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 CALA2024071600204Skin · damagedLIGHTNING STRIKE DAMAGE, 14.5 INCH AFT STATION 500F BTW STRINGER 27L & 27R REMOVED LIGHTNING STRIKE DAMAGE REF. SRM 53-00-01-2R-38 4-D-(2) HFEC REQUIRED REF. SRM 53-00-01-2R-38 4-D-(3) ACP. HFEC IAW WITH SRM 53-00-01-2R-38 STEP 4D (3) & B737 NTM PART 6 51-00-SDR CALA2024071600206Skin · damagedLIGHTNING STRIKE DAMAGE, 12.5 INCH AFT STATION 500J BTW STRINGER 27L & 27R REMOVED LIGHTNING STRIKE DAMAGE REF. SRM 53-00-01-2R-38 4-D-(2) HFEC REQUIRED REF. SRM 53-00-01-2R-38 4-D-(3) ACP. HFEC IAW WITH SRM 53-00-01-2R-38 STEP 4D (3) & B737 NTM PART 6 51-00-SDR CALA2024071600203Skin · damagedLIGHTNING STRIKE DAMAGE, 14 INCH AFT STATION 500G BTW STRINGER 27L & 27R. REMOVED LIGHTNING STRIKE DAMAGE REF. SRM 53-00-01-2R-38 4-D-(2) HFEC REQUIRED REF. SRM 53-00-01-2R-38 4-D-(3) ACP. HFEC IAW SRM 53-00-01-2R-38 STEP 4D (3) & NTM PART 6 51-00-00 PROCEDURSDR SWAA2024082212591Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 214 AT LT WING 2024-443668<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 214 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 TOOL USED CALIPER P/N: 500-196-30 S/N: B23353457 DUE DATSDR DALA2024071607198Skin · unknownSHIP 684 DTE, ERA 618773-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN AT C2 CUTOUT, LOWER AFT CORNER. CORRECTIVE ACTION: REF ERA 618773-14. (0447815)SDR DALA2024071607169Skin · dentedC/W ER/A 610260-14 REV B FUSELAGE SKIN DENTS. SUMMARY SEE NRC 004-0001:10-0653-8-7621/002 00006: COMPLIED WITH ER/A 610260-14 REV B. PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ER/A 610260-14 REV B. PRI REV "0", "SDR CALA2024071602045Skin · damagedACCOMPLISH INSPECTION REQUIREMENTS ON THE LH FWD FUSELAGE FR4-6 SKIN PANEL REPAIR PER PART 2 OF THE LATEST REVISION OF ECRA 5311-03240. 5311-03240 ON OR BEFORE 96,489 TOTAL AIRCRAFT FLIGHT CYCLES OR 211,952 TOTAL AIRCRAFT FLIGHT HOURS, WHICHEVER OCCURS FIRST. SDR ASAA2024071352595Skin · gougedFUSELAGE SKIN GOUGED 10 IN LEFT OF LOWER CENTER LINE AT FR 31 GROUNDED - YES. ACCOMPLISHED FUSELAGE SKIN PANEL FR 31 STGR 42LH DOUBLER REPAIR PER ASA EA #A320-53EA-02245 REV 00SDR VNAA202409010029Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. CORRECTIVE ACTION: SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-569 REV -SDR VNAA202409010028Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING. SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-71-079 REV -SDR CALA2024072602115Skin · corrodedLOWER FWD FUS, INSIDE AND SKIN AROUND OF HARDWARE HOLES WITH CORROSION EVIDENCE ON TCAS ANTENNA PERFORMED REPLACED OF DAMAGES PART AND REPAIRED I.A.W. EC/RA 532 1-02146 FORM 44-0008 ATTACHED WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 106734SDR YENA2024071601022Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / WASTE ACCESS DOUBLER AND BOX BETWEEN FR75-76 & STGR 31L-36L / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AIRBUS REO-500-53-61-1294 REV -- /2/ CRC 155507 /3/ AVIANOR NON-ROUTINE TASK CARD A49106-1035 DESCRSDR NACA2024071200004Skin · corrodedSURFACE CORROSION ON AFT CARGO DOOR LOWER AND AFT CUT OUT CORNER SKIN UNDER AFT SCUFF PLATE AT BS847 BETWEEN S23R AND S24R. REPAIRED CORROSION IAW SRM 53-60-01SDR VNAA202409010017Skin · corrodedCORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT WAS REMOVED AND FOUND WHITHIN LIMITSSDR SWAA2024082212151Support Angle · crackedCRACK ANGLE - SUPPORT STA 947.5 AND STR 26L AT AFT CARGO COMPARTMENT 2024-443560<[01] TOOK MEASURE OF CRACK IS : 0.750? ON ANGLE - SUPPORT ON STA 947.5 AND STR 26L AT AFT CARGO COMPARTMENT TOOL USED :CALIPER P/N: 500-197-30; S/N: A18135108; DUE DATE: 12 -JUL-2SDR SWAA2024081312036Skin · corrodedLWR FUSELAGE SKIN - FWD ANTENNA COVER PLATE AND SKIN HAVE EVIDENCE OF CORROSION AT STA 410; STR 27L.<[01] PARTIAL UPDATED STEPS 1 AND 2.;[02] JOB COMPLETE.SDR HNAA2024080900657Doubler · corrodedE044964 CENTER FUSELAGE 4, THE POTABLE WATER SERVICING PORT DOUBLER HAS CORROSION. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE CENTER FUSELAGE 4, THE POTABLE WATER SERVICING PORT DOUBLER IAW EMB145 SRM 51-40-02.SDR IPXA2024071877503Skin · corrodedCORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) PERFORM NDT INSPECTION I.A.W EGAT EI NO.F2024A53M-1771 SEQUENCE B PARTA STEP 1.2)~1.4)SDR YENA2024071601008Skin · crackedDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR54-64 & STGR 37L-38L / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9012-24 COVER AND P1-P3 /2/ AIRBUS RDAF 80524263/050/2024 ISSUE A /3/ AIRBUS TD/80524263/054/2024#A /4/ AIRBUS RDAF 8052426SDR CALA2024071600199Skin · damagedMULTIPLE SMALL DENTS ON FUSELAGE RIGHT FWD SIDE BELOW COCKPIT NEAR AAVIONICS VENT DOOR. STRINGER 30, FRAME 16, RT SIDE OF A/C. STRIPPED PAINT FROM AREA, EXPOSING EVIDENCE THAT DAMAGE IS ON THE SHEET METAL SURFACE. APPEARS TO BE MINOR ABRAISIONS CAUSED BY A SSDR DALA2024071507156Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK ON OPEN POSITION. ALSO FWD PREVIOUSLY REWORK DOES NOT MEET WITH RADII. SUMMARY OF NRC 175: EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK WAS REPAIRED PER PRI 618669-SDR NACA2024071100002Skin · crackedWHEN PERFORM NDI CHECK , FOUND CRACK (0.1" IN LENGTH) ON FUSELAGE SKIN AT STA 258.5 S-21L.. REPAIRED CRACK IAW SRM 53-10-01SDR HNAA2024090400217Doubler · corrodedAT FR61 LH DOUBLER UNDER CARBON FRAME FOUND CORRODED.SDR HNAA2024090400216Skin · crackedRF1, LH SIDE OF FR68 FOUND CRACKED UNDER CARGO DOOR HOLDER FITTING.SDR SWIA202408270711Skin · dentedADM # 7958 3.75" FWD OF FS-295, 1" UP FROM STGR-23R. RIGHT SIDE OF A/C AT 5 O'CLOCK POSITION, FWD OF STATIC PORT. 1.5" DIA X 0.020" DEPTH. DENT LOCATED 3.75" FWD OF FS-295, 1" UP FROM STGR-23R. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWOSDR SWAA2024082311688Access Panel · damagedELONGATED HOLE ACCESS PANEL 194BR BODY FAIRING AT FUSELAGE EXTERIOR 2024-443478<[01] TOOL USED: CALIPER PN: 500-464; SN: B17030933; DUE DATE: 07-NOV-24.;[02] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196021 DUE DATE:15/FEB/25;[03] ULTRASONIC EQUIPMENT USED PSDR SWAA2024080911642Doubler · corrodedFUSELAGE BILGE STA 360 STR 27L SKIN DOUBLER HAS A SPOT OF CORROSION.<[01] ACCOMPLISHED SWA EA 25-153-01978 THAT PROVIDES INSTRUCTIONS TO REMOVE THE DAMAGE; ACCOMPLISH REQUISITE INSPECTIONS; AND APPLY REQUISITE FINISHES.;[02] CERTIFIED WORK STEPS ACCOMPLISHED.SDR CALA2024071102009Skin · crackedEA 5315-01152 OP001 - 1EA FASTENER HOLE FOUND CRACK ON L1 DOOR CUTOUT AFT CORNER AREA , DETAILS REFER TO ATTACHED REPORT TRANSFER REF HXWO 3270748. L1 DOOR CUTOUT AFT LOWER CORNER LH FUSELAGE SKIN INTERIM REPAIRED AS PER ECRA 5310-08353 REV - PART 1 INTERIM RSDR SWAA2024082211338Access Panel · corrodedCORROSION STRUCTURE INTERNAL AREA OF THE ACCESS PANEL 311BL AT LOWER FUSELAGE. REPLACED ACCESS PANEL 311BL AT LOWER FUSELAGE IAW B737-700 AMM 52-49-11-400-802 MEASURE CLEARANCE WITHIN LIMITS. TASK CARD COMPLETE.SDR R61A2024081700364Skin · corrodedCF3 LOWER SKIN PNL FOUND CORRODED HINGE WASTE DOOR FR 88 BTWN STR 27-28RH. MX REPLACED PN 170-85089-401IAW SRM 51-41-02SDR R61A2024081700362Skin · dentedFWD FUSE EXT LOWER SKIN FOUND DENT AFT FR 6 BTWN STR 23-24-LH. REPAIRED IAW ETD2024-019834.SDR CALA2024072302084Skin · dented(SUPPORT TASK) R/H FUSELAGE STA 251.5 AT STRINGER 17R SKIN IS DENTED. TRANSCRIBED FROM HAECO GSO NR 9286031 EVALUATE DENT AND FOUND W= 2.0 Y= .080 W/Y= 25 OUT OF LIMITS IAW B737-900ER SRM 53-00-01-1A FG. 103. FABRICATED FUSELAGE SKIN REP AIR AND INSTALLED IAWSDR DALA2024071907285Doubler · corroded(LOG 0452940) CORROSION ON EQUIPMENT COOLING EXHAUST DUCT DOUBLER STA 360-380 BL 0. REMOVED CORRODED EQUIPMENT COOLING EXHAUST DUCT DOUBLER, FABRICATED A NEW DOUBLER FROM 2024 T3 .050" LOT# 5142707-1, AND INSTALLED NEW DOUBLER IAW B737 SRM 51-40-02-0G-0 AND BOSDR VNAA202407120040Skin · chafedHN00147837 DISCREPANCY: FUSELAGE OUTER SKIN IS CHAFED UNDER AFT LAV. RINSE/FILL PORT. CORRECTIVE ACTION: FOUND AN EXTERNAL REINFORCING DOUBLER AROUND CANNON PLUG PL118J1 TO BE CHAFED. NOT THE EXTERNAL SKIN. COMPLIED WITH REMAINING STEPS OF REO 670-53-51-281 RESDR UIEA2024071000608Skin · crackedCRACK ON THE FUSELAGE EXTERNAL SKIN BETWEEN STA 1721 AND STA 1740, AT S-41L.(<P>1. ACCOMPLISHED EI NO T2024A53M-1336 REV 2. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)SDR SWI2025F00126Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55221-ETD2019-170-149640 MXCODEID50168-PR - 116 DENTS ON FUSELAGE SKIN P/N 170-91885-001 BETWEEN FRAME 86 AND FRAME 90 AND STRINGER 3R AND STRINGER 3L ADDRESSED IN PREVIOUS CAMP ITEMS 1 TO 120 FOUND TO BE WITHIN TEMPORSDR SWI2025F00125Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55189-ETD2019-170-147980 MXCODEID50162-PR - 37EA DENTS ON FWD R/H LAT FUSELAGE SKIN P/N 170-03385-004 BETWEEN FR 01-06 AND STGR 08R-18R FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PER ETD2019-170-147980 REV :B FOR 7,SDR SWI2025F00124Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55188-ETD2019-170-154045 MXCODEID50159-PR - FOUND (90 EACH) DENTS ON UPPER FUSELAGE CTR III SKIN PANEL P/N 170-65304-003. FR 74-90 STGR 2L-5L, FOUND TO BE WITHIN TEMPORARY ALLOWABLE LIMITS, PER ETD, FOR 7500 FC. AS OSDR SWI2025F00123Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55186-ETD2019-170-154033 MXCODEID50155-PR - 19 DENTS ON FWD FUSELAGE LH SKIN PANEL BETWEEN X=3845.0 AND FRAME 14, STRINGERS 1L TO 6L, IS WITH IN LIMITS PER REF ETD2019-170-154033. TEMPORARY ALLOWABLE DAMAGE IS VALID FOSDR SWI2025F00122Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55185-ETD2019-170-149409 MXCODEID50153-PR - 300 DENTS ON FUSELAGE SKIN P/N 170-03765-005 BETWEEN FRAME 16 AND FRAME 20 BETWEEN STRINGER 1R AND STRINGER 12R ADDRESSED IN PREVIOUS CAMP ITEMS 1-300 FOUND TO BE WITHIN TEMPSDR SWI2025F00135Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55103-ETD2019-170-153360 MXCODEID50111-PR - DENTS (99 EACH) ON FOWAED FUSELAGE UPPER SKIN PANELS FRAMES 12-21 STRINGERS 05L-05R, FOUND TO BE WITHIN TEMPORARY ALLOWABLE LIMITS, PER ETD, THIS REPAIR IS VALID FOR 7500 FC SDR SWI2025F00134Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55096-ETD2019-170-152141 MXCODEID50106-PR - DENTS (20 EACH) ON CENTER FUSELAGE II AFTER PLUG SKIN P/N 170-20995-003 FROM FR 60-73 AND FROM STGR 5R-8R, FOUND TO BE WITHIN TEMPORARY ALLOWABLE LIMITS, PER ETD, FOR 7500 FCSDR SWI2025F00133Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55093-ETD2019-170-152965 MXCODEID50101-PR - 44 DENTS ON FUSELAGE SKIN P/N 170-03587-003 BETWEEN FRAME 13 AND FRAME 15 AND BETWEEN STRINGER 1R AND STRINGER 6R ADRESSED IN PREVIOUS CAMPS 1 TO 7 FOUND TO BE WITHIN TEMPORASDR SWI2025F00131Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55053-ETD2019-170-152214 MXCODEID50083-PR - 376 DENTS IN CF I UPPER SKIN PANEL P/N 170-92584-003 FR 23-34 STR 04L-04R AND FR23-FR30 FROM STR 2R-4R DENTS FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PER ETD2019-170-1SDR SWI2025F00140Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55029-ETD2019-170-152197 MXCODEID50066-PR - 69 DENTS ON FWD FUSEALGE TOP SKIN PANEL PN 170-20871-003 FR 21-22 STR 04R-4L FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PER ETD2019-170-152197 FOR 7,500 FC. PERMANENT DUESDR SWI2025F00139Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54963-ETD2019-170-152149 MXCODEID50007-PR - 1,669 DENTS ON CENTER FUSELAGE II UPPER CENTER SKIN BETWEEN FR 43-59 AND STGR 05L-05R ,P/N 170-01982-007. DENTS FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PER ETD2019-170-SDR SWI2025F00138Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54962-ETD2019-170-152101 127SY MXCODEID50003-PR - 759 DENTS FOUND ON CENTER FUSELAGE I RH UPPER LATERAL SKIN PN 170-67306-006, FROM FR 23-34, AND FROM STR 4R-11R FOUND TO BE WITHIN TEMPORARY ALLOWABLE LIMITS, PER ETD, SDR SWI2025F00137Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54885-ETD2019-170-152110 MXCODEID49962-PR - 642 DENTS FOUND AT CENTER FUSELAGE II SKIN PN# 170-02041-010 FRAMES 59-43 AND STGRS 5R-18R FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PER ETD2019-170-152110 FOR 7,500 FC.SDR SWI2025F00143Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54935-ETD2019-170-152056 MXCODEID49982-PR - FOUND 33 DENTS ON FWD FUSELAGE RH SKIN P/N 170-03387-002 BETWEEN FRAMES 9-12 STGR 12R-17R. DENTS FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PER ETD2019-170-152056 FOR 7,SDR SWI2025F00142Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54925-ETD2019-170-152158 MXCODEID49971-PR - FOUND 508 DENTS AT RH AFT FUSELAGE SIDE SKIN PANEL (CTR. FUSE. III) PN# 170-65401-001 BETWEEN FRAMES 74-90 STGR 3R-9R. DENTS FOUND TO BE WITHIN TEMPORARY ALLOWABLE DAMAGE PE
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