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 UIEA2020092212041Acoustic Liner · damagedRIGHT ENGINE ACOUSTIC LINER DAMAGED AFT OF FAN BLADES 6 O'CLOCK POSITION. OK TO CONTINUE, IAW AMM 72-00-00-206-167-H00 FOR UP TO 10 FLIGHT CYCLES OR 100 FLIGHT HOURS, WHICHEVER COMES FIRST. TRANSFERRED TO MDDR 134661 NON MEL, IAW AMM 72-00-00-206-167-H0. RESDR 2020FA0000414Rib · crackedLT PYLON AFT RIB P/N: 7412315-19 IS CRACKED, REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ27074 DATED: 18/SEP/2020.SDR FDEA2020091422186Beam · gougedNR 2 PYLON AFT FAIRING INBOARD LONGITUDINAL BEAM GOUGED AT NUTPLATE LOCATION AT NAC STA 308 LT. REMOVED LATCH BEAM, IAW B767 SRM 51-40-02-0G. REPAIRED LATCH BEAM, IAW B767 SRM 54-52-71-2R AND FED EX EA H5450-T0356442 P1. REINSTALLED LATCH BEAM, IAW B767 SRMSDR SWIA202053376Tie Bar · gougedLT LOWER C-DUCT PYLON TIE-BAR ATTACH HINGE (NR 3 HINGE) FORWARD LUG GOUGED. C-CHECK RO 10/16/2020. REPAIRED LT LOWER C DUCT PYLON TIE BAR ATTACH HINGE NR 3 FWD LUG, AS PER MHIRJ REO.SDR R61A2020093000671Scoop · corrodedENG NR 1 AFT STRUT STRUCTURE AREA, INBOARD AIR SCOOP CORRODED. REPLACED IAW SRM 51-41-02.SDR IPXA2020092460581Rib · chafedINSPECTION TYPE: 2C NR 1 PYLON LOWER AFT FAIRING V-RIB IS CHAFED AND DAMAGED. REMOVED AND REPLACED V-RIB, IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR SWIA202053516Bulkhead · chafedRT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARE CHAFED AND HAVE BENT/MISSING INSPECTION DOORS. C-CHECK RO 10/18/2020. REPAIRED RT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARESDR IPXA2020092560624Flange · chafedINSPECTION TYPE: SEG PANEL 475AL FORWARD INBOARD ATTACH FLANGE SEGMENT CHAFFED AND WORN. R & R ATTACH PLATE, IAW SRM 51-40-21.SDR IPXA2020092560628Longeron · damagedINSPECTION TYPE: SEG PANEL 475AL INBOARD PORTION 2ND ATTACH FLANGE SEGMENT HAS HOLES ELONGATED/WORN. R & R LONGERO, IAW SRM 51-40-21.SDR T17A2020090301135Bracket · crackedRT/PYLON, AFT UPPER PANEL TWO BRACKETS CRACKED.SDR ZTRR20200910002Hinge · departed2020-08-30 UPON LANDING DURING MX WALK-AROUND NR 2 ENGINE RIGHT CORE COWL WAS NOTICED TO HAVE FAILED DURING FLIGHT, PI-REP ENG 2 CORE COWL DAMAGED AND PIECES MISSING. CONCLUSIVE FAILURE IS UNDETERMINED, TWO POSSIBILITIES WHICH COULD RESULT IN SUCH FAILURE ARESDR U2RA202009200005Door · gougedWHILE ACCOMPLISHING A VISUAL INSPECTION FOUND 3 EA GOUGES ON NR 2 ENGINE PYLON FAIRING DOOR INNER SKIN AFT OF FWD ACCESS DOOR. REPAIRED PER VT-SAA EA 747-5450-56-A8551 REV I/R.SDR SWIA202052753Structure · crackedWHILE PERFORMING SB670BA-54-007 ON LT UPPER PYLON, FOUND CRACKS IN 2ND OVERSIZED HOLES ON SEQUENCE 2 HOLES NR 2 AND NR 6. C-CHECK RO 9/21/2020. COMPLIED WITH MHIRJ REO FOR REPAIR OF CRACKS IN 2ND OVERSIZED HOLES ON SEQUENCE 2 HOLES NR 2 AND NR 6 FOUND WHILE SDR IPXA2020091436163Hinge · chafedINSPECTION TYPE: 2C NR 1 ENG OUTBOARD FAN COWL FWD HINGE IS CHAFED. REPAIRED NR 1 ENG OUTBOARD FAN COWL FWD HINGE, IAW VT-SAA EA 011-7110-01-A8528 REV I/R AND UPS EO MD11-7110-77740-A (MINOR).SDR 2020F00362Cowling · overheatedRIGHT ENGINE UPPER COWL HEAT DAMAGE, REF ENGINEERING MEMO DQ26626 DATED AUGUST 16, 2020.SDR IPMA2020081860001Hook · unlatchedAIRCRAFT DEPARTED AND UPON REACHING CRUISE ALTITUDE CREW NOTICED LEFT ENGINE COWLING WAS LIFTED UP. CREW RETURNED TO DEPARTURE AIRPORT AND EMERGENCY WAS DECLARED AND THEY LANDED WITHOUT INCIDENT. THE COWL LATCH WAS IN THE LOCKED POSITION, BUT HAD COME DISENGSDR SWIA202053118Slider · chafedRT ENGINE UPPER TRANSLATING COWL SLIDER CHAFED. C-CHECK RO 10/9/2020. PERFORMED PERMANENT REPAIR ON RT ENGINE UPPER TRANSLATING COWL SLIDER, REF BOMBARDIER REO.SDR ABXA20200903 172Panel · gougedGOUGE DAMAGE WAS FOUND ON THE STRUT SKIN PANEL (P/N 311T1400-21) OF THE LT PYLON. THE GOUGE WAS REMOVED BY BLENDING, PER 767-200 SRM 51-10-02 EXCEEDING SRM LIMITS. ALL FASTENERS COMMON TO REWORKED AREAS, AS REQUIRED, WERE REMOVED AND HFEC OPEN-HOLE AND SURFASDR SWIA202052574Latch · wornTHUMB LATCH TAB ON RIGHT LOWER TRANS COWL WORN, MARKED. C-CHECK RO 9/20/2020. REPLACED RT LOWER TRANSCOWL LATCH DOOR COAMING, PER REO SEE CONTINUATION CARD FOR DETAILS.SDR IPXA2020081759073Panel · discoloredINSPECTION TYPE:C1. DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 323U8740-1) OF PYLON #4.REPAIR IAW SRID: 4-4850555663 AND EO B747-5450-77514-A.SDR IPXA2020081759072Panel · discoloredINSPECTION TYPE:C1, DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 313U8740-1) OF PYLON #3.REPAIR IAW SRID: 4-4850528193 AND EO B747-5450-77515-A.SDR HXXC20200810357Cowling · failedFIBERGLASS TORE ALONG THE LEADING EDGE FASTENERS OF THE COWLING AND THE UPPER COWLING BEGAN TO PEEL UP FROM WIND FORCES TEARING FASTENERS FREE AS THE FLIGHT PROGRESSED. PILOT PERFORMED A PRECAUTIONARY LANDING SAFELY WITH NO ISSUES AND THE COWLING WAS REPLACED SDR IPXA2020081258988Angle · corrodedINSPECTION TYPE:C3LH FWD #2 ENG PICKLE BARREL SUPPORT STRUTURE INSIDE ACCESS PANEL #361EL HAS CORROSION ON AFT ANGLE SUPPORT.REPLACED CORRODED ANGLE SUPPORT AT #2 ENG PICKLE BARREL INSIDE PANEL 361EL IAW SRM 51-33-01. (MINOR)SDR FDEA202007242002Attach Bracket · crackedLT SAILBOAT OUTBOARD ATTACHING BRACKET CRACKED. REMOVED LT SAILBOAT OUTBOARD ATTACHING BRACKET IAW SRM 51-40-02. FABRICATED LT SAILBOAT OUTBOARD ATTACHING BRACKET IAW BOEING DRAWING 313N5052 AND FEDEX GMM 7-0-1001. INSTALLED LT SAILBOAT OUTBOARD ATTACHING BSDR FDEA2020083141932Bulkhead · crackedENG 2 BULK HEAD AFT OF COMPRESSOR FAIRING LH SIDE 10 O CLOCK POSITION IS CRACKED REPAIRED #2 ENG BULKHEAD AFT OF COMPRESSOR FAIRING L/H SIDE 10 O CLOCK POSITION IAW AMM 72-03-01-8-4 REPAIR 9SDR IPXA2020072748185Hinge Fitting · gougedNR 1 O/B FAN COWL AFT HINGE FITTING FAN COWL SIE IS GOUGED. REMOVED & REPLACED FITTING IAW AMMM 71-13-08.SDR IPXA2020081158936Attach Angle · damagedINSPECTION TYPE:SEG. PANEL 475AL HAD THE INBD ATTACH FLANGE 1ST SEGMENT HAD ELONGATED HOLES. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-21SDR FDEA2020083122062Mount · corrodedCORROSION ENGINE MOUNT FWD PYRAMID ON LH PYLON PERFORMED REPAIR LOC ON BASE PLATE AND (2E/A) HOLES OF THE BOLTS OF FORWARD MOUNT RIB 1 ATTACHED FITTING PYRAMID ON LH PYLON IAW EA N. T6-5450-T0355859 P1, #1 ENGINELH FORWARD MOUNT BASE PLATE CORROSION REPAIRSDR FDEA2020073122061Mount · corrodedCORROSION FORWARD MOUNT RIB 1 ATTACHED FITTING (PYRAMID) ON RH PYLON PERFORMED REPAIR LOC. ON BASE PLATE AND 3EA HOLES OF THE BOLTS OF FWD MOUNT RIB 1 ATTACHED FITTING PYRAMID ON RH PYLON IAW EA NO T6-5450-167628 B P3, #2 PYLON FWD ENG MOUNT FITTING CORROSSDR IPXA2020071767841Fairing · crackedNR 2 PYLON O/B SIDE FIXED FAIRING HAS POSSIBLE CRACK ON LOWER AREA AROUND FASTENER. FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 54-53-10 FIG 201.SDR U2RA202010160004Fitting · nickedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, A NICK WAS NOTED ON THE NUMBER 2 PYLON FAN COWL AFT SUPPORT BEAM OUTBOARD AREA. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314.SDR U2RA202010190003Bracket · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-806-00-01, A CRACK WAS NOTED ON A PNEUMATIC TUBE SUPPORT BRACKET, INSIDE NUMBER 1 PYLON PANEL 451B. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER 20293-4.SDR IPXA2020071357695Panel · discoloredINSPECTION TYPE:C1, DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N:323U8740-1) OF THE NR 4 PYLON. REPAIR IAW SRID 3-4768900785, AND EO B747-5450-77180-A.SDR IPXA2020071357694Panel · discoloredINSPECTION TYPE:C1, DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N:313U8740-1) OF THE NR 3 PYLON. REPAIR IAW SRID:3-4768866871, AND EO B747-5450-77179-A.SDR IPXA2020071357693Panel · discoloredINSPECTION TYPE:C1, DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N:323U8740-2) OF THE NR 1 PYLON. REPAIRED IAW SRID:3-4768857999, AND EO B747-5450-77178-A.SDR U2RA202010190001Bushing · corrodedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-54A2182 REVISION 3, CORROSION NOTED ON NUMBER 3 ENGINE PYLON UPPER LINK FORWARD BUSHING. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314-1.SDR U2RA202010160012Link · corrodedDESCRIPTION CORRECTION FOR U2RA202010160012. CORROSION NOTED ON NUMBER 3 PYLON UPPER FORWARD BUSHING. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314-1.SDR U2RA20201016012Fitting · nickedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-02, NICK NOTED ON NUMBER 2 ENGINE PYLON LFAN COWL AFT SUPPORT BEAM OUTBOARD AREA. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20314.SDR U2RA202009096002Fitting · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-54A2182 POST STRUT MODIFICATION INSPECTIONS OF NUMBER 3 PYLON, CORROSION WAS NOTED ON THE FORWARD UPPER SPAR FITTING AND THE WING FRONT SPAR TO STRUT UPPER LINK FITTING. ACCOMPLISHED REPAIRS IN ACCORDANCE WITH STRSDR U2RA202009096001Fitting · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-54A2182 POST STRUT MODIFICATION INSPECTIONS OF NUMBER 2 PYLON, CORROSION WAS NOTED ON THE FORWARD UPPER SPAR FITTING AND THE WING FRONT SPAR TO STRUT UPPER LINK FITTING. ACCOMPLISHED REPAIRS IAW STRUCTURAL REPAIR SDR FDEA2020071051479Finger Doubler · crackedINNER FINGER DOUBLER ABOVE NUMBER 2 ENGINE AFT MOUNT HAS SMALL CRACK, AND ONE RIVET MISSING. COMPLIED WITH EA #1-5481-T0355009 PART 1. MISSING RIVET AT CRACK DAMAGE LOCATION MOVED TO WRI 54-00/0934SDR IXXA20200720028Longeron · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT.
IN COMPLIANCE OF TASK CARD 54-822-00-01 "GVI - ZONAL - AFT NACELLE STRUT FAIRINGS - STRUT 1", THE FOLLOWING DISCREPANCY WAS NOTED: #1 PYLON INBD HYD BAY LOWER LONGERON IS CRACKED AFT OF #4 LATCH FITTINSDR IXXA20200720026Beam · damagedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 54-822-00-01. "GVI - ZONAL - AFT NACELLE STRUT FAIRINGS - STRUT 1", THE FOLLOWING DISCREPANCY WAS NOTED: #1 PYLON OUTBD HYD BAY LOWER LONGERON CRACKED AT 3RD LATCH FITTING. SDR IXXA20200720029Doubler · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 54-408-00-02 "GVI - EXTERNAL - NO. 2 NACELLE STRUT", THE FOLLOWING DISCREPANCY WAS NOTED: #2 PYLON INBOUND STRUT SKIN IS CRACKED IN THE UPPER AFT CORNER OF THE CUTOUT FOR PANELSDR FDEA202006251349Louver · crackedNR 2 ENGINE PYLON ACCESS PANEL 443CR UPPER FWD CORNER HAS CRACK THAT EXTENDS PAST PREVIOUS REPAIR. REPAIRED NR 2 ENG PYLON PANEL 443CR IAW EA F-5450-T0354629.SDR SWIA2020072751426Structure · damaged2EA LH PYLON UPPER LOCK FASTENER HOLES, LOCATIONS 5 AND 7 COUNTING FROM FWD TO AFT, WERE FOUND OVERSIZED AND WITH DEFECTS UPON INCORPORATION OF SB 670BA-54-007 (MARKED) (C-CHECK) RO 7/23/2020 REPAIRED LH PYLON OVERSIZED AND DEFECTIVE HOLES REF. MHIRJ REO.SDR FDEA2020090862114Trim Panel · crackedNR 2 ENGINE PYLON INBOARD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.SDR ABXA2020063022113Seal · wornNR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.SDR ABXA2020063022112Structure · wornNR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.SDR CALA2020052200974Fitting · crackedDURING NDT HFEC ROTO INSPECTION OF NR 1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE 2. REPAIRED HOLE 2 IAW ECRA 5720-031930.
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