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 UIEA2024060800509Structure · damagedCHORD P/N: 65B07942U72 FOUND 11EA FASTENER LOCATION S.E.M.(<P>FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER AS PER RI-53-00-16880 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024060800510Structure · damagedCHORD P/N 65B07942U16 1EA FASTENER HOLE S.E.M.(<P>CHORD S.E.M. FASTENER HOLE 1EA REPLACED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061000511Structure · damagedCHORD PN 65B07941U111 FOUND 14EA FASTENER HOLES S.E.M.(<P>14EA FASTENER HOLES REPAIRED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061000512Fitting · damagedFITTING FOUND 2EA FASTENER HOLES S.E.M.(<P>S.E.M. CONDITION ACCEPTED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024040500265Skin · corrodedCORROSION - SKIN LEFT UNDERWING REAR SPAR OVERRIDE JETTISON PUMP AREA.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 119 2. ACCOMPLISHED EI T2024A57M-345 REV 1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024040500264Skin · corrodedCORROSION - SKIN, LH WING INSPAR UPR SURFACE T/E AREA WS 469.82 ~ WS 478.80 REAR SPAR AREA(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB CARD ATTACHISDR UIEA2024040500263Beam · corrodedCORROSION - FOUND L/H H.S.T T/E BEAM ELEV STA 257 LOWER CHORD CORROSION(<P>1. ACCOMPLISH EI T2024A55M-509 REV 0 2. ACCOMPLISHED EI T2024A55M-509 REV 1 3. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024040500262Fairing · corrodedCORROSION ON AFT WTB FAIRING LWR CHORD AT STA 1480. LBL 16 ~ RBL 16(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. FABRICATED PART IAW WORKSHEET 40232 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 120 AND DWG 65B15085 SH4 REV L & 65B15085 SSDR UIEA2024040500261Bracket · corrodedCORROSION-BRACKET, LH WING T/E CAVITY HYD TUBE BLOCK - CLAMP WBL 178(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-OG-0 REV 120 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 120 AND DWG 65B14463 SHEET 5 REV K & SHEET 9 REV J 3. JOB COMPLETED</P>)SDR UIEA2024040500260Floorbeam · nonePERFORM EO A453B457 SEC 42 UPPER DECK FLOOR BEAM REPEAT INSP FOUND FILLED DEVIATION AT STA 660 RBL 13(<P>1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-01 REV 120 2. PERFORM EI T2024A53M-758 REV 0 SEQUENCE A 3. ACCOMPLISHED EI T2024A53M-758 REV 2 4. JOB COMPLETEDSDR UIEA2024040500259Spar · crackedFOUND LH WING FRONT SPAR WEB CRACK NEAR FSSI 656(<P>1. REPAIR DAMAGED AREA IAW EI T2024A57M-424 REV 4 2. ACCOMPLISHED EI T2024A57M-424 REV 5 3. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024040500258Skin · corrodedFOUND LH WING LOWER SKIN HAVE CORROSION AT FSSI 628 ~ FSSI 660(<P>1. REPAIR DAMAGED AREA IAW EI T2024A57M-480 REV 6 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024040500257Skin · corrodedCORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3102-3) UPPER SURFACE NEAR WS 323.82 (WBL 150.00) , S-16 ~ S-17(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSSDR UIEA2024040500256Skin · corrodedCORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WS 469.82, S-3 ~ S-4(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB CSDR UIEA2024040500255Skin · corrodedCORROSION DAMAGES ON THE LH WING UPPER SKIN (P/N= 112U3101-3) UPPER SURFACE NEAR WBL 150.00, MID SPAR(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV=120 2. BLENDED OUT THE DAMAGE AREA IAW SRM 517-20-01-1A-A REV 120 3. PFM NDT INSP REFER TO JOB SDR UIEA2024040500254Channel · crackedCRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE FOWARD CHANNEL AT STA 960LH(<P>1. ACCOMPLISHED TENSION TIE REPAIR AT LH STA 960 BETWEEN STR 10R AND 10L IAW EI T2024A53M-428, SEQUENCE A PART 3 REV 0 2. ACCOMPLISHED EI T2024A53-428 REV 1 AND EI ATTACHED TO W/O 9210SDR UIEA2024040500253Frame · crackedCRACK-FRAME, SEC 42 UPPER DECK TENSION TIE AT THE AREA OF ATTACHMENT TO FRAME 1 EA HOLE, AT STA 960 RH(<P>1. ACCOMPLISHED FRAME WEB REPAIR AT RH STA 960 BETWEEN STR 10R AND 10R IAW EI T2024A53M-428, SEQUENCE A PART 4 REV 0 2. ACCOMPLISHED EI T2024A53-428 REV 1SDR UIEA2024040500252Channel · crackedCRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE - FOWARD CHANNEL AT STA 900 LH(<P>1. ACCOMPLISHED TENSION TIE REPAIR AT LH, STA 900 BETWEEN STR 9L AND 10L IAW EI T2024A53M-428. SEQUENCE A PART 1 REV=0 2. ACCOMPLISHED EI T2024A53M-428 REV=1 3. CONDITION CHECK NORSDR UIEA2024040500251Channel · crackedCRACK-CHANNEL, SEC 42 UPPER DECK TENSION TIE - FOWARD CHANNEL AT STA 940 RH(<P>1. ACCOMPLISHED TENSION TIE REPAIR AT RH STA 940 BETWEEN STR 10R AND STR 10AR IAW EI T2024A53M-428. SEQUENCE A PART 3 REV=0 2. ACCOMPLISHED EI T2024A53M-428 REV=1 AND EI ATTACHED TOSDR UIEA2024040500250Door Frame · corrodedCRACK-VERTICAL FRAME, L2 MAIN ENTRY DOOR FWD UPPER SIDE.(<P>1. PERFORM EI T2024A52M-488, SEQUENCE A REV=0 2. ACCOMPLISHED EI T2024A52M-488 REV=1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024040500249Door Frame · corrodedFIND DOOR R1 AFT LOWER SIDE FRAME WEB CORROSION(<P>1. PERFORM EI T2024A52M-491, SEQUENCE A. REV=0 2. ACCOMPLISHED EI T2024A52M-491. REV=1 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024040500248Frame · crackedCRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1060, WL 329(<P>1. ACCOMPLISH EI T2024A53M-432 REV:1, SEQUENCE A PART 1: FRAME WEB SHEAR TIE REPAIR AT STA 1060 LH 2. ACCOMPLISHED EI T2024A53M-432, REV 2 AND EI ATTACHED TO WO 9213289(722) 3. JOB COMPLETED ANSDR UIEA2024040500247Frame · crackedCRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1100, WL 329(<P>1. ACCOMPLISH EI T2024A53M-432 REV:1, SEQUENCE A PART 5: FRAME WEB SHEAR TIE REPAIR AT STA 1100 LH 2. ACCOMPLISHED EI T2024A53M-432, REV 2 AND EI ATTACHED TO W/O 9213289(1722) 3. JOB COMPLETED SDR UIEA2024040500246Frame · crackedCRACK-FRAME, RH INTERNAL FUSELAGE FRAME WEB AT STA 1080, WL 329(<P>1. FRAME WEB SHEAR TIE REPAIR AT STA 1080 RH IAW EI T2024A53M-432, SEQUENCE A PART 4 REV=01 2. ACCOMPLISHED EI T2024A53M-432. REV: 2 3. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2024040500245Frame · crackedCRACK-FRAME, RH INTERNAL FUSELAGE FRAME WEB AT STA 1060, WL 329(<P>1. FRAME WEB SHEAR TIE REPAIR AT STA 1060 RH IAW EI T2024A53M-432, SEQUENCE A PART 2 REV=01. 2. ACCOMPLISHED EI T2024A53M-432, REV=2 AND EI ATTACHED TO W/O 9213289(722) 3. JOB COMPLETED AND CONSDR UIEA2024040500244Frame · crackedCRACK-FRAME, LH INTERNAL FUSELAGE FRAME WEB AT STA 1080, WL 329(<P>1. ACCOMPLISH EI T2024A53M-432, REV=1, SEQUENCE A PART 3, FRAME WEB SHEAR TIE REPAIR AT STA 1080 LH 2. ACCOMPLISHED EI T2024A53M-432 REV 2 AND EI ATTACHED TO W/O 9213289(722) 3. JOB COMPLETED ASDR UIEA2024040500243Frame · crackedCRACK- FRAME - RH INTERNAL FUSELAGE FRAME WEB AT STA 1100, WL 329(<P>1. FRAME WEB SHEAR TIE REPAIR AT STA 1100 RH IAW EI T2024A53M-432, SEQUENCE A. REV=1 PART 6 2. ACCOMPLISHED EI T2024A53M-432, REV=2 AND EI ATTACHED TO W/O 9213289 (722) 3. JOB COMPLETED AND CSDR UIEA2024040500242Frame · crackedFND BULK CGO BILGE FRAME CRACK AT STA 2260 RBL 53(<P>1. REPAIRED CRACK AREA IAW EI T2024A53M-518 REV-1, SEQUENCE B. 2. ACCOMPLISHED EI T2024A53M-518, REV=2 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2024040500241Skin · dentedDENT- PANEL 587LT EXTERNAL, LH OUTBD MID FLAP WBL 582(<P>1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD MID FLAP TOP PANEL 587LT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISDR UIEA2024040500240Skin · dentedDENT- LH OUTBD FORE FLAP OUTBD TOP PNL EXTERNAL WBL 655(<P>1. PERFORM REPAIR OF DENT SKIN DAMAGE AT L/H WING OUTBD FORE FLAP TOP PANEL EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISFASDR UIEA2024040500239Skin · dentedDENT PANEL 677IT EXTERNAL SURFACE, RH INBD MID FLAP WBL 373.33(<P>1. PERFORM REPAIR OF DENT SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SDR UIEA2024040500238Skin · dentedDENT- SKIN, R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACEWBL 374.83(<P>1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD MID FLAP PANEL 677IT EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDISDR UIEA2024040500237Skin · chafedCHAFING - SKIN PNL, RH WING INBD AILERON OUTBD TE UPPER SKIN WBL 515(<P>1. PERFORM REPAIR OF CHAFING SKIN DAMAGE AT R/H WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFORMATION. 2. CONDITION CHECK IS SATISFSDR UIEA2024030530142Circuit Card · faultedRTO DUE TO AFT CARGO FIRE WARNING DURING T/O ROLL.(<P>REMOVED AND REPLACED AFT CARGO AFOLTS CARD (A32). SYSTEM GROUND TEST PASSED IAW AMM 26-10-01</P>)SDR IPXA2024021728160Battery · inoperativeFOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE) C/W I.A.W AMM 33-51-04-902-001-001 REV.109 REPLACED THE EMERGENCY LIGHT BATTERY (M5056) AT UPPER DECK,AND PERFORMED UPPER DECK EMERGENCY LIGHT OPERATIONAL TEST, RESULT WAS SATISFACTORY. ISDR IPXA2024021228160Light · inoperativeSDR FILED OPEN. FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE)SDR UIEA2024020700073Start Valve · faultedREJECTED TAKE OFF DUE TO AIRCRAFT SURGING. LOW SPEED REJECT(<P>#2 START VALVE FOUND NOT FULLY CLOSED, NOT ALLOWING ENG TO ACCELERATE, WITHIN NORMAL PARAMETERS. #2 ENG VALVE REPLACED PER AMM 80-11-02. PERF INLET AND EXHAUST INSP PER AMM 72-00-00, NO DEFECTS NOTSDR UIEA2024020700072Start Valve · faultedENG 2 LAGGING BEHIND OTHER 3 ON APPLICATION OF TAKEOFF POWER. AIRCRAFT YAWED SLIGHTLY TO THE LEFT, SPEED IN THE 20 TO 30 KNOT RANGE WHEN TAKEOFF REJECTED. #2 START VALVE FOUND NOT CLOSED AND WOULD NOT CLOSE.(<P>START VALVE AND STARTER BOTH REPLACED IAW AMM 80-SDR IPXA2024013125856Snubber · out of limitsFOUND L4 ENTRY DOOR SNUBBER INDICATOR OUT OF LIMIT. (REPLACE) C/W 1. I.A.W AMM 52-11-10-004-001 REV. 109 AND AMM 52-11-10-404-005 REV. 109 REPLACE SNUBBER. 2. IPC VERIFIED AND SERVICEABLE PARTS TAG NO. 983747. 3. JOB COMPLETE AND CONDITION CHECK NORMAL.SDR UIEA2024012300019Circuit Card · faultedAFT CARGO FIRE WARNING ON FINAL APPROACH AND AGAIN ON THE GROUND. PRECEDED BY AFT CARGO #2 LOOP A AND AFT CARGO #3 LOOP B STS MSG.(<P>REMOVED AND REPLACED A33 AFOLTS CARD AS PER AMM 26-10-01-004-001. OPS CHECK OK</P>)SDR IPXA2024021230568Tension Tie · cracked*MAJOR REPAIR* FAULT - CRACK - FND TENSION TIE CHANNEL FWD SIDE CRACK AT STA 1120 L/H (REPAIR) ACCOMPLISH REINFORCING REPAIR I/A/W B747-400SF (REV. 58) SRM 53-40-30-2R-2 (FIGURE 201). 1.ACCOMPLISH INSPECTION I/A/W B747-400SF (REV. 58) SRM 53-40-30-2R-2, TABLE SDR IPXA2024021610259Skin · dentedDENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) 1.REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (DIAMETER:1",DEPTH:0.0175",32.5" FROM FORWARD EDGE,25.5" FROM LOWER EDGE). FILL THE DAMAGE AREA WITH ADHESIVE CURED ASDR IPXA2024021610224Skin · dentedDENT - SKIN SURFACE AT 10 O'CLOCK, NR 1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.7",DEPTH:0.012",30.4" FROM FORWARD EDGE,38" FROM UPPER EDGE). FILL THE DAMAGE AREA WITH ADHESIVE SDR IPXA2024011810224Skin · dented*** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 10 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORKSDR IPXA2024011810259Skin · dented*** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORKSDR IPXA2024022347664Skin · crackedCRACKED SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) INSTALLED NEW PART I.A.W. SRM 51-40-02-0G REV.58 AND BOEING DWG NO:65B15168 SH.2 REV.G AND AIPC 27-81-02-01 REV.54. I.A.W AMM 27-81-02-404-010 REV.109 STEP 3.A TO 3.E.(5), INSTALL LH WING NO. 1SDR IPXA2024022347710Skin · brokenBROKEN SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) C/W 1. OK TO INSTALL PANEL NO: 521EB. 2. I.A.W AMM 20-51-01-912-008 REV.109 INSTALL PANEL NO: 521EB. 3. CONDITION CHECK NORMAL. 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING UP SURFACE AND ROLLER PAINT. 2.JOB SDR IPXA2024021647771Panel · debondedLEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING UP SURFACE AND ROLLER PAINT. 2.JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2024021645990Fairing · damagedNR 8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.5",AT UPPER EDGE,5" FROM AFTER EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTSDR IPXA2024021645522Stiffener · cracked*** SUPPLEMENTAL SDR *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W AMM 27-31-01-404-015 REV.109 STEP 3.H(14) TO 3.H(23) ADJUST R/H INBOARD ELEVATOR AND OPERATION.
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