JASC 5344

Service difficulty reports · 2,431

Reports filed under 5344 · Fuselage, Door Hinge, 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 = '5344'
  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 ASOA201201034Hinge Bracket · corrodedCENTER HINGE BRACKET FOUND TO BE CORRODED AT THE TOP OF PAX DOOR. REPAIRED HINGE LOWER CHANNEL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.Mar 27, 2012 · N738EV · Cndair CL6002C10SDR CWQR20120320016Hinge · crackedDURING A SCHEDULED INSPECTION, FOUND AN AREA OF CORRISION ON THE FWD MAIN CABIN DOOR HINGE, THAT IS ATTACHED TO THE DOOR FRAME. FOUND THE CORRISION ON THE FWD EDGE OF THE HINGE, PREFORMED A DYE-PEN CHECK AND FOUND THE HINGE TO BE CRACKED. THIS IS THE THIRD Mar 20, 2012 · N685QS · Cessna 560XLSDR DALA1215103119Hinge Fitting · corrodedR2 DOOR AFT CORNER FITTING FR 68 CORRODED. REMOVED AND REPLACED 1 EA AFT CORNER FITTING AT R2 DOOR FR68 IAW A319 SRM 51-42-11. DAMAGE DIM L=.350" W=.200" D=.030".Mar 10, 2012 · N319NB · Airbus A319114SDR CWQR20100308014Hinge · corrodedDURING A SCHEDULED INSPECTION, FOUND CORROSION ON THE FWD CABIN DOOR HINGE FROM THE CORNER EDGE OF THE PART TO BEYOND THE FIRST FASTENER ATTACH HOLE, BEYOND ALLOWABLE LIMITS. REMOVED HINGE, INSPECTED AND PREFORMED NDT INSP OF ATTACH POINT, NO DEFECTS NOTED. TMar 8, 2012 · N611QS · Cessna 560XLSDR CWQR20120306015Hinge · corrodedDURING A SCHEDULED INSPECTION, FOUND CORROSION ON THE AFT CABIN DOOR HINGE FROM THE CORNER EDGE OF THE PART TO BEYOND THE FIRST FASTENER ATTACH HOLE. BEYOND ALLOWABLE LIMITS. REMOVED HINGE, INSPECTED AND PREFORMED NDT INSP OF ATTACH POINT, NO DEFECTS NOTED. THMar 6, 2012 · N611QS · Cessna 560XLSDR DXTR20120302001Hinge Fitting · corrodedCABIN DOOR AFT LOWER HINGE AIRFRAME SIDE, UPPER FORWARD CORNER CORRODED.Mar 2, 2012 · N611QS · Cessna 560XLSDR N6WA2012021802Hinge · lack of lubePASSENGER DOOR WILL NOT CLOSE. LUBED HINGE AT MAIN CABIN DOOR IAW AMM 52-11-00. OPS CHECKED GOOD.Feb 18, 2012 · N161GJ · Cndair CL6002C10SDR CA120220005Hinge · damaged(CAN) ACFT RETURNED AFTER TAKEOFF WITH THE UPPER CABIN DOOR OPEN. NO FAULTS FOUND WITH DOOR LOCKING MECHANISM. DOOR UPPER FWD HINGE FOUND DAMAGED AND PULLED DUE TO BEING OPEN IN FLIGHT. SUSPECT THAT THE DOOR NOT LOCKED PROPERLY PRIOR TO TAKEOFF. UPPER DOORFeb 17, 2012 · Piper PA31350SDR SWAA2012021701506Hinge · unknownL1 DOOR WOULD NOT FULLY OPEN. SECURED HINGE IAW MM.Feb 13, 2012 · N928WN · Boeing 7377H4SDR 2012F00055Hinge · failedFOLLOWING TAKEOFF, DURING GEAR RETRACTION IN TRANSITE LIGHT REMAINED ILLUMINATED, CREW EXTENDED GEAR AND NORMAL INDICATION WAS OBSERVED. UPON SECOND RETRACTION, THE IN TRANSITE LIGHT REMAINED ILLUMINATED AND GEAR WAS SELECTED TO EXTENDED POSITION AND CONTROL Feb 8, 2012 · N160AJ · Lear 60LEARSDR CWQR20120207002Hinge Fitting · crackedDURING A VISUAL INSPECTION, FOUND CORROSION ON CABIN DOOR HINGE FITTING, LIMITED TO THE INWARD EDGE OF THE HINGE FITTING, ON CLOSER INSPECTION, FOUND A CRACK THAT WAS .35 INCH LONG ON THE HINGE FITTING RADIUS AREA BETWEEN THE FLANGE ATTACH BRACKETS. THE CRACKFeb 6, 2012 · N673QS · Cessna 560XLSDR CWQR20120207001Hinge Fitting · crackedDURING A VISUAL INSPECTION OF THE FORWARD CABIN DOOR HINGE FITTING, FOUND CRACK. CRACK .35 INCHES LONG AND WAS IN THE RADIUS AREA BETWEEN THE FLANGE AREA THAT ATTACHES TO THE FUSELAGE. THE CRACK WAS VERIFIED USING DYE PENETRANT METHOD. HINGE FITTING WAS REPFeb 6, 2012 · N673QS · Cessna 560XLSDR A6WA201240267Hinge · damagedPAX DOOR PIANO HINGE LUGS HAVE SCRATCHES AND GROVES ON HINGE HALF. BLENDED OUT GOUGES IAW REO 601R-52-11-1347.Jan 30, 2012 · N439AW · Cndair CL6002B19SDR A6WA201240243Hinge · gougedPAX DOOR HINGE (FUSELAGE SIDE) HAS GOUGED LUGS AFT NR2 AND NR15. REPAIRED IAW REO 601R-53-21-814.Jan 27, 2012 · N431AW · Cndair CL6002B19SDR FDEA201201270348Hinge · crackedRT MLG DOOR CENTER HINGE CRACKED. HINGE REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 48. R/H MAIN GEARWELL DOOR REMOVED AND REINSTALLED AS PER AMM 32-14-20-4 REVION 70.1. OPERATION CHECK CARRIED OUT SATISFACTOTY AS PER AMM 32- 14-20-220-801 REVISIONJan 27, 2012 · N574FE · Doug MD11FSDR FDEA201201190250Hinge Fitting · wornMAIN CARGO DOOR FWD SEGMENT HINGE 13 LOBES FROM FWD FOUND WORN BEYOND 0.402 INCH LIMIT. REWORKED TO 0.4555" IAW CMM 52-3404, REV 71 AND EA 1-5230-154289. FABRICATED AND INSTALLED IAW CMM 52-34-04, REV 71 AND EA 1-5230-154289. REPAIR CLASSIFIED AS MAJOR IAWJan 19, 2012 · N609FE · Doug MD11FSDR 2012FA0000046Hinge Fitting · crackedDURING AN ANNUAL, DISCOVERED A WELDED REPAIR TO A CRACK ON THE PILOT-SIDE DOOR ON THE INNER SKIN BELOW THE RIVETS THAT FASTEN THE LOWER HINGE TO THE DOOR. WHILE THIS DOOR IS SERVICEABLE, THE SAME CRACK EXISTED ON ANOTHER ACFT SERVICED EARLIER. THE CRACK WAS Jan 13, 2012 · N3732F · Beech 77SDR ASOA201200115Hinge Fitting · corrodedINSIDE ASD AT HINGE END 2 CLIPS ARE CORRODED AT REF FS 318. REMOVED CORRODED CLIPS FROM ASD AT HINGE END. INSTALLATION OF NEW CLIPS REQUIRED IAW SRM 51-42-06-001-001-A01. OK TO INSTALL CG161726 01/13/12. INSTALLED 2 EA CLIPS AT HINGE END AND ON ASD SRM 51-42Jan 11, 2012 · N331CA · Cndair CL6002C10SDR FDEA201201010002Hinge Fitting · corrodedMAIN CARGO DOOR UPPER HINGE FITTING RUSTED UNDERNEATH FOAM INSULATION IN SEVERAL AREAS. REPAIR OR REPLACE.Jan 1, 2012 · N583FE · Doug MD11FSDR JR2R2011123100706Hinge · gougedPAX DOOR HINGE HALF (DOOR SIDE) GOUGED ON MULTIPLE LUGS. REPAIRED IAW RO CRJ9-53-0479.Dec 31, 2011 · N915FJ · Cndair CL6002D24SDR A6WA201240120Hinge Fitting · crackedLEFT BUTTE DOOR 594ND AND 594JD HAS CRACKED HINGE PLATE AND END PLATE. REMOVED UNSERVICEABLE HINGE AND END PLATE AND INSTALLED SERVICEABLE HINGE AND END PLATE IAW SRM 51-42-06.Dec 13, 2011 · N433AW · Cndair CL6002B19SDR QXEA2011120201290Hinge · corrodedDURING C-CHECK, FOUND FWD PAX DOOR HINGE AND HARDWARE ARE CORRODED.Dec 1, 2011 · N402QX · Bombdr DHC8402SDR A6WA201240031Hinge · gougedPAX DOOR HINGE FUSELAGE SIDE 2ND LUG FWD END IS GOUGED. BLENDED 2ND FWD LUG ON PAX DOOR FUSELAGE SIDE. REMOVED .009 OF MAT REMAINING MAT IS WITHIN SERVICEABLE LIMITS OF .116 MIN REQUIREMENT IS .100 IAW REO 601R-53-21-814.Nov 18, 2011 · N426AW · Cndair CL6002B19SDR A6WA201141129Hinge · gougedSERVICE DOOR HINGE GOUGED LOWER AND TOP SIDE BLENDED DAMAGE TO CONTOUR REO 601R-52-41-198.Nov 10, 2011 · N468AW · Cndair CL6002B19SDR FDEA201111054759Hinge · crackedAVIONICS COMPARTMENT ACCESS DOOR RT HINGE ARM FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 52-41-14, FIG 201, REV 21. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605RSDR FDEA201111054758Hinge · crackedAVIONICS COMPARTMENT ACCESS DOOR LT HINGE ARM FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 52-41-14 FIG 201, REV 21. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.Nov 5, 2011 · N657FE · Airbus A300F4605RSDR UALA2011120206636Hinge · lack of lubeDURING CLOSING AFT CARGO DOOR, OPERATION WAS ERRATIC (NOT SMOOTH) AT START OF DOOR LOWERING DUE TO ROD EYE END BOLTS REQUIRING LUBE JOB. LUBED AFT DOOR HINGE ASSY PER MM. DOOR STILL ERRATIC CLOSING. LUBED LOWER HINGE POINTS AFT CARGO DOOR.Nov 2, 2011 · N662UA · Boeing 767322SDR ASOA201102156Hinge · gougedPAX DOOR FUSELAGE ATTACH HINGE HALF HAS 2 EA GOUGES APPROX .722" FROM AFT EDGE. REO 601R-53-21-814. MAX BLEND OUT DEPTH .013", WITHIN ALLOWABLE LIMITS. NO FURTHER ACTION REQUIRED.Oct 24, 2011 · N876AS · Cndair CL6002B19SDR IPXA11570337Hinge · damagedMAIN CARGO DOOR AFT HINGE DAMAGED. REPAIRED IAW ENGINEERING REPAIR 11-5004.Oct 18, 2011 · N407UP · Boeing 75724APFSDR UALA2011101105514Link · wornL1 DOOR UPPER HINGE LINK WORN. REMOVED & REPLACED L1 DOOR UPPER HINGE LINK PER MM.Oct 11, 2011 · N502UA · Boeing 757222SDR N6WA20110932Angle · corrodedSERVICE DOOR MOUNTING ANGLE HAS CORROSION. R & R SERVICE DOOR ANGLE IAW SRM 51-42-06 & 51-42-21.Sep 28, 2011 · N165GJ · Cndair CL6002C10SDR QXEA2011092900915Nut Plate · corrodedWHILE REMOVING LT SIDE ICE SHIELD, FOUND 6 EA NUT PLATES CORRODED FROM STA X290.000 TO 327.000. REMOVED BRACKETS WITH NUT PLATES, REMOVED NUT PLATES AND INSTALLED NEW NUT PLATES AND BRACKET IAW SRM 51-42-05-02-01.Sep 20, 2011 · N429QX · Bombdr DHC8402SDR A6WA201140930Bracket · crackedTWO BRACKETS FOR HYD LINES SYS 3 CRACKED IN RT WHEEL WELL LOCATED AND DRILLED BRACKETS IAW SRM 51-40-11. INSTALLED BRACKETS IAW SRM 51-41-02.Sep 17, 2011 · N464AW · Cndair CL6002B19SDR A6A201140937Hinge · chafedPAX DOOR HINGE ON FUSELAGE HAWS CHAFING DAMAGE FROM ROLL PIN. REPAIRED CHAFED DAMAGE ON PAX DOOR HAING ON FUSELAGE IAW B/A REO 601R-52-21-814.Sep 17, 2011 · N464AW · Cndair CL6002B19SDR A6WA201140938Hinge · chafedPAX DOOR HINGE HAS MINOR CHAFING ON 2 LUGS. REPAIRED DAMAGED PAX DOOR HINGE IAW REO 601R-52-11-1347.Sep 17, 2011 · N464AW · Cndair CL6002B19SDR A6WA201140899Hinge · gougedPASSENGER DOOR PIANO HINGE IN FUSELAGE SIDE IS GOUGED JUST AFT OF AFT LUB. BLENDED GOUGE IAW REO 601R-53-21-814 TYPE IV.Aug 31, 2011 · N424AW · Cndair CL6002B19SDR FDEA201108313591Hinge · corrodedLOWER AFT CARGO DOOR HINGE FOUND RUSTY. RUST REMOVED IAW SRM 51-21-01, REV 47 AND FOUND WITHIN LIMITS IAW SRM 52-30-16, REV 47, FIG 101. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Aug 31, 2011 · N643FE · Doug MD11FSDR FDEA201108313590Hinge · corrodedLOWER CENTER CARGO DOOR HINGE FOUND RUSTY. RUST REMOVED IAW SRM 51-21-01, REV 47 AND FOUND WITHIN LIMITS IAW SRM 52-30-16, REV 47, FIG 101. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-1.Aug 31, 2011 · N643FE · Doug MD11FSDR FDEA201108313589Hinge · corrodedLOWER FWD CARGO DOOR HINGE ASSY FOUND RUSTY. RUST REMOVED IAW SRM 51-21-01, REV 47 AND FOUND WITHIN LIMITS IAW SRM 52-30-16, REV 47, FIG 101. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Aug 31, 2011 · N643FE · Doug MD11FSDR FDEA201108243450Hinge · crackedRIGHT MLG DOOR-CENTER HINGE ASSY FOUND CRACKED. CRACKED HINGE REMOVED AND REPLACED WITH NEW HINGE AT RIGHT HAND DOOR CENTER AREA AS PER SRM 51-35-01 REV 47. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Aug 24, 2011 · N580FE · Doug MD11FSDR A6WA201140853Hinge Fitting · chafedAFT HINGE LUG ON PAX DOOR HAS CHAFING DAMAGE FROM HINGE PIN. REPAIRED AFT HINGE LUG ON PAX DOOR IAW SRM 51-12-00 AND REO 601R-52-11-1347.Aug 16, 2011 · N408AW · Cndair CL6002B19SDR A6WA201140852Hinge Fitting · chafedPAX DOOR AFT HINGE LUG ON FUSELAGE SIDE HAS CHAFING DAMAGE IN 2 PLACES. REPAIRED PAX DOOR AFT HINGE LUG ON FUSELAGE SIDE IAW DOOR SRM 51-12-00 AND REO 601R-53-21-814.Aug 16, 2011 · N408AW · Cndair CL6002B19SDR A6WA201140801Hinge · gougedPAX DOOR HINGE HALF MOUNTED FUSELAGE HAS SEVERAL GOUGES. BLENDED GOUGES ON PAX DOOR HINGE HALF OF FUSELAGE IAW SRM 51-12-00 FOUND TO BE WITHIN LIMITS IAW REO 601R-53-21-814.Aug 8, 2011 · N405AW · Cndair CL6002B19SDR 2011FA0000505Hinge · crackedNOTICED THAT UPPER LT DOOR HINGE HAD A CRACK IN IT WHERE IT ATTACHES TO THE FUSELAGE. THIS WAS THE SECOND PLANE SEEN WITH THIS PROBLEM.Aug 6, 2011 · N7726U · Cessna 172ESDR MALA110206Hinge · corrodedFWD LAV SERVICE DOOR HINGES ON FUSELAGE CORRODED. REPLACED FWD LAV SERVICE DOOR HINGES IAW SRM 51-42-06-001-001-A01.Aug 4, 2011 · N917XJ · Cndair CL6002D24SDR A6WA201140838Hinge · gougedPASSENGER DOOR PIANO HINGE HALF ON ACFT SIDE IS GOUGED ON AFT LUG. BLENDED GOUGE, TREATED, PRIMED AND TOP COATED IAW REO 601R-53-21-814.Aug 1, 2011 · N461AW · Cndair CL6002B19SDR N6WA20110741Hinge Pin · migratedPASSENGER DOOR TOP STEP HINGE PIN MIGRATING RESET PIN POSITION ON PASSENGER DOOR TOP STEP HINGE IAW AMM 52-11-09.Jul 27, 2011 · N167GJ · Cndair CL6002C10SDR FDEA201107262946Hinge · crackedAVIONICS COMPARTMENT DOOR, FOUND RT HINGE CRACKED. PERFORMED REPAIR PER A300-600 SRM 52- 41-14 FIG 201 REV 75. AVIONICS COMPARTMENT DOOR REMOVED AND RE-INSTALLED AFTER REPAIR COMPLETED PER AMM 52-41-14-04 REV 52.0 AVIONICS COMPARTMENT DOOR ADJUSTMENT TESJul 26, 2011 · N717FD · Airbus A300B4622RSDR 2011FA0000504Hinge · brokenUPPER DOOR HINGE ON THE LT DOOR BROKE IN FLIGHT CAUSING THE DOOR TO PULL AWAY FROM THE PLANE. THE PILOT WAS ABLE TO HOLD THE DOOR AND FLY THE PLANE AND LAND AT A NEARBY AIRPORT. THE HINGE BROKE THROUGH THE RIVET HOLES ON THE PART OF THE HINGE THAT ATTACHES TO Jul 23, 2011 · N6340E · Cessna 172SDR CA110708003Hinge · crackedDURING WALK AROUND PILOT REPORTED THAT THE FWD DOOR HINGE WAS CRACKED. REAR PASSENGER DOOR REMOVED AND NEW HINGE WAS INSTALLED. THE AFT HINGE WAS REPLACED 40.5 HRS PRIOR TO THE ACFT BEING SNAGED.Jul 4, 2011 · Diamon DA40
Back to JASC 5344