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 P5CA9701456Panel · delaminatedDELAMINATED PANEL LEFT HORIZONTAL STABILIZER, PANEL NUMBER 334GBL. REPAIRED PER BOEING SRM 51-40-09.SDR ABXA9701435Skin · corrodedDURING D-CHECK, FOUND EXFOLIATION CORROSION ON THE RT HORIZONTAL STAB LEADING EDGE INBOARD END CENTER SECTION. *S/D* REPAIRED CORROSION IAW ABX REA D955-20734.SDR MWEA97730Skin · crackedDURING CPCP, FOUND CRACK RT HORIZ STAB TRAIL EDGE STA XHS122. MTC REPAIRED IAW SRM 55-01 FIG 2 SHT 3.SDR 97ZZZX3901Skin · crackedUPON INSPECTION PER SB 94-8-A, THE SKIN WAS FOUND CRACKED. THE SKIN AND REINFORCEMENT WERE REPLACED WITH NEW PARTS. NO OTHER PROBLEMS FOUND.SDR UPS97824426Skin · corrodedINSPECTION TYPE-D, RT HORZ STAB L/E O/B SECTION CORROSION REMOVAL BETWEEN SKIN OUT OF LIMITS, REF NR 621494. REPAIRED L/E SKIN IAW SRM 55-3-0, 55-2-0, 53-2-0, 55-3-1, AND 51-1-21.SDR IH971355001Skin · corrodedRT HORIZ STAB LEADING HAS LEADING EDGE CORROSION. ACCOMPLISHED BLENDOUT REPAIR AND COIN FILLER FLUSH REPAIRS OF CORROSION ON THE RIGHT HAND HORIZONTAL LEADING EDGE SKIN BY BLENDING 30:1 SPANWISE AND 10:1 CHORDWISE WITH 63RMS FINISH FOR BLENDOUTS. REMOVED EXISDR CKSA97447Skin · crackedDURING CPCP CHECK INSPECTION, FOUND I/B L/E OF RT HORIZONTAL STAB HAS GOUGE AND POSSIBLE CRACK. REMOVED DAMAGED AREA AND REPAIRED IAW DAC SRM 55-2-1 FIG 4 (2024-T3) CORROSION TASK CARD NUMBER 6000-0551. NON-ROUTINE TASK CARD NUMBER 111356.SDR P5CA9701397Elevator · damagedRIGHT HAND HORIZONTAL STABILIZER OUTBD OF OUTBD ELEVATOR BROKEN OUT AND LOOSE. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9701396Elevator · crackedLEFT HAND HORIZONTAL STAB TRAILING EDGE O/B OF O/B ELEVATOR CRACKED AND LOOSE. REPAIRED PER BOEING SRM 51-40-09.SDR HEEA0010563Skin · mis mfgSKIN WAS CHEMICALLY MILLED ON WRONG SIDE.SDR P5CA9701369Panel · delaminatedDELAMINATED PANEL NR 344NB RIGHT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9701368Skin · delaminatedDELAMINATED PANEL NR 334NB LEFT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06 AND 55-10-12.SDR P5CA9701367Skin · delaminatedDELAMINATED PANEL NR 334MB LEFT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-05.SDR CALA9701214Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL STABILIZER SKIN BETWEEN STA 111.1 AND 126.6. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01369.SDR DL72W971439Skin · crackedA 3.75 INCH CRACK IN LOWER SKIN OF LT HORIZONTAL STABILIZER NR 2 BALANCE BOARD ACCESS PANEL. INSTALLED DOUBLER PER SRM 55-20-3 FIG 5.SDR IXXA980012Skin · corrodedDURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER PLATING BETWEEN STATIONS XFS114 AND XFS178. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREAS, FABRICATION AND INSTALLATION OF INTERNAL FILLERS AND A EXTERSDR IXXA9800011Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER PLATING BETWEEN STATIONS XFS114 AND XFS178. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF INTERNAL FILLERS AND AN EXTERNAL RSDR ABXA9701260Panel · crackedDURING COMPLIANCE WITH AD 90-16-05 AND SB 55-15R3, FOUND HORIZONTAL STABILIZER HAD .75 INCH CRACK, AT LT FORWARD LOWER CONSTANT BOX PANEL. PLACED ON CONTINUING INSPECTION EVERY 900 FLIGHT HOURS OR EVERY 3 MONTHS (WHICH EVER COMES FIRST) IAW DAC SB 55-15.SDR CKSA97361Skin · damagedDURING ROUTINE C CHECK INSPECTION FOUND: LT HORIZONTAL STAB INBOARD LEADING EDGE DAMAGED STA LES 146 APPROX. CUT-OUT DAMAGED AREA. INSTALLED REPAIR IAW L1011 SRM 55-15-00 FIG 805 REV. APR 81. NON-ROUTINE TASK CARD NUMBER 107598.SDR RRXA97193Skin · corrodedDURING MAINTENANCE VISIT, INSPECTION FOUND LT HORIZONTAL STAB, LOWER TRAILING EDGE SKIN CORRODED AT STA 231, 2 TO 16 AFT OF REAR SPAR. FABRICATED AND INSTALLED NEW HORIZONTAL STABILIZER TRAILING EDGE PANEL IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH C84-R0SDR CKSA97436Skin · delaminatedDURING ROUTINE C-3 CHECK INSPECTION, FOUND LEFT HORIZ STAB T/E LWR SKIN BETWEEN XR28.846 AND XE176.156 FASTENER AREA DELAMINATED (FOR CORROSION). REPAIRED AFFECTED AREA PER SRM 55-2-1. NON-ROUTINE TASK CARD NUMBER 105726.SDR CKSA97435Skin · delaminatedDURING ROUTINE C-3 CHECK INSPECTION, FOUND RT HORIZ STAB T/E LWR SKIN XE77.000 THROUGH XE221.000 FASTENER AREA DELAMINATED FOR CORROSION. REPAIRED AFFECTED AREA PER SRM 55-2-1. NON-ROUTINE TASK CARD NUMBER 105727.SDR CALA9701153Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH SRM 55-10-4 FIG 4 AND 55-10-3 FIG 829.SDR 97ZZZX3319Skin · dentedJFK - FLT 73 - AT DEPARTURE, A DENT APPROXIMATELY 19 INCHES LONG BY 2 TO 5 INCHES WIDE WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE. DETERMINED THAT LAVATORY WATER FROM A LAVATORY CAUSED DAMAGE. REPLACED STABILIZER LEADING EDGE. EA 97-3800-01 WHSDR P5CA9701195Skin · delaminatedA HOLE WAS FOUND R/HORIZONTAL STABILIZER. REPAIRED PER BOEING SRM 51-40-06.SDR CALA9701147Skin · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE DENTED AND CRACKED. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLR AND INSTALLED IN ACCORDANCE WITH SRM 55-10-03 AND 51-30-2.SDR ZZDA5512497Skin · dentedDURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER DENTED, 110 INCHES BY 5.5 INCHES BY 4 INCHES AT THE OUTBOARD END OF UPPER SKIN 5.5 INCHES FROM FORWARD UPPER SPAR. REMOVED DENT IAW B737 SRM 55-10-3. FABRICATED PLATE FROM 2024 T3 .071 INCH BY 5.375 INCHES BYSDR ZZDA5512197Skin · damagedDURING C-CHECK, FOUND LT HORIZONTAL STABILIZER LEADING EDGE REPAIR NEEDS REPLACEMENT. FABRICATED FLUSH DOUBLER FROM 2024 T3 .063 INCH, 12.625 INCHES BY 8.375 INCHES. INSTALLED REPAIR IAW B737 SRM 55-10-3. INSTALLED FILLER .040 INCH BY 8.25 INCHES BY 4.875 ISDR 97ZZZM929Skin · misrepairedDURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE REPAIR NEEDS REPLACEMENT. FABRICATED FLUSH DOUBLER FROM 2024 T3 .063 12.625 INCH BY 8.375 INCH INSTALLED REPAIR IAW B737 SRM 55-10-3. INSTALLED FILLER .040 BY 8.25 INCH BY 4.875 INCH IAW B737 SRM SDR ABXA9701155Panel · corrodedDURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN PANEL CORRODED AND BULGING AT STA XFX 260.000. FABRICATED SKIN DOUBLER AND HAT-SECTION AND REPAIRED IAW DC8 SRM 51-1-8 AND ABX DWG NR 08-55-1174.SDR SWAA970560Skin · dentedDURING SCHEDULED C4 CHECK, FOUND LEFT HORZI STAB L/E DENTED BEYOND LIMITS. REPAIRED PER BOEING SRM.SDR UPS97823733Skin · corrodedINSPECTION TYPE:D, RT HORIZ STAB LOWER SURFACE HAS MODERATE CORROSION WHERE THE STAB MEETS THE CENTER BOX. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW 55-2-0, 51-1-21, 51-3-1, 51-3-0 AND DWG 5653617.SDR IXXA9700121Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER UPPER PANEL, INNER BEADED SKIN BETWEEN STATION XE150 TO 250. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN INTERSDR W8PA970776Panel · wornRIGHT HORIZONTAL STAB MIDDLE BALANCE BAY PANEL IS CHAFING AND GOUGING WEBS ON INBOARD AND OUTBOARD SIDES. REPAIRED RIGHT STAB MIDDLE BALANCE BAY PANEL PER SRM 51-70-10. (M)SDR P5CA9700995Skin · corrodedLEVEL 1 RT STAB PANEL 344NBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700994Panel · delaminatedRT STAB PANEL 344QBR DELAMINATED AT PREVIOUS REPAIR (MOST O/B PANEL). REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700990Skin · corrodedLEVEL 1 LT STAB PANEL 334PBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700989Skin · corrodedLEVEL 1 LT STAB PANEL 334FBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700988Skin · corrodedLEVEL 1 RT STAB 344LBR PANEL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700987Skin · corrodedLEVEL 1 RT STAB PANEL 344PBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700986Skin · delaminationLT STAB PANEL 344GBL DENT AND DELAMIATED AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700985Skin · delaminatedRT STAB PANEL 344LBR SURFACE DELAMINATED. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700984Skin · corrodedLEVEL 1 RT STAB PANEL 344JBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700983Skin · corrodedLEVEL 1 RT STAB PANEL 344KBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9700980Panel · delaminatedLT STAB PANEL 344JBL DELAMINATED. REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700979Panel · corrodedLEVEL 1 LT STAB PNL 334HBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700978Skin · delaminatedLT STAB PANEL 334HBL O/B FWD CORNER DELAMINATED. REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700977Skin · corrodedLEVEL 1 LT STAB PANEL 334MBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR P5CA9700976Panel · corrodedLEVEL 1 LT STAB PANEL 334NBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.SDR CA970609015Stringer · cracked(CAN) APPROXIMATELY 6" OUTBOARD OF LH RIB 20.0 STRINGERS 4, 6, 8 CRACKED, SKIN CRACKED BENEATH STRINGERS, EXTENDING FORWARD O.5 INCH AT STRINGERS 4 AND 6; EXTENDING AFT 1" AT STRINGERS 4 AND 6. SLIGHT DOWNWARD BUCKLING AT DAMAGED AREAS. REPAIRED IN ACCORDANCE
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