# Service difficulty reports: JASC 5533

A list on [JASC 5533](https://openairdocs.org/jasc/5533.md).

Reports filed under 5533 · Ventral Structure, newest first.

Page 1 of 2 · 77 reports

- [SDR JGVR20260111001](https://openairdocs.org/sdr/JGVR20260111001.md): Hinge Bracket · corroded · Jan 11, 2026 · N396QS · Cessna 680CE
  > REMOVED THE VERTICAL STABILIZER UPPER RUDDER HINGE LOWER BRACKET DUE TO CORROSION AND REPLACED WITH NEW TEXTRON P/N 6931050-59.
- [SDR SWIA2024031100105](https://openairdocs.org/sdr/SWIA2024031100105.md): Drag Angle · cracked · Jan 5, 2024 · N740EV · Cndair CL6002C10
  > CRACK 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.
- [SDR SWAA2023082382523](https://openairdocs.org/sdr/SWAA2023082382523.md): Angle · cracked · Jul 26, 2023 · N7843A · Boeing 737752
  > CRACK 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 STE
- [SDR IXXA2023041101](https://openairdocs.org/sdr/IXXA2023041101.md): Skin · delaminated · Apr 11, 2023 · N347AZ · Boeing 767300
  > L/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATION
- [SDR IXXA202304110001](https://openairdocs.org/sdr/IXXA202304110001.md): Skin · delaminated · Apr 9, 2023 · N347AZ · Boeing 767300
  > L/H VERTICAL BETWEEN AUX SPAR AND FRONT SPAR FSS270 EXTERIOR SKIN DELAMINATION
- [SDR SWAA2023041920586](https://openairdocs.org/sdr/SWAA2023041920586.md): Panel · elongated · Mar 24, 2023 · N435WN · Boeing 7377H4
  > LEFT 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 STEPS
- [SDR SWAA2022100694979](https://openairdocs.org/sdr/SWAA2022100694979.md): None · cracked · Sep 20, 2022 · N265WN · Boeing 7377H4
  > CRACK 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 INTER
- [SDR SWIA202266481](https://openairdocs.org/sdr/SWIA202266481.md): None · scratched · Jul 31, 2022 · N955SW · Cndair CL6002B19
  > *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 51-900-100
- [SDR SWIA202266479](https://openairdocs.org/sdr/SWIA202266479.md): None · scratched · Jul 31, 2022 · N955SW · Cndair CL6002B19
  > *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 WI
- [SDR SWIA202266478](https://openairdocs.org/sdr/SWIA202266478.md): None · scratched · Jul 31, 2022 · N955SW · Cndair CL6002B19
  > *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 TA
- [SDR SWIA202266477](https://openairdocs.org/sdr/SWIA202266477.md): None · scratched · Jul 31, 2022 · N955SW · Cndair CL6002B19
  > *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 SK
- [SDR SWIA202266476](https://openairdocs.org/sdr/SWIA202266476.md): None · scratched · Jul 31, 2022 · N955SW · Cndair CL6002B19
  > *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 SKY
- [SDR U2RA2022072800032](https://openairdocs.org/sdr/U2RA2022072800032.md): Shear Web · cracked · Jul 15, 2022 · N919CA · Boeing 747428
  > IT 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, WHI
- [SDR SWIA202266163](https://openairdocs.org/sdr/SWIA202266163.md): None · dented · Jun 3, 2022 · N961SW · Cndair CL6002B19
  > WHILE 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 3
- [SDR SWIA202265835](https://openairdocs.org/sdr/SWIA202265835.md): None · cracked · May 31, 2022 · N773SK · Cndair CL6002C10
  > CRACK 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 M
- [SDR SWIA202265834](https://openairdocs.org/sdr/SWIA202265834.md): None · cracked · May 31, 2022 · N773SK · Cndair CL6002C10
  > CRACK 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 DETERMI
- [SDR SWIA202265833](https://openairdocs.org/sdr/SWIA202265833.md): None · cracked · May 31, 2022 · N773SK · Cndair CL6002C10
  > CRACK 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 BE
- [SDR IXXA2022051903](https://openairdocs.org/sdr/IXXA2022051903.md): Vertical Beam · delaminated · May 19, 2022 · N389AZ · Boeing 767300
  > DELAMINATED AREA ON RIGHT HAND SIDE OF VERTICAL STABILIZER AT APPROX FSS 270.784.
- [SDR CALA2022051601263](https://openairdocs.org/sdr/CALA2022051601263.md): Vortex Gen · missing · May 16, 2022 · N67812 · Boeing 737900ER
  > PDA 2 MISSING ONE APU VORTEX GEN RGHT SIDE ADDING IMAGES ONE VORTEX MISSING PLACED ON CDL REFERENCE LOG 8570467
- [SDR SWAA2022060300191](https://openairdocs.org/sdr/SWAA2022060300191.md): Angle · cracked · Apr 27, 2022 · N464WN · Boeing 7377H4
  > CRACK 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
- [SDR V0XD202202250001](https://openairdocs.org/sdr/V0XD202202250001.md): Actuator · corroded · Feb 25, 2022 · N525AE · Cndair CL600*
  > L/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 57-54-02-400-804/000-804
- [SDR SWIA202164681](https://openairdocs.org/sdr/SWIA202164681.md): None · cracked · Dec 20, 2021 · N726SK · Cndair CL6002C10
  > *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 BA6
- [SDR V0XD20211218001](https://openairdocs.org/sdr/V0XD20211218001.md): Angle · cracked · Dec 18, 2021 · N527EA · Cndair CL6002C10
  > VERTICAL 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 2016-11-10
- [SDR SWIA202164105](https://openairdocs.org/sdr/SWIA202164105.md): None · cracked · Nov 21, 2021 · N710SK · Cndair CL6002C10
  > *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.
- [SDR SWIA202164104](https://openairdocs.org/sdr/SWIA202164104.md): None · cracked · Nov 21, 2021 · N710SK · Cndair CL6002C10
  > *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.
- [SDR SWIA202164103](https://openairdocs.org/sdr/SWIA202164103.md): None · cracked · Nov 21, 2021 · N710SK · Cndair CL6002C10
  > *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.
- [SDR SWIA202164102](https://openairdocs.org/sdr/SWIA202164102.md): None · cracked · Nov 21, 2021 · N710SK · Cndair CL6002C10
  > *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.
- [SDR SWIA202163831](https://openairdocs.org/sdr/SWIA202163831.md): None · cracked · Nov 4, 2021 · N770SK · Cndair CL600*
  > *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 SRM
- [SDR SWIA202163830](https://openairdocs.org/sdr/SWIA202163830.md): None · cracked · Nov 4, 2021 · N770SK · Cndair CL600*
  > *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 SRM
- [SDR SWIA202163158](https://openairdocs.org/sdr/SWIA202163158.md): None · damaged · Oct 20, 2021 · N606SK · Cndair CL6002C10
  > DURING 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 ACCOMPLISHED
- [SDR SWAA2021110128181](https://openairdocs.org/sdr/SWAA2021110128181.md): None · corroded · Oct 8, 2021 · N8305E · Boeing 7378H4
  > ON 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 51-40-02
- [SDR SWIA202163113](https://openairdocs.org/sdr/SWIA202163113.md): None · cracked · Oct 1, 2021 · N606SK · Cndair CL6002C10
  > * 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, 51-42-13-001-0
- [SDR SWIA202163112](https://openairdocs.org/sdr/SWIA202163112.md): None · cracked · Oct 1, 2021 · N606SK · Cndair CL6002C10
  > * 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 RE
- [SDR SWIA202162464](https://openairdocs.org/sdr/SWIA202162464.md): None · cracked · Aug 21, 2021 · N772SK · Cndair CL600*
  > LH 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 TASK
- [SDR SWIA202162463](https://openairdocs.org/sdr/SWIA202162463.md): None · cracked · Aug 21, 2021 · N772SK · Cndair CL600*
  > RH 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 TASK
- [SDR SWIA202162318](https://openairdocs.org/sdr/SWIA202162318.md): None · cracked · Aug 9, 2021 · N614SK · Cndair CL6002C10
  > *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 CARD
- [SDR SWIA202162317](https://openairdocs.org/sdr/SWIA202162317.md): None · cracked · Aug 9, 2021 · N614SK · Cndair CL6002C10
  > *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 CRAD
- [SDR SWIA202161150](https://openairdocs.org/sdr/SWIA202161150.md): None · cracked · Jul 15, 2021 · N766SK · Cndair CL600*
  > *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
- [SDR SWAA2022020968069](https://openairdocs.org/sdr/SWAA2022020968069.md): None · damaged · Mar 17, 2018 · N945WN · Boeing 7377H4
  > DAMAGE 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.
- [SDR 2018FA0000023](https://openairdocs.org/sdr/2018FA0000023.md): Spar · chafed · Jan 11, 2018 · N369QS · Cessna 680CE
  > VERTICAL FIN AFT SPAR CAP CHAFED. REPAIRED IAW REPORT S-680-0081/10RD.
- [SDR SWAA2022020382264](https://openairdocs.org/sdr/SWAA2022020382264.md): Bracket · cracked · Nov 7, 2017 · N749SW · Boeing 7377H4
  > SUPPLEMENTAL INFORMATION: SKATE ANGLE ATTACH BRACKET CRACKED; PANEL 323CR / REMOVED AND REPLACED SKATE ATTACH BRACKET PER SRM 51-40-02
- [SDR GLBA20111025G](https://openairdocs.org/sdr/GLBA20111025G.md): Ventral Fin · debonded · Oct 25, 2011 · N253GL · Beech 1900D
  > DURING 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.
- [SDR RU3A1120](https://openairdocs.org/sdr/RU3A1120.md): Stiffener · cracked · Sep 27, 2011 · N59 · Lear 60LEAR
  > LT DELTA FIN HAS TWO POPPED RIVETS AND CRACKED STIFFENER ALONG LOWER LEADING EDGE.
- [SDR 08FDEA03881](https://openairdocs.org/sdr/08FDEA03881.md): Angle · cracked · Sep 15, 2008 · N426FE · Airbus A310203
  > VERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21.
- [SDR N93A28082007A](https://openairdocs.org/sdr/N93A28082007A.md): Angle · cracked · Aug 28, 2007 · N495QS · Gulstm GIV
  > DURING 5000 LANDING INSPECTION FOUND 793 BULKHEAD VERTICAL STAB CAP ANGLE CRACKED.
- [SDR MALA070113](https://openairdocs.org/sdr/MALA070113.md): Unknown · unknown · Aug 24, 2007 · N411XJ · Saab 340B
  > DURING 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.
- [SDR TRAX200701045](https://openairdocs.org/sdr/TRAX200701045.md): Attach Angle · cracked · Jul 24, 2007 · N833AS · Cndair CL6002B19
  > ATTACH 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.
- [SDR 2758071607](https://openairdocs.org/sdr/2758071607.md): Skin · cracked · Jul 16, 2007 · N117MH · Bolkms BK117A3
  > 1 INCH LONG SKIN CRACK FOUND ON IB SIDE OF VERTICAL STABILIZER SKIN.
- [SDR DALA1134489221](https://openairdocs.org/sdr/DALA1134489221.md): Attach Angle · cracked · Jan 1, 2007 · N921DN · Doug MD9030
  > CRACK ON LT DORSAL FIN ATTACH ANGLE. REPAIRED PER MESSAGE 1-207926631-2.
- [SDR QXEA200601127](https://openairdocs.org/sdr/QXEA200601127.md): Clip · cracked · Apr 14, 2006 · N356PH · Dhav DHC8202
  > PDX - 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.

Next page: https://openairdocs.org/jasc/5533/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/jasc/5533/reports

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