JASC 5342
Service difficulty reports · 578
Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, 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 = '5342' 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 = '5342' 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 REXA2026052800812Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM REPAIR ON CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS PERFORMED PESDR VNAA202510300005Drag 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 BL0.0). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATSDR REXA2026052800845Drag Angle · crackedINITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5SDR REXA2026052800840Drag Angle · crackedINITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00) CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67SDR HNAA2025102100718Drag Angle · crackedF070245 VERTICAL STABILIZER RH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. REPAIRED VERTICAL STABILIZER RH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE DET B FIG 219 SH1 AND SRM 51-40-02.SDR HNAA2025102100717Drag Angle · crackedF070244 VERTICAL STABILIZER LH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. RAR VERTICAL STABILIZER LH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE DET B FIG 219 SH1 AND SRM 51-40-02.SDR SWI2025F01896Drag Angle · crackedRIGHT AFT VERTICAL STAB DRAG ANGLE HAS POSSIBLE CRACK (MARKED). (C-CHECK RO 12/24/2025)EVALUATED, REMOVED AND INSTALLED NEW RH AFT VERTICAL STAB DRAG ANGLE REF CRJ900 SRM 51-42-13-001-001-A01 , CRJ900 SRM 51-42-21-001-001-A01 , CRJ900 SRM 51-42-22-001-001-A01 SDR SWIA202512260910Drag Angle · crackedLEFT AFT VERTICAL STAB DRAG ANGLE HAS POSSIBLE CRACK. PERFORMED REPAIR ON LH AFT VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.SDR SWI2025F01793Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLY CRACKED. REMOVED CRACKED LT VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE IAW SRM 51-42-10-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01, AND INSTALLED -5 DOUBLER ANGLE ANSDR SWIA2025120900827Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE ATTACH FORWARD DRAG ANGLE POSSIBLY CRACKED. AFTER DETERMINING THE END OF THE CRACK BY NDT INSP IAW NDTM PART 1 51-20-08-230 ON REPORTED FWD DRAG ANGLE, IT WAS REPAIRED BY INSTALLATION OF REINFORCEMENT ANGLE IAW SRM 55-31-00-201-00SDR IPXA2025091850638Bracket · cracked-EXT TAIL-L/H SIDE WHERE FUSELAGE AND TAIL MEET-ANGLE CRACKED FOR UPPER APRON(333AT)-109 VWV 91195430. INSTALLED L/H HORIZONTAL STABILIZER LEADING EDGE 331AB IAW A300-600 AMM 55-12-11/401. REVIEWEDSDR SWIA202511240808Drag Angle · crackedRH VERTICAL STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)REMOVED RH AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01,CRJ700 SRM 51-42-22-001-001-A01. INSTALLED NEW RH AFT DRAG ANGLE REF CSDR SWIA20251124808Drag Angle · crackedLH VERTICAL STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)INSTALLED -5 AFT ANGLE DOUBLER & -7 AFT ANGLE FILLER ON L/H AFT DRAG ANGLE REPAIR REF CRJ 700 SRM 55-31-00-201-001-A01. COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SDR VNA2025F00028Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH/RH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH/RH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRASDR REXA2025100200899Drag Angle · crackedR/H AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE RH AFT DRAG ANGLE P/N:AV670-21186-004. IAW CRJ900 SRM 51-42-13-001-001-A01,SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE RH AFT DRAG ANGLE PN# AV670-21186-004 ISDR SWI2025F01502Drag Angle · crackedRH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)PERFORMED SRM REPAIR TO CRACKED RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.SDR SWI2025F01501Drag Angle · crackedLH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED REPAIR ANGLES ON LH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. REF. CRJ900 SRM 55-31-00-201-001-A01 REV 38 JUL 25/2020. COMPLIED WITH 51-900-1002-SKY.SDR SWIA202511030628Drag Angle · crackedRH VERT STAB-TO-FUSELAGE FORWARD DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)PERFORMED SRM REPAIR TO CRACKED RH VERT STAB-TO-FUSELAGE FORWARD DRAG ANGLE. REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.SDR SWIA2025062300020Drag Angle · crackedDURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR REXA2025062600699Drag 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). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUMSDR SWI2025F01636Drag Angle · crackedRIGHT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE AFT END POSSIBLE CRACKED. (C-CHECK) REMOVED AND REPLACED WITH NEW RT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. IAW DWG BA670-35002, REV -F, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-22-001-0SDR SWIA202511260524Drag Angle · crackedLH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE FWD END POSSIBLE CRACK (MARKED) (C-CHECK RO 11/25/2025)REMOVED AND INSTALLED NEW AFT DRAG ANGLE PN# AV670-21186-003 ON LH VERTICAL STABILIZER REF CRJ900 SRM 51-42-13-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01, CSDR AALA202506232953Lug · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND HORIZONTAL STABILIZER REAR SPAR LOWER LUG. REPAIRED PER EA 364945.SDR AALA202506235379Lug · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND HORIZONTAL STABILIZER REAR SPAR LOWER LUG. REPAIRED PER EA 364946.SDR SWI2025F01051Drag Angle · crackedLEFT VERTICAL STABILIZER DRAG ANGLE AFT CRACKED. PERFORMED REPIAR DRAG ANGLE AFT ON LT VERTICAL STABILIZER IAW REO 670-55-31-018 REV-A, & SRM 51-26-01, NDT PERFORMED.SDR SWIA2025072200422Drag Angle · crackedRIGHT VERTICAL STABILIZER DRAG ANGLE AFT CRACKED. PERFORMED REPAIR DRAG ANGLE AFT AT RH VERTICAL STABILIZER IAW REO 670-55-31-018 REV-A, SRM 51-26-01, NDT PERFORMED.SDR SWI2025F00940Drag Angle · crackedLH VERTICAL STAB - TO - FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK AT LEADING EDGE OF ANGLE (MARKED) (C-CHECK RO 07/15/2025)REPAIRED LH VERTICAL STAB - TO - FUSELAGE AFT DRAG ANGLE PER CRJ900 SRM TASK 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SDR SWIA2025071600404Drag Angle · crackedLH VERTICAL STAB - TO - FUSELAGE FWD DRAG ANGLE CRACKED (MARKED) (C-CHECK RO 07/15/2025)REPAIRED LH VERTICAL STAB - TO - FUSELAGE FWD DRAG ANGLE PER CRJ900 SRM TASK 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY AND M-337.SDR REXA2026072801209Drag 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 SWI2025F01303Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 09/07/2025)REMOVED OLD AND INSTALLED NEW AFT DRAG ANGLE AT AFT LH VERTICAL STAB TO FUSELAGE ATTACH. REF CRJ900 SRM 51-42-13-001-001-A01 , CRJ900 SRM 51-42-21-001-001-A01SDR SWI2025F01301Drag Angle · crackedRH VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 09/07/2025)REMOVED OLD AND INSTALLED NEW AFT DRAG ANGLE AT AFT RH VERTICAL STAB TO FUSELAGE ATTACH REF CRJ900 SRM 51-42-13-001-001-A01 , CRJ900 SRM 51-42-21-001-001-A01 ASDR DALA2025031802032Mount · corroded(LOG 0855497) VERTICAL STAB MOUNTING POINTS CORROSION PRI 624280 ISSUED. C/W VERTICAL STAB/MOUNTING POINTS/CORROSION FINDINGS ERA 624280-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. VERIFIED ERA 624280-14 HAS BEEN COMPLETED.SDR YENA2025031200253Lug · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120296. CRACK ON LUG O/B ACTUATOR ON RH HORIZONTAL STABILIZER, (RESOLVED ON W/O: 1353259 TASKCARD: NR-00014) REF AEROMAN WO# 2025 17/1 NR# 2025-120296. PERFORMED PERMANENT REPAIR ON LOCKING LUG LOCATSDR DALA2025031201944Lug · corroded(LOG 0849062) CORROSION LOCATED ON AFT FACE OF REAR LOWER LUG AT LT HORIZONTAL STABILIZER. COMPLIED WITH ER/A 623847-14 REV ORIGINAL, THIS MATCHES WITH ALL STEPS ON PRI 623847-14 REV 0, 1 AND 2, IT HAS BEEN VALIDATED.PERFORMED REPAIR INSTRUCTIONS ON HORIZONTALSDR DALA2025031201943Lug · corroded(LOG 0848130) CORROSION LOCATED ON AFT FACE OF REAR LOWER LUG OF RH HORIZONTAL STABILIZER. PERFORMED REPAIR INSTRUCTIONS ON RH HORIZONTAL STABILIZER, AS PER ER/A 623846-14 REV. ORIGINAL.SDR REXA2025031300318Attach Angle · crackedCRACK ON 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) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DASDR REXA2025031300316Attach Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND ON FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SSDR DALA2025030301627Mount · corrodedAIRCRAFT 3737, ON VERTICAL STAB AFT MOUNT OUTBOARD LT FITTING LUG CORROSION ON FACE OF BUSHING. CORRECTIVE ACTION: REPLACED VERTICAL STAB AFT MOUNT OUTBOARD LT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS. REF ERA 624280-14 REV 0 PRI REV5. (LP 0829461)SDR SCNA20250415119Bushing · crackedRIGHT HOR. STAB AFT BOTTOM ATTACHMENT BUSHING CRACKED. UNABLE TO CONFIRM WHETHER IF BUSHING IS A SHRINKFIT OR FORCEMENT & P/N IS UNAVAILABLE PER EAR #12 RESPONSE STEP 1. PERFORMED A DVI IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE (POSSIBLE) CRACK NOTED AT SDR DALA2025030201589Mount · corroded(LOG 0829460) ON VERTICAL STAB AFT MOUNT OUTBOARD RT FITTING LUG CORROSION ON FACE OF BUSHING. R/R VERT STAB AFT MOUNT OUTBOARD RT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS, REF ERA 624280-14 REV 0, PRI REV 5.SDR SCNA20250505161Bushing · migratedLEFT AFT HORIZONTAL STAB UPPER AFT BUSHING MIGRATING. SAA034 027 - RESOLUTION: SUBMIT TO ENG. UNABLE TO CONFIRM IF BUSHING IS SHRRINK FIT OR FORCEMATE P/N CANNOT BEE CONFIRMED PER ENG RESPOSE STEP 1. BUSHING MIGRATED SEALANT WAS BROKEN AROUND ENTIRE CIRCSDR SCNA20250415120Bushing · crackedON CENTER BOX LEFT AFT LOWER HOR. STAB HAS BUSHING CRACKED. UNABLE TO CONFIRM WHETHE IF BUSHING IS SHRINKFIT OR FORCEMENT & P/N IS UNAVALIABKE, PER EAR #5 RESPONSE STEP 1. PERFORMED A DVI, IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE & CRAVK NOTED AT DEFESDR 9WGA2025021234408Attach Fitting · damagedHORIZONTAL STAB ATTACH FITTING R/H OUTBOARD UPPER TENSION BOLT HOLE HAS EVIDENCE OF CORROSION/CRACK INDICATION, REPAIRED R/H OUTBOARD UPPER TENSION BOLT HOLE IAW B747-400 EAM 4453014 R3. NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025021234407Attach Fitting · damagedHORIZONTAL STAB ATTACH FITTING R/H UPPER MIDDLE OUTBOARD TENSION BOLT HOLE HAS EVIDENCE OF CORROSION/CRACK INDICATION. REPAIRED R/H UPPER MIDDLE OUTBOARD TENSION BOLT HOLE IAW B747-400 EAM 4453014 R3. NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICSDR 9WGA2025021234406Attach Fitting · corrodedHORIZONTAL STABILIZER ATTACH FITTING LEFT HAND LOWER INBD CROSSBOLT HOLE HAS EVIDENCE OF CORROSION.SDR SWI2025F01042Drag Angle · crackedVERTICAL STAB. RH AFT DRAG ANGLE HAS SUSPECTED CRACK (MARKED). (C-CHECK RO 07/18/2025)REPAIRED VERTICAL STAB RH AFT DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01 REPAIR COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYSDR SCNA20250507170Bushing · wornRIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT BUSHINGS PLATING IS WORN. (120-109) - RESOLUTION: SUBMIT TO ENG, REMOVED FORWARD LOWER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PAGE 1 TO 3. REVSDR SCNA20250505163Bushing · wornRIGHT HAND HORIZONTAL STABILIZER, THE AFT MID MOUNT BUSHINGS PLATING IS WORN. REMOVED AFT MID MOUNT BUSHINGS AT R/H HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG 4 PG 1 TO 3 REV 2.SDR SCNA20250505162Bushing · wornRIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT BUSHINGS PLATING IS WORN. (120-109) - SUBMIT TO ENG, REMOVED FORWARD LOWER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PAGE 1 TO 3. REV. 2. DATE JUSDR SCNA20250415118Lug · gougedAIRCRAFT TAIL SECTION, RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD UPPER MOUNT LUG HAS A GOUGE ON THE UPPER FORWARD SURFACE. . REMOVED DAMAGE ON TO AIRCRAFT TAIL SECTION R/H HORIZONTAL STABALIZER THE FWD UPPER MOUNT LUG ON THE UPPER FWD SURFACE IAW B737-800
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