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 IXXA06SMN409SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED FROM STATION XE77.000 TO STATION XE147.906. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYISDR IXXA06SMN395SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE CRACKED AT STATION XFS47.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND RSDR IXXA06SMN394SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE SKIN CORRODED AT STATION XE198.0039. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. ASDR IXXA06SMN389SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE272.000 TO STATION XE301.656. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRISDR 2006UALA02193Skin · crackedRT HORIZ STAB HAS LOWER EXTERNAL SKIN CRACK AT REAR SPAR, 68" OB OF IB END. MAJOR REPAIR: INSTALLED ACCESS HOLE DOUBLER REPAIR PER SRM 55-10-01 REPAIR 6. INSTALLED LOWER SKIN DOUBLER PER MM 55-10-94 PG 801.SDR VNAA0611025Skin · damagedCREW REPORTED A LIGHTNING STRIKE. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND HORIZONTAL STABILIZER TIP. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.SDR 2006UALA02182Skin · damagedRH HORZ STAB LOWER SPAR SKIN BETWEEN STA. 207.7 AND 234.5 IS DAMAGED. MAJOR REPAIR: REMOVED DAMAGE. REPAIRED PER BOEING MESSAGE 1-243907360-3.SDR 06FDEA03995Skin · unknownRT STAB UPPER SURFACE, STA APPROX 4" FROM I/B END T/E, EXTERNAL 3" DOUBLERS, REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. REMOVED EXISTING REPAIR ON RT HORIZ STAB UPPER SURFACE AND RESDR IXXA06SMN359SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED FROM STATION XE52.822 TO STATION XE75.672. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYINSDR IXXA06SMN373SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN CORRODED AT STATION XE127.960. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREASDR IXXA06SMN358SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE29.812 TO STATION 763.844. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRIMESDR IXXA06SMN357SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE75.000 TO STATION XE147.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRIMESDR ASAA0641198Skin · dentedRIGHT HORIZONTAL STAB L/E SKIN DENTED O/B OF EMPENAGE. REPAIRED DENT PER SRM 55-10-01 FIG 101.SDR USAA061314Skin · gougedLEFT STAB L/E STA 133.15 GOUGED. REMOVED DAMAGE, INSTALLED FILLER, SHIMS AND DOUBLER IAW SRM 55-10-01 FIG 201, DEFECT SIZE: .22 X .05 X .022 INCH.SDR C2XA06SH120Skin · corrodedSHV - DURING C-CHECK THE LEFT HORIZONTAL STABILIZER LEADING EDGE WAS FOUND TO BE ERRODED AND HAVE PITTING CORROSION ON THE UPPER AND LOWER SURFACES. MAINTENANCE REMOVED AND REPLACED THE LEFT HORIZONTAL STABILIZER LEADING EDGE IAW EMB 145 AMM 55-15-00. THE AISDR 2006UALA02124Skin · crackedLT HORIZONTAL STAB TE LOWER SKIN APPROX 64 INCHES FROM FUSELAGE AND 2 INCHES FWD OF REAR SPAR CRACKED. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER SHIM AND ACCESS PLATES. REFERENCE SRM 5-10-01 REPAIR 6 FIGURE 803.SDR USAA061307Skin · delaminatedHORIZONTAL STAB STA 83.00 UPPER T/E DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98185, DEFECT SIZE: 2 INCHES.SDR DHL2006780003Access Panel · damagedLT HORIZONTAL STAB, ACCESS PANEL 9120 HAS THREE DAMAGED SCREW HOLES. CUTOUT DAMAGED AREA IAW BOEING SRM 55-10-5 FIG 1. FAB REPAIR ANGLES FROM 7075-T6, .080, PO NR 9003505, 10.65” BY 1” BY 1” IAW BOEING SRM 55-10-5 FIG 1. DETAIL TREATED AND PRIMED PARTS IAW SDR 2006UALA02061Skin · crackedRT HORIZ STAB LWR SKIN CRACKED APPROX 56 INCHES OUTBOARD FROM INBOARD END AND 2 INCHES FWD OF REAR SPAR. REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR. REFERENCE MM 55-10-94/801.SDR 06FDEA03735Skin · crackedDURING INSPECTION, FOUND LOWER INTERIOR AND EXTERIOR SKIN PANEL ON HORIZONTAL STABILIZER, WITH CRACKS, SEE ATTACHED SHEET FOR BEST DETAIL. PANEL ALC7205-1 REMOVED AND REPLACED IAW SB 53-16 GROUP 1 AND FIG 7 SHT 1 STEPS 1-3, PANEL ALC7438-2 REPAIRED IAW SB 55-SDR 2006UALA02016Skin · crackedRT HORIZ STAB LOWER SKIN CRACKED 62" OB FROM IB END AND 3" FWD OF AFT SPAR. MAJOR REPAIR: INSTALLED EXTERNAL DOUBLER REPAIR PER MM 55-10-94 PG 802 AND SRM 55-10-01 REPAIR NR 8.SDR 06FDEA03676Panel · crackedDURING NDT INSP ON HORIZ STAB, FOUND TWO PANEL P/N 7208-1 AND 7205-1 WITH CRACKS. SEE ATTACHED SHEET FOR ALL DETAIL. SHORING INSTALLED, OPENED ACCESS, REPLACED 2 PANELS AND REMOVED SHORING IAW SB DC10-55-16 GROUP 1 AND EA# 8-5510-96066.SDR SWAA063916Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER AFT INBOARD SKIN CRACKED. REPAIRED SKIN PER ER.SDR 06FDEA03608Skin · crackedHORIZONTAL STAB UPPER LT SKIN PANEL 7439-1 CRACKED 3.5 INCHES. VERIFIED END OF CRACK WITH HI-FREQ E/C. REFERENCE E/A 8-5510-102053 FOR INTERIM REPAIR AND FERRY FLIGHT, AND REFERENCE E/A 8-5510-102054 FOR PERMANENT REPAIR. A/C FERRIED TO LAX FOR PERMANENT RESDR KCSA061405Skin · dentedSMALL DENT ON BOTTOM SKIN ON LT HORIZONTAL STAB STA 257 APPROX 14 INCHES AFT OF AUX SPAR.SDR ASAA0691038Skin · damagedLEFT HORIZONTAL STAB LEADING EDGE DAMAGED.SDR AWXA200601781Skin · debondedMCN - MAJOR REPAIR - LEFT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12. REPAIRED LEFT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB SSDR AWXA200601780Skin · debondedMCN - MAJOR REPAIR - RIGHT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12. REPAIRED RIGHT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB SDR KCSA061378Skin · gougedTWO, 2.5" GOUGES ON BOTTOM SKIN OF LT HORIZ STAB STA 212, APPROX 42" AFT OF AUX SPAR.SDR CA061010004Skin · delaminated(CAN) LT HORIZONTAL STAB LEADING EDGE PANEL 332CL INNER SKIN COMPLETELY DELAMINATED. DELAMINATED SKIN WEARING INTO VERTICAL STIFFENERS LOCATED ALONG FRONT SPAR. (TC NR 20061010004)SDR KCSA061369Skin · gougedAPPROX 2 X 5 INCH DENT WITH GOUGE ON BOTTOM SKIN OF LT STAB STA 188 APROX 20 INCHES AFT OF AUX SPAR.SDR 2006UALA01877Skin · dentedRIGHT HORIZ STAB LEADING EDGE GOUGED AND DENTED AT L/E STAB STATION 75.5. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED LEADING EDGE FLUSH REPAIR AND NEW RIB PER SRM 55-10-01 REPAIR NR 2.SDR KCSA061354Skin · corrodedRT HORIZONTAL STABILIZER UPPER SURFACE HAS CORROSION AT STAB. STA. 110, BETWEEN STR. 14 AND 15SDR KCSA061353Skin · corrodedRT HORIZONTAL STABILIZER UPPER SURFACE HAS CORROSION AT STAB. STA. 180, BETWEEN STR. 4 AND 5.SDR 2006UALA01839Skin · dentedLEFT HORIZONTAL STABILIZER LEADING EDGE 8FT OUTBOARD OF FUSELAGE HAS A SMOOTH DENT 2.75" LONG BY 2.75" WIDE BY .190 DEEP. *S/D* MAJOR REPAIR: FILLED DENT WITH FILLER AND APPLIED SPEED TAPE PER SRM 55-10-01 PAGE 105.SDR 2006UALA01827Skin · crackedON WALK AROUND, FOUND 3-8 INCH CRACK ON RIGHT HORIZ STAB LEADING EDGE APPROX 6FT FROM INBD SIDE. MAJOR REPAIR: REPAIRED RIGHT HORIZONTAL STAB LEADING EDGE PER SRM 55-10-01.SDR CA060919004Visor · cracked(CAN) BOTH THE LT AND RT LOWER VISOR ASSEMBLIES WERE FOUND DAMAGED FROM CRACKING AT THE AFT TOP END. THIS MAY HAVE BEEN DUE TO FLUTTER AT THE AFT END OF THE FAIRING DURING FLIGHT. SINCE IT IS ATTACHED TO THE MOVABLE HORIZONTAL STABILIZER, THERE IS NO FASTENERSDR 0602363302Panel · gougedDURING REMOVAL OF RT HORIZONTAL STABILIZER FRONT SPAR ACCESS PANEL THE SPLICE PANEL AT RIB 4 WAS GOUGED. REPLACEMENT PANEL WAS MFG IAW EA 33-207930.SDR HALA0600756Panel · gougedGOUGE IN LWR SURFACE LT HORIZONTAL STAB L/E PANEL 332CL 21 INCHES FROM END. REPAIRED GOUGE IN LWR LT HORIZONTAL STAB L/E PANEL 332CL 21 INCHES FROM I/B END IAW GOODRICH ER 06-3431, FINAL ACCEPTED PER HAL M105 586040, REF'S USED SRM 55-10-01, SRM 51-70-01.SDR 06FDEA03160Skin · damagedRT HORIZ STAB REMOVABLE L/E NR 341DT FOUND WITH EXISTING EXTERIOR DOUBLER INSTALLED. RT HORIZONTAL STAB REMOVEABLE L/E #341DT EXISTING EXTERIOR DOUBLER REMOVED AS PER SRM 51-31-01 VOL.II. WEB AND RIBS REMOVED AND REWORKED AS PER SRM 55-20-00 VOL.I FIG.5SDR 06FDEA2999Skin · dentedLT HORIZONTAL STAB LEADING EDGE SKIN DENTED, MEASURES 2" BY 1" BY 0.210" DEEP. NO SRM REPAIR ON DENT POSITION AREA. DENT MARK ON LT HORIZONTAL STAB LEADING EDGE SKIN TRIMMED OUT AND REPAIR CARRIED OUT PER FEDEX EA NR 1-5510-103523, STABILIZERS, HORIZONTAL SSDR 06FDEA3000Skin · chafedTHE RT HORIZONTAL NR 5 BALANCE BAY UPPER SKIN PANEL IS CHAFED AT THE TE OF THE STIFFENER OB END. REMOVED AND REPLACED SKIN PANEL PER FED EX EA 7-5510-100575.SDR 06FDEA02879Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 35 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 35 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 22. CLASSISDR 06FDEA02878Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 32 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 32 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA 1-5510-95649 ATTACHMENT 21. CLASSSDR 06FDEA02877Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 30 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 30 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 20. CLASSISDR 06FDEA02876Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 28 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 28 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 19. CLASSISDR 06FDEA02875Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 12 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 12 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 13. CLASSDR 06FDEA02874Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 22 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 22 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR E.A.1-5510-95649 ATTACHMENT 12. CLASSDR 06FDEA02873Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 20 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 20 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 15. CLASSISDR 06FDEA02872Panel · corrodedCORROSION EXCEEDED LIMIT PER EO 1-5510-7-5000 D1 PT1 AT BARREL NUT BORE NR 16 RT OF HORIZONTAL STABILIZER. RT HORIZONTAL STABILIZER NR 16 BARREL NUT BORE REPAIRED AS PER HORIZONTAL STABILIZER-BARREL NUT BORE REWORK/REPAIR EA1-5510-95649 ATTACHMENT 11. CLASSI
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