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 CALA2021032600370Skin · cracked2 CRACKS FOUND IN LT. HORIZONTAL STAB LOWER SKIN AT RIB STA 147. 90 AND 25"AND 32.5" FROM FWD SPAR(BOTH ITEMS CIRCLED AND CRACK M ARKED,VERIFIED WITH HFEC 737NDT PART 6 51-00-00-23) REPAIRED LT. LOWER HORIZONTAL SKIN STA 147.90 REF SRM 55-10-01 R EPAIR 11.SEE SDR DALA2021032301723Skin · dented(LOG 7559457) DURING INSPECTION FOUND FOA DAMAGE RT HORIZONTAL LE 2 DENTS IB, 40" & 7" FROM FUSELAGE. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED RIGHT HORIZONTAL STAB LEADING EDGE PER B737 AMM 27-41-21.SDR SWAA2021050358171Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STA 193.90 RIB INBOARD SIDE AND 24.750 INCHES FROM LEADING EDGE. CRACK LENGTH: 0.400 INCHES. /SDR SWAA2021050358170Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STA 193.90 RIB INBOARD SIDE AND AT 17 INCHES FROM LEADING EDGE. CRACK LENGTH: 0.700 INCHES. /SDR SWAA2021050358169Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STA 193.90 RIB INBOARD SIDE AND AT 24 INCHES FROM LEADING EDGE. CRACK LENGTH: 1.200 INCHES. /SDR SWAA2021050358168Skin · crackedCRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STA 193.90 RIB INBOARD SIDE; 16.250 INCHES FROM LEADING EDGE. CRACK LENGTH:1.100 INCHES. /SDR ASAA2021031934387Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT STA. 138.70 IN TWO PLACES. (ONE IS .625" LONG AND THE OTHER IS .250" LONG, BOTH ARE MARKED) GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED SKIN IAW B737-800 SRM 55-10-01-2R-11. THIS IS A CATEGORY B REPAIR WITH AN INSSDR SWAA2021032357119Skin · crackedCRACK FOUND IN LOWER SKIN OF L/H HORIZONTAL STABILIZER AT LEADING EDGE STATION 198.23. CRACK IS LOCATED 16.0' AFT OF FWD SPAR. CRACK IS 1.0' LONG. / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR CALA2021031900336Skin · crackedREF AMES NR 0460. THE FUSELAGE SKIN IS WORE THROUGH AND CRACKED AT THE FWD LWR EDGE OF THE CUTOUT FOR THE HOR STAB ON THE RIGHT SIDE REPAIRED FUSELAGE SKIN ON THE FWD LOWER EDGE OF CUTOUT FOR HORZ STAB IAW B767 SRM 53-60-01 REPAIR 3. SEE BACK AND PARTIAL WORKSSDR SWIA202157983Skin · bentRH H. STAB LOWER SKIN BENT AT I/B TRAILING EDGE (C-CHECK RO 5/3/2021) REPAIRED RH LOWER H. STAB TRAILING EDGE SKIN REF REO 690-55-11-140 REV -- DATED 2021-04-16. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY.SDR SWIA202158221Skin · dented*HORIZONTAL STABILIZER, LEFT LOWER SKIN HAS A DENT (MARKED IN RED GREASE PENCIL) (C-CHECK RO 5/20/2021) REPAIRED HORIZONTAL STABILIZER, LEFT LOWER SKIN IAW REO 670-55-11-361 REV -- DATE 2021-05-02 AND REF CRJ700 SRM 51-42-22-001-001-A01.COMPLIED WITH TASDR ASAA2021031134303Skin · crackedONE CRACK FOUND ON THE RIGHT HAND HORIZONTAL STAB LOWER SKIN BETWEEN STATION 92.70 AND 101.90 CRACK IS APPROX. 1.5" LONG. CRACK IS MARKED. GROUNDED - YES. CUT OUT CRACK AND REPAIRED R/H HORIZONTAL LOWER SKIN REF B737-800 SRM 55-10-01-2R-11 REPAIR 11. THIS IS ASDR ASAA2021031034482Skin · crackedR/H HORIZONTAL STAB. LOWER SKIN AT AFT SPAR, FWD OF FWD ROW FASTENERS @ STAB.STA. 101.90 + 4" MARKED 1.550"L CRACK FOUND. GROUNDED - YES. REPAIRED HORIZONTAL STAB. LOWER SKIN AND RIB FITTING IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11 AND ALASKA EA 800-55EA-2333SDR SWAA2021040556626Skin · crackedDURING HFEC INSP. FOUND CRACK IN LWR SKIN OF RH HORIZONTAL STAB STA 193.90 RIB. 18 IN. FWD OF REAR SPAR; APPROXIMATELY 2 IN. IN LENGTH. AREA MARKED / REPAIRED RH HORIZ. STAB LWR SKIN AT STAB STA 193.90 RIB; 18' FWD OF REAR SPAR IAW SRM 55-10-01-2R-11. REMOVABLSDR ASAA2021022734385Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED 1.250" AT STA. 175.50 (MARKED) GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 FLIGHT CYCLES AND 9,000 FLIGHTSDR ASAA2021022634386Skin · crackedLEFT LOWER HORIZONTAL STAB SKIN CRACKED .250" AT STA. 92.70 (MARKED) GROUNDED - YES. CUT OUT DAMAGE TO SKIN AND REPAIRED IAW B737-800 SRM 55-10-01-2R-11 REPAIOR 11 THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES AND 9,000SDR ASAA2021022434354Skin · crackedR/H HORIZONTAL LOWER SKIN IS CRACKED STA 138, 18 INCHES FWD OF REAR SPAR GROUNDED - YES. REPAIRED CRACK ON R/H HORIZ LOWER SKIN AT STA 138,18" FWD OF REAR SPAR IAW B737-700 SRM 55-10-01-2R-11 THIS IS A CAT B REPAIR WITH INSPECTION THRESHOLD OF 56,000 FLIGHT CSDR SWAA2021031751824Skin · crackedLEFT HORIZONTAL STABILIZER; LOWER SKIN CRACKED AT STAB STA- 194; 17 INCHES AFT OF FRONT SPAR; CRACK IS .75' IN LENGTH. MARKED. / REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 194 PER SRM 55-10-01-22-11. REMOVABLE COMPONENT: P/N:186A1000-41; S/N:ICSDR SWAA2021040152241Skin · crackedCRACK INDICATION ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB INBOARD SIDE 24 INCH FROM FWD EDGE . CRACK LENGTH = 1.500 INCH / PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 BETWEEN 12.5' AND 29' FROM SDR SWAA2021040152240Skin · crackedCRACK INDICATION ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB INBOARD SIDE ; 16.250 INCH FROM FWD EDGE . CRACK LENGTH = 1.100 INCH . / PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 BETWEEN 12.5' AND 2SDR MK1Y20210221033Skin · corrodedHORIZONTAL STABILIZER CENTER SECTION UPPER SKIN, BETWEEN STR 8/11 AND RBL 13/32; MAINTENANCE FOUND CORROSION ON PREVIOUSLY BLENDED SKIN AREA LOCATED BETWEEN STR 9-10 AND ON PREVIOUSLY INSTALLED DOUBLER LOCATED BETWEEN STR 10-11 PER BOEING SR 1-1906538101 AND 1SDR MK1Y20210221014Skin · debondedR/H HORIZONTAL STABILIZER PANEL, STAB STA 127.465 – AUX SPAR STA 157.277, 185T1001. THE INNER 7075-T6 ALUMINUM SKIN FOUND DISBONDED AND SEPARATED FROM THE ALUMINUM HONEYCOMB CORY PANEL 185T1001. IDENTIFICATION PER SRM 55-10-01 FIG. 1 (DETAIL I)SDR DU4R2021021800005Skin · gougedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RT HORIZONTAL STABILIZER, PANEL 92226R, STAINLESS ANGLE WAS GOUGED. S/O 6600004 N/R 44479.SDR DALA2021021700905Access Panel · leakingSHIP 3303 CORROSION ACCESS PANEL 344FB HINGE ON RT HORIZONTAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS LOC ON HINGE AS PER ER/A 589982-14.SDR ASAA2021021234195Skin · crackedRH HORIZONTAL LOWER SKIN CRACKED AT REAR SPAR AND STA 97. GROUNDED - YES. REMOVED EXISTING REPAIR, CUTOUT DAMAGED,FABRICATED,LOCATED,DRILLED & INSTALLED NEW REPAIR PARTS IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11 THIS IS A CAT B REPAIR WITH AN INTERVAL INSPECTISDR UIEA2021012700141Skin · corrodedH/STAB L/H T/E LOWER SKIN BL 415 FOUND COR.(<P>H/STAB L/H T/E LOWER SKIN BL 415 COR AREA REPAIRED AS PER RI-55-00-14312 REV A.</P>)SDR DALA2021021100811Access Panel · corrodedSHIP 3316 CORROSION ACCESS PANEL 334GB HINGE ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED ACCESS PANEL 334GB HINGE (HALF HINGE) ON LH HORIZONTAL STABILIZER ASPER A330 SRM. (1726912)SDR SWAA2021021047862Skin · dentedAFTER INSPECTION FOUND DENT ON THE R/H HRZ. STAB. L/E STA212.30. / EVALUATE DAMAGE AT HORIZ. STAB L/E STA NO. 212.30 FOUND OUT OF LIMITS; CUTOUT DAMAGED SECTION & INSTALLED DOUBLER & FILLER REPAIR ON EXTERNAL SKIN IAW B-737-700 SRM # 55-10-01-2R-1 MAT. USED 20SDR DALA2021021000789Panel · dented(LOG 7679008) DURING INSPECTION FOUND DENT IN RIGHT HORIZONTAL LEADING EDGE AT STA 90 8.5" WIDE 2.5" TALL AND .20 DEEP THROUGH RIB AREA. R/R RT HOR STAB L/E PANEL 341B PER B737 AMM 06-42 AND 55-10.SDR 2021F00019Panel · corrodedREPAIR TO HORIZONTAL TRAILING EDGE PANELS. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ28656M2 DATED FEB. 7, 2021.SDR ASAA2021020134121Doubler · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT THE REAR SPAR BETWEEN STA 92.7 AND 101.9. GROUNDED - YES. ON DEFERRAL.SDR SWAA2021021246887Access Panel · brokenBROKEN TRAILING EDGE BOLT ACCESS PANELS AT LT HORIZONTAL STABILIZER (265 EA) / REPLACED TRAILING EDGE BOLT ACCESS PANELS AT LT HORIZONTAL STABILIZER (265 E/A) IAW B737-700 SRM 51-40-02SDR SWAA2021021844905Screw · damagedDAMAGE SCREW ACCESS PANEL 343CB; 343DB; 333CB AND 333DB AT RT HORIZONTAL STABILIZER. REPLACED SCREWS ON ACCESS PANELS 343CB; 343DB; 333CB AND 333DB AT RIGHT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02.SDR ASMF202101023Skin · crackedDURING 8A-P CHECK AT MEX STATION, IT WAS DETECTED SEVERAL CRACKS AT BOTH HORIZONTAL STABILIZERS. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A CRACK OF 3.5" LENGTH AT STAB STA 101.90 AND 0.5" DISTANCE FROM REAR SPAR; A CRACK OF 1.00" LENGTH AT STAB SSDR DALA2021011900293Access Panel · damagedELONGATED HOLE ACCESS PANEL 326AT ON VERTICAL STABILIZER. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR, PER A320 SRM 55-44-00-300-012.SDR FDEA202101140093Skin · damagedRIGHT HORIZONTAL STABILIZER WING TIP FORWARD END PAINT AND COMPOSITE DETERIORATED. REPAIRED RIGHT HORIZONTAL STABILIZER WING TIP FORWARD END PAINT AND COMPOSITE DETERIORATED, IAW B757 SRM 55-10-2R, 51-70-05-OG, 51-70-14, B757 AMM 51-21-00-7. REMOVED THEN RSDR SWIA202155679Skin · damagedTRANSFER FROM EAML 560139: TRANSFERRED FROM CAMP 22138927. DAMAGE ON RT HORIZONTAL STABILIZER LOWER SKIN LOCATED FROM RIB 13 TO RIB 14 FROM THE MIDDLE SPAR TO THE REAR SPAR. FILED CLOSED. TRANSFER FROM EAML 560139: TRANSFERRED FROM CAMP 22138927. REPAIRED SDR JGVR20210113001Panel · corrodedBLENDED 1 AREA OF CORROSION ON TOP OF LT HORIZONTAL STAB JUST FORWARD OF WEDGE PANEL 351AC (INBOARD OF THE LT ELEVATOR) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED PER TEXTRON ENGINEERING MEMO.SDR MK1Y01132021006Skin · debondedTHE INNER ALUMINUM SKIN FOUND DISBONDED AND SEPARATED FROM THE ALUMINUM HONEYCOMB CORE PANEL AT STAB STA 107.927 AUX SPAR STA 127.465.SDR SWAA2021012641939Rib · crackedLT HORIZONTAL STAB INSPAR RIB AT STA 120.30 NR 2 VERTICAL STIFFENER IS CRACKED. REMOVED THE DAMAGE PART AT LT HORIZONTAL STAB INSPAR RIB AT STA 120; 30 NR 2 VERTICAL STIFFENER AND INSTALLED REPAIR PARTS, IAW SRM 55-10-09-2E-4 88920U 16JAN21.SDR SCNA20210126006Skin · damagedHORIZONTAL STABILIZER REMOVABLE TIP 345A AFT LOWER RIVET SEPARATED FROM SKIN. REPAIRED RIVET HOLE ON AFT LOWER SEPERATED SKIN ON HORIZONTAL STABILIZER REMOVABLE TIP 345A, IAW B737 SRM 55-10-30-2R-1 TABLE 201 AND IAW B737 SRM 51-70-04-2R-9.SDR SWAA2021021145211Rib · crackedCRACK LEADING EDGE RIB LE STA 92.70 AT LT HORIZONTAL STABILIZER (1 ) / REPLACED RIB LE STA 92.70 AT LT HORIZONTAL STABILIZER (1EA) AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 186A1303 REV - PN 186A1352-5SDR ASAA2021010333911Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB STA 101.90 BETWEEN 92.70 AND 101.90 APPROXIMATELY 12" FROM LEADING EDGE. GROUNDED-YES. REPAIRED LT HORIZONTAL STAB LOWER SKIN CRACKED AT STAB STA 101.90 BETWEEN 92.70 AND 1019.90, IAW 737-900 SRM 55-10SDR 6PMR2020122131223Skin · corrodedAREAS WITH CORROSION ON UPPER LEFT AFT SKIN SURFACE OF CENTER HORIZONTAL STABILIZER BOX, BETWEEN HYDRAULIC LINES CONNECTION AND LEFT ATTACH MOUNT PLATE AROUND FASTENERS AND ALONG EDGE. CORRECTIVE ACTION: ACCOMPLISHED EO 20495-3, REV IR. REMOVED CORROSION, ACSDR SWAA2020121636629Skin · dentedRT HORIZONTALS LEADING EDGE DENT AT STA 151 L=1.7; W=1.6; D=.090. DENT HAS CREASE AT RIB. REMOVED & REPLACED RT HORIZ LEADING EDGE, PER MM 27-41-21. POS RT P/N OFF 186A1001-16 S/N OFF WN7855 P/N ON 186A1001-24 SN ON 8513-RT AMT 12265 INSP 10886.SDR SWAA2020121636628Skin · dentedRT HORIZONTAL STAB LEADING EDGE DENT AT STA 210.5 L=2.5 W=1.9; D=.136 AT A RIB WITH A CREASE. R & R HORIZ STAB LEADING EDGE, PER MM 2741-21. POS RT P/N OFF 186A1001-16 S/N OFF WN7855 P/N ON 186A1001-24 S/N ON 8513-RT AMT 12265 INSP 10886.SDR SWAA2020121636627Skin · dentedRT HORIZONTAL LEADING EDGE DENT AT STA 105 L=1.8; W=1.3; D=.065. LESS THAN 1' FROM RIB. R & R HORIZ STAB LEADING EDGE, PER M/M 27-41-21. POS RT P/N OFF 168A1001-16 S/N OFF WN7855 PN ON 186A1001-24 SN ON 8513-RT AMT 12265 INSP 10886.SDR SWAA2020121636626Skin · dentedRT HORIZONTAL STAB LEADING EDGE DENT AT STA 100 L=1.8 W 1.35; D=.023. R & R RT HORIZ STAB LEADING EDGE, PER MM 27-41-21. POS RT P/N OFF 186A1001-16 S/N ON WN7855 PN ON 186A1001--24 SN ON 8513-RT AMT 12265 INSP 10886.SDR SWAA2020121636625Skin · dentedRT HORIZONTAL LEADING EDGE DENT AT STA 160 L=4.0; W=2.5; D=.225. DENT IS CREASED ON A RIB WITH A PULLED FASTENER. R & R RT HORIZ STAB LEADING EDGE, PER MM 27-41-21. POS RT P/N OFF 186A1001-16 S/N OFF WN7855 P/N ON 186A1001-24 S/N ON 8513-RHAMT 12265INSP 108SDR SWAA2020121636624Skin · dentedRT HORIZONTAL STAB LEADING EDGE DENT AT STA 89 L=2.6 W=1.8 D=.082. R & R RT HORIZ STAB LEADING EDGE, PER MM 27.41.21. POS RT P/N OFF 186A1001-16 S/N OFF WN7855 P/N ON 186A1001-24 S/N ON 8513-RHAMT 12265INSP 10886.
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