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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR 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.SDR 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 DC8-5430-23086SDR AU510002089Skin · crackedUPPER AFT RT NACELLE SKIN CRACKED AND CORRODED.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SDR USAA051150Skin · crackedNR 1 ENG PYLON, ACCESS PNL OPENING NR 5727L. REPAIR DOUBLER INSTALLED IAW TYP REP 54-30-07, DEFECT SIZE: .400".SDR 0509007Plate · wornENGINE NR 2 PYLON FWD SECTION WITH PLATE WORN.SDR 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 ASDR 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 CRACSDR 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 THESDR 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 SDR 2005UALA00930Skin · damagedNR 1 PYLON OB SKIN DAMAGED. REPAIRED PER SRM 54-31-99.SDR 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 ARESDR 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.SDR 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)SDR 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.SDR 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 PERFSDR 05FDEA02459Skin · crackedNR 1 ENGINE UPPER COWL INNER AND OUTER SKIN IS CRACKED. REPLACED UPPER COWL TO BE INST ON WC 74C101-01.SDR 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 NSDR 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)SDR 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.SDR 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.SDR USAA050884Skin · crackedCLT - C - SKIN, .75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K)SDR 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.SDR 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.SDR 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)SDR 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)SDR 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-SDR 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)SDR 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.SDR 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.SDR USAA050752Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, RT PYLON SKIN AT NACELLE STATION 216 ACCESS PANEL 5827R. ACCOMPLISHED DOUBLER REPAIR IAW EA 96659. (M)SDR 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.SDR CA050823003Skin Panel · corroded(CAN) SEVER CORROSION FOUND BETWEEN BONDED MEMBERS OF THE SKIN PANEL ASSY STRETCHING THRU THE ENTIRE LENGTH OF THE PANEL.SDR 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) ENGINEERINSDR 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 03-54SDR 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.SDR 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. RSDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SDR 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.SDR 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.SDR 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)
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