JASC 5350
Service difficulty reports · 6,124
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 A6WA2019020646368Support Bracket · crackedFS469, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.SDR IPXA2019022549370Frame · chafedINSPECTION TYPE:3CFWD. TAIL CONE CANT FRAME AT STA. 2165.061 IS CHAFED AND INTERCOSTAL TORN.REPAIRED DAMAGED TAIL CONE CANT. FRAME AND INTERCOSTAL AT STA. 2165.061 IAW SRM 53-80-07 REPAIR 1. (MINOR)SDR DALA2019020500806Pin · out of positionTAILCONE SLIDE CAM PIN WAS FOUND WITH THE WRONG ORIENTATION. (IN REF 5352-4002). CAM PIN WAS ADJUSTED (ORIENTATED) CORRECTLY PER AMM 53-52-03 820-801.SDR ASOA201902027025Support · crackedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE R/H UPPER ATTACH POINT SUPPORT FLANGE CRACKED ON THE APU TAIL CONE. MAINTENANCE REMOVED THE DAMAGED AREA FABRICATED A NEW PART AND INSTALLED A DOUBLER IAW ETD2019-145-009415. ALL WORK ACCOMPLISHED AND WILL BE RELSDR SWAA2022030245806Bracket · crackedFWD RIGHT ATTACH T-BRACKET BROKE ON PANEL 192E. / REMOVED AND REPLACED PER SRM 51-40-02SDR SWAA2022030245807Bracket · crackedFWD LEFT ATTACH BRACKET BROKE ON PANEL 192F. / REMOVED AND REPLACED BRACKET P/N 149A7711Y7 IAW SRM 51-40-02..SDR DALA2019020410707Cam · excess playTAIL CONE CAM ASSEMBLY HAS EXCESSIVE PLAY, REF NRC 186. MAINTENANCE REPLACED THE CAM ASSEMBLY REF B717 AMM 53-52-03. SEE NRC 186 FOR DETAILS. (LP #0926185)SDR SWAA2022030223639Panel · delaminatedPANEL 193D HAS A DELAMINATED DENT 7.3' FROM THE AFT EDGE; 13.5' FROM THE L/H EDGE / REPAIRED DELAMINATED DENT 7.3' FROM THE AFT EDGE 13.5' FROM THE L/H ON PANEL 193D IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1SDR SWAA2022030249554Panel · crackedPNL 194BR CRACKED / REMOVED AND REPLACED PNL 194BR I/A/W AMM 53-51-21AMT 51848INSP 22640SDR SIMA20190128004Attach Angle · crackedUPPER WING TO FUSELAGE FAIRING ATTACH ANGLE ON FUSELAGE HAS A 1" CRACK AT FRAME 42. REMOVED AND REPLACED RT UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE AT FRAME 42 IAW SRM 51-40-02.SDR SWAA2019012928993Tail Cone · delaminatedUPPER SURFACE OF FUSELAGE TAIL CONE HAD MULTIPLE DENTS WITH SOME EXHIBITING EVIDENCE OF DELAMINATION. REPAIRED TAIL CONE PER SRM.SDR SWAA2019021529650Support Angle · crackedRT FORWARD UPPER WING TO BODY FAIRING SPLICE SUPPORT ANGLE CRACKED AT BS 500D, STR 18R. R&R ANGLE IAW DWG AND SRM.SDR DALA2019012500561Release Cable · wornTHE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN. MAINTENANCE REPLACED THE KEVLAR CABLE PER IPC 53-52-30-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-2001 TAILCONE SERVICE. FUNCTIONAL CHECK WAS SATISFACTORY. (LP #0918007)SDR SWAA2022030123585Panel · delaminatedPANEL 194HL HAS A CREASED DELAMINATED DENT ON THE OUTER SKIN MID SPAN / PANEL 194HL WITH A CREASED DELAMINATED DENT ON THE OUTER SKIN MID SPAN WAS REPAIRED IAW SRM 51-70-05-2R-2; SRM 51-70-14-2R-4 59259U 1/30/19SDR SWAA2022030123591Panel · delaminatedPANEL 193B FWD EDGE R/H CORNER IS DELAMINATED / REPAIRED DELAMINATED FWD EDGE R/H CORNER ON PANEL 193B IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 59278U 2/5/19SDR SWAA2022030123592Panel · delaminatedPANEL 193B AFT EDGE R/H CORNER IS DELAMINATED / REPAIRED DELAMINATED AFT EDGE R/H CORNER ON PANEL 193B IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 59278U 2/5/19SDR IPXA2019032140327Bracket · corrodedINSPECTION TYPE:D2 CORROSION WAS FOUND ON BRACKET (P/N: 69B01834-3) OF FWD WING TO BODY FAIRING FRAME AT STA 840, LBL 32. REPAIR IAW SRM 51-40-02-0G REV.85.00SDR IPXA2019032140326Bracket · corrodedINSPECTION TYPE:D2 CORROSION WAS FOUND ON BRACKET (P/N: 69B01834-4) OF FWD WING TO BODY FAIRING FRAME AT STA 840, LBL 32. REPAIR IAW SRM 51-40-02-0G REV.85.00.SDR IPXA2019032140325Bracket · corrodedINSPECTION TYPE:D2 CORROSION WAS FOUND ON BRACKET (P/N: 69B01834-4) OF FWD WING TO BODY FAIRING FRAME AT STA 840, RBL 32.REPAIR IAW SRM 51-40-02-0G REV.85.00.SDR IPXA2019032140323Bracket · corrodedINSPECTION TYPE:D2 CORROSION WAS FOUND ON BRACKET (P/N: 69B01834-3) OF FWD WING TO BODY FAIRING FRAME AT STA 840, RBL 32. REPAIR IAW SRM 51-40-02-0G REV.85.00.SDR ASAA2019012327939Panel · separatedLARGE PANEL ON UNDERSIDE OF FUSELAGE WAS FOUND MISSING BY GROUND CREWS. PANEL WAS FOUND ON THE RUNWAY. PANEL APPEARS TO HAVE BEEN RAN OVER BY THE GEAR AND STRUCK THE AFT FUSELAGE. GROUNDED - YES. PERFORMED CONDITIONAL INSPECT PER B737-900 AMM 05-51-59 FOUND IMSDR SWAA2022030164072Panel · delaminatedPANEL 195CL HAS A DELAMINATED DENT ON THE OUTER SKIN APPROXIMATELY 12' FORWARD OF THE AFT EDGE / PANEL 195CL DELAMINATED DENT ON OUTERSKIN APPROXIMATELY 12' FORWARD OF THE AFT EDGE REPAIRED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1 20545R 01/24/19SDR WX0A2020012900091Bushing · missingDOOR 312AR THE QUALITY INSPECTOR FOUND MISSING BUSHING ON TAIL CONE ATTACHMENT LOWER POSITION BTW FR 77 TO FR 78 IN THIS COMPARTMENT, ACCESS DOOR 312AR.SDR RJEY2019030700000Bushing · missingDURING OK TO CLOSE ACCESS DOOR 312AR THE QUALITY INSPECTOR FOUND MISSING BUSHING ON TAIL CONE ATTACHMENT LOWER POSITION BTW FR77 TO FR78 IN THS COMPARTMENT (ACCESS DOOR 312AR).SDR FDEA201901190176Bracket · crackedFAIRING PANEL 198AR SUPPORT STRUCTURE LOWER FWD. CORNER BRACKET FOUND CRACKED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71-1A ALLOWABLE DAMAGE FIG 101 SHEET 8. DETAIL XII REV 126. REPLACED BRACKET IAW SRM 51-40-02 REV 126.SDR DALA2019011900374Cable · tornTORN KEVLAR CABLE ON TAILCONE IN REF 5350-4287 STEP 4. NEW CABLE WAS INSTALLED PER AMM: 53-53-00-401 CONFIG 2. (LP0909599)SDR SWAA2022030121794Panel · delaminatedPANEL 194GR HAS A DELAMINATED DENT IN MIDDLE OF PANEL; MARKED WITH DENT DOT. / PANEL 194GR WILL BE REPLACED WITH NEW PANEL NEW PANEL WILL BE INSTALL ON TASK CARD # PANEL-194-CLOSE SEE THE CARD FOR INSTALLSDR SWAA2022030121798Panel · crackedPANEL 193B HAS ELONGATED AND CRACKED OUT FASTENER HOLES(MARKED). / REPAIRED FASTENER HOLES PER SRM 51-70-04-2R-9.SDR SWAA2022030134988Fairing · debondedFAIRING 193CR OUTER SKIN HAS A DISBONDED DENT. (MARKED) / FAIRING 193CR OUTER SKIN DISBONDED DENT REPAIRED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1 20549R 01/23/19SDR DALA2019011700308Cable · severedTAILCONE JETTISON BOTLLE TRIGGER CABLE SEVERED IN HALF ONE HANGING. REMOVED AND REPLACED TAILCONE DISPLACEMENT SYST BALL VALVE CABLE. OK FOR SERVICE. (LP#5310303)SDR SWAA2022030264045Fairing · elongatedFAIRING PANEL #192E HAS 2 ELONGATED HOLES / REPAIRED FAIRING PANEL 192E ELONGATED HOLES IAW SRM 51-70-05-2R-9 AND SRM 51-70-14-2R-1SDR SWAA2022030264046Fairing · elongatedFAIRING PANEL #192F HAS 2 ELONGATED HOLES / REPAIRED FAIRING PANEL 192F ELONGATED HOLES IAW SRM 51-70-05-2R-9 AND SRM 51-70-14-2R-1SDR SWAA2022030234986Fairing · delaminatedPANEL 193AR HAS A DISBOND ON INNER SURFACE / PANEL 193AR WITH A DISHAND ON INNER SURFACE WAS REPAIRED PER SRM 51-70-05-2R-2 57545U 1-18-19SDR SWAA2022030264037Fairing · elongatedFAIRING PANEL #191D HAS A ELONGATED HOLE MARKED / REPAIRED ELONGATED HOLE ON FAIRING PANEL 191D IAW SRM 51-70-05-2R-9 7062U 1-23-19SDR SWAA2022030264038Fairing · brokenFAIRING PANEL #191FL HAS BROKEN PIECE MID UPPER / FAIRING PANEL # 191 FL WITH A BROKEN PIECE MID UPPER WAS REPAIRED IAW SRM 51-70-05-2R-6 59259U 1/22/19SDR SWAA2022030264025Fairing · crackedFAIRING PANEL #195CL IS CRACKED AT LOWER AFT CORNER / FAIRING PANEL #195CL CRACK AT LOWER AFT CORNER REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 20549R 01/24/19SDR SWAA2022030264002Attach Fitting · brokenBODY FAIRING PANEL 192E AFT SUPPORT ATTACH FITTING IS BROKEN AT STA576 LBL6. (MARKED) / REMOVED AT BODY FAIRING PANEL 192E; AFT SUPPORT ATTACH FITTING STA.576; LBL6; BROKEN; LOCATED; DRILLED AND INSTALLED PER SRM 51-40-02-0G-0 88641U 23JAN19SDR SWAA2022030222721Fairing · delaminated!93 AR HAS DELAM SPOT AT VERY INBD END LOWER SIDE. / REPAIRED DAMAGED AREA ON PANEL 193AR PER SRM 51-70-05-2R-1.SDR SWAA2022030234686Support · crackedFAIRING SUPPORT AT BS 663 LOWER VAPOR BARRIER FOUND CRACKED AT INBOARD SIDE RBL30 / REPAIRED FAIRING SUPPORT AT BS 663 RBL 30 IAW ER 19-01217 REV IR AND SWA EA 1-753-34079 REV IRSDR SWAA2022030262308Nut Plate · corrodedPANEL 192HL NUT PLATE RETAINER STRIP ON INTERIOR SIDE OF PANEL HAS CORROSION / 192 HL NUT PLATE RETAINER STRIP FOUND TO BE OUT OF LIMITS DUE TO NO STATEMENT IN SRM IAW SRM 51-10-02-0G-0 PAR 9. REMOVED DAMGED RETAINER FABRICATED NEW REATAINER MAT ID 2024-T3 .03SDR SWAA2022030262309Fairing · crackedPANEL 194CR CRACKED ON EXTERIOR SIDE OF PANEL (MARKED) / REPAIRED CRACKED EXTERIOR SKIN OF PANEL 194CR IAW 737-700 SRM 53-60-70-2R-1 AND 51-70-05-2R-1; CRACK WAS BEYOND 1-PLY SO DAMAGE WAS OUT OF LIMITS IAW 737-700 SRM 53-60-70-1A-1 PARA 4A1SDR SWAA2022030262312Fairing · delaminatedPANEL 194AR HAS MULTIPLE AREAS OF DELAMINATION AT UPPER EDGE OF PANEL / REPAIRED MULTIPLE AREAS OF DELAMINATION AT UPPER EDGE OF PANEL 194AR PER SRM 53-60-70-2R-1 TABLE 202 AND SRM 51-70-05-2R-6. DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-60-70-1A-1 PARA 4BSDR SWAA2022030230302Support Frame · crackedRH ECS BAY FAIRING SUPPORT FRAME IS CRACKED AT BS 650 RBL 26 / REMOVED R/H ECS BAY SUPPORT FRAME AT STA 663 RBL 26 PER SRM 51-40-02; FABRICATED SUPPORT FRAME OUT OF BAC 150 6-4475 7075T73511 LOT # 1311004-1 PER SRM 51-40-05 AND DWG. 149A7214. RECEIVED SUPPORT SDR IPXA2019011938052Doubler · chafedINSPECTION TYPE:4C TAIL CONE RT UPPER PRODUCTION DOUBLER HAS DEEP WEAR IN NUMEROUS PLACES. REPAIRED TAIL CONE RT UPPER PRODUCTION DOUBLER CHAFE WEAR IAW EA 011-5320-01-7576 REV. IR AND EO MD11-5350-71259-A. (MINOR)SDR V0XD2019011600000Support Angle · crackedAFT LWR WING TO BODY FAIRING SUPPORT STRUCTURE AT FS 909 AND LBL17.63 ANGLE IS CRACKED. CORRECTIVE ACTION REPAIRED SUPPORT STRUCTURE ANGLE IAW REO 670-53-82-478 REV.-A DATED 2014-11-12.SDR SWAA2022030124380Fairing · delaminatedPANEL 191D HAS DELAMINATION TO COMPOSITE MATERIAL ON INNER SURFACE (MARKED WITH RED X) / WORK WILL BE ACCOMPLISHED ON NRC N181335SDR SWAA2022030120971Fairing · delaminatedPANEL 193 B IS DELAMINATED AT FWD L/H CORNER. DAMAGE MEASURES 4' X 5' MOD / REMOVED & INSTALLED NEW 193B PANEL REF AMM 53-51-21SDR SWAA2019010928331Bracket · crackedLT WING FORWARD WING TO BODY FAIRING FORWARD UPPER ATTACH BRACKET CRACKED. R&R BRACKET PER SRM.SDR SWAA2022030179212Panel · delaminatedFUSELAGE WING TO BODY PNL 193B DELAMINATED AND ERODED AT FWD RT CORNER BETWEEN FASTENER LOCATION 20 AND 21 MOD / REPLACED FUSEALGE WING TO BODY PANEL 193B IAW SRM 51-40-02SDR SWAA2022030174241Fairing · corrodedWING TO BODY FAIRING PANEL 192F HAS CORROSION ON EXTERNAL SKIN UNDER MARKER BEACON ANTENNA; #1; AND #2 DME ANTENNA / WING TO BODY FAIRING 192F REPAIRED WITH BACK SHOP REQUEST WORK ORDER 38832/1700/0001 SERIAL NO: 6851700 SHOP
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