# Service difficulty reports: Cameron Balloons U S A-300

A list on [Cameron Balloons U S A-300](https://openairdocs.org/model/cameron-balloons-u-s-a-300.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 70 · 3,457 reports

- [SDR 2026FA0000414](https://openairdocs.org/sdr/2026FA0000414.md): Seal · wrong part · May 20, 2026 · Airbus A300* · Turbine Engine Accessory Drive
  > DURING THE DISASSEMBLY OF RR XWB-97K EGB EG0527, THE PRESENCE OF A DYNAMIC SEAL P/N NOT LISTED IN THE APPROVED DATA FOR XWB 97K AT POSITION 14-320 WAS OBSERVED. THE MOUNTED P/N IS: 90C24604 "JOINT ASSEMBLY, ROTATING EE361628-1". THE P/NS SPECIFIED IN RR XWB
- [SDR 6HUY202605180001](https://openairdocs.org/sdr/6HUY202605180001.md): Slide · fod · May 6, 2026 · Airbus A300* · Escape Slide
  > ON 6 MAY 2026, ESCAPE SLIDE ASSEMBLY P/N 62292-108 WITH S/N C0975 WAS RECEIVED FOR MAINTENANCE FROM AIR FRANCE UNDER CUSTOMER REPAIR ORDER NO. 6D224308HKR. THE UNIT WAS BOOKED UNDER INTERNAL WORK ORDER WHU2603936. DURING THE INSPECTION AND TESTING PHASE OF TH
- [SDR 2025F00091](https://openairdocs.org/sdr/2025F00091.md): Gearbox · misoverhauled · Apr 11, 2025 · Airbus A300* · Turbine Engine Accessory Drive
  > WHILE DISASSEMBLING RR TRENTXWB EGB P/N 90500-02 S/N EG1048, 2 SCREWS (AS3237-14) WERE FOUND AMONG THE 4 TGB BEARING SUPPORT FIXTURES. THESE SCREWS ARE NOT INCLUDED IN THE EGB BOM. THESE SCREWS SHOULD BE AS3237-12. THIS COMPONENT WAS MOUNTED ON ENGINE RR TREN
- [SDR FDEA202405050579](https://openairdocs.org/sdr/FDEA202405050579.md): Static Wick · corroded · May 5, 2024 · N670FE · Airbus A300* · Pitot/Static System
  > RH WING OUTER FLAP OUTBOARD AREA 1EA STATIC DISCHARGER BASE CORRODED COMPLIED WITH EA 6-5750-T0379031 P1 REPAIRED THE RH WING O/B FLAP OUTER T/E CORRODED UPPER SKIN. TITLE: WINGS - FLIGHT SURFACES - RH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION UN
- [SDR FDEA202405050578](https://openairdocs.org/sdr/FDEA202405050578.md): None · none · May 5, 2024 · N670FE · Airbus A300* · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE FRAME FR20A S37R-S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME FR20A S37R-S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-13-13-201 FIG.201. COMPLIED WITH EA 6-5310-54559 B P2
- [SDR FDEA202404260296](https://openairdocs.org/sdr/FDEA202404260296.md): None · none · Apr 26, 2024 · N661FE · Airbus A300* · Standard Practices/Structures
  > EXISTING REPAIR FOUND ON M/D CROSSBEAM AT FR29, BTW Y1456 TO -Y1456 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTI
- [SDR FDEA202401050039](https://openairdocs.org/sdr/FDEA202401050039.md): Indicator · failed · Jan 5, 2024 · N721FD · Airbus A300* · Fire Detection
  > ENGINE FIRE AND MULTIPLE SYSTEMS WARNINGS AND CAUTIONS AFTER ROTATION IN LIGHT RAIN. ENGINE TEMPERATURE INDICATIONS WERE NORMAL AUTOPILOT AUTOMATION WAS NOT AVAILABLE. EMERGENCY DECLARED. INDICATOR WERE ALL REPLACED AND ALL OPS CHECKS BEING SATISFACTORY.
- [SDR FDEA202401040036](https://openairdocs.org/sdr/FDEA202401040036.md): Crossbeam · cracked · Jan 4, 2024 · N659FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT - CRACK FOUND ON CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 JUST BELOW THE EXISTING REPAIR COMPLIED WITH EA 6-5310-T0377782 P1 REPAIRED THE MAIN DECK CARGO CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959. THIS IS CAT B REP
- [SDR FDEA202401030012](https://openairdocs.org/sdr/FDEA202401030012.md): Unknown · unknown · Jan 3, 2024 · N659FE · Airbus A300* · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPAR
- [SDR FDEA202401020007](https://openairdocs.org/sdr/FDEA202401020007.md): Coalescer Bag · failed · Jan 2, 2024 · N653FE · Airbus A300* · Humidity Control System
  > DURING DESCENT WHEN THROTTLES REDUCED TO IDLE, STRONG BURST OF SMOKE SMELL AND SLIGHT HAZE IN THE COCKPIT. IMMEDIATELY CLEARED AND DID NOT REOCCUR. REMOVED AND REPLACED BOTH COALESCER BAGS IAW A300 AMM 21-51-16-03. ITEM CLOSED. GROUND RUN CARRIED OUT AS
- [SDR FDEA202312211950](https://openairdocs.org/sdr/FDEA202312211950.md): Engine · leaking · Dec 21, 2023 · N682FE · Airbus A300* · Engine Oil Indicating System
  > ENG 1 OIL LO PRESS. PRESSURE INDICATED NORMAL ON ENG PAGE AND GAUGE. HOWEVER, WE NOTICED OIL QUANTITY DECREASING. DECREASING APPROX 2 QUARTS PER 10 MINUTES. AFTER LANDING BACK AT KMEM WE HAD 5 QUARTS REMAINING. 8 QUARTS AFTER ENG SHUTDOWN. ADDED 12 QTS OI
- [SDR FDEA202312161943](https://openairdocs.org/sdr/FDEA202312161943.md): Unknown · unknown · Dec 16, 2023 · N682FE · Airbus A300* · Escape Slide
  > R1 SLIDE INDICATION NOT SHOWING ON ECAM WHEN DOOR IS CLOSED AND ARMED, ALL OTHER DOOR CLOSED AND LOCKED INDICATIONS ARE FINE. PERFORMED T/S FOUND NO R1" SLIDE" INDICATION ON ECAM. PERFORMED TEST OF AUTOMOMOUS STBY PWR UNIT AND R1 "SLIDE" INDICATION RETUR
- [SDR FDEA202312141938](https://openairdocs.org/sdr/FDEA202312141938.md): Power Supply · failed · Dec 14, 2023 · N650FE · Airbus A300* · Emergency Lighting
  > "EMERG TEST" P/BSW (25WL) DOES NOT ILLUMINATE & EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN TEST CYCLE IS ENERGIZED. FACT 14DEC23 14:10 MSN U AMM: 33-51-14-04-0 RED LED FAULT LIGHT ILLUMINATED ON EPSU REMOVED AND REPLACED POWER SUPPLY UNIT (29WL) IAW
- [SDR FDEA202312061926](https://openairdocs.org/sdr/FDEA202312061926.md): Lens · inoperative · Dec 6, 2023 · N745FD · Airbus A300* · Central Warning
  > APU FIRE WARNING LIGHT INDICATOR AT NOSE GEAR STEERING BYPASS IS MISSING. RELEASED FOR SERVICE PER MEL: 26-XX-XX CAT C EXP: 16DEC23 APU GROUND AUTO FIRE EXTINGUISHING SYSTEM - INOP. APU OPERATION MUST BE MONITORED FROM COCKPIT WHILE APU IS RUNNING."
- [SDR FDEA202312051925](https://openairdocs.org/sdr/FDEA202312051925.md): Switch · inoperative · Dec 5, 2023 · N671FE · Airbus A300* · Emergency Lighting
  > FOUND DOOR INTERIOR EMERGENCY EXIT LIGHTS ALWAYS ILLUMINATED. NOTICED RED EMERGENCY LIGHT SWITCH FWD OF L1 DOOR IS STUCK INSIDE. RELEASED FOR SERVICE PER MEL: 33-XX-XX-XX CAT: C EXP: 15DEC23 "MEL 33-XX-XX-XX: COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS
- [SDR FDEA202311281918](https://openairdocs.org/sdr/FDEA202311281918.md): Rib · damaged · Nov 28, 2023 · N659FE · Airbus A300* · Fuselage Structure (General)
  > L/H MLG RIB 5 FWD LUG HAS MINOR IMPACT DAMAGE ON FWD AND AFT SIDES. REPAIRED PER E.A. 6-5710-T0377239 PT 1.
- [SDR FDEA202311261927](https://openairdocs.org/sdr/FDEA202311261927.md): Pin · loose · Nov 26, 2023 · N658FE · Airbus A300* · Equipment/Furnishings Wiring
  > THERE IS A RED FLAG PROTRUDING FROM UNDER THE R1 DOOR SLIDE. 26NOV23 - REMOVED RED TAG LABELED - REMOVE BEFOREINSTALLATION - ON R1 DOOR SLIDE REF ABOVE AMM REFERENCE. A/C OK FOR SERVICE. PER MOC PERF INSP / CHECK OF R1 DOOR SLIDE. AMM: 25-61-20-06-1 PER
- [SDR FDEA202311251898](https://openairdocs.org/sdr/FDEA202311251898.md): Elevator · unknown · Nov 25, 2023 · N660FE · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER5-14", T/E-6" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202311201956](https://openairdocs.org/sdr/FDEA202311201956.md): Header · cracked · Nov 20, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CGO DOOR UPPER L/H SIDE CORNER FOUND PATCH CRACKED. REPLACED THE CRACK PART WITH NEW PART I.A.W A300-600F SRM 51-72-10-001 PAGE 2.
- [SDR FDEA202311201930](https://openairdocs.org/sdr/FDEA202311201930.md): Dummy Rail · damaged · Nov 20, 2023 · N660FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > M/D CARGO COMPARTMENT FOUND NO.1 DUMMY SEAT TRACK (NO.1) CROWN BROKEN AT FR54.1 PLUS 4",RBL0 POS. ACCOMPLISHED THE DUMMY SEAT TRACK REPLACEMENT I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.7, PAGE.24-50
- [SDR FDEA202311161866](https://openairdocs.org/sdr/FDEA202311161866.md): Skin · unknown · Nov 16, 2023 · N660FE · Airbus A300* · Standard Practices/Structures
  > EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BETWEEN STRINGER 6~8L, FRAME 84~85,EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAI
- [SDR FDEA202311151966](https://openairdocs.org/sdr/FDEA202311151966.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R5 SPLR JACK RIB BOLT BORE CORRODED AT LOACTION NO.1, NO.3 AND NO.4 ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377191 P1,SEQ NO:760,TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX
- [SDR FDEA202311151963](https://openairdocs.org/sdr/FDEA202311151963.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R7 SPLR JACK RIB BOLT BORE CORRODED AT LOACTION NO.1 ACCOMPLISHED THE REINFORCING REPAIR AT RH #7 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377209 P1,SEQ NO:763,TITLE: WINGS-ATTACH FITTINGS-RH WING #7 SPOILER JACK RIB AT STA SP2X 40.425-BEAM ATTACHM
- [SDR FDEA202311151962](https://openairdocs.org/sdr/FDEA202311151962.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R4 SPLR JACK RIB BOLT BORES CORRODED AT LOCATION NO.1 AND NO.2 ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377195 P1,SEQ NO:766,TITLE: WINGS-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STA ABX 103.
- [SDR FDEA202311151961](https://openairdocs.org/sdr/FDEA202311151961.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R3 SPLR JACK RIB BOLT BORES CORRDED AT LOCATION NO.2 AND NO.3 ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377189 P1,SEQ NO:765,TITLE: WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX 31.67
- [SDR FDEA202311151960](https://openairdocs.org/sdr/FDEA202311151960.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R6 SPLR JACK RIB BOLT BORE CORRODED AT LOCATION NO.1. ACCOMPLISHED THE REINFORCING REPAIR AT RH #6 SPOILER O/B JACK RIB I.A.W FEDEX EA NO: T6-5740-T0377208 P1, SEQ NO:761, TITLE: WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X 40.425 - BEAM A
- [SDR FDEA202311141965](https://openairdocs.org/sdr/FDEA202311141965.md): Rib · corroded · Nov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > LH WING SPOILER NO.5 I/B JACK RIB BOLT HOLES CORRODED AT BEAM ATTACHMENT BOLT LOCATION #1 & #3 ACCOMPLISHED THE REINFORCING REPAIR AT LH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0377193 P1,SEQ NO:764,TITLE: WINGS-ATTACH FITTINGS-LH WING #5 SPOILE
- [SDR FDEA202311141964](https://openairdocs.org/sdr/FDEA202311141964.md): Rib · corroded · Nov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > LH WING SPOILER NO.5 O/B JACK RIB BOLT HOLES CORRODED AT BEAM ATTACHMENT BOLT LOCATION #2 & #4 ACCOMPLISHED THE REINFORCING REPAIR AT LH #5 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377193 P1,SEQ NO:764,TITLE: WINGS-ATTACH FITTINGS-LH WING #5 SPOILE
- [SDR FDEA202311141959](https://openairdocs.org/sdr/FDEA202311141959.md): Rib · corroded · Nov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > LH WING SPOILER NO.3 O/B JACK RIB BOLT HOLE CORRODED AT BEAM ATTACHMENT BOLT LOCATION #2 ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377187A P1,SEQ NO:762,TITLE: WINGS-ATTACH FITTINGS-LH WING #3 SPOILER JAC
- [SDR FDEA202311131953](https://openairdocs.org/sdr/FDEA202311131953.md): Stringer Splice · corroded · Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Longeron/Stringer
  > AVIONICS COMPT BILGES GOT A STRINGER CORRODED AT FR19-2", STR-52L REPLACED THE SPLICE WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B~23
- [SDR FDEA202311131895](https://openairdocs.org/sdr/FDEA202311131895.md): Skin · dented · Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Plate/Skin
  > FUSELAGE TAIL SKIN FOUND 1EA BULGED AT FR93 PLUS 5.3",S-16R PLUS 3.5",POS. CUT OUT DAMAGE AREA,FABRICATED THE REPAIR DOUBLER,WET INSTALLED REPAIR DOUBLER WITH FASTENERS. I.A.W A300-600F SRM 53-19-12-201,PARA.6B,FIG202,PAGE213~PAGE218. "MAJOR REPAIR"
- [SDR FDEA202311131894](https://openairdocs.org/sdr/FDEA202311131894.md): Skin · dented · Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Plate/Skin
  > FUSELAGE TAIL SKIN FOUND 5EA BULGEDS AT FR92 PLUS 4.4", S-16R PLUS 1.8", FR92 PLUS 3", S- 16R PLUS 2.4", FR92 PLUS 5.5", S-17R PLUS 0.9", FR92 PLUS 5.4", S-17R PLUS 2.5", FR92 PLUS 2.8", S-17R PLUS 4.7" POS. CUT OUT DAMAGE AREA, FABEICATED THE REPAIR DOUBL
- [SDR FDEA202311120003](https://openairdocs.org/sdr/FDEA202311120003.md): Retainer · corroded · Nov 12, 2023 · N660FE · Airbus A300* · Fuselage Structure (General)
  > FR40 BULKHEAD T/E LWR SURFACE RETAINER CORRODED. ACCOMPLISHED THE DOUBLER REPAIR TO THE DAMAGE AREA I.A.W FEDEX EA NO:T6-5310- T0377351 P1, SEQ NO:774,TITLE:FUSELAGE - MAINFRAME - PRESSURE FLOOR PANEL REPAIR AT FR40 BETWEEN Y953 AND -Y1456 DUE TO HEAVY EXFO
- [SDR FDEA202311121897](https://openairdocs.org/sdr/FDEA202311121897.md): Slat · gouged · Nov 12, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > R1 SLAT CHAFING AT RIB20 PLUS 3", T/E -13". ACCOMPLISHED THE BONDED REPAIR WITH SKIN FILLER PIECE AND REPAIR PATCH I.A.W FEDEX EA NO:T6-5750-T0377084 P1, SEQ NO:752, TITLE:WING-FLIGHT SURFACES-RH #1 SLAT-GOUGE DAMAGE FOUND ON TAIL SECTION OUTBOARD LOWER SK
- [SDR FDEA202311100008](https://openairdocs.org/sdr/FDEA202311100008.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > LH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND SLIGHT CREASED AT JACK RIB 1 LOWER SECTION ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR AT JACK RIB 1 I.A.W FEDEX EA NO:T6-5750- T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREAS
- [SDR FDEA202311100002](https://openairdocs.org/sdr/FDEA202311100002.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > LH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND SLIGHT CREASED AT JACK RIB 1 LOWER SECTION ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR AT JACK RIB 1 IAW FEDEX EA T6-5750- T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASE LIN
- [SDR FDEA202311100001](https://openairdocs.org/sdr/FDEA202311100001.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > LH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND CREASED AT TRACK RIB 1 LWR SECTION ACCOMPLISHED THE FLUSH REPAIR AT TRACK RIB 1 I.A.W FEDEX EA NO:T6-5750-T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASE LINES FOUND ON
- [SDR FDEA202311101946](https://openairdocs.org/sdr/FDEA202311101946.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > R3 SLAT LWR SURFACE PROTUDER AT RIB37-3", T/E-6.5". ACCOMPLISHED THE COLD WORK TO THE PROTUDED LWR SKIN I.A.W FEDEX EA NO:T6-5750- T0377056 P1, SEQ NO:768, TITLE:WING-FLIGHT SURFACES-RH WING-#3 SLAT UPPER SKIN PUNCTURE BETWEEN RIB36 AND 37 "MAJOR REPAIR"
- [SDR FDEA202311101945](https://openairdocs.org/sdr/FDEA202311101945.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > R3 SLAT UPPER SURFACE PUNTURED AT RIB37-3", T/E-6.5" CUT OUT THE DAMAGE AREA AND INSTALLED THE EXTERNAL PATCH I.A.W FEDEX EA NO:T6-5750- T0377056 P1, SEQ NO:768, TITLE:WING-FLIGHT SURFACES-RH WING-#3 SLAT UPPER SKIN PUNCTURE BETWEEN RIB36 AND 37 "MAJOR REP
- [SDR FDEA202311101935](https://openairdocs.org/sdr/FDEA202311101935.md): Flap · cracked · Nov 10, 2023 · N660FE · Airbus A300* · Trailing Edge Flaps
  > 8EA CRACKS (MAX 27MM) WERE FOUND AT LH WING CENTER FLAP RIB12 FWD, 15 FWD, 18 AFT, 27 FWD, 27 AFT AND 25 AFT(3EA) AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE RIB FLANGE REPAIRS AND EXTERNAL DOUBLER REPAIRS I.A.W FEDEX EA NO:T6-5750-T0377102 P1, SEQ NO:
- [SDR FDEA202311081879](https://openairdocs.org/sdr/FDEA202311081879.md): Fitting · cracked · Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Main, Structure
  > FLOOR CROSSBEAM 10 PICK-UP FITTING CRACK AT Y-953 POSITION REMOVED CRACK PICK-UP FITTING,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.6,PAGE 7B~23
- [SDR FDEA202311081878](https://openairdocs.org/sdr/FDEA202311081878.md): Angle · cracked · Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous Structure
  > FLOOR CROSSBEAM 10 ANGLE FITTING CRACK AT Y-953 POSITION REMOVED CRACK ANGLE FITTING,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.6,PAGE 7B~23
- [SDR FDEA202311081877](https://openairdocs.org/sdr/FDEA202311081877.md): Strap · cracked · Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous Structure
  > FUSELAGE INNER S-39R PLATE WEB FOUND STRAP CRACK BETWEEN FR86 & FR87 AREA CRACKED STRAP REPLACED NEW PART,INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10- 001,PAGE 2 AND 51-40-21-001,PARA 6,PAGE 7B-PAGE 23
- [SDR FDEA202311071851](https://openairdocs.org/sdr/FDEA202311071851.md): Flap · unknown · Nov 7, 2023 · N660FE · Airbus A300* · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN AT RIB 26A,T/E-2" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12
- [SDR FDEA202311071840](https://openairdocs.org/sdr/FDEA202311071840.md): Unknown · unknown · Nov 7, 2023 · N749FD · Airbus A300* · Standard Practices/Structures
  > PDIS 749 05-50 7037 07NOV23 MEM MULTIPLE BIRD STRIKES AT LIFTOFF. ***EMERGENCY DECLARED**** FACT 07NOV23 19:05 MEM AMM: 05-51-14-00 PERFORMED BIRD STRIKE INSPECTION REF. AMM 05-51-14-00,CLEANED BLOOD STAIN ON NOSE RADOME AND BOTH ENGINES,
- [SDR FDEA202311051827](https://openairdocs.org/sdr/FDEA202311051827.md): Actuator · inoperative · Nov 5, 2023 · N683FE · Airbus A300* · Nose/Tail Landing Gear
  > PDIS 683 32-20 2696 03NOV23 CAN FACT U L/G DOOR NOT CLOSED ECAM AFTER GEAR RETRACTION. AMBER LIGHTS ILLUMINATED ON BOTH GEAR INDICATION PANELS. COMPLIED WITH QRH. DISCUSSED WITH GOC & MOC. WHEN GEAR WAS EXTENDED, THE AMBER DOOR LIGHTS REMAI
- [SDR FDEA202311021823](https://openairdocs.org/sdr/FDEA202311021823.md): Hinge · delaminated · Nov 2, 2023 · N688FE · Airbus A300* · Spoilers
  > LH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE (17MM*12MM, DEPTH: 1.7MM) AND O/B SIDE (30MM*10MM, DEPTH: 1.1MM) FOUND DELAMINATION REPAIRED LH WING #5 SPOILER CENTER O/B HINGE O/B SIDE DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5
- [SDR FDEA202311021822](https://openairdocs.org/sdr/FDEA202311021822.md): Hinge · delaminated · Nov 2, 2023 · N688FE · Airbus A300* · Spoilers
  > RH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE (25MM*15MM, DEPTH: 2.1MM) & O/B SIDE (20MM*15MM, DEPTH: 1.4MM) AND CENTER I/B HINGE O/B SIDE (20MM*15MM, DEPTH: 1.07MM) FOUND DELAMINATION RH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE DELAMINATION WAS
- [SDR FDEA202311021821](https://openairdocs.org/sdr/FDEA202311021821.md): Hinge · delaminated · Nov 2, 2023 · N688FE · Airbus A300* · Spoilers
  > RH WING #3 SPOILER CENTER I/B HINGE O/B SIDE FOUND DELAMINATION (15MM*15MM, DEPTH: 1.22MM) REPAIRED RH WING #3 SPOILER CENTER I/B HINGE O/B SIDE DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5 & EA 6-5750-T0376848 P1. MAJOR REPAIR I
- [SDR FDEA202310281808](https://openairdocs.org/sdr/FDEA202310281808.md): Slat · unknown · Oct 28, 2023 · N688FE · Airbus A300* · Leading Edge Devices
  > EXISTING REPAIR ON RH WING #1 SLAT END RIB 2A, FROM I/B EDGE ABOUT 7" REQUIRES EVALUATION FOR CONFORMITY COMPLIED WITH EA 6-5750-T0376898 A P1. REPAIRED THE RH WING #1 SLAT EXISTING REPAIR AT INBOARD EDGE CLOSE TO RIB 2A. THIS IS CAT A REPAIR AND THIS REP

Next page: https://openairdocs.org/model/cameron-balloons-u-s-a-300/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 = 'A300'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cameron-balloons-u-s-a-300/reports

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