# Service difficulty reports: JASC 5512

A list on [JASC 5512](https://openairdocs.org/jasc/5512.md).

Reports filed under 5512 · Horizontal Stabilizer, Plate/Skin, newest first.

Page 1 of 158 · 7,886 reports

- [SDR CALA2026102320550](https://openairdocs.org/sdr/CALA2026102320550.md): Skin · damaged · Oct 22, 2026 · N14560 · Airbus A321271NX
  > DAMAGE TO OB HORIZONTAL LOWER SKIN LOCATED 4.5 IN OB RIB 12, 5.25 IN FWD OF AFT EDGE LOWER SKIN. DISBOND WITH HOLE MEASURES 2IN X 1.5IN. AFT LOWER SKIN AFT EDGE DAMAGE LOCATED 3.5IN OB RIB 12 WITH 1IN CUT, AND 3.5 DISBOND SPANWISE TO SKIN. ACP NDT REF AVO0
- [SDR DALA2026102205822](https://openairdocs.org/sdr/DALA2026102205822.md): Skin · cracked · Oct 21, 2026 · N3764D · Boeing 737832
  > CRACK ON LOWER SURFACE STAB STA 175.50 AND 15 IN APROX TO FRONT SPAR, ALSO ON STAB STA 184.70 AND 12 IN APROX TO REAR SPAR AT LEFT HORIZONTAL STABILIZER. LOWER SURFACE STAB STA 175.50 AND 15 IN APROX TO FRONT SPAR, ALSO ON STAB STA 184.70 AND 12 IN APROX TO
- [SDR JGVR20261021002](https://openairdocs.org/sdr/JGVR20261021002.md): Skin · corroded · Oct 21, 2026 · N676QS · Cessna 680A
  > REPAIRED THE LH HORIZONTAL STABILIZER UPPER INBOARD SKIN BY TRIMMING OUT CORRODED AREA, PERFORMING NDT, FABRICATING AND INSTALLING REPAIR DOUBLER AND FILLERS IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.
- [SDR DALA2026102205814](https://openairdocs.org/sdr/DALA2026102205814.md): Skin · cracked · Oct 20, 2026 · N3764D · Boeing 737832
  > CRACK ON LOWER SURFACE STAB STA 129.50 AND 10 IN TO FRONT SPAR AT RIGHT HORIZONTAL STABILIZER. LOWER SURFACE STAB STA 129.50 AND 10 IN TO FRONT SPAR AT RIGHT HORIZONTAL STABILIZER WAS REPAIRED PER B737 -800 SRM 55-10-01-2R REPAIR 11. (1875222) AIRCRAFT WAS G
- [SDR DALA2026102205813](https://openairdocs.org/sdr/DALA2026102205813.md): Skin · cracked · Oct 20, 2026 · N3764D · Boeing 737832
  > CRACK ON LOWER SURFACE STAB STA 101.90 AND 14 IN TO REAR SPAR, ALSO ON STAB STA 129.50 AND 10 IN TO REAR SPAR AT LEFT HORIZONTAL STABILIZER. LOWER SURFACE STAB STA 101.90 AND 14 IN TO REAR SPAR, ALSO ON STAB STA 129.50 AND 10 IN TO REAR SPAR AT LEFT HORIZONTA
- [SDR SCNA20261014427](https://openairdocs.org/sdr/SCNA20261014427.md): Skin · cracked · Oct 8, 2026 · N825SY · Boeing 7378F2
  > CRACK WAS FOUND OF 0.125IN LENGTH IN RIB HOLE AT STAB STA 129.50 OF LT HORIZONTAL STAB LOWER SURFACE. REPAIR: IAW SRM REF 55-10-09-2R-5, REPAIR 5.
- [SDR DALA2026100605515](https://openairdocs.org/sdr/DALA2026100605515.md): Skin · corroded · Oct 4, 2026 · N197DN · Boeing 767332
  > CORROSION EXTERNAL SKIN HORIZONTAL STABILIZER LOC. REAR SPAR BTW RIB 1 L AND RIB 1R AT HORIZONTAL. COMPLIED WITH ER/A 637153-14 (1847862)(AIRCRAFT GROUNDED)
- [SDR K11A2026102700408](https://openairdocs.org/sdr/K11A2026102700408.md): Access Panel · corroded · Oct 3, 2026 · N325FL · Boeing 737883
  > LEFT HORIZONTAL STAB TRAILING EDGE HAS EVIDENCE OF CORROSION ON LOWER SURFACE FOR ACCESS PANEL AT ELEV STA 149-176
- [SDR SWAA2026100104773](https://openairdocs.org/sdr/SWAA2026100104773.md): Panel · delaminated · Sep 30, 2026 · N8874Q · Boeing 7378
  > DAMAGE FOUND ON AFT OTBD CORNER OF HORIZONTAL STAB PANEL 343BB. PREFORMED TEMP REPAIR IAW SRM 55-10-01-1A-3,
- [SDR SCNA20261014429](https://openairdocs.org/sdr/SCNA20261014429.md): Skin · cracked · Sep 27, 2026 · N825SY · Boeing 7378F2
  > WO 98046 NR00014 INITIAL / CRACK WAS FOUND OF: L=0.688IN LENGTH ON RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.70 COMMON TO THE HORIZONTAL RIB IN REFERENCE TO TASK CARD ENG-55SCA-11150-RH, THE HORIZONTAL STAB WAS REPAIRED IAW SRM 55-10-01-2R-11, REPA
- [SDR SCNA20261014428](https://openairdocs.org/sdr/SCNA20261014428.md): Skin · cracked · Sep 27, 2026 · N825SY · Boeing 7378F2
  > CRACK WAS FOUND OF: L=0.625IN LENGTH ON RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 184.70 COMMON TO THE HORIZONTAL RIB IN REFERENCE TO TASK CARD ENG-55SCA-11150-RH,
- [SDR SCNA20261020437](https://openairdocs.org/sdr/SCNA20261020437.md): Skin · cracked · Sep 26, 2026 · N825SY · Boeing 7378F2
  > A CRACK WAS FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.70 COMMON TO THE HORIZONTAL RIB IAW TASK CARD ENG-55SCA-11150-LH, CRACKS (2EAS) AT LOWER SKIN AT STAB STA 129.50 COMMON TO THE HORIZONTAL RIBS, CRACK (1EA) AT STAB STA 138.70 COMMON TO TH
- [SDR SCNA20261014426](https://openairdocs.org/sdr/SCNA20261014426.md): Skin · cracked · Sep 26, 2026 · N825SY · Boeing 7378F2
  > WO 98046 NR00012, INITIAL / CRACK WAS FOUND OF: L=0.750IN LENGTH ON LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 147.90 COMMON TO THE HORIZONTAL RIB IN REFERENCE TO TASK CARD ENG-55SCA-11150-LH, CRACK OF: L=0.750IN LENGTH ON LH HORIZONTAL STABILIZER LOWER
- [SDR SWAA2026102744861](https://openairdocs.org/sdr/SWAA2026102744861.md): Access Panel · cracked · Sep 25, 2026 · N273WN · Boeing 7377H4
  > CRACKED BLADE FOR ACCESS PANEL 333AT ON THE LT HORIZONTAL STAB. REPLACED THE BLADE FOR ACCESS PANEL 333AT IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
- [SDR SWAA2026101443741](https://openairdocs.org/sdr/SWAA2026101443741.md): Access Panel · damaged · Sep 21, 2026 · N8656B · Boeing 7378H4
  > ELONGATED HOLES ON LEADING EDGE SKIN ACCESS PANEL 341B, UPPER AREA LE STA 69.93 MORE 1 INCH HOLE 1, 2.607 INCHES OF UPPER EDGE & HOLE 2, 4.536 INCHES OF UPPER EDGE AT RT HORIZONTAL STAB. RESOLVED ON ANOTHER FAULT TTG8Q01E7AQ2 AND EA M-23-155-00207.
- [SDR CALA2026101220287](https://openairdocs.org/sdr/CALA2026101220287.md): Skin · cracked · Sep 21, 2026 · N16703 · Boeing 737724
  > LEFT HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED AT HSS 101.90 INBD SIDE, LOCATED TO 10.25 INCH FWD FROM AFT SPAR, CRACK LENGTH 1.079 INCH, PERFORMED REPAIR TO THE LT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11.
- [SDR SWAA2026101229388](https://openairdocs.org/sdr/SWAA2026101229388.md): Access Panel · cracked · Sep 20, 2026 · N201LV · Boeing 7377H4
  > CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM-51-40-02-0G-0 AND SRM-51-10-02-0G-0 ITEM 9.
- [SDR CALA2026101220285](https://openairdocs.org/sdr/CALA2026101220285.md): Skin · cracked · Sep 19, 2026 · N16703 · Boeing 737724
  > RIGHT HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED AT HSS 129.50, OTBD SIDE LOCATED TO 16 INCH AFT FROM FWD, MARKED AREA. PERFORMED REPAIR TO THE RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11.
- [SDR CALA2026101220283](https://openairdocs.org/sdr/CALA2026101220283.md): Skin · cracked · Sep 18, 2026 · N73299 · Boeing 737824
  > LEFT HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED AT HSS 129.50, INBD SIDE LOCATED TO 9.750 INCH APROX. FWD FROM AFT SPAR. CRACK LENGTH 0.750 INCH. PERFORMED REPAIR TO THE LT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11.
- [SDR SWAA2026092992719](https://openairdocs.org/sdr/SWAA2026092992719.md): Access Panel · damaged · Sep 18, 2026 · N8548P · Boeing 7378H4
  > RIGHT STABILIZER ACCESS PANEL 344EB, HAD ELONGATED HOLES & DAMAGE. THE ACCESS PANEL 344EB WAS REPLACED IAW AMM 27-31-11.
- [SDR SWAA2026092980670](https://openairdocs.org/sdr/SWAA2026092980670.md): Access Panel · damaged · Sep 18, 2026 · N8548P · Boeing 7378H4
  > RIGHT HORIZONTAL STAB ACCESS PANEL 344BB HAD ELONGATED HOLES & DAMAGE. REPLACED THE ACCESS PANEL IAW SRM 51-10-02.
- [SDR SWAA2026092973622](https://openairdocs.org/sdr/SWAA2026092973622.md): Access Panel · elongated · Sep 18, 2026 · N8548P · Boeing 7378H4
  > ACCESS PANEL 344FB, RT STABILIZER HAD ELONGATED HOLES & DAMAGE. REPLACED THE PANEL 344FB IAW AMM 27-31-11. C/W STEPS 2-6.
- [SDR SWAA2026092933747](https://openairdocs.org/sdr/SWAA2026092933747.md): Access Panel · damaged · Sep 18, 2026 · N8548P · Boeing 7378H4
  > PANEL 344AT, RT STABILIZER HAD ELONGATED HOLES & DAMAGE. THE PANEL 344AT WAS REPLACED IAW AMM 27-31-11. C/W STEPS 3-7.
- [SDR SWAA2026092956055](https://openairdocs.org/sdr/SWAA2026092956055.md): Panel · damaged · Sep 18, 2026 · N8548P · Boeing 7378H4
  > PANEL 344DB, ON THE RT STABILIZER HAD ELONGATED HOLES & DAMAGE. PANEL 344DB WAS REPLACED IAW AMM 27-31-11. C/W STEPS 2-6.
- [SDR ABXA20260918423](https://openairdocs.org/sdr/ABXA20260918423.md): Skin · corroded · Sep 18, 2026 · N762CK · Boeing 7673P6
  > DURING AIRCRAFT C5-CHECK, MAINTENANCE DISCOVERED CORROSION DAMAGE ON THE UPPER SKIN PANEL OF THE RIGHT HORIZONTAL STABILIZER BETWEEN FRONT SPAR HSS 157.439 AND 182.093. THE CORROSION WAS BLENDED IAW SRM AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW ABX-REA-55
- [SDR ABXA20260918422](https://openairdocs.org/sdr/ABXA20260918422.md): Skin · corroded · Sep 18, 2026 · N762CK · Boeing 7673P6
  > DURING AIRCRAFT C5 CHECK, MAINTENANCE DISCOVERED RT HORZ STAB UPPER SKIN HAS EVIDENCE OF CORROSION, 24 INCHES AFT OF THE LEADING EDGE AT AUX SPAR HSS 365 JM-1 CORROSION DAMAGE ON THE UPPER SKIN PANEL OF THE RIGHT-HAND HORIZONTAL STABILIZER AT FRONT SPAR STAT
- [SDR SWAA2026101232960](https://openairdocs.org/sdr/SWAA2026101232960.md): Access Panel · cracked · Sep 16, 2026 · N201LV · Boeing 7377H4
  > CRACK ANGLE OF ACCESS PANEL 333AT ON THE LT HORIZONTAL STAB. REPLACED THE ACCESS PANEL IAW SRM-51-40-02-0G-0, & SRM-51-10-02-0G-0, ITEM 9.
- [SDR SWAA2026100762037](https://openairdocs.org/sdr/SWAA2026100762037.md): Access Panel · cracked · Sep 12, 2026 · N208WN · Boeing 7377H4
  > CRACKED BLADE ASSY ON THE LT HORIZONTAL STAB ACCESS PANEL 333AT. REPLACED THE BLADE ASSY FOR ACCESS PANEL 333AT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.
- [SDR SWAA2026100550157](https://openairdocs.org/sdr/SWAA2026100550157.md): Blade · cracked · Sep 12, 2026 · N8309C · Boeing 7378H4
  > CRACKED ACCESS PANEL 333AB BLADE ASSY AT LT HORIZONTAL STAB. REPLACED THE BLADE ASSY ON ACCESS PANEL 333AB IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9.
- [SDR IPXA2026102491077](https://openairdocs.org/sdr/IPXA2026102491077.md): Skin Panel · delaminated · Sep 11, 2026 · N402UP · Boeing 75724APF
  > STR, ATA 55: R/H HORZ STAB UPPER HONEYCOMB SKIN PANEL BETWEEN AUX AND FRONT SPAR AT STAB STA 93 (MOST INBD AREA AT EXISTING REPAIR) DISBONDED. RL037. INSTALLED I/B AND O/B LOGO LIGHT ASSY'S, R/H HORZ STAB UPPER IAW AMM 33-45-00-402-030. LOGO LIGHT-DEACTIVATION
- [SDR DALA2026091205103](https://openairdocs.org/sdr/DALA2026091205103.md): Skin · cracked · Sep 11, 2026 · N383DN · Boeing 737832
  > CRACK (3EAS) ON LWR SURFACE BTW STAB STA=129.30 TO 111.00 AT RT HORIZONTAL STAB. LWR SURFACE BTW STAB STA=129.30 TO 111.00 AT RH HORIZONTAL STAB WAS REPAIRED IAW SRM. 55-10-01-2R PROCEDURE 11, REPAIR 11. (LP 1807624 - AIRCRAFT WAS GROUNDED)
- [SDR SWAA2026101411223](https://openairdocs.org/sdr/SWAA2026101411223.md): Access Panel · cracked · Sep 9, 2026 · N8656B · Boeing 7378H4
  > CRACKED BLADE ACCESS PANEL 333 OF LT HORIZONTAL STAB. REPLACED THE BLADE ON ACCESS PANEL 333 IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9.
- [SDR SWAA2026101424077](https://openairdocs.org/sdr/SWAA2026101424077.md): Access Panel · damaged · Sep 9, 2026 · N8656B · Boeing 7378H4
  > ELONGATED HOLES ON LEADING EDGE SKIN ACCESS PANEL 341B LOCATED UPPER AREA LE STA 69.93 AT RT HORIZONTAL STABILIZER 2026-558811. PERFORMED PERMANENT REPAIR ON LEADING EDGE SKIN ACCESS PANEL 341B LOCATED UPPER AREA LE STA 69.93 AT RT HORIZONTAL STABILIZER I.A.
- [SDR ABXA20260901388](https://openairdocs.org/sdr/ABXA20260901388.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 300.105 AND RS 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-5, & ABX-REA-5513-
- [SDR ABXA20260901387](https://openairdocs.org/sdr/ABXA20260901387.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 300.105 AND RS STA 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRM. ENGINEERING CONTACTED FOR FURTHER EVALUATION AN
- [SDR ABXA20260901386](https://openairdocs.org/sdr/ABXA20260901386.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, LT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 165" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND WITH CORROSION BETWEEN RS STA 160 AND RS STA 180, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SR
- [SDR ABXA20260901385](https://openairdocs.org/sdr/ABXA20260901385.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, LT HORIZONTAL STAB, UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 8" FROM FUSELAGE BODY. (AROUND FASTERNERS) LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 13.986 AND RS STA 30.605, UPPER REA
- [SDR ABXA20260901384](https://openairdocs.org/sdr/ABXA20260901384.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 2" LONG AT 70"" O/B SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION AT RS 275.605, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BL
- [SDR ABXA20260901383](https://openairdocs.org/sdr/ABXA20260901383.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 2" LONG AT 47" FROM OTBD SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 290 & RS 310, UPPER REAR SPAR AREA STRG-1) CO
- [SDR ABXA20260901382](https://openairdocs.org/sdr/ABXA20260901382.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APPROX 3" LONG AT 22" FROM OTBD SIDE & 2.5" FWD OF REAR SPAR. (AROUND FASTERNERS). CORROSION BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-10 AND ABX-REA-5513-66201
- [SDR ABXA20260901381](https://openairdocs.org/sdr/ABXA20260901381.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 4" LONG AT 161" FROM FUSELAGE BODY. (AROUND FASTERNERS) CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-7, & ABX-REA-5513-66193-00.
- [SDR ABXA20260901380](https://openairdocs.org/sdr/ABXA20260901380.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338
  > DURING C-CHECK, R/H HORIZONTAL STAB UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 5" LONG AT 95" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND CORROSION BTWN RS STA 104.105, UPPER REAR SPAR AREA AND STRG 1. CORROSION WAS BLENDED IAW SRM. ENGINEERING
- [SDR CALA2026090719294](https://openairdocs.org/sdr/CALA2026090719294.md): Skin · cracked · Aug 30, 2026 · N39415 · Boeing 737924ER
  > CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN PANEL AT HSS 147.90, 18 INCH FWD OF T/E, CRACK LENGTH 2.5". COMPLETED INSTALLATION OF REPAIR PARTS, DOUBLER & FILLERS AT R/H HORIZONTAL STAB LOWER SKIN PANEL IAW SRM 55-10-01-2R-11.
- [SDR I5PA2026083068802](https://openairdocs.org/sdr/I5PA2026083068802.md): Skin · corroded · Aug 30, 2026 · N688SL · Boeing 757230
  > CORROSION DISCOVERED ON RT HORIZONTAL STAB UPPER SKIN. REPAIRED THE STAB SKIN IAW EO APA-0046-011, -012, -013, -014, -015, & -016.
- [SDR I5PA2026083068801](https://openairdocs.org/sdr/I5PA2026083068801.md): Skin · corroded · Aug 30, 2026 · N688SL · Boeing 757230
  > CORROSION DISCOVERED ON LT HORIZONTAL STAB UPPER SKIN. REPAIRED THE SKIN IAW EO APA-0046-001, -002, -003, -004, -005, -006, -007, -008, -009, -010, & -036.
- [SDR CALA2026090919334](https://openairdocs.org/sdr/CALA2026090919334.md): Skin · cracked · Aug 28, 2026 · N78509 · Boeing 737824
  > TWO CRACKS FOUND AT RT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 138.70, 10 INCHES FWD OF T/E, REPAIRED RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11. REPAIR 11.
- [SDR CALA2026090719296](https://openairdocs.org/sdr/CALA2026090719296.md): Skin · cracked · Aug 28, 2026 · N39415 · Boeing 737924ER
  > THREE CRACKS FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL ADJACENT TO DOUBLER, TWO CRACKS AT HSS 129.50, 10 INCHES FWD OF T/E, CRACK LENGTH 1 INCH, & 18 INCH FWD OF T/E, CRACK LENGTH 1.250", AND ONE CRACK AT HSS 147.90, 10" FWD OF T/E, CRACK LENGTH.500 INCH.
- [SDR CALA2026092819863](https://openairdocs.org/sdr/CALA2026092819863.md): Skin · cracked · Aug 27, 2026 · N78509 · Boeing 737824
  > EA 5510-01843, CRACK FOUND ON RT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 120.30, INBD OF INBD FASTENER ROW, 10.5" FWD OF T/E. REPAIRED RT HORIZONTAL STAB LOWER IN SPAR SKIN AT HSS 120.30 IAW SRM 55-10-01-2R-11. REPAIR 11.
- [SDR SWAA2026092959991](https://openairdocs.org/sdr/SWAA2026092959991.md): Access Panel · cracked · Aug 25, 2026 · N8653A · Boeing 7378H4
  > CRACKED HORIZONTAL STAB ACCESS PANEL 343CB. REPLACED THE ACCESS PANEL IAW SRM 51-10-02, ITEM 9, 51-40-02, & DWG 185A1702, SHEET 19, REV F.
- [SDR SWAA2026091453396](https://openairdocs.org/sdr/SWAA2026091453396.md): Access Panel · cracked · Aug 22, 2026 · N207WN · Boeing 7377H4
  > CRACKED BLADE, ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02 AND SRM 51-40-02.

Next page: https://openairdocs.org/jasc/5512/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 = '5512'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5512/reports

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