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 IPXA2015060689878Skin · corrodedINSPECTION TYPE: 4C, AFT FUSLEAGE SKIN CORRODED ALONG LOWER EDGE OF PANEL 347AF INTERFACE, BS 2007 - 2033, L30R. REPAIRED THE SKIN PANEL IAW EA 011-5330-01-A5842, REV IR AND EO MD11-5330-57691-A.SDR IPXA2015060589849Skin · corrodedINSPECTION TYPE: 4C, AFT FUSELAGE, RT SIDE SKIN PANEL CORRODED ALONG PANEL 347DF LOWER INTERFACE. REPAIRED RT TAIL SKIN BS 2122-2163 IAW SRM 53-70-01, REPAIR 3, FIG 201.SDR ASAA2015051511869Skin · gougedLT FUSELAGE SKIN AT GROUND, ACFT DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT ACFT DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH INSPECTION THRESHOLD OF 30,000 FLT CYCLES, FLT CYCLES AFTER REPAIR WITH INSPECTION INTESDR ASAA2015051511868Doubler · corrodedLOWER ROTATING BEACON ATTACH DOUBLER CORRODED, INSIDE KEEL BEAM FWD ACCESS AREA. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-1A-1, DETAIL 7. REMOVED DOUBLER FABRICATED NEW DOUBLER AND INSTALLED IAW SRM 51-40-05-0G-0 AND 51-SDR SIMA20150515006Skin · crackedFUSELAGE SKIN CRACKED ON FRAME 75 AT THIRD FASTENER BELOW STRINGER 2R, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORMED PERMANENT REPAIR OF FUSELAGE SKIN CRACK ON FRAME 75 AT THIRD FASTENER IAW ERS-EM-53MR-1308.SDR KO0R201505150046Doubler · corrodedCORROSION AT STATION 1690 TO 1701 STRINGER 42R TO 43R ON INNER SKIN DOUBLER.SDR DALA2016111008456Skin · corrodedUPON REMOVAL OF ANTENNA ON LOWER FUSELAGE AT BS 288, FOUND THE FUSELAGE SKIN UNDER ANTENNA TO BE CORRODED. REMOVED CORROSION, STRINGERS 29 AND 30L. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-1 PAR D CONDITION 2. REPAIRED IAW ER/A 535864-14 REV ORIG. SECTION 1.SDR SWAA2015061640708Post · crackedRIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST 2ND & 3RD LOWER FASTENER HOLE CRACKED. REPAIRED POST IAW ER & EA.SDR SWAA2015061640707Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, BETWEEN STRINGER 22R TO 23R. REPAIRED SKIN IAW ER & EA.SDR SWAA2015061640706Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, BETWEEN STRINGER 22L TO 23L. REPAIRED SKIN IAW ER & EA.SDR R61A201505300324Skin · dentedDURING HEAVY CHECK, MAINTENANCE C/W REPAIR OF MULTIBLE DENTS ON FUSALAGE IAW RD 8/4-53-6820. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR R61A201505300323Skin · dentedDURING HEAVY CHECK, MAINTENANCE C/W REPAIR OF MULTI FUSELAGE SKIN DAMGE IAW R/D 8/4-53-6820. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR SWAA2015052940190Post · crackedNUMBER 3 LT COCKPIT WINDOW FRAME POST CRACKED. REPAIRED WINDOW POST IAW ACO.SDR SWAA2015052840110Post · crackedNUMBER 3 RT FLIGHT DECK WINDOW FRAME, E - F POST FASTENER HOLES, 3RD HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.SDR SWAA2015052840109Post · crackedRIGHT FLIGHT DECK WINDOW FRAME, E - F POST FASTENER HOLES, 2ND HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.SDR SIMA20150514004Skin · chafedAIRLINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB. PERFORMED PERMANENT REPAIR OF AIR LINE CAP RETENTION CABLE CHAFING INNER SKIN INSIDE 414DB IAW ERS-EM-53MR-1307.SDR SIMA20150514005Skin · crackedFUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" IN LENGTH, EASI 8071 USED. FREQ=400KHZ, LPF=100, V-GAIN=76.0, H-GAIN=65.0, 50-500KHZ PROBE. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN JUST AFT OF FRAME 75 ABOVESDR DALA2015051503339Skin · corrodedCORROSION ON LT OUTER SKIN, BS 1117-1193, BETWEEN LONGERONS 18-30L. CORROSION WAS REMOVED IAW SRM 51-10-03 AND 53-30-01.SDR DALA2015051503299Skin · dentedDURING INSPECTION, FOUND A DENT ON UPPER SKIN, FRAME 85+18 LT SIDE ON TAIL. PERFORMED PERMANENT REPAIR ON UPPER SKIN IAW PRI 535335-14, REV O,1 AND 2 AND ER/A 535335-14.SDR FDEA201505141514Skin · damagedSCRIBE LINE DAMAGE AT LAP SEAM 19R, BS 660 - 662. COMPLIED WITH EA F-5330-T0317014 B PT 1. FUSELAGE, PLATE & SKINS, SCRIBE LINE LRTS INSPECTIONS STRINGER 19R, STATION 660.9 - 662.0. MAJOR REPAIR CAT B.SDR FDEA201505141513Skin · damagedSCRIBE LINE DAMAGE AT LAP SEAM 14R, BS 530 - 533. COMPLIED WITH EA F-5330-T031688 A PT 1. FUSELAGE, PLATES & SKINS SECTION 43, SCRIBE LINE LRTS INSPECTIONS, STRINGER 14R, BS 530.87 - BS 533.091, 2.21" LG. MAJOR REPAIR CAT B.SDR DALA2015051503279Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON FUSELAGE SKIN BETWEEN STA Y=200 TO 197 AND BETWEEN LONG 16 TO 18 RT. STR-ENG, CARD 8, ZONE 46. THIS REPAIR WAS PERFORMED BY THE ER/A 473065-14AD.SDR R61A201506160368Skin · dentedDURING HEAVY CHECK, MAINTENANCE REPAIRED DENTS ON LT FUSELAGE AFT OF ICE SHEILD IAW R/D 8/4-53-6890.SDR UHLA201505130405Finger Doubler · corrodedCORROSION AROUND FASTENER HEADS, AFT CARGO AFT FINGER DOUBLER. R & R THE AFT FINGER DOUBLER. MAJOR REPAIR.SDR DALA2015052603462Fastener · misinstalledFOUND SEVEN FASTENERS INCORRECTLY INSTALLED ON PREVIOUS REPAIR AT BS 231.25, BETWEEN S17-18L & REPLACED IAW SRM 51-40-02, FIG 12 AND ER/A 474167-14, REV A.SDR WX0A2015051872595Skin · corrodedUPON REMOVAL OF WING TO BODY FAIRING N/P, DISCOVERED CORROSION ON EXTERNAL SKIN AROUND NUMEROUS N/P LOCATIONS. REPAIRED SKIN AT WING TO BODY FAIRING AREA IAW SRM 53-04 FIG 57. WORK ACCOMPLISHED ON WO 250305 M301 ITEM 719 WO 1011780 6000-0042.SDR FDEA201505131500Skin · damagedFUSELAGE SKIN LIGHTNING STRIKE FASTENER, BS 480, BETWEEN STRINGER 22R - 23R, DEFORMED SKIN AT FRAME. ACCOMPLISHED WITH EA F-5330-T0317032, CATEGORY B REPAIR, MAJOR REPAIR.SDR Y2PA2015051400022Skin · crackedDURING C-CHECK DISCOVERED A CRACK ON THE BELLY SKIN & A CORRODED FLOORBEAM AT STATION 729. REPAIRED CORRODED FLOORBEAM & BELLY SKIN IAW SRM 53-30-3 FIGURE 6 SHEET 1 53-30-3 FIGURE 3 SHEET 4 & 51-30-2 PAGE 2-3 PARAGRAPH 4.SDR SWAA2015061740811Skin · crackedFUSELAGE SKIN CRACKED AT AFT END OF EQUIPMENT COOLING EXHAUST. REPAIRED SKIN IAW ER & EA.SDR SWIA2015052941237Skin · dentedLEFT EXTERIOR SKIN HAS A DENT BETWEEN FS409.00 & FS421.00, STR 16 & STR 15. C-CHECK, RO: 05/28/2015, COMPLIED WITH PERMANENT REPAIR TO LT EXTERIOR FUSELAGE SKIN BETWEEN FS 409.00 & FS 421.00 AND STR 16 & STR 15 IAW STS EA.SDR UHLA201505120379Skin · dentedDENT FOUND ROUGHLY 3 FT FWD OF L1 DOOR, EVEN WITH BOTTOM OF DOOR FRAME. THE LT SKIN DENT AT FRAME 10L-11L AND BETWEEN STR 15-17L WAS REPAIRED IAW ETD2015-170-00484, REV D.SDR FDEA201505121494Skin · corrodedEMPENNAGE FUSELAGE SKIN INTERIOR SURFACE FOUND CORROSION AT STATION 1787 - 1806, STRINGER 25L - 27L. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SSDR FDEA201505121491Skin · corrodedEMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1787 - 1806, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN P/NO 148N321SDR FDEA201505121490Skin · corrodedEMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1806 - 1825, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN P/NO: 148N32SDR FDEA201505121488Skin · corrodedEMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1844 - 1862, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N3216YSDR FDEA201505121487Skin · corrodedEMPENNAGE AREA INTERIOR COMPARTMENT, THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN STATION 1806 - 1825 FROM STRINGER 25L - 27L. CORROSION REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STSDR FDEA201505121486Skin · corrodedEMPENNAGE, EXTERIOR SKIN THERE IS CORROSION AT STATION 1825 - 1844, STRINGER 25L - 25R. CORROSION REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N321SDR DALA2015051303209Skin · damagedWINDOW BELT AT RT FS 503 - 598 DAMAGED. REPLACED SKIN IAW DWG 5932737-501 AND ER/A 516230-14, REV A.SDR 4AER201505120004Skin · crackedDURING AGING ACFT INSPECTION, FOUND A CRACK IN THE SECOND FASTENER ABOVE S26R COMMON TO THE FUSELAGE FRAME AT BS 492.4. THE CRACK WAS REMOVED BY DRILLING UP THE FASTENER HOLE IN DIAMETER WITH FINAL HOLE SIZE OF 0.875".SDR 4AER201505120002Skin · crackedDURING THE ACCOMPLISHMENT OF AD2003-14-06, FOUND TWO CRACKS,IN SKIN AT FS 727F, BETWEEN STRINGER 25L AND 26L.SDR DALA2017071905550Repair · out of limitsEXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 63 TO FRAME 63+9.5" BETWEEN STRINGER 24L TO STRINGER 28L EXISTING REPAIR OUT OF LIMITS, PERMANENT REPAIR PER ER/A 535338-14 REV 0.SDR CA150511009Doubler · cracked(CAN) MAINTENANCE IDENTIFIED THE NR 2 ADF ANTENNA DOUBLER HAS 2 CRACKS. ADDITIONAL NDT INSPECTION IDENTIFIED SOME AREAS OF DISBOND. REPAIR CARRIED OUT IAW RD8-53-14111.SDR UHLA201505110406Finger Doubler · corrodedCORROSION AROUND FASTENER HEADS, AFT CARGO FWD FINGER DOUBLER. R & R FWD FINGER DOUBLER. MAJOR REPAIR.SDR SIMA20150510006Skin · dentedDENT AT FRAME 3 - 5, STRINGER 13L - 15L. REPAIRED DENT IAW ERS-EM-53MR-1306 & SRM 51-75-00.SDR SIMA20150510007Skin · damagedCREASE AT FRAME 65 - 66, STRINGER 13R - 14R & IN PROXIMITY TO RIVET LINE. REPAIRED CREASE AT FRAME 65 - 66, STRINGER 13R - 14R & IN PROXIMITY TO RIVET LINE IAW SRM 53-31-01RE & 51-75-00.SDR DALA2015051003169Doubler · damagedDURING INSPECTION, FOUND FWD ATG 4 ANTENNA DOUBLER HAS DAMAGE WITHIN 10" CIRCUMFERENTILLY AND 20" LONGITUDINALLY. DENT IS .015 DEEP, 1" IN DIAMETER. C/W ERA 535856-14AD FWD ATG4 ANTENNA REPAIR DOUBLER.SDR R61A201505090304Skin · damagedMAINTENANCE REPORTED LIGHTNING STRIKE DAMAGE TO RT FUSELAGE AFT OF THE ICESHIELD BETWEEN FS X281.0 TO FS X321.0 AND STR 16S TO STR 21S. MAINTENANCE PERFORMED MAJOR REPAIR TO THE RT FUSELAGE AFT OF THE ICESHIELD BETWEEN FS X281.0 TO FS X321.0 AND STR 16S TO 21SDR R61A201505080303Skin · damagedMAINTENANCE REPORTED LIGHTNING STRIKE DAMAGE TO THE LT FUSELAGE AFT OF THE ICESHIELD BETWEEN FS X281.0 TO X321.0 AND STR 9P TO 16P. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE LT FUSELAGE AFT OF THE ICESHIELD BETWEEN FS X281.0 TO X321.0 AND STR 9P TO 16P IAW SDR FDEA201505081417Skin · damagedSCRIBE LINE FOUND AT STRINGER 26LT, STATION 1659.7 - 1663.5, DEPTH IS .0015", LENGTH IS 3.80", FWD .02", MID .02", AFT .02", FROM LAP. ACCOMPLISHED EA F-5330-T317267 PT 1. FUSELAGE PLATES & SKINS, SCRIBE LINE LRTS INSPECTIONS. THIS IS A CAT A REPAIR. MAJORSDR ABXA20150507070Skin · crackedRIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND TWO FASTENERS IN SECTION 48B, STATION 654.5 BETWEEN STRINGER 3R & 4R. REPAIRED CRACKED SKIN ON EXTERNAL FUSELAGE AT STATION 1654 IAW SRM 53-00-01. SDR INFO, PN 148T3121, PART NAME FUSELAGE SKIN, SN NSN, CRACKED LEN
Back to JASC 5330