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 CALA2021091501569Skin · crackedCRACK INDICATION, LH HORIZONTAL STAB, LWR SKIN, STAB STA 166, AP PROXIMATELY 15.5 FWD OF AFT SPAR HFEC VERIFIED, APPROXIMATELY 1. 125" LENGHT, ENDS MARKED. REF BY PEMCO NR.11252.0160.SDR DALA2021091405485Skin · dentedSHIP 6815 DENT ON LH HOR. STAB. SKIN (LWR SIDE) AT STAB STA. 170 AND 4" FWD FROM FRONT SPAR. CORRECTIVE ACTION: SUMMARY OF NRC 00115: LH HOR.STAB. SKIN (LWR SIDE) AT STAB. STA. 170 AND 4" FWD FROM FRONT SPAR WAS REPAIRED PER ETI-57-21-477 REV.1 AND ER/A NO.593SDR AALA202109155237Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER SKIN LOCATED AT STA 138.70 AND RBL 99. REPAIRED PER SRM 55-10-01-2R.SDR AALA202109135724Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN SKIN OF RH HORIZONTAL STABILIZER AT STA 101.90, 37 IN AFT OF FRONT SPAR, MEASURING L=2.0 IN, W=0.003 IN, D=0.063 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R.SDR 2021F00205Skin · dentedDENT ON RH HORIZONTAL STABILIZER LEADING EDGE. DURING TRANSIT CHECK, IT WAS DETECTED A DENT ON RH HORIZONTAL STABILIZER. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT ON RH HORIZONTAL STABILIZER LEADING EDGE LOCATED BETWEEN LE STA 74.93 AND LE SSDR 2021FA0000257Skin · corrodedHORIZONTAL STABILIZER LOWER SKIN DAMAGE(CORROSION).SDR MASA20210908399Skin · dentedDENT ON LOWER SURFACE OF L/H HORIZONTAL INTERSPAR SKIN. CUT AWAY DENT AND INSTALL FABRICATED DOUBLER.SDR DALA2021091005350Panel · damagedSHIP 3353 FOUND THE LH AND RH HORIZONTAL STABILIZER LOWER PANELS WITH LARGE AREAS OF PRIMER MISSING AND PEELING WITHIN THE TRIM TANK. PERIODIC INSPECTIONS TO REPLACE AND INSPECT FUEL FILTER REQ. CORRECTIVE ACTION: ERA 593544-14 TO BE ACCOMPLISHED. (1935637)SDR ASAA2021090235950Skin · crackedDEFECT INDICATION FOUND R/H H-STAB. LOWER SKIN BETWEEN STA . 92.5 AND 101.9 INDICATION IS APROX. 1.00". GROUNDED - YES. REMOVED FINISH, PERFORMED HFEC, FOUND DEFECT, REMOVED PREVIOUS REPAIR DOUBLER & FILLER, REMOVED NEW DEFECT, FAB'D NEW FILLER & DOUBLER, LOCASDR UIEA2021090301954Rib · crackedEMP - RH H/STAB TIP FAIRING #3, #4 RIB FOUND CRACK(<P><SPAN>EMP - RH RH H/STAB TIP FAIRING #3, #4 RIB CRACKED AREA REPAIRED AS PER SRM 55-10-09-R2-12</SPAN></P>)SDR DALA2021083105148Skin · scratchedSHIP 3353 SEVERAL LIGHT SCRATCHES FOUND AFT SIDE ON LOWER PART OF CENTER TRIM TANK OPENING FOR PANEL 319AL. CORRECTIVE ACTION: REPAIRED PER A330 SRM 55-11-18. (1931501)SDR DALA2021083105147Skin · scratchedSHIP 3353 SEVERAL LIGHT SCRATCHES FOUND AFT SIDE ON LOWER PART OF CENTER TRIM TANK OPENING FOR PANEL 319BL. CORRECTIVE ACTION: REPAIRED PER A330 SRM 55-11-18. (1931499)SDR CALA2021083001447Skin · crackedSUPPORT TASK EA 5510-01843 REV H, RH HORIZONTAL STABILIZER STAB STA 120.3 LOWER SKIN FOUND CRACK WITH APPROXIMATELY 0.5" IN LENG TH TRANSFER REF NR LP 9130304, FROM THE REAR SPAR AND WAS REPAIRED PER SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CATEGORY B REPAIR WSDR A6WA202110297942None · noneELONGATED HOLE COMMON TO H/STAB LHS LOWER DOUBLER (DWG 600-23044) AND RIB (DWG 601R23030) AT PCU ACCESS DOOR. HOLE DIMENSIONS AT DOUBLER ARE (P2) = .370" X .250. HOLE DIMENSIONS AT RIB ARE (P1) = .370" X .370. ***AIRCRAFT REMOVED FROM SERVICE*** REAMED HOLSDR CALA2021082701444Skin · crackedSUPPORT TASK. C-SCAN, CRACK INDICATION, RH LWR HORIZONTAL STABIL IZER SKIN, STAB STA 120.3. APPROX. 24" FWD OF REAR STAR. REF TO PEMCO NR 11101.0162. CRACK LOCATED AT RH H-STAB LWR SKIN STA 123.85 APPROX. 4FT FROM LE. ORIG SKIN THICKNESS = .071" CUTOUT DIMENSISDR SWAA2021100510823Seal Plate · crackedCRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB ; 2021-392932 / [01] REPLACED SEAL PLATE ON ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W B737-700 SRM 51-10-02 AND 51-40-02; [02] CERTIFIED WORK PERFORMED.SDR IPXA2021082433039Skin · delaminatedINSPECTION TYPE:SEG4HORIZONTAL STAB. R/H UPPER SURFACE NEXT TO LEADING EDGE HAS A DENT/ DELAMINATED. DOT 61-002REPAIRED PANEL IAW B757 SRM 51-70-10-2R PER SRM 55-10-01-1A-1 FIG. 101 NOTE 1.SDR SWAA2021091409640Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SURFACE SKIN HAS A CRACK AT STA 184.70 ;4.00' FROM TRAILING EDGE. CRACK LENGTH ;1.181' ( AREA MARKED). ; / [04] REMOVED PANEL 331BZ FOR ACCESS AT L/H HORIZT STAB FRONT SPAR REF B737-700 SRM 51-40-02-0G-0; 2 PER EA NO:21-155-024SDR AALA202108209648Skin · crackedAIRCRAFT WAS GROUNDED: RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9 10.5 X 19.5. REPAIRED SKIN WITH FILLER AND DOUBLER PER SRM 55-10-01-2R.SDR AALA202108200865Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF RH HORIZONTAL STABILIZER AT STA 101.9, 37 IN AFT OF FWD SPAR, MEASURING L=1.125 IN, W=0.002 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R.SDR AALA202108204377Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF RH HORIZONTAL STABILIZER AT STA 129.50, 18 IN AFT OF FRONT SPAR, MEASURING L=1.125 IN, W=0.002 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R-11.SDR AALA202108208865Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF RH HORIZONTAL STABILIZER AT STA 175.5, 27 IN AFT OF FRONT SPAR, MEASURING L=0.75 IN, W=0.002 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R.SDR AALA202108201976Skin · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.90 APPROXIMATELY 32 INCHES AFT OF FORWARD SPAR. DAMAGED REMOVED, FILLER FABRICATED AND EXTERNAL DOUBLER INSTALLED PER SRM 55-10-01-2R-11.SDR SWAA2021091407399Skin · crackedLT HORZ STAB LOWER SKIN CRACKED RIB STA 194 APPROX. 9.5 INCHES FROM FRONT SPAR ; / [01] CUT OUT DAMAGE IAW SRM 55-10-01-2R-11.; [02] VERIFIED DAMAGE CUTOUT PER NDT PART 6 51-00-00 PROCEDURE 23 AND SRM 55-10-00-2R-11.; [03] FABRICATED REPAIR DOUBLER IAW SRM 55-SDR SWAA2021091407400Skin · crackedRT HORZ. LOWER SKIN HAS CRACK AT RIB STA 194 APPROX 16.5 INCHES FROM FRONT SPAR APPROX .75 LONG ; / [01] CUT AND REMOVED DAMAGE I.A.W SRM 55-10-01-2R-11.; [02] VERIFIED DAMAGE CUTOUT CORRECTIVE ACTION 1 PER NDT PART 6 51-00-00 PROCEDURE 23 AND SRM 55-10-00-2R-SDR DALA2021081704768Skin · nicked(LOG 1911864) DURING INSPECTION FOUND NICK ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 133. PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 133 WAS PERFORMED PER B737-800 SRM 55-10-01-2R-1.SDR DALA2021081704767Skin · nicked(LOG 1911757) DURING INSPECTION FOUND NICK ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 105. PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 105 WAS PERFORMED PER B737-800 SRM 55-10-01-2R-1.SDR SWIA202162619None · corrodedHORIZONTAL STAB. BATHTUB FITTINGS (16 TOTAL JOLL BOLTS CORRODED) (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED JO-BOLTS IN BATHTUB FITTINGS IAW CRJ 200 SRM 51-42-22SDR CALA2021081301325Skin · crackedSUPPORT TASK RH HORI STAB LOWER SKIN WAS FOUND CRACKED ON STAB STA 120.3 9.5" FROM REAR SPAR APPROX 0.375" IN LENGTH.TRANSFER NON- ROUTINE L/P:9130398 AND ORIGINATED BY V897823 THIS IS A CATEGORY B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS GIVEN IN PARAGRAPSDR ASAA2021081135801Skin · crackedL/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 175.08 INCHES FWD OF T/E. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES, AND SDR ASAA2021081135800Skin · crackedL/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 147.0 31 INCHES FWD OF T/E. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES ANDSDR ASAA2021081135799Skin · crackedL/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 138.0 9 INCHES FWD OF T/E. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THERESHOLD OF 56,0000 TOTAL FLIGHT CYCLES ANSDR 2021FA0000231Skin · corrodedHORIZONTAL STAB LH LOWER SKIN HAS MULTIPLE AREAS OF CORROSION ON THE TRAILING EDGE OF SKIN. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ30952M1 DATED AUGUST 9TH 2021.SDR DALA2021081204629Skin · dentedSHIP 193 2 EA DENTS ON UPPER SURFACE OF R/H HORIZONTAL STA. 25" AFT OF FRONT SPAR, 4" I/B OF RIB STA 157.27 AND 31" AFT OF FRONT SPAR, 2" I/B OF RIB STA 157.27. C/W ERA 592734-14. (LP 1904406)SDR CALA2021080901296Skin · crackedCRACK ON LOWER INSPAR SKIN ON RIGHT HORIZONTAL STAB STA.175.5 " 16" FROM FORWARD SPAR AND MEASURING .75" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780724 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FIG SDR CALA2021080901295Skin · crackedCRACK ON LOWER INSPAR SKIN ON RIGHT HORIZONTAL STAB STA.147.9 " 27.5" FROM FORWARD SPAR AND MEASURING 1.5" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780721 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FISDR CALA2021080901294Skin · crackedCRACK ON LOWER INSPAR SKIN ON LEFT HORIZONTAL STAB STA.193.5 " , 27" FROM FORWARD SPAR AND MEASURING 1.25" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780720 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FISDR CALA2021080901293Skin · crackedCRACK ON LOWER INSPAR SKIN ON LEFT HORIZONTAL STAB STA.129.50 " 27.5" FROM FORWARD SPAR AND MEASURING 1.0" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780718 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FISDR AALA202108208819Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF RH HORIZONTAL STABILIZER AT STA 138.7, 10 IN FWD OF REAR SPAR, MEASURING L=0.9 IN, W=0.002 IN, D=0.06 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R-11.SDR AALA202108207805Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF LH HORIZONTAL STABILIZER AT STA 138.7, 18 IN FWD OF REAR SPAR, MEASURING L=0.9 IN, W=0.002 IN, D=0.08 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R-11.SDR AALA202108207142Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LOWER SKIN OF LH HORIZONTAL STABILIZER AT STA 138.7, 10 IN FWD OF REAR SPAR, MEASURING L=0.9 IN, W=0.002 IN, D=0.08 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-2R-11.SDR AALA202108101716Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN SKIN OF LOWER RH STABILIZER AT RH STAB STA 101 AND 11 IN FWD OF REAR SPAR, MEASURING L=0.75 IN, D=0.08 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 55-10-01-R2-8.SDR AALA202108176155Skin · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER SKIN LOWER SURFACE HAS A CRACK AT STA 138.7, RIGHT BUTT LINE 101. INSTALLED DOUBLER REPAIR PER SRM 55-10-01-2R.SDR DALA2021080204342Skin · damagedSHIP 652 IN REF. TO NRC 00227: NICKS OUT LIMITS ON HORIZONTAL STAB. SEGMENT 342CR BTW STA 141 TO 143, STA 151 TO 153, STA 174 TO 176, STA 184 TO 186, STA 207 TO 209 (2EA),STA 213 TO 214 AND STA 220 TO 222. CORRECTIVE ACTION: SUMMARY OF NRC 01105: NICKS ON HORISDR SWAA2021090798693Access Panel · crackedCRACK ACCESS PANEL 331B LEADING EDGE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER ; 2021-341100 / [01] REMOVED LEADING EDGE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA SDR DALA2021080304392Skin · dentedSHIP 652 STAB LT LWR;L/H HORZ STAB LWR SKIN HAS DENT APPROX 50'' FROM I/B. CORRECTIVE ACTION: SUMMARY OF NRC 01182: STAB LT LWR;L/H HORZ STAB LWR SKIN HAS DENT APPROX 50'' FROM I/B WAS REPAIRED PER B757-200 SRM. (1890524)SDR DALA2021073004323Skin · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION: HORIZONTAL STAB. CENTER SECTION UPPER SKIN UPPER SURFACE RIGHT SIDE 30" FROM CENTER 12" AFT OF FWD EDGE. REPAIRED PER ERA 592478-14 REF LP 1889089. (LP 1890093)SDR SWAA2021091498259Skin · crackedCRACK INDICATION ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90; INBOARD SIDE OF RIB ; 16.750 INCH FROM FRONT SPAR. CRACK LENGTH IS 0.500 INCH. ; 2021-341980 / [01] REPAIRED EXTERNAL LOWER IN-SPAR SKIN AT STATION 193.30 INBOARD SIDE OF RIB 16SDR DALA2021072904292Skin · nickedSHIP 652 IN REF. TO NRC 00227: NICKS OUT LIMITS ON HORIZONTAL STAB. SEGMMENT 342BR BTW STA 101 TO 103, STA 107 TO 108, STA 113 TO 115 AND STA 125 TO 127. CORRECTIVE ACTION: SUMMARY OF NRC 01104: NICKS ON HORIZONTAL STAB SEGMMENT 342BR BTW STA 101 TO 103, STA 1SDR CALA2021072801200Skin · crackedRH HORIZONTAL STAB LWR SKIN PANEL, STAB STA 164, 11.75" FM AFT EDGE; ECA C-SCAN CRACK INDICATION VERIFIED BY MFEC PER B737 NTM PT 6, 53-30-18. REFER TO PEMCO NR 11015.0228. ACCOMPLISHED HORZ STAB LOWER INNER SKIN EXTERNAL REPAIR AT APPROX STA 164, 11.75" FROM
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