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 UPS09M54678Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ NR 293-S4-02, EXISTING REPAIR DOUBLER ON LWR AFT RUDDER AT BS 357-364 IS NOT ON MRCSSR REPORT AND NOT PER SRM. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5540-32245-A.Jan 27, 2009 · N293UP · Doug MD11FSDR UPS09M54680Skin · damagedINSPECTION TYPE:1C D-378613- DAMAGE TO LOWER AFT RUDDER SKIN, LT SIDE FABRICATED DOUBLER AND INSTALLED ON SKIN IAW UPS EO MD11-5540-32181-A.Jan 10, 2009 · N293UP · Doug MD11FSDR USAA2009010290005Skin · delaminatedCLT Q5 MAJOR REPAIR NR 03C70827010/001 DELAMINATION ON RUDDER 3 INCHES ABOVE NR 4 HINGE ON RT SIDE. REPAIRED RUDDER ABOVE NR 4 HINGE ON RT SIDE IAW US AIRWAYS EA NR 100793.Dec 29, 2008 · N438US · Boeing 7374B7SDR ASAA0944160Skin · puncturedRUDDER PUNCTURED RT SIDE APPROX. 16" FROM 88" FROM LOWER EDGE. PREPPED PUNCTURED AREA AND REPAIRED AREA IAW B737 400 SRM 51 70 03 REP 2.Dec 15, 2008 · N779AS · Boeing 7374Q8SDR CALA0801075Skin Panel · scratchedRUDDER BETWEEN ATTACH POINT 4 AND 5 SCRATCH ON RIGHT SIDE CLOSE TO TRAILING EDGE. ACCOMPLISHED REPAIR OF RT RUDDER SKIN PANEL PER CO EC/RA 5540-01257.Nov 14, 2008 · N16648 · Boeing 737524SDR WRLA2008103Skin · damagedDURING BRIDGE CHECK + 4C CHECK, EGAT MECHANIC FOUND LWR RUDDER BROKEN ON THE LWR EDGE. REPAIRED SKIN DAMAGE AREA IAW ENGINEERING INSTRUCTION W2008A55B-1172 REV 01.Nov 12, 2008 · N384WA · Doug MD11FSDR DHLA2009743DH566Skin · wornEMPENNAGE VERTICAL STABILIZER LOWER RUDDER L/E LT AND RT SIDES WITH WEAR DUE TO CHAFING AGAINST RUB SEAL. REPAIRED LWR RUDDER FROM RUD STA 60.387 TO RUD STA 154.185 RT AND FROM RUD STA 81.983 TO RUD STA 154.185 LT IAW B727 SRM 55-40-3 FIG 1.Nov 11, 2008 · N743DH · Boeing 727225SDR 08FDEA04730Skin · damagedTHERMOGRAPHY INSPECTION OF RUDDER S/N HF1005 SHOWS 3 AREAS OF POSSIBLE DEFECTS, LT SIDE- CONFIRMED BY ULTRASONIC INSP. DEFECTS AT NEAR FASTENERS 9,13 AND 20 COUNTED FROM TOP OF RUDDER REMOVED DAMAGED AREAS AND REPAIRED LT SIDE OF RUDDER IAW EA 6-5540-118Nov 5, 2008 · N420FE · Airbus A310SDR IXXA08SMN207SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EMPENNAGE RUDDER RIGHT SKIN CRACKED AT STATION ZR 253.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BAOct 28, 2008 · N71CX · Doug DC862FSDR MALA080184Skin · dentedDENT NOTED ON LT SIDE OF RUDDER ASSY, 5.25 AFT OF FRONT SPAR AT WL 164.55. REPAIRED IAW EO S57226.Oct 2, 2008 · N428XJ · Saab 340BSDR 08FDEA04034Skin · delaminatedFOUND ON RUDDER LT SIDE NEAR HOISTING POINTS FLUID INGRESS (SEVERAL AREAS) WITH DEBONDING. REPAIR PERFORMED BY BONDING REPAIRS IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055.Sep 25, 2008 · N744FD · Airbus A300F4622RSDR 08FDEA04033Skin · delaminatedFOUND ON RUDDER RT SIDE NEAR RIB 0 FLUID INGRESS (4 AREAS) WITH DEBONDING. REPAIR PERFORMED BY BONDING REPAIRS IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055.Sep 25, 2008 · N744FD · Airbus A300B4622RSDR 2008FA0000666Skin · crackedTHE LOWER FORWARD RUDDER SKIN IS CRACKED 2.5 INCHES, THIS WAS FOUND DURING ROUTINE PHASE INSPECTIONS. THE RUDDER SKIN PART NUMBER IS 5533000-95. THIS IS THE THIRD CRACK FOUND IN THE SAME LOCATION ON THE SAME MODEL AIRPLANE THIS CALENDER YEAR.Sep 10, 2008 · N905LC · Cessna 560CESSNASDR DHLA2008745543Skin · corrodedEMPENNAGE VERTICAL STABILIZER LOWER RUDDER L/E SURFACE WITH WEAR AND CORROSION FROM STA 127.5 TO 150.625Sep 5, 2008 · N745DH · Boeing 727224SDR 08FDEA03479Panel · corrodedFOUND CORROSION ON RUDDER SIDE PANEL AT BR NR 1, LT. REPAIR PERFORMED BY REPLACEMENT OF LIGHTNING STRIKE PROTECTION PLATE AND LAMINATING IAW RAS/DAHAM/4025191/2008 ISS B, APPROVED BY EA 6-5541-120083.Aug 18, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA03353Skin · damagedUPON INSPECTION OF RUDDER BY THERMOGRAPHY IAW EO 6-5530-7-5004 PT 2 PARA 8 STEP C AND D THE FOLLOWING DEFECTS WERE NOTED IN ADDITION TO ORIGINAL FINDINGS REF EA 6-5740-118399 THE UPPER RT PORTION OF THE RUDDER HAS 1 ADDITIONAL AREA OF MOISTURE MEASURING .960 WAug 9, 2008 · N812FD · Airbus A310324SDR 08FDEA02991Skin · delaminatedFLUID INGRESS ON RUDDER RT SIDE PANEL NEAR LOWER RIB Z-PROFILE. REPAIR PERFORMED IAW SRM 51-77-10, TD/K4/S1/24567/2008 ISS B AND RAS/DAHAM/4024567/2008 ISS A, APPROVED BY EA 6-5540-117180.Jul 21, 2008 · N742FD · Airbus A300B4622RSDR 08FDEA02990Skin · delaminatedFLUID INGRESS ON RUDDER RT SIDE PANEL. REPAIR PERFORMED IAW SRM 51-77-10 AND RAS/DAHAM/4024567/2008 ISS, APPROVED BY EA 6-5540-117180.Jul 21, 2008 · N742FD · Airbus A300B4622RSDR 08FDEA02989Skin · delaminatedFLUID INGRESS ON RUDDER LT SIDE PANEL. REPAIR PERFORMED IAW SRM 51-77-10 AND RAS/DAHAM/4024567/2008 ISS, APPROVED BY EA 6-5540-117180.Jul 21, 2008 · N742FD · Airbus A300B4622RSDR 08FDEA02447Skin · corrodedUPPER AFT RUDDER FOUND CORROSION MODERATE ABOVE SKIN AND SUSPECT INNER SKIN. REPAIRED AREA IAW SRM 55-10-00 VOL I FIG 2.Jun 25, 2008 · N10060 · Doug DC1010SDR HNAA2009010900387Skin Panel · damagedDURING C-CHECK INSP, THE TRAIL RUDDER SKIN WAS FOUND TO BE DAMAGED ON THE LT SIDE NEAR THE LOWER HINGE POINT. THE DAMAGE WAS REPAIRED IAW SRM PROCEDURES AND EO8-55-08-3203.Jun 18, 2008 · N980HA · Dhav DHC8102SDR UPS08852568Skin · corrodedINSPECTION TYPE:C2 RUDDER RT SIDE EXTERIOR SKIN HAS CORROSION, POPPED RIVETS AND BEADED SKIN IS SEPARATED. REMOVED AND REPLACED 2 RUDDER SKINS IAW DC8 SRM 51-1-21, 51-1-21A , AND51-01-22.May 28, 2008 · N802UP · Doug DC873FSDR 2008UALA03041Skin · damagedRUDDER SN 100, LT LE SKIN HAS AREA OF DAMAGE 1 INCH ABOVE LOWER EDGE. MAJOR REPAIR ACCOMPLISHED, TAPER SANDED DAMAGED AREA. INSTALLED MULTIPLE LAYER COMPOSITE REPAIR.May 27, 2008 · N399UA · Boeing 737322SDR 08FDEA02382Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RUDDER RT STA 270-869 RIB BR 2-7, OUTER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR WAS FOUND IAW FEDEX EA-6-118158R.May 21, 2008 · N721FD · Airbus A300B4622RSDR 08FDEA01897Skin · crackedVERTICAL STABILIZER, RUDDER CRACK AND SUSPECT INTERNAL CORROSION ON SKIN UPPER FWD RUDDER. REPAIRED AREA IAW SRM 55-10-00 FIG 3 VOL I.May 20, 2008 · N40061 · Doug DC1010SDR 08FDEA01880Skin · crackedDURING RIGGING RUDDER MECHANICAL CTRL ACCIDENTAL DAMAGED ON LOWER AFT RUDDER LT SIDE. REPAIRED SKIN & PAINT AREA IAW SRM 55-10-00 FIG 2 VOL I & DWG D10-11-014.May 19, 2008 · N307FE · Doug DC1030SDR IXXA08SMN154SSkin · canningDURING ROUTINE C CHECK INSPECTION, FOUND LT RUDDER SKIN OIL CANNING AT STATION ZR 168.656. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED BOTH PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AApr 18, 2008 · N821BX · Doug DC871FSDR 08FDEA01347Skin · delaminatedFOUND WATER INGRESS DURING THERMOGRAPHIC INSPECTION ON RUDDER RT SIDE. REPAIR PERFORMED BY REMOVING SKIN AND CORE, DRY THE AREA, PERFORM REPAIR IAW SRM 51-77-10 IAW RAS/DAHAM/4024380/2008 ISS A, APPROVED BY EA 6-5540-115259.Apr 8, 2008 · N730FD · Airbus A300B4622RSDR 08FDEA01093Panel · damagedLEFT RUDDER PANEL, 4TH FASTENER FROM THE TOP OF THE RUDDER HAS WATER IN 5 CONNECTED CELLS; 2 INDIVIDUAL CELLS AND DELAMINATION 1.8" BY 1.7", MARKED IN WHITE MARKER. REPAIRED LT RUDDER PANEL SKIN 4TH FASTENER FROM TOP BY REMOVING DELAMINATED AREA & APPLIED REPMar 21, 2008 · N803FD · Airbus A310324SDR 08FDEA01094Panel · damagedLEFT RUDDER PANEL, 3RD FASTENER FROM THE TOP OF THE RUDDER HAS WATER IN 7 CONNECTED CELLS; 4 CONNECTED CELLS; 2 CONNECTED CELLS AND 5 INDIVIDUAL CELLS, DELAMINATION 3.4 INCH BY 2.8 INCH. REPAIRED REMOVING DELAMINATED AREA & BONDING A NEW CORE & LAY UP REPAIMar 21, 2008 · N803FD · Airbus A310324SDR 08FDEA01092Panel · damagedLEFT RUDDER PANEL, 25TH FASTENER FROM THE TOP OF THE RUDDER HAS 1 CELL OF WATER, MARKED IN WHITE MARKER. REPAIRED LT RUDDER PANEL 25TH FASTENER FROM TOP BY REMOVING DAMAGE & BONDING A NEW CORE & LAY-UP REPAIR PLIES IAW EA 6-5540-118453.Mar 21, 2008 · N803FD · Airbus A310324SDR 08FDEA01091Panel · damagedLEFT RUDDER PANEL, 2ND FASTENER FROM THE TOP HAS WATER IN 7 CONNECTED CELLS; 5 CONNECTED CELLS AND 5 INDIVIDUAL CELLS, (MARKED IN WHITE MARKER) AND DELAMINATION 3.3 INCH BY 1.9 INCH. REPAIRED LT RUDDER PANEL 2ND FASTENER FROM TOP BY REMOVING THE DAMAGED AREAMar 21, 2008 · N803FD · Airbus A310324SDR DLM88080264Skin · damagedDURING HMV, TWO METALIZED DAMAGES WERE FOUND BOTH RUDDER SURFACES AT THE LT SIDE IT WAS 87 INCHES LONG BY 34 INCHES WIDTH AT THE RT SIDE IT WAS 71 INCHES LONG AND 30 INCHES WIDTH. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 51-70-1A D PARAGRAPH 23A.Feb 13, 2008 · N959DL · Doug MD88SDR IXXA08SMN058SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RUDDER RIGHT SKIN SIDE DENTED AT STATION ZR 276.531 TO ZR 267.218. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLFeb 7, 2008 · N822BX · Doug DC871FSDR USAA920080348Skin · delaminatedMCN - MAJOR REPAIR - C20 CHECK NR 6038691, DELAMINATION ON THE RIGHT SIDE OF RUDDER, RS 220 - RS 232. REPAIRED RIGHT SIDE OF RUDDER, RS 220 - RS 232 IAW B737 SRM 51-70-07.Jan 25, 2008 · N313AW · Boeing 7373S3SDR QXEA200800100Skin · dentedPDX - C1 CHECK - FORE RUDDER HAS A 1/4 BY 1/2 DENT ON RIGHT SIDE 13 INCHES FROM TOP EDGE 4 INCHES FROM TRAILING EDGE. MAINTENANCE CUT OUT SKIN DAMAGE, INSPECTED FOR CRACKS, NO CRACKS NOTED. REPAIRED IAW RD 8-55-1905 AND DHC8 200 SRM.Jan 14, 2008 · N349PH · Dhav DHC8202SDR UPS08851631Skin · corrodedINSPECTION TYPE:C2 CORROSION UNDER BONDED SKIN RT SIDE OF RUDDER ABOVE ISOLATION BELT. RUDDER REPLACED ON N/R 123801.Jan 11, 2008 · N702UP · Doug DC871FSDR UPS08851624Skin · crackedINSPECTION TYPE:C2 EDGE CRACK ON RT SIDE OF RUDDER TAB CUT OUT. RUDDER REPLACED ON N/R 123801.Jan 11, 2008 · N702UP · Doug DC871FSDR UPS08851623Skin · dentedINSPECTION TYPE:C2 CREASED DENT ON LT UPPER SKIN OF RUDDER. RUDDER REPLACED ON N/R 123801.Jan 11, 2008 · N702UP · Doug DC871FSDR UPS08851605Skin · crackedINSPECTION TYPE:C2 1" CRACK BELOW RUDDER TAB ON RT SIDE OF RUDDER. RUDDER REPLACED ON N/R 123801.Jan 11, 2008 · N702UP · Doug DC871FSDR UPS08851604Skin · crackedINSPECTION TYPE:C2 EDGE CRACK ON RT UPPER RADIUS OF RUDDER TAB CUT OUT. RUDDER REPLACED ON N/R 123801.Jan 11, 2008 · N702UP · Doug DC871FSDR UPS08851620Skin · corrodedINSPECTION TYPE:C2 POPPED FASTENER HEADS AND HEAVY CORROSION ON LT RUDDER SKIN FWD OF TAB. RUDDER REPLACED ON N/R 123801.Jan 10, 2008 · N702UP · Doug DC871FSDR PIDA07059Skin · damagedDURING MAINTENANCE CHECK, DAMAGE NOTED ON THE TRAILING OF THE RUDDER APPROXIMATELY 10 INCHES BELOW THE TOP. REPAIRED DAMAGE PER SRM 51-40-14.Dec 21, 2007 · N251TR · Boeing 737228SDR PIDA07060Skin · damagedDURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LOWER FORWARD LEFT CORNER OF THE RUDDER. REPAIRED PER BOEING TELEX MESSAGE NOS 1-724910440-9 AND -10 WITH FAA DOA APPROVED 8100-9 DATED DEC 20, 2007.Dec 20, 2007 · N251TR · Boeing 737228SDR PIDA07058Skin · crackedDURING MAINTENANCE CHECK, NOTED A CRACK IN THE LEADING EDGE OF THE RUDDER AT RUDDER STATION 58.6. REPAIRED PER BOEING TELEX 1-720703898-1 AND -3 WITH FAA DOA APPROVED 8100-9 DATED DEC 15, 2007. SUSPECT DAMAGE OCCURRED DURING RUDDER REMOVAL FROM VERTICAL FIN.Dec 17, 2007 · N251TR · Boeing 737228SDR USAA920071292Skin · delaminatedMCN - MAJOR REPAIR - C4 CHECK - NR 6055223, DELAMINATION ON RUDDER SKIN LEFT HAND SIDE, RUDDER STATION 332. REPAIRED RUDDER SKIN LEFT HAND SIDE, RUDDER STATION 332 IAW B757 SRM 51-70-04 FIGURE 5.Nov 24, 2007 · N200UU · Boeing 7572B7SDR 2007UALA04728Skin · damagedRUDDER T/E HAS AN AREA OF DELAMINATION 7" BY 80", TOP OF DAMAGE IS 90" BELOW TIP AND BOTTOM OF DAMAGE IS 79" FROM BOTTOM OF RUDDER. REPLACED RUDDER & OP CHK'D ON NR G7263I. INSTALLED RUDDER IS TS1274.Nov 17, 2007 · N846UA · Airbus A319131SDR IXXA07SMN270SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 253.000 TO STATION ZR 271.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER, BONDED PANov 16, 2007 · N604BX · Doug DC873FSDR IXXA07SMN266SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT HAND SKIN AT STATION ZR 115.000 TO STATION ZR 150.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. Nov 15, 2007 · N604BX · Doug DC873FSDR IXXA07SMN265SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 150.000 TO STATION ZR 178.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. BONDENov 15, 2007 · N604BX · Doug DC873F
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