JASC 5342
Service difficulty reports · 573
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 REXA2026101601945Drag Angle · crackedDURING (ET) HFEC INSPECTION ON DRAG ANGLE IAW NRC 252, A CRACK WAS FOUND ON THE AFT DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) AT VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026101601944Drag Angle · crackedCRACKED FWD DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) ON THE VERTICAL STABILIZER TO FUSELAGE. THE FWD DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026101601943Drag Angle · crackedCRACKED AFT DRAG ANGLE BTWN 55.62% STR DATUM TO 61.56% STR DATUM ON THE VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026102001962Drag Angle · crackedCRACKED VERTICAL STABILIZER TO FUSELAGE RT AFT DRAG ANGLE BTW, 55.62% DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026102001963Drag Angle · crackedCRACKED VERTICAL STABILIZER TO FUSELAGE LT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.SDR REXA2026091401827Drag Angle · crackedRH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED R/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.SDR REXA2026091401826Drag Angle · crackedLH VERTICAL STAB AFT DRAG ANGLE IS CRACKED REMOVED CRACKED DRAG ANGLE AND LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE L/H VERT. STAB AFT DRAG ANGLE P/N AV670-21186-003 IAW CRJ-900 SRM 51-40-11-001-001-A01, AND 51-42-13/21/22-001-001-A01.SDR REXA2026091401825Drag Angle · crackedLH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED L/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.SDR REXA2026091001786Drag Angle · crackedCRACK ON RH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. RH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR REXA2026091001785Drag Angle · crackedCRACK ON LH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. LH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR HNAA2026081400700Drag Angle · crackedVERTICAL STAB TO FUSELAGE RH SIDE FWD DRAG ANGLE HAS MULTIPLE CRACKS. RAR THE RH VERTICAL STABILIZER FWD DRAG ANGLE IAW EMB 145 SRM 51-40-02SDR VNAA202608210008Drag Angle · crackedCRACK ON FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE) WAS REPAIRED PER CRJ 700 SRM 55-31-00-201-001-A01SDR AALA202607106503Attach Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STAB AFT MOUNT O/B FWD ATTACH FITTING HAS PITTING CORROSION. MAINTENANCE REPLACED VERTICAL STAB AFT MOUNT O/B FWD ATTACH FITTING IAW AARD 51-00-05-1.SDR VNAA202608210006Drag Angle · crackedCRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE).WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01SDR VNAA202608210004Drag Angle · crackedCRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE). CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE) WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01. PAX DOOR HINGE PN 601R318073-5 WASSDR SWAA2026072944661Lug · corrodedFOUND SURFACE CORROSION ON AFT FACE OF RT HORIZONTAL STAB CENTER SECTION LOWER LUG, AS PER EA 26-155-01728 THE CONFIGURATION IS ACCEPTABLE.SDR SWAA2026072944812Lug · corrodedFOUND SURFACE CORROSION ON AFT FACE OF LT HORIZONTAL STAB CENTER SECTION LOWER LUG. AS PER EA 26-155-01709 THE CONFIGURATION IS ACCEPTABLE.SDR VNAA20260623033Intercostal · corrodedHN00275235 DISCREPANCY: AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27R AND STGR 26L CORRECTIVE ACTION: REMOVED DESCREPANT INTERCOSTAL, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE P/N(SH670-32075-3S) INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01SDR VNAA20260623031Intercostal · corrodedAVI DOOR INTERCOSTAL IS CORRODED AT STGR 26R. REMOVED DESCREPANT DIAPHRAM, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE. DIAPHRAM IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01.SDR SWIA2026061976763Drag Angle · crackedVERTICAL STAB. RT FWD DRAG ANGLE HAS A POSSIBLE CRACK. EVALUATED AND PERFORMED REPAIR AT VERTICAL STAB. RT FWD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.SDR REXA2026082601654Drag Angle · crackedCRACKED AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRMSDR REXA2026082601653Drag Angle · crackedCRACKED AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRMSDR VNAA202607280002Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUSDR REXA2026072801191Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRM SDR REXA2026062900987Drag Angle · crackedTHERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE. STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ900 SRM 51-26-01-001-001-A01. FOUND FWD DRAG ANGLE TO BE VISUALLY CRACKED 2.35"L, REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW SRM 51-42-06-0SDR SWIA2026060277686Drag Angle · crackedRIGHT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE IS CRACKED MX32369431 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01 SEE CONTINUE CARD FOR DETAILS COMPLIED WITH TASK CARD 51-SDR SWIA2026060277631Drag Angle · crackedLEFT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE IS CRACKED. COMPLIED WITH LT SIDE VERT STAB LOWER FWD DRAG ANGLE REPAIR IAW SRM 55-31-00-201-001-A01. COMPLIED WITH SKY CARD 51-900-1003-SKY.SDR VNAA202607120004Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. (ET) HFEC INSPECTION WAS PERFORMED 01 CRACK WAS FOUND ON AFT DRAG ANGLE AND FWD DRAG ANGLE NO CRACKS WERE FOUND. IAW NDT SDR VNAA202607120003Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER SRM 55-31-00-201-001-A01SDR SWIA2026053177682Drag Angle · crackedRH SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACK MX32358189 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT SIDE VERTICAL STABILIZER LOWER AFT DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01 SEE CONTINUE CARD FOR DETAILS COMPLIED WITH TASK CARD 51-SDR SWIA2026052577625Drag Angle · crackedLEFT SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACKED. COMPLIED WITH LT SIDE VERT STAB LOWER AFT DRAG ANGLE REPAIR IAW SRM 55-31-00-201-001-A01. COMPLIED WITH TASKCARD 51-900-1002-SKY.SDR REXA2026052600612Drag Angle · crackedLH FWD DRAG ANGLE IS CRACKED. COMPLIED WITH CRJ900 SRM REPAIR 55-31-00-201-001-A01 ON L/H FWD DRAG ANGLE.SDR SWIA2026051876877Drag Angle · crackedVERT STAB LH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AT VERT STAB LH AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE: 2016-11-10.SDR SWIA2026051876876Drag Angle · crackedVERT STAB RH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AFT DRAG ANGLE AT RH VERT STAB IAW BOMBARDIER REO 670-55-31-018 DATE: 2016-11-10, CRJ550 SRM 51-26-01, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S072326-2 DATE INSSDR REXA2026060400927Drag 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). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATSDR REXA2026060400926Drag 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 (TRACE SDR SWIA2026042176430Drag Angle · crackedLH FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED LT FUSELAGE TO VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.SDR SWIA2026042176379Drag Angle · crackedRIGHT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED RT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.SDR VNAA20260418004Drag Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER SDR REXA2026042300310Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-9SDR REXA2026051500591Drag Angle · crackedINITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE SDR REXA2026051500590Drag Angle · crackedINITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACSDR HNAA2025052000424Drag Angle · crackedRIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.SDR CALA2026040915240Lug · corrodedLEFT HORIZONTAL STAB LWR AFT ATTACH POINT LUG AFT FACE HAS CORROSION AROUND BUSHING AT THE 6 O'CLOCK POSITION. ATTACH POINT K. REPAIRED THE LT STAB ATTACH POINT K AND REPLACED BUSHINGS IAW REO-G25884 REV IR AND ECRA 5510-03355.SDR REXA2026042300315Drag Angle · crackedINITIAL INSPECTION: CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATSDR SWIA2026031677389Drag Angle · brokenVERTICAL STAB RT AFT DRAG ANGLE HAS WORKING FASTENER. REMOVED AND REPLACED FASTENER ON VERTICAL STAB RT AFT DRAG ANGLE REF REO 670-55-31-209 REV -A DATED 2026-05-28COMPLIED WITH 51-900-1002-SKYSDR REXA2026050700519Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. COMPLETE: LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER SRM 55-31-00-201- 001SDR REXA2026050700504Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 001-ASDR REXA2026050700497Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 0SDR REXA2026050500460Drag Angle · crackedCRACK ON RH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER CRACK ON RH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
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