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 CAL960080Cables · out of rigHOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLED AT 45 POUNDS AND THE TAILCONE DID NOT DROP. THE TAILCONE WAS ADJUSTED AND RIGGED IAW WORK CARD 08-5350-1-0007. (M)SDR 9600829908Release Mech · malfunctionedDURING 'B' CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS AND DROP THE TAILCONE. REPLACED THE HANDLE AND CLIPS PER EO 5350-01049.SDR 9600819854Release Mech · malfunctionedDURING LINE CHECK, FOUND THAT THE TAILCONE DID NOT RELEASE USING THE INTERIOR HANDLE. REPLACED CABLE 301A AND THE UPPER LEFT LATCH SPRING. RERIGGED THE RELEASE SYSTEM PER MM 53-50-3 PG 301 AND OPERATIONAL CHECKS OK.SDR 9521109307Latches · out of adjustDURING P-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. LUBRICATED THE LOCKING PINS AND ADJUSTED THE LATCHES. CHECKED OK.SDR CA951221015Fairing · worn/loose(CAN)LEFT AND RIGHT HAND WING TO FUSELAGE FAIRING RIVETS FOUND LOOSE. FILLET ABRAIDED THE SKIN TO A MAX .009". SKIN REPAIR DOUBLER FABRICATED AND INSTALLED.SDR P2RA950042Tailcone · crackedPHX - DURING B-CHECK, NR 1 ENGINE TAILCONE HAS CRACK ON AFT LOWER END OF TAILCONE. REPAIRED TAILCONE BY WELDING CRACK CONDITION PER AC 43-13-1A. (M)SDR CA951204025Former · corroded(CAN)LH WHEEL WELL FAIRING STRUCTURE STA 497 WL165 CRACKED. REPAIRED SRM 51-140-20.SDR 9521099857Release Mech · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LEFT LATCH DURING THE DROP CHECK. ADJUSTED THE CLIPS AND MODIFIED THE TAILCONE RELEASE CABLE LOCKSDR TWRA9565Fairing · missingDURING CRUISE APPROXIMATELY 160NM W OF HUNTER AFB, A LOUD THUMP WAS FELT AND HEARD. UPON LANDING, MAINTENANCE FOUND LARGE PIECE OF FUSELAGE FAIRING MISSING ON LEFT SIDE BELOW NR 3 MED. AIRCRAFT WAS INSPECTED AND FOUND OK FOR FERRY FLIGHT TO JFK. FUSELAGE FASDR 96ZZZM61Fairing · missingDURING CRUISE APPROXIMATELY 160NM W OF HUNTER AFB, A LOUD THUMP WAS FELT AND HEARD. UPON LANDING, MAINTENANCE FOUND LARGE PIECE OF FUSELAGE FAIRING MISSING ON LEFT SIDE BELOW NR 3 MED. AIRCRAFT WAS INSPECTED AND FOUND OK FOR FERRY FLIGHT TO JFK. FUSELAGE FASDR DLL13954464Fillet Panel · damagedA/C ARRIVED AT GATE WITH LEFT SIDE AFT FUSELAGE TO WING FILLET PANEL DAMAGED, 3 FT BY 5 FT SECTION WAS MISSING. REPLACED PANEL, RETURNED TO SERVICE.SDR 9518469984Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS AND THAT THE TAILCONE DID NOT DROP. ALSO, FOUND A FRAYED RELEASE CABLE AND TWO WORN GUIDE PINS. REPLACED THE CABLE AND PINS, REMOVED THE SEALANT FROM SDR 96ZZZM350Rib · damagedREF AVRO FAX DJR/RJ0379-95, RIGHT FUSELAGE NOSE DAMAGE AT RIB NR 1 BETWEEN UPPER 'E' LAP JOINT AND LOWER RADOME LATCH IS TO BE REASSESSED FOR REPAIR OR FURTHER SERVICE AT NEXT 'C' CHECK OR COMPLETION OF 3000 FLTS WHICHEVER IS SOONER. CURRENT CYCLES 16,863.SDR 9518459954Release Mech · malfunctionedDURING H-CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP FROM THE AIRCRAFT. CLEANED THE TAILCONE SEAL, REPLACED 6 GUIDE PINS, AND POLISHED 6 OTHER GUIDE PINS. CHECKED OK.SDR 95FDEA01706Fairing · damagedSYD - A/C HAS AN AERODYNAMIC VIBRATION STARTING AT APPROXIMATELY 220 KIAS AND CONTINUING ALL THE WAY TO NORMAL CRUISE. FOUND I/B T/E L/UPPER FAIRING DAMAGED BEYOND REPAIR. NEW FAIRING INSTALLED PER SRM 51-30-02 7, ADJ PER MM 57-22-01. ALSO, FOUND O/B DIAGONASDR DL757954334Radome · bird strikeSHORTLY AFTER T/O, HAD BIRD STRIKE, ALL INDICATIONS NORMAL UNTIL DESCENT. DESCENDING THROUGH FL 320, A/C EXPERIENCED LOUD BANG FOLLOWED BY AIR RUSHING NOISE, NO OTHER ABNORMAL INDICATIONS. FOUND RADOME AND RADAR ANTENNA DAMAGED. REPLACED RADOME AND ANTENNA,SDR 9517909906Guide Pins · wornDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE. ALSO, FOUND 5 WORN GUIDE PINS. REPLACED THE PINS AND ADJUSTED THE PULL FORCE.SDR WTAA950298Radome · birdstrikeFAT - BIRD STRIKE REPORTED ON NOSE SECTION OF AIRCRAFT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR 9517549903Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS. REPLACED THE AFT CLIP, CLEANED THE FORWARD CLIP, AND ADJUSTED BOTH. CHECKED OK.SDR 96ZZZM366Skin · gougedSKIN AROUND FRONT CARGO DOOR, FORWARD LOWER SECTION ABOUT 13 INCHES UP FROM CORNER, HAS A .016 INCH DEEP GOUGE APPROXIMATELY .25 INCH BY .375 INCH IN SIZE WITH METAL ROLLED UP AT BOTTOM. BLENDED REPAIRED AREA AT FORWARD CARGO BAY AS DESCRIBED ABOVE IAW AVRO FSDR ORJA95111Seal · corrodedLIGHT CORROSION AROUND AFT RADOME SEAL AREA INSIDE LIP OF RADOME. REMOVED CORROSION. MIN MATERIAL REMOVED. ALODINED AND PRIMED OK, REF SRM 51-10-3 A. (M)SDR 9516589926Release Cable · frayedDURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR HANDLE FROM THE CLIPS AND TO DROP THE TAILCONE. ALSO, FOUND A FRAYED RELEASE CABLE AND A WORN UPPER LEFT SLIDER BLOCK. REPLACED THE CABLE AND SLIDER BLOCK AND RERIGGED THE RELEASSDR 9516339962Seal · contaminatedDURING LINE CHECK, FOUND THAT THE TAILCONE DID NOT DROP FROM THE AIRCRAFT. CLEANED TAILCONE SEAL AND CHECKED OK.SDR 9516329885Latches · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE LATCHES AND CHECKED OK.SDR 9515399967Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVED THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR 96ZZZX1886Radome · delaminatedDURING C-CHECK, FOUND RADOME INTERIOR DELAMINATED. REPLACED RADOME, PN 59100913. ACFT TT: 22,675 HRS. ACFT TC: 41,431.SDR P5CA9500808Fairing · crackedFOUND CRACK IN FUSELAGE FAIRING PANEL BETWEEN A/C BAYS AT FORWARD ADF PANEL, APPROX STA 1000. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC INSPECTED AND DETERMINED CRACK ENDS AT STOP DRILL IAW MM 51-00-00.SDR 9517279864Cable · frayedDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAIL CONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS AND THAT CABLE RUN 301A WAS FRAYED. ADJUSTED SDR 9515389102Release Mech · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ADJUSTED AND LUBRICATED THE RELEASE MECHANISM, CHECKED OK.SDR 9515019864Block/Latch · wornDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS AND SUBSEQUENTLY DROP THE TAILCONE. ALSO, FOUND THE UPPER LEFT CABLE BLOCK WORN AND THE LOWER LEFT LATCH WITH EXCESSIVE PLAY. REPLACED BLOCK, LATCH, ASDR 9514539865Release Cable · out of positionDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT THE UPPER LEFT PULLEY WAS MISSING THE RETAINER PIN AND THE CABLE HAD JUMPED THE PULLEY AND WAS UNDAMAGED. REINSTALLED CSDR P5CA9500774Fairing · brokenLEFT LOWER WING TO BODY FAIRING 191KL BROKEN AND DELAMINATED. APPROX STATION 1239 AFT UPPER CORNER. REPAIRED AREA I/A/W SRM 51-40-15.SDR DL757954276Radome · implodedRADOME IMPLODED IN NOSE AREA. INSPECTION OF RADOME WAS ACCOMPLISHED, NO CAUSE FOR DAMAGE WAS FOUND. REBUILDED RADOME COMPLETE PER SRM 53-10-72.SDR DL757953845Radome · collapsedFLL - CLIMBING THROUGH 18,000 FT, HEARD LOUD BAND AND THUMP IN THE NOSE AREA. ACFT RETURNED AND FOUND RADOME DAMAGED. INDICATION IS THAT RADOME COLLAPSED AT A SUSPECTED AREA OF DELAMINATION. RADOME WAS ROUTED TO SHOP FOR REPAIRS.SDR 9514769105Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR 9514749955Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR WTAA950260Radome · bird strikeSMF - BIRD STRIKE REPORTED ON RIGHT FORWARD RADOME AREA. PERFORMED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR ORJA9581Tailcone · corrodedSURFACE CORROSION AFT OF FAIRING UNDER NUT PLATES APPROXIMATELY STATION 10003, RT SIDE. REMOVED LIGHT SURFACE CORROSION AND NUT PLATES FOR INSPECTION. REINSTALLED NUT PLATES TREATED AREA WITH REF TO DOUGLAS DC-9 SRM 51-10-3 PG 12, 13-14-14A. FASTENERS INSTASDR 9514269953Release Syst · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. ADJUSTED THE CLIPS AND RELEASE, SYSTEM CHECKED OK.SDR ORJA9584Frame · corrodedLEFT BODY FAIRING FRAME HAS MILD CORROSION FORWARD LEFT WHEEL WELL. BLENDED MILD CORROSION, FABRICATED DOUBLERS AND INSTALL WITH REF TO DOUGLAS DC-9 SRM 53-01 PAGE 2 FIG 1, 51-10-0 PAGE 1, 51-30-2 PAGE 12. (M)SDR ORJA9583Frame · corrodedRIGHT BODY FAIRING FRAME JUST FORWARD OF WHEEL WELL HAS MILD CORROSION. BLENDED MILD CORROSION, FABRICATED DOUBLERS AND INSTALLED WITH REF TO DOUGLAS DC-9 SRM 53-01 PAGE 2, FIG 1 51-10-9 PAGE 1, 51-30-2 PAGE 12. (M)SDR ORJA9582Frame · corrodedFRAME FOR RIGHT BODY FAIRING AFT OF WHEEL WELL HAS MILD CORROSION. CLEANED CORROSION, ALODINED AND PRIMED REF SRM 51-10-3. (M)SDR CAL950831Lock Pins · wornHOU - THE TAILCONE HUNG UP ON UPPER LATCHES AND FAILED TO DROP DURING TEST WHILE AIRCRAFT WAS IN D-CHECK, A NEW UPPER LEFT TAILCONE RETAINING LOCK PIN AND A NEW TAILCONE TO EMPENNAGE ALIGNMENT PIN WERE INSTALLED. THE TAILCONE WAS RIGGED AND THE RELEASE SYSTEMSDR 9514189922Latches · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ALSO, FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LATCHES. ADJUSTED THE TAILCONE RELEASE SYSTEM AND CHECKED OK.SDR MWEA95284Fairing · bentPILOT REPORTS ON WALK-AROUND IN ATLANTA, THE RIGHT OUTBD MOVEABLE VANE TRACK FAIRING WAS BENT UPWARD. MAINTENANCE IN ATL REMOVED FAIRING, AIRCRAFT WAS FERRIED TO MKE. NEW FAIRING WAS INSTALLED, A/C RETURNED TO SERVICE.SDR DL757954018Radome · damagedHOLE AT 9 O'CLOCK POSITION. SHOP INSPECTION FOUND MOISTURE AND OLD WET-LAY REPAIRS. REBUILD RADOME COMPLETE USING 757 MOLD AND BOEING SPEC MATERIALS.SDR 9513789853Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR 9513659855Latches · req adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS; INADEQUATE FORCE WAS SUBSEQUENTLY REQUIRED TO DROP THE TAILCONE. ADJUSTED THE CLIPS AND LATCHES. CHECKED OK.SDR DL757954013Radome · damagedRADOME WAS REMOVED FOR MOISTURE. SHOP INSPECTION FOUND OLD REPAIRS TO BE OF WET-LAY REPAIRS. CUT OLD SHELL OFF FROM BASE RING AND REBUILD RADOME COMPLETE PER SRM 53-10-72 USING 757 RADOME MOLD AND BOEING SPEC MATERIAL.SDR P5CA9500718Radome · delaminatedNOSE RADOME HIT BY BIRD ON LANDING. THE TOP SECTION BS 114, 9 INCH DIAMETER OF DELAMINATION, NO BROKEN SKIN INSIDE OR OUT. ENGINEERING REVIEWED OK FOR FLIGHT TO MAINTENANCE BASE FOR RADOME REPLACEMENT.
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