JASC 5532
Service difficulty reports · 1,745
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 FDEA202610151596Panel · dentedDENT AT VERTICAL STAB LH SIDE COMPOSITE PANEL FWD OF FRONT SPAR LWR AREA BETWEEN FSS 119 TO FSS 170. REPAIRED DENT AT VERTICAL LH SIDE TORQUE BOX COMPOSITE PANEL LWR AREA BETWEEN FSS 119 TO FSS 170 IAW B757-200 SRM 55-30-01-2R, REPAIR 5 FIG 201, SHEET 1 MSDR LR7A2026092403969Skin · crackedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5511, FOUND VERTICAL STABILIZER LH SKIN CRACKED, FS1095, LBL15, VSS02. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12.SDR IPXA2026092191640Panel · erodedERODED VERTICAL STAB LE PANEL 321E. REMOVED THE DAMAGE MATERIALS AND CLEAN. BONDED THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.SDR DALA2026091805205Skin · crackedCRACK WAS FOUND AFFECTING A BUSHING INSTALLED IN THE VERTICAL STABILIZER LEADING EDGE SKIN REPAIR DOUBLER INSTALLATION LOCATED BETWEEN ZFS= 44 AND ZFS=52, HOLE #65, COMPLIED WITH ER/A 620945-14AD. (1817838) (AIRCRAFT GROUNDED).SDR IPXA2026091947140Skin · erodedERODED SKIN , VST FIN TIP AREA PANEL 327 EXTERNAL SURFACE. PERFORMED NDT/UT FOR REWORKED AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1 51-01-01, REV 183. NO DEFECT FOUND. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILMSDR SWAA2026101472863Plate · corrodedCORRODED PLATE VSS 276, VERTICAL STABILIZER T/E. REPLACED THE PLATE IAW SRM 51-40-02, AND DWG 175A1601, SHEET 18, REV A.SDR FXTA20260904001Skin · crackedINSPECTION PANEL ON TOP OF THE VERTICAL STABILIZER ATTACHMENT FLANGE CRACKED ALLOWING THE PANEL TO DEPART AIRCRAFT. THIS INSPECTION PANEL IN UNDER THE RUDDER HORN. TOP PANEL P/N: 7831102-23, ONCE ATTACHMENT FAILS HITS RUDDER AND PIECE FOUND IN ELEVATOR CONTROLSDR UIEA2026082700809Panel · abnormalVERTICAL STAB SKINS, TORQUE BOX PANEL, TIME LIMITED REPAIR. TORQUE BOX PANEL REPLACED IAW SRM 51-10-02 & 51-40-02, REV 107, AND RI-55-30-18471, REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026082700814Panel · debondedLEFT VERTICAL FIN TORQUE BOX PANEL (BELOW RUDDER STA 33) FOUND DEBONDED. TORQUE BOX PANEL REPLACED IAW SRM 51-10-02 & 51-40-02. REV 107. AND RI-55-30-18471 REV A. NO FURTHER DEFECT NOTED.SDR NI6R202608270070Skin · crackedWHILE PERFORMING ZONE 4 INSPECTION OF SB 244 DETECTED .125" CRACK IN LT VERTICAL SKIN.SDR IPXA2026083103996Access Panel · erodedVERTICAL STAB TIP ACCESS PANEL 327, SKIN ERODED. REMOVE THE EROSION MATERIALS AND CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 240 MINS WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 55-30-30-2R-1, REF SRM 51-70-04-2R-1, & SRM 51-30-10-0G-0, REV 49SDR IPXA2026082003996Access Panel · erodedVERTICAL STABILIZER TIP ACCESS PANEL 327 SKIN EROSION (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 6" AROUND HEATED AREA ,PER 747 NDT MANUAL PART 1 51-01-01 REV:183 <BR>RESULT:NO DEFECT WAS FOUNDSDR UIEA2026072100635Skin · damagedVERTICAL STABILIZER THE TOP AFT TIP FOUND ELECTRICAL ARCING DAMAGE APPROX 4CM IN DIAMETER(<P>FAIRING DAMAGE AREA REPAIRED AS PER RI-55-31-18434 REV A. NO FURTHER DEFECTS NOTED</P>)SDR CALA2026071217693Skin · dented(SDR) LH VERTICAL STAB FIXED SKIN JUST BELOW APPROX FFS 119.467 HAS 1EA DENT. WC: 16068 SFR CW WSHAW ACCOMPLISHED REPAIR IAW SRM 51-70-10-2R-2 VIA PN 04-009-004 BATC H 4464640, RESTORED FINISH IAW SRM 51-21-14-370-803 & SRM 51-21- 15-370-801 PER SRM 55-30-01-2SDR CALA2026071217691Skin · dentedLEFT VERTICAL STAB FIXED SKIN BETWEEN APPROX FSS 195.390 AND FSS 270.784 HAS 3EA DENT. ACCOMPLISHED REPAIR IAWSRM 51-70-10-2R-2 VIA PN 04-009-0044 BATC H 0004464640, RESTORED FINISH IAW SRM 51-21-14-370-803 & SRM 51- 21-15-370-801, PER SRM 55-30-01-2R-5 CLASSDR DALA2026070603942Skin · damagedSKIN DAMAGE LT VERT CAP FROM AIR GATE FAIRING. REPAIRED PER ER/A 635425-14. (1679920)(AIRCRAFT GROUNDED)SDR IPXA2026072111084Panel · debondedDEBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322BL. REPAIR DISBOND ON PANEL ASSY OF VST FWD TORQUE BOX BETWEEN STA 2365 AND STA 2413 I.A.W. EGAT EI F2026A55M-1378 REV.1 AND UPS EO-98179-REQ1 REV.1 2. CONDITION CHECK IS SATISFACTORY.SDR IPXA2026072111043Panel · debondedDISBONDED PANEL , VERTICAL STABILIZER LOWER PANEL 322CL. REPAIR DISBOND DAMAGE ON LH FWD LWR VST FORWARD TORQUE BOX PANEL BETWEEN STA 2285 AND 2365 AND BETWEEN FIN WL10 AND 25 I.A.W. EGAT EI NO. F2026A55M-1379 REV. 1 AND UPS EO-98180-REQ1 REV. 2SDR CALA2026083119091Skin · damagedTWO RIVETS ON LT LOWER VERTICAL STAB SKIN ARE PULLING THROUGH. PERFORMED PART 1 INTERIM REPAIR STEPS 1 AND 2, REMOVED FASTENERS & VISUAL INSPECTED AREA. IAW EC/RA 5530-02054 STEP 1 INTERIM REPAIR STEPS 3 AND 4, PERFORMED HFEC HOLE PROBE INSPECTION IAW NDTSDR REXA2026082601716Access Panel · crackedCRACK ON FASTENER HOLE OF ACCESS PANEL NBR:326DL. ACCESS PANEL NBR:326DL WAS REPAIRED PER EA NO. CRJ955-22596 REV IRSDR LR7A2026061903864Skin · corrodedDURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND VERTICAL STAB RH AFT SKIN CORRODED AT FS 1115, VSS 30, RBL 11. REPAIRED IAW LOCKHEED SRM 51-140-12.SDR DALA2026061903676Skin · out of limitsHOLES OUT OF LIMITS ON LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE. LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE WAS REPAIRED PERSDR HNAA2026062900558Skin · crackedVERTICAL STAB, AFT OF SPAR 3, LT SKIN TRAILING EDGE LWR PROFILE CRACKED. R & R PROFILE IAW SRM 51-40-02SDR SWAA2026070610072Skin · bulgedRIGHT VERTICAL FIN IN SPAR SKIN BULGED; RIVETS PULLED. ITEM TRANSFERRED TO COMPONENT WORK PACKAGE TTG8Q01CNJE8.SDR 21GA202605260000Skin · delaminatedDELAMINATION LOCATED ON LEFT SIDE OF VERTICAL STABILIZER PANEL BETWEEN SPAR AND FRONT SPAR FSS 220.521 - 270-784 (MAJOR REPAIR)SDR IPXA2026050962784Access Panel · damagedMAJOR REPAIR, LT VERTICAL STABILIZER ACCESS PANEL 322DL, AT FSS 295.915 TO 371.308, HAD HAIL DAMAGE.SDR DALA2026041402345Skin · crackedREF ERA 606161-14AD REV B STEP 4 OHEC INSP OF LEFT SIDE OF VERT STAB-5TH HOLE FROM BOTTOM HAS CRACK INDICATION. REPAIRED DAMAGE PER ER/A 606161-14AD (8672001) (AIRCRAFT GROUNDED)SDR DALA2026031901907Skin · bulgedVERTICAL STABILIZER, LT SURFACE BTW AUXILIARY SPAR AND FRONT SPAR AROUND FSS 40 FOUND BULGE. REPAIRED VERTICAL STABILIZER LT SURFACE BTW AUXILIARY SPAR AND FRONT SPAR AROUND FSS 40 IAW SRM 55-30-01-2R-1 AND SRM 51-70-10-2R-4, REV 77. (LP 1501546)SDR 2026F00035Skin · corrodedLEFT AND RIGHT VERTICAL STAB UPPER SKINS HAVE 2 AREAS OF CORROSION JUST BELOW TIP CAP. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON VERTICAL STAB OUTER SKIN JUST BELOW TIP CAP, AFT AREA, 1 BLEND PER SIDE IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLESDR SWAA2026033175363Access Panel · crackedCRACKED ACCESS PANEL 324AR ON THE VERTICAL STAB. REPLACED THE ACCESS PANEL 324AR IAW SRM 51-40-02-0G, SRM 51-10-02-0G-0, & DWG 172A6123, SHEET 1, REV A.SDR IXX2026F00001Panel · delaminatedLT SIDE VERTICAL STAB PNL DELAMINATED P/N 175T2001-3SDR DALA2026021100983Skin · delaminatedDURING WALK AROUND FOUND PAINT LOSS OR DELAMINATION ON THE RIGHT SIDE OF TAIL. REPAIRED DELAMINATION ON THE RIGHT SIDE OF TAIL AS PER B767-400 SRM 55-30-01-2R-1 AND 51-70-10-2R (1438051)SDR DALA2026021100982Skin · delaminatedDURING WALK AROUND FOUND PAINT LOSS OR DELAMINATION ON THE RIGHT SIDE OF TAIL. REPAIRED DELAMINATION ON THE RIGHT SIDE OF TAIL AS PER B767-400 SRM 55-30-01-2R-1 AND SRM 51-70-10 (1438045)SDR DALA2026020500843Access Panel · corrodedWEAR AND CORROSION ON ANGLE OF EMPENAGE AREA SELMENT AREA OF ACCESS PANELS 321A, 323AL, 323BL, 323CL, 324AL, 323AR, 323BR, 323CR, 324AR AT VERTICAL STABILIZER. ANGLE OF EMPENAGE AREA SELMENT AREA OF ACCESS PANELS ON THE VERTICAL STABILIZER WERE REPLACED PER SSDR GTIA2026020539268Skin Panel · corrodedCORROSION CHANNEL RUDDER LOWER AREA ON VERTICAL STABILIZER RAF-01 6011262-02 GENERATED.-PERFORMED PERMANENT REPAIR ON CHANNEL RUDDER LOWER AREA ON VERTICAL STABILIZER I.A.W. A320 SRM 55-41-19-300-011-C1 THIS REPAIR IS CATEGORY A I.A.W. A320 SRN 51-11-14SDR DALA2026012800670Panel · delaminatedVERTICAL STABILIZER RT FIXED PANEL DELAMINATED FROM FUSELAGE 146 INCH AND FWD EDGE 36 INCH. DAMAGED AREA REPAIRED IAW SRM 51-70-10. (1412232)SDR DALA2026012800669Panel · delaminatedVERTICAL STABILIZER RT FIXED PANEL DELAMINATED FROM FUSELAGE 106 INCH AND FWD EDGE 15 INCH. DAMAGED AREA REPAIRED IAW SRM 51-70-10-2R. (1412231)SDR IXXA20260120001Panel · delaminatedRIGHT HAND VERTICAL STABILIZER UPPER FIXED LEADING EDGE PANEL DELAMINATEDSDR IXXA2026011801Panel · delaminatedLEFT HAND VERTAL STAB UPPER SURFACE LEADING EDGE BONDED PANEL DELAMINATEDSDR DALA2026012100450Skin · delaminatedVERTICAL STABILIZER RT SKIN PANEL AT VSS 245- VSS 270, BETWEEN AUX SPAR & FRONT SPAR FOUND DELEMINATED. DAMAGED AREA REPAIRED IAW ER/A 631646-14. (1404064)SDR DALA2026012100449Skin · delaminatedVERTICAL STABILIZER RT FIXED PANEL INNER SKIN BETWEEN FRONT SPAR AND AUX SPAR AT VSS 93 TO VSS 145, FOUND DELAMINATED. DAMAGED AREA REPAIRED IAW SRM 55-30-01-2R-1, SRM 51-70-10-2R-4, & SRM 51-70-10 (1400953)SDR DALA2026012100448Skin · delaminatedVERTICAL STABILIZER LT PANEL SKIN AT VSS 170- VSS 195, BETWEEN AUX SPAR & FRONT SPAR FOUND DELAMINATION. DAMAGED AREA REPAIRED IAW SRM 55-30-01-2R-1, SRM 51-70-10-2R-4, & SRM 51-70-10. (1400951)SDR SWAA2026011360118Skin · delaminatedDORSAL FIN, PN: 174A0103-7; SN: WN0346, FAILED TAP TEST. DAMAGED AREA SHOWS SIGNS OF DELAMINATION & DEBONDING IAW SRM 51-10-06. ESTIMATED AREA OF DELAMINATION & DEBONDING IS 11' X 12'. FAULT RESOLVED ON TTG8Q019TJ6B & EA 26-155-00110.SDR AALA202512195234Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: NUMBER 5 DOUBLER AFT MID DOUBLER HOLE SHOWS CRACK INDICATION AT THE 9 O'CLOCK POSITION IN THE EXTERNAL DOUBLER. REINSTALLED GUSSET NUMBER 5. PER SRM 51-40-02.SDR DALA2025121909239Skin · damagedVERTICAL STABILIZER LT SKIN PANEL DAMAGED AT ABOUT BTW FSS170 AND FSS195. DAMAGED AREA REPAIRED PER B767-400 SRM 55-30-01-2R-1 AND SRM 51-70-10-2R-4 FIG 203 AND SRM 51-70-10 (1341308)SDR DALA2025120508915Panel · delaminatedVERTICAL STABILIZER RH PANEL DELAMINATION FROM FUSELAGE 109 INCH AND FROM FWD EDGE 14 INCH. DAMAGED AREA REPAIRED PER B767-400 SRM 55-30-01 -2R-1 AND SRM 51-70-10 (1333457)SDR DALA2025120508914Panel · delaminatedVERTICAL STABILIZER LH PANEL DELAMINATION FROM FUSELAGE 109 INCH AND FROM FWD EDGE 14 INCH. REPAIRED VERTICAL STABILIZER LH PANEL DELAMINATION FROM FUSELAGE 109 INCH AND FROM FWD EDGE 14 INCH AS PER B767-400 SRM 55-30-01 -2R-1 AND SRM 51-70-10-2R-4 REV 76 (1SDR EE4Y2025111323450Skin · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LH SKIN PANEL OF THE VERTICAL STABILIZER, LOCATED NEAR THE AFT EDGE JUST BELOW RIB 06. THE AFFECTED AREA FALLS WITHIN A NON-REPAIRABLE ZONE AS DEFINED IN SRM 55-30-01/REPAIR 58P. THE CONDITION REPORTED WAS REPAIRED ISDR JGVR20251110003Skin · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON RH VERTICAL STABILIZER SKIN, JUST FORWARD OF ACCESS PANEL 341BR PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR SWAA2025112832413Access Panel · crackedCRACK ACCESS PANEL 321A ON RIB 8 VERTICAL STABILIZER. REPLACED RIB 8 LOCATED ON PANEL 321A.IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 174A0103 SHEET 1 REV:- MEASURE OF CRACK IS:L=0.133.
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