JASC 5530
Service difficulty reports · 2,534
Reports filed under 5530 · Vertical Stabilizer, 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 = '5530' 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 = '5530' 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 VNAA2020010800901Angle · crackedLT AFT VERTICAL DRAG ANGLE IS CRACKED FS 1200. COMPLIED WITH REO 670-55-31-018 REV A. APPLIED TOPCOAT IAW SRM 51-25-01-001-001-A01.SDR SWAA2021051321155Skate Angle · chafedSKATE ANGLE IS CHAFED AT B.S. 1016-1026; R.B.L.14; W.L. 308. / REMOVED DAMAGE ON SCATE ANGLE FROM B.S 1016-1026; RBL 14; WL 308 AND ACCOMPLISHED ALL NECESSARY INSPECTIONS AS PER SRM 53-80-71-2R-6 REPAIR 6 PARA 4; STEPS A-G; WITH NO DEFECTS NOTED. FABRICATED LOSDR SWAA000021156Skate Angle · chafedSKATE ANGLE IS CHAFED AT B.S. 1016-1026; L.B.L.14; W.L. 308. / REMOVED DAMAGE ON SCATE ANGLE FROM B.S 1016-1026; LBL 14; WL 308 AND ACCOMPLISHED ALL NECESSARY INSPECTIONS AS PER SRM 53-80-71-2R-6 REPAIR 6 PARA.4 STEPS 1-G; WITH NO DEFECTS NOTED. FABRICATED LOCSDR SWIA2020021848643Structure · cracked*R/H SIDE AT BASE OF VERTICAL STABILIZER THERE IS A SUSPECT CRACK ON AFT SECTION (C-CHECK) RO 2/14/2020 REPAIRED R/H SIDE BASE OF VERTICAL STABILIZER CRACK ON AFT SECTION REF CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA2020021848642Structure · crackedL/H SIDE AT BASE OF VERTICAL STABILIZER THERE IS A SUSPECT CRACK. FWD SECTION (C-CHECK) RO 2/14/2020 REPAIRED L/H SIDE BASE OF VERTICAL STABILIZER CRACK FWD SECTION CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA2020021848641Structure · cracked*L/H SIDE A BASE OF VERTICAL STABILIZER THER IS A SUSPECT CRACK ON AFT SECTION (C-CHECK) RO 2/14/2020 REPAIRED L/H SIDE BASE OF VERTICAL STABILIZER CRACK AFT SECTION CRJ700 SRM COMPLIED WITH SKYWEST TASK CARD.SDR SWAA000027808Skate Angle · chafedUPPER EXTERNAL FUSELAGE L/H AFT SKATE ANGLE HAS CHAFING AT AFT EDGE 1' LONG OB SIDE / CLEANED AREA COMMON TO L/H SKATE ANGLE AFT EDGE 1' O/B SIDE AND FOUND SUSPECTED CHAGE TO BE DEBRIS. PROCEEDED TO CLEAN AREA AS PER B737 SOPM 20-30-84. TREATED; PRIMED AND TOPSDR SWAA2021051326031Skate Angle · chafedVERTICAL FIN L/H SKATE ANGLE HAS CHAFING DAMAGE AT BS1008. / VERTICAL FIN L/H SKATE ANGLE HAS CHAFING DAMAGE AT BS1008 FOUND OUT OF LIMITS DUE TO MORE THAN 50% MATERIAL LOSS IAW SRM 51-10-02. REMOVED AND REPLACED NEW VERTICAL FIN L/H SKATE ANGLE FROM BS1006-BSSDR SWAA2021051326030Skate Angle · chafedVERTICAL FIN R/H SKATE ANGLE HAS CHAFING DAMAGE AT BS1008. / VERTICAL FIN R/H SKATE ANGLE HAS CHAFING DAMAGE AT BS1008 FOUND OUT OF LIMITS DUE TO MORE THAN 50% MATERIAL LOSS. IAW SRM 51-10-02. REMOVED AND REPLACED NEW VERTICAL FIN R/H SKATE ANGLE FROM BS1006-BSDR SWAA2021051326029Skate Angle · chafedVERTICAL FIN R/H SKATE ANGLE HAS MULTIPLE SPOTS OF CHAFING DAMAGE BS1016 - BS1121. / REPAIRED VERTICAL FIN R/H SIDE SKATE ANGLE BTW. BS1016-BS1022 AS PER B737-700-SRM 53-80-71-2R-6 AND CHAFING DAMAGE LOCATED FROM BS1022-BS1121 IS LIMITED TO EXTERIOR FINISH ONLSDR SWIA2020020748291Drag Angle · cracked*RH V/STAB TO FUSELAGE AFT ATTACHMENT DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK) RO 2/05/2020 COMPLIED THE REPAIR AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE REF-CRJ-700 REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK.SDR SWIA201948290Drag Angle · cracked*LH V/STAB TO FUSELAGE AFT ATTACHMENT DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK) RO 2/05/2020 COMPLIED THE REPAIR AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE REF-CRJ-700 REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASDR SWIA2020020748289Drag Angle · cracked*LH V/STAB TO FUSELAGE ATTACHMENT FWD DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK) RO 2/05/2020 COMPLIED THE REPAIR AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE REF-CRJ-700 REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASDR SIMA2020010227006Drag Angle · crackedDURING HMBV INSPECTION, QC FOUND THE LH VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE CRACKED.-C/A-REMOVED AND REPLACED LH VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IAW EMB 145 SRM 51-40-02SDR DALA2019122007451Structure · damagedRHS VERTICAL STAB LEADING EDGE THREE FASTENER HOLES BELOW ZF 52 SPLICE SHOW CRACK INDICATION. CRACK IS NOT IN SKIN. ALL DAMAGED COMPLETE ON PRI 583922-14AD REV 2. INSTALLED VERTICAL LEADING EDGE PER B717 AMM 55-32-01 400-802. LEAK TEST OF RUDDER LIMITER GOODSDR VNAA2019121899903Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED. J.SWINK 11/12/19(JW) M/A: 1. L/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. J.BARTLETT 11/16/19 C/A: 1. UPON FURTHER INVESTIGATION, FOUND LH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRJSDR VNAA2019121899902Drag Angle · crackedRIGHT VERTICAL STAB DRAG ANGLE CRACKED. J.SWINK 11/12/19(JW) M/A: 1. R/H VERTICAL STAB DRAG ANGLE REQUIRES REPAIR IAW CRJ900 SRM 55-31-00-201-001-A01. J.BARTLETT 11/16/19 C/A: 1. UPON FURTHER INVESTIGATION, FOUND RH AFT DRAG ANGLE TO REQUIRE REPLACEMENT IAW CRSDR SWAA2022041211713Seal · crackedR/H STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / REMOVED R/H STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND REPLACED IAW AMM 53-31-31-400-802. 84036U; 13JAN20.SDR SWAA2022041211714Seal · crackedL/H STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / REMOVED L/H STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND REPLACED IAW AMM 53-31-31-400-802. 84036U; 13JAN20.SDR SWAA2022041207477Retaining Clip · crackedCRACK ON PANEL 323AL SKATE ANGLE RETAINER CLIP (MARKED) / REMOVED CRACKED RETAINER CLIP AND LOCATED AND DRILLED UP NEW RETAINER CLIP IAW SRM 51-40-02-0G-0 AND DWG 172A6122 2656U 11DEC19 3074C 11DEC19 INSTALLED NEW RETAINER CLIP ON PANEL 323AL WITH 9EACH RIVETSSDR IPXA2019112769458Panel · delaminatedINSPECTION TYPE:C1LH VERTICAL STAB LOWER FWD TORQUE BOX PANEL DELAMINATED STARTING AT TOP EDGE EXTENDING DOWN APPROX 2.0 FEET AND SPANNING THE ENTIRE WIDTH OF PANELREMOVED AND REPLACEDSDR AALA201911259037Hinge Fitting · wornAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY RUDDER HINGE 5 VERTICAL STABILIZER (0.018") AT STA299, RIB7. REMOVED AND REPLACED HINGE AT RIB 5 IAW A321 SRM 51-72-11-911-001 AMM 55-36-41-400-001.SDR AALA201911259038Hinge Fitting · wornAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY RUDDER HINGE 1 ON VERTICAL STABILIZER (0.028" ) AT STA78, RIB2. REMOVED AND REPLACED HINGE 1 AT RIB2 IAW A321 SRM 51-72-11-911-001 AMM 55-36-41-400-001-A .SDR AALA201911259040Hinge Fitting · wornAIRCRAFT IN BASE VISIT: EXCESSIVE PLAY RUDDER HINGE 2 ON VERTICAL STABILIZER (0.023" ) AT STA193, RIB4. REMOVED AND REPLACED HINGE 2 AT RIB4 IAW A321 SRM 51-72-11-911-001 AMM 55-36-41-400-001-A DWG D55371041.SDR SWAA2019110138430Angle · crackedVERTICAL STABILIZER INTERNAL SIDE LATERAL EXPANSION JOINT ANGLE CRACKED IN RADIUS AT BS. 1016, STR. 2L 3" O/B OF STR. 2L, 8" ABOVE FUSELAGE SKIN / REPAIRED ANGLE IAW SRM & DWG.SDR 2019FA0000366Tube · crackedUPON VISUAL INSPECTION, FOUND THE MOST AFT VERTICAL TUBING OF AIRCRAFT STRUCTURE SHEARED ABOVE TAIL GEAR ATTACH POINT BUT BELOW 45 ANGLE BRACE. THIS WAS THE 2ND IDENTICAL FAILURE ON THE SAME AIRFRAME. FOUND CRACK 739.4 HOURS SINCE LAST REPAIR. AIRCRAFT USED DASDR V0XD20191013001Drag Angle · crackedRIGHT FORWARD VERTICAL STAB DRAG ANGLE CRACKED. CORRETIVE ACTION: REPAIRED RIGHT FORWARD VERTICAL STAB DRAG ANGLE IAW BOMBARDIER REO# 670-55-31-122 REV A DATED 2019-10-01, BOMBARDIER REO# 670-55-31-018 REV A DATED 2016-11-17, AND GOJET EO-C700-55MR-001 REV O DSDR SWAA2022040563688Lug · corroded* CORROSION * VERTICAL STABILIZER FWD ATTACH LUGS AT UPPER FUSELAGE STA 1016 RBL 8 WL 300.8 / REMOVED CORROSION IAW ATS ER 19-05192 REV IR & SWA EA 1-753-35935 REV IR.SDR SWAA2022040563687Lug · corroded*CORROSION* VERTICAL STABILIZER LEFT FWD ATTACH LUGS AT UPPER FUSELAGE STA 1016 LBL 8 WL 300.8 / REMOVED CORROSION IAW ATS ER 19-05192 REV IR AND SWA EA 1-753-35935 REV IR.SDR DALA2019100905810Hinge · wornWEAR ON BEARING HINGE ARM ON THE VERTICAL STABILIZER. REPLACED THE NR 3 HINGE IAW SRM 51-72- 11, SRM 51-42-00, AND DWG 55371052, ISSUE U.SDR IPXA2019102868322Intercostal · crackedINSPECTION TYPE:2CLOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR R/H INTERCOSTAL AFT END IS CRACKED BETWEEN STA. YID=375, XID=-7.1 AND ZID=65.REPAIRED CRACKED LOWER VERTICAL STABILIZER REAR CENTER SPAR TO REAR SPAR R/H INTERCOSTAL AFT END BETWEEN STA.SDR SWAA2022032909210Support · crackedEXTERNAL FUSELAGE; STA 1016; 8' ABOVE LH VERTICAL STAB ATTACH LUG. LONGITUDINAL SUPPORT IS CRACKED IN RADIUS / REMOVED AND REPLACED LONGITUDINAL SUPPORT ABOVE LH VERTICAL ATTACH LUG STA 1016 IAW SRM 51-40-02-0G-0 AND BOEING DWG 176A3101 REV BSDR AALA201910289010Hinge Fitting · wornAIRCRAFT IN BASE VISIT: HINGE FITTING HAS EXCESSIVE PLAY AT STA2985, RIB7 (D=0.013" WEAR (PLAY)). INSTALLED NEW HINGE FITTING IAW SRM 51-72-11-911-001 AND DRAWING D55371041.SDR AALA201910269012Hinge Fitting · wornAIRCRAFT IN BASE VISIT: HINGE FITTING AT STA1926, RIB4 HAS EXCESSIVE WEAR (D=0.012" WEAR (PLAY)). REMOVED AND REPLACED HINGE FITTING IAW SRM 51-72-11-911-001; DRAWING D55371041; AMM 55-36-41-400-001-A.SDR REXA2019101091397Channel · crackedVERTICAL STAB LEADING EDGE PANEL 324AT INNER WEB DAMAGE AT BOTTOM OF LEADING EDGE AND SEVERAL RIVETS PULLED THROUGH. REMOVED AND REPLACED CHANNEL ON L/E OF VERTICAL STAB IAW CRJ200 SRM 51-42-06. WVAC EMP STAMP 771SDR AALA201910159049Hinge · wornAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA201910159046Hinge · wornAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE NR 1 HAS EXCESSIVE PLAY / WEAR AT RIB 1 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR AALA201910159041Hinge · wornAIRCRAFT IN BASE MAINTENANCE. RUDDER HINGE NR 7 HAD EXCESSIVE PLAY AND WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.SDR SWAA2022022538989Retainer · crackedDORSAL FIN AFT RT SEAL RETAINER IS CRACKED / REMOVED AND REPLACED DORSAL FIN AFT RT SEAL RETAINER IAW SOPM 20-50-01; IPC 55-32-11-01.SDR AALA2019083099053Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE, RIGHT ELEVATOR NR 5 HINGE HAD EXCESSIVE PLAY AND WEAR. REPLACED THE HINGE FITTING IAW AMM 55-16-42.SDR AALA2019083099057Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE, LEFT ELEVATOR NR 4 HINGE HAD EXCESSIVE PLAY AND WEAR. REPLACED THE HINGE FITTING IAW AMM 55-16-42.SDR SWAA2022031584016Panel · crackedVERTICAL STAB PANEL 324AR LOWER RETAINER IS CRACKED / REMOVED & REPLACED VERTICAL STAB PANEL 324AR LOWER RETAINER IAW SRM 51-40-02-0G-0.SDR SWAA2022031584021Joint · crackedCRACK IN 'JOINT ASSY - EXPANSION VERT. FIN ' STA 1021.27 WL 308 (P/N 176A3101-26) ON L/H SIDE (MARKED) / REMOVED & REPLACED JOING ASSY - EXPANSION VERTICAL FIN AT STA 1027.27 WL 308 IAW SRM 51-40-02-0G-01 AIPC 53-33-11-02SDR SWAA2019080635649Stiffener · crackedVERTICAL STABILIZER FUSELAGE STA. 1018, 8" ABOVE FUSELAGE SKIN, LBL AND RBL 10", LATERAL SUPPORT RIB STIFFENER AT STRAIN RELIEF RADIUS, CRACKED ON BOTH ENDS. / R&R STIFFENER IAW SRM AND DWG.SDR AALA20190706001Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #4 HAS EXCESSIVE PALY / WORN ON THE VERTICAL STABILIZER AT RIB 6. REPLACED HINGE FITTING PER AMM 55-36-41.SDR AALA201906209011Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE FITTING #2 HAS EXCESSIVE PLAY ON VERTICAL STABILIZER AT RIB 4. REPLACED HINGE FITTING PER AMM 55-36-41.SDR 2019FA0000365Tube · crackedUPON VISUAL INSPECTION, FOUND THE MOST AFT VERTICAL TUBING OF AIRCRAFT STRUCTURE SHEARED ABOVE TAIL GEAR ATTACH POINT BUT BELOW 45 ANGLE BRACE. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 90 DAYS.SDR 2019FA0000364Tube · crackedUPON VISUAL INSPECTION, FOUND THE MOST AFT VERTICAL TUBING OF AIRCRAFT STRUCTURE SHEARED ABOVE TAIL GEAR ATTACH POINT BUT BELOW 45 ANGLE BRACE. AIRCRAFT USED DAILY FOR FLIGHT TRAINING WITH AN AVERAGE OF 100 HOURS OF FLIGHT TIME EVERY 45 DAYS.SDR AALA201906219035Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER #2 HINGE FITTING HAS EXCESSIVE PLAY ON THE VERTICAL STABILIZER AT RIB 4. REPLACED HINGE FITTING PER SRM 51-72-11.SDR SWAA2022031079043Fitting · corroded***CORROSION *** ON L/H FWD VERTICAL STAB BULKHEAD FITTING FWD AND AFT FACE. BS 1016-1088; WL 250 / THE DAMAGE IS REPAIRED UNDER ATS ER 19-03669 REV IR AND EA 1-753-35239 REV IR.
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