Boeing 757-23APF
Service difficulty reports · 96
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 = '75723APF' 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 = '75723APF' 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 22AA200900023Actuator · inoperativeUNABLE TO RAISE LANDING GEAR. REMOVED AND REPLACED 2 EA BRACKETS AT LT M/G ALSO HYD LINE AND MAIN GEAR TRUCK POSITION ACTUATOR IAW MM 32-32-15. JACKING ACFT IAW MM 07-11-01 AND MAIN GEAR EXTENSION AND RETRACTION ADJUSTMENT TEST MM 32-32-00.SDR 22AA200900007Unknown · odorODOR OF ELECTRICAL FUMES FROM UNKNOWN SOURCE. UNABLE TO ISOLATE. VISUAL INSPECTED WIRE BUNDLES & TERMINALS, BLOCK IN FWD E/E. NO FUMES BURNED OR CHAFING NOTED. INSPECTED STALL INVERTER. BATTERY CHARGER, WX RADAR TRANCEIVER FOR SIGNS OF BURN, NO FAULTS NOTESDR 22AA200900008Connector · burnedDURING DESCENT, HAD MOMENTARILY ELEC ODOR LASTING NO LONGER THAN 30 SECONDS. NO SMOKE OBSERVED. REMOVED AND REPLACED TERMINAL CONNECTORS D3324 AND D3326 FROM WINDOW HEAT TOTB5028 IAW W/D 30-41-11 AND MAN 20-30-00. GROUND TEST NORMAL IAW MM 30-42-00. WIRINGSDR 22AA200900006Unknown · odorFUMES FROM UNIDENTIFIABLE SOURCE ON FLIGHT. MADE EMERGENCY LANDING. INSPECTED AIR RECIRCULATION FAN IAW MM 21-05-01, FAULTS FOUND. INSPECTED E/E/ EQUIPMENT COOLING FANS EXHAUST FAN, NO FAULTS NOTED. ACCOMPLISHED MAINT PROCEDURES FOR FUMES IN COCKPIT IAW MMSDR DU4R2009319Attach Angle · corrodedDURING SCHEDULED INSPECTION, FOUND MAJOR EXFOLIATED CORROSION ON ATTACH ANGLES ( 4 EA.) ATTACHED TO STRINGERS FOR APU INLET DOORS PLENUM ASSY MOUNTED ABOVE (THS) HORIZ STAB CENTER BOX AT FS 1787.4 - 1825.SDR DU4R2009310Angle · corrodedS/O 381002 N/R 36347 DURING SCHEDULED INSPECTION, FOUND NR 10 SLAT I/B END HAS CORROSION ON L-ANGLE.SDR DU4R2009308Web · corrodedS/O 318002 N/R 35473 DURING SCHEDULED INSPECTION, FOUND NR 2 PYLON LT AFT SIDE WEB HAS NUMEROUS AREAS OF CORROSION ON INNER AND OUTER SURFACES INCLUDING AROUND FASTENER HOLES.SDR DU4R2009299Skin Panel · corrodedS/O 318002 N/R 34983 - DURING SCHEDULED INSPECTION, FOUND CORROSION ON NR 1 PYLON FWD O/B SKIN PSS 68 - 80.SDR DU4R2009298Skin Panel · corrodedS/O 318002 N/R 34848 - DURING SCHEDULED INSPECTION, FOUND CORROSION IN NR 2 ENGINE PYLON INBOARD SKIN PANEL BELOW FWD AND AFT OF MOST FWD ACCESS PANEL.SDR DU4R2009297Skin Panel · corrodedS/O 318002 N/R 34856 DURING SCHEDULED INSPECTION, FOUND CORROSION IN OUTBOARD PYLON SKIN PANEL FWD OF MOST FWD ACCESS PANEL NR 2 ENGINE.SDR DU4R2009296Skin Panel · corrodedS/O 318002 N/R 34856 DURING SCHEDULED INSPECTION, FOUND CORROSION IN OUTBOARD PYLON SKIN PANEL FWD OF MOST FWD ACCESS PANEL NR 2 ENGINE.SDR DU4R2009309Support Beam · corrodedS/O 381002 N/R 36157 DURING SCHEDULED INSPECTION, FOUND LT WING REAR SPAR TO MLG SUPPORT BEAM HAS CORROSION AROUND AFT ATTACH BOLT HOLE.SDR DU4R2009301Skin · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON SKIN UPON REMOVAL OF TEMP REPAIR PLATE P/N 112N4303-2 AT RBBL 70.50, BS 958.39.SDR DU4R2009326Skin · corrodedS/O NR 318002 NR 35425, DURING SCHEDULED INSP AT, FOUND NR 1 PYLON RT AFT SIDE WEB HAS NUMEROUS AREAS OF CORROSION ON INNER AND OUTER SURFACES INCLUDING FASTENER HOLES FROM PPS 128-209.SDR DU4R2009291Stiffener · corrodedDURING SCHEDULED INSPECTION FOUND VERTICAL STIFFENER ATTACHED TO THE REAR SPAR WEB HAS PITTING CORROSION AT ATTACH POINT OF A GROUNDING WIRE APPROX WS 184.SDR DU4R2009290Bulkhead · crackedDURING SCHEDULED INSPECTION, FOUND NR 2 PYLON MID BULKHEAD FWD I/B LOWER BOLT HOLE IS CRACKED.SDR DU4R2009288Bulkhead · crackedDURING SCHEDULED INSPECTION, FOUND NR 1 PYLON MID BULKHEAD FWD I/B LOWER BOLT HOLE IS CRACKED.SDR DU4R2009327Keelbeam · corrodedS/O NR 318002 NR35531, DURING SCHEDULED INSP, FOUND CORROSION ON SPLICE PLATE ON FUSELAGE AT AFT END OF MLG DOORS BETWEEN BOTH DOORS ON BELLY.SDR DU4R2009289Bulkhead · crackedDURING SCHEDULED INSPECTION AT TIMCO, LAKE CITY, FL FOUND NR 1 PYLON MID BULKHEAD FWD O/B LOWER BOLT HOLE IS CRACKED.SDR DU4R2009287Keelbeam · corrodedS/O 318002 N/R 35725 DURING SCHEDULED INSPECTION, FOUND CORROSION ON LOWER KEEL BEAM CHORD IN RT WW AT BS 1060.SDR DU4R2009286Web · corrodedS/O 318002 N/R 35013 DURING SCHEDULED INSPECTION, FOUND CORROSION ON KEEL BEAM VERTICAL WEB AROUND HYD LINE FITTINGS AT FS 1100 S-19R RBL 5SDR DU4R2008285Skin · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION IN SEVERAL AREAS OF UPPER SURFACE SKINS ON LT HORIZONTAL STABILIZER.SDR DU4R2008284Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON WEB, LT WING REAR SPAR, ABOVE LT AFT BOOST PUMP WS 188SDR DU4R2008282Support · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON WING TO BODY FAIRING SUPPORT ABOVE RT WING AT BS 1098.SDR DU4R2008280Keelbeam · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON KEELBEAM LOWER SURFACE CROSS BRACE AT BS 996.SDR DU4R2008279Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT WING REAR SPAR BELOW LEFT AFT BOOST PUMP RSS 185.SDR DU4R2008281Skin · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON EXT SKIN AROUND APU OIL FUEL DRAIN MAST RT APD ACCESS DOOR.SDR DU4R2008278Skin · damagedDURING SCHEDULED INSPECTION, FOUND NUMEROUS CREASES IN EXT. FUSELAGE SKIN BS 1364 - 1410, S-26L TO S-26RSDR DU4R2008277Skin · dentedDURING SCHEDULED INSPECTION, FOUND DENT IN EXT. FUSELAGE SKIN BS 1125, S-10L LAP SEAM.SDR DU4R2008276Skin · dentedDURING SCHEDULED INSPECTION, FOUND 3 EA. DENTS IN LOWER FWD FUSELAGE BELOW MLG DOOR SCUFF PLATE BS 600-612.SDR DU4R2008275Skin · corrodedDURING SCHEDULED INSPECTION, FOUND LT WING HAD CORROSION IN UPPER SKIN AT ALL VORTEX GENERATORSSDR DU4R2008274Keelbeam · corrodedDURING SCHEDULED INSPECTION, FOUND KEELBEAM LOWER SURFACE CROSS BRACE HAS CORROSION AT BS 1040.
SDR DU4R2008273Keelbeam · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND KEEL BEAM LOWER SURFACE CORSS BRACE HAS CORROSION AT BS 956
S/O 318002 N/R #35360SDR DU4R2008272Skin · dentedDURING SCHEDULED INSPECTION, FOUND DENT IN FWD LOWER FUSELAGE BELOW MAIN CARGO DOOR THRESHOLD SCUFF PLATE AT BS 522.
SDR DU4R2008283Strap · corrodedDURING SCHEDULED INSPECTION, FOUND HEAVY CORROSION ON 2 EA. SUPPORT STRAPS REMOVED FROM BS 1825, B/O 0, RT SIDE TO HORIZ STAB.SDR DU4R2008271Keelbeam · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND KEEL BEAM AREA PANEL SUPPORT FRAME HAS CORROSION ON BOTH SIDES TOP AND BOTTOM SURFACES.SDR DU4R2008270Support · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND LT WHEEL WELL (MLG) WTB FAIRING SUPPORT ARE CORRODED THROUGHOUT AT BS 1040 - 1060 LBL 40 - 651.SDR DU4R2008269Skin · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AFT SPAR UPPER CHANNEL, SKIN FROM FUSELAGE TO WING TIP.SDR DU4R2008268Pressure Panel · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION IN RT WHEEL WELL ON LOWER SURFACE OF CEILING AREA AT BS 1120 S-17R ALONG FASTENERS RBL 60 - 70 AT PRESSURE DECK.SDR DU4R2008267Fitting · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORRODED ANGLE FITTING ON RT ELEVATOR STRAKELET.SDR DU4R2008266Skin · corrodedDURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AT NUMEROUS FASTENERS IN UPPER SKIN IN PREVIOUSLY WORKED SKIN AND UNWORKED SKIN.SDR DU42008F00000Skin · crackedDURING SCHEDULED INSPECTION, FOUND 1/8" LONG CRACK RUNNING FWD AND AFT FROM FASTENER HOLE ON REPAIR FILLER AT BS 1739-5 S-29R. EXISTING EO REPAIR FAT EO 757-53-0118.SDR UPS06546376Warning Light · illuminatedON T/O FROM MIA, NOSE GEAR "GREEN" DOWN AND LOCK LIGHT REMAINED ILLUMINATED W/GEAR UP AND LOCKED. RECYCLED LANDING GEAR, NO HELP. RIGHT HALF OF NOSE GEAR GREEN LIGHT REMAINS ILLUMINATED. GEAR IND OTHERWISE NORMAL WITH NO DISAGREE. REMOVED AND REPLACED LANSDR 2000ZZZX215Line · rupturedKMIA/KSAL - FLT 067 AT 21:30 Z - LEFT HYDRAULIC QUANTITY INDICATOR DECREASED TO 0.03 GALLON. ENGINE DRIVEN PUMP DEPRESSURIZED AND ELECTRIC PUMP OFF, QUANTITY INDICATION CONTINUED TO DECREASE. AIR TURN BACK TO MIA. NO FUEL DUMPED, NO OVERWEIGHT LANDING, LANDSDR 99ZZZM701Actuator · failedKMIA - LEFT MLG DID NOT RETRACT AFTER NORMAL TAKEOFF. GEAR DISAGREE/GEAR DOOR LIGH TON, STATUS AIR/GROUND DISAGREE ON LANDING GEAR MONITOR. FOUND LEFT MAIN LANDING GEAR DOWN LOCK ACTUATOR FAILED AFTER NUMEROUS GEAR SWINGS. REPLACED LEFT MAIN LANDING GEAR DOSDR 99ZZZM702Actuator · failedKMIA - LEFT MLG WOULD NOT RETRACT, GEAR DISAGREE/GEAR DOOR LIGHT ON WHEN GEAR HANDLE PLACED DOWN. FOUND LEFT MLG TILT ACTUATOR WITH INTERNAL LEAKAGE. REPLACED LEFT MLG TILT ACTUATOR WITH INTERNAL LEAKAGE. REPLACED LEFT MLG TILT ACTUATOR IAW MM 32-30-15, OPESDR 99ZZZM703Retract Mech · lack of lubeKMIA - LEFT MLG WOULD NOT RETRACT, GEAR DISAGREE/GEAR DOOR LIGHT ON WHEN GEAR HANDLE PLACED DOWN. JACKED AND SWUNG GEAR SEVERAL TIMES WITH NO DISCREPANCY NOTED. LUBRICATED LEFT MAIN LANDING GEAR. RETURNED AIRCRAFT TO SERVICE. (M)SDR 99ZZZM700Hose · looseFLT KMIA-SJO - REJECTED TAKEOFF DUE TO AIRSPEED DIFFERENCE, CAPTAIN 80 KNOTS, F/O 120 KNOTS, ABORTED AT 120 KNOTS. FOUND CAPTAIN PITOT SYSTEM LEAKING AT ELBOW FROM FLEX LINE TO HARD LINE AT PITOT TUBE. DISCONNECTED AND RESECURED ELBOW. PERFORMED OPERATION/LSDR CLCA9903Circuit Breaker · trippedFLT 33 - MIA-SAP - AIR TURN BACK, CLIMBOUT OF FL240 THE FOLLOWING OCCURED. THE LEFT IRS DISPLAYED ON DC AND EICAS MESSAGE. THE CTR AUTOPILOT DISENGAGED AND AUTO THROTTLES DISCONNECTED. SUBSEQUENTLY IT WAS OBSERVED THAT WX RADAR AND LEFT VOR/DME WERE INOPERASDR CLCA9901Filler · failedFLT 96 - SEQU TO CLO - ON T/OF ROLL AT 0010Z. ON ROUTINE NORMAL T/O AT APPROX 75 KNOTS A/C BEGAN TO MAKE VIOLENT BANGING NOISE AND ABNORM EXTREME SHUDDERING FOLLOWED BY A MODERATE YAW TO THE LT. THE REJECTED T/O PROCEDURE WAS INITIATED AND A/C STOPPED ON RUN
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