Boeing 747-45EF
Service difficulty reports · 348
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 = '74745EF' 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 = '74745EF' 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 UIEA2024071200648Angle · crackedLHW L/E REFUEL DOOR FWD ZEE FOUND CRACK.(<P>PERFORMED REPAIR AT CRAKCK AREA AS PER RI-57-00-16992 REV.A NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071200649Tension Tie · crackedLH BS760 UPPER DECK TENSION TIE 1EA FASTENER HOLE CRACK FOUND AT AFT CHANNEL.(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071200650Tension Tie · crackedRH BS760 UPR DECK TENSION TIE 1EA FASTENER HOLE CRACK FOUND AT AFT CHANNEL.(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071200651Tension Tie · crackedRH BS840 UPPER DECK TENSION TIE 1EA FASTENER HOLE CRACK AT AFT CHANNEL.(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071300652Frame · damagedM/D LH STA 940 FRAME FASTENER HOLE BTN STR 8L-9L FOUND PREVIOUSLY FREEZE PLUG HOLE REPAIR.(<P>FRAME REPLACEMENT CARRIED OUT AS PER SRM 51-10-02, NEW FRAME HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FRAME INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTSDR UIEA2024071300653Frame · crackedLEFT BS 2231 STR 16L FRAME FWD INNER CHORD 1EA FASTENER HOLE CRACK. FRAME FWD INNER CHORD REPAIRED AS PER SRM 53-60-15-2R-2 REPAIR 2 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR UIEA2024071300654Failsafe · crackedRIGHT BS 880 UPPER DECK FRAME FAIL SAFE CHORD 1EA FASTENER HOLE CRACKED.FAIL SAFE CHORD REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 9F AND SRM 53-20-07-2R-5 REPAIR 5 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR UIEA2024071300655Frame · crackedRIGHT BS880 UPPER DECK TENSION TIE ATTACHED TO FRAME FOUND 2EA FASTENER HOLES CRACK. FRAME REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 9F AND SRM 53-20-07-2R-5 REPAIR 5 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR UIEA2024071300656Frame · crackedRIGHT BS 840 UPR DECK TENSION TIE ATT FRAME FOUND 4EA FASTENER HOLES CRACK. FRAME REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 7F AND SRM 53-20-07-2R-3 REPAIR 3 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.SDR UIEA2024071400662Bulkhead Web · crackedBS 260 NLG W/W FWD BULKHEAD WEB R/H LOWER CORNER ONE FASTENER HOLE CRACKED. WEB REPAIRED AS PER RI-53-15-16983 REV.A. NO FURTHER DEFECTS NOTED,SDR UIEA2024071400663Fitting · crackedONE CRACK WAS FOUND AT INTERCOSTAL LUG FITTING APPROX 1 1/4" IN LENGTH ON RH STA 1000 RBL 11.33. INTERCOSTAL LUG FITTING REPLACED REFER ATLAS AIR EO 4453C024 REV 4 PART 7 STEP 3 CONDITION 11. NO FURTHER DEFECTS NOTED.SDR UIEA2024071400664Frame · crackedAPU COMPARTMENT RT STA 2685 WL 325 FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 (CAT A). NO FURTHER DEFECTS NOTED.SDR UIEA2024071400665Frame · chafedNUMBER 4 ENGINE RT CORE COWL FRAME NR 2 MID AREA FOUND CHAFING MARK, COUNT FROM FWD. FRAME REPAIRED IAW EA-1971A141 REV.0 DATE 01 JUL 24. NO FURTHER DEFECTS NOTED.SDR UIEA2024071400666Channel · crackedLEFT HORIZONTAL STAB OTBD TE AFT WEDGE FWD CHANNEL OTBD UPPER FLANGE, 1EA FASTENER HOLE CRACKED. WEDGE FWD CHANNEL REPLACED AS PER RI-55-10-6987 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2024071400671Web · corrodedCENTER FUSELAGE REAR WEB AT RBL 94" FND O/B BONDING ATT POINT CORROSION. CORROSION AREA REPAIRED AS PER RI NO: RI-57-10-17000 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2024071400672Seat Track · crackedSTA 1780-1800 LBL 99" SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6 REPAIR 6 FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2024071400673Support · crackedLHW LWR SURFACE REFUELING ACCESS DOORS FWD FIXED PNL FWD PNL SUPPORT FOUND CRACK. SUPPORT REPAIRED AS PER SRM 57-41-13-2R-3 REPAIR 13 FIG 201 (CATEGORY A). NO FURTHER DEFECTS NOTED.SDR UIEA2024071500674Web · corrodedCENTER FUSELAGE REAR WEB AT LBL 94" FND 2EA BONDING ATT POINTS CORROSION. CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CHECKED WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101, DETAIL V LIMITS ORG: 0.815, L:2" X L:1" X D:0.065SDR UIEA2024071500675Structure · chafedLWR RUDDER L/H LWR CHORD FOUND CHAFING(<P>LWR CHORD CHAFING AREA REPAIRED AS PER RI-55-40-17002 REV.B. NO FURTHER DEFECTS NOTED.SDR UIEA2024071500676Web · chafedLWR RUDDER LWR WEB AFT FOUND CHAFING MARK. WEB CHAFING MARK AREA REPAIRED AS PER RI NO: RI-55-40-17002 REV.B. NO FURTHER DEFECTS NOTED.SDR UIEA2024071500677Retainer · damagedLWR RUDDER, RH LWR DEFLECTOR SEAL RETAINER RAIL BRACKETS FOUND DAMAGE(<P>FWD RETAINER REPLACED AS PER RI-53-51-16996 REV.A, AFT RETAINER REPLACED AS PER SRM 51-10-02, NEW RETAINER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW RETAINER INSTALLED AS PER SRM 51-4SDR UIEA2024071500678Fitting · corrodedRHW LWR WING L/E COMPOSITE PANEL FOUND BULGED AT OLES 1390(<P>FITTING REPLACED AND INSTALLED AS PER RI-57-21-16994 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071500679Fairing · crackedLHW O/B AILERON O/B LWR L/E FAIRING FOUND CRACK(<P>L/E SKIN LOCAL FABRICATED AS PER BOEING DWG: 65B02108 AND PL AND NEW SKIN HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW SKIN INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024050800348Skin · chafedLH WING INBD AILERON OTBD TE SKIN CHAFING WORN(<P>1) PERFORM REPAIR OF CHAFING WORN SKIN DAMAGE AT LH WING INBD AILERON TE OTBD SIDE UPPER SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING FOR DETAILED REWORK INFO. REF SRM 57-60-01-0I-1 REV 100, SRM 57-60-01-2R-SDR UIEA2024050800349Skin · debondedDISBOND - SKIN RH WING INBD AILERON OTBD LWR EDGE(<P>1) PERFORM REPAIR OF DISBOND SKIN DAMAGE AT RH WING INBD AILERON TE OTBD SIDE LWR SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING FOR DETAILED REWORK INFO. REF SRM 57-60-01-0I-1 REV 100, SRM 57-60-01-2R-1 RESDR UIEA2024050800350Skin · wornWORN - SKIN LH OTBD FORE FLAP RH TOP PANEL FASTENER HOLE, FROM LH EDGE 18" AND FROM AFT EDGE 0.5"(<P>1) PERFORM REPAIR OF WORN SKIN DAMAGE AT LH WING OTBD FORE FLAP UPPER SKIN PANEL ASSY (PN 65B01915-427) IAW EGAT EI T2024A57M-838 REV 1. 2) CONDITION CHECK IS SDR UIEA2024050800351None · noneFOUND AN EXISTING REPAIR ON L1 DOOR UPPER MAIN SILL FROM STA 440 ~ STA 480.(<P>1. ACCOMPLISHED EI T2024A53M-806, REV 0 2. EXISTING REPAIR WAS COVERED BY EO 4457A291, REV 7 REFER RAM FORM N485MC-24-04 ISSUE 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024050800352Spar · crackedHOLE CRACK ON RH HST UPR REAR SPAR CHORD NEAR RBL43.(<P>1.REPAIR DAMAGE AREA IAW EI T2024A55M-712 REV 2 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024050800353Trunnion · corrodedFOUND LH BLG INBD TRUNNION LWR FITTING CORROSION.(<P>1. REMOVE THE CORROSION AREA IAW SRM 53-40-90-2R-1 REV 100 2. ACCOMPLISHED EGAT EI T2024A32M-678 REV 1 REPAIR CORROSION DAMAGE ON THE CAP FITTING OF LH AND RH BODY LANDING GEAR INBOARD TRUNNION VERTICAL SUPPSDR UIEA2024050800354Trunnion · corrodedFOUND RH BLG INBD TRUNNION LWR FITTING CORROSION.(<P>1. REMOVE THE CORROSION AREA IAW SRM 53-40-90-R-1 REV 100. 2. ACCOMPLISHED EGAT EI T2024A32M-678 REV 1 REPAIR CORROSION DAMAGE ON THE CAP FITTING OF LH AND RH BODY LANDING GEAR INBOARD TRUNNION VERTICAL SUPPSDR UIEA2024050800355Unknown · corrodedCORROSION - FOUND 20 EA CORROSION DAMAGE WHEN PERFORM SB 747-53A878(<P>1. PERFORM EI T2024A53M-753 REV 0, EI T2024A53M-824 REV 0, DWG 140U1480, SH37 REV A, SH38 REV D, DWG 144U0105, SH2 REV C, DWG 140U099, SH20 REV A, SH23 REV C, SH24 REV C, DWG 144U0104, SH5 SDR UIEA2024050800356Bracket · corrodedCORROSION - BRACKET, RH WING GEAR W/W CENTER WALL HYD TUBE SUPPORT BRACKET, STA 1301(<P>1. REMOVE DAMAGE BRACKET IAW SRM 51-40-02-0G-0 REV 100 2. FABRICATE NEW BRACKET IAW WORK SHEET 40263 3. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 REV 100 AND BOEING DWG 2SDR UIEA2024050800357Seat Track · crackedFND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 1480 LBL 75.92(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40266, DWG 65B38251 SH32 REV-, SH75 REV-, DWG 144U0802 SH3 REV B 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024050800358Seat Track · crackedFND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 990 LBL 75.92(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40265 AND DWG 65B38250 SH17 REV A, SH9 REV B, AND DWG 65B16004 SH4 REV A 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024050800359Seat Track · crackedFND FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT M/D STA 980 ~ 1000 RBL 75.92(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40264, DWG 65B38250 SH9 REV B, DWG 65B16004 SH4 REV A & SH3 REV- 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024050800360Screw · interferenceFND EXISTING SCREW INTERFERES WITH WIRE AT STA 560 NEAR RBL 65(<P>1. ACCOMPLISH EI T2024A53M-1060 REV 1 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024050800361Structure · crackedCRACK - LWR CHORD, R/H H.S.T TIP 347R PNL LWR CHORD, STAB BL 421.5(<P>1. REPAIRED DAMAGE AREA IAW WORKSHEET 40295 2. JOB COMPLETED & NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024050800362Door · crackedCRACK - LOWER SIDE CORNER CRACK AT L1 ENTRY DOOR(<P>1. REMOVED AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 100. 2. ACCOMPLISHED JOB IAW EI T2024A52M-858 REV 1. 3. INSTALLED AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 100, DWG 65B01836 SH2 REV AB AND 65B01836SDR UIEA2024050800363Bracket · corrodedLEFT WINGLET, RIB BRACKET CORROSION WBL 1243.750(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 100. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 100 AND DWG 11245700 SHEET 1 REV C 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)SDR UIEA2024050800364Frame · crackedCRACK ON FRAME WEB OF STA 1480 NEAR LBL 110 AND WL 150(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCES IAW 51-40-02-0G-0 REV 100 2. REPAIRED DAMAGE AREA IAW W/S 40241 AND EI T2024A53M-807 REV 1. 3. INSTALLED FASTENERS IAW SRM 57-40-02-0G-0 REV 100, DWG 65B15085SDR UIEA2024050900365Web · corrodedCORROSION - WEB, L/H HST T/E CAVITY STA 381.8 AREA ACCESS PNL 334PBL(<P>1. REMOVED CORROSION WEB IAW SRM 51-40-02-0G-0 REV 100. 2. FABRICATE WEB IAW WORKSHEET 40288. 3. INSTALL FABRICATE WEB IAW SRM 51-40-02-0G-0 REV 100 AND DWG 287U8202 SH2 REV A; 284U7037 SHSDR UIEA2024050900366Web · corrodedCORROSION- WEB, L/H HST T/E CAVITY ELEV STA 331.8(<P>1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 100. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 100 AND DWG 65B03681 SHEET 2 REV E. 3. CONDITIONAL CHECK NORMAL AND JOB COMPLETED.</P>)SDR UIEA2024050900367Seat Track · corrodedFND FLOOR SEAT TRACK BRK AT M/D STA 1655~1665 RBL 98.58(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40276, EI T2024A53M-775 REV 1, DWG 65B38251 SH 62 REV A & SH 66 REV -. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)SDR UIEA2024050900368Seat Track · corrodedFND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 1820~1840 LBL 75.92.(<P>ACCOMPLISHED WORKSHEET 40277, EI T2024A53M-776 REV 1, WORKSHEET ATTACHED TO W/O 9350399(912) & EI ATTACHED TO W/O 9350399(912). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024050900369Seat Track · corrodedFND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 1870 LBL 75.92.(<P>1. REPAIR DAMAGE AREA IAW WORKSHEET 40277, EI T2024A53M-776 REV 1, BOEING DWG 65B38251 SH 62 REV A, SH 32 REV - & DWG 65B38288 SH2 REV A. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)SDR UIEA2024050900370Seat Track · corrodedFND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 1842 ~1858, RBL 98.58.(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40278, EI T2024A53M-778 REV 1, BOEING DWG 65B38251, SH 62 REV A & SH 66 REV -. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>)SDR UIEA2024050900371Seat Track · corrodedFND FLOOR STRUCTURE SEAT TRACK CORROSION AT M/D STA 2164~2169. RBL 11.33(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40281, DWG 65B38253 SH 1 REV AP, SH 51 REV A, SH 52 REV A, SH 53 REV -, SH54 REV - & SH55 REV A. 2. JOB COMPLETED AND CONDITIONAL CHECK NORMAL.</P>SDR UIEA2024050900372Seat Track · corrodedFND M/D CGO FLOOR STRUCTURE SEAT TRACK CORROSION AT STA 1850 RBL 11.33(<P>1. REPAIR DAMAGE AREA IAW WORK SHEET 40300, EI T2024A53M-877 REV 1, DWG 65B38253 SH 46 REV AL, SH 56 REV A, SH57 REV -, SH49 REV -, SH50 REV A & SH51 REV A. 2. JOB COMPLETED AND CONDITIOSDR UIEA2023120800978Probe · unknownWHILE ON CLIMBOUT, "ALT DISAGREE" EICAS FLASHED MULTIPLE TIMES. TRIED CENTER ADC ON CAPT SIDE, MESSAGE CONTINUED TO INTERMITTENTLY OCCUR. EVENTUALLY RAN ALT DISAGREE (2 ADC'S REMAINING) CHECKLIST. ONCE THIS CHECKLIST WAS COMPLETED, DETERMINED THAT MOST LIKELY SDR UIEA2023091300829Unknown · unknownRH WING WHEEL WELL FOUND CORROSION NEXT TO DRAG BRACE(<P>1) REMOVED CORRODED "Z" CHORD FROM PANEL ASSY (65B11640-120) IAW B747 SRM 51-40-02 (WAITING FOR NEW PART) ("Z" CHORD IS MATERIAL LOSS). 2) RECEIVED STOCK CHORD, FABRICATED Z CHORD (DRILLED, TRIMMED, ALOD
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