JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 GTIA2018032102531Structure · gougedGOUGE FOUND ON THE NR 1 PYLON RIBS 7 - 8. PERFORMED A DOUBLER REPAIR IAW TD 80432583, 005, 2018 A.SDR IPXA201804188664Hinge · chafedINSPECTION TYPE:3C, NR 1 ENGINE INBD FAN COWL FWD HINGE CHAFED. REPAIRED THE HINGE IAW EA 011-7110-01-A7180, REV A, AND EO MD11-7110-67898-B.SDR IPXA2018041228492Hinge Fitting · chafedINSPECTION TYPE: 3C, NR 3 ENGINE LT FAN COWL FWD HINGE FITTING CHAFED AT THE 12 O'CLOCK POSITION. RERPAIRED THE HINGE FITTING IAW EA 011-7110-01-A7181, REV IR, AND EO MD11-7110-67895-A.SDR IPXA2018032827921Hinge · chafedINSPECTION TYPE: 3C, NR 1 ENGINE, INBD FAN COWL FWD HINGE FOUND CHAFED. REPAIRED IAW EA 011-7110-01-A7180, REV IR, AND EO MD11-7110-67898-A.SDR CALA2018031900936Spar Web · crackedNR 2 PYLON STATION 174, FWD UPPER SPAR WEB FOUND TWO CRACKS AT HYD CUTOUT POSITION. REPAIRED IAW ECRA 5450-02486.SDR DALA2018042402770Spar · crackedNR 1 PYLON, UPPER SPAR OF AFT FIXED FAIRING WAS FOUND CRACKED INBD SIDE. INSTALLED A REPAIR IAW AMDS 5450-01052-03A.SDR UIEA2018031000360Rod · damagedNR 2 ENGINE RT NACELLE PANEL, FWD HOLD OPEN ROD LOCK RELEASE COLLAR WILL NOT RELEASE. REMOVED AND REPLACED THE 2 ENGINE FORWARD HOLD OPEN ROD.SDR IXXA20180409017Tube · crackedNR 1 PYLON AFT MOUNT BARREL NUT FWD GUIDE TUBE IS CRACKED, LANYARDS ARE NOT SECURE. REPAIRED THE MOUNT BARREL NUT FWD GUIDE TUBE IAW AMES 47313REA01 AND SECURED THE LANYARDS IAW AMM 71-21-03.SDR ABXR2018021400130Fairing · crackedCRACK ON THE NR 1 PYLON UPPER SKIRT FAIRING STRUCTURE AT FASTENER HOLE.SDR HYIA20180215002Beam · crackedWHILE PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE RT CANTED BEAM ASSEMBLY (CROSSOVER BEAM) ON THE AFT RIGHT HAND SIDE, AROUND ONE OF THE TURBO BRACKET MOUNTING HOLES. IT APPEARS THE CRACK WAS CAUSED BY PRE-LOADING OF THE TURBO BRACKET. BEAM ASSDR UIEA2018021400221Fairing · damagedRIGHT CORE COWL EXTERNAL UPPER FAIRING AFT EDGE CRACKED AND DEFORMED. REPAIRED IAW EO 1971A176, REV O.SDR QMLA2018021218018Skin · damagedRIGHT FORWARD SLIDING DOOR SKIN WRINKLED DUE TO EXCESSIVE FORCE USED TO CLOSE THE DOOR.SDR 17LR20210202001Support Web · crackedDURING A MAJOR REPAIR IN OUR FACILITY ON AN OPEN WORK ORDER W18815 FOR AIRCRAFT TO THE LT AND RT LANDING GEAR SUPPORT STRUCTURE AT KEELSONS SKINS AND BATTERY BOX STRUCTURE, WE JACKED AND SUPPORTED AIRFRAME, REMOVED NUMEROUS ANGLES, SKINS, THE LANDING GEAR DRAGSDR AALA20180205003Fitting · crackedCRACK ON AFT FAIRING HEAT SHIELD BULKHEAD FITTING. REPLACED THE FITTING ON THE NR 2 PYLON IAW EA 257628B.SDR VNAA2018020199902Firewall · damagedRIGHT PYLON FIREWALL WHERE HYDRAULIC PRESSURE LINE GOES THROUGH HAS ELONGATED HOLE. REPAIRED THE FIREWALL IAW EA 43-2018-010.SDR A6WA2018020545607Retainer · crackedCRACKED SEAL RETAINER ON PANEL 412BT. REPAIRED THE SEAL RETAINER IAW 16-363.SDR A6WA2018020545608Retainer · crackedPYLON PANEL 412DB HAS A CRACKED SEAL RETAINER. REPAIRED THE SEAL RETAINER IAW 16-363.SDR P5CA2018013000025Frame · chafedNR 2 ENGINE RT CORE COWL INNER WALL FRAME FOUND CHAFED. REPAIRED IAW E0-1971A169.SDR AALA201802029011Attach Fitting · wornWEAR ON SHACKLES ON PYLON TO WING AFT ATTACH FITTING AT RIB 10 ON RIGHT PYLON. REPLACED SHACKLES ON RIGHT PYLON TO WING ATTACH FITTING (ONLY FORWARD SHACKLE) IAW AMM 54-51-17-400-002-A.SDR CALA2018011200125Web · crackedNR 1 PYLON MID SPAR WEB FOUND CRACKED AT IDG FEED THROUGH CUTOUT, REPAIRED IAW SRM 54-55-01, FIG 203, REPAIR 2 ,DETAIL I.SDR SWIA201744242Skin · dentedRIGHT ENGINE. NOSE COWL LEADING EDGE DENTED AT APPROXIMATELY THE 1 O`CLOCK POSITION. REPLACED IAW AMM.SDR UIEA2017123002448Clamp · brokenVIBRATION MONITOR INDICATED BETWEEN 4.6 AND 5.0 LPT AT CRUISE. VIBRATION NOTICABLE ON CLIMBOUT. PERFORMED INLET AND EXHAUST OF LT ENGINE GENERAL INSPECTION IAW AMM 05-51-38 REF TO 938543 M3, A BROKEN COWL ROD CLAMP FOUND.SDR DALA2017122808953Frame · corrodedDURING INSPECTION, FOUND CORROSION ON THE LOWER WEB AND FRAME UNDER HEAT SHIELD FAIRING AREA AT THE LT ENGINE STRUT. MAINTENANCE REPLACED THE FRAMES IAW SRM 51-40-02 PAR 7.SDR DALA2017122808951Structure · bentFOUND NR 1 ENGINE RT CORE COWL ON THE UPPER AFT FAIRLING SKIN HAS DAMAGED. DAMAGE CONSISTS OF A BENT FLANGE 4.5 INCH LONG FWD/AFT. THE BENT FLANGE HAS A CRACK FWD SECTION, DAMAGE LENGTH OF 1.5 INCHES UP AND DOWN. REPLACED THE COWL IAW AMM 71-11,SDR CA180102004Actuator · failed(CAN) NR 2 ENGINE INTAKE BYPASS DOOR OPEN LIGHT NOT ON DUE TO ICING CONDITON, CREW DECIDED ATB. BYPASS DOOR ACTUATOR FOUND U/S, ACTUATOR REPLACED & WIRING CHECK C/O. A/C RETURNED TO SERVICE (TC NR 20180102004).SDR DALA2017121408625Fairing · coked#2 NACELLE AFT FAIRING I/B EXTERIOR SURFACE FOUND COKING. EVALUATED AND REPAIRED #2 NACELLE AFT FAIRING I/B EXTERIOR SURFACE COKING.SDR DALA2017121308572Panel · detachedL/N NACLLE STRUT FAIRING I/B UPPER PANEL FOUND DISENGAGE. REPAIRED PER SRM 51-70-10.SDR DALA2017121308571Fairing · coked#1 NACELLE AFT FAIRING I/B EXTERIOR SURFACE FOUND COKING. EVALUATED AND REPAIRED #1 NACELLE AFT FAIRING I/B EXTERIOR SURFACE COKING PER SRM 51-70-10SDR HYIA20171213001Fitting · crackedTHE RT OB NACELLE FITTING PART NUMBER 5292029-24 WAS FOUND TO BE CRACKED DURING BORESCOPE INSPECTION PRESCRIBED BY TEXTRON MULTI-ENGINE SERVICE LETTER MEL-54-02R2 DATED MARCH 29, 2017 AS CONTINUING ACTION REQUIRED BY AD2017-10-09. THE CRACK IS FAINT BUT VSDR UIEA2017110902212Rub Strip · wornNR 1 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER SECTION RUBSTRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.SDR UIEA2017110902211Rub Strip · crackedNR 2 ENGINE RT CORE COWL EXTERIOR SURFACE FWD UPPER SECTION RUB STRIP FOUND CRACKED. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.SDR UIEA2017111202227Seal · wornNR 1 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV 105.SDR UIEA2017111202228Seal · wornNR 2 ENGINE LT CORE COWL FAIRING ASSY INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.SDR UIEA2017111202229Retainer · wornNR 1 ENGINE RT CORE COWL PRESSURE RELIEF DOOR CUT-OUT UPPER RETAINER FOUND WORN. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.SDR UIEA2017111202230Retainer · wornNR 2 ENGINE RT CORE COWL PRESSURE RELIEF DOOR CUT-OUT UPPER RETAINER FOUND WORN. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV. 105.SDR UIEA2017111202231Bracket · wornNR 1 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN SUPPORT BRACKET & ADAPTER FOUND WORN THE BRACKETS AND ADAPTER WERE REMOVED AND REPLACED IAW SRM 51-40-02. REV 105.SDR UIEA2017111202232Duct · wornNR 1 ENGINE RT CORE COWL PRECOOLER EXIT DUCT FOUND WORN. THE DUCT WAS REPAIRED IAW SB TBC - 80C2-NAC-71-032. REV. 2.SDR UIEA2017112702313Frame · wornNR 2 ENGINE LT CORE COWL 2ND ZEE FRAME FROM FWD EXISTING REPAIR DOUBLER AND FILLER FOUND WORN. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 105.SDR UIEA2017111602244Support Plate · wornNR 1 ENGINE LT CORE COWL INTERIOR SURFACE MID SECTION SUPPORT PLATE FOUND WORN. THE SUPPORT PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV. 105.SDR UIEA2017111602245Longeron · wornNR 2 ENGINE R/H CORE COWL AFT LOWER EDGE LONGERON FOUND WORN. LONGERON REMOVED AND REPLACED IAW SRM 51-40-02 , REV. 105.SDR UIEA2017111602248Bracket · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD STOW PIN SUPPORT BRACKET ADAPTER FOUND WORN. REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 , REV. 105.SDR UIEA2017111702249Bracket · wornATA 71-13 #2 ENGINE L/H CORE COWL HOLD OPEN ROD STOW PIN SUPPORT BRACKET ADAPTER FOUND WORN AS MARKED. NR 2 ENGINE - L/H CORE COWL HOLD OPEN ROD STOW PIN SUPPORT WORN BRACKET AND ADAPTER REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 , REV. 105.SDR UIEA2017111702250Longeron · wornNR 2 ENGINE L/H CORE COWL AFT LOWER EDGE LONGERON FOUND WORN. NR 2 ENGINE - L/H CORE COWL AFT LOWER EDGE LONGERON REMOVED AND REPLACED IAW SRM 51-40-02 , REV. 105.</P>)SDR UIEA2017111702252Structure · damagedDENT AND BUCKLE AND EXISTING REPAIR ON #2 ENGINE INBOARD T/R INNER SURFACE SIDE AT 8 O'CLOCK POSITION. NR 2 ENGINE L/H TRANSLATING COWL REMOVED AND REPLACED I.A.W B767-300 AMM 78-31-10 , REV. 122. FOR THRUST REVERSER OPERATIONAL TEST REFER TO W/C # A-78-333-0SDR KCSA201711281084Lug · wornNR 1 PYLON LOWER SPAR FITTING, LUG HOLE WORNSDR VNAA2017112799901Fairing · damagedRIGHT LOWER FAN COWL FWD HINGE LINE FAIRING BENT AND DISTORTED DUE TO CONTACT WITH FAN COWL. PERFORMED A PERMANENT REPAIR OF FAIRING IAW EO CL600-2D24-54-L05392.SDR REXA2017111301224Access Panel · cracked#1 ENGINE ACCESS PANEL 433BB IS CRACKED.
REMOVED AND REPLACED #1 ENGINE ACCESS PANEL 433BB IAW CRJ 900 SRM
51-42-06 AND SRM 51-42-13. INSTALLED #1 ENG ACCESS PNL 433BB IAW
CRJ 900 AMM 54-12-01-400-802 STEP 4-A-2 A-D
AAR EMP 27262SDR REXA2017111301223Access Panel · cracked#2 ENGINE ACCESS PANEL 443BB IS CRACKED.
REMOVED AND REPLACED #2 ENGINE ACCESS PANEL 443BB IAW CRJ 900 SRM
51-42-06 AND SRM 51-42-13. INSTALLED #2 ENG ACCESS PNL 443BB IAW CRJ
900 AMM 54-12-01-400-802 STEP 4-A-2A-D
AAR EMP SDR JR2R11102017224Scoop · crackedNR 1 NOSE COWL, LOWER SCOOP IS CRACKED AND MISSING FASTNERS. REPAIRED THE LOWER SCOOP IAW SRM 54-01, FIG 2.SDR CALA2017110303895Spar · crackedNR 1 PYLON NAC STA 223, MID SPAR WEB FOUND CRACKED AT IDG FEED THROUGH CUTOUT POSITION. THE SPAR WEB WAS REPLACED IAW SRM54-55-01, REPAIR 2, FIG 202.
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