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 SWAA2015051239590Fairing · crackedRIGHT MLG WW FILLET FAIRING CRACKED SPAR TO STATION 729.5. R & R FAIRING IAW DWG & SRM.SDR V0XD20150507129Strap · brokenAFT BODY FAIRING CTR SUPPORT STRAP BROKEN. FABRICATED NEW STRAP IAW DWG CC670-9171 REV NC DATED APRIL 1998.SDR SWAA2015051939840Fairing · delaminatedRIGHT WING TO BODY FAIRING FWD OF WW DELAMINATED. R & R FAIRING IAW SRM.SDR V0XD20150503117Support · corrodedAFT FUSELAGE FAIRING SUPPORT AT FS 950.0 IS CORRODED. R & R AFT FUSELAGE FAIRING SUPPORT, PN SH670-39189-1, AT FS 950.0 IAW SRM 51-42-06 & 51-45-00.SDR SWAA2015050839467Skin · crackedTAIL CONE ACCESS DOOR 318BR EXTERNAL SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR SWAA2015042739045Tail Cone · delaminatedTAIL CONE DELAMINATED APPROX 8" FROM FWD EDGE AT THE 4 O'CLOCK POSITION. REPAIRED TAIL CONE IAW SRM.SDR DALA2015042202847Radome · damagedLIGHTNING STRIKE ON RADOME. R & R RADOME IAW AMM 53-12-01. LP1913734.SDR SWAA2015061640749Fitting · crackedRIGHT WING FUSELAGE EXTERIOR WING TO BODY FITTING CRACKED AT STRINGER 22. REPAIRED FITTING IAW SRM & DWG.SDR DALA2015041902830Radome · damagedLIGHTNING STRIKE INSPECTION FOUND RADOME DAMAGED. REPLACED RADOME IAW AMM 53-12, LP1908688.SDR R61A201504140275Bonding · corrodedDURING HEAVY CHECK RACK 1B FAIRING 191FL BOND PLATES UNDER PANEL 191EL ARE CORRODED. MX REMOVED RECEPTACLE TO PERFORM REPAIR. PREPPED SURFACE LAY UP IAW SRM 51-73-00, 51-45-00 REPAIRED CORRODED BONDING PLATES UNDER PANEL 191EL IAW SRM 51-73-00. AIRCRAFT REMASDR R61A201504140274Bonding · corrodedWHILE IN HEAVY CHECK WAS REPORTED THAT RACK 1B FAIRING 191FL BONDING PLATES UNDER PANEL 191AR ARE CORRODED. MAINTENANCE REMOVED RECEPTACLES TO PERFORM REPAIR, PREPPED SURFACE TO LAY UP REPAIR IAW SRM 51-45-00, REPAIRED CORRODED BONDING PLATES UNDER PANEL 191ASDR R61A201504140273Bonding · corrodedDURING HEAVY CHECK, RACK 1B FAIRING 195NL BOND PLATES UNDER PANEL 195CR ARE CORRODED. MAINTENANCE REMOVED RECEPTICLES, PERFORMED REPAIR, PREPPED SURFACE TO LAY SUPPLIES IAW SRM 51-45-00, 51-73-00. LAYED UP CURED REPAIR PLIES IAW SRM 51-73-00. AIRCRAFT REMAINSDR SWAA2015052740088Attach Angle · crackedLEFT AFT WING TO BODY SUPPORT STRUCTURE INBD UPPER ATTACH ANGLE CRACKED BETWEEN BS 727 - 727B, STRINGER 20L. R & R ANGLE IAW SRM & DWG.SDR SWAA2015042338818Structure · crackedRIGHT WING TO BODY FAIRINGS CHORD TWO FASTENERS CRACKED AT ABS 540, STRINGER 22R. REPAIRED CHORD IAW ACO.SDR DALA2015041302775Release Cable · wornDURING CHECK, MAINTENANCE FOUND THAT THE EXTERNAL TAIL RELEASE CABLE WAS WORN. MAINTENANCE R & R THE WORN CABLE AND A FUNCTIONAL TEST WAS SATISFACTORY. LP 1901103.SDR V0XD20150406093Attach Angle · corrodedAFT WING TO BODY FAIRING WEB, ATTACH ANGLE IS CORRODED. R & R ANGLE, PNSH670-39189-1, IAW SRM 51-40-11, 51-42-06 & 51-42-15.SDR SIMA20150408010Support · crackedLEFT LOWER AFT FAIRING SUPPORT IS CRACKED. REPAIRED AFT BELLY PANEL, LT LOWER ATTACHMENT SUPPORT IAW ERS-EM-5300-122.SDR SWAA2015050139199Tail Cone · delaminatedLOWER HALF OF THE TAIL CONE DELAMINATED. R & R TAIL CONE IAW AMM.SDR SWAA2015050639332Angle · crackedFORWARD AREA OF WING TO BODY FAIRING ANGLE CRACKED AT BS 540, STRINGER 24L. R & R ANGLE IAW SRM & DWG.SDR SIMA20150322008Attach Angle · crackedLEFT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3 IS CRACKED 3/8" ON THE FWD & AFT ENDS, JUST FWD OF FRAME 48. R & R LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 3, JUST FWD OF FRAME 48, IAW SRM 51-40-02 & ETN-EM-53-142.SDR USAA2015032400016Support · corrodedCORROSION ON AFT BELLY FAIRING SUPPORT AT FRAME 53.4 CTR LOWER WEB BETWEEN STRINGER 51L & 51R. R & R AFT BELLY FAIRING SUPPORT AT FRAME 53.4 CTR LOWER WEB BETWEEN STRINGER 51L & 51R IAW SRM 51-42-11.SDR R61A201503130215Attach Fitting · corrodedDURING HEAVY CHECK, AFT BELLY PANEL 195NL FWD ATTACH CENTER ATTACH STRIP IS CORRODED. MX R & R AFT BELLY PANEL, 195NL FWD ATTACH CENTER ATTACH STRIP IAW AMM 53-04-50.SDR CA110314010Access Panel · departed(CAN) LEFT UPPER INBD TAIL CONE, FAIRING DENT CAUSED BY ACCESS PANEL OPENED & DEPARTED FROM THE ACFT. DIFFICULTY DATE 3/10/2011SDR SWIA201540926Fairing · damagedFOUND DAMAGE TO FWD UNDERWING FAIRING 193AB IN 2 PLACES. COMPLIED WITH TEMPORARY REPAIR IAW REO, C-CHECK, RO 3/27/15, REPAIRED PANEL 193AB IAW STS EA PERMANENT REPAIR: COMPLIED WITH ST 51-900-1000.SDR DALA2015030902031Pin · seizedDURING TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THE INTERIOR TAILCONE RELEASE CABLE RELEASE PIN SEIZED. MAINTENANCE R & R THE RELEASE CABLE RELEASE PIN. OPS CHECKED OK. LP1853095.SDR DALA2015030902030Cable · wornMAINTENANCE FOUND KEVLAR CABLE ASSY WORN FOR TAILCONE ASSY. MAINTENANCE REPLACED THE KEVLAR CABLE ASSY, CHECKS OK. LP1853081.SDR WX0A2015030972461Tail Cone · damagedTAIL CONE RT SIDE HAS 41 INCHES OF DELAMINATION & A 41 INCH CRACK THROUGH TO INNER SIDE. R & R TAIL CONE IAW 53-53-00.SDR DALA2015030901990Cable · damagedSRQ MAINTENANCE FOUND THE KEVLAR CABLE ON THE TAILCONE ASSY DAMAGED AND REPLACED IT. LP1853504.SDR SWAA2015042038653Former · crackedRIGHT WING TO BODY FAIRING FORMER CRACKED AT BS 540, UPPER OTBD END. R & R FORMER IAW SRM & DWG.SDR SWAA2015040738166Angle · corrodedWING TO BODY FAIRING LOWER SUPPORT FITTING ANGLE CORRODED AT BS 832, LONGERON 30. R & R ANGLE IAW SRM & DWG.SDR UHLA2015031700179Flange · corrodedLEVEL 2 CORROSION - FWD BELLY FAIRING AFT LOWER FLANGES HAVE AREAS OF CORROSION. R & R SUPPORTS, PN 170-12603-002, 170-12603-001, 170-02456-001.SDR DALA2015030201785Cable · misroutedDURING TAIL CONE SLIDE CHANGE NOTED TAILCONE NITROGEN PULL CABLE ROUTED INCORRECTLY. ROUTED CABLE CORRECTLY IAW AMM. OK FOR SERVICE.SDR SWAA2015042438880Angle · crackedRIGHT FWD WING TO BODY FAIRING CUT OUT STRUCTURE CRACKED, AFT OTBD CORNER FWD OF AIR CONDITION DOOR. R & R ANGLE ASSEMBLY IAW SRM & DWG.SDR DALA2015022701709Release Cable · frayedMAINTENANCE FOUND BROKEN WIRES ON TAILCONE EXTERNAL RELEASE HANDLE CABLE NR 583 AT AFT ACCESSORY COMPARTMENT MAINTENANCE REPLACED TAILCONE EXTERNAL RELEASE HANDLE CABLE NR 583 AT AFT ACCESSORY COMPARTMENT.SDR V0XD20150225065Angle · corrodedAFT FAIRING SUPPORT STRUCTURE AT FS 969.00 L BRACKET & VERTICAL GUSSET SHOWS SIGNS OF CORROSION. BLENDED CORROSION, REMOVED 0.02 INCHES WITHIN LIMITS IAW SRM 53-82-55. R & R ANGLE, PN SH670-39189-1 & IAW SRM 51-47-06.SDR SWIA201540851Radome · damagedLIGHTINING STRIKE DAMAGE ON ONE FASTENER ON THE RADOME. C-CHECK, REPLACED 1 EA FASTENER IN RADOME IAW STS EA.SDR SWAA2015031337422Tail Cone · delaminatedTAIL CONE DELAMINATED AT LT SIDE BELOW HORIZONTAL STAB. REPAIRED TAIL CONE IAW SRM.SDR SWIA201540859Fairing · damagedRIGHT AFT WING TO FUSE FAIRING HAS A SMALL HOLE AT PANEL 196AL. C-CHECK, REPAIRED HOLE IN PANEL 196AL IAW REO AND SRM.SDR SWAA2015031937613Fairing · crackedLEFT MAIN WW SURROUND FAIRING AFT OF WW CRACKED AT BS 727, LBL 48. R & R FAIRING IAW SRM & DWG.SDR DALA2015021901497Bracket · brokenCREW REPORTED THAT TAIL CONE APPEARED LOOSE. MAINTENANCE FOUND THE UPPER RT BRACKET SUPPORT CABLE BROKEN. MAINTENANCE R & R THE TAILCONE ASSEMBLY.SDR ANCF2015021401Seal · vibrationDURING CLIMB PASSING FL300, CLIMB SPEED NOTING CONDITION & NO TURBULENCE. THE ACFT HAD A VERY STRONG VIBRATION FOR ABOUT 30 SECONDS. AFTER REDUCING SPEED & DISCONNECTING AP THE VIBRATIONS STOPPED. THE AP WAS CONNECTED AGAIN WITH A/T & WITH SPEED TURBULENCE.SDR V0XD20150214045Support Angle · corrodedAFT WING TO BODY FAIRING SUPPORT STRUCTURE CTR SPLICE IS CORRODED. R & R SUPPORT ANGLE IAW SRM 51-42-06.SDR ASOA2015032612463Skin · damagedLIGHTING DAMAGE TO TAIL CONE. INTERM REPAIR CW IAW EA 12-2014-251. PERMANENT REPAIR REQUIRED. REPAIRED TAIL CONE IAW SUPPLEMENT AMM 53-84-00.SDR V0XD20150214044Channel · crackedAFT WING TO FUSELAGE FAIRING CTR SUPPORT STRAP IS CRACKED. FABRICATED NEW STRAP IAW DWG CC670-39171 & REPLACED CHANNEL.SDR DALA2015021001161Mechanism · wornMAINTENANCE FOUND A WORN TAILCONE RELEASE MECHANISM CAM ON STA Y=1510 CANTED BULKHEAD AT THE 11 O'CLCOCK POSITION. MAINTENANCE REPLACED THE RELEASE MECHANISM CAM.SDR DALA2015020400951Latch · corrodedMAINTENANCE FOUND RUSTED LATCH PINS OF TAIL CONE SLIDE. MAINTENANCE REPLACED HARNESS ASSY IAW AMM 25-62-01-201.SDR DALA2015020300950Clamp · out of adjustMAINTENANCE FOUND TAILCONE EXTERNAL RELEASE CABLE CLAMPS LT AND RT, ITEMS 20 AND 21 OF AMDS WC 5350-01077-0101, FIG 5, OUT OF ADUSTMENT. MAINTENANCE ADJUSTED RELEASE CLAMPS IAW AMDS 5350-01077-0101.SDR DALA2015020200949Tee Fitting · damagedMAINTENANCE FOUND A TEE PIN, ITEM 11, BUSHING LT AN RT HAVE FLAT STOPS THIS TEE PIN IS LOCATED AT THE TAILCONE INTERNAL RELEASE HANDLE. MAINTENANCE R & R BUSHINGS. IAW AMDS CARD 5350-01077-0101.SDR DALA2015020100892Cable · twistedMAINTENANCE FOUND TAILCONE AFT LT UPPER LATCH LOCKING CABLE TWISTED. MAINTENANCE REPLACED AND ADJUSTED CABLE.SDR DALA2015020100891Conduit · wornMAINTENANCE FOUND WEAR ON CONDUIT OF TAIL CONE CONTROL CABLE BETWEEN STA Y=1485 CANT TO 1497 CANT AT 7 O'CLOCK POSITION. MAINTENANCE REPLACED THE CONDUIT IAW AMM 20-10-11-201.
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