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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 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 55-3SDR 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-6SDR 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.SDR 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.SDR CALA2025101610179Angle · wornLOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AR SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AR SUPPORT FWD ANGLE IAW SRM 51-40-02-0G-0 AND DWG 147A0030.SDR CALA2025101610178Angle · crackedLOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AL SUPPORT ANGLE CRACKED REF AAR N/R 99954672 REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323AL SUPPORT FWD ANGLE REF B-737 SRM 51-40-02-0G-0 AND DWG 147A0030. REMOVSDR REXA2026052800836Bearing · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NR 2 AND NR 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. FITTING BEARINGS ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED AND FREE PLAY WAS CORRECTEDSDR DALA2025093007083Flange · corrodedCORROSION AT VERTICAL FLANGE OUTBOARD SURFACES AND AROUND NUT PLATE HOLES . COMPLIED WITH ER/A 629280-14. (1219817).SDR SWAA2025102114905Angle · crackedCRACK ANGLE LOC AT LEVEL OF BS 1016 VERTICAL STABILIZER. REPLACED ANGLE AND FASTENERS LOCATED AT LEVEL OF BS 1016 VERTICAL STABILIZER IAW B737-800 SRM-51-40-02-0G-0; DWG 176A3001 SHEET: 23 REV: D.SDR VNAA202509260016Drag Angle · damagedELONGATE HOLES ON VERTICAL STABILIZER UNDER RH FWD DRAG ANGLE BTW 55.62% STGR DATUM TO 61.56% STGR DATUM. RH FWD DRAG ANGLE BTW 55.62% STGR DATUM TO 61.56% STGR DATUM WAS REPAIRED PER REO 670-55-31-196 REV.-ASDR SWAA2025092611533Support Angle · crackedCRACK ON SUPPORT ANGLE ACCESS PANEL 323AL AT VERTICAL STABILIZER. REPLACED SUPPORT ANGLE ACCESS PANEL 323AL AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 172A6122 SHEET 1 REV B.SDR IPXA2025082044859Structure · delaminatedDELAMINATE- COMPOSITE, VERICAL STABILIZER AUXILIARY SPA AFT FSS 18.037 AREA. (RAPAIR) REQUEST UPS ENGINEERING DETERMINE MAJOR OR MINOR REPAIR.SDR VNAA202509250017Drag Angle · crackedCRACK ON FWD AND AFT RH DRAG ANGLE BTW UNION OF VERTICAL STABILIZER AND FUSELAGE (67.5% REAR SPAR DATUM). FWD AND AFT DRAG ANGLE WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01SDR CALA2025080507325Flange · wornLH BODY-TO-VERTICAL FIN FAIRINGS FLANGE BROKEN. REMOVED AND REPLACED LH BODY TO VERTICAL FIN FAIRINGS FLANGE IAW SRM 51-40-02-0G-0 AND DWG 147A0030.SDR VNAA202509250009Fairing · damagedFAIRING ASSY, LOWER VISOR (LH) 326CL WITHIN 2016.46 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. FAIRING ASSY, LOWER VISOR (LH) 326CL WAS REPLACED BY NEW FAIRNG PER EA 5SDR JJBA20250730108Profile · crackedBOTTOM OF VERT STAB, AFT OF REAR SPAR 3, RH PROFILE CRACKED AT LOWER SECTION. BOTTOM OF VERT STAB AFT OF REAR SPAR 3 RH PROFILE CRACK BLENDED. BOTTOM OF VERT STAB AFT OF REAR SPAR 3 RH AT LOWER SECTION WAS REPAIRED AND INSTALLED.SDR AALA202507096600Shim · migratedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RIGHT HAND REAR SPAR TERMINAL FITTING HAS SHIM WASHERS MIGRATING OUT FROM THE AFT SIDE OF THE OUTBOARD LUG. INSTALLED SHIMS AND ALL HARDWARE. PER AMM 53-30-00.SDR REXA2025072900766Angle · crackedCRACK ON LEFT & RIGHT 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 & RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 6SDR AALA202507026676Shim · migratedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER, RIGHT HAND REAR SPAR TERMINAL FITTING SHIM WASHER MIGRATING OUT FROM THE AFT SIDE OF THE OUTBOARD LUG. INSTALLED A NEW SHIM AND REINSTALLED THE BOLT AND NUT. PER AMM 55-30-00-400-801.SDR SWIA2025090200620Drag Angle · crackedDURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (C-CHECK RO 08/29/2025)BLENDED CORRODED AREA OF LH WING FUEL ACCESS PANEL LANDING 510AB IN REFERENCE WITH REO 601R-57-21-030 REV. -L, DATED 2SDR REXA2025071500729Angle · crackedCRACKS ON DRAG ANGLES RH FWD SIDE AT VERTICAL STABILIZER. DRAG ANGLES FWD TO RH SIDE AT VERTICAL STABILIZER WERE REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR REXA2025071500727Angle · crackedCRACKS ON DRAG ANGLES RH AFT SIDE AT VERTICAL STABILIZER. DRAG ANGLES AFT TO RH SIDE AT VERTICAL STABILIZER WERE REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR REXA2025071500726Angle · crackedCRACKS ON DRAG ANGLES LH FWD SIDE AT VERTICAL STABILIZER. DRAG ANGLES FWD TO LH SIDE AT VERTICAL STABILIZER WERE REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR VNAA20250715008Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW LH DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW LH DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TSDR VNAA20250715007Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BLSDR YENA2025042900448Fitting · corrodedDURING HEAVY MAINTENANCE: SECONDARY FINDING AFTER REMOVED BEARING CORROSION FOUND ON BORE HINGEARM FITTING N5 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE FITTING #5 VERTICAL STABILIZER IAW A320 SRM 51-72-11 AND SRM A320 55-36-42-300-008. RII AND WORK ACCOMSDR YENA2025042900447Fitting · corrodedDURING HEAVY MAINTENANCE: SECONDARY FINDING: AFTER REMOVED BEARING, CORROSION FOUND ON BORE HINGE ARM FITTING #4 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE FITTING #4 VERTICAL STABILIZER IAW A320 SRM 51-72-11 AND SRM A320 55-36-42-300-008. RII AND WORK ACSDR REXA2025052900605Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD 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 DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (SDR VNAA20250602019Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CORRECTIVE ACTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUSDR VNAA20250602018Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CORRECTIVE ACTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DASDR N6WA2025040817Drag Angle · crackedCRACK IN VERT STAB RH AFT DRAG ANGLE. REMOVED AND REPLACED VERT STAB RH AFT DRAG ANGLE IAW CRJ SRM 51-42-21.SDR N6WA2025040816Drag Angle · crackedCRACK IN LH VERT STAB AFT DRAG ANGLE. REMOVED AND REPLACED VERT STAB LH DRAG ANGLE IAW CRJ SRM 51-42-21.SDR VNAA202504020008Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DASDR VNAA202504020007Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPASDR SWIA2025060900327Drag Angle · crackedLH FWD DRAG ANGLE ON VERTICAL STABILIZER CRACKED (C-CHECK RO 06/07/2025)PERFORMED NEW REPAIR ON LH FWD DRAG ANGLE AT VERTICAL STABILIZER IAW BOMBARDIER REO 670-55-31-018 REV-A DATE: 2016-11-10 PERFORMED NDT ET INSPECTION BY BARON NDT, LLC FAA CRS# 5NDR545SDR AALA202504019094Web · crackedAIRCRAFT WAS GROUNDED: FOUND CRACK ABOUT 2 INCH LONG ON TOP OF HOLE (BAY) 15 BETWEEN STAB STA 196.663 AND 205.663. ACCOMPLISHED WEB REPAIR, PER SRM 55-30-10-2R-2.SDR REXA2025042800504Drag Angle · crackedAFTER NDT EVALUATION (CRACK NOT VISIBLE), CRACK AT FWD DRAG ANGLE, VERTICAL STABILIZER RH SIDE. FWD DRAG ANGLE AT VERTICAL STABILIZER RH SIDE WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01SDR REXA2025042800498Drag Angle · crackedIN REFERENCE TO CARD 700-53-900-310: CRACK ON AFT DRAG ANGLE AT VERTICAL STABILIZER RH SIDE. AFT DRAN ANGLE AT VERTICAL STABILIZER RH SIDE WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01SDR SWAA2025040906466Angle · corrodedCORROSION ON ANGLE UNDER VERTICAL STAB BS1036 LBL2 WL308.5. MARKED <[01]. ADDED DIMENSIONS TO STEP 2.SDR JR2R20250312709Tip Cap · damagedAFTER FINISH REMOVAL FOR COMPOSITE REPAIR TO PANEL 326AL, DISCOVERED DAMAGE TO THE METAL BONDING STRIP ON TRAILING EDGE.SDR VNAA202504130008Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE AND FWD DRAG ANGLE (2 E/AS) 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 AND FWD DRAG ANGLESDR VNAA202503070034Bearing · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL#2103 REV. B.SDR SWAA2025041402709Angle · crackedVERTICAL FIN FRONT SPAR FWD SPRING ANGLE (176A3101-26) CRACKED AT L/H ATTACH POINT (MARKED) <[01]. REMOVED AND REPLACED NEW VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02 AND AIPC 55-33-11-02A.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR VNAA202504130007Drag Angle · crackedCRACK ON LEFT 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 LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM SDR IPXA2025031252166Panel · debondedDISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N: 186U1006-3 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). INSTALL L/H VERTICAL STAIBLIZER PANEL P/N:186U1006-3 I.A.W. UPS EO-93144-REQ1 REV.1.SDR SWAA2025032498497Attach Angle · crackedVERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02-0G-0 AND DWG #176A3101 SHEET 4 REV-.SDR REXA2025030600278Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE 67.5% REAR SPAR DATUM. RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR CALA2025021100333Support Angle · corrodedVERTICAL FIN L/H SUPPORT ANGLE ON FUSELAGE FOR PANELS 323AL 323BL 323CL HAS CORROSION. REF AAR N/R 9940933. CLEANED CLOSURE ANGLE ON UPPER FUSELAGE BELOW VERT. STAB FROM REF B737 SRM 53-80-71-2R-6. INSTALLED REPAIR ANGLE AND STRAP AS STA 1016 TO 1132, L/H SIDESDR REXA2025030700286Drag Angle · crackedLH VERTICAL STAB FWD DRAG ANGLE IS CRACKED. REPAIRED LH VERTICAL STAB FWD DRAG ANGLE IAW CRJ-900 SRM 55-31-00-201-A01SDR REXA2025030600270Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUMWAS REPAIRED PER CRJ-900 SRM 55-31-0
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