JASC 5330
Service difficulty reports · 79,329
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 JJBA20200930030Skin · looseREAR FUSELAGE 2 SKIN, CRACKS FOUND AROUND RIVET ON FR 77 AND BETWEEN STR 3L-4L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 77 AND BETWEEN STR 3L-4L. FASTENER AND SKIN DAMAGE ON FR 77 BETWEEN STR 3-4L REMOVED. FASTENER DIAMETER .161 SKIN RESDR JJBA20200930029Skin · looseREAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVET ON FR 77 AND BETWEEN STR 8L-9L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 77 AND BETWEEN STR 8L-9L. FASTENER AND SKIN DAMAGE ON FR 77 BETWEEN STR 8-9L REMOVED. FASTENER DIAMETER .161. SDR JJBA20200930028Skin · crackedREAR FUSELAGE 2 LT SKIN, CRACKS FOUND ON FR 78 AND BETWEEN STR 5L-6L. FOR INVESTIGATION PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 78 AND BETWEEN STR 5L-6L. FASTENER AND SKIN DAMAGE ON REAR FUSE 2 FR 78 BETWEEN STR 5-6L REMOVED. FASTENER DIAMETER .161. SKINSDR JJBA20200930027Skin · crackedCRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 78 AND BETWEEN STR 5R-6R. ON RT REAR FUSE 2, ON FR 78 AND BETWEEN STR 5R-6R, PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMGE ON RT REAR FUSE 2 ON FR 78 BETWEEN STR 5-6R REMOVED. FASTENER DIAMETER 0.161. SSDR JJBA20200930026Skin · crackedREAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVER ON FR 79 AND BETWEEN STR 3L-4L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AT FR 79 AND BETWEEN STR 3L-4L. FASTENER AND SKIN DAMAGE ON REAR FUSE 2 FR 79 BETWEEN STR 3-4L REMOVED. FASTENER DIAMESDR JJBA20200930025Skin · crackedCRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 79 AND BETWEEN STR 3R-4R. ON RT REAR FUSE 2, ON FR 79 AND BETWEEN STR 3-4R PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMAGE ON RT FUSE 2 ON FR 79 BETWEEN STR 3-4R REMOVED. FASTENER DIAMETER 0.161. SKIN RESDR JJBA20200930024Skin · crackedREAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVET ON FR 79 AND BETWEEN STR 5L-6L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGED SKIN AREA, AFTER 79 AND BETWEEN STR 5L-6L. FASTENER AND SKIN DAMAGE AT REAR FUSE 2 FR 79 BETWEEN STR 5-6L REMOVED. FASTENER DIAMETSDR JJBA20200930023Skin · crackedCRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 79 AND BETWEEN STR 5R-6R. ON RT REAR FUSE 2, ON FR 79 AND BETWEEN STR 5R-6R, PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMAGE REMOVED ON RT REAR FUSE 2 ON FR 79 BETWEEN STR 5-6R. FASTENER DIAMTETER 0.161 SSDR JJBA20200930022Skin · crackedREAR FUSELAGE 2 LT SKIN, CRACKS FOUND AROUND RIVET ON FR 79 AND BETWEEN STR 6L-7L. FOR INVESTIGATION, PAINT REMOVED ON DAMAGE SKIN AREA AT FR 79 AND BETWEEN STR 6L-7L. FASTENER AND SKIN DAMAGE LT FUSELAGE 2 FR 79 BETWEEN STR 6-7L REMOVED. FASTENER DIAMETERSDR JJBA20200930021Skin · crackedCRACK ON RT REAR FUSE 2, AROUND RIVET, ON FR 79 AND BETWEEN STR 6R-7R. ON RT REAR FUSE 2, ON FR 79 AND BETWEEN STR 6R-7R, PAINT STRIPPED FOR INVESTIGATION. RIVET AND SKIN DAMAGE ON RT FUSE 2 ON FR 79 BETWEEN STR 6-7R REMOVED. FASTENER DIAMETER 0.161, SKIN RSDR FDEA202009302358Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND SIDE UNDERWING LONGERON AND THE FUSELAGE SKIN AND FOUND 01 EACH CRACK APPROXIMATELY 1.25 INCHES LENGTH,SDR DALA2020100203252Skin · damagedDURING INSPECTION FOUND SCRATCHES/GOUGES FOUND ON FUSELAGE CROWN SKIN BETWEEN STATIONS 500E AND 500F AND BETWEEN STRINGERS 5L AND 7L. REPAIRED DAMAGE, PER ERA 587952-14 REV A.SDR SWAA2020102825532Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 360+5.5', 1' BELOW S-15R. FUSELAGE SKIN DENT AT BS 360+5.5'; 1' BELOW S-15R REPAIRED, IAW ATS ER 20-03377 REV IR DATED 21-OCT-2020 AND PER EA NR 20-153-02028 REV IR 55981U 21OCT20.SDR IPXA2020102261575Skin · corrodedINSPECTION TYPE: 2C CENTER WING BOX SKIN HAS CORROSION AT S-13 BETWEEN XCW 102 AND XCW 110. REPAIRED CENTER WING BOX SKIN CORROSION AT S-13 BETWEEN XCW 102 AND XCW 110, IAW VT-SAA EA 011-5730-01-A8605 REV I/R AND UPS EO MD11-5730-78247-A. (MAJOR)SDR JJBA20200929007Plate · corrodedCORROSION ON RAD ALT 2 ANTENNA MOUNTING PLATED AND SKIN. BOTH FWD AND AFT RAD ALT 2 ANTENNA MOUNTING PLATED REMOVED. REMOVED FWD AND AFT RAD ALT 2 MOUNTING PLATES. REMOVED SERVICE CORROSION. CUT OUT DAMAGED AREA. MEASURED SKIN THICKNESS THAT WAS BLENDED USSDR REXA2020100700679Doubler · corrodedTCAS DOUBLER IS CORRODED. REMOVED AND REPLACED TCAS DOUBLER, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR IPXA2020092960780Skin · damagedINSPECTION TYPE: SEG GROOVE WORN UNDER RT HORIZONTAL STAB ON SKIN AT STA 1862-1870. REPLACED IAW B757-200 SRM 53-80-01-2R-2 FIG 201 DETAIL II.SDR IPXA2020092960778Skin · gougedINSPECTION TYPE: SE GLH FUSELAGE HAS WEAR GOUGE UNDER HORIZONTAL STAB AT STA AT 1862-1870. REPAIRED IAW B757-200PF SRM 53-80-01-2R-2 FIG 201 DETAIL II.SDR 2020F00412Skin · corrodedAPU STINGER SKIN DAMAGE (CORROSION). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ27131M1, DATED SEPTEMBER 24, 2020; 680A-0040 (N503QS) APU STINGER SKIN DAMAGE (CORROSION).SDR SWAA2020110425528Skin · gougedTAIL JACK HOLE PREVIOUS REPAIR DOUBLER HAS GOUGED. REPAIRED SECTION SKIN ON TAIL JACK HOLE POINT, PER REF B737-700 EA 1-753-33580 REV 1R.SDR FDEA202009282633Skin · dentedDENT EXTERNAL SKIN LOCATED FR 14A MORE 4 INCHES AT LEVEL STR 33L AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC FR 15 TO FR 15A AND 13" DOWN STR 30L AT LOWER FUSELAGE, IAW EA N: 6-5310-T0357390. P1 EA TITLE: FUSELAGE NOSE SECTION-SKIN PANSDR IXXA20201001038Skin · crackedMAINTENANCE, DURING ROUTINE OPERATIONS AT CVG, DISCOVERED ON 331AZ A CRACK IN THE SECTION 46 FUSELAGE SKIN AT THE FORWARD JAMB OF THE RIGHT AFT LOWER CARGO DOOR, PN 146T3510, AT STA 1270, NEAR DOOR STOP NUMBER 10. THE SKIN IS MADE FROM 2024-T3 X 0.210 CLAD ALSDR FDEA202009282349Skin · dentedFUSELAGE SKIN DENTED, BETWEEN FR 52 AND FR 53, STGR 38R AND STGR 40R. REPAIRED THE FUSELAGE SKIN DENT (OIL CAN) BETWEEN FR 52 AND FR 53, STGR 38R AND STGR 40R, PER A300-600 SRM53-10-12 FIG.223. THIS REPAIR CATEGORY B. THE FIRST INSPECTION THRESHOLD IS 51000SDR ASMF202011008Skin · damagedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED TWO NICKS AT FUSELAGE SKIN SECTION 41 BETWEEN STRINGERS S-39L AND S-38L. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK OF 0.250" DIAMETER STA 348 AND A NICK OF 0.250" DIAMETER STA 349 A UT-SDR SWIA202052903Skin · corrodedFOUND EVIDENCE OF CORROSION BETWEEN STRINGER AND FUSELAGE SKIN (BULGE) AT STR 21L AND FWD OF FS 349.00. DETERMINED TO BE A "MAJOR REPAIR" FORM M-337 REQUIRED. FILED CLOSED 10/3/2020. REPAIRED FUSELAGE SKIN BETWEEN STR 21L AND FWD OF FS 349.00, IN REFERENCE SDR FDEA202009252348Skin · crackedUPPER FUSELAGE FR 13 STGR 9R, 1 EA FASTENER HOLE FOUND WITH CRACK SIGNAL (AFT THIRD HOLE FROM LAP JOINT COUNTING FROM BOTTOM). COMPLIED WITH FEDEX EA: 6-5310-T0356680 PT1, EA TITLE: FUSELAGE-MAINFRAME-REPAIR OF CRACKED HOLE IN CIRCUMFERENTIAL JOINT AT FR 13 RSDR FDEA202009252347Skin · crackedUPPER FUSELAGE FR 13 STGR 9R, 1 EA FASTENER HOLE FOUND WITH CRACK SIGNAL (AFT THIRD HOLE FROM LAP JOINT COUNTING FROM BOTTOM). COMPLIED WITH FEDEX EA: 6-5310-T0356680 PT1, EA TITLE: FUSELAGE-MAINFRAME-REPAIR OF CRACKED HOLE IN CIRCUMFERENTIAL JOINT AT FR 13 RSDR UIEA2020092802089Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN STA 783.5, 13R. REPAIRED IAW REA 47416 REA10.SDR UIEA2020092802093Panel · corrodedCORROSION ON BULGE PANEL. REMOVED CORROSION ON BULGE PANEL IAW B767 SRM 53-60-53.SDR UIEA2020092802095Skin · corrodedCORROSION ON SKIN. REPAIRED SKIN DAMAGE IAW 47416 REA15.SDR UIEA2020092802096Skin · corrodedBULGE IN SKIN (CORROSION). REPAIRED SKIN IAW REA 47416 REA 02.SDR UIEA2020092802103Skin · bentSKIN BENT AND CREASED. REPAIRED IAW REA 47416 REA 06.SDR UIEA2020092802105Skin · corrodedCORROSION ON INTERNAL SKIN STA 783 ABOUT STRINGER 13L. REMOVED CORROSION AND REPLACED SKIN, IAW AMES DOC 47416 REA 49.SDR UIEA2020092802106Skin · corrodedFUSELAGE SKIN CORROSION AT STA 783 STR 12R. REMOVED CORROSION AND REPAIRED, IAW AMES DOC 47416REA10.SDR UIEA2020092802107Skin · damagedFUSELAGE SKIN CREASED AT STA 676 STRINGER 7L. REPAIRED SKIN, IAW AMES DOC 47416 REA 17.SDR JJBA20200924036Skin · dentedMULTIPLE DENTS ON RT CENTER FUSE 4, BETWEEN FR 53-54 AND BETWEEN STR 12R-14R. RT FUSELAGE 4, BETWEEN FR 53-54 STR 12R-13R, 2 CUT-OUT PERFORMED FOR ENGINE REVIEW. RT FUSELAGE BETWEEN FR 53-54 AND BETWEEN STR 12R-14R REPAIRED. RT CABIN OVERHEAD BIN RE-INSTALLSDR FXGA202009242014Skin · damagedFUSELAGE SKIN DAMAGED AT F/STA 533 BETWEEN STRINGERS 10L AND 11L. TO REPAIR A GOUGED SKIN BEHIND THE CARGO DOOR AT F/STA 533 BETWEEN STRINGERS 10L AND 11L. REPAIR DAMAGED SKIN, PER AEI EO11598. PERFORM SUPPLEMENTAL INSPECTION AT 10,100 CYCLES (THRESHOLD ANDSDR EVCA2020093001Skin · crackedDURING ROUTINE MAINTENANCE, THE LOWER SKIN OF THE FUSELAGE NEAR TAILBOOM ATTACHMENT WAS FOUND CRACKED APPROXIMATELY FOUR INCHES LONG FORWARD AND AFT AND AN INCH-AND-HALF RUNNING OUTBOARD. FS 75, WL 61.77, RBL 2.0.SDR DALA2020092503195Skin · corrodedCORROSION EXTERNAL SKIN LOCATED BETWEEN FR 69 TO FR 70 AND BETWEEN STRG 31R TO STRG 32R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FR 69 TO FR 70 AND BETWEEN STR 31R TO STR 33R AT LOWER FUSELAGE, AS PER A320 SRM 53SDR SWIA202054730Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA53479-670-53-00-045 754EV FS256 ON STR23R-PR1. COMPLIED WITH TEMPORARY REPAIR, PER REO BLENDED DAMAGED SKIN AS REQUIRED AT FS 256 ON STR 23R. REPAIR IS VALID UNTIL NEXT HEAVY MAINTENANCE CHECK OR FOR 8000 FLIGHT HOURSDR FDEA202009232298Skin · crackedCABIN-MAIN DECK CARGO COMPARTMENT R3 DOOR AFT LOWER FUSELAGE JAMB, SKIN FOUND CRACKED AT RIGHT HAND STATION 1310 BETWEEN LONGERON 26 RIGHT 27 RIGHT. CABIN-MAIN DECK CARGO COMPARTMENT R3 DOOR AFT LOWER FUSELAGE JAMB AT RIGHT HAND STATION 1310 BETWEEN LONGEROSDR HNAA2020092500269Skin · dentedFWD FUSELAGE 1, TWO DENTS LOCATED BETWEEN FRAMES 2 AND 3, STR 04L AND 06L. MAINTENANCE REPAIRED, IAW E01-53-20-0357, EO1-53-20-0355, SRM53-10-01, AND SRM 51-75-04.SDR SWAA2021042719301Doubler · damagedDAMAGED EXISTING REPAIR AT EGPR SURROUND DOUBLER ZONE 1 STA 235. / REPAIRED EGPR SURROUND DOUBLER ZONE 1 STA 235 PER SRM 53-10-15-2R-4 REPAIR 4.SDR SWAA2020101419303Doubler · damagedDAMAGED EXT PWR DOOR SURROUND DOUBLER ZONE 2 STA 231. / REPAIRED SURROUND DOUBLER ZONE 2 B.S 231 IAW EA 20-153-01979 REV IR AND ATS ER 20-03351 REV IRSDR SWAA2020101218229Skin · dentedDENT ON RT FUSELAGE SKIN AT APPROXIMATELY STA 996.5, 3.5' BELOW STR 21R, L=2.7', W=2.3' AND .90' DEEP W/Y=25.5. REWRITTEN FROM DEFECT NR 8419. THIS N/R WRITTEN TO DOCUMENT PERMANENT REPAIR. REPAIRED DENT ON RT FUSE SKIN AT APPROXIMATELY STA 996.5; 3.5' BELOSDR IPXA2020093060793Skin · crackedINSPECTION TYPE: C8 CRACK FOUND ON FUSELAGE SKIN AT STA 1654.5 S-13 AR. REPAIR, IAW BOEING SR 4-4884706014, 767-300BCF SRM 53-80-01 REPAIR 7, REV 38 AND UPS EO B767-5330-78006-A.SDR JJBA20200921014Skin · dentedDENT ON RT FWD FUSE SKIN 2, 0.30" AFT OF FR 10 AND 1.80" ABOVE STR 17R. DENT ON RT FUSE SKIN 2, 0.0300" AFT OF FR 10 AND 1.8" ABOVE STR 17R REPAIRED.SDR SWAA2020100817386Skin · damagedFUSELAGE SKIN AT STA 277+6 BETWEEN STR 1 AND 2 HAS DAMAGE FROM FWD LAV DOOR HINGE PIN MIGRATION, AS PER SA-M 735 ROY DENBOW E13421. FUSELAGE SKIN AT STA 277 + 6 BETWEEN STR 2L AND STR 3L HAS DAMAGE FROM LAV DOOR HINGE MIGRATION. REMOVED DAMAGE, ACCOMPLISHED SDR JR2R20200921136Doubler · corrodedFUSELAGE SKIN INTERNAL DOUBLER AROUND AFT LAV SERVICE DOOR OPENING IS CORRODED OUT OF LIMITS. REPAIRED IAW EMB127 SRM 53-23-60 REPAIR 01, ON AAR W/O 1018802 1000-0008 S/N 7898136.SDR R61A2020100500680Skin · deformedPREVIOUS DAMAGE ON RT SIDE OF AC BETWEEN FR 4 & 5, STR 26R& 25R WAS FOUND TO BE OIL CANNING. REPAIRED PER ETD2020-170-027835 REV G, MAJOR REPAIR. A/C WAS RETURNED TO SERVICE ON 10-3-20.
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