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 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 Jun 16, 2024 · N585NN · Bombdr CL6002D15SDR 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 51-40-02-0GJun 3, 2024 · N5233A · Boeing 7378SDR 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.May 31, 2024 · N583NN · Cndair CL6002D24SDR 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 CONTROLMay 29, 2024 · N8825Q · Boeing 7378SDR 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 CONTROLMay 29, 2024 · N8825Q · Boeing 7378SDR 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.May 19, 2024 · N944AN · Boeing 737823SDR 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-A01May 14, 2024 · N582NN · Bombdr CL6002D15SDR REXA2024052800405Drag Angle · crackedVERTICAL STAB., R/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.May 14, 2024 · N582CA · Cndair CL6002D24SDR REXA2024052800403Drag Angle · crackedVERTICAL STAB., L/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.May 13, 2024 · N582CA · Cndair CL6002D24SDR 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. BMay 13, 2024 · N576NN · Bombdr CL6002D15SDR 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.Apr 29, 2024 · N567NN · Cndair CL6002D24SDR 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.Apr 25, 2024 · N615NK · Airbus A320232SDR 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-A01Apr 18, 2024 · N300PQ · Cndair CL6002D24SDR 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#Apr 14, 2024 · N7736A · Boeing 7377BDSDR YENA2024041600528Fitting · brokenDURING HEAVY MAINTENANCE: STABILIZER/VERTICAL STAB/ BROKEN FITTING HOIST POINT ON AREA OF ACCESS PANEL # 325EL ON VERTICAL STABILIZER. (CONSIDERED A MAJOR REPAIR)Apr 11, 2024 · N249JB · Emb ERJ190100IGWSDR 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>)Apr 9, 2024 · N496MC · Boeing 74747UFSDR 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 FLANGEMar 29, 2024 · N300PQ · Cndair CL6002D24SDR 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 (TMar 20, 2024 · N572NN · Bombdr CL6002D15SDR 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.Mar 11, 2024 · N181GJ · Cndair CL6002D24SDR 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.Mar 11, 2024 · N181GJ · Cndair CL6002D24SDR 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.Mar 11, 2024 · N181GJ · Cndair CL6002D24SDR 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.REMOVMar 10, 2024 · N127DU · Airbus BD5001A10SDR YENA2024030500314Hinge Arm · not reportedDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR1/ PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Mar 4, 2024 · N643JB · Airbus A320232SDR YENA2024030500313Hinge Arm · not reportedDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR3/ PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Mar 4, 2024 · N643JB · Airbus A320232SDR 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. BMar 3, 2024 · N577NN · Cndair CL6002D24SDR 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.Feb 27, 2024 · N752SK · Cndair CL6002C10SDR 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 Feb 15, 2024 · N573NN · Bombdr CL6002D15SDR 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 ATFeb 15, 2024 · N573NN · Bombdr CL6002D15SDR 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-A01Feb 11, 2024 · N563NN · Cndair CL6002D24SDR 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 COFeb 10, 2024 · N744SK · Cndair CL6002C10SDR 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 REVFeb 6, 2024 · N567NN · Cndair CL6002D24SDR 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-SKYJan 31, 2024 · N744SK · Cndair CL6002C10SDR 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. BJan 28, 2024 · N565NN · Cndair CL6002D24SDR 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-900Jan 28, 2024 · N565NN · Cndair CL6002D24SDR 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 55-31-00-2Jan 20, 2024 · N566NN · Bombdr CL6002D15SDR 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-Jan 20, 2024 · N566NN · Bombdr CL6002D15SDR 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.Jan 10, 2024 · N748SK · Cndair CL6002C10SDR 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-REQ1Jan 8, 2024 · N611UP · Boeing 7478FSDR 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.Jan 5, 2024 · N740EV · Cndair CL6002C10SDR JJBA20240104001Unknown · unknownBOTTOM OF VERT STAB REAR OF SPAR 3, LH SKIN PROFILE CHANNEL CRACKED. REPLACED WITH NEW ONEDec 21, 2023 · N11191 · Emb EMB145XRSDR 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 ANDec 20, 2023 · N748SK · Cndair CL6002C10SDR 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.Dec 12, 2023 · N747UW · Airbus A319112SDR 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.Dec 3, 2023 · N298PQ · Cndair CL6002D24SDR 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 # 55-04Nov 28, 2023 · N682NK · Airbus A321231SDR 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 1Nov 26, 2023 · N7881A · Boeing 7377CTSDR 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 DATUNov 24, 2023 · Bombdr CL6002D15SDR 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)Nov 24, 2023 · N937AT · Boeing 717200SDR 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 INDNov 8, 2023 · N7846A · Boeing 73776NSDR KCSA202311081134Web · damagedDAMAGE FOUND AROUND LIGHTENING HOLE ON VERTICAL STAB L/E AT APPROX STA 220Nov 8, 2023 · N745CK · Boeing 747446SDR 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. FANov 7, 2023 · N606LR · Cndair CL6002D24
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