JASC 5534

Service difficulty reports · 820

Reports filed under 5534 · Vertical Stabilizer Miscellaneous Structure, 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 = '5534'
  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 CA030505007Spar · cracked(CAN) DURING CHANGE OVER TO FLOATS, CRACKS WERE OBSERVED UNDER THE FORWARD ATTACHMENT POINT. NEW SPAR MANUFACTURED. NO PARTS AVAILABLE FROM MANUFACTURE.May 5, 2003 · Dhav DHC6300SDR ASAA0310109Angle · chafedPAE - DURING C-CHECK, FOUND VERTICAL STABILIZER SKATE ANGLE AT BS 1016-1056, RIGHT BUTTOCK LINE 12 CHAFED. REMOVED AND REPLACED SKATE ANGLE PER SRM. (M)Mar 6, 2003 · N744AS · Boeing 737210CSDR AALA20030337Angle · corrodedTUL - FOUND LEFT AND RIGHT VERTICAL STABILIZER L/E FAIRING TO FUSELAGE ATTACH ANGLES CRACKED BEYOND STOP DRILLS. REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES PER AARD 55-30-00-7. (M)Mar 5, 2003 · N251AA · Doug DC982SDR 02FDEA00906Structure · corrodedCORROSION IN FWD TWO VERTICAL BOLT HOLES FOR TENSION TIE COMMON TO VERT STAB. R&R VERTICAL BOLT HOLES PER ER 02-1753.Nov 26, 2002 · N264FE · Boeing 727200SDR 02FDEA00905Fitting · corrodedFRETTING CORROSION UPPER SURFACE OF LUG FOR AFT VERT BOLTS OF TENSION TIE COMMON TO VERT STAB.Nov 20, 2002 · N264FE · Boeing 727200SDR QXEA0201495Plate · gougedPDX - VERT STAB GOUGE IN LADDER PLATE, RIGHT HAND SIDE, LEADING EDGE. REPAIRED IAW DHC-8 RD 8-55-584.Sep 27, 2002 · N368PH · Dhav DHC8202SDR SWAA022217Fitting · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER REAR SPAR LT AND RT DRAG BRACE FITTINGS CORRODED. REPAIRED FITTINGS PER SRM.Sep 25, 2002 · N367SW · Boeing 7373H4SDR SWAA022219Fitting · corrodedDURING SCHEDULE D CHECK, FOUND VERTICAL STABILIZER FAILSAFE LUG FITTINGS CORRODED. REPAIRED FITTINGS PER BFG ER.Sep 23, 2002 · N367SW · Boeing 7373H4SDR SWIA200211016Web · chafedVERTICAL STAB RUDDER TRIM CABLES ARE CHAFING ON WEBBING WHERE CABLES CHANGE DIRECTION TO GO TO THE RUDDER TRIM ACTUATOR. THE WEBBING IS DAMAGED. REPAIRED IAW GST-1980/02 AND SB 120-27-0082.Jun 15, 2002 · N196SW · Emb EMB120ERSDR USAA020251Attach Fitting · corrodedPIT - FOUND FITTING CORRODED, LEFT AFT OUTBOARD VERTICAL STABILIZER ATTACH FITTING. FITTING REPLACED, DRAG ANGLE REPAIR ACCOMPLISHED PER TYPICAL REPAIR 53-80-03. (M)Jun 1, 2002 · N784AU · Boeing 7374B7SDR USA2002F00007Angle · chafedSKATE ANGLE, .5000 CHAFED ANGLE- LOWER LEFT SIDE OF VERT FIN FRONT SPAR. REPLACED SKATE ANGLE.May 8, 2002 · N602AU · Boeing 757225SDR USAA020173Angle · crackedPIT - FOUND DRAG ANGLE CRACKED .5 INCH, SECTION 48, RIGHT SIDE, AFT OF AFT LUGS FOR VERTICAL STABILIZER. FILLERS AND STRAPS INSTALLED ON BOTH SIDES OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M)Apr 18, 2002 · N373US · Boeing 7373B7SDR MWEA020222Angle · crackedVERTICAL STABILIZER LEADING EDGE TAIL TO FUSELAGE DORSAL INTERNAL ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET.Apr 8, 2002 · N206ME · Doug DC932SDR AUS20020405Fitting · corroded(AUS) VERTICAL STABILISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP -LEVEL 2 CORROSION.Mar 23, 2002 · Boeing 727281SDR DHL2002807518Rib · crackedITEM: REF.: N/R 2540 VERTICAL STAB. L/E - INNER RIB CRACKED .500 @ ZFS108.000CORR.: STOP DRILLED CRACK IN VERTICAL STAB. L/E INNER - FABRICATED DOUBLER ( 2024 T3 AL .050)I/A/W SRM55-2-0 FIG. 2 , CLEANED , TREATED AND PRIMED I/A/W SRM 51-1-8B , INSTALLED DOUBLMar 22, 2002 · N807DH · Doug DC873FSDR MALA020226Angle · crackedDURING C-CHECK IN CVG, CRACK ON RT SIDE OF LOWER VERTICAL STABILIZER, LOCATED AT STAB TO FUSELAGE CLOSING ANGLE. REPAIRED IN ACCORDANCE WITH BAE FAX BARA/AVR/5825/02-DC, RIL HC550H9004 ISS 3 AND EO A55013.Mar 18, 2002 · N534XJ · Bac AVRO146RJ85ASDR QXEA0200496Web · crackedPDX - RT REAR FUSELAGE AT VERTICAL STAB IS CRACKED AT WEB AT STRINGER 45. REPAIRED IAW RD 8-55-199.Mar 10, 2002 · N357PH · Dhav DHC8202SDR QXEA0200495Web · crackedPDX - LT REAR FUSELAGE AT VERTICAL STAB IS CRACKED AT WEB. REPAIRED IAW RD 8-55-199.Mar 9, 2002 · N357PH · Dhav DHC8202SDR QXEA0200437Angle · crackedPDX - CRACK ON VERTICAL STAB TO FUSELAGE LT CONNECTION ANGLE INTERMEDIATE SPAR II. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2 AND SRM 51-31-04.Mar 6, 2002 · N480AU · Fokker F28MK4000SDR ZW0A0201301Attach Angle · crackedDURING CHECK-C FWD LT DORSAL FIN ATTACH ANGLE, .5 INCH CRACK WAS FOUND ON UPPER LEG VERIFIED WITH EDDY CURRENT. INSTALLED NEW ATTACH ANGLE PER SRM 51-30-02, 51-30-05, & MO 72R22 & ARA 17951.Jan 28, 2002 · N902TW · Doug DC982
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