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 P5CA9700300End Cap · failedNR 4 HYDRAULIC SYSTEM LOST 7 GALLONS. ISOLATION PROCEDURE SHOWED EDP LOSING FLUID. NR 1 HYDRAULIC SYSTEM LOST ALL FLUID WHEN SECONDARY BRAKE SOURCE SELECTED DUE TO NR 4 SYSTEM FLUID LOSS. FOUND END CAP ON BRAKE SYSTEM RETURN SURGE ACCUMULATOR BROKEN OFF. RSDR P5CA9700299Sensor Actuator · wrong partAFTER TAKEOFF AND GEAR RETRACTION WITH GEAR LEVER OFF, LANDING GEAR LEVER LATCH REMAINED IN VIEW. RIGHT WING LANDING GEAR TILT ANNUNCIATOR INDICATED PRI. AND ALT TILT AMBER LIGHTS ILLUMINATED. FOUND THE RIGHT WING LANDING GEAR TRUCK POSITION SENSOR ACTUATOR SDR P5CA9700296Cowl · damagedNR 2 NOSE COWL - DAMAGE ON EXTERIOR FLANGE 'V' GROVE AT 90 DEGREE POSITION GOUGED AND DENT WITH A CRACK. REPAIRED PER BOEING DER 8110-3 MOBILE AEROSPACE ENGINEERING EA-47-5400-15-A0174.SDR P5CA9700295Latch Fitting · crackedFORWARD LOWER CARGO DOOR - CRACK IN NR 6 (FROM FORWARD END) LATCH SUPPORT FITTING - FORWARD LEG. REPAIRED PER SB-747-53-2200.SDR P5CA9700294Strip · crackedNR 3 PYLON - L/S UPPER WING TO PYLON STRIP CRACKED AT OLD WELD ABOVE ACCESS PANEL 472DL. WELDED PER BOEING SRM 51-30-02.SDR P5CA9700293Link Bolt · rotatedNR 1 ENGINE - AFT MOUNT - INBOARD TANGENTIAL LINK BOLT HAS ROTATED. POLAR AIR WORK CARD S1-7121-002 REF AD-96-03-01 COMPLIED WITH.SDR P5CA9700292Fitting · crackedINBOARD TRUNNION LONGERON BRIDGE FITTING FRACTURED. REPAIRED PER EA 47-5343-15-A0175 MOBILE AEROSPACE ENGINEERING.SDR P5CA9700291Skin · delaminatedRIGHT WING LANDING GEAR - LOWER STRUT DOOR - DELAMINATED AT LOWER END. REPLACED PER MM 32-12-06.SDR P5CA9700290Skin · delaminatedLEFT WING LANDING GEAR - LOWER STRUT DOOR DELAMINATED ON LOWER END BY FAIRING. REF: PA1579030151. REPLACED PER MM 32-12-06.SDR P5CA9700272Threshold · crackedBULK CARGO DOORWAY THRESHOLD CRACKED. REPAIRED PER BOEING SRM 51-30-02.SDR P5CA9700271Skin · corrodedUPPER FUSELAGE HAS BARE SPOTS WITH CORROSION SURFACE BS 1265 TO 1460. REPAIRED PER SRM 51-10-01.SDR P5CA9700270R-Rail · crackedNR 1 ENGINE, R-RAIL CRACKED AT 170 DEGREE POSITION. REPAIRED PER PRATT AND WHITNEY 72-53-01.SDR P5CA9700269Skin · puncturedL/W, I/B, AFT FLAP SMALL PUNCTURE BETWEEN 3 AND 4 CANOE. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9700268Panel · dentedDENT AND ABRASION, TOP RT STABILIZER L/E PANEL. REPAIRED PER SRM 55-10-03.SDR P5CA9700267Rivets · missingFASTENERS BETWEEN BLG DOOR ON KEEL BEAM PANELS MISSING. REPAIRED PER BOEING SRM 51-30-02.SDR P5CA9700266Fairing · looseNR 4 PYLON FAIRING ABOVE TURBINE EXHAUST CASE LOOSE AND MISSING RIVETS. REPAIRED PER BOEING SRM 51-30-02.SDR P5CA9700265Hinge · corrodedBARE METAL WITH SURFACE CORROSION, ALONG HINGE ASSY OF MAIN DECK CARGO DOOR ON FUSELAGE. REPAIRED PER BOEING SRM 51-10-01.SDR P5CA9700264Doubler · crackedTWO CRACKS IN DOUBLER UPPER AFT NLG, WHEEL WELL RIGHT SIDE OF RETRACT LINK. REPAIRED PER BOEING SRM 51-40-02.SDR P5CA9700263Skin · deterioratedR/W, I/B, MID FLAP, L/E DETERIORATED ON O/B END. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9700261Panel · corrodedBELLY PANELS BS 960 BACK TO MLG, BARE AND CORROSION SPOTS. REPAIRED, TREATED AND FINISHED PER BOEING SRM 51-10-02.SDR P5CA9700262Fairing · corrodedLWR BODY FAIRINGS, CORROSION BY RAD ALT ANTENNAS AND CIRCULAR ACCESS COVERS. REPAIRED PER BOEING SRM 51-40-11.SDR P5CA9700259Access Panel · crackedACCESS PANEL O/B OF NR 6 CANOE CRACKED. REPAIRED PER SRM 51-40-09.SDR P5CA9700258Skin · corrodedLEVEL 1 CORROSION 2 OF 4 DME ANTENNA BASES CORRODED. REPAIRED PER SRM 51-10-01, 51-10-02 AND 51-10-06.SDR P5CA9700257Skin · gougedLEVEL 1 DOOR GOUGE IN SKIN FORWARD OF DOOR FUSELAGE BS 430 WL 230. REPAIRED PER BOEING SRM 51-10-02.SDR P5CA9700256Skin · corrodedLEVEL 1 CORROSION UPPER DECK WINDOW LT SIDE. REPAIRED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700255Skin · separatedNR 4 ENGINE TURBINE EXHAUST CASE OUTER SKIN PULLED FASTENERS AND SKIN SEPARATED. REPAIRED PER BOEING SRM 51-30-02.SDR P5CA9700222Skin · crackedNR 1 MAIN ENTRY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED PER BOEING SRM 52-00-02 FIGURE 1 DETAIL II.SDR P5CA9700157Blanking Plate · mis installedLOSS OF OIL FROM NR 3 ENGINE ON CLIMB. ENGINE SHUT DOWN DUMPED FUEL AND RETURNED TO ANC. FOUND BLANKING PLATE FOR NR 3 ENGINE DRIVEN PUMP PER MEL NOT INSTALLED PROPERLY. CORRECTLY INSTALLED BLANKING PLATE PER DISPATCH DEVIATION GUIDE 29-110-05 PAGE 201 PARASDR P5CA9700087Panel · crackedCOMPOSITE PANEL OVER LEFT WING GEAR DELAMINATED AND CRACKED. REPAIRED PER BOEING SRM 51-40-09 AND 51-40-12.SDR P5CA9700105Door · corrodedLEVEL 1 CORROSION ON RIGHT BODY LANDING GEAR INBOARD AND OUTBOARD DOORS. REMOVED CORROSION PER BOEING SRM 51-10-01.SDR P5CA9700086Fasteners · brokenAFT CARGO DOOR SILL LATCH PIN FITING AT BS 1840 HAS BROKEN FASTNERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02.SDR P5CA9700072Angle · crackedCRACK ON FORWARD SUPPORT ANGLE FOR NR 2 ENGINE INBOARD COWL HINGE. REPAIRED PER BAC SRM 54-10-03.SDR P5CA9700070Strap · brokenBROKEN FRAME STRAP IN LEFT AFT CARGO COMPARTMENT SIDEWALL AT APPROX BS 1700. REPAIRED PER BAC SRM 51-40-04 AND SRM 51-30-02.SDR P5CA9700068Case Rail · crackedCRACK ON NR 2 ENGINE TURBINE CASE S-RAIL. WELDED CRACK PER PRATT AND WHITNEY OHM 72-53-01.SDR P5CA9700173Keel Beam · corrodedMINOR CORROSION FOUND ON KEEL BEAM SUPPORT STRUCTURE BETWEEN STA 1260 TO 1480. BLENDED OUT CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 51-10-01, REPROTECTED AREA.SDR P5CA9700104Support · corrodedLEVEL 1 CORROSION FOUND ON KEEL BEAM SUPPORT STRUCTURE BETWEEN BS 1260 AND BS 1460. BLENDED OUT CORROSION PER BOEING SRM 51-10-01.SDR P5CA9700073Threshold · brokenBROKEN LEFT CORNER ON NR 3 MAIN ENTRY DOOR THRESHOLD. WELDED PER BOEING PROCESS 5975 AND INSPECTED PER BAC NDTM 20-50-02, NO CRACKS FOUND.SDR P5CA9700071Floorbeam · damagedDAMAGED UPPER CHORD ON FLOORBEAM IN AFT CARGO COMPARTMENT AT BS 1820. BLENDED DAMAGED AREA PER BAC SRM 51-10-01 AND RETREATED PER BAC SRM 51-10-02.SDR P5CA9700069Skin · puncturedSMALL PUNCTURE IN LEFT WING UPPER LEADING EDGE APPROX 4 FEET OUTBD OF FUSELAGE. APPLIED FIBERLAYS AND PAINTED PER BAC SRM 51-40-09 AND SRM 51-24-11.SDR P5CA9700067Panel · puncturedPUNCTURE ON INNER SKIN OF NR 3 PYLON OUTBOARD SAILBOAT PANEL. REPAIRED PER BAC SRM 51-40-06.SDR P5CA9700066Cowling · delaminationDELAMINATION TO INSIDE EDGE OF NR 3 ENGINE FAN COWL. REBONDED DELAMINATED AREA PER BAC SRM 51-40-06.SDR P5CA9700065Foreflap · delaminatedDELAMINATIONS AT TWO SPOTS ON THE LEFT INBOARD FOREFLAP LEADING EDGE. REPAIRED DELAMINATIONS WITH FIBERGLASS OVERLAYS AND PAINTED PER BAC SRM 51-40-09 AND SRM 51-24-11.SDR P5CA9700064Skin · delaminatedDELAMINATION ON INBOARD RIGHT FOREFLAP LEADING EDGE. REPAIRED AND PAINTED PER BAC SRM 51-40-09 AND 51-24-11.SDR P5CA9700063Skin · crackedBULGING AND CRACKED SKIN ON LOWER CENTER FUSELAGE ADJACENT TO PNEUMATIC SERVICE DOOR. REMOVED PANEL AND REPAIRED WITH A DOUBLER, TREATED AND PAINTED PER BAC SRM 51-30-02, 51-40-02 AND 51-24-11, REINSTALLED.SDR P5CA9700062Panel · crackedCRACK ON RIGHT WING FLYING PANEL OUTBOARD EDGE. STOP DRILLED CRACK AND APPLIED FIBERGLASS OVERLAY AND PAINTED PER BAC SRM 51-40-09 AND SRM 51-24-11.SDR P5CA9700041Angle · corrodedLEVEL 2 CORROSION ON SHEAR ANGLE AT BS 1760 BETWEEN S51L AND S50L. CORROSION REMOVED PER BAC SRM 53-10-04, FIGURE 3.SDR P5CA9700034Engines · stalled*** CORRECTION***AT FLIGHT LEVEL 430, NR 1 AND NR 2 ENGINE LOW SPEED STALL, NO THROTTLE RESPONSE, AT FL 350 ALL PARAMETERS NORMAL THROUGH REMAINING FLIGHT. CARRIED OUT INLET AND EXHAUST INSPECTION CHECK, ALL CHECKED NORMAL. CHANGED FUEL FILTERS, NO CONTAMISDR P5CA9700036Connector · contaminatedON TAXI OUT AFTER FLIGHT CONTROL CHECK, RUDDER RATIO LIGHT CAME ON AND REMAINED ON. REMOVED AND CLEANED CANNON PLUGS ON BOTH UPPER AND LOWER RUDDER RATIO UNITS. PERFORMED RUDDER RATIO CHECK PER BOEING MAINTENANCE MANUAL 27-21-12, PROCEDURE GROUND CHECKS NORSDR P5CA9700035Line · wornHYDRAULIC LEAK FROM LINE IN LEFT BODY GEAR WHEEL WELL. REPLACED LINE AND LEAK CHECKED PER BOEING MAINTENANCE MANUAL 29-00-00.SDR P5CA9700033Line · crackedSLOW LOSS OF HYDRAULIC FLUID NUMBER 4 HYDRAULIC SYSTEM DURING FLIGHT. ENGINE DRIVEN PUMP DEPRESSURIZED AND QUANTITY HELD AT 4 GALLONS. FOUND NR 4 ENGINE DRIVEN PUMP PRESSURE LINE IN PYLON CRACKED. REPLACED LINE LEAK CHECK AND OPERATIONAL CHECK OK PER MAINTE
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