JASC 5420

Service difficulty reports · 3,949

Reports filed under 5420 · Nacelle/Pylon Miscellaneous 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 = '5420'
  ORDER BY difficulty_date DESC"

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SDR QXEA200602512Bracket · crackedC4 YYC - RIGHT NACELLE OUTBOARD, HYDRAULIC PRESSURE MANIFOLD BRACKET CRACKED. REPAIRED IAW EA 2-54-297 AND SRM 51-40-11.Sep 9, 2006 · N357PH · Dhav DHC8202SDR QXEA200602535Support Angle · crackedC4 YYC -LEFT NACELLE, INBOARD SIDE, HYDRAULIC RETURN MANIFOLD MOUNTING PLATFORM CENTER SUPPORT ANGLE IS CRACKED. REPAIRED IAW EA 2-54-297 AND SRM 51-40-11.Sep 8, 2006 · N357PH · Dhav DHC8202SDR HALA0600686Seal · damagedBLADE SEAL DAMAGED ON LEADING EDGE ON NR 2 ENGINE PYLON PANEL NR 441AT. REMOVED RIVETS FROM NR 2 ENG PYLON PANEL NR 441 AT BLADE SEAL IAW SRM 51-40-02.Aug 28, 2006 · N597HA · Boeing 767300SDR HALA0600685Attach Fitting · crackedIB T-CLIP IS CRACKED ON NR 2 ENGINE PYLON AT FWD IB END OF HYDRAULIC BAY, NAS STATION 308. REMOVED AND REPLACED T-CLIP ON NR 2 ENGINE PYLON AT FWD IB END OF HYDRAULIC BAY NAC, STA 308. IAW SRM 51-40-02.Aug 28, 2006 · N597HA · Boeing 767300SDR UPS06547837Doubler · mismanufacturedNR 2 PYLON LT AFT DOUBLER GAS SHORT E.D. ON FWD END TRIMMED AND CHAMFER DISCREPANT DOUBLER-TRIMMED APPROX 0.75 MANUFACTURED A NEW FILLER BASE ON 311N 3401-6. INSTALL 311N3401-15 DOUBLER INSTALL FILLER IAW EA 757-5410-27-A1521.Aug 22, 2006 · N430UP · Boeing 75724APFSDR KCSA061258Fireshield · gougedGOUGE ON NR 3 PYLON STA 2363.85 ON FIRE SHIELD APPROX 2 INCH SQUARE.Aug 16, 2006 · N703CK · Boeing 747212BSDR QXEA200602121Repair · damagedPDX C4 - NR 2 LOWER COWL PREVIOUS REPAIR PATCH HAS BEEN CHAFED BY TORQUE TUBE. REPAIRED IAW RD 8-54-602.Aug 14, 2006 · N359PH · Dhav DHC8202SDR UPS06247830Support · crackedINSPECTION TYPE-C ENGINE NR 2 SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL HAS SUSPECT CRACK ON RT CHORD BETWEEN AFT CONE BOLT HOUSING AND REAR SPAR AT 2 FOOT FROM TOP OF CHORD HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. CRACK CONFIRMED. CHORD REPLACED IAW DRAug 10, 2006 · N942UP · Boeing 72722CSDR AWXA200601497Support · crackedSAL - FOUND CRACK ON OUTBOARD EXTENSION ANGLE SUPPORT ON ENGINE NR 1 PYLON. ANGLE SUPPORT ON ENGINE NR 1 PYLON WAS REPLACED IAW A319 SRM 51-72-11, PAGE 1-2.Aug 8, 2006 · N822AW · Airbus A319132SDR 06FDEA02885Truss Fitting · gougedGOUGE FOUND AT ENG MOUNT FWD BORE LOWER SURFACE AT RT TRUSS FITTING OF NR 1 PYLON. JOB ACCOMPLISHED AS PER EA 1-5400-102197 TITLE:" PYLON- WING PYLON ASSEMBLY, NR 1 FWD ENGINE MOUNT TRUSS REPAIR". CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02884Truss Fitting · chafedCHAFE MARK (1 PLACE) AT RT TRUSS FITTING OF NR 1 PYLON. JOB ACCOMPLISHED AS PER EA1-5400-102197 TITLE:" PYLON- WING PYLON ASSEMBLY NR 1 FWD ENGINE MOUNT TRUSS REPAIR. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02883Truss Fitting · chafedCHAFE MARK (6 PLACES) AT LT TRUSS FITTING OF NR 1 PYLON. JOB ACCOMPLISHED AS PER EA1-5400-102197 TITLE:" PYLON- WING PYLON ASSEMBLY NR 1 FWD ENGINE MOUNT TRUSS REPAIR. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02882Truss Fitting · chafedCHAFE MARK (2 PLACES) AT RT TRUSS FITTING OF NR 3 PYLON FWD ENG MOUNT. JOB ACCOMPLISHED AS PER EA 1-5400-102209 TITLE:"PYLON- WING PYLON ASSEMBLY, NR 3 FWD ENGINE MOUNT TRUSS REPAIR. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA02881Truss Fitting · chafedCHAFE MARK (4 PLACES) AT LT TRUSS FITTING OF NR 3 PYLON FWD ENG MOUNT. JOB ACCOMPLISHED AS PER EA1-5400-102209 TITLE:" PYLON- WING PYLON ASSEMBLY, NR 3 FWD ENGINE MOUNT TRUSS REPAIR". CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Aug 7, 2006 · N521FE · Doug MD11SDR QXEA200602081Structure · crackedPDX C4 .25 INCH CRACK ON LEFT HAND LOWER NACELLE FORWARD INBOARD CORNER. REPAIRED IAW RD 8-54-874.Aug 7, 2006 · N351PH · Dhav DHC8202SDR 06FDEA2835Web · crackedON NR 1 PYLON FOUND 1 EA CRACK 1.25 INCH LONG ON UPPER WEB AT STA YN 310. REMOVED PUSH PULL CABLES IAW MM 76-11-02-2 PAR 3, DISASSEMBLIED PIPES IAW MM 20-10-01-2, 28-00-01-2, REMOVED PULLEY, BRACKETS IAW SRM 51-31-02 VOL 2, MM 20-50-02-2, DISASSEMBLIED WEB ANAug 4, 2006 · N365FE · Doug MD1010FSDR MALA060500Structure · chafedLT NACELLE, LOWER INLET DECK IS CHAFED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO S54095. REF EAMS WORK ORDER 214211 TASK 4503.Aug 2, 2006 · N438XJ · Saab 340BSDR UPS06M47399Web · crackedNR 2 ENG PYLON WEB CRACKED ABOVE AFT HOIST ATTACH POINT LT SIDE. REMOVED DAMAGED LOWER WEB, ANGLE FITTING AND SUPPORT STRUT. ROUTED TE S/M SHOP FOR REPAIR. REWORKED SUPPORT STRUT LINK BY COLD WORKING PER EO MD11-5410-24738. ACCOMPLISHED HFEC OF LINK PER HDJul 22, 2006 · N254UP · Doug MD11FSDR SWIA200616922Structure · detachedRIGHT ENGINE HAS A PIECE OF COWL DETATCHED FROM IT'S FASTENING POINTS AND BENT BACK WHERE THE UNDERSIDE OF THE ENGINE PYLON MEETS THE ENGINE. REPLACED RIGHT ENGINE LOWER "STANG" FAIRING IAW CRJ MM 78-30-01.Jul 20, 2006 · N459SW · Cndair CL6002B19SDR UIEA200600179Brace · chafedNR 1 PYLON DIAGONAL BRACE HAS A CHAFED AREA ON OB SIDE ZONE 3A. ACCOMPLISHED BLENDOUT REPAIR AND FOUND WITHIN LIMITS IAW SRM 54-41-01 FIG. 3. PERFORMED FPI OF REWORKED AREA, NO DEFECTS FOUND IAW ASTM 1417-05. SHOT PEENED REWORKED AREA IAW SOPM 20-10-03. TREAJul 20, 2006 · N536MC · Boeing 747228FSDR DHL2006809507Panel · crackedNR 4 PYLON INBD ADAPTER PANEL 1" CRACK STA YN 323.000 LT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 70 SB 54-93 CONDITION V. REMOVED FASTENERS FROM REPAIR AREA AND ATTACH PARTS IAW DC8 70 SB 54-93, SRM 51-1-21, SRM 51-3-0. FABRICATED DOUBLERS (4) (AL707Jul 18, 2006 · N809DH · Doug DC873FSDR 06FDEA2614Bushing · damagedPYLON 3 FOUND SLEEVE WEAR AND FITTING CLEVIS WITH HOLES BUSHING OVALIZED. CHECKED DIAMETER CLEVIS FITTING, AND VERIFIED SLEEVE DIAMETER IAW CMM 20-20-06 FIG 5 REF SRM 57-20-00, CLEVIS FITTING REMOVAL IAW MM 57-00-00-2. REWORKED HOLES, FABRICATED/INSTALLED REJul 18, 2006 · N365FE · Doug DC1010SDR 06FDEA2608Splice · crackedDURING GENERAL OPENING PYLON 3 RE OAN J/C ACCESS PNL ENG PYLON 3 FOUND 1 EA CRACK 1 INCH LONG ON SPLICE OF FAIRING 488DL (REMOVED PART). PERFORMED STOP DRILL HOLE AND FABRICATED & INSTALLED ANGLE IAW SRM 51-35-01 PAGE 1/13 REF SRM 54-00-01 FIG 2B SHT 2.Jul 18, 2006 · N365FE · Doug MD1010FSDR MALA060477Structure · chafedDURING 4K CHECK IN BNA FOUND RT NACELLE LOWER DECK IS CHAFFED OUT OF LIMITS. INSTALLED DOUBLER OVER DAMAGED AREA IAW EO NR S54095. REF: EAMS WORK ORDER 214182-4511Jul 17, 2006 · N437XJ · Saab 340BSDR MALA060478Structure · damagedDURING 4K CHECK IN BNA FOUND LT NACELLE LOWER DECK IS CHAFFED OUT OF LIMITS. INSTALLED DOUBLER OVER DAMAGED AREA IAW EO NR S54095. REF: EAMS WORK ORDER 214182-4516Jul 17, 2006 · N437XJ · Saab 340BSDR UIEA200600171Brace · chafedPYLON NR 4 DIAGONAL BRACE HAS A CHAFE ON OUTBOARD SIDE CAUSED BY HYDRAULIC COMPARTMENT DOOR ROD FOUND NOT SECURED. ACCOMPLISHED BLEND REPAIR ON BRACE P/N 321U2731-102, S/N MFR 16889 RP 06709322 AS PER 747 SRM 51-41-01 FIG 3 AND REFERENCE ATLAS AIR XEO NO. 54-Jul 11, 2006 · N505MC · Boeing 7472D3BSDR 06FDEA2492Stiffener · crackedFOUND VERTICAL STIFFENER (P/N AUB 7358-1) ON NR 3 PYLON AT LT T/R, CENTER HINGE CRACKED.Jul 10, 2006 · N68053 · Doug DC1010SDR AWXA200601167Plate · lightning strikeSAL - MAJOR REPAIR - CHECK NR BC - 4. RN NR 5945019. LIGHTNING STRIKE ON BLANKING PLATE ON STATIC PORT EXTERNAL FUSELAGE AT FRAME 4 - 0.5 Z + 62 CM. REVLORED AREA ON BLANKING PLATE OF STATIC PORT FRAME 4 - 0.5 + Z + 62 CM. APPROXIMATELY SIDE LH ER NO. 25 - 531Jul 4, 2006 · N820AW · Airbus A319132SDR UIEA200600152Drag Brace · chafedNR 4 PYLON DIAGONAL BRACE WAS CHAFED ON OUTBOARD SIDE, DUE TO CONTACT WITH HYDRAULIC COMPARTMENT DOOR ROD. AREA WAS BLENDED AND 0.070 INCH OF MATERIAL WAS REMOVED AND FOUND WITHIN LIMITS AS PER 747 SRM 54-41-01 FIG 3. ALSO, REFERENCE ATLAS XEO 54-062906. FPJun 30, 2006 · N523MC · Boeing 7472D7BSDR UIEA200600151Drag Brace · chafedNR 3 PYLON DIAGONAL BRACE HAS 2 AREAS OF CHAFING DUE TO CONTACT WITH HYD COMPART DOOR LATCH BOLTS. BRACE WAS BLENDED WITH A TIME LIMITED REPAIR AS PER 747 SRM 51-41-01 FIG 3. FWD BLEND IS ON BRACE ZONE "4", BLENDED TO 2 5/8 INCH LONG BY 1 5/8 INCH WIDE AND 0Jun 30, 2006 · N523MC · Boeing 7472D7BSDR 2006UALA01271Angle · crackedNR 1 PYLON INBOARD END OF MIDSPAR CLOSE OUT ANGLE OUTBD FASTENER HOLE HAS APPROX 1 INCH CRACK. REPAIRED CLOSE OUT ANGLE WITH DOUBLER, TRIPLER, FILLER. THE CLOSE OUT ANGLE NEEDS TO BE 85625 REPLACED AT C12 TO FACILITATE MIDSPAR FITTING INSPECTIONS.Jun 27, 2006 · N662UA · Boeing 767322SDR 2006UALA01270Angle · crackedNR 2 PYLON INBOARD MIDSPAR FITTING CLOSE OUT ANGLE OUTBD FASTENER HOLE HAS APPROX .375 INCH CRACK. CRACK FOUND IN CLOSEOUT ANGLE THAT COVERS TWO AFT-MOST FASTENERS IN LOWER HORIZONTAL TANG OF NR 2 PYLON INBOARD MIDSPAR FITTING. HFEC TO ENSURE THERE ARE NO CRJun 27, 2006 · N662UA · Boeing 767322SDR UIEA200600144Bearing · migratedPYLON NR 4 DIAGONAL BRACE LOWER SPAR FITTING BEARING MIGRATED. BEARING WAS REMOVED AND REPLACED WITH NEXT AVAILABLE OVERSIZED BEARING P/N KSC273624B-090 AS PER SRM 54-41-03 AND MM 54-10-03.Jun 24, 2006 · N517MC · Boeing 747243BSDR UIEA200600159Fitting · damagedNR 4 WING SIDE DSB FITTING OUTBD BEARING HOLE BORED TO 2.2768". (FINAL HOLE 0 FOR 3RD, OVERSIZE 2.2745" - 2.2755"). C/O SLEEVE REPAIR ON NR 4 DSB FITTING AS PER BOEING REPLY MESSAGE NR 1-202125094-7. C/O MAGNETIC PARTICLE INSPECTION ON MACHINED SURFACE AS PJun 23, 2006 · N526MC · Boeing 7472D7BSDR QXEA200602146Panel · crackedPDX: RT NACELLE OUTBOARD SIDE BULKHEAD AT X W135, OUTBOARD LWR CORNER OF PANEL IS CRACKED. MAINTENANCE REPAIRED IAW RD 8/4-57-679, HORIZON EA 6-57-495 AND NDTM PART 6, 51-00-01.Jun 16, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602145Panel · crackedPDX: RT NACELLE INBOARD SIDE, BULKHEAD AT X W135, INBOARD LOWER CORNER OF PANEL IS CRACKED. MAINTENANCE REPAIRED IAW RD 8/4-57-679, HORIZON EA 6-57-495, NDTM PART 6, 51-00-01 AND Q400 SRM 51-41-05-800-801.Jun 16, 2006 · N424QX · Bombdr DHC8402SDR DL757060498Fitting · misdrilledTHE ATTACH HOLE IN THE SIDE LINK FITTING IS BEYOND ANGULAR TOLERANCE. A TAPERED RADIUS FILLER WAS INSTALLED TO PROPERLY ALIGN THE HOLE.Jun 14, 2006 · N635DL · Boeing 757232SDR QXEA200602171Fitting · damagedPDX: NR 1 ENGINE AFT INBOARD SIDE COWL DOOR AFT DOOR STRUT PEDESTAL FITTING THREADS WORN OFF UNER PANEL 412BR. MAINTENANCE REPAIRED IAW RD 8/4-54-152 AND HORIZON EA 6-54-416.Jun 13, 2006 · N424QX · Bombdr DHC8402SDR QXEA200602165Fitting · damagedPDX: NR 1 ENGINE, AFT OUTBOARD SIDE COWL DOOR AFT DOOR STRUT PEDESTAL FITTING THREAD STRIPPED OFF. MAINTENANCE REPAIRED IAW RD 8/4-54-152 AND HORIZON EA 6-54-416.Jun 13, 2006 · N424QX · Bombdr DHC8402SDR DL757060499Fitting · misalignedINSTALLATION OF MODIFICATION TENSION CLIPS WOULD REQUIRE MORE THAN THE ALLOWED 0.005 INCH SPOT FACE. A TAPERED FILLER WILL BE USED TO INSTALL THE TENSION CLIPS.Jun 13, 2006 · N635DL · Boeing 757232SDR DL757060496Bushing · looseTHE NR 1 AND NR 2 PYLON WING DRAG FITTINGS HAVE BUSHING MIGRATION. THE BUSHINGS WERE REMOVED, THE HOLES INSPECTED; AND REPLACEMENT BUSHINGS INSTALLED.Jun 13, 2006 · N635DL · Boeing 757232SDR QXEA200601403Web · brokenPDX C4 RIGHT HAND NACELLE FORWARD OF CENTER DOOR FRAME IS BENT AND HAS A PIECE BROKEN OUT OF CORNER RADIUS OF WEB. REPAIRED IAW DHC-8-200 SRM 51-40-11.Jun 2, 2006 · N352PH · Dhav DHC8202SDR MALA060354Structure · chafedDURING 4K CHECK IN BNA FOUND RT NACELLE AT NS197 IS CHAFED OUT OF LIMITS AT THE 3:00 POSITION. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EOS54165.May 31, 2006 · N435XJ · Saab 340BSDR MALA060355Structure · chafedDURING 4K CHECK IN BNA FOUND LEFT NACELLE AT NS197 IS CHAFED OUT OF LIMITS AT THE 3:00 POSITION. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EOS54164.May 31, 2006 · N435XJ · Saab 340BSDR QXEA200601486Diaphragm · crackedPDX: LT NACELLE OUTBOARD DIAPHRAM CRACKED. MAINTENANCE REPAIRED IAW Q400 SRM 51-40-07-320-801, SRM 51-40-15-330-801 AND SRM 51-40-05-330-801.May 29, 2006 · N409QX · Bombdr DHC8402SDR AWXA200600901Support Angle · crackedSAL - MAJOR REPAIR - NR 5911063 - DURING BC4 CHECK DISCOVERED CRACK ON SUPPORT ANGLE LOCATED LT PYLON OUTBOARD SIDE FROM PYLON STA 537 TO PYLON STA 608. MAINTENANCE REMOVED AND INSTALLED NEW SUPPORT ANGLE EXTRUSION FROM PYLON STA 537 TO PYLON STA 608 IAW AIRBMay 26, 2006 · N817AW · Airbus A319132SDR CALA0600183Clip · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON NAC STA 285.4 O/B UPPER CLIP. THE CLIP WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.May 21, 2006 · N76054 · Boeing 767424ERSDR QXEA200601349Diaphragm · crackedPDX: C3. LT NACELLE, OB DIAPHRAGM IS CRACKED. MAINTENANCE REPAIRED IAW SRM 51-40-15-330-801 AND SRM 51-42-05-330-801.May 20, 2006 · N406QX · Bombdr DHC8402SDR USAA060714Bushing · wornLEFT WING STRUT, FWD LOAD FITTINGS. REMOVED & REPLACED BUSHINGS 2 EACH, PER EO 5700T254A, EA 97668.May 18, 2006 · N648US · Boeing 767201SDR USAA060715Bushing · wornLT WING STRUT, FWD LOAD FITTINGS. REMOVED & REPLACED BUSHINGS 2 EACH, PER EO 5700T254A, EA 97668.May 18, 2006 · N648US · Boeing 767201
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