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 C2XA09SH043Skin · corrodedSHV-DURING C-CHECK LT HORIZONTAL STAB L?E UPPER SURFACE HAS MULTIPLE RIVETS WITH CORROSION. MX REMOVED CORROSION IAW EC5510-01199 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR IPXA09855512Skin Panel · unknownINSPECTION TYPE:SV SS 814-S2-12, RT HORIZ STAB T/E UPPER PANEL AT XE 142. SUPPORTING DATA FOR THE REPAIR WAS UNAVAILABLE. ACCOMPLISHED NEW REPAIR PER TIMCO REO-G12709 REV C, AND UPS EO DC8-55 10-33097A.SDR IXXA09SMN023SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 83.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND STIFFENERS. CLEANED, TREATED, PRIMED ARESDR IXXA09SMN012SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND HORIZONTAL STABILIZER LOWER FORWARD PANEL WITH STIFFENER CRACKED AT RIGHT BOTTOM LINE-10. REMOVED CRACKED SKIN. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SKIN IAW S/B 55-15 REV 3 CONDITIONS 4, SRM 55-1-0 PAGE SDR IPXA09855497Skin Panel · misrepairedINSPECTION TYPE:SV SS 814-S2-05, RT HORIZONTAL STAB L/E UPPER SKIN PANEL AT STA XFS 178, REPAIR DOUBLER DOES NOT CORRELATE TO A SRM REPAIR. ACCOMPLISHED PER TIMCO REO-G12703 REV C, AND UPS EO DC8-5320-33065A.SDR UPS09654398Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL SURVEY SEQ 305-S1-12 TO 16 EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.SDR UPS09654397Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.SDR UPS09654396Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.SDR UPS09654395Skin Panel · misrepairedINSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 203.SDR UPS09654394Skin Panel · debondedINSPECTION TYPE:C EMP - RT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH DISBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.SDR FDEA200901150204Stringer Splice · corrodedLEFT HORIZONTAL STAB FRONT SPAR INBD END OF THE INTERNAL STRUCTURAL STRINGER NR 1 SPLICE IS CORRODED. REMOVED CORROSION REF SRM 51-74-10. OUT OF LIMITS REF SRM 55-11-28. REMOVED APRON SUPPORT FITTING & STRINGER SPLICE REF SRM 51-40-21; PARAGRAPH 7. MACHINSDR CALA2009011500039Skin · crackedLEFT HORIZONTAL STABILIZER CRACKED AT STATION 147.90 APPROXIMATELY 10 INCHES AFT OF FRONT SPAR. FABRICATED AND INSTALLED FILLER AND DOUBLER PER ECRA 5510-01961. DIP GENERATED ON LOG PAGE 9703646.SDR IPXA09855355Skin · misrepairedINSPECTION TYPE:SV LT HORIZ STAB LOWER SKIN DOUBLER AT XE 69.00 MINIMUM REPAIR FASTENER SPACING LESS THAN 4D AND FASTENERS DEFORMED AS MARKED. FABRICATE DOUBLER IAW DC8 SRM 5510-001. INSTALLED PANEL IAW DC8 51-1-2 1A.SDR C2XA09SH007Skin · corrodedSHV DURING C-CHECK LT HORIZONTAL STAB LEADING EDGE CORRODED AROUND ALL EXTERNAL SKIN RIVET HEADS. MX REPAIRED LT HORIZONTAL STAB LEADING EDGE SKIN IAW IC2008-145/09800. THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH006Skin · corrodedSHV DURING C-CHECK RT HORIZONTAL STAB LEADING EDGE CORRODED AROUND ALL EXTERNAL SKIN RIVET HEADS. MX REPAIRED RT HORIZONTAL STAB LEADING EDGE SKIN AROUND ALL EXTERNAL SKIN RIVET HEADS IAW IC 2008-145/09800. THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR UPS09B54303Skin · dentedLT HORIZONTAL STAB L/E HAVE 3 DENTS BEYOND SRM LIMTS. OPENSDR NWAA09115639Panel · damagedDURING LINE INSP, FOUND DAMAGE TO RT HORIZONTAL STABILIZER LWR PANEL ASSY. REPAIRED IAW EA 56-215120 SEC I. SECTION II REQUIRES INSPECTION AT 12 MONTH INTERVALS. SECTION III REQUIRES MFG TOLERANCE ANALYSIS APPROVAL WITHIN 24 MONTHS OF SECTION I REPAIR. (K)SDR SWAA090056Skin · crackedDURING SCHEDULED HC2 CHECK , FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 111. REPAIRED SKIN PER SRM.SDR C2XA09SH001Skin · corrodedDURING C-CHECK, CORROSION AROUND RIVETS ON LT HORZ STAB L/E. REPAIRED LT HOR. STAB L/E IAW EC5510-01196. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASAA0944320Skin · dentedRAMP REPORTED DENT ON RT HORIZ STAB LE STA 181. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR SKIN SPLICE PLATE B737 400 SRM 55 10 01 REPAIR 12 FIG 204.SDR DU4R2008285Skin · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION IN SEVERAL AREAS OF UPPER SURFACE SKINS ON LT HORIZONTAL STABILIZER.SDR FDEA200812265309Skin · corrodedEMPENNAGE, RIGHT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING NR 347DF LOWER MATING SURFACE FOUND WITH SURFACE CORROSION. SURFACE CORROSION ON EMPENNAGE RT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING 347DF LOWER MATING SURFACE REMOVED AS PER SRM 51-21-01 VSDR CALA2008121901154Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.5, APPROXIMATELY 18 INCHES AFT OF FRONT SPAR INBOARD SIDE OF RIB. INSTALLED INTERIM REPAIR ON LEFT HORIZONTAL STAB LOWER INBOARD SPAR SKIN STATION 129.5. REF ECRA 5510-01955, LOG 9702589 FOR DIP (5SDR ASAA0944153Skin · dentedRT HORIZ STAB AT STA101 HAS A DENTS ON THE LEADING EDGE. REMOVED PREVIOUS REPAIR FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 55 10 01.SDR ASAA0944152Skin · dentedRT HORIZ STAB AT STA 92.7 HAS 2 DENTS ON THE LEADING EDGE. REMOVED PREVIOUS REPAIR FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 55 10 01.SDR ASAA0844036Skin · dentedRT STABILIZER LEADING EDGE SKIN HAS DENT ON STA 243 TO STA 254. REMOVED DAMAGE SECTION OF SKIN AND INSTALLED EXTERNAL DOUBLER WITH BLIND FASTENERS PER SRM 55 10 01 REPAIR 3.SDR CALA2008120901133Skin · crackedRIGHT HORIZONTAL LOWER SKIN FWD OF AFT SPAR AT STAB STATION 129 .50 HAS 3 INCH CRACK. REMOVED DAMAGE SECTION OF SKIN, INSTALLED REPAIR DOUBLER PER ECRA 5510-01954.SDR CA081218001Skin · cracked(CAN) DURING ROUTINE MAINTENANCE, A 1 1/2 INCH LONG CRACK WAS NOTICED IN THE LEADING EDGE OF THE HORIZONTAL STABILIZER. TAP TESTING INDICATED POSSIBLE DELAMINATION, SO THE STABILIZER WAS REMOVED FROM AIRCRAFT AND SENT TO COMPOSITE REPAIR SHOP (XU AVIATION) FOSDR FDEA200812065098Skin · misrepairedFOUND RT STAB UPPER EXTERNAL REPAIR LOCATED AT APPROX SS 180, 6 INCHES FWD OF AFT EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DOES NOT COMPLY WITH CURRENTS SRM REPAISDR FDEA200812065097Skin · misrepairedFOUND RT STAB UPPER SURFACE EXTERNAL REPAIR LOCATED AT APPROX SS 145 8 INCHES FWD OF AFT EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA FOUND REPAIR DOES NOT COMPLY WITH CURRENT SRM RESDR SWAA086835Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED AT REAR SPAR, BS 125, FWD OF PANEL 9107L. REPAIRED SKIN PER SRM.SDR SWAA086834Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED AT REAR SPAR, BS 97 FWD OF PANEL 9106L. REPAIRED SKIN PER SRM.SDR C2XA08SH155Skin · corrodedLT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. LT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08SH154Skin · corrodedRT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. RT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR SWAA086731Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 142. REPAIRED SKIN PER SWA EA.SDR FDEA200811285002Skin · crackedRT HORIZONTAL STAB FRONT SPAR CAP AND UPPER PORTION OF THE SKIN CRACKED AT STA XF 88.834, (N/R 513 GENERATED WO 43105). INSTALLED RT HORIZONTAL STAB FRONT SPAR CAP REPAIR IN REF TO SRM 55-20-00 PG 42 FIGURE 8 CAT A REPAIR.SDR HALA2008112600876Skin · corroded11 AREAS OF LEVEL 11 CORROSION, ON HORIZONTAL STABILIZER UPPER SURFACE OF CENTER SECTION SKIN. REWORKED IAW AIRNZ TI 190120092-0001.SDR SWAA086278Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT BS 138. REPAIRED SKIN PER SRM.SDR HALA2008111300848Skin · corrodedHORIZONTAL STABILIZER CENTER SECTION LOWER SKIN EXTERNAL SURFACE CORRODED AT LBL 3.3 AND RBL 6.5 AT REAR SPAR. BLEND REPAIR IAW SRM 55-10-01 FIG 101 AND ANZ TI 190119901-0001.SDR C2XA08SH134Rivet · corrodedDURING C-CK LT HORIZONTAL STAB L/E HAS NUMEROUS RIVETS WITH CORROSION UPPER AND LOWER SURFACE. MX REMOVED AND REPLACED AFFECTED RIVETS ON LT HORIZONTAL STAB L/E UPPER AND LOWER SURFACE IAW EC5510-01192. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR 08FDEA04647Skin · dentedRIGHT HORIZONTAL STAB UPPER SURFACE HAS A DENT. CHECKED THE DEPTH OF THE DENT. FOUND TO BE 0.059 DEEP WITH NO CRACKS. DENT IS IN LIMITS PER SRM 51-80-01; PG 2; PARA 1; VOL II. ALODINED, PRIMED AND PAINTED PER SRM 51-21-01, PGS 21-24, VOL II AND SRM 51-21-0SDR FDEA200810304625Skin · crackedDURING U/S INSP OF HORIZ STB, FOUND UPPER INTERIOR SKIN PANELS PN 7229-1, PN 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS, INSP FINDING FORM FOR DETAIL. ACCOMPLISHED EA NR 8-5510-125425.SDR SWAA085952Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABLIZER ELEVATOR SKIN CRACKED AT BS 129, AFT OF LEADING EDGE. REPAIRED SKIN PER SRM.SDR SWAA085951Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABLIZER ELEVATOR SKIN CRACKED AT BS 101, AFT OF LEADING EDGE. REPAIRED SKIN PER SRM.SDR 08FDEA04625Skin · crackedDURING U/S INSP OF HORIZONTAL STAB, FOUND UPPER INTERIOR SKIN PANELS P/N 7229-1, P/N 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS,SDR UPS08854055Doubler · damagedINSPECTION TYPE:SV LT HORIZ STAB L/E HAS DOUBLER UNABLE TO VALIDATE PER SRM. INSTALLED NEW DOUBLER AS PER 55-2-1 FIG 4.SDR SWAA086101Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 161.9. REPAIRED SKIN PER EA.SDR USAA920081981Skin · crackedCLT RON MAJOR REPAIR LOG NR 4371367 RT HORIZONTAL STABILIZER LOWER SURFACE HAS A CRACK FORWARD OF CENTER ELEVATOR BALANCE PANEL AT AFT SPAR. REPAIRED RT HORIZONTAL STABILIZER LOWER SURFACE IAW US AIRWAYS TYPICAL REPAIR NR 55-10-07 REV D.SDR SWAA085858Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 175, AFT OF L/E. REPAIRED SKIN PER SWA EA.SDR SWAA085857Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 147, AFT OF L/E. REPAIRED SKIN PER SWA EA.
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