Boeing 747-230B
Service difficulty reports · 618
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 = '747230B' 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 = '747230B' 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 EIA2006366Terminal · smokeON APPROACH CAPT NOTICED SMOKE BY L1 WINDOW AT TERMINAL, TURNED OFF WINDOW HEAT AND SMOKE WENT AWAY. REPLACED TERMINAL WHICH APPEARED VERY WORN AND CORRODED. SYSTEM CHECKED OUT GOOD PER MM 56-11-01.SDR EIA2006240Line · leakingUPON ARRIVAL AT ANC NR 4 ENG OIL QUANTITY LOW. TROUBLESHOOTING FOUND LEAK AT MANIFOLD, TRYING TO DETERMINE WHICH LINE.SDR EIA2006228Wire · looseRIGHT EMERGENCY EXIT SIGN ABOVE UPPER DECK RIGHT DOOR INOP. FOUND GROUND WIRE AT LIGHT ASSY STUD LOOSE TIGHTENED SAME PER STD PRACTICE MANUAL CH 20, OPS CHECKED PER MM 33-51-00.SDR EIA2006227Light · inoperativeEMERGENCY LIGHTS INOP AT TOP OF STAIRS TO COCKPIT. REMOVED AND REPLACED EMERGENCY LIGHT AT TOP OF STAIRS PER MM 33-51-00, OPS CHECKED GOOD.SDR UIEA200600213Panel · delaminatedRIGHT WING, INBOARD LEADING EDGE WING PANEL AT WING STATION 248.81 TO 268.81, INNER SKIN HAS AREA OF COMPOSITE DELAMINATION 20.0 INCH LONG BY 22.0 INCH WIDE. ACCOMPLISHED INTERIM REPAIR OF AREA AS PER ATLAS XEO 57-081706. REQUIRES REPEAT INSPECTIONS AT EVERYSDR UIEA200600212Panel · crackedRIGHT WING FIXED TRAILING EDGE PANEL AT WBL 445.9 OUTBOARD AFT END OF PANEL HAS 1.0 INCH LONG CRACK AND LOWER AREA HAS AREA OF DETERIORATION. ACCOMPLISHED PREPREG 250 DEGREES PERMANENT REPAIR OF AREAS AS PER 747 SRM 51-40-09 AND 51-40-12.SDR UIEA200600193Panel · failedATB, DUE TO A/P A&B WOULD NOT ENGAGE. OVERWEIGHT LANDING AT 287.8. REMOVED AND REPLACED P-10 PANEL PER AMM 22-11-06 ALL OPS OK. RAMP DOWN TEST OK PER AMM 22-10-00. ACCOMPLISHED OVERWEIGHT INSP AS PER AMM 5-51-39.SDR EIA2006112Csd · malfunctionedNR 3 ENG CSD HIGH OIL TEMP INDICATION, CSD WILL NOT DISCONNECT, NR 3 ENG SHUTDOWN.SDR EIA2006092Indication Sys · unknownRETURNED TO BLOCKS DUE TO NR 2 ENG LOSS OF N2 INDICATION INDICATOR AND TRANSMITTER CHANGED, NO HELP. PARTS SENT TO HKG FOR REPAIR.SDR UIEA200600161Valve · leakingWHILE CRUISING AT FL LEVEL 310, NR 3 ENG OVERHEAT LIGHT CAME ON. ACCOMPLISHED PROCEDURES AS PER FHB 3.35.5.6. OVERHEAT LIGHT EXTINGUISHES WHEN THROTTLE WAS RETARDED, ALSO WITH THE BLEED AIR VALVE SWITCH IN CLOSED POSITION VALVE LIGHT FAILED TO COME ON. THERSDR P5CA0601487Indicator · stickingON TAXI, OUTBOARD FLAP INDICATOR WITH 20 FLAPS SELECTED. RT FLAPS INDICATES 20 DEGREES, LT FLAP INDICATES 25 DEGREES. REPLACED FLAP INDICATOR PER AMM 27-58-00. OPS CHECK OK.SDR EIA2006230Skin · crackedNR 4 PYLON, NAC STA. 247, NR 3 STIFFENER AND SKIN CRACKED. FABBED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2 (MZJ).SDR EIA2006231Skin · crackedNR 3 PYLON, NAC STA. 247, NR 3 STIFFENER AND SKIN CRACKED. FABBED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2 (MZJ).SDR EIAA200605001Skin · crackedNR 3 PYLON, NAC STA. 247, NR 3 STIFFENER AND SKIN CRACKED. FABED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2 (MZJ).SDR EIA2006229Skin · crackedNR 2 PYLON, NACELLE STATION 247, NR 3 STIFFENER AND SKIN, CRACKED. FABED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2.SDR EIA2006096Skin · crackedNR 1 PYLON, NAC STA 247 NR 3 STIFFENER AND SKIN CRACKED. FABBED & INSTALLED REPAIRS PER ECRA 489-54-007-2.SDR EIA2006079Fuse · malfunctionedDURING A-CHECK F/E STATION EMERGENCY LIGHT INOP. RESEATED ALL 3 FUSES, OPS CHECK GOOD PER MM 33-51-00.SDR EIA2006074Pdu · malfunctionedAIRCRAFT RETURNED TO BLOCKS FOR GROUP 2 LE FLAP INDICATION INTERMITTENTLY FLICKERS FROM IN-TRANSIT TO DOWN. REPLACED NR 2 LT LEADING EDGE PDU PER MM 27-81-03, OPS CHK OK PER MM 27-81-00SDR EIA2006067Metering Valve · dirtyON TAKEOFF ROLL, AIRCRAFT PULLING TO THE RIGHT. INSPECT LANDING GEAR BRAKE ASSEMBLY PER MM 52-41-15, OPS CHK OK FOR APPLY AND RELEASE OF BREAKS. RT METERING VALVE FOUND DIRTY, PLUNGER STICKY. CLEANED AND LUBRICATED, GAP CHECKED PER MM 32-41-03. NLG CHECKEDSDR EIA2006097Skin · crackedNR 4 PYLON UPPER SKIN AND SIDE FRAMES CRACKED. REMOVED DAMAGE, HFEC THE AREA, FABBED AND INSTALLED REPAIR PER ECRA 489-54-003-2.SDR UIEA200600092Skin · ground damageBETWEEN STA 270 AND STA 300 ON RT SIDE, DAMAGE CAUSED TO THE SKIN BY CATERING TRUCK BOOT. THE DAMAGE IS AFT OF THE LWR PITOT PROBE TO FWD OF AOA SENSOR. AREA OF DAMAGE IS 12 INCHES BY 5 INCHES, AND A 3 INCHES BY 3 INCH DENT WITHIN THE RVSM AREA. THE SKIN WASDR 200600092Structure · ground damageDURING GROUND HANDLING, AIRCRAFT WAS STRUCK ON THE RT SIDE OF THE FUSELAGE, FWD OF THE AOA SENSOR AND BEHIND THE LOWER PITOT PROBE. CAUSED A DENT 12 INCHES LONG, BY 5 INCHES WIDE. A FURTHER DENT WAS CAUSED IN THE RVSM AREA, JUST AFT OF THE LWR PITOT PROBE.SDR EIA2006101Door Frame · crackedFOUND 3 HOLES CRACKED R5 DOOR FRAME BS 2231. FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-04 FIG 115 PG'S 689-705 AND EO 53-747-1601 REV D SEP 16.SDR P5CA0601476Indicator · stuckCREW REPORTED LEFT HAND AILERON INDICATOR STUCK IN FULL DOWN POSITION. TRANSFERRED TO DMI 35831 PER MEL 27-01.SDR EIA2006104Floorbeam · damagedFOUND BS 2020 RBL 120 FLOORBEAM UPPER TEE HAS ELONGATED HOLE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 53-10-07 FIG 12.SDR P5CA0601474Circuit Card · looseCREW REPORTED ON ENGINE START, NR 4 ENGINE -B- LOOP HAD INTERMITTANT WARNING. NR 4 ENGINE -A- LOOP ON MEL. RESEATED FIRE WARNING CARD, OPS NORMAL PER 26-12-00.SDR EIA2006102Skin · brokenNR 2 PYLON I/B NAC STA 286 LOWER ACCESS DOOR AREA CUTOUT HAS BROKEN EDGE. REMOVED AND REPLACED DAMAGE, NDT AREA, FABBED AND INSTALLED DOUBLER PER SRM 54-30-03 FIG 17B.SDR EIA2006100Stringer · gougedFOUND BS 280, STR 34L GOUGED ON BOTTOM AROUND FASTENERS AND FLANGE BENT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-30-02 PAGE 8, 9 AND 32, 51-20-01, 51-30-05 PAGE 5, 6 AND 9 AND 51-10-02 PAGE 7.SDR EIA2006098Stringer · tool damageFOUND BS 300 STRINGER 14L HAS TOOL MARK AND CRACK. REMOVED AND REPLACED STRINGER PER B747 SRM 51-30-02.SDR EIA2006099Unknown · lightning strikeFOUND LIGHTNING STRIKE BS 420 - 440 STR 0 1R HAS BLIND RIVET INSTALLED. FABBED AND INSTALLED CAT A REPAIR PER B747 SRM 53-30-03 FIG 4B.SDR EIA2006103Stringer · crackedFOUND BS 520 STR 29L LWR CARGO AREA HAS CRACKED FLANGE. REMOVED DAMAGE STRINGER STA 520 - 548 STR 29L FABBED AND INSTALLED STRINGER AND SPLICE PER B747 SRM 53-10-03 FIG 1 DETAIL II.SDR P5CA0601472Warning Flag · false indicationFLT CREW ADVISED F/O'S AIRSPEED IND HAS FLAG IN VIEW. CYCLED POWER, ALL OPS AND IND CHECK OK ATA 34-13-00. ALSO CLEANED CONNECTOR PINS.SDR EIA2006045Indicator · inoperativePRIOR TO TAKEOFF, RT OUTBOARD AILERON SPI INDICATOR INOP.SDR P5CA0601460Actuator · crackedCREW REPORTED DURING CRUISE, NR 1 HYDRAULIC SYSTEM LOST ABOUT 1 GALLON IN 1 HOUR. TURNED ADP OFF AND EDP TO DEPR PER CHECKLIST. FOUND LEFT CCA LEAKING. REPLACED LEFT CCA IAW AMM 27-61-08. CHECKED FOUND ALL WORKING. ADDED HYDRAULIC FLUID TO SYSTEM NR 1 IAWSDR P5CA0601458Relief Valve · failedCREW REPORTED ON CLIMB, NR 2 ENGINE NACELLE TEMP WENT TO 9.0. AFTER RETARDING THROTTLES, TEMP STABILIZED. REPLACED NR 2 ENGINE RELIEF VALVE; APPARENT SPRING FAILURE. OPS NORMAL.SDR P5CA0601457Connector · failedRIGHT OUTBOARD AILERON CONTROL SURFACE POSITION INDICATED DROOPING. PERFORMED VISUAL INSPECTION OF RIGHT OUTBOARD AILERON; VERIFIED PROPER MOVEMENT, ENTERED IN LOGBOOK. RELEASED ON MEL. REMOVED AND INSTALLED CONNECTOR DT488 AND RIGHT AILERON POSITION INDICASDR UIEA200600049Panel · crackedRT WING FIXED UPPER T/E PANEL HAS A SMALL CRACK. REPAIRED IAW SRM 51-40-12 REPAIR 4A AND 51-40-14 REPAIR 4L.SDR UIEA200600048Structure · crackedLT BODY GEAR WHEEL WELL - FOUND OUTBOARD STRUT DOOR SUPPORT STRUCTURE CRACKED AT SEVERAL SPOTS ON I/B AFT SIDE BS 1480. REPAIRED BY REPLACEMENT OF CHORD IAW SRM 51-30-02 FIG 3.SDR UIEA200600047Skin · crackedLT BODY GEAR WHEEL WELL - WTB FAIRING SKIN HAS A CRACK AT BS 1480 WL 86. REPAIRED SKIN IAW SRM 51-40-02.SDR UIEA200600046Bolt · crackedLT BODY GEAR - TRUCK PIVOT BOLT FAILED MAGNETIC PARTICLE INSPECTION. REPLACED TRUCK PIVOT BOLT IAW MM 32-13-02.SDR UIEA200600044Frame · crackedBS 800 LT FRAME, FOUND A CRACK INDICATION IN THE INNER CHORD INBOARD STRAP ABOVE STRINGER 17L. REPAIRED BY REPLACEMENT OF INNER STRAP, PER BOEING DRAWING 65B05002 AND SRM 51-30-02.SDR UIEA200600043Rib · crackedLT WING UPPER FIXED TRAILING EDGE PANEL OUTBOARD SUPPORT RIB HAS A CRACK IN THE WEB. REPAIRED IAW SRM 51-40-02 FIG 1.SDR UIEA200600042Stiffener · crackedBULK CARGO COMPARTMENT FLOOR LONGITUDINAL STIFFENER AT BL 0 HAS A CRACK AT BS 2040. REPAIRED STIFFENER IAW SRM 53-10-07 FIG 20.SDR UIEA200600041Pressure Panel · crackedLT WLG WELL - FOUND A SMALL CRACK IN THE CANTED PRESSURE PANEL AT BS 1241. REPAIRED IAW SRM 53-10-07 FIG 6.SDR UIEA200600040Skin · crackedLT WING OUTBOARD AFT-FLAP HAS SMALL CRACKING IN T/E UPPER AND LOWER SURFACES. REPAIRED IAW SRM 51-40-15 PARA 4N.SDR UIEA200600039Skin · delaminatedRT WING GEAR LOWER STRUT DOOR HAS DELAMINATION. DOOR REPAIRED IAW SRM 51-40-24 FIG 2.SDR UIEA200600038Shim · brokenLT LGW FOUND PART OF SHIM BROKEN OFF FROM OVERWING LONGERON ST BS 1241 LBL 27. ACCOMPLISHED RETORQUE OF EFFECTED FASTENERS IAW 51-30-04 PG 9. RETORQUE CHECK REQUIRED BY SRM 51-10-10 PG 3 TO BE TRACKED ON ATLAS EO XEO 53-031406.SDR UIEA200600037Skin · dentedEXTERNAL FUSELAGE FOUND DENTS BETWEEN BS 1840 AND 1860 JUST BELOW STRINGER 34L. REPAIRED SKIN IAW SRM 53-30-03 FIG 1.SDR UIEA200600036Structure · crackedRT WING OUTBOARD T/E MID-FLAP HAS A CRACK IN COMPOSITE STRUCTURE APPROX 25 INCHES LONG. REPAIRED IAW SRM 51-40-12 PARA 4D AND FIG 11.SDR UIEA200600035Skin · erodedLT WING LEADING EDGE VCF PANEL NR 10 UPPER SIDE HAS EROSION DAMAGE. REPAIRED PANEL NR 10 IAW OHM 57-55-22 AND SRM 51-40-14 PARA 4K AND FIG 16.
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