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 UIEA2024052400432Skin · crackedRHW L/E #24 VC FLAP FOLDING NOSE ASSY FOUND CRACKED AT THE /B EDGE(<P>DAMAGED AREA REPAIRED AS PER RI-57-43-16891 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052400434Fastener · looseNO.2 ENG R/H CORE COWL FOUND SEVERAL FASTENER LOOSE(<P>#2 ENG RH CORE COWL FASTENER REPLACED IAW EA -1971A101 REV 0 AND SRM 51-40-02 REV 100 DATE 20 FEB 2024. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024052500443Skin · crackedNO.3 ENG - RH CORE COWL AFT EDGE EXTERNAL SKIN CRACK FOUND AT CENTER AREA AS MARKED(<P>NO.3 ENG - RH CORE COWL AFT EDGE SKIN REPAIRED IAW EA NO : EA-1971A099 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052500444Structure · cracked#2 ENG R/H CORE COWL EXHAUST AREA FOUND SEVERAL FASTNER HOLE CRACKED(<P>REPAIRED IAW SRM 54-41-01-2R-3 REPAIR 3 AND EA-1971A104. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052500445Skin · crackedNO.3 ENG - RH CORE COWL EXTERNAL SKIN CRACK FOUND JUST BELOW THE EXHAUST LOUVER AS MARKED(<P>REPAIRED IAW SRM 54-45-01-2R-4 REPAIR 4. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052500446Panel · damagedNO.4 PYLON 482EL SCREW HOLE FOUND ELONGATED.(<P>#4 PYLON PANEL 482EL FABRICATED IAW RI NO : RI-54-51-16889 REV A. HFEC INSPECTION C/W PER NTM PART 6 51-00-00 PROCEDURE 23 REV 176 ON BEND RAD11 AREA, NO CRACK FOUND</P>)SDR UIEA2024052600447Structure · cracked1EA CRACK WAS FOUND ON LH NOSE WHEEL WELL FORWARD CORNER FASTENER HOLE(<P>STA 240 LH SIDE PANEL CHORD P/N: 65B07942-609 CRACK AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052600448Structure · cracked1EA CRACK WAS FOUND ON THE FASTENER HOLE AT RH STA 240 #3 RD LAYER ( SHIM )(<P>STA 240 RH #3 RD LAYER ( SHIM ) FABRICATED AND INSTALLED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024052600449Doubler · noneLH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.W AND FORWARD CORNER MOD DEVIATION(<P>LH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.W AND FORWARD CORNER MOD DEVIATION AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052600450Doubler · noneRH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.W AND FORWARD CORNER MOD DEVIATION(<P>RH STA 240 NOSE WHEEL CORNER DOUBLER FOUND S.E.M AND FORWARD CORNER MOD DEVIATION AREA REPAIRED IAW RI-53-00-16890 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052600451Support Rod · corrodedLHW T/E UPR FIXED PANEL RIB SUPPORT ROD LOWER FITTING P/N : 69B11633-13 FOUND CORROSION(<P>LHW T/E UPR FIXED PANEL RIB SUPPORT ROD LOWER FITTING P/N: 69B11633-13 AND BRACKET P/N: 65B81991-41 REPLACED AND INSTALLED IAW RI-57-00-16905 REV A. NO FURTHER DEFECTS NSDR UIEA2024052000396Doubler · crackedDOOR 1 EXTERIOR LOWER HINGE DOUBLER FOUND CRACK(<P>DOOR 1 LH EXTERIOR LOWER HINGE AREA DOUBLER P/N: 65B22350-7 REPLACED AND INSTALLED IAW SRM 51-40-02 AND BOEING 65B01836 SHEET 23 REV E. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024052210398Bulb · failed2EA EMERGENCY LIGHT FOUND INOP(<P>2EA EMERGENCY LIGHT BULB REPLACED IAW AMM 33-51-07 REV 110 15MAR2024 AND OPERATIONAL TEST NORMAL IAW AMM 33-51-07 REV 110 15MAR2024.</P>)SDR 2024F00135Outflow Valve · failedON 13 MAY 2024, RECEIVED ATLAS REPORT THAT N475MC CREW REPORTED VIA SATCOM DUAL OUTFLOW VALVE FAILURE. FOUND CABIN PRESS CONT RH ICU C/B PULLED AND COLLARED ON P6 PANEL (CABIN PRESS ONTR LH ICU C/B CLOSED). LH ICU C/B SHOULD HAVE BEEN PULLED AND COLLARED IAW TSDR UIEA2024051000375Relay · failedCREW REPORTED VIA SATCOM DUAL OUTFLOW VALVE FAILURE.(<P>FOUND CABIN PRESS CONT RH ICU C/B PULLED AND COLLARED ON P6 PANEL (CABIN PRESS ONTR LH ICU C/B CLOSED). LH ICU C/B SHOULD HAVE BEEN PULLED AND COLLARED IAW THE LH OUTFLOW VALVE DMI 208466 ON 10MAY24 AT NKSDR UIEA2024042400313Engine · making metalCAUTION MESSAGE (EICAS) ENG 4 OIL FILTER IN FLIGHT. TIME 0910Z. FIRE HANDLE NOT PULLED. ENG SHUTDOWN.(<P>C/W OIL SYS CONTAMINATION EXAMINATION IAW AMM 79-00-00, FOUND EXTENSIVE CONTAMINATION LEADING TO ENGINE CHANGE REQUIRED. R/R FILTER IAW AMM 79-21-04. FOUNDSDR UIEA2024042200305Adc · faultedDURING FLIGHT BUFFET MARGIN AND STALL SPEED MARGIN DISPLAYS WERE DIFFERENT BY +/- 20KIAS FROM LEFT AND RIGHT DISPLAYS(<P>DFDR DATA DOWNLOADED & SENT TO HDQ PER AMM 31-31-01 REV 110. AOA SENSOR TEST OK (NO LIGHT) PER AMM 34-12-03 REV 110. AS PER REQUEST, R/R RHSDR UIEA2024061100513Detector · faultedEQUIPMENT COOLING EICAS MESSAGE ON DEPARTURE FROM HKG. NON NORMAL CHECKLIST COMPLETED. EICAS CLEARED. AFTER LANDING EICAS MESSAGE RETURNED. REF CMC MESSAGE 21519. DURING WIRING CHECKS IAW WDM 21-58-01 WIRE BETWEEN F/D LOW FLOW DETECTOR (M7933) PIN 2 AND EQUIPSDR UIEA2024032100165Tension Tie · crackedLH BS 860 UPR DECK TENSION TIE 1EA FASTENER HOLE FOUND CRACK ON FWD CHANNEL(<P>FWD CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100167Stiffener · crackedLH NOSE WHEEL WELL SIDE PANEL STA 265 TO 280 WL 170 STIFFENER 1EA HOLE CRACK. APPROX 3/8" IN LENGTH(<P>CRACK STIFFENER REPLACED AS PER ATLAS AIR EO 4453A043 REV 10 PART 2 STEP 2 AND STEP 3</P>)SDR UIEA2024032100168Tension Tie · crackedLH BS 860 UPR DECK TENSION TIE 1EA FASTENER HOLE FOUND CRACK ON AFT CHANNEL(<P>AFT CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100169Ladder · crackedM/D - CREW LADDER #7 STEP FWD & AFT AREA FOUND CRACK (FROM BOTTOM)(<P>CRACK STEP FWD AND AFT AREA REPAIRED AS PER RI-25-50-16803 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100171Panel · damagedM/D - STA 1720 L/H DADO PANEL FOUND DAMAGE(<P>DAMAGE AREA REPAIRED AS PER RI-25-21-16797 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100173Panel · crackedM/D STA 1940 L/H DADO PANEL FOUND CRACK(<P>CRACK AREA REPAIRED AS PER RI-25-21-16795 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100174Fitting · cracked1EA CRACK WAS FOUND ON BS 1000 LBL 11.33" INTERCOSTAL LUG FTG APPROX 1"(<P>CRACK INTERCOSTAL LUG FTG REPLACED AS PER ATLAS AIR EO 4453C024 REV 3 PART 3. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100175Fitting · cracked1EA CRACK WAS FOUND ON BS 1000 RBL 11.33" INTERCOSTAL LUG FITTING APPROX 1" IN LENGTH(<P>CRACK INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV 3 PART 7. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100176Shear Tie · cracked1EA CRACK WAS FOUND ON BS 1000 RBL 33.99 SHEAR TIE APRROX 1.250" LENGTH(<P> CRACK SHEAR TIE REPLACED AS PER ATLAS EO 4453C024 REV 3 PART 8 AND RI-53-14-16804 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100177Shear Tie · cracked1EA CRACK WAS FOUND ON BS 1000 RBL 57.50 SHEAR TIE APPROX 1.250" LENGTH(<P>CRACK SHEAR TIE REPLACED AS PER ATLAS EO 4453C024 REV 3 PART 9 AND RI-53-14-16805 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032100179Shear Tie · cracked1EA CRACK WAS FOUND ON BS 1000 RBL 75.92 SHEAR TIE APPROX 0.875"Â LENGTH(<P>CRACK SHEAR TIE REPLACED AS PER ATLAS EO 4453C024 REV 3 PART 10. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032200185Closeout Panel · crackedM/D - STA 1241 LBL 77-99 CLOSEOUT PANEL FOUND CRACK (APPROXIMATE 6")(<P>CRACK CLOSEOUT PANEL REPLACED AS PER SRM 51-10-02 AND NEW CLOSEOUT PANEL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW CLOSEOUT PANEL INSTALLED AS PER SRM 51-40-02 </P>)SDR UIEA2024032200186Rivet · damagedV/STAB L/H AUX SPAR TO FRONT SPAR PNL SURFACE FND 1EA BURN MARK RIVET (STA 245 FRONT SPAR RIVET)(<P>BURN MARK RIVET REPLACED AS PER RI-55-30-16816 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032200187Door · chafed#1 ENG RH CORE COWL PRESSURE RELIEF DOOR INTERNAL UPPER FND 1EA FRAME CHAFING(<P>FRAME CHAFING AREA REPAIRED AS PER EO 1971A308 REV 0. NO FURTHER DEFECTS NOTED </P>)SDR UIEA2024032300198Seat Track · crackedFWD CARGO BS 980-1000 RH S/W UPPER AREA FND M/D FLOOR SEAT TRACK RBL 98.58 CORROSION DAMAGE(<P>SEAT TRACK REPAIRED AS PER RI-53-40-16817 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032300199Seat Track · crackedM/D - STA 1780-1800 LBL 11" O/B FLANGE FOUND CORROSION CRACK(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032300200Seat Track · crackedM/D - STA 1920-1940 LBL 11" SEAT TRACK FOUND CRACK(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032300201Seat Track · crackedM/D - STA 1600-1620 RBL 11" SEAT TRACK O/B FLANGE FOUND CORROSION CRACK(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032300202Seat Track · crackedM/D STA 1780-1800 RBL 11" SEAT TRACK FOUND CRACK.(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032400208Not Reported · cracked2EA CRACK WERE FOUND ON LH BS 2231 S23L FASTENER HOLE(<P>CRACK AREA REPAIRED AS PER SRM 53-60-15-2R-2 REPAIR 2 FIG 201 DETAIL II, THIS REPAIRED IS CAT B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032400209Beam · cracked#1 PYLON INBD SKIRT BEAM AFT STRUT ADP AIR OUTLET UPPER FND PYLON PANEL FASTENER HOLES CRACKED (2 LOCATIONS)(<P>SKIN 2EA FASTENER HOLES REPAIRED AS PER RI-54-51-16818 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032400210Floor Support · crackedM/D STA 1000 RBL 75" FLOOR HAT SECTION FOUND CRACKED(<P> HAT SECTION CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032500226Skin · dentedDENT LOG D-3-21 - LH BODY GEAR O/B W/W DOOR FWD OUTBOARD (DOOR 754) 77" FROM LEADING EDGE DENT D2 1/4"X 2 1/4" X 7/32 DEEP WITHIN LIMIT IAW SRM 52-80-01-1A-3(<P>SKIN REPAIR AS PER SRM 52-80-01-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024040200232Seat Track · corrodedM/D - STA 1920-1940 RBL 11" SEAT TRACK FOUND CORRODED(<P>SEAT TRACK CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. CHECKED WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024040200233Skin · delaminatedLHW O/B FORE FLAP FOUNDÂ DELAMINATED(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-17 PAR 5.A.(1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024040400234Skin · dentedRH I/B ELEVATOR FOUND DENT(<P>PERFORMED REPAIR IAW SRM 51-70-06 PAR 5.A (1) AT DENT AREA. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024032400211Access Door · damagedON POST FLT, FOUND #4 ENG INBD PYLON DAMAGED (SAIL BOAT DOOR)(<P>TEMP REPAIR TO #4 ENG PYLON PANEL COMPLETED PEREA 4454A0080 & SRM 51-70-19-0G-0. SCHEDULED PERMANENT REPAIR UPON AIRCRAFT RETURN TO MIA FROM SCL PRIOR TO THE ACCUMULATION OF 2 F/C AFTER TIME LIMISDR UIEA2024062700571Modulating Valve · faultedDIVERSION: FLIGHT DECK AND UPPER DECK AREA TEMPERATURE UNCONTROLLABLE.(<P>R/R FLT DECK ZONE TRIM MOD VLV AND ZONE TEMP CONTROL MOD PER AMM 21-61-10/401 AND 21-61-01/401. OPS CHK GOOD. </P>)SDR UIEA2024022400126Socket · shortedVIA SATCOM, CREW REPORTED INFLIGHT ELECTRICAL ODOR CORRESPONDING TO AN UN-COMMANED ILLUMINATION OF CEILING LIGHT IN THE GALLEY / LAV AREA. CREW REPORTED STRONG ODOR, BUT NOTED NO C/B OPENED.(<P>REMOVED UPPER DECK CEILING LIGHT COVER IAW AMM 33-28-01 AND FOUND SDR UIEA2024020900074Indicator · false indicationAIR TURNBACK DUE TO CREW O2 QUANTITY LOW (SUSPECT LEAK)(<P>PERFORMED LEAK CHECK FOR OXY BOTTLES / LINES / ALL MASKS, NO LEAK FOUND. R/R CREW OXYGEN VOLTAGE AVERAGING UNIT AND OPS / IND CHECK GOOD PER AMM 35-41-12.</P>)SDR UIEA2024020500071Door · missingDURING WALK AROUND, FOUND LH BODY GEAR STRUT OUTBOARD DOOR MISSING.(<P>INSTALLED LH BODY LANDING GEAR STRUT OUTBOARD DOOR AND CK OK PER AMM 32-14-06.</P>)SDR UIEA2024012500023Skin · puncturedL/H I/B FLAP FORE FLAP UPPER SURFACE FOUND 1EA PUNCH HOLE DAMAGED AS MARK.(<P>L/H I/B FLAP FORE FLAP UPPER SURFACE PUNCH HOLE DAMAGE AREA. PERFORMED HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5.A.(1) AND FIG 5. NO FURTHER DEFECTS NOTED</P>)
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