# Service difficulty reports: N850FD

A list on [N850FD](https://openairdocs.org/aircraft/N850FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA202607120916](https://openairdocs.org/sdr/FDEA202607120916.md): Light Sys · malfunctioned · Jul 12, 2026 · N850FD · Boeing 777FS2 · Emergency Lighting
  > CHECK FOUND WHEN THE OVERHEAD PANEL EMER LIGHTS SWITCH IN "ON" POSITION, THE EMERGENCY LIGHTS NOT ILLUMINATED. AMM: 33-51-00-5 RESET THE CB'S AND PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE CONTROL SWITCH ON THE OVERHEAD PANEL REF AMM33-51-00
- [SDR FDEA202505160761](https://openairdocs.org/sdr/FDEA202505160761.md): Floor Panel · delaminated · May 16, 2025 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > REWORK:MAIN DECK CARGO COMPARTMENT AT STA 1940 FOUND CENTER FLOOR PANEL UPPER SURFACE HAVE SIGN OF DELAMINATED CONDITION. MEASURED MAIN DECK CARGO COMPARTMENT AT STA 1940 CENTER FLOOR PANEL UPPER SURFAE DELAMINATED DAMAGE SIZE LXW=4"X2.5" OUT OF ALLOWABL
- [SDR FDEA202505010696](https://openairdocs.org/sdr/FDEA202505010696.md): Skin · cracked · May 1, 2025 · N850FD · Boeing 777FS2 · Wing, Plate/Skin
  > OPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE 01EA CRACK AS MARKED REPAIRED AS PER B777 SRM 51- 40-05-0G,51-40-02-0G,51-40-04-0G REV47.5 AND EA G-5730-T0383099A P1 TITLE
- [SDR FDEA202504240638](https://openairdocs.org/sdr/FDEA202504240638.md): Skin · dented · Apr 24, 2025 · N850FD · Boeing 777FS2 · Spoilers
  > FOUND LH WING OB FLAP LOWER SURFACE A DENT AT 226 INCH FROM IB SIDE CROSS 8 INCH FROM AFT SIDE. REPAIRED LH WING OB FLAP LOWER SURFACE A DENT AT 226 INCH FROM IB SIDE CROSS 8 INCH FROM AFT SIDE AS PER B777 SRM 57-53-01-2R-2 AND SRM 51-70-04-2R-1 REV 47.5 A
- [SDR FDEA202504240636](https://openairdocs.org/sdr/FDEA202504240636.md): Skin · dented · Apr 24, 2025 · N850FD · Boeing 777F · Trailing Edge Flaps
  > FOUND LH WING OB FLAP LOWER SURFACE A DENT AT 198 INCH FROM IB SIDE CROSS 15 INCH FROM AFT SIDE. REPAIRED LH WING OB FLAP LOWER SURFACE A DENT AT 198 INCH FROM IB SIDE CROSS 15 INCH FROM AFT SIDE AS PER B777 SRM 57-53-01-2R-2 AND SRM 51-70-04-2R-1 REV 47.5
- [SDR FDEA202504230629](https://openairdocs.org/sdr/FDEA202504230629.md): Skin · cracked · Apr 23, 2025 · N850FD · Boeing 777F · Wing, Plate/Skin
  > OPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 02EA CRACKS AS MARKED. RH WING UPPER SKIN WBL262 #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-50-02-0G, 51-40-02-0G, 51-10-01-0G, 51-20-06-0G, 51-40-05-0G, 51-40-08-0G, 51-20-
- [SDR FDEA202504230628](https://openairdocs.org/sdr/FDEA202504230628.md): Skin · bulged · Apr 23, 2025 · N850FD · Boeing 777F · Leading Edge Devices
  > RH WING OB NO.12 SLAT OUTER SKIN FOUND BULGE AT 68 INCHES TO OB EDGE. RH WING OB NO.12 SLAT OUTER SKIN AT 68 INCHES TO OB EDGE BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIGURE 202 REV:47.5 AND EA G-5750-T0383124 P1. TITLE: WING- FLIGHT SURF
- [SDR FDEA202504070586](https://openairdocs.org/sdr/FDEA202504070586.md): Hydraulic Line · leaking · Apr 7, 2025 · N850FD · Boeing 777F · Hydraulic System, Main
  > LOST ALL CENTER HYDRAULIC FLUID SHORTLY AFTER AIRBORNE. EICAS MSSG HYD PRESS SYS C APPEARED AFTER RAISING LANDING GEAR HANDLE. REMOVED AND REPLACED ELEVATOR RETURN LINE P/N # 272W8290-82 REF B777 AMM 20-11-10-2, SERVICED CENTER HYD SYSTEM REF B777 AMM
- [SDR FDEA202303300527](https://openairdocs.org/sdr/FDEA202303300527.md): Pdu · unknown · Mar 30, 2023 · N850FD · Boeing 777FS2 · Leading Edge Slat Control System
  > EICAS FLAP DRIVE ALERT ON DEPARTURE AFTER SELECTING FLAPS UP. ECL PROCEDURES ACCOMPLISHED. RTB MEM. EMERGENCY DECLARED & CANCELED AFTER LANDING. EMERGENCY DECLARED. ALL WORK ACCOMPLISHED UNDER THE FOLLOWING WRI'S; 27-50/4918, 4919, 4920, 4921, 4925 &
- [SDR FDEA202303190469](https://openairdocs.org/sdr/FDEA202303190469.md): Pdu · faulted · Mar 19, 2023 · N850FD · Boeing 777FS2 · Trailing Edge Flap Control System
  > FLAPS DRIVE EICAS AFTER TAKEOFF. REF TSI 27-80/4883, PUT THE AIR/GROUND SYSTEM IN THE AIR MODE. PERFORMED STEP 7, OPS FLAPS WHEN FSEU #2 IN CONTROL, ALL OPS SATISFIED. OPS FLAPS WHEN FSEU #1 IN CONTROL, MX MSG 27-20391 LATCHED WITH STATUS MSG FLAP/SLAT CON
- [SDR FDEA202303150428](https://openairdocs.org/sdr/FDEA202303150428.md): Light · failed · Mar 15, 2023 · N850FD · Boeing 777FS2 · Emergency Lighting
  > FLT CREW PRE-FLT CK REPORTED, L1 DOOR FWD EMER EXIT SIGN INDICATOR ALL OF LIGHTS INOP. ENT BY:3711964 RPT BY:3711964 R&R'D LIGHT ASSY PER MM 33-51-01-2. LIGHT F/C AND EMER LT TEST PASS. A/C OK FOR SVC. (P/N; 702409-1001) ENT BY:3711964 RPT BY:3711964
- [SDR FDEA202209052204](https://openairdocs.org/sdr/FDEA202209052204.md): Skin · damaged · Sep 5, 2022 · N850FD · Boeing 777FS2 · Wing, Plate/Skin
  > DURING PERFORMING E G-5710-E0366409 P 7 STEP7.A.(10), FOUND 02 EA HOLES OVERSIZED (DIAMETER:0.6245") ON THE SKIN AND LONGERON(P/N:140W9255Y407) AT STA993-1035 STGR 35-37 LH. THE BOEING DRAWING 675W0002 SH7 VIEW 2B6-7 CALL OUT THE DIAMETER 0.5620". THE 02
- [SDR FDEA202208302105](https://openairdocs.org/sdr/FDEA202208302105.md): Floor Panel · none · Aug 30, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 TO STA 1790 (MPN# 152W8602-20) UNDER SIDE GUIDE ASSY FOUND DENT. REPAIRED MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 TO STA 1790 (MPN# 152W8602-20) UNDER SIDE GUIDE ASSY DENT AS PER B777 SRM 53-00-50-2R REPAIR 1
- [SDR FDEA202208302104](https://openairdocs.org/sdr/FDEA202208302104.md): Floor Panel · none · Aug 30, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 TO STA 1790 (MPN# 152W8602-14) UNDER SIDE GUIDE ASSY FOUND DENT. REPAIRED MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 TO STA 1790 (MPN# 152W8602-14) UNDER SIDE GUIDE ASSY DENT AS PER B777 SRM 53-00-50-2R REPAIR 1
- [SDR FDEA202208302103](https://openairdocs.org/sdr/FDEA202208302103.md): Floor Panel · none · Aug 30, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1664 TO STA 2046 (MPN# 152W8601-19) UNDER CENTERLINE RESTRAINT FOUND DENT. REPAIRED MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1664 TO STA 2046 (MPN# 152W8601-19) UNDER CENTERLINE RESTRAINT DENT AS PER B777 SRM 53-00-5
- [SDR FDEA202208302102](https://openairdocs.org/sdr/FDEA202208302102.md): Floor Panel · none · Aug 30, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL AT LH STA 1476 TO STA 1580 (MPN# 152W8602-13) UNDER SIDE GUIDE ASSY FOUND DENT. REPAIRED MAIN DECK FLOOR PANEL AT LH STA 1476 TO STA 1580 ( MPN# 152W8602-13) UNDER SIDE GUIDE ASSY DENT AS PER B777 SRM 53-00-50-2R REPAIR 1 R
- [SDR FDEA202208232031](https://openairdocs.org/sdr/FDEA202208232031.md): Floor Panel · none · Aug 23, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANELS AT LH STA 1476 TO STA 1580 (MPN# 152W8602-7) UNDER SIDE GUIDE ASSY AREA FOUND DENTS. REPAIRED MAIN DECK CARGO FLOOR PANELS AT LH STA 1476 TO STA 1580 ( MPN# 152W8602-7) UNDER SIDE GUIDE ASSY AREA DENTS AS PER B777 SRM 53-00
- [SDR FDEA202208232030](https://openairdocs.org/sdr/FDEA202208232030.md): Floor Panel · none · Aug 23, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANELS BETWEEN STA 1664 TO STA 2046 (MPN# 152W8601-31) UNDER CENTERLINE RESTRAINT AREA FOUND DENTS. REPAIRED MAIN DECK CARGO FLOOR PANELS BETWEEN STA 1664 TO STA 2046 (MPN# 152W8601- 31) UNDER CENTERLINE RESTRAINT AREA DENTS AS PER B
- [SDR FDEA202208232029](https://openairdocs.org/sdr/FDEA202208232029.md): Floor Panel · none · Aug 23, 2022 · N850FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANELS AT RH STA 1476 TO STA 1790 (MPN# 152W8602-8) UNDER SIDE GUIDE ASSY AREA FOUND DENTS. REPAIRED MAIN DECK CARGO FLOOR PANELS AT RH STA 1476 TO STA 1790 (MPN# 152W8602-8) UNDER SIDE GUIDE ASSY AREA DENTS AS PER B777 SRM 53-00-50-2
- [SDR FDEA202103130629](https://openairdocs.org/sdr/FDEA202103130629.md): Actuator · malfunctioned · Mar 13, 2021 · N850FD · Boeing 777FS2 · Aileron Control System
  > AILERON ACTUATOR REMOVED AND REPLACED RT O/B AILERON ACTUATOR REF AMM 27-11-11-4 UP TO AND INCLUDING STEP 3. H. (7). STILL REQUIRES OPS CHECK. RIG CHECK GOOD,ALL TESTS PASS, NO LEAKS NOTED, OF RIGHT HAND OTBD AILERON ACTUATOR REF BOEING 777 AMM 27-11
- [SDR FDEA202010302719](https://openairdocs.org/sdr/FDEA202010302719.md): Lamp · inoperative · Oct 30, 2020 · N850FD · Boeing 777FS2 · Emergency Lighting
  > POST-FLT INSPECTION, R-1 OVERHEAD EMERGENCY LIGHT INOPERABLE ON LIGHTS TEST. RE-LAMPED, REF B777 AMM: 33-51-03-2. EMERGENCY LIGHTS TEST SATISFACTORY. ITEM OK FOR SERVICE.
- [SDR FDEA202001020002](https://openairdocs.org/sdr/FDEA202001020002.md): Skin · cracked · Jan 2, 2020 · N850FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF HFEC INSPECTION ON FUSELAGE SKIN OF LEFT HAND UNDERWING LONGERON FOUND 02 EACH CRACKS INDICATION AT STATION 1024 AND STATION 1035 STRINGER 37 LEFT. APPROXIMATELY 2.0" IN LENGTH EACH, AS MARKED. FUSELAGE SKIN LEFT HAND UNDERWING LONGE
- [SDR FDEA201912233282](https://openairdocs.org/sdr/FDEA201912233282.md): Skin · cracked · Dec 23, 2019 · N850FD · Boeing 777FS2 · Fuselage Main, Plate/Skin
  > HFEC SURFACE INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE OF THE FUSELAGE SKIN COMMON TO THE UNDERWING LONGERON WITHIN A 2 INCHES RADIUS OF THE FASTENER HOLES FOUND CRACK APPROXIMATE 1/2" AT STATION 1027 STRINGER 37 RIGHT. FUSELAGE SKIN UNDERWING LONGERON WI
- [SDR FDEA2019122093263](https://openairdocs.org/sdr/FDEA2019122093263.md): Floor Support · cracked · Dec 19, 2019 · N850FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1980.5 RBL 40 FOUND CRACKED. REFER SNRM N00384 FOR WORK DETAIL CARRIED OUT AT BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER SECTION REPAIR (STATION 1980.5 RBL 40) FROM STATION 1925 TO STATION
- [SDR FDEA2019122093262](https://openairdocs.org/sdr/FDEA2019122093262.md): Floor Support · cracked · Dec 19, 2019 · N850FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER STATION 1937 RBL 16 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER STATION 1937 RBL 16 SECTION STRINGER REPAIR CARRIED OUT AT BULK CARGO COMPARTMENT AT STATION 1928 AND STATION 1967 RBL 16 AS PER SRM
- [SDR FDEA2019122093261](https://openairdocs.org/sdr/FDEA2019122093261.md): Floor Support · cracked · Dec 19, 2019 · N850FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1931 RBL 40 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER AT STATION 1931 RBL 40 SECTION STRINGER REPAIR CARRIED OUT AT BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT AREA AT STATION
- [SDR FDEA201912193260](https://openairdocs.org/sdr/FDEA201912193260.md): Floor Support · cracked · Dec 19, 2019 · N850FD · Boeing 777FS2 · Fuselage Main, Structure
  > BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1958 RBL 49.8 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1958 RBL 49.8 SECTION STRINGER REPAIR CARRIED OUT AT BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT AREA AT STATI
- [SDR FDEA201912173255](https://openairdocs.org/sdr/FDEA201912173255.md): Structure · cracked · Dec 17, 2019 · N850FD · Boeing 777FS2 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON RIGHT HAND UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATION ON FRONT SPAR LOWER CHORD, LOWER ROW OUTBOARD FASTENER HOLE AND MIDDLE FASTENER HOLE. RIGHT HAND UNDERWING
- [SDR FDEA201912173254](https://openairdocs.org/sdr/FDEA201912173254.md): Longeron · cracked · Dec 17, 2019 · N850FD · Boeing 777FS2 · Fuselage Main, Longeron/Stringer
  > ULTRASONIC INSPECTION CARRIED OUT ON LEFT HAND UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUND AT 01EACH FORWARD INBOARD FASTENER HOLE AND 02EACH AFT FASTENER HOLES. LEFT HAND UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOU
- [SDR FDEA201912173253](https://openairdocs.org/sdr/FDEA201912173253.md): Longeron · cracked · Dec 17, 2019 · N850FD · Boeing 777FS2 · Fuselage Main, Longeron/Stringer
  > ULTRASONIC INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUND AT 02EACH FORWARD FASTENER HOLES AND 01EACH AFT OUTBOARD FASTENER HOLE. RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND CRA
- [SDR FDEA201902170442](https://openairdocs.org/sdr/FDEA201902170442.md): Support Bracket · cracked · Feb 17, 2019 · N850FD · Boeing 777FS2 · Engine Thrust Reverser
  > LEFT HAND ENGINE: INBOARD T/R LATCH STRAP SUPPORT BRACKET BROKEN. REPLACED DAMAGED BRACKET IRW SRM 51-40-02-0G.
- [SDR FDEA2018092512656](https://openairdocs.org/sdr/FDEA2018092512656.md): Skin · cracked · Sep 21, 2018 · N850FD · Boeing 777FS2 · Leading Edge Devices
  > MDIS 850 27-80 9729 21SEP18 ANC POST FLT LEFT WING SLAT #5 ZONE 2, UPPER SKIN SURFACE 10 INCH CRACK. FACT 22SEP18 23:11 ANC REPLACED LEFT WING #5 SLAT REF MM 27-81-15-4 AND 27-81-00-2.
- [SDR FDEA201712183405](https://openairdocs.org/sdr/FDEA201712183405.md): Cover · out of position · Dec 18, 2017 · N850FD · Boeing 777FS2 · Fuselage, Door Hinge
  > L1 DOOR AFT COVER WILL NOT CLOSE FLUSH WITH FORWARD. REPOSITIONED THE AFT HINGE DOOR COVER, IAW AMM 52-11-25-2. OK FOR SERVICE.
- [SDR FDEA201709262723](https://openairdocs.org/sdr/FDEA201709262723.md): Handle · binds · Sep 26, 2017 · N850FD · Boeing 777FS2 · Passenger/Crew Doors
  > L1 DOOR HANDLE BINDING DURING DOOR OPENING & CLOSING. INSTALLED A MISSING SPACER RING IAW AMM 52-11-01-4.
- [SDR FDEA201707031843](https://openairdocs.org/sdr/FDEA201707031843.md): Door · binding · Jul 3, 2017 · N850FD · Boeing 777FS2 · Passenger/Crew Doors
  > DURING PREFLIGHT, FLIGHT CREW WAS UNABLE TO OPEN THE L1 DOOR. PERFORMED INSPECTION AND CHECK OF THE L1 DOOR IAW AMM 52-11-00-6, STEPS 1 & 2. A NEW ESCAPE SLIDE WAS INSTALLED IAW WRI 52-10/8424. DOOR OPENS AND CLOSES NOW WITH NORMAL EFFORT.
- [SDR FDEA201706291785](https://openairdocs.org/sdr/FDEA201706291785.md): Tire · leaking · Jun 29, 2017 · N850FD · Boeing 777FS2 · Tire
  > NR 10 TIRE PRESSURE INDICATED 194 PSI. TIRE PRESSURE 171PSI. EICAS EVENT RECORED. NINE HOURS LATER, 94 PSI. LANDING NORMAL IAW QRN, NO VIBRATION OR DAMAGE NOTED BY GROUND PERSONNEL POST LANDING. REMOVED AND REPLACED RT MAIN NR 9 TIRE IAW AMM 32-45-01-4.
- [SDR FDEA201706241755](https://openairdocs.org/sdr/FDEA201706241755.md): Girt Bar · obstructed · Jun 24, 2017 · N850FD · Boeing 777FS2 · Emergency Equipment
  > DURING BLOCK IN, UNABLE TO OPEN THE LT DOOR. FOUND FLAP OF GIRT MATERIAL LOOSE ON BOTTOM OF DOOR-MOUNTED SLIDE INTERFERING WITH GIRT RELEASE. RESTOWED GIRT MATERIAL IAW AMM 25-66-01-4. OP CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201506111766](https://openairdocs.org/sdr/FDEA201506111766.md): Warning Message · illuminated · Jun 11, 2015 · N850FD · Boeing 777FS2 · Autopilot System
  > ON DES, ON MAGENTA LINE, SPEED BRAKES MID, A/C DID UNCOMMAMDED RT ROLL 35DEG BANK. A/P DISCONNECTED NOOTHER PROB. PERFORMED AUTOPILOT FLIGHT DIRECTOR SYSTEM. GROUND TEST PER AMM 22-11-00-5, TEST PASSED. PERFORMED PRIMARY FLIGHT CONTROL SYSTEM LEFT AND R
- [SDR FDEA201210033553](https://openairdocs.org/sdr/FDEA201210033553.md): Bulb · inoperative · Oct 3, 2012 · N850FD · Boeing 777FS2 · Emergency Lighting
  > THE F/O NOTICED THAT THE DOOR 1L AFT OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINATED. REPLACED BULB IAW MM 33-51-03-2, ALL TEST OK. FINAL CLOSED.
- [SDR FDEA201112035134](https://openairdocs.org/sdr/FDEA201112035134.md): Tire · damaged · Dec 3, 2011 · N850FD · Boeing 777FS2 · Tire
  > ON POST FLIGHT, FOUND NR 7 MAIN TIRE MISSING, TIRE RECAP. REPLACED NR7 WHEEL ASSY REF MM 32-45-01-4. PREMATURE REMOVAL/INSTALLATION. FINAL CLOSED.
- [SDR FDEA201110194588](https://openairdocs.org/sdr/FDEA201110194588.md): Unknown · fumes · Oct 19, 2011 · N850FD · Boeing 777FS2 · Air Distribution System
  > ON DESCENT BETWEEN FL250-FL200 THERE FUMES SIMILAR TO ACETONE IN THE COCKPIT. FINISH DESCENT AND LANDING ON O2. AT BLOCK-IN THERE WERE NO FUMES. CHECKED ALL AREA (COCKPIT,SUPERNUMARY, MAIN CARGO, FWD CARGO, AFT CARGO, AVIONICS AND FUSELAGE) WAS NO LEAK AND N

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N850FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N850FD/reports

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