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 DALA1516040907Skin · not reportedHORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01086.SDR SWAA118641Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.SDR IPXA1570719Panel · dentedRIGHT HORIZONTAL INBD FWD COMPOSITE PANEL HAS DENT DAMAGE. REPAIRED PANEL IAW SRM 51-70-10-2R.SDR IPXA1570718Panel · dentedRIGHT HORIZONTAL OTBD UPPER FWD COMPOSITE PANEL HAS DENT DAMAGE. REPLACED PANEL WITH NEW PART.SDR IPXA1570717Panel · dentedLEFT HORIZONTAL OTBD UPPER FWD COMPOSITE PANEL, HAS DENT DAMAGE. REPLACED PANEL WITH NEW PART.SDR SWAA118361Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 126. REPAIRED SKIN IAW SWA EA.SDR CALA2011120800800Skin · crackedSUPPORT TASK, LT HORIZONTAL STABILIZER LOWER SKIN HAS A CRACKED 2.250 INCH IN LENGTH ON THE I/B SIDE OF RIB AT STAB STA 129.5, 1 INCH FWD OF EXISTING DOUBLER. REPAIRED CRACKED SKIN REF SRM 55-10-01 REPAIR 11 FIG 204. INITIATED 55-DIP CONTROL #13772 FOR REPEASDR SWAA20111207449Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN IAW SRM.SDR SWAA20111207406Skin · crackedDURING SCHEDULED OTS CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 157 TO STA 147. REPAIRED SKIN IAW EA.SDR DALA1503869235Skin · unknownHORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01085.SDR ASMF201112003Skin · dentedDURING OVERNIGHT CHECK, MX DETECTED A DENT IN THE RT HORIZONTAL STAB L/E AT STA 181.23 OF 4.150" LONG AND 0.270" DEPTH, IT WAS CONFIRMED THAT DENT WAS OUT OF LIMIT IAW SRM 55-10-01. THE HORIZONTAL STAB L/E WAS REWORKED IAW SRM 55-10-01 PARAGRAPH 4 (D) (3) FIGUSDR SWAA118253Skin · crackedDURING SCHEDULED 2HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.SDR SWAA118204Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.SDR MASA2011121364212Skin · damagedHORIZONTAL STABLIZER WAS REMOVED TO FACILITATE MAINTENANCE WHILE BEING SUPPORTED ONE OF THE SAWHORSES BEING USED HAD PROTRUDING HARDWARE WHICH CAUSED DAMAGE TO LEADING EDGE. C/W RO CRJ9-55-0144.SDR MASA2011121364210Skin · dentedLT UPPER HORIZONTAL STABLIZER WAS FOUND TO HAVE MULTIPLE OUT OF LIMITS DENTS DUE TO HAIL STORM. C/W RO CRJ9-55-0141.SDR SWAA118111Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.SDR VNAA2011112300014Skin · dentedAT DAY, CREW REPORTED A BIRD STRIKE TO LEFT ELEVATOR. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. MAINTENANCE FOUND DENT IN LEFT HORIZONTAL STABILIZER LEADING EDGE AND DETERMINED DENT TO BE WITHINSDR USAA2011112100007Skin · delaminated1C CHECK - AREA OF DELAMINATION ON LEFT UPPER HORIZONTAL STABILIZER SKIN & CORE AT FSS 56 THRU FSS 107 APPROX 12 INCHES FROM LEADING EDGE. REPAIRED LEFT UPPER HORIZONTAL STABILIZER SKIN & CORE IAW EA 103467.SDR USAA2011111500008Skin Panel · delaminatedC3 CHECK - DELAMINATION ON HORIZONTAL STABILIZER UPPER SKIN PANEL AT STABILIZER STATION 176, BETWEEN FS 204.093 TO FS 155.849. REPAIRED HORIZONTAL STABILIZER UPPER SKIN PANEL AT STABILIZER STATION 176, BETWEEN FS 204.093 TO FS 155.849 IAW EA 103468.SDR ASAA11410641Skin · dentedDURING PREFLT W/A DAMAGED NOTED ON UNDERSIDE OF RT HORIZ STAB ABOUT 8" FROM ROOT. 2" AFT OF LEADING EDGE. DAMAGED AREA EST TO BE APPROX 6" LONG 3" WIDE & 1/2 TO 3/4" DEEP. DAMAGE DIMENSIONS = .044D X 6"L X 3" W STAB L/E STA 68 LOWER SIDE APPROX 4" DOWN FROM SDR CALA2011110300707Skin · crackedRIGHT STAB LOWER SKIN SHOWS CRACK INDICATION AT STA 166.30 17 INCHES FWD OF AFT SPAR REPAIRED CRACK AND INSTALLED LEADING EDGE W/REF TO SRM 55-10-01 REPAIR 11. SEE ATTACHED 44.0008 FOR PARTIAL WORK ACCOMP. PERFORM DVI AND LFEC AT 56000 FLT CYC`S AFTER REPAIR SDR KCSA111251Skin · corrodedCORROSION ON RT HORIZ STAB LWR T/E SKIN AT STA 145 (FOUND TO BE OUT OF LIMITS).SDR KCSA111250Skin · corrodedCORROSION ON RT HORIZ STAB LWR T/E EXT SKIN AT STA 236 (FOUND TO BE OUT OF LIMITS).SDR KCSA111249Skin · corrodedCORROSION ON RT HORIZ STAB LWR T/E EXT SKIN AT STA 183 (FOUND TO BE OUT OF LIMITS).SDR KCSA111247Skin · corrodedCORROSION ON RT HORIZ STAB LWR T/E EXT SKIN AT STA 209 (FOUND TO BE OUT OF LIMITS).SDR KCSA111246Skin · corrodedCORROSION ON RT HORIZ STAB LWR T/E EXT SKIN AT STA 178 (FOUND TO BE OUT OF LIMITS).SDR KCSA111245Skin · corrodedCORROSION ON RT HORIZ STAB LWR T/E EXTERNAL SKIN AT STA 145 (FOUND TO BE OUT OF LIMITS).SDR DALA1161146301Skin · damagedBECAUSE OF NR 2 ENGINE FAILURE, GENERAL INSPECTION OF HORIZ AND VERTICAL STAB WERE DONE. LT HORIZ STAB L/E PANEL 331CL NEEDED TO BE BLENDED APPROX 3 FEET FROM I/B END. APPROX .033 MATERIAL REMAINING. REPAIRED LT LEADING EDGE HORIZ STAB PANEL 331CL PER SRM 5SDR DALA1161136301Skin · damagedBECAUSE OF NR 2 ENGINE FAILURE, GENERAL INSPECTION OF HORIZ AND VERTICAL STABS WERE DONE. LT HORIZ STAB L/E PANEL 331DL FOUND DAMAGE AT HORIZ STAB STA 472. REPAIRED DAMAGE LT L/E HORIZ STAB PNL 331DL AT STA 472 PER SRM 55-10-01. JOB COMPLETE.SDR DALA1161126301Panel · damagedBECAUSE OF NR 2 ENGINE FAILURE, GENERAL INSPECTION OF HORIZ AND VERTICAL STABS WERE DONE. LT HORIZ STAB L/E PANEL 331DL FOUND DAMAGE AT HORIZ STAB STA 497. REPAIRED LT LEADING EDGE HORIZ STAB PANEL 331DL STA 497 PER SRM 55-10-01. JOB COMPLETE.SDR DALA1161116301Panel · damagedDAMAGE FOUND ON PANEL 331DL LT LEADING EDGE HORIZONTAL STABILIZER STA 524. CORRECTED STA DTW 30OCT11 ATA 5513. REPAIRED LT LEADING EDGE HORIZONTAL STABILIZER SKIN AT STA 524 PER SRM 55-10-01. OK FOR SERVICE.SDR DALA1161096301Panel · nickedLEADING EDGE PANEL 337L 1 ITEM FOUND. CORRECTED STA DTW 25OCT11 ATA 5513 REMOVED NICK IAW SRM 55-10-01. OK FOR SERVICE.SDR DALA1161106301Panel · damagedDAMAGE FOUND ON PANEL 331CL LT LEADING EDGE HORIZONTAL STABILIZER STA 339. CORRECTED STA DTW 29OCT11 ATA 5513. REPAIRED LEADING EDGE LT HORIZONTAL STABILIZER SKIN PER SRM 55-10-01. OK FOR SERVICE.SDR SWAA117471Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 92.70. REPAIRED SKIN IAW SRM.SDR SWAA117451Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED AT STA 92-70. REPAIRED SKIN IAW SRM.SDR CALA2011102800691Skin · crackedSUPPORT TASK - LT HORIZONTAL STAB LOWER SKIN STA 138.70 17 INCHES FROM L/E AND 25.5 L/E IS CRACKED. REPAIRED PER SRM 55-10-01 REPAIR 11. SEE FORM 44.0008 FOR ACCOMPLISHED JOB.SDR CALA2011102800690Skin · crackedSUPPORT TASK - RT HORIZONTAL STAB LOWER SKIN AT STA 147.90 24.5 INCHES AFT OF L/E IS CRACKED. REPAIRED RT HORIZONTAL STAB LOWER SKIN AT STA 147.90 24.5 INCHES AFT OF L/E. REF SRM REF 55-10-01- FIG 201 B.SDR SWAA117424Skin · crackedDURING SCHEDULED MV1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED. REPAIRED SKIN IAW EA.SDR DALA1161086301Panel · nickedLEADING EDGE PANEL 331BL 1 ITEM FOUND. CORRECTED STA DTW 25OCT11 ATA 5513. REMOVED NICK IAW SRM 55-10-01. OK FOR SERVICE.SDR DALA1161076301Panel · nickedLEADING EDGE PANEL 331EL 2 ITEMS FOUND. CORRECTED STA DTW 25OCT11 ATA 5513 REMOVED NICKS IAW SRM 55-10-01. OK FOR SERVICE.SDR DALA1161066301Panel · nickedBLENDED ARE APPROX 12" FROM I/B EDGE PANEL 331DL HAS .032 MATERIAL REMAINING. LT HORIZONTAL STABILIZER L/E MARKED. PERFORMED UT THICKNESS INSPECTION AND FOUND .046 REMAINING. WITHIN LIMITS IAW B747-400 SRM 55-10-01 FIG 101. A/C OK FOR SERVICE.SDR DALA1161056301Panel · nickedLEADING EDGE PANEL 331DL 13 ITEMS FOUND. CORRECTED STA DTW 25OCT11 ATA 5513 REMOVED NICKS ON 10 ITEMS IAW SRM 55-10-01 LISTED 3 ITEMS ON NRF 109, 110 AND 111. OK FOR SERVICE.SDR DALA1161036301Panel · nickedLEADING EDGE PANEL 331CL 13 ITEMS FOUND. CORRECTED STA DTW 25OCT11 ATA 5510 REMOVED NICKS ON 12 ITEMS IAW SRM 55-10-01 LISTED 1 ITEM ON NRF 112. OK FOR SERVICE.SDR SWAA117384Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 184.7. REPAIRED SKIN PER SRM.SDR CALA2011102400683Skin · damagedSUPPORT TASK - C-SCAN AND PENCIL PROBE SHOWS ANAMOLY ON RT STAB LOWER SKIN HORZ STAB STA 129.50 3RD RIVET, I/B RIVET ROW AFT OF EXISTING REPAIR INSTALLED REPAIR REF SRM 55-10-01 REPAIR 11 REINSPECT REPAIR AS PER TABLE 204/ REPAIR 11 INSP AT 56000 FLIGHT CYCLESSDR CA111026007Skin · cracked(CAN) NUMEROURS SKIN CRACKS FOUND IN UPPER SKIN ON LT ELEVATOR AND LT HORIZONTAL STABILIZER.SDR CA111021010Skin · cracked(CAN) A 1" CRACK WAS FOUND IN BETWEEN THE 2 RIBS OF THE STAB AT THE T/E WHERE THE REAR SPAR IS LOCATED ON THE RT SIDE LOWER SKIN. THE CRACK WAS FOUND ON A ROUTINE INSPECTION AND THE STAB WAS R & R WITH A SERVICEABLE UNIT.SDR SWAA117185Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW EA.SDR FOTR2011101506876Skin · dentedRT HORIZONTAL STAB L/E DENTED AT STAB STA 75. REPAIRED ON FASI WO21142, NR 06876.SDR SWAA117122Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SM.
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