N783FD
Service difficulty reports · 54
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 = 'N783FD' 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 = 'N783FD' 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 FDEA202608221216Rub Strip · gougedAFT LOWER CARGO DOOR CONTROL PANEL LOWER CUT OUT HAS A GOUGE ACCOMPHLISHED REPAIR 18 - CARGO DOOR PANEL ACCESS DOOR CUTOUT SKIN REPAIR IAW B757 SRM 53-00-01-2RSDR FDEA202608201192Skin · damagedDURING AGING AIRCRAFT INSPECTION FOUND PREVIOUS EXISTING REPAIR ON RH HORIZONTAL STAB LOWER SKIN, INBD AREA, NOT INCLUDED ON THE MCMRT/CCMRP COMPLIED WITH EA F -5510-T0324519 A P3 TITLE: STABILIZER -HORIZONTAL STABILIZER-RIGHT HORIZONTAL STAB LOWER SKIN DAMASDR FDEA202601120026Battery Pack · failedAFTER WEEKEND LAYOVER, DURING MX PRE-FLIGHT CHECKS, FOUND EMERGENCY EXIT LIGHTS POWERED BY M730 INOP. AMM: 33-51-07-2 GMM: 12-7-600 REMOVED AND REPLACED BATTERY HOLDER ASSY. M730, MFR: RADIANT POWER CORP, MPN 2013-1A, S/N 118058, OPS CHECKS GOOD. A/C SDR FDEA202505090743Gust Lock · damagedL1 DOOR GUST LOCK COLLAR BROKEN. INSTALLED A NEW L1 DOOR GUST LOCK COLLAR, OPS CHECKS GOOD, OK FOR SERVICE.SDR FDEA202504040563Gust Lock · brokenL1 DOOR GUST LOCK IS BROKEN (LOCK IS REMOVED). INSTALLED NEW GUST LOCK. OPS CHECK OK.SDR FDEA202411171683Lamp · failedL1 DOOR EXTERIOR SLIDE LIGHT INOP FACT 17NOV24 17:47 BNA AMM: 33-51-06-2-1 RELAMPED L1 DOOR EXTERIOR SLIDE LIGHT, OP'S CHECKS GOOD REF AMM 33-51-06-2-1. BULB PART NUMBER 767 REPLACED.SDR FDEA202411121668Clamp · leakingLOSS OF CABIN PRESSURE AT FL340. CABIN CLIMBED TO @ 14,000 DURING THE DESCENT WITH THE CABIN CONTINUING TO CLIMB @700 FPM. COMPLIED WITH QRH NO OBVIOUS FUSELAGE LEAKS NOTED ON WALK AROUND. AUTOMATIC CABIN PRESSURE CONTROLLER 1 AND 2 BITE CHECK GOOD.SDR FDEA202409061250Web · crackedAFTER INSPECTION PER ED F-5310-E0329085DP5 STEP 3, A CRACK WAS FOUND AT FR-1640 LH, S- 14. COMPLIED WITH FEDEX E.A. # F -5310-T0380418 P1 TITLE: FUSELAGE- MAINFRAME - LH STA 1640 - TYPICAL FRAME SPLICE REPAIR BETWEEN STRINGER S-9L AND S-20L.SDR FDEA202405150671Wire · brokenWHEN SELECTING EMERGENCY LTS SWITCH ON OVERHEAD TO ON, COCKPIT OVERHEAD LT DOES NOT ILLUMINATE. ALL OTHERS OPERATE NORMALLY. PER WDM 33-51-21 FOUND GOOD GROUND BITWEEN GD602 AND G TERMINAL OF RESISTER R10381 AND DISCOVERED THAT WIRE WAS BROKEN FROM RESISTESDR FDEA202212072887Drag Fitting · corrodedHOLE #2 AND 5 ON UPPER SKIN AND DRAG FITTINGS PRESENT CORROSION RH WING. WORKS STEPS ACCOMPLISHED ON EA #: F5730-T0371761 MAJOR REPAIR.SDR FDEA202212072886Drag Fitting · corrodedHOLES 4 & 5 ON LT WING UPPER SKIN DRAG FITTINGS PRESENT CORROSION. WORKS STEPS ACCOMPLISHED ON EA F5730-T0371760 EA TITLE: WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS* THIS EA DEVIATES FROM EO F-5730-E0340076. MAJORSDR FDEA202212072883Floorboard · delaminatedZONE 220 FLOORBOARD 221MBF IS DELAMINATED. FABRICATED ZONE 220 FLOORBOARD 221MBF ON TRAVELER T22/1649009 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202211282850Floorbeam · crackedFWD PIT CEILING AREA STA 580 FLOOR BEAM UPPER CAP AFT SIDE FLANGE RADIUS HAS SUSPECTED CRACK, APPROX LBL 45. FLOOR BEAM WAS REPAIRED AND NEW ANGLE & RADIUS STRAP INSTALLED ON FWD PIT CEILING AREA STA 580 AT LBL 45 IAW DRAWING SR57-53-004 & SRM 51-40-02. MASDR FDEA202209122309Battery · no testR1 EMERGENCY EXIT SIGN, R1 SLIDE LIGHT AND EMERGENCY EXIT LOCATOR SIGN INOP DURING EMERGENCY LIGHT TEST. FOUND THAT AFTER AIRCRAFT HAD BEEN POWERED FOR OVER AN HOUR, ALL LIGHTS WOULD TEST, HOWEVER THE TEST ONLY LASTED APPROX 5-10 SECONDS, ALL OTHERS STASDR FDEA202204130945Fmc · failedL AND R FMC FAIL -EMERGENCY DECLARED ***EMERGENCY DECLARED*** R&R'D BOTH FMC COMPUTERS. UPDATED ALL SOFTWARE. BOTH FMCS OPS CKS NORMALLY. REF B757 MM SEC 34-61-01-4-1. ALL SOFTWARE UPDATED TO CURRENT REQUIREMENTS.SDR FDEA202202090257None · failedPDIS 783 73-20 6104 09FEB22 TPA OPEN U CLIMBING THROUGH FL300 LEFT ENGINE BEGAN SPOOLING DOWN. AUTOTHROTTLES DISCONNECTED WITH THE MASTER CAUTION. EMERGENCY WAS DECLARED AND DIVERTED TO TPA. ENGINE THRUST CAME BACK AFTER APPROXIMATELY 10 SSDR FDEA202202030203None · leakingPDIS 783 79-32 6083 03FEB22 TPA OPEN U EMERGENCY DECLARED. DURING CLIMB OUT FROM TAMPA TO MEMPHIS, HAD INDICATION OF HIGH OIL TEMP ON LEFT ENGINE. SOON AFTER, NOTICED OIL QUANTITY WAS ZERO. OIL PRESSURE WAS NORMAL. RETARDED LEFT THRUST LEVER SDR FDEA202201300164None · failedAFTER ENGINE START GOT EICAS MSG: L PACK OFF. AFTER ADVANCING THROTTLE TO TAXI, MSG EXTINGUISHED. TAKEOFF POWER WAS COMPUTED FOR DTO 50 WITH TEMPERATURE MINUS 6 CELSIUS. ON RUNWAY AFTER THRUST LEVERS WERE ADVANCED TO TAKEOFF POWER AT APPROXIMATELY 100 KNOTSDR FDEA202107031662Collar · crackedDURING SERVICE CHK FOUND 1R DOOR HOLD OPEN LOCK BROKEN. RMVD AND RPLD R1 DOOR HOLD-OPEN LOCK- DOOR HOLD OPEN LOCK CHKS GOOD- REF: B757 M/M 52-11-08-8SDR FDEA202101210166Skin · crackedR2 DOOR CUTOUT FWD FRAME UPPER HINGE CUTOUT IS CRACKED ACCOMPLISHED FEDEX EA F-5210-T0312598-B. DOORS-PASSENGER/CREW R2 DOOR EXISTING REPAIR.SDR FDEA202101210165Guard · debondedL1 DOOR EXTERIOR HANDLE SCUFF GUARD AROUND CENTER CUTOUT IS DISBONDED. FOUND OUT OF LIMITS GOUGE UNDER SCUFF GUARD. REMOVED AND REPLACED L1 DOOR ASSEMBLY, PER FEDEX B757-2 AMM 52-11-01-4.SDR FDEA202101190153Attach Bracket · gougedNR 2 ENGINE STARTER DUCT SUPPORT LINK ATTACH BRACKET ON THE ENGINE SIDE IS GOUGED AT THE 3 O'CLOCK POS (OUTBOARD SIDE). REMOVED AND REPLACED NR 2 ENGINE LINK ATTACH BRACKET ON THE ENGINE SIDE AT THE 3 O'CLOCK POSITION, IAW B757 SRM 51-40-02 AND AMM 70-50-00, SDR FDEA202101160131Skin · delaminatedLT WING INBOARD AFT FLAP OUTBOARD EDGE DELAM. REPAIRED LT WING INBOARD AFT FLAP OUTBOARD EDGE DELAM, IAW FEDEX EA F-5750-T0359087, B757 SRM 57-53-01-2R REPAIR 1 AND 51-70-17-0G. REPAIR ACCOMPLISHED, IAW FEDEX EA F-5750-T0359087-P1 WING-FLIGHT SURFACES-LT INBSDR FDEA202101140100Channel · crackedNR 2 PYLON PNL 445BL IS CRACKED REMOVED AND REPLACED CHANNEL, PER B757 SRM 51-40-02 AND DWG 313N3022.SDR FDEA202101140093Skin · damagedRIGHT HORIZONTAL STABILIZER WING TIP FORWARD END PAINT AND COMPOSITE DETERIORATED. REPAIRED RIGHT HORIZONTAL STABILIZER WING TIP FORWARD END PAINT AND COMPOSITE DETERIORATED, IAW B757 SRM 55-10-2R, 51-70-05-OG, 51-70-14, B757 AMM 51-21-00-7. REMOVED THEN RSDR FDEA202101140091Web · crackedPREVIOUS WEB REPAIR AT STA 400-420 AT APPROXIMATELY RBL 25 HAS FASTENERS WHICH ARE TOO LONG, HAVE EXCESSIVE WASHERS AND THE WEB IS DAMAGED. REMOVED DAMAGE WEB AT STA 400-420 RBL 25, IAW B757 SRM 51-40-02. RECEIVED NEW PART P/N 141N5150U54, PO NR 989969.1, IASDR FDEA202101130085Deck Plate · gougedPREVIOUS REPAIR ON AFT DECK PLATE AT STA 1681 RBL 12 HAS A GOUGE ON THE UPPER SURFACE. REMOVED, FABBED AND REPLACED DOUBLER, IAW B767 SRM 53-60-51-2R FIG 201 REPAIR 2.SDR FDEA202101100033Angle · crackedENGINE NR 1 AFT PYLON RT SIDE FWD LOWER CORNER CLIP CRACKED UNDER PANEL 435AR. REMOVED AND REPLACED -24 CLIP AT NR 1 PYLON RT SIDE FWD LOWER CORNER, IAW B757 FEDEX DWG 313N3053 REV P AND SRM 51-40-02.SDR FDEA202101070018Panel · crackedRT WING LEADING EDGE PANEL 611EB IS CRACKED. REPAIRED RT WING LEADING EDGE PANEL 611EB BY BONDING REPAIRPLIES, IAW B757 SRM 57-41-01-0I AND 57-41-01-2R REPAIR 1 FIG 201 AND 51-70-08 REPAIR GENERAL AND PARA 5G FIG 9. APPLIED FINISH, IAW B757 SRM 51-70-08 AND SDR FDEA202101070016Panel · crackedLEFT HORIZONTAL STABILIZER TRAILING EDGE PANEL 335AB IS CRACKED. REPAIRED PANEL 335AB, IAW B757 SRM 55-10-01-2R FIG 201 TABLE 2 AND B757 SRM 51-70-05-0G PARA 5G.SDR FDEA202010162534Idg · failedRT GEN OFF IN FLIGHT. CREW RAN QRH AS REQUIRED. CHECKED ELEC/HYD DISPLAY SELECT SWITCH ON THE EICAS PANEL AT P61 HAD RT GEN DRIVE PUSH THE BIT SWITCH ON THE BUS POWER CONTROL UNIT MESSAGES WAS RT LOW OIL AND DELTA TEMP OPENED COWL AND FOUND DELTA P POP ON RISDR FDEA202004100728Linkage · brokenTHE MAIN CARGO DOOR IS DENTED AND GOUGED ON SKIN AT UPPER FWD CORNER OF DOOR FROM FWD LIFT ACT. LINKAGE BREAKING. COMPLETED REPAIR OF MAIN DECK CARGO DOOR REF B757 SRM 52-30-01-2R.SDR FDEA201812173530Deck Plate · corrodedCORROSION AROUND FASTENER HOLES IN MAIN CARGO FLOOR STRUCTURE SHEAR WEB UPPER CHORD UPPER SURFACE B.S. 1681 RBL.48 REMOVED CORROSION AT STA.1681 RBL48. ORIG. MAT. .071", REM.MAT..055, MATERIAL LOSS OF .016" IS OUT OF LIMITS PER B757 SRM 53-00-51-1A. FABRICSDR FDEA201812173529Deck Plate · corrodedCORROSION AROUND FASTENER HOLES IN THE MAIN CARGO FLOOR STRUCTURE SHEAR WEB UPPER CHORD UPPER SURFACE B.S.1681 RBL.12. REMOVED CORROSION, MATERIAL LOSS .027", REMAINING MAT. .044" OUT OF LIMITS IAW B757 SRM 53-00-51-1A DETAIL II, CUT-OUT DAMAGE, FABRICATEDSDR FDEA201612024305Skin · dentedSIX INCH HORIZONTAL DENT ON THE RIGHT SIDE FOR THE VERTICAL STAB VSS 125. REPAIRED THE VERTICAL STAB IAW SRM 51-70-10-2R. PRIMED AND TOP COATED IAW SRM 51-70-10-2R AND AMM 51-21-10-7.SDR FDEA201611294288Skin · debondedLEFT HORIZONTAL STAB HSS 81.0 FOUND DEBONDED. REPAIRED IAW SRM 51-70-17-0G PRIMED AND TOP COATED IAW SRM 51-70-17-0G AND AMM 51-21-10-7.SDR FDEA201611294287Frame · chafedPUNCTURE ON FRAME BS 231 FORWARD ACCESSORY ACCESS DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR IAW EA F-5310-T0330045 P1.SDR FDEA201501190228Skin · dentedA 2 INCH X 2 INCH X .094 INCH DENT ON TOP OF THE RT HORIZONTAL STAB. REPAIRED IAW SRM 55-10-01 FIG 201 REPAIR 4. CATEGORY A MAJOR REPAIR.SDR FDEA201412024031Skin · delaminatedRIGHT INBD FLAP, OTBD LOWER END, INNER SKIN DISBONDED. REPAIRED RT INBD FLAP, OTBD LOWER END SKIN IAW SRM 51-70-10. IAW EA F-5710-T0313603 FOR RSC TRACKING. MAJOR REPAIR.SDR FDEA201412024030Skin · damagedAFT CARGO DOOR SKIN AT LOWER AFT CORNER, NOTED EDGE WITH PREVIOUS BLEND. PREVIOUS BLEND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01 PG 104 DETAIL 4. MATERIAL LOSS .017 INCHES OF ORIGINAL .063 INCHES. REPAIR DOUBLER, INSTALLED TO REPAIR DAMAGE IAW SRM 52-30- SDR FDEA201411183796Frame · mechanic errorMAIN CABIN, LT AT BS 960 FWD EMER WINDOW CUT OUT JUST BELOW STRINGER 9L DOUBLE DRILLED HOLE IN FRAME. FUSELAGE FRAME REPAIR AT STATION 960 BELOW STRINGER 9L WAS ACCOMPLISHED DUE TO EFFECTING THE PTF CONVERSION ON EA 757-5342-16-F4770 REV DATED NOV 7 2014 & NRSDR FDEA201411043504Skin · delaminatedNR 1 SLAT TE WEDGE UPPER SURFACE DELAMINATED AT INBD END. REPAIRED IAW SRM 51-70-10 REPAIR 4 .SDR FDEA201410293416Frame · corrodedFRAME BS 1661 STRINGER 25L TO 25R CORRODED ON AFT LOWER FLANGE. R & R FRAME IAW DWG 146N1032 & SRM 51-40-02 DUE TO CORROSION FOUND WITH MATERIAL LOSS CLEANUP OF .047 OF ORIGINAL .063 OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. MAJOR REPAIR.SDR FDEA201410283410Frame · corrodedBS 1620 STRINGER 22R - 23R, FRAME FOUND TO BE CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1030, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.SDR FDEA201410183300Frame · corrodedCORROSION FOUND ON AFT FUSELAGE FRAME WEB AT BS 1681 BETWEEN STRINGERS 28 - 29R. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. MAJOR REPAIR.SDR FDEA201410183299Frame · corrodedHIDDEN DAMAGE AFT FUSELAGE AT STATION 1710 BETWEEN STRINGER 28R & 29R FRAME WEB AFT FACE HAS CORROSION.SDR FDEA201410173234Stringer · corrodedHIDDEN DAMAGE STRINGER 27L STATION 1661 - 1720 CORRODED BETWEEN STRINGER & SKIN. R & R STRINGER STATION 1661 - 1720, STRINGER 27L IAW SRM 51-40-02. CORROSION WAS OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DETAIL I. MAJOR REPAIR.SDR FDEA201410163228Frame · corrodedAFT PIT BS 1580 STRINGER 28L - 30 FRAME & SHEAR TIE CORRODED. REMOVED AND REPLACED FRAME AT STA 1580, FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS OF .011" OF ORIGINAL 0.63", IAW SRM 53-00-07, FIG 101, DETAIL I, AND IAW SRM 51-40-02 AND DWG 140N2002. MAJORSDR FDEA201410163229Frame · corrodedAFT CARGO BAY BS 1640, STRINGER 26 - 28L FRAME CORRODED. REMOVED COROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DEATIAL II. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02 AND DWG 146N1032. MAJOR REPAIR.SDR FDEA201410163227Floorbeam · corrodedBS 365, LBL 7, WL 208, FLOORBEAM UPPER ANGLE CORRODED. FOUND OUT OF LIMITS PER SRM 53-00-51, FIG. 101, DETAIL III. REPAIRED THE FLOORBEAM ANGLE BETWEEN LBL 15 - RBL 69, IAW SRM 53-00-51, FIG. 201, REPAIR 8. MAJOR REPAIR.
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