Boeing 747-47UF
Service difficulty reports · 3,116
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 = '74747UF' 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 = '74747UF' 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 UIEA2012121900555Line · leakingOIL QTY OF NR 4 ENGINE WENT TO ZERO. SHUTDOWN ENGINE IAW QRH. PERFORMED ENGINE INSPECTION IAW AMM 79-00-00/601. ACCOMPLISHED ENGINE WINDMILLING INSPECTION IAW AMM 72-00-00/601. DURING ENGINE INSPECTION, THE OIL PRESSURE TRANSMITTER WAS FOUND TO BE LEAKING. SDR UIEA2012121700553Valve · malfunctionedMX PICKUP SMOKE OVERRIDE VALVE OPEN. REMOVED VALVE FOR TROUBLESHOOTING, FOUND BUTTERFLY SHAFT SHEARED. INSTALLED SMOKE/OVERRIDE VALVE IAW MM 21-58-06. GROUND TEST - OK IAW TASK 21-58-00-705-001.SDR UIEA2012121500548Shaft · shearedMX PICKUP SMOKE OVERRIDE VALVE OPEN. REMOVED VALVE FOR TROUBLESHOOTING. FOUND BUTTERFLY SHAFT SHEARED. INSTALLED SMOKE/ OVERRIDE VALVE IAW MM 21-58-06. GROUND TEST OK IAW MM TASK 21-58-00-705-001.SDR UIEA2012120300538Stiffener · damagedDAMAGE TO MAIN DECK TO UPPER DECK STOWABLE CREW LADDER HAND RAIL SUPPORT STIFFENER. ACCOMPLISHED TIME LIMITED REPAIR.SDR UIEA2012112100532Trans Panel · damagedDURING MX WALKAROUND, FOUND LIGHTNING STRIKE DAMAGE TO THE NR 3 ENGINE RT THRUST REVERSER TRANSLATING COWL, REPAIRED IAW CMM 78-32-31, REPAIR 023.SDR UIEA2012111500528Power Supply · inoperativeEMERGENCY LIGHTS ON UPPER DECK INOPERATIVE AT BS 410, 587, 550. R & R EMERGENCY BATTERY POWER SUPPLY M 5170. OPS CHECKED OK IAW AMM 33-51-04.SDR UIEA2012111300523Wedge · damagedRT INBD AND OTBD T/E ELEVATOR WEDGE DAMAGED. THE DAMAGE IS MEASURED AS 6.0" X 6.0"AND 5.0" X 6.0" . DAMAGE IS BEYOND THE ALLOWABLE LIMITS OF SRM 55-20-01, FIG 101. PERFORMED A PERMANENT REPAIR IAW SRM 55-20-01-2R-1, FIG 201, SHEET 1 AND 2, 250*F CURE IAW SRMSDR UIEA2012110900520Nose Cowl · deformedAFTER TAKEOFF AT AROUND 1000 FT AGL, LARGE BIRD STRIKE ON NR 4 ENGINE NACELLE L/E. FOUND NOSE COWL L/E 2 O'CLOCK POSITION DEFORMED. PERFORM NR 4 ENGINE BOROSCOPE INSPECTION ON HPC STAGE 1 AND 12. BIRDSTRIKE CONDITIONAL INSPECTION CARRIED OUT IAW AMM 05-51-1SDR UIEA2012103000499Depressor · damagedAFT CARGO DOOR BS 1810 SEAL DEPRESSOR FOUND (REF FIG 1), MEASURING 1.5" AND LOCATED AT THE SEAL DEPPRESSOR SPLICE AREA. DAMAGE WAS DETERMINED TO BE BEYOND THE REPAIR LIMITS IAW THE SRM 53-00-15, FIG 201, REPAIR 2. REPAIRED IAW EO 4453A784.SDR UIEA2012102200490Heat Shield · damagedDURING REPLACEMENT OF THE NR 2 ENGINE, THE NR 2 STRUT LOWER WEB INSULATION BLANKET, "HEAT SHIELD" WAS FOUND WITH MISSING MATERIAL ON ACFT. MADE A TIME LIMITED REPAIR.SDR UIEA2012101400473Skin · crackedCRACK ON THE NR 1 ENGINE LT THRUST REVERSER TRANSLATING COWL OUTER SKIN. PERFORM A TIME LIMITED REPAIR.SDR UIEA2012101500476Bulb · inoperativeMAIN DECK ZONE A CEILING LIGHT FOUND INOPERATIVE. BULB REPLACED AND TESTED OK MM 33-51-07.SDR UIEA2012101200469Fire Loop · failedSTATUS MESSAGE CARGO FIRE MAIN DECK LOOP B, FAILED. R & R MAIN DECK SMOKE DETECTOR 7B IAW MM 26-14-01, OPS CK OK IAW MM 26-14-001.SDR UIEA2012100200448Ball Screw · damagedDURING ROUTINE INSPECTION OF NR 1 THRUST REVERSER, MX FOUND THE THRUST REVERSER NOT STOWING. FURTHER INSPECTION FOUND UPPER BALLSCREW ACTUATOR AT FAULT WITH THE BOLTS AT THE GIMBAL SHEARED. PEFORMED A DETAILED INSPECTION OF THE REVERSER HALF IN QUESTION INCLUSDR UIEA2012100100447Skin · damagedNR 1 FLAP TRACK FAIRING HAS DAMAGE TO THE SKIN, MEASURING 5.375 INCHES LONG, BY 2.5 INCHES WIDE. DAMAGE IS BEYOND THE LIMITS OF SRM 57-53-70, FIG 101 ALLOWABLE DAMAGE 1 AND SRM 51-70-02, FIG 101 ALLOWABLE DAMAGE GENERAL. REPAIRED IAW EO 4457A433.SDR UIEA2012100100446Skin · crackedA CRACK WAS FOUND AT THE FUSELAGE SKIN, AFT CARGO DOOR CUTOUT FORWARD EDGE NEAR BS 1810 BETWEEN S-38R AND S-39R. DAMAGE IS BEYOND THE SRM 53-00-01 ALLOWABLE DAMAGE LIMIT. REPAIRED IAW EO 4453A744 OF N453PA.SDR UIEA2012092400442Cam · detachedPOST FLIGHT WALK AROUND INSPECTION, FOUND NR 4 T/E FLAP TRACK FAIRING DAMAGED BY FLAP DRIVE CRANK. FURTHER INSPECTION FOUND THE CAM DRIVE DETACHED FROM MID-FLAP. LT MID-FLAP ASSY AND NR 4 T/E FLAP TRACK FAIRING WAS REPLACED AND RIGGED IAW AMM 27-51-01 AND AMSDR UIEA2012091800436Sleeve · crackedNR 2 ENGINE EXHAUST NOZZLE OUTER SLEEVE FOUND CRACKED. DISPOSITION IS TO STOP DRILL THE ENDS OF THE CRACK WITH A 0.125" DIAMETER HOLE IAW PART 4 OF EO 4478A235.SDR UIEA2012091700426Exhaust Pipe · crackedTHERE IS A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE OF NR 2 ENGINE, APPROX 9 O'CLOCK TO 12 O'CLOCK POSITION (LT SIDE). THE CRACK IS APPROX 16" LONG AND IS 13" FROM AFT SIDE OF EXHAUST SLEEVE IAW SRM 54-41-30 THE DISTANCE BETWEEN THE CRACK AND THE EDGE IS OUT SDR UIEA2012091600421Structure · deformedMAIN DECK SIDE CARGO DOOR AREA BS 1780 AND 1920 SIDEWALL TRIM AND GUTTER DEFORMED. PERFORMED A TIME LIMITED REPAIR IAW EO 4425A319.SDR UIEA2012091000395Structure · damagedFOUND LIGHTNING STRIKE DAMAGE TO THE NR 2 ENG LT THRUST REVERSER TRANSLATING COWL. DAMAGE ON THE T/E. A TIME LIMITED REPAIR WAS ACCOMPLISHED AS DESCRIBED IN PART 1 OF EO 4478A233 AND FAA 8110-3.SDR UIEA2012090200376Sleeve · crackedA CRACK WAS FOUND ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX AT 1 O'CLOCK POSITION (RT SIDE) ON THE NR 3 ENGINE. THE CRACK IS APPROX 2.5" LONG AND IS 1" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 361.923. IAW SRM 54-41-30 THE DISTANCE BETWEEN TSDR UIEA2012090200375Sleeve · crackedDURING MX, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX AT 3 O'CLOCK POSITION (RT SIDE) ON THE NR 2 ENGINE. THE CRACK IS APPROX 3" LONG AND IS 1" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 361.923 . IAW SRM 54-41-30 THE DISTANCE BETSDR UIEA2012090700391Skin · corrodedRT INBT FORE FLAP LOWER SURFACE NEAR CENTER FORE FLAP TRACK AREA FOUND MINOR CORROSION. RT INBD FORE FLAP OTBD LOWER SURFACE PANEL REPLACED AND INSTALLED IAW SRM 51-10-02, SRM 51-40-02.SDR UIEA2012090700390Skin · damagedRT WING INBD MID FLAB ROLLER PLATES REPLACEMENT, SEVERAL FASTENER HOLES OF THE NOSE SKIN ARE FOUND LARGER THAN THAT CALLED OUT IN ATTACHED SB 747-57-2320, FIG 53. ALUMINUM FREEZE PLUGS INSTALLED AND FASTENERS INSTALLED IN OVERSIZED HOLE LOCATIONS IAW RS NR-5SDR UIEA2012090700386Skin · dentedSKIN DENT AFT OF FWD CARGO DOOR BETWEEN S38 - 39R, INSPECTION. SKIN PANEL REPAIRED IAW RS NO R53-20-37412.SDR UIEA2012082400367Skin · damagedDAMAGE TO THE FUSELAGE SKIN AFT OF BS 2598, WL 244 NEAR S26R; ACCOMPLISH A TIME LIMITED REPAIR IAW EO 4453A756.SDR UIEA2012090700388Shear Tie · damagedAFT CARGO FRAME SHEAR TIE, RIVET HOLE FOUND ELONGATED AT STA 1700 BETWEEN S-33R AND S-34R. FRAME SHEAR TIE REPAIRED IAW SRM 53-00-07-2R-3.SDR UIEA2012081800365Actuator · failedAFTER GEAR RETRACTION, EICAS MESSAGE, "GEAR DOOR" SYNOPTIC INDICATED LT MAIN GEAR DOOR NOT CLOSED, DUMPED FUEL AND RETURNED TO DEPARTURE. GROUND CHECK LOWER ACTUATOR; FLEX HOSES HAD NO PRESSURE UP. WING GEAR DOOR SEQUENCE VALVE REPLACED; RIGGED IAW MM 32-32SDR UIEA2012090700385Bulkhead Web · crackedBS 1480, RT BULKHEAD WEB FOUND CRACKED. BULKHEAD WEB REPAIRED IAW SRM 53-40-08-2R-1, REPAIR 1, FIG 201.SDR UIEA2012081300357Skin · delaminatedLT WING INBD T/E FWD FLAP DELAMINATED IN FWD EDGE AREA. TIME LIMITED REPAIRED ACCOMPLISHED IAW EO 4457A424 PART 1.SDR UIEA2012081300356Skin · delaminatedRT WING - INBD T/E FWD FLAP FWD EDGE FOUND DELAMINATED, APPROX 60", TIME LIMITED REPAIRED ACCOMPLISHED IAW EO 4457A424, PART 1.SDR UIEA2012081400360Door · damagedNR 3 THRUST REVERSER ACCESS DOOR WAS FOUND OPEN AND DAMAGED. ACCOMPLISHED A TIME LIMITED REPAIR IAW EO 4478A227 PART 1.SDR UIEA2012090700392Skin · damagedNR 2 PYLON PANEL 462EL ONE BOLT HOLE ELONGATED. NR 2 PYLON PANEL 462EL PATCH REPAIRED IAW RS NR R-54-00-37414, REV A.SDR UIEA2012080900349Door · damagedDURING WALKAROUND, FOUND TAIL STRIKE DAMAGE TO APU DOORS AND AFT SECTION OF DOORS. CHAPTER 5, "DRAGGED TAIL INSPECTION" WILL BE PERFORMED IAW AMM 05-51-36-202-001. ACFT INSPECTED IAW CHAPTER 5, AMM 5-51-36-202-001: DRAGGED TAIL INSPECTION". NO STRUCTURAL DASDR UIEA2012090700389Intercostal · crackedMAIN DECK BS 1220, RBL 107 BELOW FLOOR INTERCOSTAL WEB CRACKED. INTERCOSTAL REPAIRED IAW RS-R53-40-37426.SDR UIEA2012090700387Skin · crackedBS 980, STR 38L SKIN FOUND CRACK APPROX .0937" LONG. SKIN REPAIRED IAW SRM 53-20-01-2R-2, REPAIR 2, FIG 201.SDR UIEA2012090700384Tension Tie · crackedMAIN DECK LT BS 760 TENSION TIE, ONE HOLE FOUND CRACKED AT AFT CHANNEL APPROX 0.060" RUNNING UPWARD. AFT CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012090700383Channel · crackedMAIN DECK LT BS 720 TENSION TIE AREA, FOUND ONE HOLE CRACK AT AFT CHANNEL APPROX .030". AFT CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012090700382Tension Tie · crackedMAIN DECK RT BS 740 TENSION TIE AREA, ONE HOLE FOUND CRACKED AT FWD CHANNEL APPROX .040" RUNNING UPWARD. FWD CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012090700381Channel · crackedMAIN DECK RT BS 740 TENSION TIE AREA, ONE HOLE FOUND CRACKED AT AFT CHANNEL APPROX 0.040" RUNNING UPWARD. AFT CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012090700380Tension Tie · crackedMAIN DECK RT BS 760 TENSION TIE AREA, ONE HOLE FOUND CRACKED AT AFT CHANNEL APPROX .040" RUNNING UPWARD. AFT CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012080100338Fairing · damagedDAMAGE TO THE LEFT WING GEAR STRUT DOOR FAIRING TRAILING EDGE. SINCE DAMAGE EXCEEDS THE SRM 52-80-02, FIG 101, ALLOWABLE DAMAGE LIMITS, ALLOWABLE DAMAGE GENERAL DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR IAW PART 1 OF EO 4452A155 AND FAA 8110-3. DSDR UIEA2012072700333Oxygen System · malfunctionedEICAS-SUPERNUMERARY OXYGEN ON. MASKS DROPPED- NORM PRESSURE. CABIN ALT 5300'.SDR UIEA2012073000336Roller · looseLT WING INBD FOREFLAP, OTBD TRACK FWD UPPER FLIGHT LOAD ROLLER LOOSE WITH VERTICAL MOVEMENT WHEN TRACK GOES IN AND OUT. R & R BEARINGS IAW SB 747-57-2107; PERFORMED T/E SYSTEM OPS CHECK OK. FLAPS RETRACTION AND EXTENSION SEVERAL TIMES NORMAL IAW AMM 27-51-0SDR UIEA2012073000334Skin · chafedRIGHT WING OTBD FOREFLAP LEADING EDGE WITH CHAFING DAMAGE. PREPARED, CLEANED AND REPAIRED RIGHT OTBD FORE FLAP LEADING EDGE DAMAGE IN LOCATIONS WBL 820.750, 818.00 IAW SRM 57-53-01-2R-1. REPAIR 1, FIGURE 201 SHEETS 5, 6, 9, 10 IAW 250 F CORE SRM 51-70-02.SDR UIEA2012071700324Seat Track · crackedSEAT TRACK CRACKED, MAIN DECK LBL 11, APPROX FS 540. REMOVED CARGO SYS IN AREA OF SEAT TRACK DAMAGE IAW AMM 25-58-00-001. CUT OUT DAMAGED SECTION OF SEAT TRACK, LOCATED NEW SECTION OF SEAT TRACK. DRILLED, TRIMMED, TREATED, PRIMED NEW SEAT TRACK SECTION, SDR UIEA2012070900312Skin · delaminatedDELAMINATION FOUND ON L/E OF RT WING OTBD OF NR 3 ENGINE. PERFORMED TEMP REPAIR IAW EO 4457A420.SDR UIEA2012070900313Liner · damagedNR 3 ENGINE INTAKE OUTER LINER SEGMENT AT 12 O'CLOCK POS, MINOR DAMAGE SIZE .5 X .5". ACCOMPLISHED EO 4472A095, PART 1 TIME LIMITED REPAIR IAW AMM 20-60-07.SDR UIEA2012070700311Oil System · lowOIL QTY FOR NR 2 ENGINE CONTINOUSLY DROPPING BELOW NORMAL TO MAGENTA -14 QTS. OIL LEVEL RETURNED TO 17 AFTER SHUTDOWN, ALL INDICATIONS NORMAL.
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