Boeing 747-409
Service difficulty reports · 250
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 = '747409' 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 = '747409' 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 SAJF20120815027Fire Bottle · leaking(B-18203) PRE FLIGHT CHECK AMBER MESSAGE APPEAR FIRE BTL B LOWER LT ENG. CK CMC MSG 26039 ENG BTL LT-B LOW PRESSURE, AND TROUBLESHOOTING FOUND ENG BTL LT-B IS EMPTY. PFM WIRING CK COND NORMAL, REPLACE ENG BTL LEFT B IAW AMM 26-21-03. PFM SQUIB TEST NORMAL. TSDR UIEA2012051000210Lens · damagedWHEN ACFT CAME INTO GATE, FOUND LT OTBD LANDING LIGHT LENS COVER HAD DAMAGE. EO 4433A035 PART 1 COMPLETED.SDR SAJF20120126002Skin · cracked(B-18207) DURING TRANSIT CHECK, A CRACK WAS FOUND ON EXTERNAL SURFACE OF FUSELAGE SKIN, AT LOCATION OF APPROX STA 1732, S-43L. CORROSION WAS ALSO FOUND ON THE INNER SURFACE OF SUBJECT FUSELAGE SKIN COMMON TO S-43L. THE DAMAGED SKIN WAS CUTOUT AND REPAIRED ISDR SAJF20110910001Warning Message · illuminated(B-18202) DURING ROLL TAXING, MESSAGE: "CONFIG SPOILER" ILLUMINATED, CREW ABORTED TAKEOFF AT 40 KTS, CREW CHECKED SPOILER & SPEED BRAKE HANDLE POSITION AND FOUND NORMAL, MESSAGE EXTINGUISHED. CREW DECIDED TO CONTINUE FLT. AFTER ACFT ARRIVED, SPOILER CONTROL SYSDR UIEA2011082700475Access Panel · damagedLEFT VERTICAL STABILIZER 324GL ACCESS PANEL HAS ELONGATED HOLES.SDR UIEA2011082600467Line · looseEICAS MESSAGE HYD QTY LOW 1. SERVICED HYD OPENED RUDDER ACTUATOR PANELS, INSPECTED AREA, OPERATED SYS 1. TIGHTENED LOOSE PRESSURE LINE ON UPPER RUDDER ACTUATOR. LEAK CHECK OK IAW MM 291100 ALL PANELS CLOSEDSDR UIEA2011111600662Battery Pack · inoperativeFOUND CABIN EMERGENCY LIGHT BATTERY (M14523) LOW IAW AMM 33-51-04-902-001-001, REV 72. REPLACED BATTERY AND PERFORMED OPS TEST. RESULT SATISFACTORY.SDR UIEA2011081400463Battery · dischargedFOUND CABIN EMERGENCY LIGHT BATTERY (M14523) LOW. REPLACED EMERGENCY LIGHT BATTERY IAW AMM33-51-04-902-001-001, REV 72 AND PERFORMED OPS TEST RESULT WAS SATISFACTORY.)SDR SAJF20110805001Stringer · corroded(B-18211) QC FOUND SEVERAL CORROSION COMMON TO STR 50 L, BETWEEN STA 1780 AND 1940. THE CORRODED AREAS ARE ALMOST OUT OF SRM ALLOWABLE LIMITATIONS. PROPOSED TO REPAIR IAW SRM 53-60-03, REPAIR 2.SDR SAJFCALS100029Longeron Fitting · crackedDURING 10C AND 2D CHECK, CRACK WAS FOUND AT LT SIDE LONGERON FITTING. THE CRACK LENGTH IS .1875". TRIMMED OUT THE CRACKED AREA AND DEFERRED THE MEASUREMENT OF GAPS IAW MFG (SR 1-193896515).SDR SAJFCALS100025Window · broken(B18203) AFTER FLIGHT, DAILY CHECK WAS PERFORMED. LT PASSENGER WINDOW OUTER PANE (STA 1590, BESIDE SEAT 45A) WAS FOUND BROKEN. NO DAMAGE IS FOUND IN THE MIDDLE PANE. THE OUTER PANE AND MIDDLE PANE HAD BEEN REPLACED IAW AMM 56-21-01. REPORTED THIS CASE TO MSDR SAJFCALS100028Longeron Fitting · cracked(B18701) CRACKS WERE FOUND ON RT SIDE LONGERON EXTENSION FITTING WHEN PERFORMING MPD 53-440-00 INSPECTION. REMOVED AND INSTALLED LONGERON FITTING IAW 747-53A2390, FIG 22.SDR SAJFCALS100030Stringer · corrodedLEVEL II CORROSION WAS FOUND AT LOWER STRINGER 2, STATION 285 OF LT HORIZONTAL STAB STRUCTURE DURING D-CHECK. TRIMMED OUT THE CORRODED STRINGER AND FABRICATED A PORTION OF NEW STRINGER IAW DWG 65B03555. INSTALLED THE NEW STRINGER WITH REPAIR ANGLE AND FASTESDR SAJFCALS100027Longeron Fitting · cracked(B18707) CRACKS WERE FOUND AT BOTH LT AND RT SIDE LONGERON EXTENSION FITTING WHEN PERFORMING SB INSPECTION. REMOVED AND INSTALLED LONGERON FITTING IAW SB 747-53A2390, FIG 22.SDR UIEA2011060800280Skin · chafedCHAFING ON FWD SURFACE OF LT INBD MID FLAP. BONDED THE FIBERGLASS FABRIC TO THE CHAFED AREA.SDR UIEA2011060800284Support Beam · corrodedCORRODED CLIP ISLES 1036, LT WING L/E COMPT LOWER SUPPORT BEAM AREA. REPLACED WITH NEW PART IAW SRM 51-40-02, REV 9.SDR UIEA2011060600274Beam · corrodedCORROSION ON HST FIXED T/E BEAM LOWER CHORD AT ELEV STA 2568. REPAIRED IAW EI T2011A55B - 1375, REV 00.SDR UIEA2011060400285Battery Pack · inoperativeL1 DOOR SLIDE EMERGENCY LT INOP. IAW AMM 35-51-06-400-801, REPLACE L1 DOOR SLIDE LIGHT BATTERY AND CHECK SATISFACTORY.SDR UIEA2011060200279Structure · corrodedFOUND RT HST LOWER WING, LOWER CHORD HAS CORROSION AT ELEV STA 181.8. REPAIRED IAW EI T2011P55-1376, REV 00 AND REV 01.SDR UIEA2011060200278Stiffener · corrodedFORWARD LT HST LOWER WING STIFFENER HAD CORROSION AT ELEV STA 181.8. (REPAIR IAW T2011P55B-1376, REV 00 & REV 01.)SDR UIEA2011060200277Skin · corrodedFOUND LT HST LOWER WING PLATE HAD CORROSION AT ELEV STA 131.9. REPAIRED IAW EI T2011P55B-1381, REV. 00.SDR UIEA2011060200276Stiffener · corrodedFWD LT HST LOWER WING STIFFENER HAD CORROSION AT ELEV STA 2068. (FABRICATED NEW PARTS IAW EI T2011P55B, 1376 REV 00 PART 2 AND REV 01.)SDR SAJFCALS100020Skin · crackedDURING TRANSIT CHECK, FOUND A POP-UP SKIN WITH A 0.5 INCH LENGTH CRACK LOCATED ON S44R, BS 1728. CHECKED INTERIOR SKIN AND DISCOVERED CORROSION COMMON TO INTERIOR BELLY SKIN ALONG S44R EDGE. DETAILED VISUAL INSP ON ADAJCENT STRUTURE FOUND OTHER 2 SKIN CRACKS ASDR UIEA2011053100275Skin Panel · corrodedCORROSION WAS FOUND ON THE LOWER SURFACE OF LT WING LOWER SKIN PANEL AT WS 1280 (REPAIR IAW EI T2011A57B-1371, REV 00, REV 01 AND REV 02.)SDR SAJFCALS100007Arm · failedB-18208// AIRCRAFT, IN ROUTE, FLT CREW REPORTED THAT DURING CLIMB, FL130 NR 1 ENG SURGE EPR & N1 SPOOLED DOWN & FLT CREW FOLLOW QRH NR 1 ENG SHUTDOWN. A/C RETURNED. NR 1 ENG WAS REMOVED FROM SERVICE. MX FOUND THE SIXTH STAGE VSV ARM FAILED WHICH CAUSED SEVSDR SAJFCALS100004Arm · failedB18207, IN ROUTE, DURING CLIMB PHASE (ALT 12,000 FEET), ENG 2 SURGED AND EGT OVER LIMIT(MAX. EGT 722?). ENG 2 IFSD AND AIRCRAFT TURNED BACK. VISUAL INSPECTION FOUND AN METAL PARTICLE ON EXHAUST NOZZLE, THE ENGINE WAS REMOVED FROM SERVICE. FOUND THE SIXTH STAGESDR SAJFCAL2010002Socket · arcedCABIN LOG RECORD, THE FIRST CLASS GALLEY 1 WORK LT INOP. REMOVED GALLEY 1 WORK LT FOUND LIGHT ASSY LAMP HOLDERS ARCED. INSPECT GALLEY 1 CEILING CONDITION CHECK NORMAL, THERE IS NO WATER LEAK CONDITION FOUND. AFTER REPLACED GALLEY 1 LIGHT ASSY, THE SYS WAS SDR SAJFCALS099027Fire Warning · false activation(B-18208) APU FIRE MSG DISPLAYED 1 MINUTE AFTER APU WAS SHUTDOWN. BOTTLE LOW APU MSG DISPLAYED 30 SECONDS LATER. INITIAL INSP FOUND NO FIRE EVIDENCE. ACFT WAS DISPATCHED WITH APU DE-ACTIVATED. BOTH DETECTOR ASSEMBLIES WERE SENT FOR VENDER CHECK AND NO FAULT FSDR SAJFCALS099015Skin · corrodedDURING D01 CHECK, AFTER CARGO COMPARTMENT BILGE AREA SKIN FOUND CORROSION NEAR BS 1735 AND S51L-S51R. REINFORCE THE SKIN WITH 2024T3_0.125THK. IAW EO 744-53-00-0120 AND EO 744-53-00-120R1 WITH FAA 8100-9, CATEGROY B APPROVAL.SDR SAJFCALS099011Fire Warning · illuminated(B-18208) DURING PUSHBACK, APU FIRE MSG DISPLAY AND ALARM INTERMITTENTLY THEN APU BOTTLE LOW PRESS MSG DISPLAY. GROUND BITE TEST FOUND BOTTLE DISCHARGED, BUT NO LOOP MESSAGE. APU COMPARTMENT INSPECTED NO FINDING. A/C RELEASE WITH APU ENACTIVE.SDR EIAA2010010Skin · corrodedLT WING L/E LOWER SKIN AT FRONT SPAR EXFOLIATED STA OLES 1534. REMOVED CORROSION, CUT OUT DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 780-57-020-2.SDR SAJFCALS099006Connector · dirty(B18208) ENG-4 UNABLE TO SHUTDOWN AFTER FUEL CONTROL SWITCH BACK TO CUT OFF POSITION, EICAS SHOWS "ENG 4 FUEL VLV" MESSAGE, THEN THE ENGINE GOT SHUTDOWN ITSELF ABOUT 15 SECONDS AND NR 4 FIRE HANDLE HAS BEEN PULLED. MX INTERROGATE CMC FOUND "ENG 4 FMU SHUTOFF SDR EIAA200900134Skin · damagedDAMAGE TO SKIN AND WEB NEEDS REPAIR AT BS 440, STR 40 RT. ACCOMPLISHED ECRA 780-53-019-1 PER SRM 53-00-01 DETAIL 3 AT STA. 420 STR 41R, WITHIN SRM LIMITSSDR SAJFCALS098044Tire · rupturedAFTER ACFT TOOK OFF, RUNWAY FOUND TIRE DEBRIS OF TIRE NR 8 DUE TO DELAMILATION. TIRE NR 8 DE-LAMINATED, THIS TIRE IS 4TH RETREADED. DAMAGED STRUCTURE REPAIR IS IN PROCESS AT AMS STA 3. MORE DETAILED STRUCTURAL DAMAGES ARE STILL PENDING FOR REPORTS FROM AMS SSDR SAJFCALS098036Slide · unwanted deployAFT 8A CK ENG RUNUP TEST, MAINT FOUND 1L DOOR SLIDE DEPLOY IN CABIN. INITIAL INVESTIGATION CK FOUND DOOR IN PARK POS, DOOR EMER OPS RESERVOIR DID NOT DISCHARGE BUT SLIDE DE-PACK AND DEPLOY IN CABIN.SDR SAJFCALS098038Stringer · corrodedDURING 12 C-CHECK, CORROSION WAS FOUND ON BULK CARGO COMPARTMENT BILGE AREA S-51R AT STA 1999. CUTOUT CORRODED STRINGER FROM STA 1995 TO STA 1999. REPAIR THE CORROSION STRINGER REFER TO SRM 53-00-03 REPAIR 3.SDR SAJFCALS098025Actuator · malfunctionedDURING 8A CK, PERFORM MLG ALTERNATE EXTENSION SYS TEST FOUND THAT RT MLG ALTERNATE ELECTRIC MOTOR FUNCTION FAIL. REPLACED ROTARY ACTUATOR AND FUNCTION TEST NML.SDR 2009F00011Strut · peelingWHEN PERFORMING SCHEDULED TASK AMP 32-999-30 "TRUCK BEAM PIVOT PIN" AIRCRAFT, REGISTER NR B18251, IT WAS FOUND THAT RT BLG INNER CYLINDER CHROME PEELING OFF. IAW AMM 32-00-03, L/G WAS REPLACED. SENT THE REMOVED GEAR, ADVISED THAT THERE WAS EXTENSIVE DAMAGE DSDR EIA2008F00006Skin · dentedFUSELAGE SKIN BS 2640 LBL 16, DENT OUT OF LIMITS. REMOVED DAMAGED AREA, NDT AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 400 LCF 53-30-01 PG 3 ITEM 7, 53-00-01 REPAIR 6PG 201-204 51-30-50, PG 5, 51-10-02 PG 6-7. (K)SDR EIA2008F00004Stringer · crackedBS 480-499 STRINGER 10 LT STRINGER IS CRACKED. REPAIRED CRACKED STRINGER AT BS 480 & 500 IAW SB747-53A2484, FIG 18 AND 20. (K)SDR EIA2008F00009Stringer · crackedBODY STATION 480, STRINGER 10 RT CRACKED. REPAIRED STRINGER IAW SB 747-63A2484, FIG 24. (K)SDR EIA2008F00007Skin · dented(2) DENTS IN FUSELAGE SKIN BS 220-260, STRINGER 30 RT-32 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 PG 201-211, REPAIR 1 DETAIL, FIG 201. (K)SDR CALS097007CFeeder Cable · chafedAIRLINES WAS ASKED TO PERFORM THE INSPECTION (APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT), AND FOUND THAT B-18205 LT BULK CARGO COMPARTMENT STA 2060 APU GENERATOR FEEDER CABLE CLAMP STANDOFF RIVET LOOSEN. THIS HAS BESDR CALS097007BFeeder Cable · chafedASKED TO PERFORM THE INSPECTION "APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT", AND FOUND THAT B-18202 LT BULK CARGO COMPARTMENT STA 2060 APU GENERATOR FEEDER CABLE CLAMP STANDOFF BROKEN. THIS HAS BEEN CORRECTED AND RESDR CALS097007AFeeder Cable · chafedASKED TO PERFORM THE INSPECTION "APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT", AND FOUND THAT B-18273 APU GENERATOR FEEDER CABLE OUTER JACKET CHAFING AT STA 2060 LT. THIS HAS BEEN CORRECTED AND RECORDED. IT HAS ALSO BSDR CALS097007Feeder Cable · chafedAPU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT, AND FOUND THAT B-18203 LT BULK CARGO COMPARTMENT STA 2060 APU GENERATOR FEEDER CABLE CLAMP STANDOFF RIVET SHEARED.SDR CALS097004Windshield · crackedB-18251, FLIGHT CI-003 ENROUTE, GROUND VISUAL INSPECTION FOUND 1 CM CRACK AT (2R) WINDSHIELD EDGE.SDR CALS097003Fitting · crackedWHEN PERFORMING FAA AD 2006-05-06 ON AC B-18201, DSGN FOUND GRH SIDE AFTER SPLICE FITTING CRACKED APPROXIMATELY 1.25 INCH IN LENGTH.SDR CALS097001Shield · crackedCHI FOUND A CRACKED DRIPSHIELD UNDER G1 FLOOR DURING AIRCRAFT B-18275 HEAVY MAINTENANCE OF 3D CHECK. THIS DRIPSHIELD HAD A 3 INCH DIAMETER HOLE WITH NUMEROUS CRACKS LOCATED IN AN AREA APPROXIMATELY 18 INCHES BY 8 INCHES. THE DRIPSHIELD IS INTENDED TO PROTECT ESDR EIA2007197Slide · low pressureLT ENTRY DOOR 31 ESCAPE SLIDE INFLATION BOTTLE PRESSURE IS "0" PSI. REMOVED AND REPLACED SLIDE PER B747 MM 25-69-00.
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