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 IXXA05SMN267SSkin · elongatedDURING C CHECK INSPECTION, NR 4 PYLON UPPER PLATING HAS ELONGATED HOLES AT STA YN 254 S. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05471 DATED 10-18-05, SEMAN DWG # ED-4084 DATED 10-11-05 AND EO SEMAN # 20051341 DATED 10-18-05. REMOVED FASTENERS IAW DC8 Oct 26, 2005 · N829BX · Doug DC871FSDR 2005UALA01201Skin · damagedNR 2 ENGINE PYLON IB SIDE FWD ACCESS HOLE, DAMAGED. MAJOR REPAIR ACP ON NR 2 ENGINE PYLON INBD SIDE FWD ACCESS HOLE REF DOCK W.U.G2788H.Oct 22, 2005 · N514UA · Boeing 757222SDR UPS05845624Skin · crackedNR 4 PYLON O/B SKIN CRACKED APPROX 1 INCH LONG OB SIDE APPROX 6 INCHES AFT OF FWD BOX BULKHEAD. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5430-23086A. PERMANENT REPAIR WITHIN 10 FLT CYCLIES, D312151 ASSIGNED. ACCOMPLISHED PERMANENT REPAIR PER EO DC8-5430-23086Oct 17, 2005 · N744UP · Doug DC871FSDR AU510002089Skin · crackedUPPER AFT RT NACELLE SKIN CRACKED AND CORRODED.Oct 11, 2005 · Cessna 441SDR EIA2005168Skin · crackedNR 2 PYLON 463EL ACCESS PANEL CUTOUT SKIN CRACKED ON THE STRIKER PAD TWO FASTENER HOLES. NR 2 PYLON 463EL ACCESS PANEL CUT OUT SKIN REPAIR CARRIED OUT IAW SRM 54-30-03 FIG 7B.Oct 10, 2005 · N482EV · Boeing 747212BSDR EIA2005166Skin · crackedNUMBER 4 PYLON SKIN CRACKED AT ACCESS PANEL 483CL CUTOUT HINGE ATTACH FASTENER HOLE. NUMBER 4 PYLON 483CL ACCESS PANEL CUTOUT SKIN REPAIR CARRIED OUT IAW SRM 54-30-03 FIG 17B.Oct 10, 2005 · N482EV · Boeing 747212BSDR EIA2005236Skin · crackedLHW LE NOSE SKIN WEB FOUND CRACKED AT LBS 1116 IB OF NR 1 PYLON. REPLACED DEFECTIVE CRACKED RIB PER SRM 51-10-01, PG 9.Oct 8, 2005 · N486EV · Boeing 747212BSDR QXEA200501335Cowling · chafedPDX - LEFT LOWER COWL, 412AR, HAS CHAFE MARK ON UPPER DECK, LEFT SIDE OF INTAKE. MAINTENANCE BLENDED AREA OF CHAFE TO REMOVE DAMAGE AND MAPPED AREA FOR ENGINEERING. HFEC INSP BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51-00-02. NO CRACKS NOTED.Oct 2, 2005 · N401QX · Bombdr DHC8402SDR AALA20050685Skin · damagedAFW - LEFT HAND PYLON STRUT SKIN ON INBOARD AND OUTBOARD SIDE HAD GOUGE CAUSED BY THRUST REVERSER SEAL RETAINER BETWEEN STATION 244 TO 250 AND WATER LINE 195. DAMAGED AREA WAS 5 INCH BY 7 INCH AND 0.053 INCH DEEP. BLENDED DAMAGE AND PERFORMED HIGH FREQUENCY Sep 28, 2005 · N323AA · Boeing 767223SDR USAA051150Skin · crackedNR 1 ENG PYLON, ACCESS PNL OPENING NR 5727L. REPAIR DOUBLER INSTALLED IAW TYP REP 54-30-07, DEFECT SIZE: .400".Sep 26, 2005 · N782AU · Boeing 7374B7SDR 0509007Plate · wornENGINE NR 2 PYLON FWD SECTION WITH PLATE WORN.Sep 19, 2005 · N733TW · Boeing 7372H4SDR UIEA200500130Skin · damagedDURING D-CHECK, NR 4 PYLON HAD CRACK DAMAGE IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRECOOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACK IN THE SKIN ASep 6, 2005 · N524MC · Boeing 7472D7BSDR UIEA200500129Skin · crackedDURING D-CHECK, FOUND NR 3 PYLON, CRACKED DAMAGE WAS FOUND IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRECOOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACSep 6, 2005 · N524MC · Boeing 7472D7BSDR UIEA200500128Skin · damagedDURING D-CHECK FOUND NR 2 PYLON HAS CRACK DAMAGE IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRE-COOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVED CRACKS. THE CRACK IN THESep 6, 2005 · N524MC · Boeing 7472D7BSDR UIEA200500127Skin · crackedDURING D-CHECK, NR 1 PYLON HAD CRACK DAMAGE IN THE SKIN ASSEMBLY AND THE ADJACENT NR 3 STIFFENER, AT PRECOOLER EXHAUST CUTOUT LOWER EDGE NEAR THE AFT CORNER AT STATION 248. THE NR 3 STIFFENER LOWER FLANGE WAS TRIMMED TO REMOVE CRACKS. THE CRACK IN THE SKIN Sep 6, 2005 · N524MC · Boeing 7472D7BSDR 2005UALA00930Skin · damagedNR 1 PYLON OB SKIN DAMAGED. REPAIRED PER SRM 54-31-99.Sep 3, 2005 · N511UA · Boeing 757222SDR UIEA200500123Skin · chafedD-CHECK, DURING MAINTENANCE INSPECTION, THE NR 2 STRUT RT SIDE SKIN ASSEMBLY INTERNAL BONDED DOUBLER WAS FOUND CHAFED AT THE 463AR ACCESS PANEL CUTOUT. THE INTERNAL DOUBLER AND SKIN WERE TRIMMED BACK PAST THE EXISTING CUTOUT IN THE OUTER SKIN. THE REPAIR AREAug 30, 2005 · N524MC · Boeing 7472D7BSDR 08202005BCowling · departedRT ENG AC SCOOP DEPARTED AIRCRAFT. A/C RELEASED FOR FERRY FLIGHT FROM PIT TO ALB. REMOVED AND REPLACED RT ENG COWLINGS, ROBBED COWLINGS OFF 307CE IN ALB.Aug 20, 2005 · N237MJ · Saab 340BSDR USAA051030Skin · damagedCLT - Q6 - PYLON SKIN, 1.3 INCH, GROOVE IB SIDE OF NR 2 ENGINE PYLON AT WING L/E JUNCTION. REPAIRED IAW TYPICAL REPAIR IAW TR. (K)Aug 19, 2005 · N588US · Boeing 7373B7SDR PIDA20050067Skin · dentedWITH AIRCRAFT PARKED AT GATE, JETWAY STRUCK LEFT ENGINE NACELLE LEADING EDGE AT APPROX 11:00 POSITION. REPAIRED DENT PER SRM 54-10-01 AND EA NR 54-233.Aug 19, 2005 · N750WL · Boeing 757200SDR AALA20050555Retainer · wornMCI - NUMBER ONE AND TWO ENGINE THRUST REVERSER SEAL RETAINER RUBBED INTO PYLON STRUCTURE AT TOP AFT SIDE OF BOTH INBOARD AND OUTBOARD REVERSERS FOR NUMBER TWO ENGINE AND AT TOP AFT SIDE OF INBOARD THRUST REVERSERS FOR NUMBER ONE ENGINE. BLENDED WEAR AND PERFAug 15, 2005 · N332AA · Boeing 767223SDR 05FDEA02459Skin · crackedNR 1 ENGINE UPPER COWL INNER AND OUTER SKIN IS CRACKED. REPLACED UPPER COWL TO BE INST ON WC 74C101-01.Aug 13, 2005 · N479FE · Boeing 727200SDR AALA20050537Skin · damagedAFW - LT PYLON INBOARD SIDE STRUT SKIN HAS GOUGE WHICH WAS REWORKED BEYOND LIMIT. DAMAGE WAS INDUCED BY INTERFERENCE FROM THE UPPER FIRE SEAL BRACKET. BLENDED DAMAGE AT SINGLE FASTENER LOCATION. PERFORMED HIGH FREQUENCY EDDY CURRENT INPSECTION. INSTALLED NAug 8, 2005 · N322AA · Boeing 767223SDR USAA050957Skin · crackedCLT - FOUND PYLON SKIN CRACKED 2 INCHES, RT ENGINE PYLON UNDER PANEL 5858. REMOVED DAMAGE FABRICATED AND INSTALLED DOUBLER IAW TR 57-41-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7SDR 05FDEA02172Skin · crackedONE EACH CRACK 1 INCH LONG ON EXTERNAL CORE COWL SKIN RIGHT SIDE ENGINE NR 3. REPAIR IAW SRM 54-10-00 FIG 16 VOL 1.Aug 2, 2005 · N381FE · Doug MD1010FSDR UPS05445009Skin · damagedNR 2 PYLON NAC STA 240 LOWER EDGE O/B SIDE DOUBLER HOLE CHAFED REVEALED AS MARK. NR 2 PYLON NAC STA 240 LOWER EDGE REPAIRED AS PER SRM 54-30-03 FIG 36.Jul 23, 2005 · N683UP · Boeing 747121SDR USAA050884Skin · crackedCLT - C - SKIN, .75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K)Jul 18, 2005 · N393US · Boeing 7373B7SDR CALA0500223Skin · crackedINSPECTION FOUND A 0.5 IN CRACK AT EDGE OF NR 1 PYLON SKIN PANEL OPENING NR 5724L UPPER FORWARD CORNER. SKIN REPAIRED IAW ECRA 5430-01204.Jul 17, 2005 · N14334 · Boeing 7373T0SDR CALA0500222Skin · crackedINSPECTION FOUND 0.5 IN CRACK IN 2 PLACES ON NR 1 ENGINE PYLON SKIN ON EXTERNAL SURFACE ACCESS PANEL NR 5724 CUTOUT. PYLON SKIN REPAIRED IAW ECRA 5430-01204.Jul 16, 2005 · N14334 · Boeing 7373T0SDR USAA050817Skin · crackedCLT - C3 - SKIN, .75 INCH CRACK, RT PYLON AT CORNER OF CUTOUT FOR PANEL NR 5828R, NAC, STA 166.5. INSTALLED DOUBLER IAW TYPICAL REPAIR SRM. (K)Jun 29, 2005 · N430US · Boeing 7374B7SDR SIMA200518608Skin · chafedTHE LT IB NACELLE WAS FOUND CHAFED AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR DOUBLER. WORK DONE IAW SRM. (K)Jun 29, 2005 · N301AE · Saab 340BSDR 05FDEA01682Access Panel · crackedNR 1 PYLON FUEL LINE INSIDE ACCESS PANEL 517CT HAS IMPROPER STOP DRILL INSIDE RADIUS OF WELD. CRACK APPEARS TO HAVE PROPAGATED ONTO THE WELD. REMOVED AND REINSTALLED AFTER REPAIR PER TRAVELER T5/522336 NR 1 PYLON FUEL LINE INSIDE ACCESS 517CT IAW MM 20-50-Jun 24, 2005 · N391FE · Doug MD1010FSDR JRAA587062305Skin Panel · corrodedSURFACE CORROSION WAS FOUND ON THE RT IB SKIN PANEL AT APPROX STA 96.91. THIS CORRODION WAS NOTED UNDER THE INSULATION PANEL LOWER SIDE. REPLACEMENT OF SKIN PANEL IN PROGRESS. (K)Jun 23, 2005 · N587CA · Cvac 640340DSDR P5CA0501372Skin · crackedCRACK AT NR 4 NACELLE STRUT TOP FORWARD CORNER OF PRECOOLER EXHAUST CUTOUT. PRECOOLER EXHAUST CUTOUT REPAIRED PER BOEING INSTRUCTIONS 1-1MNS9D AND FAA FORM 8100-9.Jun 22, 2005 · N509MC · Boeing 747230BSDR P5CA0501371Skin · wornWORN/CHAFING NR 3 NACELLE STRUT SKIN AROUND CUTOUT NR 12. NR 3 NACELLE STRUT SKIN AROUND CUTOUT REPAIRED PER BOEING INSTRUCTIONS 1-1MNB95 AND FAA FORM 8100-9.Jun 22, 2005 · N509MC · Boeing 747230BSDR USAA050752Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, RT PYLON SKIN AT NACELLE STATION 216 ACCESS PANEL 5827R. ACCOMPLISHED DOUBLER REPAIR IAW EA 96659. (M)Jun 10, 2005 · N389US · Boeing 7373B7SDR 05FDEA01555Skin · damagedNR 1 ENGINE, NOSE COWL AT APPROXIMATELY SEVEN O' CLOCK POSITION EXTERIOR SURFACE FOUND WAVINESS. NR 1 ENGINE, NOSE COWL REMOVED AND REPLACED PER AMM 71-11-01-4.Jun 9, 2005 · N584FE · Doug MD11SDR CA050823003Skin Panel · corroded(CAN) SEVER CORROSION FOUND BETWEEN BONDED MEMBERS OF THE SKIN PANEL ASSY STRETCHING THRU THE ENTIRE LENGTH OF THE PANEL.Jun 8, 2005 · Beech 1900DSDR AWXA200500762Skin · damagedDURING C-10 CHECK, DRILL DAMAGE OCCURRED TO FASTENER HOLE ON RT WING PYLON SIDE LOAD FITTING AT BL 9R, 3RD HOLE FROM AFT END ON OUTBOARD SIDE OF FITTING. MAINTENANCE SPOT FACED AND REMOVED DAMAGE FROM DISCREPANT HOLE IAW AMERICA WEST AIRLINES (AWA) ENGINEERINJun 8, 2005 · N905AW · Boeing 7572S7SDR AWXA200500760Skin · crackedDURING C-13 CHECK, FOUND CRACK, .650 INCHES IN LENGTH, LOCATED ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R, ON THE NR 2 PYLON. MAINTENANCE STOP DRILLED CRACK ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R IAW AMERICA WEST AIRLINES ENGINEERING REQUEST (ER) NR 03-54Jun 8, 2005 · N328AW · Boeing 7373B7SDR AWXA200500742Skin · crackedFOUND TOP LT PYLON CRACKED AT ACCESS PANEL 5727L. MAINTENANCE STOP DRILLED CRACK AT LT PYLON PANEL 5727L AND INSTALLED DOUBLER AT LT PYLON ACCESS PANEL 5727L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5430-05166-SS1.Jun 8, 2005 · N328AW · Boeing 7373B7SDR 05FDEA01528Panel · corrodedNR 2 PYLON PNL 423EL HAS SEVERAL AREAS OF CORROSION AND WEAR MARKS ALONG FASTENER HOLES IN EDGE OF PANELS. REMOVED CORROSION AND WEAR MARKS FROM NR 2 PYLON PNL NR 423EL IAW A310-200 SRM 51-74-10. MATERIAL LOSS IS OUT OF LIMITS IAW A310-200 SRM 54-50-00. RJun 7, 2005 · N404FE · Airbus A310SDR P5CA0501355Skin · crackedNR 4 PYLON INBOARD ACCESS PANEL CUTOUT AT NAC STATION 275-295 CRACKED AT EDGE. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1HGUJB AND FAA FORM 8100-3.May 18, 2005 · N508MC · Boeing 747230BSDR P5CA0501354Skin · wornNR 2 PYLON INBOARD ACCESS PANEL CUTOUT AT NAC STATION 280-300 WORN AT EDGE. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1IO8DO AND FAA FORM 8100-3.May 18, 2005 · N508MC · Boeing 747230BSDR P5CA0501351Skin · crackedNR 2, 3 AND 4 PYLON PRECOOLER CUTOUT CRACKED AT AFT LOWER CORNER. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1I08HV AND FAA FORM 8100-3.May 18, 2005 · N508MC · Boeing 747230BSDR DL75K050283Skin · crackedAPPROX 1 INCH CRACK IN PYLON TORQUE BOX INBOARD SIDE, UPPER FWD CORNER OF FWD ACCESS HOLE, PREVIOUSLY STOP DRILLED. REFERENCE NR CARD 291 PSV 17 CHECK. INSTALLED PERMANENT REPAIR PER SRM 54-51-01D FIG 203.May 12, 2005 · N645DL · Boeing 757232SDR DJFA2005089Panel · bentWHILE CLIMBING OUT OF 11,000 FT FOR 23,000 FT, AIRCRAFT MADE AN IMMEDIATE LEFT BANK/YAW OF 35 DEGREES AND THE AUTO-PILOT DISCONNECTED. AIRCRAFT WAS HAND FLOWN TO STRAIGHT AND LEVEL AND CREW DECLARED AN EMERGENCY. THE CREW REPORTED THAT THE AIRCRAFT WAS FISH May 5, 2005 · N722TA · Raythn HAWKER800XPSDR QXEA200500858Skin · gougedYYC - LEFT NACELLE LIP SKIN HAS GOUGES AND SCRATCHES AT 6 O'CLOCK POSITION. REPAIRED IAW CRJ-700 SRM 54-11-01-201-001-A01 AND SRM 51-21-11-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500857Skin · gougedYYC - RIGHT NACELLE LIPSKIN HAS GOUGES BETWEEN 3 AND 6 O'CLOCK POSITION. REPAIRED IAW CRJ-700 SRM 54-11-01-201-001-A01 AND SRM 51-21-11-001-001-A01.May 2, 2005 · N611QX · Cndair CL6002C10SDR USAA050562Skin · crackedCLT - FOUND SKIN CRACKED .500 INCH, NR 1 PYLON, INBOARD SIDE, AFT ACCESS PANEL 5724 CUTOUT, LOWER AFT CORNER. INSTALLED DOUBLER IAW TR 54-50-07. (M)Apr 28, 2005 · N439US · Boeing 7374B7
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