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 2002UALA01262Skin · damagedAIRCRAFT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE AT OUTBOARD END IS DAMAGED. DENT IS APPROXIMATELY 5 INCHES FROM OUTBOARD END, STAB BL 240 TO BL 249. MAJOR REPAIR ACCOMPLISHED. LEADING EDGE PARTIAL SKIN REPLACEMENT.SDR DHL2002806855Skin · corrodedLT HORIZ STAB INBOARD L/E ELONGATED HOLES & CORRODED STA XFS 178.750. PERFORMED MAJOR REPAIRS. REMOVED CORROSION LT HORIZ STAB L/E AT STA XFS178.750. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12-14. TRIMMED OUT DAMAGED AREA. FABRICATED A REPAIR DOUBLER & TRIPSDR USAA020284Skin · delaminatedPIT - FOUND LOWER SURFACE DELAMINATED 5 INCHES BY 5 INCHES, 74.5 INCHES FROM INBOARD END AND 10.5 INCHES FROM LEADING EDGE. REPAIRED PER SRM 55-20-01, 51-70-17 AND EA 74407. (M)SDR 2002UALA01158Skin · crackedRIGHT HAND HORIZONTAL STABILIZER, LOWER SKIN AT REAR SPAR IS CRACKED AT STABILIZER STA 120.3-129.5. MAJOR REPAIR ACCOMPLISHED. FLUSH REPAIR.SDR 2002UALA01156Skin · dentedLEFT HAND HORIZONTAL STABILIZER LEADING EDGE, 14 INCHES FROM FUSELAGE, SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. DOUBLER MANUFACTURED AND INSTALLED.SDR TIMR74Skin · crackedLEADING EDGE OF STABILIZER DISBONDED ON LOWER SIDE AND A CRACK FORMED JUST OFF THE END CAP AND COMPOSITE JOINT. (CONTROL NR 74)SDR SIMA200219128Skin · dentedABI - RIGHT HORIZONTAL LOWER SKIN HAS ONE DENT. PERFORMED EDDY CURRENT AND SONIC BOND CHECK, NO DEFECTS NOTED. DENT FOUND TO BE WITHIN SAAB 340 SRM 55-10-10 AND 51-10-10 LIMITS. (M)SDR SIMA200219124Skin · dentedRIGHT HORIZONTAL TOP SKIN HAS 45 DENTS. PERFORMED EDDY CURRENT AND BOND CHECK, NO DEFECTS NOTED. (M)SDR SIMA200219123Skin · dentedABI - LEFT HORIZONTAL TOP SKIN HAS 57 DENTS. PERFORMED EDDY CURRENT AND BOND CHECK, NO DEFECTS NOTED. (M)SDR SIMA200219112Skin · dentedABI - RIGHT HORIZONTAL LOWER SKIN HAS ONE DENT. PERFORMED SONIC BOND AND EDDY CURRENT INSPECTION, NO DEFECTS. DENT WITHIN SAAB SRM 55-10-10 AND 51-10-10 LIMITS. (M)SDR 2002UALA00963Skin · crackedLEFT HAND HORIZONTAL STABILIZER REMOVABLE LEADING EDGE INBOARD END SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLUSH REPAIR.SDR 2002F00743Skin · dentedAT C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER WITH DENT BEYOND LIMITS, AT STABILIZER STATION 20. (M)SDR UPS02838657Skin · dentedINSPECTION TYPE:C1 DENT IN RT HORIZ STAB LE 35 INCHES O/B AT ROOT. REMOVED DAMAGED AREA DENT FOUND TO BE OUT OF LIMITS. FABBED REPAIR DOUBLER IAW SRM 55-2-1. INSTALLED DOUBLER IAW SRM 51-1-21.SDR A6WA200260014Skin · damagedTWO AREAS OF MECHANICAL DAMAGE ON THE LEFT LOWER SKIN ON THE HORIZONTAL STAB. FABRICATED A REPAIR PATCH. REPAIRED IAW BAE RIL BARA/AVR/1034/02-DC. (M)SDR DHL2002802511Skin · dentedRT HORZ STAB L/E WITH 10 INCH DENT BETWEEN STA XFS 72.500 - 85.000. PERFORMED MAJOR REPAIR IAW SRM 55-2-1 PG 17. CUT AFFECTED AREA IAW SRM 55-2-1 PG 17. FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1 PG 17. INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1- PG 17.SDR DL76S020568Skin Panel · delaminatedA 2 FOOT, 6 INCH DIA AREA WAS FOUND DISBONDED ON THE LEFT HORIZONTAL STABILIZER UPPER INBOARD FORWARD SKIN PANEL BETWEEN FS 53.659 AND FS 80.896. THE DISBONDED SECTION OF HONEYCOMB CORE WAS REPLACED PER SRM 51-70-10 BY DEPT 382 ON SHOP ORDER H05277. THE PANESDR CA020527005Skin · cracked(CAN) UPON INSPECTION THE RT HORIZONTAL STAB WAS FOUND TO BE CRACKED AT THE BOTTOM, OUTBOARD, AFT BOLT ATTACHMENT HOLE. THE STAB WAS REPLACED AND SENT FOR REPAIR.SDR SIMA200213812Skin · damagedLEFT HAND HORIZONTAL STABILIZER FORWARD SPAR HAS TWO OVERSIZED HOLES, UPPER SKIN PANEL. PERFORMED AN NDT INSPECTION, NO DEFECTS NOTED. INSTALLED FASTENERS WET, DONE IAW MFG SRM.SDR SWAA020916Skin · crackedDURING SCHEDULED C4 CHECK, FOUND HORIZ STAB SKIN CRACKED AT STA 108 OF THE STAB REAR SPAR. REPAIRED SKIN PER SRM.SDR LR7A02031Skin · crackedDURING SCHEDULED B2 INSPECTION PER JOB CARD HB0503 FOUND FS 1091 LH UPPER HORIZONTAL STAB SKIN CRACKED AT HSS 188, WL 285.REPAIRED IAW SRM SMP 583 55-20-06. NR 0057.SDR MWEA020215Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND-OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER.SDR MWEA020214Skin · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AROUND SOME OF THE WRAP AROUND SCREWS (CENTER SECTION INBOARD AREA). THERE WAS PREVIOUS BLEND OUT ALREADY IN THIS AREA. FABRICATED AND INSTALLED DOUBLER.SDR AWXA200200271Skin · dentedLCQ - MAJOR REPAIR - DURING C-15 CHECK A DENT WAS FOUND ON RT HORIZONTAL STABILIZER AT STAB STA 144 MID SPAN. FABRICATED A DOUBLER, FILLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM.SDR AUS20020393Skin · corroded(AUS) RT STABILISER SKIN CORRODED AT ATTACHMENT POINT TO REAR UPPER AUXILIARY SPAR CHORD ZONE 92, ELE 118.0 TO ELE 120.0. CPCP -LEVEL 2 CORROSION.SDR CA020322004Fitting · sheared(CAN) RIVETS THAT ATTACH FITTING TO FORWARD SPAR WERE SHEARED. MOST RIVETS, 10 IN ALL, SHOWED SIGNS OF RINGS AROUND SHANKS AT FITTING/SKIN SEAM. ONE RIVETS WAS SHEARED IN HALF. THERE WERE NO EXTERNAL SIGNS OF ANY PROBLEMS. THE STABILIZER IN QUESTION CAME IN FOSDR AWXA200200213Skin · dentedDURING PREFLIGHT WALK AROUND A DENT WAS DISCOVERED ON THE LEADING EDGE OF THE OUTBOARD TIP ASSEMBLY OF THE LT TRIMABLE HORIZONTAL STABILIZER.SDR USAA020116Skin · crackedPIT - FOUND SKIN CRACKED 1.75 INCHES LONG, LEFT HORIZ STABILIZER LOWER SIDE STATION 99.07 AND 66.54. CUT OUT DAMAGE, HFEC AREA, INSTALLED FILLER AND DOUBLER PER TR 55-10-07 REV A. (M)SDR USAA020119Skin · crackedPIT - FOUND SKIN CRACKED 1.75 INCH, RIGHT HORIZ LOWER SKIN AT STATION 125. INSTALLED REPAIR PER TR 55-10-07 REV A, SRM 55-10-01 FIG 204. (M)SDR AWXA200200328Flange · crackedYWG - MAJOR REPAIR - DURING C-08 CHECK A CRACK WAS FOUND ON THE RT HORIZONTAL STABILIZER L/E 3 FROM OUTBOARD END ON LOWER L/E PANEL MATING SURFACE. MAINTENANCE REMOVED DAMAGED AREA AT STAB STA 6009, RIB 14, FABRICATED AND INSTALLED REPAIR PARTS IAW AWA ER 26-SDR CALA0200118Skin · crackedINSPECTION FOUND A 3" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR JUST I/B OF #4 ELEVATOR HINGE. A PERMANENT REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01584.SDR UPS02837888Skin Panel · crackedINSPECTION TYPE:C23 LT HORIZONTAL STAB UPPER O/B FWD SKIN PANEL CRACKED AT 2ND BOLT IN AFT DIRECTION. REMOVED AND REPLACED HORIZ STAB PLANK IAW DAC SB55-16 AND DAC DWG SRO 8 550001.SDR AUS20020241Panel · corroded(AUS) HORIZONTAL STABILISER PANEL LOCATED ABOVE BAY THREE CORRODED IN AREA OF REAR AUXILIARY SPAR LH SIDE.SDR 2002UALA00260Skin · damagedLEFT HAND INBOARD SECTION OF HORIZONTAL STABILIZER LEADING EDGE 2 AREAS OF EXCESS MATERIAL LOSS MEASURED FROM INBOARD EDGE. 1ST DAMAGE 27 INCHES OUTBOARD. 2ND DAMAGE IS 32 INCHES OUTBOARD. MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGE AND INSTALLED DOUBLER.SDR 200200179Skin · corrodedLEFT HORIZONTAL STABILIZER UPPER SKIN CORROSION. THE REPAIR IS ACCOMPLISHED BY TRIMMING OUT CORRODED AREA OF SKIN THEN INSTALLING AN EXTERNAL DOUBLER SKIN REPAIR PER ECRA 482-55-148-2.SDR 200200176Skin · corrodedLEFT HORIZ STAB UPPER SKIN STA 385 HOIST ATTACH POINT. THIS REPAIR IS ACCOMPLISHED USING AN EXTERNAL DOUBLER REPAIR. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA 482-55-143-2.SDR CALA0200054Skin · crackedINSPECTION FOUND A 3/4" CRACK IN L/H HORIZONTAL STABILIZER SKIN AT REAR SPAR APPROXIMATELY 65" FROM I/B AREA. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01613.SDR ZW0A0201107Panel · damagedDURING CHECK-C MAINT FOUND DEEP GROOVE WORN AFT END OF THE HORIZONTAL STABILIZER LOWER FAIRING PANEL, LT SIDE, 8 IN BY 1 INCHES BY 0.050 DEEP. INSTALLED DOUBLER PER SRM 53-80-01.SDR USAA011412Skin · crackedPIT - FOUND BOTTOM SKIN CRACKED .25 INCH LONG, AFT SPAR RIGHT STAB, STATION 152. INSTALLED DOUBLER PER SRM 55-10-01 FIG 204. (M)SDR 2001UALA02409Skin · dentedRIGHT HAND HORIZONTAL STABILIZER LEADING EDGE DENTED 5 FEET FROM OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FLUSH REPAIR.SDR 2001UALA02379Skin · dentedLEFT HORIZONTAL STABILIZER LEADING EDGE, 8 FEET FROM INBOARD END, DENT BETWEEN RIBS. MAJOR REPAIR ACCOMPLISHED, DOUBLER REPAIR MANUFACTURED AND INSTALLED.SDR QM72001F00000Skin · delaminatedA DELAMINATION OF THE RIGHT HORIZONTAL STAB UPPER SKIN PANEL, WAS DETECTED DURING A GENERAL VISUAL INSPECTION OF THE AREA. THE DEBOND IS OPP. 40 INCHES X 12 INCHES, 21 INCHES OUTBOARD OF THE ROOT AND CENTER FORWARD AND AFT. THERE IS NO SIGNIFICANT VISUAL DASDR CALA0101008Skin · crackedINSPECTION FOUND A 2" CRACK IN L/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01608.SDR USAA011370Skin · crackedPIT - FOUND DAILY SKIN CRACKED 2 INCHES, LEFT HORIZ STAB STATION 124-126 LOWER REAR SPAR CHORD. CUT OUT DAMAGED SKIN, HFEC INSPECTION, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 55-10-07A, SRM 55-10-01. (M)SDR ARWA20011108PlateN/R 412 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH HORIZONTAL STABILIZER TIE STA. XE 77.000 AND 92.000 UPPER SKIN WITH INNER CORROSION.CORRECTIVE ACTION: REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED USDR ARWA20011106Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER T/E BETWEEN STA 175.000 & STA 190.000 UPPER SKIN WITH INNER CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED UPPER PLATING; FABRICSDR 2001FA0000579Skin · damagedDURING AN ANNUAL INSPECTION THE RIGHT INBOARD SKIN HAD EXCESSIVE OIL CANNING WHEN FLEXED. WHEN FAIRING, PN 12124265 AND PN 12124266 (RIGHT AND LEFT) WERE REMOVED, THE RIGHT UPPER SKIN SURFACE UNDER FAIRING WAS CHAFFED THROUGH 4 INCHES IN LENGTH THE LEFT SKIN SDR 2001FA0000578Skin · damagedDURING AN ANNUAL INSPECTION THE RIGHT INBOARD SKIN HAD EXCESSIVE OIL CANNING WHEN FLEXED. WHEN FAIRING, PN 12124265 AND 12124266 (RIGHT AND LEFT) WERE REMOVED, THE RIGHT UPPER SKIN SURFACE UNDER FAIRING WAS CHAFFED THROUGH 4 INCHES IN LENGTH THE LEFT SKIN IN SDR 2001UALA02273Skin · gougedRIGHT HAND HORIZONTAL STABILIZER LEADING EDGE EXTERNAL SKIN IS GOUGED STABILIZER STATION 110. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED FLUSH REPAIR.SDR 2001UALA02209Skin · gougedRIGHT HORIZONTAL STABILIZER UPPER SKIN GOUGES AT STABILIZER STATION 46, 7 INCHES AFT OF SKIN LEADING EDGE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.SDR UPS01437302Skin · corrodedINSPECTION TYPE:C, RT STAB UPPER FACE SURFACE CORROSION ALONG FASTENER HEADS AT SKIN AREA FROM S1 - S15, STAB STA 143 - 240. REPAIRED RT HORIZONTAL STAB UPPER SKIN AT HS STA 223 TO 182 STR 5.
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