# Service difficulty reports: N903FD

A list on [N903FD](https://openairdocs.org/aircraft/N903FD.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 4 · 162 reports

- [SDR FDEA202605300654](https://openairdocs.org/sdr/FDEA202605300654.md): Stowage Box · damaged · May 30, 2026 · N903FD · Boeing 7572B7 · Crew Oxygen System
  > WHILE PRE FLIGHTING AC FOUND CAPTS O2 MASK BOX TEST BUTTON BROKEN. REMOVED AND REPLACED CAPTS 02 MASK STOWAGE BOX PER 757 AMM 35-11-51-4-99. OPS CHECK GOOD. MVP COMPLETED BY 4706850 O2 CYLINDER OPENED.
- [SDR FDEA202604250500](https://openairdocs.org/sdr/FDEA202604250500.md): Circuit Breaker · tripped · Apr 25, 2026 · N903FD · Boeing 7572B7 · Fuel System Wiring
  > LEFT AND RIGHT FUEL OVERRIDE CIRCUIT BREAKERS ARE TRIPPED ON PREFLIGHT. REINSTALLED THE P33 PANEL. AWAITING RETEST REQUIREMENTS FROM ENGINEERING IAW AMM: 20-11-00-2 AND SWPM 20-60-03. PANEL P33 INSTALLATION CHECK PER MTSIS AND MOCC.
- [SDR FDEA202602100158](https://openairdocs.org/sdr/FDEA202602100158.md): Skin · cracked · Feb 10, 2026 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Plate/Skin
  > ENG # 1 NACELLE STRUT UPPER WING SURFACE SPAR MID-SPAR ATTACH FITTING HAS A BOLT MIGRATED THIS ITEM HAS BEEN ACCOMPLISHED FOLLOWING WORK INSTRUCTIONS AS PER EA # F-5730- T0386126 P1 TITTLE:"WINGS-PLATES AND SKINS-LH WING UPPER SKIN AT PYLON-LOOSE FASTENE
- [SDR FDEA202602070144](https://openairdocs.org/sdr/FDEA202602070144.md): Wedge · damaged · Feb 7, 2026 · N903FD · Boeing 7572B7 · Leading Edge Devices
  > NUMBER 9 LEADING EDGE SLAT WEDGE DEBONDED, TWO PLACES. APPLIED A PERMANENT REPAIR TO NR 9 LE SLAT EDGE WEDGE IAW SRM 51-70-10-2R R ESTORED SURFACE IN REPAIRED AREA IAW IAW AMM 51-21-00-7.
- [SDR FDEA202602070143](https://openairdocs.org/sdr/FDEA202602070143.md): Wedge · damaged · Feb 7, 2026 · N903FD · Boeing 7572B7 · Leading Edge Devices
  > NUMBER 7 LEADING EDGE SLAT WEDGE DEBONDED. REPAIRED NR 7 LEADING EDGE SLAT IAW SRM 51-70-10-2R.TAP TEST RESULTED SATIFACTORY IAW SRM 51-10-06-2R.
- [SDR FDEA202602040127](https://openairdocs.org/sdr/FDEA202602040127.md): Stringer · damaged · Feb 4, 2026 · N903FD · Boeing 7572B7 · Fuselage Main, Longeron/Stringer
  > REMOVE EXISTING REPAIR AT STA 1656 ON STRINGER 26L REPAIRED STRINGER SECTION AT BS 1640 11" TO BS1660 10" STR 26L, IAW B757 SRM 53-00-03-2R, FIG 201, DETAIL I AND B757 SRM 51-40-02-0G
- [SDR FDEA202601300106](https://openairdocs.org/sdr/FDEA202601300106.md): Floor Support · mechanic error · Jan 30, 2026 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT, BS 1465 MISDRILLED HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT, IAW SRM 51-40-02-0G AND SRM 53-60-53-01, FIG 1, DET VII.
- [SDR FDEA202601300105](https://openairdocs.org/sdr/FDEA202601300105.md): Floor Support · mechanic error · Jan 30, 2026 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT, LBL 7.55 BTW BS 1480 TO 1500 MISDRILLED HOLES REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G AND SRM 53-60-53-0I FIG 1 DET VII
- [SDR FDEA202601280095](https://openairdocs.org/sdr/FDEA202601280095.md): Skin · dented · Jan 28, 2026 · N903FD · Boeing 7572B7 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 TWO DENTS, APPLIED PERMANENT REPAIR AT UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 IAW SRM 53-80-01-1A, FIG 101, SHEET 2, NOTE C, & SRM 51-70-10-2R.
- [SDR FDEA202601190068](https://openairdocs.org/sdr/FDEA202601190068.md): Skin · corroded · Jan 19, 2026 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 134.76 CORRODED. THIS ITEM HAS BEEN ACCOMPLISHED ON EA # F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATES/PANELS- # 2 PYLON O/B SIDE SKIN-EXISTING REPAIR DOUBLER BETWEEN PP STA 174-190, WITH
- [SDR FDEA202601190067](https://openairdocs.org/sdr/FDEA202601190067.md): Skin · corroded · Jan 19, 2026 · N903FD · Boeing 7572B7 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 200.50 SUSPECTED CORROSION. ACCOMPLISHED ON EA F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATES/PANELS # 2 PYLON O/B SIDE SKIN-EXISTING REPAIR DOUBLER BETWEEN PP STA 174- 190, WITH CORROSION
- [SDR FDEA202512162256](https://openairdocs.org/sdr/FDEA202512162256.md): Battery Pack · no test · Dec 16, 2025 · N903FD · Boeing 7572B7 · Emergency Lighting
  > L1 EMERGENCY EXIT LIGHT FAILS TO TEST DURING PRE-FLT. REMOVED AND REPLACED THE BATTERY PACK FOR THE L 1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-07-2 EMERGENCY EXIT LIGHT TEST NORMAL. BATTERY PACK RADIANT POWER CORP.
- [SDR FDEA202508261543](https://openairdocs.org/sdr/FDEA202508261543.md): Battery · inoperative · Aug 26, 2025 · N903FD · Boeing 7572B7 · Emergency Lighting
  > DURING MX PRE-FLIGHT FOUND OVERHEAD EMERGENCY LIGHTS AT CENTER, AND R1 DOOR AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE BATTERY FOR OVER AN HOUR, NO FIX. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY (M730) AS PER ABOVE REF. ALL LIGHTS NOW WORKING.
- [SDR FDEA202501090040](https://openairdocs.org/sdr/FDEA202501090040.md): Transmission · failed · Jan 9, 2025 · N903FD · Boeing 7572B7 · Trailing Edge Flap Actuator
  > TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 1 ON APPROACH. FOLLOWED QRH. LANDING UNEVENTFUL. FOLLOWING FIM FOUND ON THE INBOARD UNIT OF THE INBOARD FLAP ON THE LEFT WING OIL IN BAD TEXTURE AND COLOR. REMOVED LT INBOARD TRANSMISSION IAW
- [SDR FDEA202501080037](https://openairdocs.org/sdr/FDEA202501080037.md): Indication Sys · malfunctioned · Jan 8, 2025 · N903FD · Boeing 7572B7 · Trailing Flap Position Indicating System
  > TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 1 ON APPROACH. FOLLOWED QRH. LANDING UNEVENTFUL. PERFORMED OPERATIONAL TEST OF TRAILING EDGE FLAP SYSTEM PER AMM 27-51-00-5. ALL TEST PASSED, NO CURRENT FAULT IN ANY FSEU, NO HISTORY. A/C OK
- [SDR FDEA202407151020](https://openairdocs.org/sdr/FDEA202407151020.md): Indicator · inoperative · Jul 15, 2024 · N903FD · Boeing 7572B7 · Fuel Quantity Indicator
  > OVERHEAD FUEL COUNTER (LEFT TANK) AND TOTALIZER WENT BLANK DURING THE FLIGHT. IT CAME BACK ON AFTER 15 MINUTES WHILE IN FINAL APPROACH. PERFORMED FIM 28-41 FAULT TREE 854, NO FAULT FOUND. A/C OK FOR SERVICE.
- [SDR FDEA202407120987](https://openairdocs.org/sdr/FDEA202407120987.md): Connector · dirty · Jul 12, 2024 · N903FD · Boeing 7572B7 · Engine Exhaust System Wiring
  > NOTICED RIGHT ENGINE AMBER REV MESSAGE IN FLIGHT. COMPLIED WITH QRH REVERSER UNLOCKED CHECKLIST. REVERSERS OPERATED NORMALLY ON LANDING. AFTER STOWING AMBER REV MESSAGE REMAINS ON RIGHT ENGINE. WITH WDM 78-36-22 AND 71-51-22, PERFORMED RESISTANCE CHECK WIR
- [SDR FDEA202305270965](https://openairdocs.org/sdr/FDEA202305270965.md): Unknown · unknown · May 27, 2023 · N903FD · Boeing 757200 · Emergency Equipment
  > DURING SVC CHECK FOUND AED DEFIBRILATOR WITH RED "X" INSIDE WINDOW. FACT 27MAY23 00:48 CDG U AMM: 25-60-99-2 DURING TS, FOUND AED BATTERY MISSPLACE. REINSTALLED BATTERY IAW AMM 25-60-99-2 AND PERFORMED INSPECTION IAW AMM 25-60-99-2 AND SYSTEM
- [SDR FDEA202305100870](https://openairdocs.org/sdr/FDEA202305100870.md): Extinguisher · inoperative · May 10, 2023 · N903FD · Boeing 757200 · Fire Bottle, Portable
  > DURING OFFLOADING, DG CONTAINERS HAS BEEN PULLED OUT WITH FIRE EXTINGUISHER HOSES CONNECTED, RESULTING TO BROKE FIRE EXTINGUISHER RIGID LINE. BOTH MAIN DECK DG FIRE EXTINGUISHERS - REMOVED/INOP. EA F-2622-T0374370. APPLICATION EA #F-2622-T03
- [SDR FDEA202204010985](https://openairdocs.org/sdr/FDEA202204010985.md): None · corroded · Apr 1, 2022 · N903FD · Boeing 757200 · Fuselage Main, Structure
  > LOWER FUSELAGE - FRAME ATTACHED OUTER CHORD CORRODED, AT STA1380, BETWEEN STGR27RH AND STGR29RH COMPLIED WITH FEDEX EA: F-5310-T0367786 PT1, EA TITLE: FUSELAGE - MAINFRAME - STA 1380 FRAME OUTER CHORD PARTIAL REPLACEMENT AND SPLICE REPAIR BETWEEN S-26R A
- [SDR FDEA202203290979](https://openairdocs.org/sdr/FDEA202203290979.md): Seat Track · corroded · Mar 29, 2022 · N903FD · Boeing 757200 · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - SEAT TRACK CORRODED, BETWEEN STA1600 AND STA1620, LBL60 REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - SEAT TRACK, BETWEEN STA1600 AND STA1620, LBL60 PER B757 SRM53-00-52-2R REPAIR 1. THIS IS CATEGORY A
- [SDR FDEA202203280984](https://openairdocs.org/sdr/FDEA202203280984.md): Drag Fitting · cracked · Mar 28, 2022 · N903FD · Boeing 757200 · Wing, Attach Fittings
  > RH WING - OUTER WING - UPPER SKIN, DRAG FITTINGS AND DIAGONAL BRACE FASTENER AND SHIM INSPECTIONS, OPEN-HOLE HFEC INSPECTION FOUND HOLE #17 WITH CRACK SIGNAL COMPLIED WITH FEDEX EA: F-5740-T0367865 PT1, EA TITLE: WINGS - PLATES AND SKINS - RH WING DRAG FIT
- [SDR FDEA202203280977](https://openairdocs.org/sdr/FDEA202203280977.md): Drag Fitting · cracked · Mar 28, 2022 · N903FD · Boeing 757200 · Wing, Attach Fittings
  > RH WING - OUTER WING - UPPER SKIN, DRAG FITTINGS AND DIAGONAL BRACE FASTENER AND SHIM INSPECTIONS, OPEN-HOLE HFEC INSPECTION FOUND HOLE #2 WITH CRACK SIGNAL COMPLIED WITH FEDEX EA: F-5740-T0367865 PT1, EA TITLE: WINGS - PLATES AND SKINS - RH WING DRAG FITT
- [SDR FDEA202201180102](https://openairdocs.org/sdr/FDEA202201180102.md): Switch · failed · Jan 18, 2022 · N903FD · Boeing 757200 · Central Warning
  > PDIS 903 31-50 4225 18JAN22 CGN FACT U RTO AT 65KTS FOR MASTER WARNING WITH SPEED BRAKES ON EICAS R/R'D SPEEDBRAKE HANDLE POSITION SWITCH S493 IAW AMM 31-51-03-4 TESTED SATIS AC OK FOR SERVICE
- [SDR FDEA202201120101](https://openairdocs.org/sdr/FDEA202201120101.md): None · failed · Jan 12, 2022 · N903FD · Boeing 757200 · Central Warning
  > PDIS 903 31-50 4215 12JAN22 MUC FACT U ON INITIAL T/O, UPON TAKEOFF THRUST ADVANCE, MASTER WARNING ILLUMINATED. NO OTHER INDICATIONS. MASTER WARNING WILL NOT RESET. REJECT INITIATED AT 30 KTS REF TSI 31-50/4218 REMOVED AND REPLACED MASTER W
- [SDR FDEA202112173101](https://openairdocs.org/sdr/FDEA202112173101.md): Flap System · faulted · Dec 17, 2021 · N903FD · Boeing 7572B7 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE MESSAGE WHEN SELECTING FLAPS 25 ON APPROACH. EXECUTED MISSED APPROACH AND COMPLIED WITH QRH. LANDED WITH FLAPS 20 DEGREES. BITE TEST ALL 3 PSEU'S REF FIM 27-51 FT805. NO FAULT FOUND EXCEPT FLAP DISAGREE ON PSEU #1. FOUND RIGHT OUTBOARD FL
- [SDR FDEA202112032983](https://openairdocs.org/sdr/FDEA202112032983.md): None · none · Dec 3, 2021 · N903FD · Boeing 757200 · Emergency Equipment
  > PDIS 903 25-60 4081 03DEC21 BSL FACT U AFTER LANDING DISCOVERED THAT THE RIGHT EXIT DOOR SLIDE LIGHT WAS INOP. FOUND INDICATOR LIGHT BULBS BURNED, REPLACED ACC WDM 25-66-11 PAGE: 1 SHEET: 1 REV58
- [SDR FDEA202109152312](https://openairdocs.org/sdr/FDEA202109152312.md): Lamp · inoperative · Sep 15, 2021 · N903FD · Boeing 7572B7 · Emergency Lighting
  > UNARMED LIGHT OF EMERGENCY POWER SWITCH LAMPS U/S AMM: 33-16-02-2 EMERGENCY UNARMED LIGHT LAMPS REMOVED AND REPLACED. FUNCTION OK. MAINT. ALERT #20-0120 OBSERVED. PER GMM 12-7-600 PART NAME LAMP, MPN 387 (2EA), SN N/A.
- [SDR FDEA202106151540](https://openairdocs.org/sdr/FDEA202106151540.md): Probe · dirty · Jun 15, 2021 · N903FD · Boeing 7572B7 · Fuel Controlling System
  > ON CLIMB OUT L ENGINE EGT WAS AT MAX LIMIT AS WELL AS N2. FUEL FLOW ON LEFT ENGINE WAS DOUBLE RIGHT SIDE. DECLARED EMERGENCY, PERFORMED QRH PROCEDURES AND RETURNED TO CDG. INSPECTED P1 PROBE AND FOUND DEBRIS STUCK INSIDE. DISCONNECTED P1 AIR TUBES AT
- [SDR FDEA202103270788](https://openairdocs.org/sdr/FDEA202103270788.md): Wire · disconnected · Mar 27, 2021 · N903FD · Boeing 7572B7 · Light System Wiring
  > MDIS 903 33-50 3354 27MAR21 MUC OPEN U INTERIOR EMERGENCY LIGHT COURIER AREA (L26) INOP FACT 30MAR21 17:46 CDG FOUND WIRE #2 DISCONNECTED FROM EMEGENCY LIGHPLATE. WIRE CONNECTED IAW SWPM. SWPM. FOUND 10 BULBS INOP. BULBS REPLACED IAW AMM 3
- [SDR FDEA202009212285](https://openairdocs.org/sdr/FDEA202009212285.md): Handle · gouged · Sep 21, 2020 · N903FD · Boeing 7572B7 · Cargo/Baggage Doors
  > FWD CARGO DOOR HANDLE HAS GOUGE ON INNER SURFACE. REPAIRED FWD CARGO DOOR HANDLE GOUGE, IAW FEDEX EA F-5230-T3056468 P1 TITLE: DOORS-CARGO DOOR/HYD SYS-NO 1 CARGO DOOR EXTERIOR HANDLE REPAIR.
- [SDR FDEA202009112234](https://openairdocs.org/sdr/FDEA202009112234.md): Strap · damaged · Sep 11, 2020 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > FLOOR BEAM STABILIZER STRAP AT BSTA 377.7 LBL 24.75 IS DAMAGED. REPAIRED FLOOR BEAM STABILIZER STRAP AT BSTA 377.7 LBL 24.75, IAW SRM 53-00-51-2R REPAIR 12.
- [SDR FDEA202009102235](https://openairdocs.org/sdr/FDEA202009102235.md): Strap · damaged · Sep 10, 2020 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > UPON CLOSE UP INSP FOUND STABILIZER STRAP AT BSTA 580 LBL 24 DAMAGE ON LOWER SIDE OF FLOOR BEAMS REPAIRED STABILIZER STRAP AT BSTA 580 LBL 24, IAW SRM 53-00-51-2R REPAIR 12.
- [SDR FDEA202009092361](https://openairdocs.org/sdr/FDEA202009092361.md): Panel · cracked · Sep 9, 2020 · N903FD · Boeing 7572B7 · Wing, Plate/Skin
  > '9 LEADING EDGE COVE PANEL CRACKED OUTBOARD OF INBOARD MAIN TRACK. FABRICATED NEW COVE PANEL P/N 114N4076-18, IAW BOEING DRAWING 114N4003 AND FEDEX GMM 7-0-1001. NEW PANEL INSTALLED, IAW SRM 51-40-02 AND BOEING DRAWING 114N4003.
- [SDR FDEA202009072283](https://openairdocs.org/sdr/FDEA202009072283.md): Bracket · broken · Sep 7, 2020 · N903FD · Boeing 7572B7 · Service Doors
  > BRACKET FOUND DAMAGED ON FWD SIDE OF DOOR 3R SECOND FROM TOP FABRICATED BRACKET FROM DOOR 3R SECOND FROM TOP, IAW FEDEX GMM 7-0-1001 AND BOEING DRAWING 411N2035. BRACKET INSTALLED ON DOOR 3R, IAW SRM 51-40-02. PART MARKED BRACKET WITH FX411N2035-4, IAW GMM
- [SDR FDEA201811263393](https://openairdocs.org/sdr/FDEA201811263393.md): Circuit Breaker · tripped · Nov 26, 2018 · N903FD · Boeing 7572B7 · Landing Gear Retraction/Extension System
  > AFTER TROUBLE SHOOTING FINISHED THE LDG ALT EXT C/B POPPED OUT AGAIN DURING T/S FOUND "ALT GEAR EXTENSION CONT" C/B FAULT, C/B SWAPPED CB C41177 WITH CB C00773, P006-01//H006 CB-BTL 2 CARGO FIRE EXTINGUISHING T/S REF
- [SDR FDEA2018091432511](https://openairdocs.org/sdr/FDEA2018091432511.md): Skin · worn · Sep 13, 2018 · N903FD · Boeing 7572B7 · Trailing Edge Flaps
  > RT MAIN FLAP TOP SURFACE HAS 2 WEAR MARKS OPPOSITE NR 10 SPOILER ACTUATOR. REPLACED DAMAGED REPAIR PLATE ON RT MAIN FLAP TOP SURFACE IAW SRM 57-53-01-2R REPAIR 2 FIG 201 REV 124
- [SDR FDEA2018091432492](https://openairdocs.org/sdr/FDEA2018091432492.md): Strap · corroded · Sep 13, 2018 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > INTERCOSTAL STRAP PUNCTURED AND CORRODED AT BS 1020 BETWEEN RBL 25 AND RBL 45. PUNCTURE DAMAGE IS NOT ALLOWED AS PER SRM 53-00-51-1A FIG 101 REV 124. FABRICATED NEW INTERCOSTAL STRAP IAW GMM 7-0-1001 REV 150 AND DRAWING 144N5081 SHEET 1 REV A INSTALLED NEW STR
- [SDR FDEA2018091432491](https://openairdocs.org/sdr/FDEA2018091432491.md): Bracket · cracked · Sep 13, 2018 · N903FD · Boeing 7572B7 · Trailing Edge Flaps
  > RT OB FLAP OB TOP TO LWR SKIN AFT BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET IAW GMM 7-00-1001 REV 150 AND DRAWING 113N3370 SHEET 2 REV C AND SRM 51-30-01 AND 51-40-02 REV 124.
- [SDR FDEA2018091432490](https://openairdocs.org/sdr/FDEA2018091432490.md): Frame · damaged · Sep 13, 2018 · N903FD · Boeing 7572B7 · Fuselage Main, Frame
  > FRAME 231.25 AT FWD E&E BAY DOOR HAS STRUCTURAL DAMAGE. PERFORMED REPAIR TO FRAME 231.25 IAW SRM 53-00-07-2R FIG 202 REV 125.
- [SDR FDEA2018091432489](https://openairdocs.org/sdr/FDEA2018091432489.md): Support Bracket · corroded · Sep 13, 2018 · N903FD · Boeing 7572B7 · Aerodynamic Fairings
  > TOP LT WING WTB PANEL SUPPORT NR 4 FROM FWD REQUIRES EVALUATION AND REPROTECTION. FABRICATED WTB PANEL SUPPORT BRACKETS IAW DRAWING 149N7210 SHEET 7 REV B AND GMM 7-0-1001 USING MATERIAL 7075-T0 0.080" BN 017135193. INSTALLED BRACKETS IAW SRM 51-40-02 REV 124.
- [SDR FDEA2018091432488](https://openairdocs.org/sdr/FDEA2018091432488.md): Strip · corroded · Sep 13, 2018 · N903FD · Boeing 7572B7 · Elevator Miscellaneous Structure
  > LT ELEVATOR TIP UPPER AND LOWER STATIC DISCHARGE STRIP HAS SUSPECT CORROSION UNDERNEATH. UPON EVALUATION, BOTH STATIC DISCHARGE STRIPS FOUND TO BE OUT OF LIMITS IAW SRM 55-20-01 FIG 101 TABLE 1 REV124. FABRICATED NEW DISCHARGE STRIPS IAW DRAWING 183N2901 AND G
- [SDR FDEA2018091412454](https://openairdocs.org/sdr/FDEA2018091412454.md): Floorbeam · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL 58- RBL 58 BS 1200. FLOORBEAM FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51-1A FIG 101 DETAILIII REV 124 ON SNRMS N00331, N00332, N00333, N00334, N00330. REPAIR CARRIED OUT IAW SRM 53-00-51-2R REPAIR 9 REV 124.
- [SDR FDEA201809112443](https://openairdocs.org/sdr/FDEA201809112443.md): Seat Track · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK AT BS 900-1180 RBL 58. CORROSION DAMAGE ON SEAT TRACK RBL 58 BSTA 900-1180 OUT OF LIMITS IAW SRM 53-00-52-1A REV 124. SEAT TRACK SECTION REPAIRED IAW SRM 53-00-52-2R REPAIR 1 OPTION 1 REV 124.
- [SDR FDEA201809112453](https://openairdocs.org/sdr/FDEA201809112453.md): Seat Track · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 58 BSTA 900-1060. REMOVED AND EVALUATED CORROSION ON SEAT TRACK LBL58 BSTA 900-1070 IAW SRM: 53- 00-52-1A ALLOWABLE DAMAGE 1 FIG 101 REV 124 SHEET 4 DETAIL VII AND DETAIL VIII AND FOUND TO BE OUTSIDE OF LIMITS. ALLOWABLE MATERIAL R
- [SDR FDEA201809112452](https://openairdocs.org/sdr/FDEA201809112452.md): Seat Track · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 58 BSTA 1100-1180. REMOVED AND EVALUATED CORROSION ON SEAT TRACK LBL58 BSTA 1100-1180 IAW SRM 53- 00-52-1A ALLOWABLE DAMAGE 1 FIG 101 REV 124 SHEET 4 DETAIL VII AND DETAIL VIII AND FOUND TO BE OUTSIDE LIMITS. ALLOWABLE MATERIAL REM
- [SDR FDEA201809112451](https://openairdocs.org/sdr/FDEA201809112451.md): Skin · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Wing, Plate/Skin
  > BONDING FUNCTIONAL TEST OF LEFT WING TANK OVERFILL PORT FAILED TEST. UPON EVALUATION, CORROSION FOUND ON SURFACE OF THE UPPER SKIN AT THE OVERWING FILL PORT. REPAIR CARRIED OUT IAW EA F-5730-T0341901.
- [SDR FDEA201809112449](https://openairdocs.org/sdr/FDEA201809112449.md): Intercostal · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT BS 1020 LBL 0 TO LBL 25. CORROSION ON INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A FIG 101 DETAIL II REV 124. ORIGINAL MATERIAL GAUGE= 0.050" DEPTH OF BLENDOUT= 0.013" MAX ALLOWABLE = 0.005". FABRICATED AND INSTALLED N
- [SDR FDEA201809112448](https://openairdocs.org/sdr/FDEA201809112448.md): Intercostal · corroded · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT BS 1020 RBL 0 - RBL25. CORROSION ON INTERCOSTAL FOUND TO BE OUTSIDE OF LIMITS IAW SRM 53-00-04-1A FIG 101 DETAIL II REV 124. ORIGINAL MATERIAL GAUGE= 0.050" DEPTH OF BLENDOUT= 0.012" MAX ALLOWABLE= 0.005". FABRICATED AND INSTALLED
- [SDR FDEA201809112444](https://openairdocs.org/sdr/FDEA201809112444.md): Strap · damaged · Sep 11, 2018 · N903FD · Boeing 7572B7 · Fuselage Miscellaneous Structure
  > INTERCOSTAL STRAP PUNCTURED AND CORRODED AT BS 1020 BETWEEN LBL 25-45. PUNCTURE DAMAGE NOT ALLOWED AS PER SRM 53-00-51-1A FIG 101 REV 124. FABRICATED NEW INTERCOSTAL STRAP IAW GMM 7-0-1001 REV 150 AND DRAWING NR 144N5081 SHEET 1 REV A. INSTALLED NEW STRAP IAW

Next page: https://openairdocs.org/aircraft/N903FD/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 = 'N903FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N903FD/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.