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 FDEA202108042288Skin · damagedN00302: 1EA WATER TRAPPED AREA(70MMX45MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.12 FASTENER. ACCOMPLISHED THE WORK : LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1 , SEQ NO:1122 AND SRM 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605RSDR FDEA202108042287Skin · damagedN00301: 1EA WATER TRAPPED AREA(50MMX40MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.11 FASTENER. ACCOMPLISHED THE WORK : LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1 , SEQ NO:1122 AND SRM 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605RSDR FDEA202108042285Skin · damagedN00303: 1EA WATER TRAPPED AREA(50MMX40MM) WAS FOUND AT L/H RUDDER T/E SCREW LINE NO.13 FASTENER. ACCOMPLISHED THE WORK : LH RUDDER SHELL MULTIPLE SCREW HOLES WATER INGRESS REPAIR I.A.W A300-600 EA NO:T6-5540-T0363520 P1 , SEQ NO:1122 AND SRM 55-41-12-201Aug 4, 2021 · N678FE · Airbus A300F4605RSDR QXEA2021080200381Skin · crackedTRAILING RUDDER APPEARS TO HAVE A CRACK ABOUT 2 INCHES IN LENGTH ABOUT 19 INCHES BELOW THE UPPER EDGE AND 9 INCHES FORWARD OF TRAILING EDGE. AIRCRAFT DOWN FOR REPAIRS.Aug 2, 2021 · N404QX · Bombdr DHC8402SDR FDEA202107261857Skin · delaminated1EA WATER TRAPPED AREA (50MMX50MM) WAS FOUND AT RH RUDDER T/E SCREW NEAR NO.37 FASTENER. ACCOMPLISHED THE WATER TRAPPED AREA CAT. B REPAIR I.A.W. A300-600F SRM 55-41-12-201, PARA. 22, FIG. 220, P. 286-294 AND SRI 55-71-12-201, IIR 55-41-12-2-005-00, 3E.Jul 26, 2021 · N653FE · Airbus A300F4605RSDR SWIA2021081060227Skin · damagedADDITIONAL DAMAGE FOUND ON RUDDER L/H SKIN BTWN. RS98.750 & RS110.278. (C-CHECK RO 8/6/2021) REPAIRED L/H SIDE RUDDER SKIN DAMAGE REF REO 670-55-41-090 REV -- 2021-07-26. COMPLIED WITH SKYCARD 51-900-1002Jul 21, 2021 · N709SK · Cndair CL6002C10SDR U2RA2021080640048Skin · delaminatedREFER TO SIA ENGINEERING COMPANY NRC AFM0386: DURING 12Y MAINTENANCE CHECK, FOUND INDICATION OF "LIQUID INGRESSION" ON THE RUDDER; 50MM X 50MM, TRAILING EDGE UPPER AREA (2ND FASTENER FROM THE TOP OF THE RUDDER). PERFORMED BONDED REPAIR OF RUDDER TRAILING EDGJun 25, 2021 · N819CA · Airbus A330243SDR JJBA20210610022Skin · dentedRUDDER II, LH SKIN DENTED AT RIB 615, LOWER SPAR CAP. RUDDER II, RIB PN 120-20723-001 HAVE DEFORMATION DUE TO A DENT. RIB REMOVED FOR REPLACEMENT. RUDDER II, LH SKIN AT RIB 615, LAY OUT FOR PATCH DOUBLER CUT OUT. RUDDER II, LH SKIN AT RIB 615, LOWER SPAR CAP RJun 10, 2021 · N31131 · Emb EMB145XRSDR UIEA2021060101223Skin · damagedRH LWR RUDDER BROKEN SKIN(<P>PERFORM BROKEN DAMAGE ON RH LWR RUDDER PANEL SKIN AT RUD STA 147.722 IAW EGAT EI NO.T2021A55M-1443 REV.1</P><P>CONDITIONAL CHECK NORMAL</P>)May 29, 2021 · N493MC · Boeing 74747UFSDR HNAA2021062400285Skin · puncturedRUDDER II HAS HOLE RH SIDE BOTTOM ON TRAILING EDGE (MARKED). REPAIRED RUDDER II HOLE ON RH SIDE BOTTOM ON TRAILING EDGE IAW PIEDMONT EO1-55-21--0134 AND ETD2021--145-016785.May 23, 2021 · N641AE · Emb EMB145LRSDR UIEA2021050501065Skin · delaminatedEMP - LOWER RUDDER LHS T/E MOST UPPER AREA FOUND DELAMINATED(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD </P>)May 16, 2021 · N429MC · Boeing 747481SDR 7C7A2021050500003Skin · dentedMULTIPLE DENTS ON FORE RUDDER. REPAIRED IAW RD 8-55-3616May 5, 2021 · N880EA · Dhav DHC8106SDR SIMA20210505001Skin · damagedRUDDER 2 SKIN AND ATTACH ANGLE DAMAGE CAUSED BY FOD JUST BELOW THE LOWER HINGE POINT.-C/A-REPAIRED IAW ERS-EM-55MR-884 AND ERS-EM-55-885May 5, 2021 · N668HH · Emb EMB145LRSDR SWIA202159003Skin · dented*DENT ON RH SIDE OF RUDDER, LOWER END. MARKED. (C-CHECK RO 6/22/2021) COMPLIED WITH DOUBLER REPAIR WHERE DENT WAS AT ON RH SIDE OF RUDDER, LOWER END IAW CRJ900 SRM 55-41-01-201-001-A01 FIGURE 55-41-01-991-804 / COMPLIED WITH SKYWEST TASK CARD 51-900-100Apr 1, 2021 · N800SK · Cndair CL6002D24SDR UIEA2021032200672Skin · delaminatedLOWER RUDDER FOUND DELAMINATION.(<P>LOWER RUDDER DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5.A, REV 91, REV DATE : 20 FEB 2021.</P>)Apr 1, 2021 · N476MC · Boeing 74747UFSDR AALA202104049001Skin · separatedAIRCRAFT WAS GROUNDED: RUDDER LOWER TRAILING EDGE APEX HAS 10 INCHES OF COMPOSITE AND SHEETMETAL DAMAGE (CRACKS, SPLITTING SEPARATION AND CORROSION). REPAIRED RUDDER PER EA 326684 REV B.Mar 31, 2021 · N108UW · Airbus A320214SDR SWIA202157934Skin · damagedCREASE FOUD ON TRAILING EDGE OF RUDDER MIDWAY UP. TWO DENTS FOUND ON LH RUDDER SURFACE AND ONE DENT ON RH RUDDER SURFACE. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICE/PROCEDUREMar 3, 2021 · N912SW · Cndair CL6002B19SDR QXEA2021030200093Skin · damagedTRAILING RUDDER, LH SIDE, UPPER PORTION, HAS AN APPROX. 4" LONG CRACK, LOCATED AT RIB 28, CENTERED BETWEEN THE FWD AND AFT RUDDER SPAR. MAPPED DAMAGE AND ROUTED TO ENGINEERING REMOVED RIVETS FROM REPAIR AREA DN STARTED CUT OUT REF RD88/4-55-1989 PERFORMED HFECFeb 28, 2021 · N400QX · Bombdr DHC8402SDR A6WA202102237668Access Panel · damagedREPAIR RUDDER PCU PANEL 325DR PER 601R-55-31-333. AIRCRAFT REMOVED FROM SERVICE. REMOVED PROTECTIVE FINISH, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED. PERFORMED UT THICKNESS CHECK, MINIMUM REMAINING THICKNESS .081". FOUND TO BE WITHIN LIMITS REF REO 601RFeb 12, 2021 · N460AW · Cndair CL6002B19SDR UIEA2021020900264Skin · debondedDISBOND - RUDDER, LOWER RUDDER, LH SURFACE(<P>TRIM OUT THE DAMAGED SKIN (L = 4.5", W = 1.5", RUD STA 63, 40.5" FROM FWD EDGE) AND CLEAN BOND THE REPAIR PLIES WITH FILM ADHESIVE CURE AT 260 DEGREES F FOR 130 MINUTES. MAINTAIN A MINIMUM VACUUM OF 22 IN/HG IAW 74Feb 6, 2021 · N404KZ · Boeing 747481FSDR SIMA20210205009Skin · puncturedRUDDER 2 PUNCTURED 1" ABOVE LOWER EDGE 2" FROM TRAILING EDGE ON LH SIDE.-C/A-INSTALLED REPAIR DOUBLER AND FILLER TO RUDDER II 2" FROM TRAILING EDGE ON LH SIDE IAW EMB 145 SRM 51-40-02 AND ERS-EM-55MR-876Feb 5, 2021 · N923AE · Emb EMB145LRSDR JJBA20210126043Skin · dentedTRAILING RUDDER LT SKIN, MULTIPLE DENTS FOUND BETWEEN SPAR AND TRAILING EDGE & BETWEEN ZV 2648-3229. ACCESS DOOR 327DL REMOVED FOR ACCESS. TRAILING RUDDER LT SKIN, DENT NR 1 REPAIRED.Jan 26, 2021 · N11165 · Emb EMB145XRSDR DALA2021012800538Skin · damagedDURING INSPECTION FOUND DAMAGE TO RUDDER TRAILING EDGE 6FT FROM TOP. REPAIRED DAMAGE, IAW B737 SRM 55-40-01-1A-1 FIG5 938895. ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR, PER ERA 589622-14 REV ORIGINAL.Jan 22, 2021 · N3756 · Boeing 737832SDR JJBA20210121022Skin · chafedLT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV 2601.0 AND RIB ZV 3179.0. LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV2601 AND ZV3179 BLENDED AREA FOR INVESTIGATION, CUT OUT DONE. LT SIDE RUDDER 1, FRONT SPAR SKIN RJan 21, 2021 · N14173 · Emb EMB145XRSDR QXEA2021012500034Skin · delaminatedULTRASONIC INSPECTION OF RIGHT RUDDER SKIN DETECTS DELAMINATION AT STATION 5855 AT UPPER END OF PANEL. PERFORMED PERMANT REPAIR, IAW SRM 55-40-00, 51-71-08, 51-70-01.Jan 19, 2021 · N632QX · Emb ERJ170200LRSDR QXEA2021012500033Skin · delaminatedULTRASONIC INSPECTION OF LEFT RUDDER SKIN REVEALS DELAMINATION AT STATION 5810 AND 5855 UPPER END OF PANEL. COMPLETED PERMANT REPAIR, IAW SRM 55-40-00, 55-71-08, 51-70-01.Jan 19, 2021 · N632QX · Emb ERJ170200LRSDR GTIA2021012135555Skin · damagedWATER INGRESS FOUND ON RUDDER LT SKIN SCREW NR 9. DAMAGE LENGTH 50MM, WIDTH 35MM, REPAIR CAT A, REF LTPR NRI 5001043365-0010. REVIEWED LTPR NRI 5001043365-0010. PERMANENT REPAIR HAS BEEN PERFORMED ON RUDDER LT SHELL SCREW NR 9 STEP 3 STEP 6, IAW AIRBUS A32Jan 19, 2021 · N639NK · Airbus A320232SDR MK1Y01132021009Skin · dentedDURING MAINTENENCE INSPECTION FOUND A DENT ON RUDDER SKIN LEFT SIDE BETWEEN RUDDER STA 165 TO 181, 43" FROM RUDDER AFT EDGE.Jan 13, 2021 · N388AA · Boeing 767323SDR VNAA2021010499918Skin · canningRUDDER SKIN IS OIL CANNING ON LOWER RT CORNER AROUND CUTOUT.Jan 4, 2021 · N708PS · Cndair CL6002C10SDR SWIA202056922Skin · dented*DENTS ON LH AND RH SIDES OF RUDDER EXTERNAL SKIN. AREAS MARKED. (C-CHECK) RO 3/11/2021 REPAIRED DENTS ON LH AND RH SIDES OF RUDDER EXTERNAL SKIN AS REQUIRED. REF CRJ700 SRM 55-41-01-201-001-A01 REV 38 DATED JUL 25/2020, CRJ700 SRM 51-42-10-001-001-A01 DDec 20, 2020 · N717EV · Cndair CL6002C10SDR SWIA202055409Skin · dentedRUDDER RT LEADING EDGE SKIN BETWEEN BOTTOM AND CENTER HINGES IS DENTED AND GOUGED, MARKED. C-CHECK RO 1/16/2021. BLENDED GOUGE FROM RUDDER RT LEADING EDGE SKIN BETWEEN BOTTOM AND CENTER HINGES, REF CRJ 200 SRM 51-12-00. DURING DRESS BACK OF DENT, SKIN FOUNDNov 22, 2020 · N868AS · Cndair CL6002B19SDR REXA2020113000799Skin · dentedINTERNAL RUDDER BAYS, BELOW PCU ATTACH POINTS PAINT DISBONDED FROM INTERNAL SURFACES DUE TO SKYDROL EXPOSURE. REPAIRED RUDDER, IAW MHIRJ EO NR CC670-22001-SNIEO-S01, ENDEAVOR AIRLINES EA'S NR CRJ955-10925, CRJ955-10926, CRJ955-10927 AND CRJ955-10928 REV IR DANov 16, 2020 · N931XJ · Cndair CL6002D24SDR 2020FA0000505Skin · damagedDURING ANNUAL INSPECTION IT WAS NOTED THAT THE LEFT SIDE UPPER RUDDER HINGE AREA SHOWED SIGNS OF DAMAGE AND THE RIGHT HAND SIDE SHOWED SIGNS OF CRACKING. RUDDER WAS REMOVED FROM AIRCRAFT FOR CLOSER DETAILED INSPECTION. B INSPECTION REVEALED MORE DAMAGE TO PRNov 16, 2020 · N704WR · Cessna 150MSDR AALA202011109017Skin · corrodedAIRCRAFT IN BASE MAINTENANCE. FOUND EXFOLIATION CORROSION WITH POPPED RIVET HEAD ON RUDDER 138.5 INCHES FROM TRAILING EDGE OF RUDDER ON APEX STRIP. AREA OF CORROSION WAS REMOVED AND REPLACEMENT PART WAS INSTALLED WITH SPLICE REPAIR, REF SRM 55-41-19-300-006 Nov 3, 2020 · N723UW · Airbus A319112SDR GTIA2020102635407Skin · damagedDURING THERMOGRAPHIC INSPECTION ON RUDDER SIDE PANELS FOUND HOIST POINTS 2 WITH WATER IND, RAF 2541584-1 CREATED. REVIEWED LTPR NR 5001018065-0010 AND RUDDER SIDE PANEL HOIST POINT HAS BEEN REPAIRED, IAW SRM 55-41-13-300-0010.Oct 24, 2020 · N635NK · Airbus A320232SDR GTIA2020102635406Skin · damagedDURING THERMOGRAPHIC INSPECTION ON RUDDER SIDE PANELS FOUND HOIST POINTS WITH WATER IND CREATED. REVIEWED LTPR NR 5001018065-0010 AND RUDDER SIDE PANEL HOIST POINT HAS BEEN REPAIRED, IAW SRM 55-41-13-300-029.Oct 24, 2020 · N635NK · Airbus A320232SDR SWIA202054450Skin · dentedTHE RUDDERS LT SKIN HAS 3 DENTS ABOVE A PREVIOUS REPAIR, MARKED WITH BLACK GREASE PENCIL. C-CHECK RO 12/04/2020. REMOVED RUDDER REFERENCE CRJ700 AMM. HAND DRESSED 3 EA DENTS IN RUDDER SKIN TO ORIGINAL CONTOUR, REFERENCE CRJ700 SRM AND REO. COMPLIED WITH CAOct 20, 2020 · N760EV · Cndair CL6002C10SDR TIPR2020121544231Cover · corrodedRUDDER RIGHT SIDE LEADING EDGE SKIN CORRODED BETWEEN RUD STA 116 AND 125. INSTALLED NEW GAP COVER.Oct 17, 2020 · N303KH · Boeing 737319SDR SIMA20201014001Skin · damagedRUDDER 2 AFT LOWER EDGE DAMAGED (CHAFED, SEPARATED AND RT SKIN CRACKED). C/A: INSTALLED DOUBLER AND FILLER ON RUDDER 2 RT AFT LOWER EDGE, IAW ERS-EM-55MR-866.Oct 14, 2020 · N922AE · Emb EMB145LRSDR LR7A2020100502342Skin · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LT SKIN AT VSS73-149 CORRODED FS 1138-1162. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR 2364.Oct 5, 2020 · N410LC · Lkheed 382GSDR JJBA20201001011Skin · dentedDENT WITH A CREASE FOUND ON RT SIDE OF THE TRAILING RUDDER 1.10" ABOVE RIB ZV 2357.0 AND 3.90" AFT OF FRONT SPAR. PATCH REPAIR ON RT SKIN OF TRAILING RUDDER 1.00 ABOVE RIB ZV 2357.0 AND 3.900 PO AFT OF FRONT SPAR.Oct 1, 2020 · N12136 · Emb EMB145XRSDR ASAA2020092933313Skin · dentedRUDDER LT SKIN HAS A DENT APPROXIMATELY 15.5" INCHES FROM THE TRAILING EDGE AND 83" INCHES FROM LOWER SIDE. GROUNDED-YES. REPARIED RUDDER LT SKIN DENT APPROX 15.5" FROM THE TRAILING EDGE AND 83" FROM THE LOWER SIDE, IAW B737-900ER SRM 55-40-01-2R-1, TABLE 20Sep 29, 2020 · N472AS · Boeing 737990ERSDR SWIA202055632Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA54306-601R-55-41-255 SN7833 MXCODEID49672-PR. COMPLIED WITH TEMPORARY DISPOSITION FOR MULTIPLE DENTS TO LT SIDE RUDDER SKIN, IN REF TO REO 601R-55-41-255 REV-. ACCEPTABLE FOR 5000 FLIGHT HOURS FROM TAT 40980.3. DUE Sep 28, 2020 · N957SW · Cndair CL6002B19SDR SWAA2021072918328Mount Bracket · crackedDORSAL FIN FWD ATTACH MOUNT BRACKET CRACKED. / REMOVED AND REPLACED VERTICAL DORSAL FIN FWD MOUNT BRACKET PER B737-700 DRAWING #147A1008 (RIB) AND SRM 51-40-02-OG-0.Sep 24, 2020 · N498WN · Boeing 7377H4SDR GTIA2020091735364Skin · damagedDURING WALKAROUND FOUND RUDDER RT SKIN HOIST POINT NR 3 DEBANDED RAF 2588774-1 CREATED. REVIEWED LTPR NR 5000101238-0010 COMP. REPAIR HAS BEEN PERFORMED, IAW SRM 55-41-13-300-030 REF TO RAF 2588224-1.Sep 17, 2020 · N634NK · Airbus A320232SDR SWAA2021011114509Skin · debondedLT RUDDER CONDUCTIVE STRIP DISBONDED AT LOWER AFT END 32' INCHES FROM TIP OF THE RUDDER, 19' INCHES FROM THE FWD EDGE 3' INCHES FROM THE AFT EDGE IN ZONE 3 MOD. REMOVED AND INSTALLED RUDDER, IAW B737 AMM 27-21-11 POS ONLY PN OFF: 173A0103-7 PN ON: 173A0103-8 Sep 8, 2020 · N7841A · Boeing 7377L9SDR T17A20200811034Skin · damagedRUDDER TOP TRAILING EDGE DAMAGED. INSTALLED RUDDER P/N 45A24001-211 S/N RK-576 FROM AIRCRAFT 475TM. PERFORMED FUNCTIONAL TEST AND CONFIRMED SERVICEABILITY, IAW HAWKER 400XP AMM 27-20-00.Sep 3, 2020 · N489TM · Beech 400ASDR JJBA2020082513014Skin · crackedSUSPECTED CRACKS ON RT LEADING EDGE #3 VORTILLON MOUNTING POINTS. REMOVED ALL RT LEADING EDGE #3 VORTILLONS. PERFORMED INSPECTION OF VORTILLON MOUNTING POINTS. FOUND CRACKS AND DAMAGE AT VORTILLON MOUNTING POINTS 6, 7, AND 8. #6 VORTILLON MOUNTING POINT HAS Aug 13, 2020 · N11194 · Emb EMB145XRSDR SWIA202052566Skin · chafedBOTH RUDDER LEADING EDGE SKINS "CHAFED", LT SIDE ALMOST THE ENTIRE LENGTH OF RUDDER AND THE RT SIDE FROM MIDDLE HINGE AREA DOWN, MARKED. C-CHECK RO 9/20/2020. RUDDER LEADING EDGE SKINS REPAIRED, PER REO SEE CONTINUATION CARD FOR DETAILS.Aug 8, 2020 · N784SK · Cndair CL6002C10SDR FDEA2020080314754Skin · delaminatedTRAPPED WATER INDICATION ON RUDDER LH SIDE PANEL HONEYCOMB CORE CELLS. LOCATED AROUND THE TRAILING EDGE FASTENER N. 31 ON VERTICAL STABILIZER (1EA) (L=4.5INCH W=3 INCH) REPAIRED RUDDER LH SIDE PANEL HONEYCOMB CORE CELLS LOCATED AROUND THE TRAILING EDGE FJul 14, 2020 · N651FE · Airbus A300F4605R
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