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 DALA2020031801939Skin · delaminatedFOUND DELAMINATION ON LH LATERAL SURFACE OF VERTACAL STABILIZER FSS65-92,10" FROM FRONT SPAR. C/W ERA 585586-14. (LP 1532644)Mar 17, 2020 · N839MH · Boeing 767432ERSDR SWAA2020032442689Panel · dentedDENT ON VERTICAL STAB L/E PANEL AT L/E STA 262 TRIMMED OUT THE DAMAGE PART OF THE SKIN ON VERTICAL STAB L/E PANEL AT L/E STA 262. DIMENSIONS 1.6" X 1.25" AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-01-2R-1. 88920U 14 MAR 20Mar 7, 2020 · N552WN · Boeing 7377BXSDR DALA2020030601668Skin · crackedVERTICAL STABILIZER RAM AIR INLET LEADING EDGE IS CRACKED ON THE LEFT SIDE. REPAIRED PER B717 SRM 55-30-01-2R PROCEDURE 1. REQUIRES REPETITIVE VISUAL INSPECTION EVERY 4500 HOURS. (LP #1518223)Mar 6, 2020 · N987DN · Boeing 717200SDR IPXA2020030252689Panel · dentedINSPECTION TYPE:N/ALWR VERT STAB PANEL 364CRDENTEDREPAIRED PER EO MD11-5430-75682-A COMPOSITE DOUBLER REPAIRMar 2, 2020 · N290UP · Doug MD11FSDR REXA2020030400304Rub Strip · torn"PART RACKS : TORN AND LOOSE TEFLON STRIP AT VERTICAL STABILIZER ACCESS PANEL NBR , 326DL , AND 326DR ( SM ) " "SUMMARY: NEW STRIPS, RUBBER, UPPER VISOR ACCESS PANEL 326DL AND 326DRWERE INSTALLED PER CRJ/900 SRM 51-42-06-001-Feb 28, 2020 · N298PQ · Cndair CL6002D24SDR DALA2020022761448Skin · damagedTHE REMOVEABLE VERTICAL LEADING EDGE HAS 15 HOLES OUT OF TOLERANCE IN THE AD SIGNIFICANT AREA - FORWARD CROWN SIDE. MAINTENANCE OPENED UP 65 HOLES PER DWG #SG95550001. BOLT HOLE EDDY CURRENT PER SRM 06-10-01.003 - NO DEFECTS NOTED (QC1969 ). INSTALLED BUSHING Feb 26, 2020 · N980AT · Boeing 717200SDR DALA2021090205177Skin · damagedVERT STABILIZER / UPPER REMOVABLE / LE SKIN / ZFS-52 / OS HOLES / AD RELATED. ERA 585576-14 ISSUED AND IS CURRENT. AD RELATED, FOLLOW ON ACTION REQUIRED. SECTION II TO BE ACCOMPLISHED WITHIN 24 MONTHS AFTER SECT.I. SECT.II IS PENDING DAMAGE TOLERANCE ANALYSIS Feb 25, 2020 · N980AT · Boeing 717200SDR DALA2020030301548Fastener · missingLOOSE AND MISSING FASTENERS ABOVE SPLICE STA ZFS= 52.267 AT VERTICAL STABILIZER LEADING EDGE (EHV) SUMMARY NRC 00491: VERTICAL STABILIZER LEADING EDGE WAS REPAIRED PER MD-90 SRM 55-30-05 VOLUME I PAR. 11, AD 5530-01044-05 AND DWG SG09550004 REV. D. PERFORM DVIFeb 25, 2020 · N908DA · Doug MD9030SDR DALA2020022540390Skin · corrodedVERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR L/H SKIN AT FSS 65.75 TO FSS 92.25 FOUND BULGE. REPAIRED PER SRM 51-70-10. (LP 1502912)Feb 24, 2020 · N188DN · Boeing 767332SDR DALA2020022631446Skin · crackedA/C DUE ERA 585429-14AD PRI REV O. VERTICAL STABILIZER LEADING EDGE ZFS 52.267 FRONT SPAR CAP DORSAL / LOWER ASSEMBLY LHS CRACK INDICATION. C/W ERA 585429-14AD REV ORIGINAL SECTION 1 PERMANENT REPAIR. (LP1500936)Feb 22, 2020 · N907DE · Doug MD88SDR DALA2020022301342Skin · cracked/H VERTICAL STAB HAS CRACK INDICATION IN 6TH HOLE UP FROM STATION ZFS=52.267 ON FRONT SPAR CAP. REMOVED VERT STAB PER MD 88 AMM 55-30-01 THRU STEP 3(A)(7). REAMED HOLE IN VERTICAL SPAR CAP TO .233 . PERFORMED BHEC PER MD88 NDTSPM PART 6-10-01.003 AND AMDS CARDFeb 22, 2020 · N907DE · Doug MD88SDR REXA2020030200265Seal · worn"POST-PATR RACKS : WORN AND LOOSE TEFLON SEAL AT VERTICAL STABILIZER ACCESS PANEL NBR 326DR ( EHV ) " "SEAL AT VERTICAL STABILIZER ACCESS PANEL NBR 326DR WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-06-001-001-A0Feb 21, 2020 · N299PQ · Cndair CL6002D24SDR DALA2020020700997Skin · corrodedFOUND VERTICAL STABILIZER RH INSIDE SKIN BULGE AT F22 204 AND FROM AUXILIARY SPAR 15 INCH.REPAIRED DAMAGED ON VERTICAL STABILIZER RH INSIDE SKIN BULGE AT FSS 204 AND FROM AUXILIARY SPAR 15 INCHES PER SRM 51-70-10 (LP 1479346)Feb 7, 2020 · N188DN · Boeing 767332SDR SWIA2020031049241Skin Panel · brokenWHILE INSPECTING PANEL 326BL FOR DISBONDED TEFLON STIPS FOR JOB 2763291 OP 82 MX TRANS. 20282016 FOUND PANEL TO BE UNSERVICABLE DUE TO BROKEN OFF SECTION OF PANEL (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PANEL 326BL OUTER SKIN P/N:600-21134-45 REF. SRM.Feb 6, 2020 · N905EV · Cndair CL6002B19SDR SWAA2021072926727Panel · corrodedVERTICAL STABILIZER PANEL 324ML HAS CORROSION ON BOTH SIDES OF PANEL / REMOVED CORROSION FROM VERTICAL STABILIZER PNL #324 ORIG 'T' 0.050'; LOSS 0.004'; REMAIN 0.046' FOUND OUT OF LIMITS DUE NO ALLOWABLE DAMAGE FOUND. VERIFIED MATERIAL (20-24-73 0.050'); LOCATFeb 5, 2020 · N799SW · Boeing 7377Q8SDR SIMA2020033102003Skin · canningLEFT HAND VERTICAL STABILIZER SKIN JUST FORWARD OF TAIL ACCESS PANEL 324EL HAS OIL CANNING.-C/A-C/W REPAIR OF VERTICAL STABILIZER SKIN LOCATED JUST FWD OF TAIL ACCESS PANEL 324EL IAW ERS-EM-55MR-813.Feb 2, 2020 · N667GB · Emb EMB145LRSDR DALA2020020760986Skin · delaminatedR/H SIDE OF VERTICAL STAB BETWEEN AUX SPAR AND FWD SPAR THERE IS AN AREA OF DELAMINATION AT APROX FSS 92.25. REMOVED DAMAGE, PREPPED AND INSTALLED REPAIR UNDER VACUUM PER SRM 51-70-10. (LP 1477173)Feb 1, 2020 · N189DN · Boeing 767332SDR CALA2020011300145Vortex Gen · missingPDA 2 1EA AFT BODY VORTEX GENERATOR MISSING ON RIGHT SIDE OF VERTICAL STAB. ONLY 1 MISSING ON RIGHT SIDE - ALL OTHERS ARE PRESENT - REQUEST CDL TOMC APPROVES CDL 55J CDL APPLIED. REF IPC 53-31-21-01 AND AMM 53-21-21Jan 12, 2020 · N69824 · Boeing 737924ERSDR NACA2019123040149Panel · corrodedLEFT VERTICAL STABILIZER PANEL 9566L CORRODED ON LOWER SURFACE. REPLACED THE PANEL IAW SRM 51-30-01 REV 104, AND SRM 51-40-02 REV 104.Dec 24, 2019 · N401YK · Boeing 737436SDR DALA2019113006963Cap · damagedUPPER VERTICAL STAB CAP DAMAGED. RMVD DAMAGE AREA FABRICATED DOUBLER PER MD88 SRM 55-32 FIG 4. INSTALLED REPAIR DOUBLER PER MD 88 SRM 55-32 FIG 4 (LP1379844)Nov 29, 2019 · N963DL · Doug MD88SDR CALA2019111601984Skin · chafedVERTICAL STABILIZER R/H ROOT PNL 322AR 321AR TO FUSELAGE INTERFA CE CROWN SKIN FOUND CHAFING FROM BSTA2129 TO BSTA2150. REFER NON -ROUTINE NO.9488790 SPEC NO. B777-53-3-7032. VERT STAB R/H PNL 322AR TO FUSELAGE INTERFACE CROWN SKIN BS2129-BS2150 CHAFING AREA RNov 14, 2019 · N794UA · Boeing 777222SDR CALA2019111601983Skin · chafedVERTICAL STABILIZER L/H ROOT PNL 322AL 321AL TO FUSELAGE INTERFA CE CROWN SHIN FOUND CHAFING FROM BSTA2110 TO BSTA2150. REFER NON -ROUTINE NO.9488791 - ORIGINATED BY EMP V902926 SPEC NO.B777-55- 3-7031. VERT STAB L/H ROOT PNL 322AL, 321AL TO FUSE INTERFACE CRONov 13, 2019 · N794UA · Boeing 777222SDR FDEA2019122073267Skin · crackedLT LWR VERTICAL STAB FAIRING SKIN AT STA 2160 HAS A .300 IN CRACK PROPAGATING OUT OF THE FASTENER HOLE. BELOW PYLON CARRY THROUGH CAP, REPAIRED SKIN FAIRING PER SRM 55-00-00-2R FIG 204 DWG AJC7582-17.Nov 7, 2019 · N574FE · Doug MD11FSDR SWIA2019110546712Panel · damagedPANEL 325AR HAS DAMAGE OUT OF SRM LIMITS. REQUIRES REO FOR RECTIFICATION, (PANEL OPENING LANDING). (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.Nov 5, 2019 · N679SA · Cndair CL6002B19SDR SWIA2019110546711Panel · damagedPANEL 325BL AND 325CL HAS DAMAGE OUT OF SRM LIMITS. REQUIRES REO FOR RECTIFICATION, (PANEL OPENING LANDING). (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX. SEE ATTACHED WORK CARD FOR DETAILS.Nov 5, 2019 · N679SA · Cndair CL6002B19SDR DALA2019110406405Access Panel · dented(AIRCRAFT 6812, L/P 1342743) SEVERAL DENTS ON VERTICAL L.E. ACCESS PANEL 321DL (LH SIDE), (EHV). CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00138: DENTS ON VERTICAL L.E. ACCESS PANEL 321DL (LH SIDE) AND OUT OF LIMITS PER B-757-200 SRM 55-30-01 FIG. 101. TNov 2, 2019 · N717TW · Boeing 757231SDR IPXA2019101447859Panel · damagedINSPECTION TYPE:SEG1, VERTICAL STAB L/E PANEL 321 HAS 1 EA PULLED FASTENER. REPAIRED PANEL IAW EA B757-5360-27-A2382 AND UPS EO B757-5350-74251-AOct 14, 2019 · N448UP · Boeing 75724APFSDR ABXA2019100129156Panel · delaminatedDELAMINATION TO THE COMPOSITE STRUCTURE OF THE VERTICAL STABILIZER PANEL P/N 175T2001-2 AT FRONT SPAR STATION 15 AND FRONT SPAR STATION 50. THE PANEL WAS REPAIRED. THE AIRPLANE WAS GROUNDED.Sep 29, 2019 · N783AX · Boeing 767281SDR IPXA2019091146639Panel · damagedINSPECTION TYPE:N/A RT LOWER VERT STAB PANEL HAS 2 PUNCTURES AND DELAM IN SKIN. REPAIRED IAW EO MD11-5530-73671-B.Sep 11, 2019 · N289UP · Doug MD11FSDR IPXA2019091046563Panel · damagedINSPECTION TYPE:N/A REF D681323 LOWER VERTICAL STAB RIGHT SIDE REAR PANEL REPAIR CLASSIFIED AS A MAJOR REPAIR, TRANSFERRED TO NEC 621476, COMPLETED REPAIR PER EO MD11-5930-73667-C AND SRM 51-71-00. COMPLETED NRC 621476 AND TALLY SHEET SDR # 20190946529. THIS ISep 10, 2019 · N289UP · Doug MD11FSDR DALA2021041202110Skin · damagedERA 560974-14AD REV C ISSUED FOR REPAIRS TO LOWER FIXED LE ON VE RTICAL STAB. DTA / DTE IS REQUIRED. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. ASSOCIATED ER/A 00-560974 ADDED FOR AC 9507. DTE HAS BEEN ACCOMPLISHED. FOLLOW ON INSPECTIONS ARE REQUIRED. SECTIONSep 9, 2019 · N947AT · Boeing 717200SDR IPXA2019090946529Panel · puncturedINSPECTION TYPE:N/A TWO PUNCTURES ON VERTICAL STAB PANEL. REPAIRED IAW EO MD11-5530-73667-C.Sep 9, 2019 · N289UP · Doug MD11FSDR SCNA20190907159Skin · erodedDORSAL FIN LEADING EDGE AT AFT END IS ERODED AND HAS COMPOSITE AND BARE METAL EXPOSED. REPAIRED DORSAL FIN LEADING EDGE AT AFT END.Sep 7, 2019 · N815SY · Boeing 7378BKSDR FDEA201908302043Skin · crackedON REMOVAL OF THE BANJO ACCESS, FOUND THE LEFT VERTICAL STABILIZER SKIN AT REAR CENTER SPAR CRACKED. REPAIRED THE SKIN PANELS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 30, 2019 · N590FE · Doug MD11FSDR FDEA201908302042Skin · crackedON INSPECTION, FOUND RIGHT VERTICAL STABILIZER SKIN CRACKED. REPAIRED IAW EA 1-5530-T0349100 P2, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2019 · N590FE · Doug MD11FSDR DALA2019082764980Skin · delaminatedRT VERT STAB ABOUT 1/2 WAY UP BEHIND L/E LOOKS DELAMINATED. REMOVED RT VERTICAL STAB PANEL. IAW SRM, PNL REPAIRED ON S/O PW6683. INSTALLED PANEL.Aug 23, 2019 · N688DL · Boeing 757232SDR SWAA2022031433755Retainer · crackedVERTICAL FIN PANEL 323AL HORIZONTAL RETAINER CRACKED / R&R VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER PER SRM 51-40-02Aug 9, 2019 · N400WN · Boeing 7377H4SDR IPXA2019080545321Skin · puncturedRIGHT LOWER VERTICAL STABILER PANEL 364GR PUNCTURED. DAMAGE REPAIRED IAW EO MD11-5530-73251-B.Aug 5, 2019 · N276UP · Doug MD11FSDR JGVR20190723001Access Panel · crackedFOUND VERTICAL STABILIZER ACCESS PANELS 340ER AND 340FR TO HAVE CRACKS IN THE FASTENER HOLES, REPLACED CRACKED PANELS WITH TWO NEW P/N 5531005-3.Jul 23, 2019 · N689QS · Cessna 560XLSDR DALA2023012400526Skin · damagedERA 564482-14AD REVISED TO REV 'A'. SECTION I ORIGINALLY ISSUED FOR DAMAGE TO V STAB FRONT SPAR CAP SKIN. DAMAGE TOLERANCE EVALUATION COMPLETE. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION PRIOR TO 5100 FLIGHT CYCLES FROM SECTION I ACCOMPLISHMENJul 22, 2019 · N891AT · Boeing 717200SDR IPXA2019071644513Access Panel · damagedINSPECTION TYPE:MX ACCESS PANEL 364GR ON RT VERTICAL STAB #2 ENG BARRELL AHS DAMAGE. THIS IS A MAJOR REPAIR. TRANSFERRED TO NRC 620422.Jul 16, 2019 · N276UP · Doug MD11FSDR DALA2019070804104Seal Plate · missingSHIP 3863 VERT STAB TO RUDDER SEAL PLATE MISSING LEFT SIDE MID WAY UP P/N 175A1601-73. CORRECTIVE ACTION: REPLACED SEAL PANEL PER AMM 55-33 (5536488).Jul 1, 2019 · N863DN · Boeing 737932ERSDR LR7A2019062401791Skin · corrodedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE VERTICAL STABILIZER TRAILING EDGE LT SKIN CORRODED BEYOND LIMITS, VSS4, FS1096-1099, LBL85. REPAIRED IAW SRM FIG. 51-140-12. NR# 2582.Jun 24, 2019 · N409LC · Lkheed 382GSDR AALA201906119042Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RIGHT HAND SIDE FORWARD SKIN PANEL HAS DELAMINATION BETWEEN FIN STATION 113 AND 150. REPLACED SKIN PANEL PER EA 272864A.Jun 8, 2019 · N203UW · Boeing 75723NSDR SWAA2022031007412Panel · delaminatedVERT STAB PANEL 324AR HAS DELAMINATED DENT / REPAIRED DELAMINATED DENT ON VERT STAB PANEL 324AR USING BMS 5-28 TY7 LOT AK8GP4556K-1 POTTING COMPOUND; BMS 8-79 STYLE 120 LOT 1392933-1 AND BMS 5-129 ORD 5 LOT 1392933-1 PLIES. APPLIED FINISH BMS 10-103 PRIMER; BAJun 7, 2019 · N222WN · Boeing 7377H4SDR 2019F00215Skin · damagedVERTICAL FIN LEADING EDGE DAMAGE. ACCOMPLISHED MANUFACTURER ENGINEERING LETTER DQ21778M1; 680-0119 VERTICAL FIN LEADING EDGE DAMAGE.Jun 7, 2019 · N387QS · Cessna 680CESDR SWAA2022031076869Retainer · crackedVERT STAB PNL 323BL AFT RETAINER STRIP CRACKED IN 2 PLACES. / REMOVED AND REPLACED DAMAGED AFT RETAINER STIP ON VERT STAB PNL 323BL. RTAINER STRIP PN 172A6125-US ATAG A76603. IAW B-737 SRM 51-40-02-0G-0 AND B-DRAWING 172A6121 REV: A.Jun 6, 2019 · N732SW · Boeing 7377H4SDR 2019F00229Skin · crackedFOUND CRACK IN VERTICAL TAIL SKIN ABOVE "PYRAMID" IN DOUBLER. INSTALLED 5" ACCESS HOLE IN LH VERTICAL SKIN IN REFERENCE TO GTEC, INC ENGINEERING. FOUND MID SPAR CRACKED ON RH SIDE OPPOSITE OF CRACK IN SKIN. INSTALLED A DOUBLER ON THE LH AND RH FLANGE OF THEJun 6, 2019 · N840G · Gulstm 690CSDR DALA2019052803188Doubler · damagedAWR: HIDDEN ELONGATED HOLES: DURING MTC WORKS IN REF NRC S/N 00194. ELONGATED HOLE ON EXTERNAL REPAIR DOUBLER AT VERTICAL STABILIZER FIXED L/E BELOW THE SPLICE AT STATION ZFS= 52.267 WERE FOUND. EXTERNAL REPAIR DOUBLER AT VERTICAL STABILIZER FIXED L/E WAS REPLMay 25, 2019 · N912DE · Doug MD88SDR DALA2019052803189Doubler · crackedAWR: HIDDEN CRACK: DURING MTC WORKS IN REF NRC S/N 00194, CRACK ON INTERNAL FINGERS DOUBLER AT VERTICAL STABILIZER FIXED L/E BELOW THE SPLICE STATION ZFS= 52.267. INTERNAL FINGERS DOUBLER AT VERTICAL STABILIZER FIXED L/E WAS REPLACED PER SRM 51-30-01, 51-30-05May 24, 2019 · N912DE · Doug MD88
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