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 SWAA2022021186311Scuff Plate · crackedFWD CARGO DOOR AFT SCUFF PLATE CORNER CRACKED / REMOVED DAMAGED FWD. CARGO DOOR AFT. SCUFF PLATE I.A.W. A.M.M. 53-11-02-020-801. LOCATED AND DRILLED NEW SCUFF PLATE PART #143A8331-4; I.A.W. S.R.M. 51-40-05-0G-0 AND DRAWING #143A8330. INSTALLED NEW SCUFF PALTE;SDR SWAA2022021123885Scuff Plate · crackedFWD CARGO FWD SCUFF PLATE IS CRACKED / SCUFF PLATE GOT WELDED ON W/O #37201-8100-0001 AT AAR BACKSHOP IAW EA #1-A53-2076 REV 11.SDR EE4Y2018041806374Skin · dentedDURING A STRUCTURAL INSPECTION, SEVERAL DEFORMATIONS AND DINGS (FROM INSIDE TO OUTSIDE) WERE FOUND AT MCD SURROUNDING AREA, COMMON TO LOWER FRAME SKIN BS 360 TO 500C, STRINGERS 18L AND 26L. THE DAMAGED AREAS WERE REPAIRED IAW EOS FROM AEI, EO6387, EO6388 AND SDR IPXA2018032027657Skin · crackedINSPECTION TYPE: C11, CRACK ON THE FUSELAGE SKIN AT BS 1725.5, STRINGER 7R. REPAIRED IAW EO B767-5330-24301-D, APPX.C, AND SRM 53-80-01-2R-5, REPAIR 5, DETAIL III, REV 70.03.SDR NACA2018031400001Skin · crackedSKIN CRACK FOUND ON RIGHT SIDE FUSELAGE S16R AND BS445 (VERIFIED WITH HFEC). DAMAGE REMOVED, DOUBLER INSTALLED REF SRM 53-30-3, FIG 48, REV SEP 2016. DETAIL XI AND III, PROCEDURE VII.SDR DALA2018031201671Skin · dentedRIGHT FUSELAGE EXTERNAL SKIN FOUND DENTED AT BS 1510 TO 1518, STRINGER 31R TO 32R, FOUND ONE CRACK, APPROX 0.350 INCH IN LENGH. REPAIRED IAW SRM 53-00-01.SDR DALA2018031201670Skin · crackedHFEC INSPECKTION FOUND ONE CRACK APPROX 0.275 INCHES IN LENGTH ON THE FUSELAGE SKIN, BELOW THE 11TH FASTENER AT STRINGER 13AR, FROM FWD TO AFT, BETWEEN BS 1654.5 AND 1678. REPAIRED IAW SRM 53-80-01.SDR 2018FA0000082Skin · corrodedREPAIR OF LEFT FUSELAGE SKIN CORROSION PER ENGINEERING REPAIR DEFINITION REPORT NR S-750-0005/19RD.SDR SWIA2018041044510Skin · gougedBS 977, STRINGER 27 OUTER SKIN HAS A GOUGE. REPAIRED IAW SRM AND REO.SDR DALA2018031201667Skin · crackedDURING INSPECTION OF THE TAIL, SURFACE CRACKS WERE FOUND BETWEEN BS 1654 AND 1678 AT STRINGER 13A, THE CRACKS WERE REPAIRED IAW SRM 53-80-01.SDR DALA2018031201555Skin · crackedCRACK ON SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL FUSELAGE. SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL WAS REPAIRED PER SRM VOL I 53-30-01 PAR 14, AND VOL II 51-30-02 AND 51-30-05.SDR SWAA2022021153912Scuff Plate · crackedAFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED / REPAIR ACCOMPLISHED ON B/S 37212-1000-0001 IAW EA 1-A53-2076 REV 11 (FWD CORNER SCUFF PLATE FOR AFT CARGO - WELDED)SDR SWAA2022021153914Scuff Plate · crackedFWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED. / REPAIR ACCOMPLISHED IAW EA1-A53-2076 REV 11 ON B/S W/O 37212-1400-0001 (AFT SCUFF PLATE FWD CARGO - WELDED)SDR DALA2018031301663Skin · corrodedFUSELAGE SKIN CORRODED AT THE FWD END OF THE MARKER BEACON. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS.SDR DALA2018031101636Skin · gougedFUSELAGE SKIN GOUGED AT FORWARD CARGO DOOR CONTROL PANEL 122AR. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 18.SDR DALA2018031101635Skin · gougedFUSELAGE SKIN GOUGED AT THE AFT CARGO DOOR CONTROL PANEL 154AR. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 18.SDR DALA2018031101633Skin · corrodedEXTERNAL FUSELAGE SKIN BS 750 - 790, BETWEEN STRINGERS 18R AND 22R, HAD CORROSION. REPAIRED THE SKIN IAW ER/A 556487-14AD, REV ORIGINAL.SDR DALA2022030901529None · nonePERMANENT REPAIR WAS PERFORMED ON EXTERNAL SKIN PER B-717 SRM 53-02-01-2R-1 FIG. 202 SHEET 1. VISUAL INSPECTION WAS PERFORMED PER B717 SRM 53-02-01-2R PROCEDURE 1 PAR. 6A AND NO FUTHER DAMAGE FOUND. REPETITIVE 8000 CYCLES INSPECTION PER B717 SRM 53-02-01-2R-1 SDR DALA2021120907600Skin · crackedSHIP 1818. SUSPECTED CRACK AT STA 1629-6 STRINGER 13A RT. CORRECTIVE ACTION: VERIFIED CRACK AT STRINGER 13A RT , STA 1629-6 APPROX 1 " LONG IAW B767 NDT MANUAL PT 6. 51-00. CUTOUT DAMAGE IAW PRI 566343-14 REV 2, STEP 3 AND C/W B767-400 SRM53-00. (0456302)SDR IPXA2018042729006Skin · crackedINSPECTION TYPE: D2, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 983, STRINGER 38L. REPAIRED THE SKIN IAW SRM 53-20-01, REPAIR 2, DEVIATION SUPPORT BY SRID 4-4008924086 AND EO B747-5330-68221-A.SDR A8ZR20180411002Skin · dentedDENT IN FUSELAGE BETWEEN STA 291.4 TO STA 312.35 & S8P TO S10P. EXTERNAL REPAIR DOUBLER INSTALLED REF RD 20-2018-048. REPAIR DOUBLER 7" X 10"SDR IXXA20180403014Support Beam · corrodedPANEL SUPPORT BEAM INBD OF PANEL 197BL IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED AND REPLACED IAW DWG 149N7550, AND SRM 51-40-02, PARA 7. AIRCRAFT GROUNDEDSDR AALA201803139032Skin Panel · corrodedAIRCRAFT WAS GROUNDED. LAV VENT SHOWS EVIDENCE OF CORROSION UNDER SKIN. REPAIRED SKIN PER EA 278409.SDR DALA2018030901662Skin · crackedHFEC SHOWED TWO CRACKS IN THE SKIN AT STRINGER 13AR, BS 1643. CUT OUT THE DAMAGE IAW PRI 566343-14, REV 2, STEP 2, AND COMPLIED WITH SRM 53-00-01, REPAIR 1, STEPS 1-3. PERFORMED HFEC OF THE CUTOUT IAW SRM 53-00-01, REPAIR 1, STEP 4. NO CRACKS INDICATED. RSDR DALA2018031001602Skin · crackedCRACKED FUSELAGE SKIN, BS 1189.604 LONGERON L22R. THE SKIN WAS REPAIRED IAW SRM 53-00-00-2R-1, FIGURE 201.SDR DALA2018031001598Fastener · shearedSHEARED FASTENER ON LONGERON 2L, BS 1153 AT AFT ACCESSORY. REPAIRED IAW ER/A 566637-14, REV ORIGINAL, AND ETI-17-18-044 REV 1.SDR DALA2018031001591Skin · dentedDENT ON FUSELAGE SKIN BETWEEN BS 275 - 294, LONGERON 18L TO 19L. REPAIRED IAW SRM 53-20-01-2R, PROCEDURE 5, FIG 202,SDR CALA2018031200879Skin · damagedDURING INSPECTION OF THE BELLY SKIN PER EA 5300-02120, EXISTING REPAIR DOUBLER, AT FRAME 33-35 AND STRINGER 41R-42R, WAS NOTED WITH CHAFING DUE TO INTERFERENCE WITH WING TO BODY FAIRING. THERE IS NO DAMAGE ALLOWABLES ON THE DOUBLER, THE DOUBLER WAS REMOVED ANDSDR DALA2022030201331None · noneFAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 566546-14 AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR ASSOCIATED ER/A 95-566546 ADDED SDR IPXA2018032827935Skin · chafedINSPECTION TYPE: 2C, EXTERIOR FUSELAGE SKIN CHAFED AT BS 1159, LONGERON 44R. REPAIRED THE SKIN IAW EA 011-5330-01-A7167, REV IR, AND EO MD11-5330-67934-A. MAJOR.SDR SWIA201844440Skin · dentedDENT ON RIGHT INBOARD FLAP ON UPPER SURFACE. REPLACED THE SKIN IAW REO.SDR IPXA2018032027665Skin · chafedINSPECTION TYPE: 2C, FUSELAGE EXTERIOR SKIN CHAFED AT BS 1153, LONGERON 44L. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG. 201. MAJOR.SDR SWAA2018031320386Skin · crackedEXTERNAL GROUND POWER RECEPTACLE CUTOUT DOUBLER DOOR LOWER HINGE AREA CRACKED. REPAIRED THE SKIN IAW EA.SDR YENA201803080128Skin · damagedDURING HEAVY MAINTENANCE, FUSELAGE SKIN HAD A DENT WITH 2 GOUGES AT FRAME 23 + 10, STRINGERS 42-43R. REPAIRED IAW SRM 53-00-11-300-029, PARA 2(A)(3), & 53-00-11-300-029 PARA 2(A)(7-17).SDR DALA2018030901525Skin · crackedCRACKED SKIN, BS 1076, BETWEEN LONGERONS 13L TO 14L. THE SKIN WAS REPAIRED IAW ER/A 566546-14, REV ORIGINAL, AND ETI-17-18-022, REV 2.SDR DALA2019022601225Skin · crackedCRACKS AND TOOLING DAMAGE FOUND BETWEEN STA 1620 AND STA 1660 AT STR S-13AR. C/W ERA 566343-14. (LP 0454377)SDR A6WA2018031345682Skin · crackedLEFT FWD FUSELAGE SKIN IS CRACKED AT BS 202 BY FWD EQUIPMENT BAY AFT LATCH. REPLACED THE SKIN.SDR AALA20180307002Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN AT BS 1197 BETWEEN STRINGER 39L AND 39R, AFT SIDE OF ANTENNA MOUNT. REPAIRED THE FUSEALGE SKIN IAW EA 277870.SDR DALA2018030801503Skin · wornLEFT FUSELAGE SKIN NEAR HORIZONTAL STABILIZER, WORN FROM LOWER FAIRING AT BS 1862.7, STRINGER 16L. OUT OF LIMITS IAW SRM 53-00-01, DETAIL II. REPAIRED THE SKIN IAW SRM 53-80-01, REPAIR 2.SDR DALA2018030801502Skin · wornWEAR IN THE FUSELAGE SKIN, FROM RT STAB LOWER FAIRING PANEL AT BS 1862.7, STRINGER 16R. BOTH AREAS ARE BEYOND ALLOWABLE LIMITS OF SRM 53-00-02 DETAIL II. BOTH AREAS REPAIRED IAW SRM 53-80-01 RPR 2.SDR 2018FA0000081Skin · chafedON REMOVAL OF THE HORIZONTAL STABILIZERS FROM THE FUSELAGE, SIGNIFICANT FUSELAGE SKIN CHAFFING WAS FOUND ON BOTH SIDES OF THE AIRCRAFT FROM THE RUBBER SEAL THAT FITS BETWEEN THE FUSELAGE AND HORIZONTAL STABILIZERS. IT WOULD BE ASSUMED TIME, VIBRATION, AND ATMSDR SWAA2022021027593Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO FWD CORNER SCUFF PLATE IAW EA #1-A53-2076 REV 11.SDR SWAA2022021027594Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO AFT CORNER SCUFF PLAE IAW EA #1-A53-2076 REV 11.SDR DALA2022010700149None · noneSHIP 6822 ON ARRIVAL MCO - RAMP REPORTED DENT ON FUSELAGE APPROX. 2 FT FWD AND 1 FT BELOW 4R DOOR. CORRECTIVE ACTION: SUMMARY: DENT ON FUSELAGE STA 1625: STR 18 -19 RH WAS PERMANENT REPAIR PER ETI-57-21-578 REV.3 AND PER ER/A 596321-14 REV. ORIGINAL. (4093414)SDR ASAA2018030623993Doubler · crackedL1 DOOR UPPER HINGE CUTOUT INTERNAL SURROUND DOUBLER IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE DOUBLER IAW DWG 141A8180, REV C, AND SRM 51-40-02.SDR CALA2018030800862Skin · dentedA DENT WAS FOUND ON THE REAR SKIN OF THE TAIL ZONE ACCESS PANEL BETWEEN FRAMES 73 - 74, STRINGERS 26 - 27R. REMOVED AND REPLACED THE PREVIOUS REPAIR IAW SR M 53-00-11-300-015.SDR DALA2018030701455Skin · crackedCRACKED SKIN, BS 1087, BETWEEN LONGERONS 13 AND 14R. REPAIRED THE SKIN IAW ER/A 566384-14, REV ORIGINAL, AND ETI-17-014, REV 1.SDR SWAA2022021001264Scuff Plate · crackedFWD CARGO THRESHOLD UPPER SERFACE CRACKED BEYOND LIMIT. / REMOVED THRESHOLD INSTALLED NEW THRESHOLD IAW SRM 53-30-15.SDR SWAA2022021031392Scuff Plate · crackedFWD CARGO FWD SCUFF PLATE IS CRACKED / REPAIRED SCUFF PLATE AT FWD CARGO FWD CARGO FWD SCUFF PLATE IN SW EA 1-A53-2076 REV IISDR F3LA2018051800339Skin · crackedFRAME 35, STRINGER 30L, OPEN HOLE INSPECTION IN THE SKIN REVEALED AFT LOWER HOLE WITH CRACK INDICATION. REPAIRED THE SKIN IAW SRM 51-43-00, 51-44-11, 51-42-11, 51-21-11, 51-75-12, 51-73-12, 51-24-00, 51-23-11, NTM 51-10-01, AMM 21-21-860-050-A, TDI
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