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 FDEA202311131894Skin · dentedFUSELAGE TAIL SKIN FOUND 5EA BULGEDS AT FR92 PLUS 4.4", S-16R PLUS 1.8", FR92 PLUS 3", S- 16R PLUS 2.4", FR92 PLUS 5.5", S-17R PLUS 0.9", FR92 PLUS 5.4", S-17R PLUS 2.5", FR92 PLUS 2.8", S-17R PLUS 4.7" POS. CUT OUT DAMAGE AREA, FABEICATED THE REPAIR DOUBLSDR DALA2023111509429Unknown · unknownSHIP 0670 FUSELAGE / SKIN / STA 570 - STA 661 / S-14L - S-19L - SPLICE REPAIR. CORRECTIVE ACTION: REF ERA 556472-14AD. (0062991)SDR DALA2023111409377Unknown · unknownSHIP 3302 FWD FUSELAGE SKIN FR5-FR7 RHS BIRDSTRIKE DENTS. CORRECTIVE ACTION: REF ER/A 14-613274. (0060994)SDR DALA2023111309293Unknown · unknown(LOG 0061049) LIGHTNING STRIKE ON RIVET 0.5 INCH OF STA 500G AND ON S-9L. REMOVED DAMAGED FASTENER (542248) COMPLETED SECTION I PERMANENT REPAIR PER ERA 613488-14 REV ORIGINAL.SDR VNAA202312140009Skin · dentedDESCRIPTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22RH TO STGR 21RH.CORRECTIVE ACTION: SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF RIGTH VENTRAL FIN FAIRISDR BAGA2023112000003Unknown · unknownDENT AND CRACK IN LH FUSELAGE AFT OF MAIN CABIN DOOR CAUSED BY AIRSTAIR CONTACT DURING GROUND HANDLING. BREEZE ENGINEERING RELEASED THE REPAIR INSTRUCTIONS ON 11/15/23. ACCOMPLISHED A PERMANENT DOUBLER REPAIR OF DENT AND CRACK LOCATED ON FWD LH FUSELAGE BETWEESDR DALA2023111309305Unknown · unknownCORROSION ON UNION SKIN BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00702: CORROSION LEVEL 2. UNION SKIN (FINGER DOUBLER) BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT WAS FABRICATED AND INSTALLED PER B-717 SSDR DALA2023111309290Unknown · unknown(LOG 0060730) DURING LAYOVER IN MSP, MAINTENANCE NOTED THERE WAS LIGHTNING STRIKE DAMAGE TO THE AIRCRAFT. ONE STRIKE IS COMMON TO STR-9L AND 500H. DAMAGE REPAIRED PER ERA 613488-14.SDR JR2R20231111702Doubler · corrodedTEXAS DOUBLER ON TOP OF FR90 AND RBL23 CORRODEDSDR JR2R20231111704Doubler · corrodedTEXAS DOUBLER ON TOP OF FR90 AND RBL23 CORRODEDSDR CALA2023111503374Skin · corrodedAFT CARGO BILGE AREA FUSELAGE SKIN FOUND HEAVY CORROSION AT STA 1880 S-44L REF HAECO NR NO.9466223 - SPEC NO.B777-06-3-7169. AFT CGO BILGE AREA REVISION OF ECRA 5730-01098 ON OR BEFORE THE A/C REACHES 22,889 FUS STA 1824-STA 1895 STR 44L SKIN REPAIRED AS PER SDR DALA2023111309299Unknown · unknownCORROSION ON FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RL) BTW STA 851-870 LONG 28L IN REF TO NRC 00671. SUMMARY OF NRC 00705: CORROSION LEVEL 2. FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RLSDR HNAA2023121900483Unknown · unknownE008015 NO REPAIR INFO FOUND FOR EXTERNAL FUSELAGE SKIN REPAIR BUSHING AT FR 77 STR 8R-9R. RE-ACCOMPLISHED BUSHING REPAIR AT FR. 77 STRG. 8R-9R IAW EMB 145 SRM 53-32-01, ITEM 9, FIG. 213 AND PIEDMONT EO1-53-23-0447.SDR R61A2023120400701Doubler · corrodedCFIII FR88-90 STR25R-29R FOUND TO HAVE CORRODED WASTE INTERNAL DOUBLER. CFIII FR88-90, STR25R-29R INTERNAL DOUBLER HAS BEEN REPLACED IAW ERJ-170SRM 51-41-02 AND SRM 51-21-01.SDR SWAA2023112819626Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN UNDER AFT CARGO DOOR SCUFF PLATES; AT WL 154 - 161; RBL 27 - 30; AT BS 800.5; BS 807; BS 815; BS 820.5; BS 827; BS 835; BS 841; AND BS 844<[01] VERIFIED STEP 1 IN PARTIAL.;[02] NO DAMAGE NOTED AT DISCREPANCY AREA PER SRM 51-SDR IPXA2023112189904Skin · damagedFUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-8R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER. UPON FURTHER INSPECTION FOUND DAMAGE TO WITHIN LIMITS FOR ALLOWABLE DAMAGE IAW SRM 53-30-01. BLENDED OUT DAMAGE AND REFINISHED SURFACE IAW SRM 51-10-0SDR CALA2023111503376Skin · crackedL/H FR35 STR30 HOLE #2 CRACKED IN AFT SKIN LAYER AT THE 5 O''CLOC K POSITION A3NB-53-3-6315 PER HAECO LCQ NON ROUTINE 9296122/4012 2 GENERATED BY V061632 INTERIM REPAIR WAS COMPLETED IAW ECRA 5330-07105 PART 1. INSPECTION REQUIREMENTS OF ECRA 5330-07105 PART 2SDR DALA2023110909228Unknown · unknownA/C SKIN AROUND LAV SVC DOOR EVIDENCE OF CROSSION. - P -SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0244:2021-2025/005 00185 COMPLIED WITH ER/A 613142-14 PRI REV 0, ER/A 613142-14 PRI REV 1 AND FINAL ER/A 613142-14SDR IPXA2023110889941Unknown · unknownFUSELAGE SKIN HAS A BURN HOLE AT B STA 488 APPROX 4" ABOVE S-14R MEASURING 0.047" DEEP AND 0.084" IN DIAMETER.SDR IPXA2023110889904Unknown · unknown*SDR FILED OPEN* FUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-14R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER.SDR JR2R11082023816Doubler · corrodedAFT WIFI ANTENNA DOUBLER CORRODEDSDR DALA2023110809205Unknown · unknownSHIP 3423 DURING LIGHTNING STRIKE INSPECTION, FOUND EVIDENCE OF STRIKE ABOVE SECOND PASSENGER WINDOW AFT OF 1L DOOR. CORRECTIVE ACTION: C/W P.R.I. 613533-14. PERMANENT REPAIR C/W PER ERA 613533-14. (5042971)SDR SWIA202401301107Skin · damagedUNDER PANEL 321AT FWD DORSAL STARK, TOOLING DAMAGE IN SEVERAL AREAS TO THE EXTERIOR FUSELAGE SKIN (MARKED) 27394743 (C-CHECK RO 1/30/2024) BLENDED OUT TOOLING DAMAGE IN SEVERAL AREAS TO THE EXTERIOR FUSELAGE SKIN UNDER PANEL 321AT. REF: CRJ-700 SRM 51-12-0SDR IPXA2023111979160Skin · out of limits*SDR FILED OPEN* FAULT: PUNCTURE BETWEEN STA 1400- 1420. STR 24-25 L/H. GIVEN THE OK TO APPLY TOP COAT. SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF REV 118.00 SRM CHAPTER 53-00-01-2R-29, TABLE 206, FOR ZONE A.SDR SWIA2023111007Unknown · dentedDENT ON LH SIDE OF FWD FUSELAGE IN BETWEEN FR09 AND FR10 AND IN BETWEEN STGR17 AND STGR18 MEASURES 0.125 IN DEPTH IS OUT OF LIMITS IN REFERENCE TO ERJ175 SRM 53-10-01/AD02. SKIN DAMAGE HAS BEEN CLASSIFIED AS A MAJOR REPAIR PER GMM 3-26 FORM M-337 REQUIRED. (FISDR SWIA202311170006Unknown · dentedTHREE DENTS FOUND JUST BELOW SKYWEST LOGO ON CAPTAIN SIDE. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27392791 WITH THE FOLLOWING CORRECTIVE ACTION: "REPAIRED DENTS TO FWD FUSELAGE SKIN, LH SIDE BETWEEN FR09 - FR11 AND STR17R - STR18R IN REF TSDR 2023FA0000736Unknown · unknownFOUND LIGHTNING STRIKE ON FUSELAGE EXTERNAL SKIN, STA 180.5, STR 30L.SDR 2023FA0000735Unknown · unknownFOUND SEVERAL BLEND OUTS ON FUSELAGE EXTERNAL SKIN, STA 266 TO STA 287, STR 22L TO STR 24L.SDR VNAA202312130011Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 7-8 LH AND FS 501.00 CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 7-8 LH AND FS 501.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202312130010Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 15 LH AND FS661.00+32.00. CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 15 LH AND FS661.00+32.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202312130009Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 16-17 LH AND FS501.00-FS517.00 CORRECTIVE ACTION: LIGHTNING STRIKE ON FWD FUSELAGE, ABOVE FLOOR BTW STGR 16-17 LH AND FS501.00-FS517.00 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202312130008Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 14 LH AND FS830.40-FS830.40+16. CORRECTIVE ACTION: LIGHTNING STRIKE ON CENTER FUSELAGE, ABOVE FLOOR BTW STGR 14 LH AND FS830.40-FS830.40+16 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202312130006Skin · damagedDESCRIPTION: LIGHTNING STRIKE ON REAR FUSELAGE BTW FS 1088.20 AND STGR O- STGR 1 RH. CORRECTIVE ACTION: LIGHTNING STRIKE ON REAR FUSELAGE BTW FS 1088.20 AND STGR O- STGR 1 RH WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03.SDR VNAA202312130004Skin · corrodedCORROSION ON CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH. CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-21-032. REV --SDR CALA2023110803316Doubler · corrodedFWD CARGO FR 30-34 STR 43-43 CORROSION ON DOUBLER AROUND FASTENER HEADS (A3NB-53-3-6105) GENERATED AT HAECO LCQ PER NR 9296612 ( 40612) REMOVED AND REPLACED DOUBLER FWD CARGO FR30-34 STR 43R-44 IAW A 319 SRM 51-42-11 RESTORED SURFACE PROTECTION IAW A319 SRM SDR DALA2023110609146Unknown · unknownSHIP 0661 ON APPROACH @2000' WE HAD A BIRD STRIKE. UNEVENTFUL LANDING. BIRD HIT LOWER EDGE OF RADOME AND CAUSED CRACK 3 FEET LONG. CORRECTIVE ACTION: REF ERA 613266-14. (9967446)SDR IXXA2023122903Skin · damagedLIGHTNING STRIKE DAMAGE AT STA. 676 STRINGER 3R-4RSDR VNAA202312130002Skin · nickedDESCRIPTION: SEVERAL NICKS ON REAR FUSELAGE BTW FS1015.00-FS1051.30 AND STGR 24RH-27RH CORRECTIVE ACTION: SEVERAL NICKS ON REAR FUSELAGE BTW FS1015.00-FS1051.30 AND STGR 24RH-27RH WERE REPAIRED PER REO 690-53-61-1290 REV - -, AND EVALUATED WITHIN LIMITS PER CRSDR JJBA20231108006Unknown · unknownCRACKS SUSPECTED (6X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. AFTER NDT INVESTIGATION, 5 CRACKS FOUND. SKIN REPAIRED WITH DOUBLER AND BUSHINGS.SDR DALA2023110709165Unknown · unknownSHIP 187 HFEC SURFACE INSPECTION FOUND 01EA CRACK APPROX. 0.200 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW THE 8TH FASTENER AT STR S-13L, AFT STA1654.5. CORRECTIVE ACTION: DAMAGED AREA CUT OUT AND REPAIRED AS PER B767-300 SRM53-80-01 -2R REPAIR 7 FIGURE 201 REVSDR IXXA2023110303Skin · crackedFUSELAGE SKIN AND BEAR STRAP IS CRACKED AT THE L1 DOOR LOWER CORNER.SDR 2023FA0000724Unknown · unknownFOUND MULTIPLE DENTS AND A COUPLE OF BUCKLING ON FUSELAGE SKIN, STA 1197+132 TO STA 1241, STR 36L TO STR 36R.SDR 2023FA0000714Unknown · unknownFOUND BUCKLING (OIL CAN) ON FUSELAGE EXTERNAL BOTTOM SKIN, STA 1906 TO STA 1915, RBL 4.SDR 2023FA0000713Unknown · unknownFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN, STA 129 TO STA 434, STR 12L TO STR 21R.SDR 2023FA0000712Unknown · unknownFOUND BLEND OUTS AND DENTS ON FUSELAGE EXTERNAL SKIN, STA 1351 TO STA 1373, STR 24R TO STR 33R.SDR 2023FA0000708Unknown · unknownFOUND 24 BLEND OUTS ON FUSELAGE SKIN ON FWD CARGO DOOR BETWEEN STA 615 AND STA 654, STR 20R TO STR 30R.SDR WX0A1900010031892Unknown · unknown(MAJOR REPAIR) FWD FUSELAGE EXTERNAL SKIN PANEL AT FR34,NICK FOUND BETWEEN STGR43L/H-STGR43R/H. / FWD FUSELAGE EXTERNAL SKIN PANEL AT FR34 AND BETWEEN STGR 43LH - 43RH REPAIRED PERFORMED PER AIRBUS DOSSIER #80091659 AND TD/80091659/038/2023#B AND ALLEGIANT AIRSDR SWIA2023111400002Unknown · gougedTRANSFER FROM EAML 1239521 : WRITE UP FROM EAML 1239214. FOUND GOUGE IN SKIN AT FRAME 20.5 AND STRINGER 9 TO BE .042" DEEP, 1.5 INCHES LONG, AND 0.249 INCHES WIDE. (FILED CLOSED)REPAIR ACCOMPLISHED BY MHIRJ REFER TO SOW MIS-4505 DATED 11/11/2023 - I/A/W ETD 20SDR DALA2023110309077Unknown · unknownSHIP 6811 WINGS/CENTER WING BOX/UPPER SKIN/AFT PANEL, Y=1000 -1020 / LBL 60-64 / CORROSION. CORRECTIVE ACTION: REF ERA 612879-14SDR DALA2025102107700Skin · mechanic error(LOG 0044125) WHILE IN ATL DURING REMOVAL OF THE LEFT EMERGENCY LIGHT (P/N: 284A0132-3; FIN: L547), MTC CAUSED TOOLING DAMAGE TO THE INSIDE SURFACE OF THE FUSELAGE SKIN PANEL (P/N: 146A3201-10). THE DAMAGE IS LOCATED AT STA 727F+11 AND BETWEEN STR 21L TO 22L.
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