JASC 5512
Service difficulty reports · 7,886
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 SWAA2025120429804Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 343BB, RT HORIZONTAL STAB. REPAIRED ACCESS PANEL 343BB, RT HORIZONTAL STAB IAW SRM 51-70-04-2R-9, REPAIR 9.SDR DALA2026020900908Skin · damagedERA 630089-14, SECTION I, ISSUED FOR BIRD STRIKE DAMAGE TO RT HORIZONTAL STAB LEADING EDGE INBD STRUCTURE. REPAIRED IAW ER/A 630089-14. (1269533)SDR VGCA202511254009Skin Panel · damagedR/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED I.A.W. V1 AEROSPACE DOC. NO. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025SDR SWAA2025112028186Access Panel · crackedCRACKED SEAL - BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER. REPLACED BLADE LOCATED ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02.SDR FDEA202510242090Skin · dentedRH HORIZONTAL STAB FRONT SPAR UPPER SURFACE DENT STA 159.248 APPROX FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 159.248 OUT OF LIMITS DIM A= 1.500" Y=0.054" A/Y=27.77 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I, NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4SDR FDEA202510242089Skin · dentedRH HORIZONTAL STAB FRONT SPAR UPPER SURFACE HAS A DENT (STA 86.600) FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 86.600, OUT OF LIMITS DIM A=1.500", Y=0.069", A/Y=21.73 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4SDR CALA2025102810637Skin · crackedCRACK INDICATION FOUND AND VERIFIED: R/H HORIZ STAB LOWER SKIN STA 120.30 MARKED #1 .900"L 17" AFT OF FRONT SPAR I/B OF I/B FASTENER ROW. EVALUATED CRACK ON LOWER SKIN AND CUT OUT DAMAGE AND REMOVED EXISTING DOUBLER AT STA 120 IAW SRM 55-10-01- 2R-11. FABRICSDR CALA2025102810635Skin · crackedCRACK INDICATION FOUND AND VERIFIED, R/H HORIZ ST AB LOWER SKIN STA 120.30 .800L 25.5" AFT OF FRONT SPAR I/B OF I/B FASTENER ROW. EVAL CRACK ON LOWER SKIN STA 120.30, 25.5 INCHES OF FRONT SPAR, CUTOUT DAMAGE AND REMOVED EXISTING DOUBLER AT STA 120 IAW SRM 5SDR DALA2025102207727Skin · dentedSHIP 3128 LEFT HAND HORINZONTAL STABILIZER LEADING EDGE FOUND TO HAVE MULTIPLE DENTS. CORRECTIVE ACTION: EVALUATED REF A319 SRM 51-77-10. COMPLETED GVI REF A319 NTM 51- 90-00 AND TAP TEST REF A319 NTM 51-10-03. NO DISCREPANCIES NOTED. AREA PREVIOUSLY BLENDED ASDR SWI2026F00028Access Panel · elongated11EA OBLONG HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL REPAIRED ELONGATED SCREW HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF REO 601R-55-11-812 REV. --,SDR CALA2025102610538Skin · crackedCRACK INDICATION FOUND & VERIFIED: RT HORIZ. STAB LOWER HSS STA.147.90. 1 .600"L 15.5" AFT OF FRONT SPAR I/B OF I.B FASTENER ROW. DOT:B616. REMOVED EXISTING DOUBLER, FABRICATED AND ALODINED, PRIMED AND INSTALLED NEW DOUBLER AND FILLER AT R/H HORIZONTAL LOWER SDR ASAA2025101461732Skin · gougedRIGHT HORIZONTAL STAB LOWER SKIN DAMAGED AT RIB 6 APPROXIMATELY HSS 138.7. GROUNDED - YES. EVALUATED DAMAGE AT LWR SKIN FOUND TO BE OUT OF LIMITS LENGTH=2.7", DEPTH=.041 IAW SRM 55-10-01-1A-2, FIG.103. REMOVED RT HORIZONTAL STAB. L/E PANEL & STAB. CAP IAW SRMSDR SWAA2025110723429Skin · crackedCRACK ON THE RT LOWER HORIZONTAL STABILIZER SKIN AT HSS 193.90, 26 INCHES FROM FWD EDGE, .30' IN LENGTH. REPAIRED THE RT LOWER HORIZONTAL STAB SKIN, APPLIED A FILLET SEAL, CIC, AND A FINISH TO THE REPAIR AREA IAW SRM 55-10-01-2R-11, REPAIR 11.SDR KCSA202510101180Skin · damagedLIGHTNING STRIKE DAMAGE ON R/H HORIZONTAL TIP AFT SIDESDR 2DYA2025081300010Skin · puncturedLEFT HORIZONTAL STAB PUNCTURED AT TWO LOCATIONS REF LP 57598. INTERIM REPAIR INSTALLED TO THE LH H-STAB INSPAR LOWER SKIN AT RIB 10 BETWEEN STRINGERS 3 AND 7 PER ASI ENGINEERING REPAIR ORDER NO. 5510D4013. INSTALL A PERMANENT REPAIR DURING THE NEXT C-CHECK INSDR 2DYA2025F00239Skin · puncturedL/ HORIZONTAL STAB PUNCTURED AT TWO LOCATIONS. INTERIM REPAIR INSTALLED TO THE LH H-STAB INSPAR LOWER SKIN AT RIB 10 BETWEEN STRINGERS 3 AND 7 PER ASI ENGINEERING REPAIR ORDER NO. 5510D4013. INSTALL A PERMANENT REPAIR DURING THE NEXT C-CHECK INSPECTION. 9-OCTSDR CALA2025110410882Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 120.30, 26" FROM FRONT SPAR, I/B ROW. CRACK LENGTH:1" REF. AAR N/R:99951969 INSTALLED NEW REPAIR DOUBLER ON RT HORIZONTAL STABILIZER LOWER SKIN AND 2EA REPAIR FILLERS AT STAB STA 120.30 PER SRM SDR ABXA20251005246Skin · delaminatedDURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND R/H HORZ STAB LOWER SKIN HAS AREA OF DELAMINATION AT AUX SPAR STA 243 JM-30.FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LOWER SKIN PANEL IAW B767-300 SRM 51-40-02.SDR DALA2025100607239Skin · crackedCRACK ON LOWER SKIN STAB STA 101.90 AT LH HORIZONTAL STABILIZER. LOWER SKIN STAB STA 101.90 AT LH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R REPAIR 11.SDR JR2R20251003187Skin · scratchedHORIZONTAL STAB L/E PANEL 331AL HAS SCRATCH MARKS. REPAIRED PER ETD.SDR DALA2025100207169Skin · cracked(LOG 1229629) CRACK (3 EAS) ON LOWER SKIN STAB STA 101.90, 138.70 AND 147.90 AT RH HORIZONTAL STABILIZER. LOWER SKIN STAB STA 101.90, 138.70 AND 147.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11 REPAIR 11.SDR FDEA202509301855Panel · dentedLH HORIZONTAL STAB LE PANEL 332EL FOUND PREVIOUS DENT REPAIR AT AS STA 482. PERFORMED DVI FOUND SURFACE CRACK AS PER B777 SRM51-10-02-0G REV:47.6. PERFORMED HFEC INSPECTION FOUND CRACK LENGTH APPROX 0.315" AS MARK AS PER B777 NDTM PART6 51-00-01 REV:94. THSDR CALA2025110410881Skin · cracked[EA 5510-01843]- CRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 157.10 , 23" FROM FRONT SPAR , I/B ROW. CRACK LENGTH: 1.5". REF AAR N/R 99951973 ACCOMPLISHED REPAIR ON LEFT HORIZONTAL STABILIZER LOWER SKIN, AT STA: 157.10, 23.0" FROM FRONT SPSDR JGVR20250926001Skin · damagedMECHANICALLY BLENDED 8 AREAS ON RT H-STAB LOWER SKIN ON THE AFT EDGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED , TREATED, PRIMED AND TOP COATED AREAS PER NETJETS REQUEST FOR TECHNICAL DISPOSITION REPORT.SDR SWAA2025103018375Skin · crackedCRACK FOUND ON RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT HSS 193.90, RIB 17.5 INCHES FROM FRONT SPAR. INBD SIDE OF RIB LENGTH APPROX= 1.130 INCHES. PERFORMED REPAIR ON RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN IAW SRM 55-10-01-2R-11, REPAIR 11.SDR CALA2025093009437Skin · damagedRIGHT HORIZONTAL STAB LOWER INSPAR SKIN, INTERIM REPAIR ACCOMPLISHED INTIAL INSPECTION ON OR BEFORE THE AIRCRAFT RE ACHING 56,000 CYCLES. PERFORM REPEAT INSPECTIONS PER PAR T 2 -INSPECTION REQUIREMENTS AT INTERVAL NOT TO EXCEED 9000 FLIGHT CYCLES THERE AFTERSDR DALA2025092907042Skin · damaged(LOG 7546848) BIRD STRIKE ON FINAL APPROACH FO SIDE HORIZONTAL STAB. REPAIRED R/H HORIZONTAL L/E PER BOEING DWG 186A1001. RE-INSTALLED R/H HORIZONTAL L/E SKIN PER BOEING DWG 186A1001.SDR AALA202510048085Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN ALONG RIB AT STABILIZER STA 138.70, 18 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202510047724Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN ALONG RIB AT STABILIZER STA 138.70, 9 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11 AND EA 368024.SDR CALA2025092609315Skin · crackedTWO CRACKS SIGNAL NOTED AT STAB RH SIDE HSS 147.90, FIRST CRACK L=1 INCH LOCATED TO 9.125 INCH FWD FROM AFT SPAR, SECOND CRACK L=1.500 INCH LOCATED TO 16.500 INCH FWD FROM AFT SPAR. PERFORMED PERMANENT REPAIR AT RT SIDE HORIZONTAL STABILIZER HSS 147.90, LOCATESDR CALA2025092609314Skin · crackedCRACK SIGNAL NOTED AT STAB RH SIDE HSS 129.50, L=0.500 INCH LOCATED TO 9 INCH AFT FROM FRONT SPAR. PERFORMED PERMANENT REPAIR AT RH SIDE HORIZONTAL STABILIZER HSS 129.50, LOCATED 9 INCHES AFT OF FRONT SPAR, THIS REPAIR IS CATEGORY "B", REQUIRES REPETITIVE INSSDR AALA202510146970Panel · splitAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZE, FORWARD SPAR UPPER SLIDER PANEL IN FUSELAGE IS SPLIT ALONG THE EDGE. INSTALLED RIGHT HAND UPPER SLIDER. PER AMM 53-31-31.SDR DALA2025091806865Skin · damagedWHILE INSPECTING ACFT AFTER NR 2 ENG. FAILURE. FOUND DENT AND 2 HOLES IN RT HORIZ. STAB LEADING EDGE. REPLACED RT HORIZONTAL STABALIZER IAW B737 AMM 27-41.SDR CALA2025092209113Skin · dentedDENT ALONG RH HORIZONTAL LOWER SURFACE.DAMAGE CUT OUT FOR AVO 15542 STEPS 2 AND 3 ACP ON LP 6153673 AND NDT ACP ON SAME LP. REMOVED FASTENERS COMMON TO REPAIR DOUBLER REF, AVO. 15542 REV. A, READY FOR NDT OPEN HOLE INSPECTION. ACPD HFEC PER AVO 15542 ITEM 5A ASDR CALA2025092209110Skin · crackedTWO CRACKS SIGNAL NOTED AT STAB LH SIDE STA129.50, FIRST CRACK L =0.500 INCH LOCATED TO 10.300INCH FWD FROM AFT SPAR, SECOND CRAC K L=0.625INCH LOCATED TO 18.250 INCH FWD FROM AFT SPAR PERFORMED PERMANENT REPAIR ON HORIZONTAL STABILIZER LOWER SKIN L H SIDE SSDR CALA2025101309982Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 120.30 , 19" FROM REAR SPAR, I/B ROW. CRACK LENGTH : 0.343". REPAIRED AREA AND FABRICATED REPAIR PARTS LOWER INSPAR SKIN AT STAB. STA 120.30 AND 129 AND 138 RIGHT HORIZONTAL STABILIZER IN REF TSDR DALA2025090806605Skin · crackedCRACKS ON LOWER SKIN, STAB STA 101.90 AT LH HORIZONTAL STABILIZER. LOWER SKIN, STAB STA 101.90 AT LH HORIZONTAL STABILIZER WAS REPAIRED PER B 737-800 SRM 55-10-01-2R REPAIR 11.SDR CALA2025101309985Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB. STA 175.50 , 10" FROM REAR SPAR,I/B ROW. CRACK LENGTH : 0.281" ESFR SUBMITTED ACCOMPLISHED REPAIR ON LOWER INSPAR SKIN STA175.50 AT LH HORIZ. STAB. REF SRM 55-10-01-2R-11 & DWG 182A4001 AND REQUIRESSDR CALA2025090808601Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA.129.50;16.5" FROM FRONT SPAR,I/B ROW.CRACK LENGTH:1.156" . ACCOMPLISHED PERMANENT REPAIR CATEGORY B AT RT HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STAB HSS 129.50 IAW SRM 55-10-01-2R-11, REPAISDR SCNA20250905361Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED IN 2 SPOTS, 1 3/8, 1 1/4 AT STAB STATION 147.90 APPROX 24" AND 31" AFT OF FRONT SPAR. ACCOMPLISHED REPAIR OF CRACKED SPOTS ON 2 AREAS ON LEFT HORIZONTAL STABILIZER IAW B737 SRM 55-10-01-2R-11 AT STAB STATION 147.9SDR ASAA2025082761114Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT IB SIDE OF RIB 7 STA 138.70, 10 IN FROM TE. GROUNDED - YES. CUT OUT DAMAGE AT STA 138.7 AND ADDITION CRACK AT STA 120.3 FOUND ON MIG-5 OK436985 1023406 3000/0003, AND REPAIRED AREA IAW B737-800 SRM 55-10-01-SDR ASAA2025082760960Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT IB SIDE OF RIB 6 STA 129.50 8 IN FROM LE. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11 REP 11 THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTASDR AALA202509088505Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 184.7, 8 INCHES FROM THE AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11SDR DALA2025082806359Skin · crackedAIRCRAFT 3766, CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11. (LP 1163553)SDR DALA2025082806358Skin · crackedAIRCRAFT 3766, CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11 CATEGORY B REPAIR. (LP 1163546SDR AALA202509081503Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 8 INCHES FORWARD OF THE AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11SDR AALA202508281383Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 101.90, 9 INCHES FROM THE FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11SDR SWAA2025100607677Access Panel · crackedCRACK ON BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0, MEASURE OF CRACK IS 0.332 INCH.SDR CALA2025090808598Skin · crackedCRACKS FOUND AT RIGHT HORIZONTAL STAB LOWER SKIN AT HSS 175.50, 10" FROM FRONT SPAR, INBB ROW. CRACK LENGTH: 0.343". ACCOMPLISHED PERMANENT REPAIR CATEGORY B IAW SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 DETAIL B.SDR ASAA2025082061212Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN IS CRACKED ON THE I/B SIDE OF STA 147.90 APPROX 8 INCHES FROM REAR SPAR.262A001. GROUNDED - YES. REPAIRED LEFT HORIZ STAB LWR SKIN AT STA 147 IAW B737-800 SRM 55-10-01-2R-11, THIS IS A CAT B REPAIR WITH A THRESHOLD AT 56,000 FLI
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