JASC 5534

Service difficulty reports · 820

Reports filed under 5534 · Vertical Stabilizer Miscellaneous Structure, 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 = '5534'
  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 YENA2024071601020Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 4 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00036) REMOVED AND REPLACED HINGE FITTING #4 ON VERTICAL STABILIZER IAW A320 SRM 51-72-11-911-001 AND DRAWING #D 55371052 ISSUE E. Jul 12, 2024 · N709JB · Airbus A320232SDR VNAA202409010001Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WERE RJun 30, 2024 · N547NN · Cndair CL6002D24SDR VNAA202408080002Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01Jun 30, 2024 · N580NN · Cndair CL6002D24SDR VNAA202408080001Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM . CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WERE Jun 30, 2024 · N580NN · Cndair CL6002D24SDR DALA2024062706550Skate Angle · cracked(LOG 0414574) RIGHT HAND SIDE VERT STAB SKATE ANGLE IS CRACKED AT STA 1016 WL 305. REMOVED DAMAGED R/H FWD SKATE ANGLE BS 1005-1016 WL 305 AND INSTALLED REPLACEMENT SKATE ANGLE PER B737-800 SRM 51-40-02 REF BOEING DWG# 147A0030.Jun 25, 2024 · N394DA · Boeing 737832SDR HNAA2024071900566Bracket · cracked55-2317 TOP OF VTR STAB AFT OF SPAR3, BRACKET FOR 321BL IS CRACKED. RAR BRACKET IAW SRM51-40-02Jun 21, 2024 · N662EH · Emb EMB145LRSDR JGVR20240606001Angle · corrodedMECHANICALLY REMOVED 4 AREAS OF CORROSION ON LH SIDE OF RUDDER COVE ON VERTICAL STAB SPAR CLIP AND 1 AREA OF CORROSION EXTENDING UNDERNEATH CROSS BRACKET SUPPORT LH SIDE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIREDJun 6, 2024 · N357QS · Cessna 680CESDR VNAA202407090002Drag Angle · crackedCRACK 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) REPAIRED PER CRJ 900 SRM 55-31-00-201-001-A01May 30, 2024 · N584NN · Cndair CL6002D24SDR VNAA202407090001Drag Angle · 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) REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01May 30, 2024 · N584NN · Cndair CL6002D24SDR VNAA202407020011Drag Angle · crackedCRACK 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 DATMay 29, 2024 · N583NN · Cndair CL6002D24SDR VNAA202407020010Drag Angle · 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 May 29, 2024 · N583NN · Cndair CL6002D24SDR IPXA2024061281765Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: L/H T-CHORD VERTICAL STA. 1220 UNDER PANEL 195CL HAS CORROSION. DOT 33-009 INSTALLED TCHORD ON STA 1220 LH VERTICAL, IAW SRM 51-40-02-0G.May 21, 2024 · N422UP · Boeing 75724APFSDR VNAA202407110018Hinge Fitting · wornAFTER 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.May 14, 2024 · N584NN · Cndair CL6002D24SDR VNAA20240619010Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01May 14, 2024 · N582NN · Bombdr CL6002D15SDR VNAA20240618010Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.May 14, 2024 · N582NN · Bombdr CL6002D15SDR DALA2024050704999Web · crackedSHIP 1815 FOUND OUT VERTICAL STABILIZER LE WEB CRACKED AT FSS109. CORRECTIVE ACTION: THE CRACKED WEB AT VERTICAL STABILIZER L/E AT FSS109 REPAIRED AS PER PRI 617724-14 REV 0.COMPARED AND COMPLIED WITH ER/A 617724- 14 REV ORIGINAL. NO DEVIATION. (0328449)May 6, 2024 · N839MH · Boeing 767432ERSDR SWAA2024053079390Angle · crackedCRACK ANGLE LOCATED STA 1016 AT VERTICAL STABILIZER 2024-270178<[01] REPLACED ANGLE LOCATED STA 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING # 176A3001;REV D.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMEDApr 25, 2024 · N470WN · Boeing 7377H4SDR VNAA20240524009Stiffener · damagedBULLET FAIRING STIFFENER, LHS WITHIN 1100 FH, REPAIR OR REPLACE DISCREPANT PART PER APPROVED PROCEDURES. NEW BULLET FAIRING STIFFENER WITH P/N AV670-21650-005 IT WAS VERIFIED PER CRJ-900 IPC 55-32-86.Apr 22, 2024 · N576NN · Bombdr CL6002D15SDR SWIA20240421Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE, POSSIBLE CRACKED (MARKED) (C-CHECK RO 7/9/2024) REPAIRED L/H V-STAB AFT DRAG ANGLE PER CRJ900SRM 55-31-00-201-001-A01 AND REO 690-55-31-085 REV -- DATE 2024-06-04. COMPLIED WITH SKYWEST TASK CARD 51-900-1002Apr 21, 2024 · N679CA · Cndair CL6002D24SDR YENA2024041600578Hinge Arm · unknownDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR1/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR YENA2024041600569Arm · unknownDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR3/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR SWI20240712000578Drag Angle · crackedRH AFT FUSELAGE TO VERTICAL STABILIZER AFT DRAG ANGLE CRACKED (C-CHECK RO 7/12/2024) REPAIRED DAMAGE ON RH AFT FUSELAGE TO VERTICAL STABILIZER AFT DRAG ANGLE IAW REO 607-55-31-018 REV-A DATE: 2016-11-10, REO 607-55-31-172 REV-- DATE:2024-05-09, CRJ700 SApr 4, 2024 · N762SK · Cndair CL6002C10SDR SWIA2024071200404Drag Angle · crackedLH AFT FUSELAGE TO VERTICAL STABILIZER FWD AND AFT DRAG ANGLES CRACKED (C-CHECK RO 7/12/2024) REPAIRED DAMAGE ON LH AFT FUSELAGE TO VERTICAL STABILIZER FWD AND AFT DRAG ANGLES IAW REO 607-55-31-018 REV-A DATE:2016-11-10, REO 607-55-31-172 REV-- DATE:202Apr 4, 2024 · N762SK · Cndair CL6002C10SDR LR7A2024032803383Stiffener · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING ST-5, FOUND LH V-STAB STIFFENER CRACKED AT FS1109.5, LBL10.5, VSS74. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-20. NR# 1001086298 / PSE# 55-10-03, AD 2012-06-09Mar 28, 2024 · N408LC · Lkheed 382GSDR VNAA20240425009Hinge 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. BMar 26, 2024 · N572NN · Bombdr CL6002D15SDR SWAA2024042667077Angle · crackedCRACK ANGLE LOCATED BS1016 BETWEEN STR3L TO STR3R AT VERTICAL STABILIZER 2024-195913<[01] REPLACED ANGLE LOCATED BS1016 BETWEEN STR3L TO STR3R AT VERTICAL STABILIZER I.A.W. B737-700 SRM 51-40-02 AND DRAWING # 176A7101 REV ? AND DRAWING 176A3001 REV ?D? SEE INDMar 23, 2024 · N468WN · Boeing 7377H4SDR DALA2024031103196Bearing · corrodedSHIP 3139 CORROSION BEARING RUDDER HINGE 6 ON VERTICAL STABILIZER (1 EA). CORRECTIVE ACTION: REMOVED AND REPLACED HINGE BEARING #6 ON RUDDER AS PER A320FAM AMM 55-46-11-000-001-A AND AMM 55-46-11-400-001-A. (0237735)Mar 9, 2024 · N339NB · Airbus A319114SDR REXA2024102801051Drag Angle · crackedL/H AFT DRAG ANGLE IS CRACKED. REMOVED AND INSTALLED L/H AFT DRAG ANGLE WITH P/N AV670-21186-003 IAW CRJ-900 SRM 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01.Feb 9, 2024 · N305PQ · Cndair CL6002D24SDR REXA2024102801045Drag Angle · crackedR/H AFT DRAG ANGLE IS CRACKED. REMOVED AND REPLACED RH AFT VERTICAL STAB DRAG ANGLE PN: AV670-21186-004 IAW CRJ900 SRM TASKS 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND 51-23-00-001-001-A01.Feb 7, 2024 · N305PQ · Cndair CL6002D24SDR REXA2024102200920Drag Angle · crackedRH AFT VERTICAL STAB DRAG ANGLE IS CRACKED RH AFT VERTICAL STAB DRAG ANGLE REQUIRE REPLACEMENT, REMOVED DAMAGE RH AFT VERTICAL STAB DRAG ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-21-001-001-A01 , AND SRM 51-42-22-001-001-A01. INSTALLED REPLACEMENT Jan 22, 2024 · N490PX · Cndair CL6002D24SDR REXA2024102901152Drag Angle · crackedRH FWD VERTICAL STAB DRAG ANGLE IS CRACKED COMPLIED WITH REPAIR OF RH FWD DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01Jan 17, 2024 · N299PQ · Cndair CL6002D24SDR REXA2024102901151Drag Angle · crackedLH AFT VERTICAL STAB DRAG ANGLE IS CRACKED INSTALLED SERVICEABLE DRAG ANGLE AFT, LH SIDE WITH PN AV670-21186-003 IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.Jan 17, 2024 · N299PQ · Cndair CL6002D24SDR REXA2024102901150Drag Angle · crackedLH FWD VERTICAL STAB DRAG ANGLE IS CRACKED COMPLIED WITH REPAIR OF LH FWD DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01Jan 17, 2024 · N299PQ · Cndair CL6002D24SDR REXA2024012500122Angle · crackedRH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. REPLACED RH AFT DRAG ANGLE USING P/N AV670-21186-004 IAW CRJ 900 SRM 51-42-13-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-22-001-001-A01.Jan 16, 2024 · N299PQ · Cndair CL6002D24SDR REXA2024102901140Drag Angle · crackedLH AFT DRAG ANGLE ON VERTICAL STABILIZER IS CRACKED. : REMOVED LH AFT DRAG ANGLE FROM VERTICAL STABILIZER IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, & 51-42-22-001-001-A01. AND FIT, DRILLED AND TRANSFERED HOLES INTO NEW ANGLE IAW CRJ900 SRM 51-Dec 3, 2023 · N298PQ · Cndair CL6002D24SDR VNAA202310260009Drag Angle · crackedDAMAGE DESCRIPTION: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 6Sep 6, 2023 · N611NN · Cndair CL6002D24SDR VNAA202310260008Drag Angle · crackedDAMAGE DESCRIPTION: CRACK 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 67Jun 30, 2023 · N611NN · Cndair CL6002D24SDR SWAA2023070360058Balance Weight · erodedVERTICAL STAB. T/E RUDDER BALANCE WEIGHT AT CENTER POSITION HAS SEVERAL EROSION. VERTICAL STAB. T/E RUDDER BALANCE WEIGHT AT CENTER POSITION HAS SEVERAL CORROSION.<[01] REMOVED RUDDER BALANCE WEIGHT IN REFERENCE CMM 55-40-09. AND INSTALLED RUDDER BALANCE WEIGHJun 10, 2023 · N942WN · Boeing 7377H4SDR SWAA2023071166328Fitting · corrodedCORROSION TRAILING EDGE FITTING LOC BTW FIN STA 132.2 AT FIN STA 150.6 AT VERTICAL STABILIZER 2023-365589<[01] REPLACED HOUSING ASSY -BEARING OF STANDBY RUDDER POWER CONTROL UNIT IAW B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801.SEE INDIVIDUAL SIGN OFF BJun 7, 2023 · N7827A · Boeing 73779PSDR SWAA2023061650318Ventral Fin · exposedVERTICAL FIN L/E LOWER SIDE COMPOSITE EXPOSED.<[01] REPAIRED (COMPOSITE EXPOSED) ON VERTICAL FIN AS PER B737 SRM 51-70-04-2R-10; MATERIAL USED RESIN PO# 1800550 AND CLOTH PO#1738579.;[02] VERIFIED STEP 1. COMPLETEMay 10, 2023 · N437WN · Boeing 7377H4SDR SWAA2023060545706Angle · crackedCRACK BRACKET ANGLE LOC BS 1016 AT VERTICAL STABILIZER 2023-299393<[01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 1016 AT VERTICAL STABILIZER I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9; B737-700 SRM 51-40-02 AND DRAWING #176A3101; SHEET 4; REV -.<BR>SEE INDIVIDUALMay 4, 2023 · N283WN · Boeing 7377H4SDR SWAA2023031502258Angle · crackedCRACK LEADING EDGE ANGLE LOC STA 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2023-119388<[01] REPLACED ANGLE LOC STA 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 176A3101 SHEET 4 REV -.<BR>SEE INDIVIDUAL SIGNS-OFF BELFeb 12, 2023 · N7745A · Boeing 7377BDSDR SWAA2023021089336Fitting · corrodedCORROSION ON DRAG BRACE FITTING RT AFT SPAR FWD OUTBOARD POSITION ON VERTICAL STABILIZER 2022-708741<[01] REPLACED DRAG BRACE FITTING RT AFT SPAR FWD OUTBOARD POSITION ON VERTICAL STABILIZER IAW SRM B737-700 51-40-02; SRM B737-700 51-10-02 PARAGRAPH 9 AND DRAWJan 7, 2023 · N7748A · Boeing 7377BDSDR SWAA2022101247432Angle · crackedCRACK LEADING EDGE ANGLE LOC. BS 1016 AND BTW STR2L TO STR2R AT VERTICAL STABILIZER 2022-533290 / [01] REPLACED NEW LEADING EDGE ANGLE (SPRING ) LOC. BS 1016 AND BTW STR2L TO STR2R AT VERTICAL STABILIZER AND STRAP 2E/A I.A.W.B737-700 SRM 51-40-02 176A3101 REV?Sep 22, 2022 · N7813P · Boeing 7377K9SDR SWAA2022092145387Fitting · corrodedCORROSION REAR SPAR ON BORE BOTTOM AREA OF FWD INBOARD SPAR BOLT FITTING RH AT VERTICAL STABILIZER 2022-452018 / [01] REPLACED DRAG BRACE FITTING LOCATED AT LEVEL OF STR 2R BTW BS 1064 TO BS 1088 AT REAR SPAR FWD INBOARD POSITION AT VERTICAL STABILIZER IAW B73Aug 25, 2022 · N7852A · Boeing 737SDR SWAA2022092145386Fitting · corrodedCORROSION REAR SPAR ON BORE UPPER AREA OF AFT OUTBOARD SPAR BOLT FITTING RH AT VERTICAL STABILIZER 2022-452019 / [01] REPLACED REAR SPAR AFT OUTBOARD DRAG BRACE FITTING RH AT VERTICAL STABILIZER LOCATED BTW BS 1088.2 TO BS 1104.0 AT LEVEL OF STR 2R IAW B737-70Aug 25, 2022 · N7852A · Boeing 737SDR SWAA2022083138735Angle · crackedCRACK LEADING EDGE ANGLE LOC. BS 1080 AND BTW STR 2L TO STGR 2R AT VERTICAL STABILIZER 2022-418414 / [01] REPLACED ANGLE LOC. BS1080 AND BTW STR2L TO STR2R AT VERTCAL SYTABILIZER I.A.W. DWG 176A3001 REV. D AND SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAug 4, 2022 · N497WN · Boeing 7377H4SDR SWAA2022080125469Bracket · crackedCRACK ACCESS PANEL 324AL BRACKET VERTICAL STABILIZER 2022-372898 / [01] REPLACED BRACKET ON ACCESS PANEL 324AL VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 AND 51-40-02;[02] TASK CARD COMPLETEDJul 3, 2022 · N494WN · Boeing 7377H4SDR SWAA2022071115594Bracket · corrodedCORROSION DORSAL FIN DRAG BRACE LT SIDE AT VERTICAL STABILIZER (1 EA) 2022 307311 / [01] REPLACED DORSAL FIN DRAG BRACE LT SIDE AT VERTICAL STABILIZER IAW. SRM B 737 -700 51-40-02; 51-10-02 ITEM 9 AND DWG #148A8200 REV B SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPJun 6, 2022 · N257WN · Boeing 7377H4SDR SWAA2022071113840Bracket · crackedCRACK BRACKET ANGLE LOCATED BS 1016 INTERNAL AREA AT VERTICAL STABILIZER 2022-305624 / [01] REPLACED BRACKET ANGLE LOCATED BS 1016 INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 176A3001-9; SH: 23; REV: D; AND DWG#May 31, 2022 · N482WN · Boeing 7377H4
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