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 CA141024023Frame · cracked(CAN) DURING A STRUCTURAL INSPECTION, MAINTENANCE FOUND A CRACK AT BS 451. CRACK MEASURES APPROXIMATELY 2 INCHES IN LENGTH.SDR SWAA2014120434679Frame · crackedFRAME CRACKED AT BS 663 STRINGER 3L. REPAIRED FRAME IAW ER & EA.SDR DALA2014111306107Angle · damagedELONGATED DRILL HOLE ON FRAME ANGLE BS 294 BETWEEN LONGERONS 19 - 22L. A NEW FRAME ANGLE AND SPLICE WERE FABRICATED, TREATED AND PAINTED AND INSTALLED IAW SRM 53-14-2, FIG 2, 51-10-2, 51-10-3 PAR 14/21, & 51-30-2.SDR A6WA201442124Frame · corrodedLOWER FRAME SECTION AT FS 605 CORRODED BEYOND LIMITS.SDR DALA2014102505750Frame · crackedCRACKED FRAME WEB AND INNER FRAME FLANGE, AFT SIDE OF BS 1485 . TAIL INTERIOR. REPAIRED IAW PRI 530093-14, REV 0 AND COMPLY WITH ERA 530093-14, REV ORIG.SDR AALA20141024015Frame · crackedCANTED FRAME 1485 CRACKED AT THE AFT AIRSTAIR MOUNT RT SIDE. ACCOMPLISHED REPAIR SPLICE IAW AARD 53-10-0033.SDR WVER2014102400002Frame · crackedFRAME AT BS 235 HAS A CRACK ON UPPER END BELOW PILOT WINDOW.SDR SWAA2014121635063Frame · crackedFRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.SDR SWAA2014120434661Frame · crackedFRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, RT SIDE. REPAIRED CHORD IAW EA.SDR SWAA2014120434660Frame · crackedFRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, LT SIDE. REPAIRED CHORD IAW EA.SDR SIMA20141023004Frame · crackedREF ITEM 3 LOG 3667645 AFTER INTERNAL INSPECTION OF DAMAGED AREA FOUND CRACKED FRAME, SEVERAL PULLED RIVETS & DAMAGED SKIN PANEL ON SAME AREA AS EXTERNAL DAMAGE. TRANSFERRED TO NRWC 674-ABI-02296. PERFORMED REPAIR IAW ERS-EM-53MR-847.SDR CALA2014102401391Frame · crackedFOUND CRACK INDICATION ON INBD RIVET HOLE FRAME 400R. REPAIRED CRACK IAW ECRA 5310-06287. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,000 CYCLES BUT BEFORE 44,000 TOTSDR CALA2014102401390Frame · crackedCABIN FRAME INSPECTION FOUND CRACK INDICATION ON INBD RIVET STATION 400L. REPAIRED CRACK IAW ECRA 5310-06287. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT C CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,000 CYCLESSDR CALA2014102401389Frame · crackedFOUND CRACK INDICATION ON INBD RIVET HOLE FRAME 440R. REPAIRED CRACK IAW ECRA 5310-06287. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,000 CYCLES BUT BEFORE 44,000 TOTSDR CALA2014102401388Frame · crackedCABIN FRAME INSPECTION FOUND CRACK INDICATION ON INBD RIVET STATION 440L. REPAIRED CRACK IAW ECRA 5310-06287. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,000 CYCLES BSDR CALA2014102401387Frame · crackedFOUND CRACK INDICATION ON INBD RIVET HOLE FRAME 480R. REPAIRED CRACK IAW ECRA 5310-06287. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,000 CYCLES BUT BEFORE 44,000TOTASDR CALA2014102401386Frame · crackedCABIN FRAME INSPECTION FOUND A CRACK INDICATION BS 867. REPAIRED IAW ECRA 5310-06287.SDR CALA2014102401385Frame · crackedCRACK INDICATION ON FRAME BS 827. REPAIRED IAW ECRA 5310-06287.SDR CALA2014102401384Frame · crackedIAW EA 5310-04716 OP2 FOUND CRACK INDICATION ON INBD RIVET HOLE FRAME 867R. REPAIRED IAW ECRA 5310-06287. ACCOMPLISHED INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,000 CYCLES BUTSDR SWAA2014121635062Frame · crackedFRAME CRACKED AT BS 986, STRINGER 19L. R & R FRAME IAW EO & EA.SDR ASOA2014110611605Frame · corrodedCORROSION ON FRAME AT FS 333.00 BETWEEN LBL STGR 24 AND RBL STGR 24. REMOVED POSTS AT FS 333 RBL 20 AND LBL 20 IAW SRM 51-42-06 & 51-42-21. UPON FURTHER INVESTIGATION, FOUND TO BE BETWEEN STR 24 & 23L AND STR 24 & 23R, INSTALLED SAME SERVICEABLE VERTICAL POSSDR ASOA2014110611604Frame · corrodedCORROSION ON FRAME AT FS 349.00 BETWEEN LBL STR 24 AND RBL STGR 24. REMOVED CORRODED FRAME SECTOR AT FS 349.00 BETWEEN STR 23L-23R IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FS 349.00 FRAME SECTOR IAW SRM 51-40-11. INSTALLED IAW SNIESDR CALA2014102401376Frame · crackedCABIN INT FRAME AT STATION 1540 IS CRACKED NEAR FASTENER BETWEEN STRINGER -8R & -9R. REPAIRED IAW SRM 5300-00-07 REPAIR 1.SDR SWAA2014121635044Frame · crackedFRAME OUTER CHORD CRACKED AT BS 452, BETWEEN STRINGER 19R TO 20R. REPAIRED FRAME IAW EA.SDR SWAA2014111734239Frame · crackedFRAME CRACKED AT BS 947 BETWEEN STRINGER 17R TO 23R. R & R FRAME IAW SRM & DWG.SDR SWAA2014110333607Frame · crackedFRAME CRACKED AT BS 727C STRINGER 25L. REPAIRED FRAME IAW EA .SDR FDEA201410203312Frame Splice · gougedAFT CARGO BAY BS 1520 STRINGER 24R - 25R FRAME SPLICE GOUGED. FOUND OUT OF LIMITS. REMOVED AND REPLACED THE FRAME SPLICE IAW DWG 146N1017 SHT 2 REV. E, AND DWG 146N1042 SHT 01 REV. A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR SWAA2014121635041Frame · crackedFRAME WEB CRACKED AT BS 452, BETWEEN STRINGER 19R TO 20R. REPAIRED WEB IAW EA.SDR SWAA2014121635040Frame · crackedFRAME CRACKED AT BS 360, STRINGER 20R. REPAIRED FRAME IAW EA.SDR FDEA201410193305Frame · corrodedAFT CARGO BS 1380 S17-18R FRAME FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10- 02 REV 113 AND FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 ALLOWANLE DAMAGE 2 REV 113. FRAME REMOVED AND REPLACED IAW SRM 51-40-02 REV 113, DWG 146N8511 SHT 1 REV J. REPASDR ASOA2014111411650Frame · corrodedCORROSION DAMAGE ON BS 333, FRAME AFT SIDE, STR 26L-26R. BLENDED CORROSION IAW SRM 51-12-00-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF FS 333, FRAME IAW BSC NDT PROGRAM MANUAL SEC. 4.3. MIN, REMAINING THICKNESS IS .049", ORIGINAL IS .050", REMOVED IS SDR ASOA2014111411648Frame · corrodedCORROSION DAMAGE ON FS 295.00 FRAME AFT SIDE, STR 26L-26R. BLENDED CORROSION IAW SRM 51-12-00-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. AFTER FURTHER EVALUATION SEVERE CORROSION WAS FOUND WITH 100 PERCENT MATERIAL LOSS FRAME REPSDR SWAA2014120834760Frame · crackedFRAME OUTER CHORD CRACKED AT BS 188, STRINGER 17R. REPAIRED FRAME IAW SRM.SDR SWAA2014120834759Frame · crackedFRAME OUTER CHORD CRACKED AT BS 188, STRINGER 17L. REPAIRED FRAME IAW SRM.SDR SWAA2014103033518Frame · crackedLOWER STUB FRAME CRACKED AT BS 294. R & R STUB FRAME IAW SRM & DWG.SDR FDEA201410183300Frame · corrodedCORROSION FOUND ON AFT FUSELAGE FRAME WEB AT BS 1681 BETWEEN STRINGERS 28 - 29R. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.SDR FDEA201410183299Frame · corrodedHIDDEN DAMAGE AFT FUSELAGE AT STATION 1710 BETWEEN STRINGER 28R & 29R FRAME WEB AFT FACE HAS CORROSION.SDR CALA2014102101359Frame · crackedCABIN INT FRAME AT STATION 1580 IS CRACKED NEAR FASTENER BETWEEN STRINGER -8R & -9R. COMPLIED WITH ALL STEPS TO REPAIR CABIN INT FRAME IAW SRM 53-00-07, REPAIR 1. SUPPLEMENTAL INSPECTION REQUIRED AT 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50000 AIRFRSDR CALA2014102101358Frame · crackedLEFT PSU RAIL SUPPORT AT STATION 760 STRINGER 9L SHOWS POSSIBLE CRACK INDICATION AT RIVET. REPAIRED FRAME IAW SRM 53-00-07 REPAIR 1. SUPPLEMENTAL INSPECTION REQUIRED 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLES WHICHEVER COMESSDR CALA2014102101353Frame · crackedCABIN INT FRAME AT STATION 1520 IS CRACKED NEAR FASTENERS BETWEEN STRINGER 8R & 9R. FABRICATED & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07. SUPPLEMENTAL INSPECTION 12000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FSDR SWAA2014112134386Frame · crackedFRAME CRACKED AT BS 360, STRINGER 13R. REPAIRED FRAME IAW EA.SDR HYIA20141017053Frame · corrodedFUSELAGE FRAME 24 CORROSION BETWEEN STRINGERS 19 - 20 RHS. CORRODED FRAME PORTION CUT AWAY & NEW PORTION SPLICED AT LEVEL OF STRINGERS 17 LT & RT IAW ADAPTATION OF SRM REPAIR IAW 53-00-00 FIG 435 FOLLOWING ATR INSTRUCTION. IAW EO ATR-53-68-2014.SDR HYIA20141017048Strap · corrodedFUSELAGE FRAME 25 INTERNAL STRAP CORROSION AT STRINGER. CORRODED INTERNAL STRAP PORTION BLENDED OUT & INSPECTED WITHOUT ADDITIONAL FINDINGS FOLLOWING ATR INSTRUCTION IAW EO ATR-53-63-2014.SDR DALA2014101805720Frame · gougedMAIN CABIN FRAME GOUGED AT BS 1280, S10R. FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGE. REPAIRED IAW SRM.SDR HYIA20141017042Frame · corrodedFUSELAGE FRAME 28 CORROSION BETWEEN STRINGERS 21 LT & RT. CUT AWAY CORRODED FRAME PORTION & SPLICED IN NEW IAW ADAPTATION OF TSK-530000-300-840-A01 FOLLOWING ATR INSTRUCTION IAW EO ATR-53-57-2014.SDR SWAA2014102233239Frame · crackedFRAME CRACKED AT BS 400 STRINGER 14L. REPAIRED FRAME IAW SRM & DWG.SDR HYIA20141017021Frame · mechanic errorFOUR MIS DRILLED HOLES AT FRAME 23 BETWEEN STRINGER 16 & 18. ALL FOUR HOLES WERE OVERSIZED TO .281 INCH IN DIAMETER IN ORDER TO REMOVE THE DAMAGE. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS IAW EO ATR53-34-2SDR AALA20141017005Strap · corrodedFAIL SAFE STRAP FROM STATIONS 456 TO 610 CORRODED. REPLACED FAIL SAFE STRAP.SDR FDEA201410163228Frame · corrodedAFT PIT BS 1580 STRINGER 28L - 30 FRAME & SHEAR TIE CORRODED. REMOVED AND REPLACED FRAME AT STA 1580, FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS OF .011" OF ORIGINAL 0.63", IAW SRM 53-00-07, FIG 101, DETAIL I, AND IAW SRM 51-40-02 AND DWG 140N2002. MAJORSDR FDEA201410163229Frame · corrodedAFT CARGO BAY BS 1640, STRINGER 26 - 28L FRAME CORRODED. REMOVED COROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DEATIAL II. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032. MAJOR REPAIR.
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