# Service difficulty reports: Airbus A300 B4-622R

A list on [Airbus A300 B4-622R](https://openairdocs.org/model/airbus-a300-b4-622r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 88 · 4,383 reports

- [SDR FDEA202610271696](https://openairdocs.org/sdr/FDEA202610271696.md): Warning Light · false activation · Oct 27, 2026 · N725FD · Airbus A300B4622R · Emergency Equipment
  > R1 DOOR SLIDE WILL NOT INDICATE ARMED ON THE ECAM. AMM: 52-73-00-05-02 ESCAPE SLIDE LIGHTS ON L1 & R1 DOORS DO NOT ILLUMINATE WHEN TESTED. RESET ASPSU & BITE TESTED IAW 52-73-00-05-02 LIGHTS ON BOTH DOORS NOW ILLUMINATED & RH DOOR SLIDE INDICATION.
- [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 FDEA202609291451](https://openairdocs.org/sdr/FDEA202609291451.md): Drain Line · misinstalled · Sep 29, 2026 · N721FD · Airbus A300B4622R · Hydraulic System, Main
  > DURING THE CLIMB TO FL160 WE NOTICED THE GREEN HYD SYS QITY DECREASING. GREEN HYD SYSTEM CONTINUED TO ZERO ON BOTH ECAM AND OVERHEAD GAUGE. THE BLUE OVER-HEAD HYD SYSTEM QUANTITY INCREASED TO SHOWING OFF SCALE FULL. FOLLOWED ECAM & QRH PROCEDURES INCLUDING
- [SDR FDEA202609091296](https://openairdocs.org/sdr/FDEA202609091296.md): Slide · malfunctioned · Sep 9, 2026 · N721FD · Airbus A300B4622R · Escape Slide
  > AT BLOCK IN L1 DOOR SLIDE WILL NOT DISARM. MEL 09SEP26 18:17 IND RELEASED FOR SERVICE IAW MEL 52-11-01-01, CATEGORY: C EXPIRATION: 19SEP26 MEL 52-11-01-01: CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIDE REMAINS INSTALLED ON DOOR. MEL: 52-11-01-01 C/
- [SDR FDEA202608271240](https://openairdocs.org/sdr/FDEA202608271240.md): Adapter · damaged · Aug 27, 2026 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > RAMP ONLOAD CREW REPORTS A RESTRAINT SEPERATED FROM THE FLOOR ON THE FORWARD SIDE OF 13C IN MAIN CARGO. BESIDES THE BROKEN FLOOR TRACK LOBES-NO OTHER DAMAGE FOUND ON THE FLOOR TRACK OR ADJACENT FLOOR PANELS. OIL LBB NO RESTRICTION IAW DWG SR30-53-003.
- [SDR FDEA202608071109](https://openairdocs.org/sdr/FDEA202608071109.md): Skin · corroded · Aug 7, 2026 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
  > AVIONICS COMPARTMENT FR 18 - 19, STRINGERS 50L - 51L INNER SKIN CORRODED. REPAIRED THE CORRODED SKIN AT AVIONICS COMPARTMENT FR18 - FR19, S50L - S51L. THIS IS CATEGORY B REPAIR DUE TO AWAITING FURTHER DAMAGE TOLERANCE ASSESSMENT(DT) APPROVAL. SOLUTION LIFE OR
- [SDR FDEA202607301137](https://openairdocs.org/sdr/FDEA202607301137.md): Fitting · none · Jul 30, 2026 · N749FD · Airbus A300B4622R · Standard Practices/Structures
  > 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. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF TH
- [SDR FDEA202607291057](https://openairdocs.org/sdr/FDEA202607291057.md): Shear Pin · damaged · Jul 29, 2026 · N748FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > WHILE PERFORMING FREE FALL CHECK, FOUND "NLG" FREE FALL QUADRANT 3 TO MOVE MORE ON SHAFT THAN ADJACTENT MLG FREE FALL QUADRANT 1 DOES ON SHAFT. INSTALLED BUSHING & SHEAR PIN INTO NLG FREE FALL AMM 32-33-00-05, EA 6-3230-T0388190A, COMPLETED OPS CHECK OF LA
- [SDR FDEA202607221060](https://openairdocs.org/sdr/FDEA202607221060.md): Skin · punctured · Jul 22, 2026 · N749FD · Airbus A300B4622R · Leading Edge Devices
  > LH WING SLAT #2 LOWER SKIN BETWEEN INBOARD RIB AND RIB 2 FOUND PUNCTURE. COMPLIED WITH EA 6-5750-T0388161 P1. LH WING SLAT #2 LOWER SKIN PUNCTURED AREA BETWEEN INBOARD RIB AND RIB 2. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57
- [SDR FDEA202607220985](https://openairdocs.org/sdr/FDEA202607220985.md): Uplock · leaking · Jul 22, 2026 · N748FD · Airbus A300B4622R · Hydraulic System, Main
  > GREEN HYD RSVR LO LEVEL ECAM ON DEPARTURE. QUANTITY WAS AT ORANGE DOT IN YELLOW BAND. COMPLIED WITH ECAM/QRH. CAPTAIN REPORTED THE ALTERNATE GEAR EXTENSION PROCEDURE WAS USED AS DIRECTED BY RED TABS. RESTORE THE GEAR IAW AMM 32-33-00-02-0. REMOVED AND RE
- [SDR FDEA202607080864](https://openairdocs.org/sdr/FDEA202607080864.md): Warning Buzzer · inoperative · Jul 8, 2026 · N725FD · Airbus A300B4622R · Door Warning System
  > DURING POST-FLIGHT, L1 DOOR SLIDE WARNING BUZZER INOP, WARNING LIGHT OPERATES NORMAL. RELEASED FOR SERVICE PER MEL: 52-73-01-02 CATEGORY C L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM BUZZERS INOP. MEL: 52-73-01-02. PERFORMED BITE OF ASPSU (70WN). TEST
- [SDR FDEA202606180772](https://openairdocs.org/sdr/FDEA202606180772.md): Slide · fouled · Jun 18, 2026 · N748FD · Airbus A300B4622R · Escape Slide
  > PER CREW DEBRIEF, R1 DOOR SLIDE HANDLE HARD TO ARM/DISARM, DOOR OPENING/CLOSING AND LATCHING NOT AFFECTED, DOOR OPERATES NORMAL. RELEASED FOR SERVICE IAW MEL: 52-11-01-01, CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. AMM: 25-61
- [SDR FDEA202605280641](https://openairdocs.org/sdr/FDEA202605280641.md): Hydraulic Line · leaking · May 28, 2026 · N725FD · Airbus A300B4622R · Hydraulic System, Main
  > CLIMBING THROUGH FL200 COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM. DECLARED AN EMERGENCY AND RETURNED TO MEMPHIS. FOLLOWED QRH PROCEDURES, LANDED UNEVENTFULLY, AND WAS TOWED TO GATE. FOUND FLEX LINE GOING TO LH MANIFOLD-DUAL CONNECTING BLOCK DAMAGED. REMOVED
- [SDR FDEA202605010531](https://openairdocs.org/sdr/FDEA202605010531.md): Bottle · discharged · May 1, 2026 · N724FD · Airbus A300B4622R · Passenger/Crew Doors
  > WHILE WORKING WRIS 25-60-2704 AND 52-10-2698. MECHANICS OPENED THE L1 DOOR AND THE EMERGENCY DOOR ASSIST BOTTLE DISCHARGED WITH THE HANDLE IN THE DISARMED POSTION AND THE SAFETY PIN INSTALLED. SERVICED L1 FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER
- [SDR FDEA202604300529](https://openairdocs.org/sdr/FDEA202604300529.md): Power Supply · inoperative · Apr 30, 2026 · N730FD · Airbus A300B4622R · Door Warning System
  > DURING CRUISE, THE L1 SLIDE ARMED WARNING BUZZER STARTED GOING OFF WITH THE SLIDE LIGHT FLASHING. WE PUSHED THE INTERIOR DOOR CONTROL HANDLE AND CHECKED THE LOCKING INDICATIONS WITH NO SUCCESS IN DEACTIVATING THE BUZZER. ALL DOOR AND SLIDE INDICATORS ON
- [SDR FDEA202604250502](https://openairdocs.org/sdr/FDEA202604250502.md): Girt Bar · out of adjust · Apr 25, 2026 · N724FD · Airbus A300B4622R · Emergency Equipment
  > DOOR 1L WOULD NOT DISARM AFTER THE FLIGHT. RELEASED FOR SERVICE IAW MEL 52-11-01-05. CREW ENTRY DOOR L1 INOP. MEL 52-11-01-05. FOUND L1 DOOR GIRT BAR MISALIGNED AND RE ADJUSTED GIRT BAR IN REF TO 25-61-22-04-01.COMPLETED INSTALL OF L1 DOOR SLIDE/RAFT
- [SDR FDEA202604120430](https://openairdocs.org/sdr/FDEA202604120430.md): Bottle · leaking · Apr 12, 2026 · N722FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > ON TAKEOFF OUT OF SNA WHEN WE RETRACTED THE GEAR THERE WAS A LOUD GRINDING SOUND AND EXCESSIVE VIBRATIONS. IN MEM ON FINAL WHEN WE SELECTED GEAR DOWN THERE WERE VIBRATIONS AND THE GEAR DID NOT EXTEND. THE DOORS SHOWED OPEN. ON THE GO AROUND THE GEAR CAME
- [SDR FDEA202603250373](https://openairdocs.org/sdr/FDEA202603250373.md): Packing · leaking · Mar 25, 2026 · N724FD · Airbus A300B4622R · Hydraulic System, Main
  > AT CRUISE GOT GREEN HYD LOW QTY. BOTH ECAM AND OVERHEAD GAGE SHOWED ALL FLUID LOST. USED MANUAL GEAR EXTENSION. AFTER LANDING, GREEN HYD QTY BACK INTO GREEN RANGE, BUT BELOW TOP HAT. EMERGENCY DECLARED AFTER BREIF WITH FLIGHT CREW, WHEN ECAM MESSAGE APPE
- [SDR FDEA202603230366](https://openairdocs.org/sdr/FDEA202603230366.md): Skin · damaged · Mar 23, 2026 · N746FD · Airbus A300B4622R · Rudder, Plate/Skin
  > RUDDER LEFT SIDE PANEL LEADING EDGE INTERNAL STRUCTURE BETWEEN STA869/BR7 AND UPR EDGE FOUND WATER INGRESS. DAMAGE AT RUDDER LEFT SIDE PANEL LEADING EDGE INTERNAL STRUCTURE BETWEEN STA869/BR7 AND UPR EDGE PER A300-600 SRM55-41-12-201 PARA.30 FIGURE 219.
- [SDR FDEA202603010299](https://openairdocs.org/sdr/FDEA202603010299.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB25 AND 26 BETWEEN STGR2
- [SDR FDEA202603010298](https://openairdocs.org/sdr/FDEA202603010298.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > RT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB18 BETWEEN STGR2.7 AND REAR SPAR, RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB18 AND 19 BETWEEN STGR2.7
- [SDR FDEA202603010297](https://openairdocs.org/sdr/FDEA202603010297.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > RT WING CENTER FLAP RIBS UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN S2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 & REAR SPAR, RIB13 BETWEEN S2.6 AND S2.8 COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 7EA CRACKS OF RIB11
- [SDR FDEA202603010296](https://openairdocs.org/sdr/FDEA202603010296.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND FRONT SPAR COMPLIED WITH EA 6-5750-T0386614 INSPECTED THE LH WING CENTER FLAP RIB UPR FLANGE OF RIB15 BETWEEN STGR2.5 AND FRONT SPAR AND REPAIRED THE BOTTOM SKIN POCKET CUT OUT
- [SDR FDEA202603010295](https://openairdocs.org/sdr/FDEA202603010295.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIBS UPR FLANGE FOUND 6EA CRACKS AT RIB16 BETWEEN STGR2.7 AND STGR2.8, RIB17 BETWEEN STGR2.8 AND REAR SPAR, RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6
- [SDR FDEA202603010294](https://openairdocs.org/sdr/FDEA202603010294.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIBS UPR FLANGE FOUND 5EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.7 AND REAR SPAR, RIB27 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGES 5EA CR
- [SDR FDEA202603010293](https://openairdocs.org/sdr/FDEA202603010293.md): Rib · cracked · Mar 1, 2026 · N746FD · Airbus A300B4622R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK OF RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH
- [SDR FDEA202602210372](https://openairdocs.org/sdr/FDEA202602210372.md): Actuator · faulted · Feb 21, 2026 · N746FD · Airbus A300B4622R · 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. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAI
- [SDR FDEA202602210249](https://openairdocs.org/sdr/FDEA202602210249.md): Girt Bar · unsecure · Feb 21, 2026 · N748FD · Airbus A300B4622R · Emergency Equipment
  > R1 DOOR SLIDE WOULD NOT DISARM. PBI RELEASED FOR SERVICE PER MEL: 52-11-01-01 CATEGORY C. CREW ENTRY DOOR ESCAPE SLIDE R1 - INOP. SLIDE REMAINS INSTALLED ON DOOR." MEL: 52-11-01-001 OK FOR SERVICE. AMM: 12-22-52-00-01, AMM: 25-61-22-04-02, AMM: 52
- [SDR FDEA202602190236](https://openairdocs.org/sdr/FDEA202602190236.md): Bottle · leaking · Feb 19, 2026 · N748FD · Airbus A300B4622R · Passenger/Crew Doors
  > R1 DOOR ASSIST BOTTLE REQUIRES DIAPHRAGM REPLACEMENT AND SERVICE PER AMM 52_10_14_03_10. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE DIAPHRAGM. SERVICED NITROGEN TO PLACARD ONBOARD. NO LEAK NOTED. CHECKS GOOD. OKAY FOR SERVICE.
- [SDR FDEA202602140219](https://openairdocs.org/sdr/FDEA202602140219.md): Elec Connector · dirty · Feb 14, 2026 · N722FD · Airbus A300B4622R · Equipment/Furnishings Wiring
  > WHEN R1 SLIDE ARMED NO INDICATION ON ECAM OF SLIDE BEING ARMED. AMM: 52-73-13-05-01 CLEANED CONNECTOR AT ESCAPE SLIDE ARM SWITCH 14WN PER ESPM 20-55-50-0. PERFORMED ADJUSTMENT TEST OF ESCAPE SLIDE IAW AMM 52-73-13-05-01. OPS CHECKS GOOD OK FOR SERVIC
- [SDR FDEA202602140198](https://openairdocs.org/sdr/FDEA202602140198.md): Safety Wire · wrong part · Feb 14, 2026 · N725FD · Airbus A300B4622R · Escape Slide
  > L1 DOOR SLIDE EJECTOR BAG RELEASE CABLE ATTACHMENT HAS INCORRECT SAFETY WIRE. REQUIRES CAD PLATED COPPER SAFETY WIRE REF FEA 6-2560-F0386375 A P1 STEP 8. FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 RE SAFETIED EJECTOR BAG CABLE ATTACHMENT WITH CAD PLATED CO
- [SDR FDEA202602130237](https://openairdocs.org/sdr/FDEA202602130237.md): Bottle · damaged · Feb 13, 2026 · N748FD · Airbus A300B4622R · Passenger/Crew Doors
  > FOUND ON SERVICE CHECK L 1 EMERGENCY OPERATION CYLINDER LOW PER SERVICE CHART. AMM: 52-10-14-03-10 SERVICED L 1 EMERGENCY OPERATION CYLINDER PER REF.
- [SDR FDEA202602100164](https://openairdocs.org/sdr/FDEA202602100164.md): Cable · incorrect · Feb 10, 2026 · N751FD · Airbus A300B4622R · Escape Slide
  > DURING INSPECTION OF THE L1 DOOR SLIDE (PN: D30546-509, SN: C1384) FOUND THE BREAKAWAY WIRE ON THE RELEASE CABLE INCORRECT. CMM: 25-61-39 REPLACED THE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 REFERENCE FEA: 6-2560-F0386261 REV A P1 AND CMM 25
- [SDR FDEA202602050136](https://openairdocs.org/sdr/FDEA202602050136.md): Gearbox · failed · Feb 5, 2026 · N748FD · Airbus A300B4622R · Engine Thrust Reverser
  > ON DEPARTURE, NR 1 ENG REV UNLOCK. RAN QRH, DECLARED EMERGENCY AND RETURNED TO ORF WITHOUT INCIDENT. AMM 78-31-35-04, AMM 78-32-11-05 IAW MOCC REQ (MTSI#78-31/9965) REPLACE ENG 1 SPLITTER GEARBOX. R & R ENG 1 SPLITTER GEARBOX. OPS CK OK. R & R SPLITTER
- [SDR FDEA202602040120](https://openairdocs.org/sdr/FDEA202602040120.md): Slide · broken · Feb 4, 2026 · N721FD · Airbus A300B4622R · Escape Slide
  > R1 DOOR SLIDE ASSEMBLY HAS BROKEN BATTERY HARD SHELL. RELEASED FOR SERVICE PER MEL: 52-11-01-01, CATEGORY: C. R1 DOOR ESCAPE SLIDE INOP. SLIDE REMAINS INSTALLED ON DOOR. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-61-22-04-01. OPS CHECKS GOOD
- [SDR FDEA202602020137](https://openairdocs.org/sdr/FDEA202602020137.md): Slide Raft · inoperative · Feb 2, 2026 · N721FD · Airbus A300B4622R · Escape Slide
  > SMIS 721 25-60 MOD TYPE F MOD NO. 6-2560-F0386261 REV NO. PS P1 EQUIPMENT AND FURNISHINGS - EMERGENCY EVACUATION EQU IPMENT - VERIFICATION OF SAFETY WIRE MATERIAL ON SLIDE PACK BOARD RELEASE CABLE.:CPN 2513882 MPN D30546- 509 L1/R1 DOOR SLIDE. COMPLIED
- [SDR FDEA202601110022](https://openairdocs.org/sdr/FDEA202601110022.md): Apu · leaking · Jan 11, 2026 · N748FD · Airbus A300B4622R · Air Distribution System
  > PRIOR TO PUSHBACK, WITH ALL DOORS CLOSED EXCEPT CREW ENTRANCE DOOR, RECEIVED AN ECAM ALERT FOR MAIN DECK CARGO SMOKE DETECTED MID & EXPERIENCED SMOKE IN COCKPIT FROM GASPERS. SMOKE ON SET RAPID & HIGHLY CONCENTRATED. SMOKE CLEARLY VISIBLE IN COCKPIT, AP
- [SDR FDEA202512192262](https://openairdocs.org/sdr/FDEA202512192262.md): Battery Pack · inoperative · Dec 19, 2025 · N751FD · Airbus A300B4622R · Emergency Lighting
  > DURING POST FLIGHT NONE OF THE EMEGENCY LIGHTING WILL TEST. REMOVED AND REPLACED BATTERY FOR POWER SUPPLY 29WL, ALL EMERGENCY LIGHTING OPS CHECKED GOOD, REF AMM 33-51-14-04. OK TO CONTINUE SERVICE.
- [SDR FDEA202512162258](https://openairdocs.org/sdr/FDEA202512162258.md): Actuator · failed · Dec 16, 2025 · N729FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > LOUD THUD UPON GEAR EXTENSION COMING FROM NOSE WHEEL AND IT TOOK A LONG TIME FOR THE NOSE GEAR TO EXTEND AND THEN IT TOOK AN EVEN LONGER TIME FOR THE MAIN GEAR TO EXTEND WITH A THUD SOUND THEN ALL 3 WERE EVENTUALLY GREEN. (ABNORMALLY LONG, AND NOT IN SEQ
- [SDR FDEA202511222198](https://openairdocs.org/sdr/FDEA202511222198.md): Warning Light · failed · Nov 22, 2025 · N746FD · Airbus A300B4622R · Door Warning System
  > INCOMING WALKAROUND INSPECTION FOUND LEFT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHTS INOP. ASSOCIATED WARNING BUZZER OPERATES NORMAL. AMM: 52-73-11-04-01 AMM: 52-22-13-04 REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT WARNING LIGHT, WITH
- [SDR FDEA202511202193](https://openairdocs.org/sdr/FDEA202511202193.md): Light · failed · Nov 20, 2025 · N746FD · Airbus A300B4622R · Door Warning System
  > INCOMING WALKAROUND INSPECTION FOUND LT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM, LIGHTS INOPERATIVE. ASSOCIATED WARNING BUZZER OPERATES NORMALLY. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT WARNING LIGHT WITH NEW UNIT FROM STOCK. OPS TESTED GOOD
- [SDR FDEA202511142182](https://openairdocs.org/sdr/FDEA202511142182.md): Diaphragm · damaged · Nov 14, 2025 · N744FD · Airbus A300B4622R · Passenger/Crew Doors
  > L1 DOOR EMERGENCY ASSIST BOTTLE PRESSURE LOW. REPLACED DIAPHRAGM (PN# FE240-221-001, SN# N/A) IN THE PERCUSSION MECHANISM OF THE L1 DOOR ASSIST CYLINDER. NO PRESSURE DROP AFTER 4 HRS. LEAK CKS GOOD. REMOVED FROM MEL.
- [SDR FDEA202511142180](https://openairdocs.org/sdr/FDEA202511142180.md): Spring · failed · Nov 14, 2025 · N730FD · Airbus A300B4622R · Flight Compartment Equipment
  > IN CRUISE CAPTAINS FOOTREST SPRING NOT RETRACTING FOOT REST. COMPLIED WITH E.A. 6-2510-T0385692 REV NO: PS P3.
- [SDR FDEA202511132170](https://openairdocs.org/sdr/FDEA202511132170.md): Door · faulted · Nov 13, 2025 · N721FD · Airbus A300B4622R · Passenger/Crew Doors
  > L1 DOOR WILL NOT DISARM. REVERSED MEL 52-11-01-01. FOUND WITH LOWER COVER REMOVED DOOR DISARMS AND ARMS NORMALLY. REINSTALLED LOWER COVER AND DOOR CONTINUES TO OPERATE NORMALLY. LOWER COVER WAS DAMAGED AND PLACED ON OIL REF WRI 52-10/5586.
- [SDR FDEA202511132169](https://openairdocs.org/sdr/FDEA202511132169.md): Slide · dislodged · Nov 13, 2025 · N721FD · Airbus A300B4622R · Escape Slide
  > LEFT FORWARD ENTRY DOOR WILL NOT DISARM. THE LEVER WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION. MEL: 52-11-01-02 ESCAPE SLIDE CAME LOOSE FROM L1 DOOR, ESCAPE SLIDE REMOVED FROM DOOR, BUT REMAINS ONBOARD IN HAZMAT CONTAINER.
- [SDR FDEA202511132168](https://openairdocs.org/sdr/FDEA202511132168.md): Slide · faulted · Nov 13, 2025 · N721FD · Airbus A300B4622R · Passenger/Crew Doors
  > LEFT FORWARD ENTRY DOOR WILL NOT DISARM. THE LEVER WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION. THIS ITEM WAS ON MEL 52-11-01-01. THE ESCAPE SLIDE HAS COME LOOSE FROM THE STORE, TRANSFERRING WRI 52-10/5579 TO THIS WRI AND PLACING ITEM ON MEL 52-11-

Next page: https://openairdocs.org/model/airbus-a300-b4-622r/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 aircraft_model_key = 'A300B4622R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a300-b4-622r/reports

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