# Service difficulty reports: N743FD

A list on [N743FD](https://openairdocs.org/aircraft/N743FD.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 · 263 reports

- [SDR FDEA202501140068](https://openairdocs.org/sdr/FDEA202501140068.md): Bottle · low pressure · Jan 14, 2025 · N743FD · Airbus A300B4622R · Passenger/Crew Doors
  > R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED DAMPER AS REQUIRED IAW AMM 52-10-14-03-01. OK FOR SERVICE.
- [SDR FDEA202408231167](https://openairdocs.org/sdr/FDEA202408231167.md): Floorboard · damaged · Aug 23, 2024 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > WHILE REMOVING FLOOR PANEL AT 5L FOR ACCESS TO SEAT TRACK A CRACK WAS FOUND ON THE AFT SIDE OF THE FLOOR PANEL MPN: R532B3709.00000 FABRICATED NEW FLOORBOARD (PNL# R532B3709.00000.) AT 5L BETWEEN FR42-STA. 2718 -FR43- STA. 2771, IN REF TO FEDEX DRW# SRZ-25-
- [SDR FDEA202401220092](https://openairdocs.org/sdr/FDEA202401220092.md): Slide · damaged · Jan 22, 2024 · N743FD · Airbus A300B4622R · Escape Slide
  > WHILE ARMING RIGHT SIDE CABIN DOOR, EMERGENCY SLIDE WAS ACCIDENTALLY DEPLOYED. RELEASED FOR SERVICE PER MEL: 52-11-01-03. CREW ENTRY DOOR ESCAPE SLIDE (R-1) REMOVED. REMOVED R-1 DOOR ESCAPE SLIDE IAW MEL 52-11-01-03 AND AMM 25-61-22-04-01. ARMING HANDL
- [SDR FDEA202305070823](https://openairdocs.org/sdr/FDEA202305070823.md): Hose · failed · May 7, 2023 · N743FD · Airbus A300* · Hydraulic Power System
  > PDIS 743 29-30 5621 07MAY23 23:03 IND FACT DURING FLIGHT GREEN HYD RESERVOIR LOW. AMM: 20-23-11-00
- [SDR FDEA202304280771](https://openairdocs.org/sdr/FDEA202304280771.md): Unknown · unknown · Apr 28, 2023 · N743FD · Airbus A300* · Powerplant System
  > PASSING ABOUT 3,000, THE NUMBER 2 ENGINE MADE A LOUD NOISE AND THE AIRCRAFT SHOOK. WE FOLLOWED ECAM, SHUT DOWN THE NUMBER 2 ENGINE AND LANDED. MAX EGT WAS ABOUT 710. REMOVED AND REPLACED #2 PW ENGINE PER EC-PWBOOT ENGINE CHANGE WORK CARD INSTRUCTIONS. ALL OP
- [SDR FDEA202301090059](https://openairdocs.org/sdr/FDEA202301090059.md): None · none · Jan 9, 2023 · N743FD · Airbus A300B4622R · Emergency Lighting
  > DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHTS DO NOT TEST. ALL EMERGENCY LIGHTS COME ON WHEN MANUALLY ACTIVATED PER AMM 33-51-00-05. OPERATED EMERGENCY EXIT LIGHT IAW AMM ADJ/TEST 33-51-00-05-09 AND OPERATION OPS NORMAL. ORIG SUB DATE: 1/9/2023
- [SDR FDEA202209052203](https://openairdocs.org/sdr/FDEA202209052203.md): Stringer · corroded · Sep 5, 2022 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER 44RH FOUND HEAVY CORROSION BETWEEN FR38.2 AND FR39 REPAIRED THE CORRODED FUSELAGE STRINGER 44RH BETWEEN FR38.2 AND FR39 PER A300- 600 SRM53-10-14-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-
- [SDR FDEA202209052202](https://openairdocs.org/sdr/FDEA202209052202.md): Door Frame · cracked · Sep 5, 2022 · N743FD · Airbus A300B4622R · Fuselage Main, Structure
  > RH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPLACED RH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299(ISSUE.G). TRACKING EA 6-5210-T0370251 P1 RAISED AND AC
- [SDR FDEA202208312119](https://openairdocs.org/sdr/FDEA202208312119.md): Skin · delaminated · Aug 31, 2022 · N743FD · Airbus A300B4622R · Spoilers
  > RH WING #5 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 30MM*10MM, DEPTH: 1.5MM COMPLIED WITH EA: 6-5750-T0370081 P1. TITLE: WING - FLIGHT SURFACES - RH 5# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE RH WING
- [SDR FDEA202208312118](https://openairdocs.org/sdr/FDEA202208312118.md): Skin · delaminated · Aug 31, 2022 · N743FD · Airbus A300B4622R · Spoilers
  > LH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 35MM*40MM, DEPTH: 1.7MM COMPLIED WITH EA: 6-5750-T0370080 P1. TITLE: WING - FLIGHT SURFACES - LH 4# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WING
- [SDR FDEA202208312117](https://openairdocs.org/sdr/FDEA202208312117.md): Hinge · delaminated · Aug 31, 2022 · N743FD · Airbus A300B4622R · Spoilers
  > LH WING #3 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE AND CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: (1) 65MM*28MM, DEPTH: 2.36MM (2) 35MM*15MM, DEPTH: 2.05MM (3) 40MM*35MM, DEPTH: 1.5MM COMPLIED WITH EA: 6-5750-T0370
- [SDR FDEA202206211492](https://openairdocs.org/sdr/FDEA202206211492.md): None · failed · Jun 21, 2022 · N743FD · Airbus A300* · Fuel Indicating System
  > PDIS 743 28-40 4804 21JUN22 OMA R OUTER FUEL TANK BURNING FUEL OUT OF SEQUENCE. WITH ALL PUMPS ON FUEL CONTINUED TO BURN FROM OUTER TANK. RAN FUEL IMBALANCE CHECKLIST AS WELL AS FUEL FEED MANUAL CONTROL CHECKLIST. NO FAULTS ON ANY FUEL PUMPS. PULLED
- [SDR FDEA202202140528](https://openairdocs.org/sdr/FDEA202202140528.md): Power Supply · unknown · Feb 14, 2022 · N743FD · Airbus A300* · Emergency Lighting
  > DURING SERVICE CHECK COURIER COMPARTMENT EMERGENCY LIGHT TEST, EMERG TEST PUSH- BUTTON ON 818VU PANEL DOES NOT ILLUMINATE. EMERGENCY LIGHTS ILLUMINATE. TEMP INSTALLED NEW POWER UNIT 29WL1 NO HELP REINSTALLED ORIGINAL 29WL REF A300 MM 33-51-14-04. RELAMPED
- [SDR FDEA202112032984](https://openairdocs.org/sdr/FDEA202112032984.md): None · unknown · Dec 3, 2021 · N743FD · Airbus A300* · Hydraulic Indicating System
  > PDIS 743 29-30 3974 03DEC21 IND OPEN U DURING CRUISE FROM OAK TO IND THE GREEN HYDRAULIC SYSTEM HYDRAULIC QUANTITY SLOWLY DECREASED TO JUST ABOVE RED DOT. WE INFORMED GOC/ MOCC. AT TOP OF DESCENT INTO IND, RECEIVED ECAM FOR GREENE SYSTEM
- [SDR FDEA202110192600](https://openairdocs.org/sdr/FDEA202110192600.md): None · none · Oct 19, 2021 · N743FD · Airbus A300* · Standard Practices/Structures
  > L/H WING #2 SLAT HAS 3" CRACK AT THE INBOARD END CAP INSPECTION PLATE 0000069861: GRAHAM, JONATHAN F - 22-OCT-2021 21:12 COMPLIED WITH FINAL APPROVED EA 6-5750-T0364909 PART 1 REV A, TITLED: "WINGS-FLIGHT SURFACES-LH #2 SLAT BOTTOM SKIN GOUGED-REPAIR BY IN
- [SDR FDEA202110142537](https://openairdocs.org/sdr/FDEA202110142537.md): None · none · Oct 14, 2021 · N743FD · Airbus A300* · Wing Structure
  > L/H WING #2 SLAT HAS 2 HOLES IN THE UNDERSIDE OF THE SLAT PANEL JUST O/B OF THE #1 ENG PYLON. IN WORK
- [SDR FDEA202108182030](https://openairdocs.org/sdr/FDEA202108182030.md): Adc · malfunctioned · Aug 18, 2021 · N743FD · Airbus A300B4622R · Air Data Computer
  > PDIS 743 34-14 3667 18AUG21 OKC OPEN U APPROACHING KOKC (50 MINUTES INTO FLIGHT), CAPTAIN S AIRSPEED TAPE WENT TO ZERO AND ALTIMETER JUMPED TO 250 FEET HIGH AT FL340. FD, AT AND AP WENT AWAY ACCORDINGLY. CAPTAIN S AIRSPEED RECOVERED AND FAILE
- [SDR FDEA202011262976](https://openairdocs.org/sdr/FDEA202011262976.md): Valve · failed · Nov 26, 2020 · N743FD · Airbus A300B4622R · Landing Gear Brake System
  > MDIS 743 32-42 3038 26NOV20 OKC OPEN U. ON PRE-DISPATCH FOUND NR 4 MWA THERMALED. REMOVED AND REPLACED NR 4 MWA. BRAKES WOULD NOT RELEASE T/S AND FOUND PARKING BRAKE SELECTOR NOT DISENGAGING, INTERMITENT. GOT NR 4 MWA ASSEMBLY COMPLETED. NR 3 MWA WILL NEE
- [SDR FDEA2020070211411](https://openairdocs.org/sdr/FDEA2020070211411.md): Relief Valve · stuck · Jul 1, 2020 · N743FD · Airbus A300B4622R · Hydraulic Pressure Relief Valve, Main
  > IN CRUISE FLIGHT NOTICED GREEN SYSTEM QUANTITY SLOWLY DROPPING INTO YELLOW RANGE. EVENTUALLY GOT TO THE RED DOT FOLLOWED BY THE ECAM ALERT FOR LOW SYSTEM QUANTITY. FOLLOW ECAM PROCEDURE. MFG L95B13-401, MSN - N/A. FOUND DEPRESSURIZATION RELIEF VALVE STUCK
- [SDR FDEA202003020478](https://openairdocs.org/sdr/FDEA202003020478.md): Flap · damaged · Mar 2, 2020 · N743FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING MID FLAP TRAILING EDGE HAS DAMAGE AND POPPED RIVETS. REPAIRED L/H WING MID FLAP TRAILING EDGE DAMAGE PER EA 6-5750-T0352685 P1. TOPCOATED IAW A300-600 SRM 51-75-10. (TITLE: WINGS- LH CENTER FLAP UPPER SKIN DAMAGE BETWEEN RIB13 TO RIB15.) (MAJOR REP
- [SDR FDEA202002270418](https://openairdocs.org/sdr/FDEA202002270418.md): Skin · gouged · Feb 27, 2020 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR LOWER FWD CUT OUT SKIN GOUGED. REPAIRED AFT CARGO LOWER FWD CUT OUT SKIN IAW SRM 53-17-12 FIG 201. REMOVED GOUGE AT AFT CARGO LOWER FWD CUTOUT SKIN AT FR60 STRINGER S-39R TO S-43R. L=3.0, D=.0250 FOUND TO BE OUT OF LIMITS IAW SRM 53-17-12
- [SDR FDEA202002180351](https://openairdocs.org/sdr/FDEA202002180351.md): Adapter · gouged · Feb 18, 2020 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK FR32 BL -953, NUT PLATE HOLE IS GOUGED UNDERSIDE, AFT. REMOVED AND REPLACED PLATE ADAPTER IAW SRM 51-40-21. BLENDED AREA, MATERIAL LOSS.028 FOUND TO BE OUT OF LIMITS IAW SRM 51-75-10. FABRICATED NEW ADAPTER PLATE ON TRAVELER T20/1473168 IA
- [SDR FDEA2020021860344](https://openairdocs.org/sdr/FDEA2020021860344.md): Seat Track · cracked · Feb 16, 2020 · N743FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK LBL 1959 BETWEEN FR 52 AND FR 53 SCALLOP BETWEEN 6,7, I INCHES AFT OF FR 52 BROKEN REMOVED AND REPLACED SEAT TRACK LBL 1959 IAW SRM 51-40-21 FR45 TO FR54. DAMAGED SCALLOPS ON SEAT TRACK FOUND OUT OF LIMITS IAW 53-10-16. MAJOR REP
- [SDR FDEA2020021850342](https://openairdocs.org/sdr/FDEA2020021850342.md): Floor Panel · delaminated · Feb 15, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > COURIER FLOOR PANEL 222RF DELAMINATED FABRICATED COURIER FLOOR PANEL 222RF ON TRAVELER T20/1472821 IAW SRZ-25-005 REV. R CAT."A" MAJOR REPAIR. INSTALLED 222RF FLOOR PANEL ON WORK CARD NO. 220-FL-FIT
- [SDR FDEA2020021420330](https://openairdocs.org/sdr/FDEA2020021420330.md): Floor Support · corroded · Feb 12, 2020 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE. LAV SUPPORT BEAM BETWEEN LBL 450 AND LBL 953 FR 10 TO FR12 CORRODED REMOVED AND REPLACED FLOOR SUPPORT AT MAIN DECK AT FR10 TO FR14 Y953. IAW SRM 51-40-21 AND DWG NO. A53612214. MAJOR REPAIR
- [SDR FDEA2020021410318](https://openairdocs.org/sdr/FDEA2020021410318.md): Floor Panel · damaged · Feb 11, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 151CF IS DAMAGED. FABRICATED FLOOR PANEL 151CF ON VT MAE TRAVELER T20/1472461. CLASSIFED AS CAT "A" MAJOR REPAIR. PANEL INSTALLED ON WORK CARD 150-FL-FIT. IAW SRZ-25-005
- [SDR FDEA2020021410316](https://openairdocs.org/sdr/FDEA2020021410316.md): Floor Panel · damaged · Feb 11, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD PIT FLOOR PANEL 131HG IS DAMAGED. FABRICATED FLOOR PANEL 131HG ON VT MAE TRAVELER T20/1474746. CLASSIFIED AS CAT "A" MAJOR REPAIR. PANEL INSTALLED ON WORK CARD 130-FL-FIT. IAW SRZ-25-005
- [SDR FDEA202002100308](https://openairdocs.org/sdr/FDEA202002100308.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD PIT FLOOR PANEL 131JG IS DAMAGED. FLOOR PANEL 131JG FABRICATED ON VT MAE TRAVELER T20/1472534. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL INSTALLED ON WORK CARD 130-FL-FIT. IAW SRZ-25-005.
- [SDR FDEA202002100307](https://openairdocs.org/sdr/FDEA202002100307.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 151BF IS DAMAGED. FABRICATED FLOOR PANEL 151BF ON VT MAE TRAVELER T20/1472535. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL INSTALLED ON WORK CARD 150-FL-FIT. IAW SRZ-25-005.
- [SDR FDEA202002100306](https://openairdocs.org/sdr/FDEA202002100306.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 152HF IS DAMAGED. FABRICATED FLOOR PANEL ON VT MAE TRAVELER T20/1472450 (FLOOR PANEL 152HF). CLASSIFED AS CAT "A" MAJOR REPAIR. FLOOR PANEL INSTALLED ON WORK CARD 150-FL-FIT. IAW SRZ-25-005.
- [SDR FDEA202002100305](https://openairdocs.org/sdr/FDEA202002100305.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 152GF IS DAMAGED. FABRICATED FLOOR PANEL 152GF ON VT MAE TRAVELER T20/1472449. CLASSIFED AS CAT "A" MAJOR REPAIR. FLOOR PANEL INSTALLED ON WORK CARD 150-FL-FIT. IAW SRZ-25-005.
- [SDR FDEA202002100304](https://openairdocs.org/sdr/FDEA202002100304.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 151EF IS DAMAGED. FABRICATED FLOOR PANEL 151EF ON VT MAE TRAVELER T20/1472446. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL INSTALLED ON WORK CARD 150-FL-FIT IAW SRZ-25-005.
- [SDR FDEA202002100303](https://openairdocs.org/sdr/FDEA202002100303.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 151GF IS DAMAGED. FABRICATED FLOOR PANEL 151GF ON VT MAE TRAVELER T20/1472448. CLASSIFIED AS CAT "A" MAJOR REPAIR. PANEL INSTALLED ON WORK CARD 150-FL-FIT. IAW SRZ-25-005
- [SDR FDEA202002100302](https://openairdocs.org/sdr/FDEA202002100302.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > AFT PIT FLOOR PANEL 151LF IS DAMAGED. FABRICATED FLOOR PANEL 151LF ON VT MAE TRAVELER T20/1472447. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL INSTALLED ON WORK CARD 150-FL-FIT. IAW SRZ-25-005
- [SDR FDEA202002100314](https://openairdocs.org/sdr/FDEA202002100314.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132ZF IS BROKEN IN HALF. FABRICATED NEW FLOOR PANEL 132ZF ON VT MAE TRAVELER T20/1470634 IAW DWG SRZ-25- 005 FROM FR30 TO FR35 MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 130-FL-FIT
- [SDR FDEA202002100313](https://openairdocs.org/sdr/FDEA202002100313.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 252DK IS DAMAGED. FABRICATED NEW FLOOR PANEL 252DK ON VT MAE TRAVELER T20/1470992 IAW SRZ-25-005. MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 250-FL-FIT. FROM FR56 TO FR57 BETWEEN -Y1959 TO -Y2462
- [SDR FDEA202002100312](https://openairdocs.org/sdr/FDEA202002100312.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251XH IS BROKEN. FABRICATED NEW FLOOR PANEL 251XH ON VT MAE TRAVELER T20/1470918 IAW SRZ-25-005 FROM FR60 TO FR61 BETWEEN Y1959 TO Y2462. MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 250-FL-FIT
- [SDR FDEA202002100311](https://openairdocs.org/sdr/FDEA202002100311.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242WJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242WJ ON VT MAE TRAVELER T20/1470870 IAW SRZ-25-005 FROM FR44 TO FR45 BETWEEN -Y1959 TO -Y2462. CAT "A" MAJOR REPAIR. PANEL INSTALLED ON WORK CARD 240-FL-FIT
- [SDR FDEA202002100310](https://openairdocs.org/sdr/FDEA202002100310.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 252DF IS DAMAGED. FABRICATED NEW PANEL 252DF ON VT MAE TRAVELER T20/1470889 IAW SRZ-25-005 FROM FR55 TO FR56 BETWEEN -Y1959 TO -Y2462. MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 250-FL-FIT
- [SDR FDEA202002100309](https://openairdocs.org/sdr/FDEA202002100309.md): Floor Panel · damaged · Feb 10, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 252WG IS DAMAGED. FABRICATED NEW FLOOR PANEL 252WG ON VT MAE TRAVELER T20/1470881 IAW SRZ-25-005. FROM FR60 TO FR62 BETWEEN -Y1456 TO -Y1959. MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 250-FL-FIT
- [SDR FDEA202002070282](https://openairdocs.org/sdr/FDEA202002070282.md): Floor Panel · damaged · Feb 7, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242LK IS DAMAGED. FABRICATED NEW FLOOR PANEL 242LK ON VT MAE TRAVELER T20/1470991 IAW SRZ-25-005 FROM FR53 TO FR54 BETWEEN -X1959 TO -X2462. MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 240-FL-FIT
- [SDR FDEA202002070283](https://openairdocs.org/sdr/FDEA202002070283.md): Floor Panel · damaged · Feb 7, 2020 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242EJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242EJ ON VT MAE TRAVELER T20/1470898 IAW DWG SRZ-25- 005 FROM FR54 TO FR 54.2, X0 TO -X450 MAJOR REPAIR CAT "A". PANEL INSTALLED ON WORK CARD 240-FL-FIT
- [SDR FDEA201907061495](https://openairdocs.org/sdr/FDEA201907061495.md): Seat Track · corroded · Jul 6, 2019 · N743FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, SEAT TRACK HAS EVIDENCE OF CORROSION @Y2462, FR 26-27 INSTALLED SEAT TRACK REPAIR PER SRM 53-10-16 FIG 208A.
- [SDR FDEA201907051487](https://openairdocs.org/sdr/FDEA201907051487.md): Floor Panel · punctured · Jul 5, 2019 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231FF HAS MULTIPLE PUNCTURES AND IS WORN FROM WALKWAY PANEL THAT SITS ON TOP. FABRICATED NEW FLOOR PANEL PER SRZ 25-005 REV P.
- [SDR FDEA201907051486](https://openairdocs.org/sdr/FDEA201907051486.md): Floor Panel · punctured · Jul 5, 2019 · N743FD · Airbus A300B4622R · Fuselage Floor Panel
  > MAIN CABIN, FLOOR PANEL 231FF HAS MULTIPLE PUNCTURES AND IS WORN FROM THE WALKWAY PANEL THAT SIT ON TOP. FABRICATED A NEW FLOOR PANEL PER SRZ 25-005 REV. P.
- [SDR FDEA201810212966](https://openairdocs.org/sdr/FDEA201810212966.md): Cable · failed · Oct 21, 2018 · N743FD · Airbus A300B4622R · Landing Gear Brake System
  > PARKING BRAKE CONTROL HANDLE FAILED TO SET BRAKES. REMOVED AND REPLACED CABLE REF IPC 32-45-01-04 ITEM 300 PART 4100446 MM REF 32-45-11-04. PARKING BRAKE OPS CHECKS GOOD, A/C OK FOR SERVICE.
- [SDR FDEA201806261584](https://openairdocs.org/sdr/FDEA201806261584.md): Diaphragm · punctured · Jun 26, 2018 · N743FD · Airbus A300B4622R · Passenger/Crew Doors
  > R1 DOOR ASSIST BOTTLE DIAPHRAGM IS PUNCTURED. REPLACED R1 DOOR ASSIST BOTTLE DIAPHRAGM AND SERVICED BOTTLE REF MM 52-10-14-03-01, OPS CK NORMAL. A/C OK TO CONTINUE.
- [SDR FDEA201804271141](https://openairdocs.org/sdr/FDEA201804271141.md): Warning Horn · activated · Apr 27, 2018 · N743FD · Airbus A300B4622R · Emergency Exits
  > AFTER LEVEL OFF, THE SLIDE WARNING LIGHT ON THE RIGHT CREW ENTRY DOOR ILLUMINATED AND THE HORN SOUNDED. THERE WERE NO INDICATIONS ON ECAM AND THE AIRCRAFT PRESSURIZATION REMAINED NORMAL. THE SLIDES HORN CIRCUIT BREAKER WAS PULLED UNTIL FL180. LIGHT STAY
- [SDR FDEA201712153394](https://openairdocs.org/sdr/FDEA201712153394.md): Spoiler · detached · Dec 15, 2017 · N743FD · Airbus A300B4622R · Drag Control System
  > PDIS 743 27-60 9666 15DEC17 DUB OPEN U LOGPAGES:2816292 ON DESCENT INTO EIDW WHEN SPEED BRAKES WERE DEPLOYED A/C STARTED TO ROLL TO THE RIGHT. THE MORE THEY WERE DEPLOYED THE LARGER TEH ROLL MOMENT. OBSERVED THE FLT CONTROL PAGE ON ECAM & NO
- [SDR FDEA201708042115](https://openairdocs.org/sdr/FDEA201708042115.md): Warning Light · false activation · Aug 4, 2017 · N743FD · Airbus A300B4622R · Door Warning System
  > DURING CLIMBOUT, RIGHT CABIN DOOR INDICICATED UNLOCKED FROM THE COURIER AREA. RED LIGHT FLASHING AND AURAL WARNING. COCKPIT INDICATIONS WERE NORMAL.FLASHING LIGHT AND AURAL WARNING EXTINGUSHED IN DESCENT PASSING 10000 FEET. CHECKED THE OPERATION AND INDICA

Next page: https://openairdocs.org/aircraft/N743FD/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 = 'N743FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N743FD/reports

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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.