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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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. SDR 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 RSDR 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-A01SDR 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 SDR 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.SDR HNAA2024071900566Bracket · cracked55-2317 TOP OF VTR STAB AFT OF SPAR3, BRACKET FOR 321BL IS CRACKED. RAR BRACKET IAW SRM51-40-02SDR 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 REQUIREDSDR 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-A01SDR 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-A01SDR 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 DATSDR 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 SDR 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.SDR 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.SDR 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-A01SDR 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.SDR 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)SDR 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 PERFORMEDSDR 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.SDR 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 51-900-1002SDR YENA2024041600578Hinge Arm · unknownDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR1/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR YENA2024041600569Arm · unknownDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR3/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR 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 SSDR 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:202SDR 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 2012-06-09SDR 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. BSDR 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 INDSDR 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)SDR 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.SDR 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.SDR 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 SDR 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-A01SDR 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.SDR 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-A01SDR 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.SDR 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-SDR 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 6SDR 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 67SDR 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 WEIGHSDR 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 BSDR 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. COMPLETESDR 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 INDIVIDUALSDR 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 BELSDR 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 DRAWSDR 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?SDR 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 B73SDR 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 B737-70SDR 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 INDIVIDUSDR 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 COMPLETEDSDR 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] REPSDR 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#
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