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 QXEA2016110300702Beam · corrodedMINOR CORROSION ON EMERGENCY EXIT SILL BEAM. THRESHOLD REMOVED IAW SRM 51-42-05. A NEW THRESHOLD INSTALLED IAW SRM 51-42-05.SDR QXEA2016110300699Doubler · corrodedAFT BAGGAGE AFT SHEAR THRESHOLD DOUBLER AT BS 728 TO 783 LBL 36 CORRODED BEYOND LIMITS. AFT BAGGAGE AFT SHEAR WEB THRESHOLD DOUBLER AT BS 728 TO 783 LBL 36. REMOVED IAW SRM 51-42-05. NEW THRESHOLD DOUBLER DRILLED IAW SRM 51-40-07. A NEW THRESHOLD SHEAR WESDR DALA2016103008057Repair · corrodedCORROSION ON LOWER MID CARGO DOORJAMB PREVIOUS REPAIR AROUND BLIND NUTS BTW STA Y =636 TO 693. REPAIR DOUBLER WAS REPLACED PER SRM 53-05 FIG 123.SDR AALA20161029002Beam · wornTHE CENTER WING SUPPORT BEAM IS WORN AT THE RIGHT AIR CONDITIONING BAY PNEUMATIC ACCESS DOOR LATCH LANDINGS. REPAIRED THE BEAM IAW EA 264817.SDR ASAA2016102818757Door Frame · corrodedMAIN CABIN L1 DOOR FRAME INBD FLANGE, CORRODED BS 303.9, STRINGERS 9 - 10L. ACFT GROUNDED. REMOVED CORROSION IAW 700-53EA-17989 REV 00, REO-G20402 REV A.SDR QXEA2016110100694Doubler · corrodedDRAIN MAST INTERNAL AND EXTERNAL DOUBLER AT X 19.400 BETWEEN STRINGERS 32-33R CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-05, AND 51-23-10.SDR DALA2016102807811Door Frame · crackedCRACKED UPPER AREA OF AFT VENTRAL DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW SRM 51-41-02 PAR. 7.C. (1), 51-41-05 PAR 10 FIG. 19, AND SRM 53-00-00 REPAIR 1, FIGURE 201, 51-41-02 AND 51-41-05.SDR IXXA20161130178Failsafe · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFTER REMOVING WEB FOR REPAIR ON NONROUTINE 0759, FOUND CORROSION ON THE FAIL SAFE STRAP AT BS 544 BETWEEN STRINGERS 34 AND 35R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED BLENDED AREA BY REINFORCEMENT IN ACSDR SWAA2016112809842Door Frame · corrodedL1 DOOR FRAME CORRODED AT BS 303.9. REPAIRED THE DOOR FRAME IAW EA.SDR V0XD2016111901Beam · corrodedRT EMERGENCY EXIT DOOR SURROUND HAS SIGNS OF CORROSION AROUND GUIDE PIN HOLES. REMOVED AND REPLACED RT LOWER EMERGENCY EXIT DOOR BEAM IAW SRM 51-20-03 AND 51-40-02SDR AALA201611159006Structure · corrodedCORROSION ON AFT RIGHT MAIN CABIN REINFORCEMENT STRUCTURE BETWEEN FRAMES 83 AND 84, AND Y292 TO Y1193. REPLACED THE STRUCTURE IAW SRM 51-41-02 AND DRAWING 190-65401-801.SDR AALA20161026010Door Frame · crackedLAVATORY SERVICE PANEL SURROUND STRUCTURE AT APPROXIMATELY BS 429 IS CRACKED. REPAIRED THE STRUCTURE IAW SRM 51-70-11-0G.SDR DALA2016102707743Door Frame · corrodedCORRODED PREVIOUS REPAIR ON LOWER AREA OF AFT VENTRAL DOOR FRAME AT W2. THE REPAIR WAS REMOVED IAW SRM 51-30-1 AND A NEW REPAIR WAS FABRICATED IAW SRM 53-05 FIG.34. 51-30-2. THE REPAIR WAS INSTALLED IAW SRM.53-05 FIG. 34.SDR AALA201611219001Door Seal · corrodedDOOR SEAL HAS SURFACE CORROSIO. REPLACED THE DOOR SEAL IAW SRM 51-42-11, AND DRAWING D53480505.SDR DALA2016102607603Box Beam · crackedA ROTOTEST INSPECTION OF THE LEFT SIDE BOX BEAM, FOUND CRACKED. REPAIRED IAW AMDS 5310-01450-02.SDR ASOA201610256074Beam · corrodedDURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AALA201610319024Box Beam · crackedCRACK INDICATIONS ON LEFT SIDE BOX BEAM UPPER FLANGE AFT 2 HOLES AT FR 43 AND Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.SDR AALA201610319011Box Beam · crackedCRACK INDICATION ON AFT RIGHT BOX BEAM UPPER FLANGE 2 HOLES AT FRAME 43 AND -Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.SDR DALA2016102507602Box Beam · crackedRIGHT SIDE BOX BEAM CRACK INDICATION OF BEAM CENTER HOLE FRAME 43. REPAIRED IAW AMDS 5310-01450-02.SDR DALA2016102507601Box Beam · crackedLEFT SIDE BOX BEAM CRACK INDICATION ON UPPER PRESSURE PLATE CENTER LOCATION, REPLACED IAW AMDS 5310-01450-02.SDR DALA2016102407519Door Frame · crackedCRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN. CRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN WAS REPAIRED PER SRM 53-05 FIG 142.SDR IPXA2016110210173Intercostal · crackedINSPECTION TYPE: 3C, INTERCOSTAL CRACKED BS 6-30 - 6-50 BETWEEN LONGERONS 41 AND 42L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG ACA7049 AND SRM 51-33-01.SDR SWAA2016102809160Beam · crackedSPAN WISE BEAM CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.75. R&R BEAM IAW SRM.SDR SWAA2016102809159Beam · crackedSPAN WISE BEAM CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.75. R&R BEAM IAW SRM.SDR CALA2016102495847Door Frame · crackedL2 DOOR CUTOUT FRAME 68 LOWER STOP LOWER INBD HOLE HAS A CRACK INDICATION AT 6 O'CLOCK AND 12 O'CLOCK POSITION. REPAIRED IAW SRM 53-41-12 PAR 5.E. FIG 204.SDR DALA2016102307492Box Beam · crackedSIDE BOX BEAM UPPER FLANGE LEFT SIDE CRACK INDICATION AT MIDDLE AND AFT HOLES WITH HFEC ROTOTEST, REPAIRED IAW AMDS 5310-01450-02.SDR REXA2016102102119Angle · crackedCO-PILOTS SIDE WINDOW FRAME HAS CRACKED LOWER AFT ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.SDR REXA2016102102118Angle · crackedPILOTS SIDE WINDOW FRAME HAS A CRACKED LOWER AFT ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.SDR REXA2016102102063Crossbeam · corrodedFS 280 TRANVERSE BEAM IS CORRODED AROUND SEVERAL FASTENER HOLES AND AT MACHINED EDGE AT APPROX RBL 1.5 CORROSION ON MACHINED EDGE GOES COMPLETELY THROUGH PART IN TO RADIUS. REMOVED RH FS 280 TRANSVERSE BEAM AND INSTALLED SERVICEABLE BEAM IAW SRM 51-40-11-001-0SDR REXA2016102102062Beam · corroded900-53-900-504; LH FS 280 TRANSVERSE BEAM IS CORRODED AROUND FASTENER HOLES AND CRACKED AT APPROX LBL 12. REMOVED THE TRANSVERSE BEAM AND INSTALLED SERVICEABLE BEAM IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-42-21-001-001-A0SDR DALA2016102207505Door Frame · crackedCRACK ON LT AFT EMERGENCY EXIT DOOR JAMB UPPER AREA. CRACK (0.843") ON DOOR JAMB WAS REPAIRED PER SRM 53-05 FIG 32.SDR KO0R201610210073Door Frame · corrodedEVIDENCE OF CORROSION ON THE AFT CARGO DOOR CUTOUT FRAME AFT LOWER CORNERSDR SWAA2016110709438Crease Beam · corrodedR2 CREASE BEAM CORRODED. R&R CREASE BEAM IAW SRM AND DWG.SDR SWAA2016110709406Crease Beam · corrodedCREASE BEAM CORRODED BETWEEN BS 927 TO 986, LBL 53. R & R THE CREASE BEAM IAW DWG AND SRM.SDR BJNA20161020001Beam · crackedSTUB BEAM BS 616 RT CRACKED AT LOWER 2 FASTENERSSDR IPXA2016110210151Door Frame · crackedINSPECTION TYPE:3C, L3 DOOR FWD FRAME LOWER WEB IS CRACKED. REPAIRED THE DOOR FRAME IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)SDR SWAA2016110109175Crease Beam · corrodedR1 DOOR THRESHOLD CREASE BEAM CORRODED. R & R THE CREASE BEAM IAW DWG & SRM.SDR IPXA2016103010029Door Frame · crackedINSPECTION TYPE: 3C, R3 DOOR FRAME LOWER WEB IS CRACKED AT BS 1305.25 AND Z-18. REPAIRED THE DOOR FRAME WEB IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR).SDR DALA2016102207504Door Frame · corrodedCORROSION ON AFT BULKHEAD DOOR JAMB LOWER SECTION UPPER AND LOWER SURFACE. DOOR JAMB WAS REPAIRED PER SRM 53-05 PAR 45 FIGURE 34.SDR DALA2016102107483Door Frame · crackedDURING INSPECTION FOUND R1 DOOR FORWARD STUB FRAME CRACKED AT LOWER INBOARD FLANGE. MAINTENANCE REPAIRED CRACKED STUB FRAME AT R1 DOOR FORWARD LOWER CUT OUT IAW PRI 550652-14 REV 0 AND REV 1, AND ER/A 550652-14 REV ORIGINAL.SDR DALA2016102107422Door Frame · crackedCRACK ON DOOR JAMB STA Y=954 AT AFT CARGO COMPARTMENT C2 (SM) (S/N 00135). DOOR JAMB WAS REPLACE PER SRM 51-41-02 AND 51-41-05. PERFORM DECAL VISUAL INSPECTION EVERY C CHECK PER TOPP 30-10-70 PAR I PG 14.SDR DALA2016102107415Pan · crackedCRACKED LT WINDOW RING PAN AFT/LOWER CORNER STA Y=905 AT CPAX. RING PAN WAS REPAIRED PER SRM 53-05 FIG 122, 51-30-02, 51-30-05, 51-10-03, PAR 21,14.AND ER/A 487747-14MA REV A, 493648-14MA. REV A.SDR SWAA2016120910347Window Frame · corrodedRT NR 1 WINDOW FRAME CORRODED ON ENTIRE EXTERIOR SURFACE. REPAIRED FRAME PER ER AND EA.SDR SWAA2016120910346Window Frame · corrodedLT NR 1 WINDOW FRAME CORRODED ON ENTIRE EXTERIOR SURFACE. REPAIRED FRAME PER ER AND EA.SDR TSAA20161124031Window Frame · crackedCRACK FOUND AT BS 787, STRINGER 13L, LOWER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE FUSELAGE SKIN AND THE WINDOW FRAME. CRACKED SKIN REPAIRED IAW SRM 53-00-01 REV. 111, REPAIR 34. THE WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A117SDR TSAA20161124030Window Frame · crackedCRACK FOUND AT BS 520, STRINGER 12R, UPPER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED 2 CRACKS IN THE WINDOW FRAME. WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.SDR TSAA20161124029Window Frame · crackedCRACK FOUND AT BS 500B, S12R, UPPER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE WINDOW FRAME. WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.SDR TSAA20161124028Window Frame · crackedCRACK FOUND AT BS 500A, STRINGER 12R, UPPER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE WINDOW FRAME. WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.SDR SWAA2016111009571Angle · crackedR1 DOOR CUTOUT ANGLE CRACKED BETWEEN BS 277 TO 291.5, STRINGERS 9 -15R. REPAIRED THE ANGLE IAW EA.SDR SWAA2016110909537Door Frame · crackedFORWARD GALLEY DOORWAY FORWARD FRAME CRACKED AT LOWER AT BS 294, WL 208. REPAIRED FRAME PER ER AND EA
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