N785FD
Service difficulty reports · 78
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 = 'N785FD' 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 = 'N785FD' 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 FDEA202608221217Seat Track · corrodedGALLEY AREA STA 360-370 RBL 50, SEAT TRACK HAS CORROSION COMPLIED WITH EA# F-5310-T0388291. MAJOR REPAIR.SDR FDEA202608201194Crease Beam · corrodedMAIN DECK FLOOR STRUCTURE CREASE BEAM PROFILE AT LBL 64 HAS CORROSION BETWEEN BODY STA 1040 AND BODY STA 1080. REPAIRED CREASE BEAM INBOARD CHRORD AT LBL 64 BETWEEN STA 1040 TO STA 1080 MAIN DECK FLOOR STRUCTURE IAW B757 SRM 53-00-13-2R FIG 201 SHEET 1 TO SDR FDEA202608181144Skin · dentedDENT AT R/H WING SLAT #9 UPPER TRAILING EDGE AT OSS 669. REPAIRED DENT ON RH WING SLAT #9 UPPER EDGE AT OSS 669 IAW B757 SRM 51-70-10-2R. MAJOR REPAIRSDR FDEA202608181143Skin · dentedLEFT WING INBD FLAP HAS TWO DENTS AT WS 177.50 ZONE 553. REPAIRED LT WING INBD FLAP PANEL IAW SRM 51-70-10-2R. MAJOR REPAIR.SDR FDEA202601210079Bulb · dimL1 OVERHEAD EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 REMOVED AND REPLACED 17 FAULTY BULBS AT THE L1 OVERHEAD EXIT SIGN AS PER ABOVE REF. OPS CHECK GOOD. (P/N OL3071BPEGPL) A/C OK FOR SERVICE.SDR FDEA202408241170Skin · ground damageDURING TOWING OF THE AIRCRAFT INTO THE HANGAR 8.2, TAIL LH SIDE OF FUSELAGE STA 1768.80 TO STA 1787.45 STRINGER 20L MADE CONTACT WITH THE TAIL STAND. ACCMPLISHED REPAIR IAW EA 757-5380-16-A3665 SECTION 48 - FUSELAGE STA 1768 TO STA 1787.5 S-19L TO S-20L LASDR FDEA202311221884Collar · shearedGUST LOCK BROKEN ON R1 ENTRY DOOR. VERIFIED HOLD-OPEN COLLAR NEEDS REPLACED BUT NIS AT GSO. R1 ENTRY OPEN & CLOSED SEVERAL TIMES REF FDX RELEASED FOR SERVICE PER MEL : 52-11-01-A. REMOVED AND REPLACED R1 DOOR GUST LOCK REF B757 AMM 52-11-08-4. OP CHECK GSDR FDEA202311161867Adapter · loosePDIS 785 27-10 7609 16NOV23 IND FACT U IN THE FLARE BELOW APPROXIMATELY 50 IT TOOK SIGNIFICANTLY MORE EFFORT THAN NORMAL TO MOVE THE CONTROL WHEEL LEFT OR RIGHT. THE RESISTANCE INCREASES SIGNIFICANTLY AFTER A SHORT AMOUNT OF CONTROL WHEEL TRSDR FDEA202301300179Battery · dischargedONE EMERGENCY LIGHT WILL NOT ILLUMINATE EXTERIOR OF L1 DOOR. DUE TO EXTENDED LAYOVER BATTERIES NEEDED TO BE CHARGED FOR OPS CHECK. PERFORMED ADJUSTMENT/TEST PER B757 AMM 33-51-00-5 WITH NO DEFECTS NOTED. AC OK FOR SERVICE.SDR FDEA202211012705Sensor · failedLE SLAT ASYM MESSAGE ON DEPARTURE BETWEEN FLAPS 1 AND UP. RAN QRH AND COMPLIED WITH CHECKLIST. DECLARED EMERGENCY AND RETURNED TO MCI. REST OF FLIGHT WAS UNEVENTFUL. EMERGENCY DECLARED AMM: 27-81-41-4 REMOVED AND REPLACED LOSS SENSING SWITCH FOR THE ISDR FDEA202210222643Fitting · corrodedLT WING PYLON DRAG LINK FITTING HAS CORROSION IN 5EA HOLES IN FITTING LAYER ONLY. HOLE NUMBERS 1,3,8,10, AND 15. COMPLIED WITH EA F-5730-T0370901 PT1 WINGS - PLATES AND SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS. THIS EA DEVIATES FROM EO F-5730-E034007SDR FDEA202210212636Floorbeam · crackedVIEW FROM FWD CARGO COMPT. MAIN CARGO FLOOR BEAM AT BS 580 LBL 45 HAS CRACK. REPAIRED FLOOR BEAM AT STA 580 LBL 45 IAW EA TF-5310-T0370825 PT1. FUSELAGE - MAINFRAME- FLOOR BEAM AT STA 580 AND LBL 45 CRACKED - REPAIR PER DRAWING SR57-53- 004. MAJOR REPAIRSDR FDEA202210212634Floor Support · corrodedMAIN DECK FLOOR FS1681. FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION EXFILIATED BETWEEN WEB AND FLOOR BEAM APPROX LBL12. REPAIRED MAIN DECK FLORO FS 1681 FLOOR BEAM UPPER CHORD, UPPER SECTION FROM LBL 3 TO LBL 20 IAW SRM 53-60-51-2R. CORROSION FOUND OUT OSDR FDEA202210212633Attach Fitting · corroded#2 ENGINE PYLON DRAG LINK ATTACHMENT FITTING HAS 8 HOLES WITH CORROSION. HOLES 2,3,5,7,10,14. AND 15 IN FITTING LAYER. HOLE 8 HAS CORROSION IN SKIN LAYER. COMPLIED WITH EA F-5730-T03700894 PT1 R/H WING UPPER SKIN AT DRAG FITTING CORROSION FINDINGS. THISSDR FDEA202210192623Floorboard · delaminatedZONE 20 FLOOR BOARD 222MAF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1638358 IAW DWG SRZ- 25-005 REV R. MAJOR REPAIRSDR FDEA202210192622Floorboard · delaminatedZONE 220 FLOOR BOARD 221MBF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1638356 IAW DWG SRZ-25-005 REV R. MAJOR REPAIRSDR FDEA202210192621Floorboard · delaminatedZONE 220 FLOOR BOARD 222AF IS DELIAMINATED FABRICATED ZONE 220 FLOOR BOARD 222AF ON VT MAE TRAVELER T22/1638359 IAW DWG SRZ- 25- 005 REV R. MAJOR REPAIRSDR FDEA202210192619Floorboard · delaminatedZONE 220 FLOOR BOARD 221AF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1638355 IAW DWG SRZ- 25- 005 REVISION R. MAJOR REPAIRSDR FDEA202207291807Slide · dislodgedDOOR WAS DISARMED AND NEW CALLOUT WAS MADE BUT SLIDE FELL OUT OF DOOR. SLIDE DID NOT DEPLOY. REMOVED AND INSTALLED NEDW R-1 DOOR SLIDE RFEF B757 AMM 25-66-01-4 GIRT BAR OPERATESSDR FDEA202205171225Gust Lock · damagedL1 DOOR GUST LOCK FOUND BROKEN ON POST FLIGHT. (REMOVED BROKEN COLLAR) INSTALLED NEW GUST LOCK TO L1 DOOR REFERENCE TO AMM 52-11-08-8. DOOR OPS CHECK GOOD TO AMM 52-11-08-8.SDR FDEA202203040417Bulb · failedMDIS 785 33-50 6302 04MAR22 EWR FACT U ON SERVICE CHECK FOUND LH EMERGENCY SLIDE LIGHT INOP. FACT 04MAR22 18:42 EWR U RELAMPED LH EMERGENCY SLIDE LIGHT AS PER 757 AMM 33-51-06-2-1. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.SDR FDEA202202220348Door · gougedMAIN CARGO DOOR IS GOUGED AND DENTED ON SKIN AT STA 599 REPAIRED REF 757 SRM 52-30-01-2R REPAIR 4 AND EA F-5230-T0367049SDR FDEA202012183189Cylinder · dischargedR1 DOOR EMERGENCY POWER RESERVOIR CYLINDER DISCHARGED. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR, REF B757 AMM 52-11-32-4.SDR FDEA2020062321650Vane · damagedDURING POST STORM WALKAROUND FOUND RT ENGINE RT THRUST REVERSER HALF AT 2 O'CLOCK POSITION L.E. DAMAGE APPX 16 INCHES X 9 INCHES. TEMP REPAIR PER EA F-7830-T0348334. COMPLIED WITH EA F-7830-T0348334 PT 1 INSTALLED RT ENGINE O/B SLEEVE IAW AMM 78-31-07-4, SDR FDEA2020061621650Cascade · damagedDURING POST STORM WALKAROUND FOUND RT ENGINE RT T/R HALF AT 2 O'CLOCK POSITION L.E. DAMAGE APPX 16 INCHES X 9 INCHES.SDR FDEA201609203316Frame · puncturedFRAME AT BS 231, BL 0 IS PUNCTURED. REPAIRED IAW EA F-5310-T0328373 P1.SDR FDEA201605251733Unknown · odorTHREE TIMES DURING FLIGHT WE SMELLED AN ACRID ELEC BURNING SMELL. NO SMOKE NOTED & UNABLE TO ISOLATE. FIRST OFFICER ALWAYS SMELLED IT FIRST. ALWAYS WENT AWAY IN 1 MIN. NO SMELL IN COURIER AREA. IAW FIM 21-00 PROC 4, SINCE FAULT CAN'T BE DUPLICATED & ALL ESDR FDEA201511253776Light · inoperativeR1 DOOR EXTERNAL SLIDE LIGHT INOPERATIVE. R & R R1 DOOR SLIDE LIGHT ASSEMBLY IAW MM 33-51-06-2-1. OPERATIONS CHECKED NORMAL.SDR FDEA201505011355Lamp · inoperativeDURING SERVICE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP. ALL OPS CHECKED NORMAL IAW AMM 33-51-06-2-1.SDR FDEA201410133133Doubler · scratchedFUSELAGE EXTERIOR SKIN, WHILE PERFORMING EA F-5330-T0308700PT1 FOUND DOUBLER HAS SCRATCHES AT STATION 1350 STRINGER 1 - 2R. SCRATCH ON DOUBLER CLEARED & TREATED IAW SRM 51-10-02 REV 112 & SRM 51-20-01 REV 112. FOUND NO SIGNIFICANT MATERIAL LOST. PART 1 OF ESDR FDEA201410103075Skin · dentedFUSELAGE SKIN HAS A DENT BS 1701 - 1720 STRINGER 28 - 30R. REPAIRED IAW EA F5330-T0310832. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201410083010Floorbeam · corrodedBS 377.7 LBL 55 - 60 FLOORBEAM UPPER TEE FOUND CORROED ON LOWER SURFACE. FLOORBEAM TEE REMOVED AND REPLACED IAW DWG 141N5113 SHT 1 REV F. DWG 141N5123 SHT 1 REV A AND EA F-5310-T0311051 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201410072997Skin · damagedFUSELAGE SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26L & 26R BETWEEN BS 1701 - 1720. DAMAGE REMOVED AND TREATED IAW SRM 51-10-02 REV 112. FOUND ONE SPOT OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112, REPAIRED OUT OF LISDR FDEA201410022892Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1654 STRINGER 28 - 29L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 AND SRM 51-20-01 REV 112, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARSDR FDEA201410022891Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1622 STRINGER 27 - 28L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. PART 1SDR FDEA201410022890Skin · damagedFUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1627 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 11 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CASDR FDEA201410022889Skin · damagedFUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1630 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIRSDR FDEA201410022888Skin · damagedFUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1653 STRINGER 28 - 29L. DAMAGE REMOVED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARRIED OUT IAW ESDR FDEA201410022913Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1581 STRINGER 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201410022912Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1576 STRINGER 27 - 28L. BLENDED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201410022914Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1571 STRINGERS 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201410012879Frame Splice · gougedAFT CARGO BAY BS 1520 STRINGER 24 - 25R, FRAME SPLICE FOUND DAMAGED. REMOVED AND REPLACED IAW SNRM N04012. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201409282844Skin · damagedMULTIPLE TOOL DAMAGE ON THE INTERIOR SKIN AT BS 1420 - 1423, STRINGER 25L - 26L. REPAIRED IAW EA F-5330-T0311215 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201409262791Frame · gougedAFT CARGO BAY FRAME BS 1360 STRINGER 23 - 24L OUTER FLANGE GOUGED. REPAIRED IAW EA F5310-T0311806 P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201409262793Skin · crackedTHERE IS A CRACK AT FWD CARGO DOOR EXTERIOR SKIN AT LOWER AFT CORNER BS 600 - 620 STRINGER 25 - 26R. REPAIRED IAW EA F-5230-T0311723. REPAIR CLASSIFED AS MAJOR.SDR FDEA201409252761Skin · crackedL4 DOOR INTERNAL HANDLE BOX CUT OUT AFT EDGE INNER SKIN FOUND CRACKED AT EDGE. REPAIRD IAW EA F-5210-T0311310 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201409232722Skin · gougedEXISTING REPAIR FINDING FUSELAGE THERE IS GOUGE ON THE INTERIOR SURFACE OF THE DOUBLER OF THE EXISTING REPAIR AT STATION 1350 STRINGER 29L - 28R. REMOVED BY HAND CLEAN & TREATED PER SRM 51-10-01 REV 112 AND SRM 51-20-01 REV 112. NEW REPAIR CARRIED OUT PER FSDR FDEA201409232711Frame · corrodedAFT CARGO COMPARTMENT STATION 1380 RBL 10 FRAME UPPER CHORD FOUND CORROSION DURING REMOVING CORROSION AT FRAME FLANGE IAW SNRM N03563.
COMPLIED AS PER EA F-5310-T0311624 P1 TITLE: FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FSDR FDEA201409232709Frame · corrodedAFT CARGO COMPARTMENT STATION 1380 BL0 - RBL 15 FRAME FLANGE HAS CORROSION. COMPLIED AS PER EA F-5310 - T0311624 PT 1. TITLE : FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FLANGE OF STA 1380 146N1028-88 BOTTOM FRAME AND 146N8511SDR FDEA201409182654Skin · gougedGOUGES ON EXTERIOR SURFACE OF THE REPAIR DOUBLER BS 1701 - 1720 STRINGERS 28 - 30R. REPAIRED IAW EA F-5330-T0310832. REPAIR CLASSIFIED AS MAJOR.
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