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 YENA2024041600560Skin · unknownDURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322CL / OUTER SKIN / RE-SKIN – STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600547Skin · unknownDURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322AL / OUTER SKIN / RE-SKIN – STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600545Panel · unknownDURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322AL / OUTER SKIN / RE-SKIN – STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR DALA2024041204365Panel · crackedSHIP 5648 RUDDER LH SIDE AFT OF VERT STAB PANEL 324DL HAS NUMEROUS AREAS OF CHIPPED PAINT EXPOSING COMPOSITE. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON RUDDER LH SIDE AFT EDGE AT RUD STA 229 IAW NB757-200 SRM 55-40-01-2R-1 AND B757-200 SRM 51-70-04-0G. (028878Apr 11, 2024 · N548US · Boeing 757251SDR IXXA2024040501Skin Panel · delaminatedVERTICAL STAB. SKIN PANEL DELAMINATED.Apr 5, 2024 · N389AZ · Boeing 767319SDR 2024FA0000292Skin · corrodedMULTIPLE AREAS OF CORROSION FOUND ON THE COVE, LEFT AND RIGHT OF THE VERTICAL SKIN. THE NETJETS REQUEST FOR TECHNICAL SERVICES (RFTS) RFTS-110558 REV. 0 DATED APRIL 04, 2024 WAS ACCOMPLISHED TO REPAIR THE COVE, LEFT AND RIGHT OF THE VERTICAL SKIN.Apr 5, 2024 · N688QS · Cessna 680CESDR DALA2024040504133Skin · crackedAD -- OPEN HOLE HFEC (BHEC) INDICATED CRACK 2 FASTENER HOLES BELOW EXISTING DOUBLER ON RT VERT L/E. MARKED. FOUND ON STEP 12 OF AA 5530-01048 AD 2018-10-08. SEPERATED EXTERIOR LATERS ON R/H VERT STAB FRONT SPAR CAP PER AA 5530-01048-02 STEP 13. PERFORMED OPEN Mar 29, 2024 · N924AT · Boeing 717200SDR UIEA2024032200196Skin · damagedVERT FIN TIP FAIRING UPPER T/E CORNER BURN MARK. BLEND OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED. ALLOWABLE DAMAGE PER SRM 55-30-30-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL XIV ALL IN REV 42.Mar 29, 2024 · N850GT · Boeing 74787UFSDR CALA2024032900917Skin · damagedPDA 1 ON ARRIVAL IN AMS FOUND LH SIDE OF VERTICAL STAB,PANELS 324WL,324VL,324UL PANELS MISSING AND DAMAGE,AND MISSING FASTERNERS PANEL 324WL P/N 75W1151-10, PANEL 324VL P/N 175W1151-26, PANEL 324UL P/N 1751151-25.Mar 28, 2024 · N79011 · Boeing 777224SDR IXXA2024032001Skin Panel · delaminatedR/H VERTICAL STAB HAS AREA DELAMINATED ON SKIN PANELMar 20, 2024 · N255CM · Boeing 767223SDR R61A2024041200178Rivet · missingMAJOR. ORIGINAL PATCH #3 MISSING RIVETS. MX REPLACED 2 RIVETS IAW ETD 2024-170-007859.Mar 18, 2024 · N211JQ · Emb ERJ170200LRSDR R61A2024041200177Skin · dentedEXISTING REPAIR AND ORIGINAL SKIN UNDER RH SIDE VERTICAL STAB DENTED. MX REPLACED SKIN PATCH IAW IC2009-170-102607, ETD2024-170-007859Mar 18, 2024 · N211JQ · Emb ERJ170200LRSDR DALA2024032003537Skin · delaminatedVERTICAL STABILIZER BETWEEN AUX SPAR AND FRONT SPAR L/H ALLUMINIO HONEYCOMB PANEL FOUND DELAMINATION AT FSS 245 TO FSS 270. DAMAGED AREA REPAIRED AT FSS 245 TO FSS 270 AS PER PRI 616526-14.REV.0 & PRI 616526-14. REV.1.THE PRI 616526-14.REV .0 & PRI 616526-14Mar 18, 2024 · N837MH · Boeing 767432ERSDR DALA2024031503369Skin · delaminatedSHIP 172 DELAMINATION FOUND ON THE RH SIDE VERTICAL STABILIZER SKIN THAT 12" BELOW THE FSS295 AND 30" FAR AWAY FROM AUX SPAR. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 55-30-01-2R-1 & SRM 51-70-10-2R-4 & SRM 51-70-10-2R. (0244147)Mar 14, 2024 · N172DN · Boeing 767332SDR SWAA2024040559996Skin · corrodedSURFACE CORROSION ON CROWN SKIN UNDER VERTICAL STAB 23 INCHES FWD OF VERTICAL STAB L/H O/B AFT MOUNT BOLT STA 1064 (MARKED).<[01] 'REFER TO FAULT TTG8Q00RZLRM WHERE EA 24-153-00694 WAS ADDED AS A SUBTASK.'<BR><BR>'FAULT RESOLVED ON OTHER FAULT' REPAIR REFERENCMar 6, 2024 · N7731A · Boeing 73776NSDR IPXA2024030725989Panel · delaminated*SDR FILED OPEN* FOUND DELAMINATION ON VERTICAL STABILIZER PANELMar 6, 2024 · N573UP · Boeing 74744AFSDR UIEA2024022600128Skin · dentedEMP - VERT FIN R/H SURFACE MOST UPPER AREA FWD FIXED PANEL FOUND DENT MARK(<P>DENT AREA REPAIRED AS PER RI-55-00-16750 REV.A. NO FURTHER DEFECTS NOTED</P>)Mar 3, 2024 · N454PA · Boeing 74746NFSDR DALA2024030402942Fastener · looseAD. FOUND 5 FASTENERS LOOSE AT THE RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) REFERENCE AA 5530-01048 & AD 2018-10-08. CHECKED FASTENER HOLES REF SERVICE GENERAL DRAWING SG 95550001 AND FOUND HOLES TO BE OK REF AMDS CARD 5530-01048-0Mar 3, 2024 · N717JL · Boeing 717200SDR DALA2024030402940Fastener · looseAD. FOUND 24 FASTENERS LOOSE AT THE LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE. (STA ZFS=52.267) REFERENCE AA 5530-01048 AND AD 2018-10-08. CHECKED FASTENER HOLES REF SERVICE GENERAL DRAWING SG9550001 AND FOUND HOLES TO BE OK REF AMDS CARD 5530-01048Mar 3, 2024 · N717JL · Boeing 717200SDR DALA2024013101411Skin · damagedFASTENER HOLES AND COUNTERSINKS ARE ELONGATED OUT OF LIMITS ON 1/4 FASTENERS ROW AT VERT STAB FIX LE. ALSO, ON VERT STAB REMOVABLE LE STA ZFS=52.267 REF SERVICE GENERAL DRAWING SG95550001. SUMMARY OF NRC 00538: FASTENER HOLES AND COUNTERSINKS AT VERT STAB FIX Jan 25, 2024 · N964AT · Boeing 717200SDR COEA2024032211819Skin · chafedWO 251965 NR 300047 HEAVY CHECK COE/MAJOR REPAIR: VERTICAL STABILIZER SKIN CHAFED. CORRECTIVE ACTION: REPAIRED PER SRAS S553R0013...23046 ISSUE A, DATED 2/29/2024.Jan 20, 2024 · N819FX · Aerosp ATR72212SDR IPXA2024021287243Panel · damagedVERTICAL STABILIZER L/E PANEL322 AL EXTERNAL MIDDLE CTR COMPOSITE DAMAGED . 89-168 PANEL WAS DOCUMENTED FOR REMOVAL ON TWO NRC'S. PANEL WILL BE REINSTALLED ON NRC T#F18E003S5ZL / 6100408536.Jan 16, 2024 · N122UP · Airbus A300F4622RSDR IPXA2024021287366Panel · damagedVERTICAL STABILIZER LE PANEL 322AL , 322BL ,ALLUMINIUM BONDED COVER AT LE HAS APPEAR TO HAVE DENTS AT SEVERAL PLACECS . 89-171 INSTALLED VERTICAL STAB LEADING EDGE PANELS 322AL, 322BL, IAW A300 AMM 53-32-11/401 VERIFIED.Jan 16, 2024 · N122UP · Airbus A300F4622RSDR IPXA2024011787243Panel · damaged*** SDR FILED OPEN *** FAULT - VERTICAL STABILIZER L/E PANEL322 AL EXTERNAL MIDDLE CTR COMPOSITE DAMAGED . 89-168Jan 16, 2024 · N122UP · Airbus A300F4622RSDR IPXA2024011787366Panel · dented*** SDR FILED OPEN *** FAULT - VERTICAL STABILIZER LE PANEL 322AL , 322BL ,ALLUMINIUM BONDED COVER AT LE HAS APPEAR TO HAVE DENTS AT SEVERAL PLACECS . 89-171Jan 16, 2024 · N122UP · Airbus A300F4622RSDR SWIA202401300014Skin · chafedFOUND VERTICAL STAB SKIN CHAFED UNDER FORWARD SIDE OF PANEL 326DL TRANS: 27680274 (C-CHECK RO 1/30/2024) REMOVED CHAFE ON VERTICAL STAB SKIN UNDER FORWARD SIDE OF PANEL 326DL, REF. CRJ-700 SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-55-32-342 REV-- DAJan 14, 2024 · N746SK · Cndair CL6002C10SDR COEA2024032110819Skin · corrodedWO 251965 NR 300014 HEAVY CHECK COE/MAJOR REPAIR: VERTICAL STABILIZER, L/H FWD SKIN HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00231919...23138 ISSUE B, DATED 3/12/2024.Jan 8, 2024 · N819FX · Aerosp ATR72212SDR IPXA2024021629897Skin · damagedVERT STAB LWR L.E. EXTERNAL SURFACE HAS MULTIPLE EROSION DAMAGED AND WIRE MESH DAMAGED AS MARKED. 74-066 APPLIED ASTROSTRIKE COPPER SCREEN P/N CU029CX BATCH # 0003983031 AND RESIN EA9396A/B BATCH #0004196337 TO DAMAGED AREAS ON VERTICAL STAB. LOWER L/E, CURED Jan 8, 2024 · N288UP · Doug MD11FSDR IPXA2024020226312Skin · damaged*** SUPPLEMENTAL SDR *** DAMAGE FOUND ON RH SIDE OF VERTICAL STAB TO THE RIGHT OF THE UPS SHIELD. AS REQUESTED BY ENGINEERING AND STRUCTURES DEPARTMENT, PROVIDED MATERIAL REMAINING MEASUREMENTS OF NOTED DAMAGED AREA ON R/H SIDE OF VERTICAL STAB. DONE PER B747 Jan 8, 2024 · N611UP · Boeing 7478FSDR IPXA2024010929897Unknown · unknown*SDR FILED OPEN* (COMP) VERT STAB LWR L.E. EXTERNAL SURFACE HAS MULTIPLE EROSION DAMAGED AND WIRE MESH DAMAGED AS MARKED. 74-066 APPROVEDJan 8, 2024 · N288UP · Doug MD11FSDR DALA2024010200035Unknown · unknownSHIP 3120 CRACK LEADING EDGE ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 613722-14. (0134503)Dec 31, 2023 · N320NB · Airbus A319114SDR DALA2024010200034Unknown · unknownSHIP 3120 CRACK ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 613723-14. (0134500)Dec 31, 2023 · N320NB · Airbus A319114SDR SWAA2024011235464Panel · crackedRH VERTICAL FIN PANEL 324AR CRACKED AT FWD UPPER CORNER.<[01] COMPLETD REPAIT PANEL 324AR REF B 737 -800-SRM 51-70-04-2R-0 / AMM 51-21-73-370-803 / SRM 51=40-02;[02] VERIFIED STEP 1Dec 27, 2023 · N8560Z · Boeing 7378H4SDR DALA2023122810687Unknown · unknownAIRCRAFT 1705, FOUND 2EA DELAMINATION ON THE LH SIDE VERTICAL SKIN BETWEEN AUX SPAR AND FRONT SPAR FROM FSS 39 TO FSS 92. CORRECTIVE ACTION: DELAMINATION REPAIRED ON THE LH SIDE VERTICAL SKIN BETWEEN AUX SPAR AND FRONT SPAR FROM FSS 39 TO FSS 92 AS PER PRI 614Dec 26, 2023 · N175DZ · Boeing 767332SDR DALA2023122810670Unknown · unknownSHIP 1603 RH VERTICAL FIN AUXILIARY SPAR TO FRONT SPAR SURFACE FOUND DELAMINATION AT FSS92.25-FSS118.75. CORRECTIVE ACTION: DAMAGED AREA REPAIRED AS PER B767-300 SRM 55-30-01-2R-1 & SRM 51- 70-10-2R-4 & SRM 51-70-10-2R-0 (0125201)Dec 25, 2023 · N1603 · Boeing 767332SDR DALA2023122810678Unknown · unknownSHIP 1706 VERTICAL STABILIZERS LH EXTERNAL AT FSS 145.128 - FSS 220.521 BETWEEN AUXILIARY SPAR AND FRONT SPAR FOUND BULGE. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI 614264-14 (0125183)Dec 25, 2023 · N176DZ · Boeing 767332SDR IPXA2024061138494Panel · delaminatedDELAMINATION LEFT SIDE OF VERTICAL STABILIZER AFT & ABOVE HF COUPLER. REMVOVED SKIN PANEL IAW SRM 51-40-02.INSTALLED NEW PANEL I.A.W SRM 51-40-02-0G REV.100 ALL PAPERWORK C/W, THIS ACTION CLEARS DEFERRAL 2805530Dec 15, 2023 · N577UP · Boeing 74744AFSDR IPXA2023121838494Skin · delaminated*** SDR FILED OPEN *** DELAMINATION LEFT SIDE OF VERTICAL STABILIZER AFT & ABOVE HF COUPLER MATERIAL ID. TO BE: L ANGLE BAC1503-5818 - 81205 (ANGLE, 90 DEGREE, ALUMINUM EXTRUDED (1.50 X 1.50, 0.093) 7075-T6511) P.O 1260290 AND SKIN PANEL 075T6(.125X48X144) (SHDec 15, 2023 · N577UP · Boeing 74744AFSDR DALA2023112709738Unknown · unknownSHIP 3120 CRACK LEADING EDGE ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 613640-14. (0079917)Nov 24, 2023 · N320NB · Airbus A319114SDR DALA2023112709700Unknown · unknownSHIP 3034 CRACK LEADING EDGE ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 613640-14. (0080065)Nov 24, 2023 · N334DN · Airbus A321211SDR DALA2024010500203Unknown · unknown-AD- A SKIN LAYER CRACK WAS FOUND ON THE LEADING-EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER OF A B717-200. THE CRACK WAS REPAIRED PER ER/A 613198-14. THIS ER/A REQUIRES FOLLOW ON INSPECTION. UPDATED MONITOR LOG THRESHOLD TO ACCOUNT FOR TIME FLOWN SINCE SENov 23, 2023 · N933AT · Boeing 717200SDR DALA2023112809746Unknown · unknownSHIP 192 CHECK FOUND LEFT SIDE VERTICAL STABILIZER POSITION TO FUSELAGE 17 INCH AND TO LEADING EDGE 36 INCH DELAMINATION ABOUT LENGTH * WIDETH IS 16*11 INCH. CORRECTIVE ACTION: REPAIRED LEFT SIDE VERTICAL STABILIZER POSITION TO FUSELAGE 17 INCH AND TO LEADING Nov 21, 2023 · N192DN · Boeing 767332SDR DALA2023112109582Unknown · unknownSHIP 1602 RH VERTICAL FIN FWD TORQUE BOX SKIN PANEL FOUND DELAMINATION AT APPROXIMATE FSS 102. CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4 (0068905)Nov 17, 2023 · N1602 · Boeing 767332SDR UIEA2023111400943Unknown · unknownLEFT SKIN PANEL 175T2001-3 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270 DELAMINATION.(<P>LH VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-23-0150-15B. NO FURTHER DEFECTS NOTED</P>)Nov 16, 2023 · N1381A · Boeing 767316SDR UIEA2023111400944Unknown · unknownRIGHT SKIN PANEL 175T2001-4 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270.(<P>VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-0150-15B. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316SDR DALA2023111609444Unknown · unknownSHIP 3119 CRACK ACCESS PANEL 322AL LH AND RH SIDE VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 612713-14. (0066512)Nov 15, 2023 · N319NB · Airbus A319114SDR SWAA2023121120815Access Panel · crackedCRACK ACCESS PANEL 321A WEB ON RIB 8 AT VERTICAL STABILIZER 2023-694829<[01] TOOL USED TEMPERATURE CONTROLLER P/N:P3015GOES00000;S/N:142811620;DUE DATE:25-JAN-24.;[02] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 ANNov 12, 2023 · N917WN · Boeing 7377H4SDR DALA2023111009260Unknown · unknownSHIP 194 1EA DISBONDING FOUND AT RH OF VERTICAL STABILIZER FSS 220.521- FSS 270.784 AUXILIARY SPAR TO FRONT SPAR. CORRECTIVE ACTION: RH OF VERTICAL STABILIZER REPAIRED AT FSS 220.521 - FSS 270.784 AUXILIARY SPAR TO FRONT AS PER B767-300 SRM 55-30-01-2R-1 & SRMNov 9, 2023 · N194DN · Boeing 767332SDR DALA2023111009259Unknown · unknownSHIP 194 FOUND RH OF VERTICAL STABILIZER FSS 170.259- FSS 220.521 AUXILIARY SPAR TO FRONT SPAR 01EA DISBONDING. CORRECTIVE ACTION: RH OF VERTICAL STABILIZER REPAIRED AT FSS 170.259-220.521 AUXILIARY SPAR TO FRONT SPAR AS PER B767-300 SRM 55-30-01-2R-1 & SRM 51Nov 9, 2023 · N194DN · Boeing 767332SDR DALA2023110709170Unknown · unknownSHIP 194 FOUND RH OF VERTICAL STABILIZER FSS 170.259 - FSS 270.784 AUXILIARY SPAR TO FRONT SPAR 01EA DISBONDING. CORRECTIVE ACTION: RH OF VERTICAL STABILIZER REPAIRED AT FSS 170.259 - FSS 270.784 AUXILIARY SPAR TO FRONT SPAR AS PER B767-300 SRM 55-30-01-2R-1 &Nov 4, 2023 · N194DN · Boeing 767332
Back to JASC 5532