N978FD

Service difficulty reports · 114

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 = 'N978FD' 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 FDEA201310312662Web · corrodedBS 1615 - 1620, S19R WEB TO STRINGER IS MISSING FIVE LOCK FASTENERS AND IS BULGING. CORROSION WAS OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DET. 8, CAT "B". REPAIRED IAW 60000410860001, EA 757-5361-16-F4347, REV-.Oct 31, 2013 · N978FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310302655Frame · corrodedNR 3 CARGO DOOR LOWER FRAME BETWEEN FWD CAVITY, INTERNAL SIDE CORRODED, REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-53, DET V, FIG 101. REMOVED DAMAGE AREA IAW SRM 51-70-13 FIG 1. INSTALLED REPAIR IAW SRM 51-40-02 AND 51-70-13, FIG Oct 30, 2013 · N978FD · Boeing 757236 · Cargo/Baggage DoorsSDR FDEA201310292638Structure · corrodedLEFT INBD MAIN FLAP CORRODED. R & R LT INBD MAIN FLAP IAW AMM 27-51-02/401. ADJUSTED IAW AMM 27-51-02/501. PERFORMED TEST IAW AMM 27-51-02-5. CHECKED GOOD.Oct 29, 2013 · N978FD · Boeing 757236 · Trailing Edge FlapsSDR FDEA201310182553Attach Fitting · corrodedLEFT PYLON OTBD ATTACH FITTING HAS CORROSION ON INBD AND OTBD SIDES. COMPLIED WITH EA F-5710-T0300911, PT 1. REPAIR IS CLASSIFIED AS CATEGORY B, MAJOR.Oct 18, 2013 · N978FD · Boeing 757236 · Nacelle/Pylon, Attach FittingsSDR FDEA201310152516Skin · corrodedLT HORIZONTAL STAB UPPER SKIN CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-01, FIG 101, DETAIL III. COMPLIED WITH EA F-5510-T0300660B. REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR.Oct 15, 2013 · N978FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201310152515Skin · corrodedLEFT HORIZONTAL STAB UPPER SKIN, CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-01, FIG 101, DETAIL III. COMPLIED WITH EA F-5510-T0300660B . REPAIR CLASSIFIED AS CATEGORY B MAJOR.Oct 15, 2013 · N978FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201310152513Skin · corrodedLEFT HORIZONTAL STAB UPPER SKIN, SS 91. 6 INCHES AFT OF FWD SPAR CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS IAW SRM 55-10-01, FIG 101 DETAIL II. COMPLIED WITH EA F-5510-T0300660B. REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR.Oct 15, 2013 · N978FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201310072444Structure · damagedHOLE ON LT WING FOUND TO BE .375 SHOULD BE .308 -.313. FOUND DURING SB 757-54-0035, REV 6. COMPLIED WITH EA F-5710-T0300911. CLASSIFIED AS A CATEGORY B, MAJOR REPAIR.Oct 7, 2013 · N978FD · Boeing 757236 · Wing Main, Frame StructureSDR FDEA201309212277Shear Tie · gougedAFT CARGO, BS 1620 S27-28R, SHEAR TIE AFT SIDE IS GOUGED. R & R SHEAR TIE IAW DWG 146N1022, SH5, REV A AND SRM 51-40-02, CAT "A" MAJOR REPAIR.Sep 21, 2013 · N978FD · Boeing 757231 · Fuselage Internal Mounting StructureSDR FDEA201309192260Shear Tie · puncturedAFT CARGO BAY FRAME BS 1540, BETWEEN S28-29L, SHEAR TIE PUNCTURED. REMOVED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE AND INSTALLED. MAJOR REPAIR.Sep 19, 2013 · N978FD · Boeing 757236 · Fuselage Internal Mounting StructureSDR FDEA201309142223Skin · corrodedFUSELAGE SKIN CORRODED BS 1872. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. REMOVED SKIN IAW SRM 51-40-02. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG148N3611. REPAIR CLASSIFIED AS CATEGORY "A" MAJOR RSep 14, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201309132211Stringer · corrodedSTRINGER 23L, BS 1872 CORRODED. REMOVED STRINGER IAW SRM 51-40-02. REMOVED CORROSION ON STRINGER IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101. INSTALLED NEW STRINGER IAW SRM 51-40-02 AND DWG 148N3601. THIS REPAIR CLASSIFIED AS CASep 13, 2013 · N978FD · Boeing 757236 · Fuselage Main, Longeron/StringerSDR FDEA201308312095Frame · dentedAFT CARGO, BS 1320 S25L, FRAME UPPER FLANGE DENTED. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, SHT 1. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-40-02 AND DWG 146N1007. MAJOR REPAIR.Aug 31, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201308312097Frame · damagedAFT CARGO, STA 1420, FRAME, S25L-S26L, INBD FLANGE HAS 4 EA DRILLED HOLES. FOUND FRAME OUT OF LIMITS IAW SRM 53-00-07, FIG 101. REMOVED FRAME IAW SRMM 51-40-02. FABRICATED NEW FRAME AND INSTALLED IAW SRM 51-40-02 AND DWG 146N1012 SH 3. MAJOR REPAIR.Aug 31, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201308282060Skin · damagedSCRIBE LINE ON SKIN AT S26L BS 475 TO 661. REPAIRED IAW 60000411490001 AND EA 757-5331-16-F4238. . REPAIR CLASSIFIED AS A CATEGORY A MAJOR.Aug 28, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201308262043Sill · corrodedBS 1862.70 - 1885.20, S25L SILL CORRODED. REMOVED SILL IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DET II. INSTALLED NEW SILL IAW SRM 51-40-02 AND DWG 148N3601. REPAIR IS CLASSIFIED AS MAJOR.Aug 26, 2013 · N978FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201308262059Frame · corrodedAFT CARGO, BS 1300, LBL 21-RBL 21, FRAME CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-07, DETAIL 2, FIG. 101. REMOVED AND REPLACED FRAME IAW DWG 146N1006, SH.3, REV. E, AND SRM 51-40-02. MAJOR REPAIR (CAT. "A")Aug 26, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201308262036Skin · damagedSCRIBE LINE FOUND AT STRINGER 19R LAP SEAM FROM BS 439.625 TO 560.875. REPAIRED IAW EA 757-5331-16 -F4253, REV-. MAJOR REPAIR.Aug 26, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201308232017Spar · corrodedRT WING REAR SPAR BELOW RT FUEL PUMP HAS CORROSION. COMPLIED WITH EA F-5710-T0300819 STEPS 1, 2 WING -BASIC STRUCTURE-WING SPAR CORROSIONS AT AFT BOOST PUMPS MOUNT. MAJOR REPAIR.Aug 23, 2013 · N978FD · Boeing 757231 · Wing SparSDR FDEA201308201977Skin · dentedRIGHT SKIN BS 395-377.7 S18-19R DENTED. REPAIRED IAW EA F-5330-T0301940. REPAIR CLASSIFIED AS CATEGORY A MAJOR.Aug 20, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201308201992Crease Beam · corrodedRT CREASE BEAM INBD ANGLE UPPER SURFACE HAS CORROSION BS 680 - 730. REMOVED CORROSION IAW SRM 51-00-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101, DETAIL VIII. R & R RT INBD CREASE BEAM ANGLE IAW SRM 51-40-02 AND DWG 143N8328. REPAIR IS CLASSIFIEDAug 20, 2013 · N978FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201308201975Angle · gougedRT UPPER LOBE WEB SUPPORT ANGLE GOUGED BS 739, S13R.Aug 20, 2013 · N978FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201308201974Web · gougedRT UPPER LOBE FRAME SUPPORT WEB AT BS 739, S13R GOUGED.Aug 20, 2013 · N978FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201308201990Skin · delaminatedRIGHT WING OTBD AFT FLAP UPPER SKIN HAS DELAMINATION. REMOVED DELAMINATED AREA AND REPAIRED IAW SRM 57-53-01 AND 51-70-17, PARA 3B - 3H.Aug 20, 2013 · N978FD · Boeing 757236 · Trailing Edge FlapsSDR FDEA201308141887Skin · corrodedNR 2 STRUT BETWEEN PPSTA 128.05 TO PPSTA 209.5 LT SKIN INTERNAL SURFACES WITH SEVERAL AREAS OF CORROSION. FOUND OUT OF LIMITS IAW SRM 54-50-01, PAGE 103, DETAIL II, SECTION A-A. REMOVED SKIN IAW SRM 51-40-02. DRILLED AND INSTALLED NEW SKIN SRM 51-40-02 ANAug 14, 2013 · N978FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR FDEA201308061971Skin · dentedEXTERNAL FUSELAGE SKIN BS 500 -520 BETWEEN S26-27R HAS A DENT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. REPAIRED BY REPAIR NR 16 OF SRM 53-00-01, PG 201. THIS IS A CATEGORY B REPAIR.Aug 6, 2013 · N978FD · Boeing 757231 · Fuselage Main, Plate/SkinSDR FDEA201308021751Frame · corrodedAFT CARGO, BS 1280 BETWEEN S28-29L FRAME LOWER WEB CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL I. R & R FRAME IAW DWG 146N1005, SH3 REV E AND SRM 51-40-02. MAJOR REPAIR.Aug 2, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201307311780Frame · dentedAFT CARGO BS 1440, S23-24L FRAME UPPER ANGEL DENTED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028. MAJOR REPAIR.Jul 31, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201307311711Skin · corrodedNR 2 STRUT BETWEEN STA 209.50 -128.08, RT INTERNAL SKIN WITH CORROSION ON SEVERAL AREAS. REMOVED RT OTBD SKIN IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 54-50-01. FOUND TO BE OUT OF LIMITS IAW SRM 51-50-01, DETAIL V, PAGE 104. LOCATED AND DRILLED IAW SRJul 31, 2013 · N978FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR FDEA201307311710Skin · corrodedFUSELAGE SKIN INTERNAL JUST OTBD OF S25L, BS 1850 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. REPAIRED SKIN IAW EA F-5330-T0300943. MAJOR REPAIR.Jul 31, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201307311709Skin · corrodedFUSELAGE SKIN INTERNAL JUST OTBD OF S25L, BS 1850 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II . REPAIRED SKIN IAW EA F-5330-T0300943. MAJOR REPAIR.Jul 31, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201307161575Skin · corrodedRIGHT HORIZONTAL STAB UPPER SKIN CORRODED. REPAIRED IAW EA F-5510-T0301861, PT1 AND EA F-5510-T0301002. PT1, MAJOR REPAIR, CAT. "B".Jul 16, 2013 · N978FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201307141557Panel · crackedLEFT ELEVATOR FWD LOWER L/E HINGE LINE PANEL HAS A CRACKED IN TWO CUT-OUT AREAS BETWEEN STA 52 & 76. REPAIRED LT ELEVATOR IN 2 CUT-OUT IAW SRM 51-70-04, PARA 4E. MAJOR REPAIR.Jul 14, 2013 · N978FD · Boeing 757236 · Elevator, Plate/SkinSDR FDEA201307141556Skin · crackedRIGHT ELEVATOR L/E, STA 102.5, CRACKED. REPAIRED RT ELEV L/E IAW SRM 51-70-04, PARA 4E. MAJOR REPAIR.Jul 14, 2013 · N978FD · Boeing 757236 · Elevator, Plate/SkinSDR FDEA201307141555Skin · crackedRIGHT ELEVATOR , STA 78.5, UPPER L/E SKIN CRACKED. REPAIRED RT ELEVATOR IAW SRM 51-70-04, PARA 4E. MAJOR REPAIR.Jul 14, 2013 · N978FD · Boeing 757236 · Elevator, Plate/SkinSDR FDEA201307101523Crease Beam · damagedMDC LT CREASE BEAM INBD ANGLE FROM BS 1370-1630 HAS DOUBLE DRILLED HOLES, NUMEROUS SHORT EDGED MARGIN HOLES AND SEVERAL AREAS AROUND FASTENERS HOLES SHOW BARE METAL. R & R INBD CHORD FROM BS 1370 - 1630 LT IAW SRM 51-40-02, DWG 146N5590. PART OUT OF LIMITS FOJul 10, 2013 · N978FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201307081513Frame · dentedAFT CARGO, BS 1540 S25-26L, FRAME UPPER ANGLE DENTED. REMOVED FRAME, IAW SRM 51- 40-02. FABRICATED FRAME. INSTALLED NEW FRAME IAW SRM 51-40-02 AND DWG 146N1048. MAJOR REPAIRJul 8, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201307061484Skin · puncturedRT WING INBD MAIN FLAP LOWER SKIN PUNCTURED. REPAIRED IAW SRM 57-53-01 AND 51-70-06, PAR 5, B.Jul 6, 2013 · N978FD · Boeing 757236 · Trailing Edge FlapsSDR FDEA201307061483Skin · puncturedRT WING INBD MAIN FLAP LOWER SKIN PUNCTURED LOC. 85IN FROM INBD END, 6IN FROM T/E. REPAIRED IAW SRM 57-53-01 AND 51-70-06, PAR 5.B. MAJOR REPAIR.Jul 6, 2013 · N978FD · Boeing 757236 · Trailing Edge FlapsSDR FDEA201307011436Frame · dentedFWD CARGO BAY BS 680 S24L FRAME UPPER FLANGE DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101. R & R FRAME AT BS 680 S17-24L IAW DWG 143N1024 AND SRM 51-40-02. CAT "A" MAJOR REPAIR.Jul 1, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201306251414Frame · dentedAFT CARGO, BS 1520 S-26L, FRAME UPPER ANGLE DENTED. NO DENTS ALLOWED IAW SRM 53-00-07. REMOVED FRAME IAW SRM 51-40-02. FABRICATED NEW FRAME AND INSTALLED IAW SRM 51-40-02 AND DWG 146N1017. REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR.Jun 25, 2013 · N978FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201306251398Crease Beam · corrodedMDC LT CREASE BEAM INBD ANGLE AT BS 1290 -1370 , HAS CORROSION , SCRATCHES , AND DOUBLE DRILLED HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL VIII. R & R LT CREASE BEAM INBD ANGLE IAW SRM 51-40-02 AND DWG 146N8326.Jun 25, 2013 · N978FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201306231373Skin · dentedEMPENNAGE STA 1900, RBL 12, DENTED. REPAIRED IAW SRM 53-80-01 & 51-70-10, REP 2. EMPENNAGE STA 1900 RBL 12, CAT "A". MAJOR REPAIR.Jun 23, 2013 · N978FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201306211368Skin · dentedNR 2 CARGO DOOR LOWER FWD CORNER DENT ON SKIN EDGE CAUSED REPAIR TO SEPARATE. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01, FIG 101, DETAIL VI. REPAIRED NR 2 CARGO DOOR LOWER FWD CORNER SKIN EDGE IAW SRM 52-30-01 REPAIR NR 4. MAJOR REPAIRJun 21, 2013 · N978FD · Boeing 757236 · Cargo/Baggage DoorsSDR FDEA201306211367Crease Beam · corrodedMDC RT CREASE BEAM AT BS 1290-1405 HAS CORROSION, TOP AND BOTTOM SURFACES INCLUDED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ON INBD CHORD FOUND OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL VIII. R & R STRUCTURE IAW SRM 51-40-02 AND DWG 146N8Jun 21, 2013 · N978FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201306131371Floorbeam · corrodedFLOORBEAM AT BS 1640 UPPER TEE HAS CORROSION AND GOUGED ON ENTIRE UPPER SURFACE. FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-51, FIG 101, DETAIL VI. R & R FLOORBEAM AT BS 1640 IAW-SRM-51-40-02 AND DWG 146N5089. MAJOR REPAIR.Jun 13, 2013 · N978FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201306051196Seat Track · damagedSEAT TRACK BS 1540 - 1640 RBL 24.75 DAMAGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL I, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02, DWG 146N5130. THIS IS CATEGORY "A" MAJOR REPAIR.Jun 5, 2013 · N978FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201306051203Skin · dentedLEFT EXTERNAL FUSELAGE HAS DENTED BETWEEN S16-17L, BS 250. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DETAIL III. REPAIRED SKIN IAW SRM 53-00-01, FIG 201, REPAIR 16. REPAIR MAJOR.Jun 5, 2013 · N978FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201305311152Crease Beam · corrodedRT CREASE BEAM UPPER SURFACE HAS CORROSION, BS 560- 600. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG.101, DETAIL VIII. R & R CREASE BEAM RT INBD ANGLE BS 450 - 665 IAW SRM 51-40-02 & DWG. 143N5520. CATEGORY "A" MAJOR May 31, 2013 · N978FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201305301144Floorbeam · damagedFLOORBEAM AT BS 1280 UPPER CHORD HAS NICKS, GOUGES, MISDRILLED HOLE AND NUMEROUS SHORT EDGED MARGIN HOLES. CLEANED AND REWORKED 3 EA. MISDRILLED HOLES, CHECKED LIMITS, EDGE MARGINS HOLES, FLOORBEAM FOUND TO BE OUT OF LIMITS IAW-SRM-51-40-06, REMOVED FLOORBEAMMay 30, 2013 · N978FD · Boeing 757236 · Fuselage Main, Floor Beam
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