N773FD
Service difficulty reports · 110
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 = 'N773FD' 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 = 'N773FD' 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 FDEA202502050179Floor Panel · damagedVERIFY AFT R/H FLOOR PNL 252MWF HAS THE WRONG INSERTS INSTALLED AND HAS MISSING INSERTS AND HAS COMPOSITE DAMAGE THE ENTIRE LENGTH FABRICATED FLOOR PANEL 252MWF ON VTMAE TRAVELER #T25/1798171 IAW VTMAE DWG #11864182-49, MAJOR REPAIRSDR FDEA202406290903Girt Bar · dislodgedL1 DOOR UNABLE TO ARM PRIOR TO PUSH. GIRT BAR DISLODGED POSITIONED & RECONNECTED L1 DR GIRT BAR REF AMM 25-66-10-2. FUNCTIONAL CHK GOOD, INDCN NORMAL. NO OTHER FAULTS NOTED. ITEM CLOSED. A/C OK TO CONTINUE.SDR FDEA202312051916Rod End · shearedR1 DOOR, ROD END BROKEN AT LOWER DOOR HINGE. COMPLIED WITH E.A. F-5210-T0377325 PART 1. DOOR VERIFIED CLOSED, LOCKED AND SECURED FROM INSIDE AND OUTSIDE. PLACED OLD R1 SLEEVE AND ADJUSTER IN LABLED BOX IN GALLEY AREA. RELEASED FOR SERVICE PER MEL : 52-11-SDR FDEA202309221636Unknown · unknownON TAKE OFF ROLL 110KT, CIRS DC, ATC FAULT CAUTION. AFTER ROTATION ALT CALL OUTS, GND PROX SYS, EQPT OVHT CAUTION. LT AFT FUEL PUMP, RT FWD FUEL PUMP CAUTION BELOW 3000 FT. RETURNED TO FIELD. ON LANDING, ELECT SYS CIRCUIT EQPT COOLING FAN, FWD FUEL BOOST PUMSDR FDEA202304190704Unknown · crackedAFT CARGO DOOR LOWER SILL FWD CORNER LOWER CHORD IS CRACKED. ALL STEPS COMPLIED WITH IAW EA TF-5310-T0313798 FUSELAGE / MAIN FRAME - EXISTING REPAIR AT FUSELAGE NO 2 CARGO DOORWAY LOWER MAIN OUTBOARD CHORD BETWEEN BS 1380 TO BS 1436 MAJOR REPAIRSDR FDEA202303240501Fitting · wornLH WING LWR ATTACHING FITTING COMMON TO I/B DRAG FITTING HAVE 3 HOLES WITH DAMAGE & OUT ROUND CONDITION. I/B DRAG FITTING HAVE 2 HOLES WITH DAMAGE AND OUT ROUND CONDITION. MARKED IN RED. REPAIR BEFORE NDT INSP. COMPLIED WITH EA # F - 5740-T0373064 P1. TITLSDR FDEA202303240500Fitting · corrodedDURING ROTO -TEST OF HOLES 3 AND 8 OF THE L/H WING NDT RECEIVED CORROSION INDICATIONS DOCUMENTED ON F-5730-E0340076 P1, JPF STEP 7. COMPLIED WITH EA # F-5740-T0373064 P1. TITLE: WINGS - ATTACH FITTINGS - LH WING, UPPER SKIN, DRAG FITTINGS, CRACK INDICATIONSDR FDEA202303140425Floorboard · crackedMDCC FLOOR PANEL 251MXF CRACKED/BROKEN. FABRICATED MDCC FLOOR PANEL 251MXF ON VTMAE TRAVELER # T23/1663103 IAW DWG SRZ-25- 005 REVISION R. MAJOR REPAIRSDR FDEA202202040233Pressure Switch · failedJUST PRIOR TO LEVEL OFF, RECEIVED L CTR FUEL PUMP EICAS MESSAGE. COMPLIED WITH QRH. WITH MEL 28-22-02-A ALREADY ON AIRCRAFT FOR RIGHT CENTER PUMP, WE DID NOT HAVE SUFFICIENT FUEL TO CONTINUE TO DESTINATION. DIVERTED TO KMCI PER GOC REQUEST. UPON FSDR FDEA202108182031Actuator · faultedON CLIMB OUT GOT EICAS MESSAGE LE SLAT DISAGREE AND LEADING EDGE DISCRETE LIGHT RETRACTING THE FLAPS AT 200 KNOTS AND 3000 FEET QRH COMPLIED WITH. TROUBLESHOT PER B757 FIM 27-81 FAULT TREE 803 AND FOUND OVERLOAD INDICATOR TRIPPED ON THE INBD SLAT PDU TORQUE LSDR FDEA202105281417Circuit Card · faultedFWD CARGO DET 1 EICAS MESSAGE REPLACED AFOLTS CARD M10427 CARGO TESTS NORMAL REF M.M. 26-10-01-4.SDR FDEA202103170683Rib · crackedLH FIXED WING L/E O/B OF PYLON BULL NOSE ATTACHMENT BRACKET HAS 2EA CRACKS AT FASTENER HOLES REPAIRED PER EA #F-5710-T0360377-P1 WINGS-BASIC WING STRUCTURE -L/H WING ,OUTBOARD FIXED LEADING EDGE,OSS 305,CLOSURE RIB,CRACKED FASTENER HOLESSDR FDEA202103160671Tee Fitting · damagedTEE CLIP COMMON TO STA 1640 FUSELAGE FRAME WEB AND STRINGER S-14L SHOWS 2 EA REJECTABLE INDICATIONS ON ON UPPER AND LOWER INBOARD HOLES. POSSIBLE TOOLING DAMAGE. UPPER INB HOLE INDICATION APX 1 O'CLOCK POSITION. POSITION. LOWER INB HOLE INDICATION APX AT THSDR FDEA202103130635Web · crackedR1 DOOR CUTOUT, HINGE BOX, INBOARD WEB IS CRACKED REMOVED, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 141N8415 AND DWG 141N8441SDR FDEA202103130636Doubler · crackedMAIN CABIN L2 DOOR FWD UPPER HINGE REPAIR DOUBLER IS CRACKED ACCOMPLISHED FEWDEX EA# F-5210-T0315976 : DOORS-PASSENGER/CREW - EXISTING REPAIR FOUND ON THE UPPER HINGES OF DOOR # 2 LH AT STA 693.5 LBL 60- RSC TRACKINGSDR FDEA202103130634Heat Shield · crackedL/W I/B L/E PNEMATIC DUCT AFTER REMOVAL AND CLEANING COKED HYDRAULIC FLUID, FOUND HEAT SHIELD TO BE CRACKED REMOVED DAMAGE FROM L/W I/B L/E PNEUMATIC DUCT AN APPLIED REPAIR PLIES TO NOTED AREA IAW B757 51-70-17 PARA 4H AND EA# F-3610-T0360331-P1 PNEUMATIC SDR FDEA202103090607Angle · cracked#2 PYLON AFT FAIRING O/B SIDE LOWER CHORD FWD ATTACH ANGLE IS CRACKED REMOVE AND REPLACE ANGLE PER BAC DWG #313N3053 REV E AND B757 SRM 51-40-02-OGSDR FDEA202103040565Wire Harness · burnedAPU POWER FEEDER WIRE BUNDLE W2800 CHAFED AGAINST A CLAMP BRACKET AFT OF THE STA 1720 BULKHEAD WL 280 RBL30. REPAIR PER EA F-2450-T0360171 P1 ELECTRICAL POWER - AUXILIARY POWER UNIT (APU) POWER FEEDER WIRE - WIRE BUNDLE ROUTING CHANGE, SB 757-24-0089, AD 2SDR FDEA202102260477Transmitter · failedTE FLAP ASYM ON FINAL, RAN QRH DECLARED AN EMERGNCY REMOVED AND REPLACED L/H FLAP POSITION TRANSMITTER REF B757 AMM 27-58-03-4, AND PERFORMED ADJUSTMENT TEST, OPS CHECKS GOOD.SDR FDEA202101220177Girt Bar · brokenGIRT BAR PART BROKE OFF LEFT FORWARD ENTRY DOOR. REATTACHED GIRT BAR SLIDE, PER MM 25-66-01-4.SDR FDEA201907161572Transmitter · inoperativePDIS 773 27-80 4178 16JUL19 BUF OPEN U LOGPAGES:2977364 AFTER TAKEOFF WHEN CLIMBING OUT FLAPS INDCATORS STOPPED BETWEEN 1 AND THE UP POSITION, WITH FLAP HANDLE IN UP POSITION. NO EICAS INDICATIONS. PUT FLAP HANDLE TO 1 AND LE SLAT DISAGREE EICSDR FDEA201708312453Rope · out of positionROPE ATTACHED TO SLIDE BINDING AT L1 DOOR PROPERLY INSTALLED AND STOWED GIRT BAR STATIC LINESDR FDEA201703220967Slide · low pressurePRESSURE LOW ON RIGHT CREW ENTRY DOOR. REMOVED FAULTY R1 EVACUATION SLIDE ASSEMBLY. INSTALLED A SERVICEABLE SLIDE ASSEMBLY IAW MM 25-66-01-4. OK FOR SERVICE.SDR FDEA201503060697Pan · corrodedFORWARD CARGO COMPARTMENT STATION 700 - 720, STRINGER 20L - 22L MIDDLE WASTE SERVICE PAN UPPER DOUBLER PLATE CORRODED. REMOVED PER SRM 51-10-02 REV 113 AND FOUND OUT OF LIMITS IAW SRM 53-00-53 FIG 101 ALLOWABLE DAMAGE 1 REV 114 PART 1 OF EA F-5310-T0315975.SDR FDEA201503020626Skin · damagedTWO ELONGATED HOLES FOUND ON THE EXTERIOR SKIN AT BS 1360, STRINGER 21 - 22L AFTER DOUBLER REMOVED. REPAIRED IAW EA F-5330-T0315211A PART 1. REPAIR CLASSIFIED AS MAJORSDR FDEA201502230583Seat Track · chafedBS 515 - 530, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502230582Seat Track · chafedBS 538 - 542, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502230581Seat Track · chafedBS 560 - 580, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502230580Seat Track · chafedBS 610 - 620, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502230579Seat Track · chafedBS 464 - 484, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK FABRICATED IAW DWG 143N5086 SHT 1 REV - AND REPLACED IAW DWG 143N5080 SHT 24 REV C. REFER TO DRC 0025 FOR DETAIL REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502070469None · noneEXISTING REPAIR WING, LT SIDE THERE IS A REPAIR AT LT INBD MAIN FLAP LE SKIN, MF STATION 267 - 300. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A3 PT 1 ATTACHMENT B, NO HISTORY.SDR FDEA201502070516None · noneEXISTING REPAIR, FUSELAGE EXTERIOR SKIN. THERE IS A REPAIR AT STATION 1462 - 1480, STRINGER 29L - 29R. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A2 PT 1 ATTACHMENT B, NO HISTORY.SDR FDEA201502070502Skin · scratchedRIGHT WING, LOWER SKIN LOWER SURFACE FOUND SCRATCHED AT FSS 567, 3 - 12 INCHES FROM SKIN LE. REPAIRED IAW EA F-5730-T0315336 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502070519Skin · unknownAFT CARGO DOOR EXTERNAL SKIN FWD LOWER CORNER HAS EXISTING TRIM OFF. COMPLIED WITH EA F-5230-T0315269 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502070501Skin · crackedCABIN R4 DOOR INNER SKIN LIGHTENING HOLE, 1 INCH TO AFT EDGE & 17 INCHES TO LOWER EDGE, FOUND CRACK AT EDGE. REPAIRED IAW EA F-5210-T0315341 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201502070518None · noneEXISTING REPAIR DOOR. THERE IS A REPAIR AT AFT CARGO DOOR, 16 INCHES FROM FWD & 14 INCHES FROM LOWER EDGE, STATION 1391 - 1400, STRINGER 24R - 26R. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-70A2 PT1 ATTACHMENT B, HISTORY 23.SDR FDEA201502070468Shim · migratedLEFT WING, TE CAVITY BETWEEN MLG SUPPORT FITTING & UPPER WING SKIN SHIM MIGRATED AT IRSS 310. REPAIRED IAW EA F-5740-T0313756 PT1. REPAIR IS MAJOR.SDR FDEA201502050444Support Beam · chafedNUMBER 2 PYLON FAN COWL SUPPORT BEAM OTBD RAIL AT NACELLE STATION 75 LOWER SURFACE FOUND CHAFED. REPAIRED IAW EA F-5450-T0315243 PT 1. RAIL GOUGE BLENDED OUT REPAIR. REPAIR CLASSIFIED AS MINOR.SDR FDEA201502040438Skin · chafedRIGHT WING, LOWER SKIN LOWER SURFACE FOUND CHAFED AT WS 574, 4 INCHES LONG FROM SKIN TE. COMPLIED WITH EA F-5730-T0314870 PART 1.SDR FDEA201502040425Skin · scratchedSCRATCHES ON THE EXISTING REPAIR DOUBLER AT BS 1355 - 1380, STRINGERS 21 - 24L. REPAIRED IAW EA F-5330-T0315211A PART 1.SDR FDEA201502020410Panel · chafedRIGHT WING INBD TE, MAIN FLAP UPPER OTBD PANEL, UPPER SURFACE FOUND CHAFE MARK 19 INCHES LONG FROM PANEL OTBD 8" FROM PANEL LE, ITEM ON RACK. REMOVED, DRIED OUT USING 150 DEG F VACUUM PROCESS. REPAIR PARTS INSTALLED USING 250 DEG F HOT BONDING PROCEDURES IAWSDR FDEA201501300394Seat Track · chafedCABIN STATION 1225 RBL 24.75. SEAT TRACK INBD FLANGE FOUND CHAFED MARK. CHAFE REMOVED IAW SRM 51-10-02 REV 113. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE I FIG 101 REV 113. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52 REPAIR I FIG 201 REV. 114. SDR FDEA201501300393Seat Track · chafedBS 1560 - 1580 RBL 24.75, SEAT TRACK CROWN. REMOVED IAW SRM 51-10-02 REV 113. REWORKED AREA, EVALUATED & FOUND MATERIAL LOSS OF 0.025 INCHES EXCEEDS CROWN LIMIT OF 0.020 INCHES IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 113. SEAT TRACK REMOVED BETWEEN SDR FDEA201501290365Skin Panel · chafedRIGHT WING INBD TE, MAIN FLAP NOSE SKIN LOWER FWD AREA, FOUND A CHAFE AT MF STA 260. REMOVED IAW SRM 51-10-02 REV 113 & FOUND OUT OF LIMITS IAW SRM 57-53-01 FIG 101 ALLOWABLE DAMAGE 1 REV 113. REPAIR CARRIED OUT IAW SRM 57-53-01 REPAIR 3 REV 114. EXAMINE THSDR FDEA201501290364Skin Panel · chafedLEFT WING INBD TE MAIN FLAP, OTBD PANEL UPPER SURFACE, FOUND CHAFE MARK 12 INCHES LONG FROM PANEL OTBD EDGE, 8 INCHES FROM PANEL LE. REMOVED, DRIED OUT USING 150 DEG F VACUUM PROCESS. REPAIR PARTS INSTALLED USING 250 DEG F HOT BONDING PROCEDURES IAW SRM 57-SDR FDEA201501270308Seat Track · chafedCABIN - STA 815 - 830 LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK CROWN CHAFE MARK REMOVED IAW SRM 51-10- 02 REV 113 REWORKED AREA EVALUATED AND FOUND MATERIAL LOSS OF 0.030", EXCEEDED CROWN LIMIT OF 0.20" IAW SRM 53-00-52 ALLOWABLE DAMAGE I FIG 101 RSDR FDEA201501270309Strap · crackedBS 365 - 377, LBL 24.75 STABILIZER STRAP FOUND CRACKED. R & R IAW DWG 141N5150 SHT 1 REV D. INSTALLED IAW SRM 51-40-02 REV 114 & EA F-5310-T0314639 PART 1. REPAIR IS MAJOR.SDR FDEA201501240284Skin · wornEMPENNAGE LT SIDE BS 1850 - 1870, THERE IS WEAR CAUSED BY THE LOWER HORIZONTAL STABILIZER TO BODY SEAL AT AFT LOWER PORTION OF THE STABILIZER CUT OUT. WEAR REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL VII REV 113. REPAIRED IAW SRM 53-80-01SDR FDEA201501210244Bulkhead · damagedNR 2 PYLON AFT BULKHEAD AFT LOWER FLANGE, FOUND TWO TOOL DAMAGE & TWO DRILLED HOLES. REPAIRED IAW EA. F-5450-T0314203 PT1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201501200237Skin · damagedFUSELAGE EXTERIOR SKIN NICKED & SCRATCHED AT BS 520 - 540, STRINGER 23 - 24R. NICKS AND SCRATCHES REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113. REPAIRED IAW EA F-5330-T0314821 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100.
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