# Service difficulty reports: N990FD

A list on [N990FD](https://openairdocs.org/aircraft/N990FD.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 3 · 143 reports

- [SDR FDEA202512122239](https://openairdocs.org/sdr/FDEA202512122239.md): Torque Tube · damaged · Dec 12, 2025 · N990FD · Boeing 757232 · Leading Edge Slat Control System
  > WHEN CONFIGURING AFTER START SETTING FLAPS TO 5 RECEIVED LE SLAT DISAG EICAS. UPON INSPECTION FOUND THE CONTROL CABLE INPUT FOR THE LE SLAT PDU BROKEN AND FRAYED. THE CABLE IS IDENTIFIED AS LESA IAW FIM 27-81, FAULT TREE 803, FIGURE 104, & IPC 27-51-25-0
- [SDR FDEA202511112160](https://openairdocs.org/sdr/FDEA202511112160.md): Skin · delaminated · Nov 11, 2025 · N990FD · Boeing 757232 · Horizontal Stabilizer, Plate/Skin
  > LH HORIZONTA STABILIZER UPPER SKIN HAS POSSIBLY DELAMINATION STAB STA 104.248 AREA APPLIED PERMANENT REPAIR AT LH HORIZONTAL STABILIZER UPPER SKIN I.A.W B757 SRM 55-10- 01-1A, TABLE I, NOTE 'A' AND "I", FIG 101, SHEET 2, I.A.W B757 SRM 51-70-10-2R
- [SDR FDEA202511112159](https://openairdocs.org/sdr/FDEA202511112159.md): Skin · dented · Nov 11, 2025 · N990FD · Boeing 757232 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STABILIZER LOWER SURFACE HAS TWO DENTS STAB STA 176.249 AREA TWO DENTS FOUND OUT OF LIMITS AT RH HORIZONTAL STABILIZER LOWER SURFACE STAB STA 176.248. AND APPLIED PERMANENT REPAIR I.A.W B757 SRM 55-10-01-1A, TABLE I, NOTE 'I' FIG 101, SHEET 3
- [SDR FDEA202511082146](https://openairdocs.org/sdr/FDEA202511082146.md): Stringer · corroded · Nov 8, 2025 · N990FD · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > LH OUBD W/W TUNNEL WAS FOUND STRINGER S-23LH AT STA 399.5 (TUNNEL BEGINING) WITH CORROSION CORROSION FOUND OUTSIDE PERMITTED LIMITS ON S-23 LH STA 399.5 IAW B757 SRM 53-00-03-1A, STRINGER SECTION WAS FABRICATED AND REPLACED IN S23 LH BETWEEN STA 365.25 TO
- [SDR FDEA202511062138](https://openairdocs.org/sdr/FDEA202511062138.md): Skin · gouged · Nov 6, 2025 · N990FD · Boeing 757232 · Trailing Edge Flaps
  > L/H WING OUTB AFT FLAP UPPER SKIN MIDDLE SECTION WITH GOUGE. GOUGE WITH CRACK AT L/H WING OUTB AFT FLAP UPPER SKIN MIDDLE SECTION WAS REPAIRED IAW B-757 SRM 57-53-01-2R AND SRM 51-70-04-0G
- [SDR FDEA202511062137](https://openairdocs.org/sdr/FDEA202511062137.md): Skin · gouged · Nov 6, 2025 · N990FD · Boeing 757232 · Trailing Edge Flaps
  > L/H WING OUTB AFT FLAP, UPPER SKIN INB SECTION WITH GOUGE. GOUGE WITH CRACK AT L/H WING OUTB AFT FLAP, UPPER SKIN INB. SECTION WAS REPAIRED IAW B-757 SRM 57-53-01-2R AND SRM 51-70-04-0G
- [SDR FDEA202511062136](https://openairdocs.org/sdr/FDEA202511062136.md): Skin · gouged · Nov 6, 2025 · N990FD · Boeing 757232 · Trailing Edge Flaps
  > RIGHT OTBD FLAP TE AFT FLAP UPPER SURFACE WITH 02 EA GOUGES. GOUGES REPAIRED IAW SRM 57-53-01-2R AND SRM 51-70-17-0G.
- [SDR FDEA202509231767](https://openairdocs.org/sdr/FDEA202509231767.md): Lamp · failed · Sep 23, 2025 · N990FD · Boeing 757232 · Emergency Lighting
  > R1 SLIDE LIGHT WILL NOT ILLUMINATE. IAW AMM 52-10-00-5 RELAMPED. CKD OK.
- [SDR FDEA202502070191](https://openairdocs.org/sdr/FDEA202502070191.md): Lens · broken · Feb 7, 2025 · N990FD · Boeing 757232 · Emergency Lighting
  > ON SERVICE CHECK FOUND EMERGENCY EXIT LIGHT HOUSING BROKEN ABOVE R1 DOOR. R/R R1 DOOR EMERGENCY EXIT SIGN COVER AND OPS CHECK GOOD, NO FURTHER DEFECTS NOTED. REF B757 AMM 33-51-01-2.
- [SDR FDEA202412021761](https://openairdocs.org/sdr/FDEA202412021761.md): Collar · damaged · Dec 2, 2024 · N990FD · Boeing 757232 · Passenger/Crew Doors
  > L1 HOLD-OPEN LOCK COLLAR BROKEN. AMM: 52-11-08-8 REMOVED AND REPLACED HOLD-OPEN LOCK COLLAR PER B757 AMM 52-11-08-8. OPS CK GOOD. A/C OK TO CONTINUE.
- [SDR FDEA202411011626](https://openairdocs.org/sdr/FDEA202411011626.md): Unknown · unknown · Nov 1, 2024 · N990FD · Boeing 757232 · Standard Practices/Structures
  > INFLIGHT EMERGENCY DECLARED TO GET PRIORITY HANDLING IN ORDER TO LAND AT KRNO DESPITE A RAMP CLOSURE DUE TO TFR FOR VIP MOVEMENT BEFORE ACHIEVING EMERGENCY FUEL STATE OF 4400 POUNDS. EMERGENCY DECLARED. NO MAINTENANCE ACTION
- [SDR FDEA202312141939](https://openairdocs.org/sdr/FDEA202312141939.md): Frame · cracked · Dec 14, 2023 · N990FD · Boeing 757200 · Fuselage Main, Frame
  > CRACK FOUND ON AFT SIDE OF T-SUPPORT CLIP BTWN STR-14L AND STR-15L ON FRAME 1640 LH FUSELAGE-MAINFRAME-STA 1640 FRAME SPLICE REPAIR BETWEEN STRINGER I-9F AND S-20L-EO F-5310-E0367020A P1 CRACK INDICATIONS REPAIR-PARTIAL FRAME REPLACEMENT. ACCOMPLISHED REP
- [SDR FDEA202312051908](https://openairdocs.org/sdr/FDEA202312051908.md): Floorboard · damaged · Dec 5, 2023 · N990FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 222MAF DAMGED FABRICATED ZONE 220 COUREIR FLOORBOARD 222MAF ON VTMAE TRAVELER # T23/1717925 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051907](https://openairdocs.org/sdr/FDEA202312051907.md): Floorboard · damaged · Dec 5, 2023 · N990FD · Boeing 757200 · Standard Practices/Structures
  > ZONE 220 COURIER FLOORBOARD 221MBF DAMGED FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VTMAE TRAVELR # T23/1717921 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR
- [SDR FDEA202312051906](https://openairdocs.org/sdr/FDEA202312051906.md): Floorboard · damaged · Dec 5, 2023 · N990FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 FLOORBOARD 222AF DAMAGED FABRICATED ZONE 220 FLOORBOARD 222AF ON VTMAE TRAVELR # T23/1717922 IAW DWG SRZ-25- 005 REVISION R, MAJOR REPAIR
- [SDR FDEA202312051905](https://openairdocs.org/sdr/FDEA202312051905.md): Floorboard · damaged · Dec 5, 2023 · N990FD · Boeing 757200 · Fuselage Floor Panel
  > ZONE 220 COURIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221BF ON VTMAE TRAVELER # T23/1717928 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR
- [SDR FDEA202312051904](https://openairdocs.org/sdr/FDEA202312051904.md): Floorboard · damaged · Dec 5, 2023 · N990FD · Boeing 757200 · Standard Practices/Structures
  > ZONE 220 COURIER FLOORBOARD 221AF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221AF ON VTMAE TRAVELER # T23/1717926 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR
- [SDR FDEA202303310538](https://openairdocs.org/sdr/FDEA202303310538.md): Stringer · damaged · Mar 31, 2023 · N990FD · Boeing 757200 · Fuselage Main, Longeron/Stringer
  > PUNCTURE DAMAGE TO FUSELAGE AFT OF LOWER AFT CARGO DOOR. DAMAGE IS LOCATED FROM APPX FS 1650R-1680R, BETWEEN STR 22-23R. REMOVED FASTENERS AS NEEDED REF B757 SRM 51-40-02. REFERENCE E.A. # F-5310-T0373827. REF: SRM 53-00-01-2R TABLE 206/REPAIR 28 REP
- [SDR FDEA202207121711](https://openairdocs.org/sdr/FDEA202207121711.md): Stator · failed · Jul 12, 2022 · N990FD · Boeing 757232 · Turbine Engine Combustion Section
  > AT FL 390 LEFT ENGINE FLAMED OUT. ALL ENGINE INDICATIONS LOOKED NORMAL EXCEPT FUEL FLOW WAS 0. OIL PRESSURE STILL REMAINED APPROXIMATELY 13PSI WHEN SHUTDOWN. NO VIBRATIONS NO OTHER ABNORMAL INDICATIONS. WE ATTEMPTED TO RESTART WITHIN IN A DESCENT
- [SDR FDEA202205051127](https://openairdocs.org/sdr/FDEA202205051127.md): Gust Lock · cracked · May 5, 2022 · N990FD · Boeing 757200 · Passenger/Crew Doors
  > FOUND L1 DOOR GUST LOCK BROKEN DURING PREFLIGHT. ENT BY: MEL 05MAY22 23:43 BWI U RELEASED FOR SERVICE PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 08MAY22 "MEL 52-11-01-A: L1 DOOR - INOP." REMOVED DAMAGED GUST LOCK PIECES TO ALLOW DOOR TO BE CLOS
- [SDR FDEA202112073041](https://openairdocs.org/sdr/FDEA202112073041.md): Skin · none · Dec 7, 2021 · N990FD · Boeing 757200 · Trailing Edge Flaps
  > LEFT WING INBOARD MAIN FLAP UPPER SURFACE HAS 1 DENT REPAIRED LEFT WING INBOARD MAIN FLAP UPPER SURFACE SKIN IAW B757 SRM 57-53-01-2R AND B757 SRM 51-70-10-2R
- [SDR FDEA202112063025](https://openairdocs.org/sdr/FDEA202112063025.md): None · cracked · Dec 6, 2021 · N990FD · Boeing 757200 · Nacelle/Pylon Structure
  > #2 PYLON FAIRING 441AT HAS CRACKED COMPOSITE ON THE AFT UPPER EDGE. ACCOMPLISHED A PERMANENT REPAIR TO THE #2 PYLON FAIRING 441AT CRACKED COMPOSITE ON THE AFT UPPER EDGE IAW B757 SRM 54-51-70 FIG 201 SHEET 1 AND EA F-5451-T0365702-P1 PYLON STRUCTURE-TAIL P
- [SDR FDEA202112063024](https://openairdocs.org/sdr/FDEA202112063024.md): None · damaged · Dec 6, 2021 · N990FD · Boeing 757200 · Nacelle/Pylon Structure
  > #1 PYLON FAIRING 431AT HAS COMPOSITE DAMAGE AT OUBD AFT ATTACH HOLE.. ACCOMPLISHED PERMANENT REPAIR TO #1 PYLON FAIRING 431AT COMPOSITE DAMAGE AT OUTBD AFT ATTACHMENT HOLE IAW B757SRM 54-51-70 FIG 201 SHEET 1 AND EA F-5451- T0365724-P1 PYLON STRUCTURE TAILP
- [SDR FDEA202112022981](https://openairdocs.org/sdr/FDEA202112022981.md): None · delaminated · Dec 2, 2021 · N990FD · Boeing 757200 · Trailing Edge Flap Control System
  > LH WING MAIN FLAP INBD SIDE, EXISTING UPPER SKIN REPAIR IS DISBONDING AT APPROX WS 175. REPAIRED LH WING INBD MAIN FLAP I/B SIDE UPPER SURFACE PREVIOUS REPAIR IAW B757 SRM 57-53-01 FIG 201 SHEET 2, 51-70-10-2R, 51-40-02 WITH A PERMANENT REPAIR.
- [SDR FDEA202112012955](https://openairdocs.org/sdr/FDEA202112012955.md): Skin · none · Dec 1, 2021 · N990FD · Boeing 757200 · Passenger/Crew Doors
  > R4 CABIN SVC DOOR EXTERIOR SURFACE IS CREASED VERTICALLY AT THE AFT LOWER CORNER OF THE DOOR APPROX. 2.25" FWD. OF THE AFT EDGE OF THE DOOR REPAIRED R4 DOOR EXTERIOR SURFACE DENT IAW B757 SRM 52-10-01-2R, REP. 7 AND FEDEX EA# F-5210- T0365572-P1, RELEASE DA
- [SDR FDEA202111302953](https://openairdocs.org/sdr/FDEA202111302953.md): Stringer Splice · corroded · Nov 30, 2021 · N990FD · Boeing 757200 · Fuselage Main, Structure
  > AFT CARGO, STRINGER SPLICE CORRODED AT STA 1620 LBL28 REMOVED CORROSION ON STRINGER SPLICE IAW B757-200 SRM 53-00-03-1A. ORIGINAL MAT. THICKNESS IS.100, MAT. REMOVED.004, REMAINING THICKNESS IS.096. IN LIMITS IAW B757-200 SRM 53-00-53 DETAIL I FIG
- [SDR FDEA202111302951](https://openairdocs.org/sdr/FDEA202111302951.md): Skin · worn · Nov 30, 2021 · N990FD · Boeing 757200 · Trailing Edge Flap Control System
  > L/H WING, OUTBD MAIN FLAP, UPPER SKIN HAS WEAR MARKS AT APPROX. WS 425 REPAIRED THE L/W OUTBD MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01-2R, FIG. 201, SHT. 3, AND SRM 51-70-10-2R.
- [SDR FDEA202111262935](https://openairdocs.org/sdr/FDEA202111262935.md): Stringer · corroded · Nov 26, 2021 · N990FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN IS BUCKLED BETWEEN FASTENERS ON S-28L @ STATION 1468 AFTER FURTHER EVALUATION, "BUCKLE" IN SKIN FOUND TO BE TRAPPED FOD BETWEEN THE SKIN & STRINGER 28L NO DAMAGE NOTED TO SKIN, ONLY STRINGER. REPAIRED STRINGER 28L IAW FEDEX EA # F-5310
- [SDR FDEA202111222921](https://openairdocs.org/sdr/FDEA202111222921.md): Skin · corroded · Nov 22, 2021 · N990FD · Boeing 757200 · Fuselage Main, Plate/Skin
  > AFT LOWER VHF DOUBLER & TRIPLER HAVE CORROSION. REMOVED AND REPLACED REPAIR DOUBLER & TRIPLER FROM STA 1460 - 1480, S-29R - S-30 IAW FEDEX EA # F-5330-T0365525
- [SDR FDEA202111112823](https://openairdocs.org/sdr/FDEA202111112823.md): Skin · none · Nov 11, 2021 · N990FD · Boeing 757200 · Fuselage Main, Structure
  > EXTERNAL FUSELAGE HAS PROTRUDING DENT BETWEEN STA 1600 - STA 1620, S-24R - S-25R REPAIRED DENT IAW FEDEX EA # F-5330-T0365574-P1, RELEASED NOV 24, 2021 TITLED " FUSELAGE - PLATES & SKINS - STA 1600 - 1620, S-24R - S-25R, SRM REPAIR DEVIATION."
- [SDR FDEA202111112821](https://openairdocs.org/sdr/FDEA202111112821.md): Skin · dented · Nov 11, 2021 · N990FD · Boeing 757232 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS PROTRUDING DENT BETWEEN STATION 540 - 560, S24L - S25L REPAIRED FUSELAGE SKIN IAW B757 SRM 53-00-01-2R, FIGURE 201, REPAIR NO.7
- [SDR FDEA202111082796](https://openairdocs.org/sdr/FDEA202111082796.md): None · cracked · Nov 8, 2021 · N990FD · Boeing 757200 · Fuselage Main, Structure
  > STATION 1640, S-14R, LOWER INBD & OUTBD TEE CLIP ATTACHED FASTENERS HAVE CRACK INDICATIONS. ACCOMPLISHED AMOC REPAIR IAW FEDEX EA NO. F-5310-T0365342-P1
- [SDR FDEA202106301621](https://openairdocs.org/sdr/FDEA202106301621.md): Adc · failed · Jun 30, 2021 · N990FD · Boeing 757232 · Airspeed/Mach Indicator
  > ON TAKEOFF ROLL DURING 80KT CHECK, FO AIRSPEED INDICATION MALFUNCTIONED. CONTINUED ON CAPT INSTRUMENTS. MESSAGES: IAS DISAGREE, MACH/SPEED TRIM, & RUDDER RATIO. ON SHUTDOWN, ELEV ASYM STATUS MESSAGE. COMPLIED WITH QRH. FO AIRSPEED INCREASED STEADILY FR
- [SDR FDEA202105191311](https://openairdocs.org/sdr/FDEA202105191311.md): Probe · failed · May 19, 2021 · N990FD · Boeing 757232 · Outside Air Temperature Indicator/Sensor
  > PDIS 990 30-30 7688 19MAY21 MEM FACT U LOGPAGES:2903863 TAT PROBE AND ASSOCIATED EICAS MSG ON CLIMB OUT, EMERGENCY DECLARED APON LANDING SHGN 19MAY21 19:10 MEM U REFERENCE WDM 34-12-11, 34-12-12 & 30-33-11. DURING DISASSEMBLY OF CONNECTOR
- [SDR FDEA202105041101](https://openairdocs.org/sdr/FDEA202105041101.md): Gust Lock · broken · May 4, 2021 · N990FD · Boeing 757232 · Passenger/Crew Doors
  > L1 DOOR GUST LOCK BROKEN. FACT 04MAY21 19:49 MEM U REMOVED AND REPLACED GUST LOCK ON L1 DOOR IAW AMM 52-11-08-8. OK FOR SERVICE.
- [SDR FDEA202008252024](https://openairdocs.org/sdr/FDEA202008252024.md): Controller · failed · Aug 25, 2020 · N990FD · Boeing 757230 · Cabin Pressure Controller
  > CABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH NR 1 AND 2 AUTO PRESSURE CONTROLLERS PER MM 21-31-02-4, BOTH OPS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.
- [SDR FDEA202008131878](https://openairdocs.org/sdr/FDEA202008131878.md): Clamp · out of adjust · Aug 13, 2020 · N990FD · Boeing 757232 · Cabin Pressure Control System
  > CABIN ALT WARNING AT FL 370. CABIN ALT WARNING AT FL 370 FOUND #1 PACK SUPPLY DUCT AT THE CHECK VALVE ( FWD LEFT PACK BAY) ORANGE SLEEVE AND CLAMPS LOOSE AND NOT SECURED WITH LARGE AIR LEAK. READJUSTED DUCT SLEEVE AND SECURED CLAMPS AND ACCOMPLISHED LEA
- [SDR FDEA202008111870](https://openairdocs.org/sdr/FDEA202008111870.md): Controller · failed · Aug 11, 2020 · N990FD · Boeing 757232 · Cabin Pressure Controller
  > PDIS 990 21-30 7143 11AUG20 SGF FACT U. CABIN ALTITUDE WARNING AT FL 340. FACT 12AUG20 00:20 SGF U. REMOVED AND REPLACED BOTH NR 1 AND NR 2 AUTO PRESSURE CONTROLLERS, PER MM 21-31-02-4. BOTH OPERATIONS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHA
- [SDR FDEA2020082511870](https://openairdocs.org/sdr/FDEA2020082511870.md): Controller · failed · Aug 11, 2020 · N990FD · Boeing 757232 · Cabin Pressure Controller
  > CABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH NR 1 AND 2 AUTO PRESSURE CONTROLLERS IAW MM 21-31-02-4, BOTH OPS CHECKED GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.
- [SDR FDEA2020081411870](https://openairdocs.org/sdr/FDEA2020081411870.md): Controller · malfunctioned · Aug 11, 2020 · N990FD · Boeing 757232 · Cabin Pressure Controller
  > CABIN ALTITUDE WARNING AT FL 340. REMOVED AND REPLACED BOTH #1 AND #2 AUTO PRESSURE CONTROLLERS IAW MM 21-31-02-4, BOTH OPS CHECK GOOD. ALSO RIGHT PACK FLOW CONTROL VALVE CHANGED ON WRI 2130-7144.
- [SDR FDEA201912233284](https://openairdocs.org/sdr/FDEA201912233284.md): Floor Support · corroded · Dec 23, 2019 · N990FD · Boeing 757232 · Fuselage Miscellaneous Structure
  > MAIN DECK BETWEEN STA 700-720 RBL 60 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 700-720 RBL 60 IAW SRM 51-10-02. 100% MAT LOSS FOUND OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT
- [SDR FDEA201912233283](https://openairdocs.org/sdr/FDEA201912233283.md): Floor Support · cracked · Dec 23, 2019 · N990FD · Boeing 757232 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN STA 680-700 RBL 60 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 680-700 RBL 60 IAW SRM 51-10-02. FOUND TO BE CRACKED OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT IAW S
- [SDR FDEA201912233286](https://openairdocs.org/sdr/FDEA201912233286.md): Floor Support · bent · Dec 23, 2019 · N990FD · Boeing 757232 · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1055 BETWEEN RBL 24.75 - RBL 45.5 FLOOR SUPPORT BENT. FOUND FLOOR SUPPORT PLATE TO BE OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT PLATE IAW SRM 51-40-02, 51-40-05 AND DWG 144N5070
- [SDR FDEA2019122323279](https://openairdocs.org/sdr/FDEA2019122323279.md): Crease Beam · corroded · Dec 22, 2019 · N990FD · Boeing 757232 · Fuselage Main, Structure
  > MAIN DECK BETWEEN STA 1600-1630 IB CREASE BEAM CORRODED RT SIDE. REMOVED CORR ON CREASE BEAM STA 1600-1630 RBL 60 IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-13-1A FIG 101. REMOVED SECTION OF CREASE BEAM, FABRICATED AND INSTALLED NEW SECTION AND REP
- [SDR FDEA2019122323280](https://openairdocs.org/sdr/FDEA2019122323280.md): Floor Support · corroded · Dec 22, 2019 · N990FD · Boeing 757232 · Fuselage Miscellaneous Structure
  > FWD WET AREA BETWEEN STA 324-345 LBL 39 FLOOR SUPPORT CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 324-345 LBL 39 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-
- [SDR FDEA201912203273](https://openairdocs.org/sdr/FDEA201912203273.md): Shear Tie · corroded · Dec 20, 2019 · N990FD · Boeing 757232 · Fuselage Internal Mounting Structure
  > AFT CARGO PIT BELOW FLOOR STA 1280 FRAME SIDE BOTTOM SHEAR TIE BELOW RT TRANSITION FLOOR PANEL CORRODED 1SQ IN. REMOVED CORROSION ON SHEAR TIE AT AFT CARGO STA 1280 BELOW RT TRANSITION PANEL. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-OG AND SRM 53-00-07-1A
- [SDR FDEA2019121323236](https://openairdocs.org/sdr/FDEA2019121323236.md): Panel · cracked · Dec 12, 2019 · N990FD · Boeing 757232 · Leading Edge Devices
  > RT WING NR 9 SLAT OB MAIN TRACK LOWER COVER PANEL EVIDENCE CRACK. COMPLIED WITH EA F-5750-T0351385 P1. WINGS - FLIGHT SURFACES - SLAT NR 9 COVE PANEL- LOCAL FABRICATION AND REPLACEMENT.
- [SDR FDEA2019121323229](https://openairdocs.org/sdr/FDEA2019121323229.md): Tee Fitting · corroded · Dec 12, 2019 · N990FD · Boeing 757232 · Fuselage Miscellaneous Structure
  > MAIN DECK BETWEEN STA 900 - 1040 LBL 45.5 T CHORD CORRODED. REMOVED CORROSION ON MAIN DECK STA 900 TO 1040 LBL 45.5 TEE CHORD IAW SRM 51-40-02-OG, EVALUATED DAMAGE AREA ORIG MAT.090",MAT REM.067", MAT LOSS.023" FOUND TO BE OUT FO LIMITS IAW SRM 53-00-51-1A
- [SDR FDEA2019121323233](https://openairdocs.org/sdr/FDEA2019121323233.md): Skin · gouged · Dec 12, 2019 · N990FD · Boeing 757232 · Trailing Edge Flaps
  > RT WING OB FLAP L/E HAS GOUGE. BLENDED GOUGE FOUND AREA OUT OF LIMITS. RT WING O/B FLAP L/E SKIN IAW SRM 57-53-01-1A FIG 101 DET I, REMOVED EXISTING REPAIR SKIN PLATE IAW SRM 51-40-02-OG. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SKIN REPAIR PART IAW S
- [SDR FDEA2019121313224](https://openairdocs.org/sdr/FDEA2019121313224.md): Crease Beam · corroded · Dec 11, 2019 · N990FD · Boeing 757232 · Fuselage Main, Structure
  > MAIN DECK LT IB CREASE BEAM BETWEEN STA 900 - 1040 CORRODED. REMOVED CORROSION ON CREASE BEAM LT SIDE AT STA 900 TO STA 1040 IAW SRM 51-10-02-OG, ORIGINAL MAT.070",REM MAT.059", MAT LOSS.011", EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A FI

Next page: https://openairdocs.org/aircraft/N990FD/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 = 'N990FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N990FD/reports

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