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 UPS01234886Flange · corrodedINSPECTION TYPE:C, FAIRING 3608 AFT SUPPORT FRAME AFT FLANGE CORRODED. REPAIR CARRIED OUT IAW SRM 51-40-3 FIG 1.SDR COMA0110026Angle · crackedDURING 1C CHECK TASK 194-01Z, THE RIGHT OVERWING FAIRING ATTACH ANGLE ON TOP OF THE WING WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT 1226-21, REV IR, 7/6/99.SDR QXEA0100057Fairing · corrodedPDX- TWO AREAS OF CORROSION AT FORWARD END OF LEFT WING ROOT FAIRING BETWEEN STA X312 AND X333 AND IN LINE WITH Z168. REPAIRED IAW DHC-8 SRM 51-10-00 AND SRM 51-20-16.SDR SWIA972287Tail Cone · out of positionELEVATOR CONTROL BINDING IN MIDDLE OF THROW. FOUND ELEVATOR CONTACTING RIGHT SIDE OF TAIL CONE AT MID THROW. REPOSITIONED AND SECURED TAIL CONE. CHECKS OK.SDR COMA0110009Fairing · crackedTHE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53-20-13 PAGES 205 AND 206 AND AERODESIGN REPORT 1226-21.SDR DL72E010057Radome · bird strikeBIRD STRIKE ON T/O IN BWI. AIRSPEED INDICATORS DIFFER AT FL 240. ENGINE PARAMETERS NORMAL. REPLACED RADOME PER MM. ALSO, CLEARED DEBRIS FROM CO-PILOTS PITOT TUBE. TESTED PITOT SYSTEM IAW M/M. NO SPLITS NOTED.SDR UPS01434952Strap · wornINSPECTION TYPE:C, WEAR AT FUSE STA 2568 WHERE FRONT END OF APU DOORS CONTACT FUSELAGE STRAP WORN. REPLACED STRAP WITH NEW PART IAW SRM & QUERY NOTE 12/01.SDR TWAA0101009Fairing · crackedDURING CHECK-C MAINT, FOUND 2 INCH BREAK IN RUDDER LEADING EDGE WRAP AROUND FAIRING ON RT SIDE, 60 INCHES DOWN FROM TOP. REPAIRED PER SRM 51-70-1A.SDR MALA000809Skin · dentedFOUND DURING 4K HEAVY CHECK, DENT IN TAIL CONE OUTER SKIN, AT STA 815. MAINTENANCE REPAIRED IAW EO S53083.SDR DHL200080228CFairing · delaminatedAT C CK; LT WING TO FUSELAGE LWR FAIRING 741 DELAMINATED STA 650 XCW 30. REMOVED FAIRING IAW SRM 51-3-0 PG 1, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FAIRING IAW SRM 51-3-0 PG 1. REF: N/R 0627.SDR USAASB00349Sealant · looseCLT - FLT 1607 - EN ROUTE FROM PHL-CUN, A LOUD NOISE WAS HEARD FROM THE MID CABIN, LEFT SIDE, ALONG WITH AN AIRFRAME VIBRATION. ALL ENGINE PARAMETERS WERE NORMAL. SELECTING SYSTEM ''A'' ELECTRIC HYDRAULIC PUMP OFF HAD NO EFFECT. FLIGHT DIVERTED TO CLT AND LSDR AU001227Fairing · missing(AUS) LT WING TO BODY FAIRING PANEL 195CL MISSING.SDR DHL200080217CStructure · wornAT C CHECK; RT WING TO FUSELAGE LOWER FAIRING 711 RIB DOUBLER WORN STA 610 XCW 63 RT. CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0, FIG 1F. REF: N/R 1832.SDR AT0000509Tail Cone · corrodedFOUND VERTICAL STAB TAIL CONE HAS SURFACE CORROSION ON THE RIGHT AFT SIDE AND UNDER AFT SIDE. REMOVED CORROSION ON VERTICAL STAB. FABRICATED, TREATED AND INSTALLED DOUBLER IAW DC9 51-10-3, 51-30-1, 51-10-4.SDR CALA0001837Cable · out of rigTHE TAILCONE PULL FROM THE INTERIOR AND AFT DOOR HANDLES EXCEEDED LIMITS TO DROP TAIL CONE. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00 AND OPERATION CHECKED GOOD.SDR CA001214013Seal · deteriorated(CAN) THE FLIGHT CREW REPORTED AN AIRFRAME VIBRATION BETWEEN 235 - 250 KNOTS IN CLIMB. INVESTIGATION REVEALED THAT THE AERODYNAMIC SEALS ON WING ROOT PANELS 285/286 CT WERE BADLY DETERIORATED. THE SEALS WERE REPLACED AND A SATISFACTORY TEST FLIGHT PERFORMED.SDR CALA0001743Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT MOST LEFT RIB AT FASTENER HOLE OF VERTICAL STABILIZER SADDLE FAIRING. THE RIB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 55-01. A DOUBLER AND RIB WERE INSTALLED IAW SRM 55-01, 51-30-2, AND 51-30-5.SDR QXEA0003073Angle · chafedYXX- CHAFE DAMAGE TO WING/FUSELAGE FAIRING ATTACHMENT ANGLE, LOCATED ALONG THE REAR SPAR BETWEEN STATION YW43.0 PORT AND STATION YW43.0 STARBOARD. REPAIRED IAW DHC-8 RD8-57-1434.SDR QXEA0003068Tail Cone · dentedYXX- DENT/SCRATCH RIGHT HAND TAIL CONE STRUCTURE BETWEEN FRAME 6 AND 7 AND Z134. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 1-5 AND SRM 53-00-18 PAGE 3.SDR QXEA0002995Angle · crackedPDX- OUTBOARD ATTACH ANGLE FOR PANEL 92N HAS CRACK INBOARD OF WING TANK DRAIN. REPAIRED IAW FOKKER SRM 51-31-01.SDR QXEA0002994Angle · crackedPDX- OUTBOARD ATTACH ANGLE FOR PANEL 92N HAS CRACK AT MOUNT SCREW. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01.SDR QXEA0002993Angle · crackedPDX- OUTBOARD ATTACH ANGLE FOR PANEL 92N HAS CRACK AT TOP AFT MOUNT BOLT. REPAIRED IAW FOKKER SRM 53-52-07, PAGE 3, AND SRM 51-10-4 AND SRM 51-31-01.SDR CALA0001649Cable · out of rigTHE TAIL CONE DROP TEST FAILED FROM ALL THREE RELEASE HANDLES (AFT ENTRANCE, INTERIOR, AND EXTERIOR). THE TAIL CONE SYSTEM CABLES WERE RIGGED AND A FUNCTIONAL CHECK WAS GOOD IAW MM 53-53-00.SDR DHL2000715006Angle · corrodedFAIRING SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE BS 660 UNDER STRINGER 27R. INSTALL REPAIR PER B727 SRM 51-40-3, 51-10-2. MATERIAL SIZE 30 X 2 INCHES.SDR DHL2000715025Panel · corrodedCORROSION AT FAIRING PANEL 3430 FWD FLANGE LOCATED AT BS 660. INSTALL REPAIR PER B727 SRM 53-10-01, 51-40-3. SIZE OF MATERIAL USED 30 X 2 INCHES.SDR UPS00434388Frame · corrodedINSPECTION TYPE:C, FAIRING SUPPORT STRUCTURE AT BS 1460 IS CORRODED. REPLACED FAIRING FRAME.SDR UHLA002607Panel · missingAFTER ARRIVAL IN BED PANEL 262AT WAS FOUND MISSING FROM TOP LEFT OF FUSELAGE AT WING ROOT AREA. PANEL WAS REPLACED AND A/C FERRIED TO BUF FOR FURTHER REPAIRS.SDR RRXA001066Radome · lightning strikeDURING CLIMBOUT, LIGHTNING STRIKE TO NOSE SECTION. DURING LIGHTNING STRIKE INSPECTION FOUND RADOME UNSERVICEABLE DUE TO LIGHTNING STRIKE. REMOVED AND REPLACED RADOME IAW DC-8 MM CHAPTER 53-50-1.SDR DHL2000701006Fairing · missingRT FWD WING TO BODY FAIRING MISSING FROM A/C ON ARRIVAL AT CVG.SDR QXEA0002794Fairing · damagedYXX- LEFT HAND FORWARD ROOT FAIRING HAS IMPACT DAMAGE. REPAIRED IAW DHC-8 RD8-53-699 AND HORIZON AIR EA 2-53-214.SDR QXEA0002806Fairing · chafedYXX- FORWARD WING TO FUSELAGE FAIRING STATION X370.8 WEB HAS MINOR CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1-4, AND RD8-53-5163.SDR QXEA0002807Fairing · crackedPDX- LEFT HAND STUBWING AFT LOWER FAIRING SKIN HAS A 3 INCH LONG CRACK EXTENDING FROM EXISTING REPAIR. REPAIRED IAW FOKKER SRM 51-31-01, 51-10-05 AND 51-10-04.SDR DHL2000708007Angle · crackedFUSELAGE LOWER EXTERIOR BS 610 RT SIDE FAIRING PANEL ANGLE SUPPORT SHOWS CRACKS. INSTALL ANGLE SUPPORT. SIZE OF REPAIR 35 X 1 X 4 INCH.SDR 0003281149Tail Cone · separatedDURING CLIMB, A BUMP/NOISE WAS NOTICED. FLIGHT CREW DETERMINED IT WAS EITHER WAKE TURBULENCE OR CONTAINER SHIFT. FLIGHT CREW NOTICED NO PROBLEMS AND ALL INDICATIONS WERE NORMAL. FLIGHT CONTINUED TO DESTINATION. UPON LANDING, THE TOWER REPORTED A PROBLEM WISDR DLM88001678Radome · bird strikeBIRD STRIKE AT 500 FT DEPARTIANG CVG. RETURNED TO CVG. SMELL INDICATED INGESTION INTO ENGINE BUT NO ENGINE PARAMETERS CHANGED OR GAVE ANY ABNORMAL INDICATION. SMELL SUBSIDED IN 5 MINUTES. PERFORMED BIRD STRIKE CONDITION CHK PER M/M 05-51-08-6. ALL NORMAL.SDR QXEA0002406Angle · crackedPDX- CRACKED SUPPORT ANGLE FOR RIGHT HAND FUSELAGE FAIRING PANEL 92G. REPAIRED IAW HORIZON AIR EA 4-57-459.SDR CALA0001309Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN TAIL CONE UPPER LT LOCK PIN SUPPORT MOUNT BRACKET LOWER LEG ON THE AFT END. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.SDR 00FDEA00571Mount · crackedDURING ROUTINE INSP, FWD I/B MOUNT FOR THE RIGHT I/B FLAP FAIRING FOUND CRACKED. STOP DRILL CRACK, FAB AND INSTALLED PER IAW SRM 51-40-2.SDR QXEA0002197Bracket · crackedPDX- FUSELAGE BOTTOM PANEL 98G SUPPORTING BRACKET IS CRACKED AT STATION 16495. REPAIRED IAW FOKKER SRM 53-53-04, PAGE 12 AND SRM 51-31-01.SDR EIA2000215Fairing · delaminatedC3-CHECK, NR 2 ENGINE PYLON AFT LARGE V FAIRING HAS EXT SKIN DELAMINATION AT SEVERAL LOCATIONS. NR 2 ENGINE PYLON AFT V FAIRING 464 BL, REPLACED PER MM 54-51-00. (M)SDR CALA0001185Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN RIGHT WING I/B MOST LEADING EDGE FAIRING UPPER C BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-20-0.SDR CALA0001119Cable · frayedINSPECTION FOUND UPPER LEFT O/B AREA OF TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REPLACED AND TAIL CONE RELEASE MECHANISM WAS RIGGED IAW MM 53-53-00.SDR QXEA0001988Fairing · chafedYXX- LEFT HAND WING TO FUSELAGE FAIRING WEB AT YW2.00 CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-10, RD8-53-5163.SDR QXEA0001982Fairing · damagedYXX- LEFT HAND FUSELAGE TO WING ROOT FAIRING HAS NUMEROUS AREAS WITH CORE DAMAGE. REPAIRED IAW DHC-8 RD8-53-699, AND RD8-53-5155, AND HORIZON AIR EA 2-53-193.SDR CALA0001036Cable · out of rigTHE FORCE REQUIRED TO RELEASE TAIL CONE EXCEEDED ALLOWABLE LIMIT. THE CABLES WERE CLEANED, LUBRICATED, AND ADJUSTED AND A FUNCTIONAL TEST CHECKED GOOD IAW MM 53-53-00 AND WORK CARD NR EA 5350-01063.SDR P2EA00220Fairing · delaminatedSJO - DURING C-CHECK, ADF ANTENNA DELAMINATED ON LEFT WING TO BODY FAIRING, DEFECT SIZE 40 INCHES BY 29.750 INCHES. REPAIRED LEFT WING TO BODY SENSE ANTENNA PER COOPESA EO COO-CMP-3-530466-00 DATED 7-11-00. (M)SDR DHL200070907CFairing · crackedNR 4 FLAP TRACK CANOE FAIRING, FWD L/E OF SKIN HAS CRACK IN EXISTING REPAIR. REMOVED AND REPLACED EXISTING REPAIR PER SRM 51-30-2.SDR DHL200070954DFairing · gougedLT FUSELAGE BODY FAIRING FOR THE NR 4 JACKSCREW AND ELEPHANT EAR FAIRING IS GOUGED IN 2 PLACES 16 INCHES FROM THE END. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-2.SDR DHL200070953DFairing · gougedLT FUSELAGE BODY FAIRING FOR THE NR 4 JACKSCREW AND ELEPHANT EAR FAIRING IS GOUGED IN 2 PLACES 16 INCHES FROM THE END. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-2.SDR DHL200070957DFairing · crackedLT FUSELAGE BODY FAIRING FOR THE NR 4 JACK SCREW AND ELEPHANT EAR FAIRING IS CRACKED AND FASTENERS ARE MISSING OR COMING LOOSE AT FWD END, LOCATED JUST AFT OF BS 950. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-0.
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