Boeing 747-45E
Service difficulty reports · 711
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 = '74745E' 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 = '74745E' 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 IPXA2025032415971Beam · crackedLOWER CHORD CRACK OF R/H WING T/E BEAM ASSY AT NO. 7 SPOILER. AREA , WBL 296 AND WBL 303. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93195-REQ1 REV.1 JOB COMPLETED.SDR IPXA2025032415924Beam · crackedLOWER CHORD CRACK OF R/H WING T/E BEAM ASSY AT NO. 8 SPOILER. AREA , WBL 382 AND WBL 389. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93212-REQ1 REV.1SDR IPXA2025032989763Seat Track · corrodedCORROSION - MAIN DECK SEAT TRACK CORROSION BETWEEN 480 AND STA 500 , LBL 33.99. (REPLACE). .FABRICATE P/N:65B11244-7 PER BOEING DWG NO.65B11244 SH3 REV."-"; PL 65B11244-7 REV."B"; PSDL REV."-" AND EGAT WORK SHEET NO.50156 AND ORIGINAL PART AS A SAMPLE I.A.W GMSDR IPXA2025032569716Channel · corrodedRIGHT WING OUTBOARD LEADING EDGE CAVITY INSIDE, LOWER CHANNEL CORROSION, OLES 1350-1400.REPAIRED DAMAGE AREA I.A.W. UPS EO-93164-REQ1 REV.1SDR IPXA2025032645221Skin · damagedFAULT - SINK - SCREWS, L/H WING OUTBOARD AFT FLAP INBOARD SIDE EDGE (AGING A/C INSPECTION) (REPLACE). REPAIR GOUGE DAMAGE ON INBD EDGE OF L/H OUTBD AFT FLAP UPPER PANEL NEAR WBL 515 I.A.W. EGAT EI NO. F2025A57M-532 REV.1 AND UPS EO-93259-REQ1 REV.1 REVIEW COSDR IPXA2025032748217Hinge · corrodedCORROSION - HINGE, L/H AIR CONDITION ACCESS DOOR PNL NO.191ML MID SIDE. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.113 INSTALL THE HINGE MIDDLE SIDE AT PNL NO.191ML. CONDITION CHECK NORMAL. REVIEWEDSDR IPXA2025032548217Hinge · corrodedCORROSION - HINGE, L/H AIR CONDITION ACCESS DOOR PNL NO.191ML MID SIDE. (REPLACE) PAPER REVIEWED OK.SDR IPXA2025032350590Structure · crackedCRACK - CHORD, L/H WING T/E CAVITY INBD AILERON OUTBD WEB UPPER CHORD, WBL 515. (REPLACE). COMPELTED EI NO.F2025A57M-475 SEQUENCE A STEP 9.SDR IPXA2025032733616Support Fitting · crackedNO.8 SPOILER ACTUATOR FITTING, OUTBOARD LOWER CRACK (REPAIR). .I.A.W AMM 27-61-06-402-011 REV.113 CONNECT INPUT ROD AND AMM 27-61-13-404-014 REV.113 CONNECT HYDRAULIC TUBE AND I.A.W DWG 65B83501 SHEET 2 , VIEW 1C6 ZONE A3 , REV.E AND PSDL SHEET DL , REV.A AND SDR IPXA2025032329386Skin · dentedDENT - SKIN, R/H WING INBOARD AFT FLAP LOWER SKIN, 2 PLACE, (AGING A/C INSPECTION) (REPAIR). REPAIR DENTS WITH AN ESISTING REPAIR ON THE LOWER SURFACE OF THE RH WING INBD FLAP I.A.W. UPS EO-93256-REQ1 REV.1 AND EGAT EI NO. F2025A57M-505 REV.1. CONDITION CHESDR IPXA2025032433593Fitting · crackedNO.8 SPOILER ACTUATOR FITTING, INBOARD LOWER CRACK (REPAIR). REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET NO.50147. ACCOMPLISH THE REPAIR PER 747-400SF SRM 57-51-13-2R-1 REV.62.SDR IPXA2025032433614Fitting · crackedNO.7 SPOILER ACTUATOR FITTING, OUTBOARD LOWER CRACK (REPAIR). .REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET NO.50146. .JOB COMPLETED. ACCOMPLISH THE REPAIR PER 747-400SF SRM 57-51-13-2R-1 REV.62.SDR IPXA2025031130046Skin · dentedDENT - SKIN, L/H WING OUTBOARD MID FLAP, PANEL #587MT (AGING A/C INSPECTION) (REPAIR). CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 747-400SF SRM 51-70-10-2R-0 PARAGRAPH 22 REV.62. ACCOMPLISH THE REPAIR PER 747-400SF SRM (REV. 62) 57-53-01-2R-1, 51-70-10-2R-SDR IPXA2025031129315Skin · dentedDENT - SKIN, R/H WING INBOARD MID FLAP UPPER PANEL EXTERNAL SURFACE, PANEL NO.677JT (AGING A/C INSPECTION) (REPAIR). CLEAN, SEAL AND FINFISH REPAIR AREA I.A.W. 747-400SF SRM 51-70-10-2R-0 PARAGRAPH 22 REV.62. I.A.W AMM 51-24-11-477-083 REV.113, REPAINT REWORSDR IPXA2025032821491Fitting · corrodedCORROSION - FITTING, L/H WING L/E CAVITY FRONT SPAR FITTING OLES 1493.45 (REPAIR). EMOVE DAMAGE FITTING I.A.W. SRM 51-40-02-0G REV.62. PERFORM UPS EO-93174-REQ1 REV.1. INSTALL NEW FITTING I.A.W. SRM 51-40-02-0G REV.62 AND BOEING DWG NO.112U2001 SH 30 REV.D .SDR IPXA2025032821541Web · crackedCRACK - WEB, L/H WING INBD AILERON OUTBD WEB, WBL 515, TOTAL: 2 AREA (REPLACE). ACCOMPLISH THE REPAIR PER EO-93194-REQ1 (N579UP: LEFT WING FIXED TRAILING EDGE RIB WEB AT WBL 515 DAMAGE - ALTERNATE MATERIAL).SDR IPXA2025032621567Access Panel · corrodedCORROSION - BRACE, R/H AIR CONDITION ACCESS PNL NO.192ER STA 1059.9 RBL 57.7.FOUND CHAFE DAMAGE THRU CHAFE PLATE 100% MATERIAL LOSS, REMOVED CHAFE PLATE AS REQUIRED IAW SRM 53-19-12 PARA 5.INSPECTED AND VERIFIED RECEIVING MATERIAL FOR LEFT LOWER HORIZ. STAB.INSDR IPXA2025032321569Support Fitting · crackedCRACK - FITTING, INBD LOWER SIDE OF L/H WING NO.6 SPOILER MID SUPPORT FITTING (REPAIR). .REPAIR DAMAGE AREA I.A.W. SRM 57-51-13-2R-1 REV.62 AND EGAT WORK SHEET NO.50142. ACCOMPLISH THE REPAIR PER 747-400SF SRM 57-51-13-2R-1 REV.62.SDR IPXA2025031321601Fitting · crackedCRACK - FITTING, INBD LOWER SIDE OF L/H WING NO.5 SPOILER MID SUPPORT FITTING (REPAIR). I.A.W AMM 27-61-06-402-011 REV.113 CONNECT THE INPUT ROD AND AMM 27-61-13-404-014 REV.113 CONNECT THE HYDRAULIC TUBE AND I.A.W DWG 65B83501 SHEET 3, VIEW 1A10, ZONE A7, RESDR IPXA2025031321427Stiffener · corrodedFAULT - CORROSION - STIFFENER, L/H AIR CONDITION ACCESS PNL NO.191LL FWD INBD SIDE (REPLACE). REMOVE DAMAGE PARTS I.A.W. SRM 51-40-02-0G REV.62. FABRICATE P/N:65B11233-69 PER BOEING DWG NO.65B11233 SH.2 REV."G";PL REV."D";PSDL REV."-" AND EGAT WORK SHEET NO.50SDR IPXA2025032593531Support Beam · corrodedCORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1530 ~ OLES 1535 (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93163-REQ1 REV.1.SDR IPXA2025032593591Support Beam · corrodedCORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1535 ~ OLES 1540 (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93161-REQ1 REV.1. ALL PAPERWORK REVIEWED AND C/WSDR IPXA2025032593475Support Beam · corrodedCORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1425 (REPAIR). .REPAIR DAMAGE AREA I.A.W. UPS EO-93160-REQ1 REV.1. ALL PAPERWORK REVIEWED AND C/WSDR IPXA2025031093354Splice Plate · corrodedCORROSION - PLATE, UPPER FACE OF L/H WING L/E LOWER PNL, OLES 1545 (REPLACE). FABRICATE P/N:65B11862-36 PER BOEING DWG NO:65B11862 SH 2 REV. "F";PL REV."N";PSDL REV."-", AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV 10.1 REQUIREMENT . INSTALL FABSDR IPXA2025031252166Panel · debondedDISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N: 186U1006-3 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). INSTALL L/H VERTICAL STAIBLIZER PANEL P/N:186U1006-3 I.A.W. UPS EO-93144-REQ1 REV.1.SDR IPXA2025031252215Panel · debondedDISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N:186U1002-2 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). REPAIR DISBOND ON LH FWD LWR VST FORWARD TORQUE BOX PANEL I.A.W. EGAT EI NO. F2025A55M-398 REV.1 AND UPS EO-93198-REQ1 RESDR IPXA2025031252237Panel · debondedDISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N: 186U1001-2 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). REPAIR DISBOND DAMAGE ON LH AFT LWR VST FORWARD TORQUE BOX PANEL I.A.W. EGAT EI NO. F2025A55M-394 REV.1 AND UPS EO-93197SDR UIEA2025012300105Engine · making metal1.5 HOURS INTO FLIGHT, #4 OIL QUANTITY DROPPED TO 6 QTS. AT ABOUT 2.5 HOURS, QTY SHOWED 0. AT ABOUT 3 HOURS, OIL PRESSURE DROPPED TO 13 PSI AT LANDING. STATUS MESSAGE ENG 4 OIL PRESS(<P>CHECK OIL IND, IND AT 0, VISUALLY CHECK OIL CAPACITY, CAPACITY AT 0. SDR IPXA2025011255732Relay · faultedSTATUS MESSAGE MD CGO MID LP B REPLACED SMOKE DETECTOR 6B1 AND 6B2 SEPERATLY AFTER EACH OTHER IAW AMM 26-14-01/401 REV. 112; NO HELP. TEST ALWAYS PASS, BUT STS MSG ALWAYS BACK ACTIVE AFTER A FEW SECONDS. ALL SMOKE DETECTORS ARE INSTALLED BACK IN THERE ORIGINSDR IPXA2025011347308Warning Message · illuminatedMD CGO MID LP B NO STS MSG PRESENT. FIRE/OVHT DETECTION SYSTEM OPS TEST ACC AMM 26-10-00-715-001 R112 PASS.SDR IPXA2025010567156Skin · contaminatedCORROSION ON R/H WING LOWER SKIN UPPER SURFACE NEAR OLES 1455 AND 1462.(REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-92447-REQ1 REV.1.SDR IPXA2025010967139Skin · corrodedCORROSION ON R/H WING LOWER SKIN LOWER SURFACE NEAR OLES 1423.5. (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-92449-REQ1 REV.1.SDR IPXA2025010967137Skin · corrodedCORROSION ON R/H WING LOWER SKIN UPPER SURFACE NEAR OLES 1390.75. (REPAIR). ACCOMPLISHED REAPIE I.A.W UPS EO-92448-REQ1 REV.1. JOB COMPLETED AND ATTACHMENT ARE UPLOADED. REVIEWED COMPLETEDSDR IPXA2025010649808Plate · corrodedCORROSION FOUND UNDER NUTPLATES FOR LAV SERVICE AREA. 1.REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.61 2.FABRICATE P/N(146U8023-2) PER BOEING DWG NO.146U8023 SH 4 REV."-";PL REV."N";PSDL REV."D" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV.9 REQSDR IPXA2024122013341Circuit Card · faultedDURING PRE-DEPARTURE CHECK FOUND CARGO FIRE MD ZONE 6 LOOP-A FAIL NO CURENT FAULT FOUND. C/O FIRE TEST IAW AMM 26-11-00-715-001 REV 112. CHECKED SATIS. THIS CLOSES DMI. PLACARD REMOVED.SDR UIEA2024122401183Smoke Detector · false activationON ARRIVAL, FIRE CGO AFT EICAS MSG, FIRE NOT SUSPECTED. LOOP FAILURES NOTED(<P>R/R SMOKE DETECTORS EQUIPMENT #9129, 9123, 9119 & 9133 IAW AMM 26-16-01/401 & IPC 26-16-00-02N. OPS CHK GOOD.</P>)SDR UIEA2024122001178Fire Warning · false activationAFT CARGO FIRE WARNING DURING TAXI WITH MOMENTARY STATUS MSG "FIRE DET AFT 2". FIRE CARGO AFT" WARNING DURING TAXI WITH STATUS MSG "CARGO DET AFT 2". TRANSFERRED TO MEL 26-16-01-02-02A MX ACTIONS COMPLIED WITH MDDR 222676. SWAPPED LOWER AFT CARGO SMOKE DETESDR UIEA2024121701172Fire Warning · false activationAFT CARGO FIRE WARNING DURING TAXI WITH MOMENTARY STATUS MSG "FIRE DET AFT 2". AFT CARGO DETECTOR 1A AND 2A INOP.(<P>PERFORMED OPS CHECK AND GROUND TEST FOR CARGO FIRE DETECTION SYSTEM. THIS CLEARS DMI, PLACARDS REMOVED. 0733Z/JE. </P>)SDR IPXA2024120643306Switch · dirtyDOOR U/D FLT LK ADVISORY AND SUBSEQUENT STATES MESSAGE ON CLB OUT. RAN QRH PROCESSED NORMALLY. OPENED LEFT UPPER DECK DOOR. CLEANED SWITCHES AND CYCLED SEVERAL TIMES WITH NORMAL EICAS INDICATION IAW AMM. 52-23-00-862-001/003. OK FOR CONTINUE IN SERVICE.SDR IPXA2024121096511Fire Loop · warning message*** SUPPLEMENTAL SDR *** MD CGO AFT LP A STATUS MESSAGE IN CRUISE. REFERENCE BARCODE T3F18E005PVTB FOR CORRECTIVE ACTION FOR R&R OF MD CARGO DETECTORS A111 AND A211. DMP REVERSED, PLACARD REMOVED.SDR IPXA2024120396511Warning Message · illuminatedMD CGO AFT LP A STATUS MESSAGE IN CRUISE. ACCOMPLISHED DMP WITH REFERENCE TO MEL/DMP 26-14-1-2-3-1. PLACARD INSTALLED. OPENSDR IPXA2024120493434Fire Detector · false activationMD CARGO AFT LP A STATUS MSG PERFORMED FIRE TEST IAW AMM 26-14-00-710-801. OPS CHECK NORMAL. MESSAGE CLEARED.SDR IPXA2025011324042Hinge · crackedLAVATORY SERVICE DOOR LATCH BROKEN AND PIANO HINGE CRACKED. PLEASE DEFER PER CDL 52-49-3 REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.61. FABRICATE P/N(146U8023-2) PER BOEING DWG NO.146U8023 SH 4 REV."-";PL REV."N";PSDL REV."D" AND ORIGINAL PART AS A SAMPLE SDR IPXA2024102523568Handle · looseMAIN ENTRY DOOR HANDLE LOOSE RETIGHTENED MAIN ENTRY DOOR EXTERNAL HANDLE IAW AMM 52-11-13. OPS OKSDR IPXA2024082676285Structure · brokenLOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) INSTALLED 2(EA) BALL MAT PANELS IN LWR AFT PIT AT STATIONS 1840 AND 1900 PER AMM 25-53-15-400-801, PDU OPS CHECK GOOD PER AMM SUBTASK 25-53-01-864-03SDR IPXA2024082176285Structure · brokenLOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) OPENSDR IPXA2024080588574Window · delaminatedCAPT€™S #1 (FRONT) WINDSHIELD DELAMINATING ON TOP SECTION OF WINDOW COMPLETED WINDOW INSLALL WITH REF TO B747 MM 56-11-01. PERFORMED WIPER OPS CHECK WITH REF TO B747 MM 30-42-00.SDR UIEA2024080100765Circuit Card · faultedAFT CGO FIRE WARNING ON SHORT FINAL. R & R AFOLTS AFT CGO CIRCUIT CARD YLPA032 IAW AMM 26-10-01 & IPC 26-14-02-01. OPS CHECK / GND TEST PASS. NO DEFECTS NOTED. OK FOR SERVICE.SDR IPXA2024071862660Hmu · inoperativeON DECENT GOT #3 GEN ELECT FAIL. THEN ENG 3 FAILED APPEARED. N1 WAS AROUND 28%. ENGINE RETURNED TO NORMAL IDLE. ENG FAIL MESSAGE LASTED ABOUT 20 SECONDS NO OTHER PROBLEMS WITH ENG. CREW REPORTS CLEAR GOOD WEATHER DURING FAULT. REF FIM TASK 71-00 TASK A72 AND 7SDR UIEA2024070700597Tire · failedABNORMAL VIBRATION ON TAKE OFF BEGINNING APPROX AT 110-120 KNOTS. DECIDED TO CONTINUE. TOWER ADVISED DEBRIS FOUND ON RUNWAY. AFTER LANDING CONFIRMED 2 BLOWN TIRES. #9 & #10 MLG TIRE BLOWN CONDITIONAL INSPECTION C/W PER AMM, FOUND DURING TO RH WING TO BODY FAI
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