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 DALA2016032202233Cap · crackedCRACKED LOWER CAP BS 1463, CANT 11 HRS POSITION AT AFT ACCESORIES COMPARTMENT. LOWER CAP WAS REPAIRED IAW ETI 88-16-059, REV 7 AND ER/A 543145-14, REV ORIG SECTION I, TEMPORARY REPAIR, LENGHT CRACK 4".SDR DALA2016032102218Doubler · corrodedPOSSIBLE CORROSION AROUND AFT LAV DUMP CHUTE, FLANGE AREA, VISIBLE FROM AFT CARGO BIN INSIDE SURFACE. REPLACED PAN DOUBLER REF DWG 146N3650. PERFORMED LEAK CHECK ON ALL AFFECTED LINES IAW AMM 12-17-01-301, NO LEAKS NOTED.SDR DALA2016032002198Crossbeam · damagedELONGATED HOLE ON CROSSBEAM SECTION FRAME 68. REPLACED THE CROSSBEAM SECTION IAW SRM 51-72-11 AND DWG D53474250.SDR DALA2016032102137Door Frame · corrodedCORROSION ON LOWER DOOR JAMB BEAM AT MID CARGO COMPARTMENT. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123A AND ERA 504344-14, REV ORIGINAL.SDR DALA2016032102130Door Frame · corrodedCORROSION ON PREVIOUS REPAIR LOWER DOOR JAMB BS 1154-1212 CARGO BAY. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-05, FIG 123.SDR DALA2016032102125Door Frame · crackedCRACK ON UPPER CENTER DOOR JAMB AT LT FWD EMERGENCY EXIT. CRACK ON UPPER DOOR JAMB LT WAS REPAIRED IAW SRM 53-05, FIG 32.SDR ASAA2016031916081Shear Tie · corrodedFWD CARGO COMPARTMENT BS 500D SHEAR TIE BETWEEN 28L AND 27L HAS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS. FOUND SHEAR TIE TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 101 DETAIL II. REPAIRED SHEAR TIE IAW SRM 53-00-07-2R-4.SDR A6WA201643710Beam · corrodedCARGO BEAM AT FS 616.00, RBL 27, INBD FLANGE HAS A CORRODED FASTENER HOLE, REPAIRED.SDR DALA2016032102135Pan · crackedCRACK ON RT FWD LOWER CORNER RING PAN BS 1060-1079. REASON FOR RE-WRITE: IMPROPERLY DRILLED RT FWD LOWER CORNER AT RING PAN BS 1060-1079. RT FWD LOWER CORNER RING PAN BS 1060-1079 WAS REPAIRED IAW ER/A 543190-14, REV ORIGINAL.SDR SWAA2016040550632Cam · corrodedAFT CARGO CUT OUT AFT FRAME AFT SIDE CAM CORRODED. R & R CAM IAW SRM.SDR TLLA2016040100002Stiffener · crackedDURING DAILY INSPECTION, FOUND CRACKS IN THE AFT CROSSTUBE SUPPORT LOWER CORNERS AND STIFFENERS. THE CRACKS ARE COMMON IN THIS MODEL ACFT AND THE REPAIR PROCEDURES ARE DETAILED IN THE SRM BHT-206 SRM-1, REPAIR 5-2-1. ACFT MAY HAVE HAD A HISTORY OF FLIGHT TRASDR TLLA2016040100001Support · crackedDURING DAILY INSPECTION, FOUND CRACKS IN THE ARFT CROSSTUBE SUPPORT STRUCTURE LOWER CORNERS AND STIFFENERS. THE CRACKS ARE COMMON IN THIS MODEL ACFT AND THE REPAIR PROCEDURES ARE DETAILED IN THE SRM BHT 206, SRM-1, REPAIR 5-2-1. THIS ACFT MAY HAVE HAD A HISTSDR ASAA2016031616065Shield · corrodedAFT CARGO COMPARTMENT AFT SHIELD ASSY BETWEEN BS 847 AND BS 867, RBL 21.0 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO COMPARTMENT AFT SHIELD ASSY FROM IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS 0.050, MATERIAL LOSS 0.007, MAXIMUM ALLOWABLSDR DALA2016031702225Truss · corrodedCABIN LT TRUSS AT BS 1153-1175, FOUND WITH CORROSION, R & R.SDR DALA2016031702224Truss · corrodedRT CABIN OTBD TRUSS AT S20R BS 1197+66- BS 1197+88. FOUND WITH CORROSION, R & R.SDR DALA2016031702223Truss · corrodedCABIN TWO OTBD TRUSS AT S20R BS 1175-1197+22. FOUND WITH CORROSION, R & R.SDR DALA2016031702222Truss · corrodedRIGHT CABIN O/B TRUSS AT BS 1197+44 -1197+66 S20R FOUND WITH CORROSION, R & R.SDR DALA2016031702052Pan · crackedCRACK ON RT FWD LOWER CORNER RING PAN BS=1212- BS 1231. REASON FOR RE-WRITE: IMPROPERLY DRILLED ON RT FWD LOWER CORNER RING PAN BS=1212-BS 1231. DAMAGE AREA WAS REPAIRED IAW ETI 88-16-104, REV 3 AND ER/A 543194-14, REV ORIGINAL.SDR DALA2016031702047Door Frame · corrodedCORROSION ON WEB BETWEEN LONGERON 9 - 24R BS 629 - 700 MID CARGO BAY DOOR FRAME. CORROSION REMOVED IAW SRM 51-10-3, PAR 26, 14, 21 UT MD/DC NDT SPM 04-00-07, PAR 5, FIG 3.SDR WVER2016161600001Structure · chafedCHAFE DAMAGE AT BS 1162, STRINGER 7L.SDR SWAA2016040550606Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 807 - 827. R & R WEB IAW SRM.SDR IPXA2016033101432Tee Fitting · corrodedINSPECTION TYPE:C10, LT AFT W2B FAIRING AREA, ABOVE DOOR 197KL STRUCTURE CORRODED AT FASTENER HOLES. BLENDED CORRODED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71, REMOVED, FABRICATED AND INSTALLED NEW LOWER TEE FITTING IAW DWG 149N7630 AND SRM 51-40-SDR SWAA2016032950371Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 727E - 747. R & R WEB IAW SRM & DWG.SDR SWAA2016032850271Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 867 - 887. R & R WEB IAW SRM & DWG.SDR SWAA2016042551264Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 380 - 400. REPAIRED WEB IAW SRM.SDR SWAA2016041550940Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 847 - 867. R & R CREASE BEAM WEB IAW SRM & DWG.SDR IPXA2016040401632Structure · corrodedINSPECTION TYPE:C10, BS 1060 LOWER CHORD HAS CORROSION AROUND NUT PLATES RBL 10 TO LBL 10 MATERIAL LOSS IS OUT OF LIMITS IAW SRM 53-00-71 CUT AND SPLICE CHORD 149N7550-89 FROM RBL 21 TO EXISTING SPLICE AT LBL 55.50 IAW SRM 51-70-12, DETAIL VIII.SDR SWAA2016032850329Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 360 - 380. R & R WEB IAW SRM & DWG.SDR IPXA2016031800905Door Frame · crackedINSPECTION TYPE:C-1, AFT PIT DOOR FRAME 61 IS CRACKED. R & R THE DOOR FRAME IAW EO A300-5230-57988-D.SDR IPXA2016031800903Door Frame · crackedINSPECTION TYPE:C-1, AFT CARGO DOOR FRAME 61A IS CRACKED. R & R FRAME IAW EO A300-5230-57988-D.SDR DALA2016031501944Pressure Panel · corrodedCORROSION ON SLANT PRESSURE PANEL BS 939 BETWEEN BS 939 BETWEEN X=22 TO X=44 AT WING BOX. SLANT PRESSURE PANEL WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 38 51-10-4 DWG 9923419, REV AG, AMM 20-30-01.SDR SWAA2016040550626Crease Beam · corrodedCREASE BEAM WEB CORRODED AT BS 727+12, STRINGER 17R. REPAIRED WEB IAW SRM.SDR SWAA2016032850328Crease Beam · corrodedLEFT MAIN CABIN CREASE BEAM WEB CORRODED, BETWEEN BS 727C - 727D. R & R SHEAR WEB IAW SRM & DWG.SDR SWAA2016032850327Crease Beam · corrodedLEFT MAIN CABIN CREASE BEAM WEB CORRODED, BETWEEN BS 480 - 500. R & R WEB IAW SRM & DWG.SDR IPXA2016032100987Door Frame · crackedINSPECTION TYPE:C10, CRACK DAMAGE WAS FOUND ON BULK CARGO DOOR LOWER FRAME AT 1439.REPAIR IAW SRID:3-3471480799 WITH FAA APPROVED 8100-9 FROM DATE: MAR/19/2016 AND
EO:B767-5210-60241-A.SDR SWAA2016042551260Crease Beam · crackedRIGHT CREASE BEAM INBD CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.SDR SWAA2016041350858Door Frame · crackedAFT ENTRY DOOR CUT OUT, LOWER FRAME CRACKED AT BS 959, WL 21.1. REPAIRED FRAME IAW EA.SDR SWAA2016032850261Splice · corrodedCREASE BEAM SPLICE CORRODED, BETWEEN BS 1006 - 1016, BETWEEN LBL 40 - 45. R & R SPLICE IAW DWG & SRM.SDR SWAA2016032850260Crease Beam · corrodedCREASE BEAM WEB CORRODED AT BS 1000, LBL 45. R & R WEB IAW SRM.SDR SWAA2016031749979Crease Beam · corrodedLEFT CREASE BEAM CORRODED AT STATION 727. REPAIRED BEAM IAW EA.SDR DALA2016031102579Door Frame · corrodedAFT CARGO COMP DOOR JAMB BS 994 FRAME LOWER DOUBLER/TRIPLER SPLICE PLATES HAVE CORROSION. REMOVED SPLICE PLATES FROM AFT CARGO DOOR JAMB BS 994 AT DOUBLER/TRIPLER AND FABRICATED NEW SPLICES IAW SRM 53-20-15R-7, AND ALODINED, PRIMED, AND TOPCOATED IAW SRM 51-1SDR DALA2016031102578Door Frame · corrodedAFT CARGO COMPARTMENT DOOR JAMB FWD FRAME BS 954 LOWER DOUBLER, TRIPLER SPLICE PLATES HAVE CORROSION. REMOVED SPLICES PLATES AT AFT CARGO DOOR JAMB FWD FRAME BS 954, LOWER DOUBLER, TRIPLER AND FABRICATED NEW SPLICES PLATES IAW SRM 53-20-15-R-7 AND ALODINED ANSDR ASAA2016031016064Failsafe · corrodedAFT CARGO COMPARTMENT FRAME AT BS 847 FAIL SAFE ANGLE CORRODED STR 24R TO 25R. ACFT GROUNDED. BLENDED CORROSION ON FAIL SAFE FOUND TO BE OUT OF LIMITS REMOVED FABRICATED NEW, LOCATED, DRILLED, APPLIED ALODINE, PRIME, TOPCOATED, INSTALLED AND APPLIED CIC TO AFSDR ASOA2016031014615Fitting · crackedLOWER WINDSHIELD POST LT FITTING CRACKED AT 202 BULKHEAD. R & R LOWER WINDSHIELD POST LT FITING IAW SRM TASK 51-40-11 AND 51-42-21.SDR AALA20160310010Stop Fitting · crackedFOUND MID CARGO DOOR STOP BRACKET CRACKED AT CTR FWD SIDE OF DOOR. R & R DOOR STOP FITTING AT CTR FWD SIDE OF MID CARGO DOOR IAW AARD 51-00-05-1, DWG 4920233 & 5910141. ACFT IN BASE MX.SDR DALA2016031101864Pan · crackedCRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 579 TO 598. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A. LONG OF CRACK IS 0.450".SDR DALA2016031101861Pan · crackedCRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 927 TO 946. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101860Pan · crackedCRACK ON LT RING PAN UPPER AFT CORNER BETWEEN BS 984 TO 1003. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14, 21 AND ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101859Pan · crackedCRACK ON LT RING PAN LOWER FWD CORNER BETWEEN BS 750 TO 769. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A.SDR DALA2016031101856Pan · crackedCRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 769 TO 788. RING PAN WAS REPAIRED IAW SRM 51-30-5, 51-30-2 53-05, FIG 122, 51-10-3 PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A.
Back to JASC 5310