JASC 5330
Service difficulty reports · 79,281
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 UIEA2026031100084Skin · dentedEXTERNAL SKIN ON RIGHT SIDE STA 1934 BETWEEN STR 32R AND 33R HAS A DENT. DENT ON EXTERNAL SKIN AT STA 1934 BETWEEN STR 32R AND 33R IS IN A USE AS IS CONDITION PER EAC-TLS-26-0008-1C, 03B AND 04C. NO FURTHER DEFECTS NOTED.SDR SWIA2026040977419Skin · corrodedCORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN BS 280 & 295, STR 24R -25R. PERFORMED A CUT OUT OF THE CORRODED FUSELAGE SKIN BTWN BS 280 - 310, STR 24R - 26R AND APPLIED DOUBLER IAW REO 670-53-21-2866, REV -.SDR SWIA2026040976000Skin · gougedFUSELAGE SKIN HAS 2EA GOUGES UNDER AFT WING TO BODY FAIRING APPROX BS 985 - 988, BL27. REPAIRED FUSELAGE SKIN 2EA GOUGES UNDER AFT WING TO BODY FAIRING APPROX BS 977 - 988, STR 27 IAW REO 670-53-00-290, REV -F. SRM 51-42-21-001-001-A01 REVISON 38 AND SRM 51-SDR MASA20260420079Skin · corrodedDURING HEAVY CHECK INSPECTIONS ON REAR FUSELAGE EXTERNAL, CORROSION FOUND ON SKIN AT EDGE FWD FR 90A BETWEEN STR 27-29 RH, CORROSION ON EXTERNAL SKIN REMOVED BY BLEND-OUT IAW SRM 51-10-03 AND FOUND TO BE WITHIN LIMITS IAW SRM 51-75-16 PAR. 4 REV 53 AUG 21/25 ASDR DALA2026041402343Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1037 BTW LONG 13 RT & 14 RT. REPAIRED PER PRI 633254-14 REV. 2 AND ER/A 633254-14 (1536512) (AIRCRAFT GROUNDED)SDR ABXA20260409159Skin · crackedDURING A-9 CHECK, WO 16376144 EXTERNAL DVI OF FUSELAGE SKIN, FORWARD SERVICE DOOR (R1) FOUND 1INCH CRACK ON AFT LWR CORNER AFTER REMOVING AFT SCUFF PLATE. , FOUND CRACK TOTAL LENGTH 3.5 INCHES,FOUND TO BE OUT OF LIMITS. CALLING . MAINTENANCE REPAIRED CRACKESDR DALA2026041402369Skin · crackedFUSELAGE SKIN, BS 1087, L13R - 14R CRACKED. ASSOCIATED ER/A 00-633468 (1536411) (AIRCRAFT GROUNDED)SDR DALA2026041002294Skin · crackedCRACK WAS FOUND DURING NDT INSPECTION OF FWD SERV DOOR CUTOUT CORNER, REMOVED THE CRACKED AREA, AND PERFORMED CATEGORY B DOUBLER REPAIR ON FORWARD DOOR CUTOUT AFTER CORNER AT STA300 TO STA347, S-18LH TO S-22LH AS PER B767-300 SRM 53-10-01 (1533738) (AIRCRAFTSDR DALA2026041002290Skin · crackedCRACK WAS FOUND DURING NDT INSPECTION OF FWD PAX DOOR CUTOUT CORNER. REMOVED THE CRACKED AREA, AND PERFORMED CATEGORY B DOUBLER REPAIR ON FORWARD DOOR CUTOUT AFTER CORNER AT STA300 TO STA347, S-18RH TO S-22RH AS PER B767-300 SRM 53-10-01 (1533863) (AIRCRAFT GSDR YENA2026040900384Skin · damagedDURING HEAVY MAINTENANCE, REF: SRM 53-41-11-300-004, DOSSIER 81769917, MX244. FOUND WITH CORROSION DAMAGE ON THE AFT LAV VENT AT FR 69-FR70 BETWEEN STGR31R AND STGR32R AFFECTING SKIN PANEL. REPAIRED, TRIMMING OUT THE DAMAGED AREA AND PERFORMING A HFEC INSSDR AALA202604091545Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER LOWER CUTOUT AT BS 235 AND S25R. REPAIRED DOUBLER PER SRM 53-10-15-2R-4.SDR SCNA20260814360Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT SECTION 43 FROM BS 360 - 540 STR 4R EXTERNAL FUSELAGE SKIN PANEL DUE TO CORROSION REPAIR IAW EO 000-EO-2026-24311SDR SCNA20260811354Skin · corrodedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 361, STA 418, STRA 442 ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG-24RH DUE TO SKIN PANEL WITH CORROSION AND SSDR SCNA20260811353Skin · damagedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 421 ON STR-24R SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG-24RH DUE TO SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COSDR SCNA20260811352Skin · corrodedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG 24RH DUE TO SKIN PANEL WITH CORROSION AND SCSDR SCNA20260811348Skin · corrodedLOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. - - MRO EMP# 5323-PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG 24RH DUE TO SKIN PANEL WITSDR SCNA20260811347Skin · damagedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 500I + 18.375 ON STR-4L SKIN WITH SCRIBE LINES. PERFRORMED PERMANENT REPAIR AT BS 500I THRU BS 540 BETWEEN STR.2L AND 6L OVER EXISTING REPAIR. BS 500I +11 INCG=HES TO BS 520 + 8 INCHES BETWEENSDR SCNA20260811346Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT STA 43 FROM STA 360 TO 540 BETWEEN STR 14 RH AND STR24 RH EXTERNAL SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COSDR SCNA20260810343Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN BS 887 - 1016, STRINGER 4L, CORRODED. PERFORMED PERMANENT REPAIR AT EXTERNAL FUSELAGE SKIN PANEL FROM BS 887 - 1006, STRINGER 14L DUE TO CORROSION IAW EO COO-EO-2026-24383-R01, AND RDR 1 COO-SCA-26-SDR VNAA202606120056Skin Panel · damagedBURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FSFS210.92 - STR23L. BURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FSFS210.92 - STR23L WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR HNAA2026052000427Skin · damagedPOSSIBLE LIGHTNING STRIKE ON FUSELAGE EXTERNAL SKIN AT FR 37-38, STRG 6R-7R. PERFORMED DRILL OUT OF LIGHTNING STRIKE AREA AND REPAIRED WITH SOLID BUTTON HEAD RIVET AND WASHER PER EMB 145 SRM 53-00-01,ITEM 2, FIG 201, SHEET 1 AND 2.SDR HNAA2026052000426Skin · damagedPOSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR33-34, STRG 5R-6R. PREPPED PRIMED AND PAINTED FUSELAGE SKIN FR 33-34, STRG 5R-6R IAW EMB 145 CPM 51-21-05 AND 51-21-06 51-21-03 AND PIEDMONT DRAWING AE-ERJ145-IR PIEDMONT BULLETIN CPM 51-02SDR HNAA2026052000425Skin · damagedPOSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR-25-26, STRG 6R-7R. PERFORMED RIVET AND WASHER IN AFFECTED HOLE ON EXTERNAL FUSELAGE SKIN BTW FR 25-26 AND BTW STR 6R-7R IAW ETD 2026-145-0, SRM 53-00-01, ITEM 2, FIG 201, SHEET 1 AND 2 AND EO1-53-26-0239SDR SWIA2026040776004Skin · damagedLIGHTING STRIKES (3) AT FWD FUSELAGE BETWEEN FR 1-2 STGR 26L-28L. REMOVED LIGHTNING STRIKE DAMAGE FROM LOWER FWD FUSELAGE SKIN FR 01-02 STGR 26L-28L BY PERFORMING PERMANENT DOUBLER REPAIR REF. ETD2026-170-006439. CHANGE IN WEIGHT MEASURES 85.51 GRAMS. THIS RESDR HNAA2026050500371Skin · corrodedSIGNS OF CORROSION ON RIVET HEADS AT BELLY FR36-37 AND STR 21L. PERFORMED CORROSION REMOVAL OF RIVET HEADS AT BELLY FR36-37 AND STR 21L, NO ADDITIONAL CORROSION FOUND, PER EMB 145 CPM 51-14-00 AND EMB 145 CPM 51-14-02 PARAGRAPH 8, SECTION 4SDR IPXA2026041183869Skin · dentedEXTERNAL FUSELAGE BETWEEN BS 1700 - 1720, S16-17L DENTED. COMPLIED WITH EO-97220-REQ1 AND EA 757-5360-27-A4433.SDR IPXA2026041183937Skin · dentedEXTERNAL FUSELAGE SKIN BETWEEN BS 1720 - 1743, S29L - 28L HAS A PROTRUDING DENT. ACCOMPLISH REPAIR PER EO-97221-REQ1 & EA 757-5380-27-A4434.SDR N6WA2026040902Skin · damagedAFT FUSELAGE SKIN AT FS977 AND STRINGER 27 IS DAMAGED. REPAIRED AFT FUSELAGE SKIN AT FS977 AND STRINGER 27 IAW GOJET EO C550-53MR-108-O.SDR SWIA2026040677680Skin · nickedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA96715-690-53-61-1494 MXCODEID107416-PR - COMPLY WITH PERMANENT REPAIR ON RA ID 96715FOUND MULTIPLE KNICKS AROUND LP AIR DOOR COMPLIED WITH REO 690-53-61-1494 DATED 2025-01-26 REV -- THE REWORKED CONDITION IS STRUCTURALLSDR IPXA2026060565618Skin Panel · puncturedMAJOR REPAIR, EXTERNAL FUSELAGE, JUST IN FRONT OF TAIL JACKING POINT, 2 PUNTURES WITH DENT. FABRICATED 3 EACH FILLERS IAW SRM 53-10-12. INSTALLED REPAIR PARTS IAW STEP 20 TO STEP 22 OF SRM 53-10-12-201, PAR 13.C.SDR HNAA2026052000423Skin · dentedFUSELAGE SKIN BETWEEN FR-06/07 AND STGRS-14L/15L HAS A DENT. INSTALLED REPAIR DOUBLER & FILLER ON FUSELAGE SKIN BETWEEN FR-06/07 AND STGRS-14L/15L IAW SRM 53-12-01 RE, ITEM 2, FIGURE 201. AND EO1-53-26-0226.SDR DALA2026041402370Skin · crackedFUSELAGE, SKIN, BS 1087, L13 - 14L CRACKED. ACCOMPLISH ER/A 633469-14 (1534688) (AIRCRAFT GROUNDED)SDR CALA2026041315331Skin · damagedDURING CURRENT C-CHECK AT PNS, PRODUCTION REPORTED INSPECTION OF 1 EACH EXISTING REPAIR INSTALLED. THE EXISTING REPAIR IS LOCATED ON THE LOWER AFT CORNER OF FWD CARGO DOOR SKIN CUTOUT AT STA 620 BETWEEN S-22R AND S-27R. PERFORMED A REPAIR IN ACCORDANCE WITH VTSDR UIEA2026040600136Skin · corrodedCORRODED SKIN, LT MLG FWD BULKHEAD AT CENTER WING TANK JETTISON PUMP, LEFT M224, BONDING JUMPER ATTACHED. ACCOMPLISHED THE EI T2026A57M-398 REV 5. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026040600137Skin · corrodedCORRODED SKIN, RT MLG FWD BULKHEAD AT CENTER WING TANK JETTISON PUMP, LEFT M225, BONDING JUMPER ATTACHED. REPAIR THE CORROSION AREA IAW EI T2026A57M-397 REV 3 SEQUENCE D. ACCOMPLISHED EI T2026A57M-397 REV 4. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR CALA2026040715149Skin · crackedDURING GVI OF THE SKIN AROUND THE DOOR CUTOUT LOWER CORNERS (STEP2), FINDING A REPAIR IN EXTERNAL SURFACE. . WORKED IAW EC/RA #5330-07731 AND EA 757-5330-13-A4329, REV-.SDR DALA2026040702209Doubler · corrodedWASTE BOX DOUBLER HAS CORROSION ON FWD AND AFT FLANGE. REPAIRED PER PRI 632674-14 REV 0 REV 1 AND FINAL ER/A 632674-14. (LP# 1530122)SDR SCNA20260811351Skin · corrodedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 727 TO STA 887 ON STR-14R SKIN WITH CORROSION AND SCRIBE LINES. PERFORMED PERMANENT REPAIR AT EXTENRAL SKIN SECTION FROM STA 727 TO STA 887 BETWEEN STR-14R AND STR-17RH DUE TO CORROSION AND SCRISDR IPXA2026042143284Doubler · corrodedRT FWD LAV DUMP VALVE ADAPTER PLATE CORRODED. REMOVED PLATE FOR ACCESS FROM R/H FWD LAV DUMP VALVE ADAPTER REF. B757-200PF SRM 51-40-02-OG-0, UPON FURTHER EVALUATION FOUND 100% OF MAT. LOSS. USED CALIPER ID#23-2023 DATE DUE 10-MAY-2026. INSTALLED REPLACEMENT SDR SCNA20260811350Skin · damagedUPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 727C ON STR-4L SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION FROM B575B+13" TO BS727C+9" BETWEEN STR-2L AND STR6L DUE TO SCRIBE LINE IAW COOPESA EO COO-EO-2026-24295SDR VNAA202606120055Skin · burnedBURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FS202.75-FS210.92 - STR25L. BURN SPOT AT FASTENER LOCATION AFTFUSELAGE SKIN FS202.75-FS210.92 - STR25L WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR IPXA2026042119204Skin · damagedLIGHTNING STRIKE- SKIN, RT NOSE AREA (ABOVE UPS LOGO) SUSPECTED LIGHTENING STRIKE ON FASTENER. BLEND OUT THE DAMAGE AREA I.A.W SRM 51-10-02-0G REV.106. ACCOMPLISHMENT LIGHTNING STRIKE REPAIR I.A.W UPS EO-97134-REQ1 REV.1.SDR CALA2026042115567Skin · damagedIAW C/R DURING AAI INSPECTION NO RECORDS FOUND FOR THE REPAIR AND DTA REQUIREMENTS OF THE EXTERNAL FUSELAGE DOUBLER REPAIR AT STA 907-927 AND STR 6R-8R. ACOMPLISHED REPAIR AT FUSELAGE SKIN BETWEEN BS 907-927 BTWN S6R & 9R.SDR CALA2026042115565Skin · corrodedLOWER FUSELAGE INTERNAL SKIN CORRODED AROUND RIVET TAIL BETWEEN STR 27L-27R, BS 520. ACCOMPLISHED LOWER FUSELAGE SKIN REPAIR FROM BS 500H+10 - 540 BETWEEN S27R - 27R IAW ESR-WI 10-14655 AND ECRA 5330-07728.SDR SWIA2026040277002Skin · gougedMULTIPLE DAMAGES TO FUSELAGE SKIN BETWEEN BS 513 - 544, S6R & 10R. DUE TO FALLING DEBRIS IN HANGER.SPOT1: GOUGE/DENT MEASURING 1.1" LENGTH, 1.1" WIDTH, 0.052" DEPTH. SPOT 2: GOUGE MEASURING 0.700" IN LENGTH, 0.060" WIDTH, 0.007" DEPTH. SPOT 3: GOUGE MEASURING SDR SWIA2026040276328Skin · scratchedCIRCUMFERENTIAL FUSELAGE SPLICE AT BS 280, BETWEEN STR 23-22 LT, HAS SCRATCHES, COMPLIED WITH REO 601R-53-00-936 REV-, ALL STEPS, STEP 1 ENSURED BLEND-OUTS WERE PERFORMED TO A SMOOTH CONTOUR, STEP 2 PERFORMED NDT (SEE STEP 2A OF THIS CONTINUE CARD), STEP 3 RSDR AALA202605220507Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN BETWEEN STA 867 AND 887 OUTBOARD OF S26R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.SDR AALA202605223942Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN BETWEEN STA 867 AND 887 OUTBOARD OF S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.SDR AALA202605223139Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 747 AND 767, BETWEEN S26R AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.SDR CALA2026042115569Skin · corrodedCORROSION AT RH LOWER FUSELAGE EXTERNAL SKIN BY DRAG LINK BS 540 BTWN S21-22R. ACCOMPLISHED A REPAIR IAW ESR 14681, ECRA 5710-02968.
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