N772FD
Service difficulty reports · 133
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 = 'N772FD' 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 = 'N772FD' 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 FDEA201506021674Shear Tie · damagedFUSELAGE RT SIDE, EXISTING REPAIR DEFECT. THE SHEAR TIE AT BS 580 BETWEEN STRINGER 26 - 27 HAS 3 HOLES. ACCOMPLISHED EA F-5310- TO317519 . REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505281643Spar · corrodedLEFT WING, AFTER CORROSION REMOVAL, FOUND LT REAR SPAR BLENDED AREA, BOTH DEPTH & WIDTH OUT OF LIMITS AT LT AFT BOOST PUMP LOWER BONDING LEAD CONNECTION POINT. REPAIRED IAW EA F-5710-T0317079 P1. REPAIR CLASSIFIED AS MINOR.SDR FDEA201505281642Stringer Splice · damagedAFT CARGO BAY BS 1617 - 1643, STRINGER 19L. STRINGER SPLICE FASTENER HOLES ELONGATED. R & R THE STRINGER SPLICE IAW DWG 146N3700 SHT 3 REV G, AND DWG 146N3821 SHT 2 REV B. MAJOR REPAIR.SDR FDEA201505251631Deck Plate · chafedCABIN STATION 1681 - 1690, RBL 45 - 55, AFT DECK PLATE UPPER SURFACE FOUND CHAFED MARKS. COMPLIED WITH PART 1 OF EA F-5310-T0316711 A. REPLACEMENT OF DECK PLATE WITHOUT CHEM-MILLED POCKETS. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505191541Floorbeam · corrodedBS 1681, RBL 21 - 42 FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVED. FLOORBEAM R & R IAW EA F-5310-T0317368. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505191540Floorbeam · corrodedBS 1681, RBL 50 - 52 FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVED. R & R THE FLOORBEAM FLANGE IAW EA F-5310-T0317368. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505191539Skin · chafedR2 DOOR OUTER SKIN, 6 INCHES TO AFT EDGE & 8 INCHES TO LOWER EDGE, FOUND CHAFED. COMPLIED WITH EA F-5210-T0317397 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505191537Frame · gougedFWD E & E COMPARTMENT BS 231.25, LBL 9 FRAME WEB HAS A GOUGE. REPAIRED IAW EA F-5310-T0317393. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505181531Skin Panel · corrodedLEFT WING, AFTER FILL PORT REMOVAL, UPPER SKIN UPPER SURFACE FOUND CORRODED AT OVERWING FILL PORT ADAPTER MATING AREA. REPAIRED IAW EA F-5730-T0317149. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505141506Failsafe · gougedAFT CARGO COMPARTMENT BS 1420, STRINGER 25L - 26L, FRAME FAIL SAFE CHORD HAS EXISTING GOUGE. R & R IAW EA F-5310-T0316972 P1 & DWG 146N1012 SHT 2 REV D. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201505121494Skin · corrodedEMPENNAGE FUSELAGE SKIN INTERIOR SURFACE FOUND CORROSION AT STATION 1787 - 1806, STRINGER 25L - 27L. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SSDR FDEA201505121491Skin · corrodedEMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1787 - 1806, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN P/NO 148N321SDR FDEA201505121490Skin · corrodedEMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1806 - 1825, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN P/NO: 148N32SDR FDEA201505121488Skin · corrodedEMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1844 - 1862, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N3216YSDR FDEA201505121487Skin · corrodedEMPENNAGE AREA INTERIOR COMPARTMENT, THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN STATION 1806 - 1825 FROM STRINGER 25L - 27L. CORROSION REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STSDR FDEA201505121486Skin · corrodedEMPENNAGE, EXTERIOR SKIN THERE IS CORROSION AT STATION 1825 - 1844, STRINGER 25L - 25R. CORROSION REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N321SDR FDEA201505061388Skin · damagedEMPENNAGE EXTERIOR SKIN HAD NICKS & SCRATCHES AT BS 1720 - 1743, STRINGERS 7 - 8L. FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. REPAIR CARRIED OUT IAW EA F-5330-T0317255 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201505021359Floorbeam · corrodedBS 1681 FLOORBEAM FOUND CORRODED. BLENDED OUT, AND FOUND OUT OF LIMITS AT RBL 25. R & R THE FLOORBEAM IAW EA F-5310-T0317368. MAJOR REPAIR.SDR FDEA201504291317Failsafe · corrodedBS 1500, STRINGER 17R, FRAME FAILSAFE FOUND CORRODED. REPAIRED IAW EA F-5310-T0317107 B PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201504231282Door Sill · crackedBS 1641 R4 DOOR LOWER SILL FOUND CRACK. REPAIRED IAW EA F-5310-T0316973. MAJOR REPAIR.SDR FDEA201504231281Stringer · dentedCABIN STATION 1600 - 1620, STRINGER 16L, STRINGER FOUND DENT & EXISTING TRIM OFF. R & R CARRIED OUT IAW EA F-5310-T0316871. UNDOCUMENTED REWORK ON STRINGER 16L UPPER FREE FLANGE, STATION 1600 - 1620. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201504201273Skin Panel · dentedLEFT WING- AFTER SANDING. I/B MAIN FLAP I/B UPPER SKIN PANEL (113N2401) FOUND WITH MULTIPLE DENT MARKS FROM MF STA 165 TO STA 184. LEFT WING, I/B MAIN FLAP I/B UPPER SKIN PANEL (113N2401) MARKED DENT AREA FROM MF STA 165 TO MF STA 184 FOUND OUT OF LIMIT PESDR FDEA201504201265Skin · wornEMPENNAGE EXTERIOR SKIN RT SIDE, THERE IS A WEAR AT BS 1862.70 - 1875, WHERE THE LOWER BLADE SEAL CONTACTS THE SKIN ABOVE STRINGER 17R. FOUND OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL VII REV 114. REPAIRED IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 11SDR FDEA201504201264Skin · wornEMPENNAGE EXTERIOR SKIN LT SIDE, THERE IS A WEAR AT BS 1862.7 - 1875, WHERE LOWER BLADE SEAL CONTACTS THE SKIN ABOVE STRINGER 17L. FOUND OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL VII REV 114. REPAIRED IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 114. MAJSDR FDEA201504191262Skin · scratchedFUSELAGE EXTERIOR SKIN HAS NUMEROUS SMALL SCRATCHES ALONG THE WING TO BODY PERIMETER AT BS 1300 - 1280, STRINGER 27 - 30R. SCRATCHES REMOVED, AND FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. REPAIRED IAW EA F-5330-T0316875 PART 1. REPAIRSDR FDEA201504191261Skin · scratchedFUSELAGE EXTERIOR SKIN, NUMEROUS SMALL SCRATCHES ALONG THE WING TO BODY PERIMETER AT BS 1300 - 1280, STRINGER 27 - 30L. SCRATCHES REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. REPAIRED IAW EA F-5330-T0316875 PART 1. REPAIR CLASSIFSDR FDEA201504151236Spar · damagedRIGHT WING, INBD TE MAIN FLAP FRONT SPAR LOWER CHORD & LOWER SKIN FOUND TO HAVE HOLES ELONGATED AT MF STATION 224. REPAIRED IAW EA F-5710-T0318167 PART 1. MAJOR REPAIR.SDR FDEA201504141228Frame Splice · gougedAFT CARGO COMPARTMENT, BS 1520 24R FRAME SPLICE HAS GOUGED. REMOVED AND REPLACED IAW DWG 146N1017 SHT 3 REV. D, SPLICE FABRICATED IAW DWG 146N1042 SHT 1 REV A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201504131219Window Frame · corrodedBS 1080 - 1100, STRINGER 13R WINDOW FRAME LOWER EDGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 114. OUT OF LIMITS IAW SRM 56-20-02 FIG 101 ALLOWABLE DAMAGE 1 REV 114. WINDOWS FRAME ASSY REMOVED IAW SRM 51-40-02 REV 114 AND REPLACED IAW DWG 144NSDR FDEA201504081168Seat Track · chafedBS 560 - 580, RBL 45.5 SEAT TRACK FOUND CHAFED. REPAIRED IAW EA F-5310-T0317294. MAJOR REPAIR.SDR FDEA201504081167Frame · corrodedAFT CARGO COMPARTMENT STATION 1440, RBL 10 BOTTOM FRAME CORROSION. R & R WITH NEW FRAME IAW DWG NR & 146N1013 SHT 3 REV D. REPAIR CLASSIFIED MAJOR IAW GM 6-2-100.SDR FDEA201504071163Bulkhead · chafedNR 2 PYLON, AFT BULKHEAD INBD LOWER FLANGE EXTERNAL SURFACE FOUND WITH A DEEP CHAFE. REPAIRED IAW EA F-5450-T0316504 PART 1. CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201504071162Bulkhead · chafedNR 2 PYLON AFT BULKHEAD, OTBD LOWER FLANGE EXTERNAL SURFACE FOUND A DEEP CHAFE. REPAIRED IAW EA F-5450-T0316504 PART 1. CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201504061157Door Sill · crackedCABIN, STATION 324 - 365 R1 DOOR CUT OUT LOWER SILL WEB FOUND CRACK AT AFT EDGE & FOUND CORROSION AT MID-AREA AFTER WEB REMOVED FOR ACCESS, SNRM N03651. NEW LOWER SILL WEB FABRICATED AS PER DWG 141N8422 SHT 1 REV R AND INSTALLED AS PER BOEING DWG 141N8422 SHTSDR FDEA201504061160Stringer · corrodedEMPENNAGE AREA INTERIOR COMPARTMENT BETWEEN BS 1844 - 1862 STRINGER 27L CORRODED. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 114. CORRODED STRINGER REMOVED. REPLACED WITH NEW STRINGER IAW DWG 148N3206 SHT 1 2 REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201504061159Skin · corrodedEMPENNAGE AREA INTERIOR COMPARTMENT THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN STATION 1844 - 1862 FROM STRINGER 25L - 27L. CORROSION REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED. REPLACED NEW SKIN. MSDR FDEA201504061158Stringer · corrodedEMPENNAGE AREA INTERIOR COMPARTMENT THERE ARE CORROSION ON STRINGER 25L BETWEEN BS 1825 - 1862. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 114. CORRODED STRINGER REMOVED. REPLACED WITH NEW STRINGER IAW DWG 148N3206 SHT 1 2 REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201504061156Skin · corrodedEMPENNAGE AREA INTERIOR COMPARTMENT, THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN BS 1825 - 1844 FROM STRINGERS 25 - 27L. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, ALLOWABLE DAMAGE 1 REV 114. CORRODED SKIN PANEL REMOVED. REPLACED WITH NEW SKIN PANELSDR FDEA201504021139Skin · chafedRIGHT WING INBD TE MAIN FLAP NOSE SKIN FOUND CHAFED, 3.5 INCHES LONG FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0316509 PART 1.SDR FDEA201503311124Skin · chafedRIGHT WING OTBD TE MAIN FLAP NOSE SKIN FOUND WITH CHAFE MARK AT 2.5" FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0316372 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503311123Bushing · wornLEFT WING PYLON OTBD SIDE LOAD FITTING BUSHING WORN. REPAIRED IAW EA F-5740-T0316366 PART 1. CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201503271103Failsafe · corrodedCABIN, BS 1480, STRINGER 17R, FRAME FAIL SAFE FOUND CORRODED. REPAIRED IAW EA F-5310-T0317422. REPAIR CLASSIFIED AS MINOR.SDR FDEA201503271104Seat Track · chafedBS 1460 - 1480 RBL 24.75, SEAT TRACK CROWN CHAFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.09" EXCEEDS SEAT TRACK CROWN LIMIT 0.06" IAW SRM 53-00-52 DETAIL II FIG 101 ALLOWABLE DAMAGE 1 REV 114. SEAT TRACK REPAIR CARRISDR FDEA201503261088Panel · corrodedBS 960, RBL 53 - 65 CTR FUEL TANK UPPER PANEL JOINT AREA FOUND CORROSION AFTER SEALANT REMOVED. REPAIRED IAW EA F-5730-T031634.SDR FDEA201503251072Seat Track · chafedBS 1570 - 1590, LBL 45.5 SEAT TRACK CROWN CHAFED. REPAIRED IAW EA F-5310-T0317370 PT 1. CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201503231068Pan · chafedCABIN L1 DOOR EXTERNAL HANDLE PAN FOUND CHAFFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA EVALUATED & FOUND CLEAN UP DEPTH OF 0.029" EXCEED 10% LIMIT IAW SRM 52-10-01 FIG 101 ALLOWABLE DAMAGE 1 REV 114. L1 DOOR EXTERNAL HANDLE PAN REMOVED IAW SRM 51-4SDR FDEA201503231067Pan · chafedCABIN L4 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. CHAFED AREA AT L4 DOOR EXTERNAL HANDLE PAN REMOVED IAW SRM 51-10-02 REV 114 & FOUND EXCEEDED LIMIT IAW SRM 52-10-01 FIG 101. ALLOWABLE DAMAGE 1 REV 114. L4 DOOR EXTERNAL HANDLE PAN R & R IAW SRM 51-40-02 REV 1SDR FDEA201503231066Tie · crackedCOCKPIT STATION 200 - 208, RBL 40 - 44 FLOOR TIE FOUND CRACK. CRACKED FLOOR TIE REMOVED IAW SRM 51-40-02 REV 114. NEW FLOOR TIE FABRICATED IAW DWG 141N5811 SHT 1 REV B. INSTALLED IAW DWG 141N5810 SHT 1 REV G. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503231065Tie · crackedCOCKPIT STATION 200 - 205, LBL 40 - 43 FLOOR TIE FOUND CRACK. CRACKED FLOOR TIE AT COCKPIT REMOVED IAW SRM 51-40-02 REV 114. NEW FLOOR TIE FABRICATED IAW DWG 141N5811 SHT 1 REV B & INSTALLED IAW DWG 141N5810 SHT 1 REV G. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201503231070Seat Track · chafedBS 1010 - 1020, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA EVALUATED & FOUND EXCEEDS LIMIT IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 114. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00- 52 FIG 201 REPAIR 4 REV
Back to N772FD