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 FDEA201009303806Skin · corrodedRIGHT THS TOP SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT S11 FOUND CORRODED BTW RIB 3 & RIB 4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.SDR SWAA105782Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR DALA1319389212Skin · crackedCRACKS FOUND IN THE HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL. REPAIRED IAW 02-460214-12, ME06 02-460214-12.SDR SWAA105754Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 105 TO STA 111. REPAIRED SKIN PER SRM.SDR CA100923005Skin · cracked(CAN) HORIZ STAB CTR SKIN CRACKED AT THE LIGHTNING HOLE BETWEEN THE 2 FWD STAB ATTACK POINTS. THIS SKIN MAKES UP THE CTR SECTION OF THE STABILIZER SPAR AND CARRIES STRUCTURAL LOADING. MFG HAS A REVISED PART FOR THIS SECTION THAT IS REINFORCED BUT WAS NOT INSSDR SWAA105765Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED AT STA 101.9 -6.5. REPAIRED SKIN PER SRM.SDR CA100916008Skin · gougedRT HORIZ STABILIZER L/E HAS A GOUGE ON THE LOWER SURFACE.SDR CA100923004Skin · crackedHORIZ STAB CTR SKIN CRACKED AT THE LIGHTNING HOLE BETWEEN THE 2 FWD STAB ATTACK POINTS. THIS SKIN MAKES UP THE CTR SECTION OF THE STABILIZER SPAR AND CARRIES STRUCTURAL LOADING. MFG HAS A REVISED PART FOR THIS SECTION THAT IS REINFORCED BUT WAS NOT INSTALLEDSDR CALA2010091700438Skin · crackedSUPPORT TASK. RT HORIZONTAL STAB HAS A 1" LONG CRACK IN THE LOWER SKIN STAB STA 101.9 I/B SIDE OF RIB. 27.5" AFT OF L/E OF SKIN PANEL AND 19.5" FWD OF AFT EDGE OF SKIN PANEL REPAIRED CRACK ON R/H HORIZONTAL STAB AND DAMAGED RIB PER ECRA# 5510-02120. PLACED ON SDR CALA2010091700437Skin · crackedSUPPORT TASK. RT HORIZONTAL STAB HAS A .75 INCH LONG CRACK IN THE LOWER SKIN STAB STA 101.9 I/B SIDE OF RIB, 8 INCH AFT OF DRAIN HOLE AND 10.5 INCH FWD OF AFT EDGE OF SKIN PANEL REPAIRED CRACK ON RT HORIZONTAL STAB PER ECRA#5510-02120. PLACED ON DIP TO ACCOMPSDR C2XA10SH294Skin · corrodedSHV - DURING C-CHECK LT HORIZONTAL STAB LEADING EDGE HAS CORROSION (LEVEL 2 LOCAL) AT UPPER AND LOWER SURFACE AROUND RIVETS. MAINTENANCE REMOVED CORROSION BY POLISHING THE HORIZONTAL STAB L/E IAW THE POLISHING TYPICAL REPAIR EC5530-01116 REV D. THE AIRCRAFT SDR UIEA201000205Skin · dentedDURING THE D02 PLUS C03, DENT DAMAGE ON THE LOWER SKIN WAS DETECTED AT STAB STA 156.0 OF THE LOWER SKIN 65B03500-143 AND DOCUMENTED IAW EGAT NRC 390. THE ACTION REQUIRED TO CLOSE EGAT NRC 390 WAS TO CUT THE DAMAGE OUT AND TO INSTALL A FLUSH REPAIR IAW REPAIR SSDR DALA1022569007Skin Panel · corrodedPITTING CORROSION ON BARREL NUT HOLE OF LT HORIZONTAL STAB UPPER FWD SKIN PANEL AT STA XH 28. REPAIRED PER AMR REPAIR DOCUMENT 0955141 AT HMV3 IN GDL ON N/R T0182701.SDR ASMF201009005Skin · dentedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON THE RT SIDE HORIZONTAL STABILIZER L/E. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DENT OF 12.00 X 3.50 INCHES, WITH 0.400 INCH DEPTH LOCATED IN STA 78.5. THE RT SIDE HORIZONTAL STABILIZER L/E WAS SDR DALA1022579007Skin · damagedPITTING CORROSION ON BARREL NUT HOLES OF RT HORIZ STAB UPPER FWD AND UPPER AFT SKIN PANELS 1 EA. REPAIRED IAW AMR DOCUMENT 0955141 BARREL NUT HOLE NR3 AND NR 26 ON T0182702 AT HMV3 IN GDL.SDR DALA1052709226Skin · dentedACFT MODIFIED IAW ERA484704-14, REV A, STABILIZER, HORIZONTAL, RT, LOWER SKIN PANELS REPLACEMENT.SDR ASMF201009003Structure · crackedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON THE RT SIDE HORIZONTAL STABILIZER L/E. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DENT WITH CRACK AND HOLE OF 6 X 3 INCHES LOCATED IN STA 321.67. THE RT SIDE HORIZONTAL STABILIZER L/E WAS REPLACED SDR SWAA105234Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 101.6. REPAIRED SKIN PER SRM.SDR FDEA201009053293Skin · misrepairedRIGHT HORIZONTAL STAB DRY BAY, STA XE 87, UPPER STRINGER NR 7 FOUND EXISTING REPAIR. EXISTING REPAIR. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR ACCOMPLISHED PER EA 8-5510-143416, REPAIR CLASSIFIED AS MASDR FDEA201009053288Skin · misrepairedEXISTING REPAIR FOUND ON RIGHT HAND HORIZONTAL STABILIZER UPPER SURFACE, ADJACENT TO REAR SPAR AT STA XE 84. EXISTING REPAIR AT RIGHT HAND HORIZONTAL STABILIZER UPPER SURFACE, ADJACENT TO REAR SPAR AT STA XE 84 EVALUATED, FOUND WITH SHORT EDGE MARGIN. RIGSDR REXA201000131Skin · dentedFLIGHT 4095, WAS PUSHED AT 19:14 OFF GATE B15 IN MSP WHEN 8903C WAS PUSHED INTO IT. THE VERTICAL STABILIZER AFT FAIRING OF 8932C HIT THE LEFT LEADING EDGE OF 8903A. THEN, AS 8932C WAS BEING PUSHED FARTHER, THE LEFT HORIZONTAL STABILIZER OF 8903A DRAGGED ALONSDR REXA201000127Skin · dentedDENT DISCOVERED IN LT HORIZONTAL STABILIZER L/E SKIN AT HSS 25.0 MEASURING 0.013 INCH DEEP X 0.80 INCH LONG X 0.70 INCH WIDE. REO 601R-55-12-487 ISSUED BY BOMBARDIER FOR A FLY ON "AS IS" FOR 5000FH, REPEAT DETAILED VISUAL INSPECTIONS EVERY 1200FH. PERMANENT SDR SWAA105179Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STAB 96.20 TO STA 98.95. REPAIRED SKIN PER ER AND EA.SDR DHLA201000110Skin · misrepairedPERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-11-10, EVA D85500374 REV IR DATED 09-28-10. REMOVED RUB PLATE IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED (3EA) FILLERS & INTERNAL REPAIR DOUBLER IAW DWG ES D85500374-001-D REV IR DATED 09-28-10. HEAT SDR DHLA201000103Skin · damagedREMOVED AND REPLACED EXISTING REPAIR LOCATED ON RT HORZ STABILIZER AT XE 159.000 UTILIZING APPROVED DATA (REF REPAIR REPORT HS002) PERFORMED MAJOR REPAIR IAW SRM 55-3-1, FIG 1, SHEET 1-2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICASDR UIEA201000208Skin · dentedDURING D02, C03 CHECK OF DATUM ACFT AT EGAT, DENT WAS FOUND ON LT HORIZONTAL STAB L/E LOWER SKIN OUTER SURFACE AT STAB STA 147. THE DETAILED LOCATION IS SHOWN IN FIG 1. EGAT PROPOSED TO REPAIR SRM 55-10-01, REPAIR 5 SRM, BUT SINCE THE SRM REPAIR IS A CATEGORY SDR SWAA105153Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SPAR SKIN CRACKED. REPAIRED SKIN PER SRM.SDR LR7A2010082600025Skin · crackedDURING SCHEDULED A CHECK FOUND LT HORIZONTAL STABILIZER LEADING EDGE CRACK AT HSS156-162. REPAIRED IAW LAC MEA 382-55-10-37.SDR ZZDA2010408Skin · damagedLEFT SIDE HORIZONTAL STAB SKIN AND STRUCTURE LEADING EDGE, DAMAGED. ACCOMPLISHED LEADING EDGE DOUBLER AND FILLER REPAIR PER EA 17-55-02506IR.SDR CALA2010081600391Skin · crackedRT SIDE HORIZONTAL STABILIZER LOWER IN SPAR SKIN HAS 2 INCH LONG CRACK AT STA 129.50. REPAIRED PER EC/RA 5510-02112 INITIATED DIP TO READ AS FOLLOWS ACCOMPLISH DETAILED VISUAL AND LFEC INSP PRIOR TO TOTAL A/C FLT CYCLES OF 22432 AND REPEAT THEREAFTER AT INTERSDR SWAA104754Skin · crackedDURING SCHEDULED 2HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 124.3. REPAIRED SKIN PER SRM.SDR SWAA104713Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 96.20 TO STA 101.90. REPAIRED SKIN PER EA.SDR SWAA104619Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 129.50. REPAIRED SKIN PER SRM.SDR IPXA10562159Skin · corrodedINSPECTION TYPE:C2, WHILE GIVING OK TO CLOSE ON LT HORZ STAB UPPER SEAL FAIRING, FOUND CORROSION ON UPPER STAB SKIN UNDER AERODYNAMIC SEALANT AT HSBL 43, 33" AFT OF FRONT SPAR. REPAIR IAW ER 10-3894.SDR IPXA10562158Skin · corrodedINSPECTION TYPE:C2, WHILE GIVING OK TO CLOSE ON LT HORZ STAB UPPER SEAL FAIRING, FOUND CORROSION ON UPPER STAB SKIN UNDER AERODYNAMIC SEALANT AT HSBL 45.5, 12" AFT OF FRONT SPAR. REPAIR IAW ER 10-3894, DATED 8-25-10.SDR FDEA201008032934Skin · crackedLT HORIZ STAB HAS PROTRUDING DENT AT ELEV STA 140 WITH CRACK INDICATION. CUTOUT DAMAGED AREA DIM .7500" X .7500" AND FABRICATED REPAIR DOUBLER FROM 2024-T3, 0.032" DIM. 3" X 3" IAW SRM 55-20-3, FIG 4. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIRSDR IPXA10562030Panel · puncturedINSPECTION TYPE:C3, RT HORIZ STAB LOWER INTERNAL SKIN IS PUNCTURED 6 INCHES FROM AUX SPAR BELOW OTBD LOGO LIGHT. REPAIRED RT HORIZ LOWER PANEL INNER SURFACE SKIN IAW ER 10-3874.SDR SWAA104500Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.SDR SWAA104367Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 142. REPAIRED SKIN PER SRM.SDR SWAA104342Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA201007262669Skin · misrepairedEXISTING FLUSH REPAIR AT RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN XFS 289. EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT AS PER E.A. 8-5510-132438. E.O. 8-5100-7-5001 A7 PART 2, REPAIR CLASSIFIED AS MAJOR SDR WX0A070577Skin Panel · damagedTOP OF RT HORIZONTAL I/B LEADING EDGE PANEL GOUGED AND DENTED XHR 1.152 - XHR 27.234. ACCOMPLISHED PERMENANT REPAIR PER AAR EA 14064 REV 1/R DATED 21/JUL/2010.SDR DALA1020109004Skin · corrodedCORROSION ON BARREL NUT 2EA OF RT HORIZONTAL STABILIZER UPPER SKIN STA XH=27 REF NRC T0180054 VHS MRB 55-056-02. REPAIR WAS ACCOMPLISHED IAW AMR 0955139, REV1 AND ERA 483916-14 REV ORIG.SDR SWAA104191Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.SDR SWAA104190Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.SDR SWAA104189Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.SDR SWAA104188Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.SDR SWAA104177Skin · crackedDURING SCHEDULED 2HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 147.90. REPAIRED SKIN PER EA.SDR SWAA104140Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER CRACKED. REMOVED AND REPLACED SKIN PER SRM.SDR SWAA104139Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED. REMOVED AND REPLACED SKIN PER SRM.
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