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 DALA2016111708896Bracket · crackedDURING TAILCONE FUNCTIONAL FOUND RT UPPER SPADE RECEPTACLE LOWER SUPPORT ANGLE BRACKET ATTACH RIVETS LOOSE. BRACKET CRACKED. FABRICATED NEW BRACKET. INSTALLED NEW BRACKET PER IPC 53- 50-00-30 ITEM 240 AND DWG 9911957-38. RII COMPLETE.SDR DALA2016111708893Ramp · wornDURING TAILCONE FUNCTIONAL CHECK FOUND CAM BASE(RAMP) WORN. REPLACED CAM BASE IAW CARD 5350-01077-0101.SDR SCNA20161101283Fairing · chafedWING TO BODY PANEL 193AR I/B EDGE BAND IS CHAFED AND GOUGED. REPAIRED PANEL 193AR I/B EDGEBAND.SDR SCNA20161101282Fairing · puncturedRIGHT MAIN WHEEL WELL WING TO BODY PANEL 193AR HAS COMPOSITE DAMAGE IN INTERIOR SIDE. REPAIRED THE PUNCTURES TO INTERIOR SIDE OF PANEL 193AR.SDR SIMA20161029002Beam · damagedOVERHEAD BEAM WHERE AFT BAGGAGE BAY DOOR CARGO NET ATTACHES HAS BEEN CUT BY FORWARD RECOIL CABLE. PERFORMED REPAIR ON OVER HEAD BEAM ABOVE AFT BAGGAGE BAY DOOR IAW ERS-CR-53MR-2376.SDR DALA2016102607733Cable · chafedTAILCONE CABLE HAS AREA OF WEAR AND CHAFING. REPLACED THE CABLE.SDR EBVR20151026001Fairing · corrodedCORROSION FOUND ON AND UNDER FWD FUSELAGE CHIN FAIRING, ON CHIN FAIRING MINOR BLENDING . UNDER FUSELAGE FAIRING COMPLIED WITH AQRD ERO-867561 REPAIR.SDR DALA2016102407527Release Cable · frayedUPPER LEFT HAND TAILCONE RELEASE CABLE IS FRAYED. REPLACED AND RIGGED TAILCONE RELEASE CABLE PER AMM 53-53-00 AND AMDS 5350-01077-0101.SDR DALA2016102407526Cable · frayedTAIL CONE CABLE FRAYED AND DETERIORATED. REPLACED CABLE PER AMM 53-53-00.SDR DALA2016102407463Handle · damagedEXTERNAL TAIL CONE JETTISON HANDLE ANGLE MISSING ALONG WITH INSTALL HARDWARE. REPLACED THE MISSING ANGLE AND HARDWARE IAW AMM 53-50. OK FOR SERVICE.SDR IPXA2016111510681Skin · chafedINSPECTION TYPE: 3C, FWD EXTENDED TAILCONE INNER SKIN CHAFED AT PREVIOUS REPAIR AREA, BS 2165 RT SIDE. REPAIRED THE TAILCONE IAW EA 011-5350-01-A6532 REV. IR AND EO MD11-5350-62358-A.SDR A6WA201644447Angle · crackedLT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 449.85 IS CRACKED. REPLACED LT WING TO FUSELAGE FAIRING ATTACH STRUCTURE ANGLE IAW SRM 51-42-06.SDR A6WA201644448Angle · crackedLT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 476.00 IS CRACKED. REPLACED LT WING TO FUSELAGE ATTACH STRUCTURE ANGLE AT FS 476.00 IAW SRM 51-42-06.SDR A6WA201644446Angle · crackedRT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 470.00 IS CRACKED. REPLACED RT WING TO BODY FAIRING ATTACH ANGLE IAW SRM 51-42-06.SDR A6WA201644445Angle · crackedRT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 439.00 IS CRACKED. REPLACED RT WING TO FUSELAGE FAIRING ATTACH ANGLE IAW SRM 51-42-06.SDR A6WA201644444Angle · crackedRT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 461.00 IS CRACKED. REPLACED ANGLE AT FS 461.00 RT SIDE WING TO FUSELAGE FAIRING SUPPORT IAW SRM 51-42-06.SDR A6WA201644443Angle · crackedRT WING TO FUSELAGE FAIRING ATTACH STRUCTURE AT FS 449.85 IS CRACKED. REPLACED ANGLE STRUCTURE AT RT WING STATION FS 449.85 IAW SRM 51-42-06.SDR IPXA2016102009647Skin · delaminatedINSPECTION TYPE: SEG2, TAIL CONE SKIN DELAMINATED. REMOVED AND REPLACED THE TAIL CONE ASSY IAW DRAWING 148N3710.SDR SWIA201642817Angle · corrodedCORROSION FOUND FROM BLUE WATER AT BS 939. LOWER WING TO FUSELAGE FAIRING STRUCTURE LT ANGLE TO RT ANGLE CORRODED. INSTALLED A NEW LT LOWER WING BODY FAIRING SUPPORT ANGLE, AND NEW CENTER ANGLE IAW SRM.SDR DALA2016101707301Handle · looseTAILCONE INTERIOR RELEASE HANDLE. FOUND THE HANDLE FWD RETENTION CLIP DAMAGED. REMOVED AND REPLACED INTERIOR RELEASE HANDLE IAW AMM 25-62.SDR DALA2016101307234Frame · crackedTAILCONE ATTACH FRAME CRACKED AT 3 OCLOCK AND 2 O`CLOCK POSITIONS. REMOVED DAMAGED FRAME SECTION AND STARTED INSTALLING NEW SECTION. INSTALLED NEW FRAME IAW DWG 5966769.SDR DALA2016101207189Intercostal · out of positionTAIL CONE ACTIVATION CABLE SUPPORT INTERCOSTAL IS OUT OF POSITION AT AFT END BS 1510. REPLACED THE INTERCOSTAL IAW DWG 9917701. TREATED AND PRIMED IAW SRM 51-10-03.SDR DALA2016101007134Cable · damagedTAILCONE FUNCTION- BALL END OF CABLE TO LOCK IN CLIP. FIGURE 2. ITEM 13. REPLACED THE CABLE IAW AMDS 5350-010177-0101.SDR DALA2016101007133Conduit · out of positionTAIL CONE FUNCTION CHECK FAILED STEP 7D (5). LOCKING CABLE CLAMP DOES NOT CLEAR LOWER END OF CONDUITS AT LEAST 1/2". REPOSITIONED CONDUITS PER STEP 5 RECHECKED. IAW AMDS 5350-01077-0101.SDR IPXA2016102009626Strap · corrodedINSPECTION TYPE: 3C, AFT EXTENDED TAIL CONE LOWER INTERNAL STRAP IS CORRODED. REMOVED, FABRICATED AND REPLACED LOWER STRAP IAW DWG. AKC7627 AND SRM 51-31-01.SDR IPXA2016101909603Skin Panel · delaminatedINSPECTION TYPE:SEG2, REMOVE AND REPLACE TAIL CONE SKIN PANEL PN 148N3710Y88 DUE TO DELAMINATION. REMOVED AND REPLACED TAIL CONE ASSY, BOND ASSY IAW DRAWING 148N3710.SDR IPXA2016102910015Support · corrodedINSPECTION TYPE: 3C, RT WING TO FUSELAGE FILLET SUPPORT RIB CORRODED AT Y=5-53. REPAIRED THE SUPPORT RIB IAW EA 011-5350-01-A6526 REV. IR AND EO MD11-5350-62318-A.SDR DALA2016092906982Cable · wornTAILCONE INT CABLE WORN. REPLACED CABLE REF AMM 53-53-00.SDR DALA2016092906981Release System · wornTAILCONE RELEASE CAM BASE IS WORN. REMOVED AND INSTALLED TAIL CONE RELEASE CAM BASE REF AMM 53-53-02. TESTED AND ADJUSTED PER AMM 53-53-02.SDR K11A2016110416008Skin · crackedTAILCONE EXTERNAL SKIN RT SIDE CRACKED.SDR JGVR201609210008Attach Angle · corrodedCORROSION ON UPPER TAIL CONE COVER FAIRING ATTACH ANGLES. THE AREAS THAT CORRODE ONLY HAVE PRIMER PAINT. SHOULD BE PAINTED WITH AN ADDITIONAL CORROSION RESISTANT PAINT FOR A TOP COAT TO PREVENT CORROSION.SDR SWAA2016093008306Bracket · crackedDOOR SEAL ON WING TO BODY FAIRING STRUCTURE BRACKET CRACKED AT LOWER FUSELAGE. R&R BRACKET IAW SRM.SDR DALA2016092606846Bayonet · wornDURING A TAILCONE EMERGENCY RELEASE FUNCTIONAL CHECK, FOUND THE BAYONETS WORN. REMOVED AND REPLACED.SDR DALA2016091906729Bayonet · wornDURING TAIL CONE EMERGENCY RELEASE, FOUND LT SIDE UPPER AND LOWER TAIL CONE BAYONETS WORN. REPLACED IAW CMM.SDR P5CA2016091600256Radome · damagedBIRD STRIKE ON NOSE OF ACFT. RADOME REPLACED IAW 53-12-01.SDR IPXA2016101109238Intercostal · crackedINSPECTION TYPE: 3C, CRACKED INTERCOSTAL INSIDE FORWARD TAIL CONE. REMOVED FABRICATED AND INSTALLED A NEW INTERCOSTAL IAW DWG AKC7546 AND SRM 51-31-01.SDR IPXA2016100709058Frame · crackedINSPECTION TYPE: 3C, FWD TAILCONE RT AFT FRAME CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FRAME IAW DWG AKC7539 AND SRM 51-33-01.SDR SWIA201642639Strap · corrodedLT, FS 879, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39333-9. C-CHECK, REPLACED LWR STRAP ON LT WING TO BODY FAIRING SUPPORT STRUCTURE AT FS 879 IAW SRM.SDR SWIA201642638Strap · corrodedRT, FS 879, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39333-9. C-CHECK, REPLACED LWR STRAP ON RT WING TO BODY FAIRING SUPPORT STRUCTURE AT FS 879 IAW SRM.SDR SWIA201642637Strap · corrodedRT SIDE, FS909, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39341-3. C-CHECK, REPLACED LWR STRAP ON RT AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE AT FS909 IAW SRM.SDR SWIA201642636Strap · corrodedFS909, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON MID STRAP P/N SH670-39338-3. C-CHECK, REPLACED STRAP ON AFT WING TO BODY FUSELAGE SUPPORT STRUCTURE AT FS909 IAW SRM.SDR SWIA201642635Strap · corrodedLT SIDE, FS909, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER STRAP P/N SH670-39341-3. C-CHECK, INSTALLED LT LWR STRAP LOCATED AT FS909 LT AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE IAW SRM.SDR SWIA201642634Angle · corrodedLT SIDE, FS939, AFT WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE HAS CORROSION ON LOWER ANGLE P/N SH670-39265-5. C-CHECK, REPLACED LWR ANGLE IAW SRM.SDR V0XD20160912164Strap · corrodedAFT BELLY FAIRING CENTER STRAP IS MISSING RIVETS, AND SHOWING SIGNS OF CORROSION. FABRICATED AND INSTALLED CENTER STRAP, A670-39171, IAW SRM 51-42-15, 51-42-06, 51-25-06, 51-21-11, 51-42-13, 51-40-11, 51-24-36, 51-25-16, AND PLCC670-39171.SDR QMLA2016090716104Retainer · damagedDURING TROUBLESHOOTING FOR THE DOOR WARNING CAUTION LIGHT, IT WAS NOTED THAT THE DOOR LATCH ITSELF SHOWED SIGNS THAT IT WAS NOT STRAINGHT AGAINST THE PILLAR CHANNEL. AFTER REMOVING THE DOOR SEAL IT WAS DETERMINED THAT THE A/F SLIDING DOOR POST WAS BENT TO ONE SDR DALA2016090806468Clamp · damagedTAILCONE RELEASE CABLE, FWD END AT FWD SIDE OF APB RUBBER BOOT INCORRECTLY CLAMPED. REPLACED THE CLAMP.SDR DALA2016090806467Boot · misinstalledTAILCONE RELEASE CABLE, FWD END AT FWD SIDE OF APB RUBBER BOOT INCORRECTLY CLAMPED. REPLACED THE CLAMP BOOT.SDR DALA2016090706442Unknown · malfunctionedTAILCONE WOULD NOT RELEASE WITH INTERIOR HANDLE OPERATION IAW AMDS 5350-01077-0101, STEP 11A. CORRECTED ON NON-ROUTINE. CHECKS PASSED IAW AMDS 5350-01077-0101. PULL CHECK WITH-IN LIMITS AT 33LBS.SDR SWAA2016090655450Attach Bracket · crackedRT WING TO BODY FAIRING ATTACH BRACKET CRACKED FORWARD RT WHEEL WELL. R & R BRACKET IAW SRM.SDR IPXA2016092108524Skin · crackedINSPECTION TYPE: 3C, EXTERIOR SKIN CRACKED AT FWD TAILCONE RT UPPER AFT SIDE. REPAIRED IAW SRM 53-00-00 PG 213 FIG 204.
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