N778FD

Service difficulty reports · 82

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 = 'N778FD' 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 FDEA201603020758Bolt · looseFORWARD E & E COMPARTMENT, RT FWD RUDDER CONTROL QUADRANT LOWER MOUNT, THREE BOLTS PARTIAL INSTALLED FOUND DURING RUDDER SYS RIGGING. R & R IAW AMM 27-21-05 REV 114. R/H FWD RUDDER CONTROL QUADRANT BOTTOM BEARING HOUSING R & R IAW AMM 27-21-05 REV 114. RUDDEMar 2, 2016 · N778FD · Boeing 757222 · Rudder Control SystemSDR FDEA201603020757Regulator · damagedFLIGHT CONTROLS, DURING BUY BACK, FOUND ELEVATOR TENSION REGULATOR SPRING GUIDE BROKEN. LT SIDE ELEVATOR TENSION REGULATOR R & R IAW AMM 27-31-12 REV 115. CONTROL CABLE FOR ELEVATOR TENSION REGULATOR REMOVED & INSTALLED AFTER MX IAW AMM 27-31-12 REV 115. ADMar 2, 2016 · N778FD · Boeing 757222 · Elevator Control SystemSDR FDEA201602260690Skin · dentedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS AN EXISTING DENT WITH PREVIOUS OPERATOR STICKER AT BS 395 - 418, STRINGER 14 - 17. DENT FOUND OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101 DET III REV 116. REPAIR CARRIED OUT IAW EA F-5330-T0323629 PART 1. FUSELAGE SKINFeb 26, 2016 · N778FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201602100499Beam · gougedNR 1 CARGO DOOR, LOWER EDGE BEAM HAS GOUGES. NR 1 CARGO DOOR LOWER EDGE BEAM REPLACED IAW EA F-5230-T0323763 P 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 10, 2016 · N778FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA201601280360Skin Panel · debondedEXISTING REPAIR WING. THERE IS A REPAIR AT RT SIDE INBD MAIN FLAP, UPPER PANEL AT MF STATION 300. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B. HISTORY 5100-9 DATED 12 1 2006. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF Jan 28, 2016 · N778FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201601260318Skin · damagedLEFT WING, AFT OVERWING ATTACH FITTING, ABOVE FRONT SPAR & NR 4 SLAT INBD MAIN TRACK REMOVAL, FOUND OSS 346 LE FIXED RIB COMMON TO WING UPPER SKIN LE LOCK FASTENER HOLE, ONE EACH, ELONGATED. LT WING OSS 346 LE FIXED RIB COMMON TO WING UPPER SKIN LE LOCK FASTEJan 26, 2016 · N778FD · Boeing 757222 · Wing, Plate/SkinSDR FDEA201601240288Seat Track · corrodedBS 870 - 898, LBL 45.5, SEAT TRACK CROWN SUPPORT FOUND CORROSION AROUND THE BUSHING AREA. CORROSION EVALUATED & FOUND CORROSION MORE THAN 50% THROUGH EXCEED LIMIT IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 117. NEW SEAT TRACK SUPPORT FABRICATED IAW DWJan 24, 2016 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201601220281Floorbeam · damagedCABIN STATION 936, LBL 45.5, FLOORBEAM INNER FLANGE FOUND 01 ELONGATED FASTENER HOLE. REPAIRED IAW EA F-5310-T0322784 PART 1. REPAIR CLASSIFIED AS MAJOR.Jan 22, 2016 · N778FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201601090092Crease Beam · corrodedCABIN STATION 960 - 984 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, MEASURED ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.053", MATERIAL REMOVED 0.010", FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 FIG 101 ALJan 9, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601080080Door Sill · damagedBS 360, R1 DOOR CUT OUT LOWER SILL WEB, FOUND ONE ELONGATED FASTENER HOLE. REPAIRED IAW DWG 141N8422 SHT 1 REV R. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jan 8, 2016 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201601070072Splice · corrodedBS 1140 LT, CREASE BEAM INNER CHORD SPLICE FITTING, FOUND CORRODED. REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THROUGH. CREASE BEAM, INNER CHORD SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. NEW CREASE BEAM, INNER CHORD SPLICE FITTIJan 7, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601050032Skin · wornEMPENNAGE, LT SIDE, THE HORIZONTAL STABILIZER BLADE SEAL PERIMETER HAS WEAR AT BS 1862 - 1875, ABOVE STRINGER 17. CHAFE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-80-01 FIG 101 DETAIL VII REV 116. REPAIR CARRIED OUT IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 117.Jan 5, 2016 · N778FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201601040019Fitting · crackedBS 1140 RT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CRACKED. REMOVED IAW SRM 51-40-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040018Fitting · corrodedBS 1120 LT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CRACKED & CORRODED. REMOVED IAW SRM 51-40-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040017Fitting · corrodedBS 1080 LT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CRACKED & CORRODED. REMOVED IAW SRM 51-40-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201601040016Fitting · corrodedBS 1120 RT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CORRODED. REMOVED IAW SRM 51-10-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201601040015Crease Beam · corrodedBS 940 - 960 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT ORIGINAL THICKNESS 0.056", REMAINING THICKNESS 0.034", FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMJan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040014Crease Beam · corrodedBS 1100 - 1120 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT, ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.055", FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEBJan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040013Crease Beam · corrodedBS 1080 - 1100 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT, ORIGINAL THICKNESS 0.071", REMAINING THICKNESS 0.060", FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEBJan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040012Crease Beam · corrodedBS 960 - 984 , LEFT CREASE BEAM WEB FOUND CORRODED. FOUND OUT OF LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, AND DWG 144N5140 SHT 03 REV D. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201512314109Floor Support · crackedCOCKPIT BS 200 - 205, RBL 35 - RBL 38, FLOOR SUPPORT FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, AND DWG 141N5810 SHEET 1 REV G. REPAIR CLASSIFIED AS MAJOR.Dec 31, 2015 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512284098Door Sill · corrodedBS 680 - 730, R2 DOOR CUT OUT LOWER SILL INNER CHORD FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT, ORIGINAL THICKNESS 0.080", REMAINING THICKNESS 0.069", FOUND OUT OF 10% LIMITS IAW SRM 53-30-15 ALLOWABLE DAMAGE 1 REV 11Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512284097Crease Beam · corrodedCABIN STATION 1140 - 1160, LT CREASE BEAM WEB FOUND CORROSION. CREASE BEAM REMOVED AS PER SRM 51-10-02 REV 116. ORIGINAL THICKNESS 0.063" REMAINING THICKNESS 0.054". FOUND OUT OF 10% LIMIT AS PER SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMODec 28, 2015 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201512284096Crease Beam · corrodedCABIN STATION 1140 - 1160, RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 116. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.053", FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IADec 28, 2015 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201512284095Seat Track · chafedBS 1165 - 1170, RBL 45.5, SEAT TRACK FOUND CHAFED. REMOVED & FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116, MEASURED LIP DISTANCE 0.49". SEAT TRACK, BETWEEN STATION 1075 - 1180, RBL 45.5 R & R WITH NEWLY FABRICATED SEAT TRACK IAW DWG 144N50Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284094Seat Track · chafedCABIN STATION 1165 - 1170, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, DWG 144N5021 SHT 1 REV A,Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284093Seat Track · chafedBS 1165 -1170, LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, DWG 144N5021 SHT 1 REV A, AND DWG 144Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284092Seat Track · chafedCABIN STATION 1180 - 1200, LBL 45.5 SEAT TRACK CROWN CHAFED. COMPLIED WITH EA F-5310-T0323360 A PART 1. OUT OF LIMIT CHAFED MARK FOUND ON SEAT TRACK LIP CROWN, AT STATION 1198, LBL 45.50. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284091Seat Track · chafedCABIN STATION 982 - 990, RBL 24.75 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK CROWN REMOVED AS PER SRM 51-10-02 REV 116. EVALUATION CARRIED OUT REMAINING DIMENSION 0.17" AND FOUND OUT OF 0.26" LIMIT PER SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK CRODec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2015030493199Floorbeam · corrodedFORWARD FUSELAGE STATION 324, RBL 59 HAS CORROSION AT FASTENER HOLES. BLENDED THE CORROSION & DETERMINED IT TO BE OUT OF LIMITS IAW SRM 51-10-02. EA 130893 & ECRA 5310-05820 WERE ISSUED TO ADDRESS THE DAMAGE. IAW ECRA 5310-05820 REV A, INSPECTION OF THE BS Mar 2, 2015 · N778FD · Boeing 757222 · Fuselage Main, Floor BeamSDR CALA2015030493198Frame · corrodedAFT PIT BS 1480 FRAME CORRODED BETWEEN STRINGER 26 & 27 RT. REMOVED CORROSION IAW STM 51-10-02 & FOUND IT TO BE OUT OF LIMITS IAW SRM 53-02-07 & SRM 53-30-07. EA 130911 & ECRA 5360-01340 WERE ISSUED TO ADDRESS THE DAMAGE. IAW ECRA 5360-01340, THE BS 1480 BEMar 2, 2015 · N778FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2015030493197Skin · dentedFUSELAGE DENT 5 FT FWD OF DOOR 2L AT FLOOR LINE. MEASURES .75" X .062" DEEP. DENT IS CRACK FREE & MUST BE REPAIRED BY NEXT C CHECK. THE DENT WAS FOUND OUT OF LIMITS IAW SRM 53-00-03. THE REPAIR AT BS 605 - 618 FUSELAGE BETWEEN STRINGER 15L & 18L HAS BEEN AMar 2, 2015 · N778FD · Boeing 757222 · Fuselage Main, Plate/Skin
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