# Service difficulty reports: N994FD

A list on [N994FD](https://openairdocs.org/aircraft/N994FD.md).

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

Page 1 of 2 · 72 reports

- [SDR FDEA202208031840](https://openairdocs.org/sdr/FDEA202208031840.md): Fitting · detached · Aug 3, 2022 · N994FD · Boeing 757200 · Fuselage Main, Attach Fittings
  > R1 DOOR SLIDE WOULD NOT ARM. ARMING HANDLE WILL NOT FULLY DISARM. REATTACHED GRIT BAR FITTING IAW B757 AMM 25-66-10-2, OPS CHECK GOOD, A/C OK FOR SERVICE.
- [SDR FDEA202112270006](https://openairdocs.org/sdr/FDEA202112270006.md): None · none · Dec 27, 2021 · N994FD · Boeing 757200 · Cargo Compartments
  > MAIN CARGO FLOOR SEAT TRACK LOBE DAMAGED AT STA 579 AT BL45L. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA.440-STA. 690 LBL 45.5 IN REF TO 757 SRM 51-40-02- 0G. SEE JPF FOR OTHER ACTIONS
- [SDR FDEA202105201334](https://openairdocs.org/sdr/FDEA202105201334.md): Girt Bar · disengaged · May 20, 2021 · N994FD · Boeing 75723A · Emergency Equipment
  > WHEN OPENING R1 DOOR NOTED GIRT BAR HANGING DOWN FROM BOTTOM OF DOOR. COMPLIED WITH B757 AMM 25-66-10-2 PAGES 14-15 STEPS 14-21. RENEGAGED THE GIRT BAR CAMS IN THE
- [SDR FDEA202012313226](https://openairdocs.org/sdr/FDEA202012313226.md): Actuator · malfunctioned · Dec 31, 2020 · N994FD · Boeing 75723A · Landing Gear Actuator
  > GEAR DISAGREE WHEN LANDING GEAR LEVER SELECTED DOWN BEFORE LANDING. NOSE GEAR INDICATED UNSAFE. RAN QRH FOR GEAR DISAGREE AND EXTENDED GEAR VIA ALTERNATE EXTENSION. EMERGENCY DECLARED. REMOVED AND REPLACED NOSE LANDING GEAR LOCKING ACTUATOR, REF B757 AMM 3
- [SDR FDEA202012243205](https://openairdocs.org/sdr/FDEA202012243205.md): Gate · corroded · Dec 24, 2020 · N994FD · Boeing 75723A · Passenger/Crew Doors
  > L1 DOOR LOWER GATE LOWER EDGE PITTED ACCOMPLISHED EA NR F-5210-T0358769. DOORS-PASSENGER/CREW-NR 1 PASS, DOOR LOWER GATE, EDGE PITTING.
- [SDR FDEA202012223200](https://openairdocs.org/sdr/FDEA202012223200.md): Shelf · cracked · Dec 22, 2020 · N994FD · Boeing 75723A · Fuselage Main, Structure
  > E&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007.
- [SDR FDEA202012223199](https://openairdocs.org/sdr/FDEA202012223199.md): Mount · cracked · Dec 22, 2020 · N994FD · Boeing 75723A · Fuselage Main, Attach Fittings
  > E&E COMPARTMENT E3-1 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007.
- [SDR FDEA202012223197](https://openairdocs.org/sdr/FDEA202012223197.md): Flange · cracked · Dec 22, 2020 · N994FD · Boeing 75723A · Fuselage Main, Structure
  > E&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT FLANGE CRACKED. REMOVED AND REPLACED FLANGE, IAW B SRM 51-40-02 AND DWG NR 284N1028 REV C.
- [SDR FDEA202012173180](https://openairdocs.org/sdr/FDEA202012173180.md): Skin · cracked · Dec 17, 2020 · N994FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > NOSE WHEEL WELL RT DOOR CUT OUT UPPER SKIN STRIP IS CRACKED AT BS 324 RBL 19. REMOVED AND REPLACED STRIP, PER DWG 141N0094.
- [SDR FDEA202011102805](https://openairdocs.org/sdr/FDEA202011102805.md): Actuator · failed · Nov 10, 2020 · N994FD · Boeing 75723A · Landing Gear Retraction/Extension System
  > PDIS 994 32-30 8627 10NOV20 IND OPEN U. GEAR DISAGREE AND GEAR DOORS EICAS FOR 90 SECONDS UNTIL GEAR FULLY RETRACTED AND EICAS MESSAGES. NOISE FROM NOSE GEAR AREA UNTIL DOORS MESSAGES WENT AWAY. REPEAT WRITE UP. SHGN 10NOV20 06:12 IND U. CREW REPORTED THA
- [SDR FDEA2020070211406](https://openairdocs.org/sdr/FDEA2020070211406.md): Clamp · worn · Jul 1, 2020 · N994FD · Boeing 75723A · Pneumatic Distribution System
  > LEFT BLEED DUCT LEAK AT FL 370 WITH ENGINE ANTI-ICE ON. COMPLETED QRH AND SECURED ENGINE ANTI-ICE AND LIGHT WENT OUT WITH NO SECONDARIES. REMOVED STAND OFF CLAMPS FOR ACCESS AND POSITIONING OF LEADING EDGE DUCTING. REMOVED AND REPLACED 5 WORN LEADING EDGE C
- [SDR FDEA2020070201409](https://openairdocs.org/sdr/FDEA2020070201409.md): Clamp · worn · Jun 30, 2020 · N994FD · Boeing 75723A · Pneumatic Distribution System
  > LEFT BLEED DUCT LEAK AT FL 370 WITH ENGINE ANTI-ICE ON. COMPLETED QRH AND SECURED ENGINE ANTI-ICE AND LIGHT WENT OUT WITH NO SECONDARIES. ACCOMPLISHED WING AND BODY DUCT LEAK DETECTION BITE PROCEDURE AND FOUND HARD FAULT CODE 14 (LEFT WING LEADING EDGE ALAR
- [SDR FDEA2019121303214](https://openairdocs.org/sdr/FDEA2019121303214.md): Proximity Sensor · inoperative · Dec 10, 2019 · N994FD · Boeing 75723A · Emergency Equipment
  > RIGHT DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. VERIFIED 28VAC AT SLIDE LIGHT L404. VERIFIED GOOD CONTINUITY THROUGH AFT GIRT BAR PROX SENSOR S10217 WITH THE SWITCH ACTUATED. VERIFIED GOOD GROUND AT GD2922-AC. NO CONTINUITY FOUND THROUGH FWD PROX SE
- [SDR FDEA201911263110](https://openairdocs.org/sdr/FDEA201911263110.md): Light · inoperative · Nov 26, 2019 · N994FD · Boeing 75723A · Emergency Equipment
  > PDIS 994 25-60 7876 26NOV19 BUF OPEN U LOGPAGES:3167525 R1 DOOR SLIDE LIGHT NOT ILLUMINATED WHILE ARMED. MEL 26NOV19 00:00 BUF U RELEASED FOR SERVICE PER MEL: 25-66-05-A CATEGORY: C EXPIRATION: 06DEC19 "MEL 25-66-05-A: ______R1__ (IDEN
- [SDR FDEA201812153509](https://openairdocs.org/sdr/FDEA201812153509.md): Seat Track · corroded · Dec 15, 2018 · N994FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK STA 1540 RBL 45.7 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIG MAT.075 REM.050 LOSS.025 FOUND OUT OF LIMITS IAW SRM 53-00-52-1A. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R REPAIR 3 DIM 51.
- [SDR FDEA201812133498](https://openairdocs.org/sdr/FDEA201812133498.md): Crease Beam · corroded · Dec 13, 2018 · N994FD · Boeing 75723A · Fuselage Main, Structure
  > MAIN CABIN LBL 62 CREASE BEAM AT STA 800 HAS CORROSION. REMOVED CORROSION ON CREASE BEAM STA 800 LBL 62 IAW B757 SRM 51-10-02. ORIG MAT.071 REM.051 LOSS.020 OUT OF LIMITS IAW B757 SRM 53-30-13-1A FIG 101 DET. VIII. REPAIRED CREASE BEAM IAW B757 SRM 5
- [SDR FDEA201812113493](https://openairdocs.org/sdr/FDEA201812113493.md): Seat Track · corroded · Dec 11, 2018 · N994FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 24.75 AT STA 618 HAS CORROSION. REMOVED CORROSON ON SEAT TRACK STA 618 LBL 24.75 IAW B757 SRM 51-10-02. ORIG MAT.070 REM.035 LOSS.035 FOUND OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DET VII. REPAIRED SEAT TRACK IAW B757
- [SDR FDEA201812113492](https://openairdocs.org/sdr/FDEA201812113492.md): Floorbeam · corroded · Dec 11, 2018 · N994FD · Boeing 75723A · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR SUPPORT BTWN LBL 24.75 / BL 0 AT BS 1020 CORROSION. REMOVED CORR ON FLOOR SUPPORT BETWEEN LBL 24.75 / BL0 STA. 1020 IAW B757 SRM 51-10 10-02. FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DET VII. DIM 23". ACCOMPLISHED FEDEX EA F-5
- [SDR FDEA201812113491](https://openairdocs.org/sdr/FDEA201812113491.md): Seat Track · corroded · Dec 11, 2018 · N994FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN THE MAIN CABIN SEAT TRACK, RT FLANGE UPPER SURFACE, BETWEEN BS 1020 TO BS 1040 LBL 58. REMOVED CORR ON SEAT TRACK STA 1020 TO 1040 LBL58 IAW SRM 51-10-02 ORIG MAT.90 REM.050 LOSS.040 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-52-1A. REMOVED,
- [SDR FDEA201812053436](https://openairdocs.org/sdr/FDEA201812053436.md): Floorbeam · cracked · Dec 5, 2018 · N994FD · Boeing 75723A · Fuselage Main, Floor Beam
  > STUB BEAM IN FORWARD CARGO AT STA 580 AND LBL 45. COMPLIED WITH MAINFRAME STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45.
- [SDR FDEA201808172067](https://openairdocs.org/sdr/FDEA201808172067.md): Controller · malfunctioned · Aug 17, 2018 · N994FD · Boeing 75723A · Cabin Cooling System
  > AT FL 340, NOTICED EARS POPPING. LOOKED AT THE CABIN ALTITUDE INDICATOR & IT INDICATED NORMAL, THE RATE GAUGE FLUCTUATED. AFTER A FEW MINUTES, THE RIGHT PACK INDICATED INOPERATIVE. DESCENDED TO 9000 FT. REMOVED AND REPLACED THE RIGHT PACK TEMP CONTROLLER
- [SDR FDEA201806231573](https://openairdocs.org/sdr/FDEA201806231573.md): Charger · inoperative · Jun 23, 2018 · N994FD · Boeing 75723A · Emergency Lighting
  > RT EMERGENCY EXIT SIGN DID NOT TEST, LAMPS OUT/MISSING. REMOVED AND REPLACED BATTERY PACK/ CHARGER TRAY FOR RT EMERGENCY EXIT SIGN, REF AMM 33-51-07-2. OPS CHECKS GOOD, A/C OK FOR SERVICE.
- [SDR FDEA201801120083](https://openairdocs.org/sdr/FDEA201801120083.md): Lock · out of adjust · Jan 12, 2018 · N994FD · Boeing 75723A · Emergency Equipment
  > LEFT FORWARD ENTRY DOOR WAS DISARMED THEN OPENED. PARTS FELL OFF DOOR AND SLIDE PARTIALLY HANGING OUT. INSTALLED THE AFT BAR LOCK ONTO GIRT BAR IAW MM 25-66-01-4, PARA 3H (19). INSTALLED SLIDE COVER. WHEN ARMING DOOR, AFT BAR LOCK FOUND TO BE TOO FAR INBOA
- [SDR FDEA201709032454](https://openairdocs.org/sdr/FDEA201709032454.md): Girt Bar · dislodged · Sep 3, 2017 · N994FD · Boeing 75723A · Emergency Equipment
  > RT DOOR SLIDE LIGHT IS INOP. DURING T/S FOUND THAT THE GIRT BAR WAS DISLODGED FROM DOOR. REINSTALLED GIRT BAR ON DOOR REF AMM 25-66-10-2-0. OPS CHECKS GOOD. SLIDE LIGHT OPS CHECKS GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201708052124](https://openairdocs.org/sdr/FDEA201708052124.md): Sensor · dirty · Aug 5, 2017 · N994FD · Boeing 75723A · Door Warning System
  > SLIDE ARMED INDICATOR LIGHT ON R FWD ENT DOOR DOES NOT ILLUMINATE. INSPECTED GIRT BAR DETECTION PER AMM 25_66_11_2_0. SOME DEBRIS NOTED, CLEANED SENSOR AREA. OPS CHECKED NORMAL SEVERAL TIMES. OK FOR SERVICE
- [SDR FDEA201707061860](https://openairdocs.org/sdr/FDEA201707061860.md): Bottle · low pressure · Jul 6, 2017 · N994FD · Boeing 75723A · Passenger/Crew Doors
  > FOUND THE L1 DOOR ASSIST BOTTLE PRESSURE LOW R & R THE L1 DOOR ASSIST BOTTLE IAW AMM 52-11-30-4.
- [SDR FDEA201705051360](https://openairdocs.org/sdr/FDEA201705051360.md): Pdu · tripped · May 5, 2017 · N994FD · Boeing 75723A · Trailing Edge Flap Control System
  > TE FLAP DISAGREE MESSAGE AFTER SELECTING FLAPS 20 ON VISUAL APPROACH. QRH COMPLETED AND LANDED FLAPS 20. TROUBLESHOT TE FLAP DISAGREE IAW FIM 27-51 FT 808. FOUND LEFT INBOARD PDU OVERLOAD INDICATOR TRIPPED. BITE CHECKED ALL 3 FSEU'S AND NO FAULTS WERE F
- [SDR FDEA201611224199](https://openairdocs.org/sdr/FDEA201611224199.md): Frame · dented · Nov 22, 2016 · N994FD · Boeing 75723A · Fuselage Main, Frame
  > AFT CARGO FRAME AT BS 1340 HAS A DENT BETWEEN STRINGERS 25L AND 26L. REPAIRED IAW EA F-5310-T0329984 P1. MAJOR REPAIR.
- [SDR FDEA201611224200](https://openairdocs.org/sdr/FDEA201611224200.md): Frame · dented · Nov 22, 2016 · N994FD · Boeing 75723A · Fuselage Main, Frame
  > AFT CARGO BAY FRAME AT BS 1420 HAS A DENT ABOVE STRINGER 26L. COMPLIED WITH EA F-5310-T0329906 P1.
- [SDR FDEA201611154022](https://openairdocs.org/sdr/FDEA201611154022.md): Web · corroded · Nov 15, 2016 · N994FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > MAIN CARGO WEB AT BS 4121 RBL 67, FOUND CORRODED, UPPER RT CORNER. REMOVED AND REPLACED THE WEB IAW DRAWING 146N5590 REV E.
- [SDR FDEA201610043454](https://openairdocs.org/sdr/FDEA201610043454.md): Girt Bar · damaged · Oct 4, 2016 · N994FD · Boeing 75723A · Emergency Equipment
  > L1 DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE. THE GIRT BAR WILL NOT FULLY ENGAGE. R & R THE GIRT BAR IAW MM 25-66-10-2. PERFORMED ADJUSTMENT AND TEST IAW MM 25-66-11-2. OPS CHECKED GOOD.
- [SDR FDEA201302210387](https://openairdocs.org/sdr/FDEA201302210387.md): Control Panel · malfunctioned · Feb 21, 2013 · N994FD · Boeing 75723A · Emergency Lighting
  > EMERGENCY EXIT LIGHT CONTROL PANEL "UNARMED" ANNUNCIATOR INOPERATIVE. R & R OVERHEAD EMERGENCY EXIT LIGHTS CONTROL PANEL IAW AMM 33-51-08, OPS CHECKED NORMAL.
- [SDR FDEA201211154040](https://openairdocs.org/sdr/FDEA201211154040.md): Support Angle · cracked · Nov 15, 2012 · N994FD · Boeing 75723A · Nacelle/Pylon, Main Frame
  > ANGLE CRACKED NR 1 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND DWG 311N3510, REV C.
- [SDR FDEA201211154039](https://openairdocs.org/sdr/FDEA201211154039.md): Angle · cracked · Nov 15, 2012 · N994FD · Boeing 75723A · Nacelle/Pylon, Main Frame
  > ANGLE CRACKED NR 2 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND DWG 311N3510, REV C.
- [SDR FDEA201208163017](https://openairdocs.org/sdr/FDEA201208163017.md): Liner · out of position · Aug 16, 2012 · N994FD · Boeing 7572G5 · Passenger/Crew Doors
  > WHEN ARMING L1 DOOR, EXCESSIVE FORCE HAD TO BE APPLIED TO GET SLIDE ARM INDICATOR TO DISPLAY. FOUND ESCAPE SLIDE ARMING TAB RUBBING ON LOWER LINING OF L1 DOOR. REF MM 52-11-02-4, ADJUSTED LOWER LINING. ALL DOOR COMPONENTS RE-INSTALLED. SLIDE ARMING TAB OPS
- [SDR FDEA201203130910](https://openairdocs.org/sdr/FDEA201203130910.md): Light · inoperative · Mar 13, 2012 · N994FD · Boeing 75723A · Emergency Lighting
  > R1 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. R & R R1 EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2-1. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201109224036](https://openairdocs.org/sdr/FDEA201109224036.md): Girt Bar · out of adjust · Sep 22, 2011 · N994FD · Boeing 75723A · Emergency Equipment
  > R1 DOOR SLIDE ARMING LEVER IS BINDING BEFORE IT GOES FULL TRAVEL TO ARM. ORIGINAL GSP-LINE. ADJUSTED GIRT BAR FLOOR FITTINGS PER MM 52-11-25-5-0. OPS CHECKED GOOD
- [SDR FDEA201109153891](https://openairdocs.org/sdr/FDEA201109153891.md): Panel · loose · Sep 15, 2011 · N994FD · Boeing 75723A · Passenger/Crew Doors
  > PANEL BEHIND ARMED/DISARMED SLIDE ON LT DOOR IS LOOSE. REMOVED THE L-1 DOOR INTERIOR COVER. INSTALLED THE NEW PLATE RETAINER RAIL IAW AMM 52-11-02 & SRM 51-70-06.
- [SDR FDEA201108093143](https://openairdocs.org/sdr/FDEA201108093143.md): Battery Pack · failed · Aug 9, 2011 · N994FD · Boeing 75723A · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT TEST. EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.
- [SDR FDEA201106292483](https://openairdocs.org/sdr/FDEA201106292483.md): Engine · erratic · Jun 29, 2011 · N994FD · Boeing 75723A · Engine (Turbine/Turboprop)
  > AT CRUISE FL 400, THE RT ENGINE BECAME ERRATIC WITH EPR FLUCTUATIONS BETWEEN 1.10 TO 1.29 WITH ASSOCIATED VARIATIONS IN N1 AND FUEL FLOW. TURNED AUTO THROTTLES OFF AND THE PROBLEM CONTINUED. REDUCING POWER DID NOT HELP. R & R RT(NR 2) ENGINE EEC IAW AMM 7
- [SDR FDEA201105171850](https://openairdocs.org/sdr/FDEA201105171850.md): Eec · malfunctioned · May 17, 2011 · N994FD · Boeing 75723A · Fuel Controlling System
  > ON DESCENT INTO MEM GOT RT ENG OIL PRESS ALERT WITH OIL PRESS ABOVE 70 PSI (RED) SHUTDOWN RT ENGINE IAW QRH. RECIEVED STATUS MESSAGES, RT ENG SEC SEL RT ENG LOW N1 R ENG OIL PRESS R ENG SPEED CARD RT ENG SEC CONT RT ENG FUEL ON SOL. INSTALLED RT ENGINE EEC
- [SDR FDEA201012094622](https://openairdocs.org/sdr/FDEA201012094622.md): Support · chafed · Dec 9, 2010 · N994FD · Boeing 75723A · Wing Miscellaneous Structure
  > LT WING- L/E WING APPROX W/S 240 - L/E DUCT SUPPORT CHAFING INTO VERTICAL SUPPORT. REMOVED & INSTALLED NEW STIFFNER IAW SRM 51-40-02. RECIEVED NEW STIFFNER ON TR T10/861406. P/N 112N2038-79. NO NOTED DAMAGE TO BRACKET. MAJOR REPAIR.
- [SDR FDEA201012064598](https://openairdocs.org/sdr/FDEA201012064598.md): Skin · worn · Dec 6, 2010 · N994FD · Boeing 75723A · Trailing Edge Flaps
  > LT WING OTBD MAIN FLAP L/E INBD SIDE HAS A WORN SECTION APPROX 10" LONG. EVALUATED LT WING OTBD MAIN FLAP AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, PG 106, DETAIL VI. R & R L/E SKIN IAW SRM 51-40-02. CLASSIFIED CATEGORY "A". MAJOR REPAIR.
- [SDR FDEA201011264496](https://openairdocs.org/sdr/FDEA201011264496.md): Skin · dented · Nov 26, 2010 · N994FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN STA 1720-1740 BETWEEN S-25R TO S-16R HAS DENT AT LAP SEAM. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO LAP SEAM. REPAIRED DENT IAW EA F-5330-143218. CLASSIFIED CATEGORY "A" MAJOR REPAIR.
- [SDR FDEA201011184419](https://openairdocs.org/sdr/FDEA201011184419.md): Skin · damaged · Nov 18, 2010 · N994FD · Boeing 75723A · Ailerons
  > LT WING AILERON OTBD AREA LWR SURFACE PUNCTURED THRU SKIN DIAMETER OF HOLE 0.250 BY 1"X1" REPAIRED LT WING AILERON OTBD AREA IAW SRM 51-70-17 SB 757-51-0006 IAW SRM 57-60- 01. FINAL DIAMENTION OF REPAIR 5"X4" AND LOCATED AT THE IM EDGE OF STATIC FRAME REF E
- [SDR FDEA201011184421](https://openairdocs.org/sdr/FDEA201011184421.md): Wedge · chafed · Nov 18, 2010 · N994FD · Boeing 75723A · Leading Edge Devices
  > NR 6 SLAT T/E WEDGE UNDER SKIN HAS CHAFE MARKS, REPAIRED NR6 SLAT T/E IAW SRM 51-70-10 IAW SRM 57-43-02. DAMAGE WAS LOCATED AT STA 177.5, APPROX 3" FWD OF T/E. REF EA F-5750-143211. CLASSIFIED CAT "A" MAJOR REPAIR.
- [SDR FDEA201011184420](https://openairdocs.org/sdr/FDEA201011184420.md): Skin · damaged · Nov 18, 2010 · N994FD · Boeing 75723A · Leading Edge Devices
  > LT WING NR 2 SLAT HAS NUMEROUS CHAFED MARKS ALONG BOTTOM SKIN AFT EDGE REPAIRED LT WING NR 2 SLAT IAW SRM 51-70-10 IAW SRM 57-43-02 DAMAGE LOCATED AT STA 652.50 APPROX 1" FWD OF T/E SLAT REPAIR DIAM. 1"X1.5". REF EA F-5750-142276. CLASSIFIED CAT "A" MAJOR REPA
- [SDR FDEA201010274180](https://openairdocs.org/sdr/FDEA201010274180.md): Gate · corroded · Oct 27, 2010 · N994FD · Boeing 757223 · Passenger/Crew Doors
  > L1 LOWER GATE PANEL HAS SEVERE CORROSION ALONG LOWER EDGE AND ON GATE SKIN PANEL AT LOWER EDGE. REMOVED AND REPLACED L1 DOOR LOWER GATE ASSY, PER AMM 52-11-38. ADJUSTMENT AND TEST GOOD PER AMM 51-11-00-5. (CORROSION WAS OUT OF LIMITS PER SRM 51-10-01, FIG.101
- [SDR FDEA201010103984](https://openairdocs.org/sdr/FDEA201010103984.md): Seat Track · corroded · Oct 10, 2010 · N994FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > AT RBL 24, BL 1600- 1640 HAS HEAVY PITTING IN INBD RADIUS OF SEAT TRACK CROWN TO FLANGE. CHECKED LIMITS FOUND TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DET VII. PAGE 104. REMOVED SEAT TRACK IAW SRM 51-40-09. TRIMED NEW SEAT TRACK PER SAMPLE I
- [SDR FDEA201009223634](https://openairdocs.org/sdr/FDEA201009223634.md): Skin · dented · Sep 22, 2010 · N994FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > PREVIOUS SKIN DENTED AT BS 309, S18L. ACCOMPLISHED SKIN REPAIR IAW EA F-5330-141203, BS 309, BELOW S17L. DENT WAS OUT OF LIMITS DUE TO PROXIMITY TO BS 310.5 FRAME. 2EA. SHEAR TIES WERE FABRICATED ON TRAVELERS T10/855076 AND T10/855075. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N994FD/reports.md?page=2

## 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 = 'N994FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N994FD/reports

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