JASC 5530

Service difficulty reports · 2,534

Reports filed under 5530 · Vertical Stabilizer, 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 = '5530'
  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 2026FA0000836Fairing · separatedUPPER VERTICAL TIP CAP FAIRING SEPARATED IN FLIGHT, SUBSEQUENTLY DAMAGING UPPER PORTION OF RUDDER, UPPER VERTICAL SKIN, ELEVATOR PUSH RODS AND ELEVATOR HORNS.Oct 14, 2026 · N703BA · Textrn 408SDR CALA2026092119598Tape · peelingSPEED 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 SSep 17, 2026 · N33714 · Boeing 737724SDR IPXA2026090711902Panel · debondedTHE 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 SRAug 25, 2026 · N441UP · Boeing 75724APFSDR IPXA2026091095169Panel · delaminatedMAJOR 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 Aug 24, 2026 · N441UP · Boeing 75724APFSDR VNAA202609010022Hinge Fitting · wornFREE 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 51-42-2Jul 8, 2026 · N642NN · Cndair CL6002D24SDR YENA2026070900530Hinge Arm · damagedDURING HEAVY MAINTENANCE, STABILIZERS, VERTICAL STABILIZER, HINGE ARM BR3 & FORK END FITTING ASSY ELONGATED HOLES. TIME LIMITED REPAIR (CONSIDERED MAJOR REPAIR)Jul 5, 2026 · N806JB · Airbus A320232SDR AALA202608072053Hinge Arm · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER HINGE ARM 7 AT RIB 11. REPLACED HINGE ARM PER EA 377460 AND SRM 55-36-42-300-003Jun 29, 2026 · N9016 · Airbus A319115SDR SCNA20260717314Access Panel · wornWEAR 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 DEJun 18, 2026 · N801SY · Boeing 7378Q8SDR SCNA20260717313Access Panel · wornIN 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 ALLOWAJun 18, 2026 · N801SY · Boeing 7378Q8SDR DALA2026053103300Hinge Arm · corrodedLEVEL 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: FORMay 29, 2026 · N351NW · Airbus A320212SDR VNAA202607010011Hinge · excess playFREE 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 #May 16, 2026 · N530EA · Cndair CL6002C10SDR IPXA2026060473078Panel · damagedTHE 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.May 7, 2026 · N423UP · Boeing 75724APFSDR 2026FA0000317Structure · corrodedACCOMPLISHED 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 SURMay 4, 2026 · N572QS · Cessna 680ASDR IPXA2026051490733Panel · delaminatedTHE 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.Apr 26, 2026 · N440UP · Boeing 75724APFSDR SWIA2026042576716Drag Angle · crackedRIGHT 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.Apr 25, 2026 · N614QX · Cndair CL6002C10SDR 2026FA0000295Skin Panel · corrodedFOUND 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 Apr 24, 2026 · N592QS · Cessna 560XLSDR VNAA20260418005Drag Angle · crackedCRACK 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 REPAApr 18, 2026 · N605NN · Cndair CL6002D24SDR IPXA2026051825110Bracket · damagedVERTICAL 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 51-40-21Apr 9, 2026 · N141UP · Airbus A300F4622RSDR VNAA202606120052Hinge · wornFREEPLAY 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.AApr 3, 2026 · N649NN · Cndair CL6002D24SDR 2026F00046Mount · corrodedFOUND 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 51-70Mar 31, 2026 · N339QS · Cessna 680CESDR YENA2026032400331Washer · brokenDURING 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.Mar 21, 2026 · N975JT · Airbus A321231SDR VNAA20260501001Bearing · excess playFREE 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.Mar 19, 2026 · N617NN · Bombdr CL6002D15SDR VNAA20260501002Drag Angle · crackedCRACK 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-A01Mar 12, 2026 · N617NN · Bombdr CL6002D15SDR CALA2026021913908Beam · crackedVERTICAL 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.Feb 17, 2026 · N33132 · Boeing 757224SDR YENA2026021100195Bearing · corrodedDURING 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 STABFeb 10, 2026 · N4074J · Airbus A321271NXSDR VNAA20260304027Hinge Fitting · excess playFREE 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.Jan 29, 2026 · N604NN · Bombdr CL6002D15SDR VNAA202601280001Hinge Fitting · wornFREE 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 Jan 28, 2026 · N646NN · Cndair CL6002C10SDR SWIA2026011375612Drag Angle · crackedVERTICAL 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-SJan 13, 2026 · N726SK · Cndair CL6002C10SDR 1Q2R2026071650087Cap · damagedDURING 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.Jan 11, 2026 · N523AE · Cndair CL6002C10SDR REXA2026030900173Drag Angle · crackedCRACK 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 Dec 22, 2025 · N295PQ · Cndair CL6002D24SDR HNAA2026012800093Profile · crackedBOTTOM OF VERTICAL STAB, AFT OF REAR SPAR 3, RT PROFILE CRACKED AT LWR END. REPAIRED IAW ETD 2026-145-934573 AND EO1-55-26-0011Dec 16, 2025 · N932AE · Emb EMB145LRSDR HNAA2026012000017Spar · crackedBTM OF VRT STA, AFT OF REAR SPAR 3, LWR LH PROFILE CRACKED IN 2 PLACES. RAR PROFILE IAW SRM 51-40-02Dec 16, 2025 · N932AE · Emb EMB145LRSDR VNAA20260125019Fairing · wornWEAR 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 -.Dec 14, 2025 · N601EN · Bombdr CL6002D15SDR DALA2025121509132Bolt · missingMISSING 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)Dec 6, 2025 · N892AT · Boeing 717200SDR VNAA20260203008Hinge Fitting · excess playFREE 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.Dec 5, 2025 · N525AE · Bombdr CL6002D15SDR VNAA202511290003Drag Angle · crackedCRACK 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 55-31-00Nov 30, 2025 · N537EA · Cndair CL6002C10SDR VNAA202511290002Drag Angle · crackedCRACK 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 55-31-00-201-00Nov 30, 2025 · N537EA · Cndair CL6002C10SDR SWIA2026031075493Drag Angle · crackedVERTICAL 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, 51-42-21Nov 17, 2025 · N632SK · Cndair CL6002C10SDR JGVR20251117003Hinge Bracket · corrodedBLENDED 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.Nov 17, 2025 · N378QS · Cessna 680CESDR FDEA202511062135Stiffener · corrodedVERTICAL 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 Nov 6, 2025 · N574FE · Doug MD11FSDR DALA2025101707596Not Reported · not reportedSHIP 9544 ACCOMPLISH ER/A 617313-14 REV A. CORRECTIVE ACTION: REPARIED PER ER/A 14-617313. (1255302)Oct 16, 2025 · N979AT · Boeing 717200SDR REXA2025111900989Drag Angle · crackedRIGHT 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. IOct 3, 2025 · N910XJ · Cndair CL6002D24SDR YENA2025093000982Hinge Fitting · corrodedDURING 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 CURRESep 27, 2025 · N618JB · Airbus A320232SDR YENA2025093000981Hinge Fitting · corrodedDURING 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 Sep 25, 2025 · N805JB · Airbus A320232SDR YENA2025093000980Bearing · corrodedDURING 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 DWSep 25, 2025 · N805JB · Airbus A320232SDR YENA2025093000979Hinge Arm · corrodedDURING 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 55-36-42Sep 25, 2025 · N805JB · Airbus A320232SDR YENA2025092300957Hinge Arm · corrodedDURING 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 ALLSep 20, 2025 · N621JB · Airbus A320232SDR YENA2025092300956Bearing · corrodedDURING 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. ALLSep 20, 2025 · N621JB · Airbus A320232SDR AALA202509176420Hinge Arm · excess playAIRCRAFT 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.Sep 1, 2025 · N187US · Airbus A321211SDR VNAA202509250028Static Wick · corrodedCORROSION 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-A01Aug 7, 2025 · N526EA · Cndair CL6002C10
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