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 SWIA202507210024Drag Angle · crackedVERTICAL STAB. LH AFT DRAG ANGLE HAS SUSPECTED CRACK (MARKED). (C-CHECK RO 07/18/2025)REPAIRED VERTICAL STAB LH AFT DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01 REPAIR. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR GTIA2025011638688Hinge Arm · damagedELONGATED HOLE HINGE ARM 5 LOC VERTICAL STABILIZER. INSTALLED NEW HINGE FITTING BR5 AND FASTENERS IAW EA #55-0002-25 PART #2 STEP 4 AND A320 SRM 55-36-42-300-008SDR VNAA20250121006Drag Angle · crackedCRACKS ON RH / LH VERTICAL STABILIZER INTERSECTS WITH THE FUSELAGE ATTACHMENT FWD DRAG ANGLES, (BOTH SIDES). RH / LH VERTICAL STABILIZER INTERSECTS WITH THE FUSELAGE ATTACHMENT FWD DRAG ANGLES, (BOTH SIDES) WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR WRXR20250113003Fairing · wornPANEL 326AR HAS COMPOSITE DAMAGE TO 10 HOLES THAT WILL REQUIRE REPAIR. CLEANED THE DAMAGED AREA USING ALCOHOL AND A LINT FREE CLOTH WIPING DRY PRIOR TO EVAPORATION. CUT PLIES OF CU040CX36 COPPER WIRE MESH TO FIT THE REPAIR AREA. TRIMMED TO FIT.SDR VNAA20250127007Drag Angle · crackedCRACK ON LH/RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LH/RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ASDR VNAA202502110008Drag 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 HNAA2025012100032Profile · cracked55-2160 VERTICAL STAB, AFT OF REAR SPAR 3, RH UPPER PROFILE CRACKED UNDER UPPER RIB. REPAIRED IAW ETD2024-145-900968 REV 1 AND EO 1-53-24-0743SDR VNAA202502110009Drag 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). REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR CALA2024112602956Skate Angle · wornRIGHT VERTICAL STAB. LOWER AREA OF FUSELAGE (SKATE ANGLE) WORN AT STA 1104+ 3. (DOT 013) (REF AAR N/R 9919671) REPAIRED R/H SKATE ANGLE, BETWEEN STA 1104+1.0" TO STA 1104+4.5" AS PER REF B737 SRM 53-80-71-2R-6, FIG 201.SDR CALA2024112602955Skate Angle · wornLEFT VERTICAL STAB. LOWER AREA OF FUSELAGE (SKATE ANGLE) WORN AT STA 1104+ 3. (DOT 012) (REF AAR N/R 9919670) REPAIRED L/H SKATE ANGLE, BETWEEN STA 1104-4.5" TO STA 1104+2.0" AS PER REF B737 SRM 53-80-71-2R-6, FIG 201.SDR SWAA2024121359054Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED FRONT SPAR SUPPORT FITTING RT APROX AT STA 1016 AT VERTICAL STABILIZER 2024-691834<[01] REPLACED SUPPORT BRACKET LOCATED FRONT SPAR SUPPORT FITTING RT APROX AT STA 1016 AT VERTICAL STABILIZER IAW B737 700 SRM 51-40-02-0G AND DWG 1SDR VNAA202412150017Hinge · wornFREE 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 YENA2024111201456Hinge · wornDURING HEAVY MAINTENANCE: CRACK INDICATION ON FASTENER HOLE FR16 RH STOP FITTING 7 UPPER I/B HOLE. CRACK DEPTH IS 0.18; EF AEROMAN W.O. 2024 275/1 NR 538514 * PERFORMED REPAIR ON FR.16 RH DOOR STOP FITTING 7 UPPER I/B HOLE IAW A320 SRM 53-11-12-300-010. THIS RSDR YENA2024111201455Service difficultyDURING HEAVY MAINTENANCE: WEAR ON STRINGER 39R LOCATED BTW FR47 TO FR 48 AFT CARGO COMPARTMENT; REF AERMAN W.O. 2024 275/1 NR 538884 * REMOVED AND REPLACED STRINGER 39R LOCATED ON AFT CARGO COMPARTMENT BWT FR 50 AND FR 51 IAW A320 SRM 51-72-11 AND DWG D5347SDR YENA2024111201454Hinge · wornDURING HEAVY MAINTENANCE: CORROSION STRINGER 31R LOCATED BTW FR64 TO FR65 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN WO 2024 275/1 NR 538820 * REMOVED AND REPLACED STRINGER LOC. FR64 TO FR65 STRG 31RH IAW A320 SRM 51-42-11 AND DWG D53480505, D5348006SDR YENA2024111201453Hinge · wornDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / PRESSURE BULKHEAD / HOLES #2 & 6 / CRACK DAMAGE – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-9052-24 REV. 0 (COVER + PARTS 1-5) /2/ AIRBUS RDAF 81474600/004/2024#A
/3/ AIRBUS MESSDR VNAA20241102002Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACESDR SWIA202412230012Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE, AFT DRAG ANGLE POSSIBLY CRACKED. LT V-STAB AFT DRAG ANGLE CRACK VERIFIED. REPAIRED CRACKED DRAG ANGLE PER CRJ700SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.SDR VNAA202411290008Drag 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). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ASDR VNAA202411290007Drag 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 DATUSDR IXXA2024101802Support Angle · crackedVERT STSB ACCESS PANEL 324AL, FWD SUPPORT ANGLE LH O/B & RH O/B CRACKED AT LWR FASTENERS.SDR VNAA202411240004Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACESDR VNAA202411240003Drag Angle · crackedINITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625% STGR DATUM TOSDR REXA2024110801439Drag Angle · crackedL/H VERTICAL STAB AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED L/H VERTICAL STAB AFT DRAG ANGLE P/N AV670-21186-003 AND INSTALLED NEW LH AFT DRAG ANGLE P/N: AV670-21186-003 IAW CRJ 700 SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-22-001-001-SDR CALA2024100300747Seal · missingPDA 2 THE OUTERMOST HINGE CLOSE OUT PANEL ON THE L/H STABILIZER WAS FOUND MISSING ON ARRIVAL INSTALLED NEW FILLET SEAL P/N 185A1621-117 (M&E 29-2741-3-0300) IAW AMM 27-31-11 AND AMM 20-50-11.SDR VNAA20241103024Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.SDR VNAA20241102003Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.SDR SWAA2024102941552Fitting · corrodedCORROSION FOUND AT VERTICAL FIN FRONT SPAR FITTING LH BOLT HAS PITTING CORROSION.<[01] REMOVED AND REPLACED BOLT AT VERTICAL FIN FRONT SPAR FITTING LH.<BR>REF: AMM 55-30-00-000-801 AND AMM 55-30-00-400-801.<BR>TOOL USED<BR>-TORQUE WRENCH: B/C: 175286; CAL DUE SDR CALA2024101702672Fitting · corrodedFOUND CORROSION AT VERTICAL STAB.FWD RIGHT BULKHEAD FITTING ON THE AFT SURFACE AS PER SCEPTER TRACKING PURPOSE REPAIRED VERTICAL STAB FRONT SPAR RH FUSELAGE AT TUCH FITTING AT B51016 AS PER REF ESF-W1 2022816-12-10802 REV IR AND EC/RA 5380-01403 AS PER AAR WORSDR VNAA20251004002Drag Angle · crackedCRACK WAS FOUND AFFECTING AFT DRAG ANGLES AT LH VERTICAL STAB BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. PERMANENT REPAIR WAS PERFORMED IN ACCORDANCE WITH CRJ- 900 SRM 55-31-00-201-001-A01.SDR SWI2024F01227Drag Angle · crackedVERTICAL STAB RH AFT DRAG ANGLE HAS A CRACK (MARKED) (C-CHECK RO 11/11/2024) FABRICATED AND INSTALLED -6 AFT ANGLE DOUBLER AND -8 AFT ANGLE FILLER FROM 2024-T3 .090" PO# 5-24830 REF. CRJ 900 SRM 55-31-00-201-001-A01. SEE CONTINUE CARD FOR WORK PERFORMEDSDR SWI2024F01233Drag Angle · crackedVERTICAL STAB RH FWD DRAG ANGLE HAS A SUSPECTED CRACK (MARKED). (C-CHECK RO 11/11/2024) CUT AWAY DAMAGE ON RH FWD. DRAG ANGLE AND PERFORMED A DOUBLER REPAIR TO RH FWD. DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD: 51-SDR YENA2024091001236Hinge Arm · damagedDURING HEAVY MAINTENANCE: VERTICAL STABILIZER, HINGE ARM FITTING NO 7 WITH ELONGATED HOLES; REF MEXICANA WO# 1316755 S/N 00332; VERTICAL STABILIZER HINGE ARM FITTING NO 7 WAS REPAIRED IAW TRE2055026 DATE AUG 08/2024, TEMP REPAIR, LIMITATIONS 6 MOS. IAW RDAF 8SDR VNAA20251005023Lug · corrodedAFTER REMOTION OF BUSHINGS OF LH AILERON, CORROSION ON HOUSING OF LUGS : CENTER LUGS L1, L2, L3, L4,L5 L6 ALSO ON HINGE 4 UPPER AND LOWER HOUSING LUGS AT LH AILERON. HOUSINGS WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND REPAIRED PER REO: 670-57-61-23SDR VNAA20251005006Stiffener · out of limitsWEAR ON STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE. STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE WAS REPAIRED PER REO 690-55-32-210 REV - -SDR VNAA20251004008Stiffener · wornDISCREPANCY: WEAR ON STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE.. STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE WAS REPAIRED PER REO 690-55-32-210 REV - .SDR VNAA20251005011Fitting · gougedIN REFERENCE TO CARD TRFKE00BNCEY': 690-55-31-079-PERM REPAIR BEFORE 25,579.22 FH - GOUGE DAMAGE ON V/STAB TRIM ACTUATOR FITTING THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 4200 FLIGHT HOURS FROM THE EXPIRY OF E.A. 23-C9-55-1132 REV "IR" TIMESDR VNAA20251004013Fitting · damagedIN REFERENCE TO CARD TRFKE00BNCEY': 690-55-31-079-PERM REPAIR BEFORE 25,579.22 FH - GOUGE DAMAGE ON V/STAB TRIM ACTUATOR FITTING THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 4200 FLIGHT HOURS FROM THE EXPIRY OF E.A. 23-C9-55-1132 REV "IR" TIMESDR SWIA202411120810Drag Angle · crackedRIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF THE VERTICAL STABILIZER RH SIDE IS CRACKED (C-CHECK RO 10/28/2024) (FILED CLOSED)PERFORMED REPAIR ON RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF VERTICAL STABILIZER RH SIDE PER BOMBARDIER REO 670-55-31-018. REVSDR SWIA20241029810Drag Angle · crackedRIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF THE VERTICAL STABILIZER RH SIDE IS CRACKED (C-CHECK RO 10/28/2024) (FILED OPEN)PERFORMED REPAIR ON RIGHT HAND FORWARD DRAG ANGLE AT THE BOTTOM OF VERTICAL STABILIZER RH SIDE PER BOMBARDIER REO 670-55-31-018. REV.-SDR HNAA2024091100767Channel · cracked55-2392 BOTTOM OF VERT STAB LH TE CHANNEL PROFILE CRACKED ON AFT SIDE OF SPAR 3. RAR CHANNEL PROFILE IAW SRM 51-40-02SDR SWI2024F01135Drag Angle · crackedLH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED THE L/H V-STAB AFT DRAG ANGLE PER CRJ700SRM 55-31-00-201-001-A01. SEE CONTINUATION FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002SDR SWIA20240721Drag Angle · crackedRH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED AFT DRAG ANGLE IN THE RH VERTICAL ROOT REF REO 670-55-31-176 REV -- DATED 2024-08-01, CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CSDR VNAA20250820007Drag Angle · crackedDISCREPANCY: CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5%SDR VNAA20250820006Drag Angle · crackedDISCREPANCY: CRACK 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 67.5SDR AALA202407224067Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL STABILIZER STIFFENER AT BS 1085.5, VERTICAL FIN STA 178.2. REPLACED STIFFENER PER EA 356098.SDR SWI2024F01106Drag Angle · crackedL/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED L/H VERTICAL STABILIZER DRAG ANGLES FWD AND AFT IAW REO 670-55-31-018 REV-- DATE: 2024-08-29, REO 670-55-31-018 REV-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, NSDR SWI2024F00907Drag Angle · crackedL/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED OPEN)REPAIRED L/H VERTICAL STABILIZER DRAG ANGLES FWD AND AFT IAW REO 670-55-31-018 REV-- DATE: 2024-08-29, REO 670-55-31-018 REV-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, NDTSDR SWIA20240717Drag Angle · crackedR/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED OPEN)REPAIRED R/H VERTICAL STABILIZER AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-177 REV.-- DATE:2024/08/22, REO 670-55-31-018 REV.-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, SDR YENA2024071601021Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 5 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00035) REMOVED AND REPLACED HINGE FITTING #5 LOCATED ON VERTICAL STABILIZER IAW A320 SRM 51-72-11-911-001 AND DRAWING #D 5571052 IS
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