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.

SDR DHL2005781545Skin · corrodedDURING A C-CHECK, VERT STAB FIN STA 204 RT SIDE UPPER RUDDER SKIN FWD HAS SURFACE CORROSION. REMOVED CORROSION FOUND TO BE BEYOND LIMITS, REMOVED EXISTING RIVETS, CUT OUT DAMAGED AREA DIM 3.5 X 2.25 INCH, FABRICATED REPAIR DOUBLER FROM 2024 T3 .032 PO 9001634Feb 15, 2005 · N781DH · Boeing 727227SDR USAA050316Skin · delaminatedPIT - FOUND EXT COMPOSITE SURFACE DELAMINATED 4 INCHES LONG BY .0625 INCHE WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 38 INCHES FROM BOTTOM, 13.5 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17 AND EA 7Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050315Skin Panel · delaminatedPIT - FOUND COMPOSITE SKIN PANEL DELAMINATED .5 INCH BY .0625 INCH SINGLE LAYER DAMAGE, LT SIDE RUDDER 57 INCHES FROM BOTTOM, 34 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17 AND EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050317Skin · delaminatedFOUND EXT COMPOSITE SURF DELAMINATED .5 INCH LONG BY .0625 INCH WIDE SINGLE LAYER DAMAGE, RUDDER LEFT SIDE 66 INCHES FROM BOTTOM, 14 INCHES FROM T/E. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050320Skin · delaminatedPIT - FOUND EXT COMPOSITE SURF WITH 1 INCH SINGLE LAYER DAMAGE DELAMINATION, RUDDER RT SIDE 41 INCHES FROM BOTTOM, 8 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050321Skin · delaminatedPIT - FOUND EXIT COMPOSITE SURF, 2 INCHES LONG BY .125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT SIDE 57 INCH FROM BOTTOM, 10 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED, REFINISHED PER SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050322Skin · delaminatedPIT - FOUND EXT COMPOSITE SURF 4 INCH LONG BY .125 INCH SINGLE LAYER DAMAGE, RUDDER RT SIDE 64 INCHES FROM BOTTOM 34 INCHES FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050323Skin · delaminatedPIT - FOUND EXT COMPOSITE SURF WITH DELAMINATION 5 INCHES LONG BY .125 INCH WIDE SINGLE LAYER DAMAGE, RUDDER RT IDE 114 INCH FROM BOTTOM 7 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050318Skin Panel · delaminatedPIT - FOUND COMPOSITE SKIN PANEL DELAMINATED .1875 INCH DIAMETER SINGER LAYER DAMAGE, RUDDER LT SIDE 70 INCHES FROM BOTTOM, 9 INCHES FROM T/E. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR USAA050319Skin Panel · delaminatedPIT - FOUND COMPOSITE SKIN PANEL WITH DELAMINATION 3 INCH BY .0625 INCH SINGLE LAYER DAMAGE, 165 INCHES FROM BOTTOM, 13 INCHES FROM T/E RUDDER LT SIDE. INSTALLED REPAIR PLYS PER SRM 51-70-17, EA 79999. (M)Feb 11, 2005 · N520AU · Boeing 7373B7SDR CA050222001Skin · cracked(CAN) DURING AN INSPECTION OF THE EMPENNAGE OF DASH 8-311 THE RUDDERS WERE MANUALLY MOVED FROM SIDE TO SIDE. WHEN IT WAS PUSHED FULL RT, TRAVEL A LARGE CRACK APPROXIMATELY TWO INCHES LONG WAS EXPOSED. THIS CRACK BEGAN AT THE LOWER EDGE OF THE L/E SKIN AND COFeb 11, 2005 · Dhav DHC8311SDR ASAA0580090Skin · delaminatedOKC - DURING C-CHECK, FOUND RUDDER T/E IS DELAMINATED. FIBERGLASS BOND REPAIRED. (M)Feb 7, 2005 · N960AS · Doug DC983SDR A6WA200540041Skin · dentedSKIN IS DENTED ON THE LT SIDE SKIN PANEL BETWEEN RS 108.25 AND 113.98 THE DENT MEASURES 2.2 INCHES LONG X 2 INCHES WIDE. PERFORMED A MAJOR REPAIR TO THE RUDDER SKIN ON LT SIDE BY TRIMMING OUT DAMAGE, LPI, FABED DOUBLER AND INSTALLED IAW EO. (K)Feb 2, 2005 · N414ZW · Cndair CL6002B19SDR 05FDEA00094Skin · damagedSHARP CREASE ON LOWER RUDDER, LEFT HAND SIDE TOWARDS THE BOTTOM. REPLACED LOWER RUDDER PER MM 27-20-001.Jan 14, 2005 · N235FE · Boeing 727200SDR SWAA050086Skin · corrodedDURING SCHEDULED 1/2D CHECK, FOUND TOP RT SIDE OF RUDDER CORRODED. REMOVED AND REPLACED RUDDER PER MM.Jan 13, 2005 · N345SA · Boeing 7373K2SDR USAA041049Skin · damagedPIT - Q1 - RUDDER SKIN, .1250 INCH X .2500 INCH AREA, DAMAGE, LT SIDE 5.5 INCH FWD OF T/E 62.5 INCH UP FROM BOTTOM. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA.Jan 9, 2005 · N435US · Boeing 7374B7SDR USAA041061Skin · gougedPIT - Q5 - SKIN SURFACE, 5 INCH LONG GOUGE, RUDDER LT SIDE STA 186, NEAR T/E. INSTALLED REPAIR PLYS IAW SRM.Nov 23, 2004 · N516AU · Boeing 7373B7SDR USAA041056Skin · damagedPIT - Q5 - SKIN SURFACE, SEVERAL AREAS OF 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7SDR USAA041055Skin · chafedPIT - Q5 - SKIN SURFACE, 1.5 INCH LONG, TAPERING DEPTH, DEEP CHAFE WEAR, RUDDER LOWER RT L/E CORNER. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7SDR USAA041054Skin · damagedPIT - Q5 - SKIN SURFACE, 3 INCH LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178 AND 13 INCHES FROM FWD SPAR. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7SDR USAA041053Skin · chafedPIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7SDR USAA041052Skin · chafedPIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA.Nov 23, 2004 · N516AU · Boeing 7373B7SDR USAA041059Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, 1 INCH X .2500 INCH AREA, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE STA 0 L/E. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7SDR USAA041058Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, 3 INCHES LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178, 13 INCHES FROM FWD SPAR. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7SDR USAA041057Skin · damagedPIT - Q5 - TOP COMPOSITE LAYER, SEVERAL AREAS 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N516AU · Boeing 7373B7SDR DHL2004873506Doubler · crackedRUDDER ACCESS DOOR NR 61A DOUBLER CRACKED 0.500. REMOVED CRACKED DOUBLER IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (AL2024-T3 0.032) IAW DC8 SRM 55-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED NEW DOUBLER IAWNov 10, 2004 · N873SJ · Doug DC873FSDR USAA040938Skin · damagedPIT - Q1- SKIN, 2 INCH BY 2 INCH AREA, CARBON FIBER DAMAGE, 120.5 INCH UP FROM BOTTOM, 6.25 INCH FORWARD OF T/E. FILLED AND INSTALLED REPAIR PLIES IAW 51-70-17 AND EA 79467.Nov 10, 2004 · N435US · Boeing 7374B7SDR USAA040936Skin · wornPIT - Q1 - SKIN, 1 INCH BY 1.5 INCHES WEAR, KNIFE EDGE WEAR, 1 INCH AFT OF FWD CORNER AT RUDDER STA. INSTALLED REPAIR PLIES IAW EA 79467, SRM 51-70-17.Nov 10, 2004 · N435US · Boeing 7374B7SDR USAA041051Skin · corrodedPIT - Q1 -RUDDER TOP LAYER, .1250 INCH X .1250 INCH X .005 INCH DEEP PIT, 8.25 INCH FWD OF T/E, 72 INCHES DOWN FROM TIP. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041050Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .3750 INCH X .1875 INCH AREA, DELAMINATION, 3 INCH AFT OF NR 6 HINGE CUTOUT. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041048Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION, 32 INCHES FWD OF T/E, 54.5 INCH UP FROM BOTTOM LT SIDE. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTILAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041047Skin · damagedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DAMAGE, 37 INCH FWD OF T/E, 48 INCH UP FROM BOTTOM. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI-LAYERED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041046Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 1 INCH AREA DAMAGE, RUDDER LT SIDE 95.5 INCHES FROM BOTTOM AND 20 INCHES FWD OF T/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYER REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041045Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA, SINGLE LAYER DAMAGE. RUDDER LT SIDE 105./5 INCHES FROM BOTTOM AND .3750 FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI PLY REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041044Skin · damagedPIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA OF DAMAGE, RUDDER LT SIDE 98.5 INCH FROM BOTTOM AND 9.25 INCHES FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR USAA041041Skin · delaminatedPIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION 28 INCH FWD OF T/E, 39 INCH UP FROM BOTTOM. PREPARED DAMAGED AIR, INSTALLED REPAIR IAW SRM AND EA.Nov 9, 2004 · N435US · Boeing 7374B7SDR DHL2004873513Structure · crackedRUDDER RIGHT L/E CRACKED 3.000M ZR 172.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (ALCLAD 2024-T3 0.040) IAW SRM 55-6-1 PG 2 FIG 1. CLEANED, TREATEDNov 8, 2004 · N873SJ · Doug DC873FSDR DHL2004873514Skin · corrodedRUDDER LT SIDE SKIN CORRODED BETWEEN ZR 253.000 AND ZR 271.000 NEXT FRONT SPAR (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-RROU7 FAA FORM 8110-3 DATED 10-26-04. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0Nov 8, 2004 · N873SJ · Doug DC873FSDR DHL2004873515Skin · crackedRT RUDDER SKIN CRACKED 0.250, STA ZR 161.000 (HOIST POINT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU. REMOVED CRACKED SKIN IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU, SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-T3Nov 4, 2004 · N873SJ · Doug DC873FSDR DHL2004801547Skin · damagedRUDDER RT SKIN DEFLECTED, ZR 150.000 TO ZR 178.719 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-OG7Z1, 1-OD780, SEMAN DRAWING NR 3714. REMOVED DAMAGED PLATING IAW DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024-T3 0.032) IAW BOEING MESSAGESep 14, 2004 · N801DH · Doug DC873FSDR USAA040702Structure · wornRUDDER, 1 INCH LENGTH, WEAR WITH KNIFE EDGING, LOWER TR EDGE. SCALED DAMAGE IAW EA79025.Sep 10, 2004 · N514AU · Boeing 7373B7SDR USAA040638Skin · chafedPIT - FOUND RUDDER COMPOSITE CHAFED 1 INCH BY .125 INCH, RUDDER LOEWR LEFT EDGE 9.5 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, REINSTALLED HARDWARE AND REFINISHED PER SRM 51-70-17 AND EA 79025. (M)Sep 10, 2004 · N514AU · Boeing 7373B7SDR USAA040662Skin · chafedPIT - FOUND RUDDER WITH CHAFE MARKS .25 INCH BY .20 INCH, STATION 174 AT LEFT LEADING EDGE. REMOVED DAMAGE AND APPLIED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)Sep 10, 2004 · N514AU · Boeing 7373B7SDR USAA040661Skin · damagedPIT - FOUND RUDDER WITH COMPOSITE DAMAGE 4 INCH BY 5 INCH SINGLE LAYER, STATION 170 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)Sep 10, 2004 · N514AU · Boeing 7373B7SDR USAA040660Skin · damagedPIT - FOUND RUDDER WITH COMPOSITE DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, STATION 180 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)Sep 10, 2004 · N514AU · Boeing 7373B7SDR USAA040637Skin · chafedPIT - FOUND RUDDER CHAFED 1 INCH BY .125 INCH, LOWER LT EDGE 9.5 INCH FROM TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17. (M)Aug 31, 2004 · N514AU · Boeing 7373B7SDR USAA040639Skin · crackedPIT - FOUND RUDDER CRACKED WITH DELAMINATION AND PEELING, RUDDER LOWER LEFT LEADING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 31, 2004 · N514AU · Boeing 7373B7SDR USAA040642Skin · wornPIT - FOUND COMPOSITE RUDDER SKIN WITH WEAR AND KNIFE EDGING, RUDDER RIGHT LOWER EDGE. REMOVE DAMAGE, INSTALLED REPAIR PLYS, SEAL AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 26, 2004 · N514AU · Boeing 7373B7SDR USAA040641Skin · damagedPIT - FOUND RUDDER COMPOSITE SKIN DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, RUDDER RIGHT SIDE AT FS 180 10 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 26, 2004 · N514AU · Boeing 7373B7SDR USAA040640Skin · chafedPIT - FOUND RUDDER COMPOSITE SKIN CHAFED .25 INCH BY .125 INCH SINGLE LAYER CHAFE MARKS, RUDDER LEFT LEADING EDGE AT STATION 174. REMOVED DAMAGE, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 25, 2004 · N514AU · Boeing 7373B7
Back to JASC 5542