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 FDEA201704241285Skin · corrodedAFT FUSELAGE STA 1986 L46L SKIN CORROSION. REPAIRED DAMAGED SKIN PER SRM 53-20-00, VOL I, FIG 6 SHEET 13.SDR AALA20170425004Skin · crackedAIRCRAFT WAS IN BASE MAINTENANCE. LEFT AFT NOSE LANDING GEAR DOOR HINGE CUTOUT CRACK AT FUSELAGE STATION 94.55. REPAIRED IAW SRM 53-05-00-001 PARAGRAPH 162 FIGURE 158.SDR DALA2017042503354Doubler · wornWEAR INTERNAL DOUBLER JUS ON UPPER CORNERS AT AFT LAVATORY SERVICE ACCESS TRAY. WEAR INTERNAL DOUBLER WAS REPAIRED PER DWG 5911423 REV CD AND ER/A 397822-14MA REV B.SDR DALA2017042503353Skin · crackedSTA 1022 BELOW L7R FUSELAGE SKIN CRACKED AT FORMER UPPER FASTENER. HFEC VERIFIED IAW BOEING NDT SPM ETHF 06-10-01.001 PROCEDURE 1, TAG #6742. (2 EA CRACKS WERE IDENTIFIED AND REPAIRED USING SAME DOUBLERS) TRIMMED / CUT OUT BOTH FASTENER HOLE CRACKS-ONE @ LAP SDR DALA2017042503351Skin · corrodedLOWER EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND FASTENER STA 851 LONGERON 30. BLENDED CORROSION FROM SKIN IAW B717 SRM 51-01-01-14-1 AT L28L STA 861-865 .150" ORIG THICK NESS .021" REMOVED .129" RMAINING AT STA 877-883 L27L ORIG THIC .130", .005" REMOVED .12SDR ASOA201704243111Doubler · corrodedRIGHT CENTER FUSELAGE CORROSION AROUND POTABLE WATER HEATED NIPPLE. DOUBLER BLENDED IAW SRM 51-10-05SDR JJBA20170423029Skin · dentedDENT LOCATED ON LT FUSELAGE SKIN BETWEEN BS 270.5 - 291, STRINGERS 9 - 10P. REPAIRED IAW RD 8-53-15173.SDR R61A20170423323Skin · dentedWHILE IN HEAVY CHECK, DENT IN NEWLY IDENTIFIED RVSM AREA ACCORDING TO 170EO-11-10-0023 AT FR04 STR 18R-20R. MAJOR REPAIR, REMOVED AND REPLACED RT SKIN ON FWD FUSELAGE IN RVSM AREA AND RESTORED SURFACE PROTECTION REF SRM 51-40-02, 51-43-04,51-23-04, 51-41-02, 5SDR R61A20170423320Skin · dentedWHILE IN HEAVY CHECK, MAJOR DENT FWD FUSELAGE FWD OF FR03, OTBD OF STG 28R AND PREVIOUS REPAIR DOUBLER COMPLETE: REMOVED DAMAGED DOUBLER ON FWD FUSELAGE
LOWER SKIN AROUND FR 03 BETWEEN STGR 26R/-26L, FABRICATED AND INSTALLED NEW DOUBLER WITH EXISTING FILLERS SDR SWAA2017051613707Skin · damagedSKIN DAMAGED AT BS 1073.5, STRINGER 16R. REPAIRED THE SKIN IAW EA.SDR SWAA2017051713706Skin · tornSKIN TORN AT BS 1074, STRINGER 17R. REPAIRED THE SKIN IAW SRM & EA.SDR R61A201705010336Skin · dentedLT FWD FUSELAGE LOWER SKIN HAS DENT BETWEEN FR10 AND FR11 STG 17L AND 18L. MAJOR REPAIR FABRICATED INNER/OUTER DOUBLERS AND FILLER MATERIAL. LOCATED, COUNTERSUNK, SURFACE PREPPED AND PRIMED MATERIALS, SEALED AND INSTALLED REF ETD2017-17-035886 REV A. AIRCRAFTSDR DALA2017042303311Finger Doubler · crackedCRACKED FINGER DOUBLER BS 256 - 275 BETWEEN LONGERONS 24 - 25L IN THE FWD CARGO BAY. THE FINGER DOUBLER WAS REPLACED IAW ER/A 273415-14, REV B, AND 51-30-2.SDR EE4Y2017042803351Skin · dentedDURING A MAINTENANCE INSPECTION, FOUND THE FUSELAGE SKIN DENTED AT BS 498 + 2, BETWEEN STRINGERS 23 AND 24R. THE SKIN WAS REPAIRED IAW EO4405-2.SDR EE4Y2017042803350Skin · dentedDURING A MAINTENANCE INSPECTION, FOUND BS 357, STRINGER 17R SKIN DENTED. THE SKIN WAS REPAIRED IAW S/R 3-3811555219SDR EE4Y2017042803349Skin · canningDURING A MAINTENANCE INSPECTION, FOUND SECTION 46 SKIN, BETWEEN BS 964 AND 979 AND STRINGERS 21 AND 24L OIL CANNED. THE SKIN WAS REPAIRED IAW SRM.SDR EE4Y2017042803348Skin · dentedDURING A MAINTENANCE INSPECTION, FOUND THE FUSELAGE SKIN DENTED AND SCRIBES BETWEEN BS 845 AND 907, STRINGERS 19 AND 22R. THE SKIN WAS REPAIRED IAW EO4502.SDR EE4Y2017042803346Skin · dentedDURING A MAINTENANCE INSPECTION, FOUND THE SKIN BS 360+6, BETWEEN STRINGERS 25 - 26R DENTED. THE SKIN WAS REPAIRED IAW EO4405-1.SDR EE4Y2017042803345Skin · damagedDURING A MAINTENANCE INSPECTION, FOUND AT THE LOWER FUSELAGE, BS 360 - 500C, STRINGERS 17 - 26L, SKIN WITH CREASES AT FRAME AREAS. THE SKIN SECTION WAS REPAIRED IAW EO4388.SDR EE4Y2017042703338Skin · canningDURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND THE FUSELAGE SKIN WITH OIL CAN BETWEEN STA 500B AND STA 500B+10" AND BETWEEN STR 22L AND STR 23L. THE AFFECTED SKIN SECTION IS REPAIRED UNDER EO4502 INSTRUCTIONS AND APPROVED BY 8110-3.SDR EE4Y2017042703337Skin · canningDURING THE MAINTENANCE INSPECTION PROCESS IT WAS FOUND THE FUSELAGE SKIN WITH OIL CAN BETWEEN STA 480 AND STA 490 AND BETWEEN STR 22L AND STR 23L. THE AFFECTED SKIN SECTION IS REPAIRED UNDER EO4502 INSTRUCTIONS AND APPROVED BY 8110-3.SDR ASOA201704215049Skin Panel · damagedDURING C CHECK SKIN DAMAGE AT FS 1051 AND STR 18R REQUIRED A PATCH REPAIR. SKIN PANEL REPAIRED IAW EC/TC REO 670-53-61-1359.SDR DALA2017042403373Skin · dentedFUSELAGE SKIN DENTED NEAR THE ATG ANTENNA DOUBLER BS 1340 TO 1360 STRINGER 29L.SDR ASOA201704211477Skin Panel · damagedPATCH REPAIR REQUIRED DUE TO SKIN DAMAGE. COMPLIED WITH EC/TC REO 670-53-61-1359 FS 1051 STRINGER 18R.SDR IPXA2017050916905Skin · corrodedINSPECTION TYPE: 3C, AFT EXTERIOR SKIN LT SIDE AT BS 2020 - 2025 HAS CORROSION. REPAIRED THE SKIN IAW EA 011-5330-01-A6785, REV I/R, AND EO MD11-5330-64172-A.SDR FDEA201704201244Skin · dentedFUSELAGE SKIN HAS THREE PROTUDING DENTS IN EXTERNAL SKIN LOWER FUSELAGE AT BS 520 AND TWO INCHES INBD OF STRINGER 26L. SKIN REPAIRED IAW EA F-5330-T0332752 P1.SDR CALA2017042101073Skin · damagedTHE FUSELAGE SKIN DAMAGED LT SIDE FWD OF THE L2 DOOR, EXTENDING FROM BS 755 TO 888, BETWEEN STRINGERS 18 AND 19L. REPAIRED IAW ECRA 5300-02417, REV A,SDR FOTR20170419130Skin Panel · crazedPOSSIBLE CRACK ON SKIN STA 727D BTWN 23L-24L.SDR FOTR20170419125Skin · crackedPOSSIBLE CRACK ON SKIN STA 727D BTWN 23L-24L.SDR SWAA2017050813603Skin · crackedFUSELAGE SKIN PANEL CRACKED BETWEEN BS 1016 TO BS 1156, BETWEEN LBL 11 TO RBL 11. R&R SKIN IAW SRM.SDR CALA2017042101072Skin · gougedLEFT FUSELAGE SKIN BS 1580 ABOVE STRINGER 15L HAS TWO GOUGES AND ALSO DENTED. CUT AND REMOVED DAMAGED AREA, AND REPAIRED IAW SRM 53-00-01, REPAIR 3, FIG 201.SDR CALA2017042101070Skin · crackedBS 540, RT SKIN HAD A CRACK INDICATION BETWEEN STRINGER 22 AND 23R. REPAIRED THE SKIN IAW EA 5310-05878, OPS 5, REV D.SDR ASOA201704193092Skin · corrodedON CARGO LOWER SKIN, AFT LOWER SKIN, AFT RADIO ALTIMETER 2 RETAINER CORRODED AND FWD RADIO ALTIMETER 2 R/H FWD DOME NUT BROKEN. FR 65 ANTENNA BASE CLEANED UP AND ANTENNA INSTALLED WITH NEW RETAINER. HFEC PERFORMED ON FR 65 AND 68 AFTER BLENDING, AS PER ETD ANDSDR ASOA201704193090Skin · crackedFUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 21. SKIN REPAIRED WITH DOUBLER AS PER SRM 53-31-01. PARA II, FIG 219 SHEET 1.SDR ASOA201704193089Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT FRAME 75, NEAR STRINGER 2R. THE SKIN WAS REPAIRED IAW SRM 53-31-01, PARA II, FIG 219, SHEET 1.SDR IPXA2017050516779Skin · damagedINSPECTION TYPE: 3C, BS 1825, LONGERON 48L, FUSELAGE SKIN HAS MULTIPLE DENTS AND IS CREASED. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 1, FIG 201, CLASS 1. MAJOR.SDR SWAA2017042513317Skin · corrodedEXTERNAL SKIN FORWARD OF BUTT SPLICE CORRODED AT BS 1016, BETWEEN STRINGERS 23R TO 23L. REPAIRED THE SKIN IAW EA.SDR CALA2017042101060Doubler · damagedEXTERNAL SKIN DOUBLER DAMAGED BS 608 ABOVE 17L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-00-01, REPAIR 3, FIG 201, REPAIR STEPS 1-5, REPAIR 3.SDR EE4Y2017042003249Skin Panel · dentedUPPER FUSELAGE SKIN WITH SEVERAL DENTS BETWEEN X2743.5 AND FR11 AND BETWEEN STR 15L AND STR 17L. THE CORRECTIVE ACTION WAS HANDLE UNDER THE OEM DISPOSITION ETD2017-190-010281.SDR AALA20170418005Doubler · crackedAIRCRAFT WAS IN BASE MAINTENANCE. NOSE LANDING GEAR AFT RIGHT DOOR HINGE CUTOUT HAS A SMALL CRACK. REPAIRED IAW SRM 53-05-00, EA 269216, DRAWING 5913421 AND SG09530030.SDR AALA201704199006Skin · crackedCRACK INDICATION ON LEFT SIDE FUSELAGE SKIN SIDE SHELL, LOWER AFT FASTENER HOLE AT FRAME 35 AND STRINGER 30L. REPAIRED THE SKIN IAW EA 268396 AND DRAWING R53370269.SDR AALA201704199005Skin · crackedCRACK INDICATION ON RIGHT FUSELAGE SKIN PANEL SHELL LOWER AFT FASTENER HOLE AT FRAME 35, STRINGER 30R. REPAIRED THE SKIN IAW EA 268395 AND DRAWING R53370269.SDR DALA2017042003264Skin · corrodedCORROSION ON FUSELAGE SKIN AT FWD INBD CORNER OF AFT LAV SERVICE PAN, TEMP REPAIR COMPLIED WITH PRI 557343-14 REV 0, PRI 557343-14 REV 1, PRI 557343-14 REV 2 AND ERA 557343-14 REV 0. REV NR 184SDR DALA2017041903230Skin · corrodedCORROSION ON FUSELAGE SKIN STA 827 BETWEEN LONGERON 27R TO 28R. REPAIRED IAW SRM 53-30-01.SDR DALA2017041903181Skin · damagedSKIN WRINKLED BETWEEN BS 813 AND 899 LT SIDE ABOVE WING AND BELOW WINDOW.SDR DALA2017041903180Skin · damagedSKIN DAMAGED BS 813 - 898. LONGERON 15 - 18L. REMOVED, FABRICATED, AND REPLACED THE SKIN PANEL IAW ER/A 557708-14, AND SRM 51-41-02 / 51-41-05.SDR DALA2022012500500None · noneSHIP 3311 AFT WASTE EXHAUST VENT CUTOUT FOUND CORROSION. CORRECTIVE ACTION: THE CORROSION REMARK AT AFT WASTE EXHAUST VENT WT OUT FR76-77 STGR 41L-42L FUSELAGE SKIN WAS REMOVED BY BLENDING OUT AS PER A330 SRM 51-73-00,AND SRM 53-41-11. THE FASTENERS AROUND REWSDR SIMA20170417006Skin · crackedEXTERNAL FUSELAGE SKIN POSSIBLE CRACK AROUND FASTENER FR 78 STR 3L-4L. PREPPED, FABRICATED, DRILLED FILLERS (3 TOTAL) AND INSTALLED EXTERNAL FUSELAGE SKIN REPAIR AT FR 78 STRINGER 4L AREA IAW ERS-EM-53MR-2723.SDR SIMA20170417008Skin · crackedRT AFT FUSELAGE SKIN HAS CRACK AT CUT OUT FR 77 BELOW STR 7. PERFORMED PERMANENT REPAIR OF SKIN CRACK AT FR77 BELOW STR 7R IAW ERS-EM-53MR-2724.SDR SIMA20170417003Skin · crackedCRACK AROUND RIVET ON FRAME 75 AT STRINGER 2L. PERFORMED PERMANENT REPAIR OF CRACK AROUND RIVET ON FRAME 75 AT STRINGER 2L IAW SRM 53-31-01 RE FIG 219, SHEET 2.
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