JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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 = '5400' 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 IXXA2022052803Access Panel · crackedPYLON PANEL 436AL DAMAGEDSDR MK1Y20220429025Thrust Reverser · corrodedENG #1 , R/H SIDE, THRUST REVERSER - BEAVERTAIL, NAC STA 232; DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING DEEP CORROSION DAMAGE WAS FOUND ON THE THRUST REVERSER - BEAVERTAIL.SDR IXXA2022052601Support Angle · crackedSUPPORT ANGLE CRACKEDSDR IXXA2022052503Web · crackedPANEL WEB CRACKEDSDR IXXA20222501Seal · brokenPANEL SEAL BROKENSDR CALA2022052501351Seal · departedPDA 1 P/N D5461038200100 PEELED BACK AND BROKE OFF DEPARTING A/C APPROXIMATELY 15" X 4" THIN METAL PART. REMOVED REMAING PIECE OF SEAL AND REPLACED WITH NEW SEAL.SDR CALA2022052501337Seal · damagedLEFT NUMBER 1 ENGINE COWL SEAL BROKE OFFBY HINGE ACCESS PANEL REPLACED FWD INBD PYLON SEAL. P/N D5461038200000. NO.1 ENG.AMM 54-57-22-400-003-ASDR DALA2022052403606None · noneSHIP 3102 - CORROSION RECEPTACLE BORE SPIGOT BALL JOINT ON LH PYLON. CORRECTIVE ACTION: REPAIRED RECEPTACLE BORE SPIGOT BALL JOINT ON LH PYLON AS PER A319 SRM 54-51-12.(2246151)SDR CALA2022052301316Skin · damaged(A3NB-71-3-6011) LEFT PYLON AFT FIXED FAIRING RH EXTERNAL SKIN H AS DAMAGE.(REMOVE DAMAGE.) REMOVED AND REPLACED SKIN PANEL ON LEFT SIDE FIXED FAIRING IAW S RM 54-54-11-300-038. REMOVED AND REPLACED ANGLE SUPPORT PANEL IA W SRM 51-42-11. EMP# V933866 WORK ACCOSDR IPXA2022052182336None · crackedINSPECTION TYPE:1C/3PANEL 423BL HAS 4EA CRACKES ON PRECOOLER VENT GRILLS.ACCOMPLISH WELD REPAIR IAW SRM 54-52-51 FIG 205.SDR IPXA2022052182334None · crackedINSPECTION TYPE:1C/3PYLON #1 O/B SIDE INSIDE ACCESS 413CL LOWER METAL PLATE HAS A CRACK.ACCOMPLISHED WELD REPAIRED PER SRM P&W 54-50-00.SDR IPXA2022052182333None · crackedINSPECTION TYPE:1C/3LH PYLON AFT FAIRING 475AL, INSIDE OF FAIRING VERTICAL RIB LWR AREA IS CRACK.REMOVED, FABRICATED AND REPLACE RIB IAW SRM 51-40-21.SDR IPXA2022052182332None · crackedINSPECTION TYPE:1C/3PANEL 413BL HAS 6EA CRACKES ON PRECOOLER VENT GRILLS.ACCOMPLISH WELD REPAIR IAW SRM 54-52-51 FIG 205.SDR IPXA2022052182325Web · crackedINSPECTION TYPE:1C/3LH PYLON ARCH WEB BETWEEN BUTERFLY PANEL IS CRACK.ACCOMPLISH WELD REPAIR IAW SRM P&W 54-50-00 FIG 105.SDR DALA2022052403571None · noneSHIP 666 WEAR ON WEB AT NAC STA 102 INB. SIDE AT RH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00398-PREVIUS REPAIR DOUBLER ON WEB AT NAC STA 102 INB. SIDE AT RH PYLON WAS REPLACED PER B757-200 SRM. (2242910)SDR CALA2022052001303None · damaged(A3NB-71-3-6011) LEFT PYLON AFT FIXED FAIRING RH EXTERNAL SKIN H AS DAMAGE.(REMOVE DAMAGE.) REMOVED AND REPLACED SKIN PANEL ON LEFT SIDE FIXED FAIRING IAW S RM 54-54-11-300-038. REMOVED AND REPLACED ANGLE SUPPORT PANEL IA W SRM 51-42-11. EMP# V933866 WORK ACCOSDR UIEA2022051300461Panel · cracked#2 PYLON AFT FAIRING #3 FRAME I/B UPPER AFT CORNER CRACK ( MONOLITHIC PANEL )(<P>#2 PYLON AFT FAIRING #3 FRAME I/B UPPER AFT CORNER MONOLITHIC PANEL REPAIRED AS PER RI-54-53-15611 REV A</P>)SDR UIEA2022051300462Panel · cracked#1 PYLON AFT FAIRING #4 FRAME O/B UPPER FWD CORNER FOUND CRACK ( MONOLITHIC PANEL )(<P>#1 PYLON AFT FAIRING #4 FRAME O/B UPPER FWD CORNER AT MONOLITHIC PANEL REPAIRED AS PER RI-54-53-15612 REV A</P>)SDR UIEA2022051300463Panel · cracked#1 PYLON AFT FAIRING #3 FRAME I/B UPPER FWD CORNER CRACK ( MONOLITHIC PANEL )(<P>#1 PYLON AFT FAIRING #3 FRAME I/B UPPER FWD CORNER MONILITHIC PANEL REPAIR AS PER RI-54-53-15617 REV A</P>)SDR UIEA2022051300464Fairing · cracked#1 PYLON AFT FAIRING #3 FRAME I/B UPPER AFT CORNER FASTENER HOLE CRACK(<P>#1 PYLON AFT FAIRING #3 FRAME I/B UPPER AFT CORNER REPLACED AS PER RI--54-53-15617 REV A</P>)SDR IPXA2022051882233Plate · elongatedINSPECTION TYPE:CL/H PYLON FAIRING PANEL 475AL LH SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGES AS MARKED.INSTALLED NEW PLATE IAW-SRM 5-40-21.SDR IPXA2022051882202Plate · elongatedINSPECTION TYPE:CL/H PYLON FAIRING PANEL 475AL R/H SIDE UPPER EDGE 34EA ELONGATED HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21SDR MK1Y20220429023None · noneDURING MAINTENANCE INSPECTION AT IAI, UNDOCUMENTED WELDING PATCH REPAIR WAS FOUND ON ENG #2 EXHAUST EXTERNAL SKIN AT 8 O’CLOCK BETWEEN NAC STA 318 TO 320. THE PATCH DIAMETER WAS MEASURED AND FOUND 2.3”.SDR MK1Y20220429022Skin · dentedDURING MAINTENANCE INSPECTION AT IAI, DOCUMENTED DENT (CUSTOMER FAIL NO: 81-78-ET148) WAS FOUND ON ENG #1 EXHAUST EXTERNAL SKIN BETWEEN 8 TO 9 O’CLOCK AT NAC STA 348.246. THE DENT WAS MEASURED AND FOUND BEYOND SRM 54-42-30 ALLOWABLE DAMAGE 1 NOTE “N” LIMITS.SDR MK1Y20220429021Acoustic Panel · dentedDURING MAINTENANCE INSPECTION AT IAI, TWO (2) ADJACENT DENTS WERE FOUND ON ENG #2 INLET COWL ACOUSTIC PANEL PERFORATED SKIN BETWEEN 8 TO 9 O’CLOCK.SDR HNAA2022052600206None · noneE913854 - FR 72 IS CRACKED BTW STR 17L-16L ....REPAIRED FR 72 CRACK BETWEEN STR 17L-16L IAW PIEDMONT EO1-53-22-0093.SDR IXXA2022051502Tie Clip · crackedCRACKED ANGLE SUPPORT MID TORQUE BOX #1 ENG.SDR DALA2022051703414None · noneSHIP 3102 - CORROSION SPIGOT BALL JOINT RECEPTACLE BORE ON RH PYLON . CORRECTIVE ACTION: REPLACED RECEPTACLE BORE SPIGOT BALL JOINT ON RH PYLON AS PER A319 SRM 54-51-12-300-001.(2234473)SDR QXEA2022051200190Exhaust Pipe · damagedPASSENGER REPORTED #2 ENGINE EXHAUST FLAPPING IN FLIGHT. AIRCRAFT REMOVED FROM SERVICE. FOUND MISSING HARDWARE/SPRING CLIPS ON LOCATIONS M2, M3, A1, A2, A3, AND AFT MOST ATTACHMENT AS NOTED IN FIGURE 101 SHEET 1 OF Q400 SRM 54-45-25, TR 54-067. FERRIED AIRCRAFSDR CALA2022051101213None · missingPDA 3 #1 ENG AFT STRUT AT LOWER DRAIN TUBE HAS RIVETS BROKEN OFF/ MISSING AND LOOSE -- SEE PHOTO,S PHOTO,S ADDED MISSING SHIMS & TEFLON STRIP -- SEE PHOTO -- PARTS IPC PHOTO ADDED ORDERED AVAILABLE TEFLON STRIPS AND ARE PLACED IN FLIGHT DECK REMOVED #1 ENG LOWSDR CALA2022051101212None · missingPDA 3 #2 ENG AFT STRUT FAIRING MISSING ONE FASTENER AND OTHERS LOOSE -- SEE PHOTO PHOTO ADDED REMOVED AND INSTALLED NEW FASTENERS REF SRM 54-54-11-283-004.SDR MK1Y20220429018Acoustic Panel · dentedENGINE # 2, INLET COWL ACOUSTIC PANEL, PERFORATED SKIN: DURING MAINTENANCE INSPECTION AT IAI, DENT WAS FOUND WITH NICK ON THE INNER BARREL ACOUSTIC PANEL OF INLET COWL #2 ENG LOCATED AT 3 TO 4 CLOCKWISE AND 4” FROM EDGE PANEL.SDR MK1Y20220429017Fairing · inadequateENGINE #2, OUTBD & INBD THRUST REVERSERS, UPPER AND LOWER FAIRINGS, EXISTING REPAIRS:
DURING MAINTENANCE INSPECTION AT IAI, SEVERAL EXISTING UNDOCUMENTED REPAIRS WERE FOUND ON BOTH THRUST REVERSERS INSTALLED ON ENGINE # 2.
IAI NRC: M0203 L/H STA 206.5-210.5;SDR MK1Y20220429016Thrust Reverser · damagedENGINE # 2, OUTBD THRUST REVERSER, NAC STA 249.5, 5 O’CLOCK: DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING EDGE REPAIR WAS FOUND, ON THE AFT EDGE OF THE DATUM THRUST REVERSER.SDR MK1Y20220429015Cowling · inadequateENGINE #2, OUTBD & INBD CORE COWLS, EXISTING REPAIRS: DURING MAINTENANCE INSPECTION AT IAI, THERE UNDOCUMENTED REPAIRS WERE FOUND. ALL REPAIRS WERE REMOVED AND THE AREAS WERE INSPECTED.STA 246 TO STA 251 12" O'CLOCK ; NAS STA 299.7 TO STA 304.5 BT 2-3 CLOCWISESDR MK1Y20220429014Cowling · inadequateENGINE #1, INBD CORE COWL, EXISTING REPAIR:
DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING UNDOCUMENTED REPAIR WAS FOUND. THE REPAIR WAS REMOVED AND AREA WAS INSPECTED.SDR MK1Y20220429012Fairing · inadequateENGINE # 1, OUTBD & INB THRUST REVERSERS, UPPER & LOWER FAIRINGS:
DURING MAINTENANCE INSPECTION AT IAI, MULTIPLE EXISTING UNDOCUMENTED REPAIRS WERE FOUND ON THE UPPER AND LOWER FAIRINGS OF BOTH THRUST REVERSERS.SDR IXXA2022050501Vent · crackedCORE COWL VENT CRACKEDSDR IXXA2022050406Cowl Latch · wornCORE COWL AFT LATCH HAS WEARSDR IXXA2022050403Bracket · crackedBRACKET CRACKED ON SKIRT FAIRINGSDR UIEA2022042200368None · none#4 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA.(<P>#4 NACELLE STRUT THRUST TANK - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)SDR UIEA2022042600391None · noneNO.1 PYLON RH NO.1 CORN COWL HINGE FITTING FWD LUG FWD SURFACE FOUND CHAFING(<P>SPOTFACE LUG FACE REQUIRED TO PROVIDE FLAT SURFACE AND FABRICATE CUSTOM WAHSER AS PER RI-54-50-15543 REV A</P>)SDR UIEA2022042500388None · none#4 PYLON VALVE ACCESS PNL #482EL FOUND 2EA SCREW HOLE ELONGATED.(<P>#4 PYLON VALVE ACCESS PNL #482EL 2EA SCREW HOLE ELONGATED AREAS REPAIRED IAW RI-54-50-15536 REV A</P>)SDR UIEA2022042500389None · none#3 PYLON VALVE ACCESS PNL #472ER FOUND 1EA SCREW HOLE ELONGATED(<P>#3 PYLON VAVLE ACCESS PNL #472ER 1EA SCREW HOLE ELONGATED AREAS REPAIRED IAW RI-54-50-15536 REV A</P>)SDR UIEA2022042200367None · none#3 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA(<P>#3 NACELLE STRUT THRUST TANG - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)SDR UIEA2022042200366None · none#2 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA(<P>#2 NACELLE STRUT THRUST TANG - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)SDR UIEA2022042200365None · none#1 NACELLE STRUT THRUST TANG - COVER PLATE CANNOT BE INSTALLED, DUE TO NO ACCESS ON THE UNDERNEATH AREA(<P>#1 NACELLE STRUT THRUST TANG - COVER PLATE FASTENER SUBSTITUTION IAW RI-54-00-15545 REV A</P>)SDR SWAA2022053100136Bracket · brokenBROKEN SPAR LOWER BRAKET LOC ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON 2022-207304 / [01] REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 52-40-02;[02] CORRECTED STEP 1<BR>REPLACED BRACKET AND FASTENERS LOCSDR CALA2022042701091Fastener · missingPDA 3 REF LP 8457922 MISSING FASTENER #1 ENGINE PYLON PANEL 472BR LOG GENERATED UNDER GMM 02-30-95 .REMOVED PANEL AND INSTALLED NEW NUT PLATE. RE INSTALLED PANEL AS PER LP 8457922SDR 1UPA20220419032Arm · failedELECTRONIC SPEED CONTROLLER SEPARATING FROM ARM ASSEMBLY DUE TO FAILED SCREW INSERTS.
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