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 A8ZR20180822004Skin · dentedDENT AT BS 313.5, STRINGER 25S-1.15" THAT MEASURES 1.0"L X .85"W X .011"D REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLE IAW EA 41-2018-045 REV B.SDR A8ZR20180822001Skin · dentedDENT FOUND AT BS 310, STRINGER 25S -1.5, MEASURES .70 L X .65 W X .004 D. REFORMED TO OROGONAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING CONSIDERED ACCEPTABLE IAW EA 42-2018-045, REV B.SDR A8ZR20180822003Skin · dentedDENT AT BS 311.25, STRINGERS 24R & 25R. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLEREF STS EA 41-2018-045 REV B.SDR SWIA2018060144741Doubler · dentedDENTS FOUND ON THE DOUBLER ON THE RT AFT FUSELAGE AFT OF LOW PRESSURE AIR SERVICE DOOR. REMOVED AND REPLACED THE DOUBLER IAW REO.SDR SWAA2018053122397Skin · damagedFORWARD CARGO BAY FUSELAGE INTERNAL SKIN DAMAGED BETWEEN BS 400 TO BS 420, BETWEEN LBL 6 TO RBL 6. REPAIRED SKIN PER ER AND EA.SDR DALA2018050303022Skin · dentedSTA 760 ABOVE STR 16L FUSELAGE SKIN DENT. 53-00-01 REPAIR 3 FIG 201. NO DAMAGE NOTED ON FRAME FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 REPAIR 3.SDR DALA2018050202996Skin · dentedSTA 640 STR 17L SKIN DENT. DENT AT STA 640 STR 17L. REPAIRED IAW ERA 567742-14 REV O.SDR COEA2018062013911Skin · gougedEXTERIOR SKIN WAS FOUND GOUGED, FORWARD OF FRAME 32 AND COMMON TO STRINGER 20R. REPAIRED IAW SRAS ES-1889-16-10259 ISSUE B.SDR IPXA2018052189757Skin · dentedINSPECTION TYPE: SEG2,M UPPER MID FUSELAGE EXTERNAL SKIN HAD ONE DENT AT BS 1180 STRINGER 7R. REPAIRED IAW EA 757-5361-27-A2298.SDR IPXA201805189690Skin · chafedINSPECTION TYPE: 3C, FUSELAGE SKIN CHAFED AT BS 1153, LONGERON 44R. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 2, FIG 201. MAJOR.SDR DALA2018050102956Doubler · wornWORN RT PRODUCTION DOUBLER Z=11 IN THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. THE DOUBLER WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 16, REPAIR 16.SDR EBVR2018043001Skin · corrodedCORROSION FOUND ON THE FUSELAGE SKIN AROUND THE RT NOSE AVIONICS DOOR AFT LATCH. BLENDED THE CORROSION ON THE FUSELAGE SKIN. INSTALLED A REPAIR DOUBLER IAW ERO-922424, REV IR.SDR SWAA2022021114983Skin · corroded***CORROSION*** CORROSION ON FUSELAGE SKIN AROUND WATER SERVICE DOOR CUTOUT. / REMVOED CORROSION AND ACCOMPLISHED INSPECTIONS TO FUSELAGE SKIN AROUND THE WATER SERVICE DOOR IAW EA 1-753-32716 REV IR AND ER 18-02591 REV IRSDR SWAA2022021114987Skin · corroded***CORROSION*** FUSELAGE SKIN (147A3400) HAS CORROSION AT BS1016 BUTT JOINT; S-24L TO S-24R / REMOVED CORROSION INSPECTED AND RESTORED AREA OF FUSELAGE SKIN AT BS 1016 BUTT JOINT; 5-24L-5-24R (147A3400) IAW EA 1-753-32725 REV IR AND ER 18-02660 REV IRSDR SWAA2022021114988Skin · corroded***CORROSION*** FUSELAGE SKIN (148A3321) HAS CORROSION AT BS1016 BUTT JOINT; S-24L TO S-24R / REMOVED CORROSION; INSPECTED AND RESTORED AREA OF FUSELAGE SKIN AT BS 1016 BUTT JOINT S-24L-24R (148A3321) IAW EA 1-753-32725 REV IR AND ER 18-02660 REV IRSDR SWAA2022021114989Skin · dentedCREASED DENT AT BS947; 1' ABOVE S-24R / DENT AT BS 947; 1' ABOVE S-24R REPAIRED IAW EA 1-753-32734 REV IR AND ATS ER 18-02576 REV IR FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2018052422216Skin · corrodedFUSELAGE SKIN CORRODED AT BS 888, BETWEEN STR 24L TO STR 24R. REPAIRED SKIN IAW ER AND EA.SDR SWAA2018052422215Skin · corrodedFUSELAGE SKIN CORRODED AT BS 888, BETWEEN STR 23L TO STR 24R. REPAIRED SKIN IAW ER AND EA.SDR V0XD20180517010Tripler · gougedAFTER FUSELAGE, BS 977, STRINGER 27, TRIPLER GOUGED. REMOVED AND REPLACED THE TRIPLER IAW REO 670-53-61-56,2 REV A.SDR DALA2018050102955Doubler · wornWEAR ON PRODUCTION DOUBLER LOWER SURFACE FROM BS 370 TO 416, THE FWD CARGO DOOR. THE DOUBLER WAS REPLACED IAW DWG 5910141, REV FE, AND SRM 51-41-02-0G.SDR DALA2018050102971Skin · crackedFUSELAGE SKIN CRACKED AT STRINGER13AL, BS 1658 - 1659. CUT OUT THE CRACKED SKIN AND REPAIRED IAW SRM 53-80-01.SDR CALA2018043001201Skin · dentedLEFT LOWER FUSELAGE SKIN HAS A DENT AT FRAME 27, BETWEEN STRINGERS 38L - 39L. INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11-300-043, FIG 20145, AND SRI53-00-205-017.SDR DALA2018042802884Skin · damagedTHE SKIN WAS FOUND DAMAGED BETWEEN LONGERONS 4 TO 7L, BS 1338. REPAIRED IAW ER/A 496010-14, REV A, SECTION II.SDR 2018FA0000241Skin · damagedRIGHT EXTERNAL FUSELAGE SKIN SCRATCHED AN GOUGED BETWEEN FS 1015 AND FS 1027, STRINGERS 23R AND 26R. REPAIRED EXTERNAL SKIN IAW STS ENGINEERING SOLUTIONS, ENGINEERING AUTHORIZATION 43-2018-068.
SDR DALA2018042702843Skin · crackedFOUND CRACKED INNER FUSELAGE SKIN BS 1150 - 1155, LONGERONS 29 AND 30R. THE SKIN WAS REPAIRED IAW ETI-88-18-026, REV 3, AND ER/A 568097-14, REV ORIGINAL.SDR A8ZR20180829002Skin · dentedDENT FOUND ON THE FUSELAGE SKIN AT BS 327.3, STRINGER 14P+5. REFORMED TO ORIGINAL CONTOUR AND FOUND TO BE WITHOUT CRACKING OR MATERIAL LOSS IAW EA 42-2018-042, REV A.SDR A8ZR20180829001Skin · dentedA DENT FOUND ON THE FUSELAGE SKIN AT BS 331.8 & STRINGER 14P+2.5. REFORMED TO ORIGINAL CONTOUR AND FOUND TO BE WITHOUT CRACKING OR MATERIAL LOSS IAW EA 42-2018-042, REV A.SDR SWIA2018052244701Skin · dentedDENT FOUND ON THE LOWER FUSELAGE SKIN AT BS 755, STRINGER 27. CUT OUT THE DAMAGE, FABRICATED A DOUBLER REPAIR AND INSTALLED IAW REO.SDR IPXA2018051829735Skin · dentedINSPECTION TYPE: 3C, RIGHT SIDE FUSELAGE SKIN DENTED AT BS 481 ABOVE LONGERON 45R. REPAIRED THE SKIN IAW EA 011-5330-01-A7264, REV I/R, AND EO MD11-5330-68526-A.SDR SWAA201805161463Skin · crackedEXTERNAL POWER DOOR CUTOUT CRACKED. REPAIRED THE SKIN IAW EA.SDR CALA2018043001210Skin · dentedA DENT WAS FOUND ON THE LT FUSLAGE SKIN AT BS 223.5 BELOW STRINGER 23L. FOUND TO BE OUT OF LIMITS. COMPLIED WITH ECRA 5330-06354.SDR DALA2018042702853Skin · damagedDURING INSPECTION, FOUND CRACKED DENT ON THE FUSELAGE SKIN ABOVE THE APU DOOR, RT SIDE, 10 INCHES AFT OF THE FWD CORNER. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-80-01, REPAIR 1.SDR A8ZR20180827004Skin · dentedA DENT WAS FOUND AT BS 120.3, STRINGER 27P+.6. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACK INDICATIONS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 301-2018-036, REV A.SDR A8ZR20180827003Skin · dentedDENT FOUND ATBS 118, STRINGER 26P-.55. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACK INDICATIONS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 301-2018-036, REV A.SDR A8ZR20180827005Skin · dentedDENT FOUND AT BS 108.5, STRINGER 15P. REFORMED WITH NO MATERIAL LOSS OR CRACK INDICATIONS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 43-2018-067, REV ORIGINAL.SDR A8ZR20180827001Skin · dentedFUSELAGE SKIN DENTED AT BS 102.2, STRINGER 24P. REFORMED AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-044, REV A.SDR ASOA201804254028Skin · tornDURING POST FLIGHT INSPECTION MAINTENANCE DISCOVERED A HOLE/TEAR IN THE FUSELAGE SKIN UNDER THE NUMBER TWO ENGINE FROM APPARENT GROUND DAMAGE. THE DAMAGE WAS LOCATED BETWEEN FRAME 66-07 STRINGER 14-15 RIGHT. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN ANSDR IPXA201804309058Skin · corrodedINSPECTION TYPE: C4, SURFACE CORROSION FOUND ON THE LOWER FASTENER HOLE OF THE SKIN AT BS 955 TEE FITTING. REMOVED THE SURFACE CORROSION.SDR CALA2018043001213Skin · gougedFOUND A GOUGE ON THE FUSELAGE SKIN ABOVE THE AFT CARGO DOOR CUT OUT 12 INCHES FROM FWD UPPER EDGE AT BS 807 BETWEEN STRINGERS 18R & 19R. REPAIRED IAW EC/RA 5331-02205.SDR DALA2018042602825Finger Doubler · corrodedCORROSION ON THE FINGER DOUBLER BETWEEN BS 1210 AND 1215, LONGERON 26L. FOUND TO BE OUT OF LIMITS. THE FINGER DOUBLER WAS REPLACED IAW SRM 53-04, FIG 12E, & SRM 51-30-2.SDR KCSA201804251081Skin · corrodedINVESTIGATE REPAIR AND CUTOUT RADII ON PREVIOUS REPAIR LOCATED IN THE AFT PIT AT APPROX BS 1451 AT STRINGER 38L. CORROSION FOUND UNDER REPAIR.SDR SRXR201804250008Skin · chafedR/H UNDER WING TO BODY FAIRING BELLY SKIN REPAIR DOUBLER IS CHAFED BEYOND REPAIR. REMOVED SKIN REPAIR DOUBLER AT R/H STA 1159 STR 44 R/H PER MD-11 SRM 51-30-01. FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER MD-11 SRM 51-40-01 AND SRM 53-40-01 8.4" X 13.5"SDR DALA2018042502840Skin · crackedHFEC INSPECTION OF THE RT FUSELAGE SKIN CRACKED ALONG STRINGER 13AR SHOWS TWO ADJACENT CRACKS TOTALING APPROX. 3 INCHES IN LENGTH, BEGINNING APPROXIMATELY 7 INCHES AFT OF BS 1654.5. REPAIRED IAW SRM 53-80-01.SDR SWAA2022021138335Skin · damaged*** CUSTOMER REQUEST *** SKIN DAMAGED BS 360 R/H BETWEEN STR 22R AND STR 23R / SKIN DAMAGE AT BS 360 RH BETWEEN STR 22R AND STR 23R IS REPAIRED UNDER SWA REPAIR-53EA-05139 REV 1 AND ATS ER 18-02493 REV IRSDR A8ZR20180820007Skin · dentedDENT FOUND ON THE CROWN SKIN, BS 325, 2L+4. REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020, REV A.SDR A8ZR20180820006Skin · dentedDENT FOUND ON THE CROWN SKIN AT BS 317.50, STRINGER 2P+5.25. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020 REV A DATED 04/19/2018.SDR A8ZR20180820003Skin · dentedFUSELAGE SKIN DENTED AT BS 301.5, S2P+7. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 42-2018-053.SDR A8ZR20180820005Skin · dentedDENT FOUND ON THE CROWN FUSELAGE SKIN AT BS 311.75, STRINGER 3L +1.35. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020, REV A.SDR A8ZR20180820004Skin · dentedFUSELAGE SKIN CROWN DENTED AT BS 307.5, STRINGER 2+3.5. REFORMED TO ORIGINAL CONTOUR IAW 42-2018-053, REV A.SDR A8ZR20180820002Skin · dentedDENT ON THE CROWN FUSELAGE SKIN AT BS 318.25, STRINGER 2L -4" REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-053 REV A.
Back to JASC 5330