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 SWAA2022040510016Skin · corrodedSUPPLEMENTAL INFORMATION: LIGHT CORROSION FOUND UNDER TOP ATC ANTENNA AT STA 430 . / REPAIRED PER EA 1-753-35762SDR SWAA2019110638645Skin · corrodedCORROSION CROWN SKIN SURFACE CORROSION AT VARIOUS LOCATIONS ALONG DORSAL FIN AREA, BS872 TO BS1017, LBL12 TO RBL12. MOD. / REPAIRED CROWN SKIN CORROSION DAMAGE IAW ER 19-05190 AND EA 1-753-35962.SDR MK1Y2019100610003Skin · dentedDENT ON FUSELAGE SKIN BETWEEN STA 1417 AAND STA 1439, STR 37-38R, DENT DIMENSION:Y=0.067", A=1.24", RATIO: A/Y=18SDR EE4Y2019100409923Skin · crackedLOWER FUSELAGE SKIN DAMAGED AT BS 500B+5, BETWEEN STRINGERS 22L AND 23L. THE DAMAGED AREA WAS REPAIRED IAW INSTRUCTIONS ON EO PD37-53-3026.SDR FDEA201910032417Skin · corrodedBOTTOM EXT FUSELAGE SKIN UPPER SURFACE HAS 2 SQUARE INCHES OR CORROSION AND BULGING LOCATED AT THE MAIN E&E BAY DOOR 119BL FWD CUTOUT BETWEEN 2EA STOP FTGS. COMPLIED WITH EA F-5330-T0349870, P1.SDR A6WA2019100846904Skin · crackedLEFT TRU DOOR CUT OUT CRACKED AT AFT LATCH. REPAIRED IAW 19-016B.SDR TSAA20191003005Skin · dentedREPAIRED DENT DAMAGE ON FUSELAGE BELLY SKIN AT STA 1016-1088 STR 25L-25R IAW KF DRAWING NO. R27904.1-053-011-001 REV NC, SEE FAA FORM 8110-3 FOR APPROVAL.SDR FDEA2019100322402Skin · scratchedFUSELAGE SKIN BETWEEN BS 869 TO 929, LONGERON 9 RT WAS FOUND WITH SCRATCHES. THE SCRATCHES WERE REMOVED, 0.048", SKIN ORIGINAL THICKNESS 0.068", REMAINED THICKNESS 0.020" FOUND OUT OF LIMITD IAW SRM 53-00-00-2R, FIGURE 202. SKIN REPAIRED IAW SRM 53-00-01-SDR SIMA201910032001Skin · crackedDURING HMBV INSPECTION, QC FOUND 2 CRACKS AROUND RIVETS ON RH REAR FUSELAGE I SKIN AT FR 75 BETWEEN STGR 1R AND 3R. -C/A-PERFORMED PERMANENT REPAIR TO CRACKS ON RH REAR FUSELAGE I SKIN AT FR 75 BETWEEN STGR 1R AND 3R IAW EMB 145 SRM 53-31-01-RE REPAIR #11. (RESDR DALA2019100305661Skin · damagedDURING INSPECTION FOUND SCRATCH ON FUSELAGE SKIN STA 823 LONG 22LH. REPAIR WAS PERFORMED PER ER/A 581827-14 REV. ORIG. AND ETI 581827-14 REV. ORIG.SDR COEA2019112215810Doubler · corrodedWO 205731 NR 100043 HEAVY CHECK COE/MAJOR REPAIR: EXTERNAL FUSELAGE #2 DME ANTENNA DOUBLER HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0108050_01...15501 ISSUE A, DATED 11/20/2019.SDR FDEA2019102412743Skin · crackedL/H SIDE LOWER FUSELAGE APROX. STA 575, L46L - L48L, FWD LWR CORNER OF EXHAUST HAS SKIN REPAIR. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED IAW SRM 53-20-15 FIG. 201, REPAIR 3.SDR CALA2019101101745Skin · crackedSUPPORT TASK TAR - QC PICK UP SHEET - EXTERNAL FUSELAGE REPAIR NOT LISTED FOR INSPECTION FROM AIRCRAFT RECORD BTN BS1605-1629 LWR FUSELAGE RBL 6".PLS ADV REPAIR RECORD OR REPAIR INSTRUCTION REF TO NR LP:9131989 BS 1605-29 REPAIRED IAW ECRA 5331-02462 AND SRM 5SDR CALA2019100501691Skin · dentedSUPPORT TASK TAR - LP 6587012 FUSELAGE SKIN DENT BETWEEN STA355 AND STA368 S-22R TO S-23R AFTER MEASURED OF THE DENT, THE DEPTH IS 0.119" LENGTH IS 3.2" AND WIDTH IS 2.1".A/Y IS LESS THAN 30 OUT OF LIMITS AS PER SRM 53-00-01 ALLOWABLE DAMAGE 1, NO APPLICABLE RSDR CALA2019100501690Skin · dentedDENT JUST AFT OF DOOR 1 L. DENT LOCATION STATION 362-370 ABOVE STRINGER 18L , DENT MEASURES 8.5"X4.75" X .250" DEPTH MAX. DENT LOCATION INCORPORATES DAMAGE TO STR 18L APPROX DENT DEPTH AT STR 18L IS .180". DENT WAS CAUSED BY JET WAY CONTACT. DENT IS BEYOND ALLSDR SWAA2022032263658Skin · corroded***CORROSION*** POSSIBLE CORROSION AROUND FASTENERS BS 358 TO 362 BETWEEN STR 27L TO 28L ON FUSELAGE INNER SKIN AND ATTACHING HARDWARE / REMOVED CORROSION ON UPPER SURFACE OF THE BS 360 SPLICE P/N 141A3523-14 BETWEEN BS 358 TO 362 AND STR 27L TO STR 28L (ON FUSDR SWAA2022032250457Skin · corroded***CORROSION*** MULTIPLE AREAS OF CORROSION ON FUSELAGE SKIN FROM BS 847 TO BS 1007; FROM S-2L TO S-2R; WL 306.5 / REPAIRED FUSELAGE SKIN B.S 847-1007 STR 2L- STR 2R W.L 306.5 IAW EA 1-753-35791 REV IR AND ATS ER 19-05054 REV IRSDR IPXA2019102868316Doubler · gougedINSPECTION TYPE:SEGLWR FUSELAGE FWD CARGO DOOR CUTOUT HAS A COUGED OUT DOUBLER APPROX. 19" ABOVE LWR CORNER (FWD)R&R DOUBLER IAW 53-10-12SDR REXA2019102391527Skin · crackedINITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS)
"SUMMARY: RECEPTACLE PLATE AT FUSELAGE WAS REPLACE PER CRJ/900 SRM 51-42-20-001-001-A01 PAR.6A
"SDR REXA2019101491464Doubler · corrodedCORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. A NEW INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS INSTALLED PER CRJ 900 SRM 51-42-06-00SDR CALA2019100541683Skin · dentedBS 1417-1486, STR 24R DENT REPAIRED IAW ECRA 5331-02466, REF ELB LP 3408629 AND HAECO NR LP 9132054, DURING HKG 2C VISIT. ECRA 5331-02466 PART 2 REQUIRES INSPECTION ON OR BEFORE 37,500 FC AND REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 12,000 FC. IAW ECRA 53SDR CALA2019100541679Skin · dentedREMOVE UNAPPROVED REPAIR, MAP OUT DAMAGE OF SKIN PNL AND CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE FURTHER FLIGHT. FR34 ST43L{AD 2016-18-09} {EA5300-02120-001} REF HAECO LCQ NR 929913 2 AND GENERATED BY N078625 REMOVED AND REPLACED REPAIR DOUBLER ON FSDR DALA2019100405716Skin · crackedPERFORM PERMANENT REPAIR ON FUSELAGE SKIN STA 370 BTW STGR 18L AND 19L REF LOG PAGE 3973539. SUMMARY OF NRC S/N: 00571: LOCATED IN REPAIR ZONE A, DAMAGED FUSELAGE SKIN WAS REPAIRED PER B757-200 SRM 53-00-01 REPAIR 29. HFEC INSPECTION WAS ACCOMPLISHED ON FUSELASDR SIMA2019100190004Skin · dentedSKIN DENTED BETWEEN FRAMES 9 & 10, STRINGERS 14L - 15L. PERFORMED A PERMANENT REPAIR IAW ERS-EJ-53DF-3495 PTD AND ERS-EJ-53MR-3902.SDR IPXA2019093047391Skin · delaminatedINSPECTION TYPE:C1WHILE INSPECTING CARD # 128347, UPPER SKIN BETWEEN STA. 1896.20 & STA 1918.9 REPAIR HAS A DENT IN THE MIDDLE THAT IS DELAMINATED DOT 8-055REMOVED OLD REPAIR AND MADE A NEW REPAIR PER UPS RCD 128358, IAW B757 SRM 53-80-01-2R FIG 201 SHEET 1, &SDR SWAA2019101437748Skin · dentedSECTION 48 EXTERNAL SKIN HAS A DENT AT STA 1016 +4.5", 2.0" ABOVE S-14L. / REPAIRED SKIN PER ER AND SWA EA.SDR CALA2019093001667Skin · corrodedB757-06-3-0221 LAVATORY SERVICE PAN BULGING OUT WITH INDICATION OF CORROSION BETWEEN PAN AND SKIN FROM STA 1540-1560 STR 29R-27R . REF ST-ENG N/R 0071138 ACCOMPLISHED ECRA 5331-02469 REV - PART 1 INTERIM REPAIR ON FUSE LAGE SKIN AT LAV SERVICE PAN SKIN CUT OUTSDR R61A201910011044Skin · dentedDENT ON LH FWD FUSELAGE STARTING AT EDGE OF FRAME 10 TO SKIN SPLICE BETWEEN FRAMES 9 &10, STRINGERS 17L-18L. PERFORMED PERMANENT REPAIR BY CUT OUT AND SKIN DOUBLER AT FWD FUSELAGE SKIN LH SIDE BETWEEN FRAMES 9L-10L STGR 17L-18L IN ACCORDANCE WITH REFERENCE ESDR R61A201910011038Skin · dentedDENT ON LT FWD FUSELAGE STARTING AT EDGE OF FRAME 10 TO SKIN SPLICE BETWEEN FRAMES 9 - 10, STRINGERS 17L-18L. PERFORMED PERMANENT REPAIR BY CUT OUT AND SKIN DOUBLER AT FWD FUSELAGE SKIN LH SIDE BETWEEN FRAMES 9L-10L STGR 17L-18L IN ACCORDANCE WITH REFERENCE ESDR CALA2019093001663Skin · corrodedFROM CUSTOMER PICKUP SHEET EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND AFT SIDE AND BETWEEN LAV SERVICE PAN AT STA 1560 STR 27R TO STR 29R. REF ST-ENG N/R 0078758 ACCOMPLISHED PERMANENT REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN STA 1540-1560 R/H ST STRG 26R-30RSDR COEA2019112296810Skin · dentedWO 205731 NR 205731 HEAVY CHECK COE/MAJOR REPAIR: DENTS ON CENTER FUSELAGE L/H UPPER SKIN PANEL FORWARD OF FRAME 23C BETWEEN STRINGERS 4L-7AL. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0106844_01...15312 ISSUE A, DATED 11/20/2019.SDR SWAA2019110838702Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 219+3, 16.5" ABOVE STR. 24R. / SKIN DENT DAMAGE BS 219+3, 16.5" ABOVE 24R STR IS REPAIRED PER SWA EA 1-753-35906 REV IR (ATS ER 19-05208 REV IR).SDR AALA2019100759010Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT BS 915 BETWEEN S21L AND S22L. REPAIRED SKIN PER EA 298639.SDR CALA2019092801648Skin · wornB767-06-3-7140 - EMP RH STAB TO BODY CUTOUT LOWER FWD SKIN DEEP CHAFED, REFER NRC 9130455 DAMAGED SKIN PANEL CUT AND REMOVED AT STA1763.5, HFEC INSP CARRY OUT PER B767 NTM PART 6 51-00-19, NO CRACK FOUND. REPAIR PARTS INSTALLED PER ECRA 5331-02461 RH STAB TO BSDR SWIA2019092646346Skin Panel · nickedTHE FUSELAGE'S RT SIDE SKIN PANEL HAS EXTERNAL SCRATCHES/NICKS THROUGH ITS CLADDING. (C-CHECK) RO: 9/24/2019 PERFORMED BLEND OUT OF DAMAGE AT RT SIDE PANEL AFT IAW SRM.SDR EHNA2019092600003Skin · crackedFROM FAA FORM 337: FOUND RT UPPER FUSELAGE SKIN (P/N 2611001-2) CRACKED AT FS 186.45, RBL 25.40, AND WL 141.00. REPLACED SKIN P/N 2611001-2 WITH NEW PART IAW FIELD REPAIR #FR-208B0319-7011.SDR CALA2019092801647Skin · not reportedREFERENCE LP#3339628 S/M REPAIR OVER DOOR 1L. REPAIR WAS PREFORM ED PER SRM53-00-01 REPAIR 12. DIP IS REQUIRED FOR REINSPECT. FIR ST REINSPECT IS 6,000 F/C AFTER REPAIR & REPEAT INSP EVERY 9,000 F/C REFERENCE SRM 53-00-01 REPAIR 12 TABLE 202. DIP REQUESTED FORSDR DALA2019092605514Skin · dented(LOG 1287145) DURING CCK AT QRO, THREE DENTS WERE FOUND AFFECTING THE FUSELAGE SKIN 143A3212-2, BETWEEN BS 500B & 500C AND S23L & S24L. MAINTENANCE REPAIRED DAMAGE PER ERA 581609-14.SDR IPXA2019092447167Skin · crackedINSPECTION TYPE:N/A *** SUPPLEMENTAL SDR*** FUSELAGE CRACKED AT TOP AFT CORNER OF #3 DOOR (PACK) CUTTOUT. FINISHED FABRICATION OF ALL INTERNAL AND EXTERNAL DOUBLERS AND FILLERS AND SHIMS. PRIMED ALL REPAIR PARTS AND REWORKED AREAS. ALL WORK ACCOMPLISHED PER PRSDR DALA2019092505579Skin · debonded(AIRCRAFT 6714, L/P 1285570) 1 DISBOND WAS FOUND OF 20" X 19" ON L1 DOOR CUTOUT AT FWD UPPER CORNER IN REFERENCE WORK CARD 5331-01232-02G STEP 5.B.(2). CORRECTIVE ACTION: DISBOND AREA WAS BONDED AND REPAIR PERMANENT WAS PERFORMED PER ER/A 581555-14AD REV. ORG,SDR DALA2019092405527Skin · corroded(AIRCRAFT 5642, L/P 1284386) INITIAL INSPECTION: CORROSION ON SKIN FROM STA 1825 TO STA 1862 BTW S-29R AND S-23L ON AFT AREA OF AFT PRESSURE BULKHEAD. CORRECTIVE ACTION: (CORROSION LEVEL 2) SKIN WAS REPAIRED PER ETI-57-19-121 REV: 5 AND ER/A 581581-14 REV: ORISDR SWAA2022032163589Skin · corroded***CORROSION*** ON EXTERNAL FUSELAGE SKIN BETWEEN STA 500D - 520; STR 28R - 28L; WL 150 / EXTERNAL FUSELAGE SKIN BS 500D-520 STR 28R-28L WL 150 REPAIRED PER ATS ER 19-05155 REV IR AND SWA EA 1-753-35948 REV IR.SDR SWAA2019110838691Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 807, STR. 27R TO 27L. / THE DAMAGE IS REPAIRED UNDER ATS ER 19-05191 REV IR AND EA 1-753-35955 REV IR.SDR SWAA2019110838690Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 787+14.6, 1.5" BELOW STR. 27R. / THE DAMAGE IS REPAIRED UNDER ATS ER 19-05191 REV IR AND EA 1-753-35955 REV IR.SDR SWAA2019110838689Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @ STA. 792+10.3, 3.0" ABOVE STR. 26R. / THE DAMAGE IS REPAIRED UNDER ER 19-05191 REV IR AND EA 1-753-35955 REV IR.SDR SWAA2019110838688Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 792+9, 4.0" ABOVE STR. 27R. / REMOVED DENT DAMAGE ON THE EXTERIOR FUSELAGE SKIN @ STA 792+9, 4.0" ABOVE STR. 27R AND INSTALLED REPAIR PARTS IAW SWA EA 1-753-35955 REV. IR AND ER 19-05191 REV. IR.SDR SWAA2019110838687Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @STA. 312+4.8, .5" ABOVE STR. 22R. / REMOVED DAMAGE & REPAIRED EXTERIOR FUSELAGE SKIN @ STA 312+4.8, 5" ABOVE STR 22R IAW EA 1-753-35902 REV IR & ATS ER 19-05221.SDR SWAA2019110838686Skin · dentedFOUND DENT ON EXTERIOR FUSELAGE SKIN @ STA. 787+13.8, 1.6" BELOW STR. 27L. / THE DAMAGE IS REPAIRED UNDER ATS ER 19-05191 REV IR AND EA 1-753-35955 REV IR.SDR DALA2019092305526Doubler · worn(AIRCRAFT 6811, L/P 1282872) WORN ON PREVIOUS REPAIR DOUBLER STA 1280 AND STR 11L AT PAX CABIN. CORRECTIVE ACTION: PREVIOUS REPAIR DOUBLER STA 1280 AND STR 11L AT PAX CABIN WAS REPLACED PER ER/A 518272-14 REV ORIGINAL; SECTION I. AND REPAIR APPROVAL IS LIMITEDSDR FDEA201909222317Skin · corrodedAFT ACCESSORY COMPARTMENT STA 2144 TO STA 2164 RT LONGERON 39 - 43 EXFOLIATION CORROSION ON SKIN AND AROUND NUTPLATES. PERFORMED FUSELAGE SKIN REPAIR IN REF TO SRM 53-70-01, REPAIR # 3.
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