JASC 5534

Service difficulty reports · 816

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 CALA2026092819933Fitting · corrodedCORROSION FOUND ON RH VERTICAL STAB FWD MOUNT, AFT FITTING. ACCOMPLISHED A REPAIR IAW ECRA 5380-01456, PART 1.Sep 21, 2026 · N73299 · Boeing 737824SDR HNAA2026093000921Profile · crackedAFT OF REAR SPAR 3 OF VERTICAL STAB, LT PROFILE CRACKED ABOVE RUDDER UPPER AND MID HINGE FITTING. REPAIRED IAW ETD 2026-145-015973 AND EO 1-55-26-0465Sep 8, 2026 · N653AE · Emb EMB145LRSDR AALA202609173925Angle · crackedAIRCRAFT IN BASE MAINTENANCE: J-ANGLE CRACKED ON VERTICAL STAB ATTACH FITTING JUST ABOVE AND AFT OF R/H ATTACH LUG. REMOVED AND INSTALLED J-ANGLE IAW AARD 55-30-09-3 PARAGRAPH 5 STEP A.Sep 8, 2026 · N355PU · Boeing 737823SDR UIEA2026082700813Support · crackedVERTICAL STAB, LEFT L/E FIXED PANEL STA 78 AFT UPPER SUPPORT FOUND CRACKED. VERTICAL STAB LEFT L/E FIXED PANEL UPPER SUPPORT WAS REPLACED IAW SRM 51-10-02 & 51-40-02, REV 107, AND RI-55-30-18461, REV A. NO FURTHER DEFECTS NOTED.Sep 1, 2026 · N489MC · Boeing 747412FSDR SWAA2026092108164Panel · damagedLEFT BALANCE BAY PANEL (333BB) HAD AN ELONGATED SCREW HOLE. REPAIRED THE FASTENER HOLE IAW SRM 51-70-05, REPAIR 8.Aug 24, 2026 · N8550Q · Boeing 7378H4SDR FDEA202608201195Beam · crackedVERTICAL STABILIZER REAR SPAR FIN STA:95.00 SUPPORT PANEL 324AL BEAM CRACKED REMOVED AND REPLACED BEAM AT VERTICAL STABILIZER REAR SPAR SUPPORT PANEL 324AL IAW B757 SRM 51-40-02-0G AND DRAWING 173N1300Aug 20, 2026 · N993FD · Boeing 7572Q8SDR CALA2026082018740Beam · crackedVERTICAL STAB. FIXED T/E LT LOWER SEAL TO FUSELATE OUT OF THE RIGHT PLACE. REMOVED, FABRICATED AND INSTALLED BEAM COMMON TO LT VERTICAL LOWER FUSELAGE, FABRICATED & ATTACHED IAW DWG 173N1300, & SRM 51-40-02-0G.Aug 14, 2026 · N12125 · Boeing 757224SDR CALA2026081718650Torque Box · dentedRT VERTICAL STAB EXTERNAL SURFACE OF LWR TORQUE BOX SKIN FROM FSS 92.250-FSS 270.784 HAS NUMEROUS DENTS (APPROX 100+). VERTICAL STAB RH VERTICAL TORQUE BOX PANEL. REMOVED AND REPLACED 175N2001U4 TORQUE BOX PANEL COMMON TO NETIO RT STAB IAW SRM 51-40-02-OG.Aug 13, 2026 · N12125 · Boeing 757224SDR SWAA2026081478820Seal · deterioratedDETERIORATED SEAL ON ACCESS PANEL 324ADR AT VERTICAL STABILIZER. REPLACED SEAL PANEL 324ADR AT VERTICAL STABILIZER IAW SRM 51-10-02, ITEM 9, & AMM 55-05-02-211-812, PARAGRAPH 63.C.(3).Aug 7, 2026 · N7732A · Boeing 7377BDSDR IPXA2026083180847Torque Box · delaminatedMAJOR REPAIR, LT LOWER VERTICAL STABILIZER LOWER FWD TORQUE BOX PANEL HAS AREA OF DELAMINATION AROUND CIRCULAR PATCH/ PLUG NEAR UPPER FWD CORNER. ACCOMPLISHED REPAIR IAW SRM REV 124, 51-70-10-2R-4.Jul 27, 2026 · N461UP · Boeing 75724APFSDR SWAA2026081744181Angle · elongatedELONGATED HOLE ON ANGLE IN UPPER AREA AT ACCESS PANEL 324AAL T/E AT VERTICAL STAB. REPLACED ANGLE LOCATED UPPER AREA AT LEVEL ACCESS PANEL 324AAL TRAILING EDGE AT VERTICAL STABILIZER IAW SRM 51-40-02 AND DWG 175A3100, SHT 5, REV H.Jul 11, 2026 · N8651A · Boeing 7378H4SDR IPXA2026071426239Attach Angle · wornVERTICAL STAB TRAILING EDGE PANEL 324AL LOWER AFT CORNER SUPPORT STRUCTURE SECTION MISSING AND FUSELAGE ATTACH ANGLE WORN THIN IN SEVERAL AREAS. DAMAGED WELL MARKED RL004. REMOVED 1EA DAMAGED ANGLE FIN FAIRING AT VERTICAL STABILIZER TRAILING EDGE PANEL 324AL LJun 18, 2026 · N418UP · Boeing 75724APFSDR HNAA2026070300572Lug · wornRUDDER 1, UPPER HINGE FITTING, BOTH LUGS WORN. R & R LUGS IAW SRM 51-40-02 AND AMM 20-10-01.Jun 12, 2026 · N652RS · Emb EMB145LRSDR REXA2026060800949Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PMay 25, 2026 · N538CA · Cndair CL6002D24SDR REXA2026060800948Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WERE REPAIRED May 9, 2026 · N538CA · Cndair CL6002D24SDR CALA2026051116128Support Angle · gougedVERTICAL STAB LT SIDE ACCESS PANEL 324AL LOWER SUPPORT ANGLE GOUGED. REMOVED AND REPLACED DAMAGED ANGLE BY NEW ANGLE IAW SRM 51-40-02 RESTORED SURFACE PROTEC ION AT AREA IAW AMM TASK 51-21-15-370-801 STA 1804.81May 8, 2026 · N19141 · Boeing 757224SDR IPXA2026060872812Panel · deformedTHE R/H LWR FWD TORQUE BOX PANEL HAS EXCESSIVE HAIL DAMAGE AND MULTIPLE DISBONDS / DELAMINATIONS ACROSS THE ENTIRE SURFACE OF THE PANEL FROM TOP TO BOTTOM. INSTALLED 1 EA TORQUE BOX PANEL IAW SRM 51-40-02.May 7, 2026 · N423UP · Boeing 75724APFSDR REXA2026052100604Angle · crackedL/H DRAG ANGLE ON VERT. STAB HAS A CRACK (MARKED W/ TAPE) REMOVED UNSERVICEABLE LH AFT DRAG ANGLE IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LH AFT DRAG ANGLE PN: AV670-21186-003 IAW CRJ900 SRM 51-40-11-0Apr 30, 2026 · N919XJ · Cndair CL6002D24SDR SWIA2026042576726Drag Angle · crackedRIGHT AFT VERTICAL DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE AT RH AFT VERTICAL IAW REO 670-55-31-018, REV-A, SRM 51-26-01.Apr 25, 2026 · N614QX · Cndair CL6002C10SDR SWIA2026042576718Drag Angle · crackedLEFT AFT VERTICAL DRAG ANGLE IS CRACKED. PERFORMED REPAIR DRAG ANGLE ON LT AFT VERTICAL IAW REO 670-55-31-018, REV-A, SRM 51-26-01, NDT PERFORMED.Apr 25, 2026 · N614QX · Cndair CL6002C10SDR REXA2026052900874Angle · crackedCRACK ON LT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD - AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPApr 24, 2026 · N933XJ · Cndair CL6002D24SDR 2026FA0000292Vertical Beam · corrodedDURING EMPENNAGE COVE INSP, FOUND VERTICAL AFT SPAR HAS CORROSION ON RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AND REMOVED ALL VISIBLE SIGNS OF CORROSION ON AFT SPAR RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AREA WAS BEYOND ALLOWABLE LIMITS AND WAS SUBMITTED TO Apr 24, 2026 · N592QS · Cessna 560XLSDR SWAA2026043083752Angle · crackedCRACKED ANGLE, INTERNAL STRUCTURE FRONT SPAR SUPPORT FITTING RT AREA APPROX AT BS 1016 IN THE VERTICAL STAB. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 176A3101, SHEET 4, REV-.Mar 26, 2026 · N244WN · Boeing 7377H4SDR R3WA20260429001Pulley Bracket · chafedDURING SCHEDULED MAINTENANCE, A DETAILED VISUAL INSPECTION OF THE RUDDER CONTROL SYSTEM DISCOVERED A RUDDER CONTROL CABLE RUBBING AGAINST A PULLEY BRACKET WHICH WAS ALSO PART OF THE RUDDER CONTROL SYSTEM. CABLE WEAR WAS MINIMAL AND WITHIN SERVICEABLE LIMITS SPMar 19, 2026 · N716XJ · Cessna 750SDR COEA2026072224803Fitting · corrodedHORIZONTAL TO VERICAL STAB AFT L/H FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FITTING PER ATR72 SRM 51-25-04 REV. 122.Mar 8, 2026 · N803FX · Aerosp ATR72212SDR AALA202603258400Channel · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL RIGHT HAND RELIEF CUTOUT IS CRACKED, LOCATED ABOVE THE FRONT SPAR TERMINAL FITTING RIGHT HAND LUG. REMOVED AND REPLACED VERTICAL STABILIZER J-CHANNEL RIGHT HAND RELIEF CUTOUT. PER SRM 51-40-01-0G.Mar 8, 2026 · N908AN · Boeing 737823SDR N6WA2026030301Drag Angle · crackedVERTICAL STAB RH DRAG ANGLE CRACKED. REMOVED AND REPLACED VERT. STAB RH AFT DRAG ANGLE IAW CRJ SRM 51-42-06Mar 2, 2026 · N523GJ · Cndair CL6002C11SDR 2026FA0000140Vertical Support · corrodedSEVERAL AREAS OF CORROSION ON UPPER VERTICAL STAB R/H SIDE BELOW TIP CAP. PERFORMED MAJOR PERMANENT REPAIR OF AREA IAW AQRD RFTS-116135 REV 0 & AQRD ERO-988077 REV IR.Feb 25, 2026 · N601QS · Cessna 680ASDR AALA202603069362Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL ABOVE THE FORWARD SPAR TERMINAL FITTING RIGHT HAND LUG IS CRACKED ON THE AFT SIDE OF THE RELIEF CUTOUT. REPLACED J-CHANNEL WITH SERVICEABLE J-CHANNEL ABOVE THE FORWARD SPAR TERMINAL FITTING RIGHT HANDFeb 24, 2026 · N990AN · Boeing 737823SDR AALA202602261905Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO VERTICAL STABILIZER AFT DRAG BRACE FITTING AT WL 301, RBL 10. REPLACED FITTING PER SRM 53-80-90-0I.Feb 24, 2026 · N910AN · Boeing 737823SDR AALA202602266913Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO VERTICAL STABILIZER FORWARD DRAG BRACE FITTING AT WL 301, RBL 10. REPLACED FITTING PER SRM 53-80-90-0I-1.Feb 22, 2026 · N910AN · Boeing 737823SDR SWAA2026031370921Web · crackedCRACKED HORIZONTAL WEB, BS 1016 UPPER AREA OF THE VERTICAL STAB. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 176A3001, SHEET 23, REV D.Feb 14, 2026 · N240WN · Boeing 7377H4SDR CALA2026021813855Angle · corrodedCORROSION AT VERTICAL STABILIZER T/E AREA INTERNAL CAVITY OF BALANCE WEIGHT. ACCOMPLISHED REPLACEMENT OF ANGLE (STIFFENER) IAW SRM 51-40-02-0G-0.Feb 12, 2026 · N33294 · Boeing 737824SDR VNAA20260328004Drag Angle · crackedDURING INSPECTION OF THE TASK CARD 300-07-JIC IT WAS DETECTED CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS FOUND. AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TFeb 10, 2026 · N542EA · Bombdr CL6002D15SDR REXA2026032700271Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUMFeb 9, 2026 · N918XJ · Cndair CL6002D24SDR REXA2026032700270Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKS ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5%Feb 9, 2026 · N918XJ · Cndair CL6002D24SDR AALA202602274820Channel · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL HAS A CRACK AT THE RELIEF CUTOUT ABOVE THE LEFT HAND FORWARD SPAR TERMINAL FITTING. INSTALLED J-CHANNEL ASSEMBY. PER AARD 51-00-05-1 REPAIR #1.Feb 9, 2026 · N983AN · Boeing 737823SDR REXA2026080301389Angle · crackedCRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01Feb 5, 2026 · N398CA · Cndair CL6002C10SDR HNAA2026012200068Housing · wornLEFT & RIGHT VERTICAL STABILIZER SPHERICAL BEARING HOUSINGS WORN. ENLARGED LT & RT VERTICAL STAB SPHERICAL BEARING HOUSINGS TO FIRST OVERSIZED (DIMENSION 58.00MM, PN 145-408881-001 (RE-WORK #1) IAW SRM 55-30-02 ND EO1-55-26-0030.Dec 10, 2025 · N933JN · Emb EMB145LRSDR VNAA20260203009Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACDec 5, 2025 · N525AE · Bombdr CL6002D15SDR SWAA2026011242946Bracket · corrodedCORROSION GROUND PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STABILIZER. REPLACED BRACKET PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STAB IAW SRM 51-10-02 PARAGRAPH 9, SRM 51-40-02, AND DWG 175A1601, SHEET 18, REV A.Dec 4, 2025 · N241WN · Boeing 7377H4SDR YENA2025120201138Fitting · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVE BEARING, CORROSION FOUND IN FITTING N5 AT VERTICAL STABIL IZER. REMOVED AND REPLACED FITTING # 5 AT VERTICAL STABILIZER IAW A321 NEO SRM 51-72-11, SRM A321 NEO 55-36-42-300-008 AND D553721041 WOTK BY 8632812 RII AE370Nov 27, 2025 · N2027J · Airbus A321271NSDR YENA2025120201137Hinge · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVE BEARING CORROSION FOUND IN FITTING Ñ 5 AT VERTICAL STABILIZER. REMOVED AND REPLACED HINGE FITTING NR 5 AT VERTICAL STABILIZER IAW SRM 51-72-11, SRM 55-36-42-300-008 AND DRAWING D55371041.Nov 27, 2025 · N2027J · Airbus A321271NSDR 2025F00273Support · corrodedDURING A PREFLIGHT WALKAROUND, SURFACE CORROSION WAS OBSERVED ON THE VERTICAL STABILIZER AFT SECTION. AFTER CLOSER INSPECTION SEVERE DELAMINATION WAS SEEN ON THE AFT VERTICAL SUPPORT ANGLES AND AFT STAB BULKHEAD SECTION. THE RUDDER TRIM TAB BRACKET ALSO HAD SINov 26, 2025 · N86VS · Cessna 414SDR KISA202602050001Angle · corrodedDURING A PREFLIGHT WALK AROUND CORROSION WAS OBSERVED ON THE AFT SPAR ANGLE CHANNEL OF THE VERTICAL STABILIZER. UPON FURTHER INVESTIGATION SIGNIFICANT INTERGRANULAR CORROSION WAS FOUND RESULTING IN EXFOLIATION OF THE SURFACE OT THE SPAR ANGLE. THIS RESULTED INNov 25, 2025 · N86VS · Cessna 414SDR FDEA202511052124Frame · crackedVERTICAL STABILIZER REAR CENTER SPAR STIFFENER CRACKED AT STATION 2122 5 O' CLOCK AREA. CRACKED STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT STATION 2122 5 O' CLOCK AREA REPAIRED AS PER EA# 1-5530-T0385238 P1 TITLE: STABILIZERS - VERTICALNov 5, 2025 · N574FE · Doug MD11FSDR YENA2025102801067Hinge Arm · wornDURING HEAVY MAINTENANCE: WEAR ON HINGE ARM FORK END FITTING # 6 ON VERTICAL STABILIZER (1EA); REF AEROMAN WO# 2025-262/1 NR# 2025-608758 REMOVED AND REPLACED HINGE ARM FORK END FITTING #6 ON VERTICAL STABILIZER I.A.W. A320 SRM 51-42-11 AND I.A.W A320 SRM 55-3Oct 27, 2025 · N623JB · Airbus A320232SDR AALA202511175408Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL STABILIZER LEFT HAND LOWER CLOSURE ANGLE ON TOP OF FUSELAGE AFT OF THE DORSAL FIN FROM STA 1005 TO STA 1016. REPAIRED ANGLE PER SRM 53-80-71-2R-6Oct 19, 2025 · N907AN · Boeing 737823SDR CALA2025101610181Angle · wornLOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BR SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BR SUPPORT AFT ANGLE REF SRM 51-40-02-0G-0 AND DWG 148A8300.Oct 15, 2025 · N18243 · Boeing 737824SDR CALA2025101610180Angle · wornLOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BL SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BL SUPPORT AFT ANGLE REF B-737 SRM 51-40-02-0G-0 AND DWG 148A8300.Oct 15, 2025 · N18243 · Boeing 737824
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