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.

SDR 04FDEA01832Panel · corrodedEMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78022 TITLE: STABILIZERS, HORIZONTAL STABILIZJun 21, 2004 · N587FE · Doug MD11FSDR 04FDEA01831Panel · corrodedEMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 8 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND NR 8 BARREL NUT BORE. REPAIRED AS PER FEDEX EA 1-5510-78023 - STABLIZERS, HORIZONTAL STABILIZER, BARREL NUT BJun 21, 2004 · N587FE · Doug MD11FSDR IXXA060368SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE149 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 16, 2004 · N41CX · Doug DC862FSDR IXXA060365SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA.Jun 16, 2004 · N41CX · Doug DC862FSDR UPS04242680Skin · damagedINSPECTION TYPE:C PULLED RIVETS & BULGE ON RT STAB LWR SKIN APPROX 4 INCHES FROM REAR SPAR AND AT STAB STA 66 APPROX. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-10-3 FIG 3, 51-10-1 & MM 51-20 -01 & 27-30-51.Jun 16, 2004 · N948UP · Boeing 72725CSDR 2004UALA00589Skin · dentedFOUND A 3.5 X 1.5 X 0.1875 DEEP DENT ON RIGHT HORIZONTAL STABILIZER LEADING EDGE APPROX 15 FEET FROM THE FUSELAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR.Jun 16, 2004 · N391UA · Boeing 737322SDR A6WA200460024Skin · gougedFOUND RIGHT HORIZONTAL STABILIZER TOP SKIN SMALL GOUGE IN THE UPPER SKIN OF THE RIGHT HORIZONTAL STABILIZER BETWEEN RIBS 9 AND 10. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 612-1909007. (M)Jun 14, 2004 · N612AW · Bac 146300ASDR UPS04M42921Panel · corrodedINSPECTION TYPE: C, RT HORIZONTAL STAB NR 1 BARREL NUT HOLE FOUND CORRODED. CORROSION AT ABOVE MENTION LOCATION REMOVED & REAMED TO 1.562 INCH & BLENDED FOUND OUT LIMIT. REPAIR SLEEVE BUSHING & FAB PER EO MD11-5510-19409-G APPLIED SEALANT PR1422B2 PER EN:120Jun 11, 2004 · N276UP · Doug MD11FSDR IXXA060363SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANELS AT STATIONS ZR267.218, ZR276.531, AND ZR284.75 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 10, 2004 · N41CX · Doug DC862FSDR IXXA060321SPanel · bulgedDURING ROUTINE C CHECK, FOUND RUDDER LEFT SIDE AFT SKIN PANEL BULGED FROM STATION ZR100 TO ZR110. REPAIRED PER ALL APPLICABLE DATA.Jun 10, 2004 · N41CX · Doug DC862FSDR UPS04842652Doubler · damagedINSPECTION TYPE:C2 RIGHT UPPER HORIZONTAL STAB LEADING EDGE HAS ELONGATED HOLES BETWEEN XFS 47.5 TO XFS 110.0. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG 5644330 AND SRM 55-2-1 FIG 4.Jun 10, 2004 · N894UP · Doug DC873FSDR UPS04842604Skin · corrodedINSPECTION TYPE: C2, LEFT HORIZONTAL STAB LEADING EDGE UPPER SKIN IS CORRODED XFS 272.5. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4.Jun 10, 2004 · N894UP · Doug DC873FSDR IXXA060320SSkin · corrodedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE CORRODED FROM STATION XFS60 TO XFS142. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862FSDR IXXA060319SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED AT STATION XFS239. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862FSDR SIMA200416203Skin · damagedABI - DURING MBV INSPECTION, AIRCRAFT PREVIOUSLY HAD SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN AND INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 22, 23 Jun 6, 2004 · N396AE · Saab 340BSDR IXXA060362SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060318SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE28.843 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060316SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060315SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060314SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060313SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060312SPanel · bulgedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060311SPanel · bulgedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060310SPanel · bulgedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE SECTION BETWEEN STATION XE272 TO XE312 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060309SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN FROM FRONT SPAR TO REAR SPAR AT STATION XE28.843 CORRODED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060308Panel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060307SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060306SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE221 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060305SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060304SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060303SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060302SPanel · bulgedLEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862FSDR IXXA060449SSkin · scratchedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SKIN SCRATCHED AT STATION XFS139.250. REPAIRED PER ALL APPLICABLE DATA.Jun 4, 2004 · N41CX · Doug DC862FSDR UPS04M42922Panel · corrodedINSPECTION TYPE:C, HORIZONTAL STAB NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDEWALL SURFACE POSITION RT. CORROSION REAMED TO 1.178 INCH & BLEND TO 0.040 INCH FOUND OUT OF LIMIT. REWORKED CUTOUT AT NR 30 HOLE B/N RT AS PER EN:1175-04 & EO MDMay 29, 2004 · N276UP · Doug MD11FSDR UPS04M42919Panel · corrodedINSPECTION TYPE:C, LT HORIZONTAL STAB NR 1 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING S/W SURFACE. HOLE LT NR 01 BARREL NUT, REAMED TO 1.549 INCH PER MD11-5510-19409-G & MAT REMOVED 0.040 INCH DEEP K 0.450 INCH FOUND OUT LIMIT. FAB & REPAIR CUTOUT SLEMay 29, 2004 · N276UP · Doug MD11FSDR UPS04242559Panel · corrodedINSPECTION TYPE: C, NR 5 LEFT BALANCE BAY PANEL HAS VERY LITE SURFACE CORROSION. UPON INVESTIGATION, CORROSION FOUND TO BE BEYOND LIMITS. BALANCE PANEL PLATE REPLACED IAW MM 27-30-27.May 28, 2004 · N950UP · Boeing 72725CSDR SIMA200415409Skin · damagedAIRCRAFT SUSTAINED HAIL DAMATE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZ, STAB UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED AND INSTALLED NEW SKIN. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, 51-40-21, 22,23, 25, 40, 60, 51-20-50 AND SAAB May 19, 2004 · N388AE · Saab 340BSDR SIMA200415411Skin · damagedABI - AIRCRAFT SUSTAINED HAL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZ STAB UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 22, 25, 40, 51-20-50, 51-40-60 AMay 19, 2004 · N388AE · Saab 340BSDR CALA0400494Skin · puncturedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN PUNCTURED AT STAB STA 203. THE PUNCTURED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW 55-10-01.May 18, 2004 · N23661 · Boeing 737524SDR SWAA041354Skin · crackedDURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STA 133, FWD OF REAR SPAR, CRACKED. REPAIRED SKIN PER ER.May 12, 2004 · N389SW · Boeing 7373H4SDR SIMA200415415Skin · dentedABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZONTAL STAB UPPER SKIN. REMOVED DAMGAED UPPER SKIN. I NSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS3079, REV 43, 51-40-21, 22, 23, 25, 40, 51-20-50, 56, AND SAAB REPAIR STATEMay 9, 2004 · N400BR · Saab 340BSDR DL76L040410Skin · lightning strikeFOUND ON ARRIVAL LIGHTING STRIKE AND DAMAGE ON LT HORIZONTAL STAB, L1 DOOR AREA. REPAIRED SAMEMay 7, 2004 · N182DN · Boeing 767332SDR CALA0400479Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5510-01741.May 7, 2004 · N27610 · Boeing 737524SDR IXXA0400074SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND RT HORIZONTAL STAB LE HAS AN INTERIM REPAIR. STA XFS. 109.750. REPAIR WAS ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG1. FABRICATED DOUBLER. CLEANED, TREATED AND PRIMED AREA AND DOUBLER INTERNAL PART IAW SMay 3, 2004 · N830BX · Doug DC871FSDR IXXA0400073SSkin Panel · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE HAS AND INTERIM REPAIR. STA XFS 210.000. REPAIR WAS ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER AND FILLER IAW SRM 55-2-1 PG 17 FIG 4. CLEANED, TREATED AND May 3, 2004 · N830BX · Doug DC871FSDR 04FDEA01122Skin · corrodedHORIZONTAL STAB RIGHT UPPER AFT PLANK NR 32R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER, BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08.Apr 30, 2004 · N590FE · Doug MD11SDR 04FDEA01123Skin · corrodedHORIZONTAL STABILIZER UPPER FWD PLANK NR 8R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08.Apr 30, 2004 · N590FE · Doug MD11SDR 04FDEA01121Skin · corrodedHORIZONTAL STAB UPPER FWD PLANK NR 14R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76018, HORIZONTAL STABILIZER BARREL NUT BORE 14 RT FITTING FABRICATION.Apr 30, 2004 · N590FE · Doug MD11SDR 04FDEA01120Skin · corrodedHORIZONTAL STAB LEFT UPPER FWD PLANK NR 14L BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED FEDEX EA NR 1-5510-76030, HORIZONTAL STABILIZER BARREL NUT BORE 14 LT FITTING FABRICATION.Apr 30, 2004 · N590FE · Doug MD11SDR 2004UALA00404Skin · dentedL/E HORIZ STAB LE IS DENTED AT LE STA 115. TRIMED OUT DAMAGE, INSTALLED INTERNAL DOUBLER AND FILLER.Apr 26, 2004 · N387UA · Boeing 737322
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