# Service difficulty reports: N745FD A list on [N745FD](https://openairdocs.org/aircraft/N745FD.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 5 · 216 reports - [SDR FDEA202610211637](https://openairdocs.org/sdr/FDEA202610211637.md): Door Frame · cracked · Oct 21, 2026 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > LEFT AFT PAX DOOR FRAME AT FR 73A BTWN STR 24 & 25L FOUND ONE CRACK AROUND THE RIVET HEAD OF THE SEAL RETAINER RUNOUT HOLE. - [SDR FDEA202610191604](https://openairdocs.org/sdr/FDEA202610191604.md): Door · cracked · Oct 19, 2026 · N745FD · Airbus A300B4622R · Cargo/Baggage Doors > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23-FR24 FOUND CRACK SIGNAL ON 5EA FASTENER HOLES - [SDR FDEA202610191603](https://openairdocs.org/sdr/FDEA202610191603.md): Skin · gouged · Oct 19, 2026 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > RH WING INNER FLAP UPPER SKIN FOUND 1EA GOUGE BTW RIB4-5 - [SDR FDEA202610141565](https://openairdocs.org/sdr/FDEA202610141565.md): Floorbeam · corroded · Oct 14, 2026 · N745FD · Airbus A300B4622R · Fuselage Main, Floor Beam > BULK CARGO FLOOR SUPPORT AT FR 66, BTW Y805 AND -Y805 UPPER SURFACE FOUND HEAVY CORROSION. - [SDR FDEA202610131562](https://openairdocs.org/sdr/FDEA202610131562.md): Floorbeam · corroded · Oct 13, 2026 · N745FD · Airbus A300B4622R · Fuselage Main, Floor Beam > AFT CARGO FLOOR SUPPORT AT FR63 -Y805 LWR SURFACE FOUND CORROSION. - [SDR FDEA202503010330](https://openairdocs.org/sdr/FDEA202503010330.md): Bottle · low pressure · Mar 1, 2025 · N745FD · Airbus A300B4622R · Escape Slide > POST-FLT INSPECTION, L1 DOOR SLIDE PRESSURE INDICATION OUT OF GREEN BAND. RELEASED FOR SERVICE PER MEL: 52-11-01-01, CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIDE REMAINS INSTALLED ON DOOR." PLACED ON MEL 52-11-01-01. AIRCRAFT OKAY TO CONTINUE. REMOVED - [SDR FDEA202407191032](https://openairdocs.org/sdr/FDEA202407191032.md): Panel · contaminated · Jul 19, 2024 · N745FD · Airbus A300B4622R · Rudder, Plate/Skin > RUDDER RH SIDEPANEL STA529 AROUND HINGE #5 AREA FOUND FLUID INGRESS EVIDENCE. COMPLIED WITH EA: 6-5540-T0379793 P1 TEMPORARILY REPAIRED THE FLUID INGRESS RUDDER RH SIDEPANEL HINGE #5 AREA. TITLE: STABILIZERS - RUDDER - RH SHELL WATER INGRESS - EO 6- 5530-E - [SDR FDEA202406300892](https://openairdocs.org/sdr/FDEA202406300892.md): Rib Splice · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Wing, Rib/Bulkhead > RH WING - CENTER SPAR RIB1 SPLICE TYPE 5 UPPER HOLE FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0379800 P1 REPAIRED THE RH WING CENTER SPAR RIB1 SPLICE TYPE 5 CRACKED UPPER HOLE. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE ON FITTING RH WING CWT SPAR T - [SDR FDEA202406300891](https://openairdocs.org/sdr/FDEA202406300891.md): Fitting · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > CENTER WING BOX - REAR SPAR LOWER FLANGE FR47 LHS HOLE "D" INNER SURFACE FOUND SCRATCH COMPLIED WITH EA: 6-5710-150047 E P7 REPAIRED THE CENTER WING BOX REAR SPAR LOWER FLANGE FR47 LHS SCRATCHED AND CRACKED HOLE "D". TITLE: WINGS - CENTER WING BOX - REAR - [SDR FDEA202406300890](https://openairdocs.org/sdr/FDEA202406300890.md): Fitting · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > CENTER WING BOX - REAR SPAR LOWER FLANGE FR47 RHS HOLE "P" INNER SURFACE FOUND SCRATCH COMPLIED WITH EA: 6-5710-150047 E P7 REPAIRED THE CENTER WING BOX REAR SPAR LOWER FLANGE FR47 RHS SCRATCHED AND CRACKED HOLE "P". TITLE: WINGS - CENTER WING BOX - REAR - [SDR FDEA202406300889](https://openairdocs.org/sdr/FDEA202406300889.md): Fitting · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > CENTER WING BOX - REAR SPAR LOWER FLANGE FR47 RHS HOLE "D" INNER SURFACE FOUND SCRATCH COMPLIED WITH EA: 6-5710-150047 E P7 REPAIRED THE CENTER WING BOX REAR SPAR LOWER FLANGE FR47 RHS SCRATCHED AND CRACKED HOLE "D". TITLE: WINGS - CENTER WING BOX - REAR - [SDR FDEA202406300888](https://openairdocs.org/sdr/FDEA202406300888.md): Fitting · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > CENTER WING BOX - REAR SPAR LOWER FLANGE FR47 LHS HOLE "C" FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-150047 E P7 REPAIRED THE CENTER WING BOX REAR SPAR LOWER FLANGE FR47 LHS CRACKED HOLE "C". TITLE: WINGS - CENTER WING BOX - REAR SPAR LOWER FLANGE AT FRA - [SDR FDEA202406300887](https://openairdocs.org/sdr/FDEA202406300887.md): Fitting · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > CENTER WING BOX - REAR SPAR LOWER FLANGE FR47 RHS HOLE "G" FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-150047 E P7 REPAIRED THE CENTER WING BOX REAR SPAR LOWER FLANGE FR47 RHS CRACKED HOLE "G". TITLE: WINGS - CENTER WING BOX - REAR SPAR LOWER FLANGE AT FRA - [SDR FDEA202406300886](https://openairdocs.org/sdr/FDEA202406300886.md): Beam · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Fuselage Main, Structure > RIGHT SIDE OF LH GANTRY 5 AT FR51.A CRACK WAS FOUND (LENGTH: 11MM). REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 AT FR51.A PER AIRBUS DWG: R53810583 ISSUE: D & EO: 6-5310-7-5021 G PT8. CATEGORY A REPAIR. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA202406300885](https://openairdocs.org/sdr/FDEA202406300885.md): Rib · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB11, RIB13 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB11, RIB13 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FL - [SDR FDEA202406300884](https://openairdocs.org/sdr/FDEA202406300884.md): Rib · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB17, RIB18, RIB20 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17, RIB18, RIB20 BETWEEN STGR2.8 AND REAR SPAR. TIT - [SDR FDEA202406300883](https://openairdocs.org/sdr/FDEA202406300883.md): Rib · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26, RIB27 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA 6-5750-T0379691 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR. TITLE: WING - FL - [SDR FDEA202406300882](https://openairdocs.org/sdr/FDEA202406300882.md): Rib · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB20 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379692 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB20 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - [SDR FDEA202406300881](https://openairdocs.org/sdr/FDEA202406300881.md): Rib · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB12 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379692 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB12 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - [SDR FDEA202406300880](https://openairdocs.org/sdr/FDEA202406300880.md): Rib · cracked · Jun 30, 2024 · N745FD · Airbus A300B4622R · Trailing Edge Flaps > RH WING CENTER FLAP RIB UPR FLANGE FOUND 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA: 6-5750-T0379692 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB25, RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR. TITL - [SDR FDEA202406250868](https://openairdocs.org/sdr/FDEA202406250868.md): Skin · corroded · Jun 25, 2024 · N745FD · Airbus A300B4622R · Rudder, Plate/Skin > EXISTING REPAIR ON RUDDER LH SKIN BETWEEN RUDDER STA95-STA110 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RUDDER LH SKIN BETWEEN RUDDER STA95-STA110 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA: 6-5541-114926. TITLE: STABILIZERS - RUDDER - - [SDR FDEA202406210829](https://openairdocs.org/sdr/FDEA202406210829.md): None · none · Jun 21, 2024 · N745FD · Airbus A300B4622R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR56 - FR57.2 SEAT TRACK AT Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR56-FR57.2 SEAT TRACK AT Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53 - [SDR FDEA202406210828](https://openairdocs.org/sdr/FDEA202406210828.md): None · none · Jun 21, 2024 · N745FD · Airbus A300B4622R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR59 - FR60 SEAT TRACK AT Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR59-FR60 SEAT TRACK AT Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-1 - [SDR FDEA202406210827](https://openairdocs.org/sdr/FDEA202406210827.md): None · none · Jun 21, 2024 · N745FD · Airbus A300B4622R · Standard Practices/Structures > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR61 - FR62 SEAT TRACK AT Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR61-FR62 SEAT TRACK AT Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10- - [SDR FDEA202312061926](https://openairdocs.org/sdr/FDEA202312061926.md): Lens · inoperative · Dec 6, 2023 · N745FD · Airbus A300* · Central Warning > APU FIRE WARNING LIGHT INDICATOR AT NOSE GEAR STEERING BYPASS IS MISSING. RELEASED FOR SERVICE PER MEL: 26-XX-XX CAT C EXP: 16DEC23 APU GROUND AUTO FIRE EXTINGUISHING SYSTEM - INOP. APU OPERATION MUST BE MONITORED FROM COCKPIT WHILE APU IS RUNNING." - [SDR FDEA202303280557](https://openairdocs.org/sdr/FDEA202303280557.md): Unknown · unknown · Mar 28, 2023 · N745FD · Airbus A300* · Wing Main, Frame Structure > R/H RIB 5, FWD LUG HAS IMPACT DAMAGE TO LEADING EDGE APPROX 3 O'CLOCK POSITION. 0000095559: SMITH, JAMES A - 29-MAR-2023 21:28 COMPLIED WITH EA 6-5710-T0312369B P7 LH AND RH RIB 5 BORE CORROSION 0000302834: SANDERSON, JAMES H - 29-MAR-2023 21:31 INSPECT - [SDR FDEA202303280556](https://openairdocs.org/sdr/FDEA202303280556.md): Unknown · unknown · Mar 28, 2023 · N745FD · Airbus A300* · Wing Main, Frame Structure > L/H RIB 5 FWD LUG HAS IMPACT DAMAGE ON LEADING EDGE OF LUG APPROX 3 O'CLOCK POSITION. 0000095559: SMITH, JAMES A - 29-MAR-2023 21:22 COMPLIED WITH EA 6-5710-T0312369B P7 LH AND RH RIB 5 BORE CORROSION 0000302834: SANDERSON, JAMES H - 29-MAR-2023 21:25 CO - [SDR FDEA202302170295](https://openairdocs.org/sdr/FDEA202302170295.md): Proximity Sensor · failed · Feb 17, 2023 · N745FD · Airbus A300B4622R · Pitot/Static Anti-Ice System > PDIS 745 30-30 5301 17FEB23 DSM OPEN U ON TAKEOFF CLIMBING OUT AT ABOUT 200 AGL WITH GEAR RETRACTING RECEIVED CAPT, AUX AND FO (ALL) PITOT HEAT OVERHEAT AND ADC 2 IND MONITOR. TURNED THEM OFF PER ECAM AND QRH. EMERGENCY DECLARED. ***EMERGEN - [SDR FDEA202211272848](https://openairdocs.org/sdr/FDEA202211272848.md): Battery · failed · Nov 27, 2022 · N745FD · Airbus A300B4622R · Door Warning System > PDIS 745 52-70 5049 17NOV22 OAK FACT U RESIDUAL CABIN PRESSURE LIGHTS FLASHING AFTER ENGINE SHUT DOWN. NO PRESSURE INDICATED ON SYNOPTIC PAGE. FACT 27NOV22 18:29 MEM AMM: 52-73 - [SDR FDEA202206051378](https://openairdocs.org/sdr/FDEA202206051378.md): None · none · Jun 5, 2022 · N745FD · Airbus A300B4622R · Hydraulic Reservoir, Main > SHORTLY AFTER TAKEOFF, GOT YELLOW HYD PUMP PRESS LOW. TURNED OFF PUMP IAW ECAM AND COMPLIED WITH QRH. YELLOW SYSTEM OPERATED NORMALLY ON PTU. DISCOVERED YELLOW HYDRAULIC RESEVOIR BAD. REMOVED AND REPLACED YELLOW SYSTEM RESERVOIR 293000 IAW AMM 29-13-46-04 - [SDR FDEA202205131196](https://openairdocs.org/sdr/FDEA202205131196.md): Floor Panel · damaged · May 13, 2022 · N745FD · Airbus A300* · Fuselage Floor Panel > THE MDC #242NH FLOOR PANEL WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W A300-600 S.R.M 51-72-10-001, PAGE1-3. - [SDR FDEA202205131199](https://openairdocs.org/sdr/FDEA202205131199.md): Floor Panel · damaged · May 13, 2022 · N745FD · Airbus A300* · Fuselage Floor Panel > THE MDC #242UF FLOOR PANEL WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W A300-600 S.R.M 51-72-10-001, PAGE1-3. - [SDR FDEA202205131198](https://openairdocs.org/sdr/FDEA202205131198.md): Floor Panel · damaged · May 13, 2022 · N745FD · Airbus A300* · Fuselage Floor Panel > THE MDC #241QH FLOOR PANEL WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W A300-600 S.R.M 51-72-10-001, PAGE1-3. - [SDR FDEA202205131197](https://openairdocs.org/sdr/FDEA202205131197.md): Floor Panel · damaged · May 13, 2022 · N745FD · Airbus A300* · Fuselage Floor Panel > THE MDC #242PH FLOOR PANEL WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W A300-600 S.R.M 51-72-10-001, PAGE1-3. - [SDR FDEA202204211118](https://openairdocs.org/sdr/FDEA202204211118.md): Crossbeam · bent · Apr 21, 2022 · N745FD · Airbus A300* · Wing, Attach Fittings > LH WING KRUEGER FLAP SUPPORT STRUCTURE FRONT CROSSBEAM DEFORMED REPLACED THE CROSSBEAM WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2 - [SDR FDEA202204161195](https://openairdocs.org/sdr/FDEA202204161195.md): Floor Panel · damaged · Apr 16, 2022 · N745FD · Airbus A300* · Fuselage Floor Panel > MAIN DECK CARGO #241TG FLOOR PANELS WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE1-3 - [SDR FDEA202204161054](https://openairdocs.org/sdr/FDEA202204161054.md): Floor Panel · damaged · Apr 16, 2022 · N745FD · Airbus A300* · Fuselage Floor Panel > MAIN DECK CARGO #251UH FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE DAMAGED AREA I.A.W A300-600 SRM 53-10-20-201 P.205-206, PARA.9A, FIG.201 - [SDR FDEA202204161055](https://openairdocs.org/sdr/FDEA202204161055.md): Floor Panel · damaged · Apr 16, 2022 · N745FD · Airbus A300B4622R · Fuselage Floor Panel > AFT CARGO COMPT #152KF FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE DAMAGED AREA I.A.W A300-600 SRM 53-10-20-201 P.205-206, PARA.9A, FIG.201 - [SDR FDEA202204151101](https://openairdocs.org/sdr/FDEA202204151101.md): Fitting · gouged · Apr 15, 2022 · N745FD · Airbus A300* · Fuselage Structure (General) > LH FWD PAX/CREW DOOR CUTOUT FOUND GOUGE NEAR FWD-UPR CORNER. DAMAGED FITTING REPLACED NEW PART, INSTALLED WITH RIVETS. I.A.W A300-600 SRM 51-40-21- 001 PARA.6 PAGE.7B-23 AND 51-72-10-001 PAGE.2. - [SDR FDEA202204101117](https://openairdocs.org/sdr/FDEA202204101117.md): Support Fitting · corroded · Apr 10, 2022 · N745FD · Airbus A300* · Wing, Attach Fittings > LH WING FIXED L/E KRUEGER BOX SUPPORT FITTING GOT CORROSION AT I/B OF CLOSING RIB REPLACED THE SUPPORT FITTING WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2 - [SDR FDEA202102270500](https://openairdocs.org/sdr/FDEA202102270500.md): Iru · malfunctioned · Feb 27, 2021 · N745FD · Airbus A300B4622R · Independent Position Determining System > AT APPROXIMATELY 2000' ON TAKEOFF FROM KMEM, FO LOST MOST PFD/ND ATTITUDE AND NAVIGATION INFORMATION. ALSO REC'D ECAM #2 IRS FAULT, ALONG WITH #2 PITCH TRIM PADDLE AND BOTH YAW DAMPER PADDLES DISENGAGING. CAPT TOOK AIRCRAFT CONTROL WITH ONLY PFD ATTITUDE - [SDR FDEA202102260478](https://openairdocs.org/sdr/FDEA202102260478.md): Iru · malfunctioned · Feb 26, 2021 · N745FD · Airbus A300B4622R · Air Collision Avoidance System > PDIS 745 34-45 3202 26FEB21 MEM OPEN U LOGPAGES:366120 AT APPROXIMATELY 40 KNOTS ON TAKEOFF ROLL @ KMEM, F/O LOST ADI PRESENTATION, #2 YAW DAMPER DISENGAGED, AND WE REC D ECAM IRS #2 FAULT MESSAGE. ABORTED TAKEOFF AND PERFORMED QRH PROCEDUR - [SDR FDEA2019111522944](https://openairdocs.org/sdr/FDEA2019111522944.md): Inertia Reel · malfunctioned · Nov 12, 2019 · N745FD · Airbus A300B4622R · Flight Compartment Equipment > PDIS 745 25-10 2057 12NOV19 LBB FACT U LOGPAGES:2969130 THE INERTIAL REEL ON F/O'S RIGHT SHOLDER STRAP IS NOT FUNCTIONING PROPERLY. FACT 13NOV19 07:07 LBB R/R'ED FIRST OFFICER - [SDR FDEA2019101432633](https://openairdocs.org/sdr/FDEA2019101432633.md): Floor Panel · damaged · Oct 13, 2019 · N745FD · Airbus A300B4622R · Fuselage Floor Panel > BULK CARGO FLOOR PANEL 161AF HAS NUMEROUS DENTS AND DAMAGE. FABRICATED FLOOR PANEL ON VTMAE TRAVELER #T19/1447754 IAW SRZ 25-005P, CAT "A" AND MAJOR REPAIR. - [SDR FDEA2019101432632](https://openairdocs.org/sdr/FDEA2019101432632.md): Floor Panel · broken · Oct 13, 2019 · N745FD · Airbus A300B4622R · Fuselage Floor Panel > AFT CARGO FLOOR PANEL 152AF BROKEN. FABRICATED FLOOR PANEL ON VTMAE TRAVELER #T19/1447629 IAW SRZ 25-005 REV P, CAT "A" AND MAJOR REPAIR. - [SDR FDEA201910132631](https://openairdocs.org/sdr/FDEA201910132631.md): Floor Panel · crushed · Oct 13, 2019 · N745FD · Airbus A300B4622R · Fuselage Floor Panel > BULK CARGO FLOOR PANEL 161BF EDGE CRUSHED. FABRICATED FLOOR PANEL ON VTMAE TRAVELER # T19/1447633 IAW SRZ 25-005 REV P, CAT "A" AND MAJOR REPAIR. - [SDR FDEA2019101432630](https://openairdocs.org/sdr/FDEA2019101432630.md): Floor Panel · damaged · Oct 13, 2019 · N745FD · Airbus A300B4622R · Fuselage Structure (General) > BULK CARGO FLOOR PANEL 161GF EDGE CRUSHED. FABRICATED FLOOR PANEL ON VTMAE TRAVELER # T19/1447718 IAW SRZ 25-005P, CAT "A" AND MAJOR REPAIR. - [SDR FDEA2019101432629](https://openairdocs.org/sdr/FDEA2019101432629.md): Floor Panel · crushed · Oct 13, 2019 · N745FD · Airbus A300B4622R · Fuselage Floor Panel > BULK CARGO FLOOR PANEL 161CF DGE CRUSHED. FABRICATED FLOOR PANEL ON VTMAE TRAVELER # T19/1447630 IAW SRZ 25-005P, CAT "A" AND MAJOR REPAIR. - [SDR FDEA2019100752468](https://openairdocs.org/sdr/FDEA2019100752468.md): Floor Support · corroded · Oct 5, 2019 · N745FD · Airbus A300B4622R · Fuselage Miscellaneous Structure > MAIN CABIN LAVATORY FLOOR SUPPORT, INBD SIDE WAS CORRODED. REMOVED AND REPLACED MAIN CABIN LAVATORY FLOOR SUPPORT IAW SRM 51-40-21, CAT"A" MAJOR REPAIR. - [SDR FDEA2019100752469](https://openairdocs.org/sdr/FDEA2019100752469.md): Floor Panel · damaged · Oct 5, 2019 · N745FD · Airbus A300B4622R · Fuselage Floor Panel > MDCC 242MH FLOOR PANEL BROKEN. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ25-005, REV P. CAT"A" MAJOR REPAIR. Next page: https://openairdocs.org/aircraft/N745FD/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 = 'N745FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N745FD/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.