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 NACA2019123040150Access Panel · corrodedRIGHT HORIZONTAL STABILIZER LOWER SURFACE ACCESS PANEL 9222R AT HSS 56.01 WAS CORRODED UNDER AND AROUND ANCHOR NUTS. REPLACED THE ACCESS PANEL IAW SRM 51-30-01, REV 104. AND DWG 6553746, REV H.SDR CALA2020010600011Skin · crackedRIGHT HORIZONTAL STAB LOWER INSPAR SKIN HAS A CRACK @ STA 147.9 RIB 24 INCHES AFT OF THE FRONT SPAR. CRACK IS APPROX. 1 INCH LONG. SEE FLEETCYCLE LP 9713933 FOR REPAIR STEPS ACCOMPLISHED. REPAIRED RT HORIZONTAL STAB LWR INSPAR SKIN AT STA 147.9 AND 24 INCHES ASDR ABXR2019122100326Skin · corrodedLEFT HORIZ STAB UPPER O/B SKIN CORRODED AT HSBL 314.214SDR CALA2019122102263Skin · crackedRIGHT HORIZONTAL STAB INSPAR LOWER SKIN CRACKED AT STA 175.5 AND 10"FWD OF REAR SPAR. REPAIRED LOWER HORZONTAL SKIN AS REF SRM 55-10-01 REPAIR 11,SDR CALA2019120312261Skin · crackedLEFT HORIZONTAL STAB INSPAR SKIN CRACKED AT STA.92.70 AND 11" FWD OF REAR SPAR CRACK MEASURES HALF INCH. REPAIRED LEFT HORIZONTAL LOWER SKIN AS REF SRM 55-10-01 REPAIR 11, INSPECTION THRESHOLD 56000 FLT CYCLES AND REPEAT INSPECTION EVERY 9000 FLT CYCLES THERE SDR CALA2019121902247Skin · crackedRIGHT HORIZONTAL STAB INSPAR SKIN CRACKED AT STA 101.9 AND 10" FWD OF REAR SPAR. AND 10" FWD OF REAR SPAR REF SRM 55-10-01 REPAIR 11. SEE FLEET CYCLE L/P 9716665 FOR WORK ACCOMPLISHED, INSPECTION THRESHOLD AT 56000 TOTAL FLIGHT CYCLES AND REPEAT INSPECTION EVESDR CALA2019121902244Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN HAS 0.813" CRACK 18.5" FWD OF AFT EDGE OF SKIN PANEL RIB 120.30. REMOVED EXISTING REPAIR AND INSTALLED LARGER REPAIR TO INCORPORATE 2 EACH NEW DAMAGES AS PER B737 SRM 55-10-01 REPAIR 11 FIG 204. ASDR SWAA2019121839794Skin · crackedR/H STABILIZER LOWER INSPAR SKIN CRACKED 1.3" LONG AT STAB. STA. 198.23, 17.0" AFT OF FORWARD SPAR ADJACENT TO RIB. / REPAIRED SKIN PER SRM.SDR CALA2019120902169Skin · crackedSUPPORT TASK - 0.500" LONG CRACK FOUND AT R/H HORIZ STAB LWR SKIN PANEL AT STAB STA129.50 18" FWD OF T/E 0.250" I/B OF I/B ROWS OF FASTENERS REMOVED FRONT SPAR WEB/REMOVED EXISTING REPAIR DOUBLER / REMOVED DAMAGE / FRABRICATED NEW REPAIR DOUBLER AND FILLER ANSDR DALA2019120987171Skin · dented(LOG 6255634) DURING INSPECTION FOUND DENT ON LEFT HORIZONTAL STAB LEADING EDGE. REPAIRED DAMAGE PER ERA 583731-14.SDR AALA201912099053Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND HORIZONTAL STABILIZER LOWER SKIN AT STATION 101.90. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR FDEA2019120653192Skin Panel · delaminatedRT HORIZONTAL STAB UPPER SKIN APROX, HSBR 148.5 OB END 2 EACH OIL CAN DELAMINATED AREA APROX 17" BETWEEN 22". REMOVED & REPLACED RT HORIZ STAB UPPER SKIN PANEL ASSY BETWEEN AUX SPAR & FRONT SPAR INBOARD IAW SRM 51-40-02-0G & DWG 185N7001 REV C AND 185N5002 RESDR SWAA2020010740233Skin · canningL/H HORIZONTAL STABILIZER LOWER SKIN HAD LARGE AREA OF OIL CANNING OUTBOARD OF AFT OUTBOARD DOUBLER OF SKIN REPLACEMENT REPAIR. / REPAIRED SKIN PER EA.SDR DALA2019120507092Skin · cracked(LOG 1387396) DURING INSPECTION FOUND CRACK IN LOWER SKIN OF HORIZONTAL STABILIZER RIGHT IN POSITION RIB STAB STA = 129.50. HORIZONTAL STABILIZER RIGHT IN POSITION RIB STAB STA = 129.50 WAS REPAIRED PER B737-800 SRM 55-10-01 REP.11.SDR DALA2019120507094Skin · cracked(LOG 1387402) DURING INSPECTION FOUND CRACK IN LOWER SKIN OF HORIZONTAL STABILIZER RIGHT IN POSITION RIB STAB STA = 129.50. CRACK IN LOWER SKIN OF HORIZONTAL STABILIZER RIGHT IN POSITION RIB STAB STA = 129.50 WAS REPAIRED PER B737-800 SRM 55-10-01 REP.11.SDR CALA2019120762152Skin · crackedC-SCAN ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB. FOUND ONE CRACK INDICATION AT STAB STA 147.90 ABOUT 16" FROM THE AFT SPAR. (REF. F/C N/R 9713359). INITIATE DIP FOR INSPECTION REQUIREMENTS PER SRM 55-10-01 REPAIR 11 PAR. 5 TABLE 204. INITIATE DIP FOR INSPECTSDR SWAA2019120439323Skin · crackedR/H HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG STAB. STATION 193.90, 24" AFT OF LEADING EDGE SPAR. / REPAIRED SKIN PER SRM.SDR DALA2019120296993Skin · cracked(LOG 1379238) DURING INSPECTION FOUND CRACK ON LOWER SKIN APPROX AT STAB STA 138 RH HORIZONTAL STAB. HORIZONTAL STAB WAS REPAIRED PER B737-800 SRM 55-10-01 REPAIR 11.SDR FDEA2019122063268Skin · corrodedL/E SKIN CORRODED ON R/H HORIZONTAL L/E SECTION 341BT...(MRK) 5121818: CONSIGNADO, FREDERICK J - 17-DEC-2019 22:02 REMOVED DAMAGED ON L/E, R/H HORIZ @ APPROX XFS 97. INSTALLED REPAIR PER SRM 55-10-02-2R REPAIR 1 FIG 201 SEE ATTACHMENTS NR 1274 AMT# RRB 828SDR AALA201911289012Skin · crackedAIRCRAFT IN BASE VISIT: 0.900" CRACK IN L/H HORIZONTAL STABILIZER LOWER SURFACE IN-SPAR SKIN. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER WITH FILLER. INSTALLED REPAIR IAW SRM 55-10-01-2R-11.SDR AALA201911289011Skin · crackedAIRCRAFT IN BASE VISIT: 0.900" CRACK IN L/H HORIZONTAL STABILIZER LOWER SURFACE IN-SPAR SKIN. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER WITH FILLER. INSTALLED REPAIR IAW SRM 55-10-01-2R-11.SDR CALA2019112862077Skin · crackedVERTICAL STIFFENER #2 (CRACK ON LOWER RADIUS) ON R/H HORIZONTAL STAB AT STA 129.5 REQUIRES ACCESS FOR RIB REPAIR. SEE FLEETCYCLE N/R 9708910 INSTALLED REPAIR DOUBLER REF BOEING 737-700 SRM 55-10-01 REPAIR 11. SEE FLEETCYCLE N/R 9708910. INITIATED DIP TO PERFORSDR CALA2019112862074Skin · crackedEA 5510-01843 REV.H OP.01 R/H HORIZONTAL STAB LOWER SKIN AREA AT STA. 157.10 CRACK INDICATION NOTED,9" INCHES FROM AFT SPAR. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT EXTERNAL DOUBLER AT 56,000 TOTAL COMSDR CALA2019112862073Skin · crackedEA 5510-01843 REV.H OP.01 R/H HORIZONTAL STAB LOWER SKIN AREA AT STA. 147.90 CRACK INDICATION NOTED, 17" INCHES FROM AFT SPAR. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT EXTERNAL DOUBLER AT 56,000 TOTAL COMPOSDR CALA2019112862072Skin · crackedEA 5510-01843 REV.H OP.01 R/H HORIZONTAL STAB LOWER SKIN AREA AT STA.101.90 CRACK INDICATION NOTED,20" INCHES FROM AFT SPAR. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER IAW SRM 5510-10- 01 REPAIR 11. DIP INITIATED TO INSPECT EXTERNAL DOUBLER AT 56000 TOTAL CSDR CALA2019120322103Skin · crackedN/R 6724821: EA 5510-01843 REV H R/H HORIZONTAL STAB LWR SURFACE STA 184.7 APPROX 25.5" AFT OF SKIN L.E. HAS .5" CRACK REVEALED DURING C-SCAN. REPAIRED DAMAGE ON RH HORIZ STAB LWR SURFACE AT STA 184.7 REF SR M 55-10-01 REPAIR 11. (44.0009 ATTACHED).SDR C77A2020020530045Skin · dentedDURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED A DENT ON THE LH HORIZONTAL STABILIZER UPPER SKIN PANEL BETWEEN RIB 12 & 13 AND THE REAR SPAR AND TRAILING EDGE. REFER ETD2019-170-154098 FOR THE DENT LOCATION AND MEASUREMENTS. EAMS REQUESTED AND RECEIVED RELISDR FDEA2019120123145Skin Panel · delaminatedRIGHT HAND HORIZONTAL STABILIZER HAS A PANEL ON THE BOTTOM SIDE WITH A DELAMINATED AREA OF APPROXIMATELY 2' X 3'. AREA IS LOCATED JUST AFT OF THE LEADING EDGE AND 5' OUTBOARD OF THE FUSELAGE. REMOVED & INSTALLED NEW SKIN PANEL RT LOWER HORZ STAB IAW SRM 51-4SDR SWAA2019122639908Skin · crackedR/H HORIZONTAL STABILIZER CRACKED ON LOWER SKIN OF AT HSS. 129.20. REPAIRED IN-SPAR SKIN PER EA.SDR DALA2019112516890Skin · corrodedCORROSION LEVEL: 2 HORZ STAB BOX HAS CORR ON TOP SKIN JUST ABOVE PANEL 341AZ CORROSION OUT OF LIMITS. C/W ERA 582917-14. (LP 1369339)SDR CALA2019112532027Skin · crackedLT HORIZ. STAB. SKIN HAS CRACK INDICATION BETWEEN STAS. 129.5-13 8.7 2" FWD OF AFT SPAR. (REF FLEET CYCLE LOG PAGE #9704508) SEE FLEET CYCLE LOG PAGE #9704508 FOR WORK ACCOMPLISHED. DIP FOR INSPECTION IS INCLUDED IN ELB LOG PAGE#9865718. NO CHANGES MADE TO DISDR C77A2019111500002Skin · dentedWHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZERSDR C77A2019111500001Skin · dentedWHILE TAXIING IN PDX, AIRCRAFT 213NN WAS STRUCK BY ANOTHER AIRCRAFT BEING TOWED. EXTENSIVE DAMAGE WAS SUSTAINED TO THE RH HORIZONTAL STABILIZER. THE RH ELEVATOR WAS FRACTURED COMPLETELY AND WILL BE REPLACED SEPARATELY FROM THIS EO. THE RH HORIZONTAL STABILIZERSDR R61A2019120411349Skin · dentedDENT FOUND ON L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 3A-4 AND BETWEEN STR 01 L AND 02 L. MAINTENANCE REPAIRED THE L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 3A-4 AND BETWEEN STR 01 L AND 02 L. IAW EMB ETD 2019-170-157527.SDR R61A201912041348Skin · dentedDENT FOUND ON L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 5-6 AND BETWEEN FRONT SPAR AND STR 01 L. MAINTENANCE REPAIRED THE L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 5-6 AND BETWEEN FRONT SPAR AND STR 01 L. IAW EMB ETD 2019-170-157527.SDR R61A2019120411347Skin · dentedDENT FOUND ON L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 4-5 AND BETWEEN FRONT SPAR AND STR 01 L. MAINTENANCE REPAIRED THE L/H HORIZ. STAB, LOWER SKIN BETWEEN RIB 4-5 AND BETWEEN FRONT SPAR AND STR 01 L. IAW EMB ETD 2019-170-157527.SDR FDEA2019111542960Landing · crackedH-STAB ACCESS PANEL 311AB LANDING ON LH HAS A CRACK REMOVED DAMAGE IAW SRM 53-00-01 FIG 4 SHT 2. PERFORMED HFEC IAW SOPM 06-10-01-001. NO FURTHER CRACKS REMAIN. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO 8- 5310-T0350635 PT1 TITLE: FUSELAGE - MAIN FSDR SWIA2019122747203Skin · damagedRIGHT HORIZONTAL STAB TIP 343BR HAD EXPOSED COMPOSITE ON THE L/E. REPAIRED IAW EO.SDR CALA2019111101951Skin · crackedR/H HORIZONTAL STAB LOWER SKIN AREA AT STA. 138.70 CRACK INDICAT ION NOTED, 6" INCHES FROM THE FWD SPAR. REPAIRED R/H HORIZONTAL LWR SKIN CRACK AT STA. 138.10 PER SRM 55-10-01 REPAIR 11 PG. 201 REF. MCO FLEET CYCLE LOG PAGE 9704427 THRESHOLD OF 56,000 TOTAL CYSDR CALA2019110981931Skin · crackedEA 5510-01843 REV H HORIZ STAB LOWER IN SPAR SKIN PANEL C-SCAN I NSP REVEALED 3 EA CRACKS LEFT HAND LOWER SURFACE 2 INBD SIDE OF STA 120.3, 9"-9.5" & 17"-18" AND 1 ON INBD SIDE OF STA 129.5 25" TO 26" ALL FWD OF REAR SPAR. REPAIRED 3 EA CRACKS ON HORIZ STAB LOSDR 21GA20191107007Skin · corrodedMULTIPLE AREAS OF SCATTERED SURFACE CORROSION ON FASTENER HEADS ON THE UPPER SURFACE OF THE HORIZONTAL STABILIZER RH BETWEEN THE REAR SPAR AND TRAILING EDGE AT STATION 224.SDR IPXA2019120449714Skin · dentedINSPECTION TYPE:757D687950 RT HORZ STAB UPPER SKIN AND LEADING EDGE DAMAGEREPAIRED RT HORZ STAB UPPER SKIN DAMAGE AT LOCATION #4 IAW UPS EO NO B757-5510-74589-ASDR IPXA2019120449713Skin · dentedINSPECTION TYPE:757D687950 RT HORZ STAB UPPER SKIN AND LEADING EDGE DAMAGEREPAIRED RT HORZ STAB UPPER SKIN DAMAGE AT LOCATION #3 IAW UPS EO NO B757-5510-74589-ASDR IPXA2019120449712Skin · dentedINSPECTION TYPE:757D687950 RT HORIZ STAB UPPER SKIN AND LEADING EDGE DAMAGEREPAIRED RT HORZ STAB UPPER SKIN AT LOCATION #2 IAW UPS EO NO B757-5510-74589-ASDR IPXA2019120449711Skin · dentedINSPECTION TYPE:757D687950:RT HORZ STAB UPPER SKIN AND LEADING EDGE DAMAGEREPAIRED RT HORZ STAB UPPER SKIN DAMAGE AT LOCATION #1 IAW UPS EO NO.B757-5510-74589-ASDR DALA2019110106356Skin · cracked(LOG 1340234) DURING INSPECTION FOUND CRACKS ON LOWER SKIN BTW STA STAB 111.10 AND 129.50 4EAS AT LH HORIZONTAL STABILIZER. LH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01 REPAIR 11.SDR DALA2020012900683Skin · dentedDURING WALK AROUND INSPECTION, FOUND DENT ON LT HORIZONTAL STAB LEADING EDGE APPROX. 126" FROM INBD EDGE. MEASURES 2.25" WIDE AND 0.145"DEEP. CORRECTIVE ACTION: REMOVED AND REPLACED LH HORIZONTAL STAB LEADING EDGE PER B737 AMM 55-10 AND APPLIED SPEED TAPE SRMSDR CALA2019110101868Skin · crackedEA 5510-01843 REV H; FOUND ON LEFT SIDE HORIZONTAL STAB, LOWER S KIN, AT STAB STA 129.5 MEASSURED FROM THE AFT SPAR GOING FORWARD 10 INCHES. THE CRACK MEASURES 3/4 INCH IN LENGTH. MARKED. REF F LEET CYCLE NON ROUTINE 9700271. COMMON DOUBLER INSTALLED ON L/H HOSDR CALA2019110101867Skin · crackedREF EA5510-01843 REV H . FOUND A CRACK RH SIDE HORIZONTAL STAB LOWER SKIN AT STAB STA 157.1,MEASURED FROM THE AFT SPAR GOING FWD 9 INCHES . TE CRACK MEASURES 3/4 INCH IN LENGHT . REF FLEET CYCLE N/R 9700274 FOR ALL WORK PERFORMED PER SRM 55-10 -01 REPAIR 11 . SDR ASAA2019102331201Skin · crackedCRACK INDICATION NOTED BETWEEN AT STAB STA 138.70 AND STAB STA 147.90 APROX .5 IN LENGTH. LOCATION IS APOX 5 INCHS FROM CENTERLINE OF FWD ROW OF FASTNER AFT SPAR AND 2 INCH AFT SIDE FROM DOUBLER ON THE STA 147.90 END POINTS OF CRACK ARE IDENTIFIED IN RED MARKE
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