# Service difficulty reports: N728FD

A list on [N728FD](https://openairdocs.org/aircraft/N728FD.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 6 · 266 reports

- [SDR FDEA202510192053](https://openairdocs.org/sdr/FDEA202510192053.md): Skin · cracked · Oct 19, 2025 · N728FD · Airbus A300B4622R · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR UPPER INNER SKIN 2EA CRACKS WERE FOUND AT FR61 - FR62 COMPLIED WITH EA 6-5230-T0385399 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - AFT CARGO DOOR INNER SKINS AND ACTUATOR FITTING AT FR61A - CRACKS, PERMANENT REPAIR. REPAIRED AFT CARG
- [SDR FDEA202510192052](https://openairdocs.org/sdr/FDEA202510192052.md): Fitting · cracked · Oct 19, 2025 · N728FD · Airbus A300B4622R · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR ACTUATOR FITTING CRACKED
- [SDR FDEA202510172038](https://openairdocs.org/sdr/FDEA202510172038.md): Floorbeam · corroded · Oct 17, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT FLOOR SUPPORT BEAM CORRODED AT FR29 Y-1470 REPAIRED THE FWD CARGO COMPARTMENT CORRODED FLOOR SUPPORT BEAM AT FR29 Y-1470 PER A300-600 SRM53-10-15-201 FIGURE 207 AND EA: 6-5321-T0385349 P1. TITLE: FUSELAGE - CARGO COMP FLOOR - FWD CAR
- [SDR FDEA202510172037](https://openairdocs.org/sdr/FDEA202510172037.md): Roller Track · corroded · Oct 17, 2025 · N728FD · Airbus A300B4622R · Cargo Compartments
  > FWD CARGO COMPARTMENT LOADING SYS TRACK CORRODED AT FR38.1 - FR38.2 Y140 REPAIRED THE FWD CARGO COMPARTMENT CORRODED LOADING SYS TRACK AT FR38.1 - FR38.2 Y140 PER A300-600 SRM53-10-15-201 FIG.203. THIS IS CAT A REPAIR, MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202510152008](https://openairdocs.org/sdr/FDEA202510152008.md): Frame · cracked · Oct 15, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT INSPECTION, LT SIDE FUSELAGE FRAME FR73A ONE RIVET HOLE CRACKED AT S24L - S25L REPAIRED LH DOOR FRAME FR73A RIVET HOLE AT STGR24 - STGR25.THIS IS CATEGORY B REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 53100887 FOR WORK DETAILS.
- [SDR FDEA202510152007](https://openairdocs.org/sdr/FDEA202510152007.md): Frame · cracked · Oct 15, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, Frame
  > NDT INSP - RH SIDE FUSELAGE FRAME FR73A 1EA RIVET HOLE CRACKED AT STGR24 - STGR25 COMPLIED WITH EA:6-5310-T0385324 P1,TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH & RH DOOR FRAME FR73A - SPLICE REPAIR PE
- [SDR FDEA202510141980](https://openairdocs.org/sdr/FDEA202510141980.md): Hinge Arm · delaminated · Oct 14, 2025 · N728FD · Airbus A300B4622R · Spoilers
  > RH WING - #4 SPOILER INBD HINGE ARM INBD SIDE AND OTBD HIINGE ARM OUTBD SIDE DELAMINATED. 1.80MM*40MM*1.55MM 2.90MM*40MM*1.45MM. COMPLIED WITH EA 6-5750-T0319441 P2. TITLE: WINGS - FLIGHT SURFACES - RH #4 SPOILER LOWER SKIN REPAIR - OUTSIDE CENTER HINGE A
- [SDR FDEA202510141979](https://openairdocs.org/sdr/FDEA202510141979.md): Hinge Arm · delaminated · Oct 14, 2025 · N728FD · Airbus A300B4622R · Spoilers
  > RH WING - #3 SPOILER INBD HINGE ARM INBD SIDE AND OUTBD HINGE ARM OUTBD SIDE DELAMINATED.1.80MM*15MM*0.92MM 2.30MM*25MM*1.09MM 3.25MM*18MM*0.96MM
- [SDR FDEA202510141978](https://openairdocs.org/sdr/FDEA202510141978.md): Hinge Arm · delaminated · Oct 14, 2025 · N728FD · Airbus A300B4622R · Leading Edge Devices
  > LH WING - NR 3 SPOILER OUTBD HINGE ARM OUTBD SIDE AND INBD HINGE ARM INBD SIDE DELAMINATED. 1.65MM, 820MM, 81.38MM, 2.100, MM, 20MM, 1.73MM. COMPLIED WITH EA 6-5750-T0385295 P1. REPAIRED THE LH WING #3 SPOILER OTBD HINGE ARM OTBD SIDE & INBD HINGE ARM OTBD
- [SDR FDEA202510141977](https://openairdocs.org/sdr/FDEA202510141977.md): Hinge Arm · delaminated · Oct 14, 2025 · N728FD · Airbus A300B4622R · Spoilers
  > LEFT WNG - #5 SPOILER OUTBD HINGE ARM OUTBD SIDE DELAMINATED. 80MM*20MM*1.62MM COMPLIED WITH EA 6-5750-T0385306 P1. TITLE: WINGS - FLIGHT SURFACES - LH #5 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WING #5 SPOILER OUTBD HINGE A
- [SDR FDEA202510131975](https://openairdocs.org/sdr/FDEA202510131975.md): Floorbeam · corroded · Oct 13, 2025 · N728FD · Airbus A300B4622R · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT FLOOR SUPPORT BEAM CORRODED AT FR58 Y-805 - Y-1470 REPAIRED THE AFT CARGO COMPARTMENT CORRODED FLOOR SUPPORT BEAM AT FR58 Y-805 - Y- 1470 PER A300-600 SRM53-10-15-201 FIGURE 207 AND EA: 6-5321-T0385357 P1. TITLE: FUSELAGE - CARGO COMP
- [SDR FDEA202510091931](https://openairdocs.org/sdr/FDEA202510091931.md): Fitting · not reported · Oct 9, 2025 · N728FD · Airbus A300B4622R · Cargo/Baggage Doors
  > COMPLY WITH: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016- 24. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VIS
- [SDR FDEA202510091930](https://openairdocs.org/sdr/FDEA202510091930.md): Skin · contaminated · Oct 9, 2025 · N728FD · Airbus A300B4622R · Elevator, Plate/Skin
  > LEFT ELEVATOR TOP SKIN AT ER13 FOUND WATER INJECTED. REPAIRED LH ELEVATOR TOP SKIN AT ER13 FOUND WATER INJECTED PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201 & EA 6-5520-T0385455 P1. EA TITLE: STABILIZERS - ELEVATORS - LH ELEVATOR UPPER SKIN REP
- [SDR FDEA202510091929](https://openairdocs.org/sdr/FDEA202510091929.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - LH WING CENTER FLAP INNER STRUCTURE RIB25/STGR2.8 - REAR SPAR,RIB26/STGR2.6-2.7,RIB26/STGR2.7-2.8,RIB27/STGR2.7-2.8,RIB27/STGR2.8-REAR SPAR TOTAL OF 5 CRACKS FOUND. REPAIRED THE CRACKED RIB UPR FLANGE AT LH WING CENTER FLAP RIB25/STGR2.8 - REA
- [SDR FDEA202510091928](https://openairdocs.org/sdr/FDEA202510091928.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - LH WING CENTER FLAP INNER STRUCTURE RIB18/STGR2.8 - REAR SPAR 1EA CRACK WAS FOUND. COMPLIED WITH EA: 6-5750-T0319244 P2, TITLE: WINGS - FLIGHT SURFACES - LHS CENTER FLAP RIB 18 CRACKED AT UPPER FLANGE BETWEEN STGR2.8 AND REAR SPAR. REPAIRED THE
- [SDR FDEA202510091927](https://openairdocs.org/sdr/FDEA202510091927.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - LT WING CENTER FLAP INNER STRUCTURE 1EA CRACK WAS FOUND RIB11/STGR2.7 - 2.8 COMPLIED WITH EA: 6-5750-T0337526 P2. TITLE: WINGS - FLIGHT SURFACES - LHW, CENTER FLAP, SKIN AND RIB REPAIRS PER SRM - RSC TRACKING. REPAIRED THE LH WING CENTER FLAP INNER
- [SDR FDEA202510091926](https://openairdocs.org/sdr/FDEA202510091926.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 1EA CRACK AT RIB17 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB17 BETWEEN STGR2.8 AND REAR SPAR. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-
- [SDR FDEA202510091925](https://openairdocs.org/sdr/FDEA202510091925.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 1EA CRACK AT RIB11 & RIB12 & RIB13 & RIB15 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB11 & RIB12 & RIB15 BETWEEN STGR2.8 AND REAR SPAR,RIB13 BETWEEN STGR2
- [SDR FDEA202510091924](https://openairdocs.org/sdr/FDEA202510091924.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - RH WING CENTER FLAP RIBS UPR FLANGE FOUND 4EA CRACK AT RIB19 BETWEENSTGR2.6 AND REAR SPAR,RIB20 B/W STGR2.8 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RT WING CENTER FLAP RIB19 BETWEEN STGR2.6 AND REAR SPAR,RIB20 BETWEEN STGR2.8 AND
- [SDR FDEA202510091923](https://openairdocs.org/sdr/FDEA202510091923.md): Rib · cracked · Oct 9, 2025 · N728FD · Airbus A300B4622R · Trailing Edge Flaps
  > NDT INSP - RT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACK AT RIB26 BETWEEN STGR2.6 AND REAR SPAR. REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING CENTER FLAP RIB26 BETWEEN STGR2.6 AND REAR SPAR. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202306141129](https://openairdocs.org/sdr/FDEA202306141129.md): Bracket · cracked · Jun 14, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT CENTERLINE FR54 POSITION. REPLACED THE NEW BRACKET. I.A.W A300-600 SRM 51-72-10-001,P2.
- [SDR FDEA202306131085](https://openairdocs.org/sdr/FDEA202306131085.md): Profile · cracked · Jun 13, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT MAIN DECK UTILITY FLOOR LEVEL AREA FOUND Z PROFILE CRACKED AT FR80 AND Y1470 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2
- [SDR FDEA202306131084](https://openairdocs.org/sdr/FDEA202306131084.md): Profile · cracked · Jun 13, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT MAIN DECK UTILITY FLOOR LEVEL AREA FOUND Z PROFILE CRACKED AT FR80 AND Y-1470 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2
- [SDR FDEA202306121107](https://openairdocs.org/sdr/FDEA202306121107.md): Elevator · unknown · Jun 12, 2023 · N728FD · Airbus A300* · Elevator Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER10 12", T/E-5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202306121106](https://openairdocs.org/sdr/FDEA202306121106.md): Elevator · unknown · Jun 12, 2023 · N728FD · Airbus A300* · Elevator Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER7 23", T/E-5.5" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENT
- [SDR FDEA202306121105](https://openairdocs.org/sdr/FDEA202306121105.md): Elevator · unknown · Jun 12, 2023 · N728FD · Airbus A300* · Elevator Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER5, T/E-4" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
- [SDR FDEA202306121104](https://openairdocs.org/sdr/FDEA202306121104.md): Elevator · unknown · Jun 12, 2023 · N728FD · Airbus A300* · Elevator Structure
  > AGING AIRCRAFT ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR LWR SKIN AT ER2 18", T/E-6" POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS
- [SDR FDEA202306111108](https://openairdocs.org/sdr/FDEA202306111108.md): Stringer · unknown · Jun 11, 2023 · N728FD · Airbus A300* · Fuselage Main, Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR 36~37, STGR 33L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707,
- [SDR FDEA202306101196](https://openairdocs.org/sdr/FDEA202306101196.md): Spoiler · damaged · Jun 10, 2023 · N728FD · Airbus A300* · Spoilers
  > RH WING #2 SPOILER FRONT SPAR FITTING O/B SIDE GOT A PUNCTURED CUT OUT AND INSTALLED WITH REPAIR PARTS I.A.W FEDEX EA NO:T6-5750-T0374908 P1, SEQ NO:966, TITLE:WING-FLIGHT SURFACES-RH #2 SPOILER-WEAR DAMAGE AND MATERIAL TEAR-OUT AT OUTBD FACE OF FRONT SPAR
- [SDR FDEA202306101175](https://openairdocs.org/sdr/FDEA202306101175.md): Angle · corroded · Jun 10, 2023 · N728FD · Airbus A300* · Fuselage Main, Attach Fittings
  > THE SHIELD SUPPORT PLATE OF FWD BULKHEAD WAS FOUND CORROSION JUST ABOVE THE RADAR MOUNT UPPER RH SIDE FABRICATED AND INSTALLED NEW PART I.A.W FEDEX EA NO:T6-5340-T0375002 P1, SEQ NO:962, TITLE:FUSELAGE-ATTACH FITTINGS-FWD PRESSURE BULKHEAD-RADAR ANTENNA UP
- [SDR FDEA202306091179](https://openairdocs.org/sdr/FDEA202306091179.md): Splice · corroded · Jun 9, 2023 · N728FD · Airbus A300* · Fuselage Main, Structure
  > AVIONICS COMP'T BILGE STRUCTURE OF SPLICE GOT CORRODED AT FR19,STGR-52L POSITION REPLACED THE CORRODED SPLICE WITH NEW PART I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~23
- [SDR FDEA202306091125](https://openairdocs.org/sdr/FDEA202306091125.md): Angle · cracked · Jun 9, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AVIONICS COMP'T FLOOR BEAM ANGLE FITTING CRACK AT FR10,Y403 POSITION. REPLACED THE NEW ANGLE. I.A.W A300-600 SRM 51-72-10-001, P.2
- [SDR FDEA202306091086](https://openairdocs.org/sdr/FDEA202306091086.md): Seat Track · unknown · Jun 9, 2023 · N728FD · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AGING AIRCRAFT ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 62~65, -Y450 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707,
- [SDR FDEA202306081089](https://openairdocs.org/sdr/FDEA202306081089.md): Aileron · unknown · Jun 8, 2023 · N728FD · Airbus A300* · Wing, Control Surfaces
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH WING AILERON LWR SKIN BTW RIB 8~9,T/E-4" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202306081083](https://openairdocs.org/sdr/FDEA202306081083.md): Support Web · cracked · Jun 8, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT MAIN DECK UTILITY AREA FLOOR STRUCTURE 1EA SUPPORT WEB FOUND CRACK AT FR79 PLUS 6", Y-1610 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2
- [SDR FDEA202306081082](https://openairdocs.org/sdr/FDEA202306081082.md): Support Web · cracked · Jun 8, 2023 · N728FD · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT MAIN DECK UTILITY AREA FLOOR STRUCTURE 1EA SUPPORT WEB FOUND CRACK AT FR79 PLUS 6", Y1610 REPLACED THE DAMAGE PART WITH NEW. I.A.W A300-600 SRM 51-72-10-001,PAGE.2
- [SDR FDEA202306081054](https://openairdocs.org/sdr/FDEA202306081054.md): Slat · unknown · Jun 8, 2023 · N728FD · Airbus A300* · Leading Edge Devices
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING FLUSH DOUBLER REPAIR FOUND ON RH WING #1 SLAT NOSE SKIN BTW RIB 19~JACK RIB 2 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREME
- [SDR FDEA202306081053](https://openairdocs.org/sdr/FDEA202306081053.md): Flap · unknown · Jun 8, 2023 · N728FD · Airbus A300* · Trailing Edge Flaps
  > AGING AIRCRAFT ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW STGR 2.8~2.9,RIB 10~11 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14
- [SDR FDEA202306081052](https://openairdocs.org/sdr/FDEA202306081052.md): Flap · unknown · Jun 8, 2023 · N728FD · Airbus A300* · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPR SKIN BTW STGR 2.1~2.2,RIB 5~9 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 C
- [SDR FDEA202306081051](https://openairdocs.org/sdr/FDEA202306081051.md): Flap · unknown · Jun 8, 2023 · N728FD · Airbus A300* · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 19~19A,T/E-12" COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202306071046](https://openairdocs.org/sdr/FDEA202306071046.md): Rudder · corroded · Jun 7, 2023 · N728FD · Airbus A300* · Rudder Structure
  > RUDDER T/E APEX STRIP CORROSION AT STA.470 AREA PFM APEX STRIP REPAIR BY APEX STRIP WITH CONNECTION PLATE AND RIVETS I.A.W A300-600 SRM 55-41-12-201, PARA.16, P.237-239, FIG.208C, THIS IS CAT.B REPAIR I.A.W A300-600 SRI:55-41-12- 201, IIR:55-41-12-2-003-00,
- [SDR FDEA202306041191](https://openairdocs.org/sdr/FDEA202306041191.md): Rudder · damaged · Jun 4, 2023 · N728FD · Airbus A300* · Rudder Structure
  > 1EA WATER TRAPPED AREA(120MM*140MM) WAS FOUND AT RUDDER L/H T/E SCREW LINE NO.37 FASTENER AREA. ACCOMPLISHED THE CAT.B COMPOSITE REPAIR I.A.W FEDEX EA NO:T6-5540-T0374745 P1, SEQ NO:965, TITLE:STABILIZERS-RUDDER-LH RUDDER SHELL SCREW HOLE #37 WATER INGRE
- [SDR FDEA202306041079](https://openairdocs.org/sdr/FDEA202306041079.md): Rudder · damaged · Jun 4, 2023 · N728FD · Airbus A300* · Rudder Structure
  > 1EA WATER TRAPPED AREA(130MMX120MM) WAS FOUND AT RUDDER R/H T/E SCREW LINE NO.39 FASTENER AREA ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-41-12-201, PARA.31, PAGE.313-319, FIG.222 & SRI:55-41-12-201, IIR:55-41-12-2-006-00
- [SDR FDEA202211222827](https://openairdocs.org/sdr/FDEA202211222827.md): Warning System · intermittent · Nov 22, 2022 · N728FD · Airbus A300B4622R · Door Warning System
  > MDIS 728 52-70 7660 22NOV22 SAN OPEN U DURING PREFLIGHT L1 AND R 1 DOORS SLIDE RELEASE WARNING LIGHTS INOP - BUZZERS TEST O.K. MEL 22NOV22 04:52 SAN U RELEASED FOR SERVICE PER MEL: 52-73-01-01 CATEGORY: C EXPIRATION: 02DEC22 "MEL 52-73
- [SDR FDEA202211172803](https://openairdocs.org/sdr/FDEA202211172803.md): Floorboard · damaged · Nov 17, 2022 · N728FD · Airbus A300B4622R · Fuselage Floor Panel
  > RAMP REPORTED 2 HOLES IN MAIN DECK FLOOR BS 882 & 903,JUST INBD OF CA'S SIDE LONGITUDINAL RAIL. REMOVED FLOORBOARD AT 13L ON MAIN DECK. IAW SRM 53-10-20 REMOVED DAMAGE TO FLOORBOARD, FABRICATED A REPAIR AND PREPPED FLOORBOARD & REPAIR IAW SRM 53-10-20, PAR
- [SDR FDEA202206151434](https://openairdocs.org/sdr/FDEA202206151434.md): Selector Valve · none · Jun 15, 2022 · N728FD · Airbus A300* · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT EXTEND. 3 RED GEAR UNSAFE ON SYSTEM 1 AND 2. LANDING GEAR WAS GRAVITY EXTENDED. T/S IAW TSM 32-30, FIGURE 113. FOUND LANDING GEAR SELECTOR VALVE 3GA INOP. REMOVED AND REPLACED 3GA REF AMM 32-31-12-04. DURING T/S'ING FOUND LANDING
- [SDR FDEA202205261307](https://openairdocs.org/sdr/FDEA202205261307.md): Seat · unknown · May 26, 2022 · N728FD · Airbus A300* · Flight Compartment Equipment
  > PDIS 728 25-10 7156 26MAY22 MEM OPEN U ON TAKEOFF ROLL, FO S SEAT CAME UNLOCKED AND SLID ALL THE WAY BACK AND OUTBOARD. ENROUTE DETERMINED THAT THE SEAT HAS A FORE/AFT LOCK POSITION THAT IS WEAK AND DOESN T FULLY LOCK WHICH ALLOWS SEAT TO MO
- [SDR FDEA202011202913](https://openairdocs.org/sdr/FDEA202011202913.md): Spar · cracked · Nov 20, 2020 · N728FD · Airbus A300B4622R · Wing Spar
  > RT WING, BASIC WING STRUCTURE FRONT AND REAR SPAR BOTTOM BOOM INBOARD AND OUTBOARD OF RIB 9 INSPECTION, FOUND W HOLE WITH CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0358209 P1. TITLE: WINGS-BASIC WING STRUCTURE-RT WING REAR SPAR BOTTOM BOOM HOLE W/558 AT RIB 9 C
- [SDR FDEA202011182897](https://openairdocs.org/sdr/FDEA202011182897.md): Structure · cracked · Nov 18, 2020 · N728FD · Airbus A300B4622R · Fuselage Main, Structure
  > CENTER WING BOX, INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION OF FUSELAGE, LT SIDE, HOLE "C" FOUND CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0357880 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK HOLE C AT FR 47 LT SIDE DURING SB57-6086 EMBODIMENT. REP
- [SDR FDEA202011182896](https://openairdocs.org/sdr/FDEA202011182896.md): Fitting · cracked · Nov 18, 2020 · N728FD · Airbus A300B4622R · Fuselage, Wing Attach Fittings
  > LT WING ROOT FWD FACE FRAME 40 FWD FITTING STGR 32-33LT FOUND CRACK COMPLIED WITH EA: 6-5710-T0358132 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK ON LT FR 40 FWD FITTING LOWER OUTBOARD RADIUS. REPAIRED THE LT WING ROOT FWD FACE- FRAME 40 FWD FITTING STGR 32

Next page: https://openairdocs.org/aircraft/N728FD/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 = 'N728FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N728FD/reports

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