N924FD
Service difficulty reports · 136
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N924FD' AND registry_match = 'registration' 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.
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 n_number = 'N924FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201612214511Bulb · inoperativeL1 DOOR SLIDE LIGHT. R & R THE BULB, LIGHT OPS NORMALSDR FDEA201511093542Bracket · crackedFORWARD CARGO COMPARTMENT DOOR AFT UPPER CORNER OF DOOR STRUCTURE, ONE EACH BRACKET IS CRACKED. REMOVED, HFEC BRACKET, FOUND TO BE CRACKED. FABRICATED NEW BRACKET & INSTALLED NEW BRACKET IAW SRM 51-40-02, NDTM PT6 51-00-19 & DWG 69-53919 REV B & C.SDR FDEA201412314224Windshield · crackedFL390, STARTED TO OBSERVE DELAMINATION IN CAPTAIN`S FWD WINDSHIELD, FOLLOWED IMMEDIATELY BY WINDSHIELD SHATTER. R & R L1 WINDOW ASSEMBLY IAW AMM 56-11-01-4.SDR FDEA201408042044Light · defectiveDURING SERVICE CHECK & OPS CHECK OF EMER EXIT LIGHTS, UPON ACTUATION OF SWITCH, NOTICED HALF OF UNARMED LIGHT WOULD FLICKER. UPON TRYING TO DISASSEMBLE TO RE-LAMP, LOWER HALF OF LIGHT ASSEMBLY BASICALLY CRUMBLED IN MY HAND. REPLACED EMER LIGHT UNARMED LEN & SDR FDEA201408032042Light · failedDURING SERVICE CHECK & OPS CHECK OF EMERGENCY LIGHTS, ON ACTUATION OF SWITCH, NOTICED HALF OF UNARMED LIGHTS WOULD FLICKER. TRIED TO DISASSEMBLE TO REPLACED THE LAMPS, LOWER HALF OF LIGHT ASSEMBLY BASICALLY CRUMBLED. REPLACED EMERGENCY LIGHT "UNARMED" LESDR FDEA201311182818Frame · crackedFWD M.E.C. CUT OUT FRAME BS 231 ON FWD SIDE IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW EA F-5310-T0303943 P1.SDR FDEA201310262622Window · failedTHE LT FWD WINDOW STARTED ARCHING IN FLIGHT. TURNED WINDOW HEAT OFF IAW THE QRH. WINDOW SHATTERED ABOUT FIVE MINUTES LATER. REMOVED AND INSTALLED NEW L1 WINDOW IAW MM 56-11-01-4 .SDR FDEA201306061208Slide · dislodgedWHEN THE LT DOOR OPENED THE SLIDE FELL OUT OF THE BOX. INSTALLED L1 DOOR SLIDE USING AMM 25-66-01-4. COVER INSTALLED. OPS CHECKED GOOD.SDR FDEA201304180800Pseu · faultedAFTER NORMAL LANDING, RECEIVED NUMEROUS EICAS ALERTS THAT CLEARED BEFORE THEY COULD BE READ, BELIEVE THEY WERE DOOR RELATED. ESTIMATE IT WAS SIX ALERTS, NO CURRENT FAULTS AND PILOT STATED THAT FAULTS WERE MOMENTARY. R & R PSEU REF AMM 32-09-04-4 AS PRECAUSDR FDEA201304180799Pseu · malfunctionedDURING DESCENT, RECEIVED MOMENTARY "GEAR NOT DOWN" EICAS WARNING. ALTITUDE WAS APPROX 30,000 FT WARNING ONLY APPEARED ONE TIME AND LASTED ONLY A FEW SECONDS. NO EICAS FAULTS ON GROUND AND PILOT STATED THAT FAULTS WERE MOMENTARY IN FLIGHT. R & R PSEU REF 3SDR FDEA201301240170Lamp · inoperativeDOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.SDR FDEA201209203374Processor · failedUPON REACHING CRUISE ALITIUDE OF FL 400, BOTH THE LT & RT MAIN FUEL TANK QUANT INDICATORS WENT BLANK AND RECEIVED "FUEL QUAN IND" STATUS MSG. AFTER REACHING 4000' BOTH INDICATION CAME BACK ON WHILE FLYING APPROACH. PERFORMED THE WALK THROUGH FIM 28-41-00 TRSDR FDEA201111094853Skin · damagedSKIN DAMAGE BS 1695 S19R. CUT OUT DAMAGED AREA IAW SRM 51-10-02 AND EA F-5330-143903. FABRICATED REPAIR DOUBLER AND FILLER IAW EA F-5330-143903 AND SRM 53-00-01 REPAIR 15. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 REPAIR 15 AND EA F-5330-143903.SDR FDEA201110134465Sliding Window · out of adjustCAPT SLIDING WINDOW LOCK VERY DIFFICULT TO MOVE AND HAND CRANK AND OVER CENTER LOCK MOVE TOWARD OPEN WHEN CRANK HANDLE RELEASED. RIGGED CLUTCH MECH, AND COMPLETED ADJ AND TEST.SDR FDEA201107222891Handle · looseL1 ENTRY DOOR IS VERY DIFFICULT TO CLOSE FROM INSIDE. HANDLE IS LOOSE. RESECURED L1 DOOR HANDLE AS REQ'D. L1 DOOR CHECKS GOOD IAW AMM 52-11-00-6 NR 1,2 AND 4 PASSENGER DOORS - INSPECTION/CHECK. ACFT OK FOR SERVICE.SDR FDEA201007152627Frame · misrepairedEXISTING FRAME REPAIR AT STA 1460 IS IAW SRM 51-70-11, FIG 1. REPAIR AND FOUND REPAIR WAS NOT COMPLIANT WITH SRM SPECIFIC REPAIR. REMOVED EXISTING IAW SRM 51-40-02. FABED REPAIR SPLICE ON STAM TRAVELER T10/844785. REPAIRED FRAME AT STA 1460 BETWEEN S-25L TOSDR FDEA201006101938Skin · damagedENLOGATED HOLES FOUND IN INCOMING SKIN ALONG STR 26L LAP SPLICE STA 520-640 COMPLY WITH ATTACHMENT "B" OF E.O. F-5100-7-5001 PT 1. REF E.A. F-5330-131197 FOR FOLLOW-UP TRACKING REQUIREMENTS, AS SUCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201006091914Sill · gougedGOUGE DAMAGE ON DSS UPPER SILL SKIN AND MCD EXTERNAL SKIN BETWEEN STA 500-515 AND 580-600 NEAR STR 3L COMPLY WITH ATTACHMENT "B" OF SO F-5100-7-5001 PT 1 REF EA F-5330-139162 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MSDR FDEA201006091912Frame · crackedFASTENER HOLE CRACKED IN 143N1025-12, FRAME AT STA 540 BETWEEN STR 25L-26L. COMPLY WITH ATTACHMENT "B" OF EO. F-5100-7-5001 PT. REF EA F-5310-139163 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-SDR FDEA201006091911Fitting · inoperativePOTENCIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-21 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640 STR 17R TO 18R , COMPLY WITH ATTACHMENT "B" OF EO F-5100-705001 PT 1. REF EA F-5310-139165 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDISDR FDEA201006091909Structure · damagedSHORT EDGE MARGIN CONDITION IN INBD CHORD AT STA 460, STR. 23L COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 PT 1, REF EA F-5310-139164 FOR FOLLOW-UP TRACKING REQUIREMENTS (DTA PENDING) AS SUCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201006051838Skin · dentedFUS SKIN DENTED APPROX STA 1635 2" ABOVE STR 24R EVALUATED DENT AT STA 1635 2" ABOVE S-24R A=1.0 Y=.040 A/Y RATION=40. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG 201, REPAIR 3 CATEGORY "B" REPAIR WITH SUPPLEMESDR FDEA201006051837Skin · dentedSTA 1676 3" INBD OF STR. 28R FUSE SKIN DENTED. CHECK DENT LIMITS FOUND TO BE OUT OF LIMITS, DEPTH "Y" .131 MAX ALLOWABLE IS .125 IAW SRM 53-00-01 DETAIL 3, REPAIRED DENT DAMAGE IAW SRM 53-00-01 FIG 201, REPAIR 7, THIS IS CATEGORY "B" REPAIR AND MUST BE INSPECSDR FDEA201005261659Angle · corrodedNR 3 SLAT HAS CORROSION BETWEEN UPPER SKIN ASSY & LOWER SKIN IN SEAM AREA. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.5,W=1.0,D=.01 ORIG. MAT.063. REMAINING .053 OUT OF LIMITS IAW SRM 57-43-01 FIG.101 DET III. ACCOMPLISHED EA 5740-139134,WINGS L/E SDR FDEA201005211604Skin · dentedDENT AT STA 1704 BETWEEN S-15L TO S16L. ACCOMPLISHED EA F-5330-131187. FUSELAGE PLATES/ SKIN DAMAGE TO AND NEAR EXISTING REPAIR BS 1701, BETWEEN S-14L AND 16L. THIS IS A CLASS "B" REPAIR, PRIOR TO ACFT REACHING 37,500 FC NEW 8100-9 WILL NEED TO BE ISSUED. MSDR FDEA201005181573Bracket · installedVENT/COOLING FAN AT STA 1681 STGR 28L INTERFERES WITH INSTALLATION OF THE E-7 RACK. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD. A REPAIR WAS ACCOMPLISHED AT STA 1678 STGR 26L-28L ON MAE EA 757-5362-16-F2577 REV-, MAE MOD W/C 118550428ACSR01. THIS N/R IS FOSDR FDEA201004171216Skin · corrodedNR 7 SLAT HAS CORROSION IN SKIN SEAM BETWEEN UPPER NOSE SKIN ASSY & LOWER AFT EDGE ASSY. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA, L=10.25 ,W=.75, D=.018, ORIG MAT.063 REMAINING .045 OUT OF LIMITS IAW SRM 57-43 -01, FIG 101 DET III. ACCOMPLISHED EA SDR FDEA201004171214Angle · corrodedNR 6 SLAT HAS CORROSION IN SEAM BETWEEN NOSE UPPER SKIN ASSY AND LOWER AFT EDGE SKIN. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02 FIG 101, DET II. REMOVED COVE ANGLE IAW 51-40-02 INSTALLED COVE ANGLE & REPAIR SPLICE IAW SRSDR FDEA201004171213Skin · corrodedNR 10 SLAT HAS CORROSION IS SEAM BETWEEN UPPER NOSE WEDGE SKIN & AFT EDGE SKIN ASSY. REMOVED CORROSION ON NR 10 SLAT COVE ANGLE IAW SRM 51-10-02 BLEND OUT DIM L 131" ,W 1.0", D.20". FOUND OUT OF LIMITS IAW SRM 57-43-02 FIG 10, DET 2 COMPLIED WITH EA NR F-SDR FDEA201004171212Floorbeam · corrodedPREVIOUS REPAIR AT BS1681-8, FLOORBEAM LBL 24.75 TO 32.5 HAS CORROSION ON UPPER FLANGE. PREVIOUS BLEND OUT AT LBL 32.5 IS PITTED. REMOVED EXISTING REPAIR IAW EA NR F5310-131583, FABRICATED REPAIR STRAP FROM MAT 7075-76 0.090", FABRICATED REPAIR ANGLE NR 1,SDR FDEA201004091126Skin · mismanufactured3EA FASTENER HOLES MIS- LOCATED IN THE INBD SKIN PANEL ASSY, PN 311N5046Y54, COMMON TO THE INBD 311N5220-52, BATHTUB FITTING AND 1EA C/M TO THE PN 311N5220-54, MID-CHORD. REMOVED DAMAGE FROM HOLES "B" AND "C" TO SIZE .408, AND HOLE "A" TO SIZE .567, AND PERFORSDR FDEA201004091122Skin · corrodedNR 5 SLAT HAS CORROSION ON LOWER NOSE SKIN AND UPPER SKIN BUTT UNDER SEALANT. REMOVED CORROSION FROM COVE ANGLES AND SPLICE IAW SRM 51-10-02 ORIGINAL MATERIAL .080 AFTER REWORK .060 MATERIAL LOSS .020 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101. FABRICATEDSDR FDEA201004081108Seat Track · misalignedAT STA 640 AND 780 THERE IS A MISMATCH IN HEIGHT BETWEEN THE SEAT TRACK CROWNS THAT WILL PREVENT THE HANDLING SYS ROLLER TRAYS FROM SITTING LEVEL. RBL 24-75 AND 45.5. THIS IS AN EXISTING CONDITION. DUE TO DISCREPANCY EFFECTING THE PTF MOD A REPAIR HAS BEEN ASDR FDEA201004071089Angle · corrodedRT WING FIXED L/E,THROUGH ACCESS HOLES, BEHIND NR 10 SLAT, CORROSION ON INNER SURFACE. REMOVED CORROSION RT WING FIXED L/E AT ANGLE IAW SRM 51-10-02, BLENDED AREA L=5.0", W=1.0", D=0.050", MAT ORIG. .050", OUT OF LIMITS IAW SRM 57-41-13, FIG 101 DET II. RSDR FDEA201004061081Slat Track · corrodedLT WING NR 1 SLAT LOWER COVE APPROX 10" OTBD OF NR 1 SLAT TRACK ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=40",W= 1.0,D=.040, ORIG MAT REMAINING .023 OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DET III. ACCOMPLISHED EA F-57-40-131184.SDR FDEA201004051057Stringer · deformedSTR 25L AT STA 1650 HAD DEFORMED HOLE. R & R STRINGER AT STA 1650 S-25L IAW SRM 53-00-03 FIG 201, REPAIR 1 DETAIL II. FOUND HOLE TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201003180873Web · corrodedCORROSION LOWER SURFACE OF LOWER SILL AT DOOR L-3 ON ACFT. R & R L-3 DOOR LOWER SILL WEB FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101 DETAIL III AND SRM 51-40-02. CLASSIFIED MAJOR REPAIR.SDR FDEA201003170858Skin · corrodedRT WING MLG TRUNNION FAIRING FWD MOUNT AREA WING LOWER SKIN HAS CORROSION REPAIRED RT WING MLG TRUNNION FWD ATTACH POINT IAW EA F-5730-131581, DATED MAR 1, 2010. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201003170857Skin · corrodedLT WING MLG TRUNNION FAIRING FWD ATTACH POINT SKIN IS CORRODED UNDER AND AROUND MOUNT REPAIRED LT WING LOWER SKIN AT MLG FAIRING FWD ATTACH POINT 7 IAW EA F-5730-131581, DATED MAR 1, 2010. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201003160840Wedge · delaminatedLT WING NR 5 SLAT T/E WEDGE INNER SURFACE ABOVE INBD AUX TRACK IS DELAMINATED. REMOVED DAMAGE AND BONDED REPAIR SKIN AND DOUBLER ON LT WING NR 5 SLAT T/E WEDGE IAW SRM 51-70-10. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201003150834Angle · corrodedLT WING NR 2 SLAT COVE ANGLE CORRODED.SDR FDEA201003100748Bolt · unknownUNABLE TO INSTALL IEA FASTENER IAW EO F-5450-7-5003C PT3 & PT4, FOR THE LT & RT WING ISLF. INSTALLED 2EA BACB30US10K BOLTS IAW EA F-5450-131166 IN THE LT & RT WING ISLF. FAA FORM 8100-9 ATTACHED. ( LOCATION PP-RBL 9, WS 285.65 ). MAJOR REPAIR.SDR FDEA201003100747Fitting · damagedRT WING AT NR 2 PYLON MOUNT AREA INBD STRUT MOUNT FITTING, BUSHING HAS SCRATCH AND WEAR MARKS. ACCOMPLISHED OVER SIZED LUG HOLE REPAIR IAW FINAL EA NR F-5720-131160, WINGS- FITTINGS-(AD 2004-12-07) NR 2 ENG PYLON INBD SIDE LOAD FITTING BUSHING O/S HOLE ANDSDR FDEA201003100746Fitting · gougedRT WING NR 2 PYLON MOUNTING AREA OTBD STRUT MOUNT FITTING HAS GOUGES ON 2 PLACES AT INNER AND OUTER SURFACE. ACCOMPLISHED FINAL EA F-5740-131580, WINGS-(AD 2004-12-7/EO F-5450-7-5003) RT OTBD SIDE LOAD FITTING GOUGED THIS IS MAJOR REPAIR.SDR FDEA201003090705Seat Track · damagedSEAT TRACK AT LBL 45.5 STA 1160 AND 1139 HAS MINOR NICK DAMAGE AT TOP OF CROWN. CHECK LIMITS AT STA 1160 DIMENSION ARE 1.0 X 0,6 X 0.030, AT STA 1139 DIMENSIONS ARE 1.0 X 0.6 X0.025 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I PG 102. FABED SDR FDEA201003080681Crease Beam · corrodedMAIN CABIN STA 1360-1380 LT SIDE CREASE BEAM WEB HAS CORROSION R & R LT SIDE CREASE BEAM WEB FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL II AND SRM 51-40-02. FABRICATED NEW CREASE BEAM WEB ON MAE TRAVELER NR T10/818082. CLASSIFIED CATEGORY "A" MASDR FDEA201003010583Seat Track · corrodedMAIN CABIN SEAT TRACK STA 780-900 RBL 25 IS GOUGED AND HAS CORROSION R & R SEAT TRACK AT STA 780-879 RBL 25 FOUND OUT OF LIMITS IAW SRM 51-30-02, FIG 101 DETAIL I AND SRM 51-40-02. SEAT TRACK FABRICATED ON MAE TRAVELER NR T10/817651. CLASSIFIED CATEGORY "A" MSDR FDEA201002260534Crease Beam · corrodedCREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION STA 1180 TO 1200 LT SIDE. REMOVED AND REPLACED LT SIDE IB CREASE BEAM AT STA 1180-1280, FOUND OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIRSDR FDEA201002220492Crease Beam · corrodedMAIN CABIN STA 620-640 RT SIDE CREASE BEAM WEB HAS CORROSION. R & R RT SIDE CREASE BEAM WEB. FOUND OUT OF LIMITS IAW SRM 53-13-30, FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201002220491Crease Beam · corrodedMAIN CABIN STA 560-580 RT SIDE CREASE BEAM WEB HAS CORROSION AT SCREW HOLE ON UNDERNEATH SIDE. R & R RT SIDE CREASE BEAM WEB, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101 DETAIL II AND SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
Back to N924FD