# Service difficulty reports: JASC 5534

A list on [JASC 5534](https://openairdocs.org/jasc/5534.md).

Reports filed under 5534 · Vertical Stabilizer Miscellaneous Structure, newest first.

Page 1 of 17 · 816 reports

- [SDR CALA2026092819933](https://openairdocs.org/sdr/CALA2026092819933.md): Fitting · corroded · Sep 21, 2026 · N73299 · Boeing 737824
  > CORROSION FOUND ON RH VERTICAL STAB FWD MOUNT, AFT FITTING. ACCOMPLISHED A REPAIR IAW ECRA 5380-01456, PART 1.
- [SDR HNAA2026093000921](https://openairdocs.org/sdr/HNAA2026093000921.md): Profile · cracked · Sep 8, 2026 · N653AE · Emb EMB145LR
  > AFT OF REAR SPAR 3 OF VERTICAL STAB, LT PROFILE CRACKED ABOVE RUDDER UPPER AND MID HINGE FITTING. REPAIRED IAW ETD 2026-145-015973 AND EO 1-55-26-0465
- [SDR AALA202609173925](https://openairdocs.org/sdr/AALA202609173925.md): Angle · cracked · Sep 8, 2026 · N355PU · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: J-ANGLE CRACKED ON VERTICAL STAB ATTACH FITTING JUST ABOVE AND AFT OF R/H ATTACH LUG. REMOVED AND INSTALLED J-ANGLE IAW AARD 55-30-09-3 PARAGRAPH 5 STEP A.
- [SDR UIEA2026082700813](https://openairdocs.org/sdr/UIEA2026082700813.md): Support · cracked · Sep 1, 2026 · N489MC · Boeing 747412F
  > VERTICAL STAB, LEFT L/E FIXED PANEL STA 78 AFT UPPER SUPPORT FOUND CRACKED. VERTICAL STAB LEFT L/E FIXED PANEL UPPER SUPPORT WAS REPLACED IAW SRM 51-10-02 & 51-40-02, REV 107, AND RI-55-30-18461, REV A. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2026092108164](https://openairdocs.org/sdr/SWAA2026092108164.md): Panel · damaged · Aug 24, 2026 · N8550Q · Boeing 7378H4
  > LEFT BALANCE BAY PANEL (333BB) HAD AN ELONGATED SCREW HOLE. REPAIRED THE FASTENER HOLE IAW SRM 51-70-05, REPAIR 8.
- [SDR FDEA202608201195](https://openairdocs.org/sdr/FDEA202608201195.md): Beam · cracked · Aug 20, 2026 · N993FD · Boeing 7572Q8
  > VERTICAL STABILIZER REAR SPAR FIN STA:95.00 SUPPORT PANEL 324AL BEAM CRACKED REMOVED AND REPLACED BEAM AT VERTICAL STABILIZER REAR SPAR SUPPORT PANEL 324AL IAW B757 SRM 51-40-02-0G AND DRAWING 173N1300
- [SDR CALA2026082018740](https://openairdocs.org/sdr/CALA2026082018740.md): Beam · cracked · Aug 14, 2026 · N12125 · Boeing 757224
  > VERTICAL STAB. FIXED T/E LT LOWER SEAL TO FUSELATE OUT OF THE RIGHT PLACE. REMOVED, FABRICATED AND INSTALLED BEAM COMMON TO LT VERTICAL LOWER FUSELAGE, FABRICATED & ATTACHED IAW DWG 173N1300, & SRM 51-40-02-0G.
- [SDR CALA2026081718650](https://openairdocs.org/sdr/CALA2026081718650.md): Torque Box · dented · Aug 13, 2026 · N12125 · Boeing 757224
  > RT VERTICAL STAB EXTERNAL SURFACE OF LWR TORQUE BOX SKIN FROM FSS 92.250-FSS 270.784 HAS NUMEROUS DENTS (APPROX 100+). VERTICAL STAB RH VERTICAL TORQUE BOX PANEL. REMOVED AND REPLACED 175N2001U4 TORQUE BOX PANEL COMMON TO NETIO RT STAB IAW SRM 51-40-02-OG.
- [SDR SWAA2026081478820](https://openairdocs.org/sdr/SWAA2026081478820.md): Seal · deteriorated · Aug 7, 2026 · N7732A · Boeing 7377BD
  > DETERIORATED SEAL ON ACCESS PANEL 324ADR AT VERTICAL STABILIZER. REPLACED SEAL PANEL 324ADR AT VERTICAL STABILIZER IAW SRM 51-10-02, ITEM 9, & AMM 55-05-02-211-812, PARAGRAPH 63.C.(3).
- [SDR IPXA2026083180847](https://openairdocs.org/sdr/IPXA2026083180847.md): Torque Box · delaminated · Jul 27, 2026 · N461UP · Boeing 75724APF
  > MAJOR REPAIR, LT LOWER VERTICAL STABILIZER LOWER FWD TORQUE BOX PANEL HAS AREA OF DELAMINATION AROUND CIRCULAR PATCH/ PLUG NEAR UPPER FWD CORNER. ACCOMPLISHED REPAIR IAW SRM REV 124, 51-70-10-2R-4.
- [SDR SWAA2026081744181](https://openairdocs.org/sdr/SWAA2026081744181.md): Angle · elongated · Jul 11, 2026 · N8651A · Boeing 7378H4
  > ELONGATED HOLE ON ANGLE IN UPPER AREA AT ACCESS PANEL 324AAL T/E AT VERTICAL STAB. REPLACED ANGLE LOCATED UPPER AREA AT LEVEL ACCESS PANEL 324AAL TRAILING EDGE AT VERTICAL STABILIZER IAW SRM 51-40-02 AND DWG 175A3100, SHT 5, REV H.
- [SDR IPXA2026071426239](https://openairdocs.org/sdr/IPXA2026071426239.md): Attach Angle · worn · Jun 18, 2026 · N418UP · Boeing 75724APF
  > VERTICAL STAB TRAILING EDGE PANEL 324AL LOWER AFT CORNER SUPPORT STRUCTURE SECTION MISSING AND FUSELAGE ATTACH ANGLE WORN THIN IN SEVERAL AREAS. DAMAGED WELL MARKED RL004. REMOVED 1EA DAMAGED ANGLE FIN FAIRING AT VERTICAL STABILIZER TRAILING EDGE PANEL 324AL L
- [SDR HNAA2026070300572](https://openairdocs.org/sdr/HNAA2026070300572.md): Lug · worn · Jun 12, 2026 · N652RS · Emb EMB145LR
  > RUDDER 1, UPPER HINGE FITTING, BOTH LUGS WORN. R & R LUGS IAW SRM 51-40-02 AND AMM 20-10-01.
- [SDR REXA2026060800949](https://openairdocs.org/sdr/REXA2026060800949.md): Angle · cracked · May 25, 2026 · N538CA · Cndair CL6002D24
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED P
- [SDR REXA2026060800948](https://openairdocs.org/sdr/REXA2026060800948.md): Angle · cracked · May 9, 2026 · N538CA · Cndair CL6002D24
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WERE REPAIRED
- [SDR CALA2026051116128](https://openairdocs.org/sdr/CALA2026051116128.md): Support Angle · gouged · May 8, 2026 · N19141 · Boeing 757224
  > VERTICAL STAB LT SIDE ACCESS PANEL 324AL LOWER SUPPORT ANGLE GOUGED. REMOVED AND REPLACED DAMAGED ANGLE BY NEW ANGLE IAW SRM 51-40-02 RESTORED SURFACE PROTEC ION AT AREA IAW AMM TASK 51-21-15-370-801 STA 1804.81
- [SDR IPXA2026060872812](https://openairdocs.org/sdr/IPXA2026060872812.md): Panel · deformed · May 7, 2026 · N423UP · Boeing 75724APF
  > THE R/H LWR FWD TORQUE BOX PANEL HAS EXCESSIVE HAIL DAMAGE AND MULTIPLE DISBONDS / DELAMINATIONS ACROSS THE ENTIRE SURFACE OF THE PANEL FROM TOP TO BOTTOM. INSTALLED 1 EA TORQUE BOX PANEL IAW SRM 51-40-02.
- [SDR REXA2026052100604](https://openairdocs.org/sdr/REXA2026052100604.md): Angle · cracked · Apr 30, 2026 · N919XJ · Cndair CL6002D24
  > L/H DRAG ANGLE ON VERT. STAB HAS A CRACK (MARKED W/ TAPE) REMOVED UNSERVICEABLE LH AFT DRAG ANGLE IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE LH AFT DRAG ANGLE PN: AV670-21186-003 IAW CRJ900 SRM 51-40-11-0
- [SDR SWIA2026042576726](https://openairdocs.org/sdr/SWIA2026042576726.md): Drag Angle · cracked · Apr 25, 2026 · N614QX · Cndair CL6002C10
  > RIGHT AFT VERTICAL DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE AT RH AFT VERTICAL IAW REO 670-55-31-018, REV-A, SRM 51-26-01.
- [SDR SWIA2026042576718](https://openairdocs.org/sdr/SWIA2026042576718.md): Drag Angle · cracked · Apr 25, 2026 · N614QX · Cndair CL6002C10
  > LEFT AFT VERTICAL DRAG ANGLE IS CRACKED. PERFORMED REPAIR DRAG ANGLE ON LT AFT VERTICAL IAW REO 670-55-31-018, REV-A, SRM 51-26-01, NDT PERFORMED.
- [SDR REXA2026052900874](https://openairdocs.org/sdr/REXA2026052900874.md): Angle · cracked · Apr 24, 2026 · N933XJ · Cndair CL6002D24
  > CRACK ON LT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD - AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SP
- [SDR 2026FA0000292](https://openairdocs.org/sdr/2026FA0000292.md): Vertical Beam · corroded · Apr 24, 2026 · N592QS · Cessna 560XL
  > DURING EMPENNAGE COVE INSP, FOUND VERTICAL AFT SPAR HAS CORROSION ON RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AND REMOVED ALL VISIBLE SIGNS OF CORROSION ON AFT SPAR RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AREA WAS BEYOND ALLOWABLE LIMITS AND WAS SUBMITTED TO
- [SDR SWAA2026043083752](https://openairdocs.org/sdr/SWAA2026043083752.md): Angle · cracked · Mar 26, 2026 · N244WN · Boeing 7377H4
  > CRACKED ANGLE, INTERNAL STRUCTURE FRONT SPAR SUPPORT FITTING RT AREA APPROX AT BS 1016 IN THE VERTICAL STAB. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 176A3101, SHEET 4, REV-.
- [SDR R3WA20260429001](https://openairdocs.org/sdr/R3WA20260429001.md): Pulley Bracket · chafed · Mar 19, 2026 · N716XJ · Cessna 750
  > DURING SCHEDULED MAINTENANCE, A DETAILED VISUAL INSPECTION OF THE RUDDER CONTROL SYSTEM DISCOVERED A RUDDER CONTROL CABLE RUBBING AGAINST A PULLEY BRACKET WHICH WAS ALSO PART OF THE RUDDER CONTROL SYSTEM. CABLE WEAR WAS MINIMAL AND WITHIN SERVICEABLE LIMITS SP
- [SDR COEA2026072224803](https://openairdocs.org/sdr/COEA2026072224803.md): Fitting · corroded · Mar 8, 2026 · N803FX · Aerosp ATR72212
  > HORIZONTAL TO VERICAL STAB AFT L/H FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FITTING PER ATR72 SRM 51-25-04 REV. 122.
- [SDR AALA202603258400](https://openairdocs.org/sdr/AALA202603258400.md): Channel · cracked · Mar 8, 2026 · N908AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL RIGHT HAND RELIEF CUTOUT IS CRACKED, LOCATED ABOVE THE FRONT SPAR TERMINAL FITTING RIGHT HAND LUG. REMOVED AND REPLACED VERTICAL STABILIZER J-CHANNEL RIGHT HAND RELIEF CUTOUT. PER SRM 51-40-01-0G.
- [SDR N6WA2026030301](https://openairdocs.org/sdr/N6WA2026030301.md): Drag Angle · cracked · Mar 2, 2026 · N523GJ · Cndair CL6002C11
  > VERTICAL STAB RH DRAG ANGLE CRACKED. REMOVED AND REPLACED VERT. STAB RH AFT DRAG ANGLE IAW CRJ SRM 51-42-06
- [SDR 2026FA0000140](https://openairdocs.org/sdr/2026FA0000140.md): Vertical Support · corroded · Feb 25, 2026 · N601QS · Cessna 680A
  > SEVERAL AREAS OF CORROSION ON UPPER VERTICAL STAB R/H SIDE BELOW TIP CAP. PERFORMED MAJOR PERMANENT REPAIR OF AREA IAW AQRD RFTS-116135 REV 0 & AQRD ERO-988077 REV IR.
- [SDR AALA202603069362](https://openairdocs.org/sdr/AALA202603069362.md): Fitting · cracked · Feb 24, 2026 · N990AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL ABOVE THE FORWARD SPAR TERMINAL FITTING RIGHT HAND LUG IS CRACKED ON THE AFT SIDE OF THE RELIEF CUTOUT. REPLACED J-CHANNEL WITH SERVICEABLE J-CHANNEL ABOVE THE FORWARD SPAR TERMINAL FITTING RIGHT HAND
- [SDR AALA202602261905](https://openairdocs.org/sdr/AALA202602261905.md): Fitting · corroded · Feb 24, 2026 · N910AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO VERTICAL STABILIZER AFT DRAG BRACE FITTING AT WL 301, RBL 10. REPLACED FITTING PER SRM 53-80-90-0I.
- [SDR AALA202602266913](https://openairdocs.org/sdr/AALA202602266913.md): Fitting · corroded · Feb 22, 2026 · N910AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO VERTICAL STABILIZER FORWARD DRAG BRACE FITTING AT WL 301, RBL 10. REPLACED FITTING PER SRM 53-80-90-0I-1.
- [SDR SWAA2026031370921](https://openairdocs.org/sdr/SWAA2026031370921.md): Web · cracked · Feb 14, 2026 · N240WN · Boeing 7377H4
  > CRACKED HORIZONTAL WEB, BS 1016 UPPER AREA OF THE VERTICAL STAB. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 176A3001, SHEET 23, REV D.
- [SDR CALA2026021813855](https://openairdocs.org/sdr/CALA2026021813855.md): Angle · corroded · Feb 12, 2026 · N33294 · Boeing 737824
  > CORROSION AT VERTICAL STABILIZER T/E AREA INTERNAL CAVITY OF BALANCE WEIGHT. ACCOMPLISHED REPLACEMENT OF ANGLE (STIFFENER) IAW SRM 51-40-02-0G-0.
- [SDR VNAA20260328004](https://openairdocs.org/sdr/VNAA20260328004.md): Drag Angle · cracked · Feb 10, 2026 · N542EA · Bombdr CL6002D15
  > DURING INSPECTION OF THE TASK CARD 300-07-JIC IT WAS DETECTED CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS FOUND. AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM T
- [SDR REXA2026032700271](https://openairdocs.org/sdr/REXA2026032700271.md): Angle · cracked · Feb 9, 2026 · N918XJ · Cndair CL6002D24
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM
- [SDR REXA2026032700270](https://openairdocs.org/sdr/REXA2026032700270.md): Angle · cracked · Feb 9, 2026 · N918XJ · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKS ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5%
- [SDR AALA202602274820](https://openairdocs.org/sdr/AALA202602274820.md): Channel · cracked · Feb 9, 2026 · N983AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL HAS A CRACK AT THE RELIEF CUTOUT ABOVE THE LEFT HAND FORWARD SPAR TERMINAL FITTING. INSTALLED J-CHANNEL ASSEMBY. PER AARD 51-00-05-1 REPAIR #1.
- [SDR REXA2026080301389](https://openairdocs.org/sdr/REXA2026080301389.md): Angle · cracked · Feb 5, 2026 · N398CA · Cndair CL6002C10
  > CRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01
- [SDR HNAA2026012200068](https://openairdocs.org/sdr/HNAA2026012200068.md): Housing · worn · Dec 10, 2025 · N933JN · Emb EMB145LR
  > LEFT & RIGHT VERTICAL STABILIZER SPHERICAL BEARING HOUSINGS WORN. ENLARGED LT & RT VERTICAL STAB SPHERICAL BEARING HOUSINGS TO FIRST OVERSIZED (DIMENSION 58.00MM, PN 145-408881-001 (RE-WORK #1) IAW SRM 55-30-02 ND EO1-55-26-0030.
- [SDR VNAA20260203009](https://openairdocs.org/sdr/VNAA20260203009.md): Drag Angle · cracked · Dec 5, 2025 · N525AE · Bombdr CL6002D15
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRAC
- [SDR SWAA2026011242946](https://openairdocs.org/sdr/SWAA2026011242946.md): Bracket · corroded · Dec 4, 2025 · N241WN · Boeing 7377H4
  > CORROSION GROUND PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STABILIZER. REPLACED BRACKET PLATE LOCATED BTW HINGE 7A TO HINGE 8 AT VERTICAL STAB IAW SRM 51-10-02 PARAGRAPH 9, SRM 51-40-02, AND DWG 175A1601, SHEET 18, REV A.
- [SDR YENA2025120201138](https://openairdocs.org/sdr/YENA2025120201138.md): Fitting · corroded · Nov 27, 2025 · N2027J · Airbus A321271N
  > DURING HEAVY MAINTENANCE: AFTER REMOVE BEARING, CORROSION FOUND IN FITTING N5 AT VERTICAL STABIL IZER. REMOVED AND REPLACED FITTING # 5 AT VERTICAL STABILIZER IAW A321 NEO SRM 51-72-11, SRM A321 NEO 55-36-42-300-008 AND D553721041 WOTK BY 8632812 RII AE370
- [SDR YENA2025120201137](https://openairdocs.org/sdr/YENA2025120201137.md): Hinge · corroded · Nov 27, 2025 · N2027J · Airbus A321271N
  > DURING HEAVY MAINTENANCE: AFTER REMOVE BEARING CORROSION FOUND IN FITTING Ñ 5 AT VERTICAL STABILIZER. REMOVED AND REPLACED HINGE FITTING NR 5 AT VERTICAL STABILIZER IAW SRM 51-72-11, SRM 55-36-42-300-008 AND DRAWING D55371041.
- [SDR 2025F00273](https://openairdocs.org/sdr/2025F00273.md): Support · corroded · Nov 26, 2025 · N86VS · Cessna 414
  > DURING A PREFLIGHT WALKAROUND, SURFACE CORROSION WAS OBSERVED ON THE VERTICAL STABILIZER AFT SECTION. AFTER CLOSER INSPECTION SEVERE DELAMINATION WAS SEEN ON THE AFT VERTICAL SUPPORT ANGLES AND AFT STAB BULKHEAD SECTION. THE RUDDER TRIM TAB BRACKET ALSO HAD SI
- [SDR KISA202602050001](https://openairdocs.org/sdr/KISA202602050001.md): Angle · corroded · Nov 25, 2025 · N86VS · Cessna 414
  > DURING A PREFLIGHT WALK AROUND CORROSION WAS OBSERVED ON THE AFT SPAR ANGLE CHANNEL OF THE VERTICAL STABILIZER. UPON FURTHER INVESTIGATION SIGNIFICANT INTERGRANULAR CORROSION WAS FOUND RESULTING IN EXFOLIATION OF THE SURFACE OT THE SPAR ANGLE. THIS RESULTED IN
- [SDR FDEA202511052124](https://openairdocs.org/sdr/FDEA202511052124.md): Frame · cracked · Nov 5, 2025 · N574FE · Doug MD11F
  > VERTICAL STABILIZER REAR CENTER SPAR STIFFENER CRACKED AT STATION 2122 5 O' CLOCK AREA. CRACKED STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT STATION 2122 5 O' CLOCK AREA REPAIRED AS PER EA# 1-5530-T0385238 P1 TITLE: STABILIZERS - VERTICAL
- [SDR YENA2025102801067](https://openairdocs.org/sdr/YENA2025102801067.md): Hinge Arm · worn · Oct 27, 2025 · N623JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: WEAR ON HINGE ARM FORK END FITTING # 6 ON VERTICAL STABILIZER (1EA); REF AEROMAN WO# 2025-262/1 NR# 2025-608758 REMOVED AND REPLACED HINGE ARM FORK END FITTING #6 ON VERTICAL STABILIZER I.A.W. A320 SRM 51-42-11 AND I.A.W A320 SRM 55-3
- [SDR AALA202511175408](https://openairdocs.org/sdr/AALA202511175408.md): Angle · cracked · Oct 19, 2025 · N907AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL STABILIZER LEFT HAND LOWER CLOSURE ANGLE ON TOP OF FUSELAGE AFT OF THE DORSAL FIN FROM STA 1005 TO STA 1016. REPAIRED ANGLE PER SRM 53-80-71-2R-6
- [SDR CALA2025101610181](https://openairdocs.org/sdr/CALA2025101610181.md): Angle · worn · Oct 15, 2025 · N18243 · Boeing 737824
  > LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BR SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BR SUPPORT AFT ANGLE REF SRM 51-40-02-0G-0 AND DWG 148A8300.
- [SDR CALA2025101610180](https://openairdocs.org/sdr/CALA2025101610180.md): Angle · worn · Oct 15, 2025 · N18243 · Boeing 737824
  > LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BL SUPPORT ANGLE SEVERAL AREA WORN. REMOVED AND REPLACED LOWER VERTICAL STABILIZER TO UPPER FUSELAGE ACCESS PANEL 323BL SUPPORT AFT ANGLE REF B-737 SRM 51-40-02-0G-0 AND DWG 148A8300.

Next page: https://openairdocs.org/jasc/5534/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 = '5534'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5534/reports

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