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 05FDEA02570Skin · damagedHORIZONTAL STAB CONSTANT SECTION FOUND 1EA DOUBLER REPAIR ON AFT BLKHD AT STA 2123 X=-40 RT SIDE. REPAIRED IAW SB 55A028 AND DWG SR10550007.SDR IXXA05RNG049SSkin · dentedDURING INSPECTION CHECK, SKIN DENT AND SCRATCH DAMAGE WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT UPPER PLATING AROUND L/E STATION XFS 146.00. REMOVED DAMAGE AREA AND DOUBLER WAS INSTALLED IAW EWO ATI 55-05 & EO ATI-071905. EDDY CURRENT INSPESDR MALA050659Skin · dentedDURING 4Y/2Y INSPECTION, FOUND RT HORIZONTAL STABILIZER UPPER SURFACE IS DENTED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$55056. REF: EAMS WORK ORDER 212631 TASK 3504.SDR MALA050660Skin · dentedDURING 4Y/2Y INSPECTION IN BNA, FOUND RT HORIZONTAL STABILIZER UPPER SURFACE IS DENTED. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#$55056. REF: EAMS WORK ORDER 212631 TASK 3505.SDR USAA051006Skin · crackedCLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K)SDR USAA051005Skin · crackedCLT - Q6 - LOWER SKIN, 1.7 INCH CRACK LOWER SKIN APPROX STAB STA 129 AT AFT SPAR, HORIZONTAL STAB. REPAIRED AND INSTALLED DOUBLER AND FILLER IAW EA. (K)SDR 05FDEA02433Skin · delaminatedLT HORIZONTAL STABILIZER HAS UPPER TRAILING EDGE PANEL WITH DELAMINATION, BETWEEN INBOARD AND OUTBOARD ELEVATOR ACTUATOR FORWARD ACCESS PANELS, STA XE 160. REPAIRED IAW CHP 51-62-01.SDR ASAA0540384Skin · dentedYXX: DURING C-CHECK FOUND LT HORZ STAB AT STA 166 SKIN UPPER SURFACE HAS 2 PARALLEL DENT WITH CREASES. REPAIRED IAW SRM. (K)SDR 05FDEA02337Skin · damagedLT STAB, XE 101 I/B ELEV, EXISTING 1 EXT REPAIR DOUBLER ON UPPER SKIN. REPLACE REPAIR PER SRM 55-00-01 VOL 1 SHT 2A, 2B FIG 3 SHT 2.SDR SWAA052284Skin · crackedDURING SCHEDULED C2 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBOARD AFT SPAR. REPAIRED HORIZONTAL STAB PER SRM.SDR ASAA0580392Skin · puncturedOKC - DURING HV CHECK, FOUND VERTICAL STABILIZER HAS PUNCTURE ON RIGHT SIDE AT RADIUS FOR HORIZONTAL STABILIZER. REPLACED DAMAGED SKIN SECTION. (M)SDR DHL2005746525Skin · bulgedLT HORIZONTAL UPPER SURFACE REAR CHORD SKIN BULGING OFF FASTENERS STAB 188, MARKED. CUT HORIZONTAL STAB UPPER SKIN FOR ACCESS AT STAB 188 DIM 17 1/2" X 3" IAW B727 SRM 55-10-3 FIG 3. CUT OUT FWD FLANGE OF UPPER T/E SPAR CHORD IAW B727 SRM 55-10-5 FIG 1. REMSDR ASAA0540341Skin · damagedOKC - FOUND LEFT HORIZONTAL STAB L/E STAB STATION 192.54 HAS 2 EACH CREASES. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW 737-400 SRM 55-10-01 FIGURE 203. (M)SDR ASAA0540340Skin · dentedOKC - FOUND SPEED TAPE INSTALLED AT THE L/E IN THE RIGHT HORIZONTAL STABILIZER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER IAW 737-400 SRM 55-10-01 FIG 203. (M)SDR ASAA0540339Skin · damagedOKC - FOUND LEFT HORIZONTAL STAB LEADING EDGE STAB STATION 131.54 HAS NUMEROUS CREASES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 737-400 SRM 55-10-01 FIGURE 203. (M)SDR 2005UALA00583Skin · dentedLT LEADING EDGE OF HORIZONTAL STABILIZER HAS DENT MIDWAY ON THE LEADING EDGE. CUTOUT DAMAGE & EVALUATED PER SRM 55-10-01. ACP NDT PER B737 NDT MANUAL NO DEFECTS NOTED. FABRICATED & INSTALLED INTERNAL DOUBLER REPAIR, FILLER & NEW RIB PER AAR EA I050118.SDR DHL2005741611Skin · dentedRIGHT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN AT STAB STA 109.97 IS DENTED. CUT OUT DAMAGED AREA TWO PLACES DIM 3.5 X 1.25 & 8.5 X 2 INCH IAW B727 SRM 55-10-3 FIG 3. FAB DOUBLER FROM 2024T3 .080 PO 9002555 DIM 15 X 101.5 INCH IAW B727 SRM 55-10-3 FIG 3. SDR WRLA2005111Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 26.SDR WRLA2005109Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE 23.SDR WRLA2005108Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 20.SDR WRLA2005107Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 19.SDR 05FDEA01611Skin · dentedLEFT HORIZONTAL STAB UPPER SURFACE HAS DENT WITH GOUGE 17.5 INCHES FROM I/B END AND 16.5 INCHES FROM AFT END. REPAIRED PER FED EX EA 7-5510-86317.SDR USAA050753Skin · crackedPIT - FOUND H/S LOWER SKIN CRACKED 2 INCHES, RT HORIZ STAB LOWER SURFACE AFT SPAR STATION 124. ACCOMPLISHED REPAIR PER TYPICAL REPAIR 55-10-08 AND SRM 55-10-01 PAGE 212. (M)SDR WRLA2005110Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 25.SDR WRLA2005106Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 17.SDR WRLA2005105Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST RT BARREL NUT HOLE NR 15.SDR WRLA2005102Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 33.SDR WRLA2005101Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 32.SDR WRLA2005100Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 31.SDR WRLA200598Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 29.SDR WRLA200597Panel · corrodedDURING C04 CHECK WHILE PERFORMING INSP PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 28.SDR WRLA200596Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 26.(OPEN)SDR WRLA200595Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 25.(OPEN)SDR WRLA200594Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LH BARREL NUT HOLE NR 23.(OPEN)SDR WRLA200593Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 18.(OPEN)SDR WRLA200591Panel · corrodedDURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 14.(OPEN)SDR WRLA200590Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 13.(OPEN)SDR WRLA200589Panel · corrodedITEM: DURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 9.(OPEN)SDR WRLA200588Panel · corrodedITEM: DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 7.(OPEN)SDR WRLA200587Panel · corrodedDURING C04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 1. (OPEN)SDR 2005UALA00564Skin · lightning strikeLIGHTNING STRIKES LT HORIZONTAL STAB UPPER SURFACE, INBOARD END. LIGHTNING STRIKES LT HORIZ STAB UPPER SURFACE, INBD END. A MAJOR REPAIR WAS INSTALLED PER REO-G1067A & EVA-50377. THIS COMPOSITE REPAIR IS INTERIM (FOR 24 MONTHS - 10JUN07) OR NEXT SCHEDULED 'SDR SWAA051603Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED 36 INCHES FROM INBOARD AFT SPAR. REPAIRED SKIN PER SRM.SDR USAA050676Skin · crackedCLT - FOUND HORIZ STAB LOWER SKIN CRACKED .25 INCH, STATION 125. 3 INCHES FORWARD OF AFT SPAR. REPLACED DOUBLER AND INSTALLED SOLID FASTENERS IAW T/R 55-10-07 REV B, BOEING SRM 55-10-01 FIG 204. (M)SDR 05FDEA01397Panel · damagedHORIZONTAL STABILIZER, UPPER CONSTANT SECTION, WITH PLANK NR 11 WITH CRACK ( 0,75" LENGTH), P/N ALC7228-. REMOVED ALC7228-1 OLD PANEL PER SB 55-16 FIG 4 GR 2. REWORKED NEW PANEL PER SB 55-16 FIG 4 GR 2. INSTALLED NEW PANEL PER SB 55-16 FIG 4 GR 2.SDR 05FDEA01396Panel · damagedHORIZONTAL STABILIZER, UPPER CONSTANT SECTION, WITH PLANK NR 15 WITH CRACK (0,51" LENGTH), P/N ALC7227-1. REMOVED OLD PANEL ALC7228-1 PER SB 55-16. REMOVED PANEL ALC7227-1 PER SB 55-16. REWORKED ALC7227-1 NEW PANEL PER SB 55-16. INSTALLED NEW PANEL ALC7227SDR 05FDEA01372Panel · corrodedHORIZONTAL STABILIZER RIGHT HAND FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REWORKED AS PER FEDEX EA 1-5510-83008.SDR P5CA0501353Skin · deformedDORSAL FIN FOUND WITH DEFECTS DEFORMED AT TOP EDGE. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1I9VRK AND FAA FORM 8100-3.SDR USAA20050006Skin · crackedA 2.1875 INCH CRACK IN LOWER SKIN, AFT SPAR OF HORIZ STAB, STA 123. INSTALLED REPAIR DOUBLER WITH BLIND FASTENERS PER TRR 55-10-07 REV B.SDR 05FDEA01295Panel · corrodedHORIZONTAL STABILIZER RT FORWARD PLANK NR 14R BARREL NUT BORE CORROSION REMOVAL FOUND EXCEEDED LIMITATIONS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II.SDR SWAA051397Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR, STAB STA 157.10. REPAIRED SKIN PER SRM.
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