WITH 0.208 INCH DEPTH. INSPECTION PERSONNEL CONFIRMED THAT THE DENT WAS WITHIN LIMITS IAW SRM 55-10-01 ALLOWABLE DAMAGE 1 PAGE 106, SO IT WAS TEMSDR ASMF201107003Windshield Wiper · damagedACFT PERFORMED AN UNSCHEDULED LANDING, BOTH WINDSHIELD WIPER BLADE OUT OF SERVICE AND RAIN EXCESSIVE. DURING MX REVISION, THE BLADES WERE DAMAGED IAW MM 30-42-11, DISPATCHING THE ACFT IN THIS CONDITION DUE TO RAIN STOP. THE OVERWEIGHT INSP WAS PERFORMED IAW MSDR ASMF201105014Girt Bar · misinstalledDURING ARRIVING TO PLATFORM, THE LT R1 DOOR WAS ARMED WHEN THE CATERER REALIZED TENSION ON THE DOOR AND IT DID NOT OPEN. MX TOOK OUT THE GIRT BAR AND IT WAS REINSTALLED BACK ON THE DOOR IAW MM 25-00-00, ALL CORRECT.SDR ASMF201105010Seal · damagedDURING TRANSIT CHECK, TECH PERSONNEL ADDED 10 QTS OF OIL IN THE RT ENGINE AND ARRIVED WITH AN OIL LEAK OF 4 QTS. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A REVISION, DETECTING OIL LEAK IN THE IDG DRAIN SEAL. THE RT ENGINE IDG MAGNETIC SEAL WAS SDR ASMF201105007Shutoff Valve · inoperativeDURING FUELING, A FUEL SPILLAGE IN THE LT TANK VENTILATION OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE PREVIOUSLY DEFERRED. THE PLATFORM WAS CLEANED BY FIREMEN AND MX CLOSED THE VALVE MANUALLY, FUELING CONTINUED AND IT PERFORMED FUEL TRANSFERENCE IAW MM 12SDR ASMF201105004Shutoff Valve · failedDURING FUELING A FUEL SPILLAGE IN THE LT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN AND MX CLOSE THE VALVE MANUALLY AND FUELING CONTINUED; SO THE FUELING SHUTOFF VALVE SYS WAS VERIFIED IAW 28-13-00, ALL CORRECT. SDR SWAA113331Lens · looseFWD ENTRY EMERGENCY EXIT LIGHT LENS COVER BASE. REMOVED AND REPLACED LIGHT ASSY PER M/M.SDR ASMF201105002Pump · damagedCAPTAIN REPORTED THAT BEFORE ENGINES WERE STARTED, WHEN SWITCH TURNED ON, THE LT CTR FUEL PUMP LOW PRESSURE LIGHT TURNED ON. AFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE LT CTR FUEL PUMP IAW MM 28-22-41, TESTED CORRECT.SDR SWAA113002Battery Pack · failedDURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.SDR SWAA113001Battery Pack · failedDURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.SDR ASMF201104001Seal · damagedDURING TRANSIT CHECK, TECH PERSONNEL DETECTED A MAIN RT WHEEL WELL HYD LEAK; SO THE RT ACMP SEAL WAS REPLACED IAW MM 29-11-21, TESTED CORRECT.SDR ASMF201103003Packing · damagedDURING RT ENGINE START, SMOKE WAS DETECTED AROUND COWLING AND MX PERSONNEL PERFORMED A REVISION DETECTING HYDRAULIC LEAK IN THE COUPLING OF STARTER WITH GEARBOX; SO THE PREFORMED PACKING BETWEEN STARTER AND GEARBOX WERE REPLACED IAW MM 80-11-02, TESTED CORRECTSDR ASMF201103001Motor · damagedCAPTAIN REPORTED THAT DURING CRUISE THE STAB OUT OF TRIM LIGHT TURNED ON MOMENTARY, LATER DURING DESCENT IT CAME ON STEADY, HAVING THE ELECTRICAL MOTOR ACTUATOR OUT OF SERVICE AND SPEED TRIM FAIL LIGHT TURNED ON, AFTER LANDING, RT REVERSER LIGHT TURNED ON. MXSDR ASMF201102002Valve · malfunctionedDURING FUELING, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO THE SUPPLY VALVE DID NOT CLOSE. MX PERFORMED RESEATED AND SUPPLY VALVE TEST IAW MM 28-21-00, ALL CORRECT. ADDITIONALLY, DURING TOWING, THE TOW FITTING WAS BROKEN; SO MX PERFORMED GENERAL VISDR ASMF201012006Filter · obstructedACFT RETURNED TO PLATFORM DUE TO AFTER ENGINES WERE STARTED, THE RT ENGINE "OIL FILTER BY PASS" LIGHT TURNED ON. MX PERSONNEL PERFORMED THE FIM 73-05, TASK 801CONFIRMING THE FAILURE; SO RT ENGINE FILTER AND ALARM WERE REPLACED THE IAW MM 73-11-02 AND MM 73-34SDR ASMF201012004Sensor · damagedACFT RETURNED OF FLIGHT DUE TO DURING CRUISE AT 38,000 FEET, THE L/E FLAPS TRANSIT LIGHT AND L/E DEVICES LIGHT TURNED ON, SO THE FLIGHT CREW PERFORMED THE QRH 9.12 PROCEDURE LANDING WITH NO ADDITIONAL PROBLEMS. ACFT WAS SENT TO THE HANGAR AND DURING MX REVISIOSDR ASMF201012002Shutoff Valve · leakingDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN RT FUELING SHUTOFF VALVE; SO MX CLOSED THE VALVE. MX REPLACED THE RT FUELING SHUTOFF VALVE IAW MM 28-21-51-000-801 AND 28-21-00-700-801, TESTED CORRECT.SDR ASMF201012001Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 532DB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT.SDR ASMF201011002Pressure Switch · damagedCAPTAIN REPORTED THAT AFTER RT ENGINE START, THE FILTER BYPASS LIGHT TURNED ON; SO THE FLIGHT CREW PERFORMED THE QRH 12.8 PROCEDURE, CONFIRMING THE FAILURE RETURNING TO THE GATE. DURING MX REVISION, THE MESSAGE 73-31072 SHOWED; SO THE REPORT WAS DEFERRED IAW MSDR ASMF201011001Access Panel · crackedDURING TRANSIT CHECK, TECH PERSONNEL DETECTED A FUEL LEAK IN RT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 632EB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT.SDR ASMF201010006Actuator · leakingCAPTAIN REPORTED THAT DURING CRUISE AND DESCENT, THE CONTROL COLUMN WITH AFT AND FWD MOVEMENT ABOUT 2 INCHES. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A CONTROL COLUMN POWER FORCE TEST AND ELEVATOR MECHANISM CONDITION INSP IAW 27-31-00; ELEVATOR PITOT SYS SDR ASMF201010005Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 532FB. ACFT WAS SENT TO THE HANGAR; SUCH PANEL WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT. AFTER DURING OVERSDR ASMF20101001Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 532DB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT. AFTER DURING OVERNIGHT CHECK WAS DETECTED A FUEL LEAKSDR ASMF201009010Transmitter · damagedDURING APPROACH, THE T/E FLAPS ASYMMETRY LIGHT TURNED ON WHEN FLIGHT CREW SELECTED FLAPS 5 GRADE, DISCONNECTING THE YAW DAMPER; SO THE FLIGHT CREW PERFORMED THE QRH 9.28 AND 9.40 PROCEDURES, LANDING WITH T/E FLAPS UP. DURING MX REVISION, THE FIM PROCEDURES 27-SDR ASMF201009008Seal · out of positionACFT RETURNED, DURING TAKEOFF AND INITIAL CLIMB, A FUEL LEAK WAS FOUND ON RT WING. MX PERFORMED FUSELAGE AND WING INSP DETECTING FUEL LEAK ON RT LOWER WING DUE TO THE SEAL OF THE FUEL TANK ACCESS DOOR PANEL, NR 533BB, WAS FOUND OUT OF POSITION, SO IT WAS REPLASDR ASMF201009006Valve · damagedDURING APPROACH, THE T/E FLAPS ASYMMETRY LIGHT WAS SHOWN WHEN FLIGHT CREW SELECTED FLAPS 1 GRADE, DISCONNECTING THE YAW DAMPER, SO THE FLIGHT CREW PERFORMED THE QRH 9.28 AND 9.40 PROCEDURES, LANDING WITH T/E FLAPS UP AND REFERENCE SPEED OF 161 KNOTS AND MAXIM SDR Z6WR0052010Ring · wornREFERENCE SERVICE BULLETIN 737-78-1072, 20MAR2002, REV 00. THE 315A2222-5 CASCADE RING ASSEMBLY IS WORN AND HAS MATERIAL MISSING MEASURING 1.15 INBOARD / OTDB X .16 FWD / AFT X .0085 DEEP ON THE LOWER END FROM CONTACT WITH THE 315A2563-7 LOWER ATTACH FITTING.SDR SWAA105066Floorbeam · corrodedDURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 328, BETWEEN RBL 13 TO RBL 55. REPAIRED T-CAP PER SRM.SDR SWAA105065Floorbeam · corrodedDURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER T-CAP CORRODED AT BS 328, LBL 9. REPAIRED T-CAP PER SRM.SDR SWAA104997Flap · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.SDR SWAA104944Support Angle · crackedDURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED ANGLE PER SRM.
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