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 DALA2020012210487Cable · frayedTHE TAIL CONE KEVLAR CABLE WAS DISCOVERED FRAYED. MAINTENANCE REPLACED THE KEVLAR CABLE IAW AMM 53-52-01.SDR IPXA2020020751900Longeron · gougedINSPECTION TYPE:2CEXTENDED TAIL CONE HAS WEB/ZEE LONGERON GOUGED AT R/H HOLE, FWD. END OF PLATFORM.REMOVED, FABRICATED AND REPLACED ZEE/LONGERON IAW DWG. AKC7609 AND SRM 51-31-01. (MINOR)SDR IPXA2020020751899Frame · gougedINSPECTION TYPE:2CTAIL CONE FWD. UPPER MAIN FRAME IS GOUGED ON L/H SIDE.REPAIRED TAIL CONE FRAME IAW SRM 53-00-00 FIG. 210. (MINOR)SDR SWAA2021081917735Bracket · crackedRT SIDE FUSELAGE FWD STRAKELET FAIRING SUPPORT BRACKET CRACKED AT APPR. STA 500D / REMOVED AND REPLACED BRACKET REF SRM 51-40-02.SDR DALA2020011700353Louver · damagedON WALK AROUND FOUND RT FWD WTBF LOUVER MISSING PIECES. REMOVED AND REPLACED R FWD WTBF LOUVER PER AMP J53-82.SDR IPXA2020020751898Doubler · wornINSPECTION TYPE:2CTAIL CONE L/H INTERNAL PRODUCTION DOUBLER HAS WEAR AT STA. 2165, X=36 AND Z=35-60.REPAIRED DAMAGED TAIL CONE INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-A. (MINOR)SDR IPXA2020020751895Doubler · wornINSPECTION TYPE:2CTAIL CONE R/H INTERNAL PRODUCTION DOUBLER HAS WEAR AT STA. 2165, X=-36.5 AND Z=35-60.REPAIRED DAMAGED TAIL CONE INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5353-66790-A. (MINOR)SDR DALA2020011600352Longeron · crackedFOUND RT WTBF INTERNAL LONGERON ASSY P/N C02383111-002 CRACKED VERTICAL. REMOVED DAMAGED AREA PER ERA 583765-14 SEC 1 STEP 1 AND 2. PERM REPAIR C/W ON ERA 584302-14 REV ORIG - REF LOG 1428537.SDR DALA2020011600351Longeron · crackedFOUND LT WTBF INTERNAL LONGERON ASSY P/N 602383111-001 CRACKED VERTICALLY. REMOVED DAMAGED AREA PER ERA 583765-14 RI SEC 1 STEP 1 AND 2. PERM REPAIR C/W ON ERA 584302-14 REV ORIG - REF LOG 1428537.SDR SWAA2020011301362Fairing · damagedWING TO BODY FAIRING PANEL 193B HAS ENLARGED FASTNER HOLES AT LOCATIONS 1-4;6;8;10;15-21;24;26 29-32;34-38 MOD / R&R'ED WING TO BODY FAIRING PANEL 1938 IAW AMM 53-51-21.SDR SWIA2020012147957Beam · corroded*AFT FAIRING BEAM IS CORRODED ON LOWER FLANGE, FS559.00+80 - FS568..00 STGR23R. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED WITH NEW AFT FAIRING SUPPORT BEAM AT FS559+80 TO FS568 STRG23R REF CRJ-200 SRM AND BOMBARDIER DWG.SDR SWAA2020011206672Radome · damaged'REF LOG PAGE 1055537' EA NO: 1-753-36325 REV IR. NOSE RADOME HAS MISSING EROSION BOOT MATERIAL MEASURING 6.25' L X 5.0' W. ACCOMPLISH A DETAILED VISUAL INSPECTION OF THE INTEGRITY OF THE APPLIED TAPE ON THE RADOME; ENSURE THE TAPE IS IN SATISFACTORY CONDITIONSDR SWIA2020012047829Fairing · brokenAFT BELLY FAIRING CUTOUT FOR PANEL 195AL HAS (10EA) MISSING/BROKEN RECEPTACLES AS MARKED (C-CHECK) RO:1/14/2020REMOVED AND REPLACED (10EA) RECEPTACLES ON AFT BELLY FAIRING CUTOUT FOR PANEL 195AL REF. EMB 175 SRM.SDR DALA2020011000181Gusset · crackedTAIL CONE GUSSET AT 4:00 POSITION CRACKED. NEW TAIL CONE ORDERED , TAIL CONE INSTALLED ON AMDS W/C 5350- 01077-0101. TAILCONE, AFT U OFF 88-5353-9-0002 49828 ON 88-5353-9-0001 00036. (LP1439304)SDR SWIA2020021848610Fairing · corrodedCORROSION FOUND AROUND MULTIPLE FASTENER HOLES FOR AFT WING TO BODY FAIRING PANELS 196DL AND 196DR ON EXTERIOR SKIN, UNDER ANTI-CHAFE SEALANT, BEWTEEN FS.913.00 - FS.942.00, FROM STGR 21L TO STGR 21R. (C-CHECK) RO 2/14/2020 BLENDED CORROSION AROUND MULTIPSDR SWAA2020010512878Panel · crackedWING TO BODY FAIRING 193D INTERIOR SURFACE AFT EDGE HAS 4 CRACKED FASTENER HOLES / REPAIRED PNL 193D 4 CRAKCED FASTNER HOLES MARKED AT AFT EDGE. IAW B737-700 SRM 53-40-70-2R-1 REV 69; SRM 51-70-04-2R-9; SRM 51-70-04-2R-0 REV 69; AMM 51-21-81-370-802 REV 70; AMSDR DALA2021120607489Fairing · damaged(LOG 6502241) DURING INSPECTION FOUND A/C DAMAGE ON RH SIDE AFT WING TO BODY FAIRING. PANEL 194ER. REMOVED PANEL MON 149A7556 RH AFT WING TO BODY FAIRING PANEL 194ER INSTALLED REMANENT REPAIRE PER B737-800 SRM 53-60-70-2R PROCEDURE . REINSTALLED PANEL PER B737SDR SWAA2020010401923Fairing · crackedCRACK BODY FAIRING GROUND AIR CONDITIONING SERVICE PLATE LOCATED BETWEEN BS520 TO BS540 AND BETWEEN STR 28L TO STR 28R AT LOWER FUSELAGE (2 EA) / REPLACED BODY FAIRING AROUND AIR CONDITIONING SERVICE PLATES LOCATED BETWEEN BS 520 TO BS 540 BETWEEN STR 28L TO SSDR SWIA2020021148419Support Angle · crackedWING TO BODY FAIRING 195DL HAS CRACKED SUPPORT ANGLE (C-CHECK) RO 2/07/2020 REPLACED SUPPORT ANGLE ON BELLY FAIRING 195DL PER SRM AND INCORPORATED MODSUM.SDR SWAA2021082210486Frame · crackedRH LOWER WING TO BODY FAIRING FWD OF WING BOX (194GR) 1.5' CRACK NOTED IN FRAME. / REMOVED AND REPLACED WING TO BODY FAIRING MOUNTING FRAME JUST INBOARD OF SKIN LEADING EDGE REF SRM 51-40-02.SDR SWIA2020030348906Fairing · dentedADM #4953. DENT AT FUSELAGE STATION 559.00 + 112 LH SIDE AFT WING TO FUSELAGE FAIRING (PN 601R35232). DENT DIAMETER IS .750 INCHES BY 1.00 INCHES. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PSDR SWAA2022041289931Tail Cone · delaminatedINSIDE OF TAIL CONE L/H SIDE 10 O CLOCK POSITION HAS A DELAMINATION. / REPAIRED PER SRM 53-80-70-2R-1 AND SRM 51-70-05.SDR DALA2019123197636Support · corrodedCORROSION FOUND ON THE SUPPORT FOR THE BODY FAIRING BETWEEN BS 850 TO 950, WL 133. THE SUPPORT WAS REPLACED IAW SRM.SDR SWAA2022032855450Panel · crackedWING TO BODY PANEL 192BL HAS CRACK / REMOVED AND REPLACED WING TO BODY PANEL 192BL IAW AMM 53-51-21SDR SWIA2020021448449Attach Bracket · crackedRT WING OVER THE WING FAIRING ATTACH BRACKET CRACKED AT FS 473.15 (C-CHECK) RO 2/10/2020 REMOVED AND REPLACED RH WING FAIRING ATTACH BRACKET IAW CRJ 200 SRM.SDR SWIA2020021448448Attach Bracket · crackedRT WING OVER THE WING FAIRING ATTACH BRACKET CRACKED AT FS 461 (C-CHECK) RO 2/10/2020 REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.SDR SWAA2022032511844Panel · delaminatedPANEL 193CL HAS DELAMINATED AREA ON EXTERNAL SURFACE / PANEL 193CL WITH A DELAMINATED AREA ON EXTERNAL SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2SDR SWAA2022032511086Fairing · delaminatedWING TO BODY FAIRING 192AL EXTERNAL SURFACE HAS ANA REA OF DELAMINATION 6' FROM INBOARD EDGE AND 33' FROM AFT EDGE. MARKED / REPAIRED DELAM DAMAGE AREA A+6' FROM I/B & 33' FROM AFT EDGE ON BODY FAIRING 192AL IAW B737 SRM 53-40-70-2R-1; PAR 4 (TABLE 201); SRM 5SDR A6WA2019122047070Fitting · crackedRIGHT LOWER WING TO FUSELAGE FAIRING FITTING CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED FITTING IAW CRJ 200 SRM 51-42-21.SDR A6WA20192047072Bracket · crackedLEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.SDR A6WA20195047074Bracket · crackedLEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AT FS461.00,LBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.SDR A6WA20192047076Bracket · crackedRIGHT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED AT FS 449.85, RBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.SDR A6WA20192047075Bracket · crackedLEFT WING TO BODY FAIRING ATTACH BRACKET CRACKED AT FS 449.85, LBL 45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.SDR A6WA20192047071Bracket · crackedLEFT FUSELAGE TO WING FAIRING BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.SDR SWAA2022041211036Panel · delaminatedWING TO BODY FAIRING 192AL EXTERNAL SURFACE HAS A DENT WITH DELAM LOCATED 6' FROM INBOARD EDGE AND 22' FROM AFT EDGE / REPAIRED DELAM DAMAGE AREA A+6' FROM I/B & 22' FROM AFT EDGE ON BODY FAIRING 192AL IAW B737 SRM 53-40-70-2R-1; PAR 4 (TABLE 201) & SRM 51-70-SDR SWAA2022041261734Panel · delaminatedPANEL 193B HAS DELAMINATED AREAS ON THE EXTERNAL SURFACE IN THE CORE AREA / REPAIRED DELAMINATED AREAS ON THE EXTERNAL SURFACE IN THE CORE AREA OF PANEL 193B IAW SRM 51-70-05-2R-2 & 51-70-05-2R-11 PER 53-40-70-2R-1 7062U 12-21-19SDR SWAA2022041247698Panel · delaminatedFOUND SEVERAL HOLES FOR FASTENERS TO BE DELAMINATED AND OVERSIZED / FABRICATED NEW PANEL 193B PER SRM 51-20-07-0G-0SDR DALA2019121607360Cable · misinstalledMAINTENANCE FOUND THE TAILCONE KEVLAR CABLE AND LOOP TO BE INSTALLED INCORRECTLY. THE CABLE WAS RE-INSTALLED IN ACCORDANCE WITH B717 AMM 53-52-03. THE REQUIRED INSPECTION IS COMPLETE. (QC2019). (LP #3465610)SDR SWAA2022041211168Panel · delaminated193B PANEL HAS DELAMINATION AND ELONGATED FASTENER HOLES. / REPLACED PANEL 193B PER EO #14108 AND SRM 51-40-02SDR SWAA2022041210903Access Panel · elongatedEXTERNAL FUSELAGE; FORWARD CENTER MLG W/W ACCESS PANEL 193B; HAS 7 EA ELONGATED/ENLARGED FASTENER HOLES. MARKED. / REPAIRED AND APPLIED DECORATIVE FINISH ON EXTERNAL FUSELAGE FWD CENTER MLG W/W ACCESS PANEL 193B 7EA ELONGATED HOLES AS MARKED IAW B737 SRM 51-70SDR SWAA2022041210904Access Panel · elongatedEXTERNAL FUSELAGE; AFT CENTER MLG W/W ACCESS PANEL 193D; HAS 5 EA ELONGATED/ENLARGED FASTENER HOLES. MARKED. / REPAIRED 5 EACH FASTENER HOLES AS MARKED IAW 737-700 SRM 51-70-04-2R-9 REV 69; SRM 51-70-04-2R-0 GENERAL REV 69; RESTORED EXTERIOR SURFACE IAW AMM 51SDR REXA2019122601776Channel · crackedCRACKED AFT FAIRING PANEL C CHANNEL AT PANEL 195DL . THE CHANNEL WAS REPLACED IAW SRM 51-42-13-001-001-A01 PAR.6 AND E.O R53573 REV DATE: 22/FEB/18
"SDR IPXA2019121324935Fairing · damagedINSPECTION TYPE:SEGD687952: LT WING TO FUSELAGE FAIRING PANEL DENT & DELAMINATION REPAIRREPAIR FOR WING TO BODY PNLY 193AL ACCOMPLISHED IAW UPS 757 SRM 51-70-05-0G PAR 4C GENERAL.SDR SWAA2022041249054Panel · delaminatedHOLES 3;15;18 AND 32 ARE WORN AND SHOW SOME DELAMINATION. / REMOVED AND REPLACED PANEL 193B REF AMM 53-51-21.SDR SWAA2022041207483Panel · delaminatedPANEL 193AR HAS DELAMINATION DAMAGE ON THE EXTERNAL SKIN / PANEL 193AR DELAMINATION DAMAGE ON THE EXTERNAL SKIN REPAIRED IAW SRM 51-70-05-2R-4 AND PER SRM 53-40-70-2R-1SDR SWAA2022041210900Panel · elongatedEXTERNAL FUSELAGE; PANEL 193CL; ELONGATED/ENLARGED FASTENER HOLE NEAR LOWER END OF PANEL AT FORWARD EDGE. / REPAIRED PNL 193CL ENLONGATED FASTENER HOLES NEAR LOWER END OF PNL AT FWD EDGE. IAW B737-700 SRM 53-40-70-2R-1 REV 69 SRM 51-70-04-2R-9 REV 69; SRM 51-7SDR SWAA2022041214798Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED HOLES. / REPLACED PANEL 193B PER EO# 14108 AND SRM 51-40-02SDR SWAA2022011321403Panel · damagedPANEL 192HR CORNER OF PANEL; TOP SURFACE; SHOWS SIGNS OF FRETTING WEAR AND PAINT EROSION. AS MARKED / EVALUATED; PREPPED; CLENAED AND REPAIRED EXPOSED COMPOSITE AT AFT CORNER; TOP SURFACE ON PANEL 192HR IAW B737 SRM 51-70-08; PAR 3 (A-G) - REV 69; & SRM 53-40-SDR SWAA2022041221391Panel · crackedPANEL 192K ONE FASTENER HOLE HAS CRACKS IN COMPOSITE SURFACE FROM BACKSIDE. / REPAIRED PANEL 192K FASTNER HOLE I/AW 737-700 SRM 51-70-04-2R-9 REV 69; SRM 51-70-04-2R-0 REV 69.SDR SWAA2022041221392Panel · crackedPANEL 193AR ONE FASTENER HOLE HAS CRACKS IN THE COMPOSITE FROM THE BACKSIDE SURFACE. / REPAIRED FASTNER HOLE AS MARKED ON PANEL 193AR I/A/W SRM 51-70-04-2R-9 REV 69; 51-70-40-2R-0 REV 69 PER SRM 53-40-70-2R-1 REV 69.
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