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.

SDR CALA2022012400211Seal · crackedPDA 2 #1 ENG INBD SIDE T-R TO PYLON FLEX SEAL PIECES MISSING AND CRACKED ...REF FIG 3 ITEMS 90 AND 110 OF ECRA 5450-02357...SEE PHOTO ABD APPLIED SPEED TAPE. ISSUE DIP TO DO VISUAL INSP ONCE PER DAY 50 FLIGHT HOURS. PER PART 2A, AND ACCOMPLISH PERMANENT REPAIRJan 23, 2022 · N426UA · Airbus A320232SDR SWAA2022021662937Cowl Door · corroded#1 ENGINE NOSE COWL HAS CORROSION AT 12 O'CLOCK POSITION APPROX. 10INCHES FROM LE (MARKED) / [01] REMOVED .011? MATERIAL FROM ORIGINAL THICKNESS OF .071? FOUND TO BE OUT OF LIMITS IAW SRM 54-10-01?1A.;[02] C/W INSPECTION.;[03] REMOVED AND REPLACED NOSE COWL PEJan 21, 2022 · N8602F · Boeing 7378H4SDR SWAA2022012562914Frame · cracked#2 ENGINE AFT PYLON PANEL SUPPORT FRAME CRACKED APPROX 3/4? LONG ; / [01] REPAIRED PER EA NO. 22-154-00212Jan 21, 2022 · N8527Q · Boeing 7378H4SDR FDEA202201200105Web · cracked#2 PYLON STRUT TO WING NACELLE STRUT WEB CRACKED PP STA 200 REPAIRED PER EA # F-5450-T0366482-P1Jan 20, 2022 · N960FD · Boeing 757200SDR CALA2022012000191Frame · crackedB777-06-3-7052 NO.2 PYLON AFT TORQUE BOX INTERNAL LH NAC STA 344 FRAME FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC ZHG506672 AND ORIGINATED BY EMP V896810 NO.2 PYLON AFT TORQUE BOX INTERNAL LH NAC STA 344 NO.5 FRAME WORK ACCOMPLISHED BY MECHANIC V896810 INSJan 19, 2022 · N223UA · Boeing 777222SDR IXXA20220125002Tee Angle · gougedUPPER ANGLE GOUGE ON AFT EDGE, INSIDE #1 PYLON BELOW DIAGONAL BRACE AT NACELLE STA 362...Jan 14, 2022 · N443AZ · Boeing 767323SDR FXGA202201102141None · noneR/H HORIZONTAL STAB FAIRING CRACKED. REPAIR OF CRACK IN R/H HORIZONTAL STAB TO VERT STAB FAIRING. REPAIR HORIZONTAL STAB FAIRINGS PER ENGINEERING DRAWING NR-0014.Jan 10, 2022 · N967CE · Doug DC983SDR FXGA202201102140None · noneL/H HORIZONTAL STAB FAIRING CRACKED. REPAIR OF CRACK IN L/H HOIZONTAL STAB TO VERT STAB FAIRING. REPAIR HORIZONTAL STAB FAIRINGS PER ENGINEERING DRAWING NR-0014.Jan 10, 2022 · N967CE · Doug DC983SDR CALA2022011000093Beam · corrodedA3NB-53-3-6279 AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 HAVE C ORROSION DOT 42-019 EVALUATED AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 WITH CORROS ION OUT OF LIMITS DIM L=1.782, W=1.516, REMAIN THICKNESS 0.3, RE MOVED AND REPLACED FOR NEW BEAM IAW SRM 51-42Jan 9, 2022 · N475UA · Airbus A320232SDR CALA2022011000102None · nonePDA 2 #1 ENG INBD T-R TO PYLON FLEX SEAL SEGMENTS MISSING PIECES ...FIG 3 ITEM 90 AND ITEM 110 OF ECRA 5450-02357 FLIGHT CYCLE AND PERMANENT REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS. REF ECRA 5450-02357 REV-B. ACCOMPLISHED PART 1D INTERIM REPAIR. ISSUE DIP TO Jan 9, 2022 · N451UA · Airbus A320232SDR REXA2022042000656Fairing · damagedUPER L/H TRANSCOWL HINGE FAIRING ASSY. IS DAMAGED AT THE AFT HINGE POINT J/C:900-54-430-300 - REMOVED UPPER TRANS COWL REPLACED WITH NEW IAW CRJ900 AMM 54-12-07Jan 5, 2022 · N197PQ · Cndair CL6002D24SDR MASA20220105011None · noneTHE LH INLET COWL LIPSKIN WAS FOUND TO HAVE EROSION DAMAGE AND WAS BLENDED OUT PER SRM 54-11-05-101-001-A01. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 54-11-05, FIGURE 54-11-05-991-801, ITEM 1 (REV.37 DATED AUG. 15, 2019.)Jan 5, 2022 · N241LR · Cndair CL6002D24SDR MK1Y202201002None · noneFAN COWL SUPPORT BEAM LINK, #2 PYLON, P/N 31112522-1 DURING THE MAINTENANCE INSPECTION AT IAI, THE BORES IN THE #2 PYLON FAN COWL SUPPORT BEAM LINK PIN 311T2522-1 WERE FOUND TO BE WORN. THE BORE DIAMETERS WERE FOUND TO BE Ø.8770". THE NOMINAL DIAMETER OF THEJan 2, 2022 · N396AN · Boeing 767323SDR FDEA202112313159None · none#2 PYLON UNDER PANEL #443HL CORROSION ON INNER SURFACE LOWER CORNER AROUND FASTENER ACCOMPLISHED FEDEX EA# F-5450-T0366121 P1, NACELLES / PYLON - WING PYLON/STRUT - #2 PYLON, INB SIDE, SKIN, INNER SURFACE PP STA 144, CORROSIONDec 31, 2021 · N941FD · Boeing 757200SDR IXXA202112290002Channel · cracked#1 PYLON AFT STRUT V FRAME FOUND INBOARD AFT J CHANNEL CRACKED.Dec 29, 2021 · N762CX · Boeing 767232SDR FDEA202112273152None · cracked#2 PYLON UNDER ACCESS PANEL 611KT FWD OUTBOARD END U-CHANNEL CRACKED. REMOVED AND REPLACED U-CHANNEL ON #2 PYLON UNDER ACCESS PANEL 611KT IAW BAC DWG 313N5004 REV DDec 27, 2021 · N941FD · Boeing 757200SDR MASA20211223646None · noneTHE PYLON DETACHABLE TRAILING EDGE ASSEMBLY WAS FOUND TO HAVE EROSION DAMAGE AFFECTING THE ALUMINUM MESH. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-73-00-201-009-A01, (REV. 38 DATED 7-9-2021).Dec 23, 2021 · N905J · Cndair CL6002D24SDR FDEA202112213114Skin · corroded@2 PYLON LANDING FOR ACCESS PANEL #443GL HAS CORROSION FWD LOWER CORNER NACELLES/PYLONS - SKIN/PLATES/PANELS - #2 PYLON INBD SKIN PANEL, PP STA 114, INNER SURFACE, CORROSION REPAIR PER FEDEX EA F-5430-T0366016Dec 21, 2021 · N941FD · Boeing 757200SDR IXXA2021121803Rib · cracked#1 PYLON RIB CRACKEDDec 18, 2021 · N762CX · Boeing 767232SDR IXXA2021121802Rib · crackedCORE COWL FAIRING RIB CRACKED.Dec 18, 2021 · N762CX · Boeing 767232SDR UIEA2021121402450Latch · none# 2 ENG. STRUT O/B SERVICE PANEL AFT LATCH IS WORN .(<P>REMOVED & REPLACED DAMAGED LATCH AT #2 ENG STRUT O/B FAIRING ACCESS PANEL IAW B767-300</P> / <P>AMM 54-53-02 .</P>)Dec 17, 2021 · N640GT · Boeing 7673S1SDR SWAA2022011353401Fairing · delaminated#1 ENGINE O/B MID STRUT FWD FAIRING PANEL 431BL HAS WEAR/DELAM AT FWD LOWER CORNER. DOT#A193-5 ; / [01] EVALUATED AND FOUND PLIES MISSING AT FWD LWR CORNER EDGEBAND AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 54-50-70-2R-1 TABLE 201 250 DEGREE PRE-PREG AND SRM 5Dec 15, 2021 · N8676A · Boeing 7378H4SDR IXXA2021121505Frame · crackedRUBSTRIP V-FRAME CRACKEDDec 15, 2021 · N762CX · Boeing 767232SDR SWAA2021121452612Sleeve · crackedAPPROXIMATELY 1/2' CRACK AND IMPRESSION #1 ENGINE THRUST REVERSER SLEEVE OUTBOARD ; / [01] COMPLIED WITH EA 21-154-03700Dec 10, 2021 · N8675A · Boeing 7378H4SDR MASA20211130592None · noneOUTER SKIN PANEL OF THE LOWER RH FAN COWL DOOR WAS FOUND TO HAVE WEAR DAMAGE AT THE UPPER AFT CORNER. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-01, FIGURE 54-14-01-991-801, ITEM 1A, EA 72-2021-219.Dec 8, 2021 · N902FJ · Cndair CL6002D24SDR CALA2021120802284Skin · crackedSUPPORT TASK RH PYLON ACCESS DOOR 442AL CUTOUT SKIN FOUND CRACKED TRANSFER REF NON-ROUTINE LP9132040 AND ORIGINATED BY EMP V896826 NO.2 PYLON INBOARD SKIN AT 442AL ACCESS DOOR CUTOUT PERMANENT REPAIRED AS PER ECRA5450-02695 REV A WORK ACCOMPLISHED BY MECHANIC Dec 6, 2021 · N661UA · Boeing 767322SDR FDEA202112063025None · cracked#2 PYLON FAIRING 441AT HAS CRACKED COMPOSITE ON THE AFT UPPER EDGE. ACCOMPLISHED A PERMANENT REPAIR TO THE #2 PYLON FAIRING 441AT CRACKED COMPOSITE ON THE AFT UPPER EDGE IAW B757 SRM 54-51-70 FIG 201 SHEET 1 AND EA F-5451-T0365702-P1 PYLON STRUCTURE-TAIL PDec 6, 2021 · N990FD · Boeing 757200SDR FDEA202112063024None · damaged#1 PYLON FAIRING 431AT HAS COMPOSITE DAMAGE AT OUBD AFT ATTACH HOLE.. ACCOMPLISHED PERMANENT REPAIR TO #1 PYLON FAIRING 431AT COMPOSITE DAMAGE AT OUTBD AFT ATTACHMENT HOLE IAW B757SRM 54-51-70 FIG 201 SHEET 1 AND EA F-5451- T0365724-P1 PYLON STRUCTURE TAILPDec 6, 2021 · N990FD · Boeing 757200SDR CALA2021120602253None · crackedPDA 2 #1 ENG INBOARD T-R TO PYLON FLEX SEAL SEGMENT ((SECOND FROM AFT)) CRACKED AND MISSING -- SEE PHOTO AND ACCOMPLISH PERMANENT REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS. REF ECRA 5450-02357 REV-B FIG 3 ITEM 110 CRACKED AND MISSING. PERFORMED INTERIM REPAIR PDec 5, 2021 · N813UA · Airbus A319131SDR IXXA2021120301HPylon · gougedDAMAGE TO THE INBOARD SIDE OF OUTBOARD LOAD FITTING #2 PYLON.Dec 3, 2021 · N762CX · Boeing 767232SDR IXXA2021120201HVertical Support · erodedNO. 2 PYLON INBOARD VERTICAL FLANGE EROSION NAS 410 TO NAS 411Dec 2, 2021 · N762CX · Boeing 767232SDR UIEA2021111202402Fitting · none#1 PYLON FAN COWL SUPPORT FITTING IS CRACKED ON O/B SIDE LOWER RADIUS.(<P>REMOVED AND REPLACED #1 PYLON FAN COWL SUPPORT FITTING IAW B767 SRM 51-40-02, 51-40-05,AMM 54-51-01, 20-11-00</P>)Nov 27, 2021 · N1709A · Boeing 767375SDR UIEA2021112102430Fitting · none#2 PYLON FAN COWL SUPPORT FITTING IS CRACKED ON I/B SIDE LOWER RADIUS(<P>REMOVED AND REPLACED #2 PYLON FAN COWL SUPPORT FITTING IAW B767 51-40-02-0G-0</P>)Nov 27, 2021 · N1709A · Boeing 767375SDR GTIA2021112636147Pylon · gougedGOUGE FOUND ON PYLON #1 AT RIB 5. RAF-01 2843158-01 OPENED. REF LTPR NR 5001114912-0010.-REVIEWED LTPR NRI 5001114912-0010 AND HAS BEEN ACCOMPLISHED THE EMBODIED REPAIR IS CAT B AND NEED SUBSEQUENT INSP AS 0039 SCHEDULED INSRI TASK 54-51-12-205-002 REV 139, INNov 24, 2021 · N661NK · Airbus A321231SDR MASA20211123568None · noneRH LOWER FORWARD CORE COWL Z MEMBER ON THE AFT EDGE WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-10, FIGURE 4-23-10-991-801, ITEM 10, EA 69-2021-196.Nov 23, 2021 · N246LR · Cndair CL6002D24SDR MASA20211123572None · dentedLH ENGINE THRUST REVERSER FORWARD CORE COWL UPPER INBOARD FACING SHEET WAS FOUND WITH (6) MINOR DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-05-001-001-A01, EA 12-2021-268.Nov 22, 2021 · N902FJ · Cndair CL6002D24SDR R61A2021120100960Frame · crackedRH ENGINE AFT STRUT FAIRING, FRAME 7 CRACKED. REPLACED FRAME #7 IAW 51-43-04Nov 17, 2021 · N653RW · Emb ERJ170100SESDR MASA20211119565None · noneOUTBOARD LOWER FACING SHEET OF THE RH UPPER CORE COWL BONDMENT ASSEMBLY WAS FOUND TO HAVE 2EA GOUGES. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-15, 54-23-15-991-801, ITEM 2, EA 72-2021-212. DEFECT LOCATION: RH FWD CORE COWL BONDMENT ASSEMBLNov 17, 2021 · N246LR · Cndair CL6002D24SDR MASA20211112557None · noneR/H LOWER FORWARD CORE COWL REINFORCING LATCH WAS FOUND TO HAVE WEAR DAMAGE, WHICH IS LOCATED AT THE FREE EDGE AT THE LATCH, LOCATED ALONG THE EDGE WHERE THE DOOR LATCH ENGAGES AND CAUSES WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-10-001Nov 12, 2021 · N246LR · Cndair CL600*SDR SWIA202163502None · elongatedL/H ENGINE LOWER THURST REVERSER C-DUCT, NYLON INSERT MOUNTING SCREW HOLES THROUGH SHEET METAL STRUCTURE ARE OBLONG /DAMAGED (C-CHECK RO 1/7/2022) PERFORMED OVERSIZE BOLT HOLE REPAIR TO LH ENGINE LOWER THRUST REVERSER C-Oct 28, 2021 · N794SK · Cndair CL6002C10SDR SWAA2021111741485Shield · cracked#1 ENGINE INBD FAN COWL BRACKET AFT OF OIL SERVICE DOOR IS CRACKED / REPLACED SHIELD ON #1 ENGINE INBD FAN COWL AFT OF OIL SERVICE DOOR P/N 314-2259-4 I-A-W SRM 51-40-02 & CMM 71-13-30.Oct 28, 2021 · N8672F · Boeing 7378H4SDR 7C7A2021102300032None · noneL/H NACELLE HORSE COLLARASSY, AFT LOWER ANGLE CRACKED ON OUTBOARD SIDE BETWEEN 9 - 10 O'CLOCK. REPAIRED IAW RD8-54-4461.Oct 23, 2021 · N893EA · Dhav DHC8106SDR 7C7A2021102300029None · noneL/H NACELLE HORSE COLLAR ASSY. FWD WEB FLANGE ON INBOARD SIDE CRACK BETWEEN 9 - 10 O' CLOCK. REPAIRED IAW RD8-54-4469Oct 23, 2021 · N893EA · Dhav DHC8106SDR IXXA2022021401Web · cracked#1 PYLON LOWER PAN WEB CRACKED IN RADIUS AND BENT INWARD ON O/B AND I/B SIDE AT NAS. 410.50 WHERE BOTTOM OF 313T1380 SKIN PANEL AND V-FRAME ATTACHOct 22, 2021 · N762CX · Boeing 767232SDR 7C7A2021102200028None · noneL/H NACELLE HORSE COLLAR ASSY, FORWARD WEB FLANGE ON OUTBOARD SIDE, CRACK BTW 9 & 10 O'CLOCK. CRACK REMOVED BY CUTTOUT & ANGLE DOUBLER IAW RD8-54-4469Oct 22, 2021 · N893EA · Dhav DHC8106SDR EE4Y2021101914076Pylon · corrodedDURING THE STRUCTURE INSPECTION, WE FOUND THE LH PYLON, UPPER SPARS LUGS BUSHING WITH CORROSION. AFTER BUSHINGS REMOVAL AS PER AMM TASK 20-10-08-000-801-A PARAGRAPH 1.E. (1), WE DISCOVERED THAT THE LUGS BORE HAD CORROSION.WAS REPAIRED FOLLOWING EMBRAER REPAIR Oct 19, 2021 · N956QQ · Emb ERJ190100IGWSDR MASA20211018493None · noneDAMAGE ON THE SKIN OUTER PANEL OF THE LOWER FAN COWL DOOR WHICH WAS SUBSEQUENTLY BLEND OUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-01-001-001-A01, FIGURE 54-14-01-991-801, ITEM 1A, EA 80-2021-144.Oct 16, 2021 · N930LR · Cndair CL6002D24SDR CALA2021101801904Spar · crackedB767-06-3-7110 - NO.2 PYLON STA175 RH UPPER SPAR WEB FOUND CRACKED AT HYD TUBE CUTOUT POSITION TRANSFER REF NR LP9131205 AND ORIGINATED BY EMP V896810 RII INSPECTED BY HX126723 ADD EMP:V896826 NO.2 PYLON NAC STA175 RH UPPER SPAR WEB CASE DRAIN TUBE CUTOUT INTEOct 16, 2021 · N666UA · Boeing 767322SDR R61A2021110600878Bushing · migrated************************MAJOR************************WHILE AC WAS IN FOR HVY CK FOUND RH PYLON OB LOWER LINK FITTING GAP FOUND BTWN FLANGE BUSHING AND THE CLAMP UP BUSHING (0.006") ALSO AT THE TOP A GAP FOUND BTWN THE FLANGE OF THE BUSHING AND THE PYLON FITTINOct 15, 2021 · N650RW · Emb ERJ170100SESDR SWIA202162953None · corrodedTHE GALLEY #1 HAS CORRODED DOUBLER LOCATED BEHIND THE FLOOR FITTING AT THE FWD EDGE/OTBD FITTING. (C-CHECK RO 11-27-21) REPLACED THE CORRODED DOUBLER LOCATED BEHIND THE FLOOR FITTING AT THE FWD EDGE/OTBD FITTING ON THE GALLEY #1 WITH A SERVICEABLE DOUBLEROct 14, 2021 · N797SK · Cndair CL6002C10
Back to JASC 5400