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.
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
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 HNAA2024100300932Skin · cracked55-2310 VERT STAB AFT OF REAR SPAR 3, SKIN PROFILE CRACKED AT 2 PLACES. FARICATED NEW PROFILE IAW SRM 55-30-01. RAR PROFILE IAW SRM 51-40-02SDR HNAA2024103001039Skin · dented53-2016 MULTIPLE DENTS ON SIDES OF DORSAL FIN ATTACHMENTS. REPAIRED IAW ETD 2024-145-025466 AND EO1-53-24-0641SDR WRXR20240918002Skin · damaged620FH PERM REPAIR FOR DAMAGED SCREW HOLE TO THE VERTICAL STABILIZER RH SKIN BETWEEN RIB 2 & RIB 3 AND BETWEEN FRONT SPAR & STRG 1. C/W 620FH PERMANENT REPAIR FOR THE DAMAGED HOLE TO V-STAB RH SKIN BTW RIB 2 & RIB 3 AND BTW FRONT SPAR & STRG 1 (PERMANENT REPASDR DALA2024091809176Skin · damaged(LOG 0557531) VERTICAL STABILIZER RH INSPAR SKIN DAMAGED BY LIGHTNING STRIKE. REPAIRED PER ERA 620725-14.SDR AALA202409165562Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL STABILIZER FIXED LEADING EDGE EXPANSION JOINT ASSEMBLY AT STA 1007.65, RBL 11. REPLACED JOINT ASSEMBLY PER AARD 51-00-05-1 REPAIR 1 AND EA 357838.SDR HNAA2024101400965Skin · cracked53-2260 VERT STAB, AFT OF REAR SPAR 3, RH SKIN PROFILE CRACKED BTW YH1423 AND YH1932. REPAIRED IAW EO 1-55-24-0577SDR DALA2025040102434Erosion Shield · peelingVERTICAL STABILIZER LEADING EDGE EROSION TAPE FOUND PEELED UP, REQUIRES REPAIR. INSPECTED VERTICAL STABILIZER LEADING EDGE EROSION TAPE AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS EROSION TAPE TO MEET AERODYNAMIC SMOOTHNESS IAW A220 ASRP 55-32-01-01AAA-SDR DALA2025060504287Tape · damagedVERTICAL STABILIZER LEADING EDGE EROSION TAPE FOUND DAMAGED. INSPECTED VERTICAL STABILIZER LEADING EDGE EROSION TAPE AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS EROSION BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW A220 ASRP 55-32-01- 01AAA-662A-A. FSDR VNAA20251004015Skin · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WSDR DALA2024081908281Splice · cracked-AD- FOUND 2 CRACK INDICATIONS ON LEFT SIDE OF VERTICAL STAB BELOW SPLICE AT STA 2F552.267 WHILE PERFORMING BHEC PER AA 5530-01048 STEP 8 REF AD2018-10-08. HOLES ARE MARKED. AFTER SEPARATION OF LAYERS CONFRIMED CRACK INDICATIONS FROM FWD FLANGE LAYER REF AA553SDR HNAA2024091600824Skin · cracked55-2341 RH SKIN CRACKED ON BOTTOM OF VERT STAB AFT OF SPAR 3. REPAIRED IAW EO1-55-24-0518SDR IXXA2024080902Panel · debondedRH SIDE OF VERTICAL STAB BETWEEN FRONT SPAR AND AUX SPAR BONDED SKIN PANEL DELAMINATION VIEWED IN BETWEEN FSS 170.259 TO 220.251SDR DALA2024080907919Stabilizer · distortedTHE COUNTERSINK OF THE FASTENERS HOLES OF THE VERTICAL STABILIZER LEADING EDGE WERE NOTED WORN ALL AROUND EDGES BETWEEN ZFS 52.267 TO 153.938. SUMMARY OF NRC 00748: THE LEADING EDGE OF THE VERTICAL STABILIZER IS OUT OF LIMITS, AS REPAIRABLE HOLE LIMITS PER B71SDR IXXA2024080203Skin · debondedVERTICAL STAB LEFT HAND SIDE LOWER BONDED PANEL REQUIRES COMPOSITE REPAIRSDR IPXA2024081495158Skin · debondedDISBOND - SKIN, RH VERTICAL STABILIZER PANEL P/N: 186U1007-4 INNER SKIN, TOTAL: 2 AREA (COMPOSITE REPAIR).NDT PERFORM UT INSPECTION FOR REPAIRED AREA AND PLUS 6 INCHES AROUND HEATED AREA, PER NTM PART1 51-01-01 AND 51-40-00 REV:177, RESULT: NO DEFECT FOUND. CSDR DALA2024072307413Skin · damaged(LOG 6058394) DAMAGE SUSPECTED ON LEADING EDGE OF VERTICAL STABILIZER. REPAIRED DAMAGED LEADING EDGE PER B737 PER B737 55-30-01.SDR UIEA2024070400583Skin · delaminatedDELAMIATION ON SKIN OF VETRICAL STABILIZER 3" ABOVE FSS 1195.390 AND NEAR LEADING EDGE(<P>VETRICAL STABILIZER 3" ABOVE FSS 1195.390 AND NEAR LEADING EDGE WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 NOTE F PAG 1-2 AND SRM 51-70-10-2R--4 REPAIR 4 FIG 201 SDR HNAA2024090500232Skin · crackedVERT STAB AFT OF SPAR 3 LH SKIN UPPER PROFILE CRACKED.SDR HNAA2024090500227Skin · chafedBOTTOM OF VERT STAB FWD OF FRONT SPAR 1, BOTH LIPS CHAFED.SDR DALA2024070306745Skin · crackedWHILE IN ATL FOR SCHEDULED MAINTENANCE AND DURING ACCOMPLISHMENT OF WORKCARD 5530-01048-02, MAINTENANCE REPORTED CRACK INDICATIONS AT TWO EXISTING FASTENER LOCATIONS IN THE RH FRONT SPAR CAP LAYER FORWARD FLANGE. SUBJECT FASTENERS ARE IDENTIFIED AS HOLE 4 AND SDR DALA2024062706578Skin · crackedAIRCRAFT 9508, WHILE ACCOMPLISHING HFEC INSPECTION PER WORK CARD 5530-01048-02 IN COMPLIANCE WITH FAA AD 2018-10-08, MTC FOUND THREE (3) FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE SKIN (P/N 5910189-15) BELOW ZFS 52.267 WITH CRACK INDICATIONS. THE DSDR SWAA2024072911624Panel · crackedRIGHT VERTICAL FIN PANEL#323AR ASSY SUPPORT ANGLE LOWER SURFACE HAS BARE METAL. RIGHT VERTICAL FIN PANEL#323AR ASSY CRACKED AT LOWER CORNER<[01] RECEIVED NEW PART. LOCATED AND DRILLED AND COUNTERSUNK FASTENER HOLES ON NEW VERTICAL PANEL 323AR REF. SRM 51-40-05SDR HNAA2024072900631Skin · cracked55-2318 VERTICAL STAB LH SKIN CRACKED ON UPPER PROFILE. R & R PROFILE IAW SRM 51-40-02SDR HNAA2024072600608Skin · cracked55-2318 VERT STAB LH SKIN HAS CRACKED UPPER PROFILE. R & R PROFILE IAW SRM 51-40-02. FABRICATED PROFILE IAW SRM 55-30-01SDR SWAA2024080503693Panel · elongatedPANEL 323CL PN 172A6124-1 ENLONGATED HOLES<[01] RECEIVED NEW PANEL 323CL P/N 1726164-1.<BR>LOCATED; DRILLED AND COUNTERSUNK NEW HOLES ON NEW PANEL 323CL P/N 172A6124-1 REF. SRM 51-40-05-0G-0.<BR>NEW PANEL 323CL P/N 1726164-1 WOULD BE PAINTED PER NON ROUTINE ITSDR DALA2024061906228Access Panel · crackedSHIP 3140 CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 618265-14. (0400452)SDR DALA2024061105983Access Panel · crackedSHIP 3140 CRACK ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 618280-14. (0386684)SDR DALA2024060705864Access Panel · crackedSHIP 3132 CRACK ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 617918-14. (0379817)SDR DALA2024060705863Access Panel · crackedSHIP 3132 CRACK ACCESS PANEL 322BL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 617922-14. (0379810)SDR JGVR20240604002Skin · damagedREPAIRED LH VERTICAL STABILIZER SKIN AT THE OPENINGS OF ACCESS PANELS 341AL, 341BL, 341CL, AND 341DL BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATED AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH AEROSPACE QUALITY RESDR JGVR20240604001Skin · damagedREPAIRED THE LH SKIN OF VERTICAL STABILIZER AT THE UPPER AFT CORNER BY BLENDING CORRODED AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH AND DEVELOPMENT ENGINEERINGSDR JGVR20240603001Skin · damagedREPAIRED RH VERTICAL STABILIZER SKIN AT THE OPENINGS OF ACCESS PANELS 341AR, 341BR, AND 341DR BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATED AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH SDR DALA2024053005666Access Panel · crackedSHIP 3102 CRACK ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 618212-14. (0367244)SDR DALA2024053005665Access Panel · crackedSHIP 3102 CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 618189-14. (0367241)SDR DALA2024051305151Skin · delaminatedSHIP 190 FOUND VERTICAL STABILIZER LH SKIN AUXILIARY SPAR TO FRONT SPAR FSS 245 DELAMINATION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 55-30-01-2R-1 AND SRM 51-70-10-2R (0340098)SDR DALA2024051405173Skin · crackedCRACK WAS FOUND OVER THE VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP. SUMMARY OF NRC 00469: CRACK ON VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP WAS REPAIRED (WELDED) PER ER/A 382101-14MA REV H. SECTION I: PERMANENT REPAIR. ASSOCIATSDR DALA2024051305144Skin · delaminatedSHIP 190 FOUND VERTICAL STABILIZER LH SKIN AT FSS 65 TO FSS 118 FROM FRONT SPAR 10 INCH DELAMINATION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 55-30-01-2R- 1 AND SRM 51-70-10-2R. (0331960)SDR DALA2024051305143Skin · delaminatedSHIP 190 FOUND VERTICAL STABILIZER LH SKIN AT FSS 65 TO FSS 118 FROM AUXILIARY SPAR 10 INCH DELAMINATION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 55-30-01 (0331953)SDR DALA2024050704998Skin · delaminatedSHIP 1815 FOUND OUT LH VERTICAL STABILIZER SKIN DELAMINATION AT 60 INCHES TO LE AND 50 INCHES TO LOWER EDGE. CORRECTIVE ACTION: LH VERTICAL STABILIZER SKIN REPAIRED AT 60 INCHES TO LE AND 50 INCHES TO LOWER EDGE AS PER PRI 585586-14.REV.0.THE PRI 585586- 14.RESDR IXXA2024050502Skin Panel · damagedRH VERTICAL STAB BETWEEN AUX SPAR AND FRONT SPAR AT RIB 2-3 HAS EDGE CORE DAMAGESDR IXXA2024050501Access Panel · delaminatedRH VERTICAL STABILIZER BETWEEN AUX SPAR AND FRONT SPAR RIBS 2-3 HAS DELAMINATIONSDR DALA2024050104833Skin · delaminatedSHIP 1815 FOUND OUT RH VERTICAL STABILIZER SKIN DELAMINATION AT 28 INCHES TO LE AND 72 INCHES TO LOWER EDGE. CORRECTIVE ACTION: RH VERTICAL STABILIZER SKIN REPAIRED AT 28 INCHES TO LE AND 72 INCHES TO LOWER EDGE AS PER B767-400 SRM 51-70-10-2R-4. (0321057)SDR DALA2024050104832Skin · delaminatedSHIP 1815 FOUND OUT RH VERTICAL STABILIZER SKIN DELAMINATION AT 30 INCHES TO LE AND 106 INCHES TO LOWER EDGE. CORRECTIVE ACTION: RH VERTICAL STABILIZER SKIN REPAIRED AT 30 INCHES TO LE AND 106 INCHES TO LOWER EDGE AS PER B767-400 SRM 51-70-10 (0321050)SDR DALA2024043004792Skin · damagedELONGATED HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS FOUND STA ZFS=52.267 IN REF NRC 0525. SUMMARY OF NRC 00611: HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS REPAIRED PER B717-200 SRM 55-30-01-2R PRSDR AALA202404183249Panel · delaminatedAIRCRAFT WAS GROUNDED: DISBONDED / DELAMINATED VERTICAL STABILIZER PANEL AT FRONT SPAR STA 90.0. REPAIRED PANEL PER SRM 55-30-01-2R REPAIR 2.SDR DALA2024041804532Skin · cracked-AD- FOUND 4 EA HOLES ON LT VERT BELOW EXISTING DOUBLER AT SPLICE SHOWING CRACK INDICATIONS. C/W ER/A 617313-14AD REV ORIG SECTION I PERMANENT REPAIR. ALL RII C/W (QC1430) REF TO LOG PAGE 0297160 AND BUFF NRC 001. ASSOCIATED ER/A 14-6173133SDR DALA2024041804530Skin · cracked-AD- VERTICAL STAB LEFT SIDE 4 EA HOLES HAVE CRACK INDICATIONS, IN SKIN LAYER ONLY, JUST BELOW ZFS 52.267. BHEC INSP CONFIRMS CRACKS IN 4 EA HOLES IN SKIN LAYER ONLY REF AA 5530-01048 AND AD 2018-10-08 -MARKED-. COMPLIED WITH PRI 617313-14AD REV 0. C/W PRI 617SDR DALA2026032301952Skin · damagedPOSSIBLE DMG ON VERTICAL STABILIZER 1/3 FROM THE TOP OF THE LEADING EDGE. DEFERRED TO MON PER A220 ASRP 55-32- 01-01AAA-662A-A. REP CK EVERY 850 FLT HRS AND TERMINATING REPAIR IN 8500 FLT HRS. C/W REP INSP OF VERTICAL STABILIZER IAW A220 ASRP 51-12-00-03AAA-66SDR SWAA2024052074035Access Door · crackedCRACK ON PLATE ACCESS DOOR 323AL AT VERTICAL STABILIZER 2024-253381<[01] REPLACED PLATE ACCESS DOOR 323AL AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 172A6122 REV B;[02] COMPLETED TASK CERTIFIEDSDR YENA2024041600576Skin · unknownDURING HEAVY MAINTENANCE: STABILIZERS / VERTICAL STABILIZER / LEADING EDGE PANEL 322BL / OUTER SKIN / RE-SKIN – STANDARD PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)
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