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 CAL950730Clip · out of adjustHOU - THE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW FROM CLIPS AT 16 POUNDS. THE TAILCONE EXTERIOR RELEASE HANDLE CLIPS WERE ADJUSTED PER MM 53-53-00. (M)SDR CAL950729Cables · out of adjustHOU - THE TAILCONE INTERIOR RELEASE PULLS HIGH AT 68 POUNDS. THE TAILCONE INTERIOR RELEASE SYSTEM CABLES WERE ADJUSTED PER MM 53-53-00. (M)SDR CAL950728Clip · out of adjustHOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLS LOW FROM CLIPS. THE INTERIOR RELEASE HANDLE CLIPS WERE ADJUSTED PER MM 53-53-00. (M)SDR CAL950727Cables · out of adjustHOU - THE PASSENGER AFT ENTRANCE DOOR TAILCONE RELEASE PULLS LOW AT NINE POUNDS. THE AFT PASSENGER ENTRY DOOR TAILCONE RELEASE SYSTEM CABLES WERE ADJUSTED PER MM 53-53-00. (M)SDR 9512529857Release Mech · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE TAILCONE, CHECKED OK.SDR 9512259978Release Mech · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS. ALSO, FOUND THAT THE UPPER LATCHES RELEASED PRIOR TO THE LOWER LATCHES AND THAT THE TAILCONE FAILED TO DROP. ADJUSTED TAILCONE PER MM 53-50-3, FUNCTIONAL CHECK OK.SDR P5CA9500697Radome · delaminatedRADOME HAS AREAS OF ERROSION AND APPROXIMATELY 2 BY 2 AREA OF DELAMINATION. REPAIRED PER BOEING SRM 51-40-09.SDR 9512269160Clip · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. REPLACED AND ADJUSTED THE AFT CLIP, CHECKED OK.SDR CAL950706Clips · out of adjustHOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLED FROM CLIPS AT 45 POUNDS. THE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00. (M)SDR ABXA9500849Fairing · corrosionDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ALONG THE PARAMETER OF THE LEFT AFT WING TO BODY FAIRING. REPAIRED IAW ABX REA D953-12379-MR.SDR 9511663223Panel · vibrationWHILE CLIMBING THROUGH FL 300 AT A SPEED OF MACH 0.78, EXPERIENCED AIRFRAME VIBRATION. SLOWED SPEED TO APPROXIMATELY 0.74 MACH AND VIBRATION WENT AWAY. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE FASTENERS ON A BELLY PANESDR 9511249964Handle · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE HANDLE FROM THE CLIPS. ADJUSTED THE HANDLE PER MAINTENANCE MANUAL 53-50-03.SDR MWEA95238Connector · corrodedDURING CRUISE, TAIL CONE MISSING LIGHTS WENT ON AND OFF INTERMITTENTLY. THE TAILCONE SWITCH CONNECTORS WERE FOUND CORRODED. CLEANED CORROSION AND OPS CHECKED GOOD.SDR 9511239150Handle · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR TAILCONE HANDLE AND DROP THE TAILCONE. RERIGGED THE TAILCONE, CHECKED OK.SDR CAL950615Clips · out of adjustHOU - THE INTERIOR TAILCONE RELEASE REQUIRED EXCESSIVE FORCE TO PULL FROM CLIPS. THE RELEASE HANDLE CLIPS WERE ADJUSTED TO WITHIN SPECIFICATION PER MM 53-53-00. (M)SDR USAA950654Tailcone · damagedIAD - THE AFT TAILCONE WAS INADVERTENTLY DEPLOYED. THE TAILCONE DID NOT FALL AWAY ENOUGH TO PULL THE ESCAPE SLIDE OUT OF THE PACK TO DEPLOY. MAINTENANCE REPAIRED THE DAMAGED CONE TIP AND REINSTALLED THE TAILCONE. (W)SDR 95ZZZX4285Fairing · screws detachedDURING PRE-FLIGHT INSPECTION, THE PILOT DISCOVERED EXTENSIVE F.O.D. TO THE RIGHT ENGINE FAN AND NOISE SUPPRESSION BAND. INVESTIGATION REVEALED 2 SCREWS ON THE WING LEADING EDGE FAIRING HAD BACKED OUT. THE PREVIOUS CREW DID NOT REPORT ANY SHIFT IN ENGINE PARASDR P5CA9500450Support · crackedCRACK IN FAIRING SUPPORT AT FUSELAGE RIGHT SIDE AT BS 1394 AREA ABOVE WING. REPLACED SUPPORT PER BOEING SRM 51-40-03.SDR 9510069881Clips · out of adjustDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE TAILCONE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS.SDR 9509999948Tailcone · departed acftDURING LANDING ROLLOUT RDU AT APPROXIMATELY 60 KNOTS, THE TAILCONE SEPARATED FROM THE AIRCRAFT WITH AN ACCOMPANYING WARNING INDICATION. THE SLIDE DID NOT DEPLOY, TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. FOUND THAT THE EXTERIOR HANDLE WAS NOT STOWED IN THSDR CAL950547Cables · out of adjustHOU - THE TAIL CONE WOULD NOT RELEASE WHEN INTERIOR HANDLE WAS PULLED. THE CABLES WERE ADJUSTED IAW MM 53-50-3. (X)SDR UPS203634Box Fairing · crackedWHILE IN C-CHECK MAINTENANCE FOUND CRACK EXTRUDING PAST STOP DRILL IN NOSE WHEELWELL SIDE BOX FAIRING. B.S. 277, RBL 23.5, WL 168. REPAIRED IAW SRM 51-10-2, 51-30-2, 51-21-1.SDR 9509789966Pins · wornDURING LINE CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP. REPLACED 5 WORN PINS AND CLEANED THE SEAL, CHECKED OK.SDR 9509779971Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR 95ZZZM418Door · corrodedDURING C-CHECK, FOUND CORROSION AROUND TAILCONE LOWER DOOR. MECHANICALLY REMOVED CORROSION. TREATED AND PRIMED AREA. FABRICATED AND INSTALLED DOUBLER IAW DER DWG ARW 950051-6037.SDR DL757953180Radome · damagedUPON INSPECTION RADOME (DL 13) WAS FOUND TO EXCEED MOISTURE LIMITS AT TOP AND RIGHT SIDES CONTAINING AN AREA OF 20 PERCENT OF RADOME SURFACE. ACCOMPLISHED REPAIRS PER SRM 53-10-72.SDR 9509539986Latch Pin · malfunctionedDURING PERIODIC CHECK, FOUND THAT THE TAILCONE DID NOT DROP DUE TO THE LOWER LEFT LATCH. REPLACED THE LATCH PIN AND RERIGGED THE TAILCONE.SDR DL757952622Radome · delaminatedRADOME WAS ROUTED TO SHOP FOR DELAMINATION, DUE TO LIGHTNING STRIKE. REPAIRED PER SRM 53-10-72.SDR DL757952621Radome · delaminatedHAIL DAMAGE TO TOP HALF OF RADOME. REPAIRED DAMAGE AT SHOP INSPECTION PER SRM 53-10-72.SDR 95ZZZX3679Root Seal · detachedON ROUTINE DAY IFR FLIGHT IN VFR CONDITIONS, A FEW MONTHS AFTER AIRCRAFT HAD BEEN REPAINTED, A LOUD DRUMMING NOISE AND VIBRATION WAS FELT AND HEARD. IT WAS SIMILAR TO WHAT MIGHT BE EXPECTED IF A SEATBELT WAS CAUGHT OUTSIDE THE DOOR IN THE SLIPSTREAM OR WHEN ASDR DL757954014Radome · damagedRADOME CAVED IN DURING DESCENT. SHOP INSPECTION FOUND WHITE AND YELLOW MARKS OF PAINT IN CAVED AREA. THIS AREA SEEMED TO BE HIT. REBUILD RADOME COMPLETE USING 757 MOLD AND BOEING SPEC MATERIAL.SDR 9509329976Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. ADJUSTED BOTH SETS OF CLIPS AND RERIGGSDR DL757953179Radome · damagedRADOME DAMAGED IN NOSE AREA. ON SHOP INSPECTION, FOUND OLD WETLAY UP AND MOISTURE ABOVE LIMITS 40 PERCENT OF SURFACE AREA. REBUILT RADOME FROM BASE RING UP PER S.R.M. 53-10-72 PAINTED AND TESTED, RETURN SERVICABLE UNIT TO STOCK.SDR 9509269915Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK.SDR MWEA95213Latch · failed testDURING ROUTINE INSPECTION, THE TAILCONE LEFT HAND LATCHES DID NOT RELEASE DURING FUNCTIONAL TEST. MAINTENANCE RIGGED TAILCONE RELEASE SYSTEM IAW DOUGLAS MM 53-50-3. OPS CHECKED GOOD, RETURN A/C TO SERVICE.SDR DL757952848Radome · damagedRADOME HAD THREE SMALL HOLES AT 4 O'CLOCK. AFTER INITIAL INSPECTION, FOUND OLD WET LAY-UP AND MOISTURE ABOVE LIMITS. REBUILT RADOME COMPLETE FROM BASE RING UP PER SRM 53-10-72. REPAIRS ACCOMPLISHED AT SHOP VISIT.SDR DL757952842Radome · delaminatedRADOME TEST FOUND DELAMINATION AND MOISTURE ABOVE LIMITS. ALSO, FOUND OLD WET LAY-UPS. RADOME WAS REBUILT, COMPLETE FROM BASE RING UP PER SRM 53-10-72.SDR 9508789880Latches · out of rigDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. RERIGGED THE TAILCONE, CHECKED OK.SDR P5CA9500234Fairing · delaminatedDENTS AND DELAMINATION ON FAIRING PANELS NR 292C, 294A, 291D, 5L AND 6L. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500233Fairing · delaminatedDELAMINATION ON FAIRING PANEL NR 192E. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500232Fairing · dentedDELAMINATION AND DENTS, FAIRING PANELS NR 191H, 191E, AND 191F. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500231Fairings · dentedFAIRING PANELS NR 1 RT AND 292C DENTED. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500185Fairing · delaminatedDELAMINATIONS ON NR 9 LEFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500184Fairing · dentedDENTS NR 5 RIGHT AFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500183Fairing · crackedDENTS AND CRACKS ON FAIRING PANEL 191P. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500182Fairing · dentedSMALL HOLES DENTS AND DELAMINATION ON NR 2 LEFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500181Fairing · damagedHOLES IN INNER SIDE OF FAIRING PANEL NR 191C. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500143Fairing · dentedNR 192C FAIRING PANEL DENTED ON INNER AND OUTER PANELS. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500142Fairing · dentedNR 6 RIGHT UPPER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9500140Fairing · dentedNR 6 RIGHT LOWER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09.
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