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 UPS06547577Skin · damagedINSPECTION TYPE:C NR 2 ENG PYLON AFT FAIRING, O/B FWD SKIN-END DAMAGED. NR 2 ENG PYLON AFT FAIRING, O/B FWD SKIN REPAIR HAS BEEN ACCOMPLISHED PER FINAL EA 757-5451-27-A1505 AND UPS ENGINEERING FILE NUMBER: 757-54-20056.SDR USAA060877Skin · crackedLEFT PYLON PANEL 5727L CRACKED. INSTALLED DOUBLER KIT IAW TR 54-30-07, DEFECT SIZE: .625 INCH.SDR AWXA200601169Skin Panel · lightning strikeFOUND LIGHTNING STRIKE, FLOOR PANEL ON RIVET EXTERNAL FUSELAGE AT FRAME 2L 2171 CM APPROX. PERFORMED PERMANENT REPAIRS ON EXTERNAL FUSELAGE FRAME 2L Z + 71 CM APPROX IAW SRM A319 53-00-11 PAGE 353 TO 362 FIG 223 SHEET 2.SDR AWXA200601116Skin · dentedTRAINING EDGE OF ELEVATOR UPPER SURFACE LEFT THIS TO 24 " OB OF RIB 8 L= 1 BY W = 4 APPROXIMATELY. REPAIRED IAW SRM A 320 - 55 - 21 - 11 FIG 213. PROTECTIVE TREATMENT APPLIED SAW SRM 51-21-11.SDR UIEA200600162Skin · crackedFOUND 1 CRACK ON NR 4 PYLON PRECOOLER EXHAUST SKIN CUTOUT. REPORT CRACK, REMOVED PER SRM 51-10-01. REPAIR CARRIED OUT PER BOEING SERVICE ID NR 1-198251549-11.SDR THMN4165SQ123Skin · crackedLT ENGINE COWL CRACKED AT FWD FASTENER. MADE AIRWORTHY REPAIR IAW PA-39 SRM CHAPTER 4 PG 1F6 AND AC43.13-1B SECTION 4 PARAGRAPH 4-57 FIGURE 4-6 AND SECTION 4 PARAGRAPH 4-58 FIGURE 4-16.SDR UIEA200600165Skin · crackedFOUND 2 CRACKS ON NR 2 PYLON PRECOOLER EXHAUST SKIN CUTOUT. REMOVED, REPORTED CRACK AND CARRIED OUT REPAIR PER BOEING RESPONSE MSG NR 1-198251446-7.SDR UIEA200600164Skin · crackedFOUND 2 CRACKS ON NR 1 PYLON PRECOOLER EXHAUST SKIN CUTOUT. T-CHORD ON CUTOUT FOUND CRACK. REPORTED CRACKS, REMOVED PER BOEING RESPONSE MSG =1-200634469-2 AND 1-200634469-5. REPAIR CARRIED OUT ON NR 1 PYLON PRECOOLER CUTOUT PER BOEING RESPONSE MSG = 1-20063SDR USAA060859Skin · damagedNR 1 ENGINE PYLON AFT EXTERNAL SKIN, PPSTA 174.3 TO 185.35. INSTALLED REPAIR DOUBLER TO NR 1 ENGINE, PYLON PER EA 97775 AND 97726, DEFECT SIZE: 6" BY 6".SDR KCSA061180Skin · crackedNR 2 PYLON EXTERNAL SKIN HAS A 2 INCH CRACK INBOARD SIDE BELOW DOUBLER JUST FORWARD OF NAC STA 180.SDR UIEA200600133Panel · crackedNR 1 PYLON STRUT FAIRING PANEL 4541R CRACKED.SDR UIEA200600129Panel · missingON ARR, FOUND ON ENGINE NR 2 INBOARD PYLON PANEL 462RL MISSING. INSP LT FLAPS AND STABILIZER NO DAMAGE FOUND. REPLACED PANEL 462RL ON ENGINE NR 2, OK FOR SERVICE.SDR AALA20060437Skin · damagedAFW - LEFT AND RIGHT PYLON OUTBOARD SKIN AT STATION 250 HAD GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. AREA WAS 6 INCHES BY .7 INCH WITH A DEPTH OF .125 INCH AND WAS SIX INCHES LONG. DAMAGE WAS BLENDED PER SRM. A HIGH FREQUENCY EDDY CURRENT INSPECTION SDR QXEA200601424Skin · crackedPDX - C4 NR 2 NACELLE HAS A .5 INCH LONG HORIZONTAL CRACK ON OUTBOARD SKIN AT APPROXIMATELY STATION XN125 AND ZN0.08. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND RD 8-54-1193, STEPS 1-9.SDR USAA060730Panel · damagedFOUND HEAT DAMAGE PP STA 174.35 TO PP STA 184, OUTBOARD PYLON AFT NR 1 PANEL. INSTALLED DOUBLER IAW EA 97710, DEFECT SIZE: 6.0 BY 6.0.SDR EIAA200605001Skin · crackedNR 3 PYLON, NAC STA. 247, NR 3 STIFFENER AND SKIN CRACKED. FABED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2 (MZJ).SDR EIA2006229Skin · crackedNR 2 PYLON, NACELLE STATION 247, NR 3 STIFFENER AND SKIN, CRACKED. FABED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2.SDR EIA2006096Skin · crackedNR 1 PYLON, NAC STA 247 NR 3 STIFFENER AND SKIN CRACKED. FABBED & INSTALLED REPAIRS PER ECRA 489-54-007-2.SDR TAMF20060026SSkin · crackedDURING (C) CHECK INSPECTION WAS FOUND CRACK AT SKIN ENGINE 1 LT AT FRAME AT NAC STA 274 - CF6-80C2. DAMAGE WAS REPAIRED IAW EWO 767-54-004 AND MFG REFERENCE CV06-1004-01.SDR TAMF20060021SDoubler · corrodedDURING INSPECTION ON C CHECK FOUND CORROSION AT SKIN DOUBLER. CORRODED AREA WAS REPAIRED IAW EWO 767 54-001, BOEING SERVICE REQUEST 1-194658477 AND SRM 54-52-01 FIGURE 201.SDR TAMF20060025SSkin · crackedDURING C CHECK INSPECTION WAS FOUND CRACK AT SKIN, ENGINE 1 LT AT FRAME AT NAC STA 274. DAMAGE WAS REPAIRED IAW EWO 767 54-003 AND GOODRICH AEROSTRUCTURES REFERENCE CV06-0985-02.SDR F3LA200600035Fairing · crackedDURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE PYLON AFT LOWER FAIRING CRACKED. REPAIRED LOWER ENGINE PYLON FAIRING BY WELD PER EA A0-54T-11332. PERFORMED FLUORESCENT PENETRATE CHECK PER NDT MANUAL PART 6-51-80-00, PAGES 801-809.SDR HALA0600382Access Panel · missingNR 1 ENG PYLON ACCESS PANEL I/B SIDE MISSING ON A/C ARRIVAL (PANEL 436AR). INSTALLED NR 1 PYLON ACCESS PANEL.SDR F3LA200600045Panel · crackedDURING C-4 CHECK, INSPECTION REPORTED LT PYLON PANEL 473AL CRACKED ON RADIUS OF INNER DOUBLER. STOP DRILLED CRACK AND WELDED PER EA A9-54R-11430. PERFORMED HFEC, NO DISCREPANCIES NOTED.SDR SIMA200613203Skin · damagedOIL ACCESS PANEL NR 1 ENGINE IS MISSING, DEPARTED AIRCRAFT INFLIGHT CAUSING A 6-8 INCH TEAR IN NACELLE AND A DENT WITH SEVERAL SCRATCHES. REPLACED ENGINE 1 LOWER COWL AND BLEED AIR DUCT ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2006UALA00919Skin · crackedNR 1 STRUT SIDE SKIN PNL FWD TORQUE BOX ACCESS HOLE HAS CRACK ON THE TOP SIDE. REPAIR DOUBLER PER SRM54-53-01, REPAIR 6 WAS INSTALLED, WITH 1 EXTRA ROW OF REPAIR FASTENERS.SDR UIEA200600114Skin · crackedNR 1 PYLON RIGHT SIDE SKIN ASSEMBLY WAS FOUND CRACKED IN THE AREA COVERED BY TITANIUM DOUBLERS. INTERIM REPAIR FOR THE NR 1 PYLON 65B94100 SKIN ASSEMBLY, WAS ACCOMPLISHED AS PER BOEING MESSAGE 1-178658112 AND FAA FORM 8100-9.SDR UIEA200600113Skin · crackedDURING A C-CHECK, CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER AND PRE-COOLER EXHAUST CUT OUT EDGE ADJACENT TO N.S. 248 NR 2 PYLON. INTERIM REPAIR AS AN AMOC TO AD 95-13-07, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES OF THE NRSDR UIEA200600111Skin · crackedTHE CRACKS WERE FOUND IN THE SUBJECT STRUT CAP SKIN ASSEMBLY AND ADJACENT BULKHEAD STRAP AT STA-286 BULKHEAD INSTALLATION CROWN AREA AT B-L. 0-0. THE AFT EDGE OF CAP SKIN ASSEMBLY. THE BULKHEAD STRAP IN AREA COMMON TO CAP SKIN. INTERIM REPAIR OF THE 65B9405SDR UIEA200600110Skin · crackedCRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER, AND PRE-COOLER EXHAUST CUT OUT ADJACENT TO THE AFT CORNER AT N.S.248, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES FOR NR 3 AND NR 4 PYLONS. INTERIM REPAIR FOR THE NR 3 AND NR 4 STRUSDR MALA060312Skin · chafedDURING 2 YEAR CHECK IN BNA FOUND THE INNER SKIN ON THE LT NACELLE AT APPROXIMATELY NS271.33 IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO S54112.SDR THMN4113SQ118Cowling · crackedRT UPPER ENGINE COWL SKIN CRACKED AT FWD SEAL BRACKET. MADE AIRWORTHY REPAIR IAW SRM 54-20-43.SDR THMN4113SQ116Cowling · crackedRT INBOARD ENGINE COWL HAS SMALL CRACK IN SKIN AT TOP/FWD CORNER. MADE AIRWORTHY REPAIR IAW DASSAULT FALCON 20 SRM 51-10-21.SDR QXEA20060152Cowling · dentedPDX - C3 THERE IS A DENT LEFT TOP FAN COWL IN BOARD SIDE. REPAIRED IAW EA R-54-108.SDR USAA060649Skin · crackedFOUND LT PYLON CRACKED. BONDED DOUBLER AT AFT OUT/BD CORNER. REPAIRED IAW SRM 54-30-07, DEFECT SIZE: .500".SDR CA060425019Skin · crackedVISUAL INSPECTION INDICATED A CRACK ON LT ENGINE NACELLE IB SKIN JUST FORWARD OF WING LEADING EDGE. CRACK RAN VERTICALLY JUST AFT OF IB NACELLE INSPECTION PANEL. A RIVET THAT ATTACHES THE NACELLE FILLET STRIP TO THE WING WAS INCLUDED IN THE CRACK. THERE WASSDR EIA2006102Skin · brokenNR 2 PYLON I/B NAC STA 286 LOWER ACCESS DOOR AREA CUTOUT HAS BROKEN EDGE. REMOVED AND REPLACED DAMAGE, NDT AREA, FABBED AND INSTALLED DOUBLER PER SRM 54-30-03 FIG 17B.SDR 061139Doubler · damagedNR 3 PYLON I/B EXTERNAL SKIN DOUBLER AT NAC STA 221 ABOVE REAR ENGINE MOUNT HAS DAMAGE.SDR 06FDEA1377Panel · missingFOUND NR 1 PYLON FWD BLOWOUT PANEL MISSING AFTER TEST FLIGHT. REPLACED MISSING PANEL AND CORRECTED DUCT LEAK AT PRE-COOLER.SDR KCSA061128Skin · damagedNR 4 PYLON O/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED AT NAC STA 190.SDR 061127Skin · damagedNR 1 PYLON O/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED NAC STA 180 TO 230.SDR 061125Skin · damagedNR 4 PYLON I/B LOWER SKIRT FIRESHIELD AND SKIN DAMAGED FROM NAC STA 215 TO 236.SDR UIEA200600079Access Panel · crackedNR 2 PYLON FWD ACCESS CUT OUT FOUND CRACKED AT TOP FWD AND AFT BOTTOM AREA BETWEEN NAC STA 211.42 TO NAC STA 222.50, (LHS) (ACCESS PANEL #462AL). INTERIM REPAIRED AS PER BOEING MSG 1-168393318-4. PERFORM REPEAT DV. INSP OF SUBJECT REPAIRED AREA AT EVERY C-CHSDR KCSA061112Skin · wornNR. 2 PYLON INBOARD SKIN PANEL WORN ALONG BOTTOM EDGE AT APPROX NAC STA. 210 TO 221.SDR 061109Skin · damagedNR 3 PYLON SKIN HAS SEVERAL AREAS OF DAMAGE FROM NAC STA 180 TO 236.SDR QXEA200601067Skin · damagedYUYC C4 - LEFT NACELLE INBOARD SIDE SKIN HAS LOOSE RIVETS ABOVE AND BEHIND ACCESS DOOR 416AR. ONE RIVET WORN THROUGH COUNTER SINK. REPAIRED IAW RD 8-54-1193, ISSUE 3.SDR UIEA200600075Skin · crackedNR 1 PYLON FOUND INTERIOR SKIN CRACKED AT RT SIDE BETWEEN NAC STA 248 TO NAC STA 259, BELOW RHS PRE-COOLER ACCESS CUT OUT LOWER HORIZONTAL STIFFENER. A/F INSP CARRIED OUT AS REQUIRED A/F. S/M REPAIR CARRIED OUT AS PER BOEING MESSAGE NR1-168393257-11, -16,-18SDR KCSA061085Skin · crackedNR 3 PYLON OUTBOARD SKIN HAS FOUR CRACKS AROUND TWO FASTENER HOLES AT NAC STA 188 AT WL 144 AND AT NAC STA 190 AT WL 145, LONGEST CRACK IS 1" LONG, OTHER CRACKS ARE APPROX 0.5" LONG.SDR DL757071118Skin · crackedDURING HMV AT YVR, A CRACK WAS FOUND IN THE NR 2 PYLON O/B SKIN AT STA 133.5.SDR IXXA06RNG002SSkin Panel · crackedDURING C-CHECK INSPECTION FOUND A CRACK ON INBOARD PYLON STUD EXTENDED EDGE UPPER, AROUND STA XS 250.089 LT. DAMAGED AREA WAS REMOVED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-066 & EWO DRAWING ATI 57-066. FAA FORM 8110-3 WAS ISSUED APPRO
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