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 VNAA202509250024Hinge Fitting · excess playDURING INSPECTION OF TASK CARD :55-30-203-JIC GVI OF THE VERTICAL STABILIZER INTERNAL AREA AROUND RUDDER POWER CONTROL UNIT WAS FOUND FREEPLAY ON BEARING OF LOWER HINGE FITTING AT REAR SPAR OF VERTICAL STABILIZER. HINGE FITTING #3 (P/N: AV670-21081-013 ) WAS Aug 6, 2025 · N526EA · Cndair CL6002C10SDR CALA2025081207629Skate Angle · wornLEFT BODY-TO-VERTICAL FIN FAIRINGS FLANGE HAS CHAFING WORN DAMAGE FOR REF AAR N/R 97525018. REMOVED AND REPLACED SKATE ANGLE AT LT BODY TO VERTICAL FIN AFT SECTION REF SRM 51-40-02-0G-0 AND DWG 148A8300.Aug 4, 2025 · N17244 · Boeing 737824SDR CALA2025080707429Skate Angle · worn{B737-06-3-0068} RH BODY-TO-VERTICAL FIN FAIRINGS FLANGE HAS CHAFFING WORN DAMAGE. REMOVED AND REPLACED AFT RIGHT BODY TO VERTICAL FIN ANGLE (SKATE ANGLE) REF SRM 51-40-02-0G-0 AND DWG 148A8300. REMOVED AND REPLACED AFT RIGHT BODY TO VERTICAL FIN ANGLE (SKAug 4, 2025 · N17244 · Boeing 737824SDR VNAA202509250003Hinge Fitting · excess playDURING INSPECTION OF TASK CARD :55-30-203-JIC GVI OF THE VERTICAL STABILIZER INTERNAL AREA AROUND RUDDER POWER CONTROL UNIT WAS FOUND FREEPLAY ON BEARING OF LOWER HINGE FITTING AT REAR SPAR OF VERTICAL STABILIZER. HINGE FITTING #3 (P/N: AV670-21081-013 ) WAS Aug 2, 2025 · N526EA · Cndair CL6002C10SDR VNAA20251015007Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV.BJul 23, 2025 · N640NN · Bombdr CL6002D15SDR SWAA2025080791392Panel · crackedCRACK ON UPPER LEFT SLIDE PANEL COMMON TO 332AT. REMOVED AND REPLACED LEFT SLIDE PANEL COMMON TO 332AT PER AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.Jul 15, 2025 · N912WN · Boeing 7377H4SDR UIEA2025070700853Fairing · delaminatedDORSAL FAIRING FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW RI-55-30-17752 REV.A. NO FURTHER DEFECTS NOTED.</P>)Jul 12, 2025 · N445MC · Boeing 7474B5FSDR YENA2025070800696Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 1 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315970 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #1 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-3.Jul 5, 2025 · N768JB · Airbus A320232SDR YENA2025070800695Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 3 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315971 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #3 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-36.Jul 5, 2025 · N768JB · Airbus A320232SDR YENA2025070800694Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 4 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315972 WO 2025-177/1 REMOVED AND REPLACED HINGE FITTING #4 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-3.Jul 5, 2025 · N768JB · Airbus A320232SDR YENA2025070800693Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 5 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315973 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #5 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55.Jul 5, 2025 · N768JB · Airbus A320232SDR YENA2025070800692Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 7 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315974 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #7 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-36-4.Jul 5, 2025 · N768JB · Airbus A320232SDR REXA2025062600694Angle · crackedCRACK ON LEFT 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 LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (Jun 17, 2025 · N601LR · Cndair CL6002D24SDR 8LFA202506170002Cap · brokenDURING POST FLIGHT PILOT WALK AROUND, NOTED UPPER CAP OF VERTICAL STABILIZER DEPARTED IN FLIGHT. EXPOSED WIRING WAS VISIBLE.Jun 16, 2025 · N429LF · Bell 429SDR VNAA20250610065Drag Angle · crackedRIGHT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. NOTE: DUE TO HEAVY PAINT IN AREA STRIP AND VERIFY WITH NDT. CRACKED DRAG ANGLE P/N AV670-21186-004 REMOVED IAW CRJ700 SRM TASK 51-42-21-001-001-A01, TASK 51-42-22-001-001-A01, TASK 51-42-13-001-001-A01. NEW Jun 10, 2025 · N513AE · Cndair CL6002C10SDR VNAA20250610064Drag Angle · crackedLEFT VERTICAL STAB FWD DRAG ANGLE PREVIOUS REPAIR APPEARS CRACKED. NOTE: DUE TO HEAVY PAINT IN AREA STRIP AND VERIFY WITH NDT. REMOVED DAMAGED PREVIOUS REPAIR IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED AND INSTALLED NEW DRAG ANGJun 10, 2025 · N513AE · Cndair CL6002C10SDR IPXA2025062645098Plate · dentedRIGHT HORZ STAB PANEL 342AB L/E HAS 10EA DENTS-109-VWV. INSTALLED NEW PLATE IAW SRM 51-40-21.Jun 4, 2025 · N130UP · Airbus A300F4622RSDR SWAA2025061776668Support Angle · crackedCRACK ACCESS PANEL 323CL SUPPORT ANGLE AT VERTICAL STABILIZER. REPLACED SUPPORT ANGLE ON ACCESS PANEL 323CL AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 172A6124; SHEET 1; REV E.May 30, 2025 · N441WN · Boeing 7377H4SDR SWAA2025060975497Angle · crackedCRACK ON CLOSURE ANGLE EXISTING REPAIR LOCATED AT BS1104 MORE 6 INCH AND BTW STR2L TO STR3L AT UPPER FUSELAGE. REPAIRED CLOSURE ANGLE LOCATED BETWEEN BS1104 MORE 6 INCH AND BS1156 AND BTW STR2L TO STR3L AT UPPER FUSELAGE IAW B737-700 SRM 53-80-71-2R-6 REPAIRMay 27, 2025 · N7835A · Boeing 737752SDR JGVR20250521001Support Bracket · corrodedREMOVED THE CORRODED UPPER RUDDER SUPPORT UPPER BRACKET, RECEIVED FABRICATED NEW BRACKET PART NUMBER AQRD-6931050-64 AND INSTALLED PER TEXTRON 680 SRM 51-40-03 AND AEROSPACE QUALITY RESEARCH AND DEVELOPMENT MRO ENGINEERING REPAIR ORDER AND NETJETS REQUEST FOR May 21, 2025 · N376QS · Cessna 680CESDR WX0A2025052332435Hinge · loose(AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) (35675-3) VERTICAL STABILIZER RUDDER HINGE NO. 4 FIITING BEARING LOOSE. / VERTICAL STABILIZER, RUDDER HINGE #4 FITTING ASSEMBLY FORK END PERMANENTLY REPAIRED BY REPLACEMENT AS PER SRM 55-36May 16, 2025 · N250NV · Airbus A320214SDR JGVR20250516001Support Bracket · corrodedREMOVED THE CORRODED MIDDLE LOWER RUDDER SUPPORT BRACKET, RECEIVED FABRICATED NEW BRACKET PART NUMBER AQRD-6931050-61 AND INSTALLED PER TEXTRON 680 SRM 51-40-03 AND AEROSPACE QUALITY RESEARCH AND DEVELOPMENT MRO ENGINEERING REPAIR ORDERMay 16, 2025 · Cessna 680CESDR REXA2025060900645Drag 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). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRApr 29, 2025 · N903XJ · Cndair CL6002D24SDR REXA2025060900644Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATApr 29, 2025 · N903XJ · Cndair CL6002D24SDR YENA2025042900449Hinge Fitting · not reportedDURING HEAVY MAINTENANCE: REMOVED AND REPLACED HINGE FITTING VERTICAL STABILIZER IAW A320 SRM 51-72-11 AND IAW A320 SRM 55-36-42-300-008 AND AMM 27-21-41-000-001-A STEP 4A(7) RII AND WORK ACCOMPLISHED ON AEROMAN WO:2025 129/1 NON-ROUTINE 2025-202316.Apr 26, 2025 · N526JL · Airbus A320232SDR VNAA20250602021Skin · damagedDAMAGE ON RH VERTICAL STAB REAR SPAR DATUM. RH VERTICAL STAB REAR SPAR DATUM WAS REPAIRED PER REO 690-53-71-087 REV. -Apr 17, 2025 · N598NN · Cndair CL6002D24SDR KCSA202504051073Doubler · corrodedCORROSION FOUND IN L/H SIDE UPPER LOBE DOUBLER NEAR RADIUS AND VERTICAL STABILIZER ATTACHMENT AT STATION 2521 DURING EXTERNAL SURFACE INSPECTIONApr 5, 2025 · N701CK · Boeing 7474B5FSDR DALA2025030301616Stabilizer · ground damageAIRCRAFT 3737, WHILE PARKED ON DE-ICE PAD IN SEA, AIRCRAFT WAS STRUCK BY THE RIGHT WINGTIP OF A TAXIING JAL B787. AIRCRAFT VERTICAL STABILIZER WAS STRUCK ON THE RIGHT SIDE CAUSING SUBSTANTIAL DAMAGE. IN ORDER TO ACCESS THE BOLTS FOR THE REAR SPAR PRIMARY FITTIFeb 27, 2025 · N3737C · Boeing 737832SDR DALA2025030201577Structure · damaged(LOG 0828481) ACCESS HOLE CUTOUT IN LWR CLOSURE RIB WEB (P/N 172A3104-1) IS MADE FOR REAR SPAR PRIMARY FITTING BOLTS INSPECTION. HOLE CUTOUT IS REPAIRED BY DOUBLER IAW PRI 624294-14 REV 1.Feb 25, 2025 · N3737C · Boeing 737832SDR DALA2025030401688Bushing · corroded(LOG 0824717) ON FWD MOUNT OF VERTICAL STAB, FOUND CORROSION ON RIGHT BOLT ATTACH BUSHING AND FRAME. REMOVED AND REPLACED R/H FWD ATTACH BUSHING REF PRI 624280-14.Feb 23, 2025 · N3737C · Boeing 737832SDR DALA2025030401689Bushing · corroded(LOG 0824702) FOUND CORROSION ON FWD MOUNT OF VERTICAL STAB ON LH FWD BUSHING AND FRAME AROUND BUSHING ATTACH BOLT. REMOVED AND REPLACED L/H FWD MOUNT BUSHING REF PRI 624280-14.Feb 22, 2025 · N3737C · Boeing 737832SDR DALA2025022101361Fastener · loose-AD- LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE FOUND IN REFERENCE TO AMDS 5530-01048-02 STEP 3 "AA 5530-01048" AND "AD 2018-10-08". SUMMARY OF NRC 00058: FASTENERS (5 EA) OF RH VERTICAL STABILIZER LEADING EDGFeb 19, 2025 · N928AT · Boeing 717200SDR GTIA2025020638730Hinge Arm · damagedELONGATE HOLES ON HINGE ARM 1 ON VERTICAL STABILIZER RAF-01 3634034-01 GENERATED-REPLACED HINGE ARM FITTING #1 ON VERTICAL STABILIZER IAW EA #55-0003-25 PART 2 D55371052 THIS REPAIR IS PERMANENT AND NOT REQUIRED INSPECTIONFeb 5, 2025 · N664NK · Airbus A321231SDR REXA2025030600269Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31Jan 31, 2025 · N183GJ · Cndair CL6002D24SDR YENA2025012100076Attach Fitting · corrodedDURING HEAVY MAINTENANCE: VERTICAL STAB TRAILING EDGE #7 RUDDER ATTACH FITTING HAS SMALL AREA OF CORROSION AT FWD LOWER PANEL FASTENER; ACCOMPLISH REPLACEMENT OF HINGE ARM BR7 ON VERTICAL STABILIZER IN ACCORDANCE WITH REF HAECO W/O # 169003 JETBLUE W/O # 13776Jan 17, 2025 · N519JB · Airbus A320232SDR VNAA202501210026Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. CORRECTIVE ACTION: SUMMARY: HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV.Jan 16, 2025 · N595NN · Cndair CL6002D24SDR DALA2025011700412Hinge Arm · damagedSHIP 3147 ELONGATED HOLE HINGE ARM BR2 IN VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 622906-14. (0764087)Jan 16, 2025 · N347NB · Airbus A319114SDR WRXR20250113004Fairing · erodedDURING MAINTENANCE PANEL 326AL WAS FOUND WITH DAMAGE TO THE COPPER MESH ON THE EXTERNAL SURFACE. SANDED DAMAGED AREA TO REMOVE BONDED MESH. CLEANED AREA TO REMOVE ANY DUST. CUT PLIES TO FIT AREA.Jan 13, 2025 · N540EG · Cndair CL6002C10SDR SWIA2025033100108Drag Angle · crackedAFT DRAG ANGLE CRACKED ON RH SIDE OF VERTICAL STABLIZER (C-CHECK RO 03/29/2024)REPAIRED DAMAGED AFT DRAG ANGLE ON RH SIDE OF VERTICAL STABILIZER IAW CRJ700 SRM 51-25-16 AND REO 670-55-31-018 REV-A DATE 2016-11-10, REO 670-55-31-180 REV-- DATE 2024-08-29. NDT PJan 8, 2025 · N767SK · Cndair CL6002C10SDR SWAA2025012882026Skin Panel · delaminatedAREA OF DELAMINATION APPROX. 1.9' X 1.8'ON DORSAL FIN L/H SIDE SKIN 23.9' FROM LOWER EDGE; 37.3' FROM AFT EDGE.<[01] AREA OF DELAMINATION APPROX. 1.9' X 1.8' ON DORSAL FIN AT L/H SIDE SKIN 23.9' FROM LOWER EDGE; 37.3' FROM AFT EDGE WAS REPAIRED IAW SRM 51-70-0Dec 31, 2024 · N8606C · Boeing 7378H4SDR AALA202501273840Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER #4 RUDDER HINGE ARM FITTING HAS AN ELONGATED FASTENER HOLE AT VERTICAL STABILZER RIB 6. REPLACED HINGE ARM FITTING PER SRM 55-36-42.Dec 27, 2024 · N165US · Airbus A321211SDR GTIA2024122338620Hinge Arm · damagedELONGATED HOLES ON VERTICAL STABILIZER HINGE ARM #4 RAF-01 3415093-02 GENERATED -REPLACED HINGE ARM 4 LOC. ON VERTICAL STABILIZER IAW A321 EA 55-9012-24 AND SRM 55-36-42-300-003 SRM 51-43-00 AND DWG D553-71052-0012 THIS REPAIR IS CATEGORY "A" AND NOT REQUIRED Dec 21, 2024 · N665NK · Airbus A321231SDR GTIA2024122338619Hinge Arm · damagedELONGATED HOLES ON VERTICAL STABILIZER HINGE ARM #1 RAF-01 3415093-01 GENERATED -REPLACED HINGE ARM 1 LOC. ON VERTICAL STABILIZER IAW A321 EA 55-9012-24 AND SRM 55-36-42-300-003 SRM 51-43-00 AND DWG D553-71052-0012 THIS REPAIR IS CATEGORY "A" AND NOT REQUIRED Dec 21, 2024 · N665NK · Airbus A321231SDR SWI2025F00258Stringer · dentedSTGR SECTION 18R BETWEEN F.S. 755.00 AND V.S. 67.50 FOUND DAMAGED WHILE ADDRESSING SKIN DENT BETWEEN F.S. 755.00 AND V.S. 67.50 (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW STGR18R BETWEEN FS755.00 AND V.S.67.50 PER CRJ200SRM 51-42-06 AND DWG 60Dec 20, 2024 · N487CA · Cndair CL6002B19SDR SWI2025F00257Stringer · dentedSTGR 17R BETWEEN F.S. 755 AND V.S. 67.50 FOUND DAMAGED WHEN ADDRESSING FUSELAGE SKIN DENT BETWEEN F.S. 755.00 AND V.S. 67.50 (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW STGR17R BETWEEN FS755.00 AND V.S.67.50 PER CRJ200SRM 51-42-06 AND DWG 600-2Dec 20, 2024 · N487CA · Cndair CL6002B19SDR HNAA2025010700018Profile · cracked55-2159 VERT STAB, AFT OF SPAR #3, LH UPPER PROFILE CRACKED ABOVE RUDDER UPPER MID HINGE. RAR PROFILE IAW SRM 51-40-02Dec 20, 2024 · N672AE · Emb EMB145LRSDR SWI2025F00252Drag Angle · crackedRH VERTICAL STAB. FWD DRAG ANGLE HAS POSSIBLE CRACK AT AFT END (MARKED). CAMP# 29312422 (C-CHECK RO 2/26/2025) REPLACED RH VERTICLE STAB FWD DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01COMPLIED WITH TASK 51-900-1002-SKYDec 13, 2024 · N809SK · Cndair CL6002D24SDR SWI2025F00246Drag Angle · crackedRH AFT VERTICAL STAB. DRAG ANGLE HAS POSSIBLE CRACK AT FWD END (MARKED). (C-CHECK RO 2/26/2025) REPLACED RH AFT VERTICAL STAB FWD DRAG ANGLE REF CRJ900 SRM TASK 55-31-00-201-001-A01COMPLIED WITH TASK 51-900-1002-SKYDec 11, 2024 · N809SK · Cndair CL6002D24SDR SWI2025F00245Drag Angle · crackedLH AFT VERTICAL STAB. DRAG ANGLE HAS POSSIBLE CRACK AT FWD END (MARKED). (C-CHECK RO 2/26/2025) REPLACED LH AFT VERTICLE STAB FWD DRAG ANGLE CRJ900 SRM 55-31-00-201-001-A01COMPLIED WITH TASK 51-900-1002-SKYDec 11, 2024 · N809SK · Cndair CL6002D24SDR AALA202502102043Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED ON HINGE ARM FITTING 1 LOWER AREA. MAINTENANCE REPLACED HINGE ARM #1 ON TRAILING EDGE OF VERTICAL STABILIZER AND FASTENERS IAW EA #360672, A319 SRM 55-36-42-300-003, A319 Dec 10, 2024 · N769US · Airbus A319112
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