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 ORJA9769Lock Cable · disconnectedTAIL CONE UNSAFE LIGHT ON. RE-CONNECTED LOCK CABLE TO TURN OFF UNSAFE LIGHT. (X)SDR ORJA9768Cable · disconnectedTAIL CONE UNSAFE LIGHT. PERFORMED CHECK OF TAIL CONE JETISON SYSTEM. FOUND EXT HANDLE CABLE BALL END OUT OF RECEPTICLE. RE-ATTACHED CABLE EXTINGUISHING UNSAFE LIGHT PER MM 53-53-00. (X)SDR WTAA970078Radome · bird strikeSFO - BIRD STRIKE ON RADOME TOP LEFT PORTION REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR 9708939860Clip · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERIOR HANDLE FROM CLIPS. CLEANED AND ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR DHL9770134CFairing · crackedDURING C-CHECK, LOWER FUSELAGE BS 660 APPROXIMATELY STR 26L, ATTACH FLANGE FOR LOWER BODY FAIRING PANEL HAS OIL CANNING, CRACK AND SURFACE CORROSION. CUT OUT CRACKED AND CORRODED AREA FROM FLANGE PER SRM 51-10-1. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 16 BYSDR DHL9770233DFairing · gougedAT D-CHECK, DEEP GOUGED ON SKIN AFT OF HYD SYSTEM FAIRING FRAME AT STA 1010. CUT OUT DAMAGED AREA, HFEC, NO CRACKS NOTED. INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 11 X 8.SDR 9708829956Release Mech · lack of lubeDURING TAIL CONE FUNCTIONAL TEST, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. CLEANED AND LUBRICATED RELEASE SYSTEM, OPERATIONAL CHECK OK.SDR 9708479944Release Mech · out of adjustDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE INTERIOR AND EXTERIOR HANDLES FROM CLIPS. ADJUSTED CLIPS AND RIGGED RELEASE SYSTEM, OPERATIONAL CHECK OK.SDR 9708469763Release Mech · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THE TAIL CONE DID NOT DROP AND EXCESSIVE FORCE WAS REQUIRED TO REMOVE HANDLE FROM CLIPS. ALSO, FOUND THE UPPER TWO GUIDE PIN BEARING PLATES ON THE TAIL CONE WORN AND NIINE GUIDE PINS WORN. CLEANED SEAL, REPLACED BEARINSDR 9708499160Release Mech · out of adjustDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND 3 BEARING PLATES WORN ON TAIL CONE. REPLACED BEARING PLATES, ADJUSTED TAIL CONE RELEASE SYSTEM AND OPERATIONAL CHECK OK.SDR 9708489929Release Mech · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ADJUSTED TAIL CONE RELEASE LATCHES, OPERATIONAL CHECK OK.SDR 97ZZZX2565Seal · tornMKE/LAX - CHARTER FLIGHT DIVERTED TO STL. P/R APPROXIMATELY 6 FEET OF THE 9 FEET RUBBER SEAL ON RT WING TO FUSELAGE FAIRING TORN OFF IN-FLIGHT. PILOTS REPORTED BY FLIGHT PHONE THAT ACFT DEVELOPED A MODERATE VIBRATION DURING FLIGHT. A PRECAUTIONARY OVERWEIGHSDR ASAA9780066Release Mech · out of adjustSEA - DURING MAINTENANCE TEST, THE TAILCONE FAILED TO DEPART THE AIRCRAFT WHEN THE EMERGENCY RELEASE HANDLE WAS ACTIVATED FROM THE AFT CABIN ENTRY DOOR POSITION. FOUND THE AFT RELEASE MECHANISM CLIPS ADJUSTMENT TOO TIGHT. ADJUSTED THE CLIP TENSION IAW DC-9 MSDR 9708199955Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE INTERIOR AND EXTERIOR TAIL CONE RELEASE HANDLES FROM CLIPS AND TO DROP TAIL CONE. RIGGED RELEASE SYSTEM AND ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR CALA9701054Tail Cone · dentedINSPECTION FOUND A DENT ON RT SIDE OF TAIL CONE AT STA 2265. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, FIGURE 1 AND 53-00-01.SDR SWAA970459Fairing · damagedLT WING TO BODY FAIRING DAMAGED FROM LT FLAP AND MID FLAP. FAIRING REMOVED AND REPAIRED, D-VELCO WORK ORDER SSR 336, REPAIR STATION DIRR408N, REINSTALLED FAIRING.SDR P5CA9700505Fairing · delaminatedDELAMINATED BODY FAIRING PANEL, 2ND PANEL BEHIND ADF PANEL RT SIDE NR 194CR. REPAIRED PANEL PER BOEING SRM 51-40-07.SDR 9707959853Release Mech · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE TAIL CONE RELEASE HANDLE FROM CLIPS AND TO RELEASE TAIL CONE. RIGGED RELEASE SYSTEM, ADJUSTED LOWER LEFT CORNER ALIGNMENT PINS, FUNCTIONAL CHECK OK.SDR DHL9780133CFairing · crackedAT C-CHECK, LOWER FUSELAGE FAIRING RIGHT SIDE HAS TWO CRACKS. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLERS, INSTALLED DOUBLERS PER SRM 53-2-0.SDR 9707659969Release Mech · out of adjustDURING L CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO ACTUATE TAILCONE RELEASE SYSTEM. RIGGED RELEASE SYSTEM. OPERATIONAL CHECK OK.SDR CALA9700630Clamp · brokenDURING 1/4 D-CHECK INSP, FOUND TAIL CONE RELEASE CONDUIT CABLE HAS CLAMP AT LOWER END BROKEN. REMOVED AND REPLACED BROKEN CLAMP WITH NEW CLAMP (P/N AN74206).SDR DHL9780108CRadome · crackedAT C-CHECK, AIR COND CHIN SCOOPS HAVE CRACKS. REMOVED AND REPAIRED RADOME IAW M/M 53-50-1.SDR P5CA9700485Spring · bentBENT SPRING AT ATTACH POINT INSIDE RADOME ASSY. REPAIRED PER BAC MM 20-11-32.SDR P5CA9700474Fairing · damagedDAMAGED 2 EACH BODY FAIRING PANELS AFT OF NR 2 ADF PANEL RIGHT SIDE. REPAIRED PANELS PER BOEING SRM 51-40-07.SDR 9707429753Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM RETAINING CLIPS. ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR 97ZZZM570Panels · missingAFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS 198K AND 196B WERE MISSING. RIGHT WING TO FUSE PANELS REINSTALLED. AIRCRAFT RETURNED TO SERVICSDR 97ZZZM569Panels · missingAFTER APPROXIMATELY 125 NM, AFTER TAEKOFF, A SUDDEN VIBRATION WAS FELT. AIRCRAFT RETURNED TO BASE. LANDING WAS NORMAL. AFTER LANDING, INSPECTION REVEALED PANELS 198K AND 196B WERE MISSING. RIGHT WING TO FUSE PANELS REINSTALLED. AIRCRAFT RETURNED TO SERVICSDR 9707339160Latches · out of adjustDURING L-CHECK, FOUND THAT TAILCONE DID NOT DROP WHEN RELEASE SYSTEM WAS ACTIVATED. ALSO FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO ACTIVATE RELEASE SYSTEM. ADJUSTED LATCHES. OPERATIONAL CHECK OK.SDR 9707329954Release Mech · malfunctionedDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE EXTERNAL TAILCONE RELEASE HANDLE FROM CLIPS. REPLACED CLIPS, EXTERNAL HANDLE, CABLE, TAILCONE RELEASE LOCK CABLE FITTING, AND CABLE CONNECTING INTERNAL AND EXTERNAL HANDLE. OPERATIONAL CHESDR 9707309105Clips · out of adjustDURING LINE CHECK, FOUND EXCESSIVE FORCE REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM CLIPS. CLEANED AND LUBED LATCH PIN ASSEMBLIES AND INTERNAL HANDLE. ALSO, ADJUSTED CLIPS AND OPERATIONAL CHECK OK.SDR 9707099155Latch Pins · lack of lubeDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE AND EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERIOR HANDLE FROM CLIPS. CLEANED AND LUBRICATED TAILCONE LATCH PINS AND INTERIOR HANDLE. OPERATIONAL CHECK OK.SDR 9707119755Clip · wornDURING H-CHECK, FOUND INADEQUATE FORCE REQUIRED TO REMOVE EXTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. REPLACED SPRING CLIP, OPERATIONAL CHECK OK.SDR 9706849970Release Mech · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO ACTUATE TAILCONE RELEASE SYSTEM. RIGGED RELEASE SYSTEM. OPERATIONAL CHECK OK.SDR 9706859156Release Mech · out of adjustDURING LINE CHECK, THE TAILCONE RELEASE SYSTEM FAILED THE COMBINED CLIP FORCE AND SYSTEM ACTUATION TEST. RIGGED RELEASE SYSTEM. OPERATIONAL CHECK OK.SDR 9706529102Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE EXTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. CLEANED CABLE BALL END, FITTING AND ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR 9706509978Release Syst · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE PULL FORCE WAS REQUIRED DURING TAIL CONE DROP CHECK. RIGGED RELEASE SYSTEM, OPERATIONAL CHECK OK.SDR 9706499101Clips · out of adjustDURING L-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE INTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. REPLACED CLIP AND ADJUSTED, OPERATIONAL CHECK OK.SDR 9706039989Clips · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL INTERIOR TAIL CONE RELEASE HANDLE FROM RETAINING CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.SDR CA970325003Airframe · lightning strike(CAN) AIRCRAFT STRUCK BY LIGHTNING ON INBOUND LEG, CAUSING SEVERE DAMAGE TO RADOME AND NOSE GEAR DOORS. AIRCRAFT LANDED OK. LIGHTNING DAMAGED SEVERAL STATIC WICKS AND BELLY OF AIRCRAFT. ALSO THE #2 DC GEN. GCU, #1 NAV., #1 AND #2 ADF AND RADAR WERE INOPERATIVESDR 9706029180Release Mech · lack of lubeDURING LINE CHECK, FOUND THAT THE TAIL CONE FAILED TO DROP DURING FUNCTIONAL CHECK. CLEANED AND LUBED RELEASE SYSTEM, FUNCTIONAL CHECK OK.SDR 9705729997Clips · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERNAL TAIL CONE RELEASE HANDLE FROM RETAINING CLIPS. ALSO, FOUND CABLE FRAYED ABOVE LOWER LATCH. ADJUSTED RETAINING CLIPS, REPLACED CABLE AND RIGGED, OPERATIONAL CHECK OK.SDR 9705719938Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL EXTERNAL TAIL CONE RELEASE HANDLE FROM RETAINING CLIPS. ALSO, FOUND BROKEN RETAINING CLIP ON INTERNAL RELEASE HANDLE. REPLACED INTERNAL RETAINING CLIP AND ADJUSTED EXTERNAL CLIPS, OPERATIONALSDR 9705709103Release Mech · out of adjustDURING C-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ADJUSTED RELEASE SYSTEM, OPERATIONAL CHECK OK.SDR 9705429940Clip · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR 9705159150Clips · out of adjustDURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERIOR TAILCONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS. OPERATIONAL CHECK OK.SDR 9704989750Latch · out of adjustDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY THE TAILCONE. ADJUSTED UPPER RIGHT LATCH LEVER ASSEMBLY. OPERATIONAL CHECK OK.SDR CALA9700349Cables · out of adjustTHE TAIL CONE EXTERIOR RELEASE HANDLE PULL WAS TOO LOW. THE TAIL CONE CABLE SYSTEM WAS ADJUSTED IAW MM 53-50-3.SDR 9704859302Release Mech · out of adjustDURING LINE CHECK, FOUND THAT TAIL CONE WOULD NOT DEPLOY USING THE AFT PASSENGER DOOR HANDLE OR THE INTERNAL RELEASE HANDLE AND THE EXTERNAL HANDLE REQUIRED EXCESSIVE FORCE TO REMOVE FROM CLIPS. CLEANED CABLES, RETENSIONED CLIPS, TAIL CONE SEAL, EXTERNAL HANDSDR P5CA9700419Fairing · crackedFAIRING NR 294HR CRACKED ON EDGE. REPAIRED PER BOEING SRM 51-40-09.SDR 9704869140Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.
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