N784FD
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 = 'N784FD' 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 = 'N784FD' 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 FDEA202212222988Floor Panel · delaminatedMAIN CABIN - FLOOR PANEL 231MKF IS DAMAGED EVALUATED DAMAGE TO PANEL 231MKF AND FOUND 1EA PUNCTURE, REPAIRED PANEL IAW B757 SRM 53-00-50-1A AND SRM 53-00-50-2RSDR FDEA202212222987Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 221AF IS DELAMINATED FABRICATED NEW FLOOR PANEL 221AF IAW SRZ 25-005 REV: RSDR FDEA202212212983Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222AF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222AF IAW FEDEX SRZ 25-005 REV: R AND GMM 07-0-1001.SDR FDEA202212212982Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222BF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222BF IAW FEDEX SRZ 25-005 REV: R AND GMM: 07-0-1001SDR FDEA202212202974Structure · corrodedRIGHT SIDE CABIN, STATION 960 TO 1019 RBL63 FLOOR STRUCTURE HAS SEVERAL FASTENER HOLES WITH CORROSION REMOVED CORROSION FROM CREASE BEAM I/B CHORD FROM STA 960 TO 1019, RBL 63, AND FOUND TO BE OUT OF LIMITS IAW B757 SRM 51-10-02-0G AND 53-40-13-1A, FIG.10SDR FDEA202212202973Structure · corrodedLEFT SIDE CABIN - STATION 960 TO 1019 LBL63 FLOOR STRUCTURE HAS SEVERAL FASTENER HOLES WITH CORROSION REMOVED CORROSION FROM CREASE BEAM I/B CHORD FROM STA 960 TO 1019, LBL 63 AND FOUND TO BE OUT OF LIMITS IAW B757 SRM 51-10-02-0G AND 53-40-13-1A, FIG 101SDR FDEA202212202971Floor Support · corrodedMAIN CABIN STA 640-660 LBL44, UNDER FLOOR PANEL, FLOOR SUPPORT CORRODED REMOVED, FABRICATED AND INSTALLED SUPPORT STRAP AND FILLER IAW VA DWG 3459 AND DWG 3458 REV L. ORIG SUBMISSION DATE: 12/20/2022SDR FDEA202212202975Crease Beam · corrodedMAIN CABIN STA 860 RBL 64 CUSP CHORD CORRODED REPAIRED CREASE BEAM IAW B757 SRM 53-00-13-2R. ORIG SUBMISSION DATE: 12/20/2022SDR FDEA202212202972Seat Track · corrodedMAIN CABIN BS 1206 LBL46 SEAT TRACK OB FLANGE CORRODED. REMOVED AND REPLACED SEAT TRACK FROM BS 1180-1320 IAW DWG 146N5133, REV -, & DWG 146N5120 REV A.SDR FDEA202212202958Angle · chafedLH UPPEREXT FUSELAGE (ZONE 48), SKATE ANGLE AFT EDGE HAS CHAFING WEAR, AFT OF BS 1787 LH SKATE ANGLE REMOVED AND REPLACED IAW BLUEPRINT 148N3101 REV -SDR FDEA202212172934Intercostal · corrodedAFT PIT BILGE AREA INTERCOASTAL LOWER FLANGE UPPER SURFACE HAS CORROSION FROM APPROX STA 1330-1340 LBL11 REMOVED AND REPLACED INTERCOASTAL AT AFT PIT BILGE AREA AT STA 1320 TO STA 1340 IAW B757 SRM 51-40-02 AND BAC DWG 146N5398 REV: B. ORIG SUB DATE: 12/23/SDR FDEA202212172940Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 221MBF IS DELAMINATED FABRICATED NEW FLOOR PANEL 221MBF IAW FEDEX DWG SRZ-25-005 REV R.SDR FDEA202212172939Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MDF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222MDF IAW FEDEX DWG SRZ-25-005 REV RSDR FDEA202212172938Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MBF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222MBF IAW FEDEX DWG SRZ-25-005 REV R.SDR FDEA202212172937Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 221MAF IS DELAMINATED FABRICATED NEW FLOOR PANEL 221MAF IAW DWG SRZ-25-005 REV R.SDR FDEA202212172936Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MAF IS DELAMINATED FABRICATED NEW FLOOR PANEL 222MAF IAW FEDEX DWG SRZ-25-005 REV RSDR FDEA202212172935Floor Panel · delaminatedCOURIER AREA - FLOOR PANEL 222MEF DELAMINATED. FABRICATED NEW FLOOR PANEL 222MEF IAW FEDEX DWG SRZ-25-005 REV R.SDR FDEA202212162933Handle · crackedFWD PIT CARGO DOOR EXTERIOR HANDLE IS CRACKED ON LOWER EDGE REMOVED AND REPLACED PER DWG 140N2789.SDR FDEA202212162932Spring Assy · cracked#2 PYLON R/H SIDE HYDRAULIC BAY FWD CLIP IS CRACKED ON LOWER LONGERON REMOVED AND REPLACED PER BOEING DWG #313N3053 REV BSDR FDEA202212152916Cover Plate · bentINTERNAL FUSELAGE ABOVE WING CENTER SECTION UNDER MAIN CARGO FLOOR HAS LOOSE AND BENT FLOOR SUPPORT AT BS1020 RBL24.75-45.50 REMOVED, FABRICATED AND INSTALLED NEW COVER PLATE ON FLOOR SUPPORT IAW B757 DWG 114N5081 REV C AND DWG 114N5070 REV B.SDR FDEA202212152915Floor Support · damagedINTERNAL FUSELAGE ABOVE WING CENTER SECTION BELOW MAIN CARGO FLOOR HAS A DENT AND A CRACK ON FLOOR SUPPORT AT STA 900 LBL 24.75 REMOVED - FABRICATED AND INSTALLED NEW COVER PLATE ON FLOOR SUPPORT IAW DWG# 114N5081 REV C AND DWG 114N5070 REV ESDR FDEA202212142909Rack · crackedE3-2 SHELF, SIDERAIL IS CRACKED AT ATTACHMENT HOLE REPAIRED E3-2 SHELF SIDERAIL ATTACHMENT HOLE IAW FEDEX DRAWING NUMBER SRZ-53-007, REV -.SDR FDEA202212142908Rack · crackedE2-3 SHELF, SIDERAIL IS CRACKED AT ATTACHMENT HOLE REPAIRED E2-3 SHELF SIDERAIL ATTACHMENT HOLE IAW FEDEX DRAWING NUMBER SRZ-53-007, REV-.SDR FDEA202212092898Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP UPPER SKIN IS DELAMINATED. REPAIRED RIGHT WING OUTBOARD AFT FLAP UPPER SKIN IAW B757 SRM 57-53-01-2R REPAIR 1 FIG. 201 AND 51-70- 05-0G.SDR FDEA202210122752Light · failedON FINAL APPROCH WE SELECTED THE GEAR DOWN. RECEIVED 2 GREEN MAIN GEAR LIGHTS AND THE NOSE GEAR LIGHT REMAINED DARK. PRESSED TO TEST THE NOSE GEAR LIGHT AND HALF OF IT LIT UP GREEN. THIS LED TO THE GEAR DISAGREE CHECKLIST AND MANUALLY LOWERED THE GEAR. DSDR FDEA202210122557None · noneON FINAL APPROCH WE SELECTED THE GEAR DOWN. WE RECEIVED 2 GREEN MAIN GEAR LIGHTS AND THE NOSE GEAR LIGHT REMAINED DARK. I PRESSED TO TEST THE NOSE GEAR LIGHT AND HALF OF IT LIT UP GREEN. THIS LED US TO THE GEAR DISAGREE CHECKLIST AND WE MANUALLY LOWERED TSDR FDEA202110282651Transmitter · malfunctionedUPON INITIAL CONFIGURATION (FLAPS COMMANDED TO 1) FOR LANDING, TE FLAP ASYM CAUTION. DECLARED EMERGENCY AND LANDED WITH FLAPS UP PER QRH AT KAFW. DID A FSEU BITE AND FOUND FAULT CODE 315. PER FIM 27-51 FT805 DIRECTED TO SHEET 7 ITEM10 ,FOUND TURQUE TUBES SDR FDEA202101300237Pseu · fault messageLOG PAGES 354934 AFTER TAKEOFF AND RAISING THE GEAR LEVER, GEAR DISAGREE ON EICAS WITH RIGHT GEAR DOOR LIGHT ILLUMINATED. ACCOMPLISHED BIT TEST TO RETRIEVE HISTORY FROM INSTALLED PSEU SERIAL NUMBER 874. RETRIEVED FAULT CODES 065 AND 078 FOR SYSTEM 1 AND SYSTSDR FDEA202011132838Structure · brokenRT WING NR 8 NSLAT LOWER CORNER BROKEN, MISSING CORNER. REPAIRED IAW B757 SRM 57-43-01-2R AND SRM 51-70-07-0G.SDR FDEA202011082798Floor Support · corrodedMAIN CABIN FLOORBOARD INTERCOSTAL IS CORRODED AT 2 FASTENER HOLES BS 1689-BS 1695 BL 0. REMOVED AND REPLACED INTERCOSTAL AND INTERCOSTAL STRAP, IAW B757 SRM 51-40-02, BOEING DWG: 146N5230 REV: -, B757 SRM 51-20-01.SDR FDEA202011072787Skin · corrodedEXTERIOR FUSELAGE SKIN HAS EVIDENCE OF CORROSION AND BULGED SKIN AT SPLICE ARE BS 1455-BS 1462 STR 30-STR 28R. REMOVED FASTENERS AT STA 1459 STR 28R TO 28L AND 1 EA SHEAR TIE AT STA 1459 STR 30-29R, IAW B757 SRM 51-40-02. REMOVED 1 EA SHEAR TIE STA 1459 STR SDR FDEA202011062786Panel · debondedE&E COMPARTMENT AFT OF NOSE GEAR THE P32 PANEL RIGHT DOOR UPPER RIGHT CORNER IS DISBONDED. REMOVED EDGE DAMAGE, IAW EA F-2500-T0357818 P1 FIG1, MATERIAL ID FOR ADHESIVE BMS5-92 TY1, IAW EA F-2500-T0357818 P1 & B757-200 SRM 51-70-10-2R REPAIR 1 PARA 3D. MIXEDSDR FDEA202011052785Seat Track · corrodedMAIN CABIN SUPERNUMERARY LT SEAT TRACK UPPER SURFACE CORRODED MAIN CABIN SUPERNUMERARY LT SEAT TRACK CORROSION FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIGURE 101 DETAIL 1. REMOVED SEAT TRACK, IAW B757 SRM 51-40-02. FABRICATED NEW SEAT TRACK, IAWSDR FDEA202011052784Rub Strip · crackedR1 DOOR OPENING CENTER GUIDE FITTING RUBSTRIP IS CRACKED. REPLACED CENTERING GUIDE, IAW B757 SRM 51-40-02-0G AND DWG 141N8412 REV G.SDR FDEA202011052774Door · corrodedBELOW L2 DOOR THE LAV SERVICE DOOR DOUBLER IS CORRODED. REMOVED CORROSION, IAW B757 CPM 20-40-00, MATERIAL REMOVED .002 FROM .071, EVALUATED AREA FOUND TO BE LESS THAN 10% WITHIN LIMITS, IAW B757 SRM 53-00-01-1A. ALODINED AREA, IAW B757 SRM 51-20-01-OG. PRISDR FDEA202011042773Skin · corrodedEXTERIOR FUSELAGE UPPER ADF ANTENNA AREA STA 1116 HAS LIGHT PITTING. REMOVED CORROSION PITTING ORIGINAL MATERIAL .110, REMOVED .010, .100 REMAINING FOUND TO BE WITHIN LIMITS, IAW B757 SRM 53-00-01-1A. APPLIED CLEAR 1001 ALODINE, IAW B757 AMM 51-21-04-7.SDR FDEA202011042771Hinge · corrodedG1A GALLEY COMPARTMENT 102 DOOR HINGE CORRODED. ACCOMPLISHED FEDEX EA MF-2530-T0357769 EQUIP AND FURNISH G1A GALLEY DOOR HINGE, CORROSION DAMAGE.SDR FDEA202011032763Skin · damagedRT WING FIXED LEADING EDGE SKIN UPPER SURFACE HAS FASTENERS PULING THROUGH APPROXIMATELY 2' OUTBOARD OF THE PYLON. REMOVED LEADING EDGE SKIN AND ACCOMPLISHED SRM REPAIR 57-41-01-2R, REINSTALLED REPAIRED SKIN.SDR FDEA202011032762Skin · delaminatedRT WING FIXED LEADING EDGE SKIN UPPER SURFACE IS DELAMINATED APPROXIMATELY 2.5' OUTBOARD OF THE PYLON. REMOVED LEADING EDGE SKIN AND ACCOMPLISHED SRM REPAIR 57-41-01-2R, REINSTALLED REPAIRED SKIN.SDR FDEA202011032760Panel · dentedVERTICAL STAB LEFT SIDE PANEL 322DL HAS DENT REPAIRED VERTICAL STABILIZER LEFT SIDE PANEL 322DL BY BONDING REPAIR PLIES, IAW B757 SRM 55-30-01-0I FIG 1 AND 55-30-01-2R REPAIR 4 FIG 201 AND 51-70-06 PARA 5 A FIGURE 5 AND REPAIR GENERAL. APPLIED FINISH, IAW B7SDR FDEA202010312733Support Angle · crackedNR 2 PYLON UNDER PANEL NR 445CL SUPPORT ANGLE IS CRACK AT NAC 204 APPROXIMATELY. REMOVED AND REPLACED SUPPORT ANGLE AT NR 2 PYLON, IAW FEDEX B757 DWG 313N3052 REV B AND SRM 51-40-02-0G.SDR FDEA202010312732Skin · dentedLEFT HORIZONTAL STABILIZER LOWER SKIN BETWEEN AUX SPAR AND FRONT SPAR HAS A DENT. REPAIRED DENT, IAW B757 SRM 55-10-01-1A AND 51-70-10-2R.SDR FDEA202010302720Plate · crackedRT WING,OUTBOARD FLAP TRACK FAIRING 673CB SPACER PLATE IS CRACKED LOCATED ON TOP OF THE INBOARD BLADE SEAL RETAINER STRIP. REMOVED AND REPLACED SPACER PLATE AT RT WING OUTBOARD FLAP INBOARD TRACK FAIRING 673CB, IAW FEDEX B757 DWG 113N3131 REV A.SDR FDEA202010292712Bracket · crackedNR 1 ENGINE, INBOARD CORE COWL, LOWER FORWARD BRACKET CRACKED. REMOVED AND REPLACED BRACKET, PER DWG 314N3210 REV H AND B757 SRM 51-40-02.SDR FDEA202010252651Floorboard · corrodedMAIN CABIN FLOOR BOARD STRUCTURE IS CORRODED AT 2 FASTENER HOLES BS 1688.5-BS 1695 RBL 56. REMOVED 3 EA NUTPLATES. BLENDED AREA FREE OF CORROSION. ORIG MATERIAL .071 REMOVED .008 REMAINING .063 WITHIN LIMITS, IAW B757 SRM 53-60-15 AND 51-10-02. ALODINED ASDR FDEA201812123494Proximity Switch · inoperativeSLIDE ARMED LIGHT FOR R1 DOOR INOP. REMOVED AND REPLACED R1 GIRT BAR PROX SWITCHES S10216 AND S10217. INSTALLED MPN 8102-0401FS SWITCHES. PER MM 25-66-11-2. SEE PREVIOUS UPDATE FOR WIRING TERMINATION OF NEW SWITCHES. REINSTALLED DOORWAY LINING PANELS REF MM1 2SDR FDEA2018102653011Flap · gougedAIRCRAFT DAMAGE-RT I/B FLAP HAS A PUNCTURE ON LOWER SURFACE AFT OF AFT TRUNNION FAIRING. REPAIRED RT I/B FLAP PUNCTURE ON LOWER SURFACE AFT OF AFT TRUNNION FAIRING IAW SRM 51-70-17-OG PARA 3G & FIG 5 AND EA WORK CARD T F-5750-T0343144 P1. WING-FLIGHT SURFACES-SDR FDEA201810172934Skin · gougedLT INBD FWD FLAP UNDERSIDE OUTER SKIN HAS A DENT WITH A SMALL GOUGE AT WS 205. REPAIRED LT INBD FWD FLAP UNDERSIDE OUTER SKIN DENT WITH GOUGE AT WS 205 IAW SRM 51-70-10-2R PARA 20 AND EA WORK CARD T F-5750-T0343012 P1 WING- FLIGHT SURFACES- LT INBOARD MAIN FLSDR FDEA201807051631Lock · lack of lubeR1 DOOR GIRT BAR ESCAPE SLIDE ENGAGEMENT ARM LIGHT WILL NOT ILLUMINATE. REMOVED GIRT BAR LOCKS, CLEANED AND LUBED LOCKS AND FLOOR FITTINGS. REINSTALLED GIRT BAR LOCKS AND ENGAGED GIRT BAR ASSY. R1 DOOR SLIDE ARMS NORMAL WITH NORMAL INDICATION. REF MM 25-66-01SDR FDEA201704051076Crank Assy · inoperativeSLIDE ARMED LIGHT ILLUMINATED FOR THE RIGHT ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED LOWER ACTUATOR CRANK ASSEMBLY IAW CMM 52-11-05. ACCOMPLISHED OPS CHECK IAW 52-11-25-5. OPS CHECKED OK.
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