JASC 5533

Service difficulty reports · 77

Reports filed under 5533 · Ventral 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 = '5533'
  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 JGVR20260111001Hinge Bracket · corrodedREMOVED THE VERTICAL STABILIZER UPPER RUDDER HINGE LOWER BRACKET DUE TO CORROSION AND REPLACED WITH NEW TEXTRON P/N 6931050-59.Jan 11, 2026 · N396QS · Cessna 680CESDR SWIA2024031100105Drag Angle · crackedCRACK NOTED ON L/H AFT VERTICAL STAB DRAG ANGLE (MARKED) (C-CHECK RO 3/10/2024) REPAIRED VERTICAL STAB LH AFT DRAG ANGLE REF CRJ700SRM 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.Jan 5, 2024 · N740EV · Cndair CL6002C10SDR SWAA2023082382523Angle · crackedCRACK ANGLE LOCATED AT LEVEL BS1016 AT VERTICAL STABILIZER 2023-461410<[01] REPLACED ANGLE AND FASTENERS LOC BS 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 176A3100 SHEET 4 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEJul 26, 2023 · N7843A · Boeing 737752SDR IXXA2023041101Skin · delaminatedL/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATIONApr 11, 2023 · N347AZ · Boeing 767300SDR IXXA202304110001Skin · delaminatedL/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATIONApr 9, 2023 · N347AZ · Boeing 767300SDR SWAA2023041920586Panel · elongatedLEFT VERTICAL STABILIZER ACCESS PANEL # 322A HAS 2 EA ELONGATED FASTENER HOLES<[01] RECEIVED; LOCATED AND DRILLED NEW L/E PANEL (322A) AT VERTICAL STABILIZER PER B737-700 PER SRM 51-40-05-0G-0.;[02] VERIFIED ALL STEPSMar 24, 2023 · N435WN · Boeing 7377H4SDR SWAA2022100694979None · crackedCRACK ACCESS PANEL 321A RIB 8 ON INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER 2022-466985 / [01] REPLACED RIB 8 LOC ACCES PANEL 321A INTERNAL AREA FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;[02] REPLACED RIB 8 LOC ACCES PANEL 321A INTERSep 20, 2022 · N265WN · Boeing 7377H4SDR SWIA202266481None · scratched*VERTICAL STAB LANDING FOR PANEL 325ER HAS SCRATCHES/GOUGES (MARKED) (C-CHECK RO 9/12/2022) REMOVED SCRATCHES AND GOUGES AT VERTICAL STAB ACCESS PANEL 325ER REF MHIRJ REO 601R-55-31-406 REV-- DATE 2022-08-06 / COMPLIED WITH SKYWEST TASKCARD 51-900-100Jul 31, 2022 · N955SW · Cndair CL6002B19SDR SWIA202266479None · scratched*VERTICAL STAB LANDING FOR PANEL 325CR HAS SCRATCHES/GOUGES (MARKED) (C-CHECK RO 9/12/2022) REMOVED SCRATCHES AND GOUGES AT VERTICAL STAB ACCESS PANEL 325CR REF MHIRJ MHIRJ REO 601R-55-31-406 REV-- DATE 2022-08-06 AND CRJ200 SRM 51-12-00 / COMPLIED WIJul 31, 2022 · N955SW · Cndair CL6002B19SDR SWIA202266478None · scratched*VERTICAL STAB LANDING FOR PANEL 325BR HAS SCRATCHES/GOUGES (MARKED) (C-CHECK RO 9/12/2022) REMOVED SCRATCHES AND GOUGES AT VERTICAL STAB PANEL 325BR REF MHIRJ REO 601R-55-31-406 REV-- DATE 2022-08-06 AND CRJ200 SRM 51-12-00 / COMPLIED WITH SKYWEST TAJul 31, 2022 · N955SW · Cndair CL6002B19SDR SWIA202266477None · scratched*VERTICAL STAB LANDING FOR PANEL 325BL HAS SCRATCHES/GOUGES (MARKED) (C-CHECK RO 9/12/2022) REMOVED SCRATCHES AND GOUGES AT VERTICAL STAB ACCESS PANEL 325BL REF MHIRJ REO 601R-55-31-406 REV-- DATE 2022-08-06 AND CRJ200 SRM 51-12-00 / COMPLIED WITH SKJul 31, 2022 · N955SW · Cndair CL6002B19SDR SWIA202266476None · scratched*VERTICAL STAB LANDING FOR PANEL 325AL HAS SCRATCHES/GOUGES (MARKED) (C-CHECK RO 9/12/2022) REMOVED SCRATCHES AND GOUGES AT VERTICAL STAB ACCESS PANEL 325AL REF MHIRJ REO 601R-55-31-406 REV-- DATE 2022-08-06 AND CRJ200 SRM 51-12-00 / COMPLIED WITH SKYJul 31, 2022 · N955SW · Cndair CL6002B19SDR U2RA2022072800032Shear Web · crackedIT WAS FOUND 2 EA CRACKS ON THE VERTICAL STABILIZER T/E BEAM RHS WEB (P/N: 173U1010-31) APPROX.AT RUD STA 307 AND RUD STA 332. THE PERMANENT REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, LNC'S ENGINEERING ORDER 22089-8, REV IR, WHIJul 15, 2022 · N919CA · Boeing 747428SDR SWIA202266163None · dentedWHILE REMOVING STABILIZER VERTICAL LEADING EDGE FOUND PROTRUDING DENT APROX 12" ABOVE T/E OF THE L/H PYLON (C-CHECK RO 7/26/2022) REPAIRED DENT IAW REO 601R-53-61-7844 REV. - - DATED 6/15/22. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. FORM 3Jun 3, 2022 · N961SW · Cndair CL6002B19SDR SWIA202265835None · crackedCRACK FOUND ON THE RH AFT DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT FWD EDGE OF RH AFT DRAG ANGLE AND EXTENDS APROX. 0.281" AFT IN THE CORNER OF THE ANGLE. DAMAGE IS OUT OF LIMITS PER SRM 55-31-00. / HAS BEEN DETERMINED TO BE A MMay 31, 2022 · N773SK · Cndair CL6002C10SDR SWIA202265834None · crackedCRACK FOUND ON THE LH AFT DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT FWD EDGE OF LH AFT DRAG ANGLE AND EXTENDS APROX. 0.7515" AFT IN THE CORNER OF THE ANGLE. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 55-31-00. / IT HAS BEEN DETERMIMay 31, 2022 · N773SK · Cndair CL6002C10SDR SWIA202265833None · crackedCRACK FOUND ON THE LH FWD DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT AFT EDGE OF THE LH FWD DRAG ANGLE AND EXTENDS APROX. 2.115" FWD IN THE CORNER OF THE ANGLE. DAMAGE IS OUT OF LIMITS PER SRM 55-31-00. IT HAS BEEN DETERMINED TO BEMay 31, 2022 · N773SK · Cndair CL6002C10SDR IXXA2022051903Vertical Beam · delaminatedDELAMINATED AREA ON RIGHT HAND SIDE OF VERTICAL STABILIZER AT APPROX FSS 270.784.May 19, 2022 · N389AZ · Boeing 767300SDR CALA2022051601263Vortex Gen · missingPDA 2 MISSING ONE APU VORTEX GEN RGHT SIDE ADDING IMAGES ONE VORTEX MISSING PLACED ON CDL REFERENCE LOG 8570467May 16, 2022 · N67812 · Boeing 737900ERSDR SWAA2022060300191Angle · crackedCRACK ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L UPPER FUSELAGE AT VERTICAL STABILIZER 2022-223221 / [01] REPLACED ANGLE LOCATED AT BS 1016 BETWEEN S-2R AND S-2L UPPER FUSELAGE AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING 176A3001 SHEET 22 Apr 27, 2022 · N464WN · Boeing 7377H4SDR V0XD202202250001Actuator · corrodedL/H O/B CENTER FLAP /CENTER BUTE DOOR ACTUATOR ASSY SPRING IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE BUTE DOOR ACTUATOR IAW CRJ 700 AMM 57-54-02-400-804/000-804Feb 25, 2022 · N525AE · Cndair CL600*SDR SWIA202164681None · cracked*VERTICAL STABILIZER AFT RIGHTHAND DRAG ANGLE IS CRACKED. (C CHECK RO 02/25/2022) REPLACED VERTICAL STABILIZER AFT RIGHT HAND DRAG ANGLE AS PER CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-22-001-001-A01 AND DWG BA6Dec 20, 2021 · N726SK · Cndair CL6002C10SDR V0XD20211218001Angle · crackedVERTICAL STABLIZER L/H AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-55-31-018 REV. A DATED 2016-11-10Dec 18, 2021 · N527EA · Cndair CL6002C10SDR SWIA202164105None · cracked*CRACK PRESENT ON V-STAB RH AFT DRAG ANGLE (C CHECK RO 02-03-22) REPAIRED AFT VERTICAL STAB TO FUSELAGE RH DRAG ANGLE. REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Nov 21, 2021 · N710SK · Cndair CL6002C10SDR SWIA202164104None · cracked*CRACK PRESENT ON V-STAB RH FWD DRAG ANGLE (C CHECK RO 02-03-22) REPAIRED FWD VERTICAL STAB TO FUSELAGE RH DRAG ANGLE. REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Nov 21, 2021 · N710SK · Cndair CL6002C10SDR SWIA202164103None · cracked*CRACK PRESENT ON V-STAB LH AFT DRAG ANGLE (C CHECK RO 02-03-22) REMOVED AND REPLACED LH AFT DRAG ANGLE WITH NEW REPAIR PARTS. REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Nov 21, 2021 · N710SK · Cndair CL6002C10SDR SWIA202164102None · cracked*CRACK PRESENT ON V-STAB LH FWD DRAG ANGLE (C CHECK RO 02-03-22) PERFORMED V-STAB LH FWD DRAG ANGLE CRACK REPAIR REF. CRJ-700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Nov 21, 2021 · N710SK · Cndair CL6002C10SDR SWIA202163831None · cracked*SUSPECTED CRACK AT R/H AFT DRAG ANGLE AT BASE OF VERTICAL STAB (MARKED) (C CHECK RO 1/16/2022) PREFORMED SRM REPAIR ON R/H AFT DRAG ANGLE OF VERTICAL STAB, INSTALLED AFT ANGLE DOUBLER AND AFT ANGLE FILLER REF. CRJ-700 SRM 55-31-00-201-001-A01, CRJ-700 SRMNov 4, 2021 · N770SK · Cndair CL600*SDR SWIA202163830None · cracked*SUSPECTED CRACK AT L/H AFT DRAG ANGLE AT BASE OF VERTICAL STAB (MARKED) (C CHECK RO 1/16/2022) PREFORMED SRM REPAIR ON L/H AFT DRAG ANGLE OF VERTICAL STAB, INSTALLED AFT ANGLE DOUBLER AND AFT ANGLE FILLER REF. CRJ-700 SRM 55-31-00-201-001-A01, CRJ-700 SRMNov 4, 2021 · N770SK · Cndair CL600*SDR SWIA202163158None · damagedDURING REPAIR OF L/H FWD DRAG ANGLE UNDERLYING SKIN WAS TRIMMED. (C CHECK RO 12-19-21) REPAIRED LH FWD DRAG ANGLE UDERLYING SKIN REF REO 670-55-31-151 REV --. DATE 2021-11-09 SEE CONTINAUTION FOR DETAILS TASK 51-900-1002-SKY ACCOMPLISHEDOct 20, 2021 · N606SK · Cndair CL6002C10SDR SWAA2021110128181None · corrodedON THE VERTICAL FIN UPPER CAP THE LEFT SIDE TRAILING EDGE AREA HAS EVIDENCE OF CORROSION / FOUND CORROSION TO BE OUT OF LIMITS REMOVED & REPLACED VERT. STAB END CAP TRAILING EDGE SECTION REF SRM 51-40-02Oct 8, 2021 · N8305E · Boeing 7378H4SDR SWIA202163113None · cracked* R/H SIDE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE HAS A SUSPECTED CRACK NEAR THE RUDDER, MARKED. (C CHECK RO 12-19-21) REPAIRED CRACK AT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WHERE MARKED R/H . REF CRJ700 SRM 55-31-00-201-001-A01, 51-42-13-001-0Oct 1, 2021 · N606SK · Cndair CL6002C10SDR SWIA202163112None · cracked* L/H SIDE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE HAS A SUSPECTED CRACK NEAR THE RUDDER, MARKED. (C CHECK RO 12-19-21) PERFORMED L/H SIDE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REPAIR REF, CRJ- 700 SRM 55-31-00-201-001-A01 AND REO 670-55-31-151 REOct 1, 2021 · N606SK · Cndair CL6002C10SDR SWIA202162464None · crackedLH DRAG ANGLES JUST BELOW VERTICAL STAB APPROX. FS 1220 - 67.5 % HAS A CRACK AS MARKED (C-CHECK RO 11/10/2021) CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ON THE LH VERT STAB FS1220 - 67.5% REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASKAug 21, 2021 · N772SK · Cndair CL600*SDR SWIA202162463None · crackedRH DRAG ANGLES JUST BELOW VERTICAL STAB APPROX. FS 1220 - 67.5 % HAS A CRACK AS MARKED (C-CHECK RO 11/10/2021) CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ON THE RH VERT STAB FS1220 - 67.5% REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASKAug 21, 2021 · N772SK · Cndair CL600*SDR SWIA202162318None · cracked*POSSIBLE CRACK ON LH VERTICAL/FUSELAGE AFT DRAG ANGLE (C-CHECK RO 11/5/2021) REPAIRED THE L/H VERTICAL/FUSELAGE AFT DRAG ANGLER REF. CRJ 700 SRM 51-42-21-001-001-A01 51-42-10-001-001-A01 51-42-22-001-001-A01, AND DWG BA670-35002 REV F. / C/W TASK CARDAug 9, 2021 · N614SK · Cndair CL6002C10SDR SWIA202162317None · cracked*POSSIBLE CRACK ON RH VERTICAL/FUSELAGE AFT DRAG ANGLE (C-CHECK RO 11/5/2021) REMOVED AND REPLACED NEW RH AFT DRAG ANGLE REF CRJ 700 SRM 51-42-21-001-001-A01 51-42-10-001-001-A01 51-42-22-001-001-A01, AND DWG BA670-35002 REV F. COMPLIED WITH TASK CRADAug 9, 2021 · N614SK · Cndair CL6002C10SDR SWIA202161150None · cracked*SUSPECTED CRACK NOTED AT L/H DRAG ANGLE AT BASE OF VERTICAL STAB AT APPROX FS1181.00 (MARKED) (C-CHECK RO 9-21-21) REMOVED AND INSTALLED NEW L/H AFT DRAG ANGLE AT BASE OF VERTICAL STAB AT APPROX FS1181.00 REF CRJ 700 SRM 51-42-21-001-001-A01,CRJ 700 SRM Jul 15, 2021 · N766SK · Cndair CL600*SDR SWAA2022020968069None · damagedDAMAGE FOUND ON R/H DORSAL FIN 6.75' FWD OF THE AFT EDGE OF THE DORSAL FIN AND 5' BELOW TOP EDGE. / ACCOMPLISHED REPAIR TO DORSAL FIN REF SRM 51-70-05-2R-1.Mar 17, 2018 · N945WN · Boeing 7377H4SDR 2018FA0000023Spar · chafedVERTICAL FIN AFT SPAR CAP CHAFED. REPAIRED IAW REPORT S-680-0081/10RD.Jan 11, 2018 · N369QS · Cessna 680CESDR SWAA2022020382264Bracket · crackedSUPPLEMENTAL INFORMATION: SKATE ANGLE ATTACH BRACKET CRACKED; PANEL 323CR / REMOVED AND REPLACED SKATE ATTACH BRACKET PER SRM 51-40-02Nov 7, 2017 · N749SW · Boeing 7377H4SDR GLBA20111025GVentral Fin · debondedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE LT VENTRAL FIN DEBONDED BETWEEN FS 570 AND FS 605, 9.5" ALONG LWR T/E AND INWARD FROM EDGE 3" ON BOTH INBD & OTBD SKINS. MX REPLACED THE VENTRAL.Oct 25, 2011 · N253GL · Beech 1900DSDR RU3A1120Stiffener · crackedLT DELTA FIN HAS TWO POPPED RIVETS AND CRACKED STIFFENER ALONG LOWER LEADING EDGE.Sep 27, 2011 · N59 · Lear 60LEARSDR 08FDEA03881Angle · crackedVERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21.Sep 15, 2008 · N426FE · Airbus A310203SDR N93A28082007AAngle · crackedDURING 5000 LANDING INSPECTION FOUND 793 BULKHEAD VERTICAL STAB CAP ANGLE CRACKED.Aug 28, 2007 · N495QS · Gulstm GIVSDR MALA070113Unknown · unknownDURING N4K CHECK IN CWA FOUND, RT VENTRAL FIN LOWER EDGE. REPAIRED IAW EO NR S53466 AND SAAB REPAIR STATEMENT 340SDS012863 REPAIRED IAW EO NR S53466 AND SAAB REPAIR STATEMENT 340SDS012863.Aug 24, 2007 · N411XJ · Saab 340BSDR TRAX200701045Attach Angle · crackedATTACH ANGLE FOR RB 2 ON AFT SIDE OF MID SPAR IS CRACKED UNDER ACCESS PANEL 325AL ON VERTICAL STABILIZER. [08-07-07] PERFORMED FPI OF ATTACH ANGLE FOR R/B NR 2 ON AFT SIDE. NO DEFECTS NOTED PER CRJ 200 NDTM 51-20-08.Jul 24, 2007 · N833AS · Cndair CL6002B19SDR 2758071607Skin · cracked1 INCH LONG SKIN CRACK FOUND ON IB SIDE OF VERTICAL STABILIZER SKIN.Jul 16, 2007 · N117MH · Bolkms BK117A3SDR DALA1134489221Attach Angle · crackedCRACK ON LT DORSAL FIN ATTACH ANGLE. REPAIRED PER MESSAGE 1-207926631-2.Jan 1, 2007 · N921DN · Doug MD9030SDR QXEA200601127Clip · crackedPDX - C4 V STAB, RIGHT MID SPAR, CLIP IS CRACKED ON AFT SIDE ON MID SPAR AT Z 176.5. REPAIRED IAW DHC-8-200 SRM 51-40-11.Apr 14, 2006 · N356PH · Dhav DHC8202
Back to JASC 5533