JASC 5512
Service difficulty reports · 7,886
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 AALA202504283187Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 184.70, 9 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202504289160Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 16 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR FDEA202504070578Access Panel · gougedLH HORIZONTAL STABILIZER, ACCESS PANEL 332CL, LEADING EDGE, LOWER RH SURFACE WITH GOUGE LH HORIZONTAL STABILIZER, ACCESS PANEL 332CL, LEADING EDGE, LOWER RH WAS REPAIRED IAW SRM NOTE P 55-10-01-1A AND SRM 51-70-10 REPAIR 2 PARAGRAPH C (2) REV 90 AUG 15/2SDR AALA202504085401Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 129.50, 9 INCHES FROM FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202504086073Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 157.90, 16 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR DALA2025040802700Skin · corrodedCORROSION ON BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE (CENTER SECTION). (EHV). SUMMARY OF NRC 00383: CORROSION LEVEL 2. BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE WAS REPAIRED PER PRI 624982-14 REV 1 & ER/A 624SDR AALA202504080332Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 129.50, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202504081416Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 9 INCHES FROM FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202504087956Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 10 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202504084759Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 18 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202504081910Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 129.50, 18 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR SWI2025F00808Skin · dentedLH HORIZONTAL STAB. UPPER EXTERNAL SKIN HAS DENTS ON OB END (MARKED) (C-CHECK RO 06/29/2025)LH HORIZONTAL STAB. UPPER EXTERNAL SKIN DENTS EVALUATED AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 690-55-11-198 REV -- DATE 2025-04-28. SEE CONTINUATION CARD FOSDR SWAA2025042921495Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 26'' FROM FWD EDGE; 0.8' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.90 26' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11IASDR SWAA2025050554038Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.940 INCHES 2025-232356<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60007161486; DUE DATE: 06-SEP-25;SDR SWAA2025050554039Skin · crackedCRACK FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.900 INCHES 2025-232357<[01] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:200048001; DUE DATE: 28SDR SWAA2025050520674Skin · crackedCRACK FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.900 INCHES 2025-232357<[01] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:200048001; DUE DATE: 28SDR SWAA2025050538259Skin · crackedCRACK FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.900 INCHES 2025-232357<[01] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:200048001; DUE DATE: 28SDR SWAA2025050520673Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.940 INCHES 2025-232356<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60007161486; DUE DATE: 06-SEP-25SDR SWAA2025050538258Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.940 INCHES 2025-232356<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60007161486; DUE DATE: 06-SEP-25SDR CALA2025040403538Skin · no discrepancyR/H HORIZONTAL STABILIZER LOWER SKIN AT STA 92.70 REQUIRE SKIN CUT-OUT FOR ACCESS TO RIB WEB REPAIRS.SDR SWAA2025050538641Access Panel · crackedCRACK ACCESS PANEL 343AT ON PLATE AT RT HORIZONTAL STABILIZER 2025-224508<[01] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER ISDR SWAA2025050538636Access Panel · crackedCRACK ACCESS PANEL 333AT ON PLATE AT LH HORIZONTAL STABILIZER 2025-224509<[01] REPLACED BLADE ASSY AT ACCESS PANEL 333AT LOCATED LH HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE ASSY AT ACCESS PANEL 333AT LOCATED LH HORIZONTAL STABILIZSDR SWAA2025050154421Access Panel · crackedCRACK ACCESS PANEL 343AT ON PLATE AT RT HORIZONTAL STABILIZER 2025-224508<[01] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER ISDR CALA2025040403530Skin · crackedCRACK INDICATION FOUND: NO.1 MARKED, R/H HORIZONTAL LOWER SKIN STAB. STA 147.90 .900 INCHES L, I/B OF I/B ROW OF RIVETS, 8.25 INCHES FWD OF AFT SPAR. TRANSCRIBED FROM HAECO GSO NR 9287038 ESFR COMPLETEDSDR SWIA20250530329Skin · dentedDURING THE ADM INSPECTION, 1 DENT WAS FOUND ON THE LH HORIZONTAL STAB LOWER LEADING EDGE AT APPROX. INBETWEEN (HORIZONTAL STABILIZER FRONT SPAR STATION) 10.91 AND 21.91. (C-CHECK RO 05/28/2025)COMPLIED WITH REO 601R-55-11-788 REV -- DATED: 2025-04-22 REPAIR TOSDR CALA2025032803294Skin · crackedRIGHT HORIZONTAL STABILIZER C- SCAN INSPECTION FOUND CRACK INDICATION AT RIB #7 STA 138.70. APPROXIMATELY 10 INCHES FROM TRAILING EDGE, REF NDT PART 6-55-10-01, NEED TO REMOVE PAINT TO VERIFY THE EXACT SIZE OF CRACK AND LOCATION, PAINT TO IS TO THINK. CRACK ISSDR CALA2025040103378Skin · crackedTWO (2) CRACKS FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 101.90 : CRACK (1):- 27 " FROM FRONT SPAR , I/B ROW; CRACK LENGTH : 0.468". CRACK (2):-36" FROM FRONT SPAR,I/B ROW; CRACK LENGTH:0.343". (REF AAR N/R 9944665) ESFR ENTRY ESFR ENTRY COMPSDR DALA2025033102364Skin · misrepaired(LOG 0877898) DURING INSPECTION OF L/H HORIZONTAL STABILIZER LOWER SKIN REPAIR IT WAS NOTED THAT TEMP FASTENERS USED IN REPAIR HAD 1 FASTENER WITH A CRACKED COLLAR. AREA INVOLVED IS 5TH RIB O/B OF STA 109.9. L/H HORIZONTAL STABILIZER LOWER SKIN WAS REPAIRED PESDR IPXA2025032554051Skin · chafedFUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE.SDR SWAA2025050553913Access Panel · crackedCRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-231972<[01] REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 STEP 9; SRM 51-40-02 AND DWG 186A3101 SHEET 19 REV-.;[02] COMPLETED JOBSDR SWAA2025042854239Skin Panel · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.700 INCH. APPROX. 2025-204859<[01] TOOL USED ON STEP 5:EDDY CURRENT EQUIPMENT P/N: NORTEC 6SDR SWAA2025042854240Skin Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.00 INCH. APPROX. 2025-204860<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 210138103;SDR DALA2025032402175Skin · cracked(LOG 0867152) CRACK ON LOWER SURFACE SKIN STAB STA 129 AT RH HORIZONTAL STABILIZER. LOWER SURFACE SKIN STAB STA 129 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R REPAIR 11.SDR CALA2025032103059Skin · crackedREF W/C 5510-01843-001 RIGHT HORIZONTAL STABILIZER C- SCAN INSPECTION FOUND CRACK INDICATION AT RIB #7. STA. 138.70, APPROXIMATELY 7 INCHES FROM LEADING EDGE, REF NDT PART 6-55-10-01, PICTURE ATTACHED, NEED TO REMOVE PAINT TO VERIFY THE EXACT SIZE OF CRACK ANDSDR DALA2025032002122Skin · cracked(LOG 0867151) CRACK ON LOWER SURFACE SKIN STAB STA 129 AT RH HORIZONTAL STABILIZER. LOWER SURFACE SKIN STAB STA 129 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R REPAIR 11.SDR JGVR20250320007Skin · corrodedREPAIRED 2 AREAS OF CORROSION LOCATED ON LH HORIZONTAL STABILIZER UPPER SKIN FORWARD OF PANEL 351AC, BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS ENGINEERING ORDER BY CLEANING, TREATING, AND PRIMING ARESDR DALA2025032002114Skin · cracked(LOG 0859589) CRACKS ON LOWER SKIN, STAB STA 147.90 AND 138 AT LH HORIZONTAL STABILIZER. LOWER SKIN, STAB STA 147.90 AND 138 AT LH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11. REPAIR 11.SDR UIEA2025031900250Skin · corrodedCORROSION ON THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE.(<P>THE UPPER SKIN OF THE HORIZONTAL STABILIZER CENTER SECTION, RH SIDE MWAS REWORKED, BLEND OUT AND INSPECTIONS PER MXA EO NO. TRE6755080 (BOEING COMMUNICATION MESSAGE CMA-TLS-25SDR SWAA2025042205485Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 1.100 INCHES. 2025-202781 <[01]. TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: SDR SWAA2025042114953Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 1.100 INCHES. 2025-202781<[01] TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SDR SWAA2025040705197Support · crackedCRACK BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER 2025-203656<[01] REPLEACED BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CORREDTED STEP 1 REPSDR SWAA2025040704837Access Panel · crackedCRACK ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER 2025-203633<SDR SWAA2025040704617Access Panel · crackedCRACK BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2025-203624<[01] REPLACED BLADE ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02. TOOL USED CALIPER P/N: 500-197-30 S/N: A23272233 DUE DATE: 07-JAN-26;[02] RSDR SWAA2025040715559Access Panel · crackedCRACK ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER 2025-203633<[01] REPLACED ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 183A3010 SHEET: 2 REV E; FOR INSTALLATION SEE FAULT TTG8Q00YMRX1;[02] COSDR IXXA2025031201Skin · delaminatedL/H HORIZONTAL PANEL 335 AFB SKIN IS SEPARATEDSDR SWAA2025033103823Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REPAIRED L/H HORIZONTAL STABILIZER SKIN AT STAB STA 193.9 IAW SRM 55-10-01-2R-11 REPAIR 11; FIG. 204; DETAIL B.;[02] TASK C/WSDR DALA2025031401982Skin · damagedAIRCRAFT 6702, RH HORZ L/E PNL 342BR IS GOUGED/BENT ON THE EDGE. CORRECTIVE ACTION: REMOVED DAMAGE, PREPPED AND LAYED UP AND BONDED R/H HORIZ L/E PANEL 342BR IAW B757-200 SRM 51-40-10 AND MEV 25-0036-01C. PAINTED IAW B757-200 AMM 51-21-10, EWO ER/A 624683-14 PSDR AALA202504033318Skin Panel · gougedAIRCRAFT IN BASE MAINTENANCE: THE LEFT HAND HORIZONTAL LEADING EDGE SECOND SKIN PANEL FROM THE OUTBOARD END HAS A GOUGE NEXT TO A FASTNER AND AN EXISTING DENT REPAIR. APPLIED PERMANENT REPAIR ON THE LEFT HAND HORIZONTAL LEADING EDGE SECOND SKIN PANEL FROM THE SDR DALA2025030501739Skin · cracked(LOG 0837193) R/H HORIZONTAL STABILIZER HAS CRACK ON LWR SKIN AT STAB STA 75 APPROX. 10 IN FROM T/E. REPAIRED CRACK ON R/H HORIZONTAL STABILIZER LWR SKIN AT STAB STA 75 APPROX. 10 INCHES FROM TRAILING EDGE IAW B737-800 SRM 55-10-01-2R-12.SDR DALA2025030401686Skin · cracked(LOG 0837185) L/H HORIZONTAL STABILIZER HAS CRACK ON LWR SKIN AT STAB STA 101.90 APPROX. 28 IN FROM T/E. REPAIRED L/H HORIZONTAL STABILIZER ON LWR SKIN AT STAB STA 101.90 APPROX 28 IN FROM T/E IAW B737-800 SRM 55-10-01-2R-12.
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