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 DALA2023030601648None · noneSHIP 5813 REFERENCE ER/A 571586-14 REV A B757-300 / FUSELAGE SKIN / STA 550-620, S14L-S19L / GROUND DAMAGE, DENT. CORRECTIVE ACTION: REF ERA 571586-14. (2653776)SDR DALA2023030601629None · none(LOG 8779501) DURING INSPECTION FOUND FUSELAGE DAMAGE LEFT HAND AT STA 500, 500A AND STRINGERS S-21L, S-22L. REPAIRED FUSELAGE DAMAGE PER DETA ERA 600864-14 REV 0.SDR A6WA202303038477Angle · gougedACFT EXTERIOR- FS 409+112 BETWEEN STRGRS 27/26L VERICAL PLATE FOR FWD DRAW BEAM CORROSION. ********AIRCRAFT REMOVED FROM SERVICE********* REPAIRED LOWER FRAME ANGLE AND FUSELAGE SKIN AT FS 409+112 BETWEEN STR 26L 27SDR DALA2023030301593None · noneSHIP 3361 ON WALKAROUND FOUND DENT 24" BELOW AND 16 FWD OF DOOR 4R. CORRECTIVE ACTION: PERFORMED DAMAGE CONTAINMENT. PERFORMED HFEC AROUND CUTOUT. NO CRACKS INDICATIONS NOTED. FABRICATED REPAIR DOUBLER. TREAT AND PAINTED. INSTALLED. REPAIR COMPLETE PER ERA 606SDR FDEA202303020596Skin · damagedEVALUATE PREVIOUS DENT AT LHS FUSELAGE LWR SKIN FR10 6", 8 O'CLOCK. ACCOMPLISHED THECAT B DOUBLER REPAIR IAW A300-600F SRM 53-12-12-201, CONFIG 2, PAR. 5A, PAGE 203-208, FIG.201 & SRI 53-12-12-201, IR 53-12-12-2-006-00, PARA. 3F, TABLE 207 "MAJOR REPAIR".SDR IPXA2023032792311Panel · corrodedINSPECTION TYPE:3CFOUND SKIN CORROSION AT L/H TUNNEL APPOX FS 808 - 824 LONGERON 37 TO L38.REPAIRED CORRODED SKIN AT L/H TUNNEL AT FS 808-824 AND LONGERON 37 - L38 IAW VTSAA EA 011-5330-01-A9878 I/R AND UPS EO MD11-5330-86292-A AND FAA FORM 8100-9 SIGNED BY J.SDR SWIA20230302Unknown · corroded*R/H WING LOWER PLANK HOLE FOR PANEL 640DB HAS FRETTING CORROSION (MARKED) (C-CHECK RO 3/23/2023) REMOVED FRETTING CORROSION ON R/H WING LOWER PLANK HOLE FOR PANEL 640DB ( LANDING) FROM 270 DEGREES TO 345 DEGREES WITH-IN LIMITS REF REO 601R-57-21-030 RSDR DALA2023030301603None · noneSHIP 665 A.A PREVIOUS REPAIRS WAS FOUND ON LAP SPLICE S-14L FROM STA. 630-640 AND FROM 565-575 AT OUTER FUSELAGE SKIN. (ERA 480014-14). CORRECTIVE ACTION: SUMMARY OF NRC 00018. ADDITIONAL MTC.WORK IS NOT REQUIRED PER ER /A 480014-14AD REV D. (2651580)SDR DALA2023030301595None · noneSHIP 3361 THIS LOGPAGE IS SETUP TO TRACK THE LIMITS PER RDAF 81189401/003/ 2023#A . CORRECTIVE ACTION: REF RDAF REQUIREMENTS ASSOCIATED ER/A 14-606617. (2652619)SDR SWAA2023031311572Doubler · debondedA225-011 ANTENNA DOUBLER IS DISBONDING AT 0 BL BS 663 - 27'.<[01] REPAIRED ANTENNA DOUBLER FILLET AT 0 BL; BS 663-27' I.A.W. AMM 51-31-00-390-812;[02] VERIFIED TASK COMPLETESDR DALA2023030301604None · noneSHIP 665 REFERENCE ER/A 480014-14AD / FUSE SKIN / STA 570-633 / S-14L TO S-19L / SKIN SPLICE. CORRECTIVE ACTION: REF ERA 480014-14. (2650903)SDR DALA2023030201555None · noneSKIN PANELS BTW STA 954 TO STA 974 LONG 30 TO R29 ARE CORRODED OUT OF LIMITS. WITH ORIGINAL THICKNESS OF 0.071 IN. AND THE MAXIMUM REMOVED MATERIAL FOUND IS 0.033 IN. THEREFOR AREA IS OUT OF LIMITS IN REF NRC 00192 AT AFT CARGO (C2). SUMMARY OF NRC 00512: CORRSDR SWAA2023040311083Skin · corrodedCORROSION ON CROWN SKIN UNDER VERT STAB 3 INCHES O/B OF STRINGER 2L BETWEEN STA 1016 AND STA 1040. (MARKER)<[01] INSTALLED EWIS PROTECTION AT DISCREPANCY AREA AT INTERNAL SKIN PER AMM 20-60-07;[02] SRM 53-80-01-0I-1 IDENTIFICATION AND SRM 53-00-01-1A-1 ALLOWABSDR ASAA2023022842334Intercostal · crackedFWD CARGO R/H BAFFLE @ STA 500G-500H HAS CRACKED CORNER. GROUNDED - YES. REMOVED DAMAGED R/H BAFFLE @ STA 500G TO 500H DRILLED AND LOCATED NEW BAFFLE ASSEMBLY @ STA 500G TO 500H IAW B737-800 SRM 51-40-02 AND DWG # 147A7505INSTALLED NEW BAFFLE ASSEMBLY @STA 500SDR SWAA2023031011255Skin · corrodedFOUND CORROSION AT BS1016 BETWEEN S20L-S21L MEASURING .5'X.5' REF: TTG8Q00J55UF<[01] SRM 53-70-01-2R-4 IS FOUND TO BE APPLICABLE;[02] PERFORMED DAMAGE CUTOUT ON FUSELAGE SKIN BS 1016 STR 21L L=3.2'XW=2.9'. IAW SRM 53-70-01-2R-4 STEPS 4.B.(1-2).;[18] INSTALLED SDR DALA2023030201568None · noneSHIP 5640 COMPLY WITH ERA 606378-14 REV. ORIGINAL. CORRECTIVE ACTION: REF ERA 606378-14 RE ORG. (2648348)SDR DALA2023110909222Unknown · unknownSHIP 3024 DAMAGE @ LOCATION STA 18034/FR 36.5 RH STGR 14. CORRECTIVE ACTION: REPAIRED PER A321 SRM 53-01-11-300-12. (9851998)SDR SWAA2023030610734Skin · corrodedFOUND CORROSION AT BS1016 BETWEEN S20L - S21L MEASURING .5'X.5'<[01] TRANSFERRED TO LOGPAGE 2044796. REF: TSR 2023001542 FOR MX FERRY FLIGHTSDR DALA2023030101540None · noneSHIP 6803 CRACK ON CHANNEL INSIDE ACCESS PANEL 117CL STA 365 BTW 0 BL. OF THE NLG WHEEL WEEL. CORRECTIVE ACTION: SUMMARY OF NRC 00164 CHANNEL INSIDE ACCESS PANEL 117CL STA 365 BTW 0 BL. OF THE NLG WHEEL WEEL.WAS REPAIRED PER B757-200 SRM. (2648038)SDR SWAA2023032010166Panel · elongatedACCESS PANEL 191HL COVER PLATE - FORWARD FAIRING HOLES ENLONGATED<[01] RECEIVED NEW PANEL 191HL. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00GXTW3;[02] STEP #1 ENTER IN ERROR; ACCESS PANEL 191HL WILL BE UNAVAILABLE AND ESR WAS SEND TO ENGINEER; SEE ASDR SWAA2023030610184Skin · corrodedREF: 53-00-01-1A-5-A00015-TLD; FUSELAGE SKIN AT STA 460; BL 0 IS CORRODED ON MATING SURFACE OF RA1 TRANSMIT ANTENNA AND REQUIRES REPAIR<[01] UPDATED MEASUREMENTS;[02] VERIFIED PARTIAL FOR STEP 6;[03] OK TO PAINT REPAIR;[04] APPLIED PAINT TO REPAIR IAW AMM 51-2SDR DALA2023022801522None · noneSHIP 671 ON WALK AROUND FOUND CRACK AT STA 440 STRINGER 26R ON RIGHT SIDE. SKIN CRACKED AT BUTT JOINT. CORRECTIVE ACTION: REF ELECTRONIC NR 00001. C/W FUSELAGE SKIN DAMAGE REPAIR PER ERA 606367-14 REV ORIG PRI 606367-14 REV 0AND 1 MATCH. ERA 606367-14 REV 0RIGSDR DALA2023022801511None · noneSHIP 671 ON WALK AROUND FOUND CRACK AT STA. 440 STRINGER. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:0514-2001/001 00001 C/W FUSELAGE SKIN DAMAGE REPAIR PER ERA 606367-14 REV ORIG. (2644342)SDR DALA2023022701438None · none(LOG 4105765) DURING INSPECTION FOUND CORROSION AROUND BELLY DRAINS AT STATIONS 420,460,480,500A,500B,500D,500I AND 500U. CORROSION CORRECTED ON ELECTRONIC NON ROUTINE CARDS 1,2,3,4,5,6,7 AND 8 PER B737 SRM 53-30-01.SDR DALA2024061906238Skin · crackedSHIP 671 DTE 606367-14 - B757-200 / FUSELAGE SKIN / STA 439 & S-25R / CRACK PERMANENT REPAIR. CORRECTIVE ACTION: REF ERA 606367-14. (2644141)SDR SWAA2023040509882Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-142632<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0000293;DUE DATE:12-OCT-23.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1998072; DUE DATE: 03-MAY-23.;[03] REPAIRED AFT CORNER SCUSDR CALA2023022700550Door Sill · corrodedFWD CARGO DOOR SILL HAS CORROSION SPOTS ON UPPER SURFACE GENERAT ED AT HAECO LCQ PER NR 9298573 (20573) BY V919150. {A3NB-53-3-61 05} REMOVED AND REPLACED FWD CARGO DOOR SILL IAW A319 SRM 51-42-11-0 01. TREATED, PRIMED, AND TOP COAT AREA IAW A319 SRM 51-23-11-SDR IXXA2023040101Support · corrodedFWD CARGO DOOR CUTOUT LWR DOOR SILL UPPER SURFACE AT APPROX STA 610 HAS CORROSION. CORROSION WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED. BLEND AT MEASUREMENTS BEFORE REPAIR: UPPER SURFACE 1=2", W=1.8", LOWER SURFACE 1=2", W= 1.3", REMAINING THICKNESS=0.061SDR SWAA2023032009557Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208.<[01] REMOVED DAMAGED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208 ISDR SWAA2023031609586Support · crackedCRACK ANGLE - SUPPORT BS 380 TO BS400 BL0 WL 208 AT FWD GALLEY AREA 2023-127694<[01] REPLACED NEW ANGLE SUPPORT BS 380 TO BS400 BL0 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET:92 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPSDR DALA2023030201550None · noneFOUND SKIN DAMAGE AT C-2 DOORWAY JAMB EDGE AT DOOR CUT OUT SURROUND AREA BELOW DOOR STOP #2. SUMMARY SEE NRC 003-0001:0514-2001/003 00003: COMPLIED WITH ER/A PRI 606111-14 REV'S "0","1","2","3" AND ALL REPAIR INSTRUCTIONAL STEPS ARE COMPLETED, ENSURED FINAL ERSDR CALA2023022400533None · corrodedFWD CARO PIT R/H FR29 BETWEEN STRINGERS 41R-42R HAS CORROSION O N CLEAT (A3NB-53-3-6105) GENERATED AT HAECO LCQ BY V919150 PER N R 9292693 (40693) REMOVED AND REPLACED CLEAR CLEAT IN FWD CARGO PIT FR29 RT AT STR 41R-42R IAW A320 SRM 51-72-11-911-001 PERFORMEDSDR S9BA20230001Structure · corrodedSUPPLEMENT REPORT TO CONTROL NUMBER 2023F00064. PLEASE CHANGE CONTROL NUMBER FROM 2023F00064 TO OPERATOR UNIQUE CONTROL NUMBER S9BA20230001. ALL OTHER INFORMATION IS THE SAME. RH SIDE FUSELAGE SKIN (.050) CORRODED (.023) DEEP BEYOND SRM LIMITS (.006) AT FSSDR CALA2023022400526None · crackedR/H OVERWING EMERGENCY EXIT HAS CRACK AT INNER BOTTOM ANGLE-WEB PER HAECO LCQ NR 9298411/20411 SPEC: A3NB-05-3-6168. GENERATED B Y V919150. REMOVED AND REPLACED R/H OVERWING EMERGENCY EXIT INNER, BOTTOM ANGLE-WEB IAW SRM 51-42-11 AND DWG# 0522-79010 ADD EMP:V9SDR 2023F00064Structure · corrodedRH SIDE FUSELAGE SKIN (.050 THICK) CORRODED (.023 DEEP) BEYOND SRM LIMITS (.006) AT FS131-FS132 AT TOP OF WINDOW CUTOUT.SDR DALA2023022301357None · noneSHIP 5635 AWR - DURING NDT INSPECTION OF CARD 2330-01322-03I JOB #046-0001 , STEP 4, DISCREPANT RIVETS WERE FOUND ADJACENTO TO OUTER ROW OF DOUBLER RIVETS AS FOLLOW: AT STA 620 TWO DISCREPANT RIVTES ADJACENT TO STRG 1, TWO DISCREPANT RIVETS ADJACENT TO STRG 2RSDR R61A2023031500195Skin · dentedFWD FUSE LOWER SKIN PNL DENT FOUND BTWN FR16-17, STR 23L-24L. ALLOWED DAMAGE IAW ETD2023-170-006285SDR R61A2023031500194Skin · dentedFWD FUSE LOWER SKIN PNL DENT FOUND BTWN FR 16-17 STR 22L-23L. ALLOWED DAMAGE IAW ETD 2023-170-006285SDR R61A2023031500193Skin · dentedFORWARD FUSE LOWER SKIN PNL 4 PROTRUDING DENTS BTWN FR-2-3 STR 28R-26R. ALLOWED DAMAGE IAW ETD 2023-170-006146.SDR R61A2023031500191Panel · corrodedCORROSION FOUND ON CF3 WATER ACCESS DOOR. REPLACED IAW SRM 53-03-02/400SDR DALA2023022301355None · noneSHIP 5639 COMPLY WITH ERA 606173-14AD REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH ERA 606173-14AD REV. ORIGINAL. (2637768)SDR LR7A2023020803273Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND RH UPPER FUSELAGE SKIN CRACKED AT FS199, RBL25, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. NR# 1000897294. / PSE# 53-30-08, AD 2012-06-09SDR LR7A2023020803272Skin · dentedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND LH FUSELAGE SKIN DENTED AT FS347, RBL79, WL230. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000897290. / PSE# 53-40-08, AD 2012-06-09SDR LR7A2023020803271Skin · dentedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND LH FUSELAGE SKIN DENTED AT FS347, LBL79, WL230. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 100897286. / PSE# 53-40-08, AD 2012-06-09SDR CALA2023022000493None · corrodedFWD CARGO PIT R/H FR28 BETWEEN STRINGERS 41R-42R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292691/40691 G ENERATED BY V919150SDR CALA2023022000492None · corrodedFWD CARGO PIT R/H FR30 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292695/40695 G ENERATED BY V919150SDR CALA2023022000491None · corrodedFWD CARGO PIT R/H FR32 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT PER HAECO LCQ NON ROUTINE 9292696/40696 GENERATED BY V91 9150SDR CALA2023022000489None · corrodedFWD CARGO PIT R/H FR29 BETWEEN STRINGERS 42R-43R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292694/40694 G ENERATED BY V919150 REMOVED AND REPLACED CLEAT AT FWD CARGO PIT R/H FR29 BETWEEN STR G42R AND STRG43R IAW A320 SRM 51-72-11-911-00SDR CALA2023022000488Cleat · corrodedFWD CARGO PIT R/H FR28 BETWEEN STRINGERS 42R-43R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292690/40690 G ENERATED BY V919150 REMOVED AND REPLACED CLEAT AT FWD CARGO PIT R/H FR28 BETWEEN STR 42R AND STRG 43R IAW A320 SRM 51-72-11-911-00SDR SWAA2023032304774Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN 2023-116966<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEE
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