JASC 1430

Service difficulty reports · 705

Reports filed under 1430 · Fasteners, 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 = '1430'
  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.

SDR 2003FA0000702Bolt · shearedBYSTANDER POINTED OUT TO PILOT THAT RT MLG HAD FOLDED BACKWARDS. UPON INVESTIGATION IT WAS FOUND THAT ALL 4 STRUT CYLINDER ATTACH BOLTS WERE SHEARED OR MISSING AT THE LOWER SPAR FLANGE ATTACH POINT. AT 100 HR INSPECTION, CONDUCTED 86 HOURS PREVIOUSLY, ALL BOJun 20, 2003 · N8209E · Piper PA28161SDR 03FDEA01039Stud · corrodedLEFT WING - O/B FLAP I/B HINGE UPPER I/B STUD FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-69379 - WINGS - TRAILING EDGE FLAPS - OUTBOARD TRAILING EDGE FLAPS - INBOARD FLAP SUPPORT, UPPER INBOARD STUD BOLT - REPAIR AND INTERIM USE.Jun 17, 2003 · N588FE · Doug MD11SDR DHL2003604751Fastener · shearedLT WING NR 1 ALT TANK FWD LWR PART HI-LOK SHEARED. PERFORMED MAJOR REPAIR IAW BOEING TELEX SEUL-030613 AND SEULIM-03-00019H, FAR FORM 8110-3 DATED JUNE 16, 2003. REMOVED OLD SEALANT IAW EA-04923. CLEANED AND INSPECTED AREA IAW SEULIM-03-00019H, FAA FORM 811Jun 16, 2003 · N604AL · Doug DC873FSDR 2003FA0000665Bolt · shearedRV-8, N9868K, LANDED AND BEGAN ROLLOUT WHEN THE RIGHT MAIN LANDING GEAR ASSEMBLY DEPARTED AIRCRAFT. INVESTIGATION REVEALED THE RIGHT MAIN LANDING GEAR LEG ATTACH BOLT SHEARED/BROKE. FAILED LANDING GEAR PARTS HAVE BEEN SENT FOR ANALYSIS.Jun 15, 2003 · Amtr RV8SDR QXEA200300742Screw · unsecurePDX - LOWER TCAS ANTENNA FORWARD RIGHT HAND NUTPLATE SCREW SPINS. REPAIRED IAW TR 34-0051, TASK 34-43-07-400-801-A01, PARAGRAPH A THROUGH D.Jun 13, 2003 · N608QX · Cndair CL6002C10SDR QXEA200300734Nut Plate · brokenPDX- STRESS PANEL 622AT HAS SPINNING SCREW AND NUTPLATE AT FORWARD OUTBOARD HOLE. REPAIRED IAW DHC-8 Q400 SRM 51-42-05.Jun 13, 2003 · N401QX · Bombdr DHC8401SDR QXEA200300733Nut Plate · brokenPDX- STRESS PANEL 622CT HAS SPINNING SCREW AND NUTPLATE AT AFT ROW, SIX FASTENERS INBOARD FROM AFT OUTBOARD CORNER. REPAIRED IAW DHC-8 Q400 SRM 51-42-05.Jun 13, 2003 · N401QX · Bombdr DHC8401SDR HEEA087477Clamp · twistedWIRE HAS TWISTED CLAMP. SCRAPPED.Jun 12, 2003 · N490PH · Bell 407SDR QXEA200300697Rivet · brokenCKB - RIGHT HAND WING TRAILING EDGE HAS TWO LOOSE RIVETS NEXT TO INBOARD FLIGHT SPOILER AND TWO RIVETS BROKEN OFF ON LOWER SIDE OF FLIGHT SPOILERS. REPAIRED IAW HORIZON AIR EA R-57-37 AND WVAC EO 601R-57-4086.Jun 5, 2003 · N604QX · Cndair CL6002C10SDR 2003FA0000610Mount · debondedON THE NEW C-172 R AND S AIRCRAFT, THE WIRING UNDER THE CABIN FLOOR IS ATTACHED WITH TIE WRAPS TO ADHESIVE BACKED NYLON MOUNTS P/N S2606-1, THAT ARE ADHEARED TO THE AIRCRAFT SKIN. DURING PHASE 3 INSPECTION ON THIS AIRCRAFT WITH 1752.3 HOURS, FOUR MOUNTS WERE Jun 5, 2003 · N567JW · Cessna 172SSDR 2004FA0000612Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE May 28, 2003 · N8660P · Piper PA24260SDR CA030528015Cotter Pin · mismanufactured(CAN) THE COTTER PINS RECIEVED FROM AIRCRAFT PARTS INTERNATIONAL ARE FAULTY AROUND THE HEAD. THE COTTER PINS ARE MANUFACTURED BY WESTERN WIRE. WE RECIEVED THEM IN MARCH 2003. WHEN I CALLED THE SUPPLIER AND EXCHANGED LOT NUMBERS, HE HAD A DIFFERENT LOT NUMBER OMay 28, 2003 · Curtis C46FAIRLIFTSDR CA030602005Bolt · incorrect(CAN) WHILE COMPLYING WITH FLEET CAMPAIGN NOTICE 351-73-20-12 IT WAS FOUND THAT THE BOLT CONNECTING THE TWO NR 2 GOVERNOR CABLES TOO THE HYD PACK WAS TOO SHORT, ONLY ONE THREAD WAS SHOWING THROUGH THE ANCHOR NUT. A NEW BOLT WAS INSTALLED AND THE AIRCRAFT WAS RMay 23, 2003 · Bolkms BO105CSDR CGO2003F00008Bolt · crackedBOLT MAGNAFLUX INSP FOR ROUTINE 5-YEAR INSPECTION IAW MM. BOLT RETURNED AS UNAIRWORTHY DUE TO POSSIBLE CRACK INDICATION IN RADIUS UNDER BOLT HEAD. BOLT WAS INSTALLED NEW AT AIRCRAFT MFG IN RIGHT WING LOWER FORWARD POSITION. MAY POSSIBLY BE DUE TO MFG SURFACMay 21, 2003 · N48GE · Beech A36SDR DL76G030477Nut · crackedINSPECTION OF THE BARREL NUTS FOR THE VERTICAL STABILIZER TO FUSELAGE ATTACHMENT REVEALED CRACKED SEALANT AT ONE NUT LOCATION ON THE LT SIDE AT FS 1654. SINCE THIS IS INDICATIVE OF A POSSIBLE POOR TORQUE CONDITION, THE NUT AND BOLT WERE REPLACED PER ER/A 3850May 19, 2003 · N1501P · Boeing 7673P6SDR QXEA0300642Rivet · damagedRIVET DAMAGED AT FS 953, 2 INCHES ABOVE STRINGER 12R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300641Rivet · damagedRIVET DAMAGED ON STRINGER 11R, 4 INCHES FORWARD OF FS 893. REPAIRED IAW SRM 51-25-16. PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300640Rivet · damagedRIVET DAMAGED AT FS 830.4, 2 INCHES ABOVE STRINGER 10R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300639Rivet · damagedRIVET DAMAGED AT STRINGER 9R, 5 INCHES AFT OF FS 797. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300638Rivet · damagedRIVET DAMAGED AT STRINGER 8R, 4.5 INCHES AFT OF FS 724.08. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-46-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300637Rivet · damagedRIVET DAMAGED AT FS693, 4 INCHES BELOW STRINGER 8R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-03, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300636Rivet · damagedRIVET DAMAGED AT STRINGER 8R, 7 INCHES AFT OF FS645. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-03 PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300634Fastener · damagedFASTENER DAMAGED, 3 INCHES FORWARD OF FS597 AND 2 INCHES ABOVE STRINGER 10R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-20, PG 13-22.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300633Fastener · damagedFASTENER DAMAGED AT 4 INCHES AFT OF FS549 AND 7 INCHES ABOVE STRINGER 12R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-20, PG 13-22.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300632Rivet · damagedRIVET DAMAGED AT STRINGER 12R, 4 INCHES FORWARD OF FS533. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300631Rivet · damagedRIVET DAMAGED AT STRINGER 13R, 1 INCH AFT OF FS501. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300630Rivet · damagedRIVET DAMAGED AT FS469, 3 INCHES ABOVE STRINGER 14R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300629Rivet · damagedRIVET DAMAGED AT FS421, 2 INCHES BELOW STRINGER 14R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300628Rivet · damagedRIVET DAMAGED AT FS 409, 2 INCHES ABOVE STRINGER 15R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300627Rivet · damagedRIVET DAMAGED AT FS 394, 1 INCH ABOVE STRINGER 15R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300626Rivet · damagedRIVET DAMAGED AT STRINGER 15R, 3 INCHES AFT OF FS379. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300625Rivet · damagedPDX-RIVET DAMAGED AT FS 364, 3 INCHES ABOVE STRINGER 17R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300624Rivet · damagedRIVET DAMAGED AT FS295, 2 INCHES BELOW STRINGER 18R. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300622Rivet · damagedRIVET DAMAGED AT STRINGER 18R, 6 INCHES AFT OF FS 235. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300620Rivet · damagedRIVET DAMAGED AT .5 INCHES BELOW BOTTOM EDGE OF ADG DOOR, 15INCHES AFT OF FS169. REPAIRED IAW SRM 51-25-16, PG 7 AND SRM 51-42-06, PG 1-8.May 17, 2003 · N600QX · Cndair CL6002C10SDR QXEA0300575Rivet · damagedPDX- DAMAGED RIVET ON STRINGER 9R ONE INCH AFT OF FUSELAGE 409.00 ABOVE RIGHT HAND WINDOW 2. REPAIRED IAW HORIZON AIR EA R-53-106, REO 670-53-00-036, CRJ SRM 51-25-16 AND 51-12-00.May 15, 2003 · N614QX · Cndair CL6002C10SDR QXEA0300574Rivet · damagedPDX- DAMAGED RIVET 10 INCHES AFT OF FIRST OFFICERS SIDE WINDOW ON STRINGER 11AR. REPAIRED IAW HORIZON AIR EA R-53-106 AND REO 670-53-00-036.May 15, 2003 · N614QX · Cndair CL6002C10SDR QXEA0300567Rivet · damagedPDX-DAMAGED RIVET AT STATION 613.00 TWO INCHES BELOW STRINGER 6R ON RIGHT HAND SIDE ABOVE WINDOW 9. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16.May 15, 2003 · N614QX · Cndair CL6002C10SDR QXEA200300583Rivet · loosePDX - LOOSE RIVET ON LT HAND WING, OUTBOARD OF THE OUTBOARD SPOILER. REPAIRED IAW CRJ-700 SRM 51-42-06, PAGES 1-18.May 7, 2003 · N603QX · Cndair CL6002C10SDR USAA030147Nut Plate · corrodedPIT - FOUND NUTPLATE CORRODED .75 INCH BY 1 INCH AREA, FS 727A-727B 21 LT. INSTALLED DOUBLER PER SRM 53-00-3. CORROSION LEVEL 1, TASK NR C53-107-01. (M)May 1, 2003 · N560AU · Boeing 737301SDR QXEA0300522Rivet · missingCKB - UPPER AFT RIGHT WING HAS A RIVET MISSING AT WS 170.83. REPAIRED IAW DRJ 700 SRM 51-42-06.Apr 26, 2003 · N606QX · Cndair CL6002C10SDR 2003FA0000993Fastener · undertorquedAIRCRAFT OWNER REQURESTED THAT WE CHECK TORQUE ON BOLTS SECURING VERTICAL FIN TO TAILCONE BULKHEAD. FOUND ALL VERTICAL FIN ATTACH HARDWARE UNDER TORQUED. INSPECTED HARDWARE AND MOUNTING HOLES. FOUND NOT PERFECT. REINSTALLED BOLTS AND TORQUED TO MFG SPECIFIApr 18, 2003 · N134FC · Piper PA28181SDR QXEA0300488Fastener · gougedPDX - PANEL 622AT HAS TWO GOUGES IN TWO INBOARD FASTENERS ON RIGHT WING. REPAIRED IAW HORIZON AIR EA 6-57-134 AND RD-8/4-57-162Apr 17, 2003 · N407QX · Bombdr DHC8401SDR CTU2003F00004Bolt · bentAFTER FAILURE OF BOLT PRIOR TO FLIGHT OPERATOR CHOSE TO PERFORM INSPECTION OF OTHER 340 AIRCRAFT IN FLEET. BOLT MUST BE REMOVED FOR INSPECTION. THIS BOLT IS THE ELEVATOR BOLT, CRANK PIVOT BOLT. IT ALSO HAS A BEARING WHICH IS SOMETIMES WORN AS WELL.Apr 10, 2003 · N340FR · Cessna 340ASDR CTU2003F00003Bolt · bent(NOTE: SUBMITTER HAS SEVERAL AIRCRAFT OF SAME MAKE AND MODEL). AFTER FAILURE OF BOLT PRIOR TO FLIGHT MAINTENANCE FACILITY PERFORMED INSPECTION OF BOLT WHICH THE ELEVATOR BELLCRANK ROTATES ON. BOLT HAVE BEEN STRESSED AND BENT. MFG SHOULD HAVE BOLT OF LARGERApr 10, 2003 · N812V · Cessna 340CESSNASDR 2003FA0000368Bolt · undertorquedDURING ANNUAL INSPECTION FOUND VERTICAL FIN LOOSE. UPON CHECKING ATTACHMENT HARDWARE, FOUND THE FOUR BOLTS AT THE REAR SPAR TO BE INSUFFICIENTLY TORQUED. THE SINGLE BOLT AT THE FRONT SPAR WAS TIGHT BUT WOULD NOT PREVENT SIDE TO SIDE MOVEMENT OF THE FIN(APPROX.Apr 8, 2003 · N137FC · Piper PA28181SDR SWAA030764Fastener · looseDURING SCHEDULED C 2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING FASTENER LOOSE. SECURED FASTENER PER SRM.Apr 5, 2003 · N425LV · Boeing 7377H4SDR CA030404002Bolt · sheared(CAN) CENTER NOSE GEAR DRAG LINK BOLT FOUND SHEARED BUT STILL IN PLACE DURING 100 HR. INSPECTION.Apr 4, 2003 · Piper PA44180SDR 2003FA0000798Bolt · improper partTHE PROPELLER MOUNTING BOLTS ON NEW AC MODEL SEEM TO BE TOO SHORT. THEY DO NOT EXTRUDE AT ALL THRU THE CRANKSHAFT PRESSED THREADED BUSHINGS. USUALLY THE THREADS WILL EXTRUDE 2-3 THREADS THRU THE BUSHING. RECOMMENDATION IS TO HAVE A LONGER BOLT INSTALLED SO Apr 3, 2003 · N397SP · Cessna 172SSDR SWAA030743Rivet · looseDURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR HOOK ATTACH RIVET SHEARED. INSTALLED RIVET PER SRM.Apr 3, 2003 · N382SW · Boeing 7373H4
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