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 CALA0400425Panel · crackedGAP PANEL BETWEEN LT HORIZONTAL STAB AND TAIL CONE CRACKED. REPLACED PART PER SRM 51-10-02.SDR ASAA0440108Skin · dentedGYR - FOUND DEN ON HORIZ STAB LEADING EDGE APPROX 50 INCHES FROM INBOARD EDGE MEASURED 1 INCH DIAMETER .040 DEEP. REPAIRED DENT IAW SRM 55-10-01 AND REPAIRED RIB PER SRM 55-10-09. (M)SDR ASAA0440109Skin · dentedFOUND TWO EACH DENTS ON HORIZONTAL STABILIZER LEADING EDGE, ONE AT 13 INCHES FROM INBOARD PLUS 1.25 INCHES BY .875 BY .020 DEEP, ONE AT 50 INCHES FROM INBOARD EDGE REF LOG PAGE 5755154. REPAIRED DENTES ON RIGHT HORIZONTAL STABILIZER LEADING EDGE PER SRM 55-10SDR USAA040105Skin · damagedPIT - FOUND HORIZONTAL STABILIZER SKIN WITH 8 INCH REPAIR, JUST AFT OF FSS 145 RT HORIZONTAL STABILIZER LOWER SKIN. COMPOSITE LAY UP REPAIR PER SRM 51-70-10. (M)SDR LR7A04050Doubler · crackedDURING SCHEDULED C4 INSPECTION PER JOB CARD HC5511 FOUND FS 1063 LOWER HORIZONTAL STABILIZER DOUBLER CRACKED AT RH HSS 61, WL 280. REPLACED DOUBLER IAW SRM SMP 583 51-60 AND 51-70. NR 2190.SDR UPS04842123Skin · corrodedINSPECTION TYPE: C3, RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 91.25 TO XFS103.75, XFS 135-147, XFS 216-228. BLENDED OUT CORROSION, FABRICATED AND INSTALLED 3 REPAIR DOUBLERS IAW SRM 55-2-1 FIG 4.SDR UPS04842122Skin · corrodedINSPECTION TYPE:C3 LEFT HORIZONTAL STAB L/E UPPER SURFACE IS CORRODED BEYOND LIMITS XFS 153.75 TO XFS 161. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4.SDR CALA0400285Skin · crackedINSPECTION FOUND TWO 3 INCH CRACKS IN LEFT HORIZONTAL STABILIZER LOWER SKIN, SPAR STA 131 AND 140. REPAIRED IAW ECRA 5510-01616.SDR SWAA040893Skin · crackedDURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT IN SPAR STA 125. REPAIRED SKIN PER ER.SDR 2004UALA00219Skin · damagedRIGHT HORIZONTAL L/E HAS A TEMPORARY REPAIR 82 INCHES FROM I/B END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 04FDEA01857Skin · crackedHORIZONTAL STABILIZER CONSTANT SECTION UPPER AND LOWER SKIN CRACKED WITHIN FLYABLE LIMITS. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510- 73244. PARTS AFFECTED: ALC7204-1, ALC7205-1, ALC7441-2.SDR UPS04842011Skin · corrodedINSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4.SDR CALA0400195Skin · dentedINSPECTION FOUND LT HORIZONTAL STABILIZER LOWER SKIN DENTED 57 INCHES FROM I/B EDGE AND 33 INCHES BACK FROM T/E. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-10-01.SDR DHL2004750036Skin · dentedDURING -C- CHECK, RIGHT HORIZ STAB, I/B LEADING EDGE AT STAB STA 13.7 HAS A DENTED GOUGE. DENTED GOUGE OUT OF LIMITS IAW B727 SRM 55-10-1 FIG 2. CUT OUT DAMAGE AREA IAW B727 SRM 55-10-3 FIG 2. FABRICATED DOUBLERS FROM 2024 T3 .071 & FILLER FROM 2024 T3 .050SDR CALA0400190Skin · puncturedINSPECTION FOUND LT HORIZONTAL STABILIZER LOWER TRAILING EDGE SKIN PANEL PUNCTURED JUST OUTBOARD OF ELEVATOR, BL 215.28. THE PANEL WAS REPAIRED IAW SRM 51-70-05.SDR IXXA0400046SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND RT HORIZONTAL STAB L/E SURFACE SHOWS CORROSION AND A 1 INCH CRACK. REPAIR ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R18. REMOVED FASTENERS , REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE DAMAGED AREA IASDR CALA0400151Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN RT LOWER HORIZONTAL STABILIZER SKIN AT REAR SPAR STA 100 AND 129. A REPAIR WAS INSTALLED IAW ECRA 5510-01724.SDR 05FDEA00010Skin Panel · crackedHORIZONTAL STABILIZER - CONSTANT SECTION, UPPER AND LOWER SKIN CRACKS WITHIN FLYABLE LIMITS. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73237.SDR IXXA0400059SPlate · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE EXTENAL PART CORRODED STA XFS 341.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG1, 51-1-21 PG.SDR 2004FA0000191Skin · crackedREMOVED HORIZONTAL STABILIZER FOR TAILCONE REPAIR. FOUND TWO 1.5 INCH CRACKS RADIATING FROM LOWER FORWARD CORNER OF TAIL CONE SKIN WHERE BOTTOM OF HORIZONTAL LEADING EDGE RESTS. CRACKS PROGRESSING TOWARDS FORWARD HORIZONTAL STABILIZER MOUNT BOLT HOLES. APPESDR 2004FA0000190Skin · crackedREMOVED HORIZONTAL STABILIZER FOR TAILCONE REPAIR. FOUND TWO 1.5 INCH CRACKS RADIATING FROM LOWER FORWARD CORNER OF TAIL CONE SKIN WHERE BOTTOM OF HORIZONTAL LEADING EDGE RESTS. CRACKS PROGRESSING TOWARDS FORWARD HORIZONTAL STABILIZER MOUNT BOLT HOLES. APPESDR 04FDEA01717Skin · crackedHORIZONTAL STABILIZER - UPPER COSTANT SECTION AND OUTBOARD SKINS CRACKS WITHIN FLYABLE LIMITS. PANELS INVOLVED: ALC7436-1, ALC7437-1, ALC7207-1 AND ALC7208-1. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73235.SDR UPS04241788Skin Panel · corrodedINSPECTION TYPE:C RIGHT HORIZONTAL STAB, UPPER SURFACE STA 17.2 TO 50.5 SKIN ABOVE NR 1 BALANCE PANEL BAY HAS SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-6.SDR 2004UALA00055Skin · gougedLEFT HORIZONTAL STAB LOWER SKIN IS GOUGED AT OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 04FDEA01781Skin · crackedDURING ACCOMPLISHMENT -F- TO -ACF- AT OAN, INSPECTION FOUND CRACKS IN 2 LWR CONSTANT SECTION SKINS OF THE HORIZONTAL STAB. THE CRACKS WHERE WITHIN FLYLABLE LIMITS. HOWEVER, DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PLANKS ANDSDR 04FDEA01780Skin · crackedDURING ACCOMPLISHMENT -F- TO -ACF- AT OAN, INSPECTION FOUND CRACKS IN 2 LWR CONSTANT SECTION SKINS OF THE HORIZONTAL STAB. THE CRACKS WHERE WITHIN FLYLABLE LIMITS. HOWEVER, DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PLANKS ANDSDR SWAA040198Skin · crackedDURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR ATTACHMENT POINT, STATION 90. REPAIRED SKIN CRACK PER SRM.SDR SIMA200402002Skin · damagedABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. SKIN REPLACEMENT DONE IAW SAAB REPAIR STATEMENT 340-SDS-006500 AND STANDAR SRM PRACTISDR CALA0400026Skin · dentedTHE RT HORIZONTAL STABILIZER LOWER SKIN SURFACE WAS FOUND DENTED APPROXIMATELY 1 INCH FROM FORWARD LOWER SPAR AND APPROXIMATELY 5 FT I/B OF TIP. REPAIRED IAW ECRA 5510-01704.SDR LR7A04001Skin · crackedDURING SCHEDULED A1 INSPECTION, FOUND FS 1070 HORIZONTAL STAB LOWER SKIN CRACKED AT RBL 50, WL 265. REPAIRED IAW SRM SMP 583 55-20-06. LP 19339, M2.SDR ASAA04100012Skin · gougedOKC - DURING SCHEDULED D-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT STABILIZER STATION 156.55-159 GOUGED. REPAIRED HORIZONTAL STAB PER EA. (M)SDR UPS04241785Skin · corrodedINSPECTION TYPE: C, LEFT HORIZONTAL STAB UPPER SKIN ABOVE NR 1 BALANCE PANEL HAS SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-06, PANEL REPAIRED IAW SRM 51-40-20.SDR 04FDEA00029Panel · corrodedHORIZONTAL STABILIZER LT UPPER AFT PLANK 35 BARREL NUT BORE CORROSIONS FOUND EXCEED EO 1-5510-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB - BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08.SDR 03FDEA02337Panel · corrodedHORIZONTAL STABILIZER RT UPPER AFT PLANK 35R BARREL NUT BORE CORROSION FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB BARREL NUT BORE REWORK A.D. 2003-22-08.SDR MALA030570Skin · delaminatedRT HORIZONTAL STAB HAS DENT AT HS 99.92, FOUND TO BE DELAMINATED. MAINTENANCE REMOVED AND REPLACED RT HORIZONTAL STAB LOWER SKIN AT HS 99, IAW EO NR S55038 DATED 19 DEC 03. REF TO WORK CARD NR 184027 30272, 253007 FOR ADDITIONAL REPAIR INFORMATION.SDR ASAA0340362Skin · dentedOAK - DURING C-CHECK, FOUND DENT IN RIGHT STABILIZER LEADING EDGE. REPAIRED IAW SRM. (M)SDR AWXA200301617Tip Cap · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT HORIZONTAL STABILIZER TIP LEADING EDGE LBL 252.10. MAINTENANCE BLENDED OUT CRACK ON LT HORIZONTAL STABILIZER TIP LEADING EDGE; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16, REPAIR 11.SDR 04FDEA01613Skin Panel · crackedHORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANELS CRACKED. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-72224 (REF FEDEX NRC N0410) REPLACED PANELS: ALC7205-1, ALC7206-1, ALC7207-1, ALC7208-1.SDR 04FDEA01612Skin Panel · crackedHORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANELS CRACKED. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-70174 (REF FEDEX NRC N1048) PANELS REPLACED: ALC7204-1, ALC7205-1, ALC7207-1, ALC7208-1.SDR 04FDEA01497Skin Panel · crackedHORIZ STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF NRC N1102)SDR 04FDEA01496Skin Panel · crackedHORIZONTAL STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF FEDEX NRC N1102) *S/D COMING*SDR DL767031053Skin · gougedDENT/GOUGE FOUND ON LOWER SURFACE OF LT HORIZONTAL STAB, FORWARD TORQUE BOX, INBD SKIN PANEL. DENT WAS DUE TO GROUND DAMAGE. REPAIRED PER ERA 423716-14.SDR ASAA0340339Skin · dentedOAK - DURING C-CHECK, FOUND LEFT HORIZONTAL STAB LE INBOARD SIDE DENTED. REPAIRED IAW SRM. (M)SDR DL76S031029Skin · delaminatedDELAMINATION FOUND ON HORIZONTAL STABILIZER, FWD TORQUE BOX, UPPER SKIN, RT SIDE, IN SECOND RIB BAY OUTBD FROM FUSELAGE. INNER SKIN OF THE ALUM HONEYCOMB PANEL WAS DELAMINATED FROM THE CORE. REPAIRED PER ERA 426746-14.SDR 03FDEA01923Skin · corrodedHORIZONTAL STAB RIGHT UPPER FWD PLANK NR 6R BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS.SDR CALA0300630Skin · crackedINSPECTION FOUND A 1 INCH CRACK AND A 1.25 INCH CRACK IN LT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN BETWEEN STAB STA 147 AND 157. THE SKIN WAS REPAIRED IAW ECRA 5510-01699.SDR CALA0300618Skin · gougedINSPECTION FOUND RT HORIZONTAL STABILIZER LOWER SKIN GOUGED AT STAB STA 111. THE GOUGED AREA OF SKIN WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 55-10-01, FIGURE 207.SDR CA031027002Panel · missing(CAN) RT HORIZONTAL STABILIZER LOWER TRAILING EDGE ACCESS PANELS AFT SUPPORT BEAMS MISSING 7 HORIZONTAL ATTACH BOLTS BASED ON THE CONDITION OF THE AREA IN WHICH THE DISCREPANCIES WERE FOUND AND THEFACT THAT THE ACFT WAS ON A M01 CHECK INDICATES THAT THE ACFT WSDR UPS03841473Doubler · crackedINSPECTION TYPE:C2 REPAIR DOUBLER IS CRACKED AT LT HORIZONTAL STAB L/E AT XFS 60. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 55-2-0 FIG 22.SDR 04FDEA01656Skin Panel · crackedHORIZONTAL STABILIZER CONSTANT SECTION AND OUTBOARD SKIN PANELS CRACKED. P/N ALC7442-1, ALC7206-1, ALC7208-1. PANELS REPLACEMENT/REPAIR PER SB 55-16 IAW FEDEX EA 8-5510-72225.
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