N942FD

Service difficulty reports · 147

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 = 'N942FD' 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 FDEA201202020441Door · misrepairedCARGO DOOR MISREPAIRED. REPAIRED IAW SRM 52-30-01, REPAIR 4, PG 201, FIG 201. CATEGORY "B" MAJOR REPAIR.Feb 2, 2012 · N942FD · Boeing 757225 · Cargo/Baggage DoorsSDR FDEA201202020439Skin · misrepairedCARGO DOOR MISREPAIRED. REPAIR ACCOMPLISHED EA F-5230-157264. MAJOR REPAIR.Feb 2, 2012 · N942FD · Boeing 757225 · Cargo/Baggage DoorsSDR FDEA201202010424Skin · misrepairedFUSELAGE SKIN BS 1681 TO 1661, S-5 TO S-6R MISREPAIRED. REPAIRED IAW EA F-5330-157251. MAJOR REPAIR.Feb 1, 2012 · N942FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201202010420Stringer · gougedFWD PIT STA 620-640 S-25R, UPPER AND LOWER SIDES OF STRINGER GOUGED. BLENDED STRINGER IAW-SRM-51-10-02, ORIG MAT .080 REMAINING .062, OUT OF LIMITS IAW-SRM-53-00-03, FIG 101, DET II. R & R STRINGER CAT "A", MAJOR. REPAIR.Feb 1, 2012 · N942FD · Boeing 757225 · Fuselage Main, Longeron/StringerSDR FDEA201201310405Web · damagedAFT FLOOR WEB HAS A ROW OF DOUBLE DRILLED HOLES AT BL 0, STA 1681-1701. REPAIRED FLOOR WEB IAW SRM 53-60-51 PAGE 201 FIG. 201. MAJOR REPAIR.Jan 31, 2012 · N942FD · Boeing 757225 · Fuselage Miscellaneous StructureSDR FDEA201201260345Skin · damagedFOUND SCRIBE LINE IN BUTT JOINT AT STA 781 BETWEEN S-6R TO S-10R ACCOMPLISHED EA F-5330-157233, FUSELAGE-PLATES AND SKINS (AD 2007-19-07) EO F-5330-7-5000 PT 3 BUTT JOINT SCRIBE LINE AT STA 781 BETWEEN S-6R TO S-10R. MAJOR REPAIR.Jan 26, 2012 · N942FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201230309Floorbeam · corrodedFLOORBEAM AT STA 345, RBL 12 TO LBL 30, REPAIR STRAP IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-40-02. FABRIRICATED NEW STRAP OUT OF 7075-T6 MAT, IAW SRM 53-00-51.TREATED PRIMED AND PAINTED PER AMM 20-50-14, 20-44-04. INSTALLED FABRICATED STRAP PER SRMJan 23, 2012 · N942FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201201220304Stringer · damagedSTRINGER 6R HAS DOUBLE DRILLED HOLE AT STA 418. REMOVED STRINGER IAW SRM 51-40-02 INSTALLED NEW STRINGER IAW SRM 51-40-02. MAJOR REPAIR.Jan 22, 2012 · N942FD · Boeing 757225 · Fuselage Main, Longeron/StringerSDR FDEA201201220303Floorbeam · damagedSTA 1681, FLOORBEAM HAS 2 EA DOUBLE DRILLED HOLES NEAR BL-0. FOUND WHILE ACCOMMPLISHING DECK PLATE REPAIR. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.Jan 22, 2012 · N942FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201201220301Skin · misrepairedNR 4 SLAT LT WING L/E NOSE SKIN AT OSS375 MISREPAIRED. REPAIRED IAW EA F-5750-157213 STEPS 1 THRU 4 EA. MAJOR REPAIR.Jan 22, 2012 · N942FD · Boeing 757225 · Leading Edge DevicesSDR FDEA201201210291Skin · misrepairedFUSELAGE SKIN AT BS 620- 660 BETWEEN S-23R TP S-26R MISREPAIRED. REPAIRED IAW EA F-5330-157267.Jan 21, 2012 · N942FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201210289Stringer · gougedFWD CARGO BAY BS 620- 640, S25R LWR SIDE GOUGED. REMOVED GOUGE IAW SRM 51-10-02 BLENDED AREA ORIG MAT .065 MATERIAL REMAINING .035, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. R & R STRINGER IAW SRM 51-40-02.Jan 21, 2012 · N942FD · Boeing 757225 · Fuselage Main, Longeron/StringerSDR FDEA201201190269Crease Beam · corrodedMAIN CABIN AREA BET BS 1300-1360, S17R, RT SIDE CREASE BEAM INBD CHORD CORRODED. REMOVED CORROSION, ORIG MAT .100 AFTER MAT. REMAINING .060 MAT. LOSS IS .040 MAT. OUT OF LIMITS IAW SRM-53-60-13 DETAIL VIII FIG 101.R & R ANGLE BS 1290-1410 "CAT A, MAJOR REPAIJan 19, 2012 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201201170230Skin · misrepairedFUSELAGE SKIN AT STA 415 BETWEEN S-21R TO S-22R MISREPAIRED. REPAIRED IAW SRM 53-00-01, REPAIR 15. CATEGORY "B" MAJOR REPAIR.Jan 17, 2012 · N942FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201170232Panel · crackedSLAT NR 2 OTBD MAIN TRACK, COVE PANEL CRACKED. REMOVED CRACKED COVE PANEL AND INSTALLED NEW IAW-SRM-51-40-02. MAJOR,CAT A REPAIR.Jan 17, 2012 · N942FD · Boeing 757225 · Leading Edge DevicesSDR FDEA201201130161Panel · crackedSLAT NR 1 COVE PANEL AT INBD AUX TRACK HAS A CRACK AT INBD FASTENER HOLE. REMOVED CRACKED PANEL AND INSTALLED NEW COVE PANEL IAW 51-40-02. MAJOR REPAIR.Jan 13, 2012 · N942FD · Boeing 757225 · Leading Edge DevicesSDR FDEA201201130163Panel · crackedNR 1 SLAT INBD AUX TRACK, COVE PANEL CRACKED. REMOVED DAMAGED COVE PANEL IAW SRM 51-40-02, FABRICATED NEW COVE PANEL. INSTALLED NEW COVE PANEL ON SLAT NR 1 IAW SRM 51-40-02. MAJOR REPAIR.Jan 13, 2012 · N942FD · Boeing 757225 · Leading Edge DevicesSDR FDEA201201070042Fairing · corrodedRT WING TB FAIRING 192AR CORRODED CIRCUMFERENCE OF PANEL AT FASTENER HOLES. CHECKED LIMITS OF ALL REWORKED AREAS. FOUND IN LIMITS EXCEPT 1 EA SPOT AT RBL 2.75 ORIGINAL THICKNESS .075 REMAINING THICKNESS .042 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II, LJan 7, 2012 · N942FD · Boeing 757225 · Aerodynamic FairingsSDR FDEA201201060036Bulkhead · chafedAPU COMPT FWD BULKHEAD CHAFED FS -1885-RT SIDE 7". REPAIRED IAW SRM-53-80-08, FIG 101, REPAIR NR2 AND SRM-51-40-02, CATEGORY A MAJOR REPAIR.Jan 6, 2012 · N942FD · Boeing 757225 · Fuselage Main, BulkheadSDR FDEA201201060035Bulkhead · chafedAPU COMPT FWD BULKHEAD HAS CHAFE MARKS, FS 1885 RT SIDE 7". REPAIRED IAW-SRM-53-80-08, FIG 201, REPAIR 2.Jan 6, 2012 · N942FD · Boeing 757225 · Fuselage Main, BulkheadSDR FDEA201201060031Skin · dentedRT LOWER FUSELAGE SKIN HAS DENT AT BS 745, S25R. DENT DIMENSIONS= A=2.5" Y=.002 A/Y=1250, FOUND TO BE OUT OF LIMITS, ACCOMPLISHED SKIN IAW SRM-53-00-01, FIG 201, CAT B MAJOR REPAIR.Jan 6, 2012 · N942FD · Boeing 757225 · Fuselage Main, Plate/SkinSDR FDEA201201050024Seat Track · corrodedBS 418-440, RBL 45 SEAT TRACK CORRODED REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL MATERIAL .090 AFTER REWORK L=2.5 W=1.5 D=.090 MATERIAL REMAINING .000 FOUND OUT OF LIMITS IAW SRM 53-00- 52. REMOVED SEAT TRACK AT STA 418-440 RBL 45 IAW SRM 51Jan 5, 2012 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201040018Fitting · corrodedSTA 440 RBL 45 SEAT TRACK FITTING CORRODED REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL MATERIAL .200 AFTER REWORK L=2.5 W= 1.0 D= .023 REMAINING MATERIAL .177 FOUND OUT OF LIMITS IAW SRM 53-00- 01. REMOVED SEAT TRACK FITTING IAW SRM 51-40-02Jan 4, 2012 · N942FD · Boeing 757225 · Fuselage Main, Attach FittingsSDR FDEA201112235439Stringer · corrodedSTRINGER BS 418.00 TO 440.0, S22R CORRODED. REMOVED CORROSION IAW SRM 51-10-02 . ORIGINAL MATERIAL .040 REMAINING .030, FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II. R & R STRINGER IAW SRM 51-40-02. MAJOR REPAIR.Dec 23, 2011 · N942FD · Boeing 757225 · Passenger/Crew DoorsSDR FDEA201112215410Frame · corrodedAFTER REMOVAL OF FLOOR SUPPORT AT STA 1500, RBL 2.50 FOUND CORROSION ON FRAME IN AFT CARGO PIT. REMOVED CORROSION AT FRAME IAW SRM 51-10-02. BLENDED AREA. ORIGINAL MATERIAL .063, MATERIAL LOSS .033, MATERIAL REMAINING .030. FOUND OUT OF LIMITS IAW SRM 53-Dec 21, 2011 · N942FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201112205389Frame · misrepairedFRAME BS 800 BETWEEN S28L TO S28R MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.Dec 20, 2011 · N942FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201112175325Seat Track · corrodedSEAT TRACK GOUGED/CORRODED, RBL24 BS418-440. REMOVED DAMAGE AND CHECKED LIMITS. FOUND TO BE OUT OF LIMITS L=3" W=1" D=.025. ORIGINAL MATERIAL .090 AFTER REWORK .065 IAW SRM 53-00-52 FIG 101. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, STA 418-440, RBL 24. MADec 17, 2011 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112135256Frame · gougedFUSELAGE UPPER LOBE INTERIOR BS 365 STR 8-9R FRAME GOUGED. COMPLIED WITH EA F-5310-157243, "CAT A MAJOR REPAIR".Dec 13, 2011 · N942FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201112095234Seat Track · gougedRBL 45 SEAT TRACK GOUGED BS 1180 -1280. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW SRM 53-60-52 AND IAW DWG 146N5120, INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.Dec 9, 2011 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112085219Support · corrodedBS 365-418 RBL 24, SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS ORIGINAL MATERIAL .070 AFTER REWORK L=2 W=1.5 D=.030 REMAINING MATERIAL .040. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-02, FIG 101, DETAIL VII. INSTALLED NEW SEDec 8, 2011 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112085224Floorbeam · misrepairedFLOORBEAM STA 1661, MISREPAIRED. REMOVED FLOORBEAM AT STA 1661 IAW SRM 51-40-02. FABRICATED FLOORBEAM IAW DWG 146N5110. INSTALLED FLOORBEAM AT STA 1661 IAW SRM 51-40-02. MAJOR REPAIR.Dec 8, 2011 · N942FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201112085218Support · corrodedBS 365-418, RBL 45 SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .070 AFTER REWORK L=2.5 W=2 D=.025 REMAINING MATERIAL .045. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. DETAIL VII. INSTALLED NEW SEAT TRACK SUPPODec 8, 2011 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112075204Crease Beam · gougedMAIN CABIN AREA RT SIDE AT BS 1280 CREASE BEAM GOUGED.Dec 7, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201112065178Crease Beam · corrodedRIGHT MAIN DECK CREASEBEAM CORRODED, BS 776. BLENDED AREA IAW SRM 51-10-02. ORIGINAL MATERIAL .090 AFTER BLENDING MATERIAL .040 MATERIAL LOSS .050. OUT OF LIMITS IAW SRM 53-30-13, DETAIL III, FIG 101. REMOVED CREASE BEAM IAW SRM 51-40-02. FABED INBD CHORD FDec 6, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201112065177Seat Track · corrodedSEAT TRACK CORRODED AND GOUGED RBL 45 , BS 640 - 440. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.Dec 6, 2011 · N942FD · Boeing 757225 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112015131Crease Beam · corrodedMAIN DECK RT CREASEBEAM CORRODED BS 660 - 664. BLENDED IAW SRM 51-10-02. ORIGINAL MATERIAL .090 AFTER BLENDING MATERIAL .050 MATERIAL LOSS .040 MATERIAL OUT OF LIMITS IAW SRM 53-30-13, DETAIL III, FIG 101. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NDec 1, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201111285098Floorbeam · misrepairedFLOORBEAM STA 377 MISREPAIRED. REMOVED AND REPLACED IAW 51-40-02.Nov 28, 2011 · N942FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201111225049Frame · misrepairedFRAME STA 1600 BETWEEN S-21R TO S-23R MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.Nov 22, 2011 · N942FD · Boeing 757225 · Fuselage Main, FrameSDR FDEA201111184972Crease Beam · corrodedCREASE BEAM 17L BS 1350 CORRODED. ORIGINAL MATERIAL .100 AFTER BLENDING .065 MATERIAL LOSS .035 MATERIAL OUT OF LIMITS IAW SRM 53-60-13 ALLOWABLE DAMAGE 2 FIG 101 DETAIL VIII. R & R CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.Nov 18, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201111174960Floorbeam · corrodedFLOORBEAM CORRODED BS 1320, BL 0-LBL 24, UPPER TEE. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.Nov 17, 2011 · N942FD · Boeing 757225 · Fuselage Main, Floor BeamSDR FDEA201111174952Gate · corrodedL2 DOOR LWR GATE CORRODED. REMOVED L2 LOWER GATE IAW AMM 52-11-38. DETERMINTED CORROSION EXCEEDING LIMIT IAW SRM 52-10-02. REMOVED HINGE FROM LOWER GATE IAW SRM 51-40-02. INSTALLED HINGE ON NEW LOWER GATE IAW SRM 51-40-02. INSTALLED GATE ON L2 DOOR BOTTOMNov 17, 2011 · N942FD · Boeing 757225 · Passenger/Crew DoorsSDR FDEA201111174947Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER CHORD CORRODED, BS 780, LBL 24 - RBL 24. BLENDED FLOOR BEAM UPPER CHORD IAW SRM 51-10-02 AT STA 780, LBL 24-RBL 24. AFTER REWORK AREA AT STA 780, LBL 24 -BL 0 ORIGINAL MATERIAL IS .125 AFTER REWORK D=.005, L=23 W=1.3 AREA IS WITHIN Nov 17, 2011 · N942FD · Boeing 757204 · Fuselage Main, Floor BeamSDR FDEA201111164938Crease Beam · corrodedRT CREASE BEAM CORRODED BS 440. REMOVED CORROSION FOUND TOOL MARKS OVER 50 PERCENT OF THE THICKNESS OF THE MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL III. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 53-10-13 DNov 16, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201111164937Crease Beam · gougedRT CREASE BEAM GOUGED BS 374. BLENDED GOUGE IAW SRM 51-10-00. CHECKED LIMITS FOUND DOUBLE DRILLED HOLE OUT OF LIMITS IAW SRM 53-00-51. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM AND INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.Nov 16, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201111164935Crease Beam · gougedRT CREASE BEAM GOUGED AT STA 405. BLENDED GOUGE CHECKED LIMITS IAW SRM 53-00-51. MATERIAL REMOVED EXCEEDS 10 PERCENT, .040 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DRAWING III. REMOVED CREASE BEAM IAW 51-40-02 FABRICATED NEW CREASE BEAM IAW SRNov 16, 2011 · N942FD · Boeing 757225 · Fuselage Main, StructureSDR FDEA201111114881Shear Tie · corrodedRT FRAME SHEAR TIE CORRODED BS 1681.0 S22-23R. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA MAX MATERIAL REMOVED .020 ORIG MAT, .050 REMAINING MAT .030 OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DET II. R & R SHEAR TIE IAW SRM 51-40-02. MAJOR REPAIR.Nov 11, 2011 · N942FD · Boeing 757225 · Fuselage Internal Mounting StructureSDR FDEA201111114878Floorbeam · corrodedR2 DOOR ENTRANCE FLOORBEAM CORRODED, BS 324.0, RBL 30.0-62.0. REMOVED CORROSION, ORIGINAL MATERIAL .125 THICK AFTER REWORK .070 THICK L=5', W=2'D=.055, IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW-SRM-53-00-51. R & R TOP FLOORBEAM TEE IAW SRM-51-40-02. CAT "ANov 11, 2011 · N942FD · Boeing 757225 · Fuselage Main, Floor Beam
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