JASC 5410

Service difficulty reports · 4,110

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 IPXA2026052040363Rub Strip · crackedCRACKED RUB STRIP, NO. 2 ENG L/H CORE COWL INNER SIDE UPPER AREA. I.A.W. AMM 71-11-06-714-013-H00 REV.148 INSTALLED THE CORE COWL. CONDITION CHECKED NORMAL AND JOB COMPLETED. INSTALL NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURESMay 12, 2026 · N394UP · Boeing 767381SDR VNAA20260512037Acoustic Panel · crackedIN REF TO NRC 0254 AFTER REMOVAL OF COAMING LATCH CRACK ON ACUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL. ACOUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL WAS REPAIRED PER REO PER REO 670-54-21-1818 REV. -A.May 12, 2026 · N541EA · Cndair CL6002C10SDR VNAA202606300006Latch · wornWEAR ON LATCH REIFORCING OF ACCESS DOOR 444BB AT RT ENGINE. LATCH REIFORCING OF ACCESS DOOR 444BB AT RH ENGINE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01.May 11, 2026 · N530EA · Cndair CL6002C10SDR IPXA2026052022086Seal · brokenBROKEN SEAL, NR 1 PYLON FAIRING PNL 436CL SPRING SEAL AREA. INSTALL NEW SEAL I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 311T2570 SH 1 REV: N.May 11, 2026 · N394UP · Boeing 767381SDR IPXA2026052024998Spring · brokenBROKEN- SPRING, NR 2 PYLON AFT FAIRING PANEL NO. 446CR. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 311T2570, SH 1, REV N.May 11, 2026 · N394UP · Boeing 767381SDR IPXA2026051721345Longeron · chafedCHAFED LONGERON, NR 1 ENG LT CORE COWL EXTERNAL AFT LWR EDGE. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.May 11, 2026 · N394UP · Boeing 767381SDR IPXA2026051722233Longeron · chafedCHAFED LONGERON NR 1 ENG RT CORE COWL INNER SKIN AFT LWR EDGE. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-24, REV. 50.May 11, 2026 · N394UP · Boeing 767381SDR VNAA202606300003Shield · chafedRIGHT CORE COWL FIRE SHIELD CHAFE WITHIN 5335.13 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: EVALUATE SRM 54-23-00-201-005-A01 FOR A PERMANENT REPAIR IF OUT OF LIMay 10, 2026 · N530EA · Cndair CL6002C10SDR IPXA2026051912479Fireshield · chafedCHAFED FIRESHIELD, NR 1 ENG FAIRING PANEL 436BL INNER PLATE AREA. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 55, & DWG 311T2570, SH 1, REV N.May 10, 2026 · N394UP · Boeing 767381SDR IPXA2026051312172Seal · brokenBROKEN-SEAL STRIP, NO.2 PYLON FAIRING PNL NO.446CL SPRING SEAL. REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW SEAL STRIP I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 311T2570 SH. 1 REV. N.May 10, 2026 · N301UP · Boeing 76734AFSDR DALA2026051102935Receptacle · corrodedLEVEL 2 CORRSION, CORROSION SPIGOT RECEPTACLE FITTING ON RH PYLON. REPLACED SPIGOT RECEPTACLE FITTING ON RH PYLON AS PER A319 SRM 54-51-41-000-001- A, A319 SRM 54-51-41-400-001-A AND A319 SRM54- 51-12-300-001 MEASURED OF CORROSION AREA: D:0.0041 INCH AND OF DMay 10, 2026 · N366NB · Airbus A319114SDR IPXA2026051698681Frame · chafedCHAFED FRAME, NR 2 ENG LT CORE COWL INNER NR 4 FRAME AREA. ACCOMPLISHED ZEE FRAME REPAIR I.A.W SRM 54-45-01-2R-3 REV. 95 AND EGAT WORK SHEET NO.60388.May 9, 2026 · N301UP · Boeing 76734AFSDR IPXA2026051302042Bracket · wornWORN - BRACKET, NO.1 ENG R/H CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET.May 9, 2026 · N301UP · Boeing 76734AFSDR DALA2026051102932Receptacle · corrodedLEVEL 2 CORRSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER AS PER A319 SRM 54-51-12 AND AS PER A319 SRM 51-74-00 AND SRM 51-44-11 AND AS PER A320 FAM AMM 54-51-41-000-001-A AND AMM 54-51-41-400 -00May 9, 2026 · N366NB · Airbus A319114SDR IPXA2026051493816Hinge Fitting · brokenNR 1 ENG I\B FAN COWL INNER SURFACE FWD ATTACH FITTING BROKEN. INSTALLED NEW FWD FITTING AT #1 ENG I\B FAN COWL IAW SRM 51-40-21-001.May 8, 2026 · N163UP · Airbus A300F4622RSDR SWAA2026051195596Fairing · crackedNR 2 ENGINE PYLON AFT FAIRING PLUME SUPPRESSOR HAS A CRACK. REPAIRED IAW SRM 54-50-70-2R-7.May 5, 2026 · N8718Q · Boeing 7378SDR DALA2026050602890Fitting · corrodedLEVEL 2 CORROSION. ENGINE NR 1 PYLON AREA SPIGOT RECEPTACLE FITTING BORE WITH CORROSION AND BALL JOINT WITH INUSUAL WEAR. REPLACED NR 1 PYLON SPIGOT BALL JOINT AND FITTING IAW SRM 54-51-12-300-001, REV 157, AND AMM 54-51 -41-400-001-A, AND 54-51-41-400-001-A May 5, 2026 · N368NB · Airbus A319114SDR FDEA202605050557Fastener · looseENG PYLON HAS SEVERAL LOOSE FASTENERS ON OUTSIDE NEAR AFT MOUNTMay 5, 2026 · N617FE · Doug MD11FSDR FDEA202605050555Fastener · looseSEVERAL LOOSE FASTENERS ON O/B SIDE OF # 1ENG PYLON JUST BELOW THE FWD PYLON ATTACH FITTING.May 5, 2026 · N617FE · Doug MD11FSDR FDEA202605050554Pylon · not reportedWS-C 00091685 MOD TYPE T MOD NO. 1-5450-T0386257 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386257 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386257 REV NO: PS P4 EA: 1-5May 5, 2026 · N617FE · Doug MD11FSDR FDEA202605050553Pylon · not reportedWS-C 00091685 MOD TYPE T MOD NO. 1-5450-T0386257 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386257 REV NO. POS. P2. COMPLY WITH E..A. 1-5450-T0386257 REV NO: PS P2 SRM: 5May 5, 2026 · N617FE · Doug MD11FSDR FDEA202605050552Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P2. EA: 1-5450-T0386268 P2 COMPLIED WITH REV NO. PS PT.2 E.A May 5, 2026 · N621FE · Doug MD11FSDR FDEA202605050551Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386268 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386268 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386268 REV NO: PS P1 EA: 1-5May 5, 2026 · N621FE · Doug MD11FSDR FDEA202605050550Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NR POS. P2 PLND. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P2 May 5, 2026 · N621FE · Doug MD11FSDR FDEA202605050549Pylon · not reportedWS-C 00091735 MOD TYPE T MOD NO. 1-5450-T0386269 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386269 REV NO. POS. P1. COMPLY WITH E..A. 1-5450-T0386269 REV NO: PS P1 EA: E.AMay 5, 2026 · N621FE · Doug MD11FSDR FDEA202605050548Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386263 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386263 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386263 REV NO: PS P4 EA: 1-5May 5, 2026 · N521FE · Doug MD11FSDR FDEA202605050547Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386263 REV NO. PS P4 NACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386263 REV NO. POS. P4. COMPLY WITH E..A. 1-5450-T0386263 REV NO: PS P4 EA: 1-5May 5, 2026 · N521FE · Doug MD11FSDR FDEA202605050545Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386807 REV NO. PS P2 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAG COMPLY WITH E..A. 1-5450-T0386807 REV NO. POS. P2. COMPLY WITH E..A. 1-5450-T0386807 REV NO: PS P2 EA: 1-5May 5, 2026 · N521FE · Doug MD11FSDR FDEA202605050544Pylon · not reportedWS-C 00091807 MOD TYPE T MOD NO. 1-5450-T0386807 REV NO. PS P1 NACELLES/PYLON - WING PYLON/STRUT - NO. 3 PYLON, INSPECTION AND REPAIR OF DAMAGE COMPLY WITH E..A. 1-5450-T0386807 REV NO. POS. P1 COMPLY WITH E..A. 1-5450-T0386807 REV NO: PS P1 EA: 1-54May 5, 2026 · N521FE · Doug MD11FSDR IPXA2026051616378Panel · crackedPYLON #1, PANEL 413BL HAS CRACKS 2(EA) AT THE GRILL DOT 31-021, PANEL STORED IN THE PANEL RACK AREA. ACCOMPLISHED WELD REPAIR ON PANEL 413BL, #1 PYLON, LOUVRE IAW A300-600 SRM 54-52-51-201 AND TRAVELER #: T26/1805003.May 4, 2026 · N156UP · Airbus A300F4622RSDR QXEA2026051100105Structure · chafedRIGHT HAND LEADING EDGE AT PYLON IS CHAFED. REPAIRED IAW SRM 57-49-01 REPAIR 7. MATERIAL USED T024T3.May 3, 2026 · N635QX · Emb ERJ170200LRSDR QXEA2026051100104Structure · damagedLEFT LEADING EDGE OVER PYLON IS CHAFED. REPAIRED IAW SRM 57-49-01 REPAIR 7. MATERIAL USED T024T3 .063"May 3, 2026 · N635QX · Emb ERJ170200LRSDR IPXA2026050685587Seal · brokenBROKEN SPRING SEAL, NO.2 ENG PNL 446CR. INSTALLED NEW STRIP SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO.311T2570 SH.16 REV-.May 2, 2026 · N385UP · Boeing 767300SDR IPXA2026050685364Bracket · crackedCRACKED BRACKET, NR 2 PYLON AFT FAIRING INNER INBD TUBE NR 3 SUPPORT BRACKET CRACK. PERFORMED THE HEAT TREATMENT FROM 2024-O TO T42 CONDITION I.A.W. W/S NO.60331 STEP 3. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND DWG 313T2385 SH 4 REV: -.May 2, 2026 · N385UP · Boeing 767300SDR IPXA2026050585581Seal · brokenBROKEN SEAL, NR 1 PYLON RT FAIRING PANEL 436CR. INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 311T2570 SH 16 REV: -May 2, 2026 · N385UP · Boeing 767300SDR IPXA2026050585589Seal · brokenBROKEN SPRING SEAL, NR 2 ENG PANEL 446CL. INSTALLED NEW SPRING SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 311T2570 SH 16 REV: -May 2, 2026 · N385UP · Boeing 767300SDR SWAA2026052794427Support Web · crackedCRACK SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE 2. REPLACED SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE 2 IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 REV 34. PAGE 10090 DETAIL P; FIGURE 3; SHEET 5.Apr 30, 2026 · N8645A · Boeing 7378H4SDR IPXA2026050652037Bracket · crackedCRACKED BRACKET, NO.1 PYLON AFT LWR FAIRING INNER DRAIN TUBE SUPPORT BRACKET QTY 2 EA. PERFORMED THE HEAT TREATMENT FROM 2024-O TO T42 CONDITION I.A.W. W/S NO.60322 STEP 3. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 313T2385 SH 1 REVApr 30, 2026 · N385UP · Boeing 767300SDR DALA2026043002741Fairing · debondedNUMBER 1 ENG PYLON AFT FAIRING DISBONDING INBOARD SIDE. C/W ER/A 634190-14 (8946532) (AIRCRAFT GROUNDED)Apr 29, 2026 · N198DN · Boeing 767332SDR SWIA2026042876856Web · crackedINDICATION FOUND ON ENGINE BEAM UPPER WEB, UNDER LBL 31.41, ANGLE BETWEEN FWD 2 FASTNERS AT 100% FSH, FAILED NDT. REPAIRED THE ENGINE BEAM UPPER WEB UNDER LBL 31.41 ANGLE BTWN FWD TWO FASTENERS IAW REO 601R-53-61-8536, REV -, AND SKY CARD 51-900-1003-SKY.Apr 28, 2026 · N926SW · Cndair CL6002B19SDR KCSA202604281034Panel · crackedCRACK FOUND ON MONOLITHIC PANEL ON I/B SIDE OF #1 PYLON AFT SIDE OF 434 DR PANELApr 28, 2026 · N774CK · Boeing 777F1HSDR DALA2026042902711Fitting · corrodedLEVEL 2 CORROSION BORE SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING LOC. ON RH PYLON IAW SRM 54-51- 12-300-001-A. MEASURE OF DIAMETER WAS: 4.350 INCH. TOOL USED: DIGITAL CALIPER P/N 500-197-30; S/N: B23316908; DUE DATE: 12-NOV -26. SEE INDIVApr 26, 2026 · N341NW · Airbus A320212SDR SWIA2026042576295Tie Bar · gougedLEFT ENGINE FAN COWL, PYLON TIE BAR HAS A GOUGE ON FWD SIDE WHERE IT ATTACHES TO THE PYLON. REPAIRED LT ENGINE FAN COWL, PYLON TIE BAR IAW REO 670-54-12-895, REV -.Apr 25, 2026 · N703SK · Cndair CL6002C11SDR SWIA2026042576284Tie Bar · chafedLEFT HAND FAN COWL - PYLON TIE BAR, UPPER ATTACHMENT POINT ON PYLON BRACKET CHAFED. REMOVED CHAFE FROM L/H FAN COWL PYLON TIE BAR UPPER ATTACHMENT POINT ON PYLON BRACKET PER IAW SRM 51-12-00-001-001-A01, REWORKED AREA FOUND TO BE WITHIN LIMITS IAW REO 670-54-Apr 25, 2026 · N703SK · Cndair CL6002C11SDR VNAA202606060014Acoustic Liner · crackedAFTER Z STIFFENER REMOVAL ON LOWER RH TRANSCOWL CRACK WAS FOUND ON ACOUSTIC PANEL. LOWER RH TRANSCOWL ON ACOUSTIC PANEL WAS REPAIRED PER REO NUMBER 690-54-21-635 REV - -Apr 24, 2026 · N606NN · Cndair CL6002D24SDR IPXA2026042723638Inlet Door · dentedDENTED INNER BARREL, NR 2 ENG INLET COWL INNER AT THE 12 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.4", 13" FROM AFT EDGE AND 13" FROM INBD EDGE, AT 12 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WApr 22, 2026 · N384UP · Boeing 767300SDR IPXA2026042900034Latch · no testENG #2 O/B FAN COWL PRESSURE RELIEF DOOR LATCH TEST FAILED. REPLACED 1EA DOOR LATCH AT ENG. #2 O/B FAN COWL PRESURE RELIEF DOOR IAW A300-600 SRM 51-40-21-001.Apr 21, 2026 · N163UP · Airbus A300F4622RSDR IPXA2026042703429Fireshield · chafedCHAFED FIRESHIELD, NR 1 PYLON FAIRING PANEL 436BL INNER PLATE.   INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.Apr 21, 2026 · N320UP · Boeing 76734AFSDR IPXA2026042703484Fireshield · chafedCHAFED FIRESHIELD, NR 2 PYLON LT FAIRING PANEL 446BL.  INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.Apr 21, 2026 · N320UP · Boeing 76734AFSDR HYIA20260422001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY DISCOVERED ON THE INBOARD FACE OF THE RIGHT HAND INBOARD ENGINE BEAM IN THE AREA OF THE VERTICAL ATTACH CHANNELS FOR THE CROSSOVER BEAM. THIS CRACK WAS DISCOVERED AFTER CHANGING THE CROSSOVER BEAM VERTICAL ATTACH BRACKETApr 21, 2026 · N4630N · Cessna 402C
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