JASC 5714
Service difficulty reports · 1,451
Reports filed under 5714 · Wing, Center Box, 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 = '5714' 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 = '5714' 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 QXEA2012061500489Panel · corrodedCENTER WING UPPER DRY BAY PANEL 521BT HAS AREAS OF CORROSION ON MATING SURFACE. REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS IAW RD 8/4-57-425. CONFIRMED AREAS CRACK FREE REF NTM 51-00-06-910-801 PT 1. FOUND WITHIN LIMITS. ALODINED, PRIMESDR FWTA201205300001Stiffener · crackedDURING C CHECK (10C S1C,S4C) INSPECTION OF WING CENTER SECTION FRONT SPAR VERTICAL STIFFENERS AT LBBL 32.94 AND LBBL 54.69 FOUND CRACKED. ACCOMPLISHED MAJOR REPAIR PER ENGEENERING ORDER # RP-57-3433 AND RP-57-3434.SDR AALA20120609003Vapor Barrier · crackedCRACK DAMAGE ON THE WING CENTER SECTION REAR SPAR VAPOR BARRIER. INSTALLED CROSSBRACE REPAIRS ON LEFT AND RIGHT VAPOR BARRIERS AT BAYS 2L, 4L AND 1R, 2R, 4R PER SRM SUP 57-10-10-2R, REPAIR 2.SDR WRLA20120524545Structure · corrodedCORROSION ON TOP OF CENTER WING BOX AT STA 1249 BETWEEN X=75.25 AND X=709.25 RT.SDR SWAA2012052904376Stiffener · crackedSTIFFENER CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR SWAA2012052904375Stiffener · crackedSTIFFENER CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR SWAA2012052904374Stiffener · crackedSTIFFENER CRACKED AT BS 540, BETWEEN LBL 45.5 TO LBL 70.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR SWAA2012052904373Stiffener · crackedSTIFFENER CRACKED AT BS 540, BETWEEN RBL 45.5 TO RBL 70.53. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR SWAA2012052904372Stiffener · crackedSTIFFENER CRACKED AT BS 540, BETWEEN RBL 25.5 TO RBL 45.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR SWAA2012052904421Angle · crackedANGLE CRACKED AT BS 540, RBL 70.85. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR SWAA2012052904414Stiffener · crackedSTIFFENER CRACKED AT BS 727, LBL 6. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR SWAA2012051604053Structure · crackedCHORD CRACKED AT BS 663, LBL 24.8. REPAIRED CHORD IAW EA AND EO.SDR SWAA2012042403344Stiffener · crackedBS 663, RBL 7, WL 164 CENTER TANK REAR SPAR VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER EA & EO.SDR USAA2012041000022Angle · damagedC1 CHECK, BASED ON REPORTS OF FUEL LEAKS, RIB1/FR 42 OUTER ANGLE REPAIRED IAW EA 103588.SDR USAA2012041000019Angle · damagedC1 CHECK, BASED ON REPORTS OF FUEL LEAKS, RIB 1/FR 42 OUTER ANGLE REPLACED IAW EA 103588.SDR TRBA20120404004Skin · corrodedDURING MX INSPECTION, FOUND GALVANIC SURFACE CORROSION AT PANEL 1, NR 521DT. THE ACFT WAS REMOVED FROM SERVICE. REMOVED CORROSION, BLENDED AND THREATED. THE ACFT WAS RETURNED TO SERVICE.SDR SWAA2012042403343Stiffener · crackedBS 663.75, RBL 6.15, WL 169 CENTER TANK REAR SPAR VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER ACO.SDR SWAA2012021501472Stiffener · crackedWING CENTER SECTION REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER PER EA.SDR SWAA2012021001340Fitting · crackedCENTER WING BOX SHEAR FITTING CRACKED AT BS 545.5, RBL 6.14. REPAIRED FITTING PER EA.SDR SWAA2012021301388Channel · crackedCHANNEL CRACKED AT BS 540, BTW RBL 24.5 AND RBL 45.5. REPLACED CHANNEL IAW SRM AND DWG.SDR SWAA2012030501902Structure · crackedLT CENTER SECTION INNER CHORD CRACKED AT BS 616, STR 17R. REPAIRED CHORD IAW EA AND EO.SDR SWAA2012030501901Structure · crackedLT CENTER SECTION INNER CHORD CRACKED AT BS 616, STR 17L. REPAIRED CHORD IAW EA AND EO.SDR SWAA120597Stiffener · crackedDURING SCHEDULED 24Y CHECK, FOUND FUEL TANK EXTERNAL STIFFENER CRACKED AT BS 548, LBL 57. REMOVED AND REPLACED STIFFENER PER SRM.SDR SWAA120440Fitting · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+7, LBL 40.87. REMOVED AND REPLACED SHEAR FITTING PER ACO.SDR QXEA2012010301460Paint · damagedCENTER WING FUEL PANEL 521AT HAS BUBBLING PAINT AROUND VARIOUS BOLT HOLES, POSSIBLE CORROSION. REMOVED CORROSION ON PANEL IAW RD 8/4-57-425. MATERIAL LOSS FOUND IN LIMITS IAW RD 8/4-57-432. CONFIRMED CRACK FREE AREA REF NTM 51-00-06-910-801. ALODINED, PRIMSDR SWAA20111213346Fitting · crackedDURING SCHEDULED 16Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 57. R&R FITTING PER SRM.SDR SWAA118345Fitting · crackedDURING SCHEDULED 16Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 57. R&R FITTING PER SRM.SDR SWAA118344Fitting · crackedDURING SCHEDULED 16Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 33. R&R FITTING PER SRM.SDR SWAA20111213310Stiffener · crackedDURING SCHEDULED 24Y CHECK, FOUND STIFFENER CRACKED BETWEEN WBL 104 TO WBL 125. REPAIRED STIFFENER PER SRM.SDR REXA201100931Structure · chafedRIGHT OF CENTER WING LOWER PLANK JUST I/B OF RBL 45.0 AFT EDGE IS CHAFED .5 WIDE X .5 WIDE APPROX .025 DEEP. DAMAGE WAS IN ONE AS DEFINED IN REO 601R-57-21-880. REPAIRED IAW BOMBARDIER REO 601R-57-21-880.SDR REXA201100930Structure · chafedLEFT OF CENTER WING LOWER PLANK JUST I/B OF LBL 45.0 AFT EDGE IS CHAFED. 1" LONG X .5" WIDE X APPROX .025" DEEP. DAMAGE WAS IN ONE AS DEFINED IN REO 601R-57-21-880. REPAIRED IAW BOMBARDIER REO 601R-57-21-880.SDR FXGA20111210003Skin · crackedDURING HEAVY MX DISCOVERED CRACKED CENTER WING SKIN, DOUBLER, AND REINFORCING RING AT RT WING STATION 17 FWD OF WING STRINGER 20 AND FOUND SAME DOUBLER AND REINFORCING RING CRACKED AT LT WING STA 17 FORWARD OF STRINGER 20.SDR QXEA2011121601359Attach Angle · chafedUPPER CENTER WING FRONT SPAR UPPER ATTACH ANGLE THAT SUPPORTS WING TO FUSELAGE PANELS 261CT, 261FT, 261HT AND 261LT IS CHAFED. BLENDED OUT CHAFE ON UPPER CENTER WING FRONT SPAR ATTACH ANGLES IAW SRM 57-10-05. CONFIRMED AREA CRACK FREE MIN REMAINING THICKNESSSDR SWAA118678Web · crackedDURING SCHEDULED 10Y CHECK, FOUND CRACKS IN CENTER WING SECTION, STA 663, RBL 33 TO RBL 45, 9 INCHES BELOW CABIN CENTER FLOOR LINE. REMOVED AND REPLACE DAMAGED WEB POT PER EA.SDR USAA2012010500010Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON TOP AFT PANEL UPPER SURFACE AT CENTER WING BOX AT FR42, Y1292. REPAIRED TOP AFT PANEL UPPER SURFACE AT CENTER WING BOX AT FR42, Y1292 IAW EA 133908.SDR USAA2012010500009Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON TOP AFT PANEL UPPER SURFACE AT CENTER WING BOX AT FR41+6 INCHES, Y1550. REPAIRED TOP AFT PANEL UPPER SURFACE AT CENTER WING BOX AT FR41+6 INCHES, Y1550 IAW EA 133908.SDR SWAA117030Stiffener · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, RBL 41. REMOVED AND REPLACED STIFFENER PER ACO.SDR SWAA117029Stiffener · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, RBL 33. REMOVED AND REPLACED STIFFENER PER ACO.SDR SWAA117028Stiffener · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, LBL 42. REMOVED AND REPLACED STIFFENER PER ACO.SDR SWAA117027Stiffener · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, LBL 32. REMOVED AND REPLACED STIFFENER PER ACO.SDR SWAA117026Stiffener · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER FUEL TANK UPPER FWD STIFFENER CRACKED AT BS 547.5, LBL 7. REMOVED AND REPLACED STIFFENER PER ACO.SDR SWAA117012Doubler · crackedDURING SCHEDULED 12Y CHECK, FOUND FORWARD SECTION OF WING BOX DOUBLER CRACKED AT BS 663. REPAIRED DOUBLER IAW EA AND DWG.SDR FDEA201109264133Structure · crackedDURING NDT CRACK INDICATION, FOUND IN CENTER WING BOX. REPAIR CARRIED OUT IAW EA 6-5710-154305SDR LR7A2011092100234Tee Fitting · crackedDURING SCHEDULED B-1 CHECK IAW JOB CARD HB5701 FOUND VERTICAL ANGLE CRACKED IN RADIUS AT FS517, CWS174L, WL280. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583 51-70, NR 2-5-39.SDR FDEA201108253470Spar · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LT CENTER TANK REAR SPAR AND FOUND DAMAGED AT APPROX 6 O`CLOCK. REPAIRED IAW EO 6-5710-7-3322B1 PT 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV112.SDR FDEA201108123241Structure · crackedONE CRACK INDICATION EXCEEDS 25 PERCENT FSH WAS FOUND AT NR 63 FASTENER HOLE OF RT CENTER WING, REF NTM PART 6 51-10-01 PROCEDURE A RECORD SHEET FIG 611 AND NTM PART 6-57-10-12. CRACK REAMED TO THE NEXT NOMINAL DIAMETER 0.561" IAW EO 6-5710-7-3322 PART 1. NDSDR FDEA201108123240Structure · crackedONE CRACK INDICATION EXCEEDS 25 PERCENT FSH WAS FOUND AT NR 30 FASTENER HOLE OF RT CENTER WING, REF NTM PART6 51-10-01, PROCEDURE A, RECORD SHEET FIG 612 AND NTM PART6 57-10-12. CRACK REAMED TO THE NEXT NOMINAL DIAMETER SIZE 0.561" IAW EO 6-5710-7-3322 PART 1SDR FDEA201107262953Spar · damagedDURING ACCOMPLISHMENT OF EO6-5710-7-3305, D2, PT3 WORK STEP 6, FOUND HOLE 'A' EXISTING FASTENER HOLE DIAMETER 0.625" IS BIGGER THAN NEW FASTENER SIZE 0.562" AT CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE LT SIDE. INSTALLED NEW FASSDR MTNA0725110001Housing · corrodedFOUND PITTING CORROSION ON THE HOUSINGS. REPAIRED USING ATR STRUCTURAL REPAIR APPROVAL SHEET NUMBER DO/TS-4415/11.SDR SWAA114755Fitting · crackedDURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, LBL 54.60. REMOVED AND REPLACED FITTING IAW SRM.
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