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 DALA2014071404109Receptacle · wornMAINTENANCE DISCOVERED THAT ONE OF THE TAILCONE RELEASE SYSTEM LATCH PIN RECEPTACLES WAS WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA2014071404085Pin · wornDURING SCHEDULED INSPECTION, IT WAS NOTED THE UPPER LEFT LOCK PIN FOR THE TAILCONE WAS WORN. THE LOCK PIN WAS REPLACED AND THE REQUIRED INSPECTION COMPLETED.SDR DXTA2014071405821Attach Angle · corrodedCORROSION WAS FOUND UNDER NUTPLATES ON LT SIDE OF APU INLET FAIRING ATTACHMENT. REPAIRED LT & RT LOWER RUDDER FAIRING ATTACHMENT ANGLES IAW ERO-593764 REV IR, DATED JULY 15, 2014. FAIRING ANGLE REPAIR THIS IS CONSIDERED A MINOR REPAIR. SDR COMPLETED.SDR DALA2014070904000Release Cable · frayedDURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CABLE TO BE FRAYED. MAINTENANCE REMOVED AND REPLACED THE TAILCONE RELEASE CABLE.SDR DALA2014070903966Sleeve · damagedMAINTENANCE DISCOVERED THAT THE KEVLAR SLEEVE OVER THE RELEASE CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA2014070903965Pin · wornMAINTENANCE DISCOVERED THAT THE ALIGNMENT PIN FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE PIN WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR SIMA20140701023Attach Angle · crackedAFT BELLY FAIRING LT FWD ATTACH L ANGLE IS CRACKED UNDER SPAR 3. REMOVED & INSTALLED SERVICEABLE L ANGLE IAW SRM 51-40-02.SDR SIMA20140701016Attach Angle · crackedAFT BELLY FAIRING RT FWD ATTACH L ANGLE IS CRACKED UNDER SPAR 3. REMOVED CRACKED AFT BELLY FAIRING RT FWD ATTACH L ANGLE & INSTALLED SERVICEABLE L ANGLE IAW SRM 51-40-02.SDR DALA2014070803960Toggle · misinstalledTAIL CONE SLIDE TOGGLES INSTALLED INCORRECTLY. INSTALLED TAIL CONE TOGGELS PER AMDS 5352-4491.SDR DALA2014063003834Lanyard · frayedTAIL CONE JETTISON BOTTLE LANYARD FRAYED. REPLACED PULL CABLES IAW AMDS 5350-4491.SDR VGCA20140624004Fairing · damagedFAIRING ADJACENT TO LEFT PACK COOLING DOOR DAMAGED.SDR DALA14036519520Pin · dislodgedPILOT REPORTED THE AMBER CAUTION MESSAGE ILLUMINATED INDICATING THE TAILCONE WAS NOT SECURE. MAINTENANCE FOUND THE INTERNAL TAILCONE RELEASE HANDLE PIN DISLODGED FROM THE RETAINER CLIPS. THE LOCK CABLE WAS REINSERTED AND THE BALL END NOW MAKES PROPER CONTACTSDR DALA2014061903675Release Cable · frayedDURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CABLE HAS A WORN SPOT WITH NUMEROUS BROKEN STRANDS. MAINTENANCE R & R THE TAILCONE RELEASE CABLE.SDR SWAA2014062529379Skin · delaminatedTAIL CONE LOWER AREA SKIN DELAMINATED AT BS 1180, BL 0. REPAIRED SKIN IAW SRM.SDR R61A201406120766Doubler · corrodedDURING HEAVY CHECK, PANEL 192CR ON INTERNAL DOUBLER OF PANEL HAS HEAVY CORROSION. MX R & R INTERNAL DOULBER IAW SRM 51-41-02.SDR V0XD201406140139Angle · corrodedAFT FUSELAGE FAIRING, INTERNAL SUPPORT WEB STRUCTURE SPLICE AT BL0, FS 939 IS CORRODED. R & R WITH NEW ANGLE IAW SRM 51-42-06.SDR SWAA2014061929200Plate · crackedLEFT WING TO BODY FAIRING ACCESS PANEL 3578L PLATE CRACKED. R & R PLATE IAW SRM.SDR U2RA201406090002Support Bracket · corrodedDURING ACCOMPLISHMENT OF TASK CARD 58-866-01-01 FOUND BODY FAIRING SUPPORT FRAME BRACKET CORRODED AT BS 920 RT. REPLACED BRACKET.SDR U2RA201406090001Support Bracket · corrodedDURING ACCOMPLISHMENT OF TASK CARD 53-864-01-01 FOUND BODY FAIRING SUPPORT FRAME BRACKET CORRODED AT BS 880 LT. REPLACED BRACKET.SDR HALA2014060700079Radome · crackedBIRD STRIKE DURING TAKEOFF. BIRD HIT UNDER THE COCKPIT ON CAPTAIN'S SIDE. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND DAMAGE TO RADOME ON CAPT'S SIDE. FOUND A 6" VERTICAL CRACK AND A 9" HORIZONTAL CRACK. ALSO, FOUND DELAMINATION. R & R RADOME SDR SWAA2014070829706Angle · crackedLEFT WING TO BODY FAIRING T ANGLE CRACKED AT BS 540. R & R ANGLE IAW SRM & DWG.SDR SWAA2014070829705Structure · crackedRIGHT FWD WING TO BODY FAIRING T CHORD CRACKED AT BS 540. R & R CHORD IAW SRM & DWG.SDR DALA2014062503758Fairing · corrodedCORROSION ON WING TO FUSELAGE FAIRINGS, RUB STRIP SETTLEMENT AREA RT FROM STA Y=727 TO Y=747 BETEEN LONG 22-LONG 26 RT, MRB 53-100-01, H1L1-SM, CARD 204 ZONE 100. CORROSION WAS REMOVED AND REWORKED AREA WAS MEASURED TREATED AND PAINTED IAW SRM 51-10-3 PAR 26,SDR SWAA2014061629110Fairing · crackedLEFT UPPER WING TO BODY FAIRING 195CL CRACKED. REPAIRED FAIRING IAW SRM.SDR DALA14033830934Latch · looseMAINTENANCE DISCOVERED THAT THE TAILCONE UPPER RT RELEASE LATCH WAS VERY LOOSE. THE TAILCONE RELEASE LATCH ASSY AND CLAMP WERE BOTH REPLACED AND THEN RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR DALA14033820934Latch · out of limitsMAINTENANCE DISCOVERED THAT THE TAILCONE UPPER LEFT RELEASE LATCH WAS OUT OF ALLOWABLE RIG LIMITS. THE TAILCONE RELEASE LATCH ASSY WAS REPLACED AND THEN RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR V0XD201405250121Angle · corrodedCORROSION ON FRAME AT ZONE 180 UNDER WING TO FUSELAGE FAIRING. R & R ANGLE IAW SRM 51-42-06.SDR CA140526010Fairing · departed(CAN) RIGHT WING TO BODY PANEL FOUND MISSING 198AR UPON ARRIVAL. 705 PANEL, MISSING. DAMAGE TO THE FLAP AS A RESULT OF THE PANEL DEPARTING THE ACFT. SB 777-53-0056 OUTLINES THE PROBLEM, DESIGN ISSUE WITH PANEL RETENTION.SDR SIMA20140526003Strap · crackedAFT BELLY PANEL 196DR HAS A CRACKED SUPPORT STRAP. REPAIRED CRACKED SUPPORT FOR THE AFT FAIRING 196DR IAW SRM 53-82-83.SDR DALA2014062703848Fitting · wornWORN GUIDE PIN FITTINGS, ON TAIL CONE SETTLEMENT AREA. DAMAGE GUIDE PIN FITTINGS A E/A ON TAIL CONE SETTLEMENT AREA WERE REPLACED IAW SRM 51-30-2.SDR AALA20140526011Radome · damagedFOUND LIGHTNING STRIKE ON THE NOSE RADOME. R & R THE NOSE RADOME.SDR DALA14032429213Release Cable · corrodedTAILCONE RELEASE CABLE TERMINAL CORRODED. R & R TAIL CONE RELEASE CABLE. OPERATION CHECKED IAW AMDS 53-52-7116.SDR SWIA201438029Structure · crackedTAIL CONE HAS A CRACK ON LT SIDE, 11 O'CLOCK, AT APPROXIMATE BS 830. C-CHECK, REPAIRED DAMAGE IAW REO.SDR IPXA2014051282927Radome · damagedNOSE RADOME DAMAGED DUE TO BIRD STRIKE DURING LANDING. R & R RADOME IAW AMM 53-12-01-902-038 AND AMM 53-12-01-402-059.SDR UIEA2014050200162Bracket · corrodedCORROSION, THE FWD & AFT SPLICE BRACKETS FOR THE WING TO BODY FAIRING SUPPORT STRUCTURE FRAME, STATION 920, BL 0 LOWER FUSELAGE. REPLACE WITH NEW PART IAW SRM 51-40-02 REV 89.SDR UIEA2014050200161Bracket · corrodedCORROSION, THE SPLICE BRACKET FOR THE WING TO BODY FAIRING SUPPORT STRUCTURE FRAME, STATION 880, BL 0. REPLACE WITH NEW PART IAW SRM 51-40-02 REV 89.SDR SIMA20140504020Strap · crackedSTRAP ASSEMBLY FOR AFT FUSELAGE FAIRINGS 195DL & 196DR IS CRACKED IN 2 PLACES. ONE CRACK IS ON STRAP ON FWD END OF AFT ANGLE. CRACK 2 IS ON AFT ANGLE ABOUT 6 INCHES FWD OF AFT END. FABRICATED NEW STRAP ASSEMBLY IAW DWG BA670-00001.SDR SIMA20140504009Fairing · crackedRIGHT MLG BAY BELLY SUPPORT FAIRING IS CRACKED. R & R RT MLG BAY BELLY SUPPORT FAIRING IAW SRM 51-42-10.SDR SIMA20140504008Fairing · crackedLEFT MLG BAY BELLY SUPPORT FAIRING IS CRACKED. R & R LT MLG BAY BELLY SUPPORT FAIRING IAW SRM 51-42-10.SDR SWAA2014052928471Former · looseWING TO BODY FAIRING FORMER LOOSE AT BS 727, LBL 31. R & R FORMER IAW DWG & SRM.SDR U2RA201405270001Frame · corrodedRIGHT WING TO BODY FAIRING, ATTACH FRAME, HAS CORROSION AT SEVERAL AREAS BS 870, AREAS WERE BLENDED IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS OF 0.063 INCHES, LOSS OF MATERIAL .002 INCHES & REMAINING MATERIAL THICKNESS OF .061 INCHES. ALODINED PRIMED & TSDR SWAA2014060228618Fairing · crackedLEFT OVERWING BODY FAIRING 195CL AFT EXTERIOR AFT CORNER CRACKED. REPAIRED FAIRING IAW WO.SDR DALA14027240964Cam · wornMAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.SDR DALA14026189016Control Arm · bindingDURING PERFORMANCE OF AMDS WC 2562-7267, TAILCONE DID NOT JETTISON. FOUND THE AFT FUSELAGE CONTROL ARM ASSY BINDING. PERFORMED ADJUSTMENT OF ARM ASSY IAW AMM 53-53-02-201. TAILCONE JETTISONED PROPERLY IAW AMDS WC 2562-7267.SDR DXTA2014042905747Radome · damagedBIRD STRIKE ON RT SIDE OF ACFT AT NOSE. REMOVED AND REPLACED RADOME ASSEMBLY IAW MM 53-50-14. OPS CHECK GOOD.SDR SWAA2014051928100Support Angle · crackedRIGHT WING TO BODY FAIRING LOWER SUPPORT STRUCTURE ANGLE CRACKED AT BS 680, WW AREA. R & R ANGLE IAW SRM & DWG.SDR CA140423005Radome · damaged(CAN) A SAFETY ISSUE RELATED TO RADOMES HAS BEEN IDENTIFIED FOLLOWING AN INTERNAL REVIEW OF THE PREVIOUS OCCURRENCES DETECTED IN MAINTENANCE ORGANIZATION. THE SAFETY ISSUE CONCERNS RADOMES FOR WHICH THE METALLIC FRAME IS STUCK ON THE COMPOSITE SHELL. DURING TSDR SIMA20140422003Bracket · crackedDURING HMBV INSPECTION FOUND THE RT MLG BAY AFT FAIRING SUPPORT PLATE IS CRACKED. R & R BRACKET IAW AMM CHAPTER 20-10-11.SDR DALA14024500936Release Cable · out of toleranceDURING THE TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION ABOVE 25 LBS IN THE RELEASE CABLE SYSTEM. THE CABLE RELEASE MECHANISM WAS ADJUSTED AND THE SYSTEM WAS RIGGED TO PULL AT 19 LBS. THE RII STEPS WERE COMPLETED ASDR AALA20140408015Seal · dislodgedBOS CREW REPORTED RADOME SEAL BECAME DISLODGED & WAS FLAPPING ON CAPTAIN`S WINDSHIELD. EMERGENCY DECLARED FLIGHT RETURNED BOS LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED SEALANT & APPLIED NEW ADHESIVE TO BULKHEAD TO ATTACH NEW SEAL. SYS GND
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