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 IXXA06SMN007SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT RUDDER EXTERNAL SKIN CORRODED, STA ZR 319.063. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 55-2-0 PAGE 12. REMOVED CORRODED PANEJan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN026SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT RUDDER EXTERNAL SKIN CORRODED, STA ZR 276.531. PERFORMED MAJOR REPAIR. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 55-2-0 PAGE 12. REMOVED CORRODED PANEL PLATING IAW DC-8 SRM 55-Jan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN006SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT RUDDER EXTERNAL SKIN CORRODED, STA ZR 110.750. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1. REMOVED CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57-2-0 PAGE 12. REMOVED CORRODED PANEJan 5, 2006 · N722CX · Doug DC872SDR IXXA05SMN319SRepair · corrodedDURING ROUTINE C-CHECK INSPECTION, RIGHT RUDDER REPAIR DOUBLER EDGES CORRODED, STA ZR 61.156. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG 1, EO SEMAN 20051480 DATED 12-20-05. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW SEMANDec 29, 2005 · N722CX · Doug DC872SDR USAA051463Skin · damagedLEFT RUDDER SKIN 4 FEET FROM THE BOTTOM. MAJOR REPAIR, REMOVED DAMAGED, LAYED UP AND CURED REPAIR PLYS IAW SRM 51-70-17, DEFECT SIZE: 2 X 12 INCHES.Dec 5, 2005 · N591US · Boeing 737301SDR AWXA200501600Skin · debondedMCN - DURING C20 CHECK DISCOVERED FIBER DAMAGE ON THE LT SIDE OF RUDDER 18" FROM THE TRAILING EDGE. MAINTENANCE REMOVED DAMAGED PLIES IAW BOEING 737-300 SRM 51-70-04-0G R1 FIG 10. BONDED REPAIR PLIES TO REPAIR AREA ON THE LT SIDE OF RUDDER IAW BOEING 737-300Nov 26, 2005 · N316AW · Boeing 7373S3SDR DHL2005803509Skin · corrodedITEM REF NR 033464: RUDDER SKIN DELAMINATED AT STA ZR 166.656 AND LEVEL 2 CORROSION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG. 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0, SRM 51-1-21. REMOVED CORROSION FROM RUDDER SKIN AT ZR 166.656 IAW SRNov 17, 2005 · N803DH · Doug DC873SDR USAA051339Skin · damagedLEFT RUDDER SKIN 96 INCHES FROM THE BASE AND 11 INCHES FROM THE TRAILING EDGE DAMAGED. REMOVED DAMAGED, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 1.5 INCH.Nov 7, 2005 · N525AU · Boeing 7373B7SDR USAA051340Skin · delaminatedLEFT RUDDER SKIN 99 INCHES FROM THE BASE AND 19 INCHES IN FROM THE TRAILING EDGE DELAMINATED. REMOVED DAMAGE, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 6 INCHES.Nov 7, 2005 · N525AU · Boeing 7373B7SDR USAA051317Skin · damagedRUDDER SKIN LT SISE STATION 233.9. DOUBLER INSTALLED ON LT UPPER SIDE OF RUDDER IAW SRM 51-60-05, DEFECT SIZE: 7 INCHES X 1INCH.Nov 2, 2005 · N779AU · Boeing 7374B7SDR IXXA05SMN264SSkin · unbondedDURING ROUTINE C CHECK INSPECTION, LT RUDDER TAB SKIN UNBONDED 2 AT STA ZRT 98. REMOVED DAMAGED SKIN, CORE SECTION IAW DC8 SRM 55-2-2 PART 2 PAGE 1. FAB`D REPAIR CORE PLUG (AL. HONEY COMB CORE), REPAIR DOUBLER (ALCLAD 2024 T3 0.012) IAW DC8 SRM 55-2-2 PAR 2 POct 20, 2005 · N829BX · Doug DC871FSDR AWXA200501299Skin · crackedMCN - DURING C16 DISCOVERED RT SIDE OF RUDDER CRACKED, 1.5 INCHES IN LENGTH, FROM RUDDER STA 928 TO RUDDER STA 930. MAINTENANCE REMOVED CRACKED SKIN FROM RT SIDE OF RUDDER IAW BOEING 737-300 SRM 51-70-17-0G REPAIR 1 FIG 11. BONDED REPAIR PLIES TO RT SIDE OF Oct 11, 2005 · N306AW · Boeing 7373G7SDR UPS05845780Skin · damagedINSPECTION TYPE:C2 RUDDER RIGHT SIDE HAS 18EA CREASES JUST ABOVE UPS LOGO 2ND HINGE POINT FROM TOP. REMOVED AND REPLACED SKIN ON RUDDER STA ZR53-ZR71 IAW SRM 55-02-00 FIG 6 AND SRM 51-1-21.Oct 1, 2005 · N866UP · Doug DC873FSDR IXXA05SMN191SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, VERT STAB DELAMINATED SKIN ON RUDDER TAB. REMOVED DAMAGED SECTION PLUS FABRICATED DOUBLER (AL2024T3 0.012) IAW SRM 55-2-2 PARA 2. BONDED CORE PLUS DOUBLER WITH HYSOL IAW SRM 51-1-9. REFER TO NR 2801 FOR WEIGHT.Sep 22, 2005 · N829BX · Doug DC871FSDR IXXA05RNG105SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON LT RUDDER STA´S ZR 335.250, ZR 327 - 319, ZR 310.688, ZR 300 - 290. SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5655077 VIEW A-B&C AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 10, 2005 · N721CX · Doug DC872SDR USAA051051Skin · delaminatedRUDDER LT SIDE MID SECTION AREA HAS DELAMINATION. COMPOSITE REPAIR IAW SRM 51-70-05, DEFECT SIZE: 2 INCHES.Aug 24, 2005 · N449US · Boeing 7374B7SDR ASAA0540431Skin · damagedRUDDER SKIN DAMAGED AT 3 LOCATIONS. LWR LT SIDE AT BOTTOM CORNER EDGE 1 INCH, 2 INCH, AND 7 INCH AFT OF L/E. REPAIRED DAMAGE IAW EA. (K)Aug 23, 2005 · N771AS · Boeing 7374Q8SDR LR7A05106Fairing · lightning strikeDURING SCHEDULED B2 INSPECTION PER JOB CARD HB2703 FOUND EVIDENCE OF LIGHTNING STRIKE AT RUDDER FAIRING TIP, FS 1128, VSS 277. REPAIRED IAW LAC MEA 382-53-05-062.Aug 13, 2005 · N404LC · Lkheed 382GSDR SIMA200523404Skin · crackedFOUND DURING MBV, RUDDER NR 2 SKIN CRACKED ON RIGHT LOWER TRAILING EDGE. REPAIRED DAMAGED SKIN ON RUDDER NR 2 IAW IC2005-145/4198A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 12, 2005 · N715AE · Emb EMB135LRSDR AWXA200500824Skin · delaminatedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED FIBER DAMAGE ON LT SIDE OF RUDDER SKIN PANEL AT RUDDER STA 103. MAINTENANCE CUT OUT DAMAGED PLIES ON THE LT SIDE OF THE RUDDER AT STA 103 IAW BOEING 737-300 SRM 51-70-04-0 FIG 10. SANDED, CLEANED AND PREPPED AJul 1, 2005 · N155AW · Boeing 7373G7SDR TXH2005F00000Skin · crackedDEFECT WAS NOTED DURING INSPECTION OF HORIZONTAL AND VERTICAL STABILIZERS. SKIN AND RIB, TOP SIDE OF RUDDER BALANCE WEIGHT ATTACHMENT AND STRUCTURAL AREA CRACKED AND CORRODED. (WP13200509006) (K)Jun 19, 2005 · N827BE · Stbros SD360SDR UPS05844772Skin · damagedINSPECTION TYPE:C-2. UPPER PORTION OF RUDDER ON RT SIDE JUST ABOVE LOGO, OIL CANNING OF SKIN. REMOVED AND REPLACED SKIN ON RT SIDE OF RUDDER JUST ABOVE LOGO IAW DC8 DWG 5655077 AND SRM 51-1-8, AND 51-1-21A. NO WEIGHT AND BALANCE DUE TO 1FOR 1 SKIN CHANGE.Jun 7, 2005 · N705UP · Doug DC871FSDR 2005FA0000887Skin · crackedREPAIRED SKIN ON RUDDER LEADING EDGE AT THE NR 2 RUDDER HINGE POINT. (K)Jun 7, 2005 · N117MS · Gulstm G1159SDR A6WA200540192Skin · dentedRUDDER RT SKIN DENTED 2.0 INCHES ABOVE RIB STATION 72.75 AND 14.3750 FORWARD OF TRAILING EDGE. DENT IS 2 INCHES LONG X 1.5 INCHES WIDE AND .020 INCH DEEP. REPAIRED RUDDER RT SKIN IAW EO. (K)Jun 5, 2005 · N418AW · Cndair CL6002B19SDR DHL2005741539Skin · chafedLWR RUDDER UPPER WEB FASTENERS AND SKIN CHAFED RUDDER STA 152. DAMAGED TO LWR RUDDER UPPER WEB FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-40-1 FIG 1. REMOVED WEB ON LWR RUDDER UPPER WEB IAW B727 SRM 51-30-2. FABRICATED WEB FROM 2024 T3 .040 SIZE 14.500 X 14.May 19, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741586Skin · dentedUPPER RUDDER T/E DENTED 3 IN. ABOVE NR 6 TAB HINGE RT SIDE. CUT OUT DAMAGED AREA 2EA PLACES IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTApr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741585Skin · dentedUPPER RUDDER T/E DENTED 4 INCHES ABOVE 4 TAB HINGE RT. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR DOApr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741584Skin · dentedUPPER RUDDER T/E DENTED 4 INCH ABOVE NR 3 TAB HINGE RT SIDE. CUT-OUT DAMAGED AREA UPPER RUDDER T/E ABOVE NR 3 HINGE IAW B727 SRM 55-40-2 FIG 1 AND SRM 51-40-2 FIG 1. FABRICATED REPAIR " IAW B727 SRM 55-40-2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART ANDApr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741583Skin · dentedUPPER RUDDER T/E DENTED 2 IN. BELOW NR 3 TAB HINGE RT SIDE. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG . TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIRApr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741582Skin · dentedUPPER RUDDER T/E DENTED AT NR 6 TAB HINGE LT SIDE MARKED. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIRApr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741581Skin · dentedUPPER RUDDER T/E DENTED 3 INCH ABOVE NR 5 TAB HINGE LT SIDE MARKED. CUT OUT DAMAGED AREA 2 EA PLACES IAW B727 SRM 51-01-2 FIG 1. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-40-2 FIG 2 AND SRM 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10Apr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741580Skin · dentedUPPER RUDDER T/E DENTED 2 IN. ABOVE NR 1 HINGE TAB 4H SIDE MARKED. CUT-OUT DAMAGED AREA 2EA PLACES DIM .75 BY .75 AND .5 BY .5 AT UPPER RUDDER LT L/E IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR FROM 2024T3 .032 PO9001634 DIM 10 BY 5.5 IN IAW B727 SRM 55-4Apr 29, 2005 · N741DH · Boeing 7272Q9SDR DHL2005807506Skin · damagedRIGHT RUDDER EXTERNAL SKIN INTERIM REPAIR (STA ZR 253.000 - 265.218). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 PG 2. REMOVED PLATING SEGMENT WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING SEGMENT AND FINGER DOUBLER (AL2Apr 20, 2005 · N807DH · Doug DC873FSDR DHL2005741554Skin · dentedUPPER RUDDER RT SIDE PANEL 9801 DENTED IN SEVERAL PLACES. CUT OUT DAMAGED AREAS DIM .25 INCH AND .375 INCH ON UPPER RUDDER RT SIDE PANEL 9801 IAW B727 SRM 51-10-1. FABRICATED 2 EA DOUBLER FROM 2024-T3 .032 SIZE 2.5 X 2.5 AND 2.5 X 2.5 PO 9001634 IAW B727 SRMApr 18, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741545Panel · dentedRUDDER STA 0.00 RT TRAPEZOIDAL PANEL HAS 10 DENTS. MEASURED 10 EA DENTS ON RT TRAPEZOIDAL PANEL. A/Y RATIO OF 9 DENTS WITH-IN LIMITS. A/Y RATIO OF 1 DENT OUT-OF-LIMITS. CLEANED, PREPPED, APPLIED POTTING COMPOUND TO DENT, CURED AND SANDED SMOOTH. FABRICATEApr 13, 2005 · N741DH · Boeing 7272Q9SDR ASAA0540208Skin · delaminatedRUDDER IS DAMAGED AT LT SIDE LOWER EDGE. COMPLIED WITH A BOND REPAIR IAW SRM. (K)Apr 6, 2005 · N795AS · Boeing 737490SDR ASAA0540207Skin · puncturedBOTTOM OF RUDDER IS PUNCTURED. COMPLIED WITH A BOND REPAIR IAW SRM. (K)Apr 6, 2005 · N795AS · Boeing 737490SDR DHL2005783504Skin · dentedDENT ON RT UPPER RUDDER FS 1540 MARKED. CUT OUT DAMAGE AREA 0.750 INCH DIA IAW B727 SRM 55-20-3 FIG 1. FAB'D DOUBLER REPAIR FROM MAT 2024-T3 .032 PO NR 9002034 DIM 5 INCH BY 3 1/4 INCH IAW B727 SRM 55-20-3 FIG 1. ALODINED AND PRIMED DOUBLER REPAIR IAW B727 Apr 5, 2005 · N783DH · Boeing 727227SDR DHL2005783501Skin · dentedLWR LT RUDDER DENTED MARKED. CUT OUT DAMAGE AREA 3/4 INCH DIA IAW B727 SRM 55-20-3 FIG 1. FAB'D DOUBLER REPAIR FROM MAT 2024-T3 .032 PO NR 9022034 DIM 5 INCH BY 3 INCH IAW B727 SRM 55-20-3 FIG 1. ALODINE AND PRIMED DOUBLER REPAIR IAW B727 SRM 51-10-2 AND INApr 5, 2005 · N783DH · Boeing 727227SDR AWXA200500486Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE RIGHT TOP AFT SECTION OF RUDDER DELAMINATED AT RUDDER STA 238. MAINTENANCE REMOVED DELAMINATED SECTION OF RT TOP AFT RUDDER CONDUCTIVE FRAME; FABRICATED A NEW REPLACEMENT SECTION OF CONDUCTIVE FRAME PER DWG 65CApr 4, 2005 · N174AW · Boeing 73733ASDR USAA050430Skin · damagedCLT - Q6 - RUDDER SKIN, (.5 INCH X .5 INCH) COMPOSITE DAMAGE, RUDDER T/E STA 151. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K)Mar 28, 2005 · N442US · Boeing 7374B7SDR 05FDEA00673Skin · misrepairedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. FLUSH REPAIR LT SIDE RUDDER LOWER T/E. ITEM 36 OF LIST. FLUSH REPAIR IS FOUND TO BE NOT CONFORM WITH A310-200 SRM 55-41-0. REMOVED IMPROPER REPAIR AND INSTALL PROPER REPAIR IAMar 28, 2005 · N419FE · Airbus A310222SDR DHL2005740563Skin · dentedVERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF IS DENTED NEAR T/E. EVAULATED DENTED AREA AT VERT STAB ABOVE RT FIN STA 133 LOWER RUDDER SURF. TRIM OUT DAMAGED SKIN SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3 AND 51-10-1. FABRICATED DOUBLER REPAIR SIZE 2" BY 2.Mar 27, 2005 · N740DH · Boeing 7272Q9SDR DHL2005740561Skin · dentedVERT STAB BELOW FIN STA 133 RT LOWER RUDDER SURF IS DENTED NEAR T/E CORRECTIVE ACTION: EVALUATED DENTED AREA AT VERT STAB FIN STA 133 RT LOWER RUDDER SURF IAW B727 SRM 55-40-1 FOUND OUT OF LIMITS TRIM OUT DAMAGED AREA. SIZE 1/2" BY 3/4" IAW B727 SRM 55-30-3- AMar 27, 2005 · N740DH · Boeing 7272Q9SDR QXEA200500533Skin · damagedPDX - CREASE IN FORE RUDDER, RIGHTHAND SIDE, JUST ABOVE THE 4TH RIB FROM THE TOP. REPAIRED IAW RD 8/4-55-001 AND HORIZON AIR EA 6-55-111.Mar 25, 2005 · N416QX · Bombdr DHC8401SDR QXEA200500507Panel · chafedPDX - RUDDER TOP HINGE PANEL HAS .5 INCH LONG HORIZONTAL CHAFE MARK AT UPPER FORWARD END. REPAIRED IAW HORIZON AIR EA R-55-42 AND REO 670-55-41-005.Mar 23, 2005 · N613QX · Cndair CL6002C10SDR 05FDEA00466Panel · corrodedCORROSION AROUND FASTERNER HOLES, LEFT AND RIGHT SIDE TOP OF RUDDER, PANEL 326AT REMOVED TO REPAIR STATIC WICK BASE N00238.Mar 9, 2005 · N419FE · Airbus A310SDR SIMA200505604Skin · gougedABI - GOUGES IN RUDDER NR 1 LEADING EDGE SKIN. REMOVED DAMAGED AREA BY PERFORMING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW EMB145 SRM, SRM 145/1142 REV 28, 51-40-02 AND EMB REPAIR STATEMENT IC2005-145/0912. (M)Feb 22, 2005 · N703MR · Emb EMB135LRSDR DHL2005781565Skin · damagedDURING A C-CHECK, ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON UPPER RUDDER RT SKIN AT STA 156 PER ASTAR J/C FCD500001-010-B. DISCONNECTED UPPER RUDDER ACTUATOR ROD END THROUGH BOLT FOR S/M ACCESS IAW B727 MM 27-20-14. REMOVED PREVIOUS REPAIR NOT COMPLIANFeb 16, 2005 · N781DH · Boeing 727227SDR DHL2005781547Skin · crackedDURING A C-CHECK, VERT STAB FIN STA 194 LOWER RUDDER LT SIDE UPPER T/E AT END IS CRACKED. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET FROM 2024 T3 .025 PO 9001310 DIM 3.5 X 3.5 INCH. TREATED, PRIMED AND INSTALLED BRACKET IAW B727 SRM 51-30-2, 55-30-2 FIFeb 16, 2005 · N781DH · Boeing 727227
Back to JASC 5542