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 DALA2023110509104Unknown · unknownSHIP 194 FOUND RH SIDE FORWARD SKIN PANEL IN SECTION 48 UNDER PANEL 314CRX FRONT CORNER; BETWEEN STA 1725.5 AND 1746.125 WORN. CORRECTIVE ACTION: THE DAMAGED FOREARD SKIN PANEL REMOVED AND REPAIRED AS PER B767-300 SRM 53-80-01 (0044394)SDR DALA2023110509103Unknown · unknownSHIP 194 FOUND LH SIDE FORWARD SKIN PANEL IN SECTION 48 UNDER PANEL 313CLX FRONT CORNER; BETWEEN STA1725.5 AND 1746.125 WORN. CORRECTIVE ACTION: THE DAMAGED FOREARD SKIN PANEL REMOVED AND REPAIRED AS PER B767-300 SRM 53-80-01 (0044384)SDR SWAA2023120716580Skin Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.700 INCH. APPROX. 2023-682004<[01] TOOL USED PN: NORTEC 600D; SN: 200048001; CAL DUE DATE: 01SDR DALA2023110509102Unknown · unknownSHIP 194 FOUND LH SIDE LOWER SKIN PANEL IN SECTION 48 UNDER PANEL 313CLX FRONT CORNER BETWEEN STA 1725.5 AND STA 1746.125 WORN. CORRECTIVE ACTION: REMOVED THE DAMAGED PART OF THE SKIN PANEL AND CUT THE SKIN AT STA 1762 AND REPAIRED AS PER B767-300 SRM 53-80-01SDR DALA2023110509101Unknown · unknownSHIP 194 FOUND RH SIDE LOWER SKIN PANEL IN SECTION 48 UNDER PANEL 314 CRX FRONT CORNER BETWEEN STA 1725.5 AND STA 1746.125 WORN. CORRECTIVE ACTION: REMOVED THE DAMAGED PART OF THE SKIN PANEL AND CUT THE SKIN AT STA 1762 AND REPAIRED AS PER B767-300 SRM 53-80-0SDR DALA2023110509100Unknown · unknownSHIP 1703 CHECK FOUND MULTIPLE NICKS OF R HORI-STAB L/E PNL 342CR SURFACE. CORRECTIVE ACTION: THE NICKS REPAIRED OF R HORI-STAB L/E PNL 342CR SURFACE AS PER PRI 612883-14.REV.0. (0041360)SDR DALA2023110509099Unknown · unknownSHIP 1703 CHECK FOUND MULTIPLE NICKS OF R HORI-STAB L/E PNL 342BR SURFACE. CORRECTIVE ACTION: COMPARE AND COMPLIANCE WITH THE ER/A 612883-14 REV. (0041350)SDR COEA2024040503903Skin · dentedWO 250268 NR 26, HAIL DAMAGE/DISCREPANCY: L/H HORIZONTAL STABILIZER UPPER SKIN HAS DENTS. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00230417_07...23074 ISSUE A, DATED 3/29/2024.SDR SWAA2023103015404Skin · pulledWHILE ACCOMPLISHING THE DVI ON TTG8Q00P7WPE; FOUND 1EA RIVET PULLING AND 2EA RIVETS ALMOST COMPLETELY PULLED THROUGH DUE TO DAMAGED LEADING EDGE RIB BEING BENT. SUBMITTED TSR#2023008744<[01] R+R RH HORIZONTAL STAB LEADING EDGE REF AMM 27-41-21.SDR SWAA2023111514756Skin · crackedRH HORIZONTAL STABILIZER LOWER SKIN - CRACK FOUND TO BE .5' LONG AT 18' FROM FWD EDGE AT STA 193.90<[01] COMPLETED STEP#10;[02] REPAIRED RH HORIZONTAL STABILIZER LOWER SKIN PER SRM 55-10-01-2R-11.<BR><BR>TASK CARD COMPLETED.;[03] CARD COMPLETESDR AALA202310313883Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 111.10, 10 INCHES AFT OF FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR SWAA2023112713850Access Panel · crackedCRACK ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER 2023-661369<[01] TOOL USED CALIPER P/N: 500-197-30; S/N 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED HOT BONDER P/N HCS9200B; S/N 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N CL5000; S/N AE-40875SDR CALA2023102503181Skin · damagedSUPPORT TASK REPLACE RIGHT HORIZONTAL LEADING EDGE #2 INBD SECTION AT LE-STA 133-198. T REMOVED DAMAGED SECTION OF RIGHT HORIZONTAL LEADING EDGE LEADING EDGE SPLICES IAW BAC DWG 186A1001 REV B SH 7 AND BAC PANEL NO. 2 FROM LE STA 133-198 IAW BAC 737-800 SRM 51SDR CALA2023102503179Skin · dentedSUPPORT TASK INCOMING WRITE UP LOG PAGE # 8577830 RIGHT HORIZONTAL LEADING EDGE HAS DENT #4 SKIN SECTION LE STA 267. TRANSCRIBED FROM HAECO NR9285129 REPAIRED RIGHT WING HORIZ LEADING EDGE AT NO. 4 SKIN SECTION LE STA 267 IAW B737-800 SRM 52-10-01-2R-2 REPAIR SDR AALA202310276655Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT RIB 101.7 AND 20.5 INCHES FORWARD OF THE REAR SPAR. REPAIRED RIGHT HAND HORIZONTAL STABILIZER SKIN PER SRM 55-10-01-2R-11.SDR AALA202310274905Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT RIB 101.7 AND 2.5 INCHES FORWARD OF THE REAR SPAR. REPAIRED RIGHT HAND HORIZONTAL STABILIZER SKIN PER SRM 55-10-01-2R-11.SDR AALA202310272883Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT RIB 101.7 AND 11 INCHES FORWARD OF THE REAR SPAR. REPAIRED RIGHT HAND HORIZONTAL STABILIZER SKIN PER SRM 55-10-01-2R-11.SDR AALA202310270862Skin · crackedAIRCRAFT IN BASE MAINTENANCE: TAIL CRACK LOWER SKIN OF RIGHT HAND HORIZONTAL STABILIZER AT RIB STA 141.5 AND 18 INCHES FORWARD OF THE REAR SPAR. REPAIRED RIGHT HAND HORIZONTAL STABILIZER SKIN. PER SRM 55-10-01-2R-11.SDR AALA202310276396Skin · crackedAIRCRAFT IN BASE MAINTENANCE: TAIL CRACK LOWER SKIN OF RIGHT HAND HORIZONTAL STABILIZER AT RIB STA 141.5 AND 10 INCHES FORWARD OF THE REAR SPAR. REPAIRED RIGHT HAND HORIZONTAL STABILIZER SKIN. PER SRM 55-10-01-2R-11.SDR AALA202310273586Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT RIB 97.7 AND FORWARD OF THE REAR SPAR. REPAIRED RIGHT HAND HORIZONTAL STABILIZER SKIN PER SRM 55-10-01-2R-11.SDR SWAA2023110811368Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 105.26 AT LT HORIZONTAL STABILIZER 2023-635562<[01] REPLACED LEADING EDGE RIB (CHORD) AND FASTENERS IN ACCESS PANEL 331B LOCATED AT LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 PSDR SWAA2023110811366Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 133.15 AT LT HORIZONTAL STABILIZER 2023-635563<[01] REPLACED RIB LOCATED LEADING EDGE RIB OF ACCESS PANEL 331B AT LE STA 133.15 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-0SDR SWAA2023110711367Access Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 95.96 AT LT HORIZONTAL STABILIZER 2023-635561<[01] REPLACED LEADING EDGE RIB ACCESS PANEL 331B LOCATED AT LE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51SDR SWAA2023102011226Panel · out of positionRIGHT HORIZONTAL STAB PANEL 343AB SLIDE SEAL IS NOT PROPERLY IN SLIDE SEAL TRRACKS<[01] REMOVED AND PROPERLY REINSTALLED PANEL 343AB PER AMM 20-50-11-910-801<BR>CAL TOOL: ATS1731 DUE: 07/2024;[02] INSPECTED AND VERIFIED INSTALLATION. JOB COMPLETE.SDR SWAA2023110909225Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. 2023-637729 / [01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 22027SDR CALA2023101303048Skin · dentedRH HORIZ STAB TIP 342AB HAS LE DENTS PER NR 9298451 / 32451 EVALUATED 2EA DENTS ON RH HORIZONTAL STAB TIP, 342AB. DENT #1 WA IAW SRM 55-41-11-283-001 FIG 5 AND 6 AND 55-14-11-300-006. REPAIRS LOCATED IN ZONE #3 I/B OF RIB 25 AND REQUIRED REPAIR. CUT OUT R FOR SDR SWAA2023120507120Skin · crackedCRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 16.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH 1.281' CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH 1'<[01] PERFORMED SME SDR ASAA2023093045803Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STA 101.90 FORWARD OF DRAIN HOLE. (MARKED). GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN AT STA 101.90 FORWARD OF DRAIN HOLE IAW B737-800 SRM 55-10-01-2R-11, THIS IS A CAT B REPAIR WITH SUPPLEMENTAL ISDR ASAA2023093045802Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STA 101.90 AFT OF DRAIN HOLE. (MARKED). GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN AT STA 101.90 AFT OF DRAIN HOLE IAW B737-800 SRM 55-10-01-2R-1A, THIS IS A CAT B REPAIR WITH SUPPLEMENTAL INSPECTIOSDR ASAA2023093045801Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STA 147.90. (MARKED). GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN AT STA 147.90 IAW B737-800 SRM 55-10-01-2A-11, THIS IS A CAT B REPARI WITH SUPPLEMENTAL INSPECTION OF 56,000 TOTAL FLIGHT CYCLES WITHSDR DALA2023100308137Unknown · unknownSHIP 6807 IN REF TO NRC 00034: DENT ON LH HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 332BL WAS FOUND OUT OF LIMITS. CORRECTIVE ACTION SUMMARY OF NRC 00162: DENT ON LH HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 332BL WAS REPAIRED PERMANENTLY PER ERA 6SDR CALA2023092902915Skin · damagedREPAIR DOUBLER INSTALLED ON L/H HORIZONTAL STAB LOWER SKIN AT STAB STA 92.70 6 INCHES AFT OF FWD SPAR. THIS REPAIR DOUBLER WAS INSTALLED FOR THE REAIR OF ACCESS HOLES CUT IN SKIN FOR THE REP AIR OF RIB STIFFENER #1 REF. N/R 001622419 AND STIFFENER #2 REF N/R 0SDR CALA2023092902913Skin · damagedREPAIR DOUBLER INSTALLED ON R/H HORIZONTAL STAB LOWER SKIN AT STAB STA 92.50 TO STAB STA 101.90 12 INCHES FWD OF THE REAR SPAR .THIS REPAIR DOUBLER WAS INSTALLED FOR THE REPAIR OF ACCESS HOLES CUT IN SKIN FOR REPAIR OF RIB STIFFENER #3 REPAIR REF. A SIGNIFICANSDR SWAA2023110205093Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 25.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.03 INCHES 2023-614913<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DSDR SWAA2023110205092Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.06 INCHES 2023-614912<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DSDR UIEA2023092200843Unknown · unknownRH HORIZONTAL STAB EXFOLIATION CORROSION UPPER SKIN FROM HSBL 340.00 TO 350.00(<P>WAS REPAIRED IAW EO TRE6755062 AND BAC MSG CMA-TLS-23-0142. NO FURTHER DEFECTS NOTED</P>)SDR CALA2023092902902Skin · damagedREPAIR DOUBLER INSTALLED ON L/H HORIZONTAL STAB LOWER SKIN AT STAB STA 92.70 6 INCHES AFT OF FWD SPAR. THIS REPAIR DOUBLER WAS INSTALLED FOR THE REAIR OF ACCESS HOLES CUT IN SKIN FOR THE REPAIR OF RIB STIFFENER #1 REF. N/R 001622419 AND STIFFENER #2 REF N/R 00SDR CALA2023092902901Skin · damagedREPAIR DOUBLER INSTALLED ON R/H HORIZONTAL STAB LOWER SKIN AT STAB STA 92.50 TO STAB STA 101.90 12 INCHES FWD OF THE REAR SPAR .THIS REPAIR DOUBLER WAS INSTALLED FOR THE REPAIR OF ACCESS HOLES CUT IN SKIN FOR REPAIR OF RIB STIFFENER #3 REPAIR REF. BA M N/R 001SDR CALA2023092902903Panel · crackedSUPPORT TASK- R/H HORIZONTAL STABILIZER, UPPER INBOARD PANEL LAND CRACKED AT NUTPLATE LOCATION. TRANSCRIBED FROM HAEC OGSO NRC# 9282697. ACCOMPLISHED UAL ECRA 5516-01043.SDR CALA2023092702885Skin · crackedREPAIR DOUBLER INSTALLED ON L/H HORIZONTAL STAB LOWER SKIN FROM STAB STA 129.50 TO STAB STA 138.70 10 INCHES AND 18 INCHES FROM REAR SPAR TO REPAIR A .250 CRACK IN LOWER SKIN. A SIGNIFICANT FI NDING REPORT IS REQUIRED TO BE ISSUED FOR THE CRACK. SEE BAM NON -RSDR SWAA2023110103608Access Panel · elongatedR/H HORIZONTAL STAB. LOWER T/E ACCESS PANEL # 343DB HAS ELONGATED HOLES<[01] PPLIED PERMANENT REPAIR ON DAMAGE AREA ON R/H HORIZONTAL STAB. LOWER T/E ACCESS PANEL # 343DB AS MARKED AS PER B737 SRM 55-10-01-2R-9; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRSDR DALA2023092907993Unknown · unknownSHIP 1702 THE HORI- STAB CENTER SECTION UPPER SKIN CORROSION AT LBL13.83 TO BL0 AND S-11 TO S-8. CORRECTIVE ACTION: DAMAGED REPAIRED PER 14-611999 (2984373)SDR DALA2023092507896Unknown · unknownSHIP 1702 ER/A 611999-14, DURING HCK AT STAG, CORROSION WAS NOTED ON THE HORIZONTAL STAB CENTER SECTION UPPER FWD SKIN IN SEVERAL AREAS. SECTION I REPAIR WAS COMPLETED, FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ER/A 611999-14 SECTION I REQUIRES REVISIONSDR DALA2023092507895Unknown · unknownSHIP 1702 THE HORI-STAB CENTER SECTION UPPER SKIN CORROSION AT RBL 13.83 TO BL0 AND S-11 TO S-8. CORRECTIVE ACTION: THE HORI-STAB CENTER SECTION UPPER SKIN CORROSION AT RBL 13.83 TO BL0 AND S-11 TO S-8 BLEND OUT REFER TO NRC 300-003 (2981428)SDR DALA2023092507894Unknown · unknownSHIP 1702 THE HORI-STAB CENTER SECTION UPPER SKIN CORROSION AT LBL 13.83 TO BL0 AND S-2 TO S-5. CORRECTIVE ACTION: CORROSION BLEND OUT AND DOUBLER REPAIR AS PER PRI: 612000- 14 REV.0. CAMPARED AND COMPLIED WITH ERA 612000-14 (2981413)SDR P5CA2023082800082Unknown · unknownLH I/B ELEVATOR L/E SKIN ELEV. STA 119.358 PER EA 4855A0004 HAS BEEN REVISED EA 4855A005 PERMANENT REPAIR WITHIN 500 FC PER EA(<P>L/E SKIN REPAIRED AS PER RI #RI-55-20-16459 REV A. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202309201628Panel · crackedRIGHT HORIZONTAL PANEL 345BB CRACKED. EVALED PANEL CRACK FOUND TO BE IN TEDLAR ONLY, NO COMPOSITE DAMAGE NOTED, NO REPAIR REQUIRED IAW B757 SRM 55-10-01-1A, 55-10-01-2R REPAIR 5 FIG 201, 51-70-05-OG AND NDT PART 51-05-01 RESTORED TEDLAR DAMAGE IAW B757 SRMSDR FDEA202309201627Panel · crackedLH HORIZONTAL T/E PANEL 335BB CRACKED. ACCOMPLISHED PERMANENT REPAIR TO LEFT HORIZONTAL T/E PANEL 335BB IAW FEDEX B757 SRM 55-10-01-1A, 51-70-05-0G,55-10-01-2R FIG 201 REPAIR 5 SHEET 2.SDR SWAA2023110701991Skin · crackedCRACK FOUND AT RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16.5' FROM FRONT SPAR ; I/B ROW. CRACK LENGTH : 0.593' CRACK FOUND AT RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 0.593'<[01] ACOMPLSDR SWAA2023110701992Skin · crackedCRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 17.25' FROM FRONT SPAR ; I/B ROW. CRACK LENGTH : 0.468' CRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 17.25' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 0.468'<[01] ACC
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