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 UALA2010072602659Panel · damagedWING-BODY FAIRING 193BL IS DELAMINATED DUE TO TIRE TREAD DURING TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. SECURED PANEL.SDR UALA2010072602658Panel · damagedWING-BODY PANEL 193DL HAS DELAMINATION DUE TO TIRE TREAD THROWN ON TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. INSTALLED PANEL.SDR UALA2010072602656Fairing · damagedWING-BODY FAIRING 193CL HAS DAMAGE DUE TO TIRE TREAD THROWN ON TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. DRILLED, FITTED AND INSTALLED NEW BODY FAIRING PANEL 193CL.SDR DALA1020149004Clamp · wornWORN CLAMP TAILCONE RELEASE CONTROL CABLE LT SIDE. REMOVED CLAMP IAW AMM 53-53-00-501 AND NEW CLAMP INSTALLED IAW AMM 53-53-00-501. OPS CHECK WAS DONE.SDR LR7A2010072000012Fairing · warpedDURING SCHEDULED C-9 CHECK PER JOB CARD HC5321 FOUND RAMP DOOR PEDESTAL FWD FAIRING WARPED AT RAMP STA 5-6, BL 15L/R, WL 146. REPLACED FWD FAIRING ASSY IAW SMP583 CHAPTER 51-60 & 51-70.SDR IPXA10561158Frame · chafedINSPECTION TYPE:C4, UNDERWING FAIRING STRUCTURE STA 900 FROM LBL 6 TO 50 FRAME LOWER CHORD LOWER SURFACE IS CHAFED. REPLACED IAW SRM 51-40-02.SDR USAA2010070991392Skin Panel · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON APU TAIL CONE INTERIOR SKIN PANEL AT BS1990, BL 0. REPAIRED APU TAIL CONE INTERIOR SKIN PANEL AT BS 1990, BL 0 IAW EA 132039.SDR IPXA10561264Bracket · bentINSPECTION TYPE:C3, NOSE RADOME LT SUPPORT ROD BRACKET IS BENT ON FWD SIDE OF 199 PRESSURE BULKHEAD. REPAIRED IAW ATS ER 10-3529.SDR HALA2010062400274Radome · crackedBIRD STRIKE ON RADOME BEYOND SRM LIMITS. REPLACED RADOME WITH NEW RADOME DUE TO INTERIOR DELAMINATION. REPLACED RADOME PER TAK 53-12-01-902-038. SAFETIED ALL NUTS. CLOSED RADOME. CHECKED OK.SDR A6WA201040433Fairing · chafedLT FUSELAGE UNDER LT INBD FLAP STUB FAIRING AND FWD OF FAIRING CHAFED. REPAIRED CHAFE DAMAGE ON LT FUSELAGE UNDER INBD FLAP STUB FAIRING FWD IAW MFG REV ORIG REO 601R-53-41-1233.SDR QMLDMG1342Tail Cone · crackedDURING INSP OF THE AIRFRAME FOUND CRACKS IN THE TAIL CONE ON AREAS THAT WERE PREVIOUSLY REPAIRED. CONSULTED WITH THE MFG ENGINEERING AND ARE AWAITING A REPAIR SCHEME.SDR A6WA201040435Fairing · chafedRT FUSELAGE UNDER FLAP STUB FAIRING HAS CHAFING DAMAGE AND FWD OF FAIRING. REPAIRED CHAFE DAMAGE ON RT FUSELAGE UNDER FLAP STUB FAIRING FWD, IAW REV ORIG REO 601R-53-41-1233.SDR 2010FA0000568Plate · crackedLT FWD WING TO BODY FAIRING SUPPORT PLATE CRACKED APPROX .5" AT FR34. R & R PLATE IAW SRM 51-72-11 AND 51-42-11. PLATE LISTED AS PRIMARY STRUCTURE BY THE MFG.SDR FDEA201006111959Skin · damagedDURING WALKAROUND FOUND NR 2 ENGINE PATIO ACCESS DOOR MISSING. CALLED MOCC AND UPLOAD PICTURES. SKIN HAS A HOLE WITH THIS MEASURES 2 INCHES LONG 1.5 INCH WIDE. TAILCONE ASSY TO BE REPLACED TAILCONE ASSY REMOVED PER MM 53-52-00-2. INSTALLED TAILCONE IAW ASDR ASMF201006001Radome · damagedDURING INITIAL CLIMB, A LIGHTNING STRUCK THE ACFT RADOME. MX PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19, NO DAMAGES WERE FOUND.SDR A6WA201040563Access Panel · crackedTAILCONE ACCESS DOOR 361AB HAS A CRACKED LOUVER REPAIRED TAILCONE ACCESS DOOR CRACKED LOUVERS IN (2) LOCATIONS IAW REO 601R-53-84-012.SDR A6WA201040390Fairing · chafedHAS CHAFING DAMAGE AT AFT WING TO FUSELAGE PART UNDER AND FWD OF FLAP STUB FAIRING BLENDED OUT DAMAGE AREA AS REQUIRED IAW REO 601R-53-41-1219 REV N/C DAMAGE DID NOT EXCEED EXISTING DEPTH.SDR A6WA201040391Fairing · chafedRT FUSELAGE HAS CHAFING DAMAGE AT AFT WING TO FUSELAGE POINT UNDER FLAP STUB FAIRING. BLENDED RT FUSELAGE AFT WING TO FUSELAGE DOES NOT EXCEED ALLOWABLE LIMITS IAW 601R-53-45-1215.SDR IPXA10560848Former · damagedINSPECTION TYPE:C4, WHILE CLOSING WING TO BODY FAIRING FOUND FAIRING FORMER TO BE DAMAGED AT 3 EA NUTPLATE ATTACH POINTS BS860, RBL44, 47 AND66 REPAIRED IAW SRM 51-70-12-0G.SDR IPXA10559985Channel · damagedINSPECTION TYPE:MOD, LT/H UNDERWING FAIRING STRUCTURE, FWD RT SIDE CHANNEL HAS ELONGATED FASTENER HOLES. R & R CHANNEL IAW SRM 51-40-02-0G.SDR V0XR201005040003Fairing · cracked(V0XR) RT WING TO FUSELAGE FAIRING STRIP X=14967.0 - X=16143.5 IS CRACKED. R & R FAIRING.SDR V0XR201005030021Strip · cracked(V0XR) LT WING TO FUSELAGE FAIRING STRIP X=14967.0 - X=16143.5 IS CRACKED. R & R STRIP. W/C 2132.SDR UALA2010050301498Structure · separatedACCOUNT RT WING TO BODY PANEL SEPARATED FROM ACFT. MAJOR REPAIR ACCOMPLISHED: EXTRUDED NUTPLATE TEE ANGLE AT STA. 1476 ATTACHING AFT EDGE OF PANEL 198AR AND FWD EDGE OF PANEL 198FR HAS UPPER SECTION BROKEN OFF. EFFECTED REPAIR IAW UA-EVA -73753.SDR UALA2010043001452Radome · damagedBIRD STRIKE ON RADOME. COMPLETED BIRD STRIKE INSP 05-51-18-201 AND CLEANED RADOME REF 12-25-00. FOUND SEGMENTED L IGHTING DIVERTER STRIP DISBONDED AT STA 166 0N UPPER RT OF RADOME MISSING PAINT ABOUT 1. NO OTHER DAMAGE FOUND REF MM 53-12 -03 P 201 PAR 2(A). SDR HALA2010041800181Release Cable · frayedTAIL CONE RELEASE HANDLE LT SIDE CABLE ASSY HAS SEVERAL BROKEN STRANDS AND IS RUSTED AT TERMINAL END. REMOVED TAIL CONE RELEASE HANDLE, LT SIDE CABLE ASSY REF B717 AMM 20-00-02. INSTALLED TAIL CONE LT INTERNAL RELEASE HANDLE CABLE ASSY REF B717 M/M 53-52-01.SDR VNAA2010041400005Radome · crackedCREW REPORTED A BIRD STRIKE ON THE RADOME ON DESCENT INTO MDT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE RADOME AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR FDEA201004091124Fitting · gougedRADOME INTERIOR FRAME LOWER RT CORNER IA GOUGED AT THE LATCH FITTING. REMOVED GUSSET IAW SRM 51-40-21, PARA 6, PG 7. FABRICATED GUSSET IAW DWG A92320606. ALODINED GUSSET IAW SRM 51-21-10, PARA A, PG 2. PRIMED GUSSET IAW SRM 51-23-10, PARA B, PG 2. PAINTED SDR FDEA201004091123Fitting · gougedRADOME INTERIOR FRAME; LOWER LT CORNER IS GOUGED AT THE LATCH FITTING. REMOVED GUSSET IAW SRM 51-40-21, PARA 6, PG 7. FABRICATED GUSSET IAW DWG A92320606. ALODINED GUSSET IAW SRM 51-21-10, PARA A, PG 2. PRIMED GUSSET IAW SRM 51-23-10, PARA B, PG 2. PAINTESDR EE4Y1004045Frame · corrodedDURING THE INSPECTION TAIL CONE CANT 976, -X20, -Z 16 FOUND FRAME CORRODED.SDR EE4Y1003036Skin · corrodedDURING THE INSPECTION TAIL CONE SECTION FROM CAN STA 976 TO CANT STA 989 BETWEEN +Z 25 AND +Z27 COOPESA FOUND SKIN CORRODED.SDR EE4Y1003034Frame · corrodedDURING THE INSPECTION TAIL CONE SECTION CANT STA 976,-X20,-Z16 COOPESA FOUND FRAME CORRODED.SDR EE4Y1003033Skin · corrodedDURING THE INSPECTION TAIL CONE SECTION FROM CANT STA 976 TO CANT STA 989, -X34, -Z22 COOPESA FOUND SKIN CORRODED.SDR QXEA2010032900186Skin · chafedBELLY SKIN CHAFED AFT OF STA 977 FROM ANGLE OF PANEL 195DL. REMOVED FASTENERS FOR ACCESS TO AREA. REMOVED CHAFE. MATERIAL REMOVED IS .025" WITHIN LIMITS. NDT CHECKS OK; PRIMED TREATED AND PAINTED AREA. ALL WORK IAW REO 670-53-00-014.SDR UALA2010032200950Radome · damagedBIRDSTRIKE RADOME AREA. MAJOR REPAIR ACCOMPLISHED, BIRDSTRIKE ON RIGHT HAND SIDE OF NOSE IN RVSM AREA AROUND FRAME 4. INSP FOUND NO CRACKS, PLNG DBLR RPR. STARTING TO DRILL HOLES AND FABRICATING REPAIR. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR.SDR ZZDA2010199Rub Strip · corrodedAFT FUSELAGE RT LOWER BODY FAIRING PANEL 160SR RUB STRIPS, CORROSION. ACCOMPLISHED RT LOWER BODY FAIRING PANEL 160SR RUB STRIPS REPLACEMENT PER B717 SRM 53-20-70 AND B717 AMM 20-60-20.SDR ZZDA2010193Rub Strip · corrodedAFT FUSELAGE LOWER BODY FAIRING RUB STRIPS, STA 870 TO 889, CORROSION. ACCOMPLISHED LOWER BODY FAIRING RUB STRIPS REPLACEMENT PER B717 SRM 51-31-00 AND B717 SRM 53-20-70.SDR UALA2010031200841Panel · damagedLEFT WING ROOT PANEL HAS EXTERNAL DAMAGE TO ALLUMESH PLY 12 X 18 INCHES. OUT OF REPAIR LIMITS. CONTACTED SFOLE AND ORDLE, NO RELIEF. PANEL NEEDS TO BE REPLACED OR REPAIRED AT SHOP 273. PANEL REPAIR. REPLACED PANEL.SDR DALA104769886Tail Cone · crackedDURING LINE CHECK FOUND CRACK ON LT SIDE OF TAIL CONE APPROXIMATELY 1" LONG. REPAIRED PER SRM 53-01.SDR ZZDA2010135Splice Plate · corrodedRIGHT WING TO BODY FAIRING SPLICE PLATE, STA 851, CORROSION. ACCOMPLISHED SPLICE PLATE REPLACEMENT PER B717 SRM 51-41-01.SDR ZZDA2010134Splice Plate · corrodedLEFT WING TO BODY FAIRING SPLICE PLATE, STA 851, CORROSION. ACCOMPLISHED SPLICE PLATE REPLACEMENT PER B717 SRM 51-41-01.SDR UIEA2010022300139Fairing · puncturedWING TO BODY FAIRING AT BS 1680 WITH A PUNCTURE/DAMAGE (HONEYCOMB EXPOSURE) MEASURING 2.5 IN. X 0.5 IN (REF FIG 1) (PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4753B253 PART 1 OF WORK INSTRUCTIONS. SCHEDULE REPEAT INSP AT EVERY 3 FC AND PERMANSDR VNAA2010022600011Radome · damagedCREW REPORTED A LIGHTNING STRIKE ON APPROACH TO MYR. AIRCRAFT LANDED IN MYR WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RADOME AND REPAIRED DAMAGE TO THE LT HORIZONTAL STABILIZER TIP, LT NOSE LANDING GEAR DOOR, LT AFT FUSDR AALA20100216TUL02Cable · frayedLEFT LOWER TAIL CONE LATCH LEVER CABLE FRAYED. REMOVED AND REPLACED AND RIGGED CABLE PER AMM 53-53-00-5 6 AND PATTERN CARD AD 5918 MPN 3913359-545 PER IPC 53-50-00-25A.SDR DLM88100694Release Cable · frayedBROKEN STRANDS ON TAILCONE RELEASE CABLE STA 1510 CANT 11 O'CLOCK POSITION. CABLE WAS REPLACED IAW AMM 20-10-17-201. CABLE WAS ADJUSTED AND OPS CHECKED IAW AMM 53-53-00-501.SDR DLM88100693Tube · dentedWORN FUSELAGE TUBE OF TAILCONE RELEASE CONTROL CABLE STA 1510 CANT 5 O'CLOCK POSITION. TUBE WAS REPLACED IAW AMM 20-30-01-201. TAIL CONE RELEASE CONTROL CABLE WILL BE ADJUSTED ON NR T0164941.SDR AALA20100209AFW01Skin · dentedDENT ON FUSELAGE TAIL CONE SKIN AT STATION 1845 NEAR STRINGER 3 LEFT APPROXIMATELY 12 IN FORWARD OF THE RUDDER TRAILING EDGE LEFT SIDE. THE DENT MEASURES 1.5 BY .073 EXCEEDING THE SRM LIMITS OF 30. HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND NO CRACKS. THESDR IPXA10558414Support · corrodedINSPECTION TYPE:C3, FWD LWR LT WING TO BODY FAIRING SUPPORT STRUCTURE - UNDER PANEL 193AL CORROSION ON LWR SURFACE OF SUPPORT STRUCTURE AT BS 892-900 LBL 6. REMOVED, FABRICATED AND INSTALLED LWR SURFACE SUPPORT STRUCTURE AT BS 892-900 LBL 6 IAW DWG 149N7125, SDR KNNA20100001Radome · damagedDURING A THUNDERSTORM WITH WINDS AT 60 MPH GUSTING TO 70 MPH, A DUMPSTER MOVED FROM THE SOUTH SIDE OF THE RAMP TO THE NORTH SIDE WHERE IT CAME TO REST IN THE GRASS BY THE TAXIWAY, DISTANCE, APPROX 200 YARDS. ALL OF THE ACFT ON THE RAMP WERE INSPECTED. THIS ASDR IXXA10WSAP036SPanel · damagedDURING ROUTINE C-CHECK INSP FOUND LT FUSELAGE BODY FAIRING PANEL NR 193PL EDGE DAMAGED. APPLIED GLASS CLOTH AND RESIN. CLEANED, TREATED, PRIMED AND PAINTED IAW SRM 51-70-06 REV 101 AND MM 51-21-10 REV 97.SDR MALA090161Skin · dentedDURING THE 2Y & 6Y CHECKS IN CWA, 1 DENT WITH A SHARP CONTOUR WAS FOUND IN THE LT UPPER TAILCONE SKIN AT STA 826 WITHIN 0.5" OF CHEM-MILL EDGE, 4.75" ABOVE THE ELEVATOR FAIRING, MEASURING 1" X 2.25" X 0.048" DEEP. HFEC WAS ACCOMPLISHED. NO CRACKS NOTED. DEN
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