JASC 5531
Service difficulty reports · 1,234
Reports filed under 5531 · Vertical Stabilizer, Spar/Rib, 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 = '5531' 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 = '5531' 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 JGVR20240212001Spar · corrodedFOUND 2 SPOTS OF CORROSION ON AFT VERTICAL SPAR. FOUND DURING TASK 55-30-00-2200 DURING CORROSION BLEND OUT, FOUND CORROSION TO BE GOING UNDER FASTENER HEAD ON VERTICAL STABILIZER AFT SPAR LH LOWER AREA. MECHANICALLY BLENDED 2 AREAS OF CORROSION ON AFT VERTICASDR DALA2024011000405Unknown · unknownSHIP 185 VERTICAL STABILIZER R/H SIDE AUXILIARY SPAR PANEL BETWEEN FSS195 AND FSS295 FOUND DELAMINATION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 614667-14 (0144755)SDR SWAA2024011531924Rib · crackedCRACK ACCESS PANEL 321A INTERNAL CAVITY RIB 8 VERTICAL STABILIZER 2023-758466<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOC ON ACCESS PANEL 321A INTERNAL CAVITY VERTICAL STABILIZER IAWSDR JGVR20231113001Unknown · unknownRH VERT AFT SPAR IS HEAVILY CORRODED. LOCATED ABOVE RUDDER UPPER HINGE. REPAIRED 2 BLENDED AREAS OF VERTICAL STABILIZER R/H AFT SPAR CAP AT APPROXIMATELY VFS 172 AND VFS 237 DUE TO CORROSION PER AQRD ERO-108612 REV. IR, TITLED,"RFTS-108612 - N370QS - VERTICAL SDR VNAA202401050006Drag Angle · crackedINITIAL INSPECTION': CRACK 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). (SM). : CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DASDR VNAA202401050005Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STRG DATUM TO 67.5% REAR SPAR DATUM TRACE BL0.00 SM. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01.SDR DALA2023112809766Unknown · unknownAD RELATED. DTE ERA 613198-14 REV ORIGINAL. ERA ISSUED FOR VERT STAB FRONT SPAR REPAIR AT ZFS=43.000, RHS. DAMAGE TOLERANCE EVALUATION REQUIRED ADDL TIME RLTD MON #0078171. DAMAGE TOLERANCE EVALUATION REQUIRED. DTE LOG #0040724 NO LONGER LIMITED TO 30 DAYS. ERSDR 2023F00318Spar Cap · corrodedCORROSION FOUND ON AFT RH OUTBOARD VERTICAL SPAR CAP VFS 168.94. ACCOMPLISHED FIELD REPAIR-CORROSION, VERTICAL STABILIZER, RH VERTICAL SPAR CAP IAW TEXTRON AVIATION FIELD REPAIR FR-680-0126-12539 DATED 10/23/2023.SDR SWAA2023112115299Rib · crackedCRACK ON RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-659208<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW SRM B737-700 SDR 2023FA0000598Spar Cap · corrodedNJA CORROSION FOUND ON LEFT-AFT-VERTICAL-STAB SPAR CAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING MEMO DQ41418M1 DATED 10/5/2023.SDR SWAA2023110809580Rib · crackedCRACK ACCESS PANEL 321A RIB 8 VERTICAL STABILIZER 2023-635448<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24.;[02] REPLACED RIB ACCESS PANEL 321A RIB 8 VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWINSDR JGVR20231005003Unknown · unknownREPAIRED THE FORWARD SPAR OF THE VERTICAL STABILIZER BY MECHANICALLY BLENDING CORRODED AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIR SHIM, AND RSDR HNAA2023111600408Unknown · unknown55-2327 RH VERTICAL STAB AT SPAR 3 VF63.3 ON CLOSING ANGLE, 1 COUNTERSINK DAMAGED. REPAIRED IAW ETD2023-145-025921, ETD 2023-145-019907, AND PIEDMONT EO1-53-23-0333SDR SWAA2023100699967Rib · crackedCRACK RIB 8 ACCESS PANEL 321A ON VERTICAL STABILIZER 2023-575373<[01] REPLACED RIB 8 LOCATED ON ACCES PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 174A0103; SHEET 1; REV -<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] COMPLETE TASK SDR SWAA2023100697945Rib · crackedCRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-568772<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOCATED ON ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-10SDR SWAA2023092695043Rib · crackedL/H HORIZONTAL STABILIZER HAS A CRACKED VERTICAL STIFFENER 3RD FROM L/E AT INSPAR RIB 6 CORRECTION: STAB STA 129.5 (INSPAR RIB 5)<[01] REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INPSAR RIB AT STA 129.50 3RD VERTICAL STIFFENER FROM LEADING EDGE AND INSDR SWAA2023092192137Rib · crackedDORSAL FIN RIB #1; (MOST FWD) HAS A CRACK ON ITS LEFT SIDE ON LOWER ANGLE.<[01] REMOVED AND REPLACED DORSAL FIN RIB #1; (MOST FWD) AS PER SRM 51-40-02-0G-0;[02] VERIFIED.SDR SIMA20230809001Unknown · unknownVERTICAL STABILIZER TRAILING EDGE RIB# 9/10 IS CRACKED. (MAJOR REPAIR) -C/A-PERFORMED PERMANENT REPAIR TO VERICAL STABILIZER TRAILING EDGE RIB# 9/10 IAW ERS-EJ-55MR-997.SDR SWAA2023082382265Rib · crackedDORSAL FIN RIB # 1 CRACK.<[01] REMOVED AND REPLACED FIRST FWD RIB OF DORSAL FIN; REF B737 SRM 51-40-02-0G-0 AND DWG #174A1008;[02] VERIFIED RIB REPLACEMENT.SDR DALA2023071205667Unknown · unknownFOUND ONE CRACK INDICATION ON RH VERTICAL STAB WHILE PERFORMING AA5530-01048 AND AD 2018-10-08 (MARKED). ONE CRACK INDICATION RH VERTICAL STAB IN SPAR AND WHILE REINSPECTING AREA IN QUESTION WHILE PERFORMING AA5530-01048 AND AD2018-10-08. COMPLIED WITH ER/A 61SDR DALA2023071205666Unknown · unknownR/H VERTICAL STAB, WHILE ACCOMPLISHING INSPECTION PER WORK CARD 5530-0148-02 FAA AD 2018, FOUND A CRACK INDICATION TO ONE HOLE OF THE FRONT SPAR CAP. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 0. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 1. COSDR DALA2023071305676Unknown · unknownFOUR CRACK INDICATIONS ON LH VERTICAL STAB WHILE PERFORMING AA5530- 01048 AND AD 2018-10-08 (MARKED). REINSPECTED AREA FOUND 3 CRACK INDICATIONS IN LOWER SPAR CAP WHILE PERFORMING AA5530-01048 AND AD 2018-10-08. THE ABOVE 3 CRACK INDICATIONS ARE ON LT LOWER SKSDR SWAA2023080476690Rib · crackedCRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-431281<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOCATED ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10SDR SWAA2023072572358Rib · crackedCRACK DORSAL FIN SUPPORT BRACKET RIB #8 AT VERTICAL STABILIZER 2023-409650<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED SUPPORT BRACKET RIB #8 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ISDR SWI2023F00185Unknown · crackedR/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO RH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DASDR SWI2023F00184Unknown · crackedR/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO RH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DASDR SWI2023F00189Unknown · crackedL/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DASDR SWIA20230821620Unknown · crackedL/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DASDR SWI2023F00183Unknown · crackedR/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO RH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATESDR SWI2023F00182Unknown · crackedR/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO RH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATESDR SWI2023F00181Unknown · crackedL/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATESDR SWIA2023081620Unknown · crackedL/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO LH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATESDR SWIA20230612Unknown · gougedVERITCAL STAB REAR SPAR AS A GOUGE WITH RAISED METAL ON THE RH TRAILING EDGE (MARKED). (C-CHECK RO 7/23/2023) REPAIRED VERTICAL STAB REAR SPAR GOUGE TO MHIRJ REO 601R-55-31-448 REV -- DATED 2023-06-20COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL60SDR SWAA2023070658289Rib · crackedCRACK ON RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-378132<[01] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.- SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED <BRSDR EBVR202305180001Unknown · unknownCORROSION FOUND ON VERTICAL STAB SPAR LH CAP ANGLE BETWEEN VFS 180-184. REPAIRED USING TEXTRON FIELD REPAIR FR-680-0245-11912 AND 8100-9 DATED 17MAY2023. THIS IS A MAJOR REPAIR.SDR DALA2023051603907Unknown · unknownSHIP 191 FOUND DELAMINATION ON VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN AFT AREA AT LH SIDE ABOUT FSS 170. CORRECTIVE ACTION: VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN REPAIRED AT LH SIDE ABOUT FSS 170 AS PER B767-300 SRM 55-30-01-2R-1SDR DALA2023051503838Unknown · unknownSHIP 191 FOUND DELAMINATION ON VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN AFT AREA AT LH SIDE ABOUT FSS 245. CORRECTIVE ACTION: VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN REPAIRED AT LH SIDE ABOUT FSS 245 AS PER B767-300 SRM55-30-01-2R-1&SDR DALA2023051503837Unknown · unknownSHIP 191 FOUND DELAMINATION ON VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN MID AREA AT LH SIDE ABOUT FSS 65. CORRECTIVE ACTION: VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN REPAIRED AT LH SIDE ABOUT FSS 65 AS PER B767-300 SRM 55-30-01-2R-1 &SDR R61A2023050800268Shear Tie · corrodedWHILE IN HEAVY CHECK - THERE ARE TWO CHAFE MARKS JUST AFT OF VOR ANTENNA ON VERTICAL RIB 14 AS MARKED. REPLACED RIB 14 PER SRM 51-40-SDR A6WA202304018623Bushing · unknownHORIZONTAL AND VERTICAL STAB PIVOT BUSHINGS ARE WORN BEYOND LIMITS. ******AIRCRAFT REMOVED FROM SERVICE****** HORIZONTAL AND VERTICAL STAB PIVOT BUSHINGS ARE WORN BEYOND LIMITS. P1A- L=2.00IN X W 0.1968IN X D=0.001IN P1B- L=2.00IN X W 0.3543IN X D=0.002IN. SDR SWAA2023050122241Pan · crackedCRACK ACCESS PANEL 321A RIB 8 AT VERTICAL STABILIZER 2023-219724<[01] REPLACED RIB 8 AND FASTENERS LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 174A1008 SHEET 2 REV C. SEE INDIVIDUAL SIGN-OFF BELOW;SDR 2A6R2023032966805Rib · corrodedCORROSION AND CRACK DAMAGE WAS DISCOVERED ON THE VERTICAL FIN TOP RIB (PN: L535A3501202). THE TOP RIB WAS REPLACED WITH A NEW RIB. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-ECSDR SWAA2023041113290Rib · crackedCRACK ON RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-180769<[01] REPLACED RIB 8 LOC ON ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008 REV C AND DWG 174A0103 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COSDR A6WA202303028473Skin · dentedDENT NOTED ON R/H VERTICAL STAB BETWEEN RIB#3-RIB #4 AFT OF MID SPAR AND APPROX 14" T/E ****AIRCRAFT REMOVED FROM SERVICE******** REPAIRED PER CRJ-200 SRM 55-31-31SDR DALA2023022701431None · noneFOUND 2 HOLES WITH CRACK INDICATIONS ON LH VERT STAB FRONT SPAR CAP FWD FLANGE, REF AA 5530-01048 AND AD 2018-10-08. REMOVED LH FASTENERS FROM VERT LEADING EDGE. REMOVED VERT LEADING EDGE PER B717 AMM 55-32-01. C/W BHEC OF SEPERATED LAYERS, FOUND CRACK INDICATSDR SWAA2023021089322Rib · crackedCRACK ACCESS PANEL 321A RIB 8 AT DORSAL FIN VERTICAL STABILIZER 2022-708720<[01] REPLACED ANGLE RIB 8 AT DORSAL FIN VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008. SHEET 2 REV: C;[02] REPLACED ANGLE RIB 8 AT DORSAL FIN VERTICAL STABILIZER IAW BSDR SWAA2023012385673Rib · crackedCRACK ON RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER. REPLACED RIB 8 OF ACCESS PANEL 321A AT VERTICAL STABILIZER AND FASTENERS IAW SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG 174A 0103 SHEET 1 REV -.SDR SWAA2023013080800Rib · crackedCRACK ON RIB 8 LOC DORSAL FIN 321A AT VERTICAL STABILIZER 2022-691651<[01] REPLACED RIB 8 LOC DORSAL FIN 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 DWG #174A1008 SHEET 2 REV. C SEE INDIVIDUAL SING OF BELOW TOOL USED CALIPER P/N: 700-113-10 S/N: 0033SDR SWAA2023011077891Rib · crackedDORSAL FIN ACCESS PANEL 321A FWD RIB #8 ASSY CRACKED P/N 174A1008-2<[01] LOCATED & DRILLED NEW RIB P/N: 174A1108-2; AS PER DWG. 174A1008 & SRM 51-40-02-0G-0.(JOB ACCOMPLISHED BY: W.C.#372).;[02] LATE ENTRY: REMOVED DAMAGE RIB #8 AT DORSAL FIN PANEL 321A; AS PESDR SWAA2022122972922Rib · crackedDORSAL FIN #1 RIB CRACKED, FIRST FWD RIB. REMOVED AT DORSAL FIN RIB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW RIB IAW SRM 51-40-02-0G-0, AND DWG 174A0101. INSTALLED THE NEW RIB IAW 51-40-02-0G-0, AND DWG 174A0101.
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