Boeing 747-446
Service difficulty reports · 932
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 = '747446' 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 = '747446' 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 UIEA2011100400551Fuse · inoperativeUPPER DECK EMERGENCY EXIT OVERHEAD EMERGENCY LIGHT FOUND INOPERATIVE. POWER PACK FUSE REPLACED AND TEST NORMAL IAW AMM 33-51-02.SDR UIEA2011100300548Power Supply · inoperativeZONE B SEAT 17 ABC EMERGENCY LIGHT INOPERATIVE. POWER PACK FUSE REPLACED AND TEST NORMAL AS PER AMM 33-51-04.SDR UIEA2011100300547Lamp · inoperativeLAVATORY BS2A CEILING EMERGENCY LIGHT FOUND INOPERATIVE. RELAMP AND TEST RESULT NORMAL AS PER AMM 33-51-07.SDR UIEA2011100300541Battery Pack · inoperativeZONE E 53HJK - 66HJK CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK (M7928) REPLACED AND OPS TEST C/O RESULT NORMAL IAW AMM 33-51-04.SDR UIEA2011100300540Lamp · inoperativeSTAIRWAY CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AND TESTED NORMAL IAW AMM 33-51-07.SDR UIEA2011100300539Fuse · inoperativeU/D SEAT ROW 4 O/H CEILING LIGHT EXIT SIGN INOP. POWER PACK FUSE REPLACED AND TEST NORMAL IAW AMM 33-51-02.SDR UIEA2011100300537Power Supply · inoperativeU/D 1ABC-6ABC SEAT EMERGENCY LIGHT INOPERATIVE. POWER PACK (M5055) REPLACED AND TEST NORMAL IAW AMM 33-51-04. 33-51-00.)SDR UIEA2011100300534Light · inoperativeU/D EMERGENCY DOOR FLOOR PROXIMITY LIGHT FWD INOPERATIVE. FLOOR PROXIMITY LIGHT FWD REPLACED AND TEST NORMAL.SDR UIEA2011092300525Skin Panel · dentedDENT WAS FOUND ON SKIN PANEL AND WAS MEASURED 0.130 INCH DEEP AND 1" X 1". THE DAMAGED SKIN IS A BONDED SKIN PANEL WITH A TOTAL THICKNESS OF 0.028 INCH. DENT REPAIRED IAW SRM 53-00-01, REPAIR 1, FIGURE 201 WITH THE EXCEPTION THAT THE MINIMUM THICKNESS OF THE SDR UIEA2011100300535Skin · dentedTAIL CONE LT UPPER HALF EXT SKIN HAS A DENT MARK AT STA 2707 APPROX BWL 359.7. SKIN PATCH REPAIRED IAW R5-53-81-37225 REV A.SDR KCSA111205Door · crackedR-1 DOOR AT BOTTOM FWD CORNER BS 440 FOUND CRACK - (APPROX BWL 199.8).SDR UIEA2011100300536Skin · dentedMULTIPLE DENTS AND GOUGES AT PRODUCTION SPLICE BEFORE SECTION 43 JUST BELOW BELT. SKIN REPAIRED AT BS 730- BS 741 S-23L TO S-25L IAW RS NO R53-20-37221 REV A.SDR KCSA111188Light · inoperativeEMERGENCY LIGHT INOP UPPER DECK STA 640.SDR KCSA111187Bulkhead · crackedBS 2598 BULKHEAD RT FWD INNER CHORD HAS A CRACK AT FASTENER HOLE.SDR UIEA2011062300324Structure · damagedDURING MX WALKAROUND, FOUND LIGHTNING STRIKE DAMAGE TO THE RT THRUST REVERSER TRANSLATING COWL . THE DAMAGE IS 1.0 IN. DIAMETER. PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS CMM 78-32-31, REPAIR 023.SDR UIEA2011061700323Depressor · damagedDURING WALK-AROUND INSPECTION, DAMAGE TO THE LOWER LOBE - FWD CARGO DOOR - BS670 SEAL DEPRESSOR FOUND (REF. FIGURE 1), MEASURING 1 INCH WIDE FROM THE EDGE AND 5 " LENGTH. DAMAGE WAS DETERMINED TO BE BEYOND THE REPAIR LIMITS IAW THE SRM 53-00-15, FIGURE 201, RSDR 1MURWO3911088Lamp · wrong partBURNED /HEAT DISTRESSED INSULATION, NOTED WHILE ACCOMPLISHING TASK CARD 20-625-01-01. ABOVE UPPER DECK GALLEY AT BS 1000 FOUND BURN IN INSULATION ABOVE F/A SERVICE LIGHT CENTER. SECOND ACFT THAT HAS BEEN FOUND ON WITH THIS SAME CONDITION. THIS INSPECTION REVSDR UIEA2011052200266Fairing · damagedDURING LOADING OPERATIONS; A CARGO DOLLY STRUCK ACFT CAUSING DAMAGE TO WING TO BODY FAIRINGS FROM BS800 TO BS1000. UPON INSPECTION OF THE DAMAGED AREAS FOUND 3 WING/BODY FAIRINGS WITH PUNCTURES AND SCRATCHES. THE DRAIN MAST WAS ALSO DAMAGED DURING THIS INCIDSDR UIEA2011042800254Heat Shield · damagedDURING INSP, THE NR 4 ENGINE INB CORE COWL HEATSHIELD WAS FOUND DAMAGED. REF TO FIG 1 & AMP; 2 FOR DETAILS. A REPAIR SRM 54-45-01, REPAIR 3 WILL BE PERFORMED BUT THERE IS NIL STOCK OF 321 CRES AMS5510 REPAIR DOUBLER WITH THICKNESS OF 0.005" (REQUIRED IAW SRM 5SDR UIEA2011041200245Landing Gear · misinstalledDURING D-CHECK AT SIN, LANDING GEARS WERE REPLACED; UPON OPS CHECKS, MX FOUND THE LT AMP; RT BODY GEARS- UPPER JURY STRUT PLATES MOUNTING BOLTS BEING INSTALLED TOO LONG, RESULTING IN RIDING CONDITION AGAINST THE DOWNLOCK SENSORS (REF FIGURE 1). (DISPOSITION WSDR UIEA2011041100257Slide · failedU/DECK FLOOR MOUNTED ESCAPE SLIDE BURST DURING CABIN DOOR EVACUATION SLIDE DEPLOYMENT FUNCTIONAL TEST. (ZONE: 222, RT SIDE) IAW MJC 52-023-01-02. PN 7A1323-114, SN 4715. (ABOVE MENTIONED SLIDE UNIT WAS SENT TO SHOP.)SDR UIEA2011032800168Frame · unknownDURING SB 747-53A2507 INSP AT BS 1220, S8L LOCATION COMMON TO FRAME WEB, FRAME DOUBLER AND FRAME CHORD. (THE REPAIR WAS ACCOMPLISHED IAW RI NR N458MC-11-002 IAW REPAIR INSTRUCTIONS PROVIDED BY IN SR 1-1817615622. THE REPAIR WAS APPROVED BY FAA FORM 8100-9)SDR UIEA2011032500165Frame · crackedDURING D INSPECTION OF DATUM ACFT IAW EO 4453A197, CRACK WAS FOUND ON FRAME AT BS 1160 (RT AT STR 9). (THE DAMAGED FRAME WAS REPAIRED IAW PART 5 OF EO 4453A197, REV D (SRM 53-40-07, REPAIR 3). IAW PART 5 OF EO, THE FRAME CRACKS THAT CANNOT BE REMOVED BY DOINSDR UIEA2011031800158Frame · crackedTHE LT NR 4 FAN REVERSER EXHIBITED A CRACK ON THE TORQUE BOX FWD FRAME. (IN THIS INSTANCE THE CRACK HAD BEEN STOP DRILLED AND REGULARLY INSPECTED BY THE PRIOR OPERATOR JAL. AS THE ACFT WAS IN HEAVY CHECK, SIAEC WAS ADVISED TO PERFORM A PERMANENT REPAIR IAW SSDR UIEA2011030600154Skin · damagedTHE LIGHTNING STRIKE DAMAGE TO 65B07656-259 SKIN WAS DETECTED AT BS 385 AND S31AL. THE DEPTH OF LIGHTNING STRIKE DAMAGE WAS .015 INCHES AS RECORDED IAW SIAEC NRC 005380. (THE LIGHTNING STRIKE DAMAGED AREA WAS LOCALIZED IN 65B07656-259 SKIN ONLY. THE LIGHTNISDR UIEA2011022400178Skin · damagedFUSELAGE SKIN INSP DURING "D-CHECK", FOUND LIGHTNING STRIKE ON CROWN SKIN AT STA 345 BETWEEN STR 1R AND 2R (SOLID FASTENER REPAIR CARRIED OUT IAW B744SF SRM 53-00-01. REPAIR 9 SECTION I, PAR S.)SDR UIEA2011022400145Skin · damagedDURING D-CHECK OF THE DATUM AIRPLANE, A LIGHTNING STRIKE DAMAGE WAS FOUND ON RT FUSELAGE SKIN AT BS 345, S1R-2R . DAMAGE WAS FOUND TO BE BEYOND THE ALLOWABLE LIMIT IAW SRM 53-00-01, FIG 101. (THE DAMAGE WAS REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 9 AND IASDR UIEA2011022300142Skin · damagedLIGHTNING STRIKE DAMAGE FOUND AT STA 385 LT, S-31A, DEPTH FOUND APPROX 0.015, LENGTH APPROX 1" TO C/OUT FUSELAGE SKIN EXTERNAL REPAIR IAW SRM 53-00-01. CAT B REPAIR CARRIED OUT IAW MSG SEP-TLS-11-0036-02B. EXTERNAL DOUBLER AND TRIPLER FABRICATED.SDR KCSA101195Reveal · crackedL5 MAIN ENTRY DOOR OPENING REVEAL CRACKED AT BS 2231, STR 22L.SDR ERKR201000316Bottle · discharged(ERKR) RT UPPER DECK SLIDE INFLATION BOTTLE DISCHARGED WHILE SITTING IN SHIPPING AREA. SLIDE WAS REMOVED FOR SHIPMENT TO O/H, ALL SAFETY PRECAUTIONS WERE OBSERVED AND IN PLACE. OUTSIDE AMBIENT TEMPERATURE WAS 50-85 DEGREES FAHRENHEIT AND SUNNY. 1 DAY AFTER REMSDR KCSA10048Structure · damagedDURING UNLOADING OF AIRCRAFT FUSELAGE RECEIVED DAMAGE TO FUSELAGE AT STATION 2020 TO 2060.SDR KCSA101016Sign · brokenUPPER DECK EMERGENCY EXIT SIGN AT STA 600 MID CEILING HAS A BROKEN STUD.
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