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 DALA2016061404659Skin · damagedSEVERAL LIGHTNING STRIKES ON WINDOW BELTS FROM BS 598 TO 655 LONGERONS 11 - 14R. REPAIRED IAW ER/A 546537-14, REV ORIGINAL AND SRM 53-05, FIG 111.SDR CALA2016061595449Skin · bulgedAFT PHF ANTENNA BS1730 AND STR 49L LT SIDE BULGING METAL NEAR RIVETS. LOCATION OF REPAIR IS BS1730 AND STR 49L. CUT DAMAGED SKIN OUT, MFG DRILLED AND PRIMED REPAIR PIECES IAW SRM 53-00-01, REPAIR 1.SDR DALA2016061404596Skin · damagedENLONGATED HOLES ON FUSELAGE SKIN AND LONGERON 26 LT FROM BS 1004 TO 1045. SKIN REPAIRED IAW ETI-17-16-060, REV. 2 AND ER/A 546557-14, REV. ORIGINAL.SDR DALA2016061404595Skin · crackedCRACK ON SKIN BS 1133 BETWEEN LONGERON 2-3R AT OUTER FUSELAGE SKIN AREA. SKIN WAS REPAIRED IAW ETI-17-16-035, ER/A 546487-14AD, REV. ORIGINAL. ASSOCIATED ER/A 00-546487 ADDED FOR AC 9520.SDR SWAA2016061652920Skin · crackedSKIN CRACKED AT BS 480+5, STR 1R. REPAIRED SKIN IAW SRM.SDR SWAA2016061552869Skin · crackedFUSELAGE SKIN CRACKED AT STA 480+5, STR 1. REPAIRED SKIN IAW SRM.SDR ASAA2016061117357Skin · crackedFUSELAGE SKIN IS CRACKED AT CHEM-MILL BELOW STRINGER 23R, BS 727E +2. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01 REP 31.SDR ASAA2016061117356Skin · crackedFUSELAGE SKIN IS CRACKED AT CHEM-MILL BELOW STRINGER 22L, BS 727E+3. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01-2R-31 DET VII.SDR ASAA2016061117177Skin · crackedFUSELAGE SKIN IS CRACKED AT CHEM-MILL, BELOW STR 23R, STA 727E +2". REQUIRES INTERNAL NDT IAW FIG 4 OF GENERATING TC AFTER ACCESSED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01, REP 31. THIS REPAIR IS A CAT B REPAIR WITH INSPECTION THRESHOLD OF SDR ASAA2016061117168Skin · crackedFUSELAGE SKIN IS CRACKED AT CHEM-MILL BELOW STR 22L, STA 727E+3". REQUIRES INTERNAL NDT IAW FIGURE 4 OF GENERATING TASK CARD AFTER ACESSED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-2R-31 DET VII THIS IS A CATEGORY B REPAIR INITIAL THRESHOLD IS SDR ASAA2016061117071Skin · dentedDURING WALK AROUND, FOUND DENT AT FUSELAGE STA 382, STR 16 LT RVSM AREA. ACFT GROUNDED. REPAIRED SKIN AND STR IAW SRM 53-00-03 AND 53-00-01.SDR SWAA2016070653555Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, BETWEEN STRINGERS 22 - 23R. REPAIRED SKIN IAW EA.SDR SWAA2016062052999Skin · crackedL2 DOOR FUSELAGE SKIN CRACKED AT BS 950.5, STR 11L, UPPER HINGE CUT OUT. REPAIRED SKIN IAW SRM.SDR SWAA2016062052998Skin · crackedR2 DOOR FUSELAGE SKIN CRACKED AT BS 950.5, STR 11R, UPPER HINGE CUT OUT. REPAIRED SKIN IAW SRM.SDR SWAA2016062052997Skin · crackedFUSELAGE SKIN CRACKED BETWEEN BS 372 TO BS 373.25, STR 15R. REPAIRED SKIN IAW ER AND EA.SDR SWAA2016061752964Skin · crackedSKIN CRACKED AT BS 312, BETWEEN STR 20R TO STR 21R. REPAIRED SKIN IAW SRM.SDR DALA2016061404594Skin · crackedRIGHT FUSELAGE BS 1095 SKIN CRACKED FROM FASTENER HOLE APPROXIMATELY .75" JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT. REPAIRED RT FUSELAGE BS 1095 CRACKED SKIN FROM FASTENER HOLE JUST ABOVE LONGERON 14-R IAW ER/A 545684-14, REV. OR. ASSOCIATED ER/A 00SDR DALA2016061204558Skin · damagedNICKS ON FUSELAGE SKIN L1 HOOK CUTOUT PREVIOUS REPAIR. NICKS WERE REPAIRED IAW ETI-88-16-223 AND ER/A 546555-14 REV ORIGINAL.SDR FDEA201606101939Skin · damagedINCOMING SKIN BLEND OUTS AT FASTENER LOCATIONS BETWEEN BS 350-BS 365, 23L. EVALUATED BLEND OUT AREAS BS 350-BS 365, STR 23L AREA FOUND TO BE OUT OF LIMITS, IAW-SRM-53-00-01-1A FIG 101 DET II, REPAIRED SKIN DAMAGED AREA IAW-SRM-53-00-01-2R, FIG 201, R15, THIS ISDR SWAA2016080554588Bear Strap · crackedFORWARD ENTRY DOOR LOWER AFT CORNER BEAR STRAP CRACKED AT BS 339.5 TO BS 347.5, STR 17L. REPAIRED BEAR STRAP IAW SRM.SDR SWAA2016063053371Skin · crackedL1 DOOR CUTOUT LOWER AFT CORNER FUSELAGE SKIN CRACKED AT BS 342.5, STR 17L. REPAIRED SKIN IAW SRM.SDR SWAA2016062052996Skin · crackedSKIN CRACKED AT BS 340, STR 1. REPAIRED SKIN IAW ER AND EA.SDR SWAA2016062052986Skin · crackedFUSELAGE CROWN SKIN CRACKED AT BS 340, STR 1. REPAIRED SKIN IAW ER & EA.SDR DALA2016061004585Skin · corrodedEXTERIOR SKIN BETWEEN BS 1720-1787.45 STR 25RT & 25LT HAS PITTING CORROSION. R & R EXTERIOR SKIN FROM BS 1720-BS 1787.45, STR IAW SRM & DWG.SDR FDEA201606091896Skin · damagedFUSELAGE RT SIDE, THERE IS A LIGHTNING STRIKE AT BS 680 - BS 700 BETWEEN STR 24- STR 25. LIGHTNING STRIKE REMOVED,
FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 101, DETAIL II, REV 118. REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 118. THIS IS ASDR FDEA201606081879Skin · crackedAGING AIRCRAFT, EXISTING SKIN REPAIR DOUBLER FOUND AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, LONGERON L39R-L41R EXISTING REPAIR AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, L39R-L41R EVALUATED AND FOUND CRACK. REPAIR CARRIED OUT AT FWD CARGO DOOR CUTOUT SDR DALA2016060904606Skin · damagedLIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 206 BETWEEN LONGERON 1R AND 2R. REPAIRED IAW SRM 53-31-02, 51-30-03 AND 51-10-05.SDR SWAA2016061352810Skin · deformedL1 DOOR FUSELAGE SKIN LOWER HINGE CUTOUT DEFORMED. R & R SKIN IAW DWG AND SRM.SDR DALA2016060904479Skin · corrodedCORROSION ON CENTER WING UPPER SKIN, JUST FWD OF SLANT PANEL AND BS X= 40.5, CARD 3, ZONE 140). FUEL LINE WAS REMOVED AND INSTALLED IAW AMM 20-10-03 917-81 FASTENERS WERE REMOVED AND INSTALLED IAW SRM 51-41-05 CORROSION WAS REMOVED IAW SRM 57-10-01 AND (UT) WASDR SWAA2016063053363Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN BS 525 TO BS 540, BETWEEN LBL 9 TO RBL 9. REPAIRED SKIN IAW ER AND EA.SDR DALA2016060804580Skin · damagedFWD CARGO BAY, LIGHTNING STRIKE OUTER SKIN, CAN NOT INSTALL SOLID FASTENER DUE TO THE VICINITY OF HOLE UNDER STR 27R. REPAIRED FUSELAGE SKIN AT BS 656, STR 27 RT IAW PRI 544317-14, REV 0.SDR REXA2016060701008Skin · dented2 DENTS ON LOWER FUSE SKIN AT STA 670 BETWEEN STR 27 AND STR 26 RT. REPAIRED DENTS IAW EA CRJ253-04381, REV A.SDR SWAA2016063053362Bear Strap · crackedL1 DOOR BEAR STRAP UPPER HINGE CUTOUT CRACKED AT BS 303.90, STR 10L. REPAIRED CUTOUT IAW ER AND EA.SDR SWAA2016063053361Bear Strap · crackedL1 DOOR BEAR STRAP LOWER HINGE CUTOUT CRACKED AT BS 305, STR 13L. REPAIRED CUTOUT IAW ER AND EA.SDR SWAA2016061352786Skin · crackedFUSELAGE SKIN CRACKED AT BS 360 +14, STR 15L. REPAIRED SKIN IAW EA.SDR GTIA2016060601473Skin · corrodedDURING INSPECTION FOUND CORROSION LT WING, TOP SKIN PANEL 2 T/E OVERHANG AT RIB 14. - 60 MML X 20 MMW X 4.67D.SDR GTIA2016060601470Skin · dentedDURING INSPECTION FOUND RT NOSE FUSELAGE DENTED BETWEEN FRAME 4 AND 5. - 0.95 MML X 100 MMW X 3.2 MMD-REF RAF 818768-02.SDR FDEA201606061855Skin · damagedFUSELAGE RIGHT SIDE THERE IS A LIGHTNING STRIKE AT BS 500 - 520 BETWEEN STRINGER 25 - 26 WITH STICKER 633. LIGHTNING STRIKE MARK REMOVED AREA FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX, AD REPAIR CARRIED OUSDR FDEA201606061854Skin · damagedFUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 480 - 500, BETWEEN STRINGER 25 - 26 WITH STICKER 630. FUSELAGE EXTERIOR SKIN AT BS 480-500, STR 25R-26R LIGHTING STRIKE MARK. REMOVED AREA, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTSDR FDEA201606061853Skin · damagedFUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 460 - 480, BETWEEN STRINGER 25 - 26 WITH STICKER 613. REMOVED AREA, FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX AND REPAIR CARRIED OUT IAW SRM 53-00-01, FISDR DALA2016060604490Skin · crackedCRACK ON FUSELAGE SKIN , BS 1542 CANT BETWEEN LONGERONS 3 TO 5L. REPAIRED IAW SRM 53-00-01.SDR CALA2016060600348Skin · dentedDENT BETWEEN BS 1016 & 1040 IS ON STRINGER 15L & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 PG 105, STP 3 B I. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR DOUBLER & FILLERS IAW SRM 53-80-01 REPAIR 2.SDR WVER201606050006Skin · chafedDURING HEAVY CHECK INSPECTION, DISCOVERED CHAFE OF FUSELAGE SKIN BETWEEN FS 897 AND 927, BETWEEN STRINGERS 26L AND 26R. THREE CHAFES WERE DISCOVERED ON TOP OF PREVIOUS REPAIRS, VARYING IN DEPTH FROM .025"-.052.SDR SWAA2016071353766Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SKIN IAW ER AND EA.SDR SWAA2016061552880Skin · crackedSKIN CRACKED AT BS 538, STR 22L, 6 O'CLOCK POSITION. REPAIRED SKIN.SDR SIMA20160603003Skin · crackedDURING MBV INSPECTION, A FOUND A CRACK AT A FASTENER HOLE ON FRAME 75 ON STRINGER 2R. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR TO CRACK AT FASTENER HOLE ON FRAME 75 ON STRSDR AALA20160603015Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN ABOVE RT NLG DOOR AFT HINGE CUT OUT IS CRACKED. REPAIRED SKIN IAW SRM 53-05-00 FIGURE 158.SDR AALA20160603014Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN ABOVE LT NLG DOOR AFT HINGE CUT OUT IS CRACKED. REPAIRED SKIN IAW SRM 53-05-00 FIGURE 158.SDR DALA2016060404381Skin · crackedCRACKED EXTERNAL SKIN AROUND OF HOLD OPEN LOCK HOUSING AT MAIN L1 DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-10-01, REP 4, FIG 201. LENGTH CRACK = 0.270", RII COMPLETED.SDR CALA2016060600346Skin · damagedFOUND DAMAGE ON FUSELAGE AT APPROX BS 240, BETWEEN STRINGER 19L & 20L. REMOVED DAMAGE. PERFORMED SRM 53-00-01 REPAIR 3.
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