Boeing 747-412F
Service difficulty reports · 239
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 = '747412F' 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 = '747412F' 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 UIEA2022080800834None · noneM/D STA 1140 RBL 30 - 33 WING CTR SECTION UPPER SKIN CORROSION(<P>SKIN CORROSION AREA REPAIRED AS PER RI NO : RI-57-00-15842 REV A</P>)SDR UIEA2022080800833None · noneLH BS 2231 S25L 2EA HOLES FOUND CRACK AT CHORD LAYER RUNNING 3 O/C POSITION APPROX 0.040 INCH, RUNNING 4 O/C POSITION APPROX 0.040 INCH(<P>CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15797 REV A</P>)SDR UIEA2022080800832None · noneLH BS 2231 S24L 1EA HOLE FOUND CRACK AT CHORD LAYER, RUNNING 1 O/C POSITION APPROX 0.040 INCH(<P>CRACK AREA REPAIRED AS PER RI NO. RI-53-00-15797 REV A</P>)SDR UIEA2022080800831None · noneLH BS 2231 S16L 1EA HOLE FOUND CRACK AT STRAP LAYER RUNNING AT 9 O/C POSITION APPROX 0.050"(<P>FRAME STRAP CRACK AREA REPAIRED AS PER SRM 53-60-15 REPAIR 2 AND RI NO. RI-53-00-15784 REV A</P>)SDR UIEA2022080800830None · noneM/D STA 1200 RBL 98 - 121 FLOOR WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-9 REPAIR 9 AND RI NO : RI-53-00-15791 REV B</P>)SDR UIEA2022080800829None · none1EA CRACK FOUND ON NWW LHS SIDE PANEL WL 180 BETWEEN BS 280 AND BS 300 APPROX 5" IN LENGTH(<P>LOCATION CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15789 REV A</P>)SDR UIEA2022080800828None · none1EA CRACK FOUND ON NWW LHS SIDE PANEL WL 180 BETWEEN BS 260 AND BS 280 APPROX 1/2" IN LENGTH(<P>LOCATION CRACK AREA REPAIRED AS PER RI NO : RI-53-0015789 REV A</P>)SDR UIEA2022080800825None · noneFX KEEL BEAM L/H EXTERIOR SURFACE LOWER CHORD STA 1000 - 1026 FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI NO. RI-53-00-15790 REV A</P>)SDR UIEA2022080800824None · none1EA CRACK INDICATION WAS FOUND ON SKIN LAYER AT LH BS 980 S38L DRAG SPLICE FITTING(<P>SKIN REPAIRED AS PER SRM 53-20-01-2R-2 REPAIR 2 FIG 201 DETAIL III AND ATLAS AIR EO : 4453A499 PART 3</P>)SDR UIEA2022080800823None · none1EA CRACK INDICATION AS PER ON SKIN LAYER AT RH BS 980 S38R DRAG SPLICE FITTING(<P>SKIN REPAIRED AS PER SRM 53-20-01-2R-2 REPAIR 2 FIG 201 DETAIL IV AND ATLAS AIR EO 4453A449 PART 4 </P>)SDR UIEA2022080800822None · noneFX - KEEL BEAM R/H #4 STIFFENER FOUND CORROSION (COUNT FROM FWD)(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-00-15771 REV A </P>)SDR UIEA2022080800821None · noneFX KEEL BEAM R/H #5 STIFFENER (COUNT FROM FWD) FOUND CORROSION.(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-49-15778 REV A </P>)SDR UIEA2022080800820None · noneFX KEEL BEAM R/H #6 STIFFENER FOUND CORROSION ( COUNT FROM FWD )(<P>CORROSION AREA REPAIRED AS PER RI NO: RI-53-00-15772 REV A</P>)SDR UIEA2022080800819None · noneM/D STA 780 TO 860, LBL 22" CEILING SUPPORT FOUND CRACKED.(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-25-22-15782 REV A</P>)SDR UIEA2022080800818None · noneM/D STA 780 - 820 LBL 23 CEILING FOUND CRACK(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-25-22-15783 REV A.</P>)SDR UIEA2022080200813None · noneLHW OB MID FLAP AFT UPPER SKIN FOUND 2EA SCREW HOLES ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)SDR UIEA2022080200812None · noneLHW O/B T/E FORE FLAP L/E FAIRING AT MID EXTERIOR SURFACE DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2022080200811None · noneRHW O/B T/E FORE FLAP L/E FAIRING AT MID EXTERIOR SURFACE DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5C</P>)SDR UIEA2022070700733None · noneM/D SCD AFT O/B DOOR SILL LOWER SKIN FOUND 2 LOCATIONS FWD CUTOUT 1" & AFT CUTOUT 1" X 2" CRACK.(<P>2 LOCATIONS CUT OUT SKIN REPAIRED AS PER ATLAS AIR EO : 4425A500 REV 1.</P>)SDR UIEA2022052800552Doubler · crackedEO 4453A821-1 & 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) L/H FASTENERS & WASHERS DEVIATIONS DOUBLER S.E.M AND R/H FASTENERS WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOSDR UIEA2022053100560Transmitter · flamed outBTB, ENG 2 TAIL PIPE FIRE OBSERVED BY GROUND OPS. ALL INSPECTIONS C/W TO INCLUDE BSI. VSV AND FUEL FLOW TRANSMITTER REPLACED. T/T HALF TIME LIMIT REPAIR ACCOMPLISHED. MAX POWER ASSURANCE RUNS ACCOMPLISHED.</P>)SDR UIEA2022051700485Loop · inoperativeENGINE 2 FIRE DETECTION LOOP A INOP. PLACED ON MDDR 165711 IAW MEL 26-11-02-01, CAT C.SDR UIEA2022022000149Eec · failedENGINE #2 FAILED SHORTLY AFTER TAKEOFF (CONVERSATION WITH CAPTAIN INDICATED IFSD ON TAKEOFF AT APPROXIMATELY 1000 AGL. CREW FOLLOWED THE QRH. CREW LEVELED OUT AIRCRAFT AT 3000 FT. CREW INITIATED AN ENGINE START ON #2, WHICH WAS SUCCESSFUL. CREW CONTACTED THE DSDR UIEA2022012500077None · noneEICAS GEAR TILT(<P ><SPAN>R/H BODY GEAR TILT HYDRAULIC LINE DAMAGED. FABRICATED TEMPORARY REPAIR HOSE FROM FSK PER ATLAS GMM 3.24.1. INSTALLED TEMPORARY REPAIR HOSE PER AMM 32-13-15.</SPAN></P> / <P> </P>)SDR UIEA2021092302090Fitting · leakingDURING FLIGHT HYD QTY 1 MSG, FOLLOWED BY HYD SYS 1 MSG AND LIGHT(<P ><SPAN>FOUND FITTINGS ON FUSE ASSY FOR RH BODY GEAR LEAKING. REPLACED RH BODY GEAR TRUCK POSITIONING FUSE IAW AMM 32-13-24/401. LEAK CHECK GOOD.</SPAN></P>)SDR UIEA2021081401803Connector · contaminatedIN FLIGHT HYD OVHT #3. IN FLIGHT HYD LOW QTY DOWN TO .12(<P>REMOVED AND REPLACED CANNON PLUG DUE TO MOISTURE AND CONTAMINATION IAW SWPM 20-61-02. REMOVED AND REPLACED #3 HY/DIM CARD (PN <SPAN>D43699J, NSN</SPAN><SPAN>) IAW AMM 29-11-42/401. OPERATIONAL CHECKESDR UIEA2021072701636Warning Message · multiple failAFTER T/O, #1 PACK INOP. L/H COMM FAILURE, EQUIPMENT COOLING FAILURE, STANDBY INSTRUMENT FAILURE. GENERATED AND EXECUTED E/O 4421A043 FOR DETECTION OF DEFECTS IN A/C SYSTEM.SDR UIEA2021070901501Sensor · faultedEQUIP COOLING MSG ON CLIMB OUT. GRH PERFORMED. ON OVERIDE(<P>PERFORMED FIM 21-58 TASK 833 REMOVED AND REPLACED LOW FLOW SENSOR & EQUIPMENT COOLING CARD (ECC) TEST GOOD IAW AMM 21-58-02 AND 21-58-05/201</P>)SDR U2RA2024103100061Spoiler · corrodedRIGHT WING UPPER SURFACE JUST FWD OF #8 FLIGHT SPOILER AT RBL 392.67 TO 432.67 HAS CORROISION. PERFORMED PERMANENT REAPIR BY REPLACING 65B11628-8 IAW SRM 51-40-02 DOCUMENT ON NATIONAL M8A NR 64292-142 AND FEAM WO MIA-WA-12-2024.SDR UIEA2020071401515Autothrottle Sys · faultedAUTOTHROTTLE FAULT. DEFERRED PER DDG 22-11-04-02B & 22-31-01, MDDR 131055, CAT 'C'SDR UIEA2020070751286Light · no testMAIN DECK L1 DOOR SILL EMERGENCY LIGHT L1853 FAILED OPERATION TESTMAIN DECK L1 DOOR SILL EMERGENCY LIGHT L1853 REPLACED AND TESTED NORMAL AS PER AMM 33-51-05SDR UIEA2020070751403Skin · delaminatedLEFT WING OTBD FORE FLAP L/E, FOUND THE OTBD AREA DELAMINATED. THE DELAMINATED AREA WAS REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070751404Skin · delaminatedLEFT WING OTBD FORE FLAP L/E INBD AREA, FOUND DELAMINATION. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070751405Skin · delaminatedLEFT WING OTBD AFT FLAP T/E AREA, UPPER SURFACE WAS FOUND DELAMINATED. THE DELAMINATED AREA WAS REPAIRED IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070761406Skin · delaminatedLEFT WING OTBD MID FLAP T/E AREA UPPER SURFACE WAS FOUND DELAMINATED. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070721412Bracket · damagedFWD CARGO BAY, BS 920 - 940, RBL 60 FLOOR AREA AIR DUCT AFT BRACKET WAS FOUND DAMAGED. THE BRACKET WAS REPLACED IAW RI-21-28-14104, REV A.SDR UIEA2020070781415Seat Track · corrodedBS 1840, RBL 75, SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND THE SEAT TRACK WAS PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101.SDR UIEA2020070781416Seat Track · corrodedBS 1920, RBL 75, SEAT TRACK WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND THE SEAT TRACK WAS PROTECTED IAW SRM 51-10-02, AND SRM 51-20-0. CHECKED WITHIN LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101.SDR UIEA2020070781417Seat Track · corrodedBS 1820, RBL 75, SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND THE SEAT TRACK PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101.SDR UIEA2020070721418Structure · corrodedAFT CARGO DOOR INTERNAL LOWER, CENTER AREA HAD TWO AREAS OF CORROSION, THE CORROSION WAS REMOVED AND PROTECTED IAW SRM 52-30-02, AD1, FIG 101.SDR UIEA2020070701419Seat Track · corrodedBS 1780, LBL 99 SEAT TRACK WAS FOUND WITH CORROSION. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-6, REPAIR 6, FIG 201.SDR UIEA2020070721420Seat Track · corrodedBS 1920, LBL 75 SEAT TRACK WAS FOUND WITH CORROSION. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-6, REPAIR 6, FIG 201.SDR UIEA2020070771426Frame · crackedBS 2598 BULKHEAD RT INNER CHORD AREA, ONE CRACK FOUND ON THE FWD SPLICE FITTING, SECOND LAYER COUNT FROM INBD. APPROX 0.040" IN DEPTH RUNNING AFT AT 4 O`CLOCK POSITION, THE BULKHEAD UPPER CORNER RT SPLICE FITTING WAS REPAIRED IAW RI-53-00-14106 REV A.SDR UIEA2020070791437Skin · delaminatedRIGHT WING INBD MID FLAP INBD L/E, FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791438Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E, FOUND DELAMINATED FROM INBD 261". PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791439Skin · delaminatedRIGHT WING INBD FORE FLAP, FWD L/E FOUND DELAMINATED FROM O/B 18". PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791440Skin · delaminatedRIGHT WING INBD FORE FLAP, FWD L/E WAS FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791441Skin · dentedRIGHT WING, INBD AFT FLAP LOWER SURFACE, CENTER T/E SECTION WAS FOUND DENTED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07 PAR, 5A REV 88.SDR UIEA2020070762442Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E, FOUND DELAMINATION FROM INBD 339 INCHES. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.SDR UIEA2020070791443Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E FROM INBD 46 INCHES HAD DELAMINATION. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.
Back to Boeing 747-412F