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 IXXA07SMN129SPanel · corrodedDURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER, T/E LWR PANEL, CORRODED STA XE 149.906 - STA XE 220.343. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-3-1 FIG 1, SHEET 1 AND 2. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DSDR IXXA07SMN110SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER PANEL HAS CORROSION, STATION XE 221.000 AND XE 272.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDSDR 2007FA0000194Skin · corrodedLT AND RT HORIXONTAL STABILIZER LEADING EDGES HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. THIS AREA HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY. (K)SDR DLM88070145Skin · crackedFOUND FATIGUE CRACK IN UPPER AFT SKIN ON LT HORIZONTAL STABILIZER. ACCOMPLISHED BAC APPROVED STOP DRILL REPAIR.SDR DLM88070144Skin · crackedHORIZONTAL STAB RT UPPER AFT SKIN, INBD AFT EDGE HAS CRACK REPAIR. THE UPPER AFT SKIN OF THE RT HORIZONTAL STAB WAS FOUND WITH A 1.25" CRACK AT THE INBD, AFT EDGE OF THE PANEL. THE CRACK WAS HFEC INSPECTED AND STOP DRILLED ON A TIME-LIMITED BASIS. THE PERMASDR DLM88070133Skin · crackedDURING LETTER CHECK, THE HORIZONTAL STABILZIER UPPER AFT SKIN PANEL WAS FOUND WITH A FOUR INCH CRACK AT THE INBOARD AFT EDGE (RHS). THE UPPER SKIN PANEL WAS REPLACED, REF 460111-14.SDR DLM8K070132Skin · crackedDURING LETTER CHECK, THE RHS HORIZONTAL STABILIZER UPPER AFT SKIN PANEL WAS FOUND CRACKED AT THE INBOARD AFT END. THE PART WAS REPLACED PER BOEING RECOMMENDATION AS NO FEASIBLE REPAIR CURRENTLY EXISTS. DOCUMENTED ON ER/A 460015-14.SDR 68DASkin · wrinkledDURING ROUTINE MAINTENANCE, MECHANIC DISCOVERED THAT THE HORIZONTAL STABILIZER SKIN WAS WRINKLED AT THE AFT RT ATTACH PIVOT POINT.SDR 07FDEA00403Skin · misrepairedPREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUNDSDR 07FDEA00401Skin · misrepairedPREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND SDR IXXA07SMN099SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER. LEADING EDGE OUTER SKIN NON STANDARD REPAIR AT STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA.. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FASDR IXXA07SMN094SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER.- LEADING EDGE OUTER SKIN NON STANDARD REPAIR AND CORROSION AT STATION XFS 178.750. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGESDR IXXA07SMN093SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER. UPPER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR, AND REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSSDR IXXA07SMN092SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 47.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK OR CORROSION FOUND. FABRICATED NEWSDR 2007UALA00348Skin · crackedRIGHT STAB LOWER SKIN CRACKED AT LOWER SKIN AT REAR SPAR FASTENER FWD OF ACCESS PANEL 9028 APPROX STAB STA 153 AND BETWEEN ELEV STA 94.07 AND 121.59. MAJOR REPAIR. REMOVED DAMAGE. ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER SRM 55-10-01 REPAIR 6 PAGE 201 TSDR SWAA070663Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR STA 87. REPAIRED SKIN PER SWA EA.SDR NACA20070009Skin · damagedFOUND LT HORIZONTAL STAB LOWER SURFACE DAMAGED, "HAS HOLE". REPAIRED DAMAGED AREA PER JOSSAIR DRAWING NR 73R5511546 REV A DATED 21 FEB 2007. "CUTOUT REPAIR AT STABILIZER BOTTOM SKIN-STAB STA 111.0-STA 120.0".SDR 07FDEA00238Skin · gougedRT HORIZ STAB OUTBD BALANCE BAY PANEL UPPER SKIN, PANEL IS GOUGED ON INNER SURFACE OUTBD SIDE. REMOVED EXISTING DOUBLER, VERIFY NO DAMAGE NOTED. FABRICATED, TREATED AND PRIMED, AND REINSTALLED REPAIR. REF SRM 55-20-3 FIG 7 SHEET 1, PG 4.SDR COMA0770011Skin Panel · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN HAS A 3 INCH CRACK EMINATING O/B FROM THE O/B LOWER DRAIN HOLE O/B OF RIB 11. REPAIRED DAMAGE IAW GENERIC REO 670-55-11-001.SDR ASAA0741422Skin · damagedLEFT STABLIZER I/B LEADING EDGE PANEL IS CREASED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PLATE AND FILLER IAW SRM 55-10-01 FIGURE 201 REPAIR 2.SDR 2007UALA00192Skin · crackedLEFT HORIZ STAB LOWER SKIN CRACKED AT AFT SPAR APPROX 70 INCHES FROM ROOT. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR PER MM 55-10-94 PAGE 801.SDR CA070510002Skin · delaminated(CAN) FOUND DELAMINATION (OF 8 INCH X 16 INCH) ON TOP OF LT SIDE IB HORIZONTAL STABILIZATOR. DELAMINATION FOUND WHEN DOING PHASE 2 AND 3 INSPECTION. HORIZONTAL STABILIZATOR REPLACED, NO REPAIR IS ALLOWED ON HORIZONTAL STABILIZATOR IAW SRM. (TC NR 2007051000SDR 2007UALA00106Skin · crackedRT HORIZ STAB LOWER SKIN IS CRACKED AFT SPAR, APPROX 72" FROM INBD EDGE IS CRACKED. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL SKIN DOUBLER REPAIR PER MM 55-10-94 AND TWO ACCESS HOLE DOUBLER REPAIR PER SRM 55-10-01 REPAIR 6.SDR 07FDEA00107Skin · crackedFOR CUSTOMER REQUEST, HORIZONTAL STAB UPPER INTERIOR SKIN PANELS, FOUND CRACKED PANELS P/N7228-1, POSITION 6 AND 7 AND PANEL P/N7229-1 POSITION 2, SEE ATTACHING MAP FOR DETAIL. REMOVED AND REPLACED PANELS ALC7228-1 AND ALC7229-1 IAW SB55-16 GROUP 2 FOLLOWING SDR 07FDEA00106Skin · crackedDURING U/S INSP OF HORIZ STAB COSTANT AND OUTER SECTION SKIN PANEL, FOUND CRACKED PANEL: P/N7228-1, POSITION 6&7, P/N7229-1 POSITION 2 AND P/N7226-1 POSITION 18, SEE ATTACHED SHEET FOR DETAIL, POSITION 6, 7 AND 2 CRACKS ARE HANDLED BY NRC N00628. POSITION 18 SDR ASAA0741390Skin · dentedTHE LT HORIZ STAB LE WAS DROPPED DURING INSTALLATION RESULTING IN A SKIN DENT AT TWO EXITING REPAIRS. REMOVED THE TWO EXITING REPAIR DOUBLERS AND FILLERS CUTOUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 55 10 0SDR SWAA070213Skin · corrodedDURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STAB UPPER SKIN CORRODED AT REAR SPAR STA 198. REMOVED AND REPLACED HORIZONTAL STAB PER MM.SDR SWAA070206Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR STA 125. REPAIRED SKIN PER SRM.SDR SIMA200701509Skin · puncturedLEFT HORIZONTAL STABILIZER LOWER SKIN PUNCTURED. REMOVED AND REPLACED SKIN IAW SAAB SDS 011469, DATED 7 JANUARY 2007. RETURNED AIRCRAFT TO SERVICE.SDR ASAA0741378Skin · dentedTHE LEFT HORIZONTAL STAB L/E SKIN IS DENTED OUT OF LIMITS AT L/E STA 92. CUT OUT THE DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND INTERNAL REPAIR DOUBLER IAW SRM 55-10-01 FIG 201.SDR ASAA0741371Skin · dentedTHE LEFT HORIZONTAL STABLIZER L/E SKIN IS DENTED OUT OF LIMITS AT L/E STA 98. CUT OUT THE DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND INTERNAL REPAIR DOUBLER IAW SRM 55-10-01 FIG 201.SDR UPS07848845Skin · crackedINSPECTION TYPE:C2 LT HORIZ STAB L/E UPPER SKIN CRACKED AT STA XFS 60. CUT OUT DAMAGED AREA ON HORIZ STAB LT L/E UPPER SKIN AT STA XFS 60 IAW SRM 55-02-01-0 FIG 4. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER ON LT HORIZ STAB L/E UPPER SKIN STA XFS 60 SDR 07FDEA00006Skin · dentedLT HORIZONTAL STAB LEADING EDGE O/B SECTION NR 331FT FOUND WITH DENT ON O/B EDGE. FOUND OUT OF LIMIT AS PER SRM 55-00-01 VOL. I. DEPTH= 0.080", WIDTH= 2". REPAIR CARRIED OUT AS PER SRM 55-20-00 FIG. 5 VOL. I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR IXXA06SMN432SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN INTERNAL SURFACE CORRODED FROM STATION XE195 2190 TO STATION XE221.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN PANEL. FABRICATED NEW SKIN PANEL AND STIFFSDR IXXA06SMN431SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN INTERNAL SURFACE CORRODED FROM STATION XE272.000 TO STATION XZ297.2347. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATESDR IXXA06SMN429SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE219.919 TO STATION XE221.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED PANEL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREASDR IXXA06SMN428SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED AT STATION XE77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW SDR IXXA06SMN427SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED AT STATION XE28.843. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW SDR 06FDEA04207Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 02 CORROSION REWORK FOUND EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04202Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 19 CORROSION REWORK FOUND OUT OF LIMIT PER EO 1-5510-7-5000 D1 PT1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR SWAA064749Skin · crackedDURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB SKIN CRACKED AT REAR SPAR STA 66.54. REPAIRED SKIN PER SRM.SDR 06FDEA04125Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 30 CORROSION REWORK FOUND EXCEEDED LIMITS PER EO1-5510-7-5000 D1 PT 1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04124Panel · corrodedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 28 CORROSION REWORK FOUND EXCEEDED LIMITS PER EO1-5510-7-5000 D1 PT 1. REPAIRED AS PER EA 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04112Skin · damagedHORIZONTAL STAB CONSTANT SECTION LT BARREL NUT HOLE NR 17 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT 1. REPAIRED AS PER E.A. 1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA04111Skin · damagedHORIZONTAL STAB CONSTANT SECTION RT BARREL NUT HOLE NR 6 REWORK FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 D1 PT 1. REPAIRED AS PER E.A.1-5510-106546. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 2006UALA02209Skin · damagedLIGHTNING STRIKES LT HORIZONTAL STABILIZER UPPER SURFACE, INBOARD END. INSTALLED COMPOSITE REPAIR PER REO-G10674A. REPAIR IS CONSIDERED TEMPORARY. MUST BE REINSP. EVERY 500 CYC, WITH M AX LIMIT 3000 CYC. MF4982 CREATED TO MONITOR. SANDED & REMOVED PSDR IXXA06SMN413SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE221.000 TO STATION XE270.979. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS. CLEANED, TSDR IXXA06SMN412SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN CORRODED FROM STATION XE221.000 TO STATION XE270.979. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS CLEANED, TREATSDR IXXA06SMN411SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN CORRODED FROM STATION XE272.000 TO STATION XE301.656. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRSDR IXXA06SMN410SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE29.812 TO STATION XE52.825. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW
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