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 IPXA2017110123178Skin · damagedINSPECTION TYPE: SEG1, FUSELAGE SKIN GOUGED AND DENTED BS 1500, ABOVE STRINGER 26L, REPAIRED IAW EA 757-5361-27-A-2276, AND EO B757-5330-66190-A. THE REPAIR WAS CLASSIFIED AS MAJOR.SDR DALA2017101307533Skin · crackedCRACKED SKIN, STRINGER 15L.SDR A6WA2017101345356Skin · chafedLEFT WING UPPER INBD AFT TE TO BODY (APRON SKIN) HAS LARGE CHAFE AREA. REPAIREDSDR DALA2017101307469Skin · crackedWORKING PRI 557381-14AD, THE LOWER AFT SKIN FOUND CRACKED. REPAIRED IAW ERA 557381-14AD.SDR DALA2019053003325Skin · dentedSHIP 3862 DENT IN FUSELAGE STA 200 RBL 30 2.5 INCHES BELOW RT COCKPIT WINDSHIELD CUTOUT. CORRECTIVE ACTION: COMPLYING WITH ERA 562605-14 REV. A REF DEF LOG 0778546.SDR FDEA201710112903Skin · dentedFUSELAGE EXTERNAL SKIN HAS A DENT BETWEEN FRAMES 86 & 87, STRINGER 37 & 38R. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-12, FIG 102. REPAIRED IAW SRM 53-10-12, FIG 102, SHEET 2, & SRI 53-10-12-2-003-00. MAJOR REPAIR.SDR AALA201711109003Skin · crackedCRACK INDICATED ON SKIN PANEL AT FRAME 35, STRINGER 30L. REPAIRED THE SKIN IAW EA 274207.SDR SWIA201743941Skin · dentedDENT ON FUSELAGE SKIN BETWEEN FS625-FS640 AND STR21L-STR22L. (C-CHECK) COMPLIED WITH PERMANENT REPAIR FOR DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS 621.00 & FS640.00 AND STRINGERS 20 & 23 L. PERFORMED CUT OUT OF DAMAGED AREA, REPAIRED STRINGER STR22L FROM FS625 SDR RAIA201710100001Skin · crackedLEFT UPPER FUSELAGE SKIN HAS 4 CRACKS.SDR AALA201710119020Reinforcement · corrodedCORROSION ON AFT CABIN FORWARD INBOARD AREA, UNDER-FLOOR LAVATORY SERVICING SHROUD CUTOUT INNER SURFACE (FUSELAGE SKIN REINFORCEMENT) BETWEEN FRAMES 65 AND 66. REPAIRED FUSELAGE SKIN REINFORCEMENT IAW EA 273676.SDR SWIA2017103143938Skin · dentedDENTED EXTERIOR SKIN BETWEEN STGR23L & STGR24L. (C-CHECK) DENTS REPAIRED IAW REO.SDR SWIA2017103143937Skin · dentedEXTERIOR SKIN BETWEEN STGR22L &23L DENTED. (C-CHECK) REPAIRED DENTS IAW REO.SDR ASOA201710095135Skin · chafedFUSELAGE SKIN IS CHAFED AT PREVIOUS REPAIR AT BS 977, STRINGER 27. COMPLIED WITH EC/TC REO 670-53-00-290 01 AND REO 670-53-00-290, REV D. COMPLIED WITH EC/TC MODSUM IS670538200021 AND MODSUM IS670538200021 REVISION C.SDR UIEA2017081501484Skin · damagedAFT UPPER FUSELAGE AT APPROXIMATELY BS 1432, BETWEEN STRINGERS 18R TO 19R, FOUND WITH PREVIOUSLY BLEND OUT. AREA REPAIRED IAW SRM 53-00-01-2R-6, REPAIR 6, FIGURE 201, REV 104. REPAIR CLASSIFIED AS MAJOR.SDR UIEA2017090401594Skin · corrodedCORROSION FOUND THE SKIN BS 1197+19, STRINGER 36R. REPAIRED IAW SRM 53-00-01-2R-12, REPAIR 12, DETAIL IV, FIGURE 201.SDR SWIA2017103143934Skin · dentedBELOW RT 3RD PAX WINDOW, ONE SMALL DENT. (C-CHECK) REPAIRED DENT IAW SRM.SDR ASOA201710074052Skin · damagedA GOUGE AND DENT WAS DISCOVERED ON THE LEFT FUSELAGE SKIN ABOUT 1 FOOT BEHIND THE MAIN CABIN DOOR. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED AN DOUBLER REPAIR IAW ETD2017-145-085221, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR YENA201710070825Doubler · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER EXTERNAL SKIN, WASTE PANEL AREA, SKIN DOUBLER ON INBD EDGE. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-41-02, REV 36.SDR DALA2017100807366Skin · crackedCRACKED SKIN AT BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIGINAL, AND ETI-17-17-172, REV 2.SDR DALA2017100807365Skin · crackedCRACKED FUSELAGE SKIN AT BS 1037 LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIG, AND ETI-17-17-178, REV 2.SDR JR2R20171007326Skin · corrodedFUSELAGE SKIN CORRODED. REPAIRED THE SKIN IAW EA 42-2017-024.SDR SWIA2017111443976Skin · dentedDENT IN FUSELAGE SKIN BETWEEN BS 574 AND 589, STRINGERS 14R AND 15R. REPAIRED THE SKIN IAW SRM.SDR SWAA2017101017001Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN BS 500 TO BS 500A. REPAIRED SKIN PER EA.SDR CALA2017100603496Landing · corrodedAFTER THE REMOVAL OF THS ACCESS PANEL 312AR, THE RECESSED FLANGE WAS FOUND TO BE CORRODED ON THE THS. REMOVED AND REPLACED DOUBLER BETWEEN FR71-72 STGR 27-32R, BLENDED CORROSION ON SKIN REMOVED (.006") ACCOMPLISHED HFEC AND UT REM AINING THICKNESS (.069") NO SDR SIMA20171005001Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED AT STRINGER 2L JUST AFT OF FRAME 75. REPAIRED THE SKIN IAW SRM 53-31-01.SDR UIEA2017100901941Skin · damagedLOWER FUSELAGE SKIN DENTED AND GOUGED BETWEEN BS 355 - 368, STRINGERS 37 AND 38R. REPAIRED IAW SRM 53-00-01-2R-14.SDR EE4Y2017090504642Skin · corrodedDURING THE STRUCTURAL INSPECTION AT THE LOWER FUSELAGE AFT CARGO COMPARTMENT BETWEEN STRINGERS 40 & 43L & RT, BETWEEN FRAMES 47 AND 52. FOUND THE SKIN, INTERNAL DOUBLER AND STRINGERS WITH CORROSION. REPAIRED IAW INSTRUCTIONS UNDER REF. 80359037 AND EOD 32SDR DALA2017100507290Skin · crackedRIGHT SIDE 3/4 INCH SKIN CRACK IN EMPENNAGE CANTED STA 1531.604 ABOUT 1 FOOT UP FROM STAIR OPENING. CLEANED AREA AND REMOVED FASTENERS PER SRM 53-00 FOR INSP. VERIFIED CRACK INDICATION PER NDT 06-10-01.001. MARKED ENDS OF CRACK. DRILLED OUT 6 RIVETS TO ALLOW SDR DALA2017100507289Skin · crackedLEFT SIDE 1 INCH SKIN CRACK IN EMPENNAGE CANTED STA 1531.604 ABOUT 1 FOOT UP FROM STAIR OPENING. CLEANED AREA AND REMOVED FASTENERS PER SRM 53-00 FOR INSP. VERIFIED CRACK INDICATION PER NDT 06-10-01.001. MARKED ENDS OF CRACK. DRILLED OUT 6 RIVETS TO ALLOW BACKSDR SWAA2022020209394Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE CRACKED / REMOVED AND REPLACED AFT CARGO AFT CORNER SCUFF PLATE PER AMM 53-11-02SDR SWAA2022020209395Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE CRACKED / REMOVED AND REPLACED AFT CARGO FWD CORNER SCUFF PLATE PER AMM 53-11-02SDR CHIR3012100717Skin · corrodedDURING A BELLY WASH, IT WAS NOTICED THAT THERE WAS A SMALL "BULGE" ON THE BOTTOM SKIN OF THE LT TORQUE BOX. AFTER INSPECTION IT WAS DETERMINED TO BE CORROSION. REPAIRED THE SKIN.SDR SWAA2017111517814Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED THE SKIN IAW EA.SDR SWAA2017100616947Doubler · crackedAFT LOWER CORNER OF EXTERNAL POWER DOOR DOUBLER CRACKED. REPAIRED DOUBLER IAW SRM AND EA.SDR SWAA2022020110104Scuff Plate · crackedFWD CARGO BAY CENTER BULLNOSE SCUFF PLATE IS CRACKED ON FWD END / REPAIRED FWD CARGO BAY CENTER BULLNOSE SCUFF PLATE PER EA 1-A53-2076 REV 11SDR SWAA2022020110105Scuff Plate · crackedAFT CARGO BAY CENTER BULLNOSE SCUFF PLATE IS CRACKED / AFT CARGO BAY CENTER BULLNOSE SCUFF PLATE WAS REPAIRED PER EA 1-A53-2076 R11.SDR SWAA2022020110108Scuff Plate · crackedFWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FCB FWD CORNER SCUFF PLATE PER EA 1-A53-2076 REV 11SDR SWAA2022020110109Scuff Plate · crackedFWD CARGO BAY; AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY AFT CORNER SCUFF PLATE PER EA 1-A53-2076 REV 11SDR SWAA2022020120327Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY FWD CORNER SCUFF PLATE IS REPAIRED ON EA 1-A53-2076 REV 11SDR SWAA2022020120328Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY AFT CORNER SCUFF PLATE IS REPAIRED ON EA 1-A53-2076 REV 11SDR SWAA2022020121059None · corrodedCORROSION ON AED MOPSILL / BLENDED DAMAGED AREA ON AED MOPSILL 2.5' X 1.5' AREA ORIGINAL THICKNESS 0.080; REMOVED 0.024' MAT. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1; REMOVED & REPLACED AED MOPSILL IAW BOEING DRAWING 14A8501 & SRM 51-40-02.SDR SWAA2022020121060Scuff Plate · crackedAFT CARGO BAY FWD SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY FWD SCUFF PLATE IAW SWA EA 1-A53-2073 REV 11SDR SIMA201727689Skin · damagedEXT FUSELAGE SKIN HAS AREA OF DAMAGE AT FS 985.0 AT STR 27. REPAIRED DAMAGE SKIN AT 985.00 STR 27 IAW ERS-CR-53MAR-2968.SDR JR2R201100817344Skin · crackedCRACK FOUND IN THE SKIN AND DOUBLER AT LOWER AFT CORNER OF AIRSTAIR DOOR.SDR SWAA2022020150503Scuff Plate · cracked_AFT CARGO DOOR FWD CORNER THRESHOLD CRACKED / ROUTED TO BACK SHOP AND REPAIRED ON WO# 36533-1600-0002 IAW SWA EA 1-A53-2076 REV 11SDR SWAA2022020150504Scuff Plate · cracked__AFT CARGO DOOR AFT CORNER THRESHOLD CRACKED / ROUTED TO BACKSHOP FOR REPAIR WO # 36533-1600-0001 REPAIRED IAW SWA EA 1-A53-2076 REV 11SDR SWAA2022020107801Web · crackedFWD CARGO DOOR THRESHOLD WEB CRACKED AT STA 488 RBL 33. / REMOVED AND REPLACED DAMAGED THRESHOLD WEB; AS PER SRM 51-40-02 . REMOVED AND REINSTALLED SCUFF PLATE AS PER AMM 25-52-10 AND SRM 51-40-02.SDR DALA2017100307250Skin · damagedELONGATED HOLE EXTERNAL SKIN FR35-36 STR1-L AND STR1-R VHF3 ON UPPER FUSELAGE. PERFORMED SECTION I AS PERMANENT REPAIR AT FR35-36 STR 1L AND STR 1R VHF3 ANTENNA ON UPPER FUSELAGE INSTALL/OVER SIZE AS PER PRI 561810-14 REV 0,1,2,3 AND 4 AND ER/A 561810-14 REV SDR DALA2017100207239Skin · dentedFUSELAGE EXTERNAL SKIN DENTED, STA 620 JUST ABOVE STR 16L. REPAIRED PER PRI/ ERA 561971-14 REV 0 PRI AND ERA MATCH.SDR QXEA2017101600620Skin · gougedGOUGE IN THE FUSELAGE SKIN BETWEEN BS 216 AND 234.5, STRINGER 18 TO 19R. CUT OUT DAMAGE IAW SRM 53-20-00-02-03. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. REPAIRED THE SKIN IAW SRM 53-20-00-02-03.
Back to JASC 5330