JASC 5411

Service difficulty reports · 1,454

Reports filed under 5411 · Nacelle/Pylon, Frame/Spar/Rib, 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 = '5411'
  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 2002UALA00988Spar · crackedNAC STA 221, NR 2 ENGINE PYLON, UPPER SPAR WEB, IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.Jun 10, 2002 · N657UA · Boeing 767322SDR 2002UALA00985Spar · crackedNAC STA 221, NR 2 ENGINE PYLON, AFT UPPER SPAR WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS.Jun 10, 2002 · N657UA · Boeing 767322SDR P5CA0200678Web · crackedCRACK 3.5" LONG FOUND #3 PYLON WEB BETWEEN RIVET HOLES BELOW STIFFNER (STA 211.42, MID SPAR WEB). DOUBLER REPAIR FABRICATED IAW SRM 54-14-03, PG 20. THE RIVETS WERE REMOVED PLUS FURTHER 3 EITHER SIDE OF CRACK. 2 OF FURTHER ROWS OF FASTENERS PITCHED FORWARD May 29, 2002 · N920FT · Boeing 747249FSDR SWIA200210933Frame · crackedFRAME CRACKED THROUGH ON FORWARD SIDE OF HYDRAULIC BAY BULKHEAD TOWARD OUTBOARD END AT FIREWALL. FABRICATED AND INSTALLED FRONT AND BACK SIDE DOUBLERS IAW SRM 54-20-04, 51-70-06, AND 51-40-02.May 23, 2002 · N198SW · Emb EMB120ERSDR AUS20020437Frame · cracked(AUS) LT ENGINE NACELLE FRAME (FIGURE 8 FRAME) CRACKED. CRACK LENGTH IS AT LEAST 100MM (4IN) LONG. SUSPECT AREA HAD BEEN SUBJECTED TO HIGH TEMPERATURES AND DISTORTION AT SOME STAGE.May 10, 2002 · Saab SF340ASDR ARWA20020507Spar · crackedDURING C-CHECK, NR 4 PYLON INTERIOR, STA YN 165, RM UPPER CHORD WITH 4 INCH CRACK. REPAIRED UPPER SPAR CAP OF NR 4 PYLON IAW AS ELEVEN INC DRAWING AS 11403, SHEET 1 TO 6. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.May 7, 2002 · N1804 · Doug DC862SDR UPS02438193Spar · chafedINSPECTION TYPE:C NR 1 PYLON - MID SPAR WEB CHAFING THROUGH AT NAC STA 238. MID SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 12.Apr 19, 2002 · N676UP · Boeing 747123SDR UPS02438046Frame · crackedINSPECTION TYPE: NR 3 PYLON INTERNAL FRAME FOUND CRACKED JUST O/B OF PYLON VALVE AREA. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.Apr 15, 2002 · N672UP · Boeing 747123SDR 2002UALA00617Spar · crackedNR 1 ENGINE PYLON UPPER SPAR WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.Apr 1, 2002 · N651UA · Boeing 767322SDR AUS20020141Web · cracked(AUS) RH ENGINE NACELLE TOP OUTBOARD WEB CRACKED IN AREA OF TOP REARENGINE MOUNT ATTACHMENT POINT.Feb 25, 2002 · Piper PA44180SDR MWEA020074Strap · crackedLEFT UPPER SPAR STRAP HAS CRACK INDICATION. MUST PERFORM MAGNETIC PARTICLE INSP IAW DC9 54A031 REV 8 FIG 3. REMOVED AND REPLACED BN FASTENER AND CRACKED PYLON STRAP.Feb 8, 2002 · N203ME · Doug DC932SDR MWEA020069Doubler · damagedRIGHT PYLON AFT SPAR WEB DOUBLER HAS OVERSIZED FASTENER HOLES. FABRICATED AND INSTALLED NEW DOUBLER.Feb 6, 2002 · N209ME · Doug DC932SDR MWEA020116Spar · damagedRIGHT PYLON AFT SPAR WEB UPPER HOLES OVERSIZED. FABRICATED AND INSTALLED SPAR WEB.Feb 6, 2002 · N209ME · Doug DC932SDR CA060208008Longeron · fractured(CAN) ON TAKE-OFF THE ENGINE TORQUE INDICATION OBSERVERED DROPPING OFF, ABORTED TAKE-OFF. OBSERVED LEFT ENGINE SAGGING IN THE COWLING. (TC# 20060208008)Feb 1, 2002 · Dhav DHC6300SDR SWIA200210671Frame · crackedRIGHT ENGINE FRAME NR 1 CRACKED. REPLACED RIGHT FRAME NR 1 IAW SB 120-54-0036 REV 02.Jan 28, 2002 · N232SW · Emb EMB120ERSDR SWIA200210670Frame · crackedLEFT ENGINE FRAME NR 1 CRACKED. REPLACED LEFT FRAME NR 1 IAW SB 120-54-0035 REV 02.Jan 28, 2002 · N232SW · Emb EMB120ERSDR QXEA0200136Frame · chafedPDX - RT NACELLE FRAME AT STATION 177.00 INBOARD SIDE OF NACELLE IS CHAFED ON FORWARD SIDE. REPAIRED IAW DHC-8 RD 8-54-078.Jan 22, 2002 · N356PH · Dhav DHC8202SDR MALA020130Frame · corrodedDURING 4K-CHECK IN CWA, RIGHT O/B NACELLE CHAFE AT STA 197. MAINTENANCE REPAIRED CHAFE IAW MAL EO S54057 AND SAAB STATEMENT 340SDS003130.Jan 17, 2002 · N407XJ · Saab 340BSDR MWEA020025Spar · damagedREMOVE PYLON SPAR WEB (P/N 9958154-29). THE WEB HAS OVERSIZED HOLES. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932SDR F3LA200200003Frame · brokenDURING C-7 CHECK, INSPECTION REPORTED BROKEN FRAME AT NR 2 ENGINE INBOARD FIXED COWL AFT CROSSOVER RIB. REPLACED BROKEN INTERCOSTAL (FRAME) PER SRM 51-30-2, 51-30-5 AND 51-30-6.Jan 4, 2002 · N237TR · Boeing 737228SDR AWXA200200059Doubler · crackedMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK A 1/4" CRACK WAS FOUND ON DOUBLER FOR PYLON ACCESS PANEL 5727L AT NAC 216. MAINTENANCE PERFORMED HFEC INSPECTION TO IDENTIFY END OF CRACK THEN STOP DRILLED CRACK; FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW ADec 31, 2001 · N175AW · Boeing 73733ASDR DL75A011838Spar · gougedTHE FWD UPPER SPAR WEB OF THE NR 2 PYLON WAS FOUND WITH A DEEP GOUGE AT NAC STA 128 AT RBL 2. THE WEB WAS CUT FWD AND AFT OF THE DAMAGE AND THE DAMAGED SECTION OF WEB WAS REMOVED. A NEW SECTION OF WEB WAS SPLICED IN WITH ALUMINUM DOUBLERS PER ER/A 381993-14,Nov 20, 2001 · N757AT · Boeing 757212SDR UPS01437286Frame · crackedINSPECTION TYPE:C NR 4 PYLON NAC STA 221.94 ENG AFTER MOUNT BULKHEAD REAR O/B SIDE LOWER PORTION SUPPORT FRAME FOUND CRACK FROM REAR EDGE TO FWD ABOUT .75 INCH LONG APPROX AS MARKED AFTER THE AREA CLEAN UP. NR 4 PYLON NAC STA 221.94 O/B SIDE FRAME REPLACED ASNov 9, 2001 · N521UP · Boeing 747200SDR UPS01437299Frame · crackedINSPECTION TYPE:C, NR 4 PYLON (O/B STRUT) AFT TORQUE BULKHEAD VERTICAL CHORD FOUND 1 FASTENER HOLE CRACK AT CHORD FWD SURFACE RUNNING O/B AT 4 O'CLOCK POSITION APPROX .125 INCH LENGTH. CRACK HOLE REAMED ECCENTRICALLY TO 0.500 INCH AND NDT INSPECTION CONFIRMEDNov 1, 2001 · N521UP · Boeing 747200SDR CA011128016Angle · cracked(CAN) INSIDE LT AND RT MAIN LANDING GEAR WELLS, OUTBOARD SIDE WALL, ANGLE AT CORNER OF SIDE WALL AND FORWARD FACE OF MAIN SPAR WEB, LOWER END OF ANGLE. POSSIBLE NEED TO REMOVE PAINT TO NOTE CRACK. BOTH CRACKS APPROX. .75 INCHES IN LENGTH.Oct 30, 2001 · Beech C90ASDR CA011101001Mount · cracked(CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 FROM THE FASTENER TO THE AFT EDGE. RBL 8 (1.5 INCHES LONG) AND LOWER WEB EXTENDING FROM EACH ACCESS PANELS CUTOUTS R/H INBOARD FORWARD RADIUS 0.25 INCOct 10, 2001 · Cndair CL6002B19SDR SWIA200110239Frame · crackedRIGHT AND LEFT NACELLE NR 1 FRAMES CRACKED. REPLACED BOTH NACELLE NR 1 FRAMES IAW EMB120 SRM 51-10-02 AND SB 120-54-0036.Sep 21, 2001 · N214SW · Emb EMB120ERSDR AC2A076113Frame · crackedCRACKS IN FRAME. REMOVED AND REPLACED FRAME ASSY.Sep 18, 2001 · N430CV · Bell 430SDR UPS01436860Frame · wornINSPECTION TYPE:C NR 2 ENG FWD BHD FOR ENG FRONT MOUNT ATTACH, THE I/B CHORD LOWER SECTION HAS A MINOR DENT MARK WHICH WAS PREVIOUSLY SMOOTHED OUT. NDT INSP FOUND THE THICKNESS OF THE CHORD WORN OUT 25% APPROX IT'S OUT OF SRM LIMIT 54-10-01 FIG 1. THE FWD ENGISep 10, 2001 · N681UP · Boeing 747121SDR SWAA012423Frame · crackedDURING SCHEDULED A1 CHECK, FOUND NR 2 ENG PYLON STRUT AFT INBOARD CHORD CRACKED, NAC STA 354. REPAIRED CHORD PER SWA RA 1-354-0388.Aug 27, 2001 · N305SW · Boeing 7373H4SDR SWIA200110167Frame · crackedLEFT NACELLE FRAME 1 CRACKED AT INBOARD TORSION MOUNT.REPLACED LEFT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.Aug 18, 2001 · N200CD · Emb EMB120RTSDR SWIA200110166Frame · crackedRIGHT NACELLE FRAME 1 CRACKED AT OUTBOARD TORSION MOUNT.REPLACED RIGHT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.Aug 18, 2001 · N200CD · Emb EMB120RTSDR CALA0100762Spar · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 3 PYLON LOWER SPAR WEB AT FAN DUCT CUTOUT. A REPAIR ANGLE AND STIFFENER WERE INSTALLED IAW SRM 54-20-00, FIGURE 19A.Aug 15, 2001 · N59083 · Doug DC1030SDR SWIA200110189Frame · crackedRIGHT ENGINE NACELLE MOST FORWARD FRAME WORN AND CRACKED - INCLUDING CHIN COWL NUT PLATE FLANGES - OB, FROM TOP, EXTENDING DOWN TO LOWER CHIN COWL NUT PLATE FLANGE.REMOVED AND REPLACED RIGHT ENGINE NACELLE MOST FORWARD FRAME, INCLUDING CHIN COWL NUT PLATE FLANAug 3, 2001 · N189SW · Emb EMB120ERSDR SWIA200110188Frame · crackedLEFT ENGINE NACELLE MOST FORWARD FRAME IS CRACKED AT OUTBOARD PREVIOUS REPAIR.REMOVED AND REPLACED MOST FORWARD NACELLE FRAME, INCLUDING THE ATTACHED CHIN COWL ATTACHING FRAME SECTIONS IAW EMB120 SRM 51-40-02 AND 54-10-02.Aug 3, 2001 · N189SW · Emb EMB120ERSDR DHL2001365019Rib · crackedNR 2 PYLON VERTICAL STIFFENER RIB 15 HAS 2 CRACKSREPAIRED CRACKED RIB FITTING 15 ON NR 2 PYLON.Jul 17, 2001 · N365DH · Airbus A300B4203SDR DHL2001365023Rib · crackedA-7 CHECK - NR 2 PYLON O/B RIB 15 HAS RIVET MISSING AND RIB ON BACK SIDE CRACKED. REMOVED VERTICAL RIB AFT OF OVAL ACCESS DOOR ON O/B SIDE OF NR 2 ENG PYLON THD-A300-SRM-54-10.3) STOP DRILLED CRACKS ON RIB, INSTALLED REPAIR ANGLE.Jul 14, 2001 · N365DH · Airbus A300B4203SDR C2XA01IA287Frame · crackedIAH - DURING 2A INSPECTION, THE LEFT HAND NACELLE LOWER HALF FRAME FOR THE OUTBOARD AFT GEAR DOOR WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED FRAME IN ACCORDANCE WITH EMB120-SRM 54-20-04, AND THE AIRCRAFT WAS APPROVED FOR RJun 22, 2001 · N15725 · Emb EMB120ERSDR ABXA010560Spar Cap · gougedNR 4 PYLON INBOARD UPPER SPAR CAP GOUGED AT STATION YN 295. REPAIRED AREA IAW REA D854-40850-MR.Jun 4, 2001 · N818AX · Doug DC863SDR UPS01435930Rib · crackedINSPECTION TYPE:C-2, NR 1 PYLON - RESERVOIR LT STRUCTURE RIB CRACK FOUND AS MARKED. NR 1 PYLON HYD RESERVOIR LT RIB REPLACED PER SRM 51-10-01. LEAK CHECKED SATISFACTORY PER MM 29-11-00.May 11, 2001 · N671UP · Boeing 747123SDR UPS01435974Frame · crackedINSPECTION TYPE:C-2, NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LOWER SPAR FITTING FOUND 1 HOLE CRACK AT 2 O''CLOCK POSITION (LOOKING FWD) APPROX 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LWR SPAR FITTING REPAIRED AS PER HX RS R54-53-3May 8, 2001 · N671UP · Boeing 747123SDR C2XA01BT086Frame · crackedYUL---DURING 4C INSPECTION MAINTENANCE FOUND LT LOWER NACELLE FORWARD LEFTHAND ATTACHMENT BOLT MISSING. LT NACELLE FRAME CRACKED AND GUSSET BENT. LT LOWER NACELLE REMOVED, NEW EDGING FABRICATED AND INSTALLED IAW ATR42 SRM 51-12-61 FIGURE 106. LT GUSSET REPAIApr 30, 2001 · N14825 · Aerosp ATR42320SDR COMA0160363Rib · crackedTHE LT PYLON AT FS 605 IS CRACKED AT THE OUTBOARD LOWER FLANGE. REPAIRED DAMAGED AREA TO THE LT PYLON RIB AT FS 605 AT THE OUTBOARD LOWER FLANGE IAW WVAC EO 601R-54-2401A.Apr 26, 2001 · N933CA · Cndair CL6002B19SDR AWXA0001619Rib · crackedNR 2 PYLON RIB NR 14 CRACKED. DAMAGED RIB REPLACED IAW SRM 51-72-11 AND REPAIR ACTION IAW AWA ER 26-5453-01103-JS3.Apr 18, 2001 · N643AW · Airbus A320231SDR CA010522009Fitting · cracked(CAN) DURING INSPECTION NR 2 PYLON INBOARD MIDSPAR FITTING WAS FOUND CRACKED AT UPPER AFT INBOARD FASTENER HOLE. NR 2 PYLON MIDSPAR FITTING REPLACED AS PER EVA 01-767-54-4058.Apr 13, 2001 · Boeing 767375SDR CALA0100334Frame · wornINSPECTION FOUND RT ENGINE PYLON FORWARD O/B UPPER CHORD WORN. THE CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.Apr 11, 2001 · N19357 · Boeing 7373T0SDR SWAA011071Frame · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 2 ENGINE PYLON FRAME CRACKED AT STA 351.88. R&R FRAME PER SRM.Apr 6, 2001 · N664WN · Boeing 7373Y0SDR CALA0100279Frame · gougedINSPECTION FOUND NR 1 ENGINE PYLON FORWARD O/B UPPER CHORD GOUGED. THE NR 1 ENGINE PYLON O/B UPPER CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.Apr 5, 2001 · N19357 · Boeing 7373T0SDR C2XA01IA245Frame · crackedSJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FRAME 1 ON THE LEFT HAND AND RIGHT HAND NACELLES WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAMES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 3, 2001 · N57734 · Emb EMB120ERSDR AWXA0001577Rib · chafedRT PYLON L/E FAIRING FWD SEAL RETAINER AND RIB CHAFED BEYOND LIMITS. FORMED, DRILLED AND INSTALLED REPAIR ANGLE IAW SRM 51-40-3 PG1-5 AND 51-30-2 PG 2 & 3.Apr 2, 2001 · N179AW · Boeing 737277
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