Boeing 747-47UF
Service difficulty reports · 3,116
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 = '74747UF' 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 = '74747UF' 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 KRDY2025061714786Engine · fireN476MC FLT 5Y 8208 AFTER T/O ENGINE # 1 WAS FIRE, SO CREW TAKE THE DECISION TO DIVERT TO GYE. PLS SEE ALSO MSR-14785.SDR UIEA2025061200758Engine · failedENGINE 1 DUAL FIRE LOOP INDICATION CONFIRMED BY VISUAL OF FLAME COMING FROM INTAKE AND SMOKE OUT EXHAUST AFTER DISCHARGING BOTH FIRE BOTTLES. C/W ENGINE CHANGE PER TASK CARD 71-099-02-01. NO FURTHER DEFECTS NOTED. ORIGINAL SUBMISSION DATE; 6/16/2025.SDR KRDY2025061714785Engine · fireACFT N476MC FLT 5Y8208 B747C DEPARTED FROM UIO, AFTER DEPART ENG #1 WAS FIRED SO CREW TOOK THE DECISION TO DIVERT TO GYE. ACFT LAND ON GYE, TOWED TO POSITION 13. A RIDING MECHANIC FROM ATLAS IS IN CHARGE OF THE TECHNICAL RELEASE AND WE PROVIDE MECHANIC ASSISDR UIEA2025052700699Lug · cracked1EA CRACK WAS FOUND ON LH STA 1000 LBL 11.33 FRONT SPAR INTERCOSTAL LUG FITTING.(<P>FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052700700Lug · cracked1EA CRACK WAS FOUND ON RH STA 1000 RBL 11.33 FRONT SPAR INTERCOSTAL LUG FITTING.(<P>FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 7 STEP 3. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052900703Panel · crackedCOCKPIT CTR CONSOLE LH FWD VERTICAL METAL PNL LWR CORNER NEAR I/B RUDDER PEDAL FOUND CRACK.(<P>PANEL CRACK AREA REPAIRED AS PER RI-25-10-17662 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052900704Panel · crackedCOCKPIT - CTR CONSOLE RH FWD VERTICAL METAL PANEL LWR CORNER NEAR I/B RUDDER PADAL FOUND CRACK.(<P>PANEL CRACK AREA REPAIRED AS PER RI-25-10-17662 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100708Skin · dentedLHW I/B MID FLAP FAIRING EXTERIOR SURFACE FOUND DENT.(<P>PERFORMED REPAIR AT DENT AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100709Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100710Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100711Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100712Skin · delaminatedRHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200713Structure · damagedLHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200714Structure · damagedLHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200715Structure · damagedRHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300719Thrust Reverser · delaminated#4 ENG O/B T/REV INNER WALL FOUND DELAMINATED AT FWD 3 O'CLOCK POSITION(<P>DELAMINATE AREA REPAIRED AS PER ATLAS AIR EA-1978A219 REV O FIG 2. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300720Longeron · cracked1 EA CRACK WAS FOUND ON RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA.(<P>LONGERON EXTENSION FITTING MOD CARRIED OUT AS PER ATLAS AIR EO NO: 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300721Frame · cracked1 EA CRACK WAS FOUND AT FASTENER HOLE 6 O'CLOCK POSITION AT RH BS 1480 B/HEAD FRAME WEB I/B UPPER AREA. FRAME WEB REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.SDR UIEA2025060600730Skin · damagedNOSE CARGO DOOR (P/N: 65B13016-10, S/N: 000123) BIRD STRIKE DAMAGE STA 140 AND STA 200, BETWEEN S31R AND S42AR NOSE CARGO DOOR SKIN, FRAMES AND STRINGERS - CAT B PERMANENT REPAIRS.(<P>NOSE CARGO DOOR SKIN DENT #1 AND DENT #2 REPAIRED AS PER RI-52-30-17671 REV SDR UIEA2025060600731Stringer · damagedNOSE CARGO DOOR BIRD STRIKE DAMAGE REPETITION INSPECTION FINDING STA 160 STR 36R, FOUND DENT. STRINGER REPAIRED AS PER RI-52-30-17671 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060600732Door · damagedNOSE CARGO DOOR BIRD STRIKE DAMAGE REPETITION INSPECTION FINDING STA 180 BTN STR 31AR AND STA 34R. DOUBLER FOUND TOOL MARK. FRAME TOOL MARK AREA REPAIRED AS PER RI-52-30-17671 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025060800737Plate · crackedLH BLG I/B W/W DOOR CHAFE PLATE FOUND CRACK.(<P>LH BLG I/B W/W DOOR CHAFE PLATE REPLACE AS PER HX RI-32-14-17675 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060700734Starter · faultedENG 1 OIL PRESS EICAS MSG. ENG 1 OIL QTY DROPPED ON INITIAL CLIMB, PRESSURE DECREASED STEADILY UNTIL ENG 1 SHUT DOWN IN FLIGHT. ENG WINDMILL FOR 15 MINUTES.(<P>FOUND PACKING ON STARTER SHAFT CUT. REPLACED PACKING. INSPECTED MCD, FOUND SMALL QTY METAL SHAVING CSDR UIEA2025060300718Rivet · looseAPU COMP-WL 310RH STA 2669-2690 FRAME RIVET FOUND LOOSE.(<P>APU COMP-WL290-WL330, STA 2658 - STA2701.5 RH, FUSELAGE EXTERNAL BONDED SKIN ASSY MULTIPLE FASTENER HOLE ELONGATED AREA REPAIRED IAW RI-53-80-17668 REV. A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060500729Fitting · looseRIGHT WING FIXED T/E GROUND SPOILER I/B SUPPORT RIB AT WBL 255.692 UPR FWD SUPPORT FTG LOOSE. RT WING FIXED T/E GROUND SPOILER I/B SUPPORT RIB AT WBL 255.692 UPR FWD SUPPORT FTG 69B11632-14 ASSY REPLACED AND INSTALLED IAW RI-57-51-17673 REV A. NO FURTHER DEFESDR UIEA2025052800702Actuator · faultedGEAR CONFIG WARNING ON TAKEOFF. R & R BODY L/H ACTUATOR AND OPS CHECK GOOD IAW AMM 32-53-11 & IPC 32-53-11-05A ITEM 65.SDR UIEA2025052600695Panel · damagedDURING DESCENT, A/C EXPERIENCED HIGH FREQUENCY VIBRATIONS DURING SPEED BRAKE APPLICATIONS. ONCE LANDED IN HKG, STATION NOTICED THE #6 SPEED BRAKE PANEL ASSY DAMAGED / SEPERATED IN FLIGHT.(<P>R/R #6 SPOILER IAW AMM 27-62-01 AND OPERATIONAL CHECKS NORMAL</P>)SDR UIEA2025052300679Switch · inoperativeBLEED 2 OVHT / PRV EICAS MSG. QRH PROCEDURE IND NO NAI AVAILABLE FOR ENG #2.(<P>REMOVED AND REPLACED BLEED 2 OVHT SWITCH REF AMM 36-22-01 & AIPC 36-22-01-01, OPS CHECK GOOD. NO LEAKS DETECTED. PERFORMED MPA RUN AS REQUESTED, NO FAULTS FOUND REF AMM 71-00-00-71SDR UIEA2025050600588Support Fitting · gougedLH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING I/B AND O/B SIDE FACE FOUND GOUGE MARK. LH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING I/B AND O/B SIDE FACE MACHINED AS PER B747-400F SRM 53-40-90 REPAIR 1 REV. 103 AND FOUND WITHIN WORK LIMIT. FOR DETAILS RSDR UIEA2025050900591Panel · corrodedRH BODY GEAR W/W FIXED PANEL INNER SURFACE, JUST BELOW APU FIRE SHUT OFF MODULE. FOUND SURFACE CORROSION. RH BODY GEAR W/W FIXED PANEL INNER SURFACE JUST BELOW APU FIRE SHUT OFF MODULE SURFACE CORROSION FOUND OUT OF LIMITS AS PER B747-400F SRM 53-00-71-1A-1 RSDR UIEA2025051100592Skin · damagedFUSELAGE STA 162, STR 23L-24L FOUND LIGHTNING STRIKE AS MARKED. FUSELAGE STA 162, STR 23L-24L LIGHTNING STRIKE REPAIRED AS PER B747-400F SRM 53-00-01 REPAIR 9 REV.103. NO FURTHER DEFECTS NOTED.SDR UIEA2025051100593Skin · damagedFUSELAGE STA 154, STR 20R - 22R FOUND LIGHTNING STRIKE AS MARKED. FUSELAGE STA 154, STR 20R - 22R LIGHTNING STRIKE REPAIRED AS PER B747-400F SRM 53-00-01 REPAIR 9 REV.103. NO FURTHER DEFECTS NOTED.SDR UIEA2025051100594Skin · damagedFUSELAGE STA 493, STR L27A - L28A FOUND LIGHTNING STRIKE AS MARKED. FUSELAGE STA 493, STR L27A - L28A LIGHTNING STRIKE REPAIRED AS PER B747-400F SRM 53-00-01 REPAIR 9 REV.103. NO FUTHER DEFECT NOTED.SDR UIEA2025051100595Seat Track · corrodedMAIN DECK CARGO SEAT TRACK, FOUND CORROSION BETWEEN STA 1000 AND STA 1020, LBL 11.33. MAIN DECK CARGO SEAT TRACK REPAIRED AS PER EN# 3071-25 REV.0. NO FURTHER DEFECTS NOTED.<!--ENDFRAGMENT--></P>)SDR UIEA2025051100596Trunnion · damagedSTA 1480 RH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING 65B10595-62 THE TOOL MARK BLENDOUT AND THE GROOVED HOLE DAMAGED. REQUEST FOR PERMANENT REPAIR INSTRUCTIONS.(<P>STA 1480 RH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING 65B10595-62 THE TOOL MARK BLENDOUSDR UIEA2025051400603Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FOUND CORROSION BETWEEN STA 1580 AND STA 1600, RBL 11.33(<P>MAIN DECK CARGO SEAT TRACK REPAIRED AS PER EN #3096-25 REV.0 AND B747-400F SRM 53-00-52 REPAIR 12 REV.103. NO FURTHER DEFECTS NOTED.<!--ENDFRAGMENT--></P>)SDR UIEA2025051400604Keelbeam · corrodedRH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1472, 1444 AND 1425 FOUND SURFACE CORROSION AS MARKED.(<P><!--STARTFRAGMENT-->RH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1472, 1444 AND 1425 SURFACE CORROSION REPAIRED PER <SPAN>EN# 3072-25 REV.0.</SPAN><SPASDR UIEA2025051400605Keelbeam · corrodedLH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1458, 1437 AND 1427 FOUND SURFACE CORROSION AS MARKED. LH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1458, 1437 AND 1427 SURFACE CORROSION REPAIRED PER EN# 3072-25 REV.0. ACCOMPLISHED AS PER EN# 3072-25 REV.0SDR UIEA2025031400335Fairing · dentedR/H H.STAB L/E FAIRING 341CR O/B REPAIR PATCH FND DENT(<P>DENT AREA REPAIRED AS PER SRM 55-10-01-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025031800354Channel · crackedSTA 720 RH UPPER DECK TENSION TIE FWD CHANNEL FOUND CRACK APPROX 3/8" IN LENGTH(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 (REPAIR IS CAT B). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032100363Structure · corrodedM/D STA 1175 RBL 11.33 CHORD LWR SURFACE CORRODED(<P>CHORD REPLACED AS PER SRM 51-10-02. NEW CHORD HOLES TRANSFERRED AS PER SRM 51-40-05. NEW CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032100364Lug · crackedINTERCOSTAL LUG FITTING AT STA 1000 RBL 11.33 FOUND CRACK(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 4 PART 7 STEP 3 CONDITION 11. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032200374Shear Tie · crackedSHEAR TIE AT STA 1000 RBL 33.99 FOUND CRACK(<P>SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 4 PART 8 STEP 2 CONDITION 13 AND RI-53-14-17485 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032300380Rib · crackedR/H H/STAB TIP CLOSURE RIB FOUND LOWER CHORD CRACKED(<P>CRACK LOWER CHORD REPLACED AS PER SRM 51-10-02. NEW LOWER CHORD HOLES TRANSFERED AS PER SRM 51-40-05. NEW LOWER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032300381Rib · crackedR/H H/STAB TIP CLOSURE RIB FOUND WEB CRACKED(<P>CRACK WEB REPLACED AS PER SRM 51-10-02. NEW WEB HOLES TRANSFERED AS PER SRM 51-40-05. NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032300382Rib · crackedRH H.STAB TIP CLOSURE RIB FOUND UPPER CHORD CRACKED(<P>CRACK UPPER CHORD REPLACED AS PER SRM 51-10-02. NEW UPPER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05. NEW UPPER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032500385Bulkhead · crackedLH BS 1480 B/HEAD VERTICAL WEB I/B AREA FOUND CRACK(<P>VERTICAL WEB CRACK AREA REPAIRED A PER SRM 53-40-08-2R-1 REPAIR FIG 201 AND RI-53-40-17541 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032500386Bulkhead · crackedRH BS 1480 B/HEAD VERTICAL WB I/B AREA FOUND CRACK(<P>VERTICAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201 AND RI-53-40-17541 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032500387Skin · worn#3 RH CORE COWL UPPER AFT AREA FND WORN OUT(<P>WORN OUT AREA REPAIRED AS PER SRM 54-41-01-2R-5 REPAIR 5 FIG 202 DETAIL III. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025032700391Skin · damagedFUS SECTION 48 APPROX STA 2658 - STA 2701, WL 280-WL 340 AREA FOUND FUS SKIN SEVERAL RIVETS LOOSE(<P>SKIN REPLACED AS PER RI-53-80-17492 REV B. NO FURTHER DEFECTS NOTED</P>)
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