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 FDEA2018081762060Skin · crackedNR 3 AIR CONDITIONING ACCESS DOOR 114AR. UPPER AFT CORNER SKIN CUTOUT WAS FOUND CRACKED AT BS 535. REPAIRED IAW SRM 53-20-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWAA2018082024295Skin · corrodedFUSELAGE SKIN CORRODED AT BS 1088, STR 25L. REPAIRED SKIN PER SRM.SDR UIEA2018081601726Skin · dentedLOCATED DENT FUSELAGE SKIN STA 1450, STR 49R-20R. COMPLIED WITH FAS EA 18174 REV-IR AT FUSELAGE SKIN STA 1450 STR 19R-20R.SDR UIEA2018081601719Skin · dentedLOCATED 2EA DENTS AT FUSELAGE SKIN STA 1376, 23R-24R. COMPLIED WITH FAS EA 18178-REV AT FUSELAGE SKIN STA1376, BTWN STA 23R-24R.SDR FOTR20180816010Skin · gougedRIGHT EMPENNAGE LOWER SEAL FAIRING SKIN WAS GOUGED AND WORN, BS 1856 - 1870.SDR SIMA20180815014Skin · corrodedSSI 53-20-07 FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 37-38 STR 21L-21R.(MARKED). C/A-COMPLETE:PERFORMED REPAIR OF FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 37-38 STR 21L-21R IAW ERS-EM-5300-3455.SDR SIMA20180815013Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 3 FASTNERS ON FR 79 RT SIDE BELOW VERITCAL STAB. C/A-COMPLETE:REPAIRED FUSELAGE EXTERNAL SKIN CRACK ON FRAME 79 RT SIDE BELOW VERTICAL STAB IAW SRM 53-32-01. SEE WIPS AND TASKS FOR DETAILS.SDR SIMA20180815022Skin · crackedRT FUSELAGE UPPER SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK ENDS MARKED, APPROX. 1/2" LONG. EASI #6581 USED. 100-500 KHZ PROBE, FREQ=400KHZ, V-GAIN=77.0, H-GAIN=65.0, LPF=100, ANGLE=134. C/A-COMPLETE:ACCOMPLISHED REPAIR OF CRACKED SKIN AT SDR FDEA2018081752031Skin · damagedFUSELAGE SKIN AT BS 1787.45, STRINGERS 17R-18R HAD A 6 INCH SCRATCH BELOW THE FAIRING. REMOVED THE DAMAGED, FABRICATED, AND INSTALLED A REPAIR IAW SRM 53-80-70-2R, FIG 201, REP 2 DETAIL I.SDR A6WA2018081645985Skin · dentedEXTERNAL FUSELAGE SKIN HAD A PROTRUDING DENT AT BS 654 TO 672, STRINGERS 22L TO 23L. REPAIRED THE SKIN IAW EACRJ253-01011, REV-IR.SDR A6WA2018081645984Skin · dentedEXTERNAL FUSELAGE SKIN HAD A PROTRUDING DENT BETWEEN BS 654 AND 672, STRINGERS 21L TO 22L. REPAIRED THE SKIN IAW EA CRJ253-01011REV-IRSDR DALA2018081505092Skin · dentedDENT FOUND ON A PREVIOUS REPAIR, BS 236 BETWEEN LONGERONS 17L & 18L IN THE FUSELAGE SKIN. THE SKIN WAS REPLACED IAW SRM 53-30-01, FIG 8B, VOL I.SDR SWIA2018091845083Skin · corrodedFUSELAGE EXTERNAL SKIN HAS MULTIPLE AREAS OF CORROSION AROUND NUTPLATE HOLE FOR AFT WING TO FUSELAGE FAIRINGS 195DL AND 196DR FROM FS 985.00 TO FS 1015.00 BETWEEN STR 21R AND 21L. (C-CHECK) RO: 09/14/2018. REPAIRED FUSELAGE EXTERNAL SKIN, MULTIPLE AREAS OF CORSDR CALA2018081701803Skin · dentedFWD CARGO DOOR, FWD UPPER CUTOUT HAD A DENT WITH A GOUGE AT BS 451, BELOW STRINGER 18R. ACCOMPLISHED ITERIM REPAIR IAW ECRA 5331-02245.SDR FOTR201808140006Skin · dentedDENT FOUND ON THE FUSELAGE SKIN AT BS 400 - 420, STRINGERS 14R - 15R.SDR SWAA2022022243798Skin · corroded***CORROSION*** ON FUSELAGE SKIN; UNDER DORSAL FIN; FROM B.S. 960-1005. / REPAIRED FUSELAGE SKIN UNDER DORSAL FIN FROM BS 960-1005 IAW ER 18-03815 REV IR AND EA 1-753-33195 REV IRSDR ASAA2018082325869Skin · corrodedFWD CARGO COMPARTMENT DOOR SILL SKIN HAS SEVERAL AREAS OF LIGHT SURFACE CORROSION ALONG LENGTH OF OPENING. MARKED IN RED. GROUNDED - YES. REMOVED CORROSION ON CORRODED AREAS ON FWD CARGO DOOR SILL WEB IAW B737-900 SRM 51-10-02, ORIG THICK 0.045, IAW B737-900 SSDR DALA2018081405068Skin · nickedDURING AN H CHECK, A NICK WAS FOUND ON THE SKIN PANEL AT BS 727H, STRINGER 26R. MAINTENANCE REPAIRED THE DAMAGE IAW ERA 570779-14.SDR DALA2018081405067Skin · crackedDURING INSPECTION, FOUND A CRACK ON THE EXTERNAL POWER RECEPTACLE CUT OUT AREA, BS 224 - 235, AND STRINGERS 22R - 23R ON THE LOWER FUSELAGE. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-15, REP 4.SDR DALA2018081405066Skin · nickedDURING INSPECTION, FOUND A NICK ON THE EXTERNAL FUSELAGE SKIN AT BS 727I+13, BETWEEN STRINGERS 26 - 27R. THE SKIN WAS REPAIRED IAW ETI-37-18-481, REV 4, AND ERA 570778-14, REV ORIGINAL.SDR DALA2018081405064Skin · nickedDURING INSPECTION, FOUND A NICK ON THE EXTERNAL FUSELAGE SKIN AT BS 727H, STRINGER 26R. THE SKIN WAS REPAIRED IAW ETI-37-18-480, REV 2, AND ERA 570779-14, REV ORIGINAL.SDR DALA2018081405063Skin · nickedDURING AN H CHECK, A NICK WAS FOUND BEYOND OF ALLOWABLE LIMITS ON THE SKIN PANEL BETWEEN BS 727I AND 727J, STRINGERS 26R - 27R. MAINTENANCE REPAIRED DAMAGE PER ERA 570778-14, AND SRM 53-00-01, REPAIR 3.SDR EE4Y201808137049Skin · crackedDURING A STRUCTURE INSPECTION, FOUND A CRACK IN THE UPPER FUSELAGE BS 727B+8.5, STRINGER 16R AT UPPER CHEM-MILLED AREA. REPAIRED THE DAMAGED AREA IAW SRM 53-30-3, FIGURE 48, DETAIL VII.SDR EE4Y201813087048Skin · crackedDURING A STRUCTURE INSPECTION, FOUND A CRACK IN THE LOWER SKIN BS 1013, STRINGER 21R AT LOWER CHEM-MILLED STEP AREA. REPAIRED THE DAMAGE AREA IAW SRM 53-30-3.SDR IPXA2018081763884Skin · dentedEXTERIOR FUSELAGE SKIN, 12 INCHES FWD OF FRAME 10 HAD TWO DENTS, 6 AND 10 INCHES ABOVE THE LAP SEAM. REPAIRED THE AREA IAW EO A300-5330-69533-A, AND REO-G21522, REV IR.SDR SWAA2022022243769Skin · corroded***CORROSION*** NOTED ON EXTERNAL FUSELAGE SKIN SKIN (BS 887 / BL 0) PANEL P/N 146A3231 - LOCAL TO FASTENER. / REPAIRED EXTERNAL FUSELAGE SKIN BS 887 BL 0 IAW ER 18-03814 REV IR AND EA 1-753-33206 REV IRSDR A8ZR20180817001Skin · dentedDENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A.SDR R61A2018081410870Skin · dentedDENT FOUND BETWEEN FRAMES 1 AND 2, STRINGERS 2R - 6R, AND OIL CANNING. COMPLETED A MAJOR REPAIR IAW ETD2018-170-085793.SDR SWAA2022022260812Skin · corrodedLOWER ATC ANTENNA HAS CORROSION ON AIRCRAFT SKIN MATING SURFACE / REPAIRED PER EA 1-753-33128 REV. IR AND ER 18-03720 REV. IR.SDR CALA2018081761796Skin · crackedINTERNAL FUSELAGE SKIN, FRAME 35, STRINGER 30L, AFT LOWER FASTNER HOLE HAD A CRACK INDICATION. REPAIRED IAW PART 3 OF ECRA 5311-01981.SDR DALA2018081315024Skin · scratchedDURING AN H CHECK, A SCRATCH WAS FOUND ON FUSELAGE SKIN AT BS 440, BETWEEN STRINGERS 19R & 20R. MAINTENANCE REPAIRED THE SKIN IAW ERA 570644-14.SDR IPXA2018082133071Doubler · gougedFUSELAGE SKIN DOUBLER GOUGED BETWEEN FRAMES 84 AND 86, STRINGER 44L AND 44R. REFABRICATED THE DOUBLER IAW SRM 53-10-12, REPAIR 13SDR CALA2018081761794Skin · crackedFUSELAGE SKIN AT BS 1850 - 1853, STRINGERS 41L - 42L WAS CORRODED. DISCOVERED DURING A C-3 CHECK. REPAIRED IAW EC/RA 5371-01009, PART 1A.SDR ASOA201808107145Skin · crackedA CRACK WAS FOUND ON THE SKIN AT FRAME 75, STRINGER 2L. CUT OUT THE DAMAGE, FABRICATED A FILLER AND DOUBLER, AND INSTALLED.SDR DALA2018081004994Skin · damagedDURING AN H CHECK, AN ELONGATED HOLE IN THE FUSELAGE SKIN AT BS 294.5, AT THE LT NOSE JACK POINT AREA. ALSO, THE SKIN AROUND THE HOLE WAS FOUND BULGED . MAINTENANCE REPAIRED THE DAMAGE IAW ERA 570609-14.SDR HEER201808109107Skin · corrodedFORWARD LOWER SHELL OUTER CORNER SKIN WAS FOUND TO BE CORRODED. LEFT SIDE FORWARD EDGE, NEAR SIDE BODY FAIRING AND LOWER WINDOW INSTALLATIONS. OPENSDR SWAA2018090424765Skin · corrodedLOWER EXTERNAL FUSELAGE SKIN CORRODED BETWEEN BS 352 TO BS 358, BL 0. R&R SKIN IAW SRM AND EA.SDR SWAA2018082824656Skin · corrodedLOWER EXTERNAL FUSELAGE SKIN CORRODED AT BS 1016, BETWEEN LBL 2 TO RBL 8. REPAIRED SKIN IAW SRM.SDR FOTR20180808001Skin · dentedDENTS FOUND IN CLOSE PROXIMITY TO EACH OTHER ON FUSELAGE SKIN. LOCATED AT BS 1495 - 1513, STRINGERS 28L- 29RSDR SWAA2022022260727Scuff Plate · crackedAFT CARGO DOOR CUTOUT; FWD CORNER SCUFF PLATE CRACKED / REMOVED; REPAIRED AND INSTALLED AFT CARGO DOOR CUTOUT; FWD CORNER SCUFF PLATE I.A.W. EA NO 1-A53-2076 REV 11SDR SWAA2022022260728Scuff Plate · crackedAFT CARGO DOOR CUTOUT; AFT CORNER SCUFF PLATE CRACKED / REMOVED; REPAIRED AND INSTALLED AFT CARGO DOOR CUTOUT; AFT CORNER SCUFF PLATE I.A.W. EA NO 1-A53-2076 REV 11SDR SWAA2022022204959Scuff Plate · crackedFORWARD CARGO COMPARTMENT LOWER AFT CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE FOR FWD CARGO LOWER AFT CORNER IAW BOEING DRAWING 143A8331 AND SRM 51-40-05. SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD 753-140-00-01YSDR SWAA2022022204960Scuff Plate · crackedAFT CARGO COMPARTMENT CENTER SCUFF PLATE IS CRACKED / REMOVED AFT CARGO COMPARTMENT CENTER SCRUFF PLATE IAW AMM 53-11-02-020-801 LOCATED AND DRILLED CENTER SCUFF PLATE IAW SRM 51-40-05-0G-0 INSTALLED AFT CARGO CENTER SCUFF PLATE IAW 53-11-02-420-801 REMOVED AFSDR JJBA2018081407006Skin · gougedFUSELAGE SKIN HAD THREE GOUGES UNDER THE UPPER TCAS ANTENNA FROM SURFACE CONTACT. REPAIRED THE SKIN AT FRAMES 16 - 17, STRINGERS 1L - 1R.SDR SWAA2018081024162Skin · crackedEXTERNAL POWER DOOR CUTOUT CRACKED ON THE LOWER EDGE. REPAIRED CUTOUT PER SRM.SDR DALA2018081084980Skin · damagedDURING A SERVICE CHECK, FOUND A GOUGE AND DENT FORWARD AND BELOW THE L2 DOOR. FABRICATED FILLER AND EXTERNAL DOUBLER IAW PRI 570627-14, REV 1, AND ER/A 570627-14, REV A AND INSTALLED IAW SRM 53-00-01, REPAIR 2. REQUIRED INSPECTION COMPLETED.SDR FDEA2018080761926Doubler · damagedDAMAGE FOUND ON THE DOUBLER AT THE FWD CARDO DOOR CUTOUT, FRAME 20 LOWER SECTION. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-40-21, DRAWING SR30-53-001, SRM 51-40-21, AND SRM 51-23-00. MAJOR REPAIR.SDR V0XD2018080900002Skin · gougedFUSELAGE SKIN GOUGED AT BS 977, STRINGER 27. REPAIRED THE SKIN IAW REO 670-53-135, AND REO 670-53-00-290, REV D.SDR NACA2018080600066Skin · crackedFUSELAGE SKIN CRACKED AT STRINGER 16R JUST AFT OF BS 480. A DOUBLER AND TRIPLER WAS INSTALLED IAW SRM, 53-30-03, REPAIR 48, DETAIL VII.SDR FOTR 20180806003Skin · dentedDENT FOUND ON FUSELAGE SKIN AT BS 1677, STRINGERS 25L TO 26L.
Back to JASC 5330