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 02FDEA00519Bolt · corrodedTRUNNION MOUNTING LT BOLTS FOUND EMITTING WITH RUST. R&R BOLTS PER MM 32-15-01.Jul 22, 2002 · N616FE · Doug MD11SDR QXEA0201072Rivet · loosePDX- ONE SMOKING RIVET AT AFT WING TO FUSELAGE STRAP/FRAME ON RIGHT HAND UNDERWING. REPAIRED IAW DHC-8 SRM 51-40-11.Jul 20, 2002 · N361PH · Dhav DHC8202SDR 02FDEA00494Stud · shearedSTUD SHEARED AT RIGHT O/B FLAP O/B FWD HINGE HALF AT AFT SPAR ATTACHMENT LWR O/B ATTACH POINT. REMOVED AND REPLACED ALL 4 STUDS AT AFT SPAR IAW 57-41-01-2.Jul 16, 2002 · N301FE · Doug DC1030SDR N6P2002F00000Rivet · failedDURING A ROUTINE 100 HOUR INSPECTION IT WAS DISCOVERED UPON OPENING THE TAIL CONE, THAT TWO RIVETS WERE MISSING IN THE LEFT AND RIGHT BRACKET. THIS BRACKET SUPPORTS THE AFT FUSELAGE, FORWARD OF THE ELEVATOR CONTROL ARM HINGE POINT. EVIDENCE SHOWS THAT THESE RJul 9, 2002 · N27682 · Piper PA31350SDR 2004FA0000622Bolt · 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 Jul 7, 2002 · N8700P · Piper PA24260SDR 2002FA0001098Bolt · corrodedDURING ANNUAL INSPECTION STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS (PN AN175C33A) THAT ATTACHES THE STJul 7, 2002 · N6841P · Piper PA24SDR QXEA0201005Bolt · failedPDX - RIGHT WING TO FUSELAGE ATTACHMENT BOLT FAILED ULTRA SONIC INSPECTION. REPLACED BOTH IAW HORIZON AIR EA 2-57-167.Jul 6, 2002 · N360PH · Dhav DHC8202SDR MALA020418Rivet · corrodedDURING 4K-CHECK IN CWA, RT OUTBOARD FUSELAGE WING BOX RIVET HEADS HAVE LIGHT CORROSION STA 401-STA 475.5. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REFER TO 409 109840. RELEASE DATE 7/17/02Jul 6, 2002 · N112XJ · Saab SF340ASDR 02FDEA00477Bolt · corrodedLEFT WING INBOARD T/E FLAP OUTBOARD HINGE LWR INBOARD BOLT FOUND CORRODED AND RUBBING SCARS ON SHANK.Jul 6, 2002 · N608FE · Doug MD11SDR 02FDEA00476Bolt · corrodedRIGHT WING INBOARD T/E FLAP OUTBOARD HINGE LWR INBOARD BOLT FOUND CORRODED AND RUBBING SCARS ON SHANK.Jul 6, 2002 · N608FE · Doug MD11SDR 02FDEA00461Bolt · corrodedRIGHT WING INBOARD T/E FLAPS OUTBOARD HINGE LWR OUTBOARD BOLT FOUND CORRODED.Jul 5, 2002 · N608FE · Doug MD11SDR 2002FA0001095Bolt · corrodedDURING ANNUAL INSPECTION STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS (PN AN175C33A) THAT ATTACHES THE STJul 1, 2002 · N814RC · Piper PA30SDR 2002FA0001094Bolt · corrodedDURING ANNUAL INSPECTION STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30 AIRCRAFT WITH STABILATOR TORQUE TUB AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS (PN AN175C33A) THAT ATTACHES THE STAJul 1, 2002 · N8030Y · Piper PA30SDR 02FDEA00453Bolt · corrodedRIGHT WING I/B TRAILING EDGE FLAP LOWER O/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER EA 1-5710-64289.Jul 1, 2002 · N583FE · Doug MD11SDR 02FDEA00454Bolt · corrodedRIGHT WING I/B TRAILING EDGE FLAP LWR I/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM 57-51-01-4.Jul 1, 2002 · N583FE · Doug MD11SDR 02FDES00456Bolt · corrodedLEFT WING INBOARD T/E FLAP LWR I/B HINGE BOLT CORRODED.Jul 1, 2002 · N583FE · Doug MD11SDR 02FDEA00455Bolt · corrodedLEFT WING I/B TRAILING EDGE FLAP LWR O/B HINGE BOLT CORRODED. REMOVED AND REPLACED BOLT PER EA 1-5710-64289.Jul 1, 2002 · N583FE · Doug MD11SDR 02FDEA00451Attach Bolt · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE LWR ATTACHMENT BOLT O/B SIDE FOUND CORROSION. REMOVED AND REPLACED BOLT PER MM 57-51-01, REF EA 1-5710-64290.Jul 1, 2002 · N592FE · Doug MD11SDR 02FDEA00450Attach Bolt · corrodedLEFT WING INBOARD FLAP O/B HINGE LOWER ATTACHMENT BOLT INBOARD SIDE FOUND CORRODED. REMOVED AND REPLACED BOLT PER MM 57-51-01.Jul 1, 2002 · N592FE · Doug MD11SDR 02FDEA00452Attach Bolt · corrodedLEFT WING I/B FLAP O/B HINGE LOWER ATTACHMENT BOLT O/B SIDE FOUND CORRODED. REMOVED AND REPLACED HINGE BOLT PER AMM 57-51-01.Jul 1, 2002 · N592FE · Doug MD11SDR MALA020380Fastener · corrodedSEVERAL AREAS AROUND FLT DECK FLOOR SNAP FASTENERS HAVE PITTING CORROSION. REMOVED AND TREATED IAW SRM 51-70-40. PERFORMED REPAIRS IAW SRM 53-60-50.Jun 30, 2002 · N119XJ · Saab SF340ASDR JGV2002F00008Fastener · interferenceRIVET BUCK TAIL INTERFEARENCE WITH CABIN WINDOW FLANGES ON THE PERIMETER OF WINDOW FRAME. WINDOW SEALS CUT AT FACTORY. REPAIRED PER EO DDA0825W342121 REVD. INSTALLED NEW SEALS, ALL CABIN WINDOWS.Jun 28, 2002 · N100GA · Israel ASTRASPXSDR HEEA080211Bolt · corrodedMLG BOLT CORRODED BEYOND LIMITS.Jun 26, 2002 · N467PH · Bell 407SDR SWIA200210959Screw · brokenPASSENGER STOW HANDLE MESSAGE ON EICAS. UNABLE TO CLOSE AND LATCH PASSENGER DOOR. FOUND BROKEN SCREW IN LATCHING MECHANISM. REPLACED SCREW IAW A/C MM 51-11-02. OPS CHECK GOOD.Jun 20, 2002 · N591SW · Cndair CL6002B19SDR 02FDEA00419Fastener · brokenDURING B-CHECK FOUND 1 TAPER LOCK FASTENER BROKEN ON REAR SPAR LOWER CAP OF CENTER WING REF EA 1-5314-64689. R/R FASTENER PER E.A.Jun 18, 2002 · N605FE · Doug MD11SDR AUS20020593Fastener · failed(AUS) RT WING TIP FAIRING CAMLOC FASTENER FAILED AND MIGRATED REARWARDSAND LODGED IN THE OUTBOARD AILERON HINGE CAUSING THE AILERON TO JAM. FOD.Jun 13, 2002 · Bac 146200ASDR DL764020659Bolt · brokenAFTER PUSHBACK WHILE LOWERING FLAPS/SLATS GOT LEADING EDGE SLAT DISAGREE. FOUND BROKEN BOLT FOR PROX SWITCH TARGET AND TARGET MISSING. REINSTALLED SAME.Jun 13, 2002 · N830MH · Boeing 767424ERSDR 02FDEA00405Nut · corrodedRT WING PYLON AFT FITTING BALL JOINT ASSY NUT FOUND WITH GREENISH STAIN. CONFIRMED CORROSION ON 12 JUNE 2002. INSTALLED NEW FITTING ASSY PER AIRBUS S/B A310-54-2021.Jun 12, 2002 · N421FE · Airbus A310SDR GUU2002F00016Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW WITH BEECH MAINTENANCE MANUAL.Jun 11, 2002 · N69549 · Beech 1900DSDR GUU2002F00019Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.Jun 8, 2002 · N69548 · Beech 1900DSDR 2002FA0001100Bolt · corrodedDURING ANNUAL INSPECTION STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS (PN AN175C33A) THAT ATTACHES THE STJun 7, 2002 · Piper PA30SDR GUU2002F00018Bolt · looseAT REDUCED INTERVAL, FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.Jun 7, 2002 · N17534 · Beech 1900DSDR QXEA0200881Rivet · burnedPDX-BETWEEN STATION 527 AND STATION 607 THERE ARE 6 BURNED RIVET HEADS. REPAIRED IAW DHC-8 SRM 51-40-11Jun 7, 2002 · N374PH · Dhav DHC8202SDR GUU2002F00021Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.Jun 6, 2002 · N87552 · Beech 1900DSDR GUU2002F00020Bolt · looseAT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLT REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLT IAW MFG MM.Jun 5, 2002 · N81556 · Beech 1900DSDR 2002F00736Rivet · missingAT C-CHECK, FOUND LEFT ELEVATOR TRAILING EDGE WITH LOOSE AND MISSING RIVETS, AT STATION 125. (M)May 31, 2002 · N7635U · Boeing 727222SDR 02FDEA00376Bolt · shearedNR 3 PYLON FWD WING TO PYLON ATTACHMENT BULKHEAD FOUND 2 EA BOLT SHEARED BELOW LOWER BEARING. R&R WING PER EA 1-5450-62179.May 30, 2002 · N614FE · Doug MD11SDR CA030602003Bolt · 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 TO THE HYDRAULIC PACK WAS TOO SHORT ONLY ONE THREAD WAS SHOWING THROUGH THE ANCHOR NUT. A NEW BOLT WAS INSTALLED AND THE AIRCRAFT WMay 29, 2002 · Bolkms BO105CSDR JJB2002F00001Bolt · bentDURING INSPECTION OF RUDDER CONTROL SYSTEM, FOUND TORQUE TUBE MOUNT BOLTS LOOSE AND CONTROL HORN MOUNT BOLT BENT. PARTS RETURNED TO MFG FOR ANALYSIS, UNIT UNDER INVESTIGATION.May 29, 2002 · N837CA · Beech 1900DSDR P2EA2002M039Bolt · missingRIGHT ENGINE CROSSFEED VALVE HANDLE ON QUADRANT STUCK IN OPEN POSITION. FOUND BOLT AND HARDWARE MISSING ON RIGHT CROSSFEED VALVE TORQUE TUBE ATTACHMENT. REPLACED HARDWARE, OP'S CHECKED GOOD PER MM 36-10-03.May 29, 2002 · N130NJ · Doug DC982SDR AALA20020760Bolt · looseBOS - FLT 509 - EN ROUTE BOS-ORD, AFTER TAKEOFF THERE WAS SMOKE IN THE CABIN, THEN IN COCKPIT. DECLARED EMERGENCY. SMOKE STAYED. RETURNED BOS AND LANDED WITHOUT INCIDENT. TIGHTENED BOLT ON APU MASTER CHIP DETECTOR. PERFORMED COMPLETE PACK BURN. REPLACED May 24, 2002 · N439AA · Doug DC983SDR AUS20020478Fastener · worn(AUS) LOWER ENGINE COWL INNER SKIN HAD A ROW OF TEMPORARY FASTENERS WORKING EXCESSIVELY. MANY RIVETS HOLES ELONGATED.May 23, 2002 · Dhav DHC8102SDR ABXA010900Nut · missingUPON FLAP EXTENSION FOR LANDING, SPLIT FLAPS WERE INDICATED. CONFIRMED BY ROLL TENDENCY. LEFT FLAP WAS APPROXIMATELY 6 DEGREES BEHIND RIGHT FLAP. RIGHT FLAP AT 35 DEGREES, LEFT FLAP AT 29 DEGREES. FOUND LEFT INBOARD FLAP ACTUATOR IDLER ARM TRACK MISSING NUMay 23, 2002 · N816AX · Doug DC863FSDR MALA020304Bolt · looseFUEL LEAK AT RIGHT WING ROOT. MAINTENANCE FOUND LOWER 3 BOLTS ON REAR SPAR ATTACHMENT. REMOVED, CLEANED, RESEALED AND RETORQUED LOWER 3 BOLTS PER BAE REPAIR INST HC536H9077, LEAK CHECK GOOD.May 21, 2002 · N501XJ · Bac AVRO146RJ85ASDR GLBA2002066Screw · loosePAX DOOR MAKING A POPPING SOUND WHEN PRESSURIZING. TIGHTENED CLOSET SCREWS, TEST FLIGHT SATISFACTORY.May 20, 2002 · N260GL · Beech 1900DSDR GUU2002F00000Bolt · looseAT SCHEDULED ROUTINE INSPECTION VERTICAL SPAR SECURITY CHECK ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.May 12, 2002 · N53545 · Beech 1900DSDR DL76K020538Bolt · shearedL/E SLAT ASSM AFTER LANDING. MTC FOUND NR 9 SLAT TRACK TARGET BOLT SHEARED. REPLACED BOLT, BUSHING AND AUX TRACK ARM ROLLER WASHER ASSY IPC 27-81-02-01 SH5 CIRCLE L.May 11, 2002 · N172DZ · Boeing 767332SDR DL76P020536Bolt · shearedON TAXI OUT, GOT L/E ASYMMETRY T/S AND FOUND PROX SENSOR TARGET AT S286 LEFT SLAT NR 5 EXTEND PLATE MISSING AND ATTACH SCREW SHEARED. INSTALLED NEW TARGET AND ATTACHING SCREW. SYSTEM OPS NORMAL.May 10, 2002 · N144DA · Boeing 767332SDR AUS20020453Fastener · misinstalled(AUS) CHERRY RIVETS IN FUSELAGE EMERGENCY EXIT DOOR CUTOUT FRAMEPREVENTING OPERATION OF EMERGENCY EXIT.May 9, 2002 · Cessna 441SDR 2002FA0000616Rivet · looseUNDERSIDE OF WINGS AT WING STATION 209 HAVE LOOSENING RIVETS (CRACKED PAINT AND SMOKING). APPROXIMATELY HALF THE RIVETS SHOW SYMPTOMS.May 9, 2002 · N272SW · Beech B300
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