JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), newest first.
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 jasc_code = '5300' 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 jasc_code = '5300' 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 FDEA202206041642Floor Panel · damagedTHE #241PH FLOOR PANEL WAS FOUND 2EA INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W FEDEX DRAWING NO:SRZ-25-005 .SDR FDEA202206041641Floor Panel · damagedTHE #242SF FLOOR PANEL WAS FOUND 3EA INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005 .SDR FDEA202206041637Floor Panel · damagedTHE #242NH FLOOR PANEL WAS FOUND 2EA INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005 .SDR FDEA202206041636Floor Panel · damagedTHE #242TG FLOOR PANEL WAS FOUND 2EA INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005 .SDR DALA2022060804017Skin · dentedSHIP 666 (AWR)DURING HFEC INSPECTION ON FUS SKIN DENT AT FUS STA 710 BTW S26R - S27R 1EA SEVERAL CRACKS WERE FOUND ON A 0.250IN DIAMETER AREA. IN REF MON/0666/2492880 JOB#152. CORRECTIVE ACTION: SUMMARY OF NRC 00620:DENT AT FUS STA 710 BTW S26R - S27R WAS REPASDR DALA2022060804016Skin · dentedSHIP 666 (AWR)DURING HFEC INSPECTION ON FUS SKIN DENT AT FUS STA 710 BTW S26R - S27R 1EA SEVERAL CRACKS WERE FOUND ON A 0.250IN DIAMETER AREA. IN REF MON/0666/2492880 JOB#152. CORRECTIVE ACTION: SUMMARY OF NRC 00620:DENT AT FUS STA 710 BTW S26R - S27R WAS REPASDR GTIA2022060636469None · noneSTRONG DIRTY SOCKS ODOR IN COCKPIT AND ALL CABIN DURING CLIMB AND DESCENT. -PERFORMED TSM PROCEDORES IAW 05-50-00-810-831-A COULD NOT DUPLICATE ODOR NO FURTHER DEFECTS NOTED AT THIS TIME OK FOR SERVICE.SDR JJBA20220603035None · noneEXISTING REPAIR DOUBLE ON FWD PRESSURE BULKHEAD NEED TO BE REMOVED FOR INVESTIGATION. FWD PRESSURE BULKHEAD REPAIRED WITH DOUBLER.SDR FDEA202206031643Floor Panel · damagedMAIN DECK CARGO COMPT #251HH FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 S.R.M 53-10-20-201 P205-206 , PARA.9A , FIG.201 .SDR FDEA202206031640Floor Panel · damagedMAIN DECK CARGO COMPT #242RG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005 .SDR FDEA202206031638Floor Panel · damagedTHE #241NH FLOOR PANEL WAS FOUND 1EA INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W FEDEX DRAWING NO:SRZ-25-005 .SDR K11A2022070100136Stringer · crackedFOUND STRINGER CLIP TO BE CRACKED AT STA 727C S4LSDR AALA202206234537Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD RIGHT TRANSITION SHIELD HAS CORROSION LOCATED AT STA 767 TO 795 AND RIGHT BUTT LINE 21. REMOVED AND REPLACED TRANSITION SHIELD PER SRM 51-40-02.SDR CALA2022060601436Failsafe · crackedAD2012-09-04 SUPPORT TASK:EA 5340-01385 REV ORIG LHS STA955 REAR SPAR BULKHEAD FAILSAFE STRAP UNDER THE ATTACHED T-FITTING FOUND CRACK-TRANSFER REFER NON-ROUTINE WO.803284 AND ORIGINATED BY EMP V906449 STA955 LHS REAR SPAR BULKHEAD FAIL SAFE STRAP REPAIRED I.ASDR IXXA2022060303Stringer · corrodedSTRINGER 39R CORRODEDSDR IXXA2022060302Attach Angle · corrodedSEAL DEPRESSOR ATTACH ANGLE CORRODEDSDR IXXA2022060301Floor Panel · corrodedFLOOR WEB CORRODEDSDR JJBA20220602004None · noneAT REAR FUSE I EXT, CRACK FOUND ON RH TOP SKIN AT FR 75 AND BTW STR 1R-3R. CRACK ON RH TOP SKIN AT FR75 AND BTW STR 1R AND 3R REPAIRED WITH DOUBLER.SDR GTIA2022060936473None · noneHIGH RUDDER VIBRATION ACFT RUDDER TRIM WAS NOT TRIMMING DURING CLIMB OUT AND LEVEL FLIGHT-IAW TSM 05-50-00-810-801-A FLOW CHART INDICATES RUDDER AT FAULT. PERFORMED RUDDER T/E PLAY FOUND BLUE SYS SERVO WITH 17MM & YELLOW SYS WITH 15MM PLAY REF LOG PGS 2804116-SDR JJBA20220602002None · noneAT REAR USE II EXT, SUSPECTED CRACKS (17X) FOUND ON RH SIDE SKIN BTW FR 77-FR80 AND BTW STR 3R-9R. AFTER NDT INSPECTION 13 CRACKS CONFIRMED ON RH SIDE SKIN BTW FR77-80 STR 3R-9R. AT RFII (9X) CUTOUTS C/OUT ON RH SKIN BTW FR 77-80 STR 3R-9R. ITEM 5 (X9) BUSHINGSDR GTIA2022060636466None · noneAPPROX 50 MINUTES AFTER T/O AT FL320 FA REPORTED "DIRTY FEET" SMELL IN FWD CABIN & GALLEY-PER GROUND OPS TEST O PACKS OFF ENGINE AND APU, NO DEAULT/ODORS NOTED IAW TSM 05-50-00.A/C OK FOR SERVICESDR UIEA2022052200495Attach Angle · crackedM/D RHS STA 960 S-7 FRAME FWD / CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED ANGLE P/N: 65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02 REV 94 DATE 20FEB2022</P>)SDR UIEA2022052200498Attach Angle · crackedM/D LHS STA 960 S-7 FRAME FWD/ CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED AND P/N NO.65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02</P>)SDR UIEA2022052300499Beam · elongatedAFT CGO STA 1820-1840 MOST RH HORIZ TORQUE TUBE R/H SUPPORT BEARING ATTACHED BEAM FOUND HOLE ELONGATED. HOLE ELONGATED INTERCOSTAL LOCAL FABRICATED AS PER BOEING DWG: 65B06061 & RPL AND INSTALLED AS PER SRM 51-40-02SDR UIEA2022052500540Attach Bolt · elongatedAFT CARGO STA 1820-1840 RBL 30" MOST R/H HORIZONTAL TORQUE TUBE L/H SUPPORT BEARING ATT BEAM FOUND BOLT HOLE ELONGATED. LOCAL FABRICATE INTERCOSTAL AS PER BOEING DWG 65B06201 & PART LIST AND DOUBLER AS PER BOEING DWG 69B02959 PL AND NEW PARTS INSTALLED AS PERSDR UIEA2022052500541Frame · chafedAPU COMPARTMENT STA 2685 L/H FRAME MID SECTION FOUND CHAFING. FRAME CHAFING AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94, DATE: 20 FEB 2022</P>)SDR UIEA2022052500542Frame · chafedAPU COMPARTMENT STA 2690 L/H FRAME MID SECTION FOUND CHAFING, FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 REV 94 DATE 20 FEB 2022</P>)SDR UIEA2022052600547Shear Tie · cracked1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 57.5 SHEAR TIE AS MARKED APPROX 13/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH AT O/B SIDE. CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV 1 PART5</P>)SDR UIEA2022052600548Shear Tie · cracked1EA THROUGH THICKNESS CRACK WAS FOUND ON THE LBL 75.92 SHEAR TIE AS MARKED APPROX 1 3/4" IN LENGTH AT I/B SIDE & 1 1/4" IN LENGTH TO O/B SIDE(<P>CRACK SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO: 4453C024 REV. 1 PART 6</P>)SDR UIEA2022052600549Skin Panel · installedFUSELAGE - SECTION 46 - BS 1640 TO 1740 LEFT SIDE AT STRINGER 34 - SKIN PANEL INSPECTION -SB 747-53A2487 R4- AD 2002-23-15. SKIN PANEL MODIFICATION AS PER EO NO.4453A036 FIG 3 AND RI NO. RI-53-60-15609 REV.A</P>)SDR UIEA2022052600550Fitting · damagedFUSELAGE - LONGERON EXTENSION FITTING - BODY STATION 1480 TO BODY STATION 1540 - STRINGERS S-32 TO S-33 (EO4453A818 5& 6). L/R STA 1480 - STA 1540 LONGERON EXTENSION FITTINGS REPLACEMENT AS PER ATLAS AIR EO4453A818 PART 3 4 AND RI NO. RI-53-00-15644 REV.ASDR UIEA2022052700551Fastener · crackedEO 4453A821-1 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) (L/H FASTENERS & WASHERS DEVIATIONS; DOUBLER S.E.M AND R/H FASTENERS & WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOSDR CALA2022060201427Stringer · crackedSTA 265.5 RH STR27RL FND CRACKED - ORIGINATED BY EMP V916675 ON HAECO NR 9486411, SPEC NO.B777-53-3-7111. PERFORMED BY EMP V902599,CABIN STA265.5 STR27R STRINGER CRACKED AREA REPAIRED AS PER ECRA5310-08016 REV.-.SDR IXXA2022060211Support · corrodedROLLER TRAY SUPPORTSDR IXXA2022060209Shear Tie · corrodedSEAR TIE CORRODEDSDR K11A2022072700151Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 827 BETWEEN STRINGERS 8R AND 9RSDR K11A2022072700150Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 827 BETWEEN STRINGERS 8L AND 9LSDR K11A2022072700149Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727F BETWEEN STRINGERS 8L AND 9L.SDR K11A2022071300143Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVETS AT STA 380 BETWEEN STRINGERS 8R AND 9RSDR K11A2022071200142Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 907 BETWEEN STRINGERS 8R AND 9RSDR K11A2022071200141Frame · crackedCRACK INDICATION FOUND AT FUSELAGE FRAME AT SUPPORT BRACKET INBOARD ATTACH RIVET LOCATION AT STA 440 BETWEEEN STRINGERS 8R AND 9RSDR K11A2022071100140Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 867 BETWEEN STRINGERS 8L AND 9LSDR K11A2022071100139Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVET AND INBOARD FRAME RADIUS AT STA 400 BETWEEN STRINGERS 8R AND 9RSDR K11A2022071100138Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727D BETWEEN STRINGERS 8L AND 9LSDR 2022FA0000323Ejector · cloggedAFTER SUCCESSFUL ENGINE START, ENGINE SHUT-DOWN "UN-COMMANDED". REMOVED FUEL HEADER TANK ACCESS PANEL AND VISUALLY OBSERVED A SMALL SCREW IN INLET SCREEN OF FUEL JET / EJECTOR PUMP.SDR JJBA20220601001None · noneCENTER FLOOR TRACKS HAVE CORROSION FR 25-43 BL0. REMOVED CORROSION AT CABIN SEAT TRACK BL0 FROM FR 25-43. EVALUATED SEAT TRACK FROM FR 26, 28, 33, 34, 36 AND 38-40 FOUND TO BE WITHIN LIMITS. EVALUATED SEAT TRACK FROM FR 25, 27, 29, 30-32, 35 AND 37 FOUND TO BESDR IXXA2022060110Floor Support · misrepairedFLOOR SUPPORT STIFFENER HAS DOUBLE DRILLED HOLESSDR IXXA2022060108Support Fitting · corrodedWIRE SUPPORT CLIP CORRODEDSDR IXXA2022060107Web · corrodedCORROSION ON INTERCOSTAL WEBSDR IXXA2022060106Support · corrodedCORROSION UNDER ALC PDU MOUNT
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