N777FD
Service difficulty reports · 69
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 = 'N777FD' 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 = 'N777FD' 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 FDEA201905211105Girt Bar · defectiveL1 SLIDE ARM LIGHT DOES NOT ILLUMINATE WHEN DOOR IS ARMED. REMOVED AND REPLACED L1 DOOR GIRT BAR P/N ON 140N2762-17 S/N FX0009 P/N OFF 140N2762-18 S/N LIA 7402 REF. AMM 52-11-25-5-0, A/C IS OK FOR SERVICE.SDR FDEA2018111973267Diaphragm · unknownL1 SLIDE PACK FELL OUT OF DOOR RECESS WHEN DOOR OPENED FROM OUTSIDE. (DOOR NOT DISARMED FROM PREVIOUS FLIGHT). REPLACED DIAPHRAGM IN L1 DOOR EMERGENCY POWER RESERVOIR PER M.M. 12-15-10-3 & SERVICE SAME TO GRESDR FDEA201802080320Not Reported · unknownLOST LEFT HYDRAULIC QUANITY & PRESSURE ON 5 MILE FINAL. RAN QRH AND LANDED. REMOVED AND REPLACED THE TEMP LINE IAW AMM 20-10-10-4-0. TESTED THE LT DOWNLOCK ACTUATOR AND LINES IAW AMM 32-32-02-4, NO LEAKS NOTED. RAN ENGINES IAW MM-3614 AND ACTUATED ALL FLISDR FDEA201711033140Wire · damagedR1 SLIDE LIGHT INTERMITTENT, FOUND WIRE W3682-0003-20 AND WIRE W3682-0012-20 BROKEN APPROX 60 INCHES FROM SPLICE SP1478 AND SPLICE SP68. REPAIRED REF WDM 25-66-11 PG 901 AND SWPM. CKS OK. MEL CLEARED AND PLACARD REMOVED.SDR FDEA201608052824Pitot Tube · damagedBIRDSTRIKE ON DEPARTURE. LOST ALL AIRSPEED INDICATIONS AND ASSOCIATED ITEMS ON F/O'S SIDE. R & R F/O'S PITOT TUBE REF 34-11-01-4, THROUGH STEP 29, STEP 30, LEAKAGE TEST NEEDS ACCOMPLISHED. PERFORMED PITOT LEAK CHECK OF F/O'S PITOT TUBE IAW AMM 34-11-01-5. SDR FDEA201603271093Collar · inoperativeL1 DOOR HOLD OPEN LOCK INOPERATIVE. DOOR OPENS & SHUTS NORMALLY. R & R L1 DOOR HOLD OPEN LOCK COLLAR & CATCH IAW MM 52-11-08-8. OPERATIONS CHECKED GOOD.SDR FDEA201602050459Stop Fitting · galledCABIN L1 DOOR, FWD EDGE NR 1 - 7 STOP PINS FOUND METAL GALLING. R & R IAW AMM 52-11-00 REV 114. ADJUSTMENT CHECK CARRIED OUT IAW AMM 52-11-00 REV 114. FOUND GOOD. REPAIR CLASSIFIED AS MINOR.SDR FDEA201602050458Bearing · looseCABIN L1 DOOR, FWD EDGE LOWER LATCH CRANK FOUND LOOSEN AT SUPPORT BEARING AREA. L1 DOOR, FWD LOWER LATCH CRANK R & R IAW CMM 52-11-07 REV 114. L1 DOOR FWD LOWER LATCH CRANK SUPPORT BEARING R & R IAW SOPM 20-50-03 REV 127. ADJUSTMENT CHECK CARRIED OUT IAW AMSDR FDEA201512294100Seat Track · damagedBS 608, RBL 45.5, SEAT TRACK INNER FLANGE, FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321333. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201512284088Support Angle · corrodedBS 1681, R4 DOOR SCUFF PLATE SUPPORT ANGLE FOUND CORRODED. REPAIRED IAW EA F-5310-T0321518 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201512133981Seat Track · damagedBS 988, BL 45.5, SEAT TRACK CROWN, SUPPORT INNER FLANGE FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321399 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201512103964Floorbeam · corrodedCABIN BS 1640, FLOORBEAM EXISTING REPAIR HAS CORROSION. COMPLIED WITH EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201512103963Floorbeam · corrodedBS 1640, FLOORBEAM HAS CORROSION. REPAIRED IAW EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201511293814Skin Panel · chafedRIGHT WING, OTBD NOSE SKIN FOUND CHAFED AT 2.5" FROM OTBD EDGE. NOSE SKIN R & R IAW SRM 51-40-02 REV 116 & DWG 113N3500 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201511253775Beam · gougedFORWARD CARGO DOOR LOWER EDGE BEAM HAS GOUGE MARKS. R & R WITH NEW LOWER EDGE BEAM IAW DWG NR 143N6603 SHT 9 REV F. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201511183690Support Beam · wornNUMBER 2 PYLON, FAN COWL SUPPORT BEAM AFT WEB, OTBD DOUBLER AT NAC STATION 102.1, FOUND WEAR MARK.SDR FDEA201511173656Doubler · debondedEXISTING REPAIR, WINGS RT SIDE, THERE IS A RT INBD FLAP LOWER SURFACE INBD PANEL REPAIR. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PART 1. FOSDR FDEA201511173657Doubler · debondedEXISTING REPAIR, RT SIDE UPPER SIDE OF INBD MAIN FLAP PANEL. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PART 1. FOUND REPAIR DOUBLER DIS BONEDSDR FDEA201511173659Frame · damagedCABIN STATION 1460, STRINGER 1 FRAME WEB FOUND TWO EACH ELONGATED HOLES AFTER BRACKET REMOVED, REF SNRM N01466. CABIN FRAME REPAIR CARRIED OUT IAW SRM 53-00-07 FIG 201 REPAIR 3 REV 116. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10,000 FLIGHT CYCLES, AFTERSDR FDEA201511173658Frame · damagedCABIN STATION 1480, STRINGER 1 FRAME TWO EACH FASTENER HOLES FOUND ELONGATED. FRAME REPAIR CARRIED OUT AT STATION 1480, LBL 3 & RBL 3 IAW SRM 53-00-07 FIG 201 REPAIR 3 REV 116. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10,000 FLIGHT CYCLES, AFTER REPAIR HFESDR FDEA201511083517Support · corrodedBS 680, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORRODED. REPAIRED IAW EA F-5310-T0321853 A PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201510313430Crease Beam · damagedCABIN STATION 1110 RT, CREASE BEAM WEB FOUND 01 ELONGATED HOLE. CABIN CREASE BEAM WEB AT STATION 1100 - 1120, RBL 63 & RBL 70.5 REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 1 REV B RSDR FDEA201510313429Crease Beam · damagedCABIN STATION 1110 RT, CREASE BEAM INNER CHORD FOUND 01 EACH ELONGATED HOLE. REMOVED IAW SRM 51-40-02 REV 116 FROM STATION 1040 - 1180 RT. CREASE BEAM INNER CHORD FABRICATED IAW DWG 144N5124 SHT 1 REV. INSTALLED IAW 144N5200 SHT 1 REV B & SHT 2 REV B. REPASDR FDEA201510313428Crease Beam · damagedCABIN STATION 932 RT, CREASE BEAM WEB FOUND O1 EACH ELONGATED HOLE. CREASE BEAM WEB REMOVED AT STATION 920 - 940, RBL 63 & 70.5 IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 144N5140 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201510313427Crease Beam · damagedCABIN STATION 932 RT, CREASE BEAM INNER CHORD FOUND 01 EACH ELONGATED HOLE. CREASE BEAM INNER CHORD REMOVED AT STATION 900 - 1040 RT IAW SRM 51-40-02 REV 116. CREASE BEAM INNER CHORD FABRICATED IAW DWG 144N5152 SHT 1 REV. INSTALLED IAW DWG 144N5140 SHT 3 RESDR FDEA201510313426Crease Beam · chafedBS 1590 LT, CREASE BEAM INBD CHORD LOWER SURFACE CHAFED. COMPLIED WITH EA F-5310-T0321812 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201510313425Crease Beam · corrodedBS 984 - 996 RT, CREASE BEAM INNER CHORD VERTICAL FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM INNER CHORD R & R IAW DWG 144N5140 SHT 3 REV D & SHT 4 RESDR FDEA201510313424Crease Beam · corrodedCABIN STATION 1120 - 1140 LT, CREASE BEAM WEB FOUND CORROSION. FOUND OUT OF 10% LIMIT IAW SRM 53-40-13, ALLOWABLE DAMAGE 1 FIG 101 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALLSDR FDEA201510313423Crease Beam · corrodedCABIN STATION 1420 - 1440 RT, CREASE BEAM WEB UPPER SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA EVALUATED, MATERIAL THICKNESS REMOVED 0.010", FOUND OUT OF 10% LIMIT IAW SRM 53-60-13 ALLOWABLE DAMAGE 1 FIG 101 REV 116. CREASDR FDEA201510313422Crease Beam · corrodedCABIN STATION 1140 - 1160 RT, CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW 51-10-02 REV 115. REWORKED AREA, EVALUATED MATERIAL & REMOVED 0.026" FOUND OUT 10% LIMIT IAW SRM 53-40-13, ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40SDR FDEA201510313421Crease Beam · corrodedCABIN STATION 996 - 1020 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED EVALUATED MATERIAL & REMOVED 0.014" FOUND OUT OF 10% LIMIT IAW SRM 53-40-12 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-0SDR FDEA201510313420Beam · crackedFORWARD E & E COMPARTMENT, STATION 263 BHD, BL 0 VERTICAL BEAM UPPER END CRACKED. CRACKED VERTICAL BEAM REMOVED & NEW VERTICAL BEAM FABRICATED IAW DWG 141N2913 SHT 1 REV B & INSTALLED IAW DWG 141N2910 SHT 1 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201510313419Crease Beam · corrodedCABIN STATION 960 - 984 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED MATERIAL THICKNESS, REMOVED 0.020 " FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB R & R ISDR FDEA201510313418Crease Beam · corrodedCABIN STATION 940 - 960 RT, CREASE BEAM WEB FOUND CORROSION. REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, EVALUATED & REMOVED 0.006" & FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. SDR FDEA201510293402Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS & SCRATCHES ALONG THE BELLY OF THE ACFT, BETWEEN STRINGER 26 LT & 26 RT, AT BS 520 - 540. EXTERIOR SKIN, NUMEROUS SMALL NICKS & SCRATCHES REMOVED, FOUND OUT OF LIMIT AT STATION 537, 2.5" TO STRINGER 28R IAW SRM 53-00-01 FIG SDR FDEA201510283393Skin · nickedFUSELAGE EXTERIOR SKIN LT SIDE, AFTER SHORING REMOVAL & SKIN CLEAN UP, FOUND A NICK MARK AT BS 620 & STRINGER 28. EXTERIOR SKIN, NICK MARK REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 116. REPAIR CARRIED OUT AS IAW SRM 53-00-01 FIG 201SDR FDEA201510283392Skin · scratchedFUSELAGE UNDER SHORING LT SIDE, THERE ARE SEVERAL SMALL SCRATCHES AT THE SHORING PAD AREA, BS 200 - 210, FROM LBL 30 - BL 0. REMOVED & FOUND OUT OF LIMIT AT STATION 200, LBL 9.5 IAW SRM 53-00-01 FIG 101 DETAIL 11 REV 116 & COMPLIED WITH EA F-5330-T0321490 PARSDR FDEA201510223304Seat Track · chafedCABIN STATION 780 - 790, RBL 45.5, SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0322310 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201510223303Seat Track · chafedCABIN STATION 560 - 564, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0322362 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201510223306Seat Track · chafedCABIN STATION 984 - 996, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA MEASURED CLEAN UP DEPTH OF 0.028" ON SEAT TRACK CROWN EXCEEDS CROWN LIMIT OF 0.020" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 SDR FDEA201510223305Seat Track · chafedCABIN STATION 780 - 800, RBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.493" ON SEAT TRACK, CROWN LIP EXCEED LIP LIMIT OF 0.48" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 RSDR FDEA201510223302Seat Track · chafedCABIN STATION 700 - 720, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.028" ON SEAT TRACK CROWN EXCEED CROWN LIMIT 0.02" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 11SDR FDEA201510193277Skin · damagedFUSELAGE EXTERIOR SKIN RT SIDE AT BS 1530, BETWEEN STRINGER 27 - 28, THERE IS A DEEP BLEND. DEEP BLEND FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116 & REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 116. THIS IS CAT B REPAIR. INSPESDR FDEA201510193276Skin · crackedEXTERIOR SKIN NUMEROUS SMALL NICKS & SCRATCHES ALONG THE BELLY OF THE ACFT, BETWEEN STRINGERS 26 LT & 26 RT AT BS 1580 - 1600. REMOVED IAW SRM 51-10-02 REV 115, FOUND WITHIN LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116, EXCEPT HFEC INSPECTED FOUND CRACK ASDR FDEA201510183271Support · corrodedCABIN STATION 365, RBL 45.5 SEAT TRACK CROWN SUPPORT FOUND CORROSION. CABIN STATION 365, RBL 45.5 SEAT TRACK CROWN SUPPORT CORROSION REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THRU. SEAT TRACK CROWN & SUPPORT REMOVED BETWEEN STATION 365SDR FDEA201510183270Support · corrodedCABIN STATION 365, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORROSION. SEAT TRACK CROWN SUPPORT CORROSION REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THRU. SEAT TRACK CROWN & SUPPORT REMOVED, BETWEEN STATION 365 - 440, RBL 24.75 IAW SRM SDR FDEA201510173264Splice · corrodedBS 1080 RT CREASE BEAM INNER CHORD SPLICE FITTING FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND CORROSION MORE THAN 50% THROUGH. CORRODED SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1SDR FDEA201510163254Splice · corrodedBS 1120 RT, CREASE BEAM INNER CHORD SPLICE FITTING, FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND MORE THAN 50% THROUGH. CORRODED SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1 REV & ISDR FDEA201510163253Door Sill · corrodedAFT CARGO DOOR CUT OUT LOWER SILL WEB, CORROSION AT STATION 1420. AFT CARGO DOOR CUT OUT CORRODED WEB AT STATION 1380 - 1440, STRINGER 27R, R & R WITH NEW FABRICATED WEB IAW DWG 146N8522 SHT 1 REV E. NEW WEB FABRICATED IAW DWG 146N8522 SHT 1 REV E. REPAIR CSDR FDEA201510143204Seat Track · chafedBS 1555 - 1575, RBL 24.75, SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, AND FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 REV 116. SEAT TRACK REMOVED, & FABRICATED IAW DWG 146N5137 SHT 1 REV & INSTALLED IAW DWG 146N5120 SHT
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