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 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.Jan 10, 2026 · N945WN · Boeing 7377H4SDR 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.Dec 8, 2025 · N947NN · Boeing 737823SDR 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)Dec 8, 2025 · N839MH · Boeing 767432ERSDR 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)Dec 3, 2025 · N835MH · Boeing 767432ERSDR 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 (1Dec 3, 2025 · N835MH · Boeing 767432ERSDR 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 INov 13, 2025 · N258JB · Emb ERJ190100IGWSDR 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.Nov 10, 2025 · N320QS · Cessna 680CESDR 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.Nov 6, 2025 · N944WN · Boeing 7377H4SDR DALA2025110708139Skin · crackedCRACK SKIN INSIDE OF ACCESS PANEL 370BL FWD /UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN. CORRECTIVE ACTION: UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN WAS REPAIRED PER B717 SRM 55-30-01 (1278507)Oct 29, 2025 · N947AT · Boeing 717200SDR LR7A2025102803793Skin · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND RH V-STAB SKIN CRACKED AT FS1124, RBL10, VSS 257. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12.Oct 28, 2025 · N408LC · Lkheed 382GSDR IXXA20251019001Skin Panel · delaminatedBONDED PANEL ON RIGHT SIDE OF VERTICAL STAB DELAMINTED AT FSS.295Oct 19, 2025 · N251AZ · Boeing 767323SDR DALA2025101707594Skin · damagedFASTENERS (45 EA) ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR STA ZFS =52. CORRECTIVE ACTION: VERTICAL STAB LEADING EDGE REPAIR STA ZFS =52 WERE REMOVE AND INSTALL PER CARD 5530-01048-02 AND DVI WAS PERFORMED ON RH/LH VERTICAL STAB LEADING EDGE STRUCTURE SPLOct 13, 2025 · N946AT · Boeing 717200SDR DALA2025101707593Skin · wornSHIP 9528 LEADING EDGE UPPER SKIN PANEL / FASTENERS WORN ALONG OUTER PERIMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 620349-14 (1245364).Oct 10, 2025 · N990AT · Boeing 717200SDR IXXA2025101000001Panel · crackedLARGE BONDED PANEL ON L/H SIDE OF VERTICAL HAS DELAMINATION AT FSS 295Oct 10, 2025 · N251AZ · Boeing 767323SDR DALA2025100707304Panel · damagedSHIP 688 CORE DAMAGE ON INSIDE OF PANEL AT CORE EDGES. CORRECTIVE ACTION: REPAIRED CORE PER B757-200 SRM 55-30-01-2R-5. (1236368)Oct 6, 2025 · N688DL · Boeing 757232SDR DALA2025100707303Skin · damagedSHIP 688 DISBOND FOUND ON LWR PANEL ASSY. CORRECTIVE ACTION: REMOVED DAMAGE PER B757 SRM 55-30-01-2R-5. PREPARED AREA FOR SKIN, INTERNAL DOUBLER & CORE INSTALL PER B757 SRM 55-30-01-2R-5. LAID UP & CURED, FILLER, DOUBLER & CORE PER B757 SRM 55-30-01-2R-5. PREPOct 5, 2025 · N688DL · Boeing 757232SDR DALA2025091906886Access Panel · crackedCRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. COMPLIED WITH ER/A 628592-14. (1205816).Sep 18, 2025 · N352NB · Airbus A319114SDR AALA202509122565Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION TO VERTICAL STABILIZER RIGHT SIDE PANEL. REPLACED PANEL PER EA 367930A.Sep 12, 2025 · N775AN · Boeing 777223SDR HNAA2025091100602Skin · crackedFUSELAGE UPPER SKIN PLATE, JUST FWD OF RUDDER 1, AT FR 81 CRACKED INSIDE 312AR. R&R CRACKED FUSELAGE UPPER SKIN PLATE, JUST FWD OF RUDDER 1, AT FR81 INSIDE 312AR IAW EMB145 SRM 51-40-02 AND SRM 51-20-01.Sep 6, 2025 · N646AE · Emb EMB145LRSDR FDEA202509051632Skin · dentedA DENT ON EXTERNAL SKIN OF VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR AT FSS 28 AND B. STA 1643 APROX (LH SIDE). VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR AT FSS 28 AND B. STA 1643 APROX (LH SIDE) WAS REPAIRED IAW B767 SRM 55-30-01-2R FIG 201 Sep 5, 2025 · N129FE · Boeing 7673S2FSDR DALA2025090106455Access Panel · crackedCRACKED ACCESS PANEL 322CL ON VERTICAL STABILIZER. COMPLIED WITH ER/A 628653-14. (1174634).Aug 31, 2025 · N317NB · Airbus A319114SDR DALA2025090106454Access Panel · crackedCRACKED ACCESS PANEL 322AL ON VERTICAL STAB. COMPLIED WITH ER/A 628655-14. (1173616).Aug 31, 2025 · N317NB · Airbus A319114SDR IXX2025F00016Skin · delaminatedVERTICAL STAB PANEL LEFT SIDE DELAMINATEDAug 31, 2025 · N1439A · Boeing 76733ASDR HNAA2025091100601Skin · crackedWHILE PERFORMING NDT INSPECTION AT AREA JUST FORWARD OF RUDDER 1, FOUND THAT THE VERTICAL STAB TRAILING EDGE RH SKIN PROFILE JUST ABOVE RUDDER 1 LOWER HINGE FITTING IS CRACKED. INSTALLED REPAIR PARTS ON VERTICAL STAB TRAILING EDGE RH SKIN PROFILE JUST ABOVE RUAug 21, 2025 · N646AE · Emb EMB145LRSDR DALA2025081806154Skin · crackedSHIP 9541 C/W ERA 628422-14AD REV ORIG VERTICAL STABILIZER LHS & RHS LEADING EDGE SKIN ZFS52.267 FASTENER HOLES CRACKED. CORRECTIVE ACTION: C/W PRI 628422-14AD. (1145072)Aug 15, 2025 · N977AT · Boeing 717200SDR IXXA2025082801Skin · delaminatedRHS VERTICAL STAB SKIN PANEL DELAMINATED AT FSS 270Aug 9, 2025 · N1439A · Boeing 76733ASDR R61A2025082500377Skin · dentedDURING HEAVY CHECK FOUND PROTRUDING DENT FOUND ON R/H VERTICAL STAB SKIN BETWEEN RIB 8 AND RIB 9 STR 9C. REPAIRED VERTICAL STAB SKIN IAW ETD 2025-170-926774Aug 5, 2025 · N208QJ · Emb ERJ170200LRSDR SWAA2025081596842Panel · crackedPANEL 324BL CRACKED ON EDGE NEAR FASTENER HOLE. REPAIRED VERTICAL STAB TRAILING EDGE PANEL 324BL IAW SRM 55-30-01-2R-9, SRM 51-70-04-2R-6, AND SRM 51-70-04-2R-0 REPAIR GENERAL.Jul 30, 2025 · N965WN · Boeing 7377H4SDR CALA2025072506903Skin · dentedT-DOCS:B737-06-3-0066-61-20-01. VERTICAL FIN LEADING EDGE LEFT SIDE BETWEEN FIN STA 142.2 TO FIN STA 159.8 HAS DEEP DENT. ACCOMPLISHED REPAIR AT VERTICAL FIN LEADING EDGE BETWEEN STA 166.561 TO 175.938 SRM 55-30-01-2R-1 AND 51- 40-02-0G-0.Jul 24, 2025 · N27271 · Boeing 7378SDR DALA2025072405559Skin · damaged(LOG 1098837) WHILE THE AIRCRAFT WAS BEING TOWED, A LIFELINE CAUSED DAMAGE TO IT, TWO DENTS ON VERTICAL STABILIZER LEFT INSPAR SKIN, BETWEEN LE STA 196.66-205.86. VERTICAL STABILIZER LEFT INSPAR SKIN, BETWEEN LE STA 196.66-205.86 WAS REPAIRED PER B737-800 SRM Jul 22, 2025 · N3757D · Boeing 737832SDR SWAA2025072988571Access Panel · damagedELONGATED HOLE ACCESS PANEL 323CL AT VERTICAL STABILIZER. REPLACED ACCESS PANEL 323CL AT VERTICAL STABILIZER IAW B737-700 DWG 172A6120 SHEET 1 REV. F.Jul 5, 2025 · N7887A · Boeing 737752SDR SWAA2025072287466Panel · crackedVERTICAL STAB PANEL 323CL LOWER CLIP CRACKED. REMOVED AND REPLACED PANEL 323CL LOWER CLIP IAW SRM 51-40-02-0G-0 AND SRM 51-40-06-0G-0.Jul 1, 2025 · N442WN · Boeing 7377H4SDR DALA2025070104932Access Panel · crackedSHIP 3169 CRACK ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 627102-14. (1055140).Jun 30, 2025 · N369NB · Airbus A319114SDR DALA2025070104931Access Panel · crackedSHIP 3169 CRACK ACCESS PANEL 322BL LEADING EDGE ON VERTICAL STABILIZER. CORERCTIVE ACTION: COMPLIED WITH ER/A 627100-14. (1055104).Jun 30, 2025 · N369NB · Airbus A319114SDR DALA2025061604541Access Panel · crackedCRACKED ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER. COMPLIED WITH ER/A 626387-14. (1023933).Jun 14, 2025 · N335NB · Airbus A319114SDR 7C7A2025061400018Skin Panel · delaminatedSKIN PANEL DELAMINATIONJun 9, 2025 · N627NP · Boeing 7572B7SDR DALA2025061104455Skin · damagedAIRCRAFT 9577, VERT STAB LEADING EDGE SKIN, B717 - REPAIR, RII IN REF PER AMDS 5530-01048-03. CORRECTIVE ACTION: VERT STAB LEADING EDGE SKIN, B717 - REPAIR, RII WAS ACCOMPLISHED PER AMDS 5530-01048-03. (LP 1014363)Jun 9, 2025 · N921AT · Boeing 717200SDR 7C7A2025060109001Panel · delaminatedDURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 000439970Jun 9, 2025 · N629NP · Boeing 7572B7SDR 7C7A2025060900017Panel · delaminatedDURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 0004399Jun 9, 2025 · N628NP · Boeing 7572B7SDR DALA2025060804359Fastener · looseARCRAFT 9577, LOOSE FASTENERS ON RH/LH LEADING EDGE SPLICE (MOVABLE), STA ZFS=52.267 AT VERTICAL STABILIZER. VERTICAL LEADING EDGE (MOVABLE) ON STA ZFS = 52.267 AT VERTICAL STABILIZER WAS REPAIRED PER SERVICE GENERAL DRAWING SG95550001 REV. B IN ACORDANCE TO Jun 7, 2025 · N921AT · Boeing 717200SDR DALA2025053004146Access Panel · crackedSHIP 3123 CRACK ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 626324-14. (0993816).May 29, 2025 · N323NB · Airbus A319114SDR SWAA2025061073450Panel · crackedVERTICAL STAB PANEL 323AL LOWER CLIP CRACKED.<[01] RECEIVED SERVICEABLE PANEL 323AL P/N:654A0004-711; BN 396992. PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00Z3WDY;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.May 21, 2025 · N7823A · Boeing 7377CTSDR DALA2025052103919Skin · damaged(LOG 0973600) VERTICAL STABILIZER / RH IN SPAR SKIN / LIGHTNING STRIKES. COMPLIED WITH ER/A 626370-14 REV. ORIG.May 19, 2025 · N945DZ · Boeing 7379GPERSDR JGVR202505140003Skin · corrodedBLENDED CORRODED AREA LOCATED SKIN OF THE VERTICAL STABILIZER AT THE TRAILING EDGE UPPER END, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED BLENDED AREA BY FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH ANMay 14, 2025 · N376QS · Cessna 680CESDR CALA2025052704954Skin · delaminatedVERTICAL STAB R/H SIDE SKIN PANEL IS DELAMINATED INTERNALLY (VIEWED THRU THE LIGHTNING HOLE IN THE AUX SPAR) BETWEEN THE AUX SPAR AND THE FWD SPAR BETWEEN APPROX RIB 1 AND RIB 3. REMOVED AND REPLACED VERTICAL STAB R/H SKIN PANEL IAW B757 SRM 51-40-02 AND BOMay 11, 2025 · N12114 · Boeing 757224SDR COEA2025080609805Skin · corrodedWO 262649 NR 300005 HEAVY CHECK COE/MAJOR REPAIR: VERTICAL STABILIZER R/H EXTERNAL SKIN PANEL HAS LEVEL 2 CORROSION BETWEEN FWD AND MID SPAR. CORRECTIVE ACTION: REPAIR PER SRAS S553R0016...07772 ISSUE C, DATED 7/15/2025.May 8, 2025 · N805FX · Aerosp ATR72212SDR IXXA202500417002Skin · debondedVERTICAL STABILIZER R/H EXTERNAL SKIN BETWEEN AUX SPAR AND FRONT SPAR IS DELAMINATED JUST ABOVE RIB 5Apr 17, 2025 · N347AZ · Boeing 767319SDR UIEA2025040400442Skin · dentedVERTICAL STABILIZER LH PANEL ASSEMBLY OUTER SKIN WITH DENT.(<P>DENT ON VERTICAL STABILIZER, LH PANEL ASSEMBLY, OUTER SKIN, WAS EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W. SRM 55-30-01-1A-1 AD.1 FIG. 101, DETAIL III. REV. 52 15APR25. DENT DOT 9025Apr 5, 2025 · N1381A · Boeing 767316SDR UIEA2025040400443Skin · debondedLH VERTICAL STABILIZER SKIN PANEL BTW FSS 270.784 TO FSS 118.75 PANEL WITH DISBONDED.(<P>LH VERTICAL STABILIZER SKIN PANEL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52 15-APR-25. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316SDR SWAA2025033119442Skin · delaminatedVERTICAL STABILIZER LEADING EDGE METAL PLATE DELAMINATED<[01] UPON FURTHER INSPECTION FOUND EROSION TAPE NOT SECURED ON VERTICAL STAB LEADING EDGE. REMOVED AND REPLACED EROSION TAPE. ALL WORK PERFORMED IAW AMM 55-35-01Mar 29, 2025 · N8932Q · Boeing 7378
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