JASC 5330
Service difficulty reports · 79,302
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 DALA2026010900236Skin · damagedFORWARD SIDE OF FRAME 64 TOOLING DAMAGE ON FUSELAGE SKIN JUST INBOARD OF P'1. REPAIRED TOOLING DAMAGE PER ERA 631298-14 REV. ORIG. (1392504)SDR DALA2026010900233Doubler · damagedAFT SIDE OF FRAME 61 TOOLING DAMAGE IN DOUBLER UPPER EDGE @ P5. REPAIRED TOOLING DAMAGE PER ERA 631298-14 REV. ORIG. (1392496)SDR DALA2026010900231Skin · damagedFORWARD SIDE OF FRAME 64 TOOLING DAMAGE ON FUSELAGE SKIN IN 2 PLACES JUST INBOARD OF P1. REPAIRED TOOLING DAMAGE PER ERA 631298-14 REV. ORIG. (1392488)SDR DALA2026010900224Doubler · damagedAFT SIDE OF FRAME 61 TOOLING DAMAGE ON DOUBLER AT P'5. REPAIRED TOOLING DAMAGE PER ERA 631298-14 REV. ORIG. (1392454)SDR SWIA2026010775283Screw · stuckPANEL 584EB HAS 1 EA STUCK SCREW. REMOVED DAMAGED RIB COMMON TO PANEL 584EB WITH 1EA STUCK SCREW REF SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A01 COMPLIED WITH REO 670-57-52-643 REV -A. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.SDR CALA2026012713354Skin · dentedDENT IN FUSELAGE OVER FWD HALF OF FRAME AT BS 259 JUST BELOW RI VET LINE FOR S17R REF AAR N/R 99979657. ACCOMPLISHED REPAIR AT FWD FUSELAGE BS 259 BETWEEN S16R AND S19R IAW SRM 51-40-02-0G-0 AND EC/RA 5310-08767.SDR DALA2026010800185Doubler · damagedAFT SIDE OF FRAME 60 TOOLING DAMAGE ON DOUBLER AT P'5. REPAIRED TOOLING DAMAGE PER ERA 631298-14 REV. ORIG. (1390706)SDR DALA2026010800174Skin · damagedFORWARD SIDE OF FRAME 60 TOOLING DAMAGE ON FUSELAGE SKIN AT P2. REPAIRED PER ERA 631298-14 REV. ORIG. (1390338)SDR DALA2026010800171Skin · damagedFORWARD SIDE OF FRAME 60 TOOLING DAMAGE ON FUSELAGE SKIN JUST OUTBOARD OF P3. REPAIRED PER ERA 631298-14 REV. ORIG. (1390306)SDR REXA2026052700708Skin · corrodedCORROSION ON INTERNAL SKIN FROM STA FS 364 TO 394 BTW STGR 25L-25R AT E/E COMPARTMENT DOOR CUTOUT INTERNAL SKIN FROM STA FS 364 TO 394 BTW STGR 25L-25R AT E/E COMPARTMENT DOOR CUTOUT WAS REPAIRED PER REO 690-53-21-032 REV. --SDR SWIA2026030975449Skin · crackedLH TRU DOOR CUT-OUT, THE AFT LOWER CORNER EXTERIOR SKIN POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 03/07/2026)REPAIRED THE LH TRU DOOR CUT-OUT EXTERIOR SKIN IAW ALL STEPS OF REO 670-53-11-2260 REV -- DATED 2026-01-28. M-337 AND SKYWEST TASK CARD 51-90SDR AALA202601123466Skin Panel · out of toleranceAIRCRAFT IN BASE MAINTENANCE: EVIDENCE OF REWORK, BLENDED AREA, TO EXTERNAL SKIN LOCATED BETWEEN BS 2087 AND 2129 AND BETWEEN S48L AND S49L AT LOWER FUSELAGE. AREA OUT OF LIMITS. ACCOMPLISHED DOUBLER REPAIR PER EA 371017.SDR SWIA202601080006Skin · damagedDURING LIGHTNING STRIKE INSPECTION FOUND 1 BURNED RIVET ON FR24 1ST RIVET BELOW STR22L. BURN DAMAGE IS 3/8 L X 3/8 W X 0.073 D AND OUT OF LIMITS PER SRM 53-00-00 REPAIR 03.DAMAGE IS OUT OF LIMITS AND THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR RSDR DALA2026010800162Skin · damagedPREVIOUSLY ACCOMPLISHED FUSELAGE SKIN REPAIR FS 760 - 780 BETWEEN STR 14L - 16L FASTENERS DRILLED INTO CHEM MILL EDGE. AREA WAS INSPECTED ON AMDS 2020-2466. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW REPAIR AT STA 760-780 BETWEEN STR 14L- 16L IAW B757-200 SRSDR SWIA2026010700006Skin · damagedDURING LIGHTNING STRIKE INSPECTION FOUND 1 BURNED RIVET ON FR24 1ST RIVET BELOW STR22L. BURN DAMAGE IS 3/8 L X 3/8 W X 0.073 D AND OUT OF LIMITS PER SRM 53-00-00 REPAIR 03.DAMAGE IS OUT OF LIMITS AND THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR RSDR FDEA202601050005Skin · crackedLEFT AFT FUSELAGE BS 1459-1461 (02EA) FASTENERS AFT OF BUTT SEAM BS 1459 ABOVE STR 20 AND DOUBLER THAT HAVE (02) POSSIBLE CRACKS INDICATION UNDER FASTENERS RUNNING PARALLEL OF THE DOUBLER DURING NDT HFEC INSPECTION COMPLIED WITH EA # F5330-T0385962 TITTLESDR DALA2026010500078Skin · gougedLOWER FUSELAGE EXTERNAL SKIN FOUND SEVERAL GOUGE MARKS AT BETWEEN FR54-55, STGR 45L-49L. REPAIRED PER SRM 53-41-11-205-002. (1386230)SDR R61A2026010500001Skin · damagedWHILE IN HEAVY CHECK. FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FR 1-2 AND STGR 2L-2RSDR SWIA2026010475894Skin · corrodedCORROSION ON INTERNAL FUSELAGE AT F.S589.00 AND STR24L.CORROSION ON INTERNAL FUSELAGE AT FS 589.00 AND STR24L IDENTIFIED AT FS589.00 FRAME FLANGE BETWEEN AND WEB BETWEEN STR24L-STR23L ALONG WITH STR24L FLANGE. REMOVED FASTENERS IAW SRM 51-42-06 AND BLENDED COSDR SWIA2026031175507Skin · dentedAFT FUSELAGE BELOW CARGO DOOR CUT OUT, JUST AFT OF BS 605 BELOW WL 73.50 DENTED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE ALL EVIDENCE USING STANDARD ACFT PRACTICES. COMPLIED WITH REO 601R-53-61-8479.SDR EE4Y2026010323693Skin · corrodedCUSTOMER REPORTS CORROSION DAMAGE AFFECTING THE CENTER FUSELAGE II SKIN INNER FACE, LOCATED IN THE STRG-29LH LOCATION, AT FR73+130MM. VERIFIED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT OF LIMITS IAW ERJ190 PART II SRM 53-22-01, AD51, PARAG. 5A (2), TASDR EE4Y2026010323690Skin · nickedPER CUSTOMER REQUEST MUST BE EVALUATED EXISTING NICKS LOCATED FROM FR15 TO FR17+100MM, BETWEEN STRG 26LH AND 26RH. 7. EVALUATED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT LIMITS PER ERJ190 PART II SRM 53-10-01, AD 51, PARG. 4B, TABLE 102, FIG. 101, SHESDR IPXA2026011219182Skin · cracked-CRACK, L1 ENTRY DOOR AFT LOWER CORNER OUTER SKIN CRACK (REPAIR) PERFORMED SRM 53-10-01-2R-1 REV.94 AND EGAT WORK SHEET NO.60004 STEP 26.SDR VNAA2026010611103Skin · dentedDENT BELOW CAPTAINS WINDSHIELD FROM BIRDSTRIKE BETWEEN FS210 AND FS 220 NEAR STR 12, IN THE FORM OF A IRREGULAR PENTAGON SIDES MESSURING 10" X 4-5/8"X 5-1/2" X 8" X 2-15/16" AND 0.25" DEEP AT THE DEEPEST POINT. PERFORMED PERMANENT REPAIR IAW REO 690-53-11-21SDR CALA2026010512656Skin · damagedDAMAGE FROM BAGGAGE CART AT RT SIDE OF FUSELAGE. BS 344-2 - 360+3, S20R-1 - S20R+10.5. MEASUREMENTS: HEIGHT: 7.3" WIDTH: 20.75" DEPTH: 0.24". INSPECTED AREA, THE DAMAGE BS 344 -360, S20R - S21R. STR 20R APPEARS TO BE BENT, CAUSING THE ATTACHING CLIPS ON BOTHSDR IPXA2026020211187Skin · gougedON ARRIVAL DAMAGE TO SKIN FOUND JUST AFT OF AFT CARGO DOOR. REMOVED STRINGER CLIPS IN COMMON TO REPAIR REF SRM 51-40-02. COMPLETED REPAIR IAW EO-96145.SDR AALA202601051733Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACKS FOUND RADIATING FROM THE FASTNER HOLE ON THE LH SIDE OF THE FUSELAGE SKIN BETWEEN FR 13 AND FR 14 AND Z+790 AND Z+950. MAINTENANCE EXTERNAL DOUBLER REPAIR. REF SRM 51-70-20, SRM 53-11-11-300-041, REPAIR DRAWING R53DSDR SWIA202601150231Skin · dentedAFT FUSELAGE HAS AN EXTERIOR SKIN DENT BETWEEN FRAMES 98-99 AND STRINGERS 26L-27L THAT IS .0035 INCHES DEEP, WIDTH IS 0.75 INCHES AND LENGTH IS 1.25 INCHES. (C-CHECK RO 01/14/2026)PERFORMED DOUBLER REPAIR ON EXTERNAL SKIN AT FRAMES 98-99 AND STRINGERS 26L-27LSDR DALA2026010500066Skin · corrodedCORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (1378771)SDR DALA2026010500065Skin · corrodedCORROSION ON FUSELAGE SKIN( AREA UNDER FILLET PANELS) Y=590 BTW LONG 24RH, Y=615 BTW LONG 23RH-25RH, Y=901 BTW LONG 25LH-26LH , Y=586-590 LONG 24 RH , Y=588 TO Y=598 LONG 22RH-23RH. CORROSION WAS REMOVED PER BOEING 717 SRM 51- 10-04. (1378734)SDR CALA2026010212605Skin · damagedLIGHTNING STRIKE DAMAGE AT STA 845 AND BETWEEN S-27 - S-28 BETWEEN S-28 AND S-29 ACPD CONDUCTIVITY CHECK ON HEAT DAMAGED AREA. FOUND DAMAGE AREA AVERAGE READING OF 45. READING OF 38 AT POINT OF IMPACT. REMOVED THE EXISTING FASTNERS AND CUT OUT DAMAGED PART OF SDR DALA2025123109527Skin · nickedNICK EXTERNAL SKIN LOCATED BTW FR 67 TO FR 68 AND BTW STR 26L TO STR 27L LOWER FUSELAGE. REPAIRED PER ERA 631213-14. (1377959)SDR AALA202601070181Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN CORROSION AT BS 887 AND S26L TO S26R. REWORKED THE AREA. PER SRM 53-00-0-1A-1.SDR CALA2026010412648Skin · corrodedFOUND EXFOLIATED CORROSION AT STA 540 CENTER WING LOWER SKIN FROM SPAR BETWEEN S-22R & 23R. ACCOMPLISHED REPAIR AT WING CENTER SECTION LOWER SKIN BS 540 BETWEEN S22R AND 23R ESR-WI 3-13294 AND ECRA 5710-02953,SDR DALA2025123109540Skin · damagedDURING INSPECTION FOUND PREVIOUS ACCOMPLISHED SKIN SPLICE REPAIR ON LEFT FUSELAGE SKIN BS 590 - 630 BETWEEN STR 14L -19L, THE -ID- REPAIR TAG RIVETED THROUGH THE REPAIR AND SKIN. REMOVED OLD DOUBLER AND FABRICATED NEW DOUBLER PER ERA 631258- 14AD REV 0. (1377SDR DALA2025123109524Skin · dentedDENTS ON SKIN LOCATED ON DOUBLER REPAIR BTW FR 6 TO FR 7 AT LATERAL LONGITUNAL LAP JOINT RH SIDE AT LOWER FUSELAGE. REPAIRED PER ER/A 630823-14. (1377088)SDR IPXA2026010969701Skin Panel · damagedFUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. REPLACEMENT STRINGER WAS FABRICATED IAW SRM 53-10-14 AND EO-96143-PRELIM4 STEP 6.SDR DALA2026010500063Skin · not reportedDTA MONITOR INSPECTION LOG REF ERA 631258-14. FUSELAGE SKIN, BS 590 - 630, STR 14L-19L. EXISTING REPAIR. REF ERA 631258-14AD. (1375734)SDR IPXA2025123069701Skin · damagedFUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. VERIFY DAMAGE AND REPORT FINDINGS TO SDF LIAISON ENGINEERING PRIOR TO STARTING INITIAL CUTOUT. FOUND 24€? LONG DENT FWD AND AFT OF FRAME 54.2. WIDTH OF DENT MEASSDR JJBA20251231038Skin · dentedAPU COWLING LOWER SKIN FOUND WITH TWO PROTRUSIONS. DENTS 1 AND 2 WERE REPAIRED. DENT 3 IS FREE OF SHARP EDGES AND THERE ARE NO SIGNS OF MISSING OR PULLED FASTENERS. DETAILED VISUAL INSPECTION WAS PERFORMED AND NO DAMAGED WERE FOUND.SDR YENA2025123001300Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC. FR10 TO FR11 BTW STR2R TO STR3R ON UPPER FUSELAGE; (RESOLVED ON W/O: 1409520 TASKCARD: NR-00048) REF AEROMAN WO 2025 278/1 NR 2025-622588 EVALUATED DENT LOC. FR10 TO FR11 BTW STR2R TO STR3R ON UPPER FUSELAGE ASDR YENA2025123001289Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL SKIN LOC BTW FR65 TO FR 66, STRINGER 31RH ON AFT C ARGO COMPARTMENT; REF AEROMAN NR 2025-623339 WO 2025 278/1 PERFORMED REPAIR ON EXTERNAL SKIN BTW FR65 TO FR 66 , STRINGER 31RH IAW EA#53-0077-25 PART 1-3, EA COVER SDR YENA2025123001282Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / LOWER SKIN PANEL / FR64-FR65 BETWEEN STGR43L-STGR44 / CORROSION AND ELONGATED HOLE - TIME LIMITED REPAIR; REFERENCES: /1/ AEM EA 53-0094-25 (COVER + PARTS 1-4) /2/ AIRBUS DOSSIER 81702291 /3/ AIRBUS RDAF 817SDR YENA2025123001278Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 65-66 & STR 31R / INNER SKIN / CORROSION DAMAGE - TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0077-25 REV. 1 (COVER + PARTS 1-3) /2/ AIRBUS RDAF 81680476/005/2025 ISSUE B /3/ AIRBUS TD/81680476/037SDR JJBA20260130046Skin · dentedFUSELAGE EXTERNAL SKIN, LH, AT FR 9, STR 17L. REPAIRED DENT IN FUSELAGE EXTERNAL SKIN, LH AT FR 9 STR 17LSDR CALA2026010212634Skin · corrodedFUSELAGE SKIN CUTOUT AROUND LAVATORY EXHAUST VENT HAS CORROSION REF AAR N/R 99987189.REPAIR ACCOMPLISHED IAW SRM 53-70-01-2R-3 REPAIR 3 F IGURE 201-203 AS PER SRM 53-70-01-2R-3 CATEGORY B REPAIR INSPECT ION REQUIREMENTS PARAGRAPH 5.SDR JJBA20251231036Skin · damagedAPU COWLING WITH SKIN DAMAGED ON REAR EDGE LH AREA. APU COWLING SKIN ON FR06 FOUND WITH SEVERAL CRACKS ON EDGE. WORK WAS PERFORMED ON THE APU COWLING ACCOMPLISHING TYPE B BLEND OUTS. ADDITIONALLY, CRACK 3 AND 4 WERE REPAIRED.SDR DALA2025122909446Skin · dentedFWD FUSELAGE SKIN PANEL BTW FR6-8 RHS LATERAL STGR DENT ON PREVIOUS DOUBLER REPAIR. REPAIRED PER ERA 630823-14. (1371027)SDR DALA2025123109554Skin · corrodedFUSELAGE SKIN BTW STA1395 AND STA1417, S35R TO S36R WHERE AFT DRAIN MAST INSTALLED FOUND CORROSION. THE DAMAGED SKIN REPAIRED AS PER PRI 631040-14 REV 0.COMAPRED AND COMPLIED WITH ER/A 631040-14 REV ORIGINAL. (1368590)SDR SWIA2026032775582Skin · dentedPROTUDING DENT IN FUSELAGE EXTERNAL SKIN BETWEEN BS 280 TO 295, STGR 24L TO 25L. REPAIRED THE SKIN IAW REO 601R-53-21-3783, REV-, SRM 51-42-06, 51-42-21, & 51-25-01.
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