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 EE4Y2012051400173Skin · contaminatedEMPENNAGE VERTICAL STABILIZER RUDDER LT SIDE PANEL WITH TRAPPED FLUID AT HOISTING POINT NR 1. A PERMANENT REPAIR WAS INSTALLED AT DAMAGED AREA IAW REPAIR GUIDELINES 70561617/006 AND 70561617/007 UNDER THE NON ROUTINE ITEM; WO: A1A093, SUBJOB: 3, ITEM: 37.Apr 21, 2012 · N523NK · Airbus A319132SDR EE4Y20120326151Skin · damagedEMPENNAGE VERTICAL STABILIZER RUDDER SIDE PANEL HOISTING POINT NR 3 LT WITH TRAPPED FLUID. DAMAGED AREA WAS REPAIRED IAW REPAIR GUIDELINES 70560165/006, UNDER THE NON ROUTINE ITEM: WO A1A079, SUB JOB 3, ITEM 20.Mar 26, 2012 · N522NK · Airbus A319132SDR EE4Y20120326150Skin · damagedVERTICAL STABILIZER RUDDER RT SIDE AT STA 80 AND 25" OF THE T/E SKIN WITH LIGHTNING STRIKE. DAMAGED AREA WAS REPAIRED IAW REPAIR GUIDELINES 70560169/008, UNDER THE NON ROUTINE ITEM: WO A1A079, SUB JOB 3, ITEM 12.Mar 26, 2012 · N522NK · Airbus A319132SDR CHQA20120316103Skin · damagedDURING INSPECTION, THE LEFT SKIN DAMAGE WAS FOUND ON RUDDER II AT THE PROTRACTOR NUT PLATE ATTACHMENT. THE LEFT SKIN ON RUDDER II AT THE PROTRACTOR NUT PLACE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-004001A.Mar 16, 2012 · N298SK · Emb EMB145LRSDR FXGA201203081217Fabric · tornLOWER RUDDER END RIB FABRIC TORN. R & R OF TORN & DAMAGED FABRIC.Mar 8, 2012 · N151 · Doug DC6BSDR EE4Y201203060109Panel · damagedEMPENNAGE VERTICAL STABILIZER RUDDER SIDE PANEL HOIST POINT NR 2 LT WITH TRAPPED FLUID. REPAIRED THE HOIST POINT IAW GUIDELINES.Mar 6, 2012 · N517NK · Airbus A319132SDR DXTR20120223001Skin · crackedRUDDER SKIN CRACKED ON LOWER L/E. R & R SKIN WITH NEW PN 6633000-5.Feb 23, 2012 · N646QS · Cessna 560XLSDR DALA1213369235Skin · crackedRUDDER SKIN CRACKED AT NR 3 HINGE CUTOUT RT SIDE. REPAIRED RUDDER SKIN AT NR 3 HINGE CUTOUT PER MD 90 SRM 55-41-01 PAGES 111 AND 112 AND PERFORMED WEIGHT AND BALANCE USING CHECK WEIGHT METHOD WITHIN LIMITS PER MD90 SRM 55-40-01.Feb 18, 2012 · N935DN · Doug MD9030SDR FDEA201202100542Skin · contaminatedTWO WATER TRAPPED AREAS WERE FOUND AT RT RUDDER NR 27 SCREW (5.5" X 5") AND NR 38 SCREW (3" X 1.5") (EO 6-5530-7-5004, PART 2) NDT INSPECT L/E AND T/E. THE OUTER SKIN AND EVLUATED THE DIMENSION OF THE DAMAGED AREA ARE 5.5"X5" (NR 27 SCREW) AND 3"X1.5" (NFeb 10, 2012 · N804FD · Airbus A310324SDR FDEA201201270353Skin · damagedAFT LOWER RUDDER SKIN FORWARD LOWER CORNER FOUND DAMAGED. REPAIRED IAW SRM 55-40-01, FIGURE 201, REV 48. EA 1-5540-156837. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 27, 2012 · N574FE · Doug MD11FSDR DALA1202679018Skin · damagedDURING HMV DAMAGED METALIZE COAT WAS FOUND ON RT AND LT FACE OF RUDDER REF MD88 SRM 51-70-1A PARA 23 FOR REPAIR. JAN 23,2011 RUDDER RT AND LT FACE WAS REPAIRED IAW MD88 SRM 51-70-1A PARA 23.Jan 19, 2012 · N918DE · Doug MD88SDR GNMA20111209Skin · wrinkledRUDDER WAS RUBBING ON HORIZONTAL UPPER AFT FAIRING ASSEMBLY AND CAUSED A 3" X 3" WRINKLE ON THE RT LOWER AFT SKIN.Dec 7, 2011 · N6640C · Cessna 414ASDR UALA2011113006579Repair · debondedRUDDER LEFT UPPER SURFACE OLD REPAIR IS DISBONDING AND BREAKING OFF. AREA APPROX 4 INCHES BY 5 INCHES. COMPLIED WITH EVA-81567 AND MADE TEMP REPAIR WITH SPEEDTAPE.REFER TO SM-09-13-25-01-JD FOR PERMANENT REPAIR.Nov 30, 2011 · N596UA · Boeing 757222SDR DALA1170510929Skin · damagedMISSING AND DAMAGED FLAME SPRAY COAT ON RT RUDDER SKIN SURFACE. RIGHT RUDDER SKIN SUFACE WAS REPAIRED IAW DC9/MD80 SRM 51-70-1A PAR 23 AND OPN JIC 1031 CARDS 1770 AND 1778.Nov 19, 2011 · N929DL · Doug MD88SDR DALA1158280920Skin · damagedDURING HMV DAMAGE PAINT COAT AND MISSING METALIZED PROTECTION WAS FOUND ON RUDDER SKIN LT/RT SIDE. RUDDER SKIN WAS REPAIRED IAW MD88 SRM 51-70-1AD PARA 23.Oct 15, 2011 · N920DL · Doug MD88SDR FDEA201110034275Skin · damagedRUDDER TRAILING EDGE TOP SIDE LIGHTING STRIKE RT SIDE STATIC WICK DISCH. ATTACH AREA RUDDER DAMAGE TO T/E STATIC WICK ATTACHMENT WAS REPAIRED IAW SRM 55-41-12, PARA 16B, FIG 208C AND EA 6-5540-145674.Oct 3, 2011 · N726FD · Airbus A300B4622RSDR FDEA201110034274Skin · damagedRUDDER SKIN LT SIDE GROUP OF 3 EA LIGHTNING STRIKE HOLES AT UPPER SECTION BETWEEN RIB 13-14 REPAIRED 3 EA. LIGHTNING STRIKES HOLES AT UPPER SECTION BETWEEN RIB 13-14 ON LT SKIN OF RUDDER IAW SRM 55-41-12 ( 16 A ) AND FIG 201 PARA 30 A APPLIED SURFACE PROTECTIOOct 3, 2011 · N726FD · Airbus A300B4622RSDR FDEA201110034273Skin · damagedRUDDER SKIN AT LT SIDE LWR 16IN . FROM BOTTOM AND 26 IN. FROM L/E SPAR HAS A 1.0 L X .75W PUNCTURE. RUDDER SKIN LT SIDE 16 IN FROM LOWER EDGE AND 26 IN FROM FWD SPAR WAS REPAIRED IAW SRM 55-41-12,PARA 30 AS SKIN REPAIR ONLY AS NO DAMAGE WAS FOUND AT THE COROct 3, 2011 · N726FD · Airbus A300B4622RSDR EE4Y20111001546Skin · debondedVERTICAL STABILIZER, RUDDER LT & RT SIDE PANELS WITH WATER INGRESS AROUND INSIDE HONEYCOMB CORE AROUND HOISTING POINT NR 2. RUDDER PANELS REQUIRE A MAJOR REPAIR IAW MFG ENGINEERING GUIDELINES.Oct 1, 2011 · N509NK · Airbus A319132SDR CALA2011092600622Skin · puncturedSUPPORT TASK- PUNCTURE IN RUDDER APPROX 2FT BELOW COUNTER WEIGHT AND 2.5 INCHES FWD OF TRAILING EDGE. REPAIRED RUDDER RT SIDE BONDED PANEL PER AVO#HOU092111-01 AND ECRA#5540-01294, BALANCED BY CALCULATION, NEW SBHM IS +532.25 REF SRM 51-60-07.Sep 24, 2011 · N37274 · Boeing 737824SDR EE4Y20110527Skin · debondedVERTICAL STABILIZER, RUDDER LT SIDE PANEL WITH WATER INGRESS INSIDE THE HONEYCOMB CORE AROUND HOISTING POINT NR 3. NOTE: THE RUDDER LT SIDE PANELS REQUIRES A MAJOR REPAIR IAW GUIDELINES.Sep 14, 2011 · N507NK · Airbus A319132SDR USAA2011082900012Skin · damagedQ3 CHECK - MISSING PLYS LOCATED AT RUDDER STATION 7.0, 1.5" X 2.5"; MISSING PLYS AT RUDDER STA 133.0, 1.5" X 0.75". REPLACED RUDDER IAW JOB CARD 03C70827007.Aug 17, 2011 · N417US · Boeing 737401SDR USAA2011090100020Skin · delaminatedQ5 CHECK - DELAMINATION ON RIGHT SIDE OF RUDDER EXTERIOR SKIN 38 INCHES FROM BOTTOM & 4 INCHES AFT OF FORWARD SPAR. REPAIRED RIGHT SIDE OF RUDDER EXTERIOR SKIN IAW EA 103256B & B737 SRM 51-70-17.Aug 15, 2011 · N425US · Boeing 737401SDR CHQA201100345Skin · damagedDURING INSPECTION, THE SKIN WAS FOUND TO BE DAMAGED AND AN ANCHOR NUT MISSING ON RUDDER II, BETWEEN X27083 AND X27621 AS WELL AS BETWEEN ZV1932 AND ZV2277. MAINTENANCE REPAIRED THE SKIN (PN: 120-21755-001) AND ANCHOR NUT ON RUDDER II (PN: 120-20808-509) BETWEAug 10, 2011 · N572RP · Emb EMB145LRSDR DALA1146269016Skin · damagedDURING HMV DAMAGE WAS FOUND ON METALLIZED COAT OF RT SKIN OF RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1AD.Aug 5, 2011 · N916DE · Doug MD88SDR IPXA1M68556Skin · delaminatedINSPECTION TYPE:3C, AFTER REMOVAL OF UPPER AFT RUDDER FOUND SKIN DELAMINATED ON RT LOWER FWD EDGE. THIS DISCREPANCY REPAIR COMBINED WITH SIMILAR DAMAGE REPAIR AT LT LOWER FWD EDGE OF UPPER AFT RUDDER (REF NR 490475) AND REPAIRED IAW STASA EA 011-5540-01-A3319Jul 29, 2011 · N294UP · Doug MD11FSDR DALA1144580922Structure · erodedDURING HMV DAMAGED METALIZED COAT WAS FOUND ON LT AND RT FACE OF RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1A PARA 23.Jul 26, 2011 · N922DL · Doug MD88SDR IPXA11M68441Skin · damagedINSPECTION TYPE:3C, REF D-455897 AND EO MD11-5540-43137 AFT UPPER RUDDER RT SKIN LIGHTNING STRIKE REPAIR DAMAGE. FABRICATED AND INSTALLED PERMANENT REPAIR ON UPPER AFT RUDDER, RT SKIN BETWEEN ZV487-3 & ZAR550.9 IAW EO MD11-5540-43137-A AND SRM 55-40-01, REPAJul 25, 2011 · N294UP · Doug MD11FSDR IPXA1M68097Skin · delaminatedINSPECTION TYPE:C4, LOWER LT FWD CORNER OF UPPER AFT RUDDER LAMINATED SKIN DISBONDED. REPAIRED LOWER LT FWD CORNER OF UPPER AFT RUDDER LAMINATED SKIN IAW STA-SA EA 011-5540-01-A-3289-I/R AND UPS EO MD11-5540-43566-A.Jul 19, 2011 · N259UP · Doug MD11FSDR IPXA11M67276Skin · damagedLIGHTNING STRIKE UPPER RUDDER RT SIDE APPROX 10" FROM TOP. REPAIRED IAW EO MD11-5540-43137-A.Jun 16, 2011 · N294UP · Doug MD11FSDR GLBA20110613FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A CRACK IN THE TOP RT SKIN OF RUDDER II, 2.4" FROM FWD EDGE, .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-120-27-002. MATERIALS UTILIZED ARE IJun 13, 2011 · N299UX · Emb EMB120ERSDR JR2R2011053100227Skin · dentedAFT RUDDER UPPER SKIN DENTED. REPAIRED AFT RUDDER UPPER SKIN IAW DASH 8 RO DHC 82-55-1101.May 31, 2011 · N987HA · Bombdr DHC8402SDR FDEA201105292020Skin · delaminatedTHERMOGRAPHY AND ULTRASONIC INSP CARRIED OUT FOUND TRAPPED WATER ON RT RUDDER SKIN AT T/E BELOW NR 37 SCREW LINE AREAS APPROX 600 SQ MM. ACCOMPLISHED EA 6-5540-150322.May 29, 2011 · N809FD · Airbus A310324SDR EE4Y20110306Skin · debondedVERTICAL STABILIZER, RUDDER SIDE PANEL WITH WATER INGRESS AROUND HOISTING POINT NR 3. MAJOR REPAIR.May 28, 2011 · N505NK · Airbus A319132SDR DALA1503203253Skin · debondedRUDDER SIDE SHELL DISBONDED. INSP/REPAIR, IDENTIFIED AS MAJOR IAW AA 5540-01011.May 25, 2011 · N353NW · Airbus A320212SDR FDEA201105241956Skin · corrodedUPPER RUDDER RT SIDE HAS SMALL AREA OF CORROSION ON EXTERIOR SKIN AT TOP OF RUDDER. REMOVED CORROSION ON RH SIDE OF UPPER RUDDER IAW SRM REV 103, 51-10- 6. FABRICATED DOUBLER IAW SRM 55-20-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-20 AND 55-20-3 FIG 1 AND EA May 24, 2011 · N287FE · Boeing 7272D4SDR A6WA201140455Skin · chafedRUDDER RT SIDE LT HAS MINOR CHAFING ABOVE AND BELOW BOTTOM HINGE PANEL AND ABOVE CTR HINGE PANEL. REPAIRED CHAFED AREA ON RT RUDDER L/E ABOVE AND BELOW BOTTOM HINGE PANEL IAW SRM 55-40-00.Apr 20, 2011 · N418AW · Cndair CL6002B19SDR DALA1126239012Rudder · damagedDURING HMV DAMAGED METALIZED COAT WAS FOUND ON LEFT SURFACE AT RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1AD PARA 23.Apr 17, 2011 · N912DE · Doug MD88SDR DHLA201100501Skin · corrodedRUDDER LT SIDE.- SKIN CORRODED (STA ZR 150.000 - 178.000). CA-PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0, FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SApr 8, 2011 · N805DH · Doug DC873FSDR DHLA201100046Skin · corrodedRUDDER LT SIDE.- SKIN CORRODED STA ZR 115.000 - 150.000 GALVANIC CORROSION. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0, FIG. 6. REMOVED CORRODED PANEL PLATING IAW SRMApr 8, 2011 · N805DH · Doug DC873FSDR A6WA201140271Skin · chafedRUDDER L/E CHAFED RT SIDE BLENDED CHAFING OUT IAW SRM 51-12-00.Apr 5, 2011 · N417AW · Cndair CL6002B19SDR DHLA201100502Skin · corrodedRT RUDDER EXT SKIN CORRODED, STA ZR 140.750 (GALVANIC CORROSION). PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1 REMOVED COROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG. 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21Apr 2, 2011 · N805DH · Doug DC873FSDR DHLA201100053Skin · corrodedRT RUDDER EXT SKIN CORRODED STA ZR 168.656. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0, PG 1, SRM 51-1-21. FABRICAApr 2, 2011 · N805DH · Doug DC873FSDR DALA1122579851Skin · damagedFOUND FOD DAMAGE ON RIGHT SIDE OF RUDDER JUST FWD OF TOP TAB HINGE. TRIMMED OUT DAMAGE PER SRM 51-70-6 HFEC. INSPECTED CUTOUT PER NTM 06-10-01-001 DAMAGE REMOVED QC 1971. CUT OUT SIZE 1" BY 2.5'. EXTERNAL .032 2024T3 DOUBLER PER SRM 51-70-6. INSTALLED. 086Mar 26, 2011 · N760NC · Doug DC951SDR USAA2011033191304Skin · delaminatedCLT - Q5/QX6 - DELAMINATION ON LEFT SIDE OF RUDDER 3 INCHES BELOW STA 174 & 7.5 INCHES FORWARD OF TRAILING EDGE. REPAIRED LEFT SIDE OF RUDDER IAW EA 102811.Mar 22, 2011 · N419US · Boeing 737401SDR TAMF201103110074Skin · damagedDURING C4 CHECK RUDDER SKIN PANEL ULTRASONIC INSP FINDING, STA 115.142- LT. REPAIR WAS PERFORMED WITH EWO 767-55-018.Mar 11, 2011 · N769QT · Boeing 767241SDR ASAA1149283Skin · puncturedLEFT RUDDER SKIN PUNCTURED BONDED DAMAGED AREA IAW B737 400 SRM 51 70 17 REPAIR 1.Mar 1, 2011 · N765AS · Boeing 7374Q8SDR DALA1116629011Skin · damagedDAMAGED METALIZED COAT ON RUDDER SURFACE. REPAIRED PER SRM 51-70-1AD.Feb 25, 2011 · N911DE · Doug MD88SDR USAA2011022390855Plate · crackedCLT - Q1 - MAJOR REPAIR - CRACK ON RUDDER LIGHTNING DIVERTER PLATE ON LEFT SIDE OF RUDDER 15 INCHES FROM THE TOP OF RUDDER. REPLACED RUDDER IAW JOB CARD 03C70827003 & 03C70827007.Feb 23, 2011 · N422US · Boeing 737401SDR USAA2011022190848Skin · debondedPIT - MAJOR REPAIR - RUDDER DISBOND CHECK- RUDDER HAS AREA OF DISBOND, 3.11INCHES ABOVE BR1 AND 13.25 INCHES FWD OF THE TRAILING EDGE. REPAIRED RUDDER, 3.11 INCHES ABOVE BR1 AND 13.25 INCHES FWD OF THE TRAILING EDGE IAW EA 117296.Feb 20, 2011 · N763US · Airbus A319112
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