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 DALA2023110709169Unknown · unknownSHIP 194 1EA DISBONDING FOUND AT LH OF VERTICAL STABILIZER, FSS 92.25 - FSS 145.128 , AUXILIARY SPAR TO FRONT SPAR. CORRECTIVE ACTION: LH OF VERTICAL STABILIZER REPAIRED AT FSS 92.25 - FSS 145.128 , AUXILIARY SPAR TO FRONT SPAR AS PER B767-300 SRM 55-30-01-2R-Nov 4, 2023 · N194DN · Boeing 767332SDR DALA2023110709168Unknown · unknownSHIP 194 1EA DISBONDING FOUND AT RH OF VERTICAL STABILIZER, FSS 170.259 - FSS 270.784 , AUXILIARY SPAR TO FRONT SPAR. CORRECTIVE ACTION: RH OF VERTICAL STABILIZER REPAIRED AT FSS 170.259 - FSS 270.784 , AUXILIARY SPAR TO FRONT SPAR AS PER B767-300 SRM 55-30-01Nov 4, 2023 · N194DN · Boeing 767332SDR DALA2023110709167Unknown · unknownSHIP 194 1EA DISBONDING FOUND AT RH OF VERTICAL STABILIZER, FSS 0.0 - FSS 39.250 , AUXILIARY SPAR TO FRONT SPAR. CORRECTIVE ACTION: RH OF VERTICAL STABILIZER, FSS 0.0 - FSS 39.250 , AUXILIARY SPAR TO FRONT SPAR REPAIRED AS PER B767-300 SRM 55-30-01-2R-1 AND SRNov 4, 2023 · N194DN · Boeing 767332SDR IXXA2023110301Skin Panel · delaminatedRH SIDE OF VERTICAL STAB SKIN IS DELAMINATED.Nov 3, 2023 · N449AZ · Boeing 7673P6SDR 4MZA20231103059Skin · tornDURING POST-FLIGHT INSPECTION, PORTION OF SKIN MATERIAL TORN OF THE VERTICAL STABILIZER DURING FLIGHT.Nov 1, 2023 · N628PA · Amazon MK272SDR 4MZA20231103058Skin · tornPOST-FLIGHT INSPECTION FOUND PORTION OF SKIN MATERIAL TORN ON VERTICAL STABILIZER DURING FLIGHT.Oct 31, 2023 · N733PA · Amazon MK272SDR DALA2023103008882Unknown · unknownFOUR (4) CRACK INDICATIONS NOTED ON RT VERT STAB (MARKED) REF STEP 12 OF AMDS CARD 5530-01048-02 (AD2018-10-08). AFTER SEPERATION OF LAYERS PER AMDS 5530-01048-02, BHEC INSP SHOWS UPPER 3 HOLES OK AND LOWER MARKED HOLE HAS CRACK IN SKIN LAYER ONLY (QC 4031). COct 30, 2023 · N933AT · Boeing 717200SDR DALA2023103008921Unknown · unknownSHIP 3166 CRACK LEADING EDGE ACCESS PANEL 322CL EXTERNAL SKIN ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 613081-14. (0039388)Oct 28, 2023 · N366NB · Airbus A319114SDR IPXA05769Unknown · unknownLOWER VERTICAL STAB LEADING EDGE PANEL HAS SUSPECTED EROSION DAMAGE ON BOTTOM TWO THIRDS OF PANEL AS VIEWED FROM GROUND LEVEL. REMOVED AND REPLACED LOWER VERTICAL STAB LEADING EDGE PANEL 322AL IAW A300 AMM 55-32-11-401Oct 22, 2023 · N165UP · Airbus A300F4622RSDR JJBA20231018024Unknown · unknownVERT STAB LH SKIN DENT BETWEEN SPAR 2 AND AUX SPAR 41% AND BETWEEN RIB ZV 915 AND RIB ZV 1169. SKIN REPAIRED WITH A DOUBLEROct 16, 2023 · N16178 · Emb EMB145XRSDR IPXA2024010191370Panel · damagedMAJOR REPAIR LIGHTNING STRIKE ON LH UPPER VERTICAL STAB PANEL COMPLETED ALL STEPS OF EO 88253 AS REQUIRED THIS ACTION CLOSES BAR CODE T3F18E0033LSNOct 9, 2023 · N623UP · Boeing 7478FSDR JGVR20231009001Unknown · unknownMECHANICALLY BLENDED 12 AREAS OF CORROSION ON VERTICAL AFT SPAR LH & RH SPAR CAPS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED REPAIR AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPAIR.Oct 9, 2023 · N377QS · Cessna 680CESDR JGVR20231006002Unknown · unknownREPAIRED CORRODED AREAS OF THE VERTICAL STABILIZER SKINS BY MECHANICALLY BLENDING AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IN ACCORDANCOct 6, 2023 · N377QS · Cessna 680CESDR DALA2023100408171Unknown · unknownSHIP 3129 CRACK ACCESS PANEL 322AL LEADING EDGE EXTERNAL SKIN VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER 611638-14. (0000018)Oct 3, 2023 · N329NB · Airbus A319114SDR SWAA2023110705660Skin · corrodedSURFACE CORROSION ON CROWN SKIN UNDER VERT STAB. AFT OF FWD VERT STAB MOUNTS AND FWD OF STA 1040. BETWEEN STRINGERS S3L AND S3R. (MARKED)<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] ' AS PER EA 23-153-03004; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITISep 28, 2023 · N451WN · Boeing 7377H4SDR DALA2023092908020Unknown · unknownSHIP 196 DELAMINATION FOUND ON THE LH SIDE VERTICAL STABILIER EXTERNAL SKIN WHICH IS BETWEEN AUXLIARY SPAR AND FRONT SPAR FSS 39 TO FSS 92. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 55-30-01-2R-1&SRM 51-70-10. (2987797)Sep 26, 2023 · N196DN · Boeing 767332SDR DALA2023092908019Unknown · unknownSHIP 196 DELAMINATION FOUND ON THE LH SIDE VERTICAL STABILIER EXTERNAL SKIN WHICH IS BETWEEN AUXLIARY SPAR AND FRONT SPAR FSS 11 TO FSS 39. CORRECTIVE ACTION: 55-30-01-2R-1&SRM 51-70-10 (2987793)Sep 26, 2023 · N196DN · Boeing 767332SDR 2023F00273Skin · corrodedRH VERTICAL STABILIZER SKIN CORROSION. REMOVED CORROSION, VERIFIED NO CRACK INDICATIONS, AND MEASURED REMAINING MATERIAL THICKNESS. FOUND TO BE MAJOR IN SCOPE. ACCOMPLISHED AQRD ENGINEERING REPAIR ORDER ERO-977263.Sep 12, 2023 · N671QS · Cessna 680ASDR 2023F00269Skin · corrodedCORROSION ON LEFT VERTICAL STABILIZER SKIN JUST BELOW TOP CAP. LOCATED UNDERNEATH FILLET SEAL COVERING SEAM BETWEEN PARTS. REMOVED CORROSION, VERIFIED NO CRACK INDICATIONS, AND MEASURED REMAINING THICKNESS OF MATERIAL. SUBMITTED TO ENGINEERING AND FOUND TO BE Sep 11, 2023 · N671QS · Cessna 680ASDR DALA2023090607286Unknown · unknownSHIP 3126 CRACK ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 610764-14. (2953515)Sep 5, 2023 · N326NB · Airbus A319114SDR DALA2023082907030Unknown · unknownSHIP 3126 CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 610762-14. (2941691)Aug 28, 2023 · N326NB · Airbus A319114SDR IPXA2023082193971Panel · dentedINSPECTION TYPE:N/A*MAJOR REPAIR* LT LOWER VERTICAL STAB LOWER ACCESS PANEL DENTPANEL REPAIRED PER EO MD11-55-30-86966BAug 21, 2023 · N262UP · Doug MD11FSDR IXXA2023083101Panel · delaminatedL/H VERTICAL STAB BONDED SKIN PANEL IS DELAMINATED BETWEEN AUX SPAR AND FRONT SPAR RIB 10Aug 14, 2023 · N641AZ · Boeing 767300SDR DALA2023081406597Unknown · unknownSHIP 3165 CRACK ACCESS PANEL 322BL LH AND RH SIDE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 610805-14. (2916475)Aug 13, 2023 · N365NB · Airbus A319114SDR DALA2023081106572Unknown · unknownSHIP 3165 CRACK EXTERNAL SKIN LH ACCESS PANEL 322AL LEADING EDGE AND RH SIDE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 610826-14. (2912204)Aug 11, 2023 · N365NB · Airbus A319114SDR AALA202308155258Panel · delaminatedAIRCRAFT WAS GROUNDED: VERTICAL STABILIZER PANEL 322FL DELAMINATED. REPAIRED VERTICAL STABILIZER PANEL 322FL PER SRM 55-30-01-2R REPAIR 2.Aug 10, 2023 · N771AN · Boeing 777223SDR DALA2023071705778Unknown · unknown1 CRACK INDICATION ON L/H VERTICAL (MARKED) WHILE PERFORMING AA 5530-01048 AND AD 2018-10-08 BHEC INSPECTION. REINSPECTED CRACK IN STEP 16 CRACK CONFIRMED IN SKIN LAYER OF L/H VERTICAL STAB (MARKED) REF CARD AA5530-01048 AND AD 2018-10-08. C/W ERA 610480-14AD Jul 15, 2023 · N980AT · Boeing 717200SDR DALA2023071305677Unknown · unknownWHILE PERFORMING AA 5530-01048 AND AD 2018-10-08, FOUND 3 CRACK INDICATIONS ON LT. LOWER FIXED LEADING EDGE SKIN (MARKED). COMPLIED WITH ER/A 610352-14AD REV ORIGINAL PRI REV 0. COMPLIED WITH PRI 610352-14AD PRI REV 1, ER/A 610352-14 REV. ORIGINAL MATCHES PRI Jul 12, 2023 · N936AT · Boeing 717200SDR DALA2023071005571Unknown · unknownSHIP 3123 CRACK EXTERNAL SKIN RH ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 609337-14. (2856016)Jul 8, 2023 · N323NB · Airbus A319114SDR DALA2023071105615Unknown · unknownSHIP 0667 NICK ON MID LEADING EDGE ACCESS 321CL PANEL BTW FSS 210 220 AT VERTICAL STABILIZER. CORRECTIVE ACTION: MID LEADING EDGE ACCESS 321CL PANEL BTW FSS 210 220 AT VERTICAL STABILIZER WAS REPAIRED PER ERA 609861- 14. (2852839)Jul 7, 2023 · N667DN · Boeing 757232SDR AALA202307057881Panel · delaminatedAIRCRAFT WAS GROUNDED: VERTICAL STABILIZER RIGHT SIDE FORWARD BOX #3 PANEL HAS DELAMINATION AT STABILIZER STATION 2110. REPAIRED PANEL PER SRM 55-30-01-2R.Jul 5, 2023 · N773AN · Boeing 777223SDR AALA202307052044Panel · delaminatedAIRCRAFT WAS GROUNDED: VERTICAL STABILIZER RIGHT SIDE FORWARD BOX #3 PANEL HAS DELAMINATION AT STABILIZER STATION 2110. REPAIRED PANEL PER SRM 55-30-01-2R.Jul 1, 2023 · N773AN · Boeing 777223SDR AALA202307032044Panel · delaminatedAIRCRAFT WAS GROUNDED: VERTICAL STABILIZER RIGHT SIDE FORWARD BOX #3 PANEL HAS DELAMINATION. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)Jul 1, 2023 · N773AN · Boeing 777223SDR SWAA2023071760761Panel · crackedVERTICAL FIN PANEL 324AL LOWER CLIP IS CRACKED<[01] CRACKED ON VERTICAL FIN PANEL 324AL LOWER CLIP WITH NEXT DIMENSION L=3.220 TOOL USED CALIPER 2738; DUE:04/2024; DATE:04/2023 FOUND TO BE OUT LIMITS I.A.W SRM 55-30-01-0L-3 FOR IDENTIFICATION AND DUE TO NO ALLJun 19, 2023 · N417WN · Boeing 7377H4SDR DALA2023060904690Unknown · unknownCRACK INDICATION ON L/H VERT STAB ON HOLE 5 FROM BOTTOM -MARKED-. CONFIRMED CRACK IS IN SKIN LAYER ONLY QC5253. REMOVED LEADING EDGE VERTICAL STAB REF. B717, AMM 55-32-01. C/W ERA 609501-14AD REV ORIGINAL PERMANENT REPAIR SECTION I QC5270. REINSTALLED LEADING Jun 8, 2023 · N977AT · Boeing 717200SDR DALA2023060904689Unknown · unknownCRACK INDICATION ON L/H VERT STAB ON HOLES 5 FROM BOTTOM -MARKED-. C/W PRI 609501-14AD REV 0 AND 1 QC 5270. C/W PRI 609501-14AD REV 2 QC 5270. FINAL ERA 609501-14AD REV ORIGINAL MATCHES ALL STEPS OF PRI 609501-14AD REV 0, 1, AND 2 QC 5270. ASSOCIATED ER/A 14-6Jun 8, 2023 · N977AT · Boeing 717200SDR DALA2023060604616Unknown · unknownSHIP 660 DEFECT ON VERTICAL STABILIZER EXTERNAL SKIN (RH SIDE) ADJACENT TO FSS 195.390 AND FRONT SPAR. CORRECTIVE ACTION: SUMMARY OF NRC 00692: AREA ON VERTICAL STABILIZER EXTERNAL SKIN (RH SIDE) ADJACENT TO FSS 195.390 AND FRONT SPAR WAS REPAIRED PER ER/A 608Jun 4, 2023 · N660DL · Boeing 757232SDR SWAA2023071755605Panel · brokenVERTICAL FIN - BROKEN TRAINING EDGE ON 324TL PANEL ASSY - TRAINING EDGE; BEAM SEAL; VERTICAL FIN<[01] BROKEN TRAINING EDGE ON 324TL PANEL ASSY REPLACED PER SRM 51-10-02-0G-0-A00248 STEPV9. A. (1). TO BE INSTALLED ON CARD TTG8Q00KMT4H;[02] UPDATED PARTS REQUIREJun 2, 2023 · N963WN · Boeing 7377H4SDR DALA2023053104339Unknown · unknownNOTED CRACK INDICATIONS IN 6 HOLES BELOW EXISTING REPAIR (MARKED). REF AA 5530-01048-02 STEP 8, AA 2018-10 -08. SEPARATED LAYERS REF STEP 9 OF AA CARD 5530-01048-02. CONFIRMED CRACKS ARE IN SKIN ONLY (7 EA). INSTALLED REPAIR DOUBLER PER ERA 609262-14 AD REV ORMay 31, 2023 · N980AT · Boeing 717200SDR CALA2023052601654Skin · damagedR/H HORIZONTAL STAB LOWER INSPAR SKIN REQUIRES FABRICATION AND INSTALLATION OF DOUBLER TO INCORPORATE 3 EACH REMOVED SKIN DOUBLERS AND 4 EACH NEW SKIN CRACK CUT-OUTS BTWN APPROX STAB STATIONS 101.90 TO 138.5. CYCLES REF SRM 55-10-01-2R-11 REPAIR 11 PAR.5A. (SEMay 24, 2023 · N78285 · Boeing 737824SDR AALA202306137418Panel · delaminatedAIRCRAFT WAS GROUNDED: LEFT HAND VERTICAL STABILIZER PANEL 322BL DELAMINATED. **SUPPLEMENTAL REPORT FOR AALA202305187418: MAINTENANCE REPAIRED PANEL 322BL PER SRM 55-30-01-2R** (CLOSED)May 15, 2023 · N770AN · Boeing 777223SDR AALA202305187418Panel · delaminatedAIRCRAFT WAS GROUNDED: LEFT HAND VERTICAL STABILIZER PANEL 322BL DELAMINATED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)May 15, 2023 · N770AN · Boeing 777223SDR DALA2023051103711Unknown · unknownIN REF TO CARD AD A.A. 5530-01048-03: PERFORM PERMANENT REPAIR (VERTICAL STABILIZER SPLICE BAND). SUMMARY OF NRC-00504: 48 HOLES OF VERTICAL STABILIZER LEADING EDGE STA ZFS=52.267. WERE MEASURED AND 26 HOLES OF 1/4" DIAMETER AND 5 HOLES OF 3/16" DIAMETER WERE May 10, 2023 · N970AT · Boeing 717200SDR IXXA2023042404Skin · delaminatedVERTICAL AUX SPAR SKIN DELAMINATEDApr 24, 2023 · N347AZ · Boeing 767300SDR DALA2023042703287Unknown · unknown12TH HOLE ABOVE ZFS=52.267 HAS CRACK INDICATION ON VERT STAB R /H SIDE REF ERA 560946-14AD REV O AND LOG 0252731. REMOVED VERTICAL STAB L/E PER B717 AMM TASK CARD 55-32-01 00-802. CLEANED AND REINSPECTED 12TH HOLE ABOVE ZFS=52.267 PER ERA 560946-14AD ORIG. NO Apr 19, 2023 · N978AT · Boeing 717200SDR SWAA2023053128539Access Door · elongatedELONGATED HOLE ACCESS DOOR 324KL AT VERTICAL STABILIZER 2023-258055<[01] TOOL USED: CALIPER; PN: 8647A42; SN: B22058354; DUE DATE: 27-AUG-23.;[02] TOOL USED: POWER PACK P/N PE1068 S/N PE0318-95852 DUE DATE 12 AUG 23; THERMOMETER P/N FLUKE 566 S/N AE-405679 DUEApr 17, 2023 · N7815L · Boeing 73776QSDR SWAA2023051125569Panel · crackedCRACK ACCESS PANEL 321A RIB 8 AT VERTICAL STABILIZER 2023-247433<[01] REPLACED RIB 8 LOC ON ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 174A1008 SHEET 3 REV - AND DWG 174A0103 SHEET 7 REV -. SEE INDIVIDUAL SIGN OApr 10, 2023 · N284WN · Boeing 7377H4SDR DALA2023040502677Unknown · unknownSECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00428: FASTENERS HOLES COUNTER SINK AND DIAMETER ON RH VERTICAL STABILIZER LEApr 4, 2023 · N970AT · Boeing 717200SDR DALA2023040502676Unknown · unknownSECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00427: FASTENERS HOLES COUNTER SINK AND DIAMETER ON LH VERTICAL STABILIZER LEApr 4, 2023 · N970AT · Boeing 717200SDR DALA2023062105033Unknown · unknown(LOG 2697708) RH VERTICAL STABILIZER SIDE SKIN DENT LOCATED BETWEEN FIN 122.31 AND 132.26. DAMAGE REPAIRED PER ERA 607597-14.Mar 31, 2023 · N939DG · Boeing 7379
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