N979FD

Service difficulty reports · 130

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 = 'N979FD' 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.

SDR FDEA201706201712Proximity Sensor · out of adjustGEAR DOORS EICAS WITH DOOR ANNUCIATOR, AFTER TAKEOFF. WITH GEAR HANDLE PLACED IN THE OFF POSITION. INSPECTED LEFT AND RIGHT MAIN GEAR DOORS, STOPS, STOP PLATES, AND SENSORS. FOUND LEFT AND RIGHT FORWARD STOP BOLTS WORN BEYOND LIMITS. LEFT READS .017, RIGHJun 20, 2017 · N979FD · Boeing 757236 · Landing Gear Door Retract SectionSDR FDEA201705131408Collar · brokenWHILE SECURING AIRCRAFT FOUND L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. DOOR WOULD NOT LOCK IN THE OPEN POSITION. REMOVED AND REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR IAW AMM 52-11-08-8. DOOR OPS CHECKED GOODMay 13, 2017 · N979FD · Boeing 757236 · Passenger/Crew DoorsSDR FDEA201701050048Proximity Sensor · obstructedL1 DOOR SLIDE ARM LITE INOP. CLEANED AND REMOVED DEBRIS AWAY FROM THE FWD AND AFT L1 DOOR GIRT BAR PROX SENSORS. SLIDE LIGHT OPERATES NORMALLY WHEN ARMED AND DISARMED PER AMM 25-66-11-2. NO HISTORY, OK TO CONTINUE.Jan 5, 2017 · N979FD · Boeing 757236 · Door Warning SystemSDR FDEA201611284259Warning Light · false activationON APPROCH, PASSING 500 FEET AGL, RECEIVED TOO LOW GEAR CAWS. LANDING GEAR INDICATORS DISPLAYED GREEN THREE DOWN. PERFORMED GO AROUND, SECOND APPROACH ALL INDICATIONS NORMAL. ON POSTFLIGHT STATUS PAGE DISPLAYED -LDG GEAR MONITOR -GEAR DISAGREE -L EEC Nov 28, 2016 · N979FD · Boeing 757236 · Landing Gear Position and WarningSDR FDEA201611113956Proximity Switch · dirtyLEFT SLIDE ANNUNCIATOR ARM LIGHT DOES NOT ILLUMINATE WHEN ARMED. CLEANED GIRT BAR PROXIMITY SWITCHES, TESTS NORMAL IAW AMM 25-66-11-2.Nov 11, 2016 · N979FD · Boeing 757236 · Emergency EquipmentSDR FDEA201511073512Nut · looseL1 ENTRY DOOR, SLIDE LIGHT WILL NOT ILLUMINATE WHEN ARMED. FOUND ARMING LINK AT L1 LOWER DOOR CAM ASSEMBLY, BOLT LOOSE CAUSING SLOP IN THE MECHANISM. TIGHTENED NUT ON BOLT & PERFORMED OPERATIONS TEST OF GIRT BAR MECHANISM.Nov 7, 2015 · N979FD · Boeing 757236 · Emergency EquipmentSDR FDEA201511033451Girt Bar · looseL1 DOOR SLIDE LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-66-05-A CATEGORY C, EXPIRATION 13 NOV 15. ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH Nov 3, 2015 · N979FD · Boeing 757236 · Emergency EquipmentSDR FDEA201503120939Relay · inoperativeAFTER TAKEOFF GEAR HANDLE DID NOT MOVE PAST THE OFF POSITION WHEN RETRACTING GEAR. GEAR DISAGREE EICAS LIGHT ILLUMINATED. QRH RED TABS DIRECTED, THE GEAR WILL NOT MOVE UP CHECKLIST TO BE ACCOMPLISHED. AFTER RETRACTING THE GEAR USING THE LOCK OVERRIDE SWITCMar 12, 2015 · N979FD · Boeing 757236 · Landing Gear Retraction/Extension SystemSDR FDEA201502270607Unknown · malfunctionedTRAILING EDGE FLAP DISAGREE. FLAPS STOPPED AT GREATER THAN 20 BUT LESS THAN 25. WHEN POWER SWITCHED TO APU FLAPS CYCLED BACK TO 20 & DISAGREE WENT AWAY. PERFORMED BITE OF ALL 3 FSEU'S IAW FIM 27-51, NO EXISTING FAULTS. FLIGHT DECK TESTED GOOD. PERFORMED Feb 27, 2015 · N979FD · Boeing 757236 · Trailing Edge Flap Control SystemSDR FDEA201409172635Lamp · inoperativeSLIDE LIGHT ABOVE LT ENTRY DOOR HAS A LAMP OUT. RELAMPED IAW WITH SMP 33.Sep 17, 2014 · N979FD · Boeing 757236 · Emergency LightingSDR FDEA201408272326Girt Bar · dirtyTO GET SLIDE LIGHT ON DURING CLOSE-UP FIRST OFFICER HAD TO OPEN & RECYCLE DOOR L1 TO GET A GOOD SLIDE ARMED INDICATION. LUBED L1 DOOR GIRT BAR MECHANISM IAW AMM 12-21-18-3, ARMING SLIDE TESTED GOOD.Aug 27, 2014 · N979FD · Boeing 757236 · Emergency EquipmentSDR FDEA201405060954Battery Pack · dischargedEMERGENCY LIGHT ABOVE L1 DOOR DIM & GOES OUT. R & R BATTERY PACK FOR LT SIDE EMER LIGHT IAW AMM 33-51-07-2. OPERATIONS CHECKED NORMAL.May 6, 2014 · N979FD · Boeing 757236 · Emergency LightingSDR FDEA201311122742Skin · delaminatedRT SIDE EMPENNAGE, AFTER REMOVAL THE UPPER SKIN BETWEEN THE FWD SPAR AND FWD AUX SPAR FOUND DELAMINATION ON THE LOWER SKIN OF THE HONEYCOMB BETWEEN STABILIZER BS 176-224. REPAIRED IAW EA F-5510-T0303533. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201311122734Structure · damagedRT SIDE OF EMPENNAGE AFTER REMOVAL THE UPPER SKIN BETWEEN THE FWD SPAR AND FWD AUX SPAR FOUND NUT PLATE HAS ELONGATED HOLE AT INBD LOGO LIGHT. REPAIRED IAW EA F-5510-T0303569. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer StructureSDR FDEA201311122733Skin · delaminatedRT SIDE HONEYCOMB INTERIOR SIDE, LOWER SIDE OF UPPER SKIN, DELAMINATED. REMOVED AND REPAIRED OUT IAW EA F-5510-T0303533. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311122741Skin · delaminatedEMPENNAGE RT SIDE AFTER REMOVAL THE UPPER SKIN BETWEEN THE FORWARD SPAR AND FORWARD AUX SPAR FOUND DELAMINATION ON THE LOWER SKIN OF THE HONEYCOMB BETWEEN STABILIZER STA 128 -176. THE UPPER SKIN BETWEEN FORWARD SPAR AND FWD AUX SPAR ON THE LOWER SKIN BETWEEN Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311122740Skin · dentedDENT IN RT HORIZONTAL STABILIZER UPPER SURFACE BETWEEN FRONT SPAR AND REAR SPAR, STAB STA 200 -224. DENT REPAIRED IAW EAF-5510-T0303533. . REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311122739Skin · distortedUPPER SKIN BETWEEN THE FORWARD SPAR AND FORWARD AUX SPAR FOUND HONEYCOMB HAS BEEN DISTORTED ON THE OTBD END AT STABILIZER STA 224. SKIN REPAIRED IAW EAF-5510-T0303533. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311102721Skin · damagedNUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT BS 620-640. DAMAGE REMOVED ANDFOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II, REV 109 AND REPAIRED IAW EA F-5330-T0302663. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 10, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201311082715Skin · puncturedSKIN DENTED AT BS 460-480, STR 27L- 28L, PUNCTURED THROUGH. REPAIRED IAW EA F-5240-T0303070. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 8, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201311082714Skin · damagedNUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 540-520, 540 -560, STR 26L-26R EXTERIOR SKIN NICKS AND SCRATCHES. REMOVED, FOUND OUT OF LIMIT AT STA 523, ABOVE STR 28L AND STA 529 BELOW STR 27L IAW SRM 53-00-01, FIG 101 DETAIL II, Nov 8, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201310272627Floorbeam · chafedBS 1640 BL 0 - LBL 30, FLOORBEAM UPPER FLANGE FOUND CHAFED AROUND FASTENER HOLES. FLOORBEAM REMOVED IAW SRM 51-40-02 REVISION 109. NEW FABRICATED FLOORBEAM INSTALLED IAW DWG 146N5089 SHEET 1 REV B. REPAIR IS CLASSIFED MAJOR IAW GMM 6-2-100.Oct 27, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310272626Floorbeam · chafedBS 1640, BL 0 TO RBL 45.5, FLOORBEAM UPPER FLANGE FOUND CHAFED. FLOORBEAM REMOVED IAW SRM 51-40-02 REVISION 109 AND NEW FABRICATED FLOORBEAM INSTALLED IAW DWG 146N5089 SHEET 1 REVISION B. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.Oct 27, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310212565Frame · chafedFWD E & E BAY BS 255, RBL 3, FRAME WEB CHAFED. REPAIRED IAW EA F-5310-T0303276 PART 1. REPAIR IS CLASSIFIED AS MAJOR.Oct 21, 2013 · N979FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201310162520Floorbeam · corrodedBS 1661, BL 0 - RBL 51.5, FLOORBEAM UPPER FLANGE LOWER SURFACE FOUND CORRODED AROUND FASTENER HOLES. CORRODED FLOORBEAM REMOVED AND REPLACED WITH NEW FABRICATED IAW DWG 146N5110 SHT.2 REV.B AND INSTALLED IAW DWG 146N5090 SHT.5 REV.- AND DWG 146N5500 SHT.1 ROct 16, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310142499Panel · corrodedCENTER WING TANK UPPER PANEL FOUND CORRODED BS 1016, RBL 63. REPAIRED IAW EA F-5730-T0302786 PART 1 .Oct 14, 2013 · N979FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201310132488Floorbeam · corrodedFLOORBEAM UPPER TEE FOUND CORRODED AT UPPER AND LOWER SURFACES BS 377.7, BL 0-LBL 20. REMOVED AND REPLACED FLOORBEAM FABRICATED IAW DWG 141N5123 SHT 1 REV A AND INSTALLED IAW DWG 141N5113 SHT 1 REV F AND SRM 51-40-02 REV 109. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310132487Floorbeam · corrodedFLOORBEAM UPPER TEE BS 377.7, LBL 58 FOUND CORRODED AT UPPER SURFACE. REMOVED AND REPLACED FLOORBEAM FABRICATED AS PER DWG 141N5123 SHT.1 REV.A AND INSTALLED IAW DWG 141N5113 SHT.1 REV.F AND SRM 51-40-02 REV.109. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310132486Seat Track · chafedSEAT TRACK BS 1600 -1640 RBL 45.5 FOUND CHAFED AT THE CROWN AND BOTTOM. REPAIRED IAW SRM 53-00-52 REPAIR 1 FIG. 201 REV 109. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201310132485Angle · corrodedL2 DOOR LOWER SILL INBD ANGLE BS 690 -730 FOUND CORRODED AND CHAFED AT UPPER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310132483Angle · chafedR2 DOOR LOWER SILL INBD ANGLE BS 720 -730. FOUND CHAFED AT UPPER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310132482Sill · corrodedL2 DOOR LOWER SILL INBD CHORD BS 730-755 FOUND CORRODED AT UPPER SURFACE. REMOVED AND REPLACED IAW SRM 51-40-02 REV.109 AND DWG 143N8322 SHT.1 REV.K. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310132490Floorbeam · corrodedFLOORBEAM UPPER TEE FOUND CORRODED AT UPPER SURFACE BS 365.25, RBL 24.75 - 45.5. REMOVED AND REPLACED IAW SRM 51-40-02 REV 109 AND DWG 141N5112 SHT 1 REV D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310132489Floorbeam · corrodedCABIN - STA 365.25 BL0 -RBL 24.75 FLOORBEAM UPPER CHORD, UPPER SURFACE FOUND CORROSION AT EDGE. REMOVED AND REPLACED IAW SRM 51-40-02 REV 109 AND DWG 141N5112 SHT 1 REV D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310132484Angle · corrodedRT CREASE BEAM INBD ANGLE BS 1320 -1340 FOUND CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED IAW DWG 146N8322 SHT.1 REV.F. REPAIR IS MAJOR.Oct 13, 2013 · N979FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201310082448Skin · crackedMAIN E/E BAY ACCESS DOOR INNER SKIN CRACKED AT THE HOLE EDGE. REPAIRED IAW EA F-5240-T0303070. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Oct 8, 2013 · N979FD · Boeing 75728A · Electrical/Electronic Compartment DoorsSDR FDEA201310052415Stiffener · gougedBS 324, LBL 20, FLOORBEAM STIFFENER FOUND GOUGED AT EDGE. REPAIRED IAW EA F-5320-T0302984 PART 1. REPAIR IS MAJOR.Oct 5, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201310052414Strap · crackedCABIN - STA 365.25-377.7 LBL 24.75 FLOORBEAM STABILIZER STRAP FOUND CRACKED. REPAIRED IAW EO F-5320-T0302912A PART 1.Oct 5, 2013 · N979FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310052417Deck Plate · corrodedBS 1681, BL 0 -LBL 50, DECK PLATE UPPER SURFACE FOUND CORRODED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.Oct 5, 2013 · N979FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201310052419Deck Plate · damagedBS 1681, RBL 39, DECK PLATE ONE FASTENER HOLE ELONGATED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV D. REPAIR IS MAJOROct 5, 2013 · N979FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201310052418Deck Plate · corrodedBS 1681-1720, RBL 39, DECK PLATE UPPER SURFACE FOUND CORRODED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 AND REPLACED IAW DWG 146N5300 SHT 6 REV D.Oct 5, 2013 · N979FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201310052416Deck Plate · corrodedBS 1715, LBL 17 - RBL 17, DECK PLATE UPPER SURFACE FOUND CORRODED. DECK PLATE REMOVED IAW SRM 51-40-02 REV 109 & REPLACED IAW DWG 146N5300 SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.Oct 5, 2013 · N979FD · Boeing 757236 · Fuselage Floor PanelSDR FDEA201310032385Failsafe · corrodedBS 500 FRAME OTBD FAILSAFE FOUND CORRODED AT EDGE S17R. REPAIRED IAW EA F-5310-T0302910 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.Oct 3, 2013 · N979FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA201309302347Failsafe · corrodedCABIN, BS 620, STRINGER 17R FRAME OTBD FAILSAFE FOUND CORRODED AT EDGE. FAILSAFE REMOVED AND REPLACED IAW DWG 146N8513 SHT.1 REV.A AND INSTALLED IAW DWG 143N8512 SHT.1 REV.J. REPAIR IS MAJOR.Sep 30, 2013 · N979FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201309302346Crease Beam · chafedBS 755 -780 LT CREASE BEAM INBD ANGLE FOUND CHAFED AT UPPER SURFACE. REPAIRED IAW EA F-5310-T0302749, PART 1. REPAIR CLASSIFIED MINOR PER BMM 6-2-100.Sep 30, 2013 · N979FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201309292336Bulkhead · crackedNR 1 PYLON STRUT MID BULKHEAD LOWER FLANGE OTBD FWD SIDE AT PYLON STA 174.3. FOUND SHIM FRAYED AND MIGRATED. NDT INSPECTED-MID BULKHEAD FOUND CRACKED AT ATTACHMENT TO LOWER ANGLE. DAMAGED SHIM REMOVED AND SOLID TAPERED SHIM FABRICATED AND INSTALLED PER SRM 5Sep 29, 2013 · N979FD · Boeing 757236 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201309272330Skin · damagedFUSELAGE SKIN HAS NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 540 -560. DAMAGE REMOVED & FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 109 AND REPAIRED IAW EA F-5330-T0302746. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-1Sep 27, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201309242298Skin · damagedSKIN HAS NUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 600 -620. DAMAGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 109 AND REPAIRED IAW EA F-5330-T0302663. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100Sep 24, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201309242294Skin · scratchedFUSELAGE EXTERIOR SKIN LT SIDE SCRATCHED ALONG THE PERIMETER OF THE WING TO BODY FAIRING MATING SURFACE AT BS 780-760, STRINGER 25-27L. REMOVED SCRATCHES AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIGURE 101 DETAIL 2 REV. 109 AND REPAIRED IAW EA F-5330-T0302661Sep 24, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201309212272Floorbeam · corrodedBS 333.45, LBL 45.5 - 64, FLOORBEAM UPPER TEE FOUND CORRODED AT UPPER AND LOWER SURFACES. REMOVED AND REPLACED WITH NEW BEAM FABRICATED IAW DWG 141N5120 SHT.1 REV.A AND INSTALLED IAW EWG 141N5110 SHT.1 REV.B. REPAIR IS MAJOR.Sep 21, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor Beam
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