# Service difficulty reports: N733FD

A list on [N733FD](https://openairdocs.org/aircraft/N733FD.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 · 203 reports

- [SDR FDEA202609161354](https://openairdocs.org/sdr/FDEA202609161354.md): Seat Track · damaged · Sep 16, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. AMM 53-10-16-06 SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080 MEL: 25-50-02-01-J LOCKED REMOVED AND PLACED IN CLOSET PER WRI 25-50/0129. C/7462504. REMOVED THE DAMAGED SEAT TRACK IAW SRM 51-40-21. FA
- [SDR FDEA202608071099](https://openairdocs.org/sdr/FDEA202608071099.md): Skin · cracked · Aug 7, 2026 · N733FD · Airbus A300B4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPPER EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 4 EA FASTENER HOLES. REPAIRED THE FASTENER HOLES ON THE MAIN DECK CARGO DOOR UPPER EDGE AT PT1 BETWEEN FR22 & FR25 IAW EA 6-5230-T0388329, P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202608051111](https://openairdocs.org/sdr/FDEA202608051111.md): Skin Panel · cracked · Aug 5, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, Plate/Skin
  > FUSELAGE FRAME, FR 54 LATERAL PANEL THREE HOLES CRACKED AT STRINGER 36L, 44L - 44R. COMPLIED WITH EA 6-5330-T0388383 P1 REPAIRED THE FUSELAGE FRAME FR54 LATERAL PANEL 3EA CRACKED HOLES AT S36L S44L S44R. EA TITLE: FUSELAGE - PLATES & SKINS - CRACK HOLES O
- [SDR FDEA202608021117](https://openairdocs.org/sdr/FDEA202608021117.md): Fitting · damaged · Aug 2, 2026 · N733FD · Airbus A300B4605R · Cargo/Baggage 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 C P5. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. MAJOR RE
- [SDR FDEA202608011089](https://openairdocs.org/sdr/FDEA202608011089.md): Skin · contaminated · Aug 1, 2026 · N733FD · Airbus A300B4605R · Elevator, Plate/Skin
  > LEFT ELEVATOR LOWER SURFACE HAS 1EA TRAPPED WATER AT ER5. REPAIRED LH ELEVATOR LOWER SURFACE ER5 TRAPPED WATER IAW SRM 55-21-12-201-2, PARA.5.J & SRM 51-77-12-201. THIS IS CAT B REPAIR AND THE FOLLOW UP INSPECTION IS TRACKED BY EA 6-5520-T0388407. MAJOR RE
- [SDR FDEA202608011088](https://openairdocs.org/sdr/FDEA202608011088.md): Skin · contaminated · Aug 1, 2026 · N733FD · Airbus A300B4605R · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SURFACE HAS 3EA TRAPPED WATER AT ER10. REPAIRED LT ELEVATOR UPPER ER10 TRAPPED WATER IAW SRM55-21-12-201-2 PARA.5.J & SRM 51-77-12-201. THIS IS CAT B REPAIR AND THE FOLLOW UP INSPECTION IS TRACKED BY EA 6- 5520-T0388407, MAJOR REPAIR IA
- [SDR FDEA202608011087](https://openairdocs.org/sdr/FDEA202608011087.md): Floorbeam · corroded · Aug 1, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, Floor Beam
  > FUSELAGE SKIN INTERNAL BEAM CORRODED AT FR39 S50L - S54L. COMPLIED WITH EA 6-5310-T0388500 P1 REPAIRED THE FWD CARGO COMPARTMENT FR39 LOWER TEE BEAM CORROSION BETWEEN STGR51L AND STGR54L. EA TITLE: FUSELAGE - MAINFRAME - FR39 LOWER TEE BEAM CORROSION BETWEE
- [SDR FDEA202607311110](https://openairdocs.org/sdr/FDEA202607311110.md): Reinforcement · corroded · Jul 31, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT LOWER INTERNAL REINFORCING RING AND STRINGER FITTING CORRODED AT FR 54, STRINGERS 44R - 45R. FUSELAGE - MAINFRAME - FR54 TEE SECTION CORROSION BETWEEN STGR44RH AND 45RH. THIS REPAIR IS CONSIDERED AS CAT B REPAIR DUE TO AWAITING FUR
- [SDR FDEA202607291098](https://openairdocs.org/sdr/FDEA202607291098.md): Door Frame · cracked · Jul 29, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > RT PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C IAW SRM 51-40-21 AND DWG F52181299(ISSUE: G). RSC TRACKING EA: 6-5210-T0387549 RAISED AND ACCOMPLISHED. THIS IS A CATEGORY A REPAIR. MAJOR REPAI
- [SDR FDEA202607291079](https://openairdocs.org/sdr/FDEA202607291079.md): Cargo Track · corroded · Jul 29, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > MDC LOADING SYS TRACK Y450 CORRODED AT FR18 - FR19. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR18 - FR19 Y450 PER SRM 51-40-21 & DWG A53612518 (ISSUE.A00). THIS IS CAT A REPAIR, MAJOR REPAIR IAW GMM6-2- 100.
- [SDR FDEA202607291078](https://openairdocs.org/sdr/FDEA202607291078.md): Cargo Track · corroded · Jul 29, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > MDC LOADING SYS TRACK Y953 CORRODED AT FR18 - FR19. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR18 - FR19 Y953 IAW SRM 51-40-21 & DWG: A53615224 (ISSUE.A00). THIS IS CAT A REPAIR MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202607251077](https://openairdocs.org/sdr/FDEA202607251077.md): Seat Track · damaged · Jul 25, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR40 - FR45 -Y450 PER A300-600 SRM51-40-21 & DWG A53832020, ISSUE: J. THIS IS CAT A REPAIR, MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202602130218](https://openairdocs.org/sdr/FDEA202602130218.md): Mount · corroded · Feb 13, 2026 · N733FD · Airbus A300B4605R · Escape Slide
  > WHILE WORKING WRI 25-60/9552 FOR R1 FEA SLIDE INSPECTION, THE AMTS FOUND CORROSION AND 2 SCREWS BROKEN. REMOVED R1 SLIDE PER REF ABOVE.
- [SDR FDEA202502140227](https://openairdocs.org/sdr/FDEA202502140227.md): Button · jammed · Feb 14, 2025 · N733FD · Airbus A300B4605R · Emergency Lighting
  > UPON TROUBLESHOOTING OF WRI 33-20/8722 FOUND THAT COURIER EMERGENCY TEST BUTTON JAMMED TOO AND NOT WORKING. CLEANED SWITCH REF ESPM 20-55-50-0, OPS CKS OK M/M 33-20-00-00-09.
- [SDR FDEA202410231576](https://openairdocs.org/sdr/FDEA202410231576.md): Switch · failed · Oct 23, 2024 · N733FD · Airbus A310300 · Door Warning System
  > PDIS 733 52-70 8386 23OCT24 05:16 MEM OPEN PASSING FL230, RECEIVED A FLASHING RED LIGHT AND ALARM FOR THE R ENTRY DOOR. ALARM AND LIGHT STOPPED BELOW FL190 ON DESCENT. NO ECAM INDICATION OR PRESSURIZATION ISSUES NOTED. FACT 31OCT24 20:47 ME
- [SDR FDEA202408161130](https://openairdocs.org/sdr/FDEA202408161130.md): Contactor · failed · Aug 16, 2024 · N733FD · Airbus A300B4605R · AC Generator-Alternator
  > RIGHT AFTER TAKING THE RUNWAY FOR TAKEOFF, PRIOR TO ENGINE RUN UP, GOT A GEN 1 FAULT. ATTEMPTED ONE RESET IAW QRH/ECAM, BUT FAULTED AGAIN. AMM: 24-22-18-04 ESPM: 20-46-50 REMOVED AND REPLACED TRANSFER CONTACTOR 11XU AND LINE CONTACTOR CONTROL RELAY 13XU REF A
- [SDR FDEA202407191035](https://openairdocs.org/sdr/FDEA202407191035.md): Slide · malfunctioned · Jul 19, 2024 · N733FD · Airbus A300B4605R · Escape Slide
  > DURING CRUISE R1 ENTRY DOOR, ARMING LEVER, RED ALARM, AUDIBLE AND VISUAL ALARM WENT OFF. PLND: DATE: 22JUL24 ENT BY: 779762 ON: 19JUL24 14:30 Z AT: LCK-LINE MEL 19JUL24 13:54 GTF RELEASED FOR SERVICE PER MEL: 52-11-01-01 CATEGORY: C EXPIRATION: 29
- [SDR FDEA202407171026](https://openairdocs.org/sdr/FDEA202407171026.md): Tire · low pressure · Jul 17, 2024 · N733FD · Airbus A300B4605R · Tire
  > NO.1 MAIN TIRE TO BE REPLACED DUE TO LOW TIRE PRESSURE OF NO.2 MAIN TIRE AND KNOWN TO HAVE ROLLED DURING EVENT.
- [SDR FDEA202411200816](https://openairdocs.org/sdr/FDEA202411200816.md): Switch · faulted · May 11, 2024 · N733FD · Airbus A300F4605R · Escape Slide
  > AT TOP OF CLIMB, JUMPSEATER HEARD RI ALARM RINGING & NOTICED SLIDE ARM WARNING LIGHT FLASHING. COMPLIED WITH QRH WITH NO RELIEF OF ALARM OR LIGHT. ALARM QUIT ON APPROACH AT 2000 MSL. FOUND R1 EMERGENCY SLIDE LIMIT SWITCH 10WN STICKING. REMOVED AND REPLACED
- [SDR FDEA202404090451](https://openairdocs.org/sdr/FDEA202404090451.md): Fitting · cracked · Apr 9, 2024 · N733FD · Airbus A300B4605R · Fuselage Structure (General)
  > RH WING - BASIC WING STRUCTURE FR40 STGR32R - STGR33R I/B HOLE FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0378762 REPAIRED THE RH WING BASIC WING STRUCTURE RH FR40 STGR32R - STGR33R FWD FITTING LOWER RADIUS CRACKED HOLE A. TITLE: WINGS - BASIC WING STRUCTU
- [SDR FDEA202404090450](https://openairdocs.org/sdr/FDEA202404090450.md): Rib Splice · cracked · Apr 9, 2024 · N733FD · Airbus A300B4605R · Wing, Rib/Bulkhead
  > RH WING - CENTER SPAR RIB1 SPLICE TYPE 5 MIDDLE HOLE FOUND CRACK. COMPLIED WITH FEDEX EA 6-5710-T0378735 P1 REPAIRED THE RH WING CENTER SPAR RIB1 SPLICE TYPE 5 CARCKED MIDDLE HOLE. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE ON FITTING RH WING CWT S
- [SDR FDEA202404080449](https://openairdocs.org/sdr/FDEA202404080449.md): None · none · Apr 8, 2024 · N733FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING REPAIR ON AFT CARGO DOOR INNER SURFACE BETWEEN FR62A AND FR63, BEAM 4 - BEAM 5 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON AFT CARGO DOOR INNER SURFACE BETWEEN FR62A AND FR63, BEAM4 - BEAM5 WAS EVALUATED AND FOUND IN CONFORMITY WITH
- [SDR FDEA202404080448](https://openairdocs.org/sdr/FDEA202404080448.md): None · none · Apr 8, 2024 · N733FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING REPAIR ON AFT CARGO DOOR INNER SURFACE BETWEEN FR60A AND FR61, BEAM 4 - BEAM 5 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON AFT CARGO DOOR INNER SURFACE BETWEEN FR60A AND FR61, BEAM 4 - BEAM 5 REQUIRES EVALUATION FOR CONFORMITY THE EXIS
- [SDR FDEA202403300416](https://openairdocs.org/sdr/FDEA202403300416.md): Beam · cracked · Mar 30, 2024 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > WINGS - CENTER WING JOINT - FR40 STGR27L - STGR28L LH HOLE C FOUND CRACK REPAIRED CENTER WING JOINT FR40 STGR27L - STGR28L CRACKED LH HOLE C PER A300-600 SRM57-10-24-201. THIS IS CATEGORY B REPAIR AND THE FIRST INSPECTION WAS 3700FC / 8100FH WHICHEVER OCCU
- [SDR FDEA202403300415](https://openairdocs.org/sdr/FDEA202403300415.md): Structure · cracked · Mar 30, 2024 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > CENTER WING BOX - FR47 LHS REAR SPAR DATUM HOLE C FOUND CRACK COMPLIED WITH FEDEX EA 6-5710-T0378646 REPAIRED THE FR47 LHS REAR SPAR DATUM CRACKED HOLE C. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE C AT FR47 LHS DURING SB57-6086 EMBODIMENT. THIS IS A
- [SDR FDEA202403290404](https://openairdocs.org/sdr/FDEA202403290404.md): Rib · cracked · Mar 29, 2024 · N733FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE 1EA CRACK AT RIB18 BETWEEN STGR2.8 AND REAR SPAR. MAJOR REPAIR
- [SDR FDEA202403290403](https://openairdocs.org/sdr/FDEA202403290403.md): Rib · cracked · Mar 29, 2024 · N733FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE 1EA CRACK AT RIB21 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FL
- [SDR FDEA202403290402](https://openairdocs.org/sdr/FDEA202403290402.md): Rib · cracked · Mar 29, 2024 · N733FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN STGR2.7 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378628 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPPER FLANGE 5EA CRACKS AT RIB25, RIB26, RIB27 BETWEEN STGR2.
- [SDR FDEA202403290401](https://openairdocs.org/sdr/FDEA202403290401.md): Rib · cracked · Mar 29, 2024 · N733FD · Airbus A300B4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26, RIB27 BETWEEN STGR2.6 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378625 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE 3EA CRACKS AT RIB26, RIB27 BETWEEN STGR2.6 AND REAR SPAR
- [SDR FDEA202403290400](https://openairdocs.org/sdr/FDEA202403290400.md): Rib · cracked · Mar 29, 2024 · N733FD · Airbus A300B4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH FEDEX EA 6-5750-T0378625 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPPER FLANGE 1EA CRACK AT RIB17 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING -
- [SDR FDEA202403260374](https://openairdocs.org/sdr/FDEA202403260374.md): None · none · Mar 26, 2024 · N733FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN FR62 AND FR63 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN FR62 AND FR63 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 53-10-14 FIG.201A. EO 6-
- [SDR FDEA202403260373](https://openairdocs.org/sdr/FDEA202403260373.md): None · none · Mar 26, 2024 · N733FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN FR63 AND FR64 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT S-56R BETWEEN FR63 AND FR64 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201A. EO 6-51
- [SDR FDEA202403220342](https://openairdocs.org/sdr/FDEA202403220342.md): Crossbeam · corroded · Mar 22, 2024 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT CROSS BEAM FR60 CORRODED AT Y-140 ~ Y-805 REPAIRED THE AFT CARGO COMPARTMENT CORRODED CROSS BEAM FR60 AT Y-140 ~ Y-805 PER A300-600 SRM53-10-15-201 PARA.10. AND SRM 51-76-10. THIS IS A CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2
- [SDR FDEA202403220343](https://openairdocs.org/sdr/FDEA202403220343.md): Crossbeam · corroded · Mar 22, 2024 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT CROSS BEAM FR56 CORRODED AT Y140 - Y1470. REPAIRED THE AFT CARGO COMPARTMENT CORRODED CROSS BEAM FR56 AT Y-140 ~ Y1470 PER SRM53-10-15-201 PARA.9 & SRM51-76-10 AND EA:6-5321-T0378696 P1. TITLE: FUSELAGE - CARGO COMP FLOOR - AFT CARG
- [SDR FDEA202403220341](https://openairdocs.org/sdr/FDEA202403220341.md): Crossbeam · corroded · Mar 22, 2024 · N733FD · Airbus A300B4605R · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT CROSS BEAM FR63 CORRODED AT Y-140 - Y1470. REPAIRED THE AFT CARGO COMPARTMENT CORRODED CROSS BEAM FR63 AT Y-140 ~ Y1470 PER A300-600 SRM53-10-15-201 & SRM51-76-10 AND EA 6-5321-T0378732. TITLE: FUSELAGE - CARGO COMP FLOOR - AFT CARGO
- [SDR FDEA202402160164](https://openairdocs.org/sdr/FDEA202402160164.md): Switch · failed · Feb 16, 2024 · N733FD · Airbus A300B4605R · Door Warning System
  > DURING THE FLIGHT, THE DOOR ON THE RIGHT SIDE WAS ALARMING. INDICATIONS IN COCKPIT WERE NORMAL. T/S CARRIED OUT IAW ABOVE REF. OPS TEST OF R1 DOOR EMERGENCY ESCAPE SLIDE RELEASE WARNING PERFORMED, WARNING LIGHT COMES ON & BUZZER SOUNDED WHEN INTERIOR CONTR
- [SDR FDEA202310121881](https://openairdocs.org/sdr/FDEA202310121881.md): Battery · inoperative · Oct 12, 2023 · N733FD · Airbus A300* · Emergency Lighting
  > EMERGENCY LIGHTS PUSH TO TEST SWITCH IN COURIER AREA DOES NOT ILLUMINATE DURING TEST. (EMERGENCY LIGHTS DO ILLUMINATE.) RED LED ON POWER SUPPLY UNIT IS ILLUMINATED DURING TEST. REMOVED AND REPLACED EMER POWER SUPPLY BATTERY, REF A300 AMM 33-51-14-04.
- [SDR FDEA202302110248](https://openairdocs.org/sdr/FDEA202302110248.md): Frame · damaged · Feb 11, 2023 · N733FD · Airbus A300* · Wing Main, Frame Structure
  > DURING ROTO INSP OF FR40 RHS UPPER AND LOWER HOLES NOTED WITH REJECTABLE DAMAGE INDICATIONS. WORK ACCOMPLISHED ON EA 6-5710-T0310489 REV E PT 5. EA TITLE WINGS - BASIC WING STRUCTURE - CRACKED HOLES IN CENTER WING JOINT - FR 40 LH/RH OVERSIZED AND BUSHIN
- [SDR FDEA202301110098](https://openairdocs.org/sdr/FDEA202301110098.md): Sleeve · cracked · Jan 11, 2023 · N733FD · Airbus A300B4605R · Engine Thrust Reverser
  > T/R STRUCTURE/SLEEVE - RH ENGINE I/B UPPER ACTUATOR SUPPORT, COMPLY WITH E.A.6-7833-T0372382 REV.C P2 REPAIRED #2 ENGINE I/B T/R STRUCTURE/SLEEVE - RH ENGINE I/B UPPER ACTUATOR SUPPORT, COMPLIED WITH E.A.6-7833-T0372382 REV.C P2.
- [SDR FDEA202201060019](https://openairdocs.org/sdr/FDEA202201060019.md): Packing · failed · Jan 6, 2022 · N733FD · Airbus A300* · Hydraulic Power System
  > PDIS 733 29-02 5545 06JAN22 IND OPEN U ON CLIMB OUT, HYDRAULIC GREEN SYSTEM LOW QUANTITY. COMPLIED WITH ECAM AND QRH AND SECURED GREEN SYSTEM HYDRAULIC PUMPS. DECLARED EMERGENCY. DURING CRUISE, GREEN QUANTITY CONTINUED TO DECREASE TO ZERO. CO
- [SDR FDEA202111112818](https://openairdocs.org/sdr/FDEA202111112818.md): None · cracked · Nov 11, 2021 · N733FD · Airbus A300* · Fuselage Main, Structure
  > LOWER FUSELAGE LH SIDE OF R GANTRY #5 AT FR50B CRACKED PERFORMED THE REPAIR ON LH SIDE OF R GANTRY #5 AT FR50B PER FEDEX EO: 6-5310-7- 5021 F PT9 TITLE: FUSELAGE-MAIN FRAME-INSPECT LH/RH GANTRIES 1,2,3,4, & 5 LOWER FLANGES FLANGES BETWEEN FR47/54-SB A3
- [SDR FDEA202111112817](https://openairdocs.org/sdr/FDEA202111112817.md): Seat Track · cracked · Nov 11, 2021 · N733FD · Airbus A300* · Fuselage Main, Structure
  > MDCC FR20-FR21, -Y450 SEAT TRACK CRACKED COMPLIED WITH FEDEX EA:6-5310-T0365152 P1, TITLE: FUSELAGE-MAINFRAME-MCD -Y450 SEAT SEAT TRACK BENT BETWEEN FR20 AND FR21-REPAIR. THIS WAS A PERMANENT CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100
- [SDR FDEA202111082793](https://openairdocs.org/sdr/FDEA202111082793.md): None · cracked · Nov 8, 2021 · N733FD · Airbus A300* · Fuselage Main, Structure
  > LOWER FUSELAGE LH SIDE OF R GANTRY #5 AT FR51A CRACKED PERFORMED THE REPAIR ON LH SIDE OF R GANTRY #5 AT FR51A PER FEDEX EO: 6-5310-7-5021 5021 F PT9 TITLE: FUSELAGE-MAIN FRAME-INSPECT LH/RH GANTRIES 1,2,3,4, & 5 LOWER FLANGES BETWEEN FR47/54-SB A300-53-6
- [SDR FDEA202111082792](https://openairdocs.org/sdr/FDEA202111082792.md): None · delaminated · Nov 8, 2021 · N733FD · Airbus A300* · Wing, Control Surfaces
  > RH AILERRON UPPER SURFACE T/E AREA FOUND 1EA PUNCTURED COMPLIED WITH EA: 6-5750-T0365067 P1 TITLE: WING-FLIGHT SURFACES-RH AILERON TRAILING EDGE WEDGE UPPER SURFACE REPAIR-SRM REPAIR-RSC TRACKING.THIS REPAIR WAS A CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX
- [SDR FDEA202103170684](https://openairdocs.org/sdr/FDEA202103170684.md): Actuator · malfunctioned · Mar 17, 2021 · N733FD · Airbus A300B4605R · Landing Gear Position and Warning
  > PDIS 733 32-60 4477 17MAR21 IND FACT U ON DEPARTURE OUT OF IND GOT ECAM ALERT FOR L/G DOORS NOT CLOSED. NOSE GEAR AMBER DOOR LIGHT ILLUMINATED ON FORWARD AND OVERHEAD PANEL. ACCOMPLISHED QRH AND RTB D TO IND PER MOCC. SHGN 17MAR21 10:41 I
- [SDR FDEA202103160670](https://openairdocs.org/sdr/FDEA202103160670.md): Slide · detached · Mar 16, 2021 · N733FD · Airbus A300B4605R · Escape Slide
  > RAMP REPORTED BEING UNABLE TO OPEN R1 ENTRY DOOR. UPON ARRIVAL TO AIRCRAFT FOUND R1 DOOR SLIDE SEPARATED FROM R1 DOOR WITH SLIDE MOUNTS STILL ATTACHED TO DOOR AND GIRT BAR STILL ATTACHED TO DOOR. PART 16MAR21 10:56 IND U IDENTIFIED PARTS A300 POST S
- [SDR FDEA202011182963](https://openairdocs.org/sdr/FDEA202011182963.md): Target · out of position · Nov 18, 2020 · N733FD · Airbus A300B4605R · Landing Gear Retraction/Extension System
  > ON FINAL APPROACH IN KELP F/O PUT THE LANDING GEAR HANDLE TO THE DOWN POSITION, ONLY RECEIVED THE GEAR DOOR UNLOCK LIGHTS AND GEAR DID NOT EXTEND FOR 20 -30 SECONDS. ECAM INDICATED "L/G UNSAFE INDICATIONS" AND "L/G GRAVITY EXTENTION" WARNINGS. AFTER 20-30 SE
- [SDR FDEA201907181626](https://openairdocs.org/sdr/FDEA201907181626.md): Spar · cracked · Jul 18, 2019 · N733FD · Airbus A300B4605R · Wing Spar
  > CRACK SIGNAL WAS FOUND AT RH WING FRONT SPAR RIB9 "S" HOLE AFTER ROTO-TEST INSPECTION COMPLIED WITH FEDEX EA: 6-5710-T0347649 P1, TITLE: WINGS - BASIC WING STRUCTURE - RH WING RIB 9 HOLE S/163 CRACK INDICATION - REPAIR, EO 6-5710-7-5001, SB A300-57-6037.
- [SDR FDEA201906291427](https://openairdocs.org/sdr/FDEA201906291427.md): Skin · damaged · Jun 29, 2019 · N733FD · Airbus A300B4605R · Trailing Edge Flaps
  > LT WING - INBD FLAP LWR SKIN WITH DEEP SCRATCH (LOCATION: 17 INCH FROM T/E, 34 INCH FROM I/B EDGE) REPAIRED THE LT WING INBD FLAP SCRATCHED SKIN (LOCATION: 17 INCH FROM T/E, 34 INCH FROM I/B EDGE) PER SRM 57-50-00-201 FIG.205. RSC TRACKING EA:6-5750-T0347827 W
- [SDR FDEA201906131281](https://openairdocs.org/sdr/FDEA201906131281.md): Stiffener · corroded · Jun 13, 2019 · N733FD · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > REPLACED THE CORRODED STIFFENER ON TOILET SERVICE PANEL CUTOUT SKIN AT FR12- FR12A PER A300-600 SRM51-40-21. MAJOR REPAIR IAW GMM 6-2-100.

Next page: https://openairdocs.org/aircraft/N733FD/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 = 'N733FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N733FD/reports

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