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 QXEA0202286Skin · corrodedPDX - TRAIL RUDDER HAS PAINT MISSING AND EVIDENCE OF CORROSION UNDER SECOND FROM TOP AND BOTTOM STATIC WICKS. REPAIRED IAW DHC-8 MM 23-60-01-720-001, PAGE 406.Dec 26, 2002 · N367PH · Dhav DHC8202SDR QXEA0202213Skin · crackedPDX- CRACK IN SKIN OF FORE RUDDER ON LOWER FORWARD RIGHT HAND CORNER. REPAIRED IAW DHC-8 SRM 51-40-11.Dec 16, 2002 · N347PH · Dhav DHC8202SDR HNAA0200087Rudder · crackedR/H SKIN OF FORE RUDDER HAS LARGE CRACK AT FIRST AND SECOND RIB BELOW TOP CLOSING RIB. REPLACED RUDDER.Dec 3, 2002 · N969HA · Dhav DHC8201SDR USAA020467Skin · damagedRUDDER SKIN DAMAGE. LEFT SIDE TRIM DAMAGE SRM IAW EA.Nov 27, 2002 · N504AU · Boeing 7373B7SDR UPS02839936Skin · corrodedINSPECTION TYPE: ASV, BULGE LT SIDE RUDDER. RUDDER HAS SKIN BULGE AT APPROX 4 FEET BELOW TIP AND 8 INCHES FROM TRAILING EDGE (BETWEEN LOWER STATIC WICKS) ON LT SIDE OF RUDDER. REMOVED RUDDER IAW MM 27-21-01 P401-P406 INSPCTED VERTICAL STRUCTURE FOR RUDDER SNov 26, 2002 · N852UP · Doug DC873FSDR MWEA020702Rudder · scratchedLOWER LEFT RUDDER SKIN IS SCRATCHED. -- REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER AND RE-BALANCED RUDDER.Nov 18, 2002 · N813ME · Doug DC981SDR DHL2002743516Skin · crackedDURING C CHECK, UPPER RUDDER TAB LE SKIN CLOSE OUT IS CRACKED AND CORRODED. REMOVED UPPER RUDDER TAB FOR ACCESS IAW B-727 M.M. 27-20-11. REMOVED 6 DAMAGED SKINS, LOCATED, AND DRILLED NEW SKINS IAW B-727 SRM 55-40-2. PARTS ALODINED AND PRIMED IAW B-727 SRM Nov 16, 2002 · N743DH · Boeing 727225SDR MWEA020697Rudder · dentedRUDDER LOWER LEADING EDGE PANEL DENTED FROM ZR10-ZR36. -- REPAIRED IAW BOEING TELEX MWX-MKE-02-00190H DATED 9/19/02.Nov 15, 2002 · N813ME · Doug DC981SDR ABXA020328Skin · crackedRUDDER TOP RIGHT SIDE HAD LARGE CRACK. REPLACED RUDDER IAW DC-9 SRM.Nov 8, 2002 · N945AX · Doug DC931SDR C2XA02TY165Skin · dentedDURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND A DENT IN NR 1 RUDDER, RT SIDE BETWEEN RIB 2890.0 AND 2601.0. THE AREA WAS CUT OUT AND A EXTERNAL DOUBLER WAS FABRICATED. DRILLED,ALODINED,PRIMED AND PAINTED AND INSTALL THE DOUBLER. ALL WORK WAS ACCOMPLISHNov 5, 2002 · N13975 · Emb EMB145LRSDR 2003FA0000516Cap · separatedSHORTLY AFTER LEVELING OFF AT A CRUISE ALTITUDE OF 16,000 FT, THE AIRCRAFT MADE A HARD UNCOMMANDED TURN TO THE LEFT AND LOST APPROX 1000 FT ALTITUDE BEFORE THE PILOT WAS ABLE TO REGAIN CONTROL. POST FLIGHT INSPECTION REVEALED THAT THE TOP PORTION OF THE RUDDENov 1, 2002 · N77UA · Gulstm 690BSDR USAA020402Skin · delaminatedPIT - FOUND RUDDER WITH DELAMINATION, STATION 0.00 RT, 1.5 LEFT, 121.0 LEFT, 174.9 RT, 200.0 RT. REPAIRED WITH WET LAYUP USING SRM 51-70-17, 51-60-00 PER EA 75136. (M)Oct 25, 2002 · N395US · Boeing 7373B7SDR USAA020381Skin · delaminatedPIT - RUDDER SKIN DELAMINATED, BOTTOM L/E CORNERS RT AND LT SIDE. REMOVED DAMAGE, REPAIRED AND RESTORED PER EA 75009, AND SRM 51-70-03. (M)Oct 4, 2002 · N588US · Boeing 737301SDR PCAA0210118Rudder · crackedDURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING BONDING INTEGRITY INSPECTION TASK 550001 LEFT FORE RUDDER FOUND CRACKED AT RIB #26. DAMAGED AREA WAS CUT OUT AND REPAIRED IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-55-335. AIRCRAFT RETURNED TO SERVICE.Oct 2, 2002 · N847EX · Dhav DHC8102SDR USAA020364Skin · delaminatedPIT - FOUND RUDDER DELAMINATED, LEFT SIDE, BOTTOM EDGE 19 INCHES AFT OF LEADING EDGE. RESIN AND OVERLAYED WITH TWO PLIES OF GRAPHITE FABRIC PER EA 74841, SRM 55-40-01, 51-70-17. (M)Sep 19, 2002 · N300AU · Boeing 737301SDR UPS02239770Skin · delaminatedLWR RUDDER LEFT SKIN CORRODED AT TS 141.6. CORROSION AND DELAMINATION FOUND ON LOWER RUDDER, LEFT SIDE, UPPER PANEL, AFT UPPER CORNER. REPLACED RUDDER IAW MM 27-20-01.Sep 18, 2002 · N930UP · Boeing 72722CSDR 2002FA0001136Skin · crackedFOUND A 3.5 INCH CRACK APPROXIMATELY 6 INCHES DOWN AND .0200 INCH ON THE RIGHT SIDE TRAILING EDGE OF THE RUDDER.Aug 15, 2002 · N942CE · Beech B200SDR USAA020326Skin · damagedPIT - FOUND RUDDER WITH SKIN DAMAGE, STATION 7.60, 17.70. REPAIRED PER SRM 51-70-17, 55-40-01. (M)Aug 14, 2002 · N529AU · Boeing 7373B7SDR QXEA0201191Skin · chafedPDX-TRAILING RUDDER HAS 2 UPPER STATIC WICKS CHAFING INTO TRAILING EDGE SKIN ON RIGHT HAND SIDE, LOCATED AT 5TH AND 9TH RIB FROM TOP OF RUDDER. REPAIRED IAW DHC8 SRM 51-20-31 AND SRM 51-20-51.Aug 6, 2002 · N362PH · Dhav DHC8202SDR QXEA0201178Skin · chafedPDX-TRAILING RUDDER HAS 2 UPPER STATIC WICKS CHAFING INTO TRAILING EDGE SKIN ON RIGHT HAND SIDE, LOCATED 5TH AND 9TH RIB FROM TOP OF RUDDER. REPAIRED IAW DHC8 SRM 55-40-16, SRM 51-20-11 AND RD8-55-042.Aug 6, 2002 · N362PH · Dhav DHC8202SDR QXEA0201187Skin · crackedPDX-FORE RUDDER RIGHT HAND SIDE SKIN HAS CRACK AT AFT EDGE IN LINE WITH TOP HINGE. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 9, SRM 51-20-36, SRM 51-40-11 AND SRM 51-20-51.Aug 4, 2002 · N362PH · Dhav DHC8202SDR IXXA0200093SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RUDDER TRAILING EDGE ABOVE THE TAB. REPAIR ACCOMPLISHED, REMOVED SURFACE CORROSION IAW THE DOUGLAS SRM.Jul 14, 2002 · N41CX · Doug DC862FSDR USAA020265Skin · damagedPIT - FOUND RUDDER SKIN DAMAGE, LT/RT RUDDER, CRITICAL AREAS AND 6 INCHES OF PANEL EDGE. WET LAY UP REPAIR PER SRM 55-40-01, 51-70-11 AND EA 74270. (M)Jul 10, 2002 · N409US · Boeing 737401SDR USAA020225Skin · delaminatedPIT - FOUND RUDDER DELAMINATED SEVERAL PLACES FROM .25 INCHES TO 6 INCHES, 1 PLY DEEP, RIGHT/LEFT RUDDER, R STATION 121.64 TO 0.00. COMPLETED 200-230 DEGREE WET LAY UP PER SRM 51-70-17 PER EA 74241. (M)Jul 2, 2002 · N393US · Boeing 7373B7SDR C2XA02TY105Skin · nickedTYS, During a scheduled inspection the rudder 2 leading edge on the left side was found nicked. Maintenance blended the affected area, performed dye-pen. inspection, alodined and primed. I/A/W-GST-1886/02 and CPM-51-21-04/05/06. The repair was satisfactory andJun 17, 2002 · N15973 · Emb EMB145SDR USAA020201Skin · damagedPIT - FOUND RUDDER WITH SEVERAL AREAS OF SKIN DAMAGE, STATION 196.46 TO STATION 0.00. WET LAY UP REPAIR PER EA 73884. (M)Jun 5, 2002 · N406US · Boeing 737401SDR MWEA020381Skin · damagedLEFT SIDE OF RUDDER 5 INCHES AFT OF FORWARD SPAR BETWEEN ZR 117 AND ZR 113 HAS CREASE 2.5 INCHES LONG. FABRICATED AND INSTALLED REPAIR DOUBLER.May 24, 2002 · N501ME · Doug DC932SDR USAA020190Skin · delaminatedPIT - FOUND RUDDER DELAMINATED .5 INCH BY .5 INCH, LEFT AND RIGHT WITHIN 6 INCHES OF PANEL EDGE FOR FASTENER LINE. WET LAYUP REPAIR PER SRM 51-70-11 AND 51-70-17, EA 74066. (M)May 23, 2002 · N785AU · Boeing 7374B7SDR USAA020186Skin · damagedPIT - FOUND RUDDER WITH SKIN DAMAGE, 6 INCHES WIDE BY 105 INCHES LONG, AND 5.5 INCHES WIDE BY 40 INCHES LONG, BOTH SIDES OF RUDDER. WET LAY UP REPAIR PER SRM 51-70-17 FIG 18 AND 51-70-11 AND EA 73999. (M)May 10, 2002 · N446US · Boeing 7374B7SDR 2002F00615Skin · chafedAT C-CHECK, FOUND VERTICAL STAB LOWER RUDDER LEADING EDGE SKIN CHAFED AT STATION 150. (M)May 10, 2002 · N8878Z · Boeing 727225SDR SIMAW00212302Skin · crackedSAW - RUDDER HAS AN APPROX 4 INCH CRACK ON LEFT SIDE AND APPROX 1.5 INCH CRACK ON RIGHT SIDE WHERE BALANCE ARM FOR RUDDER TAB PASSES THROUGH IT. RUDDER REPAIRED IAW EO E1-55MR-012. (M)May 1, 2002 · N135MQ · Aerosp ATR42300SDR USAA020171Skin · corrodedPIT - FOUND RIB AND SKIN WITH HEAVY CORROSION 4 INCHES LONG BY 1 INCH WIDE, RUDDER COUNTER BALANCE STRUCTURE, RUDDER STATION 121.64. LEVEL 2 CORROSION. (M)Apr 24, 2002 · N394US · Boeing 7373B7SDR USAA020150Skin · wornPIT - FOUND LEADING EDGE RUDDER WORN, 1 INCH BY .25 INCH, 3 LAYERS DEEP, LE L00 SIDE, 95 INCHES FROM TOP RUDDER AND 29 INCHES FROM TRAILING EDGE. REPAIR PER EA 73763. (M)Apr 10, 2002 · N527AU · Boeing 7373B7SDR DD52002F00000Skin · crackedCRACKS ON TRAILING EDGE SKIN OF RUDDER. CRACKS IN AREA OF STIFFENER BEADS.Apr 8, 2002 · N6249J · Piper PA32R300SDR MWEA020194Panel · damagedDENT DAMAGE ON RUDDER LEADING EDGE STRUCTURE AT STATION ZR70 RIGHT SIDE. MEASURES APPROX 4 INCHES IN LENGTH. FABRICATED AND INSTALLED REPAIR.Mar 27, 2002 · N206ME · Doug DC932SDR USAA020151Skin · damagedPIT - FOUND RUDDER WITH SKIN DAMAGE .25 INCH BY .25 INCH AND 1 INCH BY .25 INCH, WITHIN 6 INCHES OF PANEL EDGE OR FASTENER LINE. WET LAY UP REPAIR PER EA 73621 AND SRM 50-70-11. (M)Mar 22, 2002 · N780AU · Boeing 7374B7SDR USAA020117Skin · delaminatedPIT - FOUND RUDDER DELAMINATED .5 INCH BY .5 INCH AND 1 INCH BY .050 INCH, 2 AREAS LEFT AND RIGHT SIDE STATION 0.00. 200-230 DEGREE F WET LAYUP PER SRM 51-70-17 AND EA 73419. (M)Mar 8, 2002 · N778AU · Boeing 7374B7SDR RIVA020306Shield · crackedPSM - FOUND RUDDER, LEFT LEADING EDGE CHAFE SHIELD CRACKED. STOP DRILLED CRACK ON RUDDER RUB STRIP PLATE AT STATION 206.350 IAW BOEING SRM 51-40-20 FIG 13. FABRICATED DOUBLER IAW BOEING SRM 51-40-20 FIG 13. INSTALLED DOUBLER IAW BOEING SRM 51-30-2 AND 51-40Mar 6, 2002 · N365PA · Boeing 727225SDR CA020501011Skin · cracked(CAN) SKIN CRACKED AT UPPER LIGHTNING HOLE.Feb 20, 2002 · Cessna 152SDR QXEA0200307Flange · crackedPDX - THE FORWARD AND AFT FLANGES ON THE APERTURE FOR PANEL 57Y ON THE RUDDER ARE CRACKED OUT. REPAIRED IAW SRM 51-31-01.Feb 13, 2002 · N480AU · Fokker F28MK4000SDR QXEA0200202Doubler · corrodedPDX- THE TOP EDGE OF THE BOTTOM SKIN PANEL ON THE RUDDER COVE HAS A TEMPORARY REPAIR STRIP INSTALLED ON THE INTERIOR BY THE GUSTLOCK HOUSING. THE STRUCTURE IS WORKING AND PRODUCING ALUMINUM OXIDE BUILDUP. REPAIRED IAW FOKKER SRM 51-31-01.Feb 7, 2002 · N480AU · Fokker F28MK4000SDR TSAA0255019Skin · damagedCOMPOSITE DAMAGE TO LEFT SIDE AT RUDDER STATION 86.59 TO STATION 66.59. REMOVED ALL CONTAMINATION AND WATER FROM DAMAGED AREA. FABRICATED, CLEANED, AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. REPAIRED IAW SRM 55-40-5 AND 51-40-14 REPAIR NR 3. (M)Jan 2, 2002 · N823AL · Boeing 737230SDR C2XA01CL257Skin · crackedDURING OVERNIGHT MAINTENANCE A CRACK ON THE RUDDER II SKIN WAS FOUND.THE CRACK WAS ON THE RIGHT SIDE OF THE RUDDER AND CLOSE TO THE TRAILING EDGE.MAINTENANCE PERFORMED A PERMANENT REPAIR OF THE RUDDER II SKIN AS PER CONTINENTAL EXPRESS EC 5540-01015.THE AIRCRADec 24, 2001 · N24517 · Emb EMB135LRSDR USAA011398Skin · crackedPIT - FOUND RUDDER CRACKED, LESS THAN .5 INCH BY .5 INCH BY 6 INCHES, T/E 1 FT ABOVE TOP OF BALANCE WT STA 141.52. REMOVE CORE AND INSTALLED NEW HONEY CONE AND 2 LAYERS OF FABRIC PER SRM 55-40-01 AND 41-70-04. (M)Dec 20, 2001 · N775AU · Boeing 7374B7SDR USAA011395Skin · damagedPIT - FOUND RUDDER SCREW PULLED THROUGH SKIN, LEFT SKIN PANEL AT R STATION 225 APPROXIMATELY. TWO EXTRA REPAIR PLIES WITH .5 INCH PER PLY OVERLAP PER EA 73064. (M)Dec 17, 2001 · N300AU · Boeing 737301SDR GTIA012110Skin · crackedFTW - FOUND RUDDER RIGHT UPPER SKIN, .50 INCH DIAMETER DENT IN SKIN BETWEEN RIBS 17 AND 18. UPON FURTHER INVESTIGATION CRACK FOUND IN SKIN AREA FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)Nov 26, 2001 · N12536 · Doug DC932SDR QXEA0101793Skin · crackedPDX - RUDDER APERTURE FOR PANEL 574 IS CRACKED AT NUT PLATE HOLES. REPAIRED IAW FOKKER SRM 51-31-01.Nov 7, 2001 · N482US · Fokker F28MK4000SDR GTIA012217Skin · crackedFTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 12. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)Nov 6, 2001 · N12536 · Doug DC932SDR GTIA012255Skin · crackedFTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 11. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DC9 SRM 5-03. (M)Nov 6, 2001 · N12536 · Doug DC932SDR GTIA012101Skin · crackedFTW - FOUND RUDDER LEFT UPPER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 21. TRIMMED OUT CRACKED SKIN WITH CIRCULAR CUTOUT. FORMED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 55-03. (M)Nov 6, 2001 · N12536 · Doug DC932
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