Boeing 737-752
Service difficulty reports · 2,590
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 = '737752' 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 = '737752' 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 SWAA2015021736655Pressure Panel · crackedWHEEL WELL WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW SRM.SDR SWAA2015012636050Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS 295 TO 312, RBL 16. R & R INTERCOSTAL IAW DWG & SRM.SDR ASMF201501017Starter · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO THE LT ENG NOT STARTED. PERFORMED THE LT ENG START IAW MM 74-00-00 & ENG LEAKING INSPECTION IAW MM 73-21-00, DETECTING THE STARTER DAMAGED. THE STARTER WAS REPLACED IAW AMM 80-11-01, TESTED CORRECT.SDR ASMF201501013Circuit Breaker · poppedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE PSEU LIGHT TURNED ON & EICAS MSG NO VSPD & LDG ALT. PERFORMED BITE TO PSEU IAW FIM 32-09 TASK 801 PROCEDURE, SHOWING FAILURE CODE 29-22001 & LEGEND ENG RUN LT, DETECTING THE CB P18-2 B-3 POPPED. CB`S P1SDR EE4Y201411060266Beam · crackedDURING THE STRUCTURE INSPECTION WAS FOUND THE FORWARD GALLEY DOOR BEAM NR 4 WITH A CRACK AT THE WEB.SDR EE4Y201411060265Angle · crackedNR 1 ENGINE FAN COWL RT INNER OIL SERVICE DOOR WITH ANGLE CRACKED.SDR ASMF201501010Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO TAKEOFF CONFIGURATION ALARM WAS ACTIVE. PERFORMED TAKEOFF WARNING SYS TEST IAW AMM 31-51-00-730-803 NOT SHOWING FAILURE CODE & THE FIM 31-51 TASK 801 WAS PERFORMED, NO FAILURE WAS FOUND. HIGH ENERGY STOP INSPECTION WAS PESDR SCNA20141104167Rib · crackedRIGHT HORIZONTAL STABILIZER, RIB NR 7 HAS 3 CRACKS. REPAIRED.SDR SCNA20141103156Frame · corrodedFRAME BS 986 RBL 6 ON UPPER SURFACE CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED FRAME.SDR SCNA20141103157Cargo Track · crackedAFT CARGO BAY, CARGO TRACK CRACKED AT BS 727E. REMOVED DAMAGED CARGO TRACK BS 727 - 887 AND INSTALLED NEW.SDR SCNA20141103164Support Angle · corrodedGALLEY WALL SUPPORT Z-ANGLE BETWEEN THE LT AFT GALLEY MOUNTS CORRODED AT AFT END. REMOVED CORROSION AND REMAINING THICKNESS IS OUT OF LIMITS. R & R WALL SUPPORT.SDR SCNA20141103163Support Angle · corrodedGALLEY WALL SUPPORT Z-ANGLE BETWEEN THE RT AFT GALLEY MOUNTS CORRODED AT BOTH ENDS. REMOVED CORROSION AND REMAINING THICKNESS IS OUT OF LIMITS. R & R WALL SUPPORT.SDR SCNA20141104166Window Frame · crackedLEFT NR 3 WINDOW FRAME CRACKED. REPAIRED WITH DOUBLER & TRIPLER.SDR SWAA2015012936177Rib · crackedLEFT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 120.30 FWD SPAR LOWER FLANGE. REPAIRED RIB IAW EA & ER.SDR SWAA2014110533767Rib · crackedLEFT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 92.7 3RD STIFFENER AFT OF FWD SPAR. REPAIRED RIB IAW SRM.SDR SCNA20141103162Strap · corrodedFWD WET AREA MOP SILL VERTICAL LEG SPLICE STRAP IS CORRODED. CORROSION BEYOND LIMITS. INSTALLED NEW SPLICE STRAP.SDR SCNA20141103161Light · brokenG-1 GALLEY EMERGENCY EXIT LIGHT BROKEN. R & R G1 GALLEY EMERGENCY EXIT LIGHT.SDR SCNA20141103160Floor Support · crackedFLOOR SUPPORT CRACKED AT FORWARD WET AREA BETWEEN BS 328 - 344 LBL 48. R & R THE FLOOR SUPPORT.SDR SCNA20141103159Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN BS 277 - 294.5, BL 0. R & R THE FLOOR SUPPORT.SDR SCNA20141103158Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN BS 312 - 328, RBL 32. R & R THE FLOOR SUPPORT.SDR SCNA20141103165Vapor Barrier · crackedFOUND AN 18 INCH CRACK IN LT VAPOR BARRIER BAY 7 BETWEEN LBL 31.83 AND LBL 45.64. REPAIRED THE VAPOR BARRIER.SDR ASMF201501006Skin · dentedDURING TRANSIT CHECK, DETECTED A BIRD STRIKE IN THE RT HORIZONTAL STABILIZER LE. A BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW AMM 05-51-18 DETECTING A DENT 8.5 INCHES IN LENGTH, 3 INCHES IN WIDTH & 0.391 INCHES IN DEPTH IN THE LE SKIN OF THE RT HORISDR ASMF201409014Skin · dentedDURING TRANSIT CHECK, DETECTED A BIRD STRIKE IN THE RT HORIZONTAL STABILIZER LE. A BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW AMM 05-51-18 DETECTING A DENT 8.5 INCHES IN LENGTH, 3 INCHES IN WIDTH & 0.391 INCHES IN DEPTH IN THE LE SKIN OF THE RT HORISDR ASMF201501005Shutoff Valve · failedAIRCRAFT REJECTED TAKE OFF AT 50 KNOTS, DUE TO BLEED TRIP OFF LIGHT TURNED ON. DEFERRED THE LT ENG PRSOV IAW MEL 36-5-2 CAT C. THE LT ENG PRSOV WAS REPLACED IAW AMM 36-11-04 & HIGH STAGE VLV OF THE LT ENG WAS REPLACED IAW AMM 36-11-06. TESTED CORRECT & THE SDR ASMF201409013Shutoff Valve · failedACFT REJECTED TAKEOFF AT 50 KNOTS, DUE TO BLEED TRIP OFF LIGHT TURNED ON. THE LEFT ENGINE PRSOV WAS REPLACED IAW AMM 36-11-04 AND HIGH STAGE VALVE IAW AMM 36-11-06, ENGINE 001, TESTED CORRECT AND THE REPORT WAS CLOSED. THE HIGH ENERGY STOP INSPECTION WAS NOSDR ASMF201501004Unknown · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO, AFTER RT ENG START THE LT ENG WAS 44% AT N2 & EGT INDICATOR FLASHING. CHECKED THE PRSOV IAW FIM 36-10 TASK 803 PROCEDURE, NO CONFIRMING FAILURE.SDR SCNA20141006136Skin · crackedFOUND CRACK ON LT HORIZONTAL STABILIZER LOWER SKIN AT L/E STA 138 AT AFT SPAR. REPAIRED THE SKIN.SDR ASMF201409012Warning System · activatedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF PSEU LIGHT TURNED ON AFTER ENGS STARTED. PERFORMED FIM 78-31-00 CORRECTING FAILURE.SDR ASMF201409008Mechanism · lack of lubeAIRCRAFT REJECTED TAKE OFF AT 60 KNOTS, DUE TO CONFIGURATION ALARM WAS SHOWED. PERFORMED BITE TO PSEU IAW AMM 32-09-10, DETECTING THE SPOILER LEVER FAILED. THE SPOILER LEVER MECHANISM WAS LUBRICATED & ADJUSTED IAW AMM 27-60-00 & THE FIM 27-67 TASK 807-808 WASDR ASMF201409006Window · crackedCAPTAIN REPORTED LT WINDOW NR 1 CRACKED. ACFT WAS SENT TO THE HANGAR, REPLACED THE LT WINDOW NR 1 IAW AMM 56-11-31, TESTED CORRECT.SDR ASMF201409004Transceiver · failedCAPTAIN REPORTED THAT DURING CRUISE, THE WXR FAIL ON BOTH SIDES LIGHT TURNED ON WITH INTERMITTENT FAULT. PERFORMED REVISION DETECTING THE RADAR FAILED, SO THE WEATHER RADAR & WEATHER RADAR SINGLE MOUNT WERE REPLACED IAW AMM 34-43-41 & AMM 34-43-31, TESTED CORRSDR ASMF201409003Transceiver · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MSGS. PWS FAIL & WXR FAIL. PERFORMED REVISION DETECTING THE TRANSCEIVER FAILED, SO THE WEATHER RADAR TRANSCEIVER & WEATHER RADAR SINGLE MOUNT WERE REPLACED IAW AMM 34-43-41 & AMM 34-43-31, TESTED CORRECTSDR ASMF201409002Window · openAIRCRAFT REJECTED TAKE OFF AT 40 KNOTS, DUE TO FIRST OFFICIAL WINDOW OPENING. PERFORMED TO LT NR 2 THE OPENABLE WINDOW OPERATIONAL CHECK IAW AMM 56-12-11-720-803 & OPENABLE WINDOW FUNCTIONAL CHECK IAW AMM 56-12-11-720-801, ALL CORRECT. THE HIGH ENERGY STOP ISDR ASMF2014061806018Unknown · vibrationCAPTAIN REPORTED THAT DURING TAKEOFF AT ROTATION SPEED, A VIBRATION WAS FELT IN THE NLG. PERFORMED A NLG REVISION IAW MM 32-00-00, NO FAILURES DETECTED. AS A PRECAUTIONARY ACTION, BOTH NLG WHEELS WERE REPLACED IAW AMM 32-45-21, ALL CORRECT.SDR ASMF2014061806016Warning System · false activationAIRCRAFT REJECTED TAKEOFF AT 65 KNOTS WITH 63,600 KG WEIGHT, DUE TO CONFIGURATION ALARM WAS SHOWED. PERFORMED TAKEOFF WARNING SYS TEST IAW AMM 31-51-00-730-803 & FIM 27-81 TASK 811 PROCEDURE, SHOWING FAILURE CODE 31-55008. THE CB P6-3, C-18 & D18 WERE REESTASDR ASMF2014061706014Pump · leakingDURING OVERNIGHT CHECK, A FUEL LEAK WAS DETECTED IN RT ENG FUEL PUMP OF 40 DROPS PER MINUTE. THE FUEL PUMP WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT.SDR ASMF2014061706009Windshield · abnormalDURING TRANSIT CHECK, IT WAS DETECTED SCRATCHES IN BOTH COCKPIT WINDSHIELD. PERFORMED REVISION DETECTING SCRATCHES OUT OF LIMITS SO BOTH COCKPIT WINDSHIELDS WERE REPLACED IAW AMM 56-11-21, TESTED CORRECT.SDR EE4Y2011041900107Skin · crackedDURING THE STRUCTURE INSPECTION COO FOUND THE LT HORIZONTAL STABILIZER LOWER SKIN WITH CRACKS AT STATION 129.5 & STATION 138.7. THE DAMAGED PART WAS REPAIRED IAW REPAIR INTRUSION SRM 55-10-01 REPAIR 11.SDR EE4Y2011041900106Skin · crackedDURING THE CURRENT MAINTENANCE CHECK, WE FOUND LE SLAT 3 & 6 WITH SKIN CRACKED AT NOSE ACTUATOR RIB. THE DAMAGED PART WAS REPAIRED IAW REPAIR INTRUSION & ITEM A1C106 JOB 2 - 11.SDR ASMF2014061706003Blade · lack of lubeCAPTAIN REPORTED THAT DURING CRUISE, BOTH ENGS VIBRATION REACHED 3.2 & 3.6 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED LUBRICATION OF THE FAN ROTOR BLADE OF THE RT ENG IAW AMM 72-21-00 & FAN TRIM BALANCE TEST 14B IAW AMM 71-00-00, BEING WITHIN LIMITS.SDR ASMF201406002Bonding Jumper · defectiveAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, BOTH FAIL FLAGS NAV CONTROL DISPLAYS WERE SHOWN. PERFORMED RESET TO RUPTURES P18-1 A-3 & P6-1 A-15 IAW FIM 34-51 TASK 812, NO FAILURES WERE FOUND. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO THE ACFT LASDR EE4Y201403290055Skin Panel · crackedLOWER FUSELAGE AT BS 540 BETWEEN STRINGER 22 RT & 23 RT EXTERNAL SKIN WITH TWO EACH CRACKS COMMON TO FASTENER HOLES. DETECTED WITH HFEC INSPECTION.SDR EE4Y2014042200058Skin · dentedRIGHT WING NR 7 SLAT TE UPPER SKIN WITH DENTS. THE SLAT WAS REPAIRED MSG COO-AMX-14-0011-02B & DOCUMENT IN EO COO-3-57-064-14, UNDER THE NON-ROUTINE.SDR EE4Y2014042200057Skin · dentedRT WING NR 6 SLAT TE UPPER SKIN WITH DENTS. THE SLAT WAS REPAIRED MSG COO-AMX-14-0010-02B & DOCUMENTED IN EO COO-3-57-063-14, UNDER THE NON-ROUTINE.SDR ASMF201403017Starter · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START SMOKE WAS DETECTED IN THE RT ENG. PERFORMED RT ENGINE LEAKING INSPECTION IAW MM 72-00-00 DETECTING THE STARTER DAMAGED, SO THE RT STARTER WAS REPLACED IAW MM 80-11-01, TESTED CORRECT.SDR ASMF201403014Unknown · leakingDURING RT ENGINE START, A FUEL LEAK WAS DETECTED & THE RT ENGINE CONTROL LIGHT TURNED ON WITH INDICATION OF EGT LOW. AIRCRAFT RETURNED TO PLATFORM. PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE DRAIN PORT. THE RT ENGINE WAS MOTORING, ASDR ASMF201403013Engine · failedCAPTAIN REPORTED THAT DURING LANDING, THE RT ENGINE PRESENTED LOW OIL QTY, SO FLIGHT CREW IMMEDIATELY PERFORMED THE RT ENGINE SHUTDOWN & ACCOMPLISHED THE QRH 7.21 PROCEDURE. REPLACED THE RT ENGINE IAW MM 71-00-02 & OPS TEST WAS PERFORMED IAW MM 71-00-00, TESTSDR ASMF201403012Indication Sys · faultyAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO DUE TO DURING CRUISE, THE RT ENG PRESENTED LOW OIL QTY INDICATION. FLIGHT CREW ACCOMPLISHED THE QRH 7.21 PROCEDURE. AT HMO PERFORMED RT ENG LEAK CHECK IAW AMM 71-00-00, FIM 79-05 TASK 808 PROCEDURE & OPERATIONSDR EE4Y2014041500054Seat Track · crackedDURING THE ACCOMPLISHMENT OF AD2013-23-04 & SB 737-53-1296 NDT INSPECTION WAS FOUND THE THE BS 727B, RBL 24.75 SEAT TRACK OTBD & INBD HORIZONTAL FLANGES CRACKED. THE DAMAGED PART WAS REPAIRED IAW COO-AMX-14-0006-02B R1 & DOCUMENTED IN COOPESA EO COO-3-53-036-1SDR EE4Y2014032700054Seat Track · crackedPAX CABIN, BS 727B, RBL 24.75 SEAT TRACK CRACKED. THE CRACK WAS REPAIRED IAW COO-AMX-14-0006-02B.
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