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.

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 .Jun 4, 2022 · N724FD · Airbus A300*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 .Jun 4, 2022 · N724FD · Airbus A300*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 .Jun 4, 2022 · N724FD · Airbus A300*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 .Jun 4, 2022 · N724FD · Airbus A300*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 REPAJun 4, 2022 · N666DN · Boeing 757232SDR 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 REPAJun 4, 2022 · N666DN · Boeing 757232SDR 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.Jun 4, 2022 · N613NK · Airbus A320232SDR JJBA20220603035None · noneEXISTING REPAIR DOUBLE ON FWD PRESSURE BULKHEAD NEED TO BE REMOVED FOR INVESTIGATION. FWD PRESSURE BULKHEAD REPAIRED WITH DOUBLER.Jun 3, 2022 · N12195 · Emb EMB145XRSDR 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 .Jun 3, 2022 · N724FD · Airbus A300*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 .Jun 3, 2022 · N724FD · Airbus A300*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 .Jun 3, 2022 · N724FD · Airbus A300*SDR K11A2022070100136Stringer · crackedFOUND STRINGER CLIP TO BE CRACKED AT STA 727C S4LJun 3, 2022 · N733CK · Boeing 737436SDR 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.Jun 3, 2022 · N843NN · Boeing 737823SDR 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.AJun 3, 2022 · N76055 · Boeing 767424ERSDR IXXA2022060303Stringer · corrodedSTRINGER 39R CORRODEDJun 3, 2022 · N255CM · Boeing 767200SDR IXXA2022060302Attach Angle · corrodedSEAL DEPRESSOR ATTACH ANGLE CORRODEDJun 3, 2022 · N255CM · Boeing 767200SDR IXXA2022060301Floor Panel · corrodedFLOOR WEB CORRODEDJun 3, 2022 · N255CM · Boeing 767200SDR 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.Jun 2, 2022 · N21154 · Emb EMB145XRSDR 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-Jun 2, 2022 · N536NK · Airbus A319132SDR 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) BUSHINGJun 2, 2022 · N17169 · Emb EMB145XRSDR 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 SERVICEJun 2, 2022 · N625NK · Airbus A320232SDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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 51-40-02Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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 PERJun 2, 2022 · N416MC · Boeing 74747UFSDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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>)Jun 2, 2022 · N416MC · Boeing 74747UFSDR 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.AJun 2, 2022 · N416MC · Boeing 74747UFSDR 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 BOJun 2, 2022 · N416MC · Boeing 74747UFSDR 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.-.Jun 2, 2022 · N211UA · Boeing 777222SDR IXXA2022060211Support · corrodedROLLER TRAY SUPPORTJun 2, 2022 · N255CM · Boeing 767200SDR IXXA2022060209Shear Tie · corrodedSEAR TIE CORRODEDJun 2, 2022 · N255CM · Boeing 767200SDR K11A2022072700151Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 827 BETWEEN STRINGERS 8R AND 9RJun 1, 2022 · Boeing 737436SDR K11A2022072700150Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 827 BETWEEN STRINGERS 8L AND 9LJun 1, 2022 · N733CK · Boeing 737436SDR K11A2022072700149Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727F BETWEEN STRINGERS 8L AND 9L.Jun 1, 2022 · Boeing 737436SDR K11A2022071300143Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVETS AT STA 380 BETWEEN STRINGERS 8R AND 9RJun 1, 2022 · N733CK · Boeing 737436SDR K11A2022071200142Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 907 BETWEEN STRINGERS 8R AND 9RJun 1, 2022 · N733CK · Boeing 737436SDR K11A2022071200141Frame · crackedCRACK INDICATION FOUND AT FUSELAGE FRAME AT SUPPORT BRACKET INBOARD ATTACH RIVET LOCATION AT STA 440 BETWEEEN STRINGERS 8R AND 9RJun 1, 2022 · N733CK · Boeing 737436SDR K11A2022071100140Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 867 BETWEEN STRINGERS 8L AND 9LJun 1, 2022 · N733CK · Boeing 737436SDR 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 9RJun 1, 2022 · N733CK · Boeing 737436SDR K11A2022071100138Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727D BETWEEN STRINGERS 8L AND 9LJun 1, 2022 · N733CK · Boeing 737436SDR 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.Jun 1, 2022 · N294JS · Cessna 120SDR 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 BEJun 1, 2022 · N10156 · Emb EMB145XRSDR IXXA2022060110Floor Support · misrepairedFLOOR SUPPORT STIFFENER HAS DOUBLE DRILLED HOLESJun 1, 2022 · N255CM · Boeing 767200SDR IXXA2022060108Support Fitting · corrodedWIRE SUPPORT CLIP CORRODEDJun 1, 2022 · N255CM · Boeing 767200SDR IXXA2022060107Web · corrodedCORROSION ON INTERCOSTAL WEBJun 1, 2022 · N255CM · Boeing 767200SDR IXXA2022060106Support · corrodedCORROSION UNDER ALC PDU MOUNTJun 1, 2022 · N255CM · Boeing 767200
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