JASC 5512
Service difficulty reports · 7,877
Reports filed under 5512 · Horizontal Stabilizer, Plate/Skin, 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 = '5512' 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 = '5512' 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 SCNA20261014427Skin · crackedCRACK 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 DALA2026100605515Skin · corrodedCORROSION 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 SWAA2026100104773Panel · delaminatedDAMAGE FOUND ON AFT OTBD CORNER OF HORIZONTAL STAB PANEL 343BB. PREFORMED TEMP REPAIR IAW SRM 55-10-01-1A-3,SDR SCNA20261014429Skin · crackedWO 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, REPASDR SCNA20261014428Skin · crackedCRACK 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 SCNA20261014426Skin · crackedWO 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 SWAA2026101443741Access Panel · damagedELONGATED 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 CALA2026101220287Skin · crackedLEFT 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 SWAA2026101229388Access Panel · crackedCRACK 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 CALA2026101220285Skin · crackedRIGHT 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 CALA2026101220283Skin · crackedLEFT 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 SWAA2026092992719Access Panel · damagedRIGHT STABILIZER ACCESS PANEL 344EB, HAD ELONGATED HOLES & DAMAGE. THE ACCESS PANEL 344EB WAS REPLACED IAW AMM 27-31-11.SDR SWAA2026092980670Access Panel · damagedRIGHT HORIZONTAL STAB ACCESS PANEL 344BB HAD ELONGATED HOLES & DAMAGE. REPLACED THE ACCESS PANEL IAW SRM 51-10-02.SDR SWAA2026092973622Access Panel · elongatedACCESS PANEL 344FB, RT STABILIZER HAD ELONGATED HOLES & DAMAGE. REPLACED THE PANEL 344FB IAW AMM 27-31-11. C/W STEPS 2-6.SDR SWAA2026092933747Access Panel · damagedPANEL 344AT, RT STABILIZER HAD ELONGATED HOLES & DAMAGE. THE PANEL 344AT WAS REPLACED IAW AMM 27-31-11. C/W STEPS 3-7.SDR SWAA2026092956055Panel · damagedPANEL 344DB, ON THE RT STABILIZER HAD ELONGATED HOLES & DAMAGE. PANEL 344DB WAS REPLACED IAW AMM 27-31-11. C/W STEPS 2-6.SDR ABXA20260918423Skin · corrodedDURING 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-55SDR ABXA20260918422Skin · corrodedDURING 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 STATSDR SWAA2026101232960Access Panel · crackedCRACK 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 SWAA2026100762037Access Panel · crackedCRACKED 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 SWAA2026100550157Blade · crackedCRACKED 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 DALA2026091205103Skin · crackedCRACK (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 SWAA2026101411223Access Panel · crackedCRACKED 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 SWAA2026101424077Access Panel · damagedELONGATED 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 ABXA20260901388Skin · corrodedDURING 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 ABXA20260901387Skin · corrodedDURING 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 ANSDR ABXA20260901386Skin · corrodedDURING 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 SRSDR ABXA20260901385Skin · corrodedDURING 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 REASDR ABXA20260901384Skin · corrodedDURING 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 BLSDR ABXA20260901383Skin · corrodedDURING 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) COSDR ABXA20260901382Skin · corrodedDURING 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-5513-66201SDR ABXA20260901381Skin · corrodedDURING 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 ABXA20260901380Skin · corrodedDURING 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 CALA2026090719294Skin · crackedCRACK 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 I5PA2026083068802Skin · corrodedCORROSION DISCOVERED ON RT HORIZONTAL STAB UPPER SKIN. REPAIRED THE STAB SKIN IAW EO APA-0046-011, -012, -013, -014, -015, & -016.SDR I5PA2026083068801Skin · corrodedCORROSION 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 CALA2026090919334Skin · crackedTWO 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 CALA2026090719296Skin · crackedTHREE 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 CALA2026092819863Skin · crackedEA 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 SWAA2026092959991Access Panel · crackedCRACKED 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 SWAA2026091453396Access Panel · crackedCRACKED 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.SDR CALA2026092819858Skin · crackedLH HORIZONTAL STAB, LOWER SKIN, ONE CRACK INDICATION AT HSS 157.10, 9.5 INCHES IN FRONT OF REAR SPAR. PERFORMED REPAIR ON LH HORIZONTAL STAB, LOWER SKIN AT HSS 157.10 AND 9.5" IN FRONT OF REAR SPAR IAW SRM 55-10-01-2R-11, 51-40-02-0G-0, 51-40-05-0G-0, & 51-40SDR FDEA202608201192Skin · damagedDURING AGING AIRCRAFT INSPECTION FOUND PREVIOUS EXISTING REPAIR ON RH HORIZONTAL STAB LOWER SKIN, INBD AREA, NOT INCLUDED ON THE MCMRT/CCMRP COMPLIED WITH EA F -5510-T0324519 A P3 TITLE: STABILIZER -HORIZONTAL STABILIZER-RIGHT HORIZONTAL STAB LOWER SKIN DAMASDR REXA2026092101851Retainer · damagedAFTER SEAL REMOVAL ELONGATE SEAL RETAINER HOLES OF ACCESS PANEL 331AL WAS FOUND. SEAL RETAINER OF ACCESS PANEL 331AL WAS REPLACED AND MUST ME INSTALLED UNDER NRC 00217 PER CRJ-900 AMM 55-11-07-400-801 (CONFIG A01).SDR SWAA2026091164233Skin · crackedCRACK INDICATION FOUND ON HORIZONTAL STAB LOWER SKIN, RT SIDE. HSS 193.90, RIB INBD SIDE & 16.5 INCH FRONT SPAR TO REAR SPAR. CRACK LENGTH 0.563 INCH. REPAIRED THE HORIZONTAL STAB LOWER SKIN PANEL. LOCATED BTW STAB STA 184.70 AND STAB STA 203.10 AT RT HORIZOSDR FDEA202608181141Skin Panel · dentedDENT ON RH LWR HORIZONTAL IB FWD SKIN APPLIED PERMANENT REPAIR AT RH LWR HORIZONTAL I/B FWD SKIN IAW B757 SRM 51-70-10-2R REP 4SDR ASAA2026081468108Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN HAS CRACK INDICATION INBOARD OF STAB STA 92.70 AS MARKED. GROUNDED - YES. ACCOMPLISHED REPAIR ON R/H HORIZONTAL STAB INCORPORATED NEW DOUBLER WITH EXISTING DOUBLER FROM STA 92.70 TO STA 102.70 IAW B737-NG SRM 55-10-01-2R-SDR ASAA2026081468109Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN HAS CRACK INDICATION AT THE REAR SPAR BETWEEN STAB STA 120.30 AND 129.50. GROUNDED - YES. ACCOMPLISHED REPAIR IAW SRM 55-10-01-2R-11 INCORPATING REPAIR ON G2427588 CAT B REPAIR. INSPECTION OF 56000 TOTAL FLIGHT CYCLES, INSDR ASAA2026081468099Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN BETWEEN STAB STA 120.30 AND 129.50 HAS CRACK INDICATION AT THE REAR SPAR AS MARKED. GROUNDED - YES. ACCOMPLISHED REPAIR ON L/H HORZ STAB BETWEEN STA 120.30 AND 129.50 IAW SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR INSPECTISDR CALA2026090719292Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STAB LOWER SKIN AT HSS 147.90 , 8" FROM FRONT SPAR , INBD ROW. CRACK LENGTH : 0.75". REPAIRED THE CRACKED STAB SKIN IAW SRM 55-10-01-2R-11.
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