JASC 5542
Service difficulty reports · 1,373
Reports filed under 5542 · Rudder, 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 = '5542' 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 = '5542' 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 AALA20110217TUL01Skin · damagedRUDDER SKIN AND SPAR DAMAGED AT STATION 530. REPAIRED PER EA COMP-55-015323 DATED 16-FEB-11.SDR FDEA201101310424Skin · damaged.5" X .5" SHALLOW PUNCTURE ON RUDDER LT OUTER SKIN ABOUT 22" AFT OF THE NR 4 ATTACH FITTING. REPAIRED RUDDER L/T OUTER SKIN ABOUT 22" AFT OF THE NR4 ATTACH FITTING IAW SRM 55-41-12 PARA 30 WET LAYUP REPAIR. NO CORE DAMAGE EXIST AT 22" AFT OF NR4 ATTACH FITTISDR DHLA201100030Skin · damagedRUDDER RT SKIN BROKEN STA ZR 217.188. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING + BONDED FINGER DOUBLER BOTH FROM AL2024T3 0.016 " IAW SRM 55-6-1 FIG 1, ITEM "A". BONDED BOSDR DHLA201100016Skin · misrepairedREMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING & BONDED FINGER DOUBLER IAW SRM 55-6-1 FIG. 1 ITEM "A". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9 TR 51-142, SRM 51-1-9A, TR 51-141, DPS 1.950 REV "AR" R-1. CLEANED, TREATSDR SIMA201101106Skin · damagedDURING MAINTENANCE BASE VISIT INSPECTION FOUND RUDDER NR 2 HAS A SMALL HOLE THROUGH THE RIGHT AND LEFT SKIN 10 MILLIMETERS ABOVE THE THIRD RIB FROM THE TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED REPAIR DOUBLER ON THE LEFT AND RIGHT SIDES OF RUDDERSDR EE4Y20110001Panel · delaminatedVERTICAL STABILIZER, RUDDER PN: D5547100300000, SN: TS-3706, LT AND RT SIDE PANEL WITH FLUID INDICATION (WATER INGRESS) IAW THERMOGRAPHY INSP AROUND HOISTING POINTS . LT SIDE PANEL FLUID INDICATION COMMON TO HOISTING POINT NR 1 & 3 AND RT SIDE PANEL FLUID INDISDR WX0A070700Skin · damagedRUDDER LOWER RT AREA OF HINGE CUT OUT SMALL AREA OF EDGE DAMAGE. REPAIRED COMPOSITE DEFECTS IAW SRM 51-70-1A.SDR USAA2010120392795Skin · delaminatedPIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - RUDDER FAILED VACUUM LOSS TEST FOR LARGE AREA DISBOND INSPECTION IAW ENGINEERING ORDER 5510Y009. REPLACED RUDDER IAW A319 AMM 27-21-41-04.SDR HNAA2010120300268Skin · puncturedSMALLHOLE ON RT SIDE OF TRAIL RUDDER, JUST ABOVE FUSELAGE. EVALUATED AND MAPPED DAMAGE. PERFORMED STEPS 1 THROUGH 5 OF WORKCARD 05-01-26I. REPAIRED IAW SRM55-40-28, SKIN SPLICE (EO8-55-10-0715) COMPLETED STEPS 6 THROUGH 9 ON WC 05-01-26I.SDR DALA1035429853Skin · crackedDURING M-CHECK FOUND VERTICAL STAB, TOP AFT T/E OF RUDDER IS CRACKED, RUDDER ASSY OFF 09-5541-9-9003. UPON EVALUATION VERT STAB TOP AFT T/E OF RUDDER HAS SEPARATION, NO FIBER DAMAGE INJECTED RESIN HYSOL EA 9396 CURED USING HEAT THERMOCOUPLER HT7581 APPLIED WETSDR AALA20101104TUL13Skin · puncturedRUDDER HAS SMALL PUNCTURE IN RIGHT SKIN AT TOP NEAR LEADING EDGE. TRIMMED OUT DAMAGED AREA AND APPLIED A WET LAYUP PERMANENT REPAIR PER SRM 51-70-01A.SDR QXEA2010101400603Skin · damagedC5 CHECK - FORE RUDDER SKIN T/E HAS AN AREAS OF DAMAGE BY THE LOWER HINGE POINT. PERFORMED CLEAN UP OF DAMAGED AREAS IAW SRM 51-14-00 REPAIR-03. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-01-250-801. COMPLIED WITH TC RD 8/4-55-571 FOR PERMANENT REPAIRSDR QXEA2010101400602Skin · damagedC5 CHECK - FORE RUDDER SKIN T/E HAS 2 AREAS OF DAMAGE BY THE LOWER HINGE POINT. PERFORMED CLEAN UP FOUND TO BE OUT OF LIMITS IAW SRM 51-14-00 REPAIR-03 PART 5-C-7-C. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-01-250-801. COMPLIED WITH TC RD 8/4-55-571SDR QXEA2010101400601Skin · damagedC5 CHECK - FORE RUDDER SKIN T/E HAS 2 AREAS OF DAMAGE BY THE CTR HINGE POINT. PERFORMED CLEAN UP OF DAMAGED AREAS IAW SRM 51-14-00 REPAIR-03. MATERIAL LOSS ON UPPER AREAS FOUND TO BE WITHIN LIMITS AND LOWER AREAS TO BE OUT OF LIMITS IAW SRM 51-14-00 REPAIR-0SDR QXEA2010101400600Skin · damagedC5 CHECK - FORE RUDDER SKIN T/E HAS 3 AREAS OF DAMAGE BY THE UPPER HINGE POINT. PERFORMED CLEAN UP OF DAMAGED AREAS IAW SRM 51-14-00, REPAIR-03. MATERIAL LOSS LOWER AREA FOUND WITHIN LIMITS AND UPPER AREAS TO BE OUT OF LIMITS IAW SRM 51-14-00 REPAIR-03 PART SDR USAA2010100592207Skin · debondedSAL - S5 - MAJOR REPAIR - AREA OF DEBONDING ON LEFT SIDE OF RUDDER APPROX 3.75 INCHES FROM TRAILING EDGE & 17.5 INCHES DOWN FROM TOP OF RUDDER. REPAIRED LEFT SIDE OF RUDDER IAW EA 133073.SDR QXEA2010100400577Skin · crackedCRACK ON TRAILING RUDDER LT UPPER SIDE (RIB 28) THIRD FROM THE TOP. REPLACED TRAILING RUDDER. CHECK FLIGHT GOOD. RETURNED TO SERVICE.SDR C2XA10SH315Skin · damagedSHV - DURING C-CHECK 2 OBLONG HOLES IN RUDDER II SKIN, LT SIDE, ABOUT 1/2 WAY UP. MAINTENANCE PERFORMED REPAIR TO RUDDER II SKIN, LT SIDE, HALFWAY UP IAW EC5540-01141. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA1024409008Skin · damagedDAMAGED METALLIZED ON LT RUDDER SURFACE MID AREA FWD AND AFT EDGE AND DAMAGED PAINT COAT ON RT SURFACE AT SKIN PANEL. REPAIRED IAW SRM 51-70-01A-D AND ERA 479662-14MA.SDR C2XA10IA255Skin · damagedIAH - FLIGHT 2149, DURING POST FLIGHT INSPECTION THE CREW REPORTED A HOLE IN THE RIGHT LOWER SIDE OF RUDDER II. MAINTENANCE REPLACED THE DAMAGED SECTION OF SKIN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DHLA201000124Skin · misrepairedR & R EXISTING REPAIR ON RT RUDDER PLATING AT ZR 61.156 UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG. 1. REMOVED PLATING AND EXISTING NON STANDARD REPAIR IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 55-6-1 FIG 1 ITEM "SDR DHLA201000102Skin · misrepairedR & R EXISTING REPAIR ON RT RUDDER PLATING AT ZR 61.156 (REF REPAIR REPORT VS002) UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED PLATING AND EXISTING NON STANDARD REPAIR IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING SDR EE4Y1008350Skin · crackedDURING INSPECTION EMPENNAGE VERTICAL STABILIZER RUDDER SKIN WITH CRACK AT ZR27.25 RT.SDR UALA2010081102914Panel · peelingRT SIDE OF RUDDER HAS PANEL PEELING BACK ON FWD CORNER. REMOVED 3" AREA OF CONDUCTIVE FRAME PN 173W3200-12. TAP TESTED AREA AND APPLIED SPEED TAPE OVER EFFECTED AREA WITH 1" OVERLAY. NEED DETAILED VISUAL INSP EVERY A-CK & PERMANENT REPAIR BY NEXT C-CHK REF AMSDR FDEA201008092889Skin · puncturedPUNCTURE IN SKIN LOWER RUDDER LT SIDE, APPROX VERTICAL STABILIZER FIN STA 110. CUT DAMAGED SECTION OF RUDDER SKIN DIM 1" X 1 1/2" IAW SRM 51-10-1 AND 55-20-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 2024T3 .032" DIM 4 3/4 X 4 3/4" IAW SRM 55-20-3 FIG 1 INSTASDR A6WA201040586Skin · chafedRUDDER L/E SKIN IS CHAFED. REPAIRED DAMAGE ON RUDDER L/E SKINS IAW SRM 55-40-00.SDR EE4Y1008276Skin · crackedDURING INSPECTION RUDDER WITH CORROSION SKIN AT LT BETWEEN ZR 94 AND ZR 99.SDR IPXA10660579Skin · delaminatedINSPECTION TYPE:C RUDDER SKIN SIDE UPPER AREA DELAMINATION. GRAPHITE FABRIC PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-04, PAR 5K, REV 47.SDR A6WA201040408Skin · chafedMINOR CHAFING FULL LENGTH OF RUDDER RT SIDE TOWARDS L/T REPAIR CHAFING DAMAGE ON RUDDER RT L/E IAW SRM 55-40-00.SDR 2010FA0000674Skin · corroded(SPUY) RUDDER LT SIDE PLATING CORRODED AT STA ZR 140.000.SDR DHLA201000059Skin · corrodedRT RUDDER SKIN CORRODED STA ZR159.094-168.656. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12 FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 5SDR UALA2010050601530Skin · damagedDURING C2 VISIT, MINOR IMPACT DAMAGE WAS FOUND ON LT SIDE OF THE RUDDER EXTERIOR SKIN 26FT AFT OF THE FRONT SPAR AND 20FT FROM RUDDER LOWER EDGE. MAJOR REPAIR WAS ACP'D PER UA-EVA-73683A ON SMB N-R N6494Q. DAMAGED SKIN AND CORE WERE REMOVED AND REPAIRED. RISDR DALA1011980998Skin · damagedDAMAGED METALLIZED ON RUDDER SKIN REPAIR IAW OPN 1031. (DLM88101401)SDR DLM88100985Skin · damagedDAMAGED METALIZED OF RUDDER LT AND RT SURFACE. LT AND RT METALIZED SURFACE OF RUDDER WAS REPAIRED IAW OPN 1031, CARDS 1370TO 1378.SDR A6WA201040305Skin · chafedRUDDER L/E HAS CHAFING DAMAGE ON LT SIDE ALONG LENGTH OF RUDDER R & R CHAFED L/E IAW SRM 51-42-06.SDR A6WA201040303Skin · chafedRUDDER L/E HAS CHAFE DAMAGE ALONG LENGTH OF RUDDER RT SIDE BLENDED RUDDER L/E BETWEEN 98.75 AND 151.508 AND FOUND TO BE SERVICEABLE IAW SRM 55-40-00. AREA BETWEEN 40.458 AND 81.50. R & R IAW SRM 51-42-06.SDR IXXA10SMN052SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RUDDER LEFT SIDE SKIN CORRODED AT STATION ZR 140.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMESDR UALA2010040901193Skin · damagedFOUND EVIDENCE OF LIGHTNING STRIKE EXIT. T/E AT TOP OF RUDDER TO 48 IN DOWN HAS MULTIPLE DAMAGE STRIKES AND DAMAGED FASTENERS AND FIBER DAMAGE WITH DELAM APPROX 6 IN FWD OF T/E ON LT SIDE UPPER CONDUCTIVE FRAME HAS BURNED AND PULLED FASTENERS AT REAR SPAR ATTSDR ASAA1047590Skin · damagedRUDDER HAS DAMAGE AT AFT LOWER CORNER. REPAIRED SKIN DAMAGE.SDR DALA1011610661Skin · damagedRUDDER T/E 25" BELOW TIP HAS A 2" AREA OF BURN DAMAGE & DELAM. REMOVED DAMAGE AND REPAIRED AT STA AEROSPACE SAT REF NON ROUTINE 159410. (DL757101342).SDR DLM88100499Skin · damagedDURING HMV DAMAGED METALLIZED COAT WAS FOUND ON RT SKIN OF RUDDER DAMAGE WAS REPAIRED IAW SRM51-70-1AD PARA 23.SDR FDEA201002240508Skin · damagedVERTICAL STABILIZER AFT RUDDER LOWER EDGE FWD SKIN FOUND PEELED. REPAIRED IAW EA NR 1-5540-132347. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR ASAA1047519Skin · perforatedRUDDER HAS PERFORATION ON LOWER RT SECTION. REPAIRED SKIN DAMAGE.SDR FDEA201002180446Panel · corrodedRUDDER EXTERIOR SURFACE LT BONDED CONDUCTIVITY FRAME WITH LIGHT SURFACE CORROSION BETWEEN RUDDER STA 381.269 TO STA 578.536. CORROSION REPAIR CARRIED OUT IAW EA NR F-5540-137419. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR USAA2010021590379Skin · delaminatedCLT - MAJOR REPAIR - Q5 CHECK - DELAMINATION ON BOTTOM / FRONT SURFACE OF RUDDER JUST FORWARD OF THE MAIN SEAL. REPLACED RUDDER IAW B737 SRM 51-10-02.SDR USAA2010030890535Skin · crackedSAL - C22 - MAJOR REPAIR - CRACK ON RUDDER EXTERNAL SKIN AT RUDDER STA 63.59 & 6 INCHES AFT OF LEFT LEADING EDGE. REPAIRED RUDDER EXTERNAL SKIN AT RUDDER STA 63.59 & 6 INCHES AFT OF LEFT LEADING EDGE IAW EA 132873.SDR USAA2010030890534Skin · delaminatedSAL - C22 - MAJOR REPAIR - DELAMINATION ON RUDDER AT RUDDER STA 3, 2 INCHES FROM TRAILING EDGE. REPAIRED RUDDER AT RUDDER STA 3, 2 INCHES FROM TRAILING EDGE IAW EA 132873.SDR IPXA10558378Skin · misrepairedINSPECTION TYPE:C1, RUDDER T/E LIGHTING STRIKE DAMAGE JUST ABOVE LOWER STATIC DISCHARGE ON RT SKIN WAS PREVIOUSLY REPAIRED IMPROPERLY AND REQUIRES REACCOMPLISHED (REF. CARD NR 832099). REPAIR ACCOMPLISHED CARD NR 832099 (STRB 5002) SRM 51-70-04.SDR IPXA10558376Skin · delaminatedINSPECTION TYPE:C1, UPON REMOVAL OF RUDDER FOUND DELAMINATED AREA ON THE FWD L/E OF RUDDER AT RUDDER STA. 255. REPAIRED IAW SRM 51-70-17.SDR P5CA1001616Skin · damagedDAMAGE WAS FOUND TO THE RT UPPER RUDDER EXTERNAL SURFACE MID-AREA WITH DENT 1.0 INCHES IN DIAMETER. PERMANENT REPAIR WAS ACCOMPLISHED BY ENGINEERING ORDER 4455A033. THIS EO IS CLASSIFIED AS "MAJOR" AS DEFINED IN FAR 43 APPENDIX A.
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