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.

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. RESep 19, 2020 · N1399A · Boeing 767306SDR 2020FA0000414Rib · crackedLT PYLON AFT RIB P/N: 7412315-19 IS CRACKED, REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ27074 DATED: 18/SEP/2020.Sep 18, 2020 · N521QS · Cessna 680ASDR 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 SRMSep 12, 2020 · N127FE · Boeing 7673S2FSDR 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.Sep 10, 2020 · N754SK · Cndair CL6002C10SDR R61A2020093000671Scoop · corrodedENG NR 1 AFT STRUT STRUCTURE AREA, INBOARD AIR SCOOP CORRODED. REPLACED IAW SRM 51-41-02.Sep 10, 2020 · N633RW · Emb ERJ170100SESDR 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)Sep 8, 2020 · N250UP · Doug MD11FSDR 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 ARESep 5, 2020 · N922EV · Cndair CL6002B19SDR IPXA2020092560624Flange · chafedINSPECTION TYPE: SEG PANEL 475AL FORWARD INBOARD ATTACH FLANGE SEGMENT CHAFFED AND WORN. R & R ATTACH PLATE, IAW SRM 51-40-21.Sep 5, 2020 · N150UP · Airbus A300F4622RSDR IPXA2020092560628Longeron · damagedINSPECTION TYPE: SEG PANEL 475AL INBOARD PORTION 2ND ATTACH FLANGE SEGMENT HAS HOLES ELONGATED/WORN. R & R LONGERO, IAW SRM 51-40-21.Sep 5, 2020 · N150UP · Airbus A300F4622RSDR T17A2020090301135Bracket · crackedRT/PYLON, AFT UPPER PANEL TWO BRACKETS CRACKED.Sep 3, 2020 · N489TM · Beech 400ASDR 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 AREAug 30, 2020 · N612AX · Doug DC1030SDR 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.Aug 27, 2020 · N756CA · Boeing 747412SDR 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 Aug 23, 2020 · N707SK · Cndair CL6002C10SDR 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).Aug 21, 2020 · N290UP · Doug MD11FSDR 2020F00362Cowling · overheatedRIGHT ENGINE UPPER COWL HEAT DAMAGE, REF ENGINEERING MEMO DQ26626 DATED AUGUST 16, 2020.Aug 17, 2020 · N514QS · Cessna 680ASDR 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 DISENGAug 16, 2020 · N556AL · Beech B200SDR 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.Aug 14, 2020 · N679CA · Cndair CL6002D24SDR 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 SURFAAug 14, 2020 · N795AX · Boeing 767281SDR 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.Aug 10, 2020 · N784SK · Cndair CL6002C10SDR 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.Aug 10, 2020 · N612UP · Boeing 7478FSDR 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.Aug 10, 2020 · N612UP · Boeing 7478FSDR 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 Aug 8, 2020 · N312AK · Piper PA31350SDR 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)Jul 25, 2020 · N279UP · Doug MD11FSDR 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 BJul 24, 2020 · N910FD · Boeing 757236SDR 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 9Jul 24, 2020 · N910FD · Boeing 757236SDR IPXA2020072748185Hinge Fitting · gougedNR 1 O/B FAN COWL AFT HINGE FITTING FAN COWL SIE IS GOUGED. REMOVED & REPLACED FITTING IAW AMMM 71-13-08.Jul 24, 2020 · N125UP · Airbus A300F4622RSDR IPXA2020081158936Attach Angle · damagedINSPECTION TYPE:SEG. PANEL 475AL HAD THE INBD ATTACH FLANGE 1ST SEGMENT HAD ELONGATED HOLES. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-21Jul 22, 2020 · N139UP · Airbus A300F4622RSDR 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 REPAIRJul 20, 2020 · N651FE · Airbus A300F4605RSDR 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 CORROSJul 20, 2020 · N651FE · Airbus A300F4605RSDR 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.Jul 16, 2020 · N125UP · Airbus A300F4622RSDR 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.Jul 15, 2020 · N952CA · Boeing 747428SDR 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.Jul 11, 2020 · N952CA · Boeing 747428SDR 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.Jul 7, 2020 · N611UP · Boeing 7478FSDR 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.Jul 7, 2020 · N611UP · Boeing 7478FSDR 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.Jul 7, 2020 · N611UP · Boeing 7478FSDR 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.Jul 6, 2020 · N952CA · Boeing 747428SDR 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.Jul 6, 2020 · N952CA · Boeing 747428SDR 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.Jul 6, 2020 · N952CA · Boeing 747428SDR 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 STRJul 6, 2020 · N952CA · Boeing 747428SDR 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 Jul 6, 2020 · N952CA · Boeing 747428SDR 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 54-00/0934Jul 5, 2020 · N586FE · Doug MD11FSDR 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 FITTINJun 30, 2020 · N311AZ · Boeing 767338SDR 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. Jun 30, 2020 · N311AZ · Boeing 767338SDR 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 PANELJun 27, 2020 · N311AZ · Boeing 767338SDR 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.Jun 25, 2020 · N935FD · Boeing 7572T7SDR 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.Jun 16, 2020 · N722EV · Cndair CL6002C10SDR 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.Jun 2, 2020 · N675FE · Airbus A300F4605RSDR ABXA2020063022113Seal · wornNR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.May 22, 2020 · N774AX · Boeing 767281SDR ABXA2020063022112Structure · wornNR 2 ENGINE OTBD CORE COWL AFT INNER T/E SKIN WORN AT NUMEROUS SPOTS. THE AIRPLANE WAS GROUNDED.May 22, 2020 · N774AX · Boeing 767281SDR 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.May 19, 2020 · N77865 · Boeing 75733N
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