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 07FDEA01854Panel · damagedRT LOWER I/B PNL NR 9214 IS DAMAGED ON HORIZ STAB. REPAIRED RT HORIZONTAL STAB PANEL NR 9214 REF SRM 55-20-3 FIG 1 AND SRM 55-10-2 PG 1, FIG 1, SHT 1.SDR SWAA072442Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SWA EA.SDR TSAA0753024Spar · corrodedFOUND CORROSION HAS BEEN IDENTIFIED ON THE LEFT HORIZONTAL STABILIZER AT LOCATION STAB STA 230.7. [SUP 06-01-07] THE HORIZONTAL STABILIZER WAS REMOVED AND REPLACED IN ACCORDANCE WITH AMM 27-41-11. THE AIRCRAFT WAS RETURNED TO SERVICE ON MAY 31, 2007.SDR SWAA072398Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 128, 24 INCHES AFT OF FRONT SPAR. REPAIRED SKIN PER SWA EA.SDR K11A2008112872219Skin · corrodedRT STAB TOP SKIN HAS SURFACE CORROSION AT THE 3 OTBD ELEVATOR HINGE POINT. ( RT STAB STA 168 )SDR ASAA0741641Skin · damagedDAMAGE TO LEFT LEADING EDGE HORIZ STAB. REMOVED L/E AND ACCOPMLISHED REPAIR IAW SRM 55-10-01 REPAIR 3.SDR 07FDEA01730Skin · dentedACF MODIFICATION AND REPAIR ASSESSMENT HORIZONTAL STABILIZER LT SIDE DENTS, NICKS, DEFORMATION RIB AND SKIN AND 10 EA RIVETS LOOSE ON LOWER SKIN B/T STA 48.500 TO STA XE 67.225 AND STA XE 88.625 TO STA XE 100.455. REMOVED DETACHABLE ELEVATOR , REMOVED LWR SDR FDKA200705238Elevator · damagedUPPER SURFACE OF RIGHT ELEVATOR IS DAMAGED 3.6 INCHES FROM THE OUTBOARD END. THE DAMAGE HAS BEEN REPAIRED.SDR SWAA072302Skin · crackedDURING SCHEDULED 8Y CHECK, FOUND LEFT HORIZONTAL STAB LOWER SKIN CRACKED 12 INCHES FROM AFT SPAR, 27 INCHES FROM INBOARD EDGE. REPAIRED SKIN PER SRM.SDR EIA2007113Skin · damagedLEFT HORIZONTAL STABILIZER STATION 210 UPPER SIDE OF THE WEB STIFFENER AT LEFT ACCESS CUT-OUT HAS TOOLING MARKS 2 EA. INSTALLED REPAIR PLATE, FILLER AND 2 EACH WEB STIFFENERS AT LEFT HORIZONTAL STABILIZER STATION 210 PER B747 SRM 55-10-06 PAGES 8-9 AND 51-30-SDR SWAA072256Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM.SDR SWAA072172Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SWA EA.SDR 07FDEA01683Skin · corrodedLT HORIZONTAL STAB EXTERNAL SKIN HAS CORROSION ON UPPER SURFACE AT REAR SPAR XE 48.5. ALL WORK ACCOMPLISHED ON FEDEX EA.8-5500-110623-STAB, LT SIDE-UPPER AFT SPAR.SDR USAA070347Skin · crackedBOTTOM SIDE OF RT HORIZ STAB SKIN SPAR STA 133.70 CRACKED. INSTALLED DOUBLER PER TR 55-10-07, REV B, DEFECT SIZE: 1 INCH.SDR USAA200705002Skin · cracked2" CRACK FOUND AT RT HORIZ STAB LOWER SKIN CENTER OF 3" PANEL. (CLT) INSTALLED TEMPORARY DOUBLER PER TR 55-10-07 REV B.SDR 07FDEA01575Skin · crackedHORIZONTAL STABILIZER LWR INT SKIN PANELS CONSTANT SECTION CRACKED INFLYABLE LIMIT ACCOMPLISH EA 8-5510-96122.SDR F3LA200700104Skin · puncturedDURING TAKEOFF, NR 2 ENGINE FAN COWL DEPARTED AIRCRAFT HITTING OTBD HORIZONTAL STABILIZER LEADING EDGE. PUNCTURE WAS FOUND ABOUT MID SPAN OF LEADING EDGE. REPLACED RT OTBD HORIZONTAL STAB L/E IAW AMM 55-12-11-400-001, REFERENCE SDR F3LA200700083.SDR DLM88070342Skin · crackedDURING ACCOMPLISHMENT OF EA 09-460214-12 OPN 0101, THE TRIM OUT IN THE HORIZONTAL STAB UPPER INBOARD SKIN PANEL EXTENDED PAST THE BARREL NUT PAD UP. THE TRIM OUT AND SPOTFACE INTO THE PAD UP WAS SUBMITTED TO BOEING FOR APPROVAL, AND WAS APPROVED AS A TEMPORARSDR SWAA071957Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 127. REPAIRED SKIN PER ER.SDR USAA070303Skin · crackedFOUND CRACK LEFT STAB LOWER SKIN JUST FWD OF FASTENERS IN REAR SPAR NEAR STAB STA 118. FAB'D AND INSTALLED FILLER AND DOUBLER PER TR 55-10-07, DEFECT SIZE: 1.2".SDR DHL2007788521Panel · crackedVERTICAL LE PANEL NR 9502 LOWER INTERIOR PANEL BENT AND CRACKED. REMOVED PREVIOUS REPAIR ON PANEL NR 9502 IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 7075T6 .025 (16.5" BY 8.5") PO NR 9004219 IAW B727 SRM 55-30-2 FIG 2 AND 51-40-2 FIG 1. TREATED AND PRISDR 07FDEA01507Skin · dentedTHS - FRACTION 341BB AT L/E OF RT THS W/UPPER SKIN SURFACE W/DENT REPAIRED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".SDR DLM88070553Skin · crackedTHE RT HORIZONTAL STABILIZER UPPER INBD SKIN PANEL FOUND CRACKED - 1.25 IN LONG. THE CRACK WAS CUT OUT OF THE SKIN AND INSPECTED. THE PANEL WILL BE REPLACED AT WITHIN 2000 FLIGHT HOURS.SDR 2007UALA01147Skin · dentedDENT IN RT HORIZONTAL STABILIZER LEADING EDGE APPROX SIX RIVET ROWS FROM FUSELAGE. [SUP 5-10-07] MAJOR REPAIR: INSTALLED DOUBLER REPAIR PER SRM 55-10-01 PG 201-203 REPAIR NR 2.SDR 2007UALA01140Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN CRACKED JUST FWD OF I/B BALANCE BAY, APPROX 65 INCHES O/B OF TAIL CONE. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL SKIN DOUBLER & ACCESS HOLE DOUBLER REPAIR.SDR USAA200704003Skin · cracked2.5 INCH CRACK FOUND AT LOWER SKIN AT STAB ST. 98-100 (TE). INSTALLED DOUBLER IAW EA 98607 AND TR 55-10-07B.SDR DLM88070294Skin Panel · crackedFOUND CRACK, HORIZONTAL STAB UPPER SKIN SPLICE, RT.SDR DALA1111060915Skin · damagedHORIZ STAB REAR SPAR UPPER CAP, UPPER AND LOWER AFT SKIN REPAIRED IAW EA 09-460214-12, ME02.SDR USAA070236Skin · crackedLEFT HORIZONTAL STAB, LOWER SURFACE AFT T/E SKIN BETWEEN STA 157.5 & 184.7 HAS CRACK. INSTALLED REPAIR DOUBLERS PER EA 98564 & SRM 55-10-07, DEFECT SIZE: 2 INCHES.SDR C2XA07SH016Skin · corrodedSHV DURING C-CHECK LEFT HORIZONTAL STABALIZER LEADING EDGE HAS PITTING CORROSION. MX REPAIRED LEFT HORIZONTAL STABALIZER IAW EC 5530-01116. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR 07FDEA01119Skin · crackedRT HORIZONTAL AT STA. XE87 UPPER SKIN PLANK STRINGER 4 IS CRACKED. ACCOMPLISHED REPAIR IAW EA 8-5510-105177-STABILIZERS-HORIZ.-RT AFT OUTB. UPPER PANEL S4R CRACK AT XE 87-REPAIR. MECH 2579SDR DHL2007786502Skin · dentedRT HORIZ STAB LWR SURFACE HAS A DENT, STAB STA 144, 11 AFT OF L/E. CUT OUT DAMAGED AREA AT RT HORIZ STAB LWR, MEASUREMENTS, 1.25 BY 1.75 IAW B727 SRM 55-10-3. FABRICATED DOUBLER REPAIR FROM 2024T3, .080, 7.875 BY 5.375 IAW B727 SRM 55-10-3, FIG 3. TREATED ASDR 2007UALA00784Skin · damagedRIGHTT HORIZONTAL STABILIZER LOWER SKIN HAS IMPACT DAMAGE. RT HORIZONTAL STABILIZER REPAIR ACCOMPLISHED PER UAL EVA 70128. A/C READY FOR RETURN TO SERVICE. SUSPECT DAMAGED BY GROUND EQUIPMENT OR RUNWAY KICK-UP FOREIGN OBJECT.SDR UPS07449429Skin · damagedHOLE IN FUSELAGE TAIL SECTION LEFT SIDE ABOVE HORIZONTAL STABILIZIER/ ELEVATOR APPROX 5 X 7 INCHES. FABRICATED AND INSTALLED SHEET METAL DOUBLER PER 747 SRM 53-30-03.SDR USAA200703001Skin · crackedA 2.25 INCH CRACK FOUND AT LT HORIZONTAL STAB LWR SKIN STA 115. INSTALLED DOUBLER PER SRM 55-10-01.SDR IXXA07SMN132SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER HAS ELONGATED HOLES AT LEADING EDGE STATION XFS 285.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER SDR DLM88070189Skin · crackedFOUND HORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A 1.85" CRACK NEAR THE INBD AFT END OF THE PANEL. THE CRACK WAS STOP DRILLED ON A TIME LIMITED BASIS. THE PERMANENT RESDR 2007UALA00641Skin · gougedRUDDER LEFT SIDE - HAS GOUGE WEAR FROM BLADE SEAL NEAR THE BOTTOM. *S/D* MAJOR REPAIR: ACCOMPLISHED COMPOSITE REPAIR PER AAR EA-I070147.SDR DLM88070184Skin · crackedHORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .25" CRACK NEAR THE INBD AFT EDGE OF THE PANEL. THE CRACK WAS STOP DRILLED ON THE FWD END AND ROUTED OUT TO THE AFT EDGE OFSDR DLM88070183Skin · crackedHORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL CRACK REPAIR. THE UPPER AFT SKIN OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .625" CRACK NEAR INBD AFT EDGE OF THE PANEL. THE CRACK WAS ROUTED OUT WITH A SMALL CUTOUT ON A TIME LIMITED BASIS PER ER/A 460SDR DLM90070559Skin · crackedTHE RT UPPER SKIN PANEL ON THE HORIZONTAL STABILIZER WAS FOUND CRACKED. THE CRACKED SKIN WAS CUT OUT AND A NEW SKIN PANEL WILL BE INSTALLED WITHIN 2000 FLIGHT HOURS.SDR SWAA071151Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB SKIN CRACKED AT LOWER SURFACE STA 120. REPAIRED SKIN PER SRM.SDR DU4R2007067Repair · damagedFOUND CORROSION BLEND OUTS AND EXISTING EXTERNAL REPAIRS ON LT HORIZONTAL STABILIZER INBD LEADING EDGE. REPAIRED BY FABRICATING AND INSTALLED REPAIRS 17-1/4 BY 5-1/2, 15 BY 4-1/2 AND 5-1/2 BY 5-1/2 FROM 6AL-4V032 AND 6.0 BY 6.0, 15-1/2 BY 5-1/4 AND 5-1/4 BY 5SDR DU4R2007066Repair · damagedFOUND CORROSION BLEND OUTS AND EXISTING EXTERNAL REPAIRS ON LT HORIZONTAL STABILIZER INBD LEADING EDGE. REPAIRED BY FABRICATING AND INSTALLED REPAIRS 5 BY 4 FROM 6AL-4V040 AND 6 BY 5 FROM 6AL-4V032 AS DIRECTED TIMCO RFTS 60030 AND REO-L00677 REV A DATED 10-3SDR 07FDEA00593Skin · crackedLT HORIZ STAB OUTER SECTION UPPER AFT SKIN PANEL FOUND 1 CRACK 2, 5" LONG. REPAIRED CRACKED SKIN PANEL IAW SB 55-18 AND EA NR 8-5510-103679. WORKED IN CONJUNCTION WITH NRC N00898/I030898.SDR DHL2007781014Skin · gougedRT NR 5 BALANCE BAY (HORIZ STAB) UPPER SKIN GOUGED. REMOVED GOUGED PREVIOUS REPAIR DOUBLER. FABRICATED NEW DOUBLER FROM 7075-T0, .032" BY 6" BY 5", PO NR 44953 PER B727 SRM 55-20-3 FIG 3. HEAT TREATED REPAIR TO T6 CONDITION IAW FASI FORM FAS 0115. TREATED,SDR DLM8K070156Skin · crackedFATIGUE CRACK FOUND IN RT HORIZONTAL STABILIZER UPPER INBOARD SKIN PANEL. SKIN PANEL REPLACED.SDR DLM88070558Skin · crackedRT HORIZONTAL STABILIZER SKIN WAS FOUND CRACKED IN UPPER SKIN, 0.75 IN. LONG. THE CRACK WAS CUT OUT OF THE SKIN AND A NEW SKIN WILL BE INSTALLED WITHIN 2000 FLIGHT HOURS.SDR DLM88070155Skin · crackedHORIZONTAL STABILIZER, RT UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL ON THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .75" CRACK NEAR THE AFT INBD CORNER OF THE PANEL. THE CRACK WAS HFEC INSPECTED AND STOP DRILLED ON TIME LIMITED BASIS. THSDR DLM88070154Skin · crackedFOUND HORIZ STAB RT UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A 1.5" CRACK AT THE INBD AFT CORNER OF THE PANEL. THE CRACK WAS STOP DRILLED ON A TIME LIMITED BASIS PER ER/A 460327-14. THE DAMA
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