JASC 5350
Service difficulty reports · 6,123
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 SWAA2022082943554Access Panel · erodedEROSION ACCESS PANEL 193CR BODY FAIRING AT LOWER FUSELAGE 2022-418546 / [01] TOOL USED CALIPER P/N 500-752-20 S/N B16101225 DUE DATE 21/MAY/23.;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE:16-JAN-23.;[03] TOOL USED SCALE P/N:91847 S/N:AE-40932SDR SWAA2022082943555Access Panel · erodedEROSION ACCESS PANEL 193CL BODY FAIRING AT LOWER FUSELAGE 2022-418544 / [01] TOOL USED CALIPER P/N 500-752-20 S/N B16101225 DUE DATE 21/MAY/23.;[02] TOOL USED: HOT BONDER P/N:HCS9000B S/N:15092096 DUE DATE:16-JAN-23;[03] TOOL USED SCALE P/N:91847 S/N:AE-409320SDR DALA2022080805397None · none(LOG 2351918) DURING INSPECTION FOUND WORN LOWER SURFACE ALSO AROUND ON HOLES TO ATTACH NUT PLATES STA 727 + 2.7 BTW LBL 23.0 AND RBL 23.0 AT FAIRING SUPPORT STRUCTURE. PERMANENT REPAIR WAS PERFORMED AROUND ON HOLES TO ATTACH NUT PLATES STA 727 + 2.7 BTW LBL 2SDR DALA2022080805393None · none(LOG 2351045) DURING INSPECTION FOUND ELONGATED NUTPLATES HOLE (3 EAS) ON FARING PANEL SUPPORT STRUCTURE AT BS. 727+2.7 BTW LBL 3" TO 18". ELONGATED NUTPLATES HOLE (3 EAS) WERE REPAIRED PER PRI 601113-14 REV. 1 AND PER ER/A 601113-14AD REV. ORIG.SDR IPXA2022080584950Flap · crackedINSPECTION TYPE:SEGPANEL 143CL LEADING EDGE IS CRACK.REMOVED AND REPLACED IAW SRM 51-40-21.SDR DALA2022080805400None · none(LOG 2350647) DURING INSPECTION FOUND WING-TO-BODY FAIRING STRUCTURE SUPPORT FRAME, STA. 727 PLUS 2.7 ELONGATED HOLES. REPAIRED DAMAGE PER ERA 601113-14.SDR SWAA2022080136057Radome · delaminatedNOSE RADOME BOOT IS DELAMINATED / [01] REMOVED AND REPLACED NOSE RADOME; BONDING AND GAP CHECK GOOD PER AMM 53-52-00.SDR SWAA2022080135920Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES / [01] REPLACED PANEL 193B PER SRM 51-40-02;[02] C/W INSP.SDR SWAA2022072935489Panel · elongatedWING TO BODY FAIRING PANEL 193B REQUIRES REPLACEMENT DUE TO MULTIPLE ELONGATED HOLES AND DAMAGE TO THE PANEL / [01] REPLACED PANEL REF TASK 5351-I-14108-NG;[02] REPLACED PANEL REF TASK 5351-I-14108-NG .;[03] REPLACED PANEL REF B737 AMM 53-51-21 AND TASK 5351-ISDR 1UPA20220705039Cap · detachedPARACHUTE CAP DEPARTED FLIGHTSDR DALA2022072505094None · none(LOG 2322583) DURING INSPECTION FOUND ELONGATED HOLES ON SUPPORT STRUCTURE STA Y=727 BTW RBL 20 AND LBL 20 . HOLES ON SUPPORT STRUCTURE STA Y=727 BTW RBL 20 AND LBL 20 WERE REPAIRED PER PRI 600347-14 REV. 2 AND ERA 600347-14AD REV. ORIGINAL.SDR DALA2022072105055None · none(LOG 2329899) DURING INSPECTION FOUND WORN INNER /LOWER SURFACE ALSO AROUND ON HOLES TO ATTACH NUT PLATE STA 727 + 2.7 BTW LBL 23.0 TO RBL 16.0 AT FAIRING SUPPORT STRUCTURE. FAIRING SUPPORT STRUCTURE WAS REPAIRED PER ER/A 600887-14AD REV. ORIGINAL.SDR DALA2022072405085None · none(LOG 2328866) DURING INSPECTION FOUND ENLOGATED HOLES ON FWD POSITION (4 EAS) ALSO ENLOGATED HOLES AFT POSITION (3EAS) AT ACCESS PANEL 194E. ACCESS PANEL 194E WAS REPAIRED PER B-737-800 S.R.M. 51-70-05-2R-8 PAR. 4. E. TO G. IN REFERENCE WITH B 737-800 S.R.M. 5SDR DALA2022072205073None · none(LOG 2329499) DURING INSPECTION FOUND WING-TO-BODY FAIRING STRUCTURE / SUPPORT FRAMES, STA. 727 +2.7 / WEAR. MAINTENANCE REPAIRED DAMAGE PER ERA 600887-14.SDR DALA2022072105056None · none(LOG 2328871) DURING INSPECTION FOUND ENLOGATED HOLES ON FWD POSITION (3 EAS) ALSO ENLOGATED HOLES AFT POSITION (4 EAS) AT ACCESS PANEL 193D. ACCESS PANEL 193D WAS REPAIRED PER B737-800 SRM 51-70-05 -2R PROCEDURE 6 REPAIR 6 & B737-800 SRM 51-70-05-2R PROCEDURESDR SWAA2022081630310Access Panel · crackedCRACK WING TO BODY FAIRING ACCESS PANEL 193D INNER SKIN AT LOWER FUSELAGE 2022-381646 / [01] TOOL USED CALIPER PN: 500-197-30 SN: B22072617 DUE DATE: 26-JUN-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18165044; 28-FEB-23.;[03] TOOL USED: SCALE P/N: 9184SDR SWAA2022072529649Panel · elongatedAFT CENTER WHEEL WELL PANEL 193D MATING SURFACE HAS WEAR MARKS AND SEVERAL ELONGATED HOLES. / [01] REMOVED AND REPLACED AFT CENTER WHEEL WELL PANEL 193D ; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00CLW5Q;[02] VERIFIED STEP 1.SDR DALA2022071504899None · none(LOG 2318632) DURING INSPECTION FOUND ELONGATED HOLES AND WEAR ON SETLEMENT AREA ON AFT EDGE AT ACCESS PANEL 193D. REPAIRED PER B737-800 S.R.M. 51-70-05-2R PROCEDURE REPAIR GENERAL , PER B737-800 S.R.M. 51-70-05-2R PROCEDURE 8 REPAIR 8 IN REFERENCE PER B737-80SDR SWAA2022071226770Panel · elongated193B PANEL HAS SEVERAL HOLES ELONGATED / [01] REMOVED AND REPLACED WITH NEW PANEL PER SRM 51-40-02.;[02] C/W INSPSDR SWAA2022080126783Access Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2022-383815 / [01] TOOL USED CALIPER PN: 500-193-30; SN: 0000285; D/D: 10/DEC/22.;[02] TOOL USED HOT BONDER PN: HCS9200B; SN: 18175478; D/D: 05/AUG/22.;[03] TOOL USED SCALE PN: 91847; SN: AE-409314; D/DSDR VNAA202207079995Strap · corrodedAFT BELLY FAIRNING SUPPORT STRUCTURE FROM FS879 TO FS939 STR24R STRAP WITH NUTPLATES ATTACHED HAS SEVERAL AREAS OF CORROSION AROUND NUTPLATES ON BOTTOM SIDES.SDR 1UPA20220705041Cap · departedPARACHUTE CAP DEPARTED FLIGHT ON TWO SEPARATE OCCASIONS (JUNE 21, 2021 & MAY 23, 2022)SDR 1UPA20220705040Cap · departedPARACHUTE CAP DEPARTED FLIGHTSDR ABXA2023050475Frame · crackedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE WAS REQUIRED TO INSPECT THE RIGHT INNER FRAME CHORD, LOCATED AT BS 883.5, LBL 89 PER ABX JOB CARD ABX-NEA-5350-0015-001 (AD 2012-22-17, SB 767- 53A0209 AND AD 2018-11-08, SB 767-53A0278). DURING INSPECTISDR SWAA2022072224539Panel · crackedCRACK ON FASTENER HOLES ON 193AR ACCESS PANEL AT LOWER FUSELAGE 2022-384725 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-412136; D/D: 14/MAR/23;[03] TOOL USED HOTBONDER P/N:HCS9200B S/N:1819612SDR SWAA2022072224538Panel · crackedCRACK ON FASTENER HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE 2022-384724 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-412136; D/D: 14/MAR/23.;[03] TOOL USED HOTBONDER P/N:HCS9200B S/N:181961SDR SWAA2022070123798Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED COUNTERSINK FASTENER HOLES. / [01] REPLACED PANEL 193B PER SRM 51-40-02;[02] VERIFIED REPLACE PANEL 193B PER SRM 51-40-02SDR DALA2022063004549None · none(LOG 2296821) DURING INSPECTION WEAR PANEL SUPPORT STRUCTURE P/N 149A7593 -WAS FOUND. PANEL SUPPORT STRUCTURE P/N 149A7593 WAS REPAIRED PER ERA 599812-14AD REV. ORIGINAL.SDR SWAA2022071322476Bracket · corrodedCORROSION -- WING TO BODY FAIRING SUPPORT BRACKET HAS FRETTIOG CORROSION; O/B OF ECS EXHAUST. / [01] REMOVED DAMAGE WING TO BODY FAIRING SUPPORT BRACKET O/B OF ECS EXHAUST IN REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW WING TO BODY FAIRING SUPPORT BRACKSDR SWAA2022062722104Panel · elongated193B PANEL FASTENER HOLES 1; 2; 3; 5; 8; 10; 16; 21; 26; 29; 30 AND 31 ARE ELONGATED. 193B PANEL FASTENER HOLES 1 2 3 5 8 10 16 21 26 29 30 AND 31 ARE ELONGATED. / [01] COMPLIED WITH EA 22-153-01854;[02] PERFORMED TIME LIMITED REPAIR PER TSR: 2022004838 AND EASDR ABXA2023050476Keelbeam · crackedDURING AN AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED CORROSION AND A CRACK ON THE R/H SIDE KEEL BEAM CHORD, UPPER FLANGE AT STA 792. AFTER LOCAL FASTENERS IN THE CHORD UPPER FLANGE HAD BEEN REMOVED, A 4.75” CRACK WAS DISCOVERED. A SURFASDR SWAA2022062721355Bracket · crackedRIGHT WING FWD WTB TO FIXED L/E SUPPORT STRUCTURE CRACKED / [01] REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02 AND AMM 53-51-21SDR JJBA20220721017Web · crackedCOCKPIT RH OVERHEAD HORIZONTAL WEB CRACKED AT GRAB HANDLE SUPPORT. REPAIR DOUBLER ON RH FWD FUSE 2 WINDOW FLIGHT COMPARTMENT OVERHEAD PANELSDR SWAA2022072920814Panel · elongatedAFT OF MAIN W/W ACCESS PANEL # 194 E HAS ELONGATED & CRACKED HOLES AT EDGES / [01] MEASUREMENTS;[02] CLEANED AREA AND REPAIRED DAMAGE HOLES AS MARKED ON ACCESS PANEL 194E WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-9; MATERIALS USED PO#1690463 AND PO#1SDR SWAA2022062220179Panel · elongated193B PANEL VARIOUS FASTENER HOLES (30) ARE ELONGATED. / [01] R & R 193B WING TO BODY PANEL PER AMM 53-51-21.SDR DALA2022061704229Panel · worn(LOG 2280504) DURING INSPECTION WEAR SENTTLEMENT AREA OF FAIRING PANEL 193D WAS FOUND. FAIRING PANEL 193D WAS REPAIRED PER B737-800 SRM 51-70-05-2R PROCEDURE 6 PAR. 4 B AND C IN REFERENCE 53-40-70-2R PROCEDURE 1.SDR SWAA2022061618173Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND OVERSIZED COUNTERSINKS. / [01] REPLACED PANEL 193B PER SRM 51-40-02SDR FDEA202206101412Support Angle · crackedRIGHT MAIN LANDING GEAR WHEEL WELL WING TO BODY SUPPORT ANGLE IS CRACKED APPROX. BS1088 REMOVED, FABRICATED NEW PART, AND INSTALLED PER BAC DWG 149N7552 REV FSDR SWAA2022070116629Access Panel · crackedCRACK ACCESS PANEL 191D LATCH AT LOWER FUSELAGE 2022-316804 / [01] REPLACED LATCH ON ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9;[02] REPLACED LATCH ON ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND 51-1SDR SWAA2022060916040Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES / [01] REPLACED PANEL 193B PER SRM 51-40-02SDR SWAA2022060915971Radome · delaminatedRADOME HAS DELAMINATION / [01] ACCOMPLISHED EA 22-153-01684; PER TSR #2022004444. APPLY SCOTCHBRAND 853 OR PERMACEL P280 TAPE TO DAMAGED AREA WITHIN 5 FLIGHT CYCLES. ACCOMPLISH INSPECTION EVERY 480 FLIGHT HOURS AND PERMANENT REPAIR DUE WITHIN 85 DAYS.;[02] ACCSDR SWAA2022071315384Access Panel · elongatedCENTER LWR AFT FAIRING ACCESS PANEL 194E FASTENER HOLE ELONGATED (25-162) / [01] PREPARED AREA FOR REPAIR FASTENER HOLE ELONGATED AT CENTER LWR AFT FAIRING ACCESS PANEL#194E AS PER B737-800 SRM 51-70-04-2R-9;[02] REPAIRED ELONGATED HOLE AT CENTER LWR AFT FAIRISDR SWAA2022071115496Access Panel · crackedCRACK ACCESS PANEL 195CL AT LOWER FUSELAGE 2022-307299 / [01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01-OCT-22.;[02] TOOL USED HOTBONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE: 16 JAN 23.;[03] TOOL USED SCALE P/N:CL5000 S/N:AE-39882 DUE DATE: 2SDR SWAA2022061715076Access Panel · crackedL/H OVERWING FAIRING ACCESS PANEL 195BL HAS A CRACK AROUND FASTENER HOLE / [01] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY REPAIR; NO WATER NOTE ON REPAIR AREA AT ACCESS PANEL 195 BL. REF B737-700 SRM 51-70-04-2R-9 PARAGRAPH 4 C;D;E;F;G;H;I ASDR SWAA2022060714764Panel · elongated193B PANEL HAS ELONGATED HOLE AT THE #17 POSTION / [01] REMOVED AND REPLACED 193B PANEL <BR>REF AMM 53-51-21;[02] CWSDR SWAA2022062714559Panel · delaminatedPANEL 194CL HAS OF DELAMINATION ON OUTSIDE SKIN PANEL 194CL HAS A SPOT OF DELAMINATION ON OUTSIDE SKIN / [01] REMOVED DAMAGE PER SRM 51-70-01-2R-1;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] POTTED CORE PER SRM 51-70-05-2R-11;[04] INSPECTED WORK PERFORMED ON SDR DXTA2022060263180None · noneAERODYNAMIC FAIRINGS (RADOME, TAILCONE, STRAKE): ON DEPARTURE AT LANDING GEAR RETRACTION, WE EXPERIENCED A VIOLENT VIBRATION IN THE AIRFRAME ABOUT 5-7 SECONDS INTO THE GEAR RETRACTION SEQUENCE. THE VIBRATION CAUSED AN AUDIBLE SHAKING SOUND IN THE AIRFRAME BUT SDR SWAA2022071118959Access Panel · erodedEROSION ACCESS PANEL 193AR AT LOWER FUSELAGE 2022-268150 / [01] TOOL USED CALIPER P/N 500-197-30 S/N 021043156 DUE DATE 20/AUG/22;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185781. DUE DATE 16-JAN-23.;[03] TOOL USED SCALE P/N: SCA-301 S/N: AE-412136 DUE SDR IPXA2022060482806Support Angle · corrodedINSPECTION TYPE:SEG4RH WTB T-CHORD AT STA 1040-1060 JUST O/B OF ECS EXHAUST VENT PANEL IS CORRODED OUT OF LIMITS AND REQUIRES REPLACEMENTREMOVED AND REPLACED SUPPORT CHORD I.A.W. SRM 51-40-02, SRM 51-40-05, SRM 51-20-01 AND AMM 51-21-15 FABRICATED ON TRAVELER#SDR SWAA2022071113437Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR 2022-268032 / [01] TOOL USED CALIPER P/N 500-197-30 S/N 021043156 DUE DATE 20/AUG/22;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185781 DUE DATE 16-JAN-23;[03] TOOL USED SCALE P/N: SCA-301 S
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