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 DALA2022082505742None · noneSHIP 3402 DURING PRE-DEPARTURE CHECK IN SLC, MTC FOUND A DENT ON THE FUSELAGE SKIN, FORWARD OF THE FWD CARGO DOOR LOCATED BETWEEN FR18 TO FR19 AND STR26RH TO STR27RH. THE DENT MEASURES APPROXIMATELY 0.77-INCHES (FWD/AFT) X 1.27-INCHES (UP/DOWN) X 0.10-INCHES (SDR DALA2022082505729None · none(LOG 2379188) DURING INSPECTION FOUND CRACKS WERE FOUND ON RH FUSELAGE SKIN WITH REPAIR TRIPLER AT FRAME STA 540 ON TWO FASTENER HOLES. CRACKS ON RH FUSELAGE SKIN WITH REPAIR TRIPLER AT FRAME STA 540 WERE REPAIRED PER ER/A 600988-14AD.SDR CALA2022082402156Frame · corrodedFOUND CORROSION AT STR 26R END FITTING AT FRAME FR70. SEE ATTACHED PICTURES. PICS ADDED DAMAGE IS 9 INCHES LONG PROTEUDIMG FORWARD FROM FRAME 70 ON CORROSION LOCATION IS ON FRAME 67-STRINGER 27 SRM ENGINEERING UPDATE, IT IS STR 26R STRINGER 26 R/H 53-41-13-50SDR DALA2022091606156None · noneSHIP 1817 ERA 601237-14 ISSUED FOR A REPAIR TO BS955, LBL90 / CANTED PRESSURE BULKHEAD WEB / HEAVY CORROSION. CORRECTIVE ACTION: DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED AT OR BEFORE 29999 TOTAL CYCLES. ASSOCIATED ER/A 00-601237 ADDED FOR AC 1817 (2378297SDR YENA2022090100849Skin · dentedFLT#8583, JFK-MCN. 'W/O 1198428 ASSIGNED, AFT JACK PAD AREA DAMAGE REPAIR, W/O 1198975. ENCOMPASSED IN EAMS WO H8790; ACFT REG:323JB ACFT SN: 19000384, ACFT TAT: 30828.31, ACFT TAC:20363, COMPLIED WITH THE FOLLOWING INSPECTIONS: MISC WORK/ AIRCRAFT DROP IN PERSDR FDEA202208222344Skin · corrodedEXTERIOR FUSELAGE; STA. 2130-2160 LH AFT HORIZONTAL FAIRING 337DF HAS SKIN CORROSION UNDER LOWER FILLET SEALANT. DOT # 38 REMOVAL OF FILLET 337DF = N00968. REMOVED CORRODED SKIN SECTION AND REPAIRED WITH DOUBLER AND 3 FILLERS REF SRM 53-70-01-2R,FIG 201 SDR R61A2022092000558Waste Box · corrodedDURING HEAVY MAINTENANCE FOUND AFT WASTE BOX CORRODED. AFT WASTE BOX REMOVED AND REPLACED WITH NEW PART IAW ERJ170 SRM 51-43-02SDR SWAA2022090944332Skin · crackedCRACK ON INTERNAL SKIN OF EQUIPMENT ACCESS DOOR 2022-427230 / [01] REPLACED INTERNAL SKIN OF EQUIPMENT ACCESS DOOR AND FASTENERS IAW B737-700 SRM 51-10-02 AND DWG 141A6713 SHEET: 2 REV: - AND DWG 141A6710 SHEET: 7 REV: B;[02] REPLACED INTERNAL SKIN OF EQUIPMENSDR SWAA2022090644670None · crackedCRACK WEB - INTERCOSTAL LOCATED BS500A TO 500B STR 26R FWD CARGO COMPARTMENT 2022-410309 / [01] PERFORMED DVI ON WEB - INTERCOSTAL LOCATED BS500A TO BS 500B STR 26R FWD CARGO COMPARTMENT AND NOT FOUND CRACK ONLY PROTECTIVE TREATMENT DAMAGED IAW SRM B737-700 51SDR VNAA202208251111Skin · damagedFUSE SKIN BLENDS FS240 & FS280, STR25R €“ STR26R. TWO SEPARATE DAMAGES ON BELLY AT FS 240 AND FS280 REQUIRED TEMP REPAIR AFTER BLENDING. C/W EA 22-C9-53-1012 , REV IR FOR PERMANENT REPAIR.SDR R61A2022082500518Skin · dentedADDITIONAL DENT AND SCRATCH DAMAGE OBSERVED TO PREVIOUS LIGHTNING DAMAGE REPAIR BETWEEN FR 16-17 AND ST20L-21L.REPAIRED AREA IAW ETD 2022-170-026653 REV B MAJOR REPAIR AC WAS RETURNED TO SERVICE ON 8-23-22SDR DALA2022082305707None · noneAIRCRAFT 3009, FUSELAGE SKIN DENT BETWEEN FR 5-FR6 BELOW FO SIDE WINDOW. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO DENTED ARE PER A321 SRM 53-11-11-300-041. LP 2376488, 1849814SDR DALA2022082305705None · noneSHIP 3406 . DURING THE DRILL-OUT PROCEDURE, THE UNDERLYING STR-7R WAS CONTACTED BY THE DRILL. THE SUBJECT STRINGER HAS DRILL START TOOLING DAMAGE ON THE SKIN ATTACH FLANGE OUTER RADIUS AREA. CORRECTIVE ACTION: REF ER/A 601711-14. (2376578)SDR AALA202209221880Skin · puncturedAIRCRAFT IN BASE MAINTENANCE: PARTS RACKS ITEM - FUSELAGE, WING TO BODY PANEL 194FR HAS A PUNCTURE IN OUTER SKIN AS MARKED. REPAIRED FUSELAGE WING TO BODY PANEL 194FR IN ACCORDANCE WITH SRM: 53-60-70-2R-1 AND 51-70-05.SDR DALA2022082305701None · noneSHIP 5640 SKIN PANEL DAMAGED FROM TAIL STRIKE STA 1701-1720 OBL. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/003 00003 REPAIRED SKIN STA 1700 TO 1720, S-29L TO S-29R, TAIL STRIKE DAMAGE PER ER /A 601450-14 REV. A. PRI 601450SDR DALA2023081006526Unknown · unknownSHIP 5640 FUSELAGE / SKIN STA 1700 TO 1720, S-29L TO S-29R / TAIL STRIKE DAMAGE. CORRECTIVE ACTION: REF ERA 601450-14. (2372527)SDR SWAA2022091343891Gusset · crackedCRACK GUSSET STA. 500D AND STR 19L FWD CARGO COMPARTMENT 2022-456450 / [01] REPLACED GUSSET LOCATED AT STA 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 143A7902; SHEET: 174; REV: -<BR>SEE INDIVIDUAL SIGNS-OFF BSDR SWAA2022091243836None · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER LOC FWD LOWER CUTOUT AT LOWER FUSELAGE 2022-447082 / [01] TOOL USED CALIPER P/N: 500-197-30; S/N: A21143439; DUE DATE: 11-OCT-22.;[02] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[03] TOOL EDDY CURRENT USESDR SWAA2022082943486Web · crackedREJECT SUPPORT ZEE INSTALLATION DUE TO FOUND CRACK AT WEB LOCATED BETWEEN BS. 400 AND BS. 420 LBL23 WL156.5 2022-423375 / [01] REPLACED WEB LOCATED BETWEEN BS. 400 AND BS. 420 LBL23 WL156.5 IAW SRM B737-700 51-40-02 AND DWG 143A7505 REV B<BR>SEE INDIVIDUAL SIGSDR SWAA2022082643480Intercostal · crackedCRACK ON ACB INTERCOSTAL BS440 LBL24 / [01] UPDATED FAULT ENTRY : CRACK ON FCB INTERCOSTAL BS440 LBL 24;[02] EVALUATED FCB INTERCOSTAL BS440 LBL24 IAW SRM 53-00-53-1A-2 PARAGRAPH 4C. AND FOUND TO BE OUT OF LIMITS L=0.8'' TOOL USED DIGITAL CALIPER ID:ATS2738 S/SDR DALA2022082305710None · none(LOG 2371826) DURING INSPECTION FOUND CRACK ON LOWER PLATE, STA 230 APPROX. AT EXTERNAL PWR RECEPTACLE AREA. CRACK ON LOWER PLATE STA 230 APPROX AT EXTERNAL PWR RECEPTACLE AREA WAS REPAIRED PER B737-900ER SRM 53-10-15-2R PROCEDURE 4.SDR DALA2022082305702None · noneSHIP 5640 TAIL JACKING FITTING PN 148N9320-1 DAMAGED DUE TO TAIL STRIKE. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/016 00016 REPAIRED TAIL JACK FITTING REF ERA 601447-14 REV ORIG. PRI 601447-14 REVS 0-1 MATCH ERA 601447-14SDR DALA2022082305686None · noneSHIP 691 DAMAGE FOUND TO FUSELAGE SKIN AT STA 620 STR 16L. CORRECTIVE ACTION: CUT OUT DAMAGE SKIN REF B757-200 SRM 53-00-01-2R-28. PERFORMED HFEC AND BFEC PER B757 NTDM PTG6 51-00-19 & 51-00-16 NO DEFECTS NOTED. FABRICATED REPAIR PARTS REF B757-200 SRM. TREATESDR IPXA2022081985412Skin · dentedINSPECTION TYPE:SEG2EXTERIOR CROW AREA STA 620-640 BL 0 RIVET HEAD HAS A LIGHTNING STRIKE. DURING AN IDT INSPECTION FOUND A DENT IN THE AREA.WORK PER UPS EO B757-5330-84515-A, UPS RCD 279212 AND VT MAE EA 757-5330-27-A3000 REV-SDR DALA2022122108274None · noneSHIP 3262 ER/A 596975-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQUIRED. (CRACK INSP) CORRECTIVE ACTION: COMPLIED WITH REVISION. (2370920)SDR SWAA2022083043482None · brokenPANEL BREAK ASSEMBLY BROKEN AT STA540 WL208 LBL 0-25 / [01] REMOVED DAMAGED PANEL BREAK ASSY AT STA540; WL 208; LBL 0-25 AND LOCATED/DRILLED NEW PART.;[02] VERIFIED CORRECTIVE ACTION 1. OK TO INSTALL NEW PANEL BREAK.;[03] INSTALLED NEW PANEL BREAK ASSY AT STA5SDR SWAA2022082642969None · crackedCRACKED INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24 / [01] CRACKED INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24; WL 154; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0GSDR DALA2022081905633None · noneSHIP 5640 BEAR STRAP WORN JUST AFT OF STA 1763 BETWEEN STR 29L/29R. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:0514-2001/026 00026 REPAIRED PER B757 SRM. (2370963)SDR SWAA2022093065320Access Panel · damagedLEFT WING LOWER AFT FAIRING ACCESS PANEL #194CL; SEVERAL SCREW HOLES ELONGATED WITH SURFACE BULGE. / [01] PREPARED AND CLENED REPAIR AREA TO APPLY THE FABRIC REPAR PLIES; NO WATER NOTE ON REPAIR AREA AT AFT FAIRING ACCESS PANEL 194CL. REF B737-700 SRM 51-70-04SDR SWAA2022090642973None · elongatedELONGATED HOLE WEB - INTERCOSTAL LOCATED BTW STA 400 TO STA 420 STRINGER 25L AT FWD CARGO COMPARTMENT 2022-410300 / [01] REPLACED WEB INTERCOSTAL LOCATED BTW STA 400 TO STA 420 STRINGER 25L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 143A7505 RSDR SWAA2022082942788Doubler · crackedPOWER RECEPTACLE DOOR AFT FLANGE DOUBLER CRACKED REPAIR FILLER / [01] REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0;[02] VERIFIED MATERIAL ID FOR REPAIR DOUBLER IS 2024 T3 .050 TAG# A02062 IAW SRM 53-10-15-2R-4;[03] VERIFIED STEP 2 C/W;[04] FABRICATED REPAIR DOUBLSDR FDEA202208172054Skin · corrodedMAIN DECK STA APROX STA 1220 RBL 50 TANK SURFACE HAS CORRSION RBL 38. REMOVED COROSSION FROM MAIN DECK APPROX SAT 1220 RBL 50 TANK SURFACE SKIN RBL 38. REPAIR WITHIN LIMITS AND RESTORED FINISH REF. MD-11 SRM 51-21-01-07-0 AND MD-11 SRM 57- 10-01-1.SDR FDEA202208172053Skin · corrodedUPPER CARGO COMPT. RH JUST BELOW R3 DOOR BETWEEN STA.1278 TO STA.1298 UNDER FLOOR HAS CORROSION EMANATING FROM FASTENER HEAD. REMOVED CORROSION FROM UPPER CARGO BAY RT BS 1278 - 1298 BELOW R3 DOOR. AREA FOUND TO BE WITHIN LIMITS IAW SRM 51-21-01-07-0 AND SRSDR U2RA2022082300044Door Frame · damagedDURING HEAVY MAINTENANCE VISIT, 2EA CRACKS WERE FOUND AT RH #5 ENTRY DOOR AFT UPPER CORNER BY OPEN HOLE INSPECTION AS PER SB 747-53A2839 REV IR, PART 4. THE CATEGORY B REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH HAECO XIAMEN'S ENGINEERING NOTES EB-53-2861 REV ISDR SWAA2022092802973Gusset · crackedFWD CARGO COMP STA 500D SRT 19L GUSSET CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19L; AS PER B737-7 SRM 51-40-02.;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET P/N 143A9483-6;[03] INSTALLED NEW GUSSET AT FWD CARGO COMP STA 500D SRTSDR SWAA2022092802974Gusset · crackedFWD CARGO COMP STA 500D SRT 19R GUSSET APPEARED CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19R; AS PER B737-7 SRM 51-40-02.;[02] OK TO INSTALL NEW GUSSET;[03] LATE ENTRY VERIFIED STEP 1;[04] INSTALLED NEW GUSSET AT FWD CARGO COMP STASDR SWAA2022091542520Shield · corrodedAFT CARGO COMP ;DOOR CUTOUT FWD SHIELD CORRODED / [01] REMOVED CORROSION AT AFT CARGO COMP ;DOOR CUTOUT FWD SHIELD PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW B737 NDT PART 4; 51-00-00; PROCEDSDR SWAA2022091542513Gusset · crackedFWD CARGO COMP STA 500D SRT 19R GUSSET APPEARED CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19R; AS PER B737-7 SRM 51-40-02.;[02] OK TO INSTALL NEW GUSSET;[03] LATE ENTRY VERIFIED STEP 1;[04] INSTALLED NEW GUSSET AT FWD CARGO COMP STASDR SWAA2022091542512Gusset · crackedFWD CARGO COMP STA 500D SRT 19L GUSSET CRACKED / [01] REMOVED CRACKED GUSSET AT FWD. CARGO COMPT. BS 540D; S-19L; AS PER B737-7 SRM 51-40-02.;[02] VERIFIED STEP 1. OK TO INSTALL NEW GUSSET P/N 143A9483-6;[03] INSTALLED NEW GUSSET AT FWD CARGO COMP STA 500D SRTSDR SWAA2022091342593None · crackedCUSTOMER REQUEST CRACK ON LOWER AREA EXTERNAL POWER DOOR CUT OUT AT LOWER FUSELAGE 2022-456271 / [01] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N:B16101278 ; DUE DATE :26-OCT-22;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503 DUSDR AALA202208220488Skin · dentedAIRCRAFT IN BASE MAINTENANCE: RIGHT FUSELAGE AT STA 247 JUST ABOVE STR 24 R FOUND A DENT. PERFORMED EXTERNAL DOUBLER REPAIR PER EA 337550.SDR SWAA2022090741411Attach Angle · crackedCRACK ON FWD CARGO BAY O/B BAFFLE TO FRAME ATTACH ANGLE AT RBL 24 BS 500H+1. / [01] CLIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED FWD CARGO BAY O/B BAFFLE TO FRAME ATTACH ANGLE AT BS 500H+SDR SWAA2022090741402Baffle · crackedCRACK ON FWD CARGO BAY O/B BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500H+1. / [01] CLIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED BAFFLE ANGLE AT BS 500H+1 LBL 24 PER SRM 51-40-02-0G-0;[04SDR SWAA2022083041422Angle · crackedCRACK DOOR 315A ANGLE LOCATED AT LEVEL BS 1125 AT BL0 ON APU COMPARTMENT 2022-418585 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23.;[02] REPLACED LOC. DOOR 315A AT LEVEL BS 1125 AT RBL 0 ON APU COMPARTMENT IAWSDR CALA2022081602090Skin · damagedFUSELAGE SKIN DAMAGED AT FR26 BETWEEN STR 38-39 LEFT. GENERATED BY V913126 ON HAECO LCQ NR 9298041/28041 X=.900 AND Y=.200. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-21- 703 FR24 THRU FR35 ZONE A THE INSPECTION THRESHOLD FROM TIME OF INSPECTION UNTIL 60,000 FC SDR CALA2022081602089Skin · dentedFUSELAGE SKIN DENTED AT FR26 JUST BELOW STR 29 LEFT. GENERATED B Y V913126 ON HAECO LCQ NR 9298042/28042 X=.900, AND Y=.900. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-21- 073 FR24 THRU FR35 ZONE A INSPECTION THRESHOLD FROM TIME OF ADL/ UNTIL 60,000FC/120,000FH SDR CALA2022081602088Skin · dentedFUSELAGE SKIN DENTED AT FR 19 RH BETWEEN STR 37-38R. GENERATED B Y V913126 ON HAECO LCQ NR 9298043/28043 =.150, Y=.800. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-11-11- FR1 THRU FR24 ZONE F INSPECTION THRESHOLD FROM TIME OF REPAIR 60,000 FC/ 120,000 FH AT INTERSDR CALA2022081602067Frame · corrodedDURING HMV VISIT AFT CARGO COMPT. PREVIOUS REPAIR HAS CORROSION BETWEEN FR 63-64 & STR. 41L-42L, NEW REPAIR ACCOMPLISHED PER SRM 53-00-11-300-029. LOG CREATED FOR DIP TO BE ACCOMPLISHED PER SRI 53-00-11-205-017. SUBSEQUENT INSPECTIONS AT INTERVALS OF 2200FC/44SDR CALA2022081602064Skin · damagedNO DOCUMENTS FOUND DURING THE AAI RECORD REVIEW AND INSPECTION FOR THE FUSELAGE EXTERNAL REPAIR DOUBLER AT APROX STATION 1060, STR 15R-18R, CUSTOMER REQUEST (UAL QC) (REF AAR NR 99940419) COMPLIED WITH EA NO. 22195, REV P2 AND EC/RA 5331-C2929 (WORK AC COMPLISSDR UIEA2022081000853Skin Panel · burnedLH FUSELAGE AFT STATIC PORT THREE BURN MARKS(<P>BURN MARKS WERE REPAIR BY BLENDING OPERATIONS IAW TRE6753549 REV 0</P>)
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