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 2004FA0000605Bolt · crackedDURING INSPECTION FOUND NOSE GEAR TORQUE LINK BOLT PN NAS464P4-27 SHEARED MID SPAN OF BOLT SHANK. NO SIGN OF EXCESSIVE CORROSION.Jul 29, 2004 · N2163N · Piper PA44180SDR 04FDEA02271Barrel Nut · corrodedRIGHT HAND NR 10 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79818, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING S/B MD-11, 55-023 REVISION 2 AND FEDEXJul 28, 2004 · N613FE · Doug MD11SDR 04FDEA02269Barrel Nut · corrodedLEFT HAND NR 27 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79810, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EJul 28, 2004 · N613FE · Doug MD11SDR 04FDEA02268Barrel Nut · corrodedLEFT HAND NR 29 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79809, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EJul 28, 2004 · N613FE · Doug MD11SDR 2004UALA00752Connector · inoperativeSEAT 52 HJK EMERGENCY LIGHT OUT. REPAIRED CONNECTOR.Jul 27, 2004 · N121UA · Boeing 747422SDR ASOA04527Bolt · missingFLT 4474 - DURING A GROUND INSPECTION IN TYS, THE PASSENGER DOOR WAS VERY HARD TO OPEN AND THE UPPER LEFT LOCKING PIN WOULD NOT ENGAGE. MAINTENANCE FOUND THE BOLT, WASHER AND NUT P/N NT113544CM, ON THE UPPER AFT LOCKING PIN CONNECTION ROD TO THE BELL CRANK MIJul 25, 2004 · N637AS · Aerosp ATR72212SDR 2005FA0000082Bolt · mismanufacturedTHE CONNECTING ROD BOLT, PN SL12596, LOT NR 575765, WAS FOUND TOO SHORT FOR PROPER INSTALLATION. THE FREE LENGTH OF THE BOLTS IN QUESTION WERE 2.2485 TO 2.2491. MFG SL1458B REQUIRES A TWO STEP TORQUE PROCESS. FIRST, TORQUE BOLTS TO 35 FT LBS AND MEASURE, IFJul 22, 2004SDR UAT2004F00000Nut · crackedREMOVED WING STRUTS TO REBUILD WINGS AND FOUND TWO CRACKED NUTS ON ONE WING STRUT. 5 EA NAS464P5A27 BOLTS HOLD THE STRUT FITTINGS IN EACH END OF THE WING STRUTS AND THESE NUTS HOLD THE BOLTS IN. THERE ARE ONE THICK AND ONE THIN WASHER ON EACH BOLT IAW IPC. Jul 22, 2004 · N9736M · Cessna 207ASDR CA040722001Bolt · shearedDURING THE DAILY INSPECTION, IT WAS DETECTED THE TOP BOLT IN THE NOSE GEAR SCISSOR LINK WAS SHEARED. THE GEAR WAS INSPECTED AND NO DEFECTS NOTED. THE BOLT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (HAVE SEEN THIS ONCE BEFORE ON ANOTHER TWIN OTTER ABJul 21, 2004 · Dhav DHC6300SDR 2004FA0000607Nut · splitWHILE CLEANING AIRCRAFT DISCOVERED NR 4 MAIN WHEEL 1 EACH TIE-BOLT NUT SPLIT IN HALF. REPLACED ALL WHEEL TIE BOLTS P/N: EWB22-5-16 AND NUTS P/N: FN22A524 WITH NEW PARTS. TIME ON PART SINCE REPAIR UNKNOWN.Jul 21, 2004 · N91HK · Raythn HAWKER800XPSDR CA040722002Bolt · shearedWHEN THIRD PARTY AMO WAS INSPECTING THE FWD STABILIZER FITTINGS ATTACHED TO THE AFT SPAR FOR SB737-57A1266 ON A/C 743 FOUND THE O/B FITTING CRACKED. ON FURTHER INVESTIGATION, FOUND THAT ALL FOUR BOLT HEADS ON THE AFT O/B FITTING WERE SHEARED OFF, AND THE FITTJul 19, 2004 · Boeing 737204SDR A6WA200460025Bolt · corrodedFOUND CORROSION ELEVATOR HINGE A-FRAME ATTACHMENT BOLTS TWO EACH. REPLACED NEW. (M)Jul 17, 2004 · N607AW · Bac 146200ASDR CA040715006Bolt · broken(CAN) DURING INSPECTION, AN OIL LEAK WAS DISCOVERED ON THE RT ENGINE CYLINDER POSITION NR 2. UPON INVESTIGATION AND RECTIFICATION, THE MAINTENANCE CREW WAS ATTEMPTING TO REPLACE THE O-RINGS ON THE EXHAUST ROCKER ARM RETAINING BOLT. THE RETAINING NUT AND COTTEJul 15, 2004 · Gruman FIRECATSDR 2004FA0000580Bolt · missingWHILE MAKING A APPROACH TO THE AIRPORT FOR LANDING, THE PILOT ADDED POWER WITH NO ENGINE RESPONSE. THE THROTTLE CABLE DISCONNECTED FROM THE ENGINE CONTROL ARM DUE TO THE THROTTLE ATTACHING BOLT MISSING ALONG WITH THE WASHER, NUT AND COTTER PIN. THROTTLE WORKEDJul 14, 2004 · N2KD · Cessna T210JSDR CA040720006Screw · separatedTHESE TWO BOLTS HOLD THE FUEL PUMP IDLER GEAR SHAFT TO THE ACCESSORY HOUSING. FAILURE OF THE BOLTS ALLOWED THE IDLER GEAR AND SHAFT TO DROP TO THE BOTTOM OF THE ACCESSORY CASE. THE FUEL PUMP STOPPED TURNING AND THE ENGINE QUIT. ENGINE RESTARTED, USING ELECTJul 12, 2004 · Piper PA31SDR UPS04442833Bolt · corrodedINSPECTION TYPE:C, LT WING CENTER SECTION REAR SPAR WEB AT BS 1241 BULKHEAD FITTING CORROSION REVEALED BETWEEN BOLT NR 7, 8 AND 9. THICKNESS CHECK PER NTM PART 4,57-10-19 RESULT: NR 7 HOLE 0.335 INCH, NR 8 HOLE 0.350 INCH, NR 9 HOLE 0.370 INCH. NR 7, 8 & 9 Jul 9, 2004 · N522UP · Boeing 747200SDR ALGA096033Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120BSDR ALGA096032Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120BSDR ALGA096031Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120BSDR ALGA096030Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120BSDR ALGA096028Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120BSDR ALGA096029Bolt · corrodedBOLT PITTED. REPLACED BY FIELD MAINT.Jul 8, 2004 · N513AL · Urocop EC120BSDR CA040722007Lock Tab · missingON THE FOLLOWING CESSNA AIRCRAFTS, FOUND THE LOCK TABS FOR ENGINE MOUNT BOLTS TO BE EITHER MISSING, BROKEN, OR INCORRECT HARDWARE USED TO REPLACE THEM. C-205 IO470C-180 I0470C-182 IO470C-185 IO520C-206 IO550 WOULD LIKE TO NOTIFY ALL AIRCRAFT OWNERS THAT UJul 2, 2004SDR 151AW0023Bolt · looseFOUND 7 RUDDER FLANGE BOLTS LOOSE. TORQUED AND REPLACED BOLTS AS REQUIRED PER SB 737-55A1087.Jul 2, 2004 · N151AW · Boeing 7373G7SDR CA040713004Bolt · worn(CAN) DURING SCHEDULED INSPECTION RT ELEVATOR FOUND SLIGHTLY LOOSE AT TORQUE TUBE. NUT COULD NOT BE TIGHTENED DUE TO EXCESSIVELY WORN BOLT AW4-6. BOLT REPLACED AND NUT AN320-4. ELEVATORS MUST BE REMOVED EVERY 400 HOURS TO ACCOMPLISH AD 80-25. REPEATED REMOJun 30, 2004 · Dhav DHC2MK1SDR CSA2004F00000Bolt · wornPILOT RADIOED THAT LT MLG SAFE LIGHT WOULD NOT COME ON, VERIFIED BULB FUNCTION, OK. VERIFIED GEAR FULLY EXTENDED DURING FLY-BY BEFORE LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT STOPPED ON RUNWAY. PILOT REPORT GEAR SAFE LIGHT CAME ON AT TOUCHDOWN. Jun 28, 2004 · N3516A · Piper PA31350SDR 513NA0008Bolt · missingDURING WALK-AROUND, FOUND NR 7 MAIN WHEEL ASSEMBLY TIE BOLT MISSING. REPLACED NR 7 MAIN WHEEL ASSEMBLY PER MM 32-45-01.Jun 28, 2004 · N513NA · Boeing 7572T7SDR QXEA200400477Nut Plate · strippedPDX - FUSELAGE PANEL 121AL HAS 3 STRIPPED OUT NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES IAW DHC-8 SRM.Jun 28, 2004 · N363PH · Dhav DHC8202SDR QXEA200400478Nut Plate · strippedPDX - FUSELAGE PANEL 122AR HAS 2 STRIPPED OUT NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES IAW THE DHC-8 SRM.Jun 28, 2004 · N363PH · Dhav DHC8202SDR CA040902005Bolt · sheared(CAN) BOLT SHEARED ON TAKEOFF. THIS IS BOLT FROM OTHER GEAR HAS SAME TOTAL TIME.Jun 25, 2004 · Piper PA28161SDR BAQA095539Bolt · unserviceableMAIN ROTOR BLADE BOLT WERE MANUFACTURED WITH THE CENTER HOLE TO SMALL TO ACCEPT WASHER P/N 117-181001.02.Jun 23, 2004 · N587MC · Bolkms BK117A4SDR DL757040594Bolt · shearedAFTER DEPARTURE RECEVED LT HYDRAULIC QTY MESSAGE, QTY INDICATED ZERO, LT ENGINE HYDRAULIC PRESSURE 60 PSI. ELECTRIC / HYDRAULIC USED ALT FLAPS ALT GEAR EXT O/W, LANDING LAX NO NOSE STEERING. COOLED BRAKE TEMP SHOWED ALL O,S. FOUND DUAL BRAKE METERING VALVE Jun 23, 2004 · N611DL · Boeing 757232SDR 2004FA0000535Bolt · shearedAIRCRAFT WAS LOADED WITH 1600LBS OF FERTILIZER AND WAS TAKING OFF TO THE SOUTH ON A DIRT RUNWAY. PILOT WAS APPROACHING 65 MPH, WHEN THE RT MAIN WHEEL AND TIRE SEPARATED FROM THE AIRCRAFT. PROPELLER STRUCK THE GROUND SEVERAL TIMES, CAUSING THE AIRCRAFT TO FLIJun 23, 2004 · N6567 · Scwzer G164ASDR CA040623001Nut · loose(CAN) DURING A ROUTINE INSPECTION THE JAM NUTS THAT SECURE THE PROP CONTROL CABLE TO AN ATTACHMENT BRACKET AT THE PROP GOVERNOR WERE FOUND LOOSE. THE LOWER JAM NUT HAD BACKED OFF COMPLETELY AND THE CABLE WAS FREE TO MOVE, BUT IN ONE DIRECTION ONLY. THE CONTROJun 21, 2004 · Found FBA2CSDR ABXA040249Bolt · shearedWHILE ACCOMPLISHING INSPECTION OF AD2001-19-04, FOUND 1 VERTICAL STAB ATTACH BOLT SHEARED AT FS 1654 LEFT SIDE. REMOVED AND REPLACED ALL 16 VERTICAL ATTACH BOLTS AND NUTS IAW ABX EA 53420014-001.Jun 17, 2004 · N767AX · Boeing 767281SDR DL73S040579Bolt · damagedYOKE FAILED TO RETURN TO NEUTRAL AFTER DEFLECTION. REPLACED BOLT IN ELEVATOR FEEL AND CENTERING OUTPUT ROD.Jun 17, 2004 · N324DL · Boeing 737232SDR T4C2004F00001Screw · brokenTHIS AIRCRAFT WAS STOPPED, WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION A BOLT NAS 464P4-26 AND ADJUSTING SCREW 0841113-1 WERE BROKEN. NOT SURE WHICH BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOUJun 14, 2004 · N567RS · Cessna 402BSDR T4C2004F00000Bolt · brokenTHIS AIRCRAFT WAS STOPPED WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION, A BOLT NAS464P4-26 AND ADJUSTING SCREW 0841113-1 WERE BROKEN. UNSURE WHICH WAS BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOJun 14, 2004 · N567RS · Cessna 402BSDR USAABB04051Nut · burnedCLT - WHILE ACCOMPLISHING A B-CHECK MAINTENANCE VISIT AN AREA OF DISCOLORATION ON THE CARGO LOADING JACKSCREW PAN OF THE AFT CARGO COMPARTMENT APPROXIMATELY 12-18 INCHES AFT OF THE FORWARD CARGO BULKHEAD WAS NOTED. FURTHER INVESTIGATION FOUND EVIDENCE OF A FIJun 14, 2004 · N624AU · Boeing 7572B7SDR C8GA20040006Bolt · mislocatedON WALK AROUND IN KDEN, FOUND THE LT MAIN GEAR BOLT DOWNLOCK LINK PIVOT IMPROPERLY INSTALLED AS PER BOEING IPC 32-10-01-04. A SPECIAL MAINTENANCE FERRY FLIGHT WAS ISSUED ON 6-14-2004 FROM KDEN TO KTOL. PRIOR TO FLIGHT, A VISUAL INSPECTION WAS PERFORMED IN THJun 13, 2004 · N286SC · Boeing 7272A1SDR 400AC0401Bolt · failedPILOT REPORTED VIBRATION ON LANDING. INSP REVEALED THE LT MAIN GEAR TORQUE LINK PIVOT BOLT, MISSING. THE BOLT COULD NOT BE FOUND TO DETERMINE THE CAUSE. SUSPECT EITHER A FAILURE OF THE BOLT OR FAILURE OF THE SAFETY FEATURE TO PREVENT THE BOLT FALLING OUT. Jun 10, 2004 · N400AC · Beech B100SDR QXEA200400398Rivet · damagedPDX - THERE ARE THREE SMOKING RIVETS ON AFT RUDDER LOWER LEFT SIDE. REPAIRED IAW DHC8 SRM 51-40-00.Jun 7, 2004 · N362PH · Dhav DHC8202SDR CA040623006Bolt · seized(CAN) PILOT REPORTED MAIN PASSENGER DOOR DIFFICULT TO OPEN FROM OUTSIDE, HAD TO ENTER FROM SERVICE DOOR TO ACCESS AIRCRAFT. TRIED TO OPEN DOOR AND HANDLE WAS DIFFICULT TO TURN. MAINTENANCE FOUND AIRSTAIR PIVOT FITTING ASSEMBLY WAS SEIZED. UPON DISMANTLING THJun 4, 2004 · Cndair CL6002B19SDR QXEA200400389Nut Plate · damagedPDX - A NUT PLATE ON PANEL 121BL SPINS, BOTTOM ROW, MIDDLE NUT PLATE. MAINTENANCE REMOVED AND REPLACED THE NU00177T PLATE IAW-200 SRM.May 28, 2004 · N365PH · Dhav DHC8202SDR QXEA200400377Nut Plate · brokenPANEL 122AR ON RT FORWARD FUSELAGE HAS TWO BAD NUTPLATES. REMOVED AND REPLACED NUTPLATES IAW DHC-8 SRM 51-40-11.May 27, 2004 · N354PH · Dhav DHC8202SDR AUS20040494Bolt · sheared(AUS) RT MAIN LANDING GEAR OB STABILIZING FITTING OB LOWER ATTACHMENT BOLT SHEARED ALONG THE SHANK IN AN AREA COINCIDING WITH THE WING REAR SPAR.May 26, 2004 · Boeing 737376SDR LR7A04061Rivet · looseDURING SCHEDULED B3 INSPECTION IAW SB 382-53-42 FOUND APPROX 400 EA LOOSE FASTENERS AT FS 245 AND FS 345E FUSELAGE SKIN. REPLACED RIVETS IAW SRM SMP 583 51-70 AND SB 382-53-42. NR 02SB382-53-42.May 26, 2004 · N401LC · Lkheed 382GSDR AUS20040455Bolt · cracked(AUS) UNDERCARRIAGE SADDLE BOLT CRACKED.May 24, 2004 · Cessna U206GSDR ASMF200405025Fastener · lightning strikeDURING TRANSIT CHECK, A LIGHTING STRIKE WAS DETECTED ON THE FUSELAGE LT SIDE, FORWARD OF THE WING WITH SOME FASTENERS DAMAGED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT. FASTENERS WERE REPLACED IAW MM 43-04 FIG 38 TABLE B CONDITION May 24, 2004 · N216AM · Doug DC987SDR QXEA200400360Rivet · loosePDX-AFT CARGO DOOR SKIN HAS NUMEROUS RIVETS SHOWING WORK TRAILS AND MISSING PAINT INDICATING RIVET MOVEMENT. REPAIRED IAW D-8 200 SRM 51-40-11.May 24, 2004 · N360PH · Dhav DHC8202
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