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 SIMA20230919004Skin · dentedRH LOWER HOR STAB DENTED MY MAN LIFT-C/A-REPAIRED IAW ETD 2023-170-023539 AND NCR EJ-55-014 (MAJOR REPAIR)SDR JGVR20230918001Unknown · unknownREPAIRED CORRODED AREAS OF THE LH & RH HORIZONTAL STABILIZER SKINS NEAR THE END RIBS, BY MECHANICALLY BLENDING AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATED AND INSTALLED REPAIR DOUSDR SWAA2023102601341Rib · crackedLH HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB #9 IS CRACKED<[01] UPDATED MEASURMENT TABLE;[02] REMOVED AND REPLACED L/H HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB # 9; LE STA 151.75.;[03] ADDED REFERENCE FOR CORRECTIVE ACTION. 2. : REMOVED AND REPLACED L/HSDR ASAA2023091345319Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN HAS A CRACK INDICATION LOCATED AT STAB. STA. 147.90, 8" FWD OF THE REAR SPAR. APPROX. 1.2" IN LENGTH. (AS MARKED). GROUNDED - YES. REMOVED R/H HORZ. STAB LEADING EDGE AND HORZ. STAB TIP, REMOVED EXISTING DOUBLER IAW B737-80SDR JJBA20230920036Unknown · unknown2X NUT PLATES DAMAGED ON LH SIDE OF FORE RUDDER ASSEMBLY. SKIN REPAIRED WITH A SPLICE.SDR SWAA2023101698961Access Panel · crackedCRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2023-569591<[01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02;[02] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02.SDR 2023FA0000530Skin · corrodedLH AND RH HORIZONTAL SKIN CORROSION AND SPLICE PLATE CORROSIONSDR SWAA2023100697948Skin 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 = 0.900 INCH. APPROX. 2023-568775<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; SDR SWAA2023100697968Skin Panel · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.000 INCH. APPROX. 2023-575222<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00SDR CALA2023090802736Skin · damagedREPAIR L/H HORZ STAB LWR SKIN CUTOUT TO ACCESS RIB DAMAGE AT STAB STA 138.70 AND EXT.LFEC INSP.WITH REPEAT INSP EVERY 9,000 FLT CYCLES REPAIRED SKIN IAW SRM 55-10-01-2R-11. REQUIRES DIP IAW TABLE 204. INSP THRESHOLD 56,000 TOTAL FLT CYCLES DETAILED VISUAL INSPSDR CALA2023090802735Skin · damagedREPAIR R/H HORZ STAB LWR SKIN CUTOUT TO ACCESS RIB DAMAGE AT STAB STA 120.3 REPAIR AND EXT.LFEC INSP.WITH REPEAT INSP EVERY 9,000 FLT CYCLES REPAIRED SKIN IAW SRM 55-10-01-2R-11. REQUIRES DIP IAW TABLE 204. INSP THRESHOLD 56,000 TOTAL FLT CYCLES DETAILED VISUASDR SWAA2023101797257Skin · crackedCRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90; 8.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH : 1'. CRACK FOUND ON LOWER SKIN OF R/H HORIZONTAL STABILIZER AT STAB STA 193.90 8.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 1'.<[01] STEP 12SDR DALA2023090607287Unknown · unknownSHIP 3126 CRACK ACCESS PANEL 332AB ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 611030-14 REV. (2953492)SDR AALA202309206148Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.9, 17 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202309205786Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 9 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202309200375Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.7, 9 INCHES AFT OF FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR SWAA2023092695561Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 27' FROM FWD EDGE AT RIB STA 184.70<[01] REPAIRED PER EA 23-155-02717 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 23-155-02717-INSP.';[02] TASK CARD COMPLETE.SDR SWAA2023092695565Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 18' FROM FWD EDGE AT RIB STA 193.90<[01] REFER TO FAULT TTG8Q00N5DVD WHERE EA 23-155-02717 WAS ADDED AS A SUBTASK;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023091494900Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT RIB 101; 11 TO 12 INCH AFT OF FRONT SPAR<[01] VERIFIED STEPS 1;3 IN PARTIAL.;[02] MEASUREMENT TABLE UPDATED.;[03] REMOVED THE DAMAGE PART ON RIGHT HORIZ. STAB LOWER SKIN AT RIB 101;11 TO 12' AFT OF FRONT SPAR; ANDSDR SWAA2023091494899Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT RIB 138; 33 TO 35 INCH AFT OF FRONT SPAR<[01] VERIFIED STEP 3 IN PARTIAL.;[02] MEASUREMENT TABLE UPDATED.;[03] TRIMMED OUT THE DAMAGE PART OF THE RIGHT HORIZ. STAB LOWER SKIN AT RIB 138.33 TO 35' AFT OF FRONT SPARSDR AALA202309135519Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 120.30, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202309064669Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 16 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR CALA2023083002670Skin · crackedAFTER C-SCAN INSPECTION PER EA 5510-01846 REV-H, OPP 001 ON L/H HORIZONTAL STABILIZER LOWER SKIN, FOUND CRACK AT APPROX STA 147.90 (REF. AAR NR 99980178). ON INTERNAL 9000 FLIGHT CYCLES IAW B737-800 SRM 55-10-01-2R-1 TA BLE 204.(WORK ACCOMPLISHED BY V938215 ANSDR CALA2023082502626Skin · crackedCRACK FOUND AT LT LOWER SKIN HORIZONTAL STAB STA 175.50 ON I/B ROW 17.5IN FROM FRUNT SPAR CRACK LENGTH APPROX 1.218IN REF AAR N/R 9206467 AND INSTALLED REPAIR DOUBLER AND FILLERS AS PER B737 SRM 55-10-0 WORK ACCOMPLISHED BY V930393 1-2R-11 REPAIR 11 REPAIR 11 SDR CALA2023082102602Skin · crackedCRACK FOUND AT LT LOWER SKIN HORIZONTAL STAB STA 175.50 ON I/B ROW 17.5IN FROM FRUNT SPAR CRACK LENGTH APPROX 1.218IN REF AAR N/R 9206467 AND INSTALLED REPAIR DOUBLER AND FILLERS AS PER B737 SRM 55-10-0 WORK ACCOMPLISHED BY V930393 1-2R-11 REPAIR 11 REPAIR 11 SDR ASAA2023081745098Rib · crackedR/H HORIZONTAL STAB RIB CRACKED ON FORWARD STIFFENER OF RIB 92.70. GROUNDED - YES. REPAIRED R/H HORIZONTAL STAB RIB IAW B737-700 SRM 55-10-09-2R-4.SDR ASAA2023081744841Skin · crackedL/H HORIZONTAL STABILIZER LOWER SKIN HAS A CRACK INDICATION 1/2" IN LENGTH AT STAB. STATION 101.90. LOCATED 19.50" FROM FRONT SPAR. AS MARKED. GROUNDED - YES. REPAIRED L/H HORIZONTAL STABILIZER LOWER SKIN CRACK BY INSTALLING DOUBLER IAW B737-NG SRM 55-10-01-2RSDR ASAA2023081744840Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN HAS A 2.5" CRACK INDICATION AT THE REAR SPAR LOCATED AT STAB. STA. 95". AS MARKED. GROUNDED - YES. REPAIRED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR STABILIZER STATION 95". IAW B737-800 SRM 55-10-01 REPAIR 1SDR ASAA2023081545097Skin · crackedR/H HORIZONTAL LOWER SKIN CRACKED APROX STA 94 AND REAR SPAR. GROUNDED - YES. REPAIRED SKIN IAW B737-700 SRM 55-10-01-2R-11, THIS IS A CAT B REPAIR WITH AN INSPECTIN THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES, AND REPEAT INSPECTION. METHODS D.V.I AT 9000 FLIGHT CSDR SWAA2023091989278Access Panel · crackedCRACK BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2023-506808<[01] REPLACED BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02;[02] REPLACED BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02SDR SWAA2023091988651Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17' APPROX. FROM L/E; I/B ROW (CRACK LENGTH 1') CRACK FOUND ON RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB 17' APPROX. FROM L/E I/B ROW (CRACK LENGTH 1')<[0SDR I5EA2023081100018Unknown · unknownLH HORIZONTAL LEADING EDGE 9149L HAS DENT I/B OF PREVIOUS REPAIR. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED DOUBLER AND TRIPLER IAW B737-300 SRM 51-40-02 AND B737-300 SRM 53-00-01 REPAIR 35.SDR DALA2025042203165Protector · erodedRT HORIZONTAL STABILIZER TIP EROSION PROTECTOR MATERIAL MISSING. REPETITIVE INSPECTION REQUIRED EVERY 150 FH. REPAIR REQUIRED WITHIN 8500 FH. REFER TO A220 ASRP 55-12-86-01AAA-662A-A. PAIN REPAIR REQUIRED PRIOR TO EROSION TAPE APPLICATION. REFER TO IRREG LOG 4SDR SWAA2023082487755Skin · crackedSTABILIZERS - LH HORIZONTAL STABILIZER LOWER SKIN - .4' CRACK FOUND TO BE AT RIB STA 184.70 AND 26' FROM FWD EDGE.<[01] UPDATED STEP 2-3;[02] UPDATED STEP 4. REPAIRED PER EA 23-155-02502 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 23-155-02502.SDR SWAA2023082487756Skin · crackedSTABILIZERS - LH HORIZONTAL STABILIZER LOWER SKIN - .4' CRACK FOUND TO BE AT RIB STA 193.90 AND 10' FROM FWD EDGE.<[01] UPDATED STEPS 3-4;[02] UPDATED STEPS 5-6;[03] UPDATED STEP 9.;[04] UPDATED STEP 9.;[05] VERIFIED STEP 9 COMPLETE.;[06] VERIFIED STEP 9 COMPLSDR AALA202308110271Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 16 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR CALA2023081102473Skin · crackedA REPAIR DOUBLER WAS INSTALLED ON L/H HORIZONTAL STAB LOWER SKIN DUE TO A CRACK IN THE LOWER SKIN STAB STA 129.5 APPROX 10" FORM REAR SPAR. SEE BAM N/R 1452729 FOR ALL WORK ACCOMPLISHED. A SIG IFICANT FINGIGS REPORT IS REQUIRED TO BE ISSUED FOE A MAJOR REPAIR.SDR AALA202308115067Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 16 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202308084972Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.0, 8 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR SWAA2023081683170Panel · delaminatedRIGHT HORIZONTAL STAB. T/E PANEL 343DB HAS EVIDENCE DELAMINATE IN CORNET O/B.<[01] REPAIRED DAMAGE CORNER WITH A PERMANENT REPAIR ON PANEL 343DB AS PER B737 SRM 51-70-04-2R-6. MATERIALS USED PO#1775890; PO#2012656; PO#1690463 AND PO#1160897;[02] SUMMARY :ACCOMSDR CALA2023072802342Skin · unknownREPAIR DOUBLER WAS INSTLLED ON R/H HORIZONTAL STAB LOWER SKIN AT RIB STA 129.50. SEE BAM N/R 001452899 FOR ALL WORK ACCOMPLISHED FOR ISTALLION OF REPAIR DOUBLER. PER SRM 55-10-01-2R-11 REPAIR 11 STEP 5 TABLE 204 A DIP IS REQUIRED TO BE ISSUED FOR INSPECTIO N OSDR CALA2023072802341Skin · unknownREPAIR DOUBLER WAS INSTLLED ON R/H HORIZONTAL STAB LOWER SKIN AT RIB STA 92.70 . SEE BAM N/R 001499712 FOR ALL WORK ACCOMPLISHED FOR INSTALLION OF REPAIR DOUBLER. PER SRM 55-10-01-2R-11 REPAIR 11 STEP 5 TABLE 204 A DIP IS REQUIRED TO BE ISSUED FOR INSPECTIO N SDR SWAA2023082481403Skin · crackedCRACK INDICATION ON EXTERNAL SKIN LOWER PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. AT RT HORIZONTAL STABILIZER 2023-461062<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500XSDR SWAA2023082380951Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH : 1' CRACK FOUND ON RT HORIONTAL STABILIER LOWER SKIN AT STAB STA 193.90 16.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 1'<[01] REPAIRED RT HORIZSDR DALA2023072405951Unknown · unknown(LOG 2877383) WHILE ON THE LINE IN LAX, MAINTENANCE OBSERVED THAT THE #3 TIRE TREAD CAP WAS LOST. UPON FURTHER INSPECTION MAINTENANCE DISCOVERED DAMAGE TO THE LOWER INSPAR SKIN OF THE RH HORIZONTAL STABILIZER. REPAIRED DAMAGE PER ERA 609877-14AD.SDR DALA2023072405947Unknown · unknown(LOG 2874736) DAMAGE TO RT LWR STAB SURFACE. C/W ERA 609877-14 REV.ASDR DALA2023072405942Unknown · unknown(LOG 2874325) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR OB BALANCE BAY PANEL. REPAIRED AREA OF CORROSION PER ERA 609520-14 REV ORIGINAL.SDR DALA2023072405940Unknown · unknown(LOG 2874287) LH HORIZONTAL STABILIZER OB TE WEDGE UPPER ATTACH ANGLE HAS AREA OF CORROSION 28 FROM OB STABILIZER TIP. REPAIRED CORRODED AREA PER ERA 609520-14 REV ORIGINAL.SDR AALA202307213790Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN PANEL CRACKED AT STABILIZER STATION 92.70 AND 14 INCHES AFT OF THE FRONT SPAR. REPAIRED SKIN PANEL PER SRM 55-10-01-2R 11.SDR SWAA2023081780052Doubler · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .8' CRACK 18' FROM FWD EDGE ON RIB 193.90<[01] VERIFIED APPLICABILITY OF SRM 55-10-01-2R-11 REPAIR 11.;[02] REMOVED THE DAMAGE AREA OF THE SKIN IAW SRM 55-10-01-2R-11 4. (2) FIG 204/REPAIR 11 DETAIL B AND SRM 51-10-02.<BR>
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