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 CALA2026011913044Skin · damagedRIGHT HORIZONTAL STAB LOWER SKIN REQUIRES SKIN CUTOUT AND REPAIR TO FOM AT APPROX STAB STA 92.70. ACCOMPLISHED PERMANENT REPAIR ON RT HORIZONTAL STAB LOWER SKIN BETWEEN HSS 83.50 TO HSS 111.10 IAW SRM 55-10-01-2R-11. THIS IS A CATEGORY 'B' REPAIR AND REQUIRESDR CALA2026010912836Skin · damagedRIGHT HORIZONTAL STAB LOWER INSPAR SKIN AT HSS 101.9, REQUIRES CUT-OUT TO FACILITATE RIB REPAIRS. COMPLETED REPAIR ON THE RT HORIZONTAL STAB SKIN AT HSS 101.9 IAW SRM 55-10-01, REPAIR 11.SDR SWAA2026011954657Access Panel · crackedCRACKED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND DWG 186A3101, SHEET 13, REV C.SDR CALA2026010712735Skin · crackedRIGHT STAB LOWER SKIN NR 2, CRACK INDICATION FOUND, HSS 184.70 INBD OF INBD ROW OF FASTENERS, AFT OF FWD SPAR. REMOVED THE DAMAGE & ACCOMPLISHED A REPAIR OF THE DAMAGE AT THE RT STAB LOWER SKIN NR 2 HAS CRACKED AT BS 184.70 INBD OF INBD ROW OF FASTENERS AFT OSDR SWIA20251219Rib · crackedLEFT HORIZONTAL RIB 12 UPPER FLANGE SUSPECTED CRACK (C-CHECK RO 01/16/2026)PERFORMED FLANGE REINFORCING REPAIR ON LH HORIZONTAL RIB 12 UPPER FLANGE REF ETD2026-170-000257. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.ON TASK CASDR AALA202512310157Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 157.10, 16 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202512314214Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 153, ALONG AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202512302207Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN ALONG RIB AT STABILIZER STA 92.70, 9 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR CALA2025122412433Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT HSS 157.10, - 8 INCHES FROM REAR SPAR, INBD ROW. CRACK LENGTH: 1 INCH. CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN, FABRICATED REPAIR PARTS, DOUBLER, 2 FILLERS AND INSTALLED IAW SRM 55-10-01-2R-11, FISDR CALA2025122912507Skin · crackedONE CRACK SIGNAL NOTED L=0.450 INCH AT STAB RH SIDE STA129.50 LOC ATED TO 10.375INCH FWD FROM REAR SPAR. PERFORMED PERMANENT REPAIR AT RT HORIZONTAL STAB AT STAB STA 129.50 AND 10.375 IAW SRM 55-10-01-2R-11SDR CALA2025122912455Skin · crackedCRACK FOUND AT LT HORIZONTAL STAB LOWER SKIN AT STAB STA 147.90 , INBD ROW, 15.5" FROM FRONT SPAR. CRACK LENGTH 0.75". REF AAR N/R 99987207 ESFR INFORMATION ENTERED REMOVED DAMAGE AT LEFT HORIZONTAL STABALIZER LOWER SKIN AT STA 147.90" FABRICATED REPAIR PARTS SDR SWAA2026010551717Access Panel · crackedCRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER. REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER IAW SRM 51-40-02 AND DWG 186A3101 SHEET 13 REV: C.SDR CALA2025122412429Skin · crackedCRACK FOUND ON RT HORIZONTAL STAB LOWER SKIN AT HSS 120.30, INBD ROW, 11 INCHES FROM REAR SPAR. CRACK LENGTH: 1 INCH. REMOVED PREVIOUS REPAIR , FABRICATE NEW DOUBLER & INSTALLED NEW REPAIR PARTS IAW SRM 55-10-01-2R-11, REPAIR 11, PAGE 7, TABLE 204.SDR FDEA202512102230Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN HAD REPAIR DAMAGE AT LOWER INTERNAL SURFACE, HSS 104.248 & 128.248, DENT WITH DELAMINATION AT LT HORIZONTAL STAB UPPER SKIN ON LOWER INTERNAL SURFACE WAS APPLIED PERMANENT REPAIR IAW SRM 55-10-01-1A, TABLE 1, NOTE I, & SRM 51-SDR FDEA202512102229Skin · dentedLEFT HORIZONTAL STAB UPPER SKIN HAD FIVE DENTS BETWEEN HSS 81.249 AND 104.248, APPLIED PERMANENT REPAIR AT LT HORIZONTAL STAB UPPER SKIN IAW SRM 55-10-01-1A, TABLE I NOTE I & SRM 51-70-10-2RSDR AALA202512098048Skin Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER UPPER SKIN PANEL DELAMINATED BETWEEN FRONT SPAR STA 177.9 AND 228.526. REPAIRED PANEL PER SRM 55-10-01-2R REPAIR 2.SDR SWAA2026011243639Access Panel · crackedCRACKED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STAB AND FASTENERS IAW SRM 51-10-02-0G ITEM 9, SRM 51-40-02-0G, AND DWG 186A1001, SHEETSDR AALA202512091977Skin Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER UPPER SKIN PANEL DELAMINATED BETWEEN FRONT SPAR STA 177.9 AND 228.526. REPAIRED PANEL PER SRM 51-70-00.SDR SWAA2025122343445Access Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE HSS 105.26, LT HORIZONTAL STAB. REPLACED RIB LEADING EDGE ACCESS PANEL 331B IAW SRM 51-40-02, AND DWG 186A1001, SHEET 10, REV A.SDR SWAA2025122942687Skin · crackedCRACK NOTED ON LT HORIZONTAL STABILIZER LWR SKIN AT HSS 193.90; 17.5' FROM FWD EDGE; L: 0.6'. REPAIRED LT LOWER HORIZONTAL STAB SKIN IAW SRM 55-10-01-2R-11, REPAIR 11, TABLE 201, TABLE 202, FIG. 204, DETAIL B, AND SRM 51-40-02-0G-0.SDR IXXA20251203005Skin · delaminatedRIGHT HORIZ STAB UPPER SKIN L/E INNER PANEL DELAMENATED PN 185T1001-2SDR DALA2025120508912Skin · wornHORIZONTAL STABILIZER LH LOWER BLAND SEAL CUTOUT SKIN WORN AT STA 1788. DAMAGED AREA REPAIRED PER B767-400 SRM53-80-01-2R-3 (1331681)SDR DALA2025120508911Skin · wornHORIZONTAL STABILIZER LH LOWER BLAND SEAL FWD SKIN WORN. DAMAGED AREA REPAIRED PER B767-400 SRM53-80-01-2R-3 (1331679)SDR DALA2025120508910Skin · wornHORIZONTAL STABILIZER RH LOWER BLAND SEAL FWD SKIN WORN. DAMAGED AREA REPAIRED PER B767-400 SRM53-80-01-2R-3 (1331678)SDR DALA2025120508909Skin · wornHORIZONTAL STABILIZER RH LOWER BLAND SEAL LOWER SKIN WORN. DAMAGED AREA REPAIRED PER B767-400 SRM53-80-01 (1331675)SDR SWAA2026011241671Skin Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL. HSS 193.9, AND 16 INCHES FROM FRONT SPAR. INBD SIDE OF RIB. CRACK LENGTH = 0.950 INCH. PERFORMED REPAIR ON LT HORIZONTAL STAB LOWER SKIN PANEL IAW SRM 55-10-01-2R-11, REPAIR 11.SDR AALA202512238128Access Panel · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER AFT SPAR UPPER SLIDER PANEL 333AT FORWARD GUIDE IS WORN THROUGH AT THE TOP AFT CORNER. REPLACED PANEL 333AT PER SRM 51-40-02.SDR YENA2025120201154Skin · dentedDURING HEAVY MAINTENANCE: SEVERAL DENTS ON ACCESS PANEL 341BB LEADING EDGE ON RH HORIZONTAL STABILIZER; EVALUATED DENTS ON ACCESS PANEL 341BB LEADING EDGE ON RH HORIZONTAL STABILIZER AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS AS PER A320 SRM 55-12-11-283-003 PASDR SWAA2025121940907Access Panel · delaminatedDELAMINATED ACCESS PANEL 344AB ON RT HORIZONTAL STAB. REPLACED ACCESS PANEL 344AB AT RT HORIZONTAL STAB IAW AMM 27-31-11-400-801, STEP 3.G (19), (H), AND SRM 51-10-02, ITEM 9, AND INSTALLED.SDR UATA2025121100501Skin · crackedRIGHT HORIZONTAL STAB TOP SKIN CRACKED JUST OTBD OF AFT ATTACH FITTING HSS 740. REMOVED TOP REAR SKIN FROM STAB ROOT TO WS 1200. ELEVATOR COVE SKIN WAS DE-RIVITED TO WS 1500 FOR ACCESS. FABRICATED NEW SKIN AND PATTER AS ORIGINAL INSTALLATION. ACID ETCHED, ALSDR SWAA2025123039496Panel · crackedPANEL 344GB UPPER SURFACE CRACKED. REMOVED AND REINSTALLED PANEL 344GB IAW AMM 20-50-11.SDR CALA2025120311737Skin · crackedTWO CRACKS SIGNAL NOTED AT STAB RT SIDE HSS 157.10, FIRST CRACK L=0.416 INCH LOCATED TO 9.356INCH FWD FROM AFT SPAR, SECOND CRACK L=0.381INCH LOCATED TO 16.500 INCH FWD FROM AFT SPAR. (PERFORMED PERMANENT REPAIR AT RH HORIZONTAL STAB AT STAB STA 157.10 AND 16.SDR AALA202511245771Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION TO RIGHT HORIZONTAL STABILIZER UPPER PANEL LOCATED FROM FSS 58.82 TO FS 102. REPAIRED PANEL PER SRM 55-10--01-2R.SDR SWAA2025121039101Access Panel · crackedCRACKED ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER IAW SRM 55-20-01-2R-4, REPAIR 4.SDR SWAA2025121039100Access Panel · crackedCRACKED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW SRM 55-20-01-2R-4, REPAIR 4.SDR SWAA2025120939102Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW SRM 51-70-04-2R-9, REPAIR 9.SDR CALA2025120211696Skin · crackedCRACK FOUND AT LT HORIZONTAL STAB LOWER SKIN AT HSS 129.50, 18 FROM REAR SPAR, INBD ROW. CRACK LENGTH 1 INCH. REMOVED DAMAGE ON SKIN. FABRICATED REPAIR & INSTALLED IAW SRM 55-10-01-2R-11, REPAIR 11, SRM 55-10-01 PARAGRAPH 5, REPAIR 11.SDR SWAA2025123038149Access Panel · crackedCRACK ON ANGLE BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB. REPLACED ON ANGLE BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 186A3101, SHEET 25, REV -. MEASUREMENT OF CRACK IS: L= 0.24.SDR CALA2025112811574Skin · crackedRH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED L=0.855INCH APROX. AT STAB STA157.10 AND 9 INCH FROM AFT SPAR (REF AAR NR 1000060368)PERFORMED PERMANENT REPAIR AT RH HORIZONTAL STAB AT STAB STA157.10 AND 9 INCH FROM AFT SPARTHIS REPAIR IS A CATEGORY "B",SDR CALA2025112811573Skin · crackedLH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED L=1INCH APROX. AT STAB STA147.90 AND 15.600 INCH FROM FWD SPAR (REF AAR NR 1000060354) PERFORMED PERMANENT REPAIR AT LT HORIZONTAL STAB AT STAB STA147.90 AND 15.600 INCH FROM FWD SPAR THIS REPAIR IS A CATEGSDR CALA2025120211694Skin · crackedCRACK FOUND AT LT HORIZONTAL STAB LOWER SKIN AT HSS 101.90, 11, FROM REAR SPAR, INBD ROW. CRACK LENGTH 1". PER SRM 55-10-01, PARAGRAPH 5./REPAIR 11. REMOVED DAMAGE AT LT HORIZONTAL STAB LOWER SKIN HSS 101.90. FABRICATED REPAIR PARTS & INSTALLED REPAIR 11SDR SWAA2025112034436Access Panel · crackedCRACK ON ACCESS PANEL 344GB AT RT HORIZONTAL STABILIZER. REPLACED ACCESS PANEL 344GB IAW B737-700 AMM 27-31-00-200-801 STEP 7.D(6).SDR FDEA202511112160Skin · delaminatedLH HORIZONTA STABILIZER UPPER SKIN HAS POSSIBLY DELAMINATION STAB STA 104.248 AREA APPLIED PERMANENT REPAIR AT LH HORIZONTAL STABILIZER UPPER SKIN I.A.W B757 SRM 55-10- 01-1A, TABLE I, NOTE 'A' AND "I", FIG 101, SHEET 2, I.A.W B757 SRM 51-70-10-2RSDR FDEA202511112159Skin · dentedRH HORIZONTAL STABILIZER LOWER SURFACE HAS TWO DENTS STAB STA 176.249 AREA TWO DENTS FOUND OUT OF LIMITS AT RH HORIZONTAL STABILIZER LOWER SURFACE STAB STA 176.248. AND APPLIED PERMANENT REPAIR I.A.W B757 SRM 55-10-01-1A, TABLE I, NOTE 'I' FIG 101, SHEET 3SDR SWAA2025121546413Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STAB, LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 9 INCH REAR SPAR IN SIDE OF RIB. CRACK LENGTH = 1.000 INCH. PERFORMED A REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11.SDR SWAA2025121533441Skin · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 9 INCHES REAR SPAR INSIDE OF RIB. CRACK LENGTH = 1.000 INCH. PERFORMED REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11.SDR CALA2026090119130Skin · crackedCRACK FOUND ON RT HORIZONTAL STAB LOWER SKIN AT HSS 101.90, 10" FROM REAR SPAR, INBD ROW. CRACK LENGTH 1IN?. REPAIRED THE RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11.SDR SWAA2025121031136Stiffener · crackedFWD CARGO BAY BULKHEAD VERTICAL STIFFENER CRACKED BS 540, LBL 0.22. REPLACED THE VERTICAL STIFFENER IAW SRM 51-40-02-0G-0, SRM 51-10-02-G-0, ITEM 9, AND DWG 11A2001, SHEET 113, REV B.SDR SWAA2025121031134Plate · crackedCRACKED SEAL PLATE, ACCESS PANEL 333AB AT THE LT HORIZONTAL STAB. REPLACED THE SEAL ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, STEP 9.SDR SWAA2025111730206Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 26' FROM FWD EDGE; .4' LENGTH. REPAIRED LT LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90 PER REF SRM 55-10-01-2R-11. VERIFIED COMPLETED RII STEPS IN CORRECTIVE ACTION 1.
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