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 DALA1121730960Plate · corrodedPLATES RUSTED ON OUTBD SIDE OF LT STAB OUTBD ATTACH LUG AT TOP OF VERT STAB. REPLACED PLATES PER EA 09-073278-12 AD REV G.Mar 16, 2011 · N960DL · Doug MD88SDR ASAA1149284Beam · crackedVERTICAL STABILIZER TRAILING EDGE BEAM CRACKED LEFT SIDE. REMOVED AND REPLACED BEAM IAW B737 400 SRM 51 40 02 AND 51 40 05.Mar 3, 2011 · N765AS · Boeing 7374Q8SDR ASAA1149234Skate Angle · chafedVERTICAL STABILIZER LT FORWARD SKATE ANGLE CHAFED. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.Feb 24, 2011 · N706AS · Boeing 737490SDR ASAA1149232Skate Angle · chafedVERTICAL STABILIZER RT FORWARD SKATE ANGLE CHAFED. REMOVED ANGLE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.Feb 24, 2011 · N706AS · Boeing 737490SDR GLBA20110215FStructure · crackedDURING A SCHEDULED ROUNTINE INSP MX, FOUND THE RT STABILON HAS A .5" HOLE 9" FROM T/E CORNER, CRACK RADIATED FROM INBD EDGE OF HOLE 1" IN LENGTH. MAINTENANCE COULD NOT REPAIR RT STABILON, REPLACED RT STABILON IAW BMM 55-10-01-201, NO RII REQUIRED FOR INSTALLAFeb 15, 2011 · N178YV · Beech 1900DSDR GLBA20110214GStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX THE RT STABILON WAS DAMAGED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-55-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 12, 2011 · N218YV · Beech 1900DSDR DALA1119279223Angle · crackedINNER DORSAL FIN JOINT ANGLE RT FOUND CRACKED / DAMAGED ANGLE WAS REPLACED REF SRM 51-10-05, 51-30-02 AND 51-30-05. FUSELAGE SKIN CRACK FOUND AT STA 1475 DAMAGED AREA WAS CUT OUT AND REPAIR INSTALLED PER ERA 487464-14AD REF N/R S/N 499893.Jan 10, 2011 · N923DN · Doug MD9030SDR SWAA110076Fitting · corrodedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER RT SIDE FITTING CORRODED AT STA 1088. REMOVED AND REPLACED FITTING PER EA.Jan 9, 2011 · N520SW · Boeing 7375H4SDR SWAA110075Fitting · corrodedDURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER LT SIDE FITTING CORRODED AT STA 1088. REMOVED AND REPLACED FITTING PER EA.Jan 9, 2011 · N520SW · Boeing 7375H4SDR FDEA201101060054Profile · corrodedRT VERTICAL STABILIZER T/E HORIZ PANEL LANDING SUPPORT STRAP BETWEEN RIBS 21-22 HAS 8 INCH CORROSION IN AND AROUND 3 EA FASTENERS AND ALONG UPPER INTERIOR MATING SURFACE. R & R EDGE PROFILE RT VERT STAB T/E PANEL LANDING BETWEEN RIBS 21 AND 22 IAW SRM 51-72Jan 6, 2011 · N423FE · Airbus A310203SDR FDEA201101060024Stiffener · corrodedVERTICAL STABILIZER INTERIOR REAR SPAR HORIZ STIFFENER BETWEEN RIB 9 AND RIB 10 HAS CORROSION ABOUT 3 SQ INCHES. REMOVED HORIZ STIFFNER AND DIAGONAL STIFFNER BETWEEN RIB 9 AND 10 AT VERT STAB REAR SPAR. REMOVED CORROSION ON HORIZ STIFFNER, NOMINAL 0.050, REJan 6, 2011 · N443FE · Airbus A310203SDR ASAA1148985Skate Angle · chafedVERT STAB LT FWD SKATE ANGLE CHAFED. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 30 01 FIG 7 & 51 40 02.Jan 2, 2011 · N764AS · Boeing 7374Q8SDR FDEA201012034556Support Angle · crackedVERTICAL STAB INTERIOR AT BS 1343 HAS CRACK INDICATION ON RT UPPER WEB SUPPORT ANGLE, UNDERNEATH. REMOVED CRACKED SHEAR TIE. FABRICATED NEW SHEAR TIE USING 2024T-3 .050 DIMS 7 1/8" X 3 3/4" AND INSTALLED IAW SRM 51-20-1, SRM 55-30-2 AND SRM 51-30-2.Dec 3, 2010 · N233FE · Boeing 727247SDR CALA2010120600605Tee Fitting · damagedVERTICAL STABILIZER FRONT SPAR RT TEE CHORD DAMAGE REF L/P 8681063 FOR BIRD STRIKE. REPAIRED CHORD DAMAGE REF INTERIM REPAIR EC/RA 5530-01604 AND FORM 44.0008 FOR PARTIAL WORK PERFORMED. PLACED ON DIP TO ACCOMPLISH VISUAL INSP OF BLIND FASTENERS PER PART 2 ODec 3, 2010 · N17627 · Boeing 737524SDR SWAA107046Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT LUG FACES CORRODED AT BS 1016. REPAIRED FITTING PER EA.Nov 15, 2010 · N514SW · Boeing 7375H4SDR SWAA107045Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT LUG FACES CORRODED AT BS 1016. REPAIRED FITTING PER EA.Nov 15, 2010 · N514SW · Boeing 7375H4SDR SWAA107023Fitting · corrodedDURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT AFT SPAR O/B FIN FITTING CORRODED. REMOVED AND REPLACED FITTING PER EA.Nov 15, 2010 · N514SW · Boeing 7375H4SDR USAA2010111592607Beam · crackedCLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER T/E BEAM CRACKED AT STATION 90. REPAIRED VERTICAL STABILIZER T/E BEAM AT STATION 90 IAW EA 102285.Oct 28, 2010 · N940UW · Boeing 7572B7SDR SWAA106437Bushing · corrodedDURING SCHEDULED SPV CHECK, FOUND VERTICAL FIN LT PRIMARY LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BAC DWG.Oct 18, 2010 · N686SW · Boeing 737317SDR DALA1157579229Structure · crackedSTA 1475 L3LT-L3RT DORSAL FIN REPAIRED IAW BNI-BNI-10-0069-09B 8100-9 RECEIVED 09/23/2011___(TO 85.Oct 7, 2010 · N929DN · Doug MD9030SDR AALA20100923TUL03Attach Angle · crackedDORSAL FIN ANGLE CRACKED RIGHT SIDE 6 INCH AFT OF FORWARD ACCESS OPENING. REPLACED DORSAL FIN ATTACH ANGLE RIGHT SIDE PER AARD 55-30-00-7.Sep 23, 2010 · N7550 · Doug DC982SDR USAA2010092292072Drag Angle · crackedMIA - C20 - MAJOR REPAIR - CRACK ON LEFT AFT VERTICAL STABILIZER ATTACH FITTING DRAG ANGLE AT BS 1016, VERT FIN STA 0. REPAIRED LEFT AFT VERTICAL STABILIZER ATTACH FITTING DRAG ANGLE AT BS 1016, VERT FIN STA 0 IAW TYPICAL REPAIR 53-80-30.Sep 22, 2010 · N334AW · Boeing 7373Y0SDR SIMA201022401Structure · damagedDURING THE MAINTENANCE BASE VISIT FOUND THAT THE RIGHT VERTICAL STABILIZER HAS A MISDRILLED HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE REPAIR WAS MADE TO THE MIS-DRILLED HOLE, SATISFACTORILY ACCOMPLISHED PER EO EM-55MR-332. THE AIRCRAFT WAS RETURNED TAug 11, 2010 · N643AE · Emb EMB145LRSDR FDEA201008022773Support Angle · corrodedDORSAL FIN RT SIDE FWD SUPPORT ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398197220100 IAW SRM 51-74-10 AND 51-40-21, FIG 9, PARA 7, PG 24.Aug 2, 2010 · N417FE · Airbus A310222SDR FDEA201008022772Support Angle · corrodedDORSAL FIN, RT SIDE SUPPORT SPLICE ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398192920100 IAW SRM 51-74-10, AND 51-40-21, FIG 9, PARA 7, PG 24.Aug 2, 2010 · N417FE · Airbus A310222SDR USAA2010080291564Bolt · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON BOLT RT FWD ATTACH FITTING OF VERTICAL STABILIZER. REPLACED BOLT AT RIGHT FORWARD ATTACH FITTING OF VERTICAL STABILIZER IAW B737 AMM 55-30-00.Jul 30, 2010 · N530AU · Boeing 7373B7SDR C2XA10SH241Fitting · wornSHV - DURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 AT 12:00 POSITION WAS FOUND TO HAVE ELONGATED BOLT HOLES AND CAUSING FRETTING WITH ADJACENT SKIN PANELS. MAINTENANCE PERFORMED REPAIRS TO THAT AREA IAW EC5310-01317 AND EC5310-01521. THE AIRCRAJul 20, 2010 · N13969 · Emb EMB145LRSDR DALA1017089001Stiffener · crackedHMV3 VERT STAB LOWER L/E INTERIOR RT SIDE FIFTH STIFFENER FROM TOP CRACKED REPAIR IAW SRM 51-70-05 51-10-2 51-10-3 51-30-02. INSTALLED REPAIR ANGLES (DLM88101910).Jul 2, 2010 · N901DE · Doug MD88SDR SWAA103109Lug · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT PRIMARY VERTICAL FIN LUG FACES CORRODED. REPAIRED LUGS PER ER.May 27, 2010 · N509SW · Boeing 7375H4SDR ABXA201004200064Attach Angle · crackedVERT STAB LWR ACCESS 324CLX RT LWR FIN/BODY ATTACH ANGLE CRACKED IN RADIUS. HIGH FREQ EDDY CURRENT VERIFIED IAW B NDT PART 6 51-00-19. REMOVED AND REPLACED RT LWR ATTACH ANGLE. INSTALLED WITH HI-LOKS IAW 767 SRM 51-40-02.Apr 18, 2010 · N742AX · Boeing 767232SDR SWAA101689Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND LT VERTICAL STABILIZER FWD DRAG BRACE FITTING I/B AND O/B HOLES CORRODED. REPAIRED FITTING PER EA.Mar 25, 2010 · N710SW · Boeing 7377H4SDR SWAA101688Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND LT VERTICAL STABILIZER FWD DRAG BRACE FITTING CORRODED. REPAIRED FITTING PER EA.Mar 25, 2010 · N710SW · Boeing 7377H4SDR SWAA101604Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND RT VERTICAL STABILIZER FWD DRAG BRACE FACE FITTING CORRODED. REPAIRED FITTING PER EA.Mar 17, 2010 · N710SW · Boeing 7377H4SDR SWAA101603Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND LT VERTICAL STABILIZER AFT DRAG BRACE FACE FITTING CORRODED. REPAIRED FITTING PER EA.Mar 17, 2010 · N710SW · Boeing 7377H4SDR SWAA101602Fitting · corrodedDURING SCHEDULED 12Y CHECK, FOUND RT VERTICAL STABILIZER AFT DRAG BRACE FACE FITTING CORRODED. REPAIRED FITTING PER EA.Mar 17, 2010 · N710SW · Boeing 7377H4SDR A6WA201040174Bracket · crackedLT LOWER VISOR ATTACH BRACKET IS CRACKED. R & R UNSERVICEABLE BRACKET ON LT LOWER VISOR ATTACH.Feb 24, 2010 · N435AW · Cndair CL6002B19SDR EIAA2010004Structure · damagedWHILE TOWING AIRCRAFT OUT OF HANGAR HIGH DOOR WAS NOT OPENED FULLY, TOP OF VERT FIN DAMAGED APPROX 12 INCHES AND FROM TRAILING EDGE. FOUR (4) INCHES BROKE OFF TOP STATIC WICKS. REPAIRED DAMAGE ON RIGHT SIDE OF AIRCRAFT PER ECRA 485-53-193-1 AND ECRA 485-53-1Feb 5, 2010 · N485EV · Boeing 747212BSDR AALA20091223TUL03Structure · dentedDENT ON VERTICAL STABILIZER LEADING EDGE 2 INCHES BY .5 INCH BY ONE 16TH INCH DEEP AT LEADING EDGE STATION 252. REWORKED DENTED AREA ON STABILIZER LEADING EDGE STATION 252 TO WITHIN LIMITS GIVEN IN SRM 55-30-01-1A.Dec 23, 2009 · N978AN · Boeing 737823SDR C2XA09TY276Fitting · damagedLT VERT STAB FITTING RACE HAS TOOLING MARKS, REAMED BOTH LT AND RT SIDE FITTINGS TO THE 2ND OVERSIZE DIAMETER IAW EMB 145 SRM 55-30-02.Dec 23, 2009 · N15574 · Emb EMB145LRSDR USAA2009120993318Bolt · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON VERTICAL STABILIZER AFT ATTACHMENT BOLT INBOARD RIGHT SIDE AT BS 1085.56, RUDDER STA 13.33. REPLACED VERTICAL STABILIZER AFT ATTACHMENT BOLT INBOARD RIGHT SIDE AT BS 1085.56, RUDDER STA 13.33 IAW B737 AMM 55-30-00.Nov 16, 2009 · N450UW · Boeing 7374B7SDR USAA2009120393299Bolt · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION AT VERTICAL STABILIZER LEFT OUTBOARD ATTACHMENT BOLT AFT ATTACHMENT POINT. REPLACED VERTICAL STABILIZER LEFT OUTBOARD ATTACHMENT BOLT AFT ATTACHMENT POINT IAW B737 AMM 55-30-00.Nov 16, 2009 · N450UW · Boeing 7374B7SDR ASOA200901241Drag Angle · crackedRT SIDE VERTICLE STAB TO FUSELAGE ATTACHMENT FWD DRAG ANGLE CRACKED AFT SIDE AT 67.5 REAR SPAR DATUM. REPAIRED ON WO 137908 EC/TC REO 670-55-31-018.Nov 5, 2009 · N752EV · Cndair CL6002C10SDR ASOA200901240Drag Angle · crackedLT SIDE VERTICLE STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE CRACKED FWD SIDE AT 67.5 REAR SPAR DATUM. REMOVED CRACKED LT SIDE AFT DRAG ANGLE IAW SRM 51-42-21, 51-42-22, AND 51-42-13. DRILLED UP AND COUNTERSANK NEW LT AFT DRAG ANGLE AS SRM 51-40-11. OK TO INov 5, 2009 · N752EV · Cndair CL6002C10SDR ASOA200901239Drag Angle · crackedLT SIDE VERTICLE STAB TO FUSELAGE ATTACHMENT FWD DRAG ANGLE CRACKED AFT SIDE AT 67.5 REAR SPAR DATUM. REPAIRED ON WO 137908 EC/TC REO 670-55-31-018. JOB COMPLETE.Nov 5, 2009 · N752EV · Cndair CL6002C10SDR FDEA200910273694Strap · gougedEMPENNAGE- UPON STRAP REMOVAL ON THE RT SIDE FOUND WITH GOUGE MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.Oct 27, 2009 · N628FE · Doug MD11FSDR C2XA09SH373Bracket · damagedSHV - DURING C-CHECK LT SIDE DORSAL FIN LWR MOUNTING BRACKET 3RD HOLE FROM REAR HAS ELONGATED HOLE. MAINTENANCE OVERSIZED LT DORSAL FIN LWR MOUNTING BRACKET 3RD HOLE FROM REAR IAW EMB-145 SRM 51-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 21, 2009 · N11164 · Emb EMB145XRSDR K11A2009100772401Stiffener · corrodedREAR SPARS STIFFENER CORROSION ON WEB.Oct 7, 2009 · N724CK · Boeing 727225SDR SWAA095687Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND RT VERTICAL STAB FITTING LUG FACES AT AFT SPAR CORRODED, STA 1088. REPAIRED FITTING PER SWA EA.Sep 2, 2009 · N657SW · Boeing 7373L9SDR IPXA09557379Panel · misrepairedINSPECTION TYPE:C4 PREVIOUS REPAIRS TO VERTICAL STAB PANEL 322CL REQUIRE REWORK DUE TO INFORMATION REQUESTED BY ENGINEERING. REPAIRED PER SRM 51-70-17-0G AND UPS EO B757-5530-34918-A.Aug 31, 2009 · N450UP · Boeing 75724APFSDR IPXA09557377Panel · misrepairedINSPECTION TYPE:C4 PREVIOUS REPAIRS TO VERTICAL STAB PANEL 322CL REQUIRE REWORK DUE TO INFORMATION REQUESTED BY ENGINEERING. REPAIRED PER SRM 51-70-17-0G AND UPS EO B757-5530-34918-A.Aug 31, 2009 · N450UP · Boeing 75724APF
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