JASC 5512
Service difficulty reports · 7,887
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 ASAA0995146Skin · crackedLT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 101.9, 37 TO 38 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.SDR ASAA0995145Skin · crackedLT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 175 26 INCHES TO 27.5 AFT FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.SDR ASAA0995150Skin · crackedLT HORIZONTAL STAB CRACKED STAB STA 101.9 TO 28 TO 29 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.SDR ASAA0995149Skin · crackedRT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 147.9 TO 32 - 25 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.SDR ASAA0995148Skin · crackedRT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 141.2 TO 144.7. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.SDR ASAA0995147Skin · crackedRT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 101.9, 28 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.SDR ASAA0945189Skin · gougedLT HORIZONTAL STAB L/E GOUGED STA 190.34. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED PLATE AND FILLER IAW B737 400 SRM 55 10 01.SDR ASAA0945188Skin · gougedLT HORIZONTAL STAB L/E GOUGED STA 218.43. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR FILLER IAW B737 400 SRM 55 10 01.SDR ASAA0945187Skin · gougedLT HORIZONTAL STAB L/E GOUGED STA 229.13. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737 400 SRM 55 10 01.SDR ASAA0945184Skin · gougedLEFT HORIZONTAL L/E GOUGED STA 139.55. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737 400 SRM 55 10 01.SDR ASAA0945112Skin · gougedLT HORIZONTAL STAB L/E IS GOUGED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PLATE AND FILLER IAW B737 400 SRM 55 10 01.SDR ASAA0995033Skin · dentedLT HORIZONTAL STAB LEADING EDGE PREVIOUSLY REWORKED DENT ON I/B REMOVABLE LEADING EDGE SEGMENT AT L/E STA 113. REPAIRED LT HORIZONTAL LEADING EDGE.SDR DALA1317499208Skin · crackedRIGHT STABILIZER UPPER SKIN INBD FOUND CRACKED 1.2500" LONG. REPAIR IAW 02-460214-12 ME06.SDR DALA1317489208Skin · crackedLEFT STABILIZER UPPER SKIN WAS CRACKED 1.2500" LENGTH INBD AFT END. REPAIR IAW 02-460214-12 ME05 (02-460214-12).SDR ASAA0955003Skin · dentedRT HORIZONTAL STAB L/E DENTED. CUT OUT DAMAGE, REPAIRED PER SRM 55 10 01.SDR C2XA09SH106Skin · corrodedSHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE ON HORIZONTAL STABILIZER RT LEADING EDGE WITH POLISHING PROCEDURE IAW EC5SDR C2XA09SH105Skin · corrodedSHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVETS AND COMPLETED POLISHING PROCEDURES ON LT LEADING HORIZONTAL EDGE IAW EMB-145 EC5530-01116 REV D - 80 PESDR 22AA20090504Skin · damagedRT SIDE OTBD AT HORIZONTAL STABILIZER TRAILING EDGE UPPER AND CENTER SECTION UPPER DAMAGE PERFORATION DUE TO NR 2 ENGINE DEBRIS. REFERENCE N/R NR 007. EWO'S ARW 55-001, ARW 55-002, ARW 55-003 WERE ACCOMPLISHED AT OTBD SECTION OF RT HORIZONTAL STABILIZER AND SDR 22AA20090503Panel · puncturedDURING INSPECTION WAS FOUND A PUNCTURE ON HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 344 - 461 RT DUE NR 2 ENGINE DEBRIS. HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 344 - 461 PUNCTURE RT REPAIR WAS ACCOMPLISHED IAW IAAC EO ARW-090414 BY TAMPA CARGSDR 22AA20090502Panel · puncturedDURING INSP, FOUND A PUNCTURE ON HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 247 - 344 RT DUE NR 2 ENGINE DEBRIS. HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 247 - 344 PINCTURE RT REPAIR WAS ACCOMPLISHED IAW IAAC EO ARW-090413.SDR ASAA0944908Skin · dentedRT HORIZONTAL STABILIZER L/E IS DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 55 10 01.SDR USAA2009032790702Skin · crackedCLT - MAJOR REPAIR - C4 CHECK - LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED, AFT SPAR STATION 100. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN, AFT SPAR STATION 100 IAW US AIRWAYS TYPICAL REPAIR 55-10-07 REV D.SDR DU4R2009338Panel · dentedDURING SCHEDULED INSPECTION FOUND RT HORIZ STAB L/E PANEL 9250L HAD NUMEROUS HAIL DENTS.SDR ASAA0944862Skin · dentedLT HORIZONTAL STAB L/E DENTED OUT OF LIMITS. REPAIRED LT HORIZONTAL STAB L/E PANEL AT THE 10TH RIB FROM THE O/B END.SDR MALA090043Skin · dentedDURING 30K AND 6Y INSPECTIONS, DENT IN LOWER SKIN OF LT HORIZONTAL STAB 6 INCH FROM FUSELAGE, 5 INCH FROM FWD EDGE OF SKIN. REPAIRED.SDR MALA090038Skin · dentedDURING 30K AND 6Y INSPECTIONS, DENT IN LOWER SKIN OF RT HORIZONTAL STAB 4.5 INCH FROM AFT EDGE AND HS131.67. REPAIRED.SDR ASAA0944825Skin · dentedRT STABILIZER LEADING EDGE HAS DENT. REPAIRED RT STABILIZER LEADING EDGE DENT.SDR FDEA200903161432Skin · corrodedTHS - SUPERFICIAL CORROSION AT BASE OF HOLES NR 2 AND NR 3 OF GROUP A, RT SIDE. CORROSION BLENDED OUT AS PER EA 6-5510-127414.SDR DLM88090413Skin · corrodedTHE RT HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL HAD CORROSION ON 3 INBD BARREL NUT HOLES AT XH=7.234. THE NR 12, NR 14, AND NR 17 HOLES WERE OVERSIZED, AND THE NR 17 HOLE HAD AN ADDITIONAL BLEND FOR CORROSION. OVERSIZED BUSHINGS WERE INSTALLED PER BOEINSDR CALA2009031100137Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SURFACE SKIN HAS 2 CRACKS AT STATION 129.50, 17 AND 26 INCHES AFT OF FRONT SPAR. REPAIRED PER ECRA 5510-01979. DIP GENERATED ON L/P 9705135.SDR CALA2009031100136Skin · crackedLOWER SURFACE OF LEFT HORIZONTAL STABILIZER SKIN IS CRACKED AT STATION 129.50, 26 INCHES AFT OF FWD SPAR. REPAIRED LEFT HORIZONTAL STAB SKIN PER ECRA 5510-01978.SDR SWAA091625Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 120. REPAIRED SKIN PER SRM.SDR 2009FA0000215Skin · debondedDURING THE SID INSP, FOUND AREA OF DE-BOND IN HORIZONTAL STABILIZER. REPAIRED DE-BOND AREA BETWEEN PN 5732133-2, STRINGERS AND HORIZONTAL STABILIZER LOWER SKIN PANEL PN 5732130-17 AND -18 IAW FORM 8110-3 INSTRUCTIONS. THIS DE-BONDING WOULD NOT HAVE BEEN FOUNSDR ASAA0944680Skin · dentedLT HORIZONTAL STABILIZER L/E HAS DENT WITH POSSIBLE BENT STRUCTURE AT APPROX 110 INCHES FROM O/B EDGE OF O/B LEADING EDGE. REMOVED RIB & REWORKED DENT. HFEC INSPECTION IS OK. REPAIRED L/E DENT BY INSTALLING EXTERNAL DOUBLER IAW SRM 55 10 01 REPAIR 3 EA 400 SDR CA090303003Skin · cracked(CAN) CRACK FOUND IN UPPER SKIN OF THE STABILIZER.SDR UALA2009030300701Cap · damagedLIGHTNING STRIKE DAMAGE TO LT HORIZ STAB CAP. STAB T/E WEDGE IN SHOP 321.SDR DLM88090615Skin · crackedTRANSFERED FROM OMI, RT HORIZ STAB UPPER SKIN INBD PANEL CRACKED. CRACKED SKIN WAS REMOVED AND REPLACED IAW ERA 461288-14D REV B.SDR C2XA09SH058Skin · corrodedSHV - DURING C-CHECK RT HORIZ STAB L/E HAS CORROSION AROUND RIVET HEADS ON UPPER SIDE. MAINTENANCE REMOVED CORROSION AND COMPLETED RT HORIZ STAB L/E RIVET CORROSION REPAIR IAW EC5510-01201. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH057Skin · corrodedSHV - DURING C-CHECK LT HORIZ STAB L/E HAS CORROSION AROUND RIVET HEADS ON UPPER SIDE (MARKED). MAINTENANCE REMOVED CORROSION AND COMPLETED REPAIR OF LT HORIZ STAB UPPER SURFACE BY INSTALLING RIVETS IAW EC5510-01201. THE AIRCRAFT WAS APPROVED TO RETURN TO SESDR CALA2009021900100Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN HAS A 1.0625 INCH CRACK LOCATED AT STAB STATION 138.0, 24.2812 INCH AFT OF FRONT SPAR. REPAIRED PER ECRA 5510-01972.SDR SWAA091119Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED AT BS 129, FWD OF AFT SPAR. REPAIRED SKIN PER SRM.SDR SWAA091077Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 138. REPAIRED SKIN PER SRM.SDR SWAA091051Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 138. REPAIRED SKIN PER SRM.SDR UPS09554636Skin · dentedINSPECTION TYPE:N/A 2.5 X 1.0 X .015 INCH DENT IN LT HORIZ STAB 9.25 INCHES AFT OF AUXILIARY SPAR AND 86.0 INCHES OUTBOARD OF FUSELAGE. REPAIRED PER EO B757-5510-31270-B.SDR SWAA090914Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED. REPAIRED SKIN PER AAR EA.SDR SWAA090802Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT BS 198. REPAIRED SKIN PER SWA EA.SDR IPXA09856151Skin · misrepairedINSPECTION TYPE:SV SS 852-S1-06, LT HORIZ STAB L/E REPAIR AT XFS 210 HAS RIVET SPACING LESS THAN 4D ON FILLER. REPAIRED PER TIMCO REO-G12780 REV B, AND UPS EO DC8-5510-33643-A.SDR ASAA0944364Skin · dentedLT HORIZONTAL STAB DENTED 100" FROM IB END. REPAIRED LT HORIZONTAL STAB LEADING EDGE.SDR UPS09554489Skin · damagedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN IS DENTED AND GOUGED 15 INCHES FROM SPAR AND 80 INCHES FROM FUSELAGE. REPAIRED SKIN PER SRM 51-70-10-2R-2 PAR 4D CONTROL 09-1327.SDR IPXA09855410Skin · damagedINSPECTION TYPE:SV DOUBLER DRILLED HOLE FOR DE-ICER RIVET (2594254) BETWEEN STA 191.250 & STA 185.00 RT O/B HORZ STAB. FABRICATED REPAIR STRAP IAW REO G12602. INSTALLED REPAIR REF REO-G12602.
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