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 SWAA2024122374467Panel · crackedCRACK ON RIB 8 ACCESS PANEL 321A AT VERTICAL STABILIZER 2024-748272<[01] REPLACED RIB 8 ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 DRAWING 174A1008 SHEET 2 REV C AND DRAWING 174A0103 SHEET 7 REV -. SEE INDIVIDUAL Dec 5, 2024 · N933WN · Boeing 7377H4SDR VNAA20250102007Hinge · excess playAFTER RUDDER REMOVAL, FREE 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.B.Nov 29, 2024 · N590NN · Cndair CL6002D24SDR VNAA202411290020Hinge · abnormalDESCRIPTION: FREE 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: NEW HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PENov 27, 2024 · N591NN · Cndair CL6002D24SDR AALA202412037696Expansion Joint · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN VERTICAL STABILIZER EXPANSION JOINT (J-ANGLE) LOCATED AT STA 1020, RBL 16. REPLACED EXPANSION JOINT ASSEMBLY PER AARD 55-30-09-3 REPAIR 3.Nov 22, 2024 · N956AN · Boeing 737823SDR YENA2024111201457Stabilizer · wornDURING HEAVY MAINTENANCE: WEAR ON HINGE 6 UPPER SIDE LOWER AREA ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00042) REF AE WO 2024-275/1. N/R# 2024 - 538686. REMOVED AND REPLACED HINGE #6 ON VERTICAL STABILIZER IAW A320 SRM 51-42-11, A320 SRMNov 6, 2024 · N571JB · Airbus A320232SDR COEA2024110632759Skin · damagedWO 262496 NR 1 DISCREPANCY: DURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER INNER AND EXTERIOR STRUCTURE PULLED THROUGH HARDWARE ON FORWARD ATTACHMENT POINTS. REPLACED WITH NEW PER TEXTRON AVIATION 408 SRM 51-40-05 REV. 4.Nov 1, 2024 · N759FX · Textrn 408SDR COEA2024110631759Closeout Panel · crackedDURING A DETAILED VISUAL INSPECTION OF THE UPPER VERTICAL STABILIZER INNER AND EXTERIOR STRUCTURE A CRACK WAS FOUND ON THE VERTICAL STABILIZER CLOSEOUT PANEL LH FASTENER HOLE JUST AFT OF FWD ATTACHMENT POINTS. CRACK ON THE VERTICAL STABILIZER CLOSEOUT PANEL LHNov 1, 2024 · N759FX · Textrn 408SDR REXA2024111101447Angle · corrodedL/H FLOOR SILL IS CORRODED BETWEEN F.S. 1047 TO F.S. 1069.73 AROUND SCREW HOLES. REMOVED LOWER FLOOR SILL AT FS 1047 TO FOM IAW CRJ 700 SRM 51-42-06-001-001-A01, LOCATED AND DRILLED NEW SERCIABLE SIDE BEAM P/N MM670-35373-005 IAW CRJ-700 SRM 51-40-11-001-001-AOct 21, 2024 · N371CA · Cndair CL6002C10SDR DALA2024101810189Bushing · crackedCRACK ON BUSHING WAS FOUND, PREVIOUSLY TO INSTALL NEW LOWER BRACKET ON LEADING EDGE AT VERTICAL STABILIZER. SUMMARY OF NRC 00927: CRACK ON BUSHING OF VERTICAL STABILIZER L.E. ZFS=46.300 TO ZFS=52.267 WAS REPAIRED PER ER/A 620945-14 REV ORIGINAL SECTION I: PERMOct 17, 2024 · N717JL · Boeing 717200SDR DALA2024101009962Access Panel · crackedSHIP 3144 CRACK ACCESS PANEL 322BL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIR INSTRUCTIONS ON ACCESS PANEL 322BL LEADING EDGE VERTICAL STABILIZER AS PER ER/A 620416-14. (0600576)Oct 9, 2024 · N344NB · Airbus A319114SDR REXA2024111101445Drag Angle · crackedPOSSIBLE CRACK AND 4EA SMOKING HI-LITES L/H SIDE OF VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE REPAIRED L/H VERTICAL STAB FWD DRAG ANGLE IAW CRJ-700 SRM 55-31-00-201-001-A01.Oct 8, 2024 · N371CA · Cndair CL6002C10SDR AALA202409237875Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: OVERSIZED FASTENER HOLE .301 AT VERTICAL STATION 2632 AND RIB 6, BR4 HINGE ARM EXCEEDS LIMITS. REMOVED AND REPLACED BR4 HINGE ARM PER SRM 51-42-11-801.Sep 21, 2024 · N138AN · Airbus A321231SDR AALA202409238045Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER BR2 HINGE ARM OVERSIZED FASTENER HOLE MEASURES .306", EXCEEDS LIMITS OF .265". REPLACED BR2 HINGE ARM PER SRM 51-42-11-801.Sep 20, 2024 · N138AN · Airbus A321231SDR EE4Y2024091820889Hinge Arm · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD ZL325-01-1-001, EMPENNAGE VERTICAL STABILIZER TRAILING EDGE CORROSION WAS FOUND COMMON TO ATTACHMENT HOLES AT THE TRAILING EDGE PANEL ATTACHMENT FLANGES OF THE HINGE ARM 6 LH /RH SIDE. PERFORMED REPAIR AT VERTICSep 18, 2024 · N308NV · Airbus A319112SDR SWIA20241203916Drag Angle · crackedRH FWD DRAG ANGLE AT ROOT OF VERTICAL STAB. HAS POSSIBLE CRACK AT AFT SIDE IN RADIUS (MARKED). (C-CHECK RO 11/30/2024) REMOVED CRACKED DRAG ANGLE AND REPAIRED WITH FABRICATED REPAIR PARTS ON FWD DRAG ANGLE AT RH ROOT OF VERTICAL STAB REF REO 670-55-31-0Sep 16, 2024 · N744EV · Cndair CL6002C10SDR VNAA20241014001Drag Angle · crackedCRACK ON DOUBLER OF LH 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 DOBLER OF LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67Sep 7, 2024 · N588NN · Bombdr CL6002D15SDR AALA202408283225Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES ON HINGE ARM 1 VERTICAL STABILIZER. REPLACED HINGE ARM #1 LOCATED AT VERTICAL STABILIZER AT RIB 2 AND ZONE Z325 PER EA 357125 PART A.Aug 27, 2024 · N926UW · Airbus A321231SDR AALA202411209537Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: #2 RUDDER HINGE ARM FITING FASTENER HOLES OUT OF ROUND ON VERTICAL STABILZER AT RIB 4. REPLACED HINGE ARM FITTING PER EA 357284.Aug 23, 2024 · N523UW · Airbus A321231SDR VNAA20240908009Hinge 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. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.Aug 20, 2024 · N549NN · Bombdr CL6002D15SDR YENA2024082601164Lug · corrodedDURING HEAVY MAINTENANCE: CORROSION ON BORE HINGE N3 OF VERTICLE STABILIZER; REF AEROMAN W.O. 2024 131/1 NR 2024-336938 REMOVED AND REPLACED HINGE FITTING #3 LOCATED ON VERTICLE STABILIZER I.A.W. SRM 51-72-11-911-001 & DRAWING #D 55371052 WORK ACCOMPLISHED BYAug 20, 2024 · N648JB · Airbus A320232SDR YENA2024082601163Lug · corrodedDURING HEAVY MAINTENANCE: CORROSION ON BORE HINGE FITTING #4 LOCATED ON VERTICLE STABILIZER; REFERNCE AEROMAN W.O. 2024 131/1 NR# 2024-336938 - REMOVED AND REPLACED HINGE FITTING # 3 LOCATED ON VERTICAL STABILIZER I. A.W A320 SRM 51-72-11- 911-001 AND DRAWING Aug 20, 2024 · N648JB · Airbus A320232SDR U2RA2024090800046Channel · crackedREF HAECO XMN (TX9Y778Y) NRC#: KUL8334, KUL8342 & KUL8375 - (2 EA.) P/N G12447-3-3-1882-3 AND (1 EA.) G12447-3-3-1882-4 GANG CHANNELS CRACKED COMMON TO THE VERTICAL STABILIZER AUXILIARY SPARAug 11, 2024 · N756CA · Boeing 747412SDR AALA202408139521Channel · noneAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER FORWARD SPAR J-CHANNEL HAS HAD THE INTERIM REPAIR PERFORMED PREVIOUSLY ON THE RIGHT HAND RELIEF CUTOUT PER AARD 55-30-09-3 REPAIR 3. COMPLETED PERMANENT REPAIR. PER AARD 55-30-09-3 REPAIR 3.Aug 9, 2024 · N950AN · Boeing 737823SDR YENA2024080601089Hinge Arm · damagedDURING HEAVY MAINTENANCE: REMOVAL OF VERTICAL STAB ARM OF HINGES FROM #1 THRU #7 TO PERFORM INSPECTION; REF AMERICANA WO# 131-2003 S/N 00579 FOR WORK PERFORMED. FITTING ASSEMBLY FORK END (BR2, BR 5 AND BR6) WERE REPLACED BY NEW FITTINGS IAW A320 SRM 55-36-42-3Aug 5, 2024 · N509JB · Airbus A320232SDR 2024FA0000566Attach Fitting · gougedWHILE ACCOMPLISHING FAA AD 2022-15-01, FOUND GOUGE ON HOLE #12Aug 5, 2024 · Boeing 78710SDR 2024FA0000565Attach Fitting · corrodedWHILE ACCOMPLISHING FAA AD 2022-15-01, FOUND CORROSION AT HOLE #12Aug 5, 2024 · Boeing 78710SDR 2024FA0000564Attach Fitting · corrodedWHILE ACCOMPLISHING FAA AD 2022-15-01, FOUND CORROSION ON HOLE #12Aug 5, 2024 · Boeing 78710SDR DALA2024080707845Hinge Arm · crackedSHIP 3275 DISC: AFTER REMOVED BEARING CRACK WAS FOUND ON HINGE ARM FITTING 3 ON VERTICAL STABILIZER. C/A: INSPECTION AS PER A320 SRM 55-36-42-300-008 STEP 2.A 1 (D) IS TO BE ACCOMPLISHED ON NRC 21/320 AND VERIFIED MEASURES HOLES ON HINGE IS 0.248IN TOOL SMALL Aug 2, 2024 · N375NC · Airbus A320212SDR IXXA2024073106Acoustic Panel · delaminatedVERTICAL STAB LEFT UPPER BONDED PANEL REQUIRES REPAIRJul 31, 2024 · N359AZ · Boeing 767323SDR UIEA2024072300734Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 185(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 185 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 REV 49 APJul 28, 2024 · N1361A · Boeing 76731BSDR UIEA2024072300735Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 169(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 169 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 PAG 6-7 RJul 28, 2024 · N1361A · Boeing 76731BSDR UIEA2024072400742Torque Box · delaminatedVERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN BETWEEN FSS 183.3 AND FSS 230.91.(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, PANEL SKIN BETWEEN FSS 183.3 AND AND FSS 230.91 WAS REPAIRED IAW TRE 6755078 REV 1 ISSUE DATE 18 JUL 2024, FJul 28, 2024 · N1361A · Boeing 76731BSDR SWIA20241009721Drag Angle · crackedRH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED AFT DRAG ANGLE IN THE RH VERTICAL ROOT REF REO 670-55-31-176 REV -- DATED 2024-08-01, CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARJul 21, 2024 · N752EV · Cndair CL6002C10SDR SWI2024F00956Drag Angle · crackedRH AFT DRAG ANGLE HAS POSSIBLE CRACK AT VERTICAL STABILIZER ROOT (MARKED). (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED AFT DRAG ANGLE IN THE RH VERTICAL ROOT REF REO 670-55-31-176 REV -- DATED 2024-08-01, CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARJul 21, 2024 · N752EV · Cndair CL6002C10SDR AALA202407221587Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER #3 RUDDER HINGE ARM UPPER AND LOWER FASTENER HOLE #1 ARE OBLONGED / WORN AT VERTICAL STABILIZER STATION 228 AND RIB 5. REPLACED HINGE ARM PER SRM 51-42-11 AND 55-36-42.Jul 20, 2024 · N521UW · Airbus A321231SDR AALA202407221958Hinge Arm · wornAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER #4 RUDDER HINGE ARM FASTENER HOLE #3 IS OBLONGED / WORN AT VERTICAL STABILIZER STATION 263 AND RIB 6. REPLACED HINGE ARM PER SRM 51-42-11 AND 55-36-42.Jul 20, 2024 · N521UW · Airbus A321231SDR SWAA2024072314265Hinge · wornL/H VERTICAL PANEL 324CL HINGE HAS SIGNS OF WEAR AND IS LOOSE.<[01] REMOVED AND REPLACED HINGE PIN IAW M/M 55-33-31Jul 17, 2024 · N8645A · Boeing 7378H4SDR DALA2024072907529Hinge Arm · crackedSHIP 3275 DISC: AFTER REMOVED BEARING CRACK WAS FOUND ON HINGE ARM FITTING 7 ON VERTI CAL STABILIZER. C/A: REPLACED HINGE ARM FITTING #7 AND FASTENERS ON VERTICAL STABILIZER AS PER A320 SRM 55-36-42-300-005, AS PER A320 SRM 55- 36-42-300-008 AND AS PER A320 SRJul 16, 2024 · N375NC · Airbus A320212SDR SWIA202408270714Drag Angle · crackedVERTICAL STABILIZER RIGHT SIDE DRAG ANGLE APPEARS CRACKED. HN00174404 (C-CHECK RO 8/27/2024) PERFORMED REPAIR AT VERTICAL STABILIZER RIGHT SIDE DRAG ANGLE CRJ900 SRM 55-31-00-201-001-A01COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND FORM M-337Jul 14, 2024 · N839SK · Cndair CL6002D24SDR IPXA2024081904062Panel · debondedDISBOND RH VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL DISBOND P/N: 186U1007-4 (SHEET METAL RMV AND REINSTALL PNL). REMOVED THE EXISTING FASTENERS I.A.W SRM 51-40-02-0G REV.101. ACCOMPLISHED JOB I.A.W SRM 51-40-02-0G REV.101 AND UPS EO-90959-REQ1 REV1.Jul 14, 2024 · N583UP · Boeing 7474R7FSDR IPXA2024081904632Panel · debondedDISBOND, LH VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL DISBOND P/N: 186U1006-3 (REPLACE). REMOVED THE EXISTING FASTENERS I.A.W SRM 51-40-02-0G REV.101. ACCOMPLISHED JOB I.A.W UPS EO-90958-REQ1 REV1.Jul 14, 2024 · N583UP · Boeing 7474R7FSDR ASAA2024070852150Hinge Fitting · damagedVERT STAB #BR4 HINGE FITTING FORK END HAS ELONGATED HOLES GROUNDED - YES. REMOVED AND REINSTALLED RUDDER PANELS 325CL AND 325CR IAW A320 AMM 55-33-13-410-002-A REV 11-01MAY-2024. REMOVED AND REPLACED BR4 HINGE AMM P/N D5537131420054 P/O 1095868.1 IAW EA #A320-Jul 8, 2024 · N846VA · Airbus A320214SDR VNAA202408090026Hinge · wornFREE 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.B.Jul 4, 2024 · N580NN · Cndair CL6002D24SDR 2024FA0000529Structure · degradedVERTICAL FIN HOLE AT BOLT #15 FOUND WITH PRIMER DEGRADATION DURING INSPECTION PER SI IB78J550001.Jul 1, 2024 · Boeing 78710SDR 2024FA0000528Structure · degradedVERTICAL FIN HOLE AT BOLT #15 FOUND WITH PRIMER DEGRADATION DURING INSPECTION PER SI IB78J550001.Jul 1, 2024 · Boeing 78710SDR 2024FA0000527Structure · degradedVERTICAL FIN BOLT HOLE #13 FOUND WITH PRIMER DEGRADATION DURING INSPECTION PER IB78J550001Jul 1, 2024 · Boeing 78710SDR ASAA2024062452148Hinge Arm · damagedVERT STAB #BR1 HINGE FITTING FORK END HAS ELONGATED HOLE GROUNDED - YES. REMOVED AND REINSTALLED VERTICAL STAB PANEL 325BR IAW A320 AMM 55-33-13-410-002-A REV 11-01MAY2024. REMOVED AND REPLACED BR1 HINGE FITTING P/N D553712100200 P/O #0 IAW EA#A320-55EA-02221 Jun 24, 2024 · N846VA · Airbus A320214SDR VNAA20240723018Hinge Fitting · excess playINITIAL INSPECTION: FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO, 2 AND NO, 3 WERE REPLACED PER RIL #2103 REV. B.Jun 21, 2024 · N585NN · Bombdr CL6002D15SDR SWI202408230729Drag Angle · crackedVERTICAL STABILIZER RH AFT DRAG ANGLE AT STABILIZER ROOT HAVE SMOKING RIVETS AND POSSIBLE CRACKS (C-CHECK RO 8/22/2024) COMPLIED WITH VERTICAL STAB RH AFT DRAG ANGLE REPAIR REF CRJ700 SRM 55-31-00-201-001-A01COMPLIED WITH TASK 51-900-1002-SKYJun 17, 2024 · N758SK · Cndair CL6002C10SDR SWI202408230728Drag Angle · crackedVERTICAL STABILIZER RH FWD DRAG ANGLE AT STABILIZER ROOT HAVE SMOKING RIVETS AND POSSIBLE CRACKS (C-CHECK RO 8/22/2024) VERTICAL STABILIZER R/H FWD DRAG ANGLE REPAIRED REF. CRJ-700 SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-10Jun 17, 2024 · N758SK · Cndair CL6002C10
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