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 JJBA20130415010Skin · crackedA CRACK WAS FOUND IN THE SKIN OF THE TRAILING RUDDER LT SIDE CENTER TOP. THE CRACK WAS REPAIRED IAW APPROVED DATA.Apr 15, 2013 · N363PH · Dhav DHC8202SDR DALA13012310944Skin · damagedDURING SCHEDULED MX THE EXTERIOR METALLIC COATING ON BOTH FACES OF THE RUDDER WAS FOUND TO BE DAMAGED. THE RUDDER WAS REPAIRED IAW SRM 51-70-1AD AND THE REQUIRED INSPECTION WAS COMPLETED.Mar 13, 2013 · N944DL · Doug MD88SDR USAA2013031400002Skin · debondedS2 CHECK - AREA OF DISBOND ON RIGHT SIDE OF RUDDER SKIN APPROX 22 INCHES FROM TOP OF RUDDER & 16 INCHES FORWARD OF TRAILING EDGE. REPAIRED RIGHT SIDE OF RUDDER SKIN IAW EA 204345.Mar 13, 2013 · N172US · Airbus A321211SDR DALA13011209013Skin · crackedDURING SERVICE CHECK, RUDDER SKIN UPPER MID HINGE CUTOUT FOUND CRACKED. REMOVED DAMAGED PLIES AND TAPERED BACK IAW SRM 51-70-01A, PG 189. DAMAGED CONTAINED. OK TO INSTALL REPAIR. PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 51-70-01A.Mar 7, 2013 · N913DE · Doug MD88SDR USAA2013040200032Skin · crackedC2 CHECK - CRACK ON RUDDER LEADING EDGE AT RUDDER STA 245.00. REPAIRED RUDDER LEADING EDGE AT RUDDER STA 245.00 IAW B757 SRM 55-40-01, TABLE 1 & 51-70-05.Feb 27, 2013 · N904AW · Boeing 7572S7SDR IPXA13577142Skin · damagedINSPECTION TYPE:C-16 RUDDER RT SIDE HAS A HOLE. REPAIRED IAW SRM 51-70-04 & 55-40-01Feb 15, 2013 · N404UP · Boeing 75724APFSDR IPXA13177273Skin · damagedINSPECTION TYPE:10YR RUDDER SIDE PANEL, RT SIDE HAS DAMAGED SKIN. ACCOMPLISHED REPAIR ON RT SIDE RUDDER SIDE PANEL IAW EO A300-5540-50003-A PARA 6A.Feb 1, 2013 · N149UP · Airbus A300F4622RSDR R5KB2013012846287Skin · corrodedCORROSION ON RIGHT SIDE OF UPPER RUDDER TRAILING EDGE AT RS 175.Jan 28, 2013 · N727NK · Boeing 727212SDR R5KB2012012846190Skin · corrodedCORROSION ON LEFT SIDE OF UPPER RUDDER TRAILING EDGE BETWEEN RS 220 AND 242.Jan 28, 2013 · N727NK · Boeing 727212SDR R5KB2013012850560Panel · delaminatedLEFT UPPER RUDDER PANEL BETWEEN STA 212 AND 220 HAS ONE AREA OF DELAMINATION.Jan 28, 2013 · N727NK · Boeing 727212SDR R5KB2013012846194Skin · damagedUPPER RUDDER SKIN CORRODED RIGHT SIDE TRAILING EDGE BETWEEN STA 220-247.Jan 28, 2013 · N727NK · Boeing 727212SDR R5KB2013012846281Skin · damagedSKIN DAMAGED ON LOWER RUDDER LEFT SIDE BETWEEN STA 113-118.Jan 28, 2013 · N727NK · Boeing 727212SDR DALA13003220941Paint · peelingFLAKES ON RUDDER SKIN PAINT COAT ON RT SIDE BETWEEN STA ZRS 50 TO ZRS 72 AND LT SIDE BETWEEN STA ZRS 91 AND LT SIDE BETWEEN, STA ZRS 105 (VHS) REF NRC (T0 271294). RUDDER REPAIRED AREAS WERE PAINTED IAW EA 09-461041-03, REV C AND DLA DWN 11-08941 REV E. ASSOCJan 19, 2013 · N941DL · Doug MD88SDR REXA2012011600067Skin · dentedMAINTENANCE FOUND 2 DENTS ON THE LEFT RUDDER SKIN. THE DENTS MEASURE .40" X .250" X .005" DEEP AND .650" X .500" X .015" DEEP, WITH FINAL CUTOUT DIMENSIONS OF 6.8" X 4.4". REPAIRED IAW EA CRJ255-01192 AS APPROVED BY 8110-3.Jan 15, 2013 · N821AY · Cndair CL6002B19SDR SIMA201226007Skin · damagedDURING MBV FOUND RUDDER 2 EXTERNAL SKIN RIGHT LOWER AFT HAD A HOLE. REPAIRED IAW AEA EO EM-55MR-410.Dec 26, 2012 · N604AE · Emb EMB145LRSDR DALA12016070937Skin · damagedDAMAGED METALLIZED ON LT & RT SURFACES OF RUDDER. REPAIRED IAW SRM 51-70-1 AD AND CARD 2000-8149-06,Dec 12, 2012 · N937DL · Doug MD88SDR QXEA2012120701617Skin · damagedSHEET METAL TORN AND MISSING ON CAP TOP OF FORE RUDDER. REMOVED DAMAGED CAP ON TOP OF FORE RUDDER IAW SRM 51-42-45-02-01. FABRICATED PN 85547148-103 IAW SRM 55-41-10-02-01. APPLIED FAY SEAL AND INSTALLED FABRICATED TOP CAP OF FORE RUDDER IAW SRM 51-42-45-02-Dec 7, 2012 · N406QX · Bombdr DHC8402SDR DALA12014110936Skin · damagedLT SIDE OF RUDDER HAS LARGE AREAS OF PROTECTIVE FINISH PEELING UP WITH AREAS OF EXPOSED COMPOSITE SKIN. SANDED, REPAIRED, FLAME SPRAYED, & PAINTED RUDDER REF ER/A 092613-14MA AND SRM 51-30-3B, PG 1&3. REMOVED AND REINSTALLED 9EA HILOKS REF SRM 51-30-5 AND BANov 27, 2012 · N936DL · Doug MD88SDR ASOA20121126156TSkin · dentedRUDDER HAS SMALL DENT WITH CREASE ON RT SIDE JUST FORWARD OF FRONT SPAR AND BETWEEN RIBS ZV-3469 & ZV-3179. CUTOUT DENT AND INSTALLED FILLER AND DOUBLER. ACFT STILL IN C-CHECK.Nov 19, 2012 · N13949 · Emb EMB145LRSDR DALA12013530935Skin · damagedDAMAGED PAINT AND METALLIZED COAT ON BOTH SURFACES OF RUDDER. METALLIZED COAT ON BOTH SURFACES OF RUDDER WAS REPAIRED AND PAINTED IAW EA 09-461041-03, ME 01.Nov 19, 2012 · N935DL · Doug MD88SDR LR7A2012111100414Skin · damagedDURING SCHEDULED B-2 CHECK, FOUND HOLE IN T/E OF RUDDER SKIN DUE TO LIGHTNING STRIKE AT RUDDER STA 223. REPAIR ACCOMPLISHED IAW SMP 583 FIG 51-140-12.Nov 11, 2012 · N403LC · Lkheed 382GSDR IXXA2013020700002Skin · corrodedRUDDER SKIN-LT PANEL SHOWS CORROSION FROM STA ZR 140.750 TO STA ZR 150.750. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21, SRM 55-1-0. FABRICATED NEW PANEL PLATING 0.016" AND BONDED DOUBLER 0.016" BOTH FROM AL 2Nov 9, 2012 · N41CX · Doug DC862SDR UALA2012110506348Rivet · shearedON ARRIVAL FOUND RIGHT ENGINE PYLON BLOW PANEL POPPED OPEN. INF PANEL WAS POPPED OPEN AND REMOVED TO FIND OUT WHY LEFT PYLON PANEL WAS LOOSE AND WOULD NOT SECURE CLOSED. REPLACED SHEARED RIVETS AS NEEDED IAW AMM, NO DEFECTS NOTED WITHIN AREA.Nov 2, 2012 · N829UA · Airbus A319131SDR WVER2012101595612Skin · chafedRIGHT SIDE RUDDER LEADING EDGE SKIN HAS CHAFE DAMAGE IN 3 AREAS. 2 AREAS ARE BETWEEN CENTER AND TOP HINGE POINTS, MEASURING APPROXIMATELY 1.1 INCH LONG .20 INCH WIDE .006 INCH DEEP AND 6 INCHES LONG .25 INCH WIDE .005 INCH DEEP. 3RD AREA IS LOCATED BETWEEN BOOct 15, 2012 · N956LR · Cndair CL6002D24SDR UALA2012101205807Cap · damagedLIGHTNING STRIKE HOLE IN RUDDER TIP. LIGHTNING STRIKE DISCOVERED ON RUDDER UPPER CAP APPROXIMATELY ONE INCH FWD OF TRAILING EDGE (HOLE IN BOTH LEFT AND RIGHT SIDE). HOLE DAMAGE ON RT SIDE IS APPROX 1.4 IN L BY 1 IN WIDE. DAMAGE OF LEFT SIDE IS APPROX 3-8 INOct 11, 2012 · N488UA · Airbus A320232SDR EE4Y2012101000294Skin · corrodedDURING INSPECTION, FOUND VERTICAL STABILIZER, RUDDER RT EXTERNAL SKIN BULGED AT NR 7 POSITION HINGE. THE SKIN WAS REPAIRED IAW 70567897/006 .Oct 2, 2012 · N527NK · Airbus A319132SDR DALA12008233158Skin · debondedLEFT RUDDER SKIN DISBONDED BOTTOM SIDE SECTION A-A. REMOVED RUDDER IAW AMM 27-21-41. COMPLETED RUDDER INSTALL IAW AMM A319 27-21-41.Sep 21, 2012 · N358NB · Airbus A319114SDR USAA2012091800004Skin · damagedRON - RUDDER LEFT SKIN HAS EXPOSED COMPOSITE MATERIAL AT BODY STA 1140, 18 INCHES FROM LOWER END. REPAIRED SKIN IAW B737 SRM 51-70-17 AND EA 104250.Sep 14, 2012 · N439US · Boeing 7374B7SDR SPUY20120905044Skin · corrodedDURING ROUTINE C CHECK INSPECTION, UPPER RUDDER LEFT SIDE SKIN SHOWS CORROSION STA 230 REF N/R 1397.Sep 5, 2012 · N495AJ · Boeing 727233SDR SWAA2012092407909Skin · crackedLEFT EXTERNAL SKIN OF RUDDER CRACKED AT LEVEL OF FIN WL 107.09+7. REPAIRED SKIN IAW SRM.Aug 8, 2012 · N370SW · Boeing 7373H4SDR CHQA20120730236Skin · puncturedDURING INSPECTION, A PUNCTURE WAS DISCOVERED ON THE RUDDER II LEFT AND RIGHT SKIN. MAINTENANCE REPAIRED THE DAMAGED AREA OF THE SKIN AND RIBS IN ACCORDANCE WITH ETD 2012-145-010622.Jul 30, 2012 · N291SK · Emb EMB145LRSDR CHQA20120730235Skin · puncturedDURING INSPECTION, A PUNCTURE WAS DISCOVERED ON THE RUDDER II LEFT AND RIGHT SKIN. MAINTENANCE REPAIRED THE DAMAGED AREA OF THE SKIN AND RIBS IN ACCORDANCE WITH ETD 2012-145-010622.Jul 30, 2012 · N291SK · Emb EMB145LRSDR IPXA2674640Skin · damagedRUDDER T/E SKIN DAMAGED ON UPPER RT SIDE 12" UP FROM BOTTOM EDGE. REPAIRED IAW EO B767-5540-47177-B.Jul 30, 2012 · N319UP · Boeing 76734AFSDR CHQA20120705214Skin · damagedDURING INSPECTION, RUDDER II DEFLECTION TOOL NUT PLATE WAS MISSING AND A RIVET HOLE WAS ELONGATES IN THE SKIN OF THE RUDDER. MAINTENANCE REPLACED THE DAMAGED SECTION OF THE RUDDER SKIN IN ACCORDANCE WITH ETD 2012-145-009625.Jul 5, 2012 · N289SK · Emb EMB145LRSDR DU4R20120703002Skin · damagedS/O 127043 N/R 24762 - DURING SCHEDULED INSPECTION, FOUND RUDDER TIP SKIN HAS A LIGHTNING STRIKE.Jul 3, 2012 · N3796B · Lkheed 382G44K30SDR R61A201206260652Skin · dentedHAIL DAMAGE/DENTS TO LEFT SIDE FORE RUDDER UPPER SKIN P/N 85547102-105. BTAC MX REMOVED AND REPLACED THE LEFT SIDE FORE RUDDER UPPER SKIN IAW Q 400 SRM 51-42-05, 51-42-15. ALL WORK PERFORMED ON BTAC JOB 8416815 OP 68. A/C REMAINS IN TUS FOR COMPLETION.Jun 26, 2012 · N502LX · Bombdr DHC8402SDR R61A2012062612064Skin · dentedMULTIPLE DENTS ON TRAILING RUDDER LEFT SIDE UPPER SKIN. BTAC MX REMOVED AND REPLACED THE RUDDER LEFT SIDE UPPER SKIN P/N 85547156-103 IAW DASH 8 Q400 SRM 51-42-45 ON BTAC JOB 8418215 OP 53. A/C REMAINS IN TUS FOR COMPLETION.Jun 26, 2012 · N508LX · Bombdr DHC8402SDR DALA12001713122Skin · damagedRUDDER LEADING EDGE LEFT SIDE (3 INCH FROM BOTTOM) HAS COMPOSITE DAMAGE (CRACK). SANDED CLEANED PREPPED AREA AND BONDED COMPOSITE REPAIR MATERIALS PER A319 SRM 55-41-00 FIG 212 PARA 9 (L).Jun 16, 2012 · N322NB · Airbus A319114SDR DALA1237070934Skin · damagedDAMAGED METALIZED COATING ON RUDDER SURFACES. RUDDER SURFACE WERE REPAIRED IAW SRM 51-70-1AD PARAGRAPH 23A.May 30, 2012 · N934DL · Doug MD88SDR R61A201205240651Skin · dentedHAIL DAMAGE/DENTS TO FORE RUDDER LOWER SKIN PANEL P/N 85547101-105. BTAC MX REMOVED AND REPLACED THE FORE RUDDER LOWER SKIN PANEL IAW Q 400 SRM 51-40-07, 51-42-15, 51-42-05. ALL WORK PERFORMED ON BTAC JOB 8416815 OP 5010. A/C REMAINS IN TUS FOR A/C COMPLETIMay 24, 2012 · N502LX · Bombdr DHC8402SDR R61A201205240650Skin · dentedHAIL DAMAGE/DENTS TO AFT RUDDER LOWER SKIN PANEL P/N 85547155-101. BTAC MX REMOVED AND REPLACED AFT RUDDER LOWER SKIN PANEL IAW Q400 SRM 51-42-05, 51-40-07, 51-42-05. ALL WORK PERFORMED ON BTAC JOB 8416815 OP 5011. A/C REMAINS IN TUS FOR A/C COMPLETION.May 24, 2012 · N502LX · Bombdr DHC8402SDR FDEA201205231960Skin · corrodedLOWER AFT RUDDER, FWD RT SIDE HAS AREA OF SURFACE CORROSION. REPAIRED LWR AFT RUDDER ON RT SIDE IAW SRM 55-10-00 AND EA 8-5540-157335.May 23, 2012 · N564FE · Doug MD1010FSDR IPXA12673674Skin · damagedL-SHAPED CRACK AROUND 0.50 X 0.75" PLUS DENT BETWEEN RUDDER STA 131.108 AND 156.031. 620MM FROM REAR SPAR AND 290MM FROM T/E 485MM FROM FROM ACTUATOR RIB FASTENER LINE STA 165.074 AND 725MM FROM ACTUATOR RIB FASTENER LINE STA 115.142. ACCOMPLISHED PERMANENT May 19, 2012 · N317UP · Boeing 76734AFSDR R61A201205180644Skin · dentedDENTS FOUND ON FORE RUDDER LOWER SKIN PANEL P/N 85547101-105. BTAC MX REMOVED AND REPLACED THE FORE RUDDER LOWER SKIN PNL IAW Q400 SRM 51-42-05 ALL WORK DONE ON JOB 8418215 OP 5009. A/C REMAINS IN TUS FOR COMPLETION.May 18, 2012 · N508LX · Bombdr DHC8402SDR R61A201205180641Skin · dentedHAIL DENTS LEFT SIDE FORE RUDDER, SKIN DENTED IN 9 PLACES. BTAS MX REMOVED AND REPLACED LEFT SIDE RUDDER SKIN PANELS P/N 85547102 REF BTAC JOB 8418215 OP 15. A/C REMAINS IN TUS FOR COMPLETION.May 18, 2012 · N508LX · Bombdr DHC8402SDR VQI2012F00018Skin · delaminatedDURING D1-CHECK, RUDDER THERMOGRAPHIC INSP WAS PERFORMED IAW MPD TASK 554008-01-1, REVEALING EVIDENCE OF TRAPPED MOISTURE AT THE UPPER AND LOWER AFT HOIST POINTS ON THE RT SIDE OF THE RUDDER. RESONANCE FREQUENCY AND ULTRASONIC INSPECTIONS WERE ACCOMPLISHED IAMay 18, 2012 · N626VA · Airbus A320214SDR ASOA201201668Skin · chafedMINOR CHAFING TOP TO BOTTOM ON BOTH SIDES OF RUDDER SKIN FROM RUDDER SEAL RUB. L/E SKINS UPPER & LOWER ON LT & RT SIDES NEED PAINTED. PAINTED BLUE AND LIGHT RED ON LT & RT SIDES OF L/E SKINS AS REQUIRED IAW SRM 51-25-01-001-001-A01. DARK RED REQUIRES TO BE PAMay 7, 2012 · N707EV · Cndair CL6002C10SDR CHQA20120504156Skin · damagedDURING INSPECTION, THE RUDDER I PROTRACTOR SKIN AT THE ATTACHING NUT PLATE WAS FOUND TO BE DAMAGED. THE RUDDER I SKIN AT PROTRACTOR ATTACHING NUT PLATE WAS REPAIRED IN ACCORDANCE WITH SRM 55-40-01.May 4, 2012 · N370SK · Emb EMB145LRSDR EE4Y2012052100195Skin · contaminatedDURING THERMOGRAPHIC INSPECTION METHOD, VERTICAL STABILIZER RUDDER, RT SIDE PANEL HAS TRAPPED FLUID AT HOISTING POINT NR 2. DAMAGED AREA WAS REPAIRED IAW REPAIR INSTRUCTIONS NR 70561884/006 AND 70561884/007.Apr 27, 2012 · N525NK · Airbus A319132SDR DALA1232690940Skin · delaminatedDELAMINATED RT SIDE UPPER EDGE OF RUDDER. RT SIDE UPPER EDGE OF RUDDER WAS REPAIRED IAW SRM 51-70-1A PAR 23.Apr 25, 2012 · N940DL · Doug MD88
Back to JASC 5542