JASC 5350
Service difficulty reports · 6,121
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 SWAA2023053146000Panel · crackedR/H OVERWING FAIRING ACCESS PANEL # 195BR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED PANEL #195BR PER B737 SRM 51-70-06-2R-9 PARA 4.E. MATERIALS USED RESIN P/O#2008859; CLOTH P/O#1690463;[02] VERIFIED ALL STEPSSDR SWAA2023053146361Panel · crackedR/H UNDERWING FAIRING ACCESS PANEL # 192AR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] APPLIED REPAIRED AT FAIRING # 192AR PER B737 SRM 51-70-04-2R-0 MATERIAL USED RESIN EY 3804 PO#2008859 AND FIBERGLASS PO# 1690463 AND DRILLED HOLES REF B-737-700 SRM 51-4SDR SWAA2023053146363Panel · crackedL/H LOWER AFT FAIRING ACCESS PANEL # 194DL HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED ACCESS PANEL # 194DL AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED; RESIN PO# 1800550 AND CLOTH PO# 1738579.;[02] VERIFIED ALL STEPSSDR SWAA2023053146364Panel · crackedLOWER FWD CENTER WHEEL WELL ACCESS PANEL # 193B HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] APPLIED A PERMANENT REPAIR ON DAMAGE FASTENER HOLES AS MARKED ON LOWER CENTER WHEEL ACCESS PANEL #193B AS PER B737 SRM 51-70-04-2R-9. MATERIALS USED PO#1776837; PO#SDR SWAA2023053146366Panel · crackedRIGHT WING-TO-BODY FAIRING ACCESS PANEL # 194AR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED DAMAGE AREAS AT R/W TO BODY FAIRING ACCESS PANEL #194AR AS PER SRM 51-70-04-2R-9. MATERIAL USED BMS9-3-120TYD CL7 PO#1690463 PLUS EY 3804 A/B PO#2008859.;[SDR SWAA2023053147152Panel · crackedLOWER FUSELAGE AFT FAIRING CENTER ACCESS PANEL # 194E HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REMOVED DAMAGED AND PREPARED AREA FOR REPAIR AS MARKED ON ACCESS PANEL #194 E AS PER B737 SRM 51-70-04-2R-9<BR>APPLIED REPAIR IN DAMAGED AREA AT ACCESS PANEL SDR SWAA2023053147153Panel · crackedR/H UPPER AFT FAIRING ACCESS PANEL # 19FR HAS SEVERAL FASTENER HOLES BULGING/CRACKED PANEL # 194FR<[01] REMOVED AND PREPARED DAMAGED AREA FOR REPAIR ON ACCESS PANEL #194FR AS PER; B737 SRM 51-70-04-2R-9<BR>APPLIED REPAIR IN DAMAGED AREA AT ACCESS PANEL #194 FRSDR SWAA2023053147364Panel · crackedR/H LOWER AFT I/B FAIRING ACCESS PANEL # 194CR HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] REPAIRED DAMAGE HOLES AT R/H LOWER AFT I/B FAIRING ACCESS PANEL #194CR AS PER SRM 51-70-04-2R-9. MATERIAL USED EY3804 PO# 1800550 PLUS BMS9-3-7781 PO#1738579;[02] VESDR DALA2023042603254Unknown · unknownSHIP 3302 FWD CENTER BELLY PANEL 191AB HAS AREAS OF DELAMINATION. CORRECTIVE ACTION: REPAIRED IAW PRI 608277-14 AND ER/A 608277-14. (2737791)SDR SWAA2023053146359Panel · crackedRIGHT FUSELAGE ACCESS PANEL # 193CR HAS SEVERALS FASTENER HOLES BULGING/CRACKED<[01] PAINT;[02] APPLIED REPAIR IN DAMAGE AREA ON RIGHT FUSELAGE ACCESS PANEL # 193CR.; AS PER B737 SRM 51-70-06-2R-9 MATERIAL USED PO.1473815 AND PO.1800550;[03] VERIFIED ALL STEPSSDR A6WA202304248581Hinge Arm · corrodedTOILET SERVICE DOOR 196AR LOWER HINGE IS CORRODED AND BONDING JUMPER IS BROKEN. ********AIRCRAFT REMOVED FROM SERVICE*********** INSTALLED 2EA NEW SERVICEABLE HINGE ARMS IAW CRJ-200 SRM 51-41-02 AND 51-42-21. REPLACED JUMPER IAW CRJ 200 AMM 51-80-00-400-802. SDR SWAA2023042429842Bracket · brokenLOWER FUSELAGE KEEL BEAM PANEL 192E; FEW R/H HANGER BRACKET BROKEN.<[01] REMOVED AND REPLACED HANGER BRACKET PER SRM 51-40-02SDR SWAA2023050129554Panel · crackedPANEL 193D SEVERAL ATTACHMENT HOLES CRACKED<[01] FAULT RAISED IN ERROR; PANEL WAS REPLACED ON T/C TTG8Q00JRU9QSDR SWAA2023042029033Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02;[02] C/W INSPECTIONSSDR SWAA2023042028428Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02SDR SWAA2023051727729Panel · brokenPANEL 191D INNER SKIN HAS PIECE OF A BROKEN HINGE IMBEDDED NEAR CENTER OF PANEL. IDENTIFIED PANEL MATERIAL IAW SRM 53-30-70-0I-1 SHEET 1; FIGURE 2. VERIFIED CURED POTTING COMPLETE AT ROOM TEMPERATURE; SANDED POTTED AREA TILL SMOOTH AND FABRICATED REPAIR PLIESDR SWAA2023053127586Panel · crackedCRACK ACCESS PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR 2023-257914<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:26-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18196126 DUE DATE: 26-MAR-24.;[03] TOOL USED: SACLE P/N: SPX621 S/N:SDR SWAA2023053127587Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2023-257916<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189416; DUE DATE: 19-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9000B-AV; S/N: 18185761; DUE DATE: 24-SEP-23.;[03] TOOL USED: SCALE P/N: CR52SDR SWAA2023052227576Fairing · peelingR/H WING TOBODY FAIRING 192BR FWD END EXTERIOR SKIN PEELING MKD DOT<[01] DUPLICATE ITEM - THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00KFNWQ;[02] VERIFIED DUPLICATED.SDR SWAA2023041928038Fairing · crackedR/H WING TO BODY WEDGE FAIRING AFT OF MAIN WHEEL WELL CRACKED.<[01] REMOVED BROKEN R/H WING TO BODY WEDGE FAIRING PER SIP;[02] REMOVED AND REPLACED R/H WING TO BODY WEDGE FAIRING AFT OF MAIN WHEEL WELL PER SRM 51-40-02.SDR SWAA2023050428493Panel · damagedPANEL 192BL AT FWD EDGE HAS EVIDENCE OF LAYER COMPOSITE LOSS.<[01] REPAIRED DAMAGED AREA AT PANEL 192BL AS PER B737 SRM 51-70-04-2R-6 MATERIAL USED RESIN PO#1800550 AND FABRIC PO#1153636.;[02] FINAL INSPECTION; ALL WORK PERFORMED.SDR DALA2023041402971Unknown · unknownSHIP 3354 CRACK SUPPORT WEB BELLY FAIRING LOCATED FR53.2 LOWER LH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 607394-14 REV ORIGINAL. (2716722)SDR DALA2023041302942Unknown · unknownSHIP 3354 CRACK SUPPORT WEB BELLY FAIRING LOCATED FR53.2 LOWER RH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLETED WITH ER/A 607395-14. PERFORMED REPAIRINSTRUCCION AT FUSELAGE/WING/BODY BELLY FAIRING/LATERAL FRAME 53.2 RH. RII INSPECTION COMPLETE. (2716773SDR SWAA2023051725012Panel · brokenFWD. R/H BRACKET BROKEN AT LWR. FAIRING WING CENTER SECTION PANEL 192E<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE IAW SRM 51-10-02;[02] FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9.;[03] REMOVED FWD R/SDR SWAA2023050527550Panel · crackedRIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661AB HAS SEVERAL FASTENERS HOLES BULGING/CRACKED<[01] REPAIRED AT PANEL # 661AB PER B737 SRM 51-70-04-2R-9 MATERIAL USED RESIN EY3804 PO#1800550 AND FIBERGLASS PO#1690463;[02] VERIFIED 1.SDR SWAA2023050528233Panel · crackedRIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661BB HAS SEVERAL FASTENERS HOLES BULGING/CRACKED<[01] REPAIRED RIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661BB AT DAMAGED AREA PER B737 SRM 51-70-04-2R-9 PARA 4.D. LOCATED AND DRILLED REPAIRED AREAS ON ACCESS PASDR SWAA2023050124882Panel · out of positionPANEL 192DR ACCESS DOOR - HIGH PRESSURE CONNECT - GROUND PNEUMATIC DOOR- I/B EDGE HANGS DOWN TOO FAR.<[01] REMOVED AND REPLACED PANEL 192DR DOOR ASSEMBLY PER SRM 51-40-02 LATCH STOPS ADJUSTMENT WILL BE ACCOMPLISHED ON TTG8Q00KANEV;[02] PARTS UPDATESDR SWAA2023050124475Bracket · elongatedELONGATED HOLES ON NEW BRACKET LOCATED ON WING TO BODY FAIRING AT LOWER FUSELAGE RH 2023-212859<[01] PERFORMED OVERSIZE HOLE ON BRACKET LOC WING TO BODY FAIRING RH SIDE AT LOWER FUSELAGE IAW B737-700 SRM 51-40-05 TABLE B; DIAMETER OF FASTENER NOT EXCEED MAXIMUSDR DALA2023040602695Unknown · unknownSHIP 3352 CRACK SUPPORT WEB BELLY FAIRING AT LEVEL FR 53.2 LH SIDE LOWER AREA A LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON SUPPORT WEB BELLY FAIRING AT LEVEL FR 53.2 LH SIDE LOWER AREA AT LOWER FUSELAGE AS PER SECTIONI OF ER/A 606700-1SDR SWAA2023042023391Panel · delaminatedPANEL 193AL HAS DELAMINATION AT ONE SIDE<[01] APPLIED THE GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON ACCESS PANEL 193AL. REF B737 SRM 51-70-04-2R-10 REPAIR 10 PARAGRAPH 4. MATERIAL USED GLASS FABRIC PLIES PO#:1690463 AND RESIN EY3804AB PO#: 1800550.;[02] VERSDR DALA2023040502627Unknown · unknownSHIP 658 INITIAL INSPECTION: CORROSION ON WING TO BODY FAIRING SUPPORT STA 1040 FROM LBL 20 TO RBL 20. CORRECTIVE ACTION: FUSELAGE MAIN FRAME AT KEEL BEAM FAIRING PANEL SUPPORT TEE STA. 1037.77 & BTW LBL6 & RBL6 WAS REPAIRED PER ER/A N 607292-14 REV ORIGINAL SSDR DALA2023040502626Unknown · unknownSHIP 658 INITIAL INSPECTION: CORROSION ON WING TO BODY FAIRING SUPPORT STA 1040 FROM LBL 20 TO RBL 20. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 607293-14 (2699545)SDR SWAA2023042522721Panel · delaminatedPANEL 193AR HAS DELAMINATION ON OUTER SURFACE<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 18.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A(6).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-2 PER SRM SDR SWIA20230519035Unknown · cracked*BATT RIB AT L/H WING ROOT IS CRACKED. LOCATION FLAGGED. (C-CHECK RO 5/15/2023) REMOVED AND REPLACED WITH NEW ANGLE CAP P/N 600-10389-1 REF BOMBARDIER DWG 600-10212 REV -D, CRJ200 SRM 51-42-06 REV 39 MAR 10/21 AND CRJ200 SRM 51-42-21 REV 39 MAR 10/21. CSDR DALA2023033102476Unknown · unknownAIRCRAFT 9513, AFTER TAILCONE SLIDE REMOVAL, IT WAS FOUND UNPACKED. CORRECTIVE ACTION: TAILCONE SLIDE WAS REMOVED P/N: D29984-213 S/N: 1539 PER AMM 25-61-02-000-801 AND SERVICEABLE TAILCONE SLIDE P/N: D29984-213 S/N: 1561RP WAS REPLACED. (LP 2695495)SDR 2023FA0000169Unknown · unknownDURING MAINTENENCE INSPECTION FOUND CORROSION ON FRAME INNER CHORD, STA 1197+110, STR 19L TO STR 20L.SDR 2023FA0000168Unknown · unknownDURING MAINTENENCE INSPECTION FOUND CORROSION ON THE STRINGER FREE FLANGE, STA 852, STR 20R.SDR 2023FA0000167Unknown · unknownDURING MAINTENENCE INSPECTION FOUND CORROSION ONFRAME OUTER CHORD, STA 927, STR 19R.SDR SWAA2023042521704Panel · delaminatedPANEL 193AR HAS A DELAMINATION ON THE INNER SURFACE SKIN 19.5' FROM THE I/B END; 7' FROM FWD EDGE<DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.A(5DISBOND NOTED; REMOVED 2' DIA OF INNER SKIN AND PARTIAL DEPTH CORE; DISBOND NOSDR SWAA2023041720905Angle · corrodedCORROSION ACCESS PANEL 193AL T-ANGLE AT LOWER FUSELAGE 2023-185576<[01] REPLACED T-ANGLE AND FASTENERS AT LOWER FUSELAGE LOCATED ON ACCESS PANEL 193AL IAW B737-700 SRM 51-40-02 AND DWG 149A7216 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED T-ANGLE AND FSDR SWAA2023041420906Panel · delaminatedDELAMINATED ACCESS PANEL 193CL ON BELLY FAIRING 2023-185577<[01] TOOL USED CALIPER P/N: 500-193-30; S/N: 0000288; DUE DATE: 27-DEC-23.;[02] TOOL USED: SCALE P/N:8340225441 DUE DATE:20-JUL-23;[03] TOOL USED: SCALE P/N:SPX621 S/N:8340225441 DUE DATE:20-JUL-23;[0SDR DALA2023032902407Unknown · unknown(LOG 2688448) PER CARD (5300-01160-06A/B) - FLAP TRACK FAIRING TO BE COMPLIED WITH PER VA 91421.SDR SWAA2023033020926Bracket · brokenAFT SUPPORT BRACKET AT 194BR BROKEN<[01] REPLACED THE AFT SUPPORT BRACKET UNDER PANEL 194BR PER SRM 51-40-02.SDR SWAA2023033020927Bracket · brokenFWD SUPPORT BRACKET AT 194BR BROKEN<[01] REPLACED THE FWD SUPPORT BRACKET UNDER 194BR PER SRM 51-40-02.SDR YENA2023090101011Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / TAIL CONE / FR76-FR77 & STGR26LH - STRG28LH / PERFORATED SKIN - TIME LIMITED REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR SWAA2023041920644Panel · delaminatedPANEL 193CL HAVE A DENT AND DELAMINATION ON THE MIDDLE TOPSIDE OF PANEL.<[01] REPAIRED PANEL 193CL PER SRM 51-70-05-2R-1;[02] VERIFIED REPAIR COMPLETED PER SRM 51-70-05-2R-1.;[03] RESTORED FINISH PER SRM 51-70-05-2R-1.SDR ABXA2023032840Unknown · unknownDURING C CHECK FOUND KEEL BEAM WEB P/N 145T8612 HAS PROTRUDING DENT WITH CRACK AT STA 1045 AND BL 0. 767-200 SRM 53-50-12 ALLOWABLE DAMAGE HAS A REPAIR FOR .250” HOLE, BUT THE CRACK FOUND IS .3” OF LENGTH EXCEEDING LIMITS. FLIGHT VEHICLES CONSULTING INC. WAS CSDR SWAA2023050320371Panel · crackedCRACK BELLY FAIRING ACCESS PANEL 194CR AT LOWER FUSELAGE 2023-208630<[01] TOOL USED: CALIPER P/N: 500-193-30; S/N: 0000288; DUE DATE: 27-DEC-23.;[02] TOOL USED; HOT BONDER P/N: HCS9200B-AV; S/N:18185781; DUE DATE:24/JAN/24.;[03] TOOL USED HOT BONDER P/N: HCS92SDR SWAA2023041219280Fairing · elongatedRIGHT WING FWD UNDER WING FAIRING PANEL #191FR; FASTENER HOLES ELONGATED/DETERIORATED.<[01] REPAIRED AND PAINTED RT WING FWD UNDER WING FAIRING PANEL #191FR AS PER B 737 SRM 51-70-06-2R-9 AND AMM 51-21-73-370-803.<BR>WORK PERFORMED BY ID 6673;[02] VERIFIED PANSDR SWAA2023041018808Radome · crackedNOSE RADOME BOOT HAS MULTIPLE CRACKS AND HOLES EXPOSING FIBER<[01] REMOVED AND REPLACED NOSE RADOME IAW AMM 53-52-00;[02] C/W INSPECTION OF C.A STEP 1 REMOVAL AND REPLACEMENT OF THE NOSE RADOME PER AMM 53-52-00.
Back to JASC 5350