JASC 5532

Service difficulty reports · 1,753

Reports filed under 5532 · Vertical Stabilizer, Plate/Skin, 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 = '5532'
  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.

SDR AALA202503289094Skin · crackedAIRCRAFT WAS GROUNDED: FOUND CRACK ABOUT 2 INCH LONG ON TOP OF HOLE (BAY) 15 BETWEEN STAB STA 196.663 AND 205.663. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).Mar 26, 2025 · N915NN · Boeing 737823SDR UIEA2025031800355Skin · corrodedVERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".(<P>VERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".THE VERTICAL STABILIZER LEADING EDGE TIP HAS BEEN REPLACED. NO FURTHER DEFECTS NOTED</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0SDR UIEA2025031800356Skin · corrodedVERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A).<BR>(<P>VERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A) WAS REPLACED IAW SRM 51-10-02-0G-0 REV. 127 15-DEC-24.Mar 24, 2025 · N642GT · Boeing 7673Y0SDR JGVR20250320003Skin · corrodedREMOVED NUT PLATES FROM PANELS LANDS TO ACCESS CORROSION AND MECHANICALLY REMOVED ALL AREAS OF CORROSION BEHIND VERTICAL STABILIZER PANELS 341ER, 341DR, 341CR, 341BR, AND 341AR, 341AL, 341BL, 341CL, AND 341DL, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITIONMar 20, 2025 · N323QS · Cessna 680CESDR SWAA2025041515486Skin · corrodedCROWN SKIN UNDER VERT STAB HAS AREAS OF SURFACE CORROSION FROM STA 1016 TO STA 1040 AND S-2AL TO S-2AR (MARKED) <[01]. AS PER EA 25-153-00790; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTIONMar 18, 2025 · N212WN · Boeing 7377H4SDR SWAA2025050606464Skin · corrodedCORROSION ON UPPER FUSELAGE SKIN UNDER VERTICAL STAB LBL12 TO RBL12 BS1016 - BS1078 WL308.5. MARKED<[01] UPDATED TABLE; COMPLETED STEP 9.;[02] ' AS PER EA 25-153-00791; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS Mar 17, 2025 · N7815L · Boeing 73776QSDR DALA2025031401971Skin · gougedBANANA FAIRING ATTACH SCREWS HAVE GOUGED INTO THE L/H STABILIZER SKIN PANEL. MAINTENANCE REPLACED LH VERT STAB SKIN TIP PER B717 SRM 51-40. (LP #6408784)Mar 12, 2025 · N961AT · Boeing 717200SDR IPXA2025030711177Skin · debondedDISBOND, VERTICAL STABILIZER COMPOSITE PANEL DISBOND, P/N: 175T2001-2..PERFORMED NDT/UT FOR REPAIRED AND 8 INCHES HEAT BLANKET AREA, I.A.W.767 NDT MANUAL PART 1,51-01-01 & 51-04-00 REV:140 RESULT:NO DEFECT WAS FOUND. ACCOMPLISHED THE REPAIR PER 767-300F SRM (RMar 7, 2025 · N311UP · Boeing 76734AFSDR IPXA2025032604139Skin · crackedEMPENNAGE PANEL 322AL HAS A CRACK DOT 113-11(DARIO CAMACHO). INSTALLED VERTICAL STAB L/E PANEL 322AL IAW A300 AMM 55-32-11/401 P/N 04-001-0306 BATCH 0004378368.Feb 28, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025031252215Panel · debondedDISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N:186U1002-2 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). REPAIR DISBOND ON LH FWD LWR VST FORWARD TORQUE BOX PANEL I.A.W. EGAT EI NO. F2025A55M-398 REV.1 AND UPS EO-93198-REQ1 REFeb 26, 2025 · N579UP · Boeing 74745ESDR IPXA2025031252237Panel · debondedDISBOND, FOUND L/H VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL, P/N: 186U1001-2 (EXCEED SRM LIMITATION 200 SQUARE INCHES) (REPAIR). REPAIR DISBOND DAMAGE ON LH AFT LWR VST FORWARD TORQUE BOX PANEL I.A.W. EGAT EI NO. F2025A55M-394 REV.1 AND UPS EO-93197Feb 26, 2025 · N579UP · Boeing 74745ESDR DALA2025022501463Skin · dentedDENT ON LT VERTICAL STAB HAD TEMP REPAIR COMPLETED SRM 55-30-01-2R REPAIR 3 PROCEDURE 1. MONITOR NEEDS OPEN FOR PERMANENT REPAIR. "SUPPLEMENTAL INFO" SLN 02/21/25. CHANGED STAB DAMAGE LOCATION FROM LEFT SIDE TO CORRECT LOCATION AS RIGHT SIDE STAB. DUE TO ADDITFeb 21, 2025 · N391DA · Boeing 737832SDR SWAA2025021891428Access Panel · crackedCRACK ACCESS PANEL 321A RIB 8 VERTICAL STABILIZER 2025-91976<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 29 JAN 26.;[02] REPLACED RIB 8 AND FASTENERS LOCATED ON VERTICAL STABILIZER ACCESS PANEL 321A I.A.W B737-700 SRM 51-40Jan 30, 2025 · N934WN · Boeing 7377H4SDR SWI2025F00159Skin · crackedUPON REMOVAL OF VERTICAL LEADING EDGE, FOUND VERTICAL STABILIZER SUPPORT FLANGE CRACKED ON RH SIDE JUST FORWARD OF PANEL 323GR. (C-CHECK RO 2/15/2025) REPAIRED VERTICAL STABILIZER FWD SPAR AT LEADING EDGE SUPPORT FLANGE WITH DOUBLER REPAIR REF ETD2025-1Jan 12, 2025 · N614CZ · Emb ERJ170200LRSDR DALA2025010800161Access Panel · crackedSHIP 3147 CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 622453-14. (0750031)Jan 7, 2025 · N347NB · Airbus A319114SDR DALA2024122311905Access Panel · erodedSHIP 3145 EROSION ACCESS PANEL 322CL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 622096-14. (0721879)Dec 21, 2024 · N345NB · Airbus A319114SDR DALA2024122411967Skin · delaminatedSHIP 1819 RH VERT STAB AUXILIARY SPAR TO FRONT SPAR EXTERNAL SKIN AT FSS 220 TO FSS 245 AREA FOUND DELAMINATION. CORRECTIVE ACTION: REPAIRED RH VERT STAB AUXILIARY SPAR TO FRONT SPAR EXTERNAL SKIN AT FSS 220 TO FSS 245 AREA DELAMINATION AS PER B767-400 SRM 55-Dec 20, 2024 · N843MH · Boeing 767432ERSDR DALA2024121711768Skin · damaged-AD- WEAR AND ELONGATED COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE. SUMMARY OF NRC 00053: COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE WERE REPAIRED PER ERA 621994-14AD REV ORIGINAL. ASSOCIATED ER/A 14-6219Dec 17, 2024 · N978AT · Boeing 717200SDR DALA2024121611720Access Panel · delaminatedSHIP 3145 DELAMINATED ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 622095-14. ( 0708952)Dec 13, 2024 · N345NB · Airbus A319114SDR DALA2024121611734Skin · crackedELONGATED HOLES AND CRACKS ON COUNTERSINK OF PANEL 370CR. SUMMARY OF NRC 00658: PANEL 370CR WAS REPAIRED PER ERA 622046-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622046-14 REV 1. ASSOCIATED ER/A 14-622046.Dec 12, 2024 · N978AT · Boeing 717200SDR IPXA2025022628255Access Panel · damagedEO-92254-REQ1 (MD11: RIGHT SIDE LOWER VERTICAL STABILIZER AFT ACCESS PANEL DAMAGE REPAIR - ACCOMPLISHED A DETAILED INSPECTION AT AND AROUND THE TRIM OUT, VERIFIED ALL DAMAGES HAS BEEN REMOVED. I.A.W. EO-92254Dec 10, 2024 · N251UP · Doug MD11FSDR DALA2026021100989Skin · delaminatedLEFT SIDE OF TAIL SHOWING PAINT LOSS OR DELAMINATION NEAR LEADING EDGE ON CAPTAINS SID. CORRECTIVE ACTION: FOUND LEFT SIDE OF TAIL DELAMINATION NEAR LEADING EDGE ON CAPTAINS SIDE AND PERFORMED INTERIM REPAIR AS PER ER/A 631907-14 (6716370)Dec 8, 2024 · N825MH · Boeing 767432ERSDR DALA2024120511453Panel · crackedSHIP 3135 CRACK ACCESS PANEL 322BL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 322BL LEADING EDGE ON VERTICAL STABILIZER AS PER ER/A 622599-14. (0694090)Dec 5, 2024 · N315NB · Airbus A319114SDR DALA2024120511471Strip · deterioratedVERTICAL STAB - BOTH SIDES HAVE THE UPPERMOST (4EA RUNNING FORE AND AFT) LIGHTNING STRIPS DETERIORATING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0280:2021-2059/003 00099 REPAIRED LIGHTNING DIVERTER STRIPS IAW ADec 2, 2024 · N140DU · Airbus BD5001A10SDR DALA2024120211316Panel · crackedSHIP 3134 CRACK ACCESS PANEL 322CL ON VERTICAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 322CL ON VERTICAL STABILIZER AS PER ER/A 621959-14. (0687479)Dec 1, 2024 · N334NB · Airbus A319114SDR JGVR2024112600874Skin · corrodedCORROSION FOUND ON VERTICAL STAB AT RH TOP. BLENDED AND REMOVED CORROSION FROM VERTICAL STAB AT RH TOP LOCATION TILL VISUALLY REMOVED, VERIFIED WITH 10X MAGNIFYING GLASS. COMPLIED WITH ERO-982547 REV. IR, DATED NOV. 25, 2024. N387QS VERTICAL STABILIZER RH SKINNov 26, 2024 · N387QS · Cessna 680CESDR 2024F00305Skin · crackedVERTICAL STABILIZER RH SKIN CRACK (REF AQRD ENGINEERING REPAIR ORDER # ERO-982598)Nov 25, 2024 · N643QS · Cessna 560XLSDR DALA2024112711260Fastener · loose-AD- FOUND LOOSE FASTENERS ON RH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY NRC 018-0001:5530-01048-02 / 002 00005: CHECK IF THE FASTENER(S) HOLE COUNTER SINK AND DIAMETER ARE WITHIN LIMITS LISTED IN SERVICE GENERAL DRAWING SGNov 24, 2024 · N997AT · Boeing 717200SDR DALA2024112611225Fastener · loose-AD- FOUND LOOSE FASTENERS ON LH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY OF NRC 018-0001:5530-01048-02 /001 00004: CHECKED AND FOUND OK. SUMMARY OF NRC 018-0001:5530-01048-02/001 00004: CMOR VERIFIED LH FASTENER HOLES LIMITNov 24, 2024 · N997AT · Boeing 717200SDR TSAA2024112600001Cover · erodedEROSION (1.0" X 1.0") AT HF ANTENNA COVER OF VERTICAL STABILIZER LEADING EDGE AT LE STA 90. PERFORMED THE EROSION AREA AT HF ANTENNA COVER OF VERTICAL STABILIZER LEADING EDGE AT LE STA 90. APPLIED THE REPAIR PLIES WITH RESIN AND CURED. MADE THE REPAIR SURFACENov 23, 2024 · N301KH · Boeing 737330SDR HNAA2024120101146Skin · cracked55-2383 VERTICAL STAB, AFT OF SPAR 3, LWR LH SKIN PROFILE CRACKED. RAR PROFILE IAW SRM 51-40-02Nov 20, 2024 · N659AE · Emb EMB145LRSDR 2024F00296Skin · nickedDURING ELEVATOR TRAVEL CHECKS NOTICED SKIN DAMAGE AROUND THE TRIM ACTUATOR COVE AREA. UPPER ELEVATOR SKIN AND LOWER TRIM ACTUATOR COVE SKIN.Nov 20, 2024 · N370QS · Gulstm 680SDR DALA2024110710711Access Panel · crackedSHIP 3160 CRACK ACCESS PANEL 322BL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 620762-14. (0647626)Nov 6, 2024 · N360NB · Airbus A319114SDR COEA2024110633759Skin · crackedDURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER FAIRING R/H SIDE CRACK. REPLACED WITH NEW PER SRM 51-40-05 REV. 4.Nov 1, 2024 · N759FX · Textrn 408SDR MTNA20241101001Skin · crackedCRACKS HAVE BEEN FOUND ON THE SKIN BETWEEN THE VERTICAL STABILIZER ACCESS PANELS 347KL AND 347LL.Nov 1, 2024 · N758FX · Textrn 408SDR 2024FA0000799Skin · crackedDURING AIRCRAFT WASH, 18-INCH CRACK FOUND ON LEFT VERTICAL STABILIZER SKIN AND TOP PANEL, BELOW RUDDER COUNTERBALANCE. FOUND LEFT FWD & AFT SKIN TO BE CRACKED AT BEND RADIUS.Oct 30, 2024 · N409BA · Textrn 408SDR IXXA2024102901Access Panel · damagedVERTICAL STAB LE PANEL 321E BLEND OUTS OUT OF LIMITS.Oct 29, 2024 · N331AZ · Boeing 767319SDR DALA2024102810465Access Panel · crackedSHIP 3160 CRACK ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 620652-14. ( 0630993)Oct 27, 2024 · N360NB · Airbus A319114SDR 2025F00041Skin · corrodedDURING THE PERFORMANCE OF THE DOC 15 INSPECTION, IT WAS NOTICED THAT THERE WAS LEVEL II AND LEVEL III COROSSION ALONG THE AFT VERTICAL SPAR OF THE VERTICAL STABILIZER UNDER THE TRAILING EDGE SKIN PANEL ABOUT HALFWAY DOWN FROM THE TOP OF THE SPAR. THE RUDDER WAOct 24, 2024 · N483T · Cessna 680ASDR SWIA2024122301370Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE, AFT DRAG ANGLE POSSIBLY CRACKED. COMPLIED WITH VERTICAL STAB RT AFT DRAG ANGLE REPAIR REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Oct 22, 2024 · N630SK · Cndair CL6002C10SDR DALA2024101810195Access Panel · crackedSHIP 3133 CRACK ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 620487-14. (0614294)Oct 17, 2024 · N333NB · Airbus A319114SDR DALA2024102110260Skin · delaminatedSHIP 197 LH VERTICAL STABILIZER EXTERNAL SURFACE DELAMINATION FROM FUSELAGE 16 INCH AND FROM L/E 34INCH. CORRECTIVE ACTION: REPAIRED LH VERTICAL STABILIZER EXTERNAL SURFACE DELAMINATION FROM FUSELAGE 16 INCH AND FROM L/E 34 INCH AS PER PRI 621518-14. (0611758)Oct 16, 2024 · N197DN · Boeing 767332SDR DALA2024100809826Access Panel · crackedSHIP 3144 CRACK ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER AS PER ER/A 620604-14. (0597110)Oct 7, 2024 · N344NB · Airbus A319114SDR 2024FA0000757Skin · corrodedREPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER SKINS LOCATED NEAR THE UPPER EDGE AND ONE NEAR THE FORWARD EDGE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DEPOSITION, CLEANING, TREATING, PRIMING AND FABRICATING AND INSTALLING REPAIR DOUBLERS IAW AEROOct 7, 2024 · N313QS · Cessna 680ASDR VNAA2024100300012Skin · damagedNDT NOTED DAMAGE AT LH MOST O/B FACE OF TRIM ACTUATOR FITTING ON VERT. STABILIZER NEAR THE FWD AND AFT FASTENERS. BLENDED OUT DAMAGES AT LH MOST O/B FACE OF TRIM ACTUATOR FITTING ON VERT. STABILIZER NEAR THE FWD AND AFT FASTENERS. FOUND WITHIN LIMITS. REF. Oct 3, 2024 · N708PS · Cndair CL6002C10SDR VNAA2024100300011Skin · crackedRH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK. INSTALLED -6 ANGLE DOUBLER AND -8 ANGLE FILLER ON R/H VERTICAL TO FUSELAGE ATTACHMENT AFT DRAG ANGLE REPAIR REF CRJ 700 SRM 55-31-00-201-001-A0.Oct 3, 2024 · N708PS · Cndair CL6002C10SDR IXXA202409280007Structure · damagedLIGHTNING STRIKES ON VERTICAL STABILIZER DIVERTER STRIPS ALONG ENTIRE LENGTHSep 28, 2024 · N491AZ · Boeing 767323SDR IXX202409280009Structure · damagedLIGHTNING STRIKES ON VERTICAL STABILIZER DIVERTER STRIPS ALONG ENTIRE LENGTHSep 28, 2024 · N491AZ · Boeing 767323SDR DALA2024092709477Access Panel · crackedSHIP 3143 CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIR INSTRUCTIONS ON ACCESS PANEL 322BL AT VERTICAL STABILIZER AS PER ER/A 620143-14. (0577592)Sep 26, 2024 · N343NB · Airbus A319114SDR DALA2024092709476Access Panel · crackedSHIP 3143 CRACK ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 620158-14. (0577576)Sep 26, 2024 · N343NB · Airbus A319114
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