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 P5CA9701360Reveal Panel · crackedMAIN DECK L-5 DOOR FORWARD LOWER CORNER CUT OUT REVEAL PANEL CRACKED. REPLACED PANEL PER BOEING SRM 51-10-01.SDR P5CA9701331Beam · corrodedLEVEL 2 CORROSION, MAIN DECK L-4 DOOR BEAM CORROSION/CRACK REVEAL DURING LOWER GATE ASSY. REPLACED L-4 DOOR LOWER BEAM.SDR P5CA9701329Skin · crackedLEVEL 2 CORROSION, NR 1 PYLON INBD SKIN UNDER DOUBLER HAS CRACK AND CORROSION AT NAC STA 180 WATER LINE 140.2. REPAIRED IAW SB 747-54-2034 FIG 5.SDR P5CA9701325Frame · crackedNR 4 PYLON INBD AND OUTBD FRAME AT NAC/STA 162 WL 150 HAVE INCORRECT REPAIR, INBD FRAME IS CRACK AND THERE ARE MISSING AND INCORRECT FASTENER AT THE SAME LOCATION. REPLACED FRAME.SDR P5CA9701324Bulkhead Tee · crackedCRACK FOUND BY NDT METHOD AT THE FASTENER HOLE, NR 1 PYLON AFT BULKHEAD RT SIDE 'T' CHORD. REPLACED 'T' CHORD.SDR 97UAL900517Line · leakingLOSS OF ALL HYDRAULIC FLUID ON NR 1 SYSTEM. *S/D* LEAKING LINE, REPLACED LINE AND UNION.SDR P5CA9701366Bulkhead · crackedFORWARD CARGO BS 400 LBL 90 BULKHEAD CRACKED NOSE TUNNEL BS 400 RT SIDEWALL AREA BULKHEAD WEB CRACKED AT RBL 90 APPX. REPAIRED CUTOUT PER SB 747-53-2095.SDR P5CA9701349Skin · delaminatedLHW NR 3 SPOILER OUTBD AFT CORNER SKIN LIFTED UP, LHW NR 3 SPOILER OUTBD MIDDLE SURFACE FOUND DELAMINATED. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.SDR P5CA9701348Skin · delaminatedLHW NR 2 SPOILER CENTER SURFACE AREA DELAMINATED. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.SDR P5CA9701347Skin · delaminatedRHW NR 8 SPOILER OUTBD SURFACE FORWARD CORNER AREA FOUND DELAMINATION RHW NR 8 SPOILER AFT EDGE LIFTED UP OUTBD TO CENTER INBD TO INBD CORNER AREA. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.SDR P5CA9701334Floor Beam · crackedAFT CARGO FLOOR SUPPORT CRACK AT BS 1860 LBL 5. REPAIRED FLOOR SUPPORT PER BOEING SRM 51-40-04.SDR P5CA9701332Floor Beam · crackedFORWARD CARGO FLOOR SUPPORT FOUND CRACKED AT BS 620 LBL 6. REPAIRED FLOORBEAM PER BOEING SRM 51-40-04 FIG. 2, AFTER TRIM OFF CRACKED AREA.SDR P5CA9701323Skin · crackedLEVEL 2, CORROSION FOUND FUSELAGE BS 540 STR 46R - 47R FUSELAGE SKIN BULGED. REPAIRED SKIN PER RS 53-21-33431.SDR P5CA9701322Fitting · crackedCRACK FOUND AT BS 1900 AFT CARGO DOOR AFT ROTARY ACTUATOR SUPPORT BEAM. REPLACED FITTING.SDR P5CA9701319Longeron · crackedCRACK FOUND FROM BS 1457-1467 10, LEFT OVERWING LONGERON (FUSELAGE). REPAIRED LONGERON AS PER BOEING SRM 53-10-10 FIG 1.SDR P5CA9701318Bulkhead Chord · crackedCRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS FORWARD CARGO COMPARTMENT, BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46R TO S-47R, STOP DRILLED AS PER SB 747-53-2316.SDR P5CA9701317Frame · crackedCRACK FOUND MAIN DECK R-2 DOOR FORWARD LOWER CORNER DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.SDR P5CA9701316Frame · crackedCRACK FOUND MAIN DECK R-4 DOOR AFT LOWER CORNER DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.SDR P5CA9701315Frame · crackedCRACK FOUND AT FORWARD LOWER CORNER, MAIN DECK L-3 DOOR FORWARD DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.SDR P5CA9701314Buklhead Chord · crackedCRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS, FORWARD CARGO COMPARTMENT BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46L AND S-47L. STOP DRILLED AS PER SB 747-53-2316.SDR P5CA9701313Frame · crackedCRACK FOUND AT FORWARD LOWER CORNER, MAIN DECK L-3 DOOR FWD DOOR FRAME. REPAIRED PER BOEING SRM 52-10-02 FIG 8.SDR P5CA9701312Bulkhead Chord · crackedCRACK FOUND APPX 1.25 INCH LONG ALONG RADIUS, FORWARD CARGO COMPARTMENT, BS 1000 BULKHEAD LOWER CHORD BETWEEN S-46L AND S-47L. STOP DRILLED PER SB 747-53-2316.SDR P5CA9701365Fitting · crackedL-3 DOOR FORWARD CUTOUT NR 4 STOP FITTING CRACK FOUND. REPLACED FITTING PER BOEING SRM 51-10-01.SDR P5CA9701364Fitting · crackedR-3 DOOR FORWARD CUTOUT NR 4 STOP FITTING CRACK FOUND. REPLACED FITTING PER BOEING SRM 51-10-01.SDR P5CA9701351Skin · delaminatedLHW NR 5 SPOILER AFT EDGE OUTBD TO CENTER AREA FOUND DELAMINATION AND LIFTED UP, LHW NR 5 SPOILER INBD FORWARD TOP CORNER AREA FOUND DELAMINATED. HOT BONDED CARRIED OUT PER BOEING SRM 51-40-06.SDR P5CA9701350Skin · delaminatedRHW NR 7 SPOILER INBD AFT CORNER LIFTED UP. HOT BONDED CUT OUT PER BOEING SRM 51-40-06.SDR P5CA9701321Skin · scratchedSCRATCH MARK FOUND FUSELAGE BS 430-440 STR 45R SKIN. REPAIRED SKIN PER BOEING SRM 53-30-03 FIG 1 AT BS 430-440 S45R.SDR P5CA9701320Stringer · corrodedLEVEL 2, CORROSION FOUND FWD CARGO COMPARTMENT, BS 995 STR 44R STR. REPAIRED STRINGERS PER BOEING SRM 53-10-03 FIG 1 AT BS 980-996 STR 44R AREA.SDR 97ZZZX4293Connector · miswiredAPPARENT MALFUNCTION DETECTED DURING OPERATIONAL CHECKS OF THE ENGINE FUEL SHUT OFF VALVES. IT WAS NOTICED THE INDICATOR LIGHTS DID NOT RESPOND TO MOVEMENT OF THE ENGINE START LEVERS ON THE PEDESTAL; WHEREAS, NORMAL RESPONSE WAS OBSERVED DURING OPERATION OF TSDR 97ZZZX4292Connector · miswiredAPPARENT MALFUNCTION DETECTED DURING OPERATIONAL CHECKS OF THE ENGINE FUEL SHUT OFF VALVES. IT WAS NOTICED THE INDICATOR LIGHTS DID NOT RESPOND TO MOVEMENT OF THE ENGINE START LEVERS ON THE PEDESTAL; WHEREAS, NORMAL RESPONSE WAS OBSERVED DURING OPERATION OF TSDR P5CA9701274Door · delaminatedDELAMINATION OF PREVIOUS REPAIR ON RIGHT WING GEAR STRUT DOOR. REPAIRED PER BAC SRM 51-40-06.SDR P5CA9701273Skin · puncturedPUNCTURE IN LOWER SURFACE OF LEFT INBOARD FORE FLAP. REPAIRED WITH FIBERGLASS OVERLAY PER BAC 51-40-15.SDR P5CA9701272Panel · damagedDAMAGED RIGHT WING ROOT LEADING EDGE PANEL. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09.SDR P5CA9701271Fire Bottle · crackedCRACKED MOUNTING LUG ON NR 1 ENGINE RIGHT FIRE BOTTLE. REPLACED NR 1 ENGINE RIGHT FIRE BOTTLE PER BAC MM 26-21-03.SDR P5CA9701280Panel · damagedDAMAGED ON NR 3 SPOILER PANEL. REPAIRED WITH FILLER AND DOUBLER PER BAC SRM 51-40-06.SDR P5CA9701278Panel · crackedCRACK ON BOTTOM OF RIGHT WING LEADING EDGE PANEL AT WS 807. REPAIRED PER BAC SRM 51-40-09.SDR P5CA9701277Trunnion · corrodedLEVEL 1 CORROSION ON THE LEFT BODY GEAR TRUNNION. REMOVED LIGHT SURFACE CORROSION PER BAC OHM 32-00-05.SDR P5CA9701276Door · delaminatedDELAMINATION ON RIGHT WING GEAR FLYING DOOR. REPAIRED PER BAC SRM 51-40-06.SDR P5CA9701275Angle · corrodedLEVEL 2 CORROSION ON LOWER T-ANGLE AROUND LAV PAN AT RIGHT BL 40. FABRICATED AND INSTALLED NEW T-ANGLE PER BAC SRM 51-40-04.SDR P5CA9701289Fairing · delaminatedDELAMINATION ON RIGHT AFT FAIRING PANEL 194DR. REPAIRED PER BAC SRM 51-40-09.SDR P5CA9701284Panel · delaminatedDELAMINATION ON RIGHT WING PANEL 621FT. REPAIRED PER BAC SRM 51-40-12.SDR P5CA9701283Hinge Panel · corrodedBULGED HINGE PANEL ON LEFT NOSE LANDING GEAR STRUT DOOR AFT INBOARD CORNER. FOUND LOOSE FASTENERS AND LEVEL 1 CORROSION. REMOVED CORROSION, RETREATED AND CLOSED PER BAC SRM 51-10-01, 51-10-02 AND 51-30-00.SDR P5CA9701282Fairing · delaminatedDELAMINATION ON RIGHT AFT FAIRING PANEL 194FR. REPAIRED PER BAC SRM 51-40-09.SDR P5CA9701281Skin · corrodedBULGED SKIN AT BS 1963, BL 26. LAP SEAM OPENED, FOUND ONLY LEVEL 1 SURFACE CORROSION. REMOVED CORROSION, RETREATED AND CLOSED PER BAC SRM 51-10-01 AND 51-10-02.SDR P5CA9701279Panel · corrodedLEVEL 1 CORROSION ON INBOARD FUSELAGE PANEL FORWARD OF RIGHT WING GEAR. REMOVED CORROSION AND RETREATED PANEL PER BAC SRM 51-10-06 AND 51-10-02.SDR P5CA9701188A13 Fire Card · failedSHORTLY AFTER TAKEOFF, NR 1 ENGINE FIRE WARNING B-LOOP INDICATED FIRE. A-LOOP WAS INTERMITTENT CAUSING FIRE WARNING NR 1 ENGINE SHUT DOWN. MEGGED LOOPS A AND B FROM FIRE WARNING CONTROL MODULE CHECKS GOOD. CHECKED WIRING AND LOOPS ON ENGINE, CHECKED GOOD. SDR P5CA9701269Bulkhead Tee · corrodedLEVEL 1 CORROSION NR 2 PYLON TORQUE B/HEAD T-CHORDS HAVE LIGHT SURFACE AT NAC STN 301 NAC WL 296 TO 288 APPROX. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. AD: NR 94-15-18.SDR P5CA9701268Stringer · corrodedLEVEL 1 CORROSION FWD CARGO COMPT BS 995 STR 44R STRINGER. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.SDR P5CA9701267Frame · corrodedLEVEL 1 CORROSION FX PNL 192ER FAIRING SUPPORT ANCHOR NUTS AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.SDR P5CA9701266Frame · corrodedLEVEL 1 CORROSION FX BODY FAIRING SUPPORT BTN 191EL AND 191HL A FLOAT NUT AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02.
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