FAIRING DAMAGE AREA REPAIRED AS PER RI-55-31-18434 REV A. NO FURTHER DEFECTS NOTED
) - [SDR CALA2026071217693](https://openairdocs.org/sdr/CALA2026071217693.md): Skin · dented · Jul 10, 2026 · N67134 · Boeing 757224 > (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 55-30-01-2 - [SDR CALA2026071217691](https://openairdocs.org/sdr/CALA2026071217691.md): Skin · dented · Jul 10, 2026 · N67134 · Boeing 757224 > LEFT 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 CLAS - [SDR DALA2026070603942](https://openairdocs.org/sdr/DALA2026070603942.md): Skin · damaged · Jul 3, 2026 · N951AT · Boeing 717200 > SKIN DAMAGE LT VERT CAP FROM AIR GATE FAIRING. REPAIRED PER ER/A 635425-14. (1679920)(AIRCRAFT GROUNDED) - [SDR IPXA2026072111084](https://openairdocs.org/sdr/IPXA2026072111084.md): Panel · debonded · Jun 29, 2026 · N572UP · Boeing 74744AF > DEBONDED 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 IPXA2026072111043](https://openairdocs.org/sdr/IPXA2026072111043.md): Panel · debonded · Jun 29, 2026 · N572UP · Boeing 74744AF > DISBONDED 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. 2 - [SDR CALA2026083119091](https://openairdocs.org/sdr/CALA2026083119091.md): Skin · damaged · Jun 21, 2026 · N14231 · Boeing 737824 > TWO 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 NDT - [SDR REXA2026082601716](https://openairdocs.org/sdr/REXA2026082601716.md): Access Panel · cracked · Jun 19, 2026 · N926XJ · Cndair CL6002D24 > CRACK ON FASTENER HOLE OF ACCESS PANEL NBR:326DL. ACCESS PANEL NBR:326DL WAS REPAIRED PER EA NO. CRJ955-22596 REV IR - [SDR LR7A2026061903864](https://openairdocs.org/sdr/LR7A2026061903864.md): Skin · corroded · Jun 19, 2026 · N409LC · Lkheed 382G > DURING 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 DALA2026061903676](https://openairdocs.org/sdr/DALA2026061903676.md): Skin · out of limits · Jun 17, 2026 · N936AT · Boeing 717200 > HOLES 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 PER - [SDR HNAA2026062900558](https://openairdocs.org/sdr/HNAA2026062900558.md): Skin · cracked · Jun 8, 2026 · N652RS · Emb EMB145LR > VERTICAL STAB, AFT OF SPAR 3, LT SKIN TRAILING EDGE LWR PROFILE CRACKED. R & R PROFILE IAW SRM 51-40-02 - [SDR SWAA2026070610072](https://openairdocs.org/sdr/SWAA2026070610072.md): Skin · bulged · Jun 7, 2026 · N8319F · Boeing 7378H4 > RIGHT VERTICAL FIN IN SPAR SKIN BULGED; RIVETS PULLED. ITEM TRANSFERRED TO COMPONENT WORK PACKAGE TTG8Q01CNJE8. - [SDR 21GA202605260000](https://openairdocs.org/sdr/21GA202605260000.md): Skin · delaminated · May 26, 2026 · N999YV · Boeing 767241 > DELAMINATION LOCATED ON LEFT SIDE OF VERTICAL STABILIZER PANEL BETWEEN SPAR AND FRONT SPAR FSS 220.521 - 270-784 (MAJOR REPAIR) - [SDR IPXA2026050962784](https://openairdocs.org/sdr/IPXA2026050962784.md): Access Panel · damaged · Apr 30, 2026 · N419UP · Boeing 75724APF > MAJOR REPAIR, LT VERTICAL STABILIZER ACCESS PANEL 322DL, AT FSS 295.915 TO 371.308, HAD HAIL DAMAGE. - [SDR DALA2026041402345](https://openairdocs.org/sdr/DALA2026041402345.md): Skin · cracked · Apr 10, 2026 · N946AT · Boeing 717200 > REF 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 DALA2026031901907](https://openairdocs.org/sdr/DALA2026031901907.md): Skin · bulged · Mar 19, 2026 · N831MH · Boeing 767432ER > VERTICAL 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 2026F00035](https://openairdocs.org/sdr/2026F00035.md): Skin · corroded · Mar 19, 2026 · N339QS · Gulstm 680 > LEFT 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 BLE - [SDR SWAA2026033175363](https://openairdocs.org/sdr/SWAA2026033175363.md): Access Panel · cracked · Feb 28, 2026 · N8633A · Boeing 7378H4 > CRACKED 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 IXX2026F00001](https://openairdocs.org/sdr/IXX2026F00001.md): Panel · delaminated · Feb 22, 2026 · N307AZ · Boeing 767338 > LT SIDE VERTICAL STAB PNL DELAMINATED P/N 175T2001-3 - [SDR DALA2026021100983](https://openairdocs.org/sdr/DALA2026021100983.md): Skin · delaminated · Feb 6, 2026 · N825MH · Boeing 767432ER > DURING 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 DALA2026021100982](https://openairdocs.org/sdr/DALA2026021100982.md): Skin · delaminated · Feb 6, 2026 · N825MH · Boeing 767432ER > DURING 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 DALA2026020500843](https://openairdocs.org/sdr/DALA2026020500843.md): Access Panel · corroded · Feb 3, 2026 · N880DN · Boeing 737932ER > WEAR 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 S - [SDR GTIA2026020539268](https://openairdocs.org/sdr/GTIA2026020539268.md): Skin Panel · corroded · Feb 2, 2026 · N606NK · Airbus A320232 > CORROSION 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 51-11-14 - [SDR DALA2026012800670](https://openairdocs.org/sdr/DALA2026012800670.md): Panel · delaminated · Jan 21, 2026 · N189DN · Boeing 767332 > VERTICAL STABILIZER RT FIXED PANEL DELAMINATED FROM FUSELAGE 146 INCH AND FWD EDGE 36 INCH. DAMAGED AREA REPAIRED IAW SRM 51-70-10. (1412232) - [SDR DALA2026012800669](https://openairdocs.org/sdr/DALA2026012800669.md): Panel · delaminated · Jan 21, 2026 · N189DN · Boeing 767332 > VERTICAL 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 IXXA20260120001](https://openairdocs.org/sdr/IXXA20260120001.md): Panel · delaminated · Jan 20, 2026 · N607AZ · Boeing 767332 > RIGHT HAND VERTICAL STABILIZER UPPER FIXED LEADING EDGE PANEL DELAMINATED - [SDR IXXA2026011801](https://openairdocs.org/sdr/IXXA2026011801.md): Panel · delaminated · Jan 18, 2026 · N607AZ · Boeing 767332 > LEFT HAND VERTAL STAB UPPER SURFACE LEADING EDGE BONDED PANEL DELAMINATED - [SDR DALA2026012100450](https://openairdocs.org/sdr/DALA2026012100450.md): Skin · delaminated · Jan 16, 2026 · N177DZ · Boeing 767332 > VERTICAL 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 DALA2026012100449](https://openairdocs.org/sdr/DALA2026012100449.md): Skin · delaminated · Jan 14, 2026 · N177DZ · Boeing 767332 > VERTICAL 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 DALA2026012100448](https://openairdocs.org/sdr/DALA2026012100448.md): Skin · delaminated · Jan 14, 2026 · N177DZ · Boeing 767332 > VERTICAL 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 SWAA2026011360118](https://openairdocs.org/sdr/SWAA2026011360118.md): Skin · delaminated · Jan 10, 2026 · N945WN · Boeing 7377H4 > DORSAL 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 AALA202512195234](https://openairdocs.org/sdr/AALA202512195234.md): Doubler · cracked · Dec 8, 2025 · N947NN · Boeing 737823 > AIRCRAFT 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 DALA2025121909239](https://openairdocs.org/sdr/DALA2025121909239.md): Skin · damaged · Dec 8, 2025 · N839MH · Boeing 767432ER > VERTICAL 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 DALA2025120508915](https://openairdocs.org/sdr/DALA2025120508915.md): Panel · delaminated · Dec 3, 2025 · N835MH · Boeing 767432ER > VERTICAL 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 DALA2025120508914](https://openairdocs.org/sdr/DALA2025120508914.md): Panel · delaminated · Dec 3, 2025 · N835MH · Boeing 767432ER > VERTICAL 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 (1 - [SDR EE4Y2025111323450](https://openairdocs.org/sdr/EE4Y2025111323450.md): Skin · cracked · Nov 13, 2025 · N258JB · Emb ERJ190100IGW > DURING 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 I Next page: https://openairdocs.org/jasc/5532/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/jasc/5532/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.