JASC 5310
Service difficulty reports · 38,548
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 KCSA201606081029Failsafe · corrodedRIGHT WING AFT SPAR WING ROOT FAIL SAFE STRAP CORRODED AT FUSE, BS 955.5.SDR FDEA201606081888Door Frame · crackedCABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1310 BETWEEN LONGERON 26L-27L. WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201606081887Door Frame · crackedCABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR FWD LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1256 BETWEEN LONGERON 26L-27L. CRACKED WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWAA2016070753587Screw · corrodedRIGHT EMERGENCY EXIT ESCAPE STRAP HATCH HOOK SCREW CORRODED. R & R THE SCREW IAW DWG.SDR SWAA2016070753586Screw · corrodedLEFT EMERGENCY EXIT ESCAPE STRAP HATCH HOOK SCREW CORRODED. R & R THE SCREW IAW DWG.SDR AALA201606229001Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD PASSENGER DOOR CUTOUT LOWER BEAM BETWEEN FRAME 16 AND FRAME 19 AT +Y1240. REPLACED LOWER BEAM IAW DWG 170-01330-507 AND SRM'S 51-43-03, -04 & 51-41-03.SDR DALA2016060804430Window Frame · crackedCRACKED LOWER AFT CORNER OF LT RING PAN BETWEEN BS Y=1022 TO Y=1003, Y=1212 TO Y=1231 AT INTERNAL STRUCTURE CABIN. RING PAN LT OF CORNER AFT LOWER WERE REPAIRED IAW SRM 53-05, FIG 122.SDR SWAA2016072654232Window Frame · crackedR3 WINDOW FRAME E-F POST CRACKED. REPAIRED THE WINDOW FRAME IAW ACO.SDR SWAA2016072254154Window Frame · crackedLEFT 3 WINDOW FRAME E-F POST CRACKED, 2ND LOWER FASTENER HOLE. REPAIRED FRAME.SDR FXGA201606011606Window Frame · corrodedREPLACEMENT OF PILOT TO CENTER WINDOW LOWER "Z" FRAME. PILOT`S WINDOW TO CENTER WINDOW LOWER "Z" FRAME HAS CORROSION, SHEARED RIVET. THE REPAIR ITSELF INVOLVED THE 2 STAINLESS ANGLES, PN 5910075-99/-100, AT THE LOWER COCKPIT WINDOWS, LT AND RT SIDE. THE CORRSDR U2RA201606060001Support Frame · crackedRT WING TO BODY FAIRING 192K SUPPORT FRAME CRACKED. R & R SUPPORT FRAME IAW SRM 51-40-02.SDR DALA2016060804422Stop Fitting · crackedBS 1053 VENTRAL DOOR LOWER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED. REPLACED DOOR STOP IAW SRM 51-41-02, PAR. 4.SDR DALA2016060804421Stop Fitting · crackedBS 1053, VENTRAL DOOR UPPER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED, REPLACED DOOR STOP FITTING IAW SRM 51-41-02, PAR 4.SDR DALA2016060704402Door Frame · corrodedCORROSION ON PREVIOUS REPAIR AND BEAM AT MID CARGO COMPARTMENT LOWER DOOR JAMB. PREVIOUS REPAIR WAS REPLACE IAW SRM 53-05, FIG 123, SHEET, 3.SDR DALA2016060704401Window Frame · crackedCRACK ON RT WINDOW RING PAN FWD LOWER CORNER AT BS 1079. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 122 ER/A 493648-14MA REV. A AND ER/A 487747-14MA REV. ORIGINAL.SDR REXA2016060401165Beam · crackedBEAM 280 IS CRACKED JUST OTBD OF RBL 9, IN CABIN BELOW FLOOR. REPAIRED FLOORBEAM IAW REO 601R-53-11-171.SDR A6WA201643968Splice · corrodedFRAME 319.70, OUTER T-SPLICE AT SERVICE DOOR OPENING IS CORRODED AT FLOOR LEVEL IN CABIN. REPLACED FRAME 319.70 OUTER T-SPLICE AT SERVICE DOOR OPENING AT FLOOR LEVEL IAW SRM 51-42-21.SDR DALA2016060404344Pan · crackedCRACKED RT WINDOW RING PAN FORWARD LOWER CORNER AT BS 1060. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, REF ER/A 493648-14MA, REV A.SDR JR2R06032016214Door Frame · crackedMAIN LANDING GEAR FORWARD JAMB CRACKED AT FS 938, RBL 4. REPAIRED MLG FORWARD JAMB IAW SRM 53-05 FIGURE 81.SDR JR2R2016060300212Door Frame · crackedMAIN LANDING GEAR FORWARD DOOR FRAME CRACKED AT BS 938 LBL 4. REPAIRED MLG FORWARD DOOR FRAME IAW SRM 53-05, FIG 81.SDR DALA2016060304329Pan · crackedCRACKED ON RING PAN LT SIDE ON LOWER FWD CORNER OF WINDOW 91, BS 1079. CRACK OF .135" ON RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122.SDR DALA2016060304328Pan · crackedCRACKED ON RING PAN LT SIDE ON FWD LOWER CORNER AT WINDOW 55, BS 731. CRACK OF .165" ON RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122.SDR DALA2016060304326Pan · crackedCRACKED ON RING PAN RT SIDE ON UPPER FWD CORNER OF WINDOW 76, BS 927. RING PAN WAS REPAIR IAW SRM 53-05, FIG 122.SDR DALA2016060304325Pan · crackedCRACKED ON RING PAN RT SIDE ON UPPER FWD CORNER OF WINDOW 62 BS 788. RING PAN WAS REPAIR IAW SRM 53-05, FIG 122.SDR CALA2016060200340Vapor Barrier · crackedUPPER VAPOR BARRIER CRACKED IN LT WW. REPAIRED WING CTR SECTION REAR SPAR VERTICAL PRESS DECK WEB IAW SRM 57-10-10 REPAIR 3, ALTERNATIVE 2.SDR DALA2016060204322Pan · crackedRIGHT AFT OVERWING EXIT DOOR PAN CRACKED AT FWD UPPER DOOR STOP. R & R DOOR IAW AMM 52-21-00. LEAK CHECKED GOOD.SDR R61A201606010380Structure · corrodedDURING AC ACCEPTANCE FOUND CORROSION TO THE POTABLE WATER BOX CUTOUT. MAINTENANCE R & R THE WATER BOX IAW EO R170EO-53-10-0020.SDR JR2R20160601348Window Frame · crackedPASSENGER CABIN WINDOW FRAME, FWD UPPER CORNER CRACKED AT RT SIDE FS 936. R & R WINDOW FRAME AT RT FS 936 IAW SRM 51-10-4, 51-30-2 & 51-30-5.SDR SWAA2016061052742Crease Beam · corrodedL1 DOOR CREASE BEAM CORRODED AT THRESHOLD. R & R CREASE BEAM IAW DWG AND SRM.SDR SWAA2016061052741Crease Beam · corrodedR2 DOOR CREASE BEAM CORRODED. R & R CREASE BEAM IAW DWG AND SRM.SDR YENA20160531536Door Frame · corrodedDURING MAINTENANCE, CORROSION WAS FOUND ON AFT LT PASSSENGER/CREW DOOR FRAME 68. PERFORMED REINFORCEMENT REPAIR IAW SRM 53-41-14-300-001.SDR YENA20160531535Door Frame · corrodedDURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT PAS/CREW DOOR FRAME 66. PERFORMED REINFORCEMENT REPAIR IAW SRM 53-41-14-300-001.SDR DALA2016060104240Pan · crackedCRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 636 TO 655. RING PAN WAS REPAIRED IAW SRM 50-20-02. REPAIR 1, FIG 202, TYPE B.SDR DALA2016060104239Pan · crackedCRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 696 TO 715. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 203, TYPE C.SDR DALA2016060104238Pan · crackedCRACKED RT UPPER, AFT CORNER ON RING PAN BETWEEN BS 832 TO 851. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, TYPE B.SDR DALA2016060104237Pan · crackedCRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 832 TO 851 IN CPAX, SM, ZONE: 201 CARD: 3. DAMAGE ARE WAS TRIMED OUT IAW SRM 56-20-02, FIG 202. REPAIR PARTS WERE FABRICATED IAW SRM 50-20-02, FIG 202, REPAIR PARTS WERE INSTALLED IAW SRM 51-40-02 AND 51-40-SDR DALA2016053104210Pan · crackedCRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO BS 655 IN CPAX, SM, ZONE: 201 CARD: 10. ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO 655 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016053104209Pan · crackedCRACK ON FWD, UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775. ON FWD/UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016053104207Pan · crackedCRACK ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832. ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, CRACK LENGTH, L= 0.235".SDR DALA2016053104206Pan · crackedCRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927. ON FWD / LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927 WAS REPAIRED IAW SRM 50-20-02, REPAIR 1, FIG 202, CRACK LENGTH 0.198".SDR DALA2016053104205Pan · crackedCRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 617 TO 636. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR, FIG 202.SDR SWAA2016072054088Window Frame · crackedR3 WINDOW FRAME CRACKED ON THE E-F POST. REPAIRED THE WINDOW FRAME IAW SRM.SDR YENA20160529507Beam · corrodedDURING MAINTENANCE, CORROSION WAS FOUND ON AFT PASSENGER DOOR LOWER BEAM, FRAME 86 +9, LBL 48". R & R AFT PAX DOOR LOWER BEAM.SDR DALA2016053104222Pan · crackedCRACK ON RT WINDOW RING PAN AFT LOWER CORNER AT BS 1041. REPAIR PARTS WERE INTALLED IAW SRM 51-30-2, 51-30-5 AND ERA 493648-14MA, REV. A.SDR DALA2016052904196Doubler · corrodedCORROSION ON DOUBLER ATTACH INNER FUSELAGE SKIN AND CUSP WEB BETWEEN X=54 TO X=60 BS 579 TO 598, RT SIDE. CORROSION WAS REMOVED, AREA WAS MEASURED. ORIGINAL THICKNESS: 0.080" REMAINING THICKNESS: 0.041" THEREFORE ITS OUT OF LIMITS AND DOUBLER WAS REPLACED ISDR AALA201606029002Box Beam · crackedRT SIDE BOX BEAM UPPER FLANGE, AFT TWO FASTENER HOLES HAVE CRACK INDICATION AT FRAME 43 & -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.SDR AALA201606029001Box Beam · crackedLT SIDE BOX BEAM UPPER FLANGE, AFT TWO FASTENER HOLES HAVE CRACK INDICATION AT FRAME 43 & +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.SDR DALA2016053004219Door Frame · corrodedFWD CARGO DOOR FRAME UNDER ENTRY SCUFF PLATE CORRODED. DOOR FRAME OF SRM LIMITS. REMOVED AND REINSTALLED NEW LOWER PAN. REPAIRED IAW SRM 53-05, FIG 44A.SDR SIMA20160526001Roller · defectiveFLIGHT ATTENDANT REPORT MAIN DOOR IS EXTREMELY DIFFICULT TO OPEN. PERFORMED MAIN DOOR FRAME ROLLER SERVICING IAW MM 53-21-02. OPERATIONS CHECKED GOOD.SDR DALA2016052604286Angle · wornWEAR ON ANGLE CLIP ON RT FORWARD OVERWING, EMERGENCY EXIT DOOR JAMB, BS 902. R & R IAW SRM 51-30-08.
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