Boeing 747-46NF
Service difficulty reports · 1,079
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 = '74746NF' 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 = '74746NF' 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 UIEA2025071200935Tension Tie · crackedUPPER DECK LH BS900 TENSON TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE FWD CHANNEL PERFORMED INTERIM REPAIR AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200936Tension Tie · crackedUPPER DECK LH BS940 TENSION TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE FWD CHANNEL PERFORMED INTERIM REPAIR AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200938Tension Tie · crackedUPPER DECK LH BS820 TENSION TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200939Skin · damagedNR 4 NACELLE NOSE COWL LIP SKIN INTERIOR SURFACE 1 EA FASTENER HOLE ELONGATED. ELONGATE FASTENER HOLE AREA REPAIRED AS PER ATLAS EA-1971A218 REV. 0. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200940Skin · damagedLEFT WING L/E FIXED FAIRING BETWEEN INBD ILES 630.46 TO ILES 693.5 SEVERAL FASTENER HOLES FOUND ELONGATED. L/E SKIN REPAIRED AS PER RI-57-41-17749 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071300942Web · crackedLEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 WEB CRACKED. WEB CRACK AREA REPAIRE AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071300943Beam · crackedLEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 UPPER CHORD CRACKED. UPR CHORD CRACK AREA REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071300944Beam · crackedLEFT WING L/E FIXED LOWER BEAM CRACK L/E ILES 693.5 AREA. BEAM REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071300945Splice Strap · crackedLEFT WING L/E FIXED SPLICE STRAP-LOWER CRACK AT INBD ILES 693.5 AREA. SPLICE STRAP-LOWER CRACK AREA REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025051200602Skin · damagedLH INBOARD AFT FLAP DAMAGE OUT OF LIMITS 12" LENGTH AND 9" WIDTH UPPER SURFACE AND 10" LENGTH AND 5" WIDTH LOWER SURFACE.(<P>PERFORMED PERMANENT REPAIR IAW EA-1957A224, SRM 57-53-01-2R-1 AND SRM 51-70-07-0G-0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025042600572Control Unit · failedRIGHT MAIN BODY GEAR TIRE FAILURE ON TAKEOFF FROM HKG.(<P>REMOVED AND REPLACED BRAKE CONTROL UNIT AND R/H BODY GEAR ANTI SKID MODULE. REMOVED AND REPLACED #9 & #10 MAIN WHEEL ASSEMBLIES. PERFORMED THE FOLLOWING CONDITIONAL INSPECTIONS:</P> / <P>SINGLE FLAT / BSDR UIEA2025041500477Curtain · tornBULK CARGO STA 2160 CURTAIN FOUND TORN(<P>PERMANENT REPAIR CARRIED OUT AS PER RI-25-54-17582 REV. A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025041400459Seat Track · crackedCRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, LBL 75.92.(<P>1. REMOVE AFFECTED FASTNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REFER DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 103 WORKSHEET NO: 50173. 3. INSTALL FASTENERS IAW SRMSDR UIEA2025041400461Seat Track · crackedCRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1730, RBL 75.92.(<P>1. ACCOMPLISHED W/S NO: 50170 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL. </P>)SDR UIEA2025041400462Seat Track · crackedCRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, RBL 75.(<P>1. ACCOMPLISHED W/S NO. 50172 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025041400463Seat Track · crackedCRACK - FOUND M/D FLOOR STRUCTURE TRACK SUBSTITUTE CRACK BETWEEN STA 980 TO STA 1000, LBL 75.92.(<P>1. ACCOMPLISHED W/S NO. 50160 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025041400464Seat Track · crackedCRACK - FOUND M/D CGO COMPT SUB SEAT TRACK CRACK BETWEEN STA 660 TO STA 720, LBL 75.92, TTL 3 EA.(<P>1. ACCOMPLISHED W/S NO. 50182 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025041400465Floorbeam · corrodedCORROSION - MFOUND M/D FLOOR BEAM CORROSION AT STA 2240 RBL 57 TO RBL 85.(<P>1. REMOVE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103 W/S 50176 AND EI NO: T2025A53M-546 REV 1. 3. INSTALL FASTNERS IAW SRM 5SDR UIEA2025041400468Floorbeam · corrodedCORROSION - FOUND M/D FLOOR BEAMS TOP SURFACE CORROSION STA 1500 BETWEEN LBL 55 TO LBL 75.92.(<P>1. REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103, W/S NO: 50169 AND EI NO: T2025A53M-4SDR UIEA2025041400469Splice Angle · corrodedCORROSION - FOUND SPLICE ANGLE CORROSION AT M/D COMPARTMENT BETWEEN STA 2280 TO STA 2300, RBL 68.(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALLED NEW PART IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 65B38694 SHEET 3 REV C. 3. CONDITION CHECKSDR UIEA2025041400471Bracket · corrodedCORROSION - BRACKET LOWER FUSELAGE WING-TO-BODY SUPPORT BRACKET STA 920 BL 0.(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 14240130 SHEET 1 REV A. 3. JOB COMPLETED AND CONDITION CHECK NSDR UIEA2025041400473Elt · expiredFWD M/D FIXED ELT BATTERY NEAR DUE DATE (03JUN25).(<P>1. REPLACED ELT TRANSMITTER IAW SWPM 20-60-06. 2. STEP A & B PERFORMED ELT INSTALLATION TEST IAW T/C NO: 23-024-00-03. THE RESULT WAS SATISFACTORY.</P>)SDR UIEA2025040300427Pseu · faultedAFTER TAKE OFF, GEAR TILT MESSAGE & GEAR HANDLE WOULD NOT MOVE PAST OFF.(<P>ADJUSTED LT BLG PROX SWITCH AND TARGET PER B747 AMM 32-61-12-822-019. BODY GEAR OPS CHECK GOOD PER B747 AMM 32-33-715-071. REPLACED PSEU PER B747 AMM 32-09-03-004-001 AND 32-09-03-404-SDR UIEA2025021600148Engine · vibrationENG 1 VIB 4.0, N1 FAN, STEADY INCREASE THRU UPPER 20'S FLIGHT LEVEL.(<P>RAN ENG 1 PER 71-00-00-705-057-J00. NOTED 3.1 VIBRATION PEAK PER MCC ENGINEERING. OPS CHECK NORMAL.</P>)SDR UIEA2025020300114Module · failedARCING SOUND HEARD FROM OVERHEAD PANEL ACCOMPANIED MOMENTARILY BY FIRE LIGHTS IN APU FIRE SWITCH.(<P>REMOVED AND REPLACED ENG/ APU FIRE EXT MODULE PER B747 AMM 26-10-02. R/R CIRCUIT CARD A22 REF AMM 26-10-01. OPS TEST GOOD, NO DEFECTS NOTED AT THIS TIME. </P>)SDR UIEA2025010400004Pcb · damagedAPU FIRE SWITCH ILLUMINATED INTERMITTENTLY FOR SEVERAL HOURS. A FEW TIMES FIRE APU WARNING EICAS MESSAGE ALSO DISPLAYED FOR A SPLIT SECOND. ALSO, CAN HEAR APU FIRE SWITCH DISCONNECTING.(<P>REMOVED AND REPLACED AFOLTS CARD A22 PER AMM 26-10-01/401. INSPECTED SDR UIEA2024112001097Fire Warning · false activationDURING FLIGHT N452PA HAD A MDC FIRE WARNING ALERT. CREW VERIFIED NO FIRE OR SMOKE, CONTINUED TO ANC.(<P>CONFIRM NO SMOKE OR FIRE FROM PREVIOUS LEG. PERFORMED CARGO DET FIRE TEST PER AMM 26-14-00. NO ACTIVE FAULTS PRESENT.</P>)SDR UIEA2024092500947Fire Warning · false activationAPU FIRE MSG. COMPLIED WITH QRH 8.1. DISCHARGED APU FIRE BOTTLE(<P>DEACTIVATED APU AND TRANSFER TO DMI 217433 PER MEL 26-22-01 CAT C DUE DATE 5OCT24. R/R APU FIRE EXT BOTTLE & GND CHECK GOOD PER AMM 26-22-01/401 & AIPC 26-22-01-02A. DMI 217433 CLOSED.</P>)SDR UIEA2024090900887Fan · failedPOSSIBLE BURNING ELECTRICAL SMELL IN FLIGHT DECK WHILE A/C ON GROUND(<P>FOUND FWD EQPT COOLING SUPPLY FAN HEATED & SMALL BURNT SMELL SO R/R EQPT COOLING SUPPLY FAN. OPS & SMELL CHECK GOOD PER AMM 21-58-01/401 & IPC 21-58-01-01. CONDITION CHECK NORMAL PER AMM 5SDR UIEA2024081600834Fairing · delaminatedLHW I/B MID FLAP I/B L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024081600833Lamp · inoperativeMAIN DECK L1 DR STILL FWD EMER LT INOP.(<P>MAIN DECK L1 DR STILL FWD EMER LT LAMP REPLACED & OPERATION TEST NORMAL IAW AMM 33-51-05.</P>)SDR UIEA2024080900819Engine · faulted#1 ENGINE IN FLIGHT SHUTDOWN DIVERTED TO ICN.(<P>ACCOMPLISHED WO 134669. R/R #1 ENG IAW WC 71-099-02-01 & OPS & LEAK CHECK GOOD IAW AMM 71-00-02.</P>)SDR UIEA2024072900759None · noneATB PERFORMED DUE TO COLLAPSED PALLET OF BATTERIES AT POSITION GL.(<P>PER AMM 05-51-15 INSPECTED MCD POSITION GL AREA FOR CHEMICAL SPILL AND FOUND NO SPILLAGE. BATTERIES FOUND TO BE LITHIUM BATTERIES AND NO DEFECTS NOTED. NO DAMAGE OR DEFECTS TO A/C PER AMM 25SDR UIEA2024071700682Brake Assy · failed#12 BRAKE FAILED ON LANDING(<P>REPLACED #12 BRAKE ASSY PER AMM 32-41-15. OPS & LEAK CHECK OK</P>)SDR UIEA2024071400670Oil System · pressure lossENG 1 IFSD (OIL QTY & PRESSURE LOSS). R & R #1 ENG PER WO 133424. C/W ENG IDLE RUN IAW AMM 71-00-00, OPS CHECK GOOD. NO FAULTS OR LEAKS.SDR UIEA2024071300661Light · sparksCO PILOTS FLOOD LIGHT SPARKS AND SMOKE.(<P>REPAIRED WIRING AS PER SWPM 20-10-13, REPLACED MAP LIGHT AS PER AMM 33-15-00. OPS CHECK GOOD</P>)SDR UIEA2024071200645Flap System · faultedUPON DEPARTURE, FLAPS DRIVE. OUTBOARD FLAPS LOCKED AT APPROX F5 POSITION.(<P>PERFORMED FLAPS OPS TEST SEVERAL TIMES PER AMM 27-58-01, CAN'T DUPLICATE FAULT ON GROUND. COMPLETED AP 28370 FOR TE FLAP SYS, FLAP SYS OPS TEST NORMALSDR UIEA2024061200516Line · brokenADVISORY MSG "SMOKE CREW REST " AROUND 800 TO 1000 FEET AFTER T.O., FOLLOWED BY FUMES ON THE FLIGHT DECK.(<P>R/R CREW REST AREA TRIM AIR MODULATING VLV, REAPIRED BROKEN WATER SEPERATOR LINE, AND REPLACED COALLESOR BAGS PER AMM 21-61-16. OPS CHK GOOD.</P>)SDR UIEA2024052200400Rvdt · faultedDURING FLAP RETRACTION AFTER DEPARTURE, FLAP DRIVE CAME ON EICAS. FLAPS WOULD NOT RETRACT PAST 5DEG ON OUTBOARD FLAPS(<P>R/R RH OUTBOARD RVDT PER AMM 27-58-01. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024042600318Pump · faultedHYD PRESS SYS 1 CAUTION MSG IN FLIGHT. BOTH ENG AND DEMAND PUMP ON SYSTEM 1 INOP(<P>R/R #1 ENG DRIVEN PUMP. REMOVED & INSPECTED ALL SYS 1 HYD FILTERS, NO CONTAMINATION OR DISCREPANCIES FOUND. ENGINE IDLE RUNS & LEAK CHECK NORMAL. REF LP 1797125 M5: R/R ADP 1, SDR UIEA2024041400274Engine · leakingNR 4 ENGINE OIL QUANTITY DROPPED TO 2 QTS IN FLIGHT. C/W WO #128800, R & R NR 4 ENGINE, OPS & LEAK CHECKED NORMAL IAW W/C # 71-099-02-01.SDR UIEA2024041300273Skin · damagedLHW T/E I/B MID FLAP L/E FOUND BIRD STRIKE(<P>LHW T/E I/B MID FLAP L/E BIRD STRIKE AREA, PERFORMED TIME LIMIT REPAIR AS PER EA-1957A0103 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024032800229Unknown · faultedDURING TAKEOFF NOTICED UNCOMMANDED ROLLING, ALSO ON LANDING AIRCRAFT ROLLED UNCOMMANDED TO LEFT.(<P>ABNORMALITY PRESSURIZED HYD, & TRIM RUDDER TO NEUTRAL, RUDDER & RUDDER TRIM CONTROL SYS OPS CHECK NORMAL PER AMM 27-21-00 WITH FULL FLAP FULL UP, SPOILER OPS & SDR UIEA2024032100164Smoke Detector · false activationCREW REST SMOKE EICAS MSG. NO SMOKE OR FIRE CONFIRMED.(<P>WIRING CHECKED NORMAL PER B747-400 WDM 26-13-31 REV 33. NEED TO REPLACE R/H CREW REST SMOKE DETECTOR. PERFORMED CHECK FLIGHT DECK EQUIPMENT AND CABIN EQUIPMENT. PERFORMED FUMES SMELL CHECK IN BLEED DUCTSDR UIEA2024022300113Structure · crackedFX AIRCON BAY LH STA 1240 LBL 105" O/B CENTER SECTION LOWER CHORD CRACK(<P>CRACK CHORD REPLACED AS PER SRM 51-10-01 AND NEW CHORD HOLE TRANSFERRED AS PER SRM 51-40-05 AND NEW CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022300114Closeout Panel · crackedM/D STA 1241 LBL 77-99 CLOSEURE PNL FOUND CRACK(<P>CLOSURE PNL REPLACED AS PER SRM 51-10-02 AND NEW PANEL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW PANEL INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022300115Web · unknownMDDR 177930 REF EA-4453A0008 REV 0 AFT CARGO COMPARTMENT LATERAL BEAM UPPER FLOOR WEB AT STA 1840-1860 LBL 45.5 PERMANENT REPAIR (WITHIN 2000FC AFTER REPAIR OR WITHIN 24 MONTHS WHICHEVER OCCURS EARLIER(<P>WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSDR UIEA2024022300116Beam · corrodedAFT CARGO DOOR INNER SURFACE LOWER DOOR LINER CLOSE OUT BEAM SURFACE CORR FROM STA 1780-1920 SEVEN PLACES(<P>BEAM 6 LOCATIONS CORROSION REMOVED WITHIN SRM 52-30-02-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS, 1 LOCATION REPAIRED AS PER RI-52-30-16736 REV A AT STA 1SDR UIEA2024022300117Skin · punctured#2 ENG R/H CORE UPPER SECTION 10" (COUNT FROM AFT) EXT SURFACE FOUND PUNCH HOLE(<P>#2 ENG R/H CORE COWL UPPER SECTION TITANIUM FAIRING EXTERNAL DOUBLER REPAIRED AS PER SRM 54-45-01-2R-7 REPAIR 7. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024022300118Channel · crackedEMP L/H HORI STAB MOST O/B T/E WEDGE 'U' CHANNEL FOUND CRACK(<P>CRACK CHANNEL REPLACED AND INSTALLED AS PER RI-55-10-16734 REV A. NO FURTHER DEFECTS NOTED</P>)
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