JASC 5330
Service difficulty reports · 79,347
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 COEA2015081715919Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE LT UPPER SKIN PANEL, HAS LEVEL 2 CORROSION FWD OF THE FWD CARGO DOOR, ABOVE THE STRINGER 13 SKIN LAP. REPAIR IAW SRAS DTS-485 11 6792 ISSUE D DATED 09 21 15.SDR COEA2015081712919Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE LT LOWER SKIN PANEL HAS LEVEL 2 CORROSION, FWD OF & BELOW THE FWD CARGO DOOR, BELOW STRINGER 13 - 16 SKIN LAP. REPAIR IAW SRAS DT S-485 11 6792 ISSUE D DATED 9/21/15.SDR SWAA2015092844344Skin · crackedAFT RT GALLEY DOOR SKIN CUT OUT CRACKED, LOWER FWD CORNER. REPAIRED SKIN IAW ER & EA.SDR RAIA201508170006Skin · damagedCORROSION AND PIN HOLES IN SKIN AT FR 13-14, STRINGER 16-17R. MAINTENANCE REPAIRED CORROSION BY REPLACING SKIN AND INSTALLING A DOUBLER AND TRIPLER. MAJOR REPAIR.SDR ASAA2015081713119Skin · crackedLOWER FUSELAGE GROUND AIR CONDITIONED SERVICE DOOR LANDING IS DAMAGED. ACFT GROUNDED. UPON FURTHER EVALUATION, FOUND GROUND AIR DOOR LANDING CRACKED. REPAIRED AT GROUND AIR CONDITIONED SERVICE DOOR LANDING IAW SRM 53-30-01-2R-2, REPAIR 2. THIS IS A CAT B REPSDR SWAA2015091443759Skin · crackedSKIN CRACKED AT BS 484, STRINGER 2R. REPAIRED SKIN IAW SRM.SDR COEA2015081701919Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR FUSELAGE SKIN HAS LEVEL 2 CORROSION UNDER T CAS DOUBLER & INTERNALLY AROUND DOME NUTS. REPAIR DOUBLER IAW SRM 533126-300-804-A01.SDR EE4Y2015090100375Skin Panel · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT, BETWEEN STRINGER 28L & 29L & BETWEEN FRAME 85 & 86, FUSELAGE SKIN INNER SURFACE CORRODED. DAMAGE WAS REPORTED & HANDLED UNDER NRI A1D206, 1 - 45. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-077562 REV C & APPROVED UNSDR SWAA2015081942985Post · crackedFIRST OFFICER'S NR 1 WINDOW POST UPPER OTBD CORNER CRACKED IN RADIUS. REPAIRED POST IAW ACO.SDR SWAA2015081942984Post · crackedCAPTAIN'S NR 1 WINDOW POST UPPER OTBD CORNER CRACKED IN RADIUS. REPAIRED POST IAW ACO.SDR R61A201508160627Skin · corrodedDURING HEAVY CHECK, MAINTENANCE REPORTED CORROSION AROUND 5 FASTENER HOLES UNDER THE RT ICE SHIELD ON SKIN PANELS. PERFORMED BLEND OUT REPAIR IAW RD 8/4-53-7042 AND SRM 53-30-31.SDR R61A201508160626Skin · corrodedDURING HEAVY CHECK, MAINTENANCE REPORTED CORROSION AROUND 5 FASTENER HOLES UNDER THE RT ICE SHIELD ON SKIN PANELS. MAINTENANCE PERFORMED BLEND OUT REPAIR TO 5 FASTENER HOLES UNDER THE RT ICE SHIELD SKIN PANELS IAW RD 8/4-53-7042 AND SRM 53-30-31.SDR DALA2015081705128Skin · damagedOUT OF LIMITS, REWORKED AREA ON FUSELAGE SKIN BETWEEN BS Y=394.5 TO Y=401 AND LONGS 23 LT TO 25 LT. FUSELAGE SKIN BETWEEN BS Y=394.5 TO Y=401 AND LONG 23 LT TO 25 LT. CRACK OF 0.375" AT BS Y=394.5 WAS TRIMMED OUT WITHIN 0.750 OF DIAMETER IAW SRM 53-04-2 FIGUSDR DALA2015081505236Skin · puncturedFUSELAGE PUNCTURED 34 INCHES AFT OF L1 DOOR CUTOUT. SKIN REPAIRED IAW ERA 538496-14.SDR SWAA2015082143068Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.SDR SWAA2015082143050Skin · crackedR2 DOOR LOWER HINGE ARM CUT OUT, FWD RADIUS CORNER OF FUSELAGE SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR SWAA2015082042992Skin · crackedSKIN CRACKED BETWEEN BS 420+16.75 - 420+17.25, STRINGER 2R. REPAIRED SKIN IAW EA.SDR DALA2015081905065Skin · crackedCRACKED FUSELAGE SKIN AT BS 1380, BETWEEN LONGERONS 13-14L. REPAIRED IAW SRM 51-30-2, 51-30-5, 53-04, FIG 18, 51-10-3, PAR 14 AND 21.SDR AALA201508199003Skin · damagedFLIGHT 1851 EN-ROUTE, ON APPROACH, RIGHT BEFORE TOUCHDOWN, THE CREW RECEIVED A WIND SHEAR WARNING. PERFORMED A GO-AROUND FOR ANOTHER APPROACH. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT ON THE SECOND APPROACH & TAXIED TO THE GATE NORMALLY. UPON POST FLIGHT SDR SWAA2015081942989Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22R, AFT ROW SECOND FASTENER HOLE. REPAIRED SKIN IAW EA.SDR CALA2015081894224Skin · dentedEXTERNAL FUSELAGE DENTED AT FRAME 29, STRINGER 39L. DENT OUT OF LIMITS, SO DAMAGE CUT OUT & EXTERNAL DOUBLER INSTALLED IAW PER SRM 53-00-11 FIG 239. IAW SRI 53-00-11-2-017-00 PARA 3L FIG 225, REPAIR NEEDS TO BE INSPECTED AT 60,000 CYCLES FROM TIME OF REPAIR SDR SWAA2015081742864Skin · crackedFUSELAGE SKIN CRACKED AT BS 360+15, STRINGER 8L. REPAIRED SKIN IAW EA.SDR SWAA2015081742863Skin · crackedFUSELAGE SKIN CRACKED AT B5, 500C+6, STRINGER 8L. REPAIRED SKIN IAW EA.SDR AALA20150825008Skin · crackedFUSELAGE SKIN WAS FOUND CRACKED AT TWO LOCATIONS, STATION 1437 ABOVE & BELOW LONGERON 3L. PERFORMED DOUBLER & TRIPLER REPAIR IAW EA 253684.SDR ASOA2015081413574Skin · dentedFUSELAGE HAS SEVERAL DENTS AT BS 593 BETWEEN STRINGERS 25-26R AND STRINGERS 24-25R. REO 601R-53-61-5529 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.SDR SWAA2015082042991Skin · crackedSKIN CRACKED AT BS 430 + 8.5, STRINGER 2R. REPAIRED SKIN IAW EA.SDR QMLA2015081415072Skin · crackedFOUND CRACK IN UPPER AFT FUSELAGE SKIN NEAR THE UPPER LT LONGERON AS DESCRIBED, THE SUBJECT OF AD2015-05-04 & ASB 407-11-95, TB 407-12-96. DURING THE COMPLIANCE WITH AMC EO-13-5310-EO-212. CRACK IS APPROX 1.5" LONG, STARTING AT THE UPPER LT LONGERON & TRAVELSDR DALA2015081504982Skin · crackedCRACK ON FUSELAGE SKIN ON BS 1474 ON LONGERON 21 TO 22L. HOLES WERE STOP DRILLED AND REPAIR DOUBLER WAS FABRICATED, TREATED AND PAINTED AND INSTALLED IAW SRM 53-01, FIG 2, 51-10-3, P 14 AND 21 AND 51-30-2. HFEC WAS PERFORMED IAW NDT SPM 06-10-01.001.SDR KCSA201508141041Bear Strap · crackedL3 DOOR UPPER AFT CORNER BEARSTRAP HAS A CRACK.SDR AALA20150814004Skin · crackedAIRCRAFT HAS AN AREA OF DAMAGE TO THE FUSELAGE SKIN AT THE APU ACCESS DOOR FWD HINGE, BETWEEN STATION 1093 & 1103. TEMPORARY REPAIR PREVIOUSLY ACCOMPLISHED ON FMR 3HF53E94F. PERMANENT DOUBLER REPAIR ACCOMPLISHED IAW SRM 53-80-01-2R.SDR ASAA2015081312999Skin · crackedL2 DOOR CUTOUT FWD LWR CORNER FUSE SKIN IS CRACKED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-2R-32, DETAIL IV THIS IS A CATEGORY B REPAIR INITIAL THRESHOLD IS SET AT 66,000 CYCLES INTERVALS SET AT 24,000 CYCLES, SRM 53-00-01-212-32, TABLE IX FOSDR SWAA2015091043585Skin · crackedFUSELAGE SKIN CRACKED AT BS 803, STRINGER 2R. REPAIRED SKIN IAW SRM.SDR SWAA2015090243442Skin · crackedFUSELAGE SKIN CRACKED AT BS 804, STRINGER 1L. REPAIRED SKIN IAW SRM.SDR EE4Y2015090100376Skin Panel · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT, BETWEEN STRINGER 27R & 28R & BETWEEN FRAME 81 & 83, FUSELAGE SKIN INNER SURFACE CORRODED. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-077564 REV A INSTRUCTIONS & APPROVED UNDER F-200-06G FORM RCE 2009C06-28.SDR EE4Y2015090100373Skin Panel · corrodedAUXILIARY POWER UNIT COMPARTMENT, RT & LT LOWER PANEL SKIN CORRODED. REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D206 3-2. REPAIR HAS BEEN CARRIED OUT UNDER ETD2015-190-075806 REV B INSTRUCTIONS & APPROVED UNDER F-200-6G FORM RCE 2009C06-28.SDR SWAA2015083143326Skin Panel · corrodedCENTER WING SECTION UPPER SKIN PANEL CORRODED. REPAIRED SKIN IAW SRM.SDR SIMA20150813005Skin · damagedLIGHTNING STRIKE AFT OF FRAME 5 JUST ABOVE STRINGER 13R. REPAIRED LIGHTNING STRIKE IAW ERS-EM-53MR-1558.SDR DALA2015081404978Skin · damagedFUSELAGE EXTERIOR, EIGHT DAMAGED FASTENERS AFT AT BS 1193 LONGERON NR 1. REPAIRED IAW ERA 538516-14AD, REV A.SDR AALA20150813012Skin · crackedCRACKS IN FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERONS 3R & 4R. INSTALLED DOUBLER REPAIR IAW SRM 53-04-00.SDR SIMA20150812007Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. R & R FWD FUSELAGE I LT SKIN IAW SRM 51-40-02 & ETN-EM-53-206.SDR SIMA20150812008Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I RT SKIN PANEL. R & R FWD FUSELAGE I RT SKIN IAW SRM 51-40-02 & ETN-EM-53-206.SDR SWAA2015092244176Skin · crackedFORWARD LOWER CORNER OF AFT GALLEY DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.SDR IPXA2015090993294Skin · corrodedINSPECTION TYPE:4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15, XCW 102 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STR 15, XCW 102 IAW EA 011-5730-01-A5933 AND EO MD11-5730-58608-A.SDR IPXA2015090493132Skin · corrodedINSPECTION TYPE: 4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15 XCW -70 TO XCW -94 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STR 15 XCW -70 TO XCW -94 IAW EA 011-5730-01-A5933, REV I /R AND EO MD11-5730-58608-A.SDR IPXA2015090493131Skin · corrodedINSPECTION TYPE:4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15 XCW -18 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STRINGER 15 XCW -18 IAW 011-5730-01-A5933, REV I/R AND EO MD11-5730-58608-A.SDR IPXA2015090493130Skin · corrodedINSPECTION TYPE:4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15 XCW 17 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STRINGER 15 XCW 17 IAW EA 011-5730-01-A5933, REV I/R AND EO MD11-5730-58608-A.SDR RAIA201508120001Skin · damagedBIRD STRIKE DURING FINAL ON RT FRONT NOSE. REPAIRED BIRD STRIKE ON RT FWD FUSELAGE BETWEEN FRAME 2 & FRAME 5, REF EO-EMB145-53-012-R1 AND ETD2015-145-071801, REV B.SDR S9BA201508140010Skin · dentedDENT AT RT FUSELAGE UNDER 11TH CABIN WINDOW. EVALUATED DAMAGE AT FUSELAGE BS 580.0, WATERLINE 100. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.SDR S9BA201508140009Skin · dentedDENT ON SEAM AFT OF 9TH WINDOW RT SIDE. EVALUATED DAMAGE AT FUSELAGE BS 516. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT INSPECTED IAW NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.SDR SWAA2015100544561Skin · crackedSKIN CRACKED BETWEEN BS 259.5+6 - 283, BETWEEN STRINGER 2L - 5L. REPAIRED SKIN IAW SRM.
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