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 UPS05445810Thrust Link · crackedINSPECTION TYPE:AD NR 2 ENG REF TAR FORM S/N: 115643 - UPS REQUEST REPLACEMENT OF THRUST LINK. NR 2 ENG THRUST LINK REPLACED AND BOTH ATTACH BOLTS REPLACED AS PER AMM 71-21-03.Nov 19, 2005 · N521UP · Boeing 747200SDR UPS05445809Thrust Link · crackedINSPECTION TYPE:AD NR 4 PYLON REAR ENGINE MOUNT THRUST LINK AFT LUG FOUND CRACK INDICATION AT UPPER AND LOWER SURFACE APPROX 100 PERCENT FSH. NR 4 ENG MOUNT THRUST LINK REPLACED AS PER AMM 71-21-03.Nov 19, 2005 · N521UP · Boeing 747200SDR UPS05445808Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 3 PYLON THRUST LINK AFT LUG LOWER SURFACE BY APPROX 90 PERCENT FSH. NR 3 ENG PYLON THRUST LINK REPLACED AND AFT MOUNTING BOLT REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200SDR UPS05445807Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 3 PYLON THRUST LINK FWD LUG LOWER SURFACE BY APPROX 60 PERCENT FSH. NR 3 ENG THRUST LINK REPLACED AND AFT MOUNT BOLT REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200SDR UPS05445806Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED NR 1 PYLON THRUST LINK AFT LUG LOWER SURFACE BY APPROX 90 PERCENT FSH. NR 1 PYLON THRUST LINK REPLACED AND FWD AND AFT MOUNT BOLTS REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200SDR UPS05445805Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 1 PYLON THRUST LINK FWD LUG LOWER SURFACE BY APPROX 80 PERCENT FSH. NR 1 PYLON THRUST LINK REPLACED AND FWD AND AFT MOUNT BOLTS REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200SDR UPS05445782Link · crackedINSPECTION TYPE:AD NR 3 ENGINE REAR MOUNT THRUST LINK CRACK INDICATION REVEALED AT FWD LUG UPPER SURFACE 80 PERCENT FSH & AFT UPPER SURFACE 50 PERCENT FSH BOTH EXCEED LIMIT. NR 3 ENG REAR MOUNT THRUST LINK CHANGED REF MM 71-21-03.Nov 16, 2005 · N677UP · Boeing 747123FSDR 05FDEA03812Rib · crackedNR 1 PYLON FAIRING 475CL INNER BODY NR 5 AND NR 6 RIBS ARE CRACKED.Nov 14, 2005 · N721FD · Airbus A300B4622RSDR 2005FA0001550Cowl Door · crackedDURING ROUTINE INSP, FOUND 25 INCH CRACK, SEVERE DELAMINATION WITHIN THE LT ENG LOWER COWL DOOR. AFFECTED AREA IS LOCATED JUST AFT OF FWD SIDE, BETWEEN THE 4 & 8 O'CLOCK POSITION. INITIAL INSPECTION REVEALS DEBOND ON CARBON FIBER SKIN TO CORE AT 375 SQUARE Nov 9, 2005 · N888CW · Gulstm GULFSTREAMGVSDR UPS05445732Link · crackedNR 4 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT FWD END LUG UPPER EXIT LIMIT. NR 4 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-I NR 4 ENG REMOVED AND INSTALLED (FOR ACCESS) AS PENov 8, 2005 · N676UP · Boeing 747123SDR UPS05445731Link · crackedNR 3 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG LOWER EXIT LIMIT. NR 3 ENG REAR MOUNT THRUST LINK REPLACED PER EO B747-7120-22596-A WORK CARRIED OUT ON TASK CARD APPENDIX-H. NR 3 ENG REMOVED AND INSTALLED (FOR ACCESS) AS Nov 8, 2005 · N676UP · Boeing 747123SDR UPS05445720Link · crackedINSPECTION TYPE:AD NR 1 NACELLE REAR ENGINE MOUNT THRUST LINK, CRACK INDICATION REVEALED AT AFT END LUG EXCEEDED LIMIT. NR 1 ENG REAR MOUNT THRUST LINK REPLACED AS PER EO B747-7120-22596-A ON APPENDIX-F. ENG REMOVED AND REINSTALLED AS PER UPS TASK CARD TC 50Nov 4, 2005 · N672UP · Boeing 747123SDR 05FDEA03594Fitting · damagedCRACK FOUND ON RT AFT CTR FASTENER HOLE AT BANJO NR 4 FTG FAYING SURFACE. VIEW LOOKING I/B AT 2 O'CLOCK DIRECTION. CRACK LENGTH FROM THE EDGE OF THE BANJO NR 4 FTG APPROX 1/8 INCH LONG. CORRECTIVE ACTION: SNRM N1614: BANJO FTG R/H NO.4 AFT CENTER FASTENER Nov 1, 2005 · N574FE · Doug MD11SDR QXEA200501695Shield · tornYYC - DURING C3 CHECK, RIGHT ENGINE RIGHT LOWER MID CORE COWLING FIRE SHIELD LAYER IS TORN AND DISBONDED. REPAIRED IAW EA R-54-84.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR QXEA200501699Striker · wornYYC - DURING C3 CHECK, RIGHT ENGINE LOWER TRANSITION COWLING LATCH COVER DOOR REBATES AND STRIKER PLATE WORN. LATCH BEARING PADS REPLACED (2 EA) IAW CRJ-700 SRM 51-42-06-001-001-A01.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR QXEA200501605Spar · tool damageYYC - DURING C3 CHECK, FUSELAGE INTERIOR FORWARD SIDE AT STATION 1088.2 BETWEEN STRINGERS 9L AND 10L PYLON SPAR PART NUMBER 670-37140-001 TOP SURFACE HAS A DRILL MARK. MAINTENANCE BLENDED OUT DAMAGE IAW EA R-54-86 AND REO 670-54-51-007. RESTORED SURFACE.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR QXEA200501604Spar · tool damageYYC - DURING C3 CHECK, FUSELAGE INTERIOR FORWARD SIDE AT STATION 1088.2 BETWEEN STRINGERS 9R AND 10R. PYLON SPAR PART NUMBER 67037140002 TOP SURFACE HAS SEVERAL DRILL MARKS. MAINTENANCE BELNDED OUT DAMAGE IAW EA R-54-86 AND REO 670-54-51-007. RESTORED SURFAOct 31, 2005 · N603QX · Cndair CL6002C10SDR UPS05445717Link · crackedNR 3 ENG REAR ENGINE MOUNT THRUST LINK FWD LUG LOWER OF BORE FOUND SUSPECTED CRACK INDICATION WHICH WAS GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR Oct 31, 2005 · N522UP · Boeing 747212BSDR UPS05445716Link · crackedNR 3 ENG REAR ENG MOUNT THRUST LINK AFT LUG UPPER AND LOWER OF BORE FOUND SUSPECTED CRACK INDICATIONS WHICH WERE GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASKOct 31, 2005 · N522UP · Boeing 747212BSDR UPS05445715Link · crackedNR 3 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT FWD LUG UPPER SIDE, THE INDICATION GREATER THAN 40 PERCENT FSH, EXCEEDED LIMIT. REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CARD NR 500Oct 28, 2005 · N522UP · Boeing 747212BSDR UPS05445714Link · crackedNR 2 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT BOTH FWD AND AFT END LUG, BOTH INDICATION GREATER THAN 40 PERCENT FSH (EXCEEDED LIMIT). REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CAROct 28, 2005 · N522UP · Boeing 747212BSDR UPS05445713Link · crackedNR 1 ENG MOUNT THRUST LINK SUSPECTED CRACK INDICATION REVEALED AT BOTH FWD AND AFT END LUG, BOTH INDICATION GREATER THAN 40 PERCENT FSH (EXCEEDED LIMIT). REFER TO EO NR B747-7120-22596-A FOR THRUST LINK REPLACEMENT. ENGINE REMOVED AND REINSTALLED ON TASK CAROct 28, 2005 · N522UP · Boeing 747212BSDR UPS05445653Link · crackedAD NR 4 PYLON REAR MOUNT THRUST LINK AFT IND LUG FOUND CRACK INDICATION EXCEED LIMIT. NR 4 PYLON REAR UPPER MOUNT THRUST LINK ASSY CHANGED AND INSTALLED MM 71-21-03.Oct 25, 2005 · N681UP · Boeing 747121SDR UPS05445652Link · crackedAD NR 4 PYLON REAR ENGINE MOUNT THRUST LINK FWD END LUG FOUND CRACK INDICATION EXCEEDED LIMIT. NR 4 PYLON REAR UPPER ENGINE MOUNT AFT THRUST LINK ASSY CHANGED AND INSTALLED IAW MM 71-21-03.Oct 23, 2005 · N681UP · Boeing 747121SDR UPS05445651Link · crackedAD NR 2 PYLON REAR ENGINE MOUNT THRUST LINK ULTRASONIC INSP FOUND CRACK INDICATION EXCEEDED LIMIT AT BOTH FWD AND AFT LUG. NR 2 PYLON REAR UPPER ENGINE MOUNT AFT THRUST LINK ASSY CHANGED AND INSTALLED IAW MM 71-21-03.Oct 23, 2005 · N681UP · Boeing 747121SDR 2005FA0001437Stud · collapsedTHE STUD SPRINGS ARE COLLAPSING UPON INSTALLATION. SUSPECT POOR HEAT-TREATING OF THE SPRINGS. NOTICED EXCESSIVE CHAFFING (SMOKING) FROM THE ENGINE COWLING SINCE AIRCRAFTS WERE NEW. AT ABOUT 300TT THE RECEPTACLES FOR THE STUDS STARTED TO FAIL. WHEN NEW STUDS Oct 17, 2005 · Cessna 172RSDR CA051013003Bolt · shearedWHILE CARRYING OUT CANADAIR SB601R-53-061 PART C, BOLT P/N NAS6204L11ON THE RT SIDE ENGINE PYLON WAS FOUND SEPARATED IN TWO PARTS. FRACTURE OCCURRED UNDER THE HEAD OF BOLT. BOTH THE HEAD AND SHANK OF THE BOLT LOCATED ARE IN OUR POSSESSION. WILL BE DOING A DOct 12, 2005 · Cndair CL6002B19SDR 05FDEA03390Structure · chafedNR 2 ENGINE BS 1342, MATING SURFACE FOR RT FWD COWL CHAFED, WORN TO KNIFE EDGE AT 5:30 TO 6:00 O'CLOCK POSITION. REPLACED 1342 CHORD PER SRM 51-30-2.Oct 11, 2005 · N499FE · Boeing 727200SDR 05FDEA03134Angle · crackedNR 2 PYLON AFT AREA INSIDE PNL 474DR L ANGLE SUPPORT IS CRACKED.Sep 27, 2005 · N445FE · Airbus A310203SDR 05FDEA03133Angle · crackedNR 1 PYLON AFT AREA INSIDE PNL 474DR L ANGLE SUPPORT IS CRACKED.Sep 27, 2005 · N445FE · Airbus A310203SDR 2005FA0001342Mount · tornDURING A ROUTINE 100 HOUR INSPECTION, 2 OF THE (LORD) COWLING MOUNTS THAT SECURING THE LOWER ENGINE COWLING TO THE AIRFRAME WERE FOUND TORN IN HALF. THIS IS A RECURRING PROBLEM ON ALL C AND S MODEL AC OPERATED BY A LOCAL FLIGHT SCHOOL. IF NOT CORRECTED THIS Sep 23, 2005 · N7265B · Cessna 172RSDR DL757050716Fairing · misinstalledDURING MODIFICATION OF THE NR 2 PYLON FAIRING PER EO 06-075080-03AD THE MOD DOUBLER FOR THE NR 1 PYLON WAS INADVERTENTLY INSTALLED. INCORRECT DOUBLER WAS REPLACED WITH A SIMILAR DOUBLER CONTOURED TO MATCH THE NR 2 PYLON FAIRING. REF AD 2003-18-05.Sep 14, 2005 · N646DL · Boeing 757232SDR 2005FA0001302Mount · tornDURING THE COURSE OF A ROUTINE 100 HOUR INSPECTION, 3 OF THE RUBBER (LORD) COWLING MOUNTS WERE FOUND TORN. THIS HAS BEEN A COMMON OCCURRENCE SEEN WHILE MAINTAINING A FLEET OF THIS MODEL AC OPERATED BY A FLIGHT SCHOOL. IF NOT ADDRESSED THIS COULD LEAD TO A LOSep 13, 2005 · N5027X · Cessna 172SSDR 2005FA0001304Mount · tornTHE RUBBER (LORD) MOUNTS USED TO ATTACH THE ENGINE COWLING TO THE AIRFRAME ARE FAILING AT A RATE OF ABOUT 3 MOUNTS EVERY 100 HOURS. MAINTAIN A FLEET OF THESE MODEL AIRCRAFT USED IN A FLIGHT SCHOOL ENVIRONMENT AND SEE THIS REGULARLY ON THESE AIRCRAFT. IF NOT Sep 12, 2005 · N78JA · Cessna 172RSDR USAA051070Fitting · gougedNR 2 PYLON UPPER SPAR, AFT HOLE, OUTER SURFACE GOUGE. SPOT FACED DAMAGED AREA HFEC INSPECTED, SHOT PEENED, TREATED & INSTALLED FASTENER PER EA 96808. DEFECT SIZE: .045 INCH DEEP, 15.5 PERCENT MATERIAL LOSS.Sep 9, 2005 · N628AU · Boeing 7572B7SDR UIEA200500121Angle · out of limitsD-CHECK, NR 4 PYLON SIDE COWL HINGE SUPPORT ANGLE BRACE, ONE HOLE EXCEEDING LIMITS. THE HOLE WAS OVERSIZED TO 0.484 INCHES DIAMETER INCLUDING A .0312 DIAMETER INSURANCE CUT. THE HOLE WAS NDT INSPECTED TO ENSURE A CRACK AND DAMAGE FREE CONDITION. A REPAIR STAug 30, 2005 · N524MC · Boeing 7472D7BSDR AU510001835Latch · brokenENGINE CORE COWL NR 6 LATCH BROKEN. FURTHER INVESTIGATION FOUND NR 1, NR 3, NR 4 AND NR 5 LATCHES CRACKED.Aug 9, 2005 · Boeing 7377Q8SDR MALA050626Structure · chafedRT LOWER NACELLE DESK IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 54095. REF EAMS WORK ORDER 212637 TASK 4507.Jul 31, 2005 · N452XJ · Saab 340BSDR MALA050625Structure · chafedRT NACELLE ATNS 197 OB SIDE IS CHAFED AND HAS BEEN REPAIRED IAWS MESABA EO 54124 REF EAMS WORK ORDER 212637 TASK 4508.Jul 31, 2005 · N452XJ · Saab 340BSDR 05FDEA02109Spar · crackedPYLON STRUCTURE CANTILEVER BEAM LWR SPAR WEB CRACK. COMPLIED WITH EA 6-5450-82109, PYLON STRUCTURE CANTILEVER BEAM LWR SPAR WEB CRACK.Jul 26, 2005 · N656FE · Airbus A300F4605RSDR CA050726007Cowl Door · missingAIRCRAFT DIVERTED AFTER DEPARTURE, FOR NR 1 ENGINE OIL PRESSURE INDICATION PROBLEM. UPON ARRIVAL AT GATE FOUND UPPER HALF OF LT CORE COWL MISSING.Jul 24, 2005 · Cndair CL6002B19SDR EIA2005147Access Panel · crackedA CRACK WAS FOUND ON NR 3 ENG, RT CORE COWL AT LOCATION OF ACCESS PANEL 473AR. REMOVED PREVIOUS REPAIRS, FAF0581021BBED NEW REPAIR PARTS AND INSTALLED PER ECRA 487-54-016-2.BJul 12, 2005 · N487EV · Boeing 747230BSDR 05FDEA01599Frame · crackedNR 1 ENG FIXED COWL AFT LWR END SKIN AND FRAME IS CRACKED. TRIMMED DAMAGE SKIN IAW SRM 54-30-1 FIG 1 DETAIL 6. REMOVED AND REPLACED FRAME IAW SRM 51-10-1 AND SRM 51-30-2.Jun 13, 2005 · N262FE · Boeing 727200SDR 2005UALA00555Structure · dentedNR 2 ENGINE INLET COWL DENTED AT APPROXIMATELY 4 O`CLOCK. DENT IS OUT OF LIMITS. INSTALLED REPAIR PER SRM 54-10-01 FIG 203 DET II.Jun 12, 2005 · N910UA · Boeing 737522SDR DHL2005741608Duct · defectiveREPAIR OF NR 2 ENG S-DUCT INNER SKIN AREA. CUT OUT 5 EA HAT CHANNEL SECTION ON OUTER RING OF THE S-DUCT FOR ACCESS TO THE 5 REPAIRS WITH BLIND FASTENERS FROM BS 1223-1275 AND REPLACED WITH SOLID FASTENERS IAW B727 SRM 51-30-2 FIG 7. FABRICATED HAT CHANNEL REJun 3, 2005 · N741DH · Boeing 7272Q9SDR 05FDEA01499Case · crackedNR 2 ENGINE, LT FAN CASE APPROXIMATELY 7 - 8 O' CLOCK POSITION, FOUND CRACKED PROPAGATED THRU STOP DRILL HOLE AT AFT CRADLE MOUNT FLANGE. REPAIRED PER AMM 72-33-00-300-801.May 31, 2005 · N584FE · Doug MD11SDR CA050530005Pin · broken(CAN) WHILE PERFORMING AD INSPECTION, THE RT AFT ENGINE COWLING LATCH WAS FOUND WITH A BROKEN HINGE PIN. A NEW PART WAS ORDERED, INSTALLED AND ADJUSTED.May 23, 2005 · Snias AS350B3SDR AC2A100890Strut · chafedCHAFED ON NR 2 ENGINE EXHAUST BLANKET/ REPLACED STRUT ASSY. AND APPLIED HIGH TEMP RTV TO BLANKET AS PER BELLMay 13, 2005 · N427CK · Bell 427SDR QXEA200500922Latch · wornYYC - LEFT ENGINE UPPER AND LOWER BLOW OFF DOOR LATCH REBATE WORN. REPAIRED IAW CRJ700 SRM 51-23-00-001-001-A01, 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01.May 6, 2005 · N611QX · Cndair CL6002C10SDR QXEA200500923Retainer · crackedYYC - LEFT ENGINE PYLON ACCESS PANEL 432BB SEAL RETAINER IS CRACKED. REPAIRED IAW CRJ700 SRM 51-42-13-001-001-A01, 51-24-21-001-001-A01.May 5, 2005 · N611QX · Cndair CL6002C10
Back to JASC 5410