JASC 5311
Service difficulty reports · 61,549
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 Y2PA20141124032Frame · corrodedDURING C CHECK, DISCOVERED A CORRODED FUSELAGE FRAME AT STATION 256 AT LONGERON 30. REPAIRED CORRODED FUSELAGE FRAME AT STATION 256 AT LONGERON 30 IAW DC9 SRM 53-05 FIG 5.SDR Y2PA20141124031Frame · corrodedDURING C CHECK, DISCOVERED A CORRODED FUSELAGE FRAME AT STATION 389 AT LONGERON 30. REPAIRED CORRODED FUSELAGE FRAME AT STATION 389 AT LONGERON 30 IAW DC9 SRM 53-05 FIG 5 & 51-30-2.SDR Y2PA20141124030Frame · corrodedDURING C CHECK, DISCOVERED A CORRODED FUSELAGE FRAME AT STATION 465 BETWEEN LONGERONS 29L & 29R. REPAIRED CORRODED FUSELAGE FRAME AT STATION 465 BETWEEN LONGERONS 29L & 29R IAW DC9 SRM 53-03 PARA 1C.SDR Y2PA20141124028Frame · corrodedDURING C CHECK, DISCOVERED A CORRODED AFT CARGO PIT FRAME AT STATION 786 BETWEEN LONGERONS 29L & 28R. REPAIRED CORRODED AFT CARGO PIT FRAME AT STATION 786 BETWEEN LONGERONS 29L & 28R IAW DC9 SRM 53-03 PARA 1C.SDR Y2PA2014112400027Intercostal · corrodedDURING C CHECK, DISCOVERED FUSELAGE FRAME CORRODED BS 738 BETWEEN LONGERONS 25 & 26L. REPAIRED THE FRAME IAW SRM 53-03 FIG 2A.SDR Y2PA20141124026Frame · corrodedDURING C CHECK, DISCOVERED A CORRODED FUSELAGE FRAME AT STATION 738 BETWEEN LONGERONS 25L & 26L. REPAIRED CORRODED FUSELAGE FRAME AT STATION 738 BETWEEN LONGERONS 25L & 26L IAW DC9 SRM 53-03 FIG 2A.SDR Y2PA20141124018Frame · corrodedDURING C CHECK, DISCOVERED A CORRODED FUSELAGE FRAME AT STATION 408 BETWEEN LONGERONS 29R & 29L. REPAIRED IAW DC9 SRM 53-03 FIG 2A PAGE 12.SDR CALA2014112501479Frame · crackedCABIN FRAME AT STATION 760 HAS CRACK AT FASTENER BETWEEN STRINGER -8L & -9L. REPAIRED CABIN FRAME. INITIATED TABLE 203 SUPPLEMENTAL INSPECTION ZONE 3 12,000 FLIGHT CYCLES DIP, 53-DIP CN 30871 SUBMITTED ESFR IAW SRM 53-00-07 REPAIR 1 FROM REPAIR INSTALLATION,SDR AALA20141124001Frame · crackedCANT FRAME AT FS 1510 IS CRACKED AT FIRST TAIL CONE GUIDE PIN BELOW RT UPPER LATCH. REPAIRED FRAME IAW SRM 53-01-00-001.SDR ASOA2014122311928Frame · corrodedFRAME BS 250 S27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.SDR FDEA201411223861Frame · crackedFRAME 40 CRACKED. REPAIRED IAW EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201411223860Frame · crackedFRAME 40 CRACKED. REPAIRED IAW EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201411223859Frame · crackedFRAME 40 CRACKED. EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201411223864Frame · gougedLEFT CABIN, BS 535 STRINGER -23L, FRAME INBD FLANGE, PREVIOUS REPAIR, GOUGED. GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A, ORIGINAL MATERIAL 0.125 INCHES, D=0.100 INCHES. REMOVED PREVIOUS REPAIR IAW SRM 51-31-01, FABRICATED, LOCATED & DRILLED TWOSDR IXXA20150331097Fitting · corrodedAIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. LT SIDE FRAME FITTING CORROSION ON PRESS WEB ATTACH POINT & BELOW HOLE NR 9. INSTALLED SIDE FRAME FITTING IAW SRM 51-40-02 & ENGINEERING DOCUMENT 47008ORD11.SDR FDEA201411203825Frame · crackedNDT FOUND LT FUSELAGE FRAME SPLICE 47 AROUND HOLE H IS CRACKED BETWEEN STRINGERS 24 & 26L. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH EA 6-5310-T0313717 PT1.SDR FDEA201411203824Frame · crackedNDT FOUND RT FUSELAGE FRAME SPLICE 47 BETWEEN STRINGER 24 & 26RT AROUND HOLE M CRACKED. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH EA:6-5310-T0313717 PT1.SDR SWIA201440284Frame · corrodedCORROSION FOUND BS 333 FRAME LOWER FLANGE BETWEEN S25L - 26R. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AND RESTORED FINISH IAW EA.SDR SWIA201440216Frame · corrodedBS 985, LOWER FRAME CORRODED AT S22-23R. REPAIRED THE FRAME IAW EA.SDR DALA2014112206253Frame · crackedAFT ACCESSORY BAY FRAME BS 1437, L2L CRACKED. REPLACED FRAME IAW SRM 51-30-2.SDR CALA2014112492724Frame · corrodedCORROSION ON FRAME 1109 UPPER T CAP LOWER SURFACE LBL 44 EXCEEDS MAXIMUM ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07 FIG 101 DETAIL VIII. R & R T CAP IAW SRM 51-40-02 PAR 4 & 7 FIG 3, 8 & 12, UPPER T CAP FABRICATED IAW DWG 146T1202.SDR SWAA2014112434418Frame · crackedFUSELAGE FRAME CRACKED AT STATION 827 BETWEEN STRINGERS 8R & 9R. REPAIRED FRAME IAW EA.SDR IXXA20150403101Fitting · corrodedAIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. SIDE FRAME FITTING RT SIDE FOUND CORROSION AT PRESS DECK WEB HOLES & POCKETS. INSTALLED NEW SIDE FRAME FITTING IAW SRM 51-40-02 & ENGINEERING DOCUMENT 47008RD12.SDR UHLA2014111900816Frame Splice · corrodedCORROSION ON CENTER SPLICE PLATE FRAME 90. R & R FRAME SPLICE.SDR DALA2014112006306Frame · damagedCRACKED REPAIR ON FRAME BS 1485 LONGERON 24R. REPAIR REMOVED IAW SRM 51-30-2, 51-30-3 AND A NEW REPAIR WAS FABRICATED IAW SRM 53-03, FIG 43, THE REPAIR WAS PAINTED IAW SRM 51-10-3 AND INTALLED IAW SRM 51- 30-2, 51-30-5.SDR SWAA2014111934323Frame · crackedFRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.SDR CALA2014111901465Frame · crackedCABIN FRAME HAS CRACK AROUND FASTENER HOLE AT STATION 760 BETWEEN STRINGER -8R & -9R. ACCOMPLISHED REPAIR IAW SRM 53-00-07, REPAIR 1 & INITIAL DIP TO RE-INSPECT TABLE 203, ZONE 3 FOR 12000 FLIGHT CYCLE FROM REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLE, WSDR CALA2014111901464Frame · crackedCABIN FRAME AT STATION 1540 HAS CRACK AS FASTENER BETWEEN STRINGER 8R & STRINGER 9 R. ACCOMPLISHED REPAIR IAW SRM 53-00-07 REPAIR 1 & INITIAL DIP TO REINSPECT TABLE 203 ZONE 3 FOR 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLES, WHSDR IXXA20150331085Strap · corrodedAIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER STRAP ON FRAME AT STATION 1269 IN ALC, FWD OF DOOR CUT OUT BETWEEN STRINGER 34R - 33R CORRODED. R & R FRAME STATION 1269 UPPER CAP IAW SRM 51-40-02.SDR CA141124011Frame · cracked(CAN) DURING ABC STRUCTURAL INSPECTION MAINTENANCE NOTICED A 0.500" CRACK FOUND ON LT FRAME BS 288 AT STRINGER 11L LOCATION. REFERENCE "A" CHECK ITEM #37, FIGURE 27. "A HIGH FREQUENCY CURRENT SURFACE SCAN (EDDY CURRENT) WAS CARRIED OUT ON REPAIR OF STATION 288SDR SWIA2014112540165Frame · crackedBS 220 FRAME FOUND CRACKED. REPAIRED IAW SRM.SDR SWIA2014112540164Frame · crackedFOUND BS 235 FRAME TO BE CRACKED. REPAIRED THE FRAME IAW SRM.SDR SWIA2014112540163Frame · crackedBS 235 FRAME CRACKED. REPAIRED IAW SRM.SDR DALA2014112006307Frame · corrodedCORROSION ON FRAME BS 1463 BETWEEN LONGERONS 24-25L. THE CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26, UT WAS ACCOMPLISHED IAW NDT SPM 06-04-PAR 5, FIG 7 AND FOUND OUT OF LIMITS IAW SRM 53-01 AND AREA WAS REPAIRED IAW SRM 53-01, FIG 2, SHEET 4.SDR DALA2014111906251Frame · crackedFRAME CRACKED AT BS 859.5 ON RT SIDE BELOW WL 200. REPAIRED ON WC 5311-01-01195-09.SDR AALA20141118005Frame · damagedFUSELAGE FRAME INNER CHORD AT STATION 500 BETWEEN STRINGERS 20 & 21 LT IS DAMAGED. REPAIRED FRAME CHORD IAW EA B737-53-037458 DATED 11/18/14.SDR SWAA2014111934322Frame · crackedFRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.SDR SWAA2014111934321Frame · crackedFRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.SDR SWAA2014111934320Frame · crackedFRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.SDR SWAA2014111934319Frame · crackedFRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.SDR FDEA201411183796Frame · mechanic errorMAIN CABIN, LT AT BS 960 FWD EMER WINDOW CUT OUT JUST BELOW STRINGER 9L DOUBLE DRILLED HOLE IN FRAME. FUSELAGE FRAME REPAIR AT STATION 960 BELOW STRINGER 9L WAS ACCOMPLISHED DUE TO EFFECTING THE PTF CONVERSION ON EA 757-5342-16-F4770 REV DATED NOV 7 2014 & NRSDR GLBA2014111700466Frame · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME FLANGE AT FS 177.35 BETWEEN STRINGERS 13L & 14L IN THE FRAME FLANGE BEND RADIUS AT OTBD END OF FRAME, .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTSDR ASOA2014120811844Frame · corrodedFRAME AT BS 349, CORRODED BETWEEN STRINGERS 26L & 26R. CORROSION REMOVED IAW SRM 53-21-06-101-004-A02.SDR DALA2014111806271Frame · crackedFRAME CRACKED BS 1451 LONGERON 1. FRAME, REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9911860-3, REV=L.SDR SWAA2014120834804Frame · buckledFRAME BUCKLED AT BS 198, BETWEEN LBL 1 TO RBL 14. REPAIRED FRAME IAW SRM.SDR SWIA201439961Frame · corrodedFUSELAGE FRAME CORRODED. PAINT LIFTING AND BUBBLED AT STA 319 AND STRINGER 26 LT. REPAIRED IAW REO AND SRM.SDR FDEA201411143686Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LT LOWER FASTENER HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0313797 PT1, TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES IN CENTER WING JOINT - FR40LH , REPAIRED THE FRAME 40 TOSDR UHLA2014111400835Frame · damagedFRAME 84 HAS BLADE MARKS ACROSS WHOLE FRAME AND CORROSION. REPAIRED IAW ETD2014-170-096717.SDR UHLA2014111400804Frame · corrodedFRAME 84 HAS BLADE MARKS ACROSS WHOLE FRAME AND CORROSION STARTING. THREE CORROSION SPOT DRILLED AND RIVET INSTALLED. 1 SPOT BLENDED WITH .10MM METAL LOSS IAW ETD2014-170-096717.SDR ASOA20141114333Frame · crackedDURING C-CHECK, CRACK AT RIVET FRAME 10 UNDER RT DV WINDOW CUTOUT. MAINTENANCE R & R FRAME 10 UNDER RT DV WINDOW CUTOUT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
Back to JASC 5311