Boeing 747-122
Service difficulty reports · 2,143
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 = '747122' 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 = '747122' 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 P5CA9600739Sleeve · dentedDENT NR 1 ENGINE FAN REVERSER SLEEVE AT 3 O'CLOCK POSITION. REPAIRED PER BOEING SRM 54-34-03 PAGE 85.SDR P5CA9600737Rib · corrodedLEVEL 1 CORROSION NR 1 PYLON FIRE BOTTLE SUPPORT RIB. REMOVED CORROSION PER BOEING SRM 51-10-01 TREATED PER BOEING SRM 51-10-02.SDR P5CA9600727Hinge · corrodedLEVEL 1 CORROSION ON NR 3 AIR CYCLING MACHINE ACCESS DOOR. REPLACED HINGE PER BOEING MAINTENANCE MANUAL 52-48-01.SDR P5CA9600756Skin · corrodedFOUND LEVEL ONE SURFACE CORROSION ON INBOARD MIDFLAP ON CENTER PANEL AT JOINT TO AFT PANEL ON LOWER SURFACE RWBL 225. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 51-40-00. REPORTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.SDR P5CA9600755Skin · corrosionFOUND LEVEL ONE SURFACE CORROSION ON UPPER SKIN OF INBOARD MIDFLAP AT JOINT TO TRAILING EDGE FALSE WORK, RWBL 333 TO 352. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 57-50-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02.SDR P5CA9600736Lock Arm · bentBENT FORWARD LOCK ARM ON MAIN DECK SIDE RAIL AT STA 1780. REPLACED SIDE RAIL LOCK ARM PER BAC MM 25-58-00.SDR P5CA9600732Cowl Pin/Support · damagedDAMAGED ALIGNMENT PIN AND SUPPORT ON NR 2 ENGINE CORE COWL. REPAIRED PER BAC SRM 51-10-01.SDR P5CA9600738Skin · damagedDAMAGED TRAILING EDGE SKIN ON NR 3 ENGINE T-FAN THRUST REVERSER SLEEVE. REPAIRED WITH HOT BONDED DOUBLER PER BAC SRM 51-40-06.SDR P5CA9600735Cowl · crackedCRACK AT 5TH LATCH ON NR 3 ENGINE POWER COWL. REPAIRED PER BAC SRM 51-10-01.SDR P5CA9600731Housing · tornTORN LEFT CORNER OF NOSE TAXI LIGHT HOUSING. REPAIRED PER BAC SRM 51-40-09.SDR P5CA9600730Skin · crackedCRACK ON SMALL FAIRING AND FAIRING IS LOOSE AFT FUSELAGE ON LEFT UNDER APU EXHAUST DUCT. REPAIRED PER BAC SRM 51-10-01 AND 51-40-02.SDR P5CA9600809Floorbeam · corrodedLEVEL 1 CORROSION ON FORWARD CARGO HOLD LATERAL FLOORBEAM UPPER CHORD UPPER SURFACE AT BS 780 RBL 15 TO RBL 23. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PROTECTED PER 51-10-02.SDR P5CA9600694Panel · delaminatedDELAMINATED UNDERWING PANEL AT RIGHT INBOARD LEADING EDGE. REPAIRED DAMAGED AREA PER BAC SRM 51-40-09.SDR P5CA9600687Seq Carriage · crackedLEFT INBOARD FLAP SEQUENCE CARRIAGE FAILED DAMAGING THE LEFT INBOARD FORE FLAP. REMOVED AND REPLACED LEFT INBOARD FORE FLAP, CARRIAGES AND TRACK OPERATIONAL CHECK GOOD PER BOEING MAINTENANCE MANUAL 27-51-02.SDR 96UAL900687Center Tube · wornDURING TIME CONTROLLED OVERHAUL WEAR WAS FOUND IN THE CENTER INFLATION TUBE AND SLIDING SURFACE. PATCHED TUBE AND SLIDING SURFACE PER VENDOR MANUALSDR P5CA9600685Stiffener · crackedCRACKED STIFFENER ON RIGHT BODY GEAR WHEELWELL PRESSURE DECK BS 1400 RBL 100. REMOVED STIFFENER, PERFORMED HFEC INSPECTION OF AREA BELOW CRACK PER BOEING NDT MANUAL PART 6 51-00-00. NO DEFECTS NOTED. REPLACED STIFFENER WITH NEW PART PER BOEING SRM 51-10-01SDR P5CA9600682Bracket · crackedCRACKED LIGHT BRACKET IN RIGHT BODY LANDING GEAR WHEEL WELL BS 1395 RBL 90 WL 200. REPLACED LIGHT BRACKET PER BOEING SRM 51-10-01.SDR P5CA9600681Bracket · crackedCRACKED AND BENT INBOARD FLAP TORQUE TUBE WHIP GUARD BS 1350 RBL 90. REPAIRED PER BOEING SRM 51-40-03.SDR P5CA9600680Angle · crackedCRACKED ATTACH ANGLES FOR RIGHT BODY LANDING GEAR TRUCK BUMPER AT LOWER WL 140 AND UPPER WL 160 BS 1350. REPLACED LOWER ANGLE PER BOEING SRM 51-10-01 AND REPAIRED UPPER PER BOEING SRM 51-30-03.SDR P5CA9600679Stantion · crackedSTANTION CRACKED AFT END OF THE E AND E COMPARTMENT BS 460 WL 135 RBL 24. REPAIRED PER BOEING SRM 51-40-03.SDR P5CA9600678Roller Tray · damagedDAMAGED ROLLER TRAY BS 1800 RBL 6. REPLACED ROLLER TRAY PER BOEING SRM 51-10-01.SDR P5CA9600677Roller Tray · damagedDAMAGED ROLLER TRAY BS 1820 LBL 33. REPLACED ROLLER TRAY PER BOEING SRM 51-10-01.SDR P5CA9600669Gull Fairing · damagedDAMAGED GULL FAIRING LEFT WING LANDING GEAR LOWER STRUT DOOR AT AFT END. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9600668Torque Link · missingAFTER TAKEOFF, LOST NR 1 HYDRAULIC SYSTEM FLUID. LANDING INSPECTION REVEALED RIGHT BODY GEAR LEFT FORWARD BRAKE TORQUE LINK DISCONNECTED. ADDITIONAL DAMAGE TO BODY GEAR TILT ACTUATOR HOSE, NR 10 BRAKE HOSE BOTH FORWARD AND AFT BRAKE TORQUE LINKS. BRAKE ROD SDR P5CA9600670Wire · chafedPRIMARY DISPLAY AND CONTROL CIRCUIT BREAKER TRIPPED. REPAIRED CHAFED WIRE AT CONNECTOR IN LANDING GEAR CARD FILE DISCONNECT PANEL, OPERATIONAL CHECKED OK PER M/M 32-61-00.SDR P5CA9600666Engine · over tempON TAKEOFF ROLL, NR 1 ENGINE ROLL REACHED 942 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF, RETURNED TO GATE. ENGINE CHANGED PER BOEING MAINTENANCE MANUAL 71-00-02.SDR P5CA9600644Engine · oil leakAT CRUISE NR 2 ENGINE OIL QUANTITY STEADILY DECREASED FROM APPROX 5.6 GALLONS TO ZERO WITHIN 45 MINUTES FROM TAKEOFF. SHUT DOWN ENGINE AND RETURNED TO AMS. WINDMILL TIME 1 HOUR 16 PSI OIL PRESSURE. FOUND OIL LEAK TO BE INTERNAL REMOVED AND REPLACED ENGINE PSDR P5CA9600655Track · wornWORN FORE FLAP TRACK TO RIGHT OUTBOARD TRAILING EDGE MID FLAP. REPLACED TRACK PER BOEING MAINTENANCE MANUAL 27-51-04 AND 27-51-06.SDR P5CA9600654Track · wornWORN FORE FLAP TRACK TO LEFT OUTBOARD TRAILING EDGE MID FLAP. REPLACED TRACK PER BOEING MAINTENANCE MANUAL 27-51-04 AND 27-51-06.SDR P5CA9600653Skin · delaminatedDELAMINATE LEADING EDGE OF THE LEFT OUTBOARD TRAILING EDGE FORE FLAP BY THE OUTBOARD EDGE. REPAIRED PER BOEING SRM 51-40-07.SDR 96UAL900638Light · inoperativeEMERGENCY EXIT LIGHTS FROM DOOR 2L TO SEAT 18A ARE INOPERATIVE. ADDITIONALLY, LAMP AT SEAT 20C IS INOPERATIVE. SECURED LEAD IN POWER CABLE AND ALSO SECURED LAMP AT SEAT 20C.SDR P5CA9600612Module Housing · crackedNR 3 HYDRAULIC SYSTEM FLUID LOSS AFTER PUSHBACK. FOUND NR 3 HYDRAULIC SYSTEM PRESSURE MODULE HOUSING CRACKED. REMOVED AND REPLACED MODULE PER BOEING MAINTENANCE MANUAL 29-11-23.SDR P5CA9600611Csd · overheatedDURING CLIMB AT FL 310, NR 1 ENGINE HAD DUAL FIRE WARNING LIGHTS ILLUM WITH PEGGED NACELLE INDICATORS. PULLED THROTTLE BACK TO IDLE AND LIGHTS WENT OUT, INDICATIONS NORMAL AND CONTINUED FLIGHT. ON GROUND FOUND CSD OVERHEATED AND BODY CRACKED WIRING BURNT ON SDR P5CA9600613Hyd Line · crackedNR 1 HYDRAULIC QUANTITY LOW. FOUND CRACKED LINE NR 1 HYDRAULIC SYSTEM FROM T-FITTING INBOARD OF NR 1 PYLON TO T-FITTING OUTBOARD OF NR 1 PYLON. INSTALLED TEMPORARY FLEX LINE PER BOEING MAINTENANCE MANUAL 29-00-00 PAGE 5.SDR P5CA9600601Engine · malfunctionedNR 4 ENGINE OIL QUANTITY DECREASED INFLIGHT, WHEN OIL PRESSURE BEGAN TO FLUCTUATE AND LOW OIL PRESSURE CAUTION LIGHT FLICKERED. COMPLETED THE PRECAUTIONARY ENGINE SHUT DOWN. ON GROUND RUN FOUND OIL LEAKING FROM BREATHER PORT. REMOVED AND REPLACED ENGINE PERSDR P5CA9600483Seal Depressor · damagedFORWARD CARGO DOOR, SEAL DEPRESSOR DAMAGED FORWARD LOWER SIDE. REPLACED DAMAGED SECTION PER BOEING SRM 51-10-01.SDR P5CA9600482Bracket · bentFORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE OUTBOARD RIB FOR CANNON PLUGS SUPPORT BRACKET BENT. REPLACED PER BOEING SRM 51-10-01.SDR P5CA9600481Support · crackedFORWARD CARGO AFT E AND E COMPARTMENT, RIB WHICH HOLDS CANNON PLUGS BETWEEN LEFT AND CENTER SECTIONS, CRACKED AND BROKEN. REPAIRED PER BOEING SRM 51-10-01 AND SRM 51-40-03.SDR P5CA9600480Support · brokenFORWARD CARGO E AND E COMPARTMENT MOST OUTBOARD CANNON PLUG RIB SUPPORT RIB BROKEN. REPAIRED VERTICAL SUPPORT PER BOEING SRM 51-10-01 AND SRM 51-40-03.SDR P5CA9600479Bracket · brokenFORWARD CARGO E AND E COMPARTMENT RIB FOR CANNON PLUGS BETWEEN RIGHT AND CENTER SECTION SUPPORT BRACKET BROKEN. REPLACED PER BOEING SRM 51-10-01.SDR P5CA9600478Support · bentFORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 4 TH ROW BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.SDR P5CA9600477Support · bentFORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 3RD ROW BURNDY BLOCK SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.SDR P5CA9600476Support · bentFORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 2ND ROW BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.SDR P5CA9600475Support · bentFORWARD CARGO AFT E AND E COMPARTMENT, CENTER SECTION 3RD ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01.SDR P5CA9600474Support · bentFORWARD CARGO AFT E AND E COMPARTMENT 2ND ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.SDR P5CA9600473Support · bentFORWARD CARGO AFT E AND E COMPARTMENT, RIGHT SIDE 3RD ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11.SDR P5CA9600472Tire · failedDURING INITIAL APPROACH TO JFK, ATC NOTIFIED OF RUBBER SECTIONS FOUND ON RUNWAY AT LCK. AFTER LANDING, FOUND CAP MISSING ON NR 6 TIRE AND NR 5 TIRE THERMALLY DEFLATED AFTER TAXI. REPLACED NR 5 AND NR 6 TIRE ASSEMBLIES PER BOEING MAINTENANCE MANUAL 32-45-01. SDR 96UAL900591Compressor · stalledNR 3 ENGINE HAD COMPRESSOR STALL WHEN THROTTLE RETARDED FOR DESCENT. STALL CAUSED STEADY AIRFRAME VIBRATION, EGT CLIMBED TO 700 DEGREES AND ENGINE SHUTDOWN.SDR P5CA9600415Hilock Fastener · head shearedHEAD SHEARED ON HILOCK RIGHT WING AFT SPAR, LOWER CHORD, JUST OUTBOARD OF WING GEAR AFT TRUNNION. REPLACED HILOCK PER BOEING SRM 51-10-01.SDR 96UAL900586Stringer · corrodedFOUND ONE POPPED AND SEVERAL DISHED RIVETS ON BELLY SKIN FROM STATION 760 TO 780. INTERNAL INSPECTION FOUND CORRODED STRINGERS 47L AND 47R, STATION 760 TO 780. REMOVED STRINGERS 47L AND 47R FROM STATION 740 TO 780. REMOVED LIGHT SURFACE CORROSION ON SKIN, A
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