# Service difficulty reports: Airbus A300 F4-622R

A list on [Airbus A300 F4-622R](https://openairdocs.org/model/airbus-a300-f4-622r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 238 · 11,860 reports

- [SDR IPXA2026110860046](https://openairdocs.org/sdr/IPXA2026110860046.md): Profile · cracked · Nov 8, 2026 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > Z-PROFILE BETWEEN FR76 TO FR80 AT RH SIDE WAS FOUND WITH CRACK.
- [SDR IPXA2026110944260](https://openairdocs.org/sdr/IPXA2026110944260.md): Liner · broken · Nov 7, 2026 · N148UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR LINING PANEL 221DW IS BROKEN.
- [SDR IPXA2026110931274](https://openairdocs.org/sdr/IPXA2026110931274.md): Seal · cracked · Nov 6, 2026 · N148UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR LINING PANEL 831DZ IS CRACKED & EDGE RUBBER SEAL IS TORN.
- [SDR IPXA2026110931188](https://openairdocs.org/sdr/IPXA2026110931188.md): Seal · cracked · Nov 6, 2026 · N148UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR LINING PANEL 831AZ CRACKED & EDGE RUBBER SEAL IS TORN.
- [SDR IPXA2026110931326](https://openairdocs.org/sdr/IPXA2026110931326.md): Seal · torn · Nov 6, 2026 · N148UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR LINING PANEL 831EZ IS BROKEN & EDGE SEAL IS TORN.
- [SDR IPXA2026110931512](https://openairdocs.org/sdr/IPXA2026110931512.md): Trim Panel · cracked · Nov 6, 2026 · N148UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR TRIM PANEL CRACKED.
- [SDR IPXA2026110931039](https://openairdocs.org/sdr/IPXA2026110931039.md): Profile · cracked · Nov 6, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE UPON PROFILE-T REMOVAL, CRACK FOUND AT THE PROFILE-Z, FR80/82 BETWEEN -Y1137 & -Y1580 APPLIED TOP COAT IAW A300-600 SRM 51-75-10-201.
- [SDR IPXA2026110931120](https://openairdocs.org/sdr/IPXA2026110931120.md): Floor Support · cracked · Nov 6, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE UPON PROFILE-T INSTALL, CRACK FOUND AT THE PROFILE-Z, FR80/82 BETWEEN Y1137 & Y1580 VERIFIED, NEW Z-PROFILE LOCATED AND DRILLED IAW A300-600F SRM 51-40-44, GIVEN OK TO TRAT AND PRIME.
- [SDR IPXA2026110471606](https://openairdocs.org/sdr/IPXA2026110471606.md): Placard · missing · Nov 3, 2026 · N157UP · Airbus A300F4622R · Placards and Markings
  > F/O S' LIFE VEST MISSING DUE DATE PLACARD. REMOVED AND REPLACED LIFE VEST IAW AMM 25-62-00/001.
- [SDR IPXA2026110438358](https://openairdocs.org/sdr/IPXA2026110438358.md): Battery · faulted · Nov 1, 2026 · N154UP · Airbus A300F4622R · Door Warning System
  > BATTERY CAPACITY CHECK OF THE ASPSU FAULTED. R & R ASPSU PER AMM 52-73-18/0401. OPS CHECK OK
- [SDR IPXA2026110238358](https://openairdocs.org/sdr/IPXA2026110238358.md): Battery · no test · Nov 1, 2026 · N154UP · Airbus A300F4622R · Emergency Lighting
  > BATTERY CAPACITY CHECK OF THE ASPSU FAULTED AUTONOMOUS STANDBY POWER SUPPLY UNIT ON ORDERED.
- [SDR IPXA2026102997543](https://openairdocs.org/sdr/IPXA2026102997543.md): Seat Track · corroded · Oct 29, 2026 · N128UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > EXFOLIATION CORROSION FOUND ON SEAT TRACK BETWEEN FR74 AND FR75, Y450(LH).
- [SDR IPXA2026102996494](https://openairdocs.org/sdr/IPXA2026102996494.md): Compensator · faulted · Oct 29, 2026 · N124UP · Airbus A300F4622R · Landing Gear Brake System
  > EMERGENCY DECLARED, DURING CRUISE ALL FOUR RIGHT MAIN WHEEL TEMPS, 3,4,7&8 INDICATED EXCESSIVE HIGH 400+ DEGREE TEMPS. FOLLOWED PILOT QRH AND EXTENDED GEAR WAS INTERMITTENT WITH A NORMAL TEMP INDICATION BUT MOSTLY HIGH > T/S PER TSM 32-47-00/401. REPLACED RIG
- [SDR IPXA2026102922771](https://openairdocs.org/sdr/IPXA2026102922771.md): Angle · cracked · Oct 25, 2026 · N148UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT-STR-Z600: RH WING CENTER FLAP HAS A LATERAL BRACKET CRACKED. DOT 30-010. REPLACED ANGLE IN RH WING CENTER FLAP A300-600 SRM 51-40-21-001 P/N A5796040221500 BTCH 0004518843.
- [SDR IPXA2026102519463](https://openairdocs.org/sdr/IPXA2026102519463.md): Placard · damaged · Oct 25, 2026 · N120UP · Airbus A300F4622R · Placards and Markings
  > EMERGENCY EXIT LEVER PLACARD WORN AND NOT READABLE DEFERRED PLACARD PER GMM 01.08.01.07
- [SDR IPXA2026102611076](https://openairdocs.org/sdr/IPXA2026102611076.md): Light · no test · Oct 24, 2026 · N151UP · Airbus A300F4622R · Emergency Equipment
  > ESCAPE SLIDE LIGHTING SYSTEM FAILED TEST. REPLACED EMERGENCY ESCAPE SLIDE IAW A300 AMM 25-61-21. OPS GOOD.
- [SDR IPXA2026102386192](https://openairdocs.org/sdr/IPXA2026102386192.md): Lens · broken · Oct 23, 2026 · N144UP · Airbus A300F4622R · Cabin Pressure Indicator
  > CREQ REPORTED CABIN PRESSURIZATION LIGHT LENS BROKEN ON L1 DOOR. INSTALLED LENS PER AMM 52-73-15.
- [SDR IPXA2026102271587](https://openairdocs.org/sdr/IPXA2026102271587.md): Light · inoperative · Oct 22, 2026 · N153UP · Airbus A300F4622R · Passenger Compartment Lighting
  > CLOSET LIGHT IN LUGGAGE CLOSET BY CREW ENTRY DOOR INOP RAR STOWAGE CABINET LIGHT LAMP REF ESPM 20-45-90, AMM 25-27-25. OPS CHK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR IPXA2026110241389](https://openairdocs.org/sdr/IPXA2026110241389.md): Support Bracket · cracked · Oct 20, 2026 · N147UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > DURING OK TO INSTALL OF THE NR 2 ENG PYLON PRESSURE RELIEF DOOR SUPPORT, FOUND 1EA CRACKED BRACKET AT FWD MOUNTING BRACKET OF PRESSURE RELIEF DOOR RIB J08.
- [SDR IPXA2026102145646](https://openairdocs.org/sdr/IPXA2026102145646.md): Lamp · inoperative · Oct 20, 2026 · N164UP · Airbus A300F4622R · Emergency Lighting
  > SMALL EMERGENCY LIGHT IN LAV NEAR MIRROR INOP IN LOW ALWAYS ON POSITION. FOUND ON PREFLIGHT. RELAMPED LIGHT IAW CMS 33-24-03. OPS CHKD NORMAL.
- [SDR IPXA2026102027627](https://openairdocs.org/sdr/IPXA2026102027627.md): Fitting · cracked · Oct 19, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > NLG UPLOCK ACTUATOR FIXTURE CRACKED. INSTALLED UPLOCK FIXTURE IAW AMM 32-31-14/401 AND 20-21-12/001.
- [SDR IPXA2026101984100](https://openairdocs.org/sdr/IPXA2026101984100.md): Blower · inoperative · Oct 16, 2026 · N152UP · Airbus A300F4622R · Emergency Equipment
  > CAPTAIN EVAS BLOWER INOP. REMOVED AND REPLACED LH EVAS IAW A300 AMM 25-69-00/0401. OPS CHECK GOOD.
- [SDR IPXA2026101782274](https://openairdocs.org/sdr/IPXA2026101782274.md): Compensator · malfunctioned · Oct 16, 2026 · N148UP · Airbus A300F4622R · Fuel Indicating System
  > AT CRUISE, LEFT INNER TANK READ 4.2, IMBALANCE REMAINED THROUGH APPROACH, LANDING AND TAXI. UPON REACHING RAMP, LEFT INNER THEN SHOWED INCREASING AND FINALLY SHOWED 5.5 WITH IMBALANCE W/IN LD LIMITS. SPOKE WITH TECH, THEY RECOMMENED COMPENSATOR.
- [SDR IPXA2026101568239](https://openairdocs.org/sdr/IPXA2026101568239.md): Light · inoperative · Oct 15, 2026 · N144UP · Airbus A300F4622R · Emergency Lighting
  > RED EMERGENCY LIGHT IN MAIN CABIN DOOR INOP. DEFERRED IAW MEL 52-73-01-1. FOUND LOOSE WIRES ON LIGHT WARNING ASSEMBLY. VERIFIED CORRECT POLARITY OF WIRES RECONNECTED AS REQUIRED REF AMM 52-73-11/401 & ASM 52-73-00 TEST GOOD AT THIS TIME OK FOR SERVICE THIS
- [SDR IPXA2026101200130](https://openairdocs.org/sdr/IPXA2026101200130.md): O-Ring · leaking · Oct 11, 2026 · N153UP · Airbus A300F4622R · Hydraulic System, Main
  > AIR TURN BACK, COMPLETE HYDRAULIC GREEN LOSS OF FLUID IN FLIGHT. FOUND HYDRAULIC MOTOR ON FLAP CONTROL MODULE LEAKING. VERIFIED ENG DRIVEN PUMPS OPERATED LESS THAN 1 MINUTE PER AHM REPORT. SERVICED AND BLEED GREEN HYD SYS PER AMM 29-00-00/401.
- [SDR IPXA2026101946534](https://openairdocs.org/sdr/IPXA2026101946534.md): Fitting · cracked · Oct 7, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, Frame
  > FRAME 12A LT FITTING. 2 EA CRACK NOTED IN ZONE "A" (0.100") & (0.205") AND 1 EA CRACK NOTED IN ZONE "B" (0.130"). REPLACE THE DISCREPANT FITTING PRIOR TO FURTHER FLIGHT IAW EO-23539-REQ003. VERIFIED REMOVAL OF AIR CONDITION DUCTS TWO FR 12A LT. IAW SRM 51-40-
- [SDR IPXA2026101512243](https://openairdocs.org/sdr/IPXA2026101512243.md): Skin · dented · Oct 6, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, BTWN FR 51 TO 52, LH SIDE, NEXT TO MLG DOOR CUTOUT, EXTERNAL SURFACE, SKIN HAS A DENT W/ GOUGE. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-98862-REQ1 AND STE PNA EA 300-5315-27-A4660, REV-.
- [SDR IPXA2026102161735](https://openairdocs.org/sdr/IPXA2026102161735.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Wing Main, Frame Structure
  > HOLE N HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING.3780", SPLICE.2840, AFT FITTING.3780". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026102161645](https://openairdocs.org/sdr/IPXA2026102161645.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > HOLE M HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING.4530", SPLICE.3070, AFT FITTING.4580". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026102161581](https://openairdocs.org/sdr/IPXA2026102161581.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > HOLE L HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING.3830", SPLICE.2810, AFT FITTING.3840". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026102161504](https://openairdocs.org/sdr/IPXA2026102161504.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > HOLE H HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; SPLICE.3480, AFT FITTING.4050".ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA202610051117](https://openairdocs.org/sdr/IPXA202610051117.md): Rib · cracked · Oct 2, 2026 · N158UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > CREATED TO CAPTURE ENG STATUS AND COMPLETION FOR TASK CARD T3F18E009MQ3S. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98679-REQ1 AND STE PNA EA 300-5753-27-A4632, REV. _.
- [SDR IPXA2026101633178](https://openairdocs.org/sdr/IPXA2026101633178.md): Seat Track · corroded · Oct 1, 2026 · N146UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > AFTER DOG BONE REMOVAL ON TASK CARD T3F18E009MXK9 WERE FOUND SEVERAL SPOTS WITH CORROSION AT SEAT TRACK Y2462 (UNDER CHANNEL DRAIN) BETWEEN FR38 & FR38.2 REPAIR IAW: SRM REV 43 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201. THIS IS A CATEGORY A REPAIR AND NO FU
- [SDR IPXA2026101239996](https://openairdocs.org/sdr/IPXA2026101239996.md): Warning Buzzer · broken · Oct 1, 2026 · N158UP · Airbus A300F4622R · Passenger/Crew Doors
  > AVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN. REPLACED WARNING HORN (BUZZER) AND CARRIED OUT OPS CHECK GOOD IAW AMM 52-73-12/401.
- [SDR IPXA2026100639564](https://openairdocs.org/sdr/IPXA2026100639564.md): Panel · cracked · Oct 1, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > AFTER REMOVAL OF SEAL, FOUND PANEL 423BL CRACKED. INSTALLED DOUBLER ON PANEL 423BL IAW SRM 54-52-51-201-C1, PARAGRAPH D.2. STEP U, FIGURE 204.
- [SDR IPXA2026100239996](https://openairdocs.org/sdr/IPXA2026100239996.md): Warning Buzzer · broken · Oct 1, 2026 · N158UP · Airbus A300F4622R · Door Warning System
  > AVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN.
- [SDR IPXA2026100128643](https://openairdocs.org/sdr/IPXA2026100128643.md): Arming Lever · out of adjust · Oct 1, 2026 · N166UP · Airbus A300F4622R · Passenger/Crew Doors
  > AFTER BLOCK IN, USABLE TO DISARM SLIDE. SLIDE ARM/DISARM LEVER UNABLE TO MOVE TO FULL DISARM POSITION. MAIN ENTRY CREW DOOR. ADJUSTED DISARM HANDLE AND OPERATION CHECKS GOOD AT THIS TIME IAW AMM 52-10-30/501.
- [SDR IPXA2026100126338](https://openairdocs.org/sdr/IPXA2026100126338.md): Track · fod · Oct 1, 2026 · N166UP · Airbus A300F4622R · Emergency Equipment
  > CREW ENTRY SLIDE WILL NOT ARM. SLIDE ARMING HANDLE DOES NOT MOVE OUT OF DISARM POSITION. CLEARED DEBRIS FROM TRACK. OPS CHECKED NORMAL PER AMM 25-61-21/401.
- [SDR IPXA2026102920745](https://openairdocs.org/sdr/IPXA2026102920745.md): Tie Down · cracked · Sep 30, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FWD CARGO XZ LATCHES ON FR 21 AT CROSSBEAM Y1470, Y805, Y140, -Y140 WITH CRACK. INSTALLED 4EA XZ LATCHES P/N 2136T100-3 S/N'S 1784, 1734, 1443, 1396 AT FR 21 Y1470, Y805, Y140, -Y140 IAW AMM 25-52-36/401.
- [SDR IPXA2026100104566](https://openairdocs.org/sdr/IPXA2026100104566.md): Light · no test · Sep 30, 2026 · N163UP · Airbus A300F4622R · Emergency Lighting
  > SUPERNUMERARY AREA EMERGENCY LIGHT SYSTEM TEST FUNCTION INOP. REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT REF AMM 33-51-14/0401, OPS CHECK GOOD.
- [SDR IPXA2026100181758](https://openairdocs.org/sdr/IPXA2026100181758.md): Access Panel · cracked · Sep 29, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/Skin
  > LEFT WING BELOW KRUGER FLAP ACCESS PANEL 513AB STRUCTURE (RING) CRACKED. INTERNAL DOUBLER WAS REMOVED AT LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW A300-600 SRM 51-40-21-001. INSTALLED INTERNAL DOUBLER ON LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW
- [SDR IPXA2026092628088](https://openairdocs.org/sdr/IPXA2026092628088.md): Angle · cracked · Sep 25, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR 79 R/H DURING REMOVAL "Z" PROFILE FOUND ANGLE CRACKED. INSTALLED ANGLE PER SRM TASK:51-40-21-001 PAR. 6.
- [SDR IPXA2026100508332](https://openairdocs.org/sdr/IPXA2026100508332.md): Crossbeam · broken · Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR 79 R/H Y2127.6 FOUND CROSS BEAM WITH CRACK. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98797 AND STE PNA EA 300-5318-27-A4649, REV. _.
- [SDR IPXA2026100608317](https://openairdocs.org/sdr/IPXA2026100608317.md): Crossbeam · cracked · Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR 79 -Y2127.6 FOUND CROSS BEAM WITH CRACK.ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98797 AND STE PNA EA 300-5318-27-A4649, REV. _.
- [SDR IPXA2026100816052](https://openairdocs.org/sdr/IPXA2026100816052.md): Lug · broken · Sep 24, 2026 · N158UP · Airbus A300F4622R · Elevator Miscellaneous Structure
  > RIGHT ELEVATOR ATTACH FITTING NR 2 SAFETY LUG IS BROKEN. INSTALLED NEW LOCKING PLATE PER SRM 51-40-21-001, & 55-26-11-201.
- [SDR IPXA2026092402007](https://openairdocs.org/sdr/IPXA2026092402007.md): Valve · failed · Sep 24, 2026 · N161UP · Airbus A300F4622R · Air Distribution System
  > OVERBOARD EXTRACT VALVE CAUSING EXTRACT FAN HIGH SPEED CIRCUIT BREAKER TO POP. REVERSED, REMOVED AND REPLACED EXTRACT FAN (73HR) IAW AMM 21-23-11/401, NO HELP. TROUBLESHOT IAW ASM 21-33-00 SCH 02 FOUND BAD RELAY (68HR), REMOVED AND REPLACED RELAY (68HR) IAW
- [SDR IPXA2026092403392](https://openairdocs.org/sdr/IPXA2026092403392.md): Cvr · no test · Sep 24, 2026 · N124UP · Airbus A300F4622R · Data Recorders (Flight/Maintenance)
  > DURING PREFLIGHT CVR DOES NOT TEST. CVR OPS TEST GOOD PER AMM 23-71-00
- [SDR IPXA2026092487635](https://openairdocs.org/sdr/IPXA2026092487635.md): Cabin Press Sys · faulted · Sep 23, 2026 · N169UP · Airbus A300F4622R · Cabin Pressure Control System
  > IN DESCENT AT ABOUT 6000 FT WE RECIEVED CAB PRESS ADV, VS ON CAB PRESS PAGE WAS AT 1500 FT/MIN A NOTICEABLE HISSING SOUND FROM CAPTAINS SIDE OF COCKPIT AND NOTICEABLE EAR POPS FOR CAPT AND FO PERFORMED INSP/CHECK OF PREFORMED SEAL CAPT. SLIDING WINDOW PER AMM
- [SDR IPXA2026092387635](https://openairdocs.org/sdr/IPXA2026092387635.md): Cabin Pressure · low pressure · Sep 23, 2026 · N169UP · Airbus A300F4622R · Cabin Pressure Control System
  > DURING DESCENT AT ABOUT 6000 FT, RECIEVED CABIN PRESSURE ADV, VS ON CABIN PRESSURE PAGE WAS AT 1500 FT/MIN A NOTICEABLE HISSING SOUND FROM CAPTAINS SIDE OF COCKPIT AND NOTICEABLE EAR POPS FOR CAPT AND FO.
- [SDR IPXA2026092372312](https://openairdocs.org/sdr/IPXA2026092372312.md): Screw · loose · Sep 22, 2026 · N166UP · Airbus A300F4622R · Emergency Lighting
  > EXIT SIGN ABOVE THE MAIN CABIN DOOR, NOT SECURE, HANGING DOWN ON THE RIGHT SIDE. FOUND MAIN CABIN DOOR EXIT SIGN FORWARD MOUNTING SCREW VERY LOOSE. SECURED MOUNTING SCREW PER AMM 33-51-13-401. EMERGENCY LIGHT TEST OK PER AMM 33-51-13-401. OK FOR SERVICE

Next page: https://openairdocs.org/model/airbus-a300-f4-622r/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 = 'A300F4622R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a300-f4-622r/reports

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