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 P5CA9600162Retention Screws · looseFOUND NR 10 WHEEL ASSEMBLY ALIGNMENT KEYS MIGRATED DUE TO LOOSE/MISSING RETENTION SCREWS, CAUSED DAMAGE TO BRAKE ASSEMBLY. REMOVED AND REPLACED NR 10 WHEEL ASSEMBLY PER MM 32-45-01. REMOVED AND REPLACED BRAKE ASSEMBLY PER MM 32-41-15. BRAKE ASSEMBLY (P/N 26SDR P5CA9600157Position Ind · failedWHEN EXTENDING FLAPS FOR APPROACH, OUTBOARD TRAILING FLAPS SPLIT: LEFT STAYED AT 1 DEGREE, RIGHT WENT TO 5 DEGREES. EXTENDED FLAPS BY ALTERNATE SYSTEM, FLAPS EXTENDED NORMALLY. FLAP TRANSMISSION SERVICED IAW MM 12-13-13. CHECKED FLAP POSITION INDICATION SYSDR P5CA00155Relay · inopON CLIMBOUT FL 20.0, LOST ALL POWER TO ENGINE FUEL PANEL, WITH NO GAUGE MOVEMENT AND NO GAUGE PRESSURE TO TEST. ON LANDING, AFTER APPROX 4 MINUTES TAXI, ALL POWER CAME BACK AND FUEL QUANTITY GAUGES RAN DOWN TO ACTUAL FUEL. FOUND FAULTY R996 RELAY AND REPLACESDR 96UAL900169Slide · failed testSLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. FAILED DUE TO POROSITY. SLIDE SCRAPPED.SDR 96UAL900168Slide · failed testSLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. AIR RETENTION FAILED DUE TO SLIDE POROSITY. SLIDE SCRAPPED.SDR 96UAL900167Slide · failed testSLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. AIR RETENTION FAILED DUE TO SLIDE POROSITY. SLIDE SCRAPPED.SDR P5CA9600213Heat Duct · crackedFOUND CRACKED WELD AT AFT CARGO STATION 1480 HEAT DUCT. REPAIRED IAW OHM 36-10-04.SDR P5CA9600211Panel · crackedFOUND SMALL CRACKS ON THE HORIZONTAL STABILIZER, RT T/E UNDER STATIC DISCHARGE BASE THIRD FROM OUTSIDE. REPAIRED IAW SRM 51-40-15.SDR P5CA9600151Press Indicator · inoperativeAFTER PUSHBACK, NR 3 ENGINE WAS STARTED AND OIL PRESSURE INDICATOR DID NOT INDICATE. REMOVED AND REPLACED OIL PRESSURE INDICATOR IAW MM 79-32-03, OPS CHECKS GOOD.SDR P5CA9600212Skin · corrodedFOUND LEVEL ONE CORROSION ON FUSELAGE SKIN BETWEEN STA 2484 TO 2658 WL 366.50 RT SIDE. REMOVED CORROSION AND TREATED IAW SRM 51-10-01.SDR 96UAL900151Breather Tube · crackedFIRE WARNING IN NR 1 ENGINE. NR 3 BEARING BREATHER TUBE AT 1 O'CLOCK WAS FOUND TO BE CRACKED FORWARD OF SEAL RING GROOVES. THIS CRACKED TUBE ALLOWED 15TH STAGE HOT AIR TO ENTER THE 7TH STAGE BUFFER AIR COMPARTMENT.SDR P5CA9600210Panel · corrodedFOUND LEVEL ONE CORROSION AT RT HORIZONTAL STABILIZER TIP, AROUND STATIC DISCHARGE BASE SECOND FROM THE FRONT SIDE. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01.SDR P5CA9600149Panel · delaminatedON WALKAROUND FOUND RT PANEL LOWER WING MOST FORWARD BETWEEN WBL1500 WS 294.620 DELAMINATED. APPEARS TO HAVE BEEN CAUSED BY POWER UNIT PLACED UNDER WING. REPLACED PANEL IAW SRM 51-30-02.SDR 96UAL900134Light · failedOVERWING EMERGENCY LIGHT ON LEFT SIDE INOP. REPLACED LIGHT.SDR 96UAL900132Aspirator · shearedDURING TEST INFLATION OF DOOR 5 RT SLIDE, AT OVERHAUL ONE ASPIRATOR SHEARED IN TWO. SHEAR POINT IS LOCATED BELOW THE RETAINING BANDS WHICH HOLD THE ASPIRATOR IN PLACE. REPLACED ASPIRATOR, RETURNED DAMAGED ASPIRATOR TO OEM FOR ANALYSIS.SDR 96UAL900113Slide · failed testDURING OVERHAUL, DOOR 2 RIGHT SLIDE FAILED AIR RETENTION TEST DUE TO POROSITY ON BOTH FILL TUBES. PATCHED AREAS OF POROSITY.SDR P5CA9600135Skin · crackedON PREDEPARTURE CHECK, FOUND SKIN DAMAGE AT FORWARD EDGE OF OPENING FOR REAR LOWER CARGO DOOR. DOOR FRAME TEAR STRIP AND OUTER SKIN DISTORTED AND CRACKED. REPAIRED PER DOCUMENT R747-5310-28-1/1.SDR 96UAL900092Strip · inoperativeEMERGENCY ESCAPE LIGHTING INOP AT ROWS 37-49, RIGHT AISLE. REPLACED LIGHT STRIP.SDR P5CA9600199Fairing · puncturedFOUND NR 4 CANOE FAIRING PUNCTURED. REPAIRED IAW SRM 51-40-09.SDR P5CA9600091Tire · blownBLEW NR 10 TIRE ON TAKEOFF FROM HONG KONG. RETURNED TO HONG KONG, MADE UNEVENTFUL LANDING. REMOVED AND REPLACED TIRE IAW MM 32-45-01.SDR P5CA9600171Web · crackedFOUND NR 4 PYLON MIDSPAR WEB CRACKED AT APPROX NACELLE STA 205. WEB REPAIRED IAW SRM 54-10-03.SDR P5CA9600089Pt7 Line · brokenON TAKEOFF, LOST NR 1 AND NR 4 EPR INDICATION AND NR 3 AND NR 4 GENERATOR. TAKEOFF WAS ABORTED. REPLACED NR 3 GCU, GROUND CHECK OK. FOUND NR 4 GCR RACK PLUG LOOSE, SECURED AND GROUND RUN CHECK OK. FOUND NR 4 ENGINE PT7 LOOP LINE BROKEN AT ONE O'CLOCK POSITSDR P5CA9600084Coupling · looseON BLOCK IN, GROUND PERSONNEL SAW TAILPIPE FIRE, NR 1 ENGINE. CREW DISCHARGED FIRE BOTTLE AND MOTORED ENGINE, PUT OUT FIRE. INSPECTED ENGINE AND PYLON FOR DAMAGE, NO STRUCTURES FOUND DAMAGED. FOUND AFT-MOST FUEL FEED LINE COUPLING LOOSE AND FUEL LEAK IN NR SDR P5CA9600197Le Skin · dentedFOUND LOWER VERTICAL FIN LEADING EDGE SKIN DENTED AT STA 124 AND STA 220. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 55-30-03.SDR P5CA9600189Door · crackedFOUND CRACK ON AFT CARGO DOOR LEFT LOWER EDGE AT STA 1880. REPAIRED IAW SRM 52-00-03.SDR P5CA9600174Panel · delaminatedFOUND OVERWING PANEL ABOVE REAR SPAR WBL 244.6 TO 277 FIXED T/E DELAMINATED. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-40-09.SDR P5CA9600088Chord · corrodedFOUND LEVEL 1 CORROSION AT STATION 1350 PRESSURE DECK TOP CHORD. CORROSION REMOVED, FOUND WITHIN LIMITS IAW SRM 53-10-01.SDR P5CA9600087Fitting · wornFOUND BOTH FORWARD AND AFT INBOARD FAIL-SAFE FITTINGS ON RT INBOARD AILERON DUE TO LOOSE RIVETS IN PREVIOUS REPAIR. REMOVED FITTINGS, REPAIRED WEB, REINSTALLED NEW BUSHINGS AND FITTINGS IAW SRM 57-51 02A-001A AND 57-42-14-001.SDR P5CA9600086Support Ftg · crackedDURING SSID INSPECTION, NOTED INDICATION OF CRACK ON OUTBOARD WING GEAR SUPPORT FITTING. REMOVED FITTING AND REPAIRED PER S/B 747-57-2244. BORED TO FIRST OVERSIZE, MAG PART INSP COMPLETED, FITTING REINSTALLED.SDR P5CA9600085Support Beam · crackedFOUND SUPPORT BEAM CRACKED IN PREVIOUS REPAIR. REPAIRED PER SRM 51-40-03, WEB REPLACED WITH 2024-T3.040 MATERIAL.SDR P5CA9600025Skin · chafedFOUND APU COMPT FORWARD BULKHEAD FWD SIDE CHAFED THROUGH AT STA 2658, CAUSED BY IMPROPERLY INSTALLED SHROUD AT BULKHEAD. REPAIRED DAMAGED AREA IAW SRM 53-10-04.SDR P5CA9600024Sleeve · crackedFOUND TURBINE REVERSER SLEEVE CRACKED BETWEEN TWO PREVIOUS REPAIRS. REPAIRED IAW SRM 54-30-03. REPAIR INCLUDES BOTH PREVIOUS REPAIRS.SDR P5CA9600023Skin · corrodedFOUND CORROSION AND SLIGHT BULGING OF PAINT AROUND RIVET HEAD FORWARD OF NR 9 SPOILER. CLEANED AND TREATED PER SRM 51-10-01.SDR P5CA9600192Strut Door · delaminatedFOUND RIGHT HAND WING GEAR LOWER STRUT DOOR LOWER EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15.SDR P5CA9600191Door · delaminatedFOUND LEADING EDGE OF LEFT WING GEAR LOWER STRUT DOOR DELAMINATED. REPAIRED IAW SRM 51-40-15.SDR P5CA9600190Strut Door · delaminatedFOUND LEADING EDGE AREA OF LEFT WING GEAR UPPER STRUT DOOR DELAMINATED. REPAIRED IAW SRM 51-40-15.SDR P5CA9600184Panel · crackedFOUND UNDERWING PANEL FORWARD OF LANDING GEAR DELAMINATED AND CRACKED. REPAIRED IAW SRM 51-40-09.SDR P5CA9600183Access Panel · delaminatedFOUND 5TH POD ACCESS PANEL AT UNDERWING ROOT DELAMINATED. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-44-02.SDR P5CA9600182Panel · brokenFOUND EDGE BROKEN ON UNDERWING REAR SPAR ACCESS PANEL. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-31-00.SDR P5CA9600027Skin · crackedFOUND ONE INCH CRACK ON LOWER FLANGE, MIDPOINT ON LEFT WING LEADING EDGE BETWEEN STA 570 TO 590. REPAIRED CRACK PER SRM 57-40-03.SDR P5CA9600185Panel · crackedFOUND OVERWING PANEL LEFT WING CRACKED. PANEL REPAIRED IAW SRM 51-40-09.SDR P5CA9600198Panel · puncturedFOUND VERTICAL FIN ACCESS PANEL PUNCTURED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 53-30-10.SDR P5CA9600175Skin · delaminatedFOUND RT INBOARD AFT FLAP DELAMINATED ON UPPER SKIN. REPAIRED IAW SRM 51-40-06.SDR P5CA9600169Cascade Vane · crackedFOUND NR 3 ENGINE LEFT HAND UPPERMOST CASCADE VANE CRACKED. BLENDING CARRIED OUT AND VANE REINSTALLED AS PER MM 78-32-04.SDR P5CA9600168Precooler Mount · crackedFOUND NR 3 PRECOOLER LOWER AFT MOUNT CRACKED. REPAIRED AS PER MM 36-10-02.SDR P5CA9600022Fuel Control · malfunctionedNR 4 ENGINE FLAME-OUT AT 29,000 FT, ATTEMPTED ENGINE RESTART, UNSUCCESSFUL. FLIGHT RETURNED TO MIAMI. REPLACED FCU, FUEL PUMP, TT2 SENSOR IAW MM 73-11 01 AND 73-21 01. LEAK CHECK AND RUNUP OK.SDR P5CA9600021Duct · crackedAFTER ENGINE START, WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO BLOCKS. FOUND LEADING EDGE PNEUMATIC DUCT INBOARD OF NR 2 ENGINE CRACKED. REPLACED DUCT ASSEMBLY, INSPECTED AND LEAK CHECKED IAW MM 36-10-00.SDR P5CA9600201Door · delaminatedFOUND NR 2 AFT FAIRING DOOR DELAMINATED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 54-32-01.SDR P5CA9600200Fairing · crackedFOUND NR 1 T/E FLAP TRACK MOVEABLE CANOE FAIRING CRACKED AT TWO LOCATIONS. REPAIRED IAW SRM 51-40-09.SDR P5CA9600196Strut · brokenFOUND LOWER HORIZONTAL STRUT FOR POTABLE WATER TANK BROKEN. NEW STRUT INSTALLED IAW IPC 38-11-02.
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