# Service difficulty reports: JASC 5530

A list on [JASC 5530](https://openairdocs.org/jasc/5530.md).

Reports filed under 5530 · Vertical Stabilizer, newest first.

Page 1 of 51 · 2,534 reports

- [SDR 2026FA0000836](https://openairdocs.org/sdr/2026FA0000836.md): Fairing · separated · Oct 14, 2026 · N703BA · Textrn 408
  > UPPER VERTICAL TIP CAP FAIRING SEPARATED IN FLIGHT, SUBSEQUENTLY DAMAGING UPPER PORTION OF RUDDER, UPPER VERTICAL SKIN, ELEVATOR PUSH RODS AND ELEVATOR HORNS.
- [SDR CALA2026092119598](https://openairdocs.org/sdr/CALA2026092119598.md): Tape · peeling · Sep 17, 2026 · N33714 · Boeing 737724
  > SPEED TAPE HAS PEELED BACK ON VERTICAL STAB. FOUND VERTICLE STAB ANTENNA EROSION COATING PEELING. ACCOMPLISHED PART 1 OF ECRA 5530-01432. INSPECT INTERM REPAIR AT INTERVALS NOT TO EXCEED 2 DAYS AND PERFORM A PERMANENT REPAIR WITHIN 10 DAYS DUE TO VERTICAL S
- [SDR IPXA2026090711902](https://openairdocs.org/sdr/IPXA2026090711902.md): Panel · debonded · Aug 25, 2026 · N441UP · Boeing 75724APF
  > THE LT FWD TORQUE BOX PANEL HAS 2EA DELAMINATED, DISBONDED AREAS NEAR FSS 245.653 AND FSS 171.39. REMOVED ALL FASTENERS FROM LT FWD TORQUE BOX PANEL, EXCEPT MOST BOTTOM ROW, & BOTTOM AFT ROW, IAW SRM 51-40-02. INSTALLED NEW TORQUE BOX PANEL ON LT FWD IAW SR
- [SDR IPXA2026091095169](https://openairdocs.org/sdr/IPXA2026091095169.md): Panel · delaminated · Aug 24, 2026 · N441UP · Boeing 75724APF
  > MAJOR REPAIR, THE RT LWR FWD TORQUE BOX PANEL HAS 1EA DELAMINATED & DISBONDED AREA NEAR FSS 137.467. ACCOMPLISH REPAIR IAW SRM REV 125, 51-70-10-2R-2, 250 DEG F CURE USING SRM 51-70-10-2R-0. DAMAGE WAS REMOVED IAW SRM 51-70-10-2R. BONDED REPAIR PARTS IAW
- [SDR VNAA202609010022](https://openairdocs.org/sdr/VNAA202609010022.md): Hinge Fitting · worn · Jul 8, 2026 · N642NN · Cndair CL6002D24
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NR 2 AND 3 AT VERTICAL STAB REAR SPAR MIDDLE SECTION. HINGE FITTING NR 2 WAS REPLACED PER SRM 51-42-21-001-001-A01, RIL 2103 REV B AND BEARING ON HINGE FITTING NR 3 WAS REPLACED IAW SRM 51-42-2
- [SDR YENA2026070900530](https://openairdocs.org/sdr/YENA2026070900530.md): Hinge Arm · damaged · Jul 5, 2026 · N806JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, STABILIZERS, VERTICAL STABILIZER, HINGE ARM BR3 & FORK END FITTING ASSY ELONGATED HOLES. TIME LIMITED REPAIR (CONSIDERED MAJOR REPAIR)
- [SDR AALA202608072053](https://openairdocs.org/sdr/AALA202608072053.md): Hinge Arm · corroded · Jun 29, 2026 · N9016 · Airbus A319115
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER HINGE ARM 7 AT RIB 11. REPLACED HINGE ARM PER EA 377460 AND SRM 55-36-42-300-003
- [SDR SCNA20260717314](https://openairdocs.org/sdr/SCNA20260717314.md): Access Panel · worn · Jun 18, 2026 · N801SY · Boeing 7378Q8
  > WEAR ON LOWER SETTLEMENT AREA AT VERTICAL STABILIZER ACCESS PANEL NUMBER 323AL STA 1006 TO 1016 ORIGINAL THICKNESS: IS 0.063 IN AND MINIMUM REMAINING THICKNESS: IS 0.030 IN THEREFORE IT'S OUT LIMITS PER B737-800 SRM 55-30-01-1A-2 ALLOWABLE DAMAGE 2 PAR 4.B DE
- [SDR SCNA20260717313](https://openairdocs.org/sdr/SCNA20260717313.md): Access Panel · worn · Jun 18, 2026 · N801SY · Boeing 7378Q8
  > IN REFERENCE NRC 00216: WEAR ON LOWER SETTLEMENT AREA AT VERTICAL STABILIZER ACCESS PANEL NUMBER 323AL STA 1006 TO 1016 ORIGINAL THICKNESS: IS 0.063 IN AND MINIMUM REMAINING THICKNESS: IS 0.030 IN THEREFORE IT'S OUT LIMITS PER B737-800 SRM 55-30-01-1A-2 ALLOWA
- [SDR DALA2026053103300](https://openairdocs.org/sdr/DALA2026053103300.md): Hinge Arm · corroded · May 29, 2026 · N351NW · Airbus A320212
  > LEVEL 2 CORROSION, CORROSION SSI:553006 RUDDER HINGE ARM NR 7 STUD HOLES L/R SIDES WITH CORROSION. REPAIRED VERTICAL STABILIZER RUDDER HINGE ARM BR1 OVERSIZED HOLE AND HINGE BR7 REPLACEMENT IAW DELTA ER/A 634168-14 REVISION ORIGINAL DATED 27-MAY-26. NOTE: FOR
- [SDR VNAA202607010011](https://openairdocs.org/sdr/VNAA202607010011.md): Hinge · excess play · May 16, 2026 · N530EA · Cndair CL6002C10
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #
- [SDR IPXA2026060473078](https://openairdocs.org/sdr/IPXA2026060473078.md): Panel · damaged · May 7, 2026 · N423UP · Boeing 75724APF
  > THE L/H LWR FWD TORQUE BOX PANEL HAS MULTIPLE DELAMINATIONS / DISBONDS (3EA TOTAL) NEAR THE TOP AND BOTTOM OF THE PANEL. ALL DAMAGE MARKED IN WHITE. INSTALLED NEW PART FWD TORQUE BOX LWR PANEL ASSEMBLY LH IAW SRM 51-40-02-0G-0.
- [SDR 2026FA0000317](https://openairdocs.org/sdr/2026FA0000317.md): Structure · corroded · May 4, 2026 · N572QS · Cessna 680A
  > ACCOMPLISHED REMOVAL OF CORROSION TO AFFECTED AREAS OF VERTICAL STABILIZER. INSPECTED THE REMAINING MATERIAL USING ULTRASONIC TESTING AND EDDY CURRENT FOR CRACKS. NO CRACKS NOTED. ACCOMPLISHED DOUBLER REPAIR TO ONE NOTED LOCATION AND RESTORED FINISH TO ALL SUR
- [SDR IPXA2026051490733](https://openairdocs.org/sdr/IPXA2026051490733.md): Panel · delaminated · Apr 26, 2026 · N440UP · Boeing 75724APF
  > THE L/H LWR FWD TORQUE BOX PANEL HAS 5EA DISBONDED / DELAMINATED AREAS FROM TOP TO BOTTOM. INSTALLED 1 EA TORQUE BOX PANEL IAW SRM 51-40-02.
- [SDR SWIA2026042576716](https://openairdocs.org/sdr/SWIA2026042576716.md): Drag Angle · cracked · Apr 25, 2026 · N614QX · Cndair CL6002C10
  > RIGHT FWD DRAG ANGLE VERTICAL CRACKED. REPAIR PERFORMED DRAG ANGLE AT RH FWD VERTICAL IAW REO 670-55-31-211, REV--, REO 670-55-31-018, REV-A, SRM 51-26-01, NDT PEFORMED.
- [SDR 2026FA0000295](https://openairdocs.org/sdr/2026FA0000295.md): Skin Panel · corroded · Apr 24, 2026 · N592QS · Cessna 560XL
  > FOUND SEVERAL SPOT OF CORROSION ON FWD FUSELAGE RH LOWER SECTION JUST FWD PANEL 153AC. BLENDED AND REMOVED CORROSION FROM FWD FUSELAGE RH LOWER SECTION JUST FWD PANEL 153AC. BLENDED AREA ON RH SIDE OF FUSELAGE WAS BEYOND LIMITS AND SUBMITTED TO AQRD. COMPLIED
- [SDR VNAA20260418005](https://openairdocs.org/sdr/VNAA20260418005.md): Drag Angle · cracked · Apr 18, 2026 · N605NN · Cndair CL6002D24
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPA
- [SDR IPXA2026051825110](https://openairdocs.org/sdr/IPXA2026051825110.md): Bracket · damaged · Apr 9, 2026 · N141UP · Airbus A300F4622R
  > VERTICAL STABILIZER RH FWD LOWER FAIRING SUPPORT BRACKET NR 4 HAS ELONGATED HOLE. SUPPORT BRACKET ON VERTICAL STABILIZER RH FWD LOWER FAIRING WAS REMOVED IAW SRM 51-40-21-001. INSTALLED NEW BRACKET ON VERTICAL STABILIZER RH FWD LOWER FAIRING IAW SRM 51-40-21
- [SDR VNAA202606120052](https://openairdocs.org/sdr/VNAA202606120052.md): Hinge · worn · Apr 3, 2026 · N649NN · Cndair CL6002D24
  > FREEPLAY ON BEARINGS OF RUDDER HINGE ASSY NBR 2 AND 3 IN TRAILING EDGE AREA AT VERTICAL STABILIZER. RUDDER HINGE ASSY NBR 2 AND 3 IN TRAILING EDGE AREA AT VERTICAL STABILIZER WERE REPLACED PER RIL #2103 REV.B AND RIL #1213 REV.A
- [SDR 2026F00046](https://openairdocs.org/sdr/2026F00046.md): Mount · corroded · Mar 31, 2026 · N339QS · Cessna 680CE
  > FOUND CORROSION ON MOUNTING FLANGES FOR PANEL 342AB. MECHANICALLY REMOVED CORROSION LOCATED WHERE 18 NUTPLATES WERE REMOVED ON INNER AND OUTER SIDE OF FLANGES ON PANEL 342AB ATTACHMENT BRACKETS (10 NUTPLATES ON LH SIDE AND 8 NUTPLATES ON RT SIDE) IAW SRM 51-70
- [SDR YENA2026032400331](https://openairdocs.org/sdr/YENA2026032400331.md): Washer · broken · Mar 21, 2026 · N975JT · Airbus A321231
  > DURING HEAVY MAINTENANCE: THS L/H AFT SUPPORT BEARING TAB WASHER BROKEN; REMOVED & REPLACED THS L/H AFT SUPPORT BEARING TAB WASHER IAW A321 AMM 55-16-38-400-002-A & 55-16-38--000 -OO2. REF STS WO N004320 N0326 ACC BY STS 695706, INSP BY QC 0046.
- [SDR VNAA20260501001](https://openairdocs.org/sdr/VNAA20260501001.md): Bearing · excess play · Mar 19, 2026 · N617NN · Bombdr CL6002D15
  > FREE PLAY IN THE BEARINGS (2EA) OF THE CENTRAL HINGES OF THE RUDDER. FITTING #2 WAS REPLACED PER RIL #2103 REV.B AND BEARING ON FITTING #3 WAS REPLACED PER RIL #1213 REV. A.
- [SDR VNAA20260501002](https://openairdocs.org/sdr/VNAA20260501002.md): Drag Angle · cracked · Mar 12, 2026 · N617NN · Bombdr CL6002D15
  > CRACK ON AFT DRAG ANGLE OF LH VERTICAL STABILIZER. CRACK ON AFT DRAG ANGLE OF LH VERTICAL STABILIZER WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR CALA2026021913908](https://openairdocs.org/sdr/CALA2026021913908.md): Beam · cracked · Feb 17, 2026 · N33132 · Boeing 757224
  > VERTICAL STAB. LT LOWER T/E SEAL STRAP BELOW ACCESS PANEL 324AL CRACKED. REPLACED LT VERTICAL TEE ANGLE. REMOVED BEAM DAMAGED AND REPLACED WITH A NEW BEAM IAW SRM 51-40-02, & DWG 173N1300.
- [SDR YENA2026021100195](https://openairdocs.org/sdr/YENA2026021100195.md): Bearing · corroded · Feb 10, 2026 · N4074J · Airbus A321271NX
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HIINGE ARM FITTING N1 ON VERTICLE STAB; (RESOLVED ON W/O: 1440538 TASKCARD: NR-00016) REFERENCE AEROMAN W.O. 2026 28/1 NR 2026-50621 ** REMOVED & REPLACED HINGE FITTING #1 ON VERTICAL STAB
- [SDR VNAA20260304027](https://openairdocs.org/sdr/VNAA20260304027.md): Hinge Fitting · excess play · Jan 29, 2026 · N604NN · Bombdr CL6002D15
  > FREE PLAY ON SELF-ALIGN SELF-LUBE BEARING PLAIN ON HINGE FITTING NR 3 ON THE VERTICAL STAB REAR SPAR MIDDLE SECTION. HINGE FITTING NR 3 AT VERTICAL STAB WAS REPLACED IAW SRM 51-42-21-001-001-A01, AND RIL 2103, REV B.
- [SDR VNAA202601280001](https://openairdocs.org/sdr/VNAA202601280001.md): Hinge Fitting · worn · Jan 28, 2026 · N646NN · Cndair CL6002C10
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NR 2 AND NR 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NR 2 AND NR 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED IAW SRM 51-42-21-001-001-A01 AND RIL 2103
- [SDR SWIA2026011375612](https://openairdocs.org/sdr/SWIA2026011375612.md): Drag Angle · cracked · Jan 13, 2026 · N726SK · Cndair CL6002C10
  > VERTICAL STAB. LH SIDE AFT DRAG ANGLE HAS POSSIBLE CRACKED. REPLACED VERTICAL STAB. LH SIDE AFT DRAG ANGLE REF CRJ700 51-42-21-001-001-A01, CRJ700 51-42-13-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01 AND DWG BA670-35002 REV: F. COMPLIED WITH 51-900-1002-S
- [SDR 1Q2R2026071650087](https://openairdocs.org/sdr/1Q2R2026071650087.md): Cap · damaged · Jan 11, 2026 · N523AE · Cndair CL6002C10
  > DURING LIGHTNING STRIKE INSPECTION FOUND MULTIPLE EXITS AT FS893.00 AND FS953.00, ALSO FOUND DAMAGE EXIT ON TOP OF SKULL CAP AND THE END CAP HAS 3 EXIT POINTS.
- [SDR REXA2026030900173](https://openairdocs.org/sdr/REXA2026030900173.md): Drag Angle · cracked · Dec 22, 2025 · N295PQ · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00 FWD ANGLE NO CRACKS WERE FOUND PER CRJ 700/900/1000 NDT MANUAL PART 06. 53-00-000-250-A01 (EQUIPMENT: NORTEC 600 C/N
- [SDR HNAA2026012800093](https://openairdocs.org/sdr/HNAA2026012800093.md): Profile · cracked · Dec 16, 2025 · N932AE · Emb EMB145LR
  > BOTTOM OF VERTICAL STAB, AFT OF REAR SPAR 3, RT PROFILE CRACKED AT LWR END. REPAIRED IAW ETD 2026-145-934573 AND EO1-55-26-0011
- [SDR HNAA2026012000017](https://openairdocs.org/sdr/HNAA2026012000017.md): Spar · cracked · Dec 16, 2025 · N932AE · Emb EMB145LR
  > BTM OF VRT STA, AFT OF REAR SPAR 3, LWR LH PROFILE CRACKED IN 2 PLACES. RAR PROFILE IAW SRM 51-40-02
- [SDR VNAA20260125019](https://openairdocs.org/sdr/VNAA20260125019.md): Fairing · worn · Dec 14, 2025 · N601EN · Bombdr CL6002D15
  > WEAR AND NICKS ON METALLIC CONTACT SURFACE OF LT VENTRAL FIN FAIRING. WEAR AND NICKS ON METALLIC CONTACT SURFACE OF LT VENTRAL FIN FAIRING WERE BLEND OUT PER REO 690-53-87-011 REV -.
- [SDR DALA2025121509132](https://openairdocs.org/sdr/DALA2025121509132.md): Bolt · missing · Dec 6, 2025 · N892AT · Boeing 717200
  > MISSING AND SUNKEN BOLTS ALONG DOUBLER SPLICE APPROX BTW STA ZFS=49 AND ZFS=76 AT VERTICAL STABILIZER LEADING EDGE. REPAIRED PER ER/A 630634-14. (1338826)
- [SDR VNAA20260203008](https://openairdocs.org/sdr/VNAA20260203008.md): Hinge Fitting · excess play · Dec 5, 2025 · N525AE · Bombdr CL6002D15
  > FREE PLAY ON TWO BEARINGS OF CENTER HINGES NR 2 & 3 OF THE RUDDER AT VERTICAL STABILIZER REAR SPAR. THE HINGE FITTINGS WERE REPLACED IAW RIL#2103 REV. B.
- [SDR VNAA202511290003](https://openairdocs.org/sdr/VNAA202511290003.md): Drag Angle · cracked · Nov 30, 2025 · N537EA · Cndair CL6002C10
  > CRACK ON RT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE WAS REPAIRED PER CRJ700 SRM 55-31-00
- [SDR VNAA202511290002](https://openairdocs.org/sdr/VNAA202511290002.md): Drag Angle · cracked · Nov 30, 2025 · N537EA · Cndair CL6002C10
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE. CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE WAS REPAIRED PER SRM 55-31-00-201-00
- [SDR SWIA2026031075493](https://openairdocs.org/sdr/SWIA2026031075493.md): Drag Angle · cracked · Nov 17, 2025 · N632SK · Cndair CL6002C10
  > VERTICAL STAB LEFT SIDE FWD DRAG ANGLE IS CRACKED AT AFT END (C-CHECK RO 03/08/2026)PERFORMED REPAIR ON VERTICAL STAB LEFT SIDE FWD DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE 2016/11/10, CRJ700 AMM 20-70-00. SRM 51-42-06, 51-42-21
- [SDR JGVR20251117003](https://openairdocs.org/sdr/JGVR20251117003.md): Hinge Bracket · corroded · Nov 17, 2025 · N378QS · Cessna 680CE
  > BLENDED CORRODED AREA ON THE VERTICAL STABILIZER MIDDLE RUDDER HINGE UPPER BRACKET, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR FDEA202511062135](https://openairdocs.org/sdr/FDEA202511062135.md): Stiffener · corroded · Nov 6, 2025 · N574FE · Doug MD11F
  > VERTICAL STABILIZER CENTER SPAR UPON TRIM OUT OF STIFFENER FOUND CORROSION AT STATION 2122 X= -18.65 5 O'CLOCK AREA (REFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00474). CORROSION ON STIFFENER AT EMPENNAGE VERTICAL STABILIZER REAR CENTER SPAR AT BS 2122
- [SDR DALA2025101707596](https://openairdocs.org/sdr/DALA2025101707596.md): Not Reported · not reported · Oct 16, 2025 · N979AT · Boeing 717200
  > SHIP 9544 ACCOMPLISH ER/A 617313-14 REV A. CORRECTIVE ACTION: REPARIED PER ER/A 14-617313. (1255302)
- [SDR REXA2025111900989](https://openairdocs.org/sdr/REXA2025111900989.md): Drag Angle · cracked · Oct 3, 2025 · N910XJ · Cndair CL6002D24
  > RIGHT AFT DRAG ANGLE IS CRACKED AT FORWARD END. REMOVED RH AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. LOCATED, DRILLED, AND COUNTERSINK NEW SERVICEABLE RT AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01. I
- [SDR YENA2025093000982](https://openairdocs.org/sdr/YENA2025093000982.md): Hinge Fitting · corroded · Sep 27, 2025 · N618JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION FOUND ON THE BORE OF HINGE N7 VERTICAL STABILIZER; REF AEROMAN WO 2025 282/1 NR 2025-530866. REMOVED AND REPLACED HINGE #7 VERTICAL STABILIZER IAW AMM 27-21-41-400-001-A STEP 2 (A). TOOL USED EDDY CURRE
- [SDR YENA2025093000981](https://openairdocs.org/sdr/YENA2025093000981.md): Hinge Fitting · corroded · Sep 25, 2025 · N805JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ3 VERTICAL STABILIZER; REMOVED AND REPLACED #3 VERTICAL STABILISER FITTING ALL WORK DONE BY O. FLORES 8621011 AND QC RII. C. PORTILLO # 230. ALL WORK EMBODIED ON AEROMAN
- [SDR YENA2025093000980](https://openairdocs.org/sdr/YENA2025093000980.md): Bearing · corroded · Sep 25, 2025 · N805JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ4 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE ARM FITTING 4 AND FASTENERS ON VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008 STEP 2.A AND A320 SRM 51-72-11 AND DW
- [SDR YENA2025093000979](https://openairdocs.org/sdr/YENA2025093000979.md): Hinge Arm · corroded · Sep 25, 2025 · N805JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ1 VERTICAL STABILIZER; (RESOLVED ON W/O: 1401080 TASKCARD: NR-00014) REMOVED AND REPLACED HINGE ARM FITTING 1 AND FASTENERS ON VERTICAL STABILIZER I.A.W A320 SRM 55-36-42
- [SDR YENA2025092300957](https://openairdocs.org/sdr/YENA2025092300957.md): Hinge Arm · corroded · Sep 20, 2025 · N621JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ5 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00040) REMOVED AND REPLACED HINGE FITTING #5 LOC. VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008 ALL
- [SDR YENA2025092300956](https://openairdocs.org/sdr/YENA2025092300956.md): Bearing · corroded · Sep 20, 2025 · N621JB · Airbus A320232
  > DURING HEAVY MAINTENANCE: AFTER REMOVE BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ4 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00041) REMOVED AND REPLACED HINGE FITTING #4 LOC. VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008. ALL
- [SDR AALA202509176420](https://openairdocs.org/sdr/AALA202509176420.md): Hinge Arm · excess play · Sep 1, 2025 · N187US · Airbus A321211
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR NR 4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR VNAA202509250028](https://openairdocs.org/sdr/VNAA202509250028.md): Static Wick · corroded · Aug 7, 2025 · N526EA · Cndair CL6002C10
  > CORROSION AT STATIC DICHARGER BASE, ACCESS PANEL 343BR. STATIC DICHARGER BASE ON ACCESS PANEL 343BR WAS REPLACED PER CRJ700 AMM 55-00-28-960-801 (CONFIG A01) AND SRM 51-42-06-001-001-A01

Next page: https://openairdocs.org/jasc/5530/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 = '5530'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5530/reports

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