Airbus A300 F4-622R

Service difficulty reports · 11,836

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Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026110471606Placard · missingF/O S' LIFE VEST MISSING DUE DATE PLACARD. REMOVED AND REPLACED LIFE VEST IAW AMM 25-62-00/001.Nov 3, 2026 · N157UP · Airbus A300F4622R · Placards and MarkingsSDR IPXA2026110438358Battery · faultedBATTERY CAPACITY CHECK OF THE ASPSU FAULTED. R & R ASPSU PER AMM 52-73-18/0401. OPS CHECK OKNov 1, 2026 · N154UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026110238358Battery · no testBATTERY CAPACITY CHECK OF THE ASPSU FAULTED AUTONOMOUS STANDBY POWER SUPPLY UNIT ON ORDERED.Nov 1, 2026 · N154UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026102997543Seat Track · corrodedEXFOLIATION CORROSION FOUND ON SEAT TRACK BETWEEN FR74 AND FR75, Y450(LH).Oct 29, 2026 · N128UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026102996494Compensator · faultedEMERGENCY 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 RIGOct 29, 2026 · N124UP · Airbus A300F4622R · Landing Gear Brake SystemSDR IPXA2026102922771Angle · crackedFAULT-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.Oct 25, 2026 · N148UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102519463Placard · damagedEMERGENCY EXIT LEVER PLACARD WORN AND NOT READABLE DEFERRED PLACARD PER GMM 01.08.01.07Oct 25, 2026 · N120UP · Airbus A300F4622R · Placards and MarkingsSDR IPXA2026102611076Light · no testESCAPE SLIDE LIGHTING SYSTEM FAILED TEST. REPLACED EMERGENCY ESCAPE SLIDE IAW A300 AMM 25-61-21. OPS GOOD.Oct 24, 2026 · N151UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2026102386192Lens · brokenCREQ REPORTED CABIN PRESSURIZATION LIGHT LENS BROKEN ON L1 DOOR. INSTALLED LENS PER AMM 52-73-15.Oct 23, 2026 · N144UP · Airbus A300F4622R · Cabin Pressure IndicatorSDR IPXA2026102271587Light · inoperativeCLOSET 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 TIMEOct 22, 2026 · N153UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2026110241389Support Bracket · crackedDURING 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.Oct 20, 2026 · N147UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026102145646Lamp · inoperativeSMALL 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.Oct 20, 2026 · N164UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026102027627Fitting · crackedNLG UPLOCK ACTUATOR FIXTURE CRACKED. INSTALLED UPLOCK FIXTURE IAW AMM 32-31-14/401 AND 20-21-12/001.Oct 19, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026101984100Blower · inoperativeCAPTAIN EVAS BLOWER INOP. REMOVED AND REPLACED LH EVAS IAW A300 AMM 25-69-00/0401. OPS CHECK GOOD.Oct 16, 2026 · N152UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2026101782274Compensator · malfunctionedAT 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.Oct 16, 2026 · N148UP · Airbus A300F4622R · Fuel Indicating SystemSDR IPXA2026101568239Light · inoperativeRED 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 Oct 15, 2026 · N144UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026101200130O-Ring · leakingAIR 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.Oct 11, 2026 · N153UP · Airbus A300F4622R · Hydraulic System, MainSDR IPXA2026101946534Fitting · crackedFRAME 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-Oct 7, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026101512243Skin · dentedLOWER 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-.Oct 6, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2026102161735Fitting · out of limitsHOLE 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. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026102161645Fitting · out of limitsHOLE 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. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102161581Fitting · out of limitsHOLE 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. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102161504Fitting · out of limitsHOLE 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. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA202610051117Rib · crackedCREATED 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. _.Oct 2, 2026 · N158UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026101633178Seat Track · corrodedAFTER 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 FUOct 1, 2026 · N146UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101239996Warning Buzzer · brokenAVI 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.Oct 1, 2026 · N158UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026100639564Panel · crackedAFTER 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.Oct 1, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026100239996Warning Buzzer · brokenAVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN.Oct 1, 2026 · N158UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026100128643Arming Lever · out of adjustAFTER 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.Oct 1, 2026 · N166UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026100126338Track · fodCREW 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.Oct 1, 2026 · N166UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2026102920745Tie Down · crackedFWD 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.Sep 30, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026100104566Light · no testSUPERNUMERARY AREA EMERGENCY LIGHT SYSTEM TEST FUNCTION INOP. REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT REF AMM 33-51-14/0401, OPS CHECK GOOD.Sep 30, 2026 · N163UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026100181758Access Panel · crackedLEFT 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 Sep 29, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026092628088Angle · crackedFR 79 R/H DURING REMOVAL "Z" PROFILE FOUND ANGLE CRACKED. INSTALLED ANGLE PER SRM TASK:51-40-21-001 PAR. 6.Sep 25, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100508332Crossbeam · brokenMDC 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. _.Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100608317Crossbeam · crackedMDC 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. _.Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100816052Lug · brokenRIGHT ELEVATOR ATTACH FITTING NR 2 SAFETY LUG IS BROKEN. INSTALLED NEW LOCKING PLATE PER SRM 51-40-21-001, & 55-26-11-201.Sep 24, 2026 · N158UP · Airbus A300F4622R · Elevator Miscellaneous StructureSDR IPXA2026092402007Valve · failedOVERBOARD 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 Sep 24, 2026 · N161UP · Airbus A300F4622R · Air Distribution SystemSDR IPXA2026092403392Cvr · no testDURING PREFLIGHT CVR DOES NOT TEST. CVR OPS TEST GOOD PER AMM 23-71-00Sep 24, 2026 · N124UP · Airbus A300F4622R · Data Recorders (Flight/Maintenance)SDR IPXA2026092487635Cabin Press Sys · faultedIN 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 Sep 23, 2026 · N169UP · Airbus A300F4622R · Cabin Pressure Control SystemSDR IPXA2026092387635Cabin Pressure · low pressureDURING 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.Sep 23, 2026 · N169UP · Airbus A300F4622R · Cabin Pressure Control SystemSDR IPXA2026092372312Screw · looseEXIT 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 SERVICESep 22, 2026 · N166UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026092263257Contact · inoperativeSLIDE RELEASE WARNING LIGHT DOES NOT ILLUMINATE DURING TEST, REPLACED CONTACTS IAW ESPM 20-48-25-01. REMOVED AND REPLACED SLIDE RELEASE WARNING LIGHT IAW AMM 52-73-11. OPS CK GOOD.Sep 22, 2026 · N120UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026100650463Strap · corrodedRIGHT WING FIXED TRAILING EDGE LOWER SURFACE INBD SIDE JUST OUTBD OF RT FLAP HAS SKIN BULDGING WITH INTERNAL CORROSION. REMOVED LOWER SKIN PANEL (1EA) AT R/W FIXED TRAILING EDGE FOR ACCESS IAW SRM 51-40-21. INSTALLED NEW STRAP AND RE-INSTALLED LOWER SKIN PANESep 21, 2026 · N158UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026101639999Skin · corrodedLEFT WING UPPER SURFACE OUTBD FIXED TRAILING EDGE INBD AFT SIDE IS BULGING AROUND A FASTNER, POSSIBLE INTERNAL CORROSION. INSTALLED LANDING P/N UPA57246385200 AT LH WING IAW A300-600 SRM 51-40-21-001.Sep 20, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026101734052Doubler · crackedPANEL 485AL AFT INNER AREA, LOWER LONGERON DOUBLER HAS A CRACKED. SPLICE DOUBLER AND LOWER LONGERON DOUBLER WERE INSTALLED IAW SRM 54-55-51-201 PAR. 5.D. AND SRM 51-40-21.Sep 19, 2026 · N146UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026101934070Skin · crackedPANEL 485AL FWD OUTER ARA, RH SKIN IS CRACKED. INSTALLED NEW SKIN ON PANEL 485AL RT IAW SRM 51-40-21-001.Sep 19, 2026 · N146UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026101834137Plate · damagedPANEL 485AL FWD INNER AREA, LH UPPER LONGERON HAS WEAR DAMAGE WITH MATERIAL LOSS. REPLACED FAIRING ATTACH PLATE ON PANEL 485AL FWD INNER AREA, LT UPPER, IAW SRM 54-55-51, AND 51-40-21.Sep 19, 2026 · N146UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026092119481Handle · gougedCREW DOOR, EXTERNAL HANDLE HAS A GOUGE.Sep 18, 2026 · N146UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026091912039Cover · detachedCREW DOOR UPPER HANDLE COVER FELL OFF. INSTALLED CREW DOOR UPPER HANDLE COVER IAW AMM 52-11-11-27 THIS CLEARS DEFERRAL AND PLACARD REMOVEDSep 18, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew Doors
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