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.
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
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 VNAA2024072300Drag Angle · crackedINITIAL INSPECTION: CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 20.0% FRNT SPAR DATUM TO STGR DATUM TO 25.93% STGR DATUM. FWD DRAG ANGLE BTW 20.0% FRONT SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT WAS REPAIRED PER SDR UIEA2024052800465Angle · wornEMPENNAGE VERTICAL FIN TO BODY INTERFACE LEFT CLOSURE ANGLE WORN FROM STA 1088 TO STA 1138.(<P>REPLACED LEFT CLOSURE ANGLE P/N: 148A8310-3 ATTACHED WITH SOLID RIVETS AND HI-LOKS IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9, 51-40-02-0G-0 PARAG 4B AND 51-40-02-0GSDR VNAA202407030007Hinge · 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 FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.SDR SWAA2024060491007Hinge · crackedWHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN LOWER RUDDER TRAILING EDGE HINGE PN175A1207-4 REF IPC 55-40-51 FIG ITEM 1 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROLSDR SWAA2024060491009Hinge · crackedWHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN UPPER RUDDER TRAILING EDGE HINGE PN175A1210-5 REF IPC 55-40-51 FIG ITEM 1 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROLSDR AALA202405209729Channel · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL IS CRACKED AT THE LEFT HAND RELIEF CUTOUT ABOVE THE LEFT HAND FRONT SPAR FITTING. REMOVED CRACK. PER AARD 55-30-09-3 REPAIR 3.SDR VNAA20240619011Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR REXA2024052800405Drag Angle · crackedVERTICAL STAB., R/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.SDR REXA2024052800403Drag Angle · crackedVERTICAL STAB., L/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.SDR VNAA20240523009Hinge 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. BSDR VNAA20240531015Hinge Fitting · 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 VERTIC•A L STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103. REV.B.SDR GTIA2024042938094Hinge Arm · damagedREF SPIRIT W/O 293812 T/C 553006-01-2-NKS. ELONGATED HOLE HINGE ARM 7 ON VERTICAL STABILIZER. REF-01 3316184-02 GENERATED. SDR GENERATED.-REPLACED HINGE ARM # 7 AS PER EA#55-0096-24 AND SRM A320 55-36-42-300-003. THIS REPAIR IS CATEGORY A.SDR REXA2024100700851Drag Angle · crackedR/H AFT DRAG ANGLE IS CRACKED. REMOVED CRACKED RH AFT DRAG ANGLE AND INSTALLED NEW AFT DRAG ANGLE P/N: AV670-21186-004 IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01SDR SWAA2024051474620Bracket · crackedCRACK EXTERNAL SKIN SUPPORT BRACKET LOCATED BS1016 AT LEVEL STR3L TO STR3R AT VERTICAL STABILIZER 2024-259139<[01] REPLACED SUPPORT BRACKET AND FASTENERS I.A.W. B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02; DRAWING# 176A3101 SHEET 4 REV: - AND DWG#SDR YENA2024041600528Fitting · brokenDURING HEAVY MAINTENANCE: STABILIZER/VERTICAL STAB/ BROKEN FITTING HOIST POINT ON AREA OF ACCESS PANEL # 325EL ON VERTICAL STABILIZER. (CONSIDERED A MAJOR REPAIR)SDR UIEA2024032200186Rivet · damagedV/STAB L/H AUX SPAR TO FRONT SPAR PNL SURFACE FND 1EA BURN MARK RIVET (STA 245 FRONT SPAR RIVET)(<P>BURN MARK RIVET REPLACED AS PER RI-55-30-16816 REV A. NO FURTHER DEFECTS NOTED</P>)SDR REXA2024071600544Drag Angle · crackedL/H AFT VERTICAL STAB DRAG ANGLE IS CRACKED. REMOVED CRACKED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01. INSTALLED NEW AFT DRAG ANGLE P/N: AV670-21186-003, ATTACHED WITH FASTENERS TO VERTICAL FLANGESDR VNAA20240426008Drag 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). (SM) . LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TSDR REXA2024080500609Drag Angle · crackedRH FWD VERTICAL DRAG ANGLE HAS A POSSIBLE CRACK. REPAIRED RH FWD VERTICAL DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01.SDR REXA2024061400434Drag Angle · crackedRH AFT VERTICAL DRAG ANGLE HAS A POSSIBLE CRACK. INSTALLED RH AFT DRAG ANGLE (PN:AV670-21186-004) IAW CRJ 900 SRM 51-42-22-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01.SDR REXA2024061400433Drag Angle · crackedLH FWD VERTICAL DRAG HAS A POSSIBLE CRACK REPAIRED LH FWD DRAG ANGLE IAW CRJ-900 SRM 55-31-00-201-001-A01.SDR DALA2025070805079Tape · peelingON WALK AROUND FOUND VERT STAB EROSION TAPE PEELED. GVI OF PAINT OK. FWD TO MON IAW A220 ASRP 55-32-01-01AAA-662A-A FOR 8500 FLT HRS. GVI DUE IN 850 FLT HRS. PERFORMED GVI IAW A220 ASRP 51-10-01-01AAA- 018A-A. NO FURTHER DEFECTS FOUND. OK TO CONT. ON MON.REMOVSDR YENA2024030500314Hinge Arm · not reportedDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR1/ PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2024030500313Hinge Arm · not reportedDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR3/ PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR VNAA202404090009Hinge Fitting · 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. BSDR SWIA202404290227Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 4/26/2024) PERFORMED LH VERTICAL STAB FWD DRAG ANGLE REPAIR. PER CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR VNA2024F00004Drag 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. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE SDR VNA2024F00003Drag 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). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATSDR VNAA2024021100017Drag Angle · crackedVERTICAL STABILIZER, L/H AFT DRAG ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE L/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01SDR SWIA202403250263Drag Angle · crackedRH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IS CRACKED (MARKED) CAMP # 27802535 (C-CHECK RO 3/23/2024) REPAIRED R/H AFT ANGLE ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT REF CRJ 700 SRM 55-31-00-201-001-A01. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COSDR VNAA202402050018Hinge Fitting · excess playAFTER RUDDER REMOVAL, 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 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL 2103 REVSDR SWI202403250260Drag Angle · crackedRH VERTICAL STAB TO FUSELAGE DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 3/23/2024) REPAIRED RH VERTICAL STAB TO FUSELAGE DRAG ANGLEREF CRJ 700 SRM 55-31-00-201-001-A01.COMPLIED WITH 51-900-1002-SKYSDR VNAA20240214002Hinge 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. BSDR VNAA20240212001Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900SDR VNAA202402280005Drag 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). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-2SDR VNAA202402280004Drag 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). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-SDR SWIA2024021900110Drag Angle · crackedVERTICAL STABILIZER LH FWD DRAG ANGLE IS CRACKED (HN00132661) (C-CHECK RO 2/18/2024) REMOVED & REPLACED VERTICAL STABILIZER LH FWD DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH SKY WEST TC 51-900-1002-SKY.SDR IPXA2024010926312Unknown · unknown*SDR FILED OPEN* DAMAGE FOUND ON RH SIDE OF VERTICAL STAB TO THE RIGHT OF THE UPS SHIELD.***SM EVAL REQ*** DEFERRED IAW EO-89123-REQ1SDR SWI202403110198Drag Angle · crackedCRACK NOTED ON VERTICAL STAB L/H FWD DRAG ANGLE (MARKED) (C-CHECK RO 3/10/2024) REPAIRED VERTICAL STAB LH FWD DRAG ANGLE REF CRJ700SRM 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.SDR JJBA20240104001Unknown · unknownBOTTOM OF VERT STAB REAR OF SPAR 3, LH SKIN PROFILE CHANNEL CRACKED. REPLACED WITH NEW ONESDR SWI2024F00167Drag Angle · crackedVERTICAL STAB. LH AFT DRAG ANGLE HAS A POSSIBLE CRACK. (C-CHECK RO 2/18/2024) REMOVED VERTICAL STAB. LH AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01 AND INSTALLED NEW LH AFT DRAG ANSDR AALA202404116813Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON VERTICAL STABILIZER ATTACH FITTING FOR RUDDER ACTUATOR #2 BETWEEN VERTICAL STABILZER STATIONS 228 AND 263, BETWEEN VERTICAL STABILIZER RIBS 5 AND 6. REPAIRED FITTING PER EA 352554.SDR REXA2022122601053Angle · crackedLH FWD DRAG ANGLE ON VERTICAL STABILIZER IS CRACKED. PERFORMED PERMANENT REPAIR OF LH FWD DRAG ANGLE ON VERTICAL STAB IAW CRJ900 SRM TASK 55-31-00-201-001-A01.SDR GTIA2023120137660Access Panel · crackedDURING ACCOMPLISHMENT OF JOB CARD OP-Z 300 NKS. FOUND CRACK ON ACCESS PANEL 323AL VERTICAL STABILIZER. DAMAGE MEASUREMENT; LENGTH 0.90IN, WIDTH 0.60IN, DEPTH ALL PLIES. RAF-01 3256923-02 GENERATED.-REPAIRED ACCESS PANEL 323AL VERTICAL STABILIZER IAW EA # 55-04SDR SWAA2023122124927Seal · crackedVERTICAL FIN R/H HORIZONTAL BOX HINGE CUTOUT UPPER SLIDING SEAL FWD GUIDE TRACK TIP CRACKED<[01] REMOVE AND REPLACE TRACK ASSY REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR VNAA202401040020Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUSDR DALA2023112709723Unknown · unknownCORROSION ON VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN. SUMMARY OF NRC 00230: CORROSION LEVEL 2. VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G. (LP #0080112)SDR SWAA2023120719505Angle · crackedCRACK ANGLE BS 1016 BETWEEN STRINGER 2L AND STRINGER 2R AT VERTICAL STABILIZER 2023-682308<[01] REPLACED ANGLE LOC.ON BS 1016 BETWEEN STRINGER 2L AND STRINGER 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 ; 51-10-02 AND DWG 176A3101 SHEET 4 REV -.SEE INDSDR KCSA202311081134Web · damagedDAMAGE FOUND AROUND LIGHTENING HOLE ON VERTICAL STAB L/E AT APPROX STA 220SDR REXA2024021500188Angle · crackedL/H VERTICAL STAB, AFT DRAG ANGLE APPEARS TO BE CRACKED IN FWD RADIUS. PERFORMED HFEC OF LH VSTAB AFT DRAG ANGLE SUSPECTED CRACK AREA IAW CRJ 900 NDTM PART 1 51-20-006-250-A01 REV 36 DATED 2/8/22. FOUND 1 INDICATION 0.5"" LONG, 100% FSH, MARKED ON PART. FA
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