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 SIMA20160112008Attach Angle · crackedRIGHT WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE NR 2 CRACKED AT AFT END. REPLACED ATTACH ANGLE IAW SRM 51-40-02.SDR SIMA20160112007Support · crackedLEFT WING TO FUSELAGE PANEL LOWER FWD SUPPORT CRACKED. REPAIRED IAW ETN-EM-53-142 R2.SDR SIMA20160112006Attach Angle · crackedLEFT WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE NR 2 IS CRACKED. REPLACED ATTACH ANGLE IAW SRM 51-40-02.SDR IPXA2016012998614Skin · damagedINSPECTION TYPE: 2C, FWD TAILCONE SKIN ALONG RT SIDE CHAFE DAMAGE. REPAIRED FWD TAILCONE RT SKIN IAW EA 011-5330-01-A6049, REV IR AND EO MD11-5330-59647-A.SDR DALA2016011100268Receptacle · wornTAILCONE RECEPTICLES WORN. REPLACED IAW SRM 51-30-02.SDR SWAA2016021148971Skin · delaminatedRIGHT TAIL CONE EXTERNAL SKIN DELAMINATED. REPAIRED SKIN IAW SRM.SDR DALA2016010700225Cable · frayedTAILCONE NITROGEN BOTTLE CABLE FRAYED, R & R.SDR DALA2016010700224Receptacle · wornTAILCONE GUIDE PIN RECEPTICALS, 4 EACH, WORN. REMOVED AND INSTALLED 4 LOWER GUIDE PINS IAW SRM 51-30-02.SDR DALA2015123107773Frame · crackedTAILCONE FRAME CRACKED AT RT UPPER LATCH FITTING. REPLACED TAIL CONE ASSY., INSTALLATION & OPS CHECKS GOOD, AMDS CARD 2561-4001.SDR DALA2015123107772Support Fitting · shearedMAINTENANCE FOUND TAILCONE UPPER LATCH SUPPORT FITTING SHEARED OFF. THE TAILCONE WAS REPLACED.SDR DALA2015122607721Radome · damagedAT 10,000 ACFT TOOK LIGHTNING STRIKE, SUSPECT RT SIDE RADOME. REPAIRED MULTIPLE LIGHTNING STRIKES RT SIDE FUSELAGE BS 36 THRU BS 408 IAW SRM 53-04.SDR A6WA201543406Fairing · chafedRIGHT WING TO BODY SKIRT CHAFED BY CONTACT WITH STUB FAIRING SEAL.SDR REXA2015122001221Channel · crackedAFT FUSELAGE FAIRING CHANNEL IS CRACKED. R & R AFT FUSELAGE FAIRING CHANNEL PT CC690-39251-1 IAW SRM 51-40-11-001-001-A01 & 51-42-13-001-001-A01.SDR REXA2015122001210Strap · crackedAFT FUSELAGE FAIRING JOINT STRAP CRACKED AT FS 882. REPAIRED AFT FUSELAGE FAIRING JOINT STRAP AT FS 882 IAW RE9O 690-53-82-052 REV DATED 2014 04 09.SDR CA151221015Fairing · missing(CAN) FIELD SERVICE REPORTED THAT THE ACFT LANDED WITH THE AFT BELLY FAIRING ACCESS PANELS MISSING. A SERVICE REQUEST FOR PRODUCT SUPPORT ACTION, SRPSA, SUBMITTED TO CUSTOMER SUPPORT REPORTS THAT THE MISSING PANELS ARE PN GS297-0137-7 AND GS297-0137-8 ALSO KNSDR E4EB20151214004Skin · corrodedREFERENCE NRC A016101, TAIL CONE SKIN CORRODED AT LOWER TAIL LIGHT ASSEMBLY. ITEM REPAIRED IAW EA 008-5330-38A5869.SDR DALA2015121607675Cable · disconnectedTAILCONE UNSAFE LIGHT AT 60 KIAS. FOUND LOCKING CABLE DISCONNECTED AT INTERNAL RELEASE HANDLE. RECONNECTED LOCKING CABLE IAW MM. OPS CHECKS OK.SDR DALA2015120807526Pin · missingNO TAIL CONE ALIGNMENT PINS INSTALLED IN CANTED FRAME, CBS 1567. INSTALLED NEW PINS IAW SRM 51-00-01.SDR DALA2015120807513Frame · corrodedLOWER WTB FAIRING FRAME T-CAP BS 1040, RBL 9-24, CORROSION AROUND NUTPLATES. REMOVED CORROSION ON LOWER WTB FAIRING FRAME T-CAP BS 1040, RBL 9-24 IAW SRM 53-00-71. ALLOW-DAMAGE 1, FIG 101 DETAIL IX FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71. ALLOW-DAMAGE, 1SDR DALA2015121107559Clamp · brokenFORWARD CABLE RELEASE FOR TAILCONE SUPPORT CLAMP BROKE AND WORN. ACCOMPLISHED APPROVED TIME LIMITED REPAIR IAW ERA 541501-14 AND PS 900-5-1, NR 4.SDR DALA2015120307362Cable · corrodedRUSTED TAIL CONE CONTROL CABLE NR 547, AT BS 1510. RUSTED TAIL CONE MECHANIC CONTROL CABLE NR 547, AT BS 1510 WAS REMOVED IAW AMM 20-10-17 AND NEW CONTROL CABLE PN 3913359-547 WAS INSTALLED IAW AMM 20-30-01 AND WILL BE ADJUSTED UNDER CARD 5350-01077-0101.SDR 6BUY2015120100005Radome · misrepairedTHE RADOME HAS BEEN PREVIOUSLY REPAIRED. THE PREVIOUS REPAIRS ARE NOT COMPLIANT WITH THE CURRENT CMM 53-11-15, REV 22 MAY 2011.1.24. REPAIRS OF 130 MM DIAMETER AND 12 REPAIRS OF 50 MM DIAMETER HAVE BEEN PERFORMED ON THE SHELL SANDWICH AREA WITH HONEYCOMB REPLSDR CA151127004Fairing · missing(CAN) BELLY FAIRING PANELS 185BL AND 186BR DEPARTED IN FLIGHT DURING CLIMB AFTER TAKEOFF. ATTACHED SRPSA FORM, PHOTOS AND FAULT RECORDING TABLES FROM INSPECTION AFTER ACFT SER 9570 LANDED AT WITHOUT PANELS 185CL + 186CR. WE HAVE INSPECTED THE SURROUNDING STRUSDR SIMA20151125016Attach Angle · crackedRIGHT LOWER ATTACHMENT ANGLE NR 3, FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1 1/2" LONG ON THE FWD END, BETWEEN FRAMES 47 - 48. REPAIRED RT LOWER ATTACHMENT ANGLE NR 3 FOR THE WING TO FUSELAGE FAIRING, BETWEEN FRAMES 47 - 48 IAW ETN-EM-53-142.SDR SIMA20151125013Attach Angle · crackedLEFT LOWER ATTACHMENT ANGLE NR 4, FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1/2" LONG, BETWEEN FRAMES 48 - 49 ON THE FWD EDGE. REPAIRED LT LOWER ATTACHMENT ANGLE NR 4 FOR THE WING TO FUSELAGE FAIRING, BETWEEN FRAMES 48 - 49 IAW SRM 51-40-02 & ETN-EM-53-142.SDR SIMA20151125014Attach Angle · crackedLEFT LOWER ATTACHMENT ANGLE NR 1, FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1 1/4" LONG, BETWEEN FRAMES 43 - 44 ON THE PREVIOUS CUT OUT SPLICE REPAIR. REPAIRED IAW ETN-EM-53-142.SDR SIMA20151125015Attach Angle · crackedLEFT LOWER ATTACHMENT ANGLE NR 2. FOR THE WING TO FUSELAGE FAIRING IS CRACKED 1/2" LONG, BETWEEN FRAMES 47 - 48 ON THE TE. R & R WING TO FUSELAGE FAIRING LOWER NR 2 ATTACHMENT ANGLE IAW SRM 51-40-02.SDR SIMA20151125017Attach Angle · crackedRIGHT LOWER ATTACHMENT ANGLE NR 1 FOR THE WING TO FUSELAGE FAIRING IS CRACKED, BETWEEN FRAMES 43 - 44, FWD OF THE PREVIOUS CUT OUT SPLICE REPAIR. REPAIRED RT OVERWING FAIRING LOWER ATTACHMENT ANGLE NR 1, BETWEEN FRAMES 43 - 44 IAW ETN-EM-53-142.SDR SIMA20151125019Attach Bracket · crackedLEFT UPPER ANGLE FOR THE WING TO FUSELAGE FAIRING HAS ATTACHMENT BRACKET THAT IS CRACKED. UNDERNEATH THE PULLED RIVETS, BETWEEN FRAMES 48 - 49. R & R LT UPPER ATTACHMENT BRACKET FOR UPPER WING TO FUSELAGE FAIRING ANGLE IAW SRM 51-40-02 & ETN-EM-51-110.SDR FDEA201511183679Support Bracket · crackedPOST FLIGHT MX WALK AROUND SHOWS TAIL CONE NOT SECURED. GAP BETWEEN TAIL CONE & FUSELAGE. INSPECTION SHOWS LT SUPPORT BRACKET FOR LT UPPER LATCH CRACKED & HAS SHEARED RIVETS. UNABLE TO ACCESS TAIL CONE COMPARTMENT FOR FURTHER INSPECTION DUE TO TAIL CONE ISDR EE4Y2015111700414Structure · corrodedTAIL CONE STATION X34737, LOWER SECTION CHORD WITH CORROSION. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D208 1-53. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103992, INSTRUCTIONS & APPROVED.SDR AALA20151111007Radome · out of adjustAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. AFTER TAKEOFF, MYLAR TAPE INSTALLED OVER RADOME TO FUSELAGE JOINT CAME LOOSE. INSPECTION FOUND RADOME TO BE OUT OF ROUND. R & R, ADJUSTED RADOME IAW MM 53-12-01. OK FOR SERVICE.SDR AALA20151109011Radome · fodAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, INCURRED MULTIPLE BIRD STRIKES INCLUDING ONE TO NR 1 ENG & ONE CAUSING DAMAGE TO RADOME. PERFORMED BORESCOPE ON NR 1 ENG WITH NO DAMAGE NOTED. R & R RADOME IAW AMM 53-52-00.SDR DALA2015111006863Pin · crackedFRAMED 1510 CRACKED AT LOWER RT ALIGNMENT PIN FOR TAILCONE. C/W EDDY CURRENT INSPECTION OF CUT-OUT IAW ERA 497316-14MA, REV ORIG, SECTION 1, STEP 4, NO ITEMS NOTED. COMPLETED THRU STEP 9, ERA 497316-14MA, REV ORIG. COMPLETED ERA 497316-14MA, REV ORIG.SDR SWAA2015120746765Skin · crackedTAIL CONE EXTERNAL SKIN DELAMINATED AT BS 1156, BL 0. REPAIRED SKIN IAW SRM.SDR SIMA20151106007Support · crackedLEFT SIDE OVERWING FAIRING, UPPER SUPPORT IS CRACKED AFT OF FRAME 41 LOCATION. REPAIRED IAW SRM 53-2312.SDR SIMA20151106006Support · crackedRIGHT SIDE OVERWING FAIRING, UPPER SUPPORT IS CRACKED AFT OF FRAME 41 LOCATION. COMPLIED WITH REPAIR AT AFT OF FRAME 41 RT SIDE IAW SRM 53-23-12.SDR U2RA201511050001Tee Fitting · corrodedRIGHT AT BS 1220, WING TO BODY FAIRING, T-CHORD HAS CORROSION AT BOTTOM END. REPLACED WING TO BODY FAIRING T-CHORD.SDR V0XD20151105327Channel · crackedAFT WING TO BODY FAIRING STRAP IS CRACKED. R & R AFT CHANNEL ON AFT WING TO BODY FAIRING & RESTORED FINISH IAW SRM 51-42-06, 51-40-11, 51-25-06, 51-25-16 & AMM 51-21-01.SDR V0XD20151029232Angle · crackedLEFT AFT FUSELAGE FAIRING FRAME 909.00, INBD VERTICAL ANGLE CRACKED. REPAIRED IAW REO 670-53-82-478.SDR FDEA201510153236Radome · damagedON DEPARTURE, SUSPECT LIGHTNING STRIKE, WX RADAR INOPERATIVE, NO OTHER ISSUES. FOUND PUNCTURE ON THE NOSE OF THE RADOME & RADOME DELAMINATED FROM THE INSIDE. FOUND ANTENNA HIT BY LIGHTNING STRIKE, CREW VERBALLY REPORTS THAT BOTH WEATHER RADAR SYSTEMS ARE INSDR CALA2015101694597Panel · missingDURING CLIMB IN A RT TURN, FELT ACFT SHUDDER LIKE HITTING POTHOLE. CABIN NOISE CONSISTENT WITH CARGO SHIFT, BETWEEN DOOR 3 & 4. ENSUING TURNS & PITCH CHANGES DID NOT HAVE SAME ISSUE. ONLY HAPPENED ONCE, NORMAL AT THIS TIME. ACFT ARRIVED WITH RT BODY FAIRINSDR REXA2015101000950Support Channel · looseRIGHT MLG FAIRING SUPPORT CHANNEL ASSEMBLY AT FS 797 IS LOOSE AT FAIRING BRACKET, JUST BELOW INBD PINTLE PIN, SIDE STAY ASSEMBLY CONNECTION POINT. R & R RT MLG FAIRING SUPPORT CHANNEL IAW SRM 51-42-21-001-001-A01 & AMM 20-21-00-910-801.SDR REXA2015101000949Support Channel · looseLEFT MLG FAIRING SUPPORT CHANNEL ASSEMBLY AT FS 797 IS LOOSE AT FAIRING BRACKET, JUST BELOW INBD PINTLE PIN SIDE STAY ASSEMBLY CONNECTION POINT. R & R LT MLG FAIRING SUPPORT CHANNEL IAW SRM 51-42-21-001-001-A01 & AMM 20-21-00-910-801.SDR SWAA2015101244804Tail Cone · delaminatedTAIL CONE DELAMINATED AT 8 O CLOCK BELOW STROBE. REPAIRED TAIL CONE IAW EA.SDR AALA20151010001Access Panel · missingBOTTOM FUSELAGE FAIRING ACCESS PANEL 192JL JUST FWD OF LT WW FOUND MISSING ON CREW WALK AROUND. SUSPECT PANEL HOLES BECAME ELONGATED & THEN DEPARTED ACFT IN FLIGHT AS ALL 6 SCREWS OF THIS PANEL WERE STILL IN PLACE. NO OTHER DAMAGE FOUND REF IPC 53-41-51-42 ISDR DALA2015100505935Fairing · damagedAFTER TAKEOFF THE PILOT MOVED THE GEAR HANDLE PAST THE OFF POSITION. THE GEAR DOOR WAS HEARD TO ACTUATE. MAINTENANCE PERFORMED SPEED CONDITION INSPECTION IAW AMM 05-51-47. FOUND WHEEL WELL AFT BODY FAIRING PANEL DAMAGED. REMOVED PANEL AND UNDERLYING DAMAGESDR DALA2015100205902Release Cable · brokenMAINTENANCE FOUND BROKEN STRANDS ON TAILCONE RELEASE CONTROL CABLE SEGMENT. TAIL CONE RELEASE CONTROL CABLE SEGMENT WAS R & R.SDR AALA20151001002Panel · damagedUPON ARRIVAL, THE RT RAM AIR ACTUATOR DOOR WAS FOUND TO BE OPEN & TO HAVE CREATED A HOLE IN THE WING TO BODY PANEL, AFT OF THE DOOR. REPAIRED THE PANEL IAW SRM 53-00-72-2R.SDR QMLA2015092815088Tail Cone · crackedFOUND 3 CRACKS AT STATION 6616 DURING INSPECTION OF TAIL CONE & 4 CRACKS ON EQUIPMENT DECK. THIS DAMAGE WAS FOUND AS A RESULT OF REMOVING THE TAIL BOOM FOR OTHER MX TO BE PERFORMED. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION, PENDING APP
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