Boeing 727-2M7
Service difficulty reports · 459
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 = '7272M7' 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 = '7272M7' 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 K11A2024010300249Unknown · unknownCOCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE IN TEST.SDR K11A2023092900230Hinge · crackedMAIN DECK CARGO DOOR UPPER HINGE AT STA 638 - 642 FOUND TO BE CRACKED.SDR K11A2022120600171Beam · corrodedR/H HORIZONTAL STABILIZER - HORIZONTAL TRAILING EDGE BEAM @ APPOX # 3 HINGE LOCATION HAS EVIDENCE OF CORROSIONSDR K11A2021093000081Light · noneEMERGENCY EXIT LIGHT VERY DIM. CORRECTIVE ACTION: R&R EMERGENCY EXIT LIGHT IAW B727 AMM 33-50-92 OPS CHECK GOOD NO DEFECTS NOTEDSDR K11A2021081900066Shutoff Valve · failedLEFT PACK UNABLE TO MAINTAIN CABIN PRESSURE ABOVE 10000 FEET. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND LEFT PACK SHUTOFF VALVE CLOSED, R&R LEFT PACK SHUTOFF VALVE IAW B727 AMM 21-55-71, VERIFIED CORRECT OPERATION, LEAK CHECK GOODSDR K11A2020121800034Circuit Breaker · trippedON TAKEOFF NR 1 EPR INOPERABLE, REJECTED TAKEOFF. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: RESET NR 1 EPR CIRCUIT BREAKER, IAW B727 AMM 20-60-06. OPERATIONS CHECK GOOD, IAW B727 AMM 77-11-00.SDR K11A2020112400028Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 950C-950D.SDR K11A2020112400027Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 850-870 LEFT.SDR K11A2020112400032Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 950F-970 LEFT.SDR K11A2020112400031Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 950D-950E LEFT.SDR K11A2020112400029Window Frame · corrodedEXTERNAL WINDOW FRAME CORROSION STA 970-990 RIGHT.SDR K11A2020112400030Skin · corrodedCORROSION NEXT TO FUEL FILL PORT RIGHT WING UPPER EXTERIOR SURFACE.SDR K11A2020111900026Skin · corrodedCORROSION NEXT TO FUEL FILL PORT WBL 312 LEFT WING UPPER EXTERIOR SURFACE FWD OF NR 4 SPOILER.SDR K11A2020110500025Seat Track · damagedF/E SEAT TRACK ADJUST LOCK PIN HOLES ARE ELONGATED.SDR K11A2020110400024Panel · crackedLT FWD OVERWING HATCH INNER LOWER PANEL CRACKED.SDR K11A2020103000023Seat Track · corrodedSEAT TRACK CORROSION AT STA 588 RBL 40.SDR K11A2020081400008Fcu · fluctuatesAFTER TAKEOFF AND AT 70 % THE NUMBER 3 ENGINE SURGED WITH THE FUEL FLOW AND EGT INDICATIONS ALL FLUCTUATING. REMOVED AND REPLACED FUEL CONTROL IAW JT8 MAINTENANCE MANUAL 73-21-01, PERFORMED LEAK CHECK, TRIM CHECK AND ACCEL / DECAL CHECKS IAW B727 AMM 72-00-00SDR K11A2019070872605Frame · corrodedCORROSION ON FRAME.SDR K11A2019070872604Window Frame · corrodedCORROSION ON UPPER EDGE OF LT WINDOW BLANK FRAME.SDR K11A2019070872602Stiffener · corrodedCORROSION ON RIGHT WING TRAILING EDGE.SDR K11A2019070872601Stiffener · corrodedCORROSION ON FWD BULKHEAD STIFFENER.SDR K11A2019070872603Frame · corrodedCORROSION ON LT SIDEWALL AFT PIT.SDR K11A2018110872602Structure · crackedCRACK IN UPPER FWD END OF MAIN CARGO DOOR STA 480 ADJACENT TO FWD MCD ACTUATOR LINK RODSDR K11A2018110862601Structure · crackedCRACK IN UPPER AFT END OF MAIN CARGO DOOR STA 617 ADJACENT TO AFT MCD ACTUATOR LINK RODSDR K11A2018072650808Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RTSIDE ACFT STA 610.SDR K11A2018072650807Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 590.SDR K11A2018050872605Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME LT SIDE ACFT STA 1080.SDR K11A2018050872604Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 880.SDR K11A2018050872603Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 740.SDR K11A2018050872602Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 570-610.SDR K11A2018050872601Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 510-530.SDR K11A2018030972601Controller · malfunctionedTHE AIRCRAFT EXPERIENCED A FAILURE OF THE AUTO & STANDBY PRESSURIZATION SYSTEMS AT FL350. THE CABIN ALTITUDE WARNING ACTIVATED. THE PILOT INSTRUCTED THAT OXYGEN MASKS. THE CABIN ALTITUDE CONTINUED TO CLIMB PASSED 10,000 FT. DECENDED TO 9000 FT MSL, CHECKED MANSDR K11A2018010972601Warning Light · illuminatedDURING CRUISE FLIGHT, ENGINEER INFORMED CAPTAIN THAT THE HYDRAULIC SYS B LOW PRESSURE LIGHTS ILLUMINATED SIMULTANEOUSLY, FOLLOWED THE APPROPRIATE CHECKLIST. AND LANDED.SDR K11A2017093072602Warning Light · illuminatedABORTED TAKEOFF BECAUSE OF AMBER LEADING EDGE FLAP LIGHT.SDR K11A2017093072601Warning Light · illuminatedAT ROTATION, RECEIVED AN AMBER LEADING FLAP LIGHT.SDR K11A2016082272601Stiffener · corrodedRIGHT WING HAS CORRODED STIFFENER ON FRONT SPAR STA 388.SDR K11A2015120172602Spar · corrodedRIGHT WING REAR SPAR UPPER CHORD CORROSION, WING SPAR 403.SDR K11A2015120172604Skin · corrodedRIGHT HORIZONTAL STABILIZER T/E EXTERNAL SURFACE CORROSION BS 98-102.SDR K11A2015110472605Spar · damagedRIGHT WING REAR SPAR UPPER CHORD HAS 3 DAMAGED FASTENER HOLES WING BS 399, 401, 413.SDR K11A2015120172603Floorbeam · corrodedFLOORBEAM UPPER FWD FLANGE HAS CORROSION BS 344, RBL 24.SDR K11A2015120172601Web · corrodedCORROSION UPPER SURFACE OF HORIZONTAL WEB IN VERTICAL STABILIZER MAIN BOX BS 1337-1342.SDR K11A2015110472604Doubler · corrodedVERTICAL STAB MAIN BOX,HORIZONTAL WEB, EXISTING DOUBLER FWD OF REAR SPAR BULKHEAD BS 1337-1342 HAS CORROSION.SDR K11A2015110472603Web · crackedVERTICAL WEB HAS EVEDENCE OF A CRACK AT OTBD LOWER CORNER.SDR K11A2015110472601Torque Box · crackedACCESS HOLE RT INBD SIDE OF TORQUE BOX CRACKED.SDR K11A201511047261Frame · crackedBULKHEAD IN VERTICAL STAB MAIN BOX HAS TWO INCH CRACK IN AFT END OF RT LOWER TEE CHORD.SDR K11A2015061572601Spar · crackedRIGHT ELEVATOR REAR SPAR STIFFNER ASSY CRACKED.SDR K11A2015060872601Compass · precessesNR 2 COMPASS PRECESSED 30 DEGREES, RETURN TO DEPARTURE.SDR K11A2015031972601Line · crackedON SHORT FINAL, "B" SYSTEM HYD QUANTITY DROPPED RAPIDLY AND "B" SYS PRESSURE WENT TO ZERO.SDR K11A2014122200001Shaft · shearedFUEL PUMP DRIVE GEAR SHAFT SHEARED, CAUSING ENGINE TO FLAME OUT.SDR K11A2014093072601Actuator · leakingDURING CLIMB, AFTER RETRACTING FLAPS, THE AMBER L/E FLAPS LIGHT FAILED TO EXTINGUISH. F/E REPORTED NR 2 SLAT OUT OF POSITION. F/O REPORTED AIRCRAFT PULLED HARD RIGHT. MADE CONTACT WITH ATC TO RETURN TO DEPARTURE, ATC CLEARED TO RETURN BACK AND BEFORE GEAR EX
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