JASC 5414

Service difficulty reports · 4,361

Reports filed under 5414 · Nacelle/Pylon, 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 = '5414'
  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 UIEA200500065Pylon · crackedLT WING NR 1 PYLON STRUT DOOR 453BL UPPER CORNER CRACKED. (K)Apr 26, 2005 · N536MC · Boeing 747228FSDR CALA0500117Skin · crackedCRACK IN PYLON SKIN AT 5727L LEFT UPPER PYLON. INSTALLED DOUBLER PER ECRA 5430-01230.Apr 25, 2005 · N12319 · Boeing 7373T0SDR USAA050517Doubler · crackedCLT - FOUND SKIN DOUBLER CRACKED .250 INCH, LEFT PYLON AT PANEL 5738L. STOP DRILLED AND ROUTED OUT DAMAGE PER TR 54-30-07 AND EA 96511. (M)Apr 21, 2005 · N422US · Boeing 737401SDR UIEA200500054Nose Cowl · dentedENGINE 1 NOSE COWL AT 4 O`CLOCK POSITION DENT AT LIP 5.6 INCHES X 4.2 INCHES X 0.224 INCH. DENTED AREA TRIMMED OUT AND SRM WAS PERFORMED. INSTALLED DOUBLER AND FILLER IAW SRM USING BLIND .1562 FASTENERS. (K)Apr 21, 2005 · N412MC · Boeing 74747UFSDR QXEA200500776Skin · gougedYYC-RIGHT NACELLE LIP SKIN HAS GOUGES BETWEEN 3 AND 5 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 54-11-05-101-001-A01, AND 51-21-11-001-001-A01.Apr 14, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500778Skin · damagedYYC-RIGHT PYLON, TOP SIDE, CENTER SECTION MISSING AREA OF PAINT. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01.Apr 13, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500777Skin · gougedYYC - LEFT NACELLE LIPSKIN HAS GOUGES BETWEEN 6 AND 8 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 54-11-08-101-001-A01, AND 51-21-11-001-001-A01.Apr 13, 2005 · N614QX · Cndair CL6002C10SDR UIEA200500048Skin · crackedD-CHECK, DURING SCHEDULE INSPECTION, CRACK DAMAGE WAS FOUND IN THE SKIN ASSY AND THE ADJACENT NR 3 STIFFENER AT PRE-COOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STA 248 ON THE RT SIDE. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. Apr 5, 2005 · N537MC · Boeing 747271CSDR 05FDEA00766Panel · corrodedOFF AIRCRAFT PART, NR 1 PYLON ACCESS PANEL NR 413BL HAS MODERATE CORROSION AROUND ALL FASTENERS HOLES INTERIOR SIDE OF PANEL. REPLACED PANEL ASSY IAW A310-200 SRM 51-72-10.Mar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00737Access Panel · corrodedNR 2 PYLON ACCESS PANEL NR 423EL HAS MODERATE CORROSION AROUND INTERIOR SIDE OF ALL FASTENER HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10, VERIFIED THREE AREAS OUT OF LIMITS. VERIFIED REPAIR MATERIAL, FABBED THREE EA. REPAIR DOUBLERS AND FILLERS IAW Mar 31, 2005 · N402FE · Airbus A310SDR UIEA200500042Skin · crackedD-CHECK, DURING SCHEDULE INSPECTION, NR 3 PYLON, A 2.25 INCH CRACK WAS FOUND AT THE TOP EDGE OF SKIN ASSY AT NAC WL147.8, JUST FORWARD OF THE NAC STA 286. CRACK IN THE SKIN ASSY WAS CONTAINED WITH A 1.0 INCH DIAMETER HOLE AT THE CRACK TIP. REPAIR AREA WAS NDMar 29, 2005 · N537MC · Boeing 747271CSDR UIEA200500041Skin · crackedD-CHECK, DURING SCHEDULE INSPECTION. THE STRUT SKIN ASSY EDGE ADJACENT TO THE PRECOOLER EXHAUST CUTOUT WAS FOUND CRACKED. SKIN ASSY INSPECTION CONFIRMED THAT CRACKS TERMINATED IN EXISTING FASTENER HOLES. NR3 STIFFENER WAS REINFORCED WITH A STEEL LOWER REPAIMar 28, 2005 · N537MC · Boeing 747271CSDR 05FDEA00664Panel · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. NR 2 ENGINE NACELLE ENGINE EXHAUST TO NACELLE TRANSITION PANEL 30 INCHES FWD OF AFT. ITEM 46 OF LIST. REMOVED DOUBLER IAW A310-200 SRM 51-4-21 TO EVALUATE REPAIR FOR SRM CONFORMar 28, 2005 · N419FE · Airbus A310222SDR UIEA200500034Skin · dentedDURING INSPECTION, FOUND DENT (SKIN WRINKLE) NR 2 NACELLE STRUT INBOARD SKIN BETWEEN NACELLE STATION 286 TO 300.1. CONFIRMED THAT THE AFFECTED WAS FREE FROM DISCOLORATION. NDT CONDUCTIVITY MEASURED READING ACCOMPLISHED. HFEC INSPECTED AND WAS FOUND TO BE DAMar 23, 2005 · N527MC · Boeing 7472D7BSDR QXEA200500581Skin · crackedYYC - LEFT ENGINE TRAILING EDGE TRANSCOWL FORWARD EDGE WORN ON BOTTOM CRACKED ON TOP AT 2 O'CLOCK AND 4 O'CLOCK POSITIONS. REPAIRED IAW REO 670-78-33-347 AND HORIZON AIR EA R-78-26.Mar 22, 2005 · N612QX · Cndair CL6002C10SDR QXEA200500582Skin · scratchedYYC - LEFT NACELLE, AFT CORE COWL, UPPER INBOARD SIDE HAS NUMEROUS SCRATCHES. REPAIRED IAW CRJ700 SRM 54-13-00-101-001-A01 AND SRM 51-12-00-001-001-A01.Mar 21, 2005 · N612QX · Cndair CL6002C10SDR QXEA200500568Skin · gougedYYC - RIGHTHAND NACELLE LIPSKIN GOUGED BETWEEN 3 AND 5 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 51-21-11-001-A01.Mar 21, 2005 · N612QX · Cndair CL6002C10SDR UIEA200500022Panel · crackedNR 2 PYLON OUTBOARD SIDE CUTOUT FOR PANEL 463CL HAS A .875 INCH CRACK AT AFT CORNER OF SKIN. CRACK WAS NDT INSPECTED TO VERIFY AREA OF CRACK AS PER B747 NDT MANUAL PART 6 51-00-00 FIG 23. STOP DRILLED CRACK IAW B747 SRM 51-10-01 PAGE 12. HFEC INSPECTED STOPMar 16, 2005 · N505MC · Boeing 7472D3BSDR DHL2005782568Skin · dentedC-CHECK, DENT NR 1 ENGINE PYLON SKIN UPPER SURFACE 7 INCHES AFT OF STA 1303 STR 14L. DENT IS CREASED, FOUND TO BE OUT OF LIMITS ON PYLON NR 1 UPPER SKIN SURFACE 7 INCHES AFT OF STA 1303 STR 14L IAW B727 SRM 54-10-1 FIG 1. CUT OUT DAMAGE AREA SIZE .75 INCH X Mar 13, 2005 · N782DH · Boeing 727227SDR A6WA200540093Skin · damagedDURING POST FLIGHT WALK AROUND, RIGHT ENGINE COWLING DISCOVERED POSSIBLY OPENED IN FLIGHT. DAMAGED NOTED. (M) REMOVED AND REPLACED DOOR INSTALL LOWER CORE COWL. OPS CHECK GOOD. (K)Mar 11, 2005 · N419AW · Cndair CL6002B19SDR AU510002015Panel · damagedNR 1 ENGINE LT FORWARD LOWER CARBON FIBER PANEL P/N UL37842 DAMAGED. FORWARD SUPPORT BRACKETS (2OFF) P/N UL24084A FOUND SHEARED/CRACKED TO COMPRESSOR CASING. CORE PANEL SUPPORT BRACKETS (3OFF) UNSERVICEABLE. LT LOWER `A` FRAME TO CORE CUFF PANELS DAMAGED/MIMar 10, 2005 · Boeing 747438SDR UPS05444191Frame · crackedINSPECTION TYPE:C NR 3 PYLON NAC STA 250 O/B FRAME LOWER TO WEB ATTACHMENT AREA CRACKED, LENGTH 1.5 INCH. FRAME REPAIRED AT LOWER PORTION AS PER SRM 54-10-03 FIG 1.Mar 10, 2005 · N682UP · Boeing 747121SDR 0500325530Skin Panel · crackedDURING H-CHECK FOUND CRACK IN NR 2 PYLON RT SIDE SKIN PANEL NACELLE STA 136. REPAIRED PER EA 55-202910.Mar 9, 2005 · N530US · Boeing 757251SDR UIEA200500016Skin · crackedDURING INSPECTION, NR 4 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO STATION 254. THE RIB INSTALLATION ATMar 8, 2005 · N527MC · Boeing 7472D7BSDR UIEA200500015Skin · crackedDURING INSPECTION, NR 3 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO 254. THE RIB INSTALLATION AT NACELLEMar 8, 2005 · N527MC · Boeing 7472D7BSDR UIEA200500014Skin · crackedDURING INSPECTION, NR 2 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NS 235 TO STA 254. THE RIB INSTALLATION AT NACELLE STATION Mar 8, 2005 · N527MC · Boeing 7472D7BSDR SWAA050699Plate · crackedDURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENG PYLON UPPER PLATE CRACKED AT STA 234.5. REMOVED AND REPLACED PLATE PER SRM.Mar 6, 2005 · N334SW · Boeing 7373H4SDR ABXA050068Panel · crackedDURING ROUTINE LINE MAINTENANCE AT ILN, FOUND A 2.250 INCH CRACK IN NR 2 PYLON OUTBOARD PLANK AT STA YN300. REPAIRED PYLON PLANK IAW ABX AIR REA D853-51551-MR USING 17-7 PH .080 INCH, PO 408448907.Mar 5, 2005 · N853AX · Doug DC861SDR QXEA200500476Panel · chafedYYC - LEFT HAND PYLON PANEL 412JB END EDGE HAS CHAFE MARK. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01, REO 670-54-52-013 AND HORIZON AIR EA R-54-76.Mar 3, 2005 · N605QX · Cndair CL6002C10SDR MALA050248Stiffener · crackedDURING C2 CHECK IN YYC FOUND NR 4 ENGINE FWD NOSE COWL BULKHEAD 4 CRACKED STIFFENERS. ITEM 5 P/N HC716H0022-219, ITEM 6 P/N HC716H0022-208, ITEM 22 P/N HC716H0022-230. ITEM 31 P/N HC716H0022-214.Mar 1, 2005 · N502XJ · Bac AVRO146RJ85ASDR QXEA200500513Skin · scratchedYYC - LEFT HAND NACELLE AFT CORE COWL SCRATCHED ON OUTBOARD SIDE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 54-13-00-101-001-A01, AND SRM 51-21-11-001-001-A01.Feb 26, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500432Skin · gougedYYC - LEFT HAND NACELLE LIP SKIN GOUGED BETWEEN 7 AND 8 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 54-11-05-101-001-A01.Feb 25, 2005 · N605QX · Cndair CL6002C10SDR QXEA200500347Skin · crackedPDX - RIGHT NACELLE SKIN CRACKED FORWARD OUTBOARD CORNER OF WHEEL WELL APERTURE. REPAIRED IAW RD 8-54-72.Feb 21, 2005 · N363PH · Dhav DHC8202SDR QXEA200500242Skin · gougedYYC - LEFTHAND ENGINE NACELLE, LIP SKIN GOUGED AT 3, 5 AND 11 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 54-11-05-101-001-A01 AND 54-11-01-201-001-A01.Feb 14, 2005 · N609QX · Cndair CL6002C10SDR QXEA200500241Skin · gougedYYC - RT ENGINE NACELLE LIP SKIN GOUGED AT 3, 5, 9 AND 12 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 53-11-05-101-001-A01 AND 54-11-01-201-001-A01.Feb 14, 2005 · N609QX · Cndair CL6002C10SDR AU510001871Skin · crackedRT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT AND THROUGH RIVET HOLE. CRACK CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 58.4MM (2.3IN). CRACK ALSO EXISTS IN INTERNAL DOUBLER AS WELL.Feb 9, 2005 · Boeing 767338SDR QXEA200500367Panel · crackedYYC - LEFTHAND NACELLE LOWER AFT COWL PANEL, CHANNEL STATION XN302 IS CRACKED AT UPPER FLANGE. REPAIRED IAW RD 8/4-54-033.Jan 24, 2005 · N539DS · Bombdr DHC8401SDR 0500095511Skin · crackedDURING L-CHECK, FOUND CRACK IN NR 2 STRUT SKIN. REPAIRED PER EA 55-201934.Jan 20, 2005 · N511US · Boeing 757251SDR 05FDEA00118Skin · dentedINSPECTED UPPER AND LOWER SKINS, FOUND NO DAMAGE ON UPPER SKIN, LOWER SKIN HAS MINOR DAMAGE IN SKIN SURFACE NEAR FWD LT CORNER. REPAIRED SKIN DAMAGE.Jan 17, 2005 · N409FE · Airbus A310203SDR 05FDEA00115Skin · corrodedNR 2 ENGINE INLET INNER SKIN DAMAGED 16.5 IN FWD OF ACCESS DOOR LBL 2. REPAIRED PER SRM 54-10-3 FIG. 7Jan 17, 2005 · N465FE · Boeing 727200SDR USAA050151Skin · crackedPIT - Q6 - PYLON STRUT SKIN, .7500 INCH CRACK; PYLON STRUT SKIN FOR LT ENGINE, ACCESS PANEL CUTOUT. STOP DRILL OF CRACK AND INSTALLATION AT DOUBLER IAW TYP REP 54-30-07. (K)Jan 13, 2005 · N521AU · Boeing 7373B7SDR UPS05243777Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW SRM 51-40-20.Jan 6, 2005 · N940UP · Boeing 727185CSDR UPS05243776Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW MM 20-60-04.Jan 6, 2005 · N940UP · Boeing 727185CSDR SWIA200414400Skin · corrodedTWO METAL PLATES CORRODED ON TOP SKIN OF THE RIGHT NACELLE FS 736 AND 7 INCHES FWD OF T/E OF NACELLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51-22-46.Dec 20, 2004 · N591SW · Cndair CL6002B19SDR SWIA200414398Skin · corrodedTWO METAL PLATES CORRODED ON TOP SKIN OF THE LEFT NACELLE/PYLON FS 736 AND 7 INCHES FWD OF T/E OF THE NACELLE/PYLON. ITEM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51Dec 20, 2004 · N591SW · Cndair CL6002B19SDR CALA0400749Panel · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN NR 2 PYLON PANEL CUTOUT 5824R. THE CRACKS WERE LOCATED AT UPPER FORWARD CORNER OF PANEL. ONE CRACK ORIGINATED FROM RIVET HOLE FOR RUB STRIP AND THE OTHER WAS ON FAYING SURFACE FOR ACCESS PANEL.Dec 18, 2004 · N61304 · Boeing 7373T0SDR DHL2005362501Skin · corrodedDURING "C" CHECK, FOUND RT WING IB SIDE PYLON NR 2 WING T/E LWR SIDE ACCESS PANEL, CLOSE PYLON RIB 22 PANEL CUT OUT HAS CORROSION. REMOVED PREVIOUS REPAIR FOR ACCESS TO REMOVE CORROSION AREA RT WING I/B SIDE PYLON NR 2 T/E LWR SIDE. CLEANED & REMOVED CORROSIDec 6, 2004 · N362DH · Airbus A300B4203SDR 04FDEA03344Skin · crackedPYLON LOWER SPAR, INSP FOR COMPLY WITH E.O. 6-5450-7-3302 REV NO. B3 POS PT3 ENT BY: 067708. NR 1 PYLON, LOWER AFT FAIRING WITH LOOSE RVTS, CRK'D AND PAINT IN BAD CONDITION. LOWER FAIRING REPAIRED IAW EA 6-5480-81814. REINSTALLED IAW AMM 54-55-00. PAINTEDDec 5, 2004 · N452FE · Airbus A310SDR UIEA200400192Skin · crackedDURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSY FORWARD ANGLE FRAME OF THE NR 2 PYLON LT AND RT SIDE WERE FOUND CRACKED. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY Nov 15, 2004 · N512MC · Boeing 747230BSDR QXEA200400794Skin · damagedPDX - LEFT HAND NACELLE OUTBOARD SIDE ZONE 413 THREE RIVETS PULLED THROUGH SIDE SKIN IMMEDIATELY AFT OF CRACKED INTERCOSTAL. REPAIRED IAW SRM 51-42-05-800-801.Nov 13, 2004 · N406QX · Bombdr DHC8401
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