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 KCSA202504041059Skin · cracked2EA. CRACKS FOUND EXTENDING BEYOND 2EA. EXISTING STOP DRILL HOLES IN R/H SIDE UPPER LOBE DOUBLER NEAR VERTICAL STAB. ATTACHMENT AT APPROX. STA. 2515 AND 2521 DURING EXTERNAL SURFACE HFEC INSPECTION.SDR DALA2025040702682Paint · chippedPOSSIBLE LIGHTNING STRIKE FR20 STR. 47. REPAIRED SCRAP/CHIPPED PAINT PER A350 ASR 53-21-61-00004-662A-A OK FOR SVC. NO DAMAGE FOUND. (LP# 0892850)SDR DALA2025040702681Paint · chippedPOSSIBLE LIGHTNING STRIKE AT FR23 BETWEEN STR. 38L AND 40R. REPAIRED SCRAP/CHIPPED PAINT PER A350-A-53-21-61-00004-662A-A. OK FOR SVC. NO DAMAGE FOUND. (LP# 0892855)SDR DALA2025040702680Paint · chippedPOSSIBLE LIGHTNING STRIKES BETWEEN FR18 AND FR19 STR 44R. REPAIRED SCRAP/CHIPPED PAINT PER A350 ASR A350-A-53-21-61-00004- 662A-A. OK FOR SVC. NO DAMAGE FOUND. (LP# 0892845)SDR DALA2025040702679Paint · chippedPOSSIBLE LIGHTNING STRIKE AT FR14 BETWEEN STR47 AND 44L. REPAIRED SCRAP/CHIPPED PAINT PER A350 ASR A350-A-53-21-61-00004- 662A-A, OK FOR SVC NO DAMAGE FOUND. (LP# 0892838)SDR N6WA2025040403Skin · gougedGOUGE IN FUSELAGE SKIN AT FS972 AT STGR27. PERFORMED REPAIR OF FUSELAGE LOWER AFT SKIN AT FS969 TO FS985 AT STGR27 IAW EO 25-CRJ5-53-070REV IR.SDR N6WA2025040401Skin · dentedFUSELAGE SKIN DENT AT FS581 TO FS597 AT STGR25L TO STGR26L. WORKED AND REPAIRED FUSELAGE DENT AT FS581 TO FS597 AT STGR25L TO STGR26L IAW AWATS EO 25-CRJ5-53-057 AND EO-C550-53MR-062.SDR WRXR20250403005Doubler · corrodedCORROSION FOUND ON ANTENNA DOUBLER AT STRG 27 BETWEEN FS.295 AND FS.310. REMOVED CORRODED ANTENNA DOUBLER AT STRG 27 BETWEEN FS.295 AND FS.310 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW ANTENNA DOUBLER AT STRG 27 BETWEEN FS.295 ANSDR EE4Y2025040322124Skin · scratchedDURING THE STRUCTURE INSPECTION WE FOUND THE FUSELAGE SKIN WITH TWO SCRATCHES LOCATED BETWEEN STRINGER 01L AND 01R, JUST FORWARD TO FR 60. THE SCRATCHED AREAS WERE REWORKED BY BLEND OUTS IN ACCORDANCE WITH THE SRM 51-10-03. SINCE BLENDED AREAS ARE LOCATED IN ASDR FDEA202504030558Doubler · crackedCENTER LANGING GEAR RIGHT HAND FORWARD COMPARTMENT SPOILER MIXER CONTROL ROD ACCESS CUTOUT DOUBLER AT STATION 1381.00 FOUND CRACK. CRACKED CUT OUT DOUBLER AT STATION 1381.00 CENTER LANDING GEAR RIGHT HAND FORWARD COMPARTMENT SPOILER MIXER CONTROL ROD REMOVSDR WRXR20250403003Skin Panel · corrodedAFTER REMOVAL OF THE TCAS OMNI DIRECTIONAL ANTENNA THERE IS PRESENT PITTING CORROSION IN A NO DAMGE ALLOWABLE AREA. REMOVED CORROSION IAW CRJ 900 SRM 51-21-06-001-001-A01. PARAGON JOB NO. E260325 PERFORMED EDDY CURRENT AND ULTRASONIC INSPECTIONS. CORROSION REMSDR SWAA2025042955193Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS706 S-4L. MARKED<[01] REMOVED AND REPLACED CLIP AT B727D S-6L IAW SRM 51-40-02 AND DWG 146A1107 ID:0015 REV: -;[02] REMOVED AND REPLACED CLIP AT B706 S-4L IAW SRM 51-40-02 AND DWG 146A1107 ID:0015 REV: -;[03] VERIFIED CORRECTIVESDR SWAA2025042955194Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727D S-7L. MARKED<[01] REMOVED AND REPLACED CLIP AT B727D S-7L IAW SRM 51-40-02 AND DWG 146A1111 ID:0011 REV: -;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025042955171Bear Strap · crackedCRACK 1.5' ON INNER BEAR STRAP OF FWD GALLEY DOOR (R1); BETWEEN S-8R AND S-9R (BS STA 294.5; RBL 52; WL 265.5 APPROX; MARKED)<[01] DAMGE REMOVED AND AREA WAS REPAIRED IAW B737-7 SRM 53-10-01-2R-6;[02] CORRECTION TO ACCTION 1 DAMAGE REMOVED AND AREA WAS REPAIRESDR SWAA2025042920767Skin · debondedPANEL 191HL OUTER SKIN HAS A DISBOND. (MARKED)<[01] 191HL PANEL OUTER SKIN SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 51-70-05-2R-2-A00733 (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE - AIRFRSDR DALA2025040802742Doubler · corrodedWASTE BOX HAS CORROSION ON INNER SIDE OF DOUBLER ON FWD R/H CORNER.SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0087:5360-2017/001 00123 COMPLIED WITH ER/A 625089-14 PRI REV 0, ER/A 625089-14 PRI REV 1 AND FINAL ER/SDR JJBA20250408051Skin · dentedCF3 LH UPPER SKIN DENT FOUND ON FR 39, BTW STR 3L-4L. REPAIR DOUBLER ON LH CENTER FUSE III SKIN AT FR39 BTW STR 3L-4L CARRIED OUT.SDR CALA2025040403539Skin · damagedWHILE PERFORMING PHASE 1 LIGHTNING STRIKE INSPECTION IAW AMM 05-51-19-210-804. FOUND DAMAGE ON STATION 360 APROX 1FT ABOVE R1 DOOR.REPAIRED PER SRM 53-00-01-2R-38 STEP 4D (FIG 203). HFEC REQ PER SRM 53-00-01-2R-38 STEP 4D (3) A REQUEST INSPECTION C/W HFEC IAW SDR DALA2025040402554Skin · ground damageSHIP 3256 DISC: DTE REQUIRED. ER/A 624580-14 ISSUED FOR GROUND DAMAGE TO THE FWD LOWER FUSELAGE, FR 28-30, STR 38LH-42RH. FOLLOW ON DTE IS REQUIRED. C/A: ER/A 624580-14 REVISED TO REV 'B' TO INCORPORATE ODA APPROVAL. TIME CONTROLS REMAIN UNCHANGED. (LP: 089160SDR DALA2025040302549Skin · corroded(LOG 0891567) CORROSION ON FUSELAGE EXTERIOR SKIN AROUND VACUUM WASTE VENT CUTOUT AT STA 917 BETWEEN STR21 AND 22L. REPAIRED PER ERA 625221-14.SDR AALA202504036967Skin · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE OF FUSELAGE SKIN AT EXTERNAL POWER PANEL ACCESS DOOR CUTOUT CRACKED AT STA 224, S20R. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-10-15-2R-4.SDR EE4Y2025040222123Skin · corrodedDURING THE REMOVAL OF THE KA BAND-RADOME STRUCTURAL PROVISIONS AS PER SB 190-53-0125, WAS FOUND THE FUSELAGE SKIN WITH CORROSION AROUND THE EXISTING HOLE CUT OUT BETWEEN FRAME 63 AND 64 AND BETWEEN STRINGER 01L AND 02L. DUE TO THIS SITUATION WAS REPAIRED IAW ESDR EE4Y2025040222122Skin · damagedDURING THE STRUCTURE INSPECTION, IT WAS REPORTED AN EXISTING FLUSH REPAIR WITH SEVERAL DENTS AND TOOL MARKS. DUE TO THIS CONDITION, THE DISCREPANCIE WAS REPORTED AND REPAIRED IAW EMB ETD2025-190-902291 AND COOPESA ENGINEERING ORDER COO-EO-2025-21776 DTD FEB 21SDR VNAA202504020039Skin · corrodedDURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON INTERNAL SKIN BM FS 280.00 TO 295. CORROSION ON INTERNAL SKIN BTW FS 280.00 TO FS 295.00 AND STGR 25RH TO 24 RH WAS REPAIRED PER REO 690-53-21-1902 REV - -.SDR VNAA202504020014Skin · gougedSEVERAL GOUGES ON SKIN BTW FS629.00 TO FS661.00 AND STGR 25 LH TO STGR 27 AT CENTER FUSELAGE. BLEN OUT ON GOUGES OVER SKIN BTW FS629.00 TO FS661.00 AND STGR 25 LH TO STGR 27 AT CENTER FUSELAGE WAS REPAIRED PER REO 690-53-31-937 REV- -.SDR VNAA202504020006Skin · dentedBIRD STRIKE DAMAGE WITHIN 795.42 FLIGHT HOURS OF INITIAL RELEASE AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. BIRD STRIKE DAMAGE, FRAME WAS REPAIRED PER REO 670-51-00-085.REV. -A ANSDR VNAA202504020005Skin · chafedPASSENGER DOOR SURROUND SKIN CHAFE DAMAGE WITHIN 652 FLIGHT HOURS FROM EXTENSION REQUEST (2,173 FH TOTAL), ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. PASSENGER DOOR SURROUND SKIN CHAFE DAMAGE PERMSDR VNAA202504020003Skin · gougedPERM REPAIR - GOUGES TO FUSELAGE SKIN BETWEEN FS1031.00 - 1051.30 AND STR 21R-26R THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 6200 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO. WITHIN 2000 FLIGHT HOURS ACCOMPLISH A PERMANENT REPAIR IN ACCORDANCSDR IPXA2025040184095Strap · corrodedAPU DOOR SURROUND FS1787.45 FROM STR 3R - STR 6R THE 148N3138-20 STRAP IS EXFOLIATED RED DOT. INSTALLED STRAP ON APU DOOR SURROUND FS1787.45 FROM STR 3R - STR 6R IAW B757-200PF, SRM 51-40-02.SDR AALA202504032109Skin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND SIDE OF FUSELAGE SKIN AT EXTERNAL POWER PANEL ACCESS DOOR TORN FROM STA 225 TO STA 235, S24R. REPAIRED SKIN PER SRM 53-10-15-2R-4.SDR HNAA2025041700208Shear Tie · cracked53-2276 SHEAR CLIP CRACKED AT FR62 BTW STR4-5R. RAR SHEAR CLIP IAW SRM 51-40-02SDR ASAA2025033157312Skin · damagedEXTERIOR FUSELAGE, LIGHTNING STRIKE FOUND AT STA 500E BETWEEN S-5L AND S-6L. GROUNDED - YES. ACCOMPLISHED REPAIR PER ASA EA M9-53EA-28524 REV 00. THIS IS A CATEGORY B REPAIR. DTI DUE WITHIN 24MTHS FROM 12APR2025.SDR JJBA20250408048Skin · dentedDENT FOUND ON EXT SKIN BTW FR 53-54 STR 4-5 LH. REPAIR DOUBLER ON LH CENTER FUSE IV SKIN, AT FR 54 AND BTW STR 4L-5L CARRIED OUT.SDR JJBA20250408044Skin · dentedDENT FOUND ON EXTERNAL SKIN BTW FR 21-22 AND STR 11L-12L. REPAIR DOUBLER ON LH CENTER FUSE I SKIN, BTW FR 21-22 AND BTW STR 11L-12L CARRIED OUTSDR CALA2025040303496Skin · damagedLIGHTNING STRIKE AT STA 522, STR 4L. REPAIRED FUSELAGE SKIN REF SRM 53-00-01-2R-20, SEE NR 002538867 FOR WORK PERFORMED. ISSUE A DIP REF STEP 7 FOR INSPECTION REQUIR EMENTS. ZONE A AS FOLLOWS: INSPECTION THRESHOLD 375000 FLIGHT CY CLES AFTER AIRPLANE DELIVERY SDR 2025F00085Skin Panel · burnedLIGHNING STRIKE AT FS: 409.00+75 BETWEEN STR:25L AND 26L.REPAIRED I/A/W BOMBARDIER REO 601R-53-00-115, REV. E 2013-09-18 FUSELAGE SKIN LIGHTNING STRIKE DAMAGE REPAIR AND MHI RJ 200 SRM 53-00-31 REPAIR NO. 1 EXTERNAL NON-FLUSH PERMANENT REPAIRS - PRESSURIZED ARSDR 2025FA0000226Skin Panel · corrodedCORROSION FOUND AROUND FASTENERS ON FUSELAGE BELLY SKIN FROM FS: 559.00+80 TO FS: 559.00+112, STRG 27. REPAIRED I/A/W MHI RJ REO 601R-53-00-906 REV. -- 2025-03-29SDR IXXA2025033101Skin · crackedCRACK ON SKIN AT STRINGER 23L STATION 654+28SDR FDEA202503310542Skin · damagedUPPER FUSELAGE, EVIDENCE OF LIGHTNING STRIKE, AFT OF UPPER BEACON. MEASURED LIGHTNING STRIKE AFT OF UPPER BEACON AND FOUND DAMAGE TO BE OUT OF LIMITS IAW B67 SRM 53-00-01-1A ALLOWABLE DAMAGE 1. NOMINAL THICKNESS OF DAMAGED AREA 0.178", LIGHTNING STRIKE MATSDR DALA2025041102820Skin · damagedSHIP 1018 TRANSFER FROM. BUFF NR 14 ON FR 24 BETWEEN STR 35,34 ON FASTENER 0.1875 DIAMETER RIVET AND SKIN DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 625277-14 PRI REV 0, ER/A 625277-14 PRI REV 1 , ER/A 625277-14 PRI REV 2, ER/A 625277-14 PRI REV 3 AND FINALSDR DALA2025040602612Skin · noneSHIP 3256 DISC: DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED. ERA 625079 SECTION I ACCOMPLISHED IN MSP. FOLLOW ON ACTION IS REQUIRED. FUSELAGE SKIN, FR 31-32, STR. 39L - STR. 43L AFFECTED. C/A: ERA 625079-14 SECTION I REPAIR IS ACCEPTABLE FOR 12 MONTHS AFTER 30MSDR DALA2025040402568Skin · damagedAIRCRAFT 3031, BIRD STRIKE DAMAGE TO NOSE FORWARD FUSELAGE LEFT SKIN PANEL. DENT 1 IS FWD OF FR 2 MEASURING 4.0" X 2.5" WITH A DEPTH OF 0.050". DENT 2 IS FWD OF FR 3 AND MEASURES 4.0" X 3.5" WITH A DEPTH OF 0.170". BOTH DENTS ARE FWD OF THE LH STATIC PORT. THESDR DALA2025033102376Skin · ground damageSHIP 3326 DAMAGE DUE TO GOLDHOFER SPINNING OUT. BETWEEN FRAMES 26.1 AND 27 AND STRINGER 51L AND 54R. CORRECTIVE ACTION: COMPLIED WITH ERA 624866-14 REV B OK FOR SVC. (0885299)SDR DALA2025033102360Skin · damagedSHIP 6708 DURING HFEC INSPECTION ELONGATE HOLE WAS FOUND ON FUSELAGE SKIN AT AFT CORNER THE CARGO # 1 DOOR CUTOUT OF: STA: 619. CORRECTIVE ACTION: SUMMARY OF NRC 00233: ELONGATE HOLE WAS FOUND ON FUSELAGE SKIN AT AFT CORNER THE CARGO # 1 DOOR CUTOUT OF: STA: 6SDR DALA2026032502004Skin · not reportedER/A 625365-14 FUSELAGE SKIN, BS 500 - 540, S-27L TO S-26R / EXISTING REPAIRS NEAR FORWARD, LOWER ATG4 DOUBLER. REF ERA 625365-14. (0884182)SDR SWI2025F00698Skin · dentedDURING THE ADM INSPECTION, 14 INWARD/OUTWARD DENTS WERE FOUND ON THE EXTERIOR LOWER FUSELAGE SKIN PANELS BETWEEN FS574.00-FS682.00 & STR 24L - 21R. (C-CHECK RO 05/28/2025)UPON INSPECTION, FOUND ALL 14 INWARD/OUTWARD DENTS ON THE EXTERIOR LOWER FUSELAGE SKIN SDR SWI2025F00697Skin · dentedDURING THE ADM INSPECTION, 2 DENTS WERE FOUND BETWEEN FS654 - FS762 AND BETWEEN STR 0-1R (C-CHECK RO 05/28/2025)COMPLIED WITH REWORK OF DENTS TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.00 AND STR 0 - STR 1L WITH REFERENCE TO REO 601R-53-61-8311 REV "--" DATED 2SDR SWI2025F00696Skin · dentedDURING THE ADM INSPECTION, 3 DENTS WERE FOUND FROM FS 654- FS 672 BETWEEN STR 7R-8R (C-CHECK RO 05/28/2025)COMPLIED WITH REWORK OF DENTS TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.00 AND STR 7R - STR 8R WITH REFERENCE TO REO 601R-53-61-8311 REV "--" DATED 2025-SDR DALA2025040202486Skin · damagedSHIP 3326 SKIN & STRINGER DAMAGE FR26-26.1, STR-50L TO 50R. CORRECTIVE ACTION: COMPLIED WITH ERA 624866-14. (0884698)SDR CALA2025040203451Skin Panel · damagedLOWER FWD FUSELAGE LH SIDE EXTERNAL SKIN HAS DAMAGE JUST OUTBD OF FWD E&E FWD FRAME CUTOUT 31 INCHES AFT OF 178 BULKHEAD MARKED WITH TAPEDAMAGE MEASURES OUT A TOTAL DIAMETER OF 1.5 INCHES AND HAS A DEPTH OF .032". CENTER OF DAMAGE IS LOCATED 8" BELOW FACTORY L
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