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 SIMA20150130012Attach Angle · crackedLEFT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IS CRACKED BETWEEN FRAMES 48 & 49. 2 & 1/2" LONG. REPAIRED LT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE IAW SRM 53-23-12 TYPE 2. CHANGED ZONE TO ZONE 200.SDR DALA2015020200863Frame · crackedBS 1510, FRAME CRACKED AT UPPER RT TAIL CONE LATCH. REPLACED THE FRAME IAW SRM 51-01.SDR REXA2015012600099Strap · crackedTASK CARD 900-53-180-506 AFT BELLY FAIRING JOINT STRAP IS CRACKED IAW REO 690-53-82-052. REPAIRED CRACKED JOINT STRAP IAW REO 690-53-82-052.SDR REXA2015012600098Channel · crackedTASK CARD 900-53-180-506 AFT BELLY FAIRING C CHANNEL IS CRACKED. REPAIRED CRACKED C CHANNEL IAW SRM 51-42-13-001-001-A01. PERFORMED MODSAM IAW IS 670538200021.SDR SIMA20150121017Attach Angle · crackedAFT BELLY FAIRING ATTACH ANGLE IS CRACKED, LOCATED FWD LT ATTACH POINT JUST INBD OF FLAP. REPAIRED AFT BELLY FAIRING ATTACH ANGLE IAW ETN-EM-53-142.SDR SIMA20150121009Attach Angle · crackedRIGHT LOWER ATTACHMENT ANGLE NR 2 IS CRACKED ON THE LE APPROX 3/8 INCHES LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R RT LOWER ATTACHMENT ANGLE NR 2 IAW ETN EM-53-142.SDR SIMA20150121008Attach Angle · crackedRIGHT LOWER ATTACHMENT ANGLE NR 3 IS CRACKED ON THE LE APPROX 1/2 INCH LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R RT LOWER ATTACHMENT ANGLE NR 3 IAW ETN EM-53-142.SDR SIMA20150121007Attach Angle · crackedLEFT LOWER ATTACHMENT ANGLE NR 1 IS CRACKED ON THE LE APPROX 2 INCHES LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. REPLACED DAMAGED LT LOWER ATTACHMENT ANGLE NR 1 ON LE IAW ETN EM-53-142.SDR SIMA20150121010Attach Angle · crackedLEFT LOWER ATTACHMENT ANGLE NR 2 IS CRACKED ON THE LE APPROX 1 INCH LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R LT LOWER ATTACHMENT ANGLE NR 2 FOR THE LATERAL WING TO FUSELAGE FAIRING IAW SRM 51-40-02 & ETN EM-53-142.SDR SIMA20150121006Attach Angle · crackedLEFT UPPER ATTACHMENT ANGLE IS CRACKED 1/2 INCH BY A RIVET BETWEEN FRAMES 48 - 49. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R LT UPPER ATTACHMENT ANGLE BETWEEN FRAMES 48 - 49 IAW SRM 53-23-12.SDR DALA2015012300590Latch · wornTAILCONE RELEASE SPADES WORN UPPER RT AND LOWER LT. REMOVED AND INSTALLED NEW LATCH SPADES IAW AMM 53-52-01.SDR DALA2015012300589Angle · corrodedLOWER CABLE RELEASE ANGLE PIN CORRODED. R & R THE ANGLE IAW MM 53-52-01.SDR SWAA2015021836694Skin · delaminatedTAIL CONE SKIN DELAMINATED AT BS 1156+14, RBL 7. REPAIRED TAIL CONE IAW AMM SRM.SDR SWAA2015021736649Drag Angle · crackedRIGHT WING TO BODY FAIRING DRAG ANGLE CRACKED AT BS 540, STRINGER 21R. REPAIRED ANGLE IAW SRM.SDR P5CA2015011900002Radome · damagedRECEIVED LIGHTNING STRIKE ON FINAL. LEFT SIDE OF NOSE, ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW AMM 05-51-19. FOUND RADOME & RUDDER TOP T/E DAMAGED. REPLACED RADOME IAW AMM 53-13-01 AND ACCOMPLISHED TEMP REPAIR ON RUDDER IAW SRM 55-40-30.SDR DALA2015012100423Cable · wornTAILCONE DISPLACEMENT BOTTLE PULL CABLE WORN. REPLACED PULL CABLE.SDR QMLA2015011515005Rail · crackedWHILE PERFORMING AIRWORTHINESS CHECK FOUND CRACK ON RT SIDE CREST COWL RAIL AFT PORTION, LOOKED ON LT SIDE CREST COWL RAIL & FOUND ANOTHER CRACK.SDR DALA2015011600358Tail Cone · no testTAILCONE FAILED TO DROP WITH AFT CABIN DOOR RELEASE IAW AMDS 5350-01077-0101, STEP 3, REF L/P'S 1784037, 1783916,1783887 AND 1783832 FOR REPAIRS AND PERFORMED THE AMDS CARD 5350-01077-0101. TAILCONE FUNCTIONAL.SDR DALA2015011500355Latch · unsecureRIGHT LOWER TAILCONE LATCH ASSY ATTACH HARDWARE MISSING. R & R LOOSE RIVETS IAW SRM 51-30.SDR DALA2015011500354Mount Bracket · wornSUPPORT STRUCTURE AND MOUNT BRACKET ON ACFT FOR RT LOWER TAILCONE LATCH IS WORN AND LOOSE FASTENERS. R & R WORN LATCH, REPLACED LOOSE FASTENERS IAW SRM 51-30.SDR DALA2015011500353Latch · wornRT UPPER TAILCONE LATCH ASSY LOOSE AND WORN AT SLIDER BLOCK. REPAIRED IAW AMM 53-53-02.SDR DALA2015011500352Bracket · wornLT BRACKET WORN FOR KEVLAR CABLE SPRING ATTACH POINT ON TAILCONE. OBTAINED SHOP PART, MPN 9952641-5 AND DRILLED UP. TREATED AND PRIMED. NEED TO ASSEMBLE PARTS AND INSTALL. REF IPC 53-50. AND DWG 99552641. INSTALLED REF AMM 53-53-02.SDR DALA2015011500351Latch · damagedRIGHT LOWER TAILCONE LATCH ASSY ATTACH HARDWARE MISSING ON 1510 FRAME. REMOVED LATCH, REPLACED LOOSE AND MISSING FASTENERS IAW SRM 51-30-02, INSTALLED LATCH.SDR DALA2015011500337Pulley Bracket · wornLEFT PULLEY BRACKET, TAIL CONE RELEASE CABLE, GUARD PIN HOLE WORN. R & R PULLEYS BRACKET FOR TAIL CONE RELEASE CABLE AT LOWER LEFT IAW SRM 51-30-02 AND SRM 51-30-01.SDR CA150114004Rub Strip · departed(CAN) RH ENGINE FOD INJESTION, WING TO FUSELAGE FAIRING LEADING EDGE RUBBING STRIP CAME LOOSE AND WENT THROUGH ENGINE IN FLIGHT. PROBLEM KNOWN BY LEARJET (KNOW FOR COMING OFF BUT NOT GOING THROUGH THE ENGINE), SB45-57-10 ALREADY EXISTS TO REPLACE THE EXISTING SDR SWIA201540646Fairing · puncturedRIGHT WING TO FUSELAGE AFT FAIRING HAS TWO PUNCTURES. REPAIRED RT AFT WING TO BODY FAIRING IAW REO.SDR SWAA2015031737480Tee Fitting · crackedRIGHT SIDE WING TO BODY FAIRING STRUCTURE T CHORD CRACKED AT BS 540. R & R T CHORD IAW EO & EA.SDR REXA2015010700032Channel · looseMLG FAIRING LT VERTICAL SUPPORT CHANNEL IS LOOSE. R & R LT VERTICAL SUPPORT CHANNEL IAW SRM 51-42-20-001-001-A01.SDR YENA20150107001Fairing · unsecureAIR RETURN TO DEPARTURE DUE TO A VIBRATION DURING CLIMB. FOUND SPEED TAPE PARTIALLY OFF FROM WTB PANEL 191BT. APPLIED NEW SPEED TAPE IAW SRM 53-35-00.SDR U2RA201501050001Support Bracket · crackedWING TO BODY FAIRING SUPPORT BRACKET LOCATED AT BS 1300 S20R IS CRACKED IN TOP CORNER. CRACK LENGTH MEASURED TO BE .750". REMOVED DAMAGE AND INSTALLED REPAIR ANGLE, FILLER IAW SRM 53-60-71, FIG. 201, REPAIR 1.SDR DALA2016102607683Strap · corrodedCORROSION ON TAILCONE STRAPS. REMOVED AND REPLACED STRAP IAW AMM.SDR ASMF201501024Radome · dentedDURING TRANSIT CHECK, IT WAS DETECTED A DENT IN RADOME BETWEEN 4:00 AND 5:00 HRS POSITION OF 4.0 INCHES IN LENGTH & 3.0 INCHES WIDE. EVALUATED THE DAMAGE & FOUND OUT OF LIMITS IAW SRM 53-52-00. ACFT WAS SENT TO THE HANGAR & ISSUED THE NON-ROUTINE CARDS A0223SDR DALA2015010600135Lock · wornFOUR TAILCONE LOCK FITTINGS ARE WORN. R & R THE TAIL CONE LOCK HOUSING IAW SRM 51-30-01 AND AMM.SDR DALA2015011500322Fairing · crackedFOUND CRACK ON FWD WING TO BODY FAIRING PANEL 191AB. REPAIR PERFORMED IAW SRM.SDR DALA2015011500321Fairing · crackedFOUND CRACK ON FAIRING PANEL 191DB. BODY FAIRING PANEL DB REPAIRED IAW SRM.SDR V0XD201412190268Channel · crackedAFT WING TO FUSELAGE FAIRING AFT CHANNEL ON STRAP CRACKED. R & R AFT WING TO FUSELAGE FAIRING AFT CHANNEL IAW DWG CC670-39251 & SRM 51-42-13, 51-40-11, 51-25-06, 51-42-06, 51-25-16 & AMM 51-21-01.SDR DALA2014121506529Latch · wornDURING TAILCONE CHECK, FOUND LT UPPER AND LOWER TAILCONE LATCH ASSEMBLIES WORN. REPLACED LT UPPER AND LOWER LATCH ASSYS IAW AMM 53-52.SDR DALA2014121506535Release Cable · kinkedMAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS KINKED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.SDR DALA2014121006497Release Mech · damagedDURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE MECHANISM TO BE DAMAGED. MAINTENANCE REPLACED THE RELEASE MECHANISM FITTING AND CRANK ASSY.SDR SWIA201440402Radome · out of toleranceCLEARANCE BETWEEN FUSELAGE SKIN AND RADOME FAILED GAP CHECK. TRIMMED RADOME TO ACHIEVE PROPER CLEARANCE IAW REO.SDR DALA2014120406440Release Cable · misroutedDURING CHECK, MAINTENANCE FOUND THE FORCE REQUIRED TO RELEASE THE TAILCONE EXCEEDED THE LIMITS. MAINTENANCE FOUND THE RELEASE CABLE ROUTED IMPROPERLY AND ROUTED THE CABLE TO THE PROPER POSITION AND PERFORMED A TAILCONE FUNCTIONAL TEST.SDR SIMA20141203006Fairing · crackedFORWARD BELLY FAIRING CRACKED. REPAIRED FWD BELLY FAIRING IAW ERS-ERS-EM-5300-741.SDR DALA2014120306439Pin · wornDURING CHECK, MAINTENANCE FOUND THE TAILCONE LOWER LEFT RELEASE LATCH PIN WORN. MAINTENANCE REPLACED THE LATCH PIN.SDR DALA2014120106351Attach Bracket · wornDURING CHECK, MAINTENANCE FOUND THE TAILCONE SPRING ATTACH BRACKET WORN. MAINTENANCE REPLACED THE WORN BRACKET.SDR DALA2014120106350Cable · frayedDURING CHECK, MAINTENANCE FOUND THE TAILCONE KEVLAR CABLE TO BE FRAYED. MAINTENANCE REPLACED THE KEVLAR CABLE.SDR DALA2014120106352Receptacle · wornDURING CHECK, MAINTENANCE FOUND THE TAILCONE UPPER LT LATCH PIN RECEPTACLE HAS A WORN EAR. MAINTENANCE REPLACED THE RECEPTACLE.SDR DALA2014120206438Bushing · wornDURING CHECK, MAINTENANCE FOUND THE TAILCONE TEE PIN BUSHING WORN. MAINTENANCE REPLACED THE BUSHING.SDR DALA2014120206386Cable · wornJETTISON BOTTLE CABLE WAS FOUND WORN. R & R TAILCONE JETTISON CABLE.SDR DALA2014120206385Guide · wornGUIDE ON TAILCONE WORN. R & R GUIDE IAW SRM.SDR DALA2014112406238Release Cable · frayedMAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS BULGED AND FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
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