JASC 5411

Service difficulty reports · 1,454

Reports filed under 5411 · Nacelle/Pylon, Frame/Spar/Rib, 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 = '5411'
  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 USAA2014111900004Rib · crackedRON VISIT NR 1 ENG PYLON NR 13 RIB CRACKED. REMOVED, LOCATED, & INSTALLED NEW LOWER SECTION OF RIB NR 13 IAW SRM 51-42-11.Nov 17, 2014 · N637AW · Airbus A320231SDR USAA2014111900002Rib · crackedRON VISIT NR 1 ENG PYLON NR 12 RIB CRACKED. REMOVED, LOCATED & INSTALLED NEW LOWER SECTION OF RIB 12 IAW SRM 51-42-11.Nov 17, 2014 · N637AW · Airbus A320231SDR CALA2014101392397Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. ACCOMPLISHED INSPECTION REQUIREMENTS IAW RDAS, SPAR HAS INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-20Oct 10, 2014 · N492UA · Airbus A320232SDR CA151123001Frame · corroded(CAN) CORROSION WAS FOUND ON THE OUTER SURFACE OF THE FRAME DURING INCORPORATION OF AN UNRELATED SERVICE BULLETIN. AFTER BLENDING OUT THE CORROSION THE MINIMUM REMAINING THICKNESS WAS 0.071", FROM A NOMINAL THICKNESS OF 0.120". STATIC STRENGTH ANALYSIS OF THE Sep 26, 2014 · Bombdr DHC8400SDR FDEA201409252768Rib · crackedRIGHT PYLON CANTILEVER BEAM ON RIB J08 - RIB A11 FOUND CRACKED. REPAIRED IAW SRM 54-52-11 FIG.201. MAJOR REPAIR IAW GMM6-2-100.Sep 25, 2014 · N655FE · Airbus A300F4605RSDR FDEA201409252767Rib · crackedLEFT PYLON CANTILEVER BEAM ON RIB J08 - RIB A11 FOUND CRACKED. REPAIRED IAW SRM 54-52-11 FIG.201. MAJOR REPAIR IAW GMM6-2-100.Sep 25, 2014 · N655FE · Airbus A300F4605RSDR ASOA2014102311479Frame · gougedLEFT AFT CORE COWL MID FRAME GOUGED. REMOVED DAMAGE IAW SRM 54-13-00-101-001-A01. FROM AFDL 520336, Z MID JOINT OUT OF LIMITS DUE TO BLEND AREA WITHIN 2D OF FASTENER NEEDS TO BE SUBMITTED FOR REPAIR. RECEIVED AND COMPLIED WITH STS EA 32-2014-102, SECTION I-Sep 16, 2014 · N709EV · Cndair CL6002C10SDR CALA2014111092671Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTSep 15, 2014 · N492UA · Airbus A320232SDR CALA2014091892227Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR APPROVED FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTION & THRESHOLD MUSTSep 13, 2014 · N492UA · Airbus A320232SDR IPXA2014091184253Rib · crackedINSPECTION 3C, NR 3 ENGINE INBD CORE COWL AFT RIB CRACKED. REPAIRED IAW CV14-4901 AND EO 7110-55425-A.Aug 21, 2014 · N254UP · Doug MD11FSDR AALA20140820002Frame · crackedFOUND SMALL CRACK ON THE RT ENG PYLON NAC STATION 285 INBD FRAME. R & R RT ENG PYLON INBD FRAME AT NAC STATION 285 IAW AARD 51-00-005-1.Aug 20, 2014 · N357AA · Boeing 767323SDR KCSA201408061078Frame · damagedNR 1 PYLON LT FRAME DAMAGED AT MAIN PNEUMATIC DUCT NAC STA 200.Aug 6, 2014 · N794CK · Boeing 747222BSDR REXA2014080600756Spar · gougedLEFT ENG PYLON BOX FRAME FWD ENG YOKE MOUNT SPAR GOUGED IN THREE PLACES. REPAIRED IAW REO 601R-54-51-341.Aug 4, 2014 · N8828D · Cndair CL6002B19SDR USAA2014073000011Spar · damagedC4 CHECK ELONGATED HOLES ON NR 1 PYLON UPPER, AFT SPAR WEB BETWEEN PYLON STATIONS PPS 195 TO 210, PP WL 154. REPAIRED NR 1 PYLON UPPER, AFT SPAR WEB IAW EA 506056.Jul 29, 2014 · N940UW · Boeing 7572B7SDR CALA2014071591467Spar · wornNUMBER 1 PYLON LOWER SPAR HAD WEAR SPOT FROM CONTACT WITH THE CNA AT RIB 5. THE BLEND OUT IS .019 INCHES DEEP & 0.400 INCHES WIDE. AN ANTI-CHAFE PLATE WAS INSTALLED IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES RE-INSPECTION IAW SRI 54-51-12-2-001-00 PARA 3 AJul 12, 2014 · N439UA · Airbus A320232SDR CALA2014071591466Spar · wornNUMBER 2 PYLON LOWER SPAR HAD WEAR SPOT FROM CONTACT WITH THE CNA AT RIB 5. THE BLEND OUT IS .003 INCHES DEEP & 0.100 INCHES WIDE. AN ANTI-CHAFE PLATE WAS INSTALLED IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES RE-INSPECTION IAW SRI 54-51-12-2-001-00 PARA 3 AJul 12, 2014 · N439UA · Airbus A320232SDR CALA2014071191434Spar · crackedNUMBER 1 PYLON UPPER SPAR WEB HAS TWO CRACKS, ONE EACH AT INBD & OTBD DRAIN HOLES AS SEEN THROUGH ACCESS PANEL 416AR. CONTAINED CRACKS, MACHINED STEPPED DOUBLERS & FABRICATED FILLERS & INSTALLED REPAIR IAW ECRA 5453-01087, REO-G17581 REV IR & SRM 54-53-01 REPJul 6, 2014 · N667UA · Boeing 767322SDR QXEA2014062600531Rib · crackedAFT RIB ON UPPER COWL PANEL 424AL IS CRACKED. REMOVED CRACKED STIFFENER ON AFT RIB, UPPER COWLING REF DWG 85414014 & SRM 54-45-10. INSTALLED STIFFENER ON AFT RIB, UPPER COWLING PN 85414014-101 IAW SRM 54-45-10. NO DEFECTS NOTED. RECEIVED NEW STIFFENER PO TX8Jun 23, 2014 · N437QX · Bombdr DHC8402SDR CALA2014062091313Spar · chafedNUMBER 2 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. ACCOMPLISHED REPAIR IAW SRM54-51-12 FIG 202. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.Jun 17, 2014 · N490UA · Airbus A320232SDR CALA2014062091312Spar · chafedNUMBER 1 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. ACP REPAIR IAW SRM 54-51-12 FIG 202. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.Jun 17, 2014 · N490UA · Airbus A320232SDR CALA2014062091308Spar · chafedNUMBER 2 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. REPAIR ACCOMPLISHED. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.Jun 17, 2014 · N849UA · Airbus A319131SDR CALA2014061791297Spar · chafedNUMBER 2 PYLON SHOWS SIGNS OF CHAFING AT FIREWALL SEAL LOWER SPAR RIB 5. ACCOMPLISHED REPAIR TO NR 5 RIB SPAR ON NR 2 PYLON IAW SRM54-51-12 FIG 202. SRI INSPECTIONS WILL BE ACCOMPLISHED AS REQUIRED.Jun 16, 2014 · N849UA · Airbus A319131SDR UIEA2014060900228Frame · crackedNUMBER 2 PYLON AFT FAIRING LOWER & FRAME FOUND CRACKED. THE DAMAGED PORTION TRIMMED OUT IAW RT 54-53-10569 REV A HFEC INSPECTION CUT OUT & NO CRACK FOUND IAW NTM PT6 51-00-01. REPAIR PARTS INSTALLED IAW RI 54-53-10569 REV A.Jun 9, 2014 · N644GT · Boeing 7673JHFSDR ABXA20140603185Rib · corrodedSTRUT CORRODED. R & R SHIMS ON OTBD LOWER STRUT IAW SRM 51-40-02 & DWG 114T2233. CORRODED L2, PN 114T2218, PART NAME AIR LOAD RIB, SN NSN, LOCATION STRINGER & WS FROM 785.0 TO 786.0. ACFT WAS GNDED.Jun 3, 2014 · N790AX · Boeing 767281SDR AALA20140529013Frame · crackedRIGHT ENG PYLON, INBD SIDE AT STATION 285 FRAME HAS ONE INCH CRACK AT UPPER END. R & R RT ENG PYLON INBD SIDE AT STATION 285 FRAME IAW AARD 51-00-05-1 PROCEDURE REPAIR 1.May 29, 2014 · N389AA · Boeing 767323SDR AALA20140524006Frame · crackedNUMBER 2 PYLON FRAME CHORD AT STATION 285.450 OTBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW SRM 51-10-02 & DWG 311T2400.May 24, 2014 · N371AA · Boeing 767323SDR AALA20140524005Frame · crackedRIGHT PYLON FRAME CHORD AT STATION 285.450 INBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW B767-300 SRM 51-10-02 & DWG 311T2400.May 24, 2014 · N371AA · Boeing 767323SDR CALA2014051991064Spar · chafedNUMBER 1 PYLON LOWER SPAR HAD CHAFE MARK FROM CONTACT WITH THE CNA. BLENDED & WITHIN LIMITS IAW SRM 54-51-12 FIG 103. MAX MATERIAL LOSS IS 0.017, EXTENDED CHAFE PLATE INST IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES INSPECTION IAW SRI54-51-12-2-001-00 PARA May 19, 2014 · N487UA · Airbus A320232SDR CALA2014051991056Spar · wornLT NR 1 PYLON LOWER SPAR HAD A .005 WEAR MARK ON THE PYLON LOWER SPAR FROM CONTACT WITH THE CNA. THE WEAR WAS BLENDED IAW SRM54-51-12 FIG 103, & AN ANTI-CHAFING PLATE INSTALLED IAW SRM 54-51-12, 5B FIG 202. REQUIRES INSPECTION IAW SRI 54-5 1-12-2-001-00 PARAMay 16, 2014 · N846UA · Airbus A319131SDR CALA2014051991055Spar · wornNUMBER 2 PYLON LOWER SPAR HAD A .005 WEAR MARK ON THE PYLON LOWER SPAR FROM CONTACT WITH THE CNA. THE WEAR WAS BLENDED IAW SRM 54-51-12 FIG 103, & AN ANTI-CHAFING PLATE INSTALLED IAW SRM 54-51-12, 5B FIG 202. REPAIR WAS ACCOMPLISHED ON NR37572. REQUIRES INSPMay 16, 2014 · N846UA · Airbus A319131SDR DALA14018941812Spar · crackedNR 1 PYLON UPPER SPAR WEB FOUND CRACKED AT IDG POWER FEEDER CABLE CUTOUT POSITION. C/A NR 1 PYLON UPPER SPAR WEB REPLACED IAW ER/A 521608-14, REV ORIG.Mar 26, 2014 · N836MH · Boeing 767432ERSDR QXEA2014032400233Rib · crackedPANEL 414AR HAS CRACK ON THE 3RD RIB. REPLACED RIB SRM 51-42-05, STEP 4D(3-10).Mar 19, 2014 · N407QX · Bombdr DHC8402SDR QXEA2014032400232Rib · crackedPANEL 414AL HAS A CRACK ON 3RD RIB. REPLACED STIFFENER IAW SRM 51-42-05, STEP 4D(3-10).Mar 19, 2014 · N407QX · Bombdr DHC8402SDR QXEA2014032400229Rib · crackedPANEL 414AR HAS A CRACKED MOST AFT RIB. INSTALLED NEW AFT STIFFENER, RIB, COMMON TO PANEL 414AR IAW SRM 51-42-05, PAR 4D, STIFFENER, RIB, PN 85414249-102. REMOVED MOST AFT CRACKED STIFFENER, RIB, PN 85414249-102 COMMON TO PANEL 414AR IAW SRM 51-42-05, PAR 4EMar 19, 2014 · N407QX · Bombdr DHC8402SDR QXEA2014032400228Rib · crackedRIB CRACKED AT X171-X180 ON INBD NR 2 NACELLE. RIB INSTALLED ON RT OTBD NACELLE IAW SRM 51-42-05.Mar 19, 2014 · N407QX · Bombdr DHC8402SDR SWAA2014040126711Rib · crackedLEFT WING NR 1 PYLON LOWER AFT HALF RIB CRACKED AT UPPER INBD RADIUS. R & R NR 1 PYLON IAW SRM.Mar 17, 2014 · N361SW · Boeing 7373H4SDR DJFA20140220001Rib · crackedDURING INSPECTION, THE LT INBD AFT PYLON SUPPORT RIB WAS FOUND CRACKED. RIB REPLACED.Feb 20, 2014 · N737FL · Cessna 750SDR SIMA20140219020Rib · crackedRT UPPER ENG COWL OTBD RIB IS CRACKED JUST AFT OF THE AFT MOST ATTACHMENT HINGE POINT. REPAIRED RT UPPER ENG COWL OTBD RIB IAW SRM 54-10-07.Feb 19, 2014 · N651AE · Emb EMB145LRSDR KCSA201401221005Frame · crackedNR 1 PYLON FRAME IS CRACKED AT NAC STA. 236 NEAR MAIN PNEUMATIC DUCT SUPPORT ROD.Jan 22, 2014 · N794CK · Boeing 747222BSDR SWIA201436206Frame · crackedCRACK ON LT OTBD NACELLE OTBD OF FWD UPPER LATERAL FWD ATTACH POINT. C-CHECK REPLACED LT OTBD NACELLE FWD UPPER LATERAL FWD ATTACH POINT FRAME IAW SRM.Jan 20, 2014 · N567SW · Emb EMB120ERSDR AALA20131121006Spar · damagedLT HAND PYLON WAS FOUND TO AN OVERSIZED HOLE COMMON TO THE INBD MIDSPAR FITTING, MIDSPAR WEB & T-CHORD FITTING & STRAP. ACCOMPLISHED REPAIR IAW EA 767-54-032580 & ECO C3369. REMOVED HOLE THRU MIDSPAR WEB & MID SPAR CHORD ROUND & TRUE AT A DIAMETER OF .625 & Nov 21, 2013 · N374AA · Boeing 767323SDR AALA20131118012Fitting · damagedMID BULKHEAD TO LOWER SPAR FITTING HOLE OVERSIZED. INSTALLED FREEZE PLUG IN LOWER SPAR CHORD FITTING IAW SR 3-2513303349 & EA B757-54-032537.Nov 18, 2013 · N645AA · Boeing 757223SDR SWIA201335449Frame · crackedRT NACELLE CRACKED FRAME AT FWD COWL FWD BAYONET LATCH RECEPTACLE. C-CHECK REPLACED RT NACELLE FRAME AT FWD COWL FWD BAYONET LATCH.Nov 7, 2013 · N299SW · Emb EMB120ERSDR CALA2013102892428Spar · abnormalNR 1 PYLON FWD UPPER SPAR WEB INBD & OTBD DRAIN HOLES HAVE PREVIOUS REPAIRS. THE EXISTING REPAIR WAS REMOVED AT NAC STATION 156, & THE LT DRAIN HOLE WAS FOUND CRACKED PAST THE PREVIOUS STOP DRILLS. A NEW REPAIR WAS INSTALLED IAW REO G16676, REV A & SRM 54-53-Oct 25, 2013 · N647UA · Boeing 767322SDR CALA2013102492344Spar · crackedNR 2 PYLON UPPER SPAR WEB AT NAC STATION 156, BOTH DRAIN HOLES ARE CRACKED. REPAIRED THE UPPER SPAR WEB IAW REO G16606, REV A & ECRA 5450-02099 INCORPORATING TWO MACHINED DOUBLERS & TWO RADIUS FILLERS IAW NOTE B OF SRM 54-53-01, REPAIR 10.Oct 23, 2013 · N647UA · Boeing 767322SDR QXEA2013102501448Rib · crackedLT UPPER COWL PANEL 414AT HAS CRACKED RIB. REMOVED CRACKED RIB ON PANEL 414AL IAW SRM 51-42-05. LOCATED & DRILLED NEW RIB ON PANEL 414AL IAW SRM 51-40-07. NEW RIB ON PANEL 414AL REQURIES INSTALLATION. INSTALLED NEW RIB PN 85414215-102 ON PANEL 414AL, REF SROct 21, 2013 · N415QX · Bombdr DHC8402SDR QXEA2013102501447Rib · crackedLEFT UPPER COWL PANEL 414AL HAS CRACKED RIB. REMOVED CRACKED RIB ON PANEL. 414AL IAW SRM 51-42-05. LOCATED & DRILLED NEW RIB ON PANEL 414AL IAW SRM 51-40-07. INSTALLED NEW RIB PM 85414215-101 ON PANEL 414AL, REF SRM 51-42-05.Oct 21, 2013 · N415QX · Bombdr DHC8402SDR SWIA201335221Frame · crackedLT NACELLE FRAME NR 1 CRACKED AT TORSION MOUNTS. C-CHECK REPLACED LT NACELLE FRAME NR 1 IAW SB.Oct 17, 2013 · N568SW · Emb EMB120ERSDR SWIA201335220Frame · crackedRT NACELLE FRAME NR 1 CRACKED AT TORSION MOUNTS. C-CHECK REPLACED RT NACELLE FRAME NR 1 IAW SB.Oct 17, 2013 · N568SW · Emb EMB120ERSDR FDEA201310152510Spar · corrodedNR 1 PYLON UPPER SPAR CAP INBD LANDING IS CORRODED. CLEANED CORRISION AND BLENDED LANDING PER SRM 51-21-01 VOL II AND EA 8-5450-T0303216.Oct 15, 2013 · N377FE · Doug MD1010F
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